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.