I don't buy that the available payload mass will be sensible when including the amount of power generation needed, especially considering that most satellites would probably still need a heavy chemical stage to boost them to their operating orbit.
On top of that I'm not really convinced they can put enough solar generation on there to drive the thrusters sufficiently, putting aside the additional costs of things like radiating off all the heat generated by the thrusters.
They wouldn't. That's why they're aiming to use plasma thrusters.