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A 475 kg satellite is in a circular orbit at an altitude of 525 km above the Earths surface. Because of air friction, the sa

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475 kg. Solution Given that mass of satellite is altitude is 525 km. e final velocity is a 1500 m/s. Agi distance of satellitTotal Energy is TE = KET PE = GMM + (-) GMm TE= - GMM - ③ and KE when satellite touch earths surface KE = I m u 2 = I x 475

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