Equinoctial coordinate type, which uses the
center of the Earth as the origin and the plane of the satellite's
orbit as the reference plane.
![]() |
The coordinate system and coordinate epoch. |
![]() |
The coordinate system being used. |
![]() |
The Formulation can be Retrograde or Posigrade. |
![]() |
H/K collectively describe the shape of the satellite's orbit and the position of perigee. Dimensionless. |
![]() |
H/K collectively describe the shape of the satellite's orbit and the position of perigee. Dimensionless. |
![]() |
Specifies a satellite's position within its orbit at epoch and equals the sum of the classical RAAN, Argument of Perigee, and Mean Anomaly. Uses Angle dimension. |
![]() |
P/Q collectively describe the orientation of the satellite's orbit plane. Dimensionless. |
![]() |
P/Q collectively describe the orientation of the satellite's orbit plane. Dimensionless. |
![]() |
The value of Mean Motion or Semimajor Axis. |
![]() |
The orbit size option can be Mean Motion or Semimajor Axis. |
![]() |
Smart epoch component allows the user to configure the state epoch explicitly or implicitly (using a pre-defined or custom time instant component). |
![]() |
Returns an array of supported coordinate system types |
Implemented Interface |
---|
IAgOrbitState |