The amount of energy needed to get out of earth's gravity well is incredibly high. It would be silly to try to boost a massive object like the ISS out.
Escape velocity energy from an orbit is sqrt(2) times the energy it takes to get to that orbit. But it’s more than ~41% more fuel, since you need more fuel to push the fuel, and more fuel than that to get it to orbit in the first place.
Much cheaper to let the atmosphere drag it down, which is something that is going to happen anyways.
So achieving escape velocity from geosynchronous orbit requires more delta v than from LEO?
I kind of see it, as the surface velocity of a GEO satellite is near zero yet the surface velocity of a LEO bird is measured in the thousands of KPH. However so much more energy was invested in raising the satellite so high up, I have a difficult time imagining that actually more energy is now required to bring it to escape velocity. Is not escape velocity at GEO altitudes lower than escape velocity at LEO?
That would take way to much energy for little benefit. They expect the ISS to burn up in the atmosphere so there wouldn't be a safety issue to people/things on earth.
