A satellite of mass (m) is orbiting around the earth of mass (M) and radius R:
|
Column-I |
|
Column-II |
| (a) |
Gravitational potential energy of satellite close to the earth. |
(p) |
\(\frac{GMm}{2R}\) |
| (b) |
Kinetic energy of orbiting satellite close to the earth is. |
(q) |
\(-\frac{GMm}{2R}\) |
| (c) |
Kinetic energy of orbiting satellite orbiting close to the earth. |
(r) |
\(\frac{GMm}{4R}\) |
| (d) |
Total mechanical energy of satellite orbiting close to the earth. |
(s) |
\(-\frac{GMm}{R}\) |
