Physics, asked by salaarahmad2004, 3 months ago

calculate the value of orbital speed of a satellite close to Earth​

Answers

Answered by shriyakodesia2005
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. Substituting and solving yields a speed of 7780 m/s.

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