elliptical orbit around the Earth with P = 4000KM; e=0.6 and t = 4917.2 Sec. Find the satellite position in terms of distance and true anomaly, after it has passed 800 seconds from the perigee point.

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elliptical orbit around the Earth with P= 4000Km; e=0.6 and t = 4917.2 Sec.
Find the satellite position in terms of distance and true anomaly, after it has passed 800 seconds from
the perigee point.
Transcribed Image Text:elliptical orbit around the Earth with P= 4000Km; e=0.6 and t = 4917.2 Sec. Find the satellite position in terms of distance and true anomaly, after it has passed 800 seconds from the perigee point.
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