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Question 4 of 10 > An artificial satellite is in a circular orbit d = 380.0 km above the surface of a planet of radius r = 5.
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1. Time persod T= 288 ) V (om Parascorso 35x[(5.55+0.38) x15] 6.67% 16 x lx (5.55109) P = 1340.3 kg 3 m

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