An $8000 \mathrm{~kg}$ Satellite Is Launched from the Surface of the Earth and the Earth

An $8000 \mathrm{~kg}$ satellite is launched from the surface of the Earth and injected into a circular orbit at an altitude of $100 \mathrm{~km}$ above the surface of the Earth. The gravitational potential energy of the satellite in the circular orbit is $\left(\mathrm{G}=6.67 \times 10^{-11} \mathrm{~N} \cdot \mathrm{m}^{2} / \mathrm{kg}^{2}, \mathrm{M}_{\mathrm{E}}=5.97 \times 10^{24} \mathrm{~kg}, \mathrm{R}_{\mathrm{E}}=6.37 \times 10^{6} \mathrm{~m}\right)$

A) $-5.01 \times 1011 \mathrm{~J}$ .
B) $-4.75 \times 1011 \mathrm{~J}$ .
C) $-4.02 \times 1011 \mathrm{~J}$ .
D) $-4.92 \times 1011 \mathrm{~J}$ .
E) $-3.85 \times 1011 \mathrm{~J}$