The correct option is A −2GMmr
Since both the satellites are in a circular orbit of the same radius r, their velocities will be the same. v=√GMr Since, external forces along the tangential direction to the orbit are absent, so the linear momentum of the system along that direction (both satellites) will be conserved.
mv−mv=mV+mV
Where,V is the final velocity of the system.
⇒V=0
So, the kinetic energy will become zero, and total energy will be contributed by potential energy alone.
So, E=−GM(m+m)r=−2GMmr
Hence, option (a) is the correct answer.