When a satellite revolves around the sun in a circular orbit of radius a with a period of revolution T, and if K is a positive constant, then
When a satellite revolves around the sun in a circular orbit of radius a with a period of revolution T, and if K is a positive constant, then
A. `T=Ka^(2)`
B. `T=Ka^(3)`
C. `T=Ka^(3//2)`
D. `T=Ka^(2//3)`
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