An earth satellite is observed at perigee to be 250 km above the earth's surface and traveling at about 8500m/s. Find the eccentricity of its orbit and its height above the earth at apogee. Earth radius is 6.4 105 m, G-M/R

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4. An earth satellite is observed at perigee to be 250 km above the earth's surface and traveling at about
8500m/s. Find the eccentricity of its orbit and its height above the earth at apogee. Earth radius is
6.4-10 m, G-M/R = g.
Transcribed Image Text:4. An earth satellite is observed at perigee to be 250 km above the earth's surface and traveling at about 8500m/s. Find the eccentricity of its orbit and its height above the earth at apogee. Earth radius is 6.4-10 m, G-M/R = g.
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