Description
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 | Eliptical orbit is fit to the current motion of the reference point according to the selected mean theory. |
Interfaces
| Implemented Interface |
|---|
| IAgCrdnVector |
| IAgCrdnTimeProperties |
| IAgCrdn |