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(a) A satellite of mass 2000 kg is to be put into a circular orbit around the earth of radius 1100 km. What is the minimum energy required?
(b)What will the minimum energy required to transfer it to an elliptic orbit having minimum and maximum distances 1100km and 4100km?
(b)What will the minimum energy required to transfer it to an elliptic orbit having minimum and maximum distances 1100km and 4100km?
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