1.

A satellite orbits the earth at a height of R/5. What is its orbital speed?

A. [(2*G*M)/(R)]<sup>1/2</sup>
B. [(G*M)/(R)]<sup>1/2</sup>
C. [(G*M)/(7*R)]<sup>1/2</sup>
D. [(5*G*M)/(6*R)]<sup>1/2</sup>
Answer» E.


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