ClassicalOrientation#

class ansys.stk.core.stkobjects.ClassicalOrientation#: Orbit orientation in the Classical (Keplerian) system.

Overview#

Properties

`argument_of_periapsis`	Get or set the angle from the ascending node to the eccentricity vector (lowest point of orbit) measured in the direction of the satellite’s motion and in the orbit plane. Uses Angle Dimension.
`ascending_node`	Value of Longitude of Ascending Node or Right Ascension of Ascending Node.
`ascending_node_type`	Select Longitude of Ascending Node or Right Ascension of Ascending Node.
`inclination`	Get or set the angle between the angular momentum vector (perpendicular to the plane of the orbit) and the inertial Z axis. Uses Angle Dimension.

from ansys.stk.core.stkobjects import ClassicalOrientation

property ClassicalOrientation.argument_of_periapsis: float#: Get or set the angle from the ascending node to the eccentricity vector (lowest point of orbit) measured in the direction of the satellite’s motion and in the orbit plane. Uses Angle Dimension.

property ClassicalOrientation.ascending_node: IOrientationAscNode#: Value of Longitude of Ascending Node or Right Ascension of Ascending Node.

property ClassicalOrientation.ascending_node_type: OrientationAscNode#: Select Longitude of Ascending Node or Right Ascension of Ascending Node.

property ClassicalOrientation.inclination: float#: Get or set the angle between the angular momentum vector (perpendicular to the plane of the orbit) and the inertial Z axis. Uses Angle Dimension.