Path: Orbit/OrbitCoord
% Computes the orbit radius and the parameter from Keplerian elements.
Since version 1.
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Form:
[r, p] = REl( el )
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Inputs
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el Elements vector [a,i,W,w,e,M] where a is perigee
radius for a parabola
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Outputs
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r Radius
p Parameter
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SC: BasicOrbit/M2Nu
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