Well, Falcon-9 Block 5 could launch about 5.800 kg on GTO. More than enough for a bus, several warheads, and retro-rocket booster (since the system is space-based, we could afford to use storable liquid-fuel and get more specific impulse than solid fuel could).
For example: let's use the old "Chevaline" missile bus for our calculations (there are a lot of data for it). It's about 318 kg fueled, and designed for 400 kg payload (warheads, decoys, chaffs, ect.). So we could safely fit three W76 warheads on it, and have enough mass for decoys.
Extracting 750 kg of payload mass from 5800 kg allowance, we are left with about 5 tons for propulsion. Let's assume that we use RD-864 hypergolic rocket engine, with a specific impulse of 300 s and dry mass of 200 kg. Let's also assume that tanks, frames, ect. are about 800 kg of total mass.
So we are left with 4000 kg of propellant for a 1800 kg of everyting else, and we have 300 s ISP engine. We could have delta-v supply around 3.4 km/s - more than enough for de-orbiting and even some maneuvering.
And how many LEO satellites could you have for the same cost/effort? And how much cheaper is it to build the ASAT weapon that will engage the RV, since it only has to go up not back down? What does this buy you over a silo solution?