1.

A satellite is launched in the equatorial plane in such a way that it can transmit signals up to \[60{}^\circ \] latitude on the earth. The angular velocity of the satellite is

A. \[\sqrt{\frac{GM}{8{{R}^{3}}}}\]
B. \[\sqrt{\frac{GM}{2{{R}^{3}}}}\]
C. \[\sqrt{\frac{GM}{4{{R}^{3}}}}\]
D. \[\sqrt{\frac{3\sqrt{3}GM}{8{{R}^{3}}}}\]
Answer» B. \[\sqrt{\frac{GM}{2{{R}^{3}}}}\]


Discussion

No Comment Found

Related MCQs