ClassicalLocationMeanAnomaly#

class ansys.stk.core.stkobjects.ClassicalLocationMeanAnomaly#

Bases: IClassicalLocation

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

Overview#

value

Value of Mean Anomaly: angle from the eccentricity vector to a position vector where the satellite would be if it were always moving at its average angular rate. Uses Angle Dimension.

Import detail#

from ansys.stk.core.stkobjects import ClassicalLocationMeanAnomaly

Property detail#

property ClassicalLocationMeanAnomaly.value: float#

Value of Mean Anomaly: angle from the eccentricity vector to a position vector where the satellite would be if it were always moving at its average angular rate. Uses Angle Dimension.