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You are confusing two radii. On the left is R, the radius of the Earth; on the right is r, the orbital radius of your satellite.somekid99 said:Wait wait, I'm a bit confused.
So M = gR2/G
R = squareroot(MG/g)
sqrt(MG/g) = cbrt(GMT2/4pi2)
Use R = squareroot(MG/g) to get rid of the MG factor in your expression for r.