ClassicalLocationTrueAnomaly
============================

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

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

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

.. py:currentmodule:: ClassicalLocationTrueAnomaly

Overview
--------

.. tab-set::

    .. tab-item:: Properties

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

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

.. code-block:: python

    from ansys.stk.core.stkobjects import ClassicalLocationTrueAnomaly


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

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