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IAgOrbitStateEquinoctial Interface

Description

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.

Object Model



Public Properties

Public Property CoordinateSystem The coordinate system and coordinate epoch.
Public Property CoordinateSystemType The coordinate system being used.
Public Property Formulation The Formulation can be Retrograde or Posigrade.
Public Property H H/K collectively describe the shape of the satellite's orbit and the position of perigee. Dimensionless.
Public Property K H/K collectively describe the shape of the satellite's orbit and the position of perigee. Dimensionless.
Public Property MeanLongitude 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.
Public Property P P/Q collectively describe the orientation of the satellite's orbit plane. Dimensionless.
Public Property Q P/Q collectively describe the orientation of the satellite's orbit plane. Dimensionless.
Public Property SizeShape The value of Mean Motion or Semimajor Axis.
Public Property SizeShapeType The orbit size option can be Mean Motion or Semimajor Axis.
Public Property StateEpoch Smart epoch component allows the user to configure the state epoch explicitly or implicitly (using a pre-defined or custom time instant component).
Public Property SupportedCoordinateSystemTypes Returns an array of supported coordinate system types

Interfaces

Implemented Interface
IAgOrbitState

CoClasses that Implement IAgOrbitStateEquinoctial

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STK Programming Interface 11.0.1