Two-body propagator interface.
![]() | Propagates the satellite's path using the specified time interval. |
![]() | The propagator's display coordinate type. |
![]() | Get the propagator's ephemeris interval. |
![]() | Get the initial state. |
![]() | Gets or sets the propagation frame. |
![]() | Step size. Uses Time Dimension. |
![]() | Returns supported propagation frames. |
Implemented Interface |
---|
IAgVePropagator |