CentralBodyComponentEphemerisAnalyticOrbit#

class ansys.stk.core.stkobjects.astrogator.CentralBodyComponentEphemerisAnalyticOrbit#

Bases: ICentralBodyComponentEphemeris

Central Body Ephemeris - Analytic Orbit.

Overview#

Properties

`epoch`	Get or set the epoch. Dimensionless.
`semimajor_axis`	Get or set the semi-major axis; one-half the distance along the long axis of the elliptical orbit. Uses Distance Dimension.
`semimajor_axis_rate`	Get or set the semi-major axis rate of change. Uses Rate Dimension.
`eccentricity`	Get or set the eccentricity; the ratio of the distance between the two foci of the ellipse and its major axis. Dimensionless.
`eccentricity_rate`	Get or set the eccentricity rate of change. Dimensionless.
`inclination`	Get or set the inclination; the angle from the Z axis of the inertial coordinate system to the orbit angular velocity vector. Uses Angle Dimension.
`inclination_rate`	Get or set the inclination rate of change. Uses AngleRate Dimension.
`raan`	Get or set 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.
`raan_rate`	Get or set the right ascension rate of change. Uses AngleRate Dimension.
`arg_of_periapsis`	Get or set 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.
`arg_of_periapsis_rate`	Get or set the argument of periapsis rate of change. Uses AngleRate Dimension.
`mean_longitude`	Get or set the mean longitude; the sum of the Right Ascension of the Ascending Node, the Argument of Periapsis and the Mean Anomaly. Uses Angle Dimension.
`mean_longitude_rate`	Get or set the mean longitude rate of change. Uses AngleRate Dimension.

Import detail#

from ansys.stk.core.stkobjects.astrogator import CentralBodyComponentEphemerisAnalyticOrbit

Property detail#

property CentralBodyComponentEphemerisAnalyticOrbit.epoch: float#: Get or set the epoch. Dimensionless.

property CentralBodyComponentEphemerisAnalyticOrbit.semimajor_axis: float#: Get or set the semi-major axis; one-half the distance along the long axis of the elliptical orbit. Uses Distance Dimension.

property CentralBodyComponentEphemerisAnalyticOrbit.semimajor_axis_rate: float#: Get or set the semi-major axis rate of change. Uses Rate Dimension.

property CentralBodyComponentEphemerisAnalyticOrbit.eccentricity: float#: Get or set the eccentricity; the ratio of the distance between the two foci of the ellipse and its major axis. Dimensionless.

property CentralBodyComponentEphemerisAnalyticOrbit.eccentricity_rate: float#: Get or set the eccentricity rate of change. Dimensionless.

property CentralBodyComponentEphemerisAnalyticOrbit.inclination: Any#: Get or set the inclination; the angle from the Z axis of the inertial coordinate system to the orbit angular velocity vector. Uses Angle Dimension.

property CentralBodyComponentEphemerisAnalyticOrbit.inclination_rate: float#: Get or set the inclination rate of change. Uses AngleRate Dimension.

property CentralBodyComponentEphemerisAnalyticOrbit.raan: Any#: Get or set 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.

property CentralBodyComponentEphemerisAnalyticOrbit.raan_rate: float#: Get or set the right ascension rate of change. Uses AngleRate Dimension.

property CentralBodyComponentEphemerisAnalyticOrbit.arg_of_periapsis: Any#: Get or set 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.

property CentralBodyComponentEphemerisAnalyticOrbit.arg_of_periapsis_rate: float#: Get or set the argument of periapsis rate of change. Uses AngleRate Dimension.

property CentralBodyComponentEphemerisAnalyticOrbit.mean_longitude: Any#: Get or set the mean longitude; the sum of the Right Ascension of the Ascending Node, the Argument of Periapsis and the Mean Anomaly. Uses Angle Dimension.

property CentralBodyComponentEphemerisAnalyticOrbit.mean_longitude_rate: float#: Get or set the mean longitude rate of change. Uses AngleRate Dimension.