ClassicalLocationEccentricAnomaly
=================================

.. py:class:: ansys.stk.core.stkobjects.ClassicalLocationEccentricAnomaly

   Bases: :py:class:`~ansys.stk.core.stkobjects.IClassicalLocation`

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

.. py:currentmodule:: ClassicalLocationEccentricAnomaly

Overview
--------

.. tab-set::

    .. tab-item:: Properties

        .. list-table::
            :header-rows: 0
            :widths: auto

            * - :py:attr:`~ansys.stk.core.stkobjects.ClassicalLocationEccentricAnomaly.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
-------------

.. code-block:: python

    from ansys.stk.core.stkobjects import ClassicalLocationEccentricAnomaly


Property detail
---------------

.. py:property:: value
    :canonical: ansys.stk.core.stkobjects.ClassicalLocationEccentricAnomaly.value
    :type: 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.