Physics, asked by wadia4763, 8 months ago

A communication satellite is launched at 42000km above the earth finds its orbital velocity

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Answered by Anonymous
3

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. Substituting and solving yields a speed of 7780 m/s.

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