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A 425 kg satellite is in a circular orbit at an altitude of 400 km above the Earths surface. Because of air friction, the sa
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Thanks for asking ..th=4001km V= 2.10 ka Se 4253 t alti ude h enery m Mm 4Mm (2-th) 4M - Pth) GmM Er Rth) mv-mM R when it hits the 24 6-67104256X

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