ClassicalLocationEccentricAnomaly#

class ansys.stk.core.stkobjects.ClassicalLocationEccentricAnomaly#

Bases: IClassicalLocation

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

Overview#

value

Value of Eccentric Anomaly: angle measured with origin at center of ellipse from direction of perigee to point on a circumscribing circle from which a line perpendicular to Semimajor Axis intersects position of satellite on ellipse. Uses Angle Dimension.

Import detail#

from ansys.stk.core.stkobjects import ClassicalLocationEccentricAnomaly

Property detail#

property ClassicalLocationEccentricAnomaly.value: float#

Value of Eccentric Anomaly: angle measured with origin at center of ellipse from direction of perigee to point on a circumscribing circle from which a line perpendicular to Semimajor Axis intersects position of satellite on ellipse. Uses Angle Dimension.