E2RAORP:

Path: Orbit/OrbitCoord

% Ratio of apogee radius to perigee radius given eccentricity for an ellipsew
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   Form:
   x = E2RAORP( e )
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   ------
   Inputs
   ------

   e		            Eccentricity


   -------
   Outputs
   -------
   x		            Apogee radius/perigee radius

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Children:

Common: Graphics/Plot2D

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