We know that a satellite moving west to east at a distance R=2.00×104km from the centre of the earth will be revolving round the earth with an angular velocity faster than the earth's diurnal angular velocity. Let
ω= angular velocity of the satellite
ω0=2πT= angular velocity of the earth. Then
ω−ω0=2πτ
as the relative angular velocity with respect to earth. Now by Newton's law
γMR2=ω2R
So, M=R3γ(2πτ+2πT)2
=4π2R3γT2(1+Tτ)2
Substitution gives M=6.27×1024kg