Description
A vector directed from the center of the specified central body toward the nearest point of an elliptical orbit created from the motion of the specified point.
Public Properties
 CentralBody | Specify a central body. |
| MeanElementType | Specify the mean element theory type for approximating motion. |
| ReferencePoint | Elliptical orbit is fit to the current motion of the reference point according to the selected mean theory. |
Remarks
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. The vector's magnitude is equal to the current eccentricity of the fit orbit.
Interfaces
| Implemented Interface |
|---|
| IAgCrdnVector |
| IAgCrdnTimeProperties |
| IAgCrdn |