A2Apogee:

Path: Orbit/OrbitCoord

 Computes the apogee radius from a and e.

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   Form:
   rA = A2Apogee( a, e )
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   ------
   Inputs
   ------
   a             (1,:)   Semi major axis
   e             (1,:)   Eccentricity

   -------
   Outputs
   -------
   rA            (a,e)   Apogee radius

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Children:

Common: Graphics/Mesh2
Math: Linear/DupVect

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