If you have to yeet space trash to a gravitational well, Jupiter is probably the more attractive option. Lower delta-V, still a large well, and so long as you get reasonably close, orbital decay should solve the problem eventually.

For de-orbiting LEO satellites, electrodynamic tethers is probably the most viable active method:

"Study on electrodynamic tether system for space debris removal"

<https://www.sciencedirect.com/science/article/abs/pii/S00945...>