A research satellite of mass $200 \mathrm{~kg}$. Circles the earth in an orbit of average radius $(3 \mathrm{R} / 2)$ where $\mathrm{R}$ is radius of earth. Assuming the gravitational pull $10 \mathrm{~N}$, the pull on the satellite will be $=\mathrm{N}$
(A) 880
(B) 889
(C) 890
(D) 892