- #1
Philosophaie
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A satellite is in an unstable elliptical orbit around the earth. Is there a way of tracking each satellite's orbit till it reaches the critical stage then follows it's reentry path?
V<Vescape
r=a*(1-e^2)/(1+e*cos(True Anomaly))
Book recommendations welcome. College educated.
V<Vescape
r=a*(1-e^2)/(1+e*cos(True Anomaly))
Book recommendations welcome. College educated.
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