def setup_orbit():
b = Bunch(
equatorial_radius = 6378*km,
gravitational_parameter = 398600*km**3,
)
o = Orbit(body=b)
o.e = 0.3
o.h = 60000*km**2
o.θ0 = 120*deg
return o
def setup_orbit():
b = Bunch(
equatorial_radius = 6378*km,
gravitational_parameter = 398600*km**3,
)
o = Orbit(body=b)
o.e = 0.3
o.h = 60000*km**2
o.θ0 = 120*deg
return o