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A 500 kg satellite is in a circular orbit at an altitude of 550 km above the Earths surface. Because of air friction, the sa

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at for orbit. Mac CMM Ez a mac & GMM = mv2 My 82 3 m2- GMM CMP TE: PE + Ke = - Gm h ommecomme - GMM 28 20 7 X10 TE: - (6.69X1

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