calculate the speed of satellite in an orbit at height of 1000 km from the earth surface. mass of earth equal to 5.98into 10resto 24 kg. radius of earth 6400km and G 6.67 into 10 resto -11 nm2/kg2
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Explanation:
v = root[GM/(R +h)]
= root [6.67*10^-11*5.98*10^24/*6400 + 1000)×10^3]
= 7,341.7171568245 m/s
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