A satellite revolving in a circular equatorial orbit of radius R=2.0×104 from west to east appears over a certain point at the equator every 11.6h. From these data, the mass of the earth is x×1024kg Find x. G=6.67×10−11Nm2Kg−2
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Solution
Relative angular velocity is given by
ωrel=2π11.6(3600)=1.5X10−4/s
Angular velocity of earth is ωe=2π24(3600)=7.3X10−5/s
Thus, angular velocity of satellite is ω=2.23X10−4/s=√GMR3=√6.67X10−11M6400000