Force on a 1 kg mass on earth of radius R is 10 N. Then the force on a satellite revolving around the earth in the mean orbital radius `(3R)/2` will be (mass of satellite is 100 kg)
| A. |
`4.44×10^2 N` |
 |
| B. |
`3.33×10^2 N` |
| C. |
500 N |
| D. |
`6.66×10^2 N` |