Description
Two-body propagator interface.
Object Model
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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. |
| StartTime |
This property is deprecated. Use EphemerisInterval to configure the propagation interval. Start time. Uses DateFormat Dimension. |
| Step |
Step size. Uses Time Dimension. |
| StopTime |
This property is deprecated. Use EphemerisInterval to configure the propagation interval. Stop time. Uses DateFormat Dimension. |
| UseScenarioAnalysisTime |
This property is deprecated. Use the new Timeline API components to configure the propagator's analysis time. Whether the scenario analysis start/stop times shall be used. |
Interfaces
| Implemented Interface |
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| IAgVePropagator |