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				| 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. | |