Assign a new orbit state using Geodetic representation.
[Visual Basic .NET] |
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Public Sub AssignGeodetic( _ ByVal ECoordinateSystem As AgECoordinateSystem, _ ByVal Latitude As Double, _ ByVal Longitude As Double, _ ByVal Altitude As Double, _ ByVal LatitudeRate As Double, _ ByVal LongitudeRate As Double, _ ByVal AltitudeRate As Double _ ) |
[C#] |
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public void AssignGeodetic( AgECoordinateSystem ECoordinateSystem, double Latitude, double Longitude, double Altitude, double LatitudeRate, double LongitudeRate, double AltitudeRate ); |
[Managed C++] |
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public: void AssignGeodetic( AgECoordinateSystem ECoordinateSystem, double Latitude, double Longitude, double Altitude, double LatitudeRate, double LongitudeRate, double AltitudeRate ); |
[Unmanaged C++] |
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public: HRESULT AssignGeodetic( AgECoordinateSystem ECoordinateSystem, double Latitude, double Longitude, double Altitude, double LatitudeRate, double LongitudeRate, double AltitudeRate ); |
[Java] |
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public void assignGeodetic( AgECoordinateSystem ECoordinateSystem, double Latitude, double Longitude, double Altitude, double LatitudeRate, double LongitudeRate, double AltitudeRate ); |
[Python - STK API ] |
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def AssignGeodetic(self, ECoordinateSystem:"AgECoordinateSystem", Latitude:float, Longitude:float, Altitude:float, LatitudeRate:float, LongitudeRate:float, AltitudeRate:float) -> None: |
- ECoordinateSystem
- Latitude
- Longitude
- Altitude
- LatitudeRate
- LongitudeRate
- AltitudeRate