def setup_orbit():
b = Bunch(
equatorial_radius = 6378*km,
gravitational_parameter = 398600*km**3)
o = Orbit(body=b)
o.epoch = 0
o.position_at_epoch = -6045*km, -3490*km, 2500*km
o.velocity_at_epoch = -3.457*km, 6.618*km, 2.533*km
return o
def setup_orbit():
b = Bunch(
equatorial_radius = 6378*km,
gravitational_parameter = 398600*km**3)
o = Orbit(body=b)
o.epoch = 0
o.position_at_epoch = (-5368*km, -1784*km, 3691*km)
return o
def setup_orbit():
b = Bunch(
equatorial_radius = 6378*km,
gravitational_parameter = 398600*km**3,
)
o = Orbit(body=b)
o.position_at_epoch = (8182.4*km, -6865.9*km, 0)
o.velocity_at_epoch = (0.47572*km, 8.8116*km, 0)
return o
def setup_orbit():
b = Bunch(
equatorial_radius = 6378*km,
gravitational_parameter = 398600*km**3,
)
o = Orbit(body=b)
o.position_at_epoch = (7000*km, 9000*km, 0)
o.velocity_at_epoch = (-5*km, 7*km, 0)
return o
def setup_orbit():
b = Bunch(
equatorial_radius = 6378*km,
gravitational_parameter = 398600*km**3)
o = Orbit(body=b)
o.epoch = 0
o.position_at_epoch = (1600*km, 5310*km, 3800*km)
o.velocity_at_epoch = (-7.350*km, 0.4600*km, 2.470*km)
return o
def setup_orbit():
b = Bunch(
equatorial_radius = 6378*km,
gravitational_parameter = 398600*km**3)
o = Orbit(body=b)
o.epoch = 0
o.position_at_epoch = (7000*km,-12124*km,0)
o.velocity_at_epoch = (2.6679*km,4.6210*km,0)
return o
