Physics, asked by RogerRiaz, 4 months ago

what should be the orbital speed to launch a satellite in a circular orbit 900 kilometres above the surface of the earth​

Answers

Answered by skmadhuri114
1

Answer:

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.

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