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 kinetic energy of the satellite in the circular orbit is $(G=6.67 \times$ $10^{-11} \mathrm{~N} \cdot \mathrm{m}^{2} / \mathrm{kg}^{2}, \mathrm{M}_{\mathrm{E}}=5.97 \times 1024 \mathrm{~kg}, \mathrm{R}_{\mathrm{E}}=6.37 \times 10^{6} \mathrm{~m}$ )

A) $5.02 \times 1011 \mathrm{~J}$ .
B) $3.45 \times 1011 \mathrm{~J}$ .
C) $2.01 \times 1011 \mathrm{~J}$ .
D) $4.25 \times 1011 \mathrm{~J}$ .
E) $2.46 \times 10^{11} \mathrm{~J}$ .