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IAgVACbEphemerisAnalyticOrbit Interface

Description

Properties for the Analytic Orbit ephemeris source.

Public Properties

Public Property ArgOfPeriapsis 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.
Public Property ArgOfPeriapsisRate The argument of periapsis rate of change. Uses AngleRate Dimension.
Public Property Eccentricity The eccentricity; the ratio of the distance between the two foci of the ellipse and its major axis. Dimensionless.
Public Property EccentricityRate The eccentricity rate of change. Dimensionless.
Public Property Epoch The epoch. Dimensionless.
Public Property Inclination The inclination; the angle from the Z axis of the inertial coordinate system to the orbit angular velocity vector. Uses Angle Dimension.
Public Property InclinationRate The inclination rate of change. Uses AngleRate Dimension.
Public Property MeanLongitude The mean longitude; the sum of the Right Ascension of the Ascending Node, the Argument of Periapsis and the Mean Anomaly. Uses Angle Dimension.
Public Property MeanLongitudeRate The mean longitude rate of change. Uses AngleRate Dimension.
Public Property RAAN 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.
Public Property RAANRate The right ascension rate of change. Uses AngleRate Dimension.
Public Property SemiMajorAxis The semi-major axis; one-half the distance along the long axis of the elliptical orbit. Uses Distance Dimension.
Public Property SemiMajorAxisRate The semi-major axis rate of change. Uses Rate Dimension.

Interfaces

Implemented Interface
IAgVACbEphemeris

CoClasses that Implement IAgVACbEphemerisAnalyticOrbit

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STK Programming Interface 11.0.1