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.
CentralBody | Specify a central body. |
MeanElementType | Specify the mean element theory type for approximating motion. |
ReferencePoint | Specify a reference point. |
At any time, the orbit is fit to the current motion of the specified point according to the specified type orbital elements. Available types are: osculating, Brouwer-Lyddane long and short, and Kozai.
| Name |
|---|
| AgCrdnVectorApoapsis |


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