Hi Israr, welcome to PF.
The speed of any object in orbit in a gravitational field (planets around stars, moons around planets, the ISS around the Earth) is determined by the orbital height of the object.
For a circular orbit, and something of negligable mass compared to the other body (e.g. the ISS around the Earth, or the Earth around the sun) this is roughly equal to
##v \approx \sqrt{\frac{G M}{r}}##.
Where G is the gravitational constant, M the mass of the body being orbited around, and r the radius. If you plug in the mass of the earth, and the radius of orbit of the ISS (~412 km above sea level) into that equation,
you see that you get 7.7 km/s!
So, you see that if you wanted the ISS to go at a much slower speed, you'd have to push it much further away from the Earth!