Physics, asked by alishaikh21, 2 months ago

orbital velocity of a satellite near the surface of the earth is ?
1.9270
2.9720
3.7920
4.7290​

Answers

Answered by piyushkumar2231
1

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, 6.59 x 106 m.

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