 
			 
			MCQOPTIONS
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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. | [(T2*G*M)/(4*pi2)]3/2 | 
| B. | [(T2*G*M)/(4*pi2)]2/3 – R | 
| C. | [(T2*G*M)/(4*pi2)]1/3 – R | 
| D. | [(T2*G*M)/(4*pi2)]1/3 | 
| E. | [(T2*G*M)/(4*pi2)]3/2b) [(T2*G*M)/(4*pi2)]2/3 – Rc) [(T2*G*M)/(4*pi2)]1/3 – Rd) [(T2*G*M)/(4*pi2)]1/3 | 
| Answer» E. [(T2*G*M)/(4*pi2)]3/2b) [(T2*G*M)/(4*pi2)]2/3 – Rc) [(T2*G*M)/(4*pi2)]1/3 – Rd) [(T2*G*M)/(4*pi2)]1/3 | |