ClassicalLocationMeanAnomaly
============================

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

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

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

.. py:currentmodule:: ClassicalLocationMeanAnomaly

Overview
--------

.. tab-set::

    .. tab-item:: Properties

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

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

.. code-block:: python

    from ansys.stk.core.stkobjects import ClassicalLocationMeanAnomaly


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

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