A satellite of mass 2000 kg is revolving in elliptical path around earth If mean...

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A satellite of mass 2000 kg is revolving in elliptical path around earth If mean altitude at perigee and apogee are 1600 km and 5600 km respectively then the energy required to send the satellite in this orbit will be Radius of earth is 6400 km 1 7 2 x 10 0 J 2 7 8 x 1010 J 3 8 5 x 1010 J 4 5 6 x 1010 J

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