(c) Starting from the satellite on the Earth's surface at the equator, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but include the effect of the planet's daily rotation.
(c) Starting from the satellite on the Earth's surface at the equator, what is the minimum energy input necessary to place this satellite in orbit? Ignore air resistance but include the effect of the planet's daily rotation.
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Please , just the part C
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