ClassicalLocationTrueAnomaly#

class ansys.stk.core.stkobjects.ClassicalLocationTrueAnomaly#

Bases: IClassicalLocation

True Anomaly, used in specifying the spacecraft’s location within its orbit at epoch.

Overview#

value

Value of True Anomaly: angle from the eccentricity vector (points toward perigee) to the satellite position vector, measured in the direction of satellite motion and in the orbit plane.Uses Angle Dimension.

Import detail#

from ansys.stk.core.stkobjects import ClassicalLocationTrueAnomaly

Property detail#

property ClassicalLocationTrueAnomaly.value: float#

Value of True Anomaly: angle from the eccentricity vector (points toward perigee) to the satellite position vector, measured in the direction of satellite motion and in the orbit plane.Uses Angle Dimension.