Navin P. answered 02/28/23
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The force acting on the planet is G*M*m/(R2)
This has to be equal to the centripetal force to keep it in orbit.
Hence, G*M*m/(R^2) = m* V2/ R (call this Eq. 1)
In this case, we can treat V as the speed (and not velocity).
Also,
V = distance / time , where distance = perimeter of the orbit = 2* Pi * R.
Hence, time for revolution = (2* Pi * R) / V (call this eq. 2)
We will use equations 1 and 2 to get the answer now.
From Eq. 1, we have
V^2/R = G * M / R2 , which means V = Sqrt(G* M / R)
Hence time =(2 * Pi * R) / Sqrt(G* M / R) (call this eq 3)
Note that R = 3625 +2.090×105
Be careful to convert km to meters above!!
On solving eq 3, we get time = 1.17*107 seconds.
Divide this by (24*60*60) to convert seconds to days.
So we finally get, time = 135.52 days