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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

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

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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

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