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Chapter 05, Problem 31 GO Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of
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Orbital speed V= Jume De = 6400km i = 6.67X10 Me = 6 X 1024 kg FGCOCOUGE ha = 448 km VA- J 6.67X 10-11 X 6X 1024 (6400+448)

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