Interface for specifying orbit orientation in the Classical (Keplerian) system.
ArgOfPerigee | 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 | The angle between the angular momentum vector (perpendicular to the plane of the orbit) and the inertial Z axis. Uses Angle Dimension. |