The kinetic energy of the satellite in a circular orbit with speed vis given as:
- A$\text{KE}=\frac{-\text{GmM}_\text{e}}{2(\text{R}_\text{e}+\text{h})}$
- B$\text{KE}=\frac{\text{GmM}_\text{e}}{(\text{R}_\text{e}+\text{h})}$
- ✓$\text{KE}=\frac{\text{GmM}_\text{e}}{2(\text{R}_\text{e}+\text{h})}$
- D$\text{KE}=-\frac12\text{mv}^2$
Answer: C.
View full solution →
