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A 600 kg satellite is in a circular orbit at an altitude of 475 km above the Earths surface. Because of air friction, the sa

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TE = PETKE 28 PE= - GMM and in circular orbit of radius KE= GMM TE-Grantament Com TE: - - (6.67 x 10) (5.946x1024) (600) 2(

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