Properties for the Analytic Orbit ephemeris
source.
![]() |
The argument of periapsis; The angle measured in direction of the body's orbital motion, and in the orbit plane, from the ascending node to the periapsis of the orbit. Uses Angle Dimension. |
![]() |
The argument of periapsis rate of change. Uses AngleRate Dimension. |
![]() |
The eccentricity; the ratio of the distance between the two foci of the ellipse and its major axis. Dimensionless. |
![]() |
The eccentricity rate of change. Dimensionless. |
![]() |
The epoch. Dimensionless. |
![]() |
The inclination; the angle from the Z axis of the inertial coordinate system to the orbit angular velocity vector. Uses Angle Dimension. |
![]() |
The inclination rate of change. Uses AngleRate Dimension. |
![]() |
The mean longitude; the sum of the Right Ascension of the Ascending Node, the Argument of Periapsis and the Mean Anomaly. Uses Angle Dimension. |
![]() |
The mean longitude rate of change. Uses AngleRate Dimension. |
![]() |
The right ascension; the angle from the X axis of the inertial coordinate system to the point where the orbit crosses the X-Y plane in the +Z direction. Uses Angle Dimension. |
![]() |
The right ascension rate of change. Uses AngleRate Dimension. |
![]() |
The semi-major axis; one-half the distance along the long axis of the elliptical orbit. Uses Distance Dimension. |
![]() |
The semi-major axis rate of change. Uses Rate Dimension. |
Implemented Interface |
---|
IAgVACbEphemeris |