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The orbital speed for an earth satellite near the surface of the earth is `7km//sec`. If the radius of the orbit is `4` times the radius of the earth, the orbital speed would beA. `3.5 km//s`B. `7 km//s`C. `7sqrt2 km//s`D. `14 km//s` |
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Answer» Correct Answer - A `V_(0)=sqrt((GM)/r)rArrV_(0)prop1/(sqrt(r))` |
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