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An artificial satellite is in a circular orbit d = 680.0 km above the surface of a planet of radius r = 5.55 x 10 km. The per
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бщФ Powe eta 7a d= 680 km = 680 x 103 m 5.55 x 103 km =5,55 x 106m Time period T = 1.15 hours = 1.15 x 3600 S. Gravitational3 417² totd) → W T2x XG 2 3 4 / 37 m3x S T d x 41² (nto) T2XG i (btdj3 T2, G. 3 3 3 ) an 3 n E = (5.55X10693 *{(5550+680) xro

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