mubody.core.satellite.Orbit#
- class mubody.core.satellite.Orbit(frame)#
- __init__(frame)#
Methods
IC()__init__(frame)add_trajectory(time, position, velocity, ...)mt()Returns mission time
r(t)Returns position of satellite for given time
s(t)Returns state vector of satellite for given time
v(t)Returns velocity of satellite for given time
Attributes
tra_df