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Two satellite revolve around the earth in circular orbits at heights `h_(1) and h_(2)` above the surface of the earth respectively. If R is radius of the earth, then the ratio of their orbital linear velocities isA. `sqrt((R+h_(1))/(R+h_(2)))`B. `sqrt((R+h_(2))/(R+h_(1)))`C. `sqrt((h_(1))/(h_(2)))`D. `sqrt((h_(2))/(h_(1)))` |
Answer» Correct Answer - b `(V_(C_(1)))/(V_(C_(2)))=sqrt((r_(2))/(r_(1)))=sqrt((R+h_(2))/(R+h_(1)))` |
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