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. |
EphemStart |
This property is deprecated. Use EphemerisStartEpoch instead. If overriding the times contained in the external file, specify the time of the first ephemeris point. Uses DateFormat Dimension. |
FileFormat |
Ephemeris file format. |
Filename |
Name of external file. |
Override |
Opt whether to override times contained in the external file. |
StartTime |
The start time of ephemeris interval. Uses DateFormat Dimension. |
Step |
Step size. Uses Time Dimension. |
StopTime |
The stop time of ephemeris interval. Uses DateFormat Dimension. |
| Implemented Interface |
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| IAgVePropagator |
Create a satellite
from an external ephemeris file (.e)
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Set ground vehicle to
use STK External propagator
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Set the satellite to
use the STK External propagator
| [C#] | Copy Code
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Set ship to use STK
External propagator
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Create a satellite
from an external ephemeris file (.e)
| [Visual Basic .NET] | Copy Code
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Set ground vehicle to
use STK External propagator
| [Visual Basic .NET] | Copy Code
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Set the satellite to
use the STK External propagator
| [Visual Basic .NET] | Copy Code
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Set ship to use STK
External propagator
| [Visual Basic .NET] | Copy Code
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