Description
Two-body propagator interface.
Public Methods
 Propagate | Propagates the satellite's path using the specified time interval. |
Public Properties
 EphemerisInterval | The propagator's ephemeris interval. |
| InitialState | Get the initial state. |
| PropagationFrame | The propagation frame |
| Step | Step size. Uses Time Dimension. |
| SupportedPropagationFrames | Returns supported propagation frames |
Interfaces
| Implemented Interface |
|---|
| IAgVePropagator |