Geostationary satellites orbit at a height of above the Earth's surface and orbit with the same period as the Earth (so they always stay above the same spot, i.e. geostationary). If you stand on the Earth's surface what is the ratio of a geostationary satellite's speed to your speed?
Details and assumptions
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Your speed on the surface of the earth is given by v = 6 3 7 0 ω where ω is the angular velocity of the earth. The speed of the satellite is given by v s = ( 3 5 7 8 6 + 6 3 7 0 ) ω . Hence the ratio of speeds v s / v = ( 3 5 7 8 6 + 6 3 7 0 ) / 6 3 7 0 = 6 . 6 1 8 .