Assign a new orbit state using Geodetic representation.
| [Visual Basic .NET] |
|---|
|
| [C#] |
|---|
|
| [Managed C++] |
|---|
|
| [Unmanaged C++] |
|---|
|
| [Java] |
|---|
|
[Python - STK API ] |
|---|
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






