SpaceObject.get_state¶
SpaceObject.get_state
-
SpaceObject.
get_state
(t)[source]¶ Gets ECEF state at specified times using propagator instance.
- Parameters
t (int/float/list/numpy.ndarray/astropy.time.Time/astropy.time.TimeDelta) – Time relative epoch in seconds.
- Returns
Array of state (position and velocity) as a function of time.
- Return type
numpy.ndarray of size (6,len(t))