1.

The radius of orbit of a geostationary satellite is given by _____ (M = Mass of the earth; R = Radius of the earth; T = Time period of the satellite)

A. [(T<sup>2</sup>*G*M)/(4*pi<sup>2</sup>)]<sup>3/2</sup>
B. [(T<sup>2</sup>*G*M)/(4*pi<sup>2</sup>)]<sup>2/3</sup> R
C. [(T<sup>2</sup>*G*M)/(4*pi<sup>2</sup>)]<sup>1/3</sup> R
D. [(T<sup>2</sup>*G*M)/(4*pi<sup>2</sup>)]<sup>1/3</sup>
Answer» E.


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