MCQOPTIONS
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| 1. |
For a satellite moving in an orbit around the earth, the ratio of kinetic energy to potential energy is [CBSE PMT 2005] |
| A. | 2 |
| B. | \[\frac{1}{2}\] |
| C. | \[\frac{1}{\sqrt{2}}\] |
| D. | \[\sqrt{2}\] |
| Answer» C. \[\frac{1}{\sqrt{2}}\] | |