The speed of a satellite in a circular orbit around the Earth is 4,188 m/s.
The speed of the satellite is calculated as follows;
v = √GM/r
where;
v = √[(6.67 x 10⁻¹¹ x 5.98 x 10²⁴) / (3.57 x 6.37 x 10⁶)]
v = 4,188 m/s
Thus, the speed of a satellite in a circular orbit around the Earth is 4,188 m/s.
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