An artificial satellite revolves around a planet for which gravitational force \((F)\) varies with the distance \(r\) from its centre as \(F \propto r^{2}.\) If \(v_0\) is its orbital speed, then:

1. \(v_{0} \propto r^{-1/2}\) 2. \(v_{0} \propto r^{3/2}\)
3. \(v_{0} \propto r^{-3/2}\) 4. \(v_{0} \propto r\)
Subtopic:  Orbital velocity |
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