StkExternal propagator interface.
  Propagate | Propagates the satellite's path using the specified time interval. | 
  EphemerisStartEpoch | If overriding the times contained in the external file, specify the time of the first ephemeris point. | 
  FileFormat | Ephemeris file format. | 
  Filename | Name of external file. | 
  LimitEphemerisToScenarioInterval | Limit ephemeris for analysis to the Scenario Interval. | 
  MessageLevel | Message level used to report messages during file loading. | 
  Override | Opt whether to override times contained in the external file. | 
  StartTime | Get the start time of ephemeris interval. Uses DateFormat Dimension. | 
  Step | Step size. Uses Time Dimension. | 
  StopTime | Get the stop time of ephemeris interval. Uses DateFormat Dimension. | 
| Implemented Interface | 
|---|
| IAgVePropagator | 
Set ground vehicle to use STK External propagator
| [C#] | ||
|---|---|---|
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Set the satellite to use the STK External propagator
| [C#] | ||
|---|---|---|
  | ||
Set ship to use STK External propagator
| [C#] | ||
|---|---|---|
  | ||
Create a satellite from an external ephemeris file (.e)
| [C#] | ||
|---|---|---|
  | ||
Create a satellite from an external ephemeris file (.e)
| [Visual Basic .NET] | ||
|---|---|---|
  | ||
Set ground vehicle to use STK External propagator
| [Visual Basic .NET] | ||
|---|---|---|
  | ||
Set the satellite to use the STK External propagator
| [Visual Basic .NET] | ||
|---|---|---|
  | ||
Set ship to use STK External propagator
| [Visual Basic .NET] | ||
|---|---|---|
  | ||





