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


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