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Path: Orbit/OrbitCoord
Computes the apogee radius from a and e. -------------------------------------------------------------------------- Form: rA = A2Apogee( a, e ) -------------------------------------------------------------------------- ------ Inputs ------ a (1,:) Semi major axis e (1,:) Eccentricity ------- Outputs ------- rA (a,e) Apogee radius --------------------------------------------------------------------------
Common: Graphics/Mesh2 Math: Linear/DupVect
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