Vector from the center of the specified central body to the farthest point of an elliptical orbit created from the motion of the specified point.
![]() | Specify a central body. |
![]() | Specify the mean element theory type for approximating motion. |
![]() | Specify a reference point. |
Implemented Interface |
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IAgCrdnVector |
IAgCrdnTimeProperties |
IAgCrdn |