Physics, asked by christopher4geoffrey, 9 months ago

what is the formula for calculating the speed of a given satellite in geostationary orbit

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Answered by tannu627

Answer:

The orbital speed can be found using v = SQRT(G*M/R). The R value (radius of orbit) is the earth's radius plus the height above the earth - in this case, 6.77 x 106 m.

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