When a body is orbiting near the surface of the earth, what will be the ratio of its orbital velocity to the escape velocity from earth? |
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(a) |
1 : |
(b) |
: 1 |
(c) |
2 : 1 |
(d) |

When a body is orbiting near the surface of the earth, what will be the ratio of its orbital velocity to the escape velocity from earth? |
|||||||

(a) |
1 : |
(b) |
: 1 |
(c) |
2 : 1 |
(d) |

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