Find the radius R of the orbit of a geosynchronous satellite that circles the Earth. (Note that R is measured from the center of the Earth, not the surface of the Earth.) Use the following values if needed in this problem: The universal gravitational constant G is 6.67 \times 10^{-11}\;{\rm N \; m^2 / kg^2}.The mass of the earth is 5.98 \times 10^{24}\;{\rm kg}.The radius of the earth is 6.38 \times 10^{6}\;{\rm m}.