Description
Interface for specifying orbit orientation in the Classical (Keplerian) system.
Public Properties
 ArgOfPerigee | Gets or sets the angle from the ascending node to the eccentricity vector (lowest point of orbit) measured in the direction of the satellite's motion and in the orbit plane. Uses Angle Dimension. |
| AscNode | Value of Longitude of Ascending Node or Right Ascension of Ascending Node. |
| AscNodeType | Select Longitude of Ascending Node or Right Ascension of Ascending Node. |
| Inclination | Gets or sets the angle between the angular momentum vector (perpendicular to the plane of the orbit) and the inertial Z axis. Uses Angle Dimension. |