Physics, asked by mahamsarfraz40, 6 months ago

what will be the orbital speed of a satellite revolving at a height of1000 km above earth​

Answers

Answered by RaazAnishek
2

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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