The speed of the satellite may be obtained from the equation,
GMmR2=mv2R
or, v=√GMR
=[(6.67×10−11Nm2kg−2)(6×1024kg)6400×103m]1/2
=7910ms−1.
Thus, v/c=79103×108=2.637×10−5
or, √1−(vc)2=[1−6.95×10−10]1/2
≈1−3.48×10−10
The time taken by the satellite to complete one revolution is
T=2πRv=6.28×6400×103m7910ms−1=5080s
The clock on the satellite will slow down as observed from the earth. If the time elapsed on the satellite's clock is t as the satellite completes one revolution (this is proper time and 5080 s is improper time).
t=(1−3.48×10−10)×(5080s)
or, 15080s=1−3.48×10−10
or (t−5080s)5080=3.48×10−10
or, (t−5080)=−1.77×10−6s.
The satellite's clock falls behind by 1.77×10−6s in one revolution.