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If is the escape velocity and is the orbital velocity of a satellite for orbit close to the earth's surface, then these are related by:
1. | \(v_o=v_e\) | 2. | \(v_e=\sqrt{2v_o}\) |
3. | \(v_e=\sqrt{2}~v_o\) | 4. | \(v_o=\sqrt{2}~v_e\) |
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