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				| 1. | A satellite of mass “m” is in a circular orbit of radius 1.5R around the earth of radius R. How much energy is required to move it to an orbit of radius 2R? | 
| A. | -(G*M*m)/12R | 
| B. | (G*M*m)/12R | 
| C. | -(G*M*m)/4R | 
| D. | (G*M*m)/4R | 
| Answer» B. (G*M*m)/12R | |