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 = CelestialBody( equatorial_radius = 6378*km, gravitational_parameter = 398600*km**3) o = Orbit(body=b) o.epoch = 0 o.periapsis = 6600*km o.speed_at_periapsis = 1.2 * b.escape_speed(6600*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 = (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
def setup_orbit(): b = Bunch( equatorial_radius = 6378*km, gravitational_parameter = 398600*km**3) o = Orbit(body=b) o.epoch = 0 o.true_anomaly_at_epoch = 30*deg o.radius_at_epoch = 10000*km o.speed_at_epoch = 10*km return o
def setup_orbit(): b = Bunch( equatorial_radius = 6378*km, gravitational_parameter = 398600*km**3, ) o = Orbit(body=b) o.pe = 9600*km o.ap = 21000*km o.epoch = 0 o.θ0 = 0 return o
def setup_orbit(): b = CelestialBody( equatorial_radius = 6378*km, gravitational_parameter = 398600*km**3) o = Orbit(body=b) o.epoch = 0 o.radius_at_epoch = 7200*km o.radial_speed_at_epoch = 1*km o.semi_major_axis = 10000*km o.i = 0 o.Ω = 0 o.ω = 0 return o