Orbital elements: Difference between revisions

Content deleted Content added
Walterpachl (talk | contribs)
m →‎REXX version 1: fix the literal
Walterpachl (talk | contribs)
m →‎Rexx version 1: add one missing precision. Not my day:-(
Line 819: Line 819:
Else l=1-eccentricity*eccentricity
Else l=1-eccentricity*eccentricity
l=l*semimajorAxis
l=l*semimajorAxis
c=my_cos(trueAnomaly)
c=my_cos(trueAnomaly,16)
s=my_sin(trueAnomaly,16)
s=my_sin(trueAnomaly,16)
r=l/(1+eccentricity*c)
r=l/(1+eccentricity*c)