Assign a new orbit state using Equinoctial representation.
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def AssignEquinoctialPosigrade(self, ECoordinateSystem:"AgECoordinateSystem", SemiMajorAxis:float, H:float, K:float, P:float, Q:float, MeanLon:float) -> None: |
- ECoordinateSystem
- SemiMajorAxis
- H
- K
- P
- Q
- MeanLon






