If orbital velocity of planet is given by v=GaMbRc, then
a=1/3, b=1/3, c=−1/3
a=1/2, b=1/2, c=−1/2
a=1/2, b=−1/2, c=1/2
a=1/2, b=−1/2, c=−1/2
v=GMR=G1/2M1/2R−1/2