estimated that there are 600,000 pieces of space junk ranging from , and 23,000 larger than that. On average one satellite is destroyed by collision with space junk each year. there had been four collisions between catalogued objects, including a collision between two satellites in 2009. Orbital decay is much slower at altitudes where atmospheric drag is insignificant. Slight atmospheric drag, lunar perturbation, and solar wind drag can gradually bring debris down to lower altitudes where fragments finally re-enter, but this process can take millennia at very high altitudes. Implications The Kessler syndrome is troublesome because of the domino effect and feedback runaway wherein impacts between objects of sizable mass spall off debris from the force of the collision. The fragments can then hit other objects, producing even more space debris: if a large enough collision or explosion were to occur, such as between a space station and a defunct satellite, or as the result of hostile actions in space, then the resulting debris cascade could make prospects for long-term viability of satellites in particular low Earth orbits extremely low. However, even a catastrophic Kessler scenario at LEO would pose minimal risk for launches continuing past LEO, or satellites travelling at medium Earth orbit (MEO) or geosynchronous orbit (GEO). The catastrophic scenarios predict an increase in the number of collisions per year, as opposed to a physically impassable barrier to space exploration that occurs in higher orbits. Avoidance and reduction Designers of a new vehicle or satellite are frequently required by the ITU to demonstrate that it can be safely disposed of at the end of its life, for example by use of a controlled atmospheric reentry system or a boost into a graveyard orbit. For US launches or satellites that will have broadcast to US territories—in order to obtain a license to provide telecommunications services in the United States—the Federal Communications Commission (FCC) required all geostationary satellites launched after 18 March 2002 to commit to moving to a graveyard orbit at the end of their operational life. US government regulations similarly require a plan to dispose of satellites after the end of their mission: atmospheric re-entry, movement to a storage orbit, or direct retrieval. A proposed energy-efficient means of deorbiting a spacecraft from MEO is to shift it to an orbit in an unstable resonance with the Sun or Moon that speeds up orbital decay. One technology proposed to