Orbital elements: Difference between revisions
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→{{header|ooRexx}}: 2 more little glitches :-( good night!
Walterpachl (talk | contribs) m (→{{header|ooRexx}}: sin -> rxCalcsin , courtesy GS) |
Walterpachl (talk | contribs) m (→{{header|ooRexx}}: 2 more little glitches :-( good night!) |
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Else l=1-eccentricity*eccentricity
l*=semimajorAxis
c=rxCalccos(trueAnomaly,16,'R')
s=rxCalcsin(trueAnomaly,16,'R')
r=l/(1+eccentricity*c)
rprime=s*r*r/l
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