def create_subdirname(obstime, with_seconds=False, **kwargs):
"""Generate the pps subdirectory name from the start observation time, ex.:
'npp_20120405_0037_02270'"""
sat = kwargs.get('platform_name', 'npp')
platform_name = PLATFORM_NAME.get(sat, sat)
if "orbit" in kwargs:
orbnum = int(kwargs['orbit'])
else:
from pyorbital.orbital import Orbital
from cspp_runner import orbitno
try:
tle = orbitno.get_tle(TLE_SATNAME.get(platform_name), obstime)
orbital_ = Orbital(tle.platform, line1=tle.line1, line2=tle.line2)
orbnum = orbital_.get_orbit_number(obstime, tbus_style=TBUS_STYLE)
except orbitno.NoTleFile:
LOG.error('Not able to determine orbit number!')
import traceback
traceback.print_exc(file=sys.stderr)
orbnum = 1
if with_seconds:
return platform_name + obstime.strftime(
'_%Y%m%d_%H%M%S_') + '%.5d' % orbnum
else:
return platform_name + obstime.strftime(
'_%Y%m%d_%H%M_') + '%.5d' % orbnum
def get_satellite_lat_lon(norad_id, tle_line1, tle_line2, date_time):
username = '******'
password = '******'
base_url = 'https://www.space-track.org/'
login_url = base_url + 'ajaxauth/login'
query = base_url + "/basicspacedata/query/class/satcat/NORAD_CAT_ID/" + \
norad_id + \
"/orderby/NORAD_CAT_ID asc/metadata/false"
data = {'identity': username, 'password': password, 'query': query}
# Makes a POST REST call to space-track.org and return the result as a list of JSON
try:
resp = requests.post(login_url, data=data)
except requests.exceptions.RequestException as err:
print("POST RESTful call unsuccessful - unable to obtain LAT/LON : " +
err)
tip_data_list = json.loads(resp.text)
satellite_name = str(tip_data_list[0].get('SATNAME'))
orb = Orbital(satellite=satellite_name, line1=tle_line1, line2=tle_line2)
# Gets longitude, latitude and altitude of the satellite:
lon, lan, alt = orb.get_lonlatalt(date_time)
print("------------------------- DATE & TIME IN UTC : " + str(date_time) +
" -------------------------")
print("LONGITUDE = " + str(lon))
print("LATITUDE = " + str(lan))
return lon, lan
def update_graph_live(n):
data = {'time': [], 'Latitude': [], 'Longitude': [], 'Altitude': []}
sat = Orbital('TERRA')
# Collect some data
for seconds in range(0, 3600, 20):
time = datetime.datetime.now() - datetime.timedelta(seconds=seconds)
data['time'].append(time)
lon, lat, alt = sat.get_lonlatalt(time)
data['Longitude'].append(lon)
data['Latitude'].append(lat)
data['Altitude'].append(alt)
# Create the graph with subplots
result = make_subplots(cols=1, rows=2, vertical_spacing=0.2, )
result['layout']['margin'] = {'b': 30, 'l': 30, 'r': 10, 't': 10, }
result['layout']['legend'] = {'x': 0, 'xanchor': 'left', 'y': 1, }
result.append_trace({'mode': 'lines+markers', 'name': 'Altitude', 'type': 'scatter', 'x': data['time'],
'y': data['Altitude'], }, 1, 1)
result.append_trace(
{'mode': 'lines+markers', 'name': 'Longitude vs Latitude', 'text': data['time'], 'type': 'scatter',
'x': data['Longitude'], 'y': data['Latitude'], }, 2, 1)
return result
def get_angles(self):
self.get_times()
tle1, tle2 = self.get_tle_lines()
orb = Orbital(self.spacecrafts_orbital[self.spacecraft_id],
line1=tle1,
line2=tle2)
sat_azi, sat_elev = orb.get_observer_look(self.times[:, np.newaxis],
self.lons, self.lats, 0)
sat_zenith = 90 - sat_elev
sun_zenith = astronomy.sun_zenith_angle(self.times[:, np.newaxis],
self.lons, self.lats)
alt, sun_azi = astronomy.get_alt_az(self.times[:, np.newaxis],
self.lons, self.lats)
del alt
sun_azi = np.rad2deg(sun_azi)
sun_azi = np.where(sun_azi < 0, sun_azi + 180, sun_azi - 180)
rel_azi = abs(sat_azi - sun_azi)
rel_azi = np.where(rel_azi > 180.0, 360.0 - rel_azi, rel_azi)
return sat_azi, sat_zenith, sun_azi, sun_zenith, rel_azi
def getGPSPosition(platformName, tleFile, dateTime):
orb = Orbital(platformName, tleFile)
lon, lat, alt = orb.get_lonlatalt(dateTime)
#reading the TLE file
file = open(tleFile)
data = file.read().replace("\n","::")
arr = data.split("::")
for i in range(len(arr)):
if platformName.rstrip() == arr[i].rstrip():
tleOne= arr[i+1]
tleTwo = arr[i+2]
file.close()
sat = ephem.readtle(platformName, tleOne, tleTwo)
#compute satellite position
sat.compute(dateTime)
satlat = math.degrees(sat.sublat)
satlon = math.degrees(sat.sublong)
satele = sat.elevation
satsize = sat.size
satrad = sat.radius
satecl = sat.eclipsed
satasc = sat.a_ra
satdecl = sat.a_dec
return [satlon, satlat, satele, satsize, satrad, satecl, satasc, satdecl]
def __init__(self, aoi, sat, instrument="AVHRR"):
OrbitalLayer.__init__(self, aoi, sat, instrument)
# instantiate orbital module
config_file_path = ""
try:
config_file_path = os.environ['PYGRANULE_CONFIG_PATH']
except KeyError:
print "pygranule config file path missing. Has the 'PYGRANULE_CONFIG_PATH' environment variable been set?"
default_tle_file = config_file_path + "/default.tle"
try:
self.orbital = Orbital(sat, default_tle_file)
except:
print "Failed to open default tle file:", default_tle_file
print "Downloading from internet:"
try:
self.orbital = Orbital(sat)
except:
raise OrbitalLayerError(
"Pyorbital Failed to fetch TLE from internet.")
# create scan geometry - one scan line.
if instrument == "AVHRR":
scan_steps = np.arange(0, self.instrument_info['scan_steps'],
self.instrument_info['scan_steps'] / 8 - 1)
scan_steps[-1] = self.instrument_info['scan_steps'] - 1
self.scan_geom = avhrr(1, scan_steps)
elif instrument == "VIIRS":
self.scan_geom = viirs(1)
def __init__(self, aoi, sat, instrument="AVHRR"):
OrbitalLayer.__init__(self,aoi,sat,instrument)
# instantiate orbital module
config_file_path = ""
try:
config_file_path = os.environ['PYGRANULE_CONFIG_PATH']
except KeyError:
print "pygranule config file path missing. Has the 'PYGRANULE_CONFIG_PATH' environment variable been set?"
default_tle_file = config_file_path+"/default.tle"
try:
self.orbital = Orbital(sat,default_tle_file)
except:
print "Failed to open default tle file:", default_tle_file
print "Downloading from internet:"
try:
self.orbital = Orbital(sat)
except:
raise OrbitalLayerError("Pyorbital Failed to fetch TLE from internet.")
# create scan geometry - one scan line.
if instrument == "AVHRR":
scan_steps = np.arange(0,self.instrument_info['scan_steps'],self.instrument_info['scan_steps']/8-1)
scan_steps[-1] = self.instrument_info['scan_steps']-1
self.scan_geom = avhrr(1,scan_steps)
elif instrument == "VIIRS":
self.scan_geom = viirs(1)
def serialPortRead(passNumber):
#passes = satOrb.get_next_passes(datetime.utcnow(),120, -30.8047389406, 72.9167, 180.85)
#next get number of passes the user wants
satOrb = Orbital(satName, tleFile)
passes = satOrb.get_next_passes(current_time,int(passNumber), home.lat, home.lon, home.elevation)
for eachPass in passes:
rise = eachPass[0]
fall = eachPass[1]
apex = eachPass[2]
# Lon, Lat
obsRiseAngle, obsRiseElv = satOrb.get_observer_look(rise, home.lat, home.lon, home.elevation)
obsFallAngle, obsFallElv = satOrb.get_observer_look(fall, home.lat, home.lon, home.elevation)
obsApexAngle, obsApexElv = satOrb.get_observer_look(apex, home.lat, home.lon, home.elevation)
print("observer apex", obsApexElv)
print("Rise Time:", rise, "Azimuth:", round(obsRiseAngle, 2),
'(', azimuthDirection(obsRiseAngle), ')', "Elevation:", abs(round(obsRiseElv, 2)))
print("Apex Time:", apex, "Azimuth:", round(obsApexAngle, 2),
'(', azimuthDirection(obsApexAngle), ')', "Elevation:", abs(round(obsApexElv, 2)))
print("Fall Time:", fall, "Azimuth:", round(obsFallAngle, 2),
'(', azimuthDirection(obsFallAngle), ')', "Elevation:", abs(round(obsFallElv, 2)))
print()
return
def predict_next_passes(tle_dir: str, satellites: dict, station_location: dict,
min_elevation: float, for_next_hours: int) -> list:
all_passes = []
time_now_utc = datetime.datetime.utcnow()
for sat_name in satellites:
sat = satellites[sat_name]
sat_type = sat["type"]
orbital = Orbital(sat_name,
tle_file="{}/{}/{}.tle".format(
tle_dir, sat_type, sat_name))
passes = orbital.get_next_passes(time_now_utc +
datetime.timedelta(seconds=-60 * 20),
for_next_hours,
station_location["lon"],
station_location["lat"],
station_location["alt"],
horizon=min_elevation)
all_passes += [{
"type": sat_type,
"name": sat_name,
"rise_time": pas[0],
"fall_time": pas[1],
"duration": (pas[1] - pas[0]).total_seconds()
} for pas in passes]
all_passes.sort(key=lambda t: t["rise_time"])
return all_passes
def get_last_valid_tle_lines(platform_name, epoch):
if os.path.exists(os.path.join(REF_DIR, platform_name)):
with open(os.path.join(REF_DIR, platform_name)) as fd:
ref_lines = fd.readlines()
ref_orb = Orbital(platform_name,
line1=ref_lines[1],
line2=ref_lines[2])
if abs(epoch - ref_orb.tle.epoch) < timedelta(days=7):
return ref_lines
else:
logger.info("cached TLE too old, refreshing")
orbit = get_valid_orbit(platform_name, epoch)
files = sorted(get_files(), key=os.path.getctime)
for tle_file in reversed(files):
try:
orb = Orbital(platform_name, tle_file=tle_file)
except AttributeError:
continue
except ChecksumError:
continue
if orb.get_orbit_number(epoch) == orbit:
lines = [orb.tle._platform, orb.tle._line1, orb.tle._line2]
with open(os.path.join(REF_DIR, platform_name), "w") as fd:
fd.write("\n".join(lines))
return lines
def update_graph_scatter(n):
satellite = Orbital('TERRA')
tiempo = []
Latitude = []
Longitude = []
Altitude = []
valor = []
v = []
X.append(datetime.datetime.now() - datetime.timedelta())
Y.append(random.randrange(-20, 20))
#datetime.datetime.now().time()
for i in range(2 * n):
v = random.randrange(-20, 20)
time = datetime.datetime.now() - datetime.timedelta(seconds=i * 20)
lon, lat, alt = satellite.get_lonlatalt(time)
Longitude.append(lon)
Latitude.append(lat)
Altitude.append(alt)
tiempo.append(time)
valor.append(v)
trace1 = go.Scatter(x=list(tiempo),
y=list(Altitude),
name='Altitud',
mode='lines+markers')
return {
'data': [trace1],
'layout': go.Layout(transition={
'duration': 1,
'easing': 'cubic-in-out'
})
}
def time_above_the_horizon(ground_position_lat, ground_position_lon, date, date_format = "%d/%m/%Y", time_window = 24, satellite_sensor = 'aqua', elevation = 0):
'''time_above_the_horizon calculates the observation times of satellite passes for the day and time window of a given position on the earth.
It is based on pyorbital functions.
ground_position_lat = -19.2590 # The latitude of the ground position (int)
ground_position_lon = 146.8169 # The longitude of the ground position (int)
date = '21/06/2016' # date of the day to find passes on. (This is techincally in local time for your location an is converted to UTC internally here.) (string)
date_format = "%d/%m/%Y" # the format of thh date string (string)
satellite_sensor = 'aqua' # the name of the satellite sensor you are tracking (string). for VIIRS use 'SUOMI NPP'
time_window = 24 # Number of hours to find passes (int)
elevation = 0 # the elevation of horizon to compute risetime and falltime. (int)
Returns: [(rise-time, fall-time, max-elevation-time), ...] as datetime objects in the UTC time zone.
Contact:
[email protected]
'''
# check the lat and lons to be sensible.
futs.check_for_sensible_lat_long([ground_position_lat, ground_position_lon])
#set up the satellite
orb = Orbital(satellite_sensor)
# convert the local time to a utc time.
utc_date = futs.local_to_utc(futs.which_time_zone(ground_position_lat, ground_position_lon), date, date_format)
# do calcs and remove the utc awareness from the utc_date so that pyorbital can use it.
time_satellite_is_above_horizon = orb.get_next_passes(utc_date.replace(tzinfo=None), time_window, ground_position_lon, ground_position_lon, elevation)
return time_satellite_is_above_horizon
def compute_pixels(orb, sgeom, times, rpy=(0.0, 0.0, 0.0)):
"""Compute cartesian coordinates of the pixels in instrument scan."""
if isinstance(orb, (list, tuple)):
tle1, tle2 = orb
orb = Orbital("mysatellite", line1=tle1, line2=tle2)
# get position and velocity for each time of each pixel
pos, vel = orb.get_position(times, normalize=False)
# now, get the vectors pointing to each pixel
vectors = sgeom.vectors(pos, vel, *rpy)
# compute intersection of lines (directed by vectors and passing through
# (0, 0, 0)) and ellipsoid. Derived from:
# http://en.wikipedia.org/wiki/Line%E2%80%93sphere_intersection
# do the computation between line and ellipsoid (WGS 84)
# NB: AAPP uses GRS 80...
centre = -pos
a__ = 6378.137 # km
# b__ = 6356.75231414 # km, GRS80
b__ = 6356.752314245 # km, WGS84
radius = np.array([[1 / a__, 1 / a__, 1 / b__]]).T
shape = vectors.shape
xr_ = vectors.reshape([3, -1]) * radius
cr_ = centre.reshape([3, -1]) * radius
ldotc = np.einsum("ij,ij->j", xr_, cr_)
lsq = np.einsum("ij,ij->j", xr_, xr_)
csq = np.einsum("ij,ij->j", cr_, cr_)
d1_ = (ldotc - np.sqrt(ldotc ** 2 - csq * lsq + lsq)) / lsq
# return the actual pixel positions
return vectors * d1_.reshape(shape[1:]) - centre
def __init__(self, ground_station, satellite_tle):
"""Constructor: ground station as GroundStation, satellite TLE as TleManipulator"""
self.__ground_station = ground_station
self.__satellite_tle = satellite_tle
self.__orb = Orbital(str(self.__satellite_tle.get_satellite_number()), \
line1=self.__satellite_tle.get_line1(), \
line2=self.__satellite_tle.get_line2())
def update_graph_live(n):
satellite = Orbital("TERRA")
data = {"time": [], "Latitude": [], "Longitude": [], "Altitude": []}
# Collect some data
for i in range(180):
time = datetime.datetime.now() - datetime.timedelta(seconds=i * 20)
lon, lat, alt = satellite.get_lonlatalt(time)
data["Longitude"].append(lon)
data["Latitude"].append(lat)
data["Altitude"].append(alt)
data["time"].append(time)
# Create the graph with subplots
fig = plotly.tools.make_subplots(rows=2, cols=1, vertical_spacing=0.2)
fig["layout"]["margin"] = {"l": 30, "r": 10, "b": 30, "t": 10}
fig["layout"]["legend"] = {"x": 0, "y": 1, "xanchor": "left"}
fig.append_trace(
{"x": data["time"], "y": data["Altitude"], "name": "Altitude", "mode": "lines+markers", "type": "scatter"}, 1, 1
)
fig.append_trace(
{
"x": data["Longitude"],
"y": data["Latitude"],
"text": data["time"],
"name": "Longitude vs Latitude",
"mode": "lines+markers",
"type": "scatter",
},
2,
1,
)
return fig
def propagate_orbits(TLE_path, days):
num_mins = int(days * 24 * 60)
time_list = [
datetime.datetime(2020, 1, 1, 0, 0, 0, 0) +
datetime.timedelta(seconds=60 * x) for x in range(0, num_mins)
]
num = 0
table = pd.DataFrame(time_list, columns=["Time"])
file = open(TLE_path, "r")
a = file.readline()
b = file.readline()
# Iterate over TLE file
while a != '' and b != '':
orb = Orbital("sat{}".format(num), line1=a, line2=b)
pos_list = []
for time in time_list:
pos = orb.get_position(time, normalize=False)
pos_list.append(pos)
table[str(num)] = pos_list
num += 1
a = file.readline()
b = file.readline()
file.close()
return table
def GetGPSPosition(platformName, tleFile, dateTime):
orb = Orbital(platformName, tleFile)
lon, lat, alt = orb.get_lonlatalt(dateTime)
return [lon, lat, alt, dateTime]
def GetGPSPosition(platformName, tleFile, dateTime):
orb = Orbital(platformName, tleFile)
lon, lat, alt = orb.get_lonlatalt(dateTime)
return [lon, lat, alt, dateTime]
def create_orbital_track_shapefile_for_day (track_day, step, dur):
# получаем TLE для NOAA-19
tle_1 = '1 33591U 09005A 21067.53688389 .00000027 00000-0 40065-4 0 9999'
tle_2 = '2 33591 99.1917 85.7021 0014730 58.0337 302.2263 14.12454575622414'
# Создаём экземляр класса Orbital
orb = Orbital("N", line1=tle_1, line2=tle_2)
i = 0
minutes = 0
coord = np.arange(3*dur).reshape(dur, 3)
while minutes < dur:
# Расчитаем час, минуту, секунду (для текущего шага)
utc_hour = int(minutes // 60)
utc_minutes = int((minutes - (utc_hour*60)) // 1)
utc_seconds = int(round((minutes - (utc_hour*60) - utc_minutes)*60))
utc_string = str(utc_hour) + '-' + str(utc_minutes) + '-' + str(utc_seconds)
utc_time = datetime(track_day.year,track_day.month,track_day.day,utc_hour,utc_minutes,utc_seconds)
# Считаем положение спутника
lon, lat, alt = orb.get_lonlatalt(utc_time)
coord[i] [0] = lon
coord[i] [1] = lat
coord[i] [2] = alt + 6400
i += 1
minutes += step
return coord
def _get_sat_angles_with_tle(self):
tle1, tle2 = self.get_tle_lines()
orb = Orbital(self.spacecrafts_orbital[self.spacecraft_id],
line1=tle1,
line2=tle2)
sat_azi, sat_elev = orb.get_observer_look(self.times[:, np.newaxis],
self.lons, self.lats, 0)
return sat_azi, sat_elev
def get_satellite_coordinates(lon, lat, alt, satellite_id):
try:
satellite = Satellite.objects.get(id=satellite_id)
orb = Orbital(satellite.codename)
now = datetime.utcnow()
return orb.get_observer_look(now, lon, lat, alt)
except Satellite.DoesNotExist:
return None
def get_xyz(t):
orb = Orbital("TJREVERB",
tle_file=(Path(__file__).parent.resolve() /
"tjreverb_tle.txt"))
return ({
'xyz_pos': orb.get_position(t)[0],
'xyz_vel': orb.get_position(t)[1]
})
def get_lonlat(scene, row, col):
"""Get the longitutes and latitudes for the give *rows* and *cols*.
"""
try:
filename = get_filename(scene, "granules")
except IOError:
#from mpop.satin.eps1a import get_lonlat_avhrr
# return get_lonlat_avhrr(scene, row, col)
from pyorbital.orbital import Orbital
import pyproj
from datetime import timedelta
start_time = scene.time_slot
end_time = scene.time_slot + timedelta(minutes=3)
orbital = Orbital("METOP-A")
track_start = orbital.get_lonlatalt(start_time)
track_end = orbital.get_lonlatalt(end_time)
geod = pyproj.Geod(ellps='WGS84')
az_fwd, az_back, dist = geod.inv(track_start[0], track_start[1],
track_end[0], track_end[1])
del dist
M02_WIDTH = 2821885.8962408099
pos = ((col - 1024) * M02_WIDTH) / 2048.0
if row > 520:
lonlatdist = geod.fwd(track_end[0], track_end[1],
az_back - 86.253533216206648, -pos)
else:
lonlatdist = geod.fwd(track_start[0], track_start[1],
az_fwd - 86.253533216206648, pos)
return lonlatdist[0], lonlatdist[1]
try:
if scene.lons is None or scene.lats is None:
records, form = read_raw(filename)
mdrs = [record[1]
for record in records
if record[0] == "mdr"]
sphrs = [record for record in records
if record[0] == "sphr"]
sphr = sphrs[0][1]
scene.lons, scene.lats = _get_lonlats(mdrs, sphr, form)
return scene.lons[row, col], scene.lats[row, col]
except AttributeError:
records, form = read_raw(filename)
mdrs = [record[1]
for record in records
if record[0] == "mdr"]
sphrs = [record for record in records
if record[0] == "sphr"]
sphr = sphrs[0][1]
scene.lons, scene.lats = _get_lonlats(mdrs, sphr, form)
return scene.lons[row, col], scene.lats[row, col]
def get_lla(t):
orb = Orbital("TJREVERB",
tle_file=(Path(__file__).parent.resolve() /
"tjreverb_tle.txt"))
return ({
'lat': orb.get_lonlatalt(t)[0],
'lon': orb.get_lonlatalt(t)[1],
'alt': orb.get_lonlatalt(t)[2]
})
def update_graph_live(n):
satellite = Orbital('TERRA')
data = {
'time': [],
'Latitude': [],
'Longitude': [],
'Altitude': []
}
# Collect some data
for i in range(180):
time = datetime.datetime.now() - datetime.timedelta(seconds=i*20)
lon, lat, alt = satellite.get_lonlatalt(
time
)
data['Longitude'].append(lon)
data['Latitude'].append(lat)
data['Altitude'].append(alt)
data['time'].append(time)
# Create the graph with subplots
fig = plotly.tools.make_subplots(rows=2, cols=2, vertical_spacing=0.2)
fig['layout']['margin'] = {
'l': 30, 'r': 10, 'b': 30, 't': 10
}
fig['layout']['legend'] = {'x': 0, 'y': 1, 'xanchor': 'left'}
fig.append_trace ({
'x': data['time'],
'y': data['Altitude'],
'name': 'Altitude',
'mode': 'lines+markers',
'type': 'scatter'
}, 1, 1)
j = go.Scatter(
x =data['Longitude'],
y= data['Latitude'],
text= data['time'],
name= 'Longitude vs Latitude',
mode= 'lines+markers',
type= 'scatter'
)
#trace = go.Figure(data = airports)
#trace = [i,j]
fig.append_trace(j , 2, 1)
#fig.append_trace(j , 2, 1)
return fig
def runProp():
#orb = Orbital(tle)
orb = Orbital("TJREVERB", tle_file="FILE PATH TO TLE")
now = datetime.utcnow()
#print(tle.inclination)
#print(orb.get_position(now))
print(orb.get_lonlatalt(now))
print()
print(orb.get_next_passes(now, 12, -77.10428, 8.88101, 276, tol=0.001, horizon=0))
def create_orbital_track_shapefile_for_day(year, month, day, step_minutes,
tle_line1, tle_line2,
output_shapefile):
try:
orb = Orbital("N", tle_file=None, line1=tle_line1, line2=tle_line2)
except (ChecksumError):
print 'Invalid TLE'
return 2
try:
year = int(year)
month = int(month)
day = int(day)
step_minutes = float(step_minutes)
except:
print 'Invalid date'
return 3
w = shapefile.Writer(shapefile.POINT)
w.field('ID', 'C', 40)
w.field('TIME', 'C', 40)
w.field('LAT', 'C', 40)
w.field('LON', 'C', 40)
i = 0
minutes = 0
while minutes < 1440:
utc_hour = int(minutes // 60)
utc_minutes = int((minutes - (utc_hour * 60)) // 1)
utc_seconds = int(round(
(minutes - (utc_hour * 60) - utc_minutes) * 60))
utc_string = str(utc_hour) + '-' + str(utc_minutes) + '-' + str(
utc_seconds)
utc_time = datetime.datetime(year, month, day, utc_hour, utc_minutes,
utc_seconds)
lon, lat, alt = orb.get_lonlatalt(utc_time)
w.point(lon, lat)
w.record(str(i), utc_string, str(lat), str(lon))
i += 1
minutes += step_minutes
try:
prj = open("%s.prj" % output_shapefile.replace('.shp', ''), "w")
epsg = 'GEOGCS["WGS 84",DATUM["WGS_1984",SPHEROID["WGS 84",6378137,298.257223563]],PRIMEM["Greenwich",0],UNIT["degree",0.0174532925199433]]'
prj.write(epsg)
prj.close()
w.save(output_shapefile)
except:
print 'Unable to save shapefile'
return 4
def serial_az_el(name, stop_time=(
datetime.utcnow())): # sends data over serial to arduino format (az, el)
satellite = Orbital(name, tle_file=nextPass.path_to_tle)
now = datetime.utcnow()
while int(
(stop_time - now).total_seconds()) >= 0: # while pass is occurring
now = datetime.utcnow()
print(
satellite.get_observer_look(now, nextPass.lon, nextPass.lat,
nextPass.alt)) # print (az, el)
sleep(2) # wait 2 seconds
def test_63(self):
"""Check that no runtimewarning is raised, #63."""
import warnings
from pyorbital.orbital import Orbital
from dateutil import parser
warnings.filterwarnings('error')
orb = Orbital("Suomi-NPP",
line1="1 37849U 11061A 19292.84582509 .00000011 00000-0 25668-4 0 9997",
line2="2 37849 98.7092 229.3263 0000715 98.5313 290.6262 14.19554485413345")
orb.get_next_passes(parser.parse("2019-10-21 16:00:00"), 12, 123.29736, -13.93763, 0)
warnings.filterwarnings('default')
def ground_truth(lat, lon, time, sat, duration):
orb = Orbital(sat, tle_file="active.txt")
delta = timedelta(seconds=1)
azs = []
els = []
for i in range(duration):
az, el = pwm_for(*orb.get_observer_look(time, lon, lat, 0))
azs.append(az)
els.append(el)
time += delta
return azs, els
def update_satellite(self, satellite):
"""Update satellite and renew the orbital instance.
"""
if satellite != self._satellite:
self._satellite = satellite
if self._tle_files is not None:
filelist = glob(self._tle_files)
tle_file = max(filelist, key=lambda x: os.stat(x).st_mtime)
else:
tle_file = None
self._orbital = Orbital(self._satellite.upper(), tle_file)
def __init__(self,name,file):
self.file = file
self.orbital = Orbital(name,file)
self.xyz=[[],[],[]]
self.now = datetime.now()
self.position = self.orbital.get_position(self.now,False)
for i in range(0,2000):
self.now += timedelta(seconds=4)
position = self.orbital.get_position(self.now,False)
for i in range(0,3):
self.xyz[i].append(position[0][i])
def get_valid_orbit(platform_name, epoch):
orb_nums = []
for tle_file in sorted(get_files(), reverse=True):
try:
orb = Orbital(platform_name, tle_file=tle_file)
except AttributeError:
continue
except ChecksumError:
continue
orb_nums.append(orb.get_orbit_number(epoch))
return int(round(np.median(orb_nums)))
def create_orbital_track_shapefile_for_day (year, month, day, step_minutes, tle_line1, tle_line2, sat_name):
try:
orb = Orbital("N",tle_file=None,line1=tle_line1, line2=tle_line2)
except:
raise NameError
try:
year = int(year)
month = int(month)
day = int(day)
step_minutes = float(step_minutes)
except:
raise TypeError
trackLayerName = 'Track Layer (' + str(sat_name) + ': ' + str(year) + ':' + str(month) + ':' + str(day) + ')'
trackLayer = QgsVectorLayer("Point", trackLayerName, "memory")
trackLayer.setCrs(QgsCoordinateReferenceSystem(4326))
trackLayerDataProvider = trackLayer.dataProvider()
trackLayer.startEditing()
trackLayerDataProvider.addAttributes( [ QgsField("ID", QVariant.Int),
QgsField("TIME", QVariant.String),
QgsField("LAT", QVariant.Double),
QgsField("LON", QVariant.Double)] )
i = 0
minutes = 0
while minutes < 1440:
QApplication.processEvents()
utc_hour = int(minutes // 60)
utc_minutes = int((minutes - (utc_hour*60)) // 1)
utc_seconds = int(round((minutes - (utc_hour*60) - utc_minutes)*60))
utc_string = str(utc_hour) + ':' + str(utc_minutes) + ':' + str(utc_seconds)
utc_time = datetime.datetime(year,month,day,utc_hour,utc_minutes,utc_seconds)
lon, lat, alt = orb.get_lonlatalt(utc_time)
trackPoint = QgsFeature()
trackPoint.setGeometry(QgsGeometry.fromPoint(QgsPoint(lon,lat)))
trackPoint.setAttributes([i,utc_string,float(lat),float(lon)])
trackLayerDataProvider.addFeatures ([trackPoint])
i += 1
minutes += step_minutes
trackLayer.commitChanges()
trackLayer.updateExtents()
return trackLayer
def track():
# tle = tlefile.read('ISS', 'orbit.txt')
orbit = Orbital('ISS', 'Telescope/orbit.txt')
while True:
now = datetime.utcnow()
# print(now)
coords = (orbit.get_position(now)[0])
# print(orbit.get_lonlatalt(now))
# print(coords)
print(convertCartesianToRaDec(coords[0], coords[1], coords[2]))
time.sleep(1)
def get_view_zen_angles(sat_name, tle_filename, area_def_name,
time_slot):
"""Calculate the satellite zenith angles for the given satellite
(*sat_name*, *tle_filename*), *area_def_name* and *time slot*.
Stores the result in the given *cache* parameter.
"""
try:
from pyorbital.orbital import Orbital
except ImportError:
LOGGER.warning("Could not load pyorbital modules")
return
area_def = get_area_def(area_def_name)
lons, lats = area_def.get_lonlats()
orbital_obj = Orbital(sat_name, tle_filename)
elevation = orbital_obj.get_observer_look(time_slot, lons, lats, 0)[1]
view_zen_data = np.subtract(90, np.ma.masked_outside(elevation, 0, 90))
return view_zen_data
def extractDataset(self,
satelliteName='ISS (ZARYA)',
sourceDirectory=generateFilename(description = "stations",
extension = ".txt",
dateToday = False),
referenceDate = (2015,10,28,0,0,0),
numberOfSamples = 1440,
numberOfInputs = 4,
incrementSeconds = 60):
self.satelliteName = satelliteName
self.sourceDirectory = sourceDirectory
self.referenceDate = referenceDate
self.numberOfSamples = numberOfSamples
self.numberOfInputs = numberOfInputs
self.dataset = np.zeros(shape=[1,self.numberOfInputs])
self.incrementSeconds = incrementSeconds
self.min = 0
self.max = 0
self.min_dataset = 0
self.max_dataset = 0
try:
# reading input data
input_data = Orbital(self.satelliteName, self.sourceDirectory)
# calculate date
date = datetime.datetime(*self.referenceDate)
#1440 for the number of minutes in a day
for point_n in xrange(self.numberOfSamples):
#each point will be collected with a specified difference of seconds
date += datetime.timedelta(0,incrementSeconds)
output_data = input_data.get_position(date,normalize=False)
self.dataset = np.vstack([self.dataset, np.append(output_data[0],[point_n + referenceDate[4]])])
self.dataset = np.delete(self.dataset,0,0)
return 0
except:
return 1
def update_satellite(self, satellite):
"""Update satellite and renew the orbital instance.
"""
if satellite != self._satellite:
self._satellite = satellite
if self._tle_files is not None:
filelist = glob(self._tle_files)
tle_file = max(filelist, key=lambda x: os.stat(x).st_mtime)
else:
tle_file = None
self._orbital = Orbital(self._satellite.upper(), tle_file)
def __init__(self):
self.ground_lat = EARTH_STATION_LAT
self.ground_long = EARTH_STATION_LONG
self.observer = ephem.Observer()
self.observer.lat = self.ground_lat
self.observer.long = self.ground_long
self.observer.date = datetime.utcnow()
self.tle = IN_TLE_FILE
self.tles = []
self.satellite_name = TRK_SATELLITE
self.orb = Orbital(self.satellite_name,tle_file=self.tle)
def create_subdirname(obstime, with_seconds=False, **kwargs):
"""Generate the pps subdirectory name from the start observation time, ex.:
'npp_20120405_0037_02270'"""
if "orbit" in kwargs:
orbnum = int(kwargs['orbit'])
else:
from pyorbital.orbital import Orbital
from npp_runner import orbitno
try:
tle = orbitno.get_tle('npp', obstime)
orbital_ = Orbital(tle.platform, line1=tle.line1, line2=tle.line2)
orbnum = orbital_.get_orbit_number(obstime, tbus_style=TBUS_STYLE)
except orbitno.NoTleFile:
LOG.error('Not able to determine orbit number!')
import traceback
traceback.print_exc(file=sys.stderr)
orbnum = 1
if with_seconds:
return obstime.strftime('npp_%Y%m%d_%H%M%S_') + '%.5d' % orbnum
else:
return obstime.strftime('npp_%Y%m%d_%H%M_') + '%.5d' % orbnum
def on_opened(self, event):
fname = os.path.split(event.src_path)[1]
if self._file is None and fnmatch(fname, self._file_pattern):
logger.debug("Opening: " + event.src_path)
self._filename = event.src_path
self._file = open(event.src_path, "rb")
self._where = 0
self._satellite = " ".join(event.src_path.split("_")[1:3])[:-5]
if self._tle_files is not None:
filelist = glob(self._tle_files)
tle_file = max(filelist, key=lambda x: os.stat(x).st_mtime)
else:
tle_file = None
self._orbital = Orbital(self._satellite, tle_file)
class NPP_Orbit:
# Constructor of NPP_Orbit
def __init__(self):
self.ground_lat = EARTH_STATION_LAT
self.ground_long = EARTH_STATION_LONG
self.observer = ephem.Observer()
self.observer.lat = self.ground_lat
self.observer.long = self.ground_long
self.observer.date = datetime.utcnow()
self.tle = IN_TLE_FILE
self.tles = []
self.satellite_name = TRK_SATELLITE
self.orb = Orbital(self.satellite_name,tle_file=self.tle)
# Functions
def read_tle(self):
self.tles = open(self.tle, 'r').readlines()
self.tles = [item.strip() for item in self.tles]
self.tles = [(self.tles[i], self.tles[i+1], self.tles[i+2]) \
for i in xrange(0, len(self.tles)-2, 3)]
return
def get_pass_num_t(self,yyyy,mm,dd,hh,mn,ss):
indate = str(yyyy) + '-' + str(mm) + '-' +str(dd) + ' ' +\
str(hh) + ':' + str(mn) + ':' + str(ss)
self.observer.date = indate
for tle in self.tles:
if tle[0].strip() == self.satellite_name:
sat = ephem.readtle(tle[0],tle[1],tle[2])
rt, ra, tt, ta, st, sa = self.observer.next_pass(sat)
num = self.orb.get_orbit_number(datetime.strptime(str(tt), "%Y/%m/%d %H:%M:%S"),tbus_style=True)
return num
def __del__(self):
pass
def SatStats():
#tle = r"C:\Users\Jake\Python\TLE Files\stations-tle.txt"
# Download TLE file
#downloadUrl = "http://www.celestrak.com/NORAD/elements/stations.txt"
#urllib.request.urlretrieve(downloadUrl, tle)
tle = GetTLEFile()
stationList = GetStationList(tle)
try:
while(True):
stationNumber = input("Enter Station Number: ")
print()
if stationNumber == 'n':
for name in enumerate(stationList):
print(name[0], ':', name[1].replace('\n', ''))
print()
else:
break
stationNumber = int(stationNumber)
if stationNumber < len(stationList):
# Get Platform Object
station = stationList[stationNumber]
stationObject = tlefile.read(station, tle)
GoogleSearch(station)
# Print Platform Info
PrintTLEInfo(stationObject, station)
lon, lat, alt, now = GetGPSPosition(station, tle, datetime.utcnow())
dmLon, dmLat = DegreeMinutes(lon, lat)
print("Current GPS location:\n", "Latitude: ", lat, " Longitude: ", lon, " Altitude (km): ", alt, sep='')
print("Current GPS location:\n", "Latitude: ", dmLat, " Longitude: ", dmLon, " Altitude (km): ", alt, sep='')
satOrb = Orbital(station, tle)
print()
PrintFreqData(GetFreqData(station, "C:/Users/Jake/Python/Satellite Tracker/frequencies/satfreqlist.csv"))
passes = satOrb.get_next_passes(datetime.utcnow(), 120, -90.5546910, 38.6475290, 180.85)
print("Next passes in 5 days (Max Elevation Above 20 deg):")
for eachPass in passes:
rise = eachPass[0]
fall = eachPass[1]
apex = eachPass[2]
# Lon, Lat
obsRiseAngle, obsRiseElv = satOrb.get_observer_look(rise, -90.5546910, 38.6475290, 180.85)
obsFallAngle, obsFallElv = satOrb.get_observer_look(fall, -90.5546910, 38.6475290, 180.85)
obsApexAngle, obsApexElv = satOrb.get_observer_look(apex, -90.5546910, 38.6475290, 180.85)
if obsApexElv >= 20.0:
print("Rise Time:", rise, "Azimuth:", round(obsRiseAngle, 2),
'(', AzimuthDirection(obsRiseAngle), ')', "Elevation:", abs(round(obsRiseElv, 2)))
print("Apex Time:", apex, "Azimuth:", round(obsApexAngle, 2),
'(', AzimuthDirection(obsApexAngle), ')', "Elevation:", abs(round(obsApexElv, 2)))
print("Fall Time:", fall, "Azimuth:", round(obsFallAngle, 2),
'(', AzimuthDirection(obsFallAngle), ')', "Elevation:", abs(round(obsFallElv, 2)))
print()
except:
pass
import time
import calendar
SIDERAL_DAY_SEC = 86164.0905
MU = 398600 # Earth standard gravitational parameter
satellite = sys.argv[1]
userLat = float(sys.argv[2])
userLng = float(sys.argv[3])
userAlt = float(sys.argv[4])
line1 = sys.argv[5]
line2 = sys.argv[6]
tle = tlefile.read(satellite, None, line1, line2)
orb = Orbital(satellite, None, line1, line2)
now = datetime.utcnow()
# Get normalized position and velocity of the satellite:
pos, vel = orb.get_position(now)
# Get longitude, latitude and altitude of the satellite:
position = orb.get_lonlatalt(now)
data = {}
timestamp = calendar.timegm(now.utctimetuple())
az, el = orb.get_observer_look(now, userLng, userLat, userAlt);
data['user_view'] = {}
def getUpcomingPasses(satellite_name,satellite_swath,tle_information, passes_begin_time, passes_period):
observer = ephem.Observer()
observer.lat = GROUND_STATION[0]
observer.long = GROUND_STATION[1]
#updatetime = 0
period = passes_period
#Get most recent TLE for determining upcoming passes from now
tles = tle_information
# make a list of dicts to hold the upcoming pass information for the selected satellites
SCHEDULE = []
observer.date = passes_begin_time
while 1:
for tle in tles:
if tle[0].strip()== satellite_name:
#TODO clean up the use of pyephem versus orbital. Orbital can give a orbit number and does many of the pyephem functions
#TODO add the individual acquisitions as layers in the same ogr output
#TODO use an appropriate google earth icon for satellites at a visible display resolution with a name tag and minutesaway
#TODO print output to logging
satname = str(tle[0]).replace(" ","_")
sat = ephem.readtle(tle[0],tle[1],tle[2])
twole = tlefile.read(tle[0],DATA_IN_DIR+'tles.txt')
now = datetime.utcnow()
#TODO check age of TLE - if older than x days get_tle()
# print "TLE EPOCH:",twole.epoch
oi = float(str.split(tle[2],' ')[3])
orb = Orbital(tle[0])
attributes = []
rt, ra, tt, ta, st, sa = observer.next_pass(sat)
# Determine is pass descending or ascending
sat.compute(rt)
aos_lat = sat.sublat.real*(180/math.pi)
sat.compute(st)
los_lat = sat.sublat.real*(180/math.pi)
if (aos_lat > los_lat):
# print "PASS = descending"
node = "descending"
else:
# print "PASS = ascending"
node = "ascending"
oi = 360 - oi
AOStime = datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S")
minutesaway = (AOStime-now).seconds/60.0
# print "Satellie = ", satname
# print "Minutes to horizon = ", minutesaway
# print "AOStime = ", rt
# print "LOStime = ", st
# print "Transit time = ", tt
# -----------------------------------------------------------------------------
# This is a test routine for calculating Az, El angles
# -----------------------------------------------------------------------------
orad = orb.get_lonlatalt(datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S"))[2]
# print '&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&'
test_az_el_cal(orb,observer, rt, ra, tt, ta, st, sa,orad)
# print '&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&&'
#
attributes = {'Satellite name': satname, 'Orbit height': orad, 'Orbit': orb.get_orbit_number(datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S")), \
# attributes = {'Satellite name': satname, 'Orbit height': orad, 'Orbit': orb.get_orbit_number(datetime.strptime(str(tt), "%Y/%m/%d %H:%M:%S")), \
'Current time': str(now),'Minutes to horizon': minutesaway, 'AOS time': str(rt), \
'LOS time': str(st), 'Transit time': str(tt), 'Node': node}
# Append the attributes to the list of acquisitions for the acquisition period
if not any ((x['Satellite name'] == satname and x['Orbit'] == orb.get_orbit_number(datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S")))for x in SCHEDULE):
# if not any ((x['Satellite name'] == satname and x['Orbit'] == orb.get_orbit_number(datetime.strptime(str(tt), "%Y/%m/%d %H:%M:%S")))for x in SCHEDULE):
SCHEDULE.append(attributes)
# Step from AOS to LOS in 100 second intervals
# delta = timedelta(seconds=100)
delta = timedelta(seconds=DELTA_TIME_STEP)
deltatime = datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S")
geoeastpoint = []
geowestpoint = []
geotrack = []
# print "DELTATIME", deltatime
# print "SETTING TIME", datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S")
# Tesing for next satellite
# --------------------------------------------------------------------------------------------
# --------------------------------------------------------------------------------------------
# The following set of lines have been for testing while making comparision in seconds
# instead of string comparisiom
# --------------------------------------------------------------------------------------------
# --------------------------------------------------------------------------------------------
# print '================ Testing Loop starts ==========================================='
# print 'deltatime = ',deltatime
# print 'Secs Time = ', get_time_secs(str(deltatime).replace("-","/"))
# print 'st = ',str(datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S"))
# print 'st in Secs Time = ',get_time_secs(str(datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S")).replace('-','/'))
# print '================ Testing Loop Ends ==========================================='
# The following if statement has ben included on the basis of dpoch seconds
#
if get_time_secs(str(deltatime).replace("-","/")) >= \
get_time_secs(str(datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S")).replace('-','/')):
return()
print 'Delta Time = ',deltatime
print 'date time = ',datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S")
print '---------------------------'
# if deltatime >= datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S"):
# return()
while deltatime < datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S"):
sat.compute(deltatime)
geotrack.append({'lat2': sat.sublat.real*(180/math.pi), \
'lon2': sat.sublong.real*(180/math.pi), \
'alt2': orb.get_lonlatalt(datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S"))[2]*1000})
eastaz = getEffectiveHeading(sat,oi,sat.sublat.real*(180/math.pi), sat.sublong.real*(180/math.pi), orad, sat._n)+90
westaz = getEffectiveHeading(sat,oi,sat.sublat.real*(180/math.pi), sat.sublong.real*(180/math.pi), orad, sat._n)+270
#Set ground swath per satellite sensor
#TODO use view angle check to refine step from satellite track see IFOV
swath = float(satellite_swath)/2.
geoeastpoint.append(Geodesic.WGS84.Direct(sat.sublat.real*180/math.pi, sat.sublong.real*180/math.pi, eastaz, swath))
geowestpoint.append(Geodesic.WGS84.Direct(sat.sublat.real*180/math.pi, sat.sublong.real*180/math.pi, westaz, swath))
deltatime = deltatime+delta
# Create current location ogr output
nowpoint = [{'lat2':orb.get_lonlatalt(datetime.utcnow())[1],'lon2':orb.get_lonlatalt(datetime.utcnow())[0],'alt2':orb.get_lonlatalt(datetime.utcnow())[2]*1000}]
#TODO ensure the now attributes are actually attributes for the current position of the satellite and include relevant next pass information...tricky?
#if ((attributes['Orbit']==orb.get_orbit_number(datetime.utcnow()))and(AOStime<now)):
now_attributes = {'Satellite name': satname, 'Orbit height': orb.get_lonlatalt(datetime.utcnow())[2], 'Orbit': orb.get_orbit_number(datetime.utcnow()), \
'Current time': str(now),'Minutes to horizon': "N/A", 'AOS time': "N/A", \
'LOS time': "N/A", 'Transit time': "N/A", 'Node': "N/A"}
#now_attributes=attributes
#CURRENT_POSITION_FILENAME = satname+"_current_position.kml"
CURRENT_POSITION_FILENAME = OUTPUT_DIR+satname+"_current_position.kml"
#TODO draw the current orbit forward for the passes period time from the satellite position as a long stepped ogr line
getVectorFile(now_attributes,nowpoint,'point', CURRENT_POSITION_FILENAME, 'KML')
polypoints = []
for x in geowestpoint:
polypoints.append({'lat2':x['lat2'],'lon2':x['lon2']})
for x in reversed(geoeastpoint):
polypoints.append({'lat2':x['lat2'],'lon2':x['lon2']})
if len(polypoints)>0:
polypoints.append({'lat2':geowestpoint[0]['lat2'],'lon2':geowestpoint[0]['lon2']})
# Create swath footprint ogr output
SWATH_FILENAME = os.path.join(output_path,satname+"."+str(orb.get_orbit_number(datetime.strptime(str(rt),"%Y/%m/%d %H:%M:%S")))+".ALICE.orbit_swath.kml")
ORBIT_FILENAME = os.path.join(output_path,satname+"."+str(orb.get_orbit_number(datetime.strptime(str(rt),"%Y/%m/%d %H:%M:%S")))+".ALICE.orbit_track.kml")
TRACKING_SWATH_FILENAME = os.path.join(output_path,satname+"_tracking_now.kml")
# Create currently acquiring polygon
#TODO def this
# Step from AOS to current time second intervals
observer.date=datetime.utcnow()
sat.compute(observer)
# tkdelta = timedelta(seconds=100)
tkdelta = timedelta(seconds=DELTA_TIME_STEP)
tkrt, tkra, tktt, tkta, tkst, tksa = observer.next_pass(sat)
tkdeltatime = datetime.utcnow()
tkgeoeastpoint = []
tkgeowestpoint = []
tkgeotrack = []
while tkdeltatime < (datetime.utcnow() or datetime.strptime(str(tkst),"%Y/%m/%d %H:%M:%S")):
sat.compute(tkdeltatime)
tkgeotrack.append({'lat2':sat.sublat.real*(180/math.pi),'lon2':sat.sublong.real*(180/math.pi),'alt2':orb.get_lonlatalt(datetime.strptime(str(rt),"%Y/%m/%d %H:%M:%S"))[2]})
tkeastaz = getEffectiveHeading(sat,oi,sat.sublat.real*(180/math.pi), sat.sublong.real*(180/math.pi),orad,sat._n)+90
tkwestaz = getEffectiveHeading(sat,oi,sat.sublat.real*(180/math.pi), sat.sublong.real*(180/math.pi),orad,sat._n)+270
#TODO use view angle check to refine step from satellite track see IFOV
tkswath = float(satellite_swath)/2.
tkgeoeastpoint.append(Geodesic.WGS84.Direct(sat.sublat.real*180/math.pi, sat.sublong.real*180/math.pi, tkeastaz, tkswath))
tkgeowestpoint.append(Geodesic.WGS84.Direct(sat.sublat.real*180/math.pi, sat.sublong.real*180/math.pi, tkwestaz, tkswath))
tkdeltatime = tkdeltatime+tkdelta
tkpolypoints = []
for x in tkgeowestpoint:
tkpolypoints.append({'lat2':x['lat2'],'lon2':x['lon2']})
for x in reversed(tkgeoeastpoint):
tkpolypoints.append({'lat2':x['lat2'],'lon2':x['lon2']})
if len(tkpolypoints)>0:
tkpolypoints.append({'lat2':tkgeowestpoint[0]['lat2'],'lon2':tkgeowestpoint[0]['lon2']})
if not ((attributes['Node']=="ascending")and(satname not in ("AQUA"))):
# Create swath ogr output
getVectorFile(attributes,polypoints,'polygon', SWATH_FILENAME, 'KML')
# Create orbit track ogr output
getVectorFile(attributes,geotrack,'line', ORBIT_FILENAME, 'KML')
# Create currently acquiring ogr output
if ((now >= datetime.strptime(str(tkrt),"%Y/%m/%d %H:%M:%S")) and (now <= datetime.strptime(str(tkst),"%Y/%m/%d %H:%M:%S"))):
getVectorFile(now_attributes,tkpolypoints,'polygon', TRACKING_SWATH_FILENAME, 'KML')
if minutesaway <= period:
# print tle[0], 'WILL BE MAKING A PASS IN ', minutesaway, " MINUTES"
# print ' Rise Azimuth: ', ra
# print ' Transit Time: ', tt
# print ' Transit Altitude: ', ta
# print ' Set Time: ', st
# print ' Set Azimuth: ', sa
# print '================================================='
# print 'Satellite Name = ',satellite_name
for x in sorted(SCHEDULE, key=lambda k: k['AOS time']):
# print x
output_orbit_parameters(x)
# For dictionary entries with 'LOS time' older than now time - remove
if ((datetime.strptime(str(x['LOS time']),"%Y/%m/%d %H:%M:%S"))<(datetime.utcnow())):
# Delete output ogr
if os.path.exists(os.path.join(output_path,satname+"."+str(x['Orbit'])+".ALICE.orbit_swath.kml")):
os.remove(os.path.join(output_path,satname+"."+str(x['Orbit'])+".ALICE.orbit_swath.kml"))
if os.path.exists(os.path.join(output_path,satname+"."+str(x['Orbit'])+".ALICE.orbit_track.kml")):
os.remove(os.path.join(output_path,satname+"."+str(x['Orbit'])+".ALICE.orbit_track.kml"))
# Delete dictionary entry for pass
SCHEDULE.remove(x)
# Unlikely - if no entries in the SCHEDULE don't try to print it
if len(SCHEDULE)>0:
print (datetime.strptime(str(SCHEDULE[0]['AOS time']),"%Y/%m/%d %H:%M:%S"))
# If the AOS time is less than now + the time delta, shift the time to the latest recorded pass LOS time
if ((datetime.strptime(str(SCHEDULE[len(SCHEDULE)-1]['AOS time']),"%Y/%m/%d %H:%M:%S")<(datetime.utcnow()+timedelta(minutes=period)))):
observer.date = (datetime.strptime(str(SCHEDULE[len(SCHEDULE)-1]['LOS time']),"%Y/%m/%d %H:%M:%S")+timedelta(minutes=5))
# Recompute the satellite position for the update time
sat.compute(observer)
# print "MODIFIED OBSERVER DATE",observer.date
else:
# print "--------NOTHING TO MODIFY MOVING TO NEXT SATELLITE IN LIST------"
#TODO - write to html
# Exit the def if the SCHEDULE isn't able to update because there are no passes in the acquisition window
return ()
# print 'Before Time Sleep ......'
# print 'Loop for While .........'
print '============================================================================='
time.sleep(1*SLEEP_STATUS)
return ()
class FileStreamer(FileSystemEventHandler):
"""Get the updates from files.
TODO: separate holder from file handling.
"""
def __init__(self, holder, configfile, *args, **kwargs):
FileSystemEventHandler.__init__(self, *args, **kwargs)
self._file = None
self._filename = ""
self._where = 0
self._satellite = ""
self._orbital = None
cfg = ConfigParser()
cfg.read(configfile)
self._coords = cfg.get("local_reception", "coordinates").split(" ")
self._coords = [float(self._coords[0]),
float(self._coords[1]),
float(self._coords[2])]
self._station = cfg.get("local_reception", "station")
logger.debug("Station " + self._station +
" located at: " + str(self._coords))
try:
self._tle_files = cfg.get("local_reception", "tle_files")
except NoOptionError:
self._tle_files = None
self._file_pattern = cfg.get("local_reception", "file_pattern")
self.scanlines = holder
self._warn = True
def update_satellite(self, satellite):
"""Update satellite and renew the orbital instance.
"""
if satellite != self._satellite:
self._satellite = satellite
if self._tle_files is not None:
filelist = glob(self._tle_files)
tle_file = max(filelist, key=lambda x: os.stat(x).st_mtime)
else:
tle_file = None
self._orbital = Orbital(self._satellite.upper(), tle_file)
def on_created(self, event):
"""Callback when file is created.
"""
if event.src_path != self._filename:
if self._filename:
logger.info("Closing: " + self._filename)
if self._file:
self._file.close()
self._file = None
self._filename = ""
self._where = 0
self._satellite = ""
self._warn = True
logger.info("New file detected: " + event.src_path)
def on_opened(self, event):
"""Callback when file is opened
"""
fname = os.path.split(event.src_path)[1]
if self._file is None and fnmatch(fname, self._file_pattern):
logger.info("File opened: " + event.src_path)
self._filename = event.src_path
self._file = open(event.src_path, "rb")
self._where = 0
self._satellite = ""
self._orbital = None
self._warn = True
def on_modified(self, event):
self.on_opened(event)
if event.src_path != self._filename:
return
self._file.seek(self._where)
line = self._file.read(LINE_SIZE)
while len(line) == LINE_SIZE:
line_start = self._where
self._where = self._file.tell()
dtype = np.dtype([('frame_sync', '>u2', (6, )),
('id', [('id', '>u2'),
('spare', '>u2')]),
('timecode', '>u2', (4, )),
('telemetry', [("ramp_calibration", '>u2', (5, )),
("PRT", '>u2', (3, )),
("ch3_patch_temp", '>u2'),
("spare", '>u2'),]),
('back_scan', '>u2', (10, 3)),
('space_data', '>u2', (10, 5)),
('sync', '>u2'),
('TIP_data', '>u2', (520, )),
('spare', '>u2', (127, )),
('image_data', '>u2', (2048, 5)),
('aux_sync', '>u2', (100, ))])
array = np.fromstring(line, dtype=dtype)
if np.all(abs(HRPT_SYNC_START -
array["frame_sync"]) > 1):
array = array.newbyteorder()
# FIXME: this means server can only share 1 year of hrpt data.
now = datetime.utcnow()
year = now.year
utctime = datetime(year, 1, 1) + timecode(array["timecode"][0])
if utctime > now:
# Can't have data from the future... yet :)
utctime = (datetime(year - 1, 1, 1)
+ timecode(array["timecode"][0]))
# Check that we receive real-time data
if not (np.all(array['aux_sync'] == HRPT_SYNC) and
np.all(array['frame_sync'] == HRPT_SYNC_START)):
logger.info("Garbage line: " + str(utctime))
line = self._file.read(LINE_SIZE)
continue
if (now - utctime).days > 7 and self._warn:
logger.warning("Data is more than a week old: " + str(utctime))
self._warn = False
satellite = SATELLITES[((array["id"]["id"] >> 3) & 15)[0]]
self.update_satellite(satellite)
elevation = self._orbital.get_observer_look(utctime,
*self._coords)[1]
logger.debug("Got line " + utctime.isoformat() + " "
+ self._satellite + " "
+ str(elevation))
# TODO:
# - serve also already present files
# - timeout and close the file
self.scanlines.add_scanline(self._satellite, utctime,
elevation, line_start, self._filename,
line)
line = self._file.read(LINE_SIZE)
self._file.seek(self._where)
while True:
lat2 = lat
c = 1/(np.sqrt(1 - e2 * (np.sin(lat2) ** 2)))
lat = np.arctan2(pos_z + c * e2 *np.sin(lat2), r)
if np.all(abs(lat - lat2) < 1e-10):
break
alt = r / np.cos(lat)- c;
alt *= A
return np.rad2deg(lon), np.rad2deg(lat), alt
### END OF DIRTY STUFF
def compute_pixels((tle1, tle2), sgeom, start_of_scan):
"""Compute cartesian coordinates of the pixels in instrument scan.
"""
orb = Orbital("mysatellite", line1=tle1, line2=tle2)
# times for each pixel
times = sgeom.times(start_of_scan)
# get position and velocity for each time of each pixel
pos, vel = orb.get_position(times, normalize=False)
# now, get the vectors pointing to each pixel
vectors = sgeom.vectors(pos, vel)
## compute intersection of lines (directed by vectors and passing through
## (0, 0, 0)) and sphere
## http://en.wikipedia.org/wiki/Line%E2%80%93sphere_intersection
# get the radius of the earth at the given times
lat2 = lat
c = 1 / (np.sqrt(1 - e2 * (np.sin(lat2) ** 2)))
lat = np.arctan2(pos_z + c * e2 * np.sin(lat2), r)
if np.all(abs(lat - lat2) < 1e-10):
break
alt = r / np.cos(lat) - c
alt *= A
return np.rad2deg(lon), np.rad2deg(lat), alt
# END OF DIRTY STUFF
def compute_pixels((tle1, tle2), sgeom, times, rpy=(0.0, 0.0, 0.0)):
"""Compute cartesian coordinates of the pixels in instrument scan.
"""
orb = Orbital("mysatellite", line1=tle1, line2=tle2)
# get position and velocity for each time of each pixel
pos, vel = orb.get_position(times, normalize=False)
# now, get the vectors pointing to each pixel
vectors = sgeom.vectors(pos, vel, *rpy)
# compute intersection of lines (directed by vectors and passing through
# (0, 0, 0)) and ellipsoid. Derived from:
# http://en.wikipedia.org/wiki/Line%E2%80%93sphere_intersection
# do the computation between line and ellipsoid (WGS 84)
# NB: AAPP uses GRS 80...
centre = -pos
a__ = 6378.137 # km
def replace_orbitno(filename):
stamp = get_npp_stamp(filename)
# Correct h5 attributes
no_date = datetime(1958, 1, 1)
epsilon_time = timedelta(days=2)
import h5py
def _get_a_good_time(name, obj):
del name
if isinstance(obj, h5py.Dataset):
date_key, time_key = ('Ending_Date', 'Ending_Time')
if date_key in obj.attrs.keys():
if not good_time_val_[0]:
time_val = datetime.strptime(
obj.attrs[date_key][0][0] +
obj.attrs[time_key][0][0],
'%Y%m%d%H%M%S.%fZ')
if abs(time_val - no_date) > epsilon_time:
good_time_val_[0] = time_val
def _check_orbitno(name, obj):
del name
if isinstance(obj, h5py.Dataset):
for date_key, time_key, orbit_key in (
('AggregateBeginningDate', 'AggregateBeginningTime',
'AggregateBeginningOrbitNumber'),
('AggregateEndingDate', 'AggregateEndingTime',
'AggregateEndingOrbitNumber'),
('Beginning_Date', 'Beginning_Time',
'N_Beginning_Orbit_Number')):
if orbit_key in obj.attrs.keys():
time_val = datetime.strptime(
obj.attrs[date_key][0][0] +
obj.attrs[time_key][0][0],
'%Y%m%d%H%M%S.%fZ')
# Check for no date (1958) problem:
if abs(time_val - no_date) < epsilon_time:
LOG.info("Start time wrong: %s",
time_val.strftime('%Y%m%d'))
LOG.info("Will use the first good end time encounter " +
"in file to determine orbit number")
time_val = good_time_val_[0]
orbit_val = orbital_.get_orbit_number(time_val,
tbus_style=TBUS_STYLE)
obj.attrs.modify(orbit_key, [[orbit_val]])
counter_[0] += 1
# Correct h5 attributes
orbital_ = Orbital(TLE_SATNAME[stamp.platform])
orbit = orbital_.get_orbit_number(stamp.start_time, tbus_style=TBUS_STYLE)
LOG.info("Replacing orbit number %05d with %05d",
stamp.orbit_number, orbit)
fp = h5py.File(filename, 'r+')
try:
good_time_val_ = [None]
fp.visititems(_get_a_good_time)
counter_ = [0]
fp.visititems(_check_orbitno)
if counter_[0] == 0:
raise IOError(
"Failed replacing orbit number in hdf5 attributes '%s'" % filename)
LOG.info("Replaced orbit number in %d attributes", counter_[0])
finally:
fp.close()
# Correct filename
dname, fname = os.path.split(filename)
fname, n = _re_replace_orbitno.subn('_b%05d' % orbit, fname)
if n != 1:
raise IOError("Failed replacing orbit number in filename '%s'" % fname)
return os.path.join(dname, fname), orbit
class FileStreamer(FileSystemEventHandler):
"""Get the updates from files.
TODO: separate holder from file handling.
"""
def __init__(self, holder, configfile, *args, **kwargs):
FileSystemEventHandler.__init__(self, *args, **kwargs)
self._file = None
self._filename = ""
self._where = 0
self._satellite = ""
self._orbital = None
cfg = ConfigParser()
cfg.read(configfile)
self._coords = cfg.get("local_reception", "coordinates").split(" ")
self._coords = [float(self._coords[0]),
float(self._coords[1]),
float(self._coords[2])]
logger.debug(self._coords)
try:
self._tle_files = cfg.get("local_reception", "tle_files")
except NoOptionError:
self._tle_files = None
self._file_pattern = cfg.get("local_reception", "file_pattern")
self.scanlines = holder
def on_created(self, event):
if event.src_path != self._filename:
logger.debug("Closing: " + self._filename)
if self._file:
self._file.close()
self._file = None
self._filename = ""
self._where = 0
self._satellite = ""
logger.debug("Creating: " + event.src_path)
def on_opened(self, event):
fname = os.path.split(event.src_path)[1]
if self._file is None and fnmatch(fname, self._file_pattern):
logger.debug("Opening: " + event.src_path)
self._filename = event.src_path
self._file = open(event.src_path, "rb")
self._where = 0
self._satellite = " ".join(event.src_path.split("_")[1:3])[:-5]
if self._tle_files is not None:
filelist = glob(self._tle_files)
tle_file = max(filelist, key=lambda x: os.stat(x).st_mtime)
else:
tle_file = None
self._orbital = Orbital(self._satellite, tle_file)
def on_modified(self, event):
self.on_opened(event)
if event.src_path != self._filename:
return
self._file.seek(self._where)
line = self._file.read(LINE_SIZE)
while len(line) == LINE_SIZE:
line_start = self._where
self._where = self._file.tell()
dtype = np.dtype([('frame_sync', '>u2', (6, )),
('id', [('id', '>u2'),
('spare', '>u2')]),
('timecode', '>u2', (4, )),
('telemetry', [("ramp_calibration", '>u2', (5, )),
("PRT", '>u2', (3, )),
("ch3_patch_temp", '>u2'),
("spare", '>u2'),]),
('back_scan', '>u2', (10, 3)),
('space_data', '>u2', (10, 5)),
('sync', '>u2'),
('TIP_data', '>u2', (520, )),
('spare', '>u2', (127, )),
('image_data', '>u2', (2048, 5)),
('aux_sync', '>u2', (100, ))])
array = np.fromstring(line, dtype=dtype)
if np.all(abs(HRPT_SYNC_START -
array["frame_sync"]) > 1):
array = array.newbyteorder()
# FIXME: this is bad!!!! Should not get the year from the filename
year = int(os.path.split(event.src_path)[1][:4])
utctime = datetime(year, 1, 1) + timecode(array["timecode"][0])
# Check that we receive real-time data
if not (np.all(array['aux_sync'] == HRPT_SYNC) and
np.all(array['frame_sync'] == HRPT_SYNC_START)):
logger.info("Garbage line: " + str(utctime))
line = self._file.read(LINE_SIZE)
continue
elevation = self._orbital.get_observer_look(utctime, *self._coords)[1]
logger.info("Got line " + utctime.isoformat() + " "
+ self._satellite + " "
+ str(elevation))
# TODO:
# - serve also already present files
# - timeout and close the file
self.scanlines.add_scanline(self._satellite, utctime,
elevation, line_start, self._filename,
line)
line = self._file.read(LINE_SIZE)
self._file.seek(self._where)
def getUpcomingPasses(satellite_name, tle_information, passes_begin_time, passes_period):
observer = ephem.Observer()
observer.lat = ground_station[0]
observer.long = ground_station[1]
#updatetime = 0
period = passes_period
#Get most recent TLE for determining upcoming passes from now
tles = tle_information
# make a list of dicts to hold the upcoming pass information for the selected satellites
schedule = []
observer.date = passes_begin_time
while 1:
print "---------------------------------------"
for tle in tles:
if tle[0] == satellite_name:
#TODO clean up the use of pyephem versus orbital. Orbital can give a orbit number and does many of the pyephem functions
#TODO add the individual acquisitions as layers in the same ogr output
#TODO use an appropriate google earth icon for satellites at a visible display resolution with a name tag and minutesaway
#TODO print output to logging
satname = str(tle[0]).replace(" ","_")
sat = ephem.readtle(tle[0],tle[1],tle[2])
twole = tlefile.read(tle[0],'tles.txt')
now = datetime.utcnow()
#TODO check age of TLE - if older than x days get_tle()
print "TLE EPOCH:",twole.epoch
#if twole.epoch < now - timedelta(days=5):
# get_tles()
# satname = str(tle[0]).replace(" ","_")
# sat = ephem.readtle(tle[0],tle[1],tle[2])
# twole = tlefile.read(tle[0],'tles.txt')
print "---------------------------------------"
print tle[0]
oi = float(str.split(tle[2],' ')[3])
orb = Orbital(tle[0])
attributes = []
rt, ra, tt, ta, st, sa = observer.next_pass(sat)
# Determine is pass descending or ascending
sat.compute(rt)
aos_lat = sat.sublat.real*(180/math.pi)
sat.compute(st)
los_lat = sat.sublat.real*(180/math.pi)
if (aos_lat > los_lat):
print "PASS = descending"
node = "descending"
else:
print "PASS = ascending"
node = "ascending"
oi = 360 - oi
AOStime = datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S")
minutesaway = (AOStime-now).seconds/60.0
print "Minutes to horizon = ", minutesaway
print "AOStime = ", rt
print "LOStime = ", st
print "Transit time = ", tt
orad = orb.get_lonlatalt(datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S"))[2]
attributes = {'Satellite name': satname, 'Orbit height': orad, 'Orbit': orb.get_orbit_number(datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S")), \
'Current time': str(now),'Minutes to horizon': minutesaway, 'AOS time': str(rt), \
'LOS time': str(st), 'Transit time': str(tt), 'Node': node}
# Append the attributes to the list of acquisitions for the acquisition period
if not any ((x['Satellite name'] == satname and x['Orbit'] == orb.get_orbit_number(datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S")))for x in schedule):
schedule.append(attributes)
# Step from AOS to LOS in 100 second intervals
delta = timedelta(seconds=100)
deltatime = datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S")
geoeastpoint = []
geowestpoint = []
geotrack = []
print "DELTATIME", deltatime
print "SETTING TIME", datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S")
while deltatime < datetime.strptime(str(st), "%Y/%m/%d %H:%M:%S"):
sat.compute(deltatime)
geotrack.append({'lat2': sat.sublat.real*(180/math.pi), \
'lon2': sat.sublong.real*(180/math.pi), \
'alt2': orb.get_lonlatalt(datetime.strptime(str(rt), "%Y/%m/%d %H:%M:%S"))[2]*1000})
eastaz = getEffectiveHeading(sat,oi,sat.sublat.real*(180/math.pi), sat.sublong.real*(180/math.pi), orad, sat._n)+90
westaz = getEffectiveHeading(sat,oi,sat.sublat.real*(180/math.pi), sat.sublong.real*(180/math.pi), orad, sat._n)+270
#Set ground swath per satellite sensor
#TODO use view angle check to refine step from satellite track see IFOV
if tle[0] in ("LANDSAT 8","LANDSAT 7"):
swath = 185000/2
if tle[0] in ("TERRA","AQUA"):
swath = 2330000/2
if tle[0] in ("NOAA 15", "NOAA 18", "NOAA 19"):
swath = 1100000/2
if tle[0] == "SUOMI NPP":
swath = 2200000/2
geoeastpoint.append(Geodesic.WGS84.Direct(sat.sublat.real*180/math.pi, sat.sublong.real*180/math.pi, eastaz, swath))
geowestpoint.append(Geodesic.WGS84.Direct(sat.sublat.real*180/math.pi, sat.sublong.real*180/math.pi, westaz, swath))
deltatime = deltatime+delta
# Create current location ogr output
nowpoint = [{'lat2':orb.get_lonlatalt(datetime.utcnow())[1],'lon2':orb.get_lonlatalt(datetime.utcnow())[0],'alt2':orb.get_lonlatalt(datetime.utcnow())[2]*1000}]
#TODO ensure the now attributes are actually attributes for the current position of the satellite and include relevant next pass information...tricky?
#if ((attributes['Orbit']==orb.get_orbit_number(datetime.utcnow()))and(AOStime<now)):
now_attributes = {'Satellite name': satname, 'Orbit height': orb.get_lonlatalt(datetime.utcnow())[2], 'Orbit': orb.get_orbit_number(datetime.utcnow()), \
'Current time': str(now),'Minutes to horizon': "N/A", 'AOS time': "N/A", \
'LOS time': "N/A", 'Transit time': "N/A", 'Node': "N/A"}
#now_attributes=attributes
CURRENT_POSITION_FILENAME = satname+"_current_position.kml"
#TODO draw the current orbit forward for the passes period time from the satellite position as a long stepped ogr line
getVectorFile(now_attributes,nowpoint,'point', CURRENT_POSITION_FILENAME, 'KML')
polypoints = []
for x in geowestpoint:
polypoints.append({'lat2':x['lat2'],'lon2':x['lon2']})
for x in reversed(geoeastpoint):
polypoints.append({'lat2':x['lat2'],'lon2':x['lon2']})
if len(polypoints)>0:
polypoints.append({'lat2':geowestpoint[0]['lat2'],'lon2':geowestpoint[0]['lon2']})
# Create swath footprint ogr output
SWATH_FILENAME = os.path.join(output_path,satname+"."+str(orb.get_orbit_number(datetime.strptime(str(rt),"%Y/%m/%d %H:%M:%S")))+".ALICE.orbit_swath.kml")
ORBIT_FILENAME = os.path.join(output_path,satname+"."+str(orb.get_orbit_number(datetime.strptime(str(rt),"%Y/%m/%d %H:%M:%S")))+".ALICE.orbit_track.kml")
TRACKING_SWATH_FILENAME = os.path.join(output_path,satname+"_tracking_now.kml")
# Create currently acquiring polygon
#TODO def this
# Step from AOS to current time second intervals
observer.date=datetime.utcnow()
sat.compute(observer)
tkdelta = timedelta(seconds=100)
tkrt, tkra, tktt, tkta, tkst, tksa = observer.next_pass(sat)
tkdeltatime = datetime.utcnow()
tkgeoeastpoint = []
tkgeowestpoint = []
tkgeotrack = []
while tkdeltatime < (datetime.utcnow() or datetime.strptime(str(tkst),"%Y/%m/%d %H:%M:%S")):
sat.compute(tkdeltatime)
tkgeotrack.append({'lat2':sat.sublat.real*(180/math.pi),'lon2':sat.sublong.real*(180/math.pi),'alt2':orb.get_lonlatalt(datetime.strptime(str(rt),"%Y/%m/%d %H:%M:%S"))[2]})
tkeastaz = getEffectiveHeading(sat,oi,sat.sublat.real*(180/math.pi), sat.sublong.real*(180/math.pi),orad,sat._n)+90
tkwestaz = getEffectiveHeading(sat,oi,sat.sublat.real*(180/math.pi), sat.sublong.real*(180/math.pi),orad,sat._n)+270
#TODO use view angle check to refine step from satellite track see IFOV
if tle[0] in ("LANDSAT 8","LANDSAT 7"):
tkswath = 185000/2
if tle[0] in ("TERRA","AQUA"):
tkswath = 2330000/2
if tle[0] in ("NOAA 15", "NOAA 18", "NOAA 19"):
tkswath = 1100000/2
if tle[0] == "SUOMI NPP":
tkswath = 2200000/2
tkgeoeastpoint.append(Geodesic.WGS84.Direct(sat.sublat.real*180/math.pi, sat.sublong.real*180/math.pi, tkeastaz, tkswath))
tkgeowestpoint.append(Geodesic.WGS84.Direct(sat.sublat.real*180/math.pi, sat.sublong.real*180/math.pi, tkwestaz, tkswath))
tkdeltatime = tkdeltatime+tkdelta
tkpolypoints = []
for x in tkgeowestpoint:
tkpolypoints.append({'lat2':x['lat2'],'lon2':x['lon2']})
for x in reversed(tkgeoeastpoint):
tkpolypoints.append({'lat2':x['lat2'],'lon2':x['lon2']})
if len(tkpolypoints)>0:
tkpolypoints.append({'lat2':tkgeowestpoint[0]['lat2'],'lon2':tkgeowestpoint[0]['lon2']})
if not ((attributes['Node']=="ascending")and(satname not in ("AQUA"))):
# Create swath ogr output
getVectorFile(attributes,polypoints,'polygon', SWATH_FILENAME, 'KML')
# Create orbit track ogr output
getVectorFile(attributes,geotrack,'line', ORBIT_FILENAME, 'KML')
# Create currently acquiring ogr output
if ((now >= datetime.strptime(str(tkrt),"%Y/%m/%d %H:%M:%S")) and (now <= datetime.strptime(str(tkst),"%Y/%m/%d %H:%M:%S"))):
getVectorFile(now_attributes,tkpolypoints,'polygon', TRACKING_SWATH_FILENAME, 'KML')
if minutesaway <= period:
print "---------------------------------------"
print tle[0], 'WILL BE MAKING A PASS IN ', minutesaway, " MINUTES"
print ' Rise Azimuth: ', ra
print ' Transit Time: ', tt
print ' Transit Altitude: ', ta
print ' Set Time: ', st
print ' Set Azimuth: ', sa
for x in sorted(schedule, key=lambda k: k['AOS time']):
print x
# For dictionary entries with 'LOS time' older than now time - remove
if ((datetime.strptime(str(x['LOS time']),"%Y/%m/%d %H:%M:%S"))<(datetime.utcnow())):
# Delete output ogr
if os.path.exists(os.path.join(output_path,satname+"."+str(x['Orbit'])+".ALICE.orbit_swath.kml")):
os.remove(os.path.join(output_path,satname+"."+str(x['Orbit'])+".ALICE.orbit_swath.kml"))
if os.path.exists(os.path.join(output_path,satname+"."+str(x['Orbit'])+".ALICE.orbit_track.kml")):
os.remove(os.path.join(output_path,satname+"."+str(x['Orbit'])+".ALICE.orbit_track.kml"))
# Delete dictionary entry for pass
schedule.remove(x)
# Unlikely - if no entries in the schedule don't try to print it
if len(schedule)>0:
print (datetime.strptime(str(schedule[0]['AOS time']),"%Y/%m/%d %H:%M:%S"))
# If the AOS time is less than now + the time delta, shift the time to the latest recorded pass LOS time
if ((datetime.strptime(str(schedule[len(schedule)-1]['AOS time']),"%Y/%m/%d %H:%M:%S")<(datetime.utcnow()+timedelta(minutes=period)))):
observer.date = (datetime.strptime(str(schedule[len(schedule)-1]['LOS time']),"%Y/%m/%d %H:%M:%S")+timedelta(minutes=5))
# Recompute the satellite position for the update time
sat.compute(observer)
print "MODIFIED OBSERVER DATE",observer.date
else:
print "--------NOTHING TO MODIFY MOVING TO NEXT SATELLITE IN LIST------"
#TODO - write to html
# Exit the def if the schedule isn't able to update because there are no passes in the acquisition window
return ()
time.sleep(1*sleep_status)
return ()
def set_tle(self, line1, line2):
# for now restart pyorbital with these new elements.
del self.orbital
self.orbital = Orbital(self.sat,line1=line1, line2=line2)
class PyOrbitalLayer(OrbitalLayer):
"""
pyorbital based orbital layer
"""
__implements__ = (OrbitalLayer,)
def __init__(self, aoi, sat, instrument="AVHRR"):
OrbitalLayer.__init__(self,aoi,sat,instrument)
# instantiate orbital module
config_file_path = ""
try:
config_file_path = os.environ['PYGRANULE_CONFIG_PATH']
except KeyError:
print "pygranule config file path missing. Has the 'PYGRANULE_CONFIG_PATH' environment variable been set?"
default_tle_file = config_file_path+"/default.tle"
try:
self.orbital = Orbital(sat,default_tle_file)
except:
print "Failed to open default tle file:", default_tle_file
print "Downloading from internet:"
try:
self.orbital = Orbital(sat)
except:
raise OrbitalLayerError("Pyorbital Failed to fetch TLE from internet.")
# create scan geometry - one scan line.
if instrument == "AVHRR":
scan_steps = np.arange(0,self.instrument_info['scan_steps'],self.instrument_info['scan_steps']/8-1)
scan_steps[-1] = self.instrument_info['scan_steps']-1
self.scan_geom = avhrr(1,scan_steps)
elif instrument == "VIIRS":
self.scan_geom = viirs(1)
def set_tle(self, line1, line2):
# for now restart pyorbital with these new elements.
del self.orbital
self.orbital = Orbital(self.sat,line1=line1, line2=line2)
def orbital_period(self):
return 24*60/self.orbital.tle.mean_motion
def scan_line_lonlats(self, t):
"""
Returns a single instrument scan line starting at datetime t
"""
s_times = self.scan_geom.times(t)
pixels_pos = compute_pixels((self.orbital.tle.line1, self.orbital.tle.line2),
self.scan_geom, s_times)
pos_time = get_lonlatalt(pixels_pos, s_times)
return np.array((pos_time[0],pos_time[1]))
def next_transit(self, start=datetime.now(), resolution=100):
"""
Next transit time relative to center of aoi.
Resolution accuracy defined by subdivision of orbital period.
"""
# accuracy in mintues from mean orbital period
dt = self.orbital_period()/resolution
# observer position
alt = 0.0
lon, lat = self.aoi_center()
# NOTE: For now I do not use the pyorbital
# get_next_passes. Because it accepts integer (not float) hours
# for the search period, and the accuracy of the transit time
# search is not obvious to me at the moment.
# Also I would like to allow negative transit time altitudes
# - transits below horizon.
# Therefore I re-implement the search myself, here to have more control:
t_offsets = np.arange(0.0,self.orbital_period()*1.2,dt)
e = np.array( [ self.orbital.get_observer_look(start + timedelta(minutes=t_offset), lon, lat, alt)[1] \
for t_offset in t_offsets ] )
# search for local maxima
b = (np.roll(e,1)<e)&(np.roll(e,-1)<e)
idx = np.where(b[1:]==True)[0][0]+1 #i.e. do not accept index 0 as maximum...
## return a quadratic maximum for good accuracy based on data.
## Quadratic fit to 3 points around maximum elevation
## seems to improve accuracy by 100-fold.
x,y = t_offsets[idx-1:idx+2],e[idx-1:idx+2]
fit = np.polyfit(x,y,2)
t = -fit[1]/(2.0*fit[0])
#from matplotlib import pyplot as plt
#plt.plot(x,y,'x')
#fitx = np.arange(x[0]-1,x[2]+1,0.1)
#fity = fit[2]+fit[1]*fitx+fit[0]*(fitx**2)
#plt.plot(fitx,fity,'r-')
#plt.show()
return start + timedelta(minutes=t)
