Classical (Keplerian) coordinate type.
CoordinateSystem | The coordinate system and coordinate epoch. |
CoordinateSystemType | Coordinate system being used. |
Location | The location of the spacecraft in the orbit at epoch. |
LocationType | The element used for specifying spacecraft location in the orbit at epoch. |
Orientation | The orbit orientation. |
SizeShape | The size and shape of the orbit. |
SizeShapeType | The pair of elements used for specifying orbit size and shape. |
StateEpoch | Smart epoch component allows the user to configure the state epoch explicitly or implicitly (using a pre-defined or custom time instant component). |
SupportedCoordinateSystemTypes | Returns an array of supported coordinate system types |
Implemented Interface |
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IAgOrbitState |
Set initial state of satellite and propagate
[Python - STK API] | ||
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Set initial state of satellite and propagate
[MATLAB] | ||
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