The speed of the satellite \( v \) is given by the formula for the orbital speed of a satellite: \[ v = \frac{2\pi r}{T} \] where: - \( v \) is the speed of the satellite, - \( r \) is the radius of the orbit, - \( T \) is the time period of revolution.
\[ v = \frac{2 \pi \times 4.225 \times 10^7}{86,400} \]
\[ v = \frac{2 \pi \times 4.225 \times 10^7}{86,400} \approx \frac{2 \times 3.1416 \times 4.225 \times 10^7}{86,400} \approx \frac{2.653 \times 10^8}{86,400} \approx 3,067.3 \, \text{m/s} \]
The speed of the artificial satellite is approximately \( 3,067.3 \, \text{m/s} \).