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Physics, 04.06.2020 17:57 kahnerp6448

For a satellite to orbit Earth at a constant distance, its centripetal acceleration must be equal to Earth's gravitational acceleration. If a satellite is to orbit with
a constant circular radius of 7,500,000 m, what is the approximate required
velocity of the satellite? (Recall that Earth has a mass of 5.97 x 1024 kg and G
= 6.67 * 10-11 N·m²/kg2)
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