Description
Unit vector perpendicular to the plane of an elliptical orbit created from the motion of the specified point with respect to the center of the specified central body.
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 unit vector is directed along the current orbit angular momentum of the specified point with respect to the specified central body.
Interfaces
| Implemented Interface |
|---|
| IAgCrdnVector |
| IAgCrdnTimeProperties |
| IAgCrdn |