Drive the dish in a small circle around the predicted location, while measuring the signal amplitude as a function of time and position, to keep the orbital parameters up to date.
If the reason that you can't predict the orbital track is due to atmospheric drag, then just let the project slide for a week or two and the requirement will probably go away (due to reentry).
By the way, why are you using a "large" reflector for a LEO satellite. If it's LEO, then a smaller dish (with a wider beam width, making tracking easier) should suffice. Are you trying to detect an on-board LO?