The value will be based on the value of the reduced risk of damage/loss from orbital debris and reduced cost from orbital adjustments to avoid debris (which use

The value will be based on the value of the reduced risk of damage/loss from orbital debris and reduced cost from orbital adjustments to avoid debris (which uses fuel or mass which reduces the lifespan of the satellite). Once we end up with 100k or more LEO satellites it'll be very valuable to reduce the amount of debris at those altitudes.