OrbitStateEquinoctial#

class ansys.stk.core.stkobjects.OrbitStateEquinoctial#

Bases: IOrbitState

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.

Overview#

Properties

`coordinate_system_type`	Get or set the coordinate system being used.
`coordinate_system`	Get the coordinate system and coordinate epoch.
`size_shape_type`	Get or set the orbit size option can be Mean Motion or Semimajor Axis.
`size_shape`	Get the value of Mean Motion or Semimajor Axis.
`h`	H/K collectively describe the shape of the satellite’s orbit and the position of perigee. Dimensionless.
`k`	H/K collectively describe the shape of the satellite’s orbit and the position of perigee. Dimensionless.
`p`	P/Q collectively describe the orientation of the satellite’s orbit plane. Dimensionless.
`q`	P/Q collectively describe the orientation of the satellite’s orbit plane. Dimensionless.
`mean_longitude`	Specify 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.
`formulation`	Get or set the Formulation can be Retrograde or Posigrade.
`supported_coordinate_system_types`	Return an array of supported coordinate system types.
`state_epoch`	Smart epoch component allows the user to configure the state epoch explicitly or implicitly (using a pre-defined or custom time instant component).

from ansys.stk.core.stkobjects import OrbitStateEquinoctial

property OrbitStateEquinoctial.coordinate_system_type: CoordinateSystem#: Get or set the coordinate system being used.

property OrbitStateEquinoctial.coordinate_system: OrbitStateCoordinateSystem#: Get the coordinate system and coordinate epoch.

property OrbitStateEquinoctial.size_shape_type: EquinoctialSizeShape#: Get or set the orbit size option can be Mean Motion or Semimajor Axis.

property OrbitStateEquinoctial.size_shape: IClassicalSizeShape#: Get the value of Mean Motion or Semimajor Axis.

property OrbitStateEquinoctial.h: float#: H/K collectively describe the shape of the satellite’s orbit and the position of perigee. Dimensionless.

property OrbitStateEquinoctial.k: float#: H/K collectively describe the shape of the satellite’s orbit and the position of perigee. Dimensionless.

property OrbitStateEquinoctial.p: float#: P/Q collectively describe the orientation of the satellite’s orbit plane. Dimensionless.

property OrbitStateEquinoctial.q: float#: P/Q collectively describe the orientation of the satellite’s orbit plane. Dimensionless.

property OrbitStateEquinoctial.mean_longitude: float#: Specify 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.

property OrbitStateEquinoctial.formulation: EquinoctialFormulation#: Get or set the Formulation can be Retrograde or Posigrade.

property OrbitStateEquinoctial.supported_coordinate_system_types: list#: Return an array of supported coordinate system types.

property OrbitStateEquinoctial.state_epoch: ITimeToolInstantSmartEpoch#: Smart epoch component allows the user to configure the state epoch explicitly or implicitly (using a pre-defined or custom time instant component).