MCQ
The kinetic energy of the satellite in a circular orbit with speed $v$ is given as
- ✓$KE =\frac{G m M_e}{2\left(R_e+h\right)}$
- B$KE =-\frac{1}{2} m v^2$
- C$KE =\frac{G m M_e}{\left(R_e+h\right)}$
- D$KE =\frac{-G m M_e}{2\left(R_e+h\right)}$
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$\left(g=10\, m s^{-2}\right)$

