1.

A satellite is in a circular orbit around a planet. Its period of revolution is T, radius of the orbit is R, orbital velocity V and acceleration 'a', then

Answer»

V = at and `a = (V^(2))/(R)`
`V = (2PI R)/(T)` and V = a T
`V = (2pi R)/(T)` and `a = (V^(2))/(R)`
`V = (1)/(2)a T^(2)`

Answer :C


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