Q6. A \( 250 \, \text{kg} \) satellite orbits Earth at \( 6 R_E \) from the center. What is its total energy? (\( M_E = 6 \times 10^{24} \, \text{kg}, R_E = 6.4 \times 10^6 \, \text{m}, G = 6.67 \times 10^{-11} \, \text{N m}^2/\text{kg}^2 \))
- A. -1.2 × 10⁹ J
- B. -1.3 × 10⁹ J
- C. -1.4 × 10⁹ J
- D. -1.5 × 10⁹ J