The speed of the satellite in a circular orbit around the Earth is 1.32 x 10⁵ m/s.
v = √(GM/r)
where;
v = √(6.67 x 10⁻¹¹ x 5.98 x 10²⁴/3.57 x 6.37x 10³)
v = 1.32 x 10⁵ m/s
Thus, the speed of the satellite in a circular orbit around the Earth is 1.32 x 10⁵ m/s.
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