For a satellite moving in an orbit around the earth, the ratio of kinetic energy of potential

For a satellite moving in an orbit around the earth, the ratio of kine

1.	For a satellite moving in an orbit around the earth, the ratio of kinetic energy of potential
Answer» 2 `sqrt2` `1/2` `(1)/(sqrt2)` Solution :`(GMm)/(R^2) = m omega^2 R` `KE = 1/2 I omega^2= 1/2 mR^2 omega^2 = (GMm)/(2R)` `PE= - (GMm)/(R )` `(KE)/(\|P.E\|) = (GMm)/(2R) XX (R )/(GMm) = 1/2 `