Ensuring that this does not occur requires sophisticated power management under both hardware and software control. For this, a bus provider must be selected. Basic space vehicle structures sans communication payloads are known as buses. Careful analysis and trade-offs occur in this arena as well. A batch of bad gyroscopes could turn half the fleet into exorbitant space junk, and more fuel adds more weight.
Less fuel can reduce a space vehicle's useful life to a handful of years.
At this point, more choices must be made. Remaining in its original orbit as space clutter is not an option. Another major LEO implementation factor concerns intersatellite communications. It is up to LEO business planners to answer these questions. If intervehicle routing is deemed best for LEO system performance, then other factors must be considered.