Match the following columns `{:(,"Column-I",,"Column-II"),("(A)",underset("satellite in circular orbit")("Time period of an earth"),"(p)","Independent of mass of satellite"),("(B)","Orbital velocity of satellite","(q)","Independent of radius of orbit"),("(C)","Mechanical energy of satellite","(r)","Independent of mass of earth"),(,,"(s)","None"):}`

Match the following columns `{:(,"Column-I",,"Column-II"),("(A)",under

1.	Match the following columns `{:(,"Column-I",,"Column-II"),("(A)",underset("satellite in circular orbit")("Time period of an earth"),"(p)","Independent of mass of satellite"),("(B)","Orbital velocity of satellite","(q)","Independent of radius of orbit"),("(C)","Mechanical energy of satellite","(r)","Independent of mass of earth"),(,,"(s)","None"):}`
Answer» Correct Answer - `(A rarr p,B rarr p,C rarr s)` `T=(2)/(sqrt(GM))r^(3//2),v_(0)=sqrt((GM)/(r))and E=-(GMm)/(2r)`

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