Understanding Gravitational Potential Energy of Artificial Satellites

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I've bumped into a little problem while solving some tests for my physics course, so I'd appreciate some help :) :
Consider an artificial satellite circling around the Earth; how much times is the absolute value of it's gravitational potential energy greater than it's kinetic energy?
 
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Write down the expressions for gravitational potantial energy (say Eg) and the kinetic energy (say Ek).

Question is what is 'n' where

Eg * n = Ek

You will have to use the equilibrium condition for the orbital motion of the satilite around the Earth to get rid of the velocity from Ek.