Description
The 11-Parameter propagator models geostationary satellites using 11-Parameter files. The propagator uses an algorithm documented in Intelsat Earth Station Standards (IESS) IESS-412 (Rev. 2), available at www.celestrak.com.
Public Methods
 Propagate | Propagates the satellite's path using the specified time interval. |
Public Properties
 EphemerisInterval | The propagator's ephemeris interval. |
| ParameterFiles | Returns a collection of 11-Parameter satellite definitions. |
| 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 |
|---|
| IAgVePropagator |