Assign a new orbit state using Classical representation.
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[Python - STK API ] |
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def AssignClassical(self, ECoordinateSystem:"AgECoordinateSystem", SemiMajorAxis:float, Eccentricity:float, Inclination:float, ArgOfPerigee:float, RAAN:float, MeanAnomaly:float) -> None: |
- ECoordinateSystem
- SemiMajorAxis
- Eccentricity
- Inclination
- ArgOfPerigee
- RAAN
- MeanAnomaly






