Example #1
0
 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