Space debris - Wikipedia Space debris `` Space Junk '' redirects here. For other uses, see Space Junk ( disambiguation ). A computer - generated image representing space debris as could be seen from high Earth orbit. The two main debris fields are the ring of objects in geosynchronous Earth orbit ( GEO ) and the cloud of objects in low Earth orbit ( LEO ). Space debris ( also known as space junk, space waste, space trash, space litter or space garbage ) is a term for the mass of defunct, artificially created objects in space, most notably in Earth orbit, such as old satellites and spent rocket stages. It includes the fragments from their disintegration, erosion and collisions. As of December 2016, five satellite collisions have resulted in generating space waste. As of 5 July 2016, the United States Strategic Command tracked a total of 17,852 artificial objects in orbit above the Earth, including 1,419 operational satellites. However, these are just objects large enough to be tracked. As of July 2013, more than 170 million debris smaller than 1 cm ( 0.4 in ), about 670,000 debris 1 -- 10 cm, and around 29,000 larger debris were estimated to be in orbit. Collisions with debris have become a hazard to spacecraft ; they cause damage akin to sandblasting, especially to solar panels and optics like telescopes or star trackers that can not be covered with a ballistic Whipple shield ( unless it is transparent ). Below 2,000 km ( 1,200 mi ) Earth - altitude, debris are denser than meteoroids ; most are dust from solid rocket motors, surface erosion debris like paint flakes, and frozen coolant from RORSAT nuclear - powered satellites. For comparison, the International Space Station orbits in the 300 -- 400 kilometres ( 190 -- 250 mi ) range, and the 2009 satellite collision and 2007 antisat test occurred at 800 to 900 kilometres ( 500 to 560 mi ) altitude. The ISS has Whipple shielding ; however, known debris with a collision chance over 1 / 10,000 are avoided by maneuvering the station. The Kessler syndrome, a runaway chain reaction of collisions exponentially increasing the amount of debris, has been hypothesized to ensue beyond a critical density. This could affect useful polar - orbiting bands, increases the cost of protection for spacecraft missions and could destroy live satellites. Whether Kessler syndrome is already underway has been debated. The measurement, mitigation, and potential removal of debris are conducted by some participants in the space industry. Contents 1 Characterization 1.1 Size 1.2 Low Earth orbit ( LEO ) 1.3 Higher altitudes 2 Sources 2.1 Dead spacecraft 2.2 Lost equipment 2.3 Boosters 2.4 Weapons 3 Threats 3.1 To spacecraft 3.1. 1 Unmanned spacecraft 3.1. 2 Manned spacecraft 3.1. 2.1 Space Shuttle missions 3.1. 2.2 Mir 3.1. 2.3 International Space Station 3.1. 3 Kessler syndrome 3.2 To Earth 4 Tracking and measurement 4.1 Tracking from the ground 4.2 Measurement in space 4.3 Gabbard diagrams 5 Dealing with debris 5.1 Growth mitigation 5.2 Self - removal 5.3 External removal 5.4 International regulation 6 History and shielding technologies 6.1 Micrometeoroids 6.2 Micrometeoroid shielding 6.3 NORAD, Gabbard and Kessler 6.4 Follow - up studies 6.5 A new Kessler syndrome 6.6 Debris growth 7 In fiction 8 See also 9 References 9.1 Notes 9.2 Bibliography 10 Further reading 11 External links Characterization Size There are estimated to be over 170 million pieces of debris smaller than 1 cm ( 0.39 in ) as of July 2013. There are approximately 670,000 pieces from one to ten cm. The current count of large debris ( defined as 10 cm across or larger ) is 29,000. The technical measurement cutoff is c. 3 mm ( 0.12 in ). Over 98 percent of the 1,900 tons of debris in low Earth orbit ( as of 2002 ) was accounted for by about 1,500 objects, each over 100 kg ( 220 lb ). Total mass is mostly constant despite addition of many smaller objects, since they reenter the atmosphere sooner. Using a 2008 figure of 8,500 known items, it is estimated at 5,500 t ( 12,100,000 lb ). Low Earth orbit ( LEO ) Space debris in LEO, with its size exaggerated In LEO there are few `` universal orbits '' which keep spacecraft in particular rings ( in contrast to GEO, a single widely used orbit ). The closest are sun - synchronous orbits that keep a constant angle between the Sun and the orbital plane ; they are polar, meaning they cross over the polar regions. LEO satellites orbit in many planes, up to 15 times a day, causing frequent approaches between objects ( the density of objects is much higher in LEO ). Orbits are further changed by perturbations ( which in LEO include unevenness of the Earth 's gravitational field ), and collisions can occur from any direction. For these reasons, the Kessler syndrome applies mostly to the LEO region ; impacts occur at up to 16 km / s ( twice the orbital speed ) if head - on -- the 2009 satellite collision occurred at 11.7 km / s, creating much spall in the critical size range. These can cross other orbits and lead to a cascade effect. A large - enough collision ( e.g. between a space station and a defunct satellite ) could make low Earth orbit impassable. Manned missions are mostly at 400 km ( 250 mi ) and below, where air drag helps clear zones of fragments. Atmospheric expansion as a result of space weather raises the critical altitude by increasing drag ; in the 90s, it was a factor in reduced debris density. Another was fewer launches by Russia ; the USSR made most of their launches in the 1970s and 1980s. Higher altitudes At higher altitudes, where air drag is less significant, orbital decay takes longer. Slight atmospheric drag, lunar perturbations, Earth 's gravity perturbations, solar wind and solar radiation pressure can gradually bring debris down to lower altitudes ( where it decays ), but at very high altitudes this may take millennia. Although high - altitude orbits are less commonly used than LEO and the onset of the problem is slower, the numbers progress toward the critical threshold more quickly. Many communications satellites are in geostationary orbits ( GEO ), clustering over specific targets and sharing the same orbital path. Although velocities are low between GEO objects, when a satellite becomes derelict ( such as Telstar 401 ) it assumes a geosynchronous orbit ; its orbital inclination increases about. 8 ° and its speed increases about 100 miles per hour ( 160 km / h ) per year. Impact velocity peaks at about 1.5 km / s ( 0.93 mi / s ). Orbital perturbations cause longitude drift of the inoperable spacecraft and precession of the orbital plane. Close approaches ( within 50 meters ) are estimated at one per year. The collision debris pose less short - term risk than from an LEO collision, but the satellite would likely become inoperable. Large objects, such as solar - power satellites, are especially vulnerable to collisions. Although the ITU now requires proof a satellite can be moved out of its orbital slot at the end of its lifespan, studies suggest this is insufficient. Since GEO orbit is too distant to accurately measure objects under 1 m ( 3 ft 3 in ), the nature of the problem is not well known. Satellites could be moved to empty spots in GEO, requiring less maneuvring and making it easier to predict future motion. Satellites or boosters in other orbits, especially stranded in geostationary transfer orbit, are an additional concern due to their typically high crossing velocity. Despite efforts to reduce risk, spacecraft collisions have occurred. The European Space Agency telecom satellite Olympus - 1 was struck by a meteoroid on 11 August 1993 and eventually moved to a graveyard orbit. On 29 March 2006, the Russian Express - AM11 communications satellite was struck by an unknown object and rendered inoperable ; its engineers had enough contact time with the satellite to send it into a graveyard orbit. Sources Dead spacecraft See also : Kosmos 954, Kosmos 1402, and Derelict satellites orbiting Earth Vanguard 1 is expected to remain in orbit for 240 years. In 1958, the United States launched Vanguard I into a medium Earth orbit ( MEO ). As of October 2009, it, and the upper stage of its launch rocket, are the oldest surviving man - made space objects still in orbit. In a catalog of known launches until July 2009, the Union of Concerned Scientists listed 902 operational satellites from a known population of 19,000 large objects and about 30,000 objects launched. An example of additional dead satellite debris are the remains of the 1970s / 80s Soviet RORSAT naval surveillance satellite program. The satellite 's BES - 5 nuclear reactor were cooled with a coolant loop of sodium - potassium alloy, creating a potential problem when the satellite reached end of life. While many satellites were nominally boosted into medium - altitude graveyard orbits, not all were. Even satellites which had been properly moved to a higher orbit had an eight - percent probability of puncture and coolant release over a 50 - year period. The coolant freezes into droplets of solid sodium - potassium alloy, forming additional debris. These events continue to occur. For example, in February 2015, the USAF Defense Meteorological Satellite Program Flight 13 ( DMSP - F13 ) exploded on orbit, creating at least 149 debris objects, which were expected to remain in orbit for decades. Lost equipment A drifting thermal blanket photographed in 1998 during STS - 88. According to Edward Tufte 's book Envisioning Information, space debris includes a glove lost by astronaut Ed White on the first American space - walk ( EVA ) ; a camera lost by Michael Collins near Gemini 10 ; a thermal blanket lost during STS - 88 ; garbage bags jettisoned by Soviet cosmonauts during Mir 's 15 - year life, a wrench and a toothbrush. Sunita Williams of STS - 116 lost a camera during an EVA. During an STS - 120 EVA to reinforce a torn solar panel, a pair of pliers was lost, and in an STS - 126 EVA, Heidemarie Stefanyshyn - Piper lost a briefcase - sized tool bag. Boosters Spent upper stage of a Delta II rocket, photographed by the XSS 10 satellite In characterizing the problem of space debris, it was learned that much debris was due to rocket upper stages ( e.g. the Inertial Upper Stage ) which end up in orbit, and break up due to decomposition of unvented unburned fuel. However, a major known impact event involved an ( intact ) Ariane booster. Although NASA and the United States Air Force now require upper - stage passivation, other launchers do not. Lower stages, like the Space Shuttle 's solid rocket boosters or Apollo program 's Saturn IB launch vehicles, do not reach orbit. On 11 March 2000 a Chinese Long March 4 CBERS - 1 upper stage exploded in orbit, creating a debris cloud. A Russian Briz - M booster stage exploded in orbit over South Australia on 19 February 2007. Launched on 28 February 2006 carrying an Arabsat - 4A communications satellite, it malfunctioned before it could use up its propellant. Although the explosion was captured on film by astronomers, due to the orbit path the debris cloud has been difficult to measure with radar. By 21 February 2007, over 1,000 fragments were identified. A 14 February 2007 breakup was recorded by Celestrak. Eight breakups occurred in 2006, the most since 1993. Another Briz - M broke up on 16 October 2012 after a failed 6 August Proton - M launch. The amount and size of the debris was unknown. A Long March 7 rocket booster created a fireball visible from portions of Utah, Nevada, Colorado, Idaho and California on the evening of 27 July 2016 ; its disintegration was widely reported on social media. Weapons A past debris source was the testing of anti-satellite weapons ( ASATs ) by the U.S. and Soviet Union during the 1960s and 1970s. North American Aerospace Defense Command ( NORAD ) files only contained data for Soviet tests, and debris from U.S. tests were only identified later. By the time the debris problem was understood, widespread ASAT testing had ended ; the U.S. Program 437 was shut down in 1975. The U.S. restarted their ASAT programs in the 1980s with the Vought ASM - 135 ASAT. A 1985 test destroyed a 1 - tonne ( 2,200 lb ) satellite orbiting at 525 km ( 326 mi ), creating thousands of debris larger than 1 cm ( 0.39 in ). Due to the altitude, atmospheric drag decayed the orbit of most debris within a decade. A de facto moratorium followed the test. Known orbit planes of Fengyun - 1C debris one month after the weather satellite 's disintegration by the Chinese ASAT China 's government was condemned for the military implications and the amount of debris from the 2007 anti-satellite missile test, the largest single space debris incident in history ( creating over 2,300 pieces golf - ball size or larger, over 35,000 1 cm ( 0.4 in ) or larger, and one million pieces 1 mm ( 0.04 in ) or larger ). The target satellite orbited between 850 km ( 530 mi ) and 882 km ( 548 mi ), the portion of near - Earth space most densely populated with satellites. Since atmospheric drag is low at that altitude the debris is slow to return to Earth, and in June 2007 NASA 's Terra environmental spacecraft maneuvered to avoid impact from the debris. On 20 February 2008, the U.S. launched an SM - 3 missile from the USS Lake Erie to destroy a defective U.S. spy satellite thought to be carrying 450 kg ( 1,000 lb ) of toxic hydrazine propellant. The event occurred at about 250 km ( 155 mi ), and the resulting debris has a perigee of 250 km ( 155 mi ) or lower. The missile was aimed to minimize the amount of debris, which ( according to Pentagon Strategic Command chief Kevin Chilton ) had decayed by early 2009. The vulnerability of satellites to debris and the possibility of attacking LEO satellites to create debris clouds, has triggered speculation that it is possible for countries unable to make a precision attack. An attack on a satellite of 10 tonnes or more would heavily damage the LEO environment. Threats A micrometeoroid left this crater on the surface of Space Shuttle Challenger 's front window on STS - 7. To spacecraft Space junk is a threat to active satellites and spaceships. The Earth 's orbit may even become impassable as the risk of collision grows too high. Unmanned spacecraft Although spacecraft are protected by Whipple shields, solar panels, which are exposed to the Sun, wear from low - mass impacts. These produce a cloud of plasma which is an electrical risk to the panels. Satellites are believed to have been destroyed by micrometeorites and orbital debris ( MMOD ). The earliest suspected loss was of Kosmos 1275, which disappeared on 24 July 1981 ( a month after launch ). Kosmos contained no volatile propellant, therefore, there appeared to be nothing internal to the satellite which could have caused the destructive explosion which took place. However the case has not been proven and another hypothesis forwarded is that the battery exploded. Tracking showed it broke up, into 300 new objects. Many impacts have been confirmed since. Olympus - 1 was struck by a meteoroid on 11 August 1993, and left adrift. On 24 July 1996, the French microsatellite Cerise was hit by fragments of an Ariane - 1 H - 10 upper - stage booster which exploded in November 1986. On 29 March 2006, the Russian Ekspress AM11 communications satellite was struck by an unknown object and rendered inoperable ; its engineers had sufficient time in contact with the spacecraft to send it to a parking orbit out of GEO. On October 13, 2009, Terra suffered a single battery cell failure anomaly and a battery heater control anomaly which were likely the result of an MMOD strike. On March 12, 2010, Aura lost power from one - half of one of its 11 solar panels and this was also attributed to an MMOD strike. On May 22, 2013 GOES - 13 was hit by an MMOD which caused it to lose track of the stars that it uses to maintain attitude. It took nearly a month for the spacecraft to return to operation. The first major satellite collision occurred on 10 February 2009 at 16 : 56 UTC. The deactivated 950 kg ( 2,090 lb ) Kosmos 2251 and the operational 560 kg ( 1,230 lb ) Iridium 33 collided, 500 mi ( 800 km ) over northern Siberia. The relative speed of impact was about 11.7 km / s ( 7.3 mi / s ), or about 42,120 km / h ( 26,170 mph ). Both satellites were destroyed, with accurate estimates of the number of debris unavailable. On 22 January 2013 BLITS ( a Russian laser - ranging satellite ) was struck by debris suspected to be from the 2007 Chinese anti-satellite missile test, changing its orbit and spin rate. Satellites frequently have to perform Collision Avoidance Maneuvers and managers have to monitor debris as part of maneuver planning. For example, in January 2017, the European Space Agency planned to alter orbit of one of its $319 million Swarm mission spacecrafts, based on data from the US Joint Space Operations Center, to end the risk of collision from Cosmos - 375, an old Russian satellite. Cosmos - 375, which was destroyed by Soviet operators when its mission was complete, had previously threatened to impact the International Space Station in 2011. Manned spacecraft Space Shuttle missions Discovery 's lower starboard wing and Thermal Protection System tiles, photographed on STS - 114 during an R - Bar Pitch Manoeuvre where astronauts examine the TPS for any damage during ascent From the early Space Shuttle missions, NASA used NORAD to monitor the Shuttle 's orbital path for debris. In the 1980s, this used much of its capacity. The first collision - avoidance maneuver occurred during STS - 48 in September 1991, a seven - second thruster burn to avoid debris from Kosmos 955. Similar maneuvers followed on missions 53, 72 and 82. One of the first events to publicize the debris problem occurred on Challenger 's second flight, STS - 7. A fleck of paint struck its front window, creating a pit over 1 mm ( 0.04 in ) wide. On STS - 59 in 1994, Endeavour 's front window was pitted about half its depth. Minor debris impacts increased from 1998. Window chipping and minor damage to thermal protection system tiles ( TPS ) was already common by the 1990s. The Shuttle was later flown tail - first to take the debris load mostly on the engines and rear cargo bay ( not used in orbit or during descent, and less critical for post-launch operation ). When flying to the ISS, the two connected spacecraft were flipped around so the better - armored station shielded the orbiter. Space Shuttle Endeavour had a major impact on its radiator during STS - 118. The entry hole is about ​ ⁄ inch, and the exit hole is twice as large. NASA 's study concluded that debris accounted for half of the overall risk to the Shuttle. Executive - level decision to proceed was required if catastrophic impact was likelier than 1 in 200. On a normal ( low - orbit ) mission to the ISS the risk was c. 1 in 300, but STS - 125 ( the Hubble repair mission ) at 350 mi ( 560 km ) was initially calculated at a 1 - in - 185 risk ( due to the 2009 satellite collision ). A re-analysis with better debris numbers reduced the estimated risk to 1 in 221, and the mission went ahead. Debris incidents continued on later Shuttle missions. During STS - 115 in 2006 a fragment of circuit board bored a small hole through the radiator panels in Atlantis ' cargo bay. On STS - 118 in 2007 debris blew a bullet - like hole through Endeavour 's radiator panel. Mir Impact wear was notable on Mir, the Soviet space station, since it remained in space for long periods with its original module panels. Debris impacts on Mir 's solar panels degraded their performance. The damage is most noticeable on the panel on the right, which is facing the camera with a high degree of contrast. Extensive damage to the smaller panel below is due to impact with a Progress spacecraft. International Space station Although the ISS uses Whipple shielding to protect itself from minor debris, portions ( notably its solar panels ) can not be protected easily. In 1989, the ISS panels were predicted to degrade c. 0.23 % in four years, and they were overdesigned by 1 %. A maneuver is performed if `` there is a greater than one - in - 10,000 chance of a debris strike ''. As of January 2014, there have been sixteen maneuvers in the fifteen years the ISS had been in orbit. The crew sheltered in the Soyuz on three occasions due to late debris - proximity warnings. In addition to the sixteen firings and three Soyuz - capsule shelter orders, one attempted maneuver failed ( due to not having the several days ' warning necessary to upload the manoeuvre timeline to the station 's computer ). A March 2009 close call involved debris believed to be a 10 cm ( 3.9 in ) piece of the Kosmos 1275 satellite. In 2013, the ISS did not maneuver to avoid debris, after a record four debris maneuvers the previous year. Kessler syndrome Main article : Kessler syndrome Although most manned space activity takes place at altitudes below 800 to 1,500 km ( 500 to 930 mi ), a Kessler syndrome cascade in that region would rain down into lower altitudes and the decay time scale is such that `` the resulting ( low Earth orbit ) debris environment is likely to be too hostile for future space use ''. In a Kessler syndrome, satellite lifetimes would be measured in years or months. New satellites could be launched through the debris field into higher orbits or placed in lower orbits ( where decay removes the debris ), but the utility of the region between 800 and 1,500 km ( 500 and 930 mi ) is the reason for its amount of debris. To Earth Saudi officials inspect a crashed PAM - D module in January 2001. Although most debris burns up in the atmosphere, larger objects can reach the ground intact. According to NASA, an average of one cataloged piece of debris has fallen back to Earth each day for the past 50 years. Despite their size, there has been no significant property damage from the debris. In 1969 five sailors on a Japanese ship were injured by space debris. In 1997 an Oklahoma woman, Lottie Williams, was uninjured when she was hit in the shoulder by a 10 cm × 13 cm ( 3.9 in × 5.1 in ) piece of blackened, woven metallic material confirmed as part of the propellant tank of a Delta II rocket which launched a U.S. Air Force satellite the year before. The original re-entry plan for Skylab called for the station to remain in space for eight to ten years after its final mission in February 1974. High solar activity expanded the upper atmosphere, resulting in higher - than - expected drag and bringing its orbit closer to Earth than planned. On 11 July 1979 Skylab re-entered the Earth 's atmosphere and disintegrated, raining debris along a path over the southern Indian Ocean and Western Australia. On 12 January 2001, a Star 48 Payload Assist Module ( PAM - D ) rocket upper stage re-entered the atmosphere after a `` catastrophic orbital decay '', crashing in the Saudi Arabian desert. It was identified as the upper - stage rocket for NAVSTAR 32, a GPS satellite launched in 1993. In the 2003 Columbia disaster, large parts of the spacecraft reached the ground and entire equipment systems remained intact. More than 83,000 pieces, along with the remains of the six astronauts, were recovered in an area from three to 10 miles around Hemphill in Sabine County, TX. More pieces were found in a line from west Texas to east Louisiana, with the westernmost piece found in Littlefield, TX and the easternmost found southwest of Mora, LA. Although there is significant evidence that debris fell in Nevada, Utah, and New Mexico, debris was only found in Texas, Arkansas and Louisiana. In a rare case of property damage, a foot - long metal bracket smashed through the roof of a dentist office. NASA warned the public to avoid contact with the debris because of the possible presence of hazardous chemicals. 15 years after the failure, people were still sending in pieces with the last, as of February 1, 2018, found in the spring of 2017. On 27 March 2007, airborne debris from a Russian spy satellite was seen by the pilot of a LAN Airlines Airbus A340 carrying 270 passengers whilst flying over the Pacific Ocean between Santiago and Auckland. The debris was within 5 nautical miles ( 9.3 km ; 5.8 mi ) of the aircraft. Tracking and measurement Tracking from the ground Radar and optical detectors such as lidar are the main tools for tracking space debris. Although objects under 10 cm ( 4 in ) have reduced orbital stability, debris as small as 1 cm can be tracked, however determining orbits to allow re-acquisition is difficult. Most debris remain unobserved. The NASA Orbital Debris Observatory tracked space debris with a 3 m ( 10 ft ) liquid mirror transit telescope. FM Radio waves can detect debris, after reflecting off them onto a receiver. Optical tracking may be a useful early - warning system on spacecraft. The U.S. Strategic Command keeps a catalog of known orbital objects, using ground - based radar and telescopes, and a space - based telescope ( originally to distinguish from hostile missiles ). The 2009 edition listed about 19,000 objects. Other data come from the ESA Space Debris Telescope, TIRA, the Goldstone, Haystack, and EISCAT radars and the Cobra Dane phased array radar, to be used in debris - environment models like the ESA Meteoroid and Space Debris Terrestrial Environment Reference ( MASTER ). Measurement in Space The Long Duration Exposure Facility ( LDEF ) is an important source of information on small - particle space debris. Returned space hardware is a valuable source of information on the directional distribution and composition of the ( sub-millimetre ) debris flux. The LDEF satellite deployed by mission STS - 41 - C Challenger and retrieved by STS - 32 Columbia spent 68 months in orbit to gather debris data. The EURECA satellite, deployed by STS - 46 Atlantis in 1992 and retrieved by STS - 57 Endeavour in 1993, was also used for debris study. The solar arrays of Hubble were returned by missions STS - 61 Endeavour and STS - 109 Columbia, and the impact craters studied by the ESA to validate its models. Materials returned from Mir were also studied, notably the Mir Environmental Effects Payload ( which also tested materials intended for the ISS ). Gabbard diagrams A debris cloud resulting from a single event is studied with scatter plots known as Gabbard diagrams, where the perigee and apogee of fragments are plotted with respect to their orbital period. Gabbard diagrams of the early debris cloud prior to the effects of perturbations, if the data were available, are reconstructed. They often include data on newly observed, as yet uncatalogued fragments. Gabbard diagrams can provide important insights into the features of the fragmentation, the direction and point of impact. Dealing with debris An average of about one tracked object per day has been dropping out of orbit for the past 50 years, averaging almost three objects per day at solar maximum ( due to the heating and expansion of the Earth 's atmosphere ), but one about every three days at solar minimum, usually 51⁄2 yr later. In addition to natural atmospheric effects, corporations, academics and government agencies have proposed plans and technology to deal with space debris, but as of November 2014, most of these are theoretical, and there is no extant business plan for debris reduction. A number of scholars have also observed that institutional factors -- political, legal, economic and cultural `` rules of the game '' -- are the greatest impediment to the cleanup of near - Earth space. There is no commercial incentive, since costs are n't assigned to polluters, but a number of suggestions have been made. However, effects to date are limited. In the US, governmental bodies have been accused of backsliding on previous commitments to limit debris growth, `` let alone tackling the more complex issues of removing orbital debris. '' Growth Mitigation Spatial density of LEO space debris by altitude, according to 2011 a NASA report to the United Nations Office for Outer Space Affairs Spatial density of space debris by altitude according to ESA MASTER - 2001, without debris from the Chinese ASAT and 2009 collision events Upper stage passivation ( e.g. of Delta boosters ) by releasing residual propellants reduces debris from orbital explosions ; however not all boosters implement this. Although there is no international treaty minimizing space debris, the United Nations Committee on the Peaceful Uses of Outer Space ( COPUOS ) published voluntary guidelines in 2007. As of 2008, the committee is discussing international `` rules of the road '' to prevent collisions between satellites. By 2013, various legal regimes existed, typically instantiated in the launch licenses that are required for a launch in all spacefaring nations. The U.S. has a set of standard practices for civilian ( NASA ) and military ( DoD and USAF ) orbital - debris mitigation, as has the European Space Agency. In 2007, the ISO began preparing an international standard for space - debris mitigation. Germany and France have posted bonds to safeguard property from debris damage. When originally proposed in 2015, the OneWeb constellation, initially planned to have ~ 700 satellites anticipated on orbit after 2018, would only state that they would re-enter the atmosphere within 25 years of retirement. By October 2017, both OneWeb -- and also SpaceX, with their large Starlink constellation -- had filed documents with the US FCC with more aggressive space debris mitigation plans. Both companies committed to a deorbit plan for post-mission satellites which will explicitly move the satellites into orbits where they will reenter the Earth 's atmosphere within approximately one year following end - of - life. With a `` one - up, one - down '' launch - license policy for Earth orbits, launchers would rendezvous with, capture and de-orbit a derelict satellite from approximately the same orbital plane. Another possibility is the robotic refueling of satellites. Experiments have been flown by NASA, and SpaceX is developing large - scale on - orbit propellant transfer technology and tanker spacecraft. Another approach to debris mitigation is to explicitly design the mission architecture to always leave the rocket second - stage in an elliptical geocentric orbit with a low - perigee, thus ensuring rapid orbital decay and avoiding long - term orbital debris from spent rocket bodies. Such missions require the use of a small kick stage to circularize the orbit, but the kick stage itself may be designed with the excess - propellant capability to be able to self - deorbit. Self - Removal Although the ITU requires geostationary satellites to move to a graveyard orbit at the end of their lives, the selected orbital areas do not sufficiently protect GEO lanes from debris. Rocket stages ( or satellites ) with enough propellant may make a direct, controlled de-orbit, or if this would require too much propellant, a satellite may be brought to an orbit where atmospheric drag would cause it to eventually de-orbit. This was done with the French Spot - 1 satellite, reducing its atmospheric re-entry time from a projected 200 years to about 15 by lowering its altitude from 830 km ( 516 mi ) to about 550 km ( 342 mi ). Passive methods of increasing the orbital decay rate of spacecraft debris have been proposed. Instead of rockets, an electrodynamic tether could be attached to a spacecraft at launch ; at the end of its lifetime, the tether would be rolled out to slow the spacecraft. Other proposals include a booster stage with a sail - like attachment and a large, thin, inflatable balloon envelope. External Removal A well - studied solution uses a remotely controlled vehicle to rendezvous with, capture and return debris to a central station. One such system is Space Infrastructure Servicing, a commercially developed refueling depot and service spacecraft for communications satellites in geosynchronous orbit originally scheduled for a 2015 launch. The SIS would be able to `` push dead satellites into graveyard orbits. '' The Advanced Common Evolved Stage family of upper stages is being designed with a high leftover - propellant margin ( for derelict capture and de-orbit ) and in - space refueling capability for the high delta - v required to de-orbit heavy objects from geosynchronous orbit. A tug - like satellite to drag debris to a safe altitude for it to burn up in the atmosphere has been researched. When debris is identified the satellite creates a difference in potential between the debris and itself, then using its thrusters to move itself and the debris to a safer orbit. A variation of this approach is for the remotely controlled vehicle to rendezvous with debris, capture it temporarily to attach a smaller de-orbit satellite and drag the debris with a tether to the desired location. The `` mothership '' would then tow the debris - smallsat combination for atmospheric entry or move it to a graveyard orbit. One such system is the proposed Busek ORbital DEbris Remover ( ORDER ), which would carry over 40 SUL ( satellite on umbilical line ) de-orbit satellites and propellant sufficient for their removal. The laser broom uses a ground - based laser to ablate the front of the debris, producing a rocket - like thrust which slows the object. With continued application, the debris would fall enough to be influenced by atmospheric drag. During the late 1990s, the U.S. Air Force 's Project Orion was a laser - broom design. Although a test - bed device was scheduled to launch on a Space Shuttle in 2003, international agreements banning powerful laser testing in orbit limited its use to measurements. The Space Shuttle Columbia disaster postponed the project and according to Nicholas Johnson, chief scientist and program manager for NASA 's Orbital Debris Program Office, `` There are lots of little gotchas in the Orion final report. There 's a reason why it 's been sitting on the shelf for more than a decade. '' The momentum of the laser - beam photons could directly impart a thrust on the debris sufficient to move small debris into new orbits out of the way of working satellites. NASA research in 2011 indicates that firing a laser beam at a piece of space junk could impart an impulse of 1 mm ( 0.039 in ) per second, and keeping the laser on the debris for a few hours per day could alter its course by 200 m ( 660 ft ) per day. One drawback is the potential for material degradation ; the energy may break up the debris, adding to the problem. A similar proposal places the laser on a satellite in Sun - synchronous orbit, using a pulsed beam to push satellites into lower orbits to accelerate their reentry. A proposal to replace the laser with an Ion Beam Shepherd has been made, and other proposals use a foamy ball of aerogel or a spray of water, inflatable balloons, electrodynamic tethers, boom electroadhesion, and dedicated anti-satellite weapons. Cleanspace One On 7 January 2010 Star, Inc. reported that it received a contract from the Space and Naval Warfare Systems Command for a feasibility study of the ElectroDynamic Debris Eliminator ( EDDE ) propellantless spacecraft for space - debris removal. In February 2012 the Swiss Space Center at École Polytechnique Fédérale de Lausanne announced the Clean Space One project, a nanosatellite demonstration project for matching orbit with a defunct Swiss nanosatellite, capturing it and de-orbiting together. The mission has seen several evolutions to reach a pac - man inspired capture model. As of 2006 the cost of any of these solutions is about the same as launching a spacecraft and, according to NASA 's Nicholas Johnson, not cost - effective. Since then Space Sweeper with Sling - Sat ( 4S ), a grappling satellite which captures and ejects debris, has been studied. Sling - Sat removing space debris A consensus of speakers at a meeting in Brussels on 30 October 2012 organized by the Secure World Foundation ( a U.S. think tank ) and the French International Relations Institute reported that removal of the largest debris would be required to prevent the risk to spacecraft becoming unacceptable in the foreseeable future ( without any addition to the inventory of dead spacecraft in LEO ). Removal costs and legal questions about ownership and the authority to remove defunct satellites have stymied national or international action. Current space law retains ownership of all satellites with their original operators, even debris or spacecraft which are defunct or threaten active missions. On 28 February 2014, Japan 's Japan Aerospace Exploration Agency ( JAXA ) launched a test `` space net '' satellite. The launch was an operational test only. In December 2016 the country sent a space junk collector via Kounotori 6 to the ISS by which JAXA scientists experiment to pull junk out of orbit using a tether. The system failed to extend a 700 - meter tether from a space station resupply vehicle that was returning to Earth. On 6 February the mission was declared a failure and leading researcher Koichi Inoue told reporters that they `` believe the tether did not get released ''. Since 2012, the European Space Agency has designed a mission to remove large space debris from orbit. The mission, e. Deorbit, is scheduled for launch by 2021 with an objective to remove debris heavier than 4,000 kilograms ( 8,800 lb ) from LEO. Several capture techniques are being studied, including a net, a harpoon and a combination robot arm and clamping mechanism. International regulation Holger Krag of the European Space Agency states that as of 2017 there is no binding international regulatory framework with no progress occurring at the respective UN body in Vienna. History and shielding Technologies Micrometeoroids This section may stray from the topic of the article into the topic of another article, Micrometeoroid. Please help improve this section or discuss this issue on the talk page. ( October 2014 ) Main article : Micrometeoroid In 1946 during the Giacobinid meteor shower, Helmut Landsberg collected several small magnetic particles that were apparently associated with the shower. Fred Whipple was intrigued by this and wrote a paper that demonstrated that particles of this size were too small to maintain their velocity when they encountered the upper atmosphere. Instead, they quickly decelerated and then fell to Earth unmelted. In order to classify these sorts of objects, he coined the term `` micro-meteorite ''. Whipple, in collaboration with Fletcher Watson of the Harvard Observatory, led an effort to build an observatory to directly measure the velocity of the meteors that could be seen. At the time the source of the micro-meteorites was not known. Direct measurements at the new observatory were used to locate the source of the meteors, demonstrating that the bulk of material was left over from comet tails, and that none of it could be shown to have an extra-solar origin. Today it is understood that meteoroids of all sorts are leftover material from the formation of the Solar System, consisting of particles from the interplanetary dust cloud or other objects made up from this material, like comets. The early studies were based on optical measurements only. In 1957, Hans Pettersson conducted one of the first direct measurements of the fall of space dust on the Earth, estimating it to be 14,300,000 tons per year. This suggested that the meteoroid flux in space was much higher than the number based on telescope observations. Such a high flux presented a very serious risk to missions deeper in space, specifically the high - orbiting Apollo capsules. To determine whether the direct measurement was accurate, a number of additional studies followed, including the Pegasus satellite program. These showed that the rate of meteors passing into the atmosphere, or flux, was in line with the optical measurements, at around 10,000 to 20,000 tons per year. Micrometeoroid shielding This section may stray from the topic of the article into the topic of another article, Micrometeoroid. Please help improve this section or discuss this issue on the talk page. ( October 2014 ) The `` energy flash '' of a hypervelocity impact during a simulation of what happens when a piece of orbital debris hits a spacecraft in orbit. Whipple 's work pre-dated the space race and it proved useful when space exploration started only a few years later. His studies had demonstrated that the chance of being hit by a meteoroid large enough to destroy a spacecraft was extremely remote. However, a spacecraft would be almost constantly struck by micrometeorites, about the size of dust grains. Whipple had already developed a solution to this problem in 1946. Originally known as a `` meteor bumper '' and now termed the Whipple shield, this consists of a thin foil film held a short distance away from the spacecraft 's body. When a micrometeoroid strikes the foil, it vaporizes into a plasma that quickly spreads. By the time this plasma crosses the gap between the shield and the spacecraft, it is so diffused that it is unable to penetrate the structural material below. The shield allows a spacecraft body to be built to just the thickness needed for structural integrity, while the foil adds little additional weight. Such a spacecraft is lighter than one with panels designed to stop the meteoroids directly. For spacecraft that spend the majority of their time in orbit, some variety of the Whipple shield has been almost universal for decades. Later research showed that ceramic fibre woven shields offer better protection to hypervelocity ( ~ 7 km / s ) particles than aluminium shields of equal weight. Another modern design uses multi-layer flexible fabric, as in NASA 's design for its never - flown TransHab expandable space habitation module, and the Bigelow Expandable Activity Module, which was launched in April 2016 and attached to the ISS for two years of orbital testing. NORAD, Gabbard and Kessler To avoid artificial space debris, many -- but not all -- research satellites are launched on elliptical orbits with perigees inside Earth 's atmosphere so they will destroy themselves. Willy Ley predicted in 1960 that `` In time, a number of such accidentally too - lucky shots will accumulate in space and will have to be removed when the era of manned space flight arrives ''. After the launch of Sputnik 1 in 1957, the North American Aerospace Defense Command ( NORAD ) began compiling a database ( the Space Object Catalog ) of all known rocket launches and objects reaching orbit : satellites, protective shields and upper - and lower - stage booster rockets. NASA published modified versions of the database in two - line element set, and during the early 1980s the CelesTrak bulletin board system re-published them. Gabbard diagram of almost 300 pieces of debris from the disintegration of the five - month - old third stage of the Chinese Long March 4 booster on 11 March 2000 The trackers who fed the database were aware of other objects in orbit, many of which were the result of in - orbit explosions. Some were deliberately caused during 1960s anti-satellite weapon ( ASAT ) testing, and others were the result of rocket stages blowing up in orbit as leftover propellant expanded and ruptured their tanks. To improve tracking, NORAD employee John Gabbard kept a separate database. Studying the explosions, Gabbard developed a technique for predicting the orbital paths of their products, and Gabbard diagrams ( or plots ) are now widely used. These studies were used to improve the modelling of orbital evolution and decay. When the NORAD database became publicly available during the 1970s, NASA scientist Donald J. Kessler applied the technique developed for the asteroid - belt study to the database of known objects. In 1978 Kessler and Burton Cour - Palais co-authored `` Collision Frequency of Artificial Satellites : The Creation of a Debris Belt '', demonstrating that the process controlling asteroid evolution would cause a similar collision process in LEO in decades rather than billions of years. They concluded that by about 2000, space debris would outpace micrometeoroids as the primary ablative risk to orbiting spacecraft. At the time, it was widely thought that drag from the upper atmosphere would de-orbit debris faster than it was created. However, Gabbard was aware that the number and type of objects in space were under - represented in the NORAD data and was familiar with its behaviour. In an interview shortly after the publication of Kessler 's paper, Gabbard coined the term `` Kessler syndrome '' to refer to the accumulation of debris ; it became widely used after its appearance in a 1982 Popular Science article, which won the Aviation - Space Writers Association 1982 National Journalism Award. Follow - up studies Baker - Nunn cameras were widely used to study space debris. The lack of hard data about space debris prompted a series of studies to better characterize the LEO environment. In October 1979, NASA provided Kessler with funding for further studies. Several approaches were used by these studies. Optical telescopes or short - wavelength radar was used to measure the number and size of space objects, and these measurements demonstrated that the published population count was at least 50 % too low. Before this, it was believed that the NORAD database accounted for the majority of large objects in orbit. Some objects ( typically, U.S. military spacecraft ) were found to be omitted from the NORAD list, and others were not included because they were considered unimportant. The list could not easily account for objects under 20 cm ( 7.9 in ) in size -- in particular, debris from exploding rocket stages and several 1960s anti-satellite tests. Returned spacecraft were microscopically examined for small impacts, and sections of Skylab and the Apollo Command / Service Module which were recovered were found to be pitted. Each study indicated that the debris flux was higher than expected and debris was the primary source of collisions in space. LEO already demonstrated the Kessler syndrome. In 1981 Kessler found that 42 percent of cataloged debris was the result of 19 events, primarily explosions of spent rocket stages ( especially U.S. Delta rockets ). He discovered this by using Gabbard 's methods against known debris fields, overturning the previously held belief that most unknown debris was from old ASAT tests. A number of other Delta components in orbit ( Delta was a workhorse of the U.S. space program ) had not yet exploded. A new Kessler syndrome During the 1980s, the U.S. Air Force conducted an experimental program to determine what would happen if debris collided with satellites or other debris. The study demonstrated that the process differed from micrometeoroid collisions, with large chunks of debris created which would become collision threats. In 1991, Kessler published `` Collisional cascading : The limits of population growth in low Earth orbit '' with the best data then available. Citing the USAF conclusions about creation of debris, he wrote that although almost all debris objects ( such as paint flecks ) were lightweight, most of its mass was in debris about 1 kg ( 2.2 lb ) or heavier. This mass could destroy a spacecraft on impact, creating more debris in the critical - mass area. According to the National Academy of Sciences : A 1 - kg object impacting at 10 km / s, for example, is probably capable of catastrophically breaking up a 1,000 - kg spacecraft if it strikes a high - density element in the spacecraft. In such a breakup, numerous fragments larger than 1 kg would be created. Kessler 's analysis divided the problem into three parts. With a low - enough density, the addition of debris by impacts is slower than their decay rate and the problem is not significant. Beyond that is a critical density, where additional debris leads to additional collisions. At densities beyond this critical mass production exceeds decay, leading to a cascading chain reaction reducing the orbiting population to small objects ( several cm in size ) and increasing the hazard of space activity. This chain reaction is known as the Kessler syndrome. In an early 2009 historical overview, Kessler summed up the situation : Aggressive space activities without adequate safeguards could significantly shorten the time between collisions and produce an intolerable hazard to future spacecraft. Some of the most environmentally dangerous activities in space include large constellations such as those initially proposed by the Strategic Defense Initiative in the mid-1980s, large structures such as those considered in the late - 1970s for building solar power stations in Earth orbit, and anti-satellite warfare using systems tested by the USSR, the U.S., and China over the past 30 years. Such aggressive activities could set up a situation where a single satellite failure could lead to cascading failures of many satellites in a period much shorter than years. Debris growth During the 1980s, NASA and other U.S. groups attempted to limit the growth of debris. One effective solution was implemented by McDonnell Douglas on the Delta booster, by having the booster move away from its payload and vent any propellant remaining in its tanks. This eliminated the pressure buildup in the tanks which caused them to explode in the past. Other countries were slower to adopt this measure and, due especially to a number of launches by the Soviet Union, the problem grew throughout the decade. A new battery of studies followed as NASA, NORAD and others attempted to better understand the orbital environment, with each adjusting the number of pieces of debris in the critical - mass zone upward. Although in 1981 ( when Schefter 's article was published ) the number of objects was estimated at 5,000, new detectors in the Ground - based Electro - Optical Deep Space Surveillance system found new objects. By the late 1990s, it was thought that most of the 28,000 launched objects had already decayed and about 8,500 remained in orbit. By 2005 this was adjusted upward to 13,000 objects, and a 2006 study increased the number to 19,000 as a result of an ASAT test and a satellite collision. In 2011, NASA said that 22,000 objects were being tracked. The growth in the number of objects as a result of the late - 1990s studies sparked debate in the space community on the nature of the problem and the earlier dire warnings. According to Kessler 's 1991 derivation and 2001 updates, the LEO environment in the 1,000 km ( 620 mi ) altitude range should be cascading. However, only one major incident has occurred : the 2009 satellite collision between Iridium 33 and Cosmos 2251. The lack of obvious short - term cascading has led to speculation that the original estimates overstated the problem. According to Kessler a cascade would not be obvious until it was well advanced, which might take years. A 2006 NASA model suggested that if no new launches took place the environment would retain the then - known population until about 2055, when it would increase on its own. Richard Crowther of Britain 's Defence Evaluation and Research Agency said in 2002 that he believed the cascade would begin about 2015. The National Academy of Sciences, summarizing the professional view, noted widespread agreement that two bands of LEO space -- 900 to 1,000 km ( 620 mi ) and 1,500 km ( 930 mi ) -- were already past critical density. In the 2009 European Air and Space Conference, University of Southampton researcher Hugh Lewis predicted that the threat from space debris would rise 50 percent in the next decade and quadruple in the next 50 years. As of 2009, more than 13,000 close calls were tracked weekly. A 2011 report by the U.S. National Research Council warned NASA that the amount of orbiting space debris was at a critical level. According to some computer models, the amount of space debris `` has reached a tipping point, with enough currently in orbit to continually collide and create even more debris, raising the risk of spacecraft failures ''. The report called for international regulations limiting debris and research of disposal methods. In Fiction The plot of episode 4 ( `` Conflict '' ) of Gerry Anderson 's 1970 TV series UFO includes routine missions for the disposal of spent satellites by bombing. Salvage 1 ( 1979 TV series ) deals humorously with a scrap dealer who establish a space junk salvage company. Planetes is a manga ( 1999 - 2004 ) and anime series ( 2003 - 2004 ) about a team which is responsible for the collection and disposal of space debris. The DVDs for the TV series include interviews with NASA 's Orbital Debris Program Office. Gravity is a 2013 survival film, directed by Alfonso Cuaron, about a disaster on a space mission caused by Kessler syndrome. See also Space portal Category : Derelict satellites Interplanetary contamination Liability Convention List of large reentering space debris List of space debris producing events Long Duration Exposure Facility Near - Earth object OneWeb satellite constellation Orbital Debris Co-ordination Working Group Satellite warfare Solar Maximum Mission Spacecraft cemetery References Notes Jump up ^ `` Orbital Debris Quarterly News '' ( PDF ). Vol. 20 no. 3. NASA. July 2016. p. 8. Retrieved 10 October 2016. Jump up ^ `` UCS Satellite Database ''. Nuclear Weapons & Global Security. Union of Concerned Scientists. 11 August 2016. Retrieved 10 October 2016. ^ Jump up to : `` How many space debris objects are currently in orbit ? '' ESA, July 2013. Retrieved 6 February 2016 Jump up ^ `` The Threat of Orbital Debris and Protecting NASA Space Assets from Satellite Collisions '' ( PDF ). Space Reference. 2009. 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Johnson, `` Risks in Space from Orbiting Debris '', Science, Volume 311 Number 5759 ( 20 January 2006 ), pp. 340 -- 341 Jump up ^ Antony Milne, Sky Static : The Space Debris Crisis, Greenwood Publishing Group, 2002, ISBN 0 - 275 - 97749 - 8, p. 86. Jump up ^ Technical, p. 7. Jump up ^ Paul Marks, `` Space debris threat to future launches '', 27 October 2009. Jump up ^ Space junk at tipping point, says report, BBC News, 2 September 2011 Bibliography Donald Kessler ( Kessler 1991 ), `` Collisional Cascading : The Limits of Population Growth in Low Earth Orbit '', Advances in Space Research, Volume 11 Number 12 ( December 1991 ), pp. 63 -- 66. Donald Kessler ( Kessler 1971 ), `` Estimate of Particle Densities and Collision Danger for Spacecraft Moving Through the Asteroid Belt '', Physical Studies of Minor Planets, NASA SP - 267, 1971, pp. 595 -- 605. Bibcode 1971NASSP. 267... 595K. Donald Kessler ( Kessler 2009 ), `` The Kessler Syndrome '' webpages.charter.net, 8 March 2009. Donald Kessler ( Kessler 1981 ), `` Sources of Orbital Debris and the Projected Environment for Future Spacecraft '', Journal of Spacecraft, Volume 16 Number 4 ( July -- August 1981 ), pp. 357 -- 360. Donald Kessler and Burton Cour - Palais ( Kessler 1978 ), `` Collision Frequency of Artificial Satellites : The Creation of a Debris Belt '' Journal of Geophysical Research, Volume 81, Number A6 ( 1 June 1978 ), pp. 2637 -- 2646. Donald Kessler and Phillip Anz - Meador, `` Critical Number of Spacecraft in Low Earth Orbit : Using Fragmentation Data to Evaluate the Stability of the Orbital Debris Environment '', Presented and the Third European Conference on Space Debris, March 2001. Heiner Klinkrad, `` Space Debris : Models and Risk Analysis '', Springer - Praxis, 2006, ISBN 3 - 540 - 25448 - X. ( Technical ), `` Orbital Debris : A Technical Assessment '' National Academy of Sciences, 1995. ISBN 0 - 309 - 05125 - 8. Jim Schefter, `` The Growing Peril of Space Debris '' Popular Science, July 1982, pp. 48 -- 51. Further reading `` What is Orbital Debris ? '', Center for Orbital and Reentry Debris Studies, Aerospace Corporation Committee for the Assessment of NASA 's Orbital Debris Programs ( 2011 ). Limiting Future Collision Risk to Spacecraft : An Assessment of NASA 's Meteoroid and Orbital Debris Programs. Washington, D.C. : National Research Council. ISBN 978 - 0 - 309 - 21974 - 7. Klotz, Irene ( 1 September 2011 ). `` Space junk reaching ' tipping point, ' report warns ''. Reuters. Retrieved 2 September 2011. News item summarizing the above report Steven A. Hildreth and Allison Arnold. Threats to U.S. National Security Interests in Space : Orbital Debris Mitigation and Removal. Washington, D.C. : Congressional Research Service, 8 January 2014. David Leonard, `` The Clutter Above '', Bulletin of the Atomic Scientists, July / August 2005. Patrick McDaniel, `` A Methodology for Estimating the Uncertainty in the Predicted Annual Risk to Orbiting Spacecraft from Current or Predicted Space Debris Population ''. National Defense University, 1997. `` Interagency Report on Orbital Debris, 1995 '', National Science and Technology Council, November 1995. Nickolay Smirnov, Space Debris : Hazard Evaluation and Mitigation. Boca Raton, FL : CRC Press, 2002, ISBN 0 - 415 - 27907 - 0. Richard Talcott, `` How We Junked Up Outer Space '', Astronomy, Volume 36, Issue 6 ( June 2008 ), pp. 40 -- 43. `` Technical report on space debris, 1999 '', United Nations, 2006. ISBN 92 - 1 - 100813 - 1. Robin Biesbroek ( 2015 ). Active Debris Removal in Space : How to Clean the Earth 's Environment from Space Debris. CreateSpace. ISBN 978 - 1 - 5085 - 2918 - 7. External links Wikimedia Commons has media related to Space debris. Wikinews has related news : Out of space in outer space : Special report on NASA 's ' space junk ' plans Sativew -- Tracking Space Junk in real time NASA Orbital Debris Program Office ESA Space Debris Office `` Space : the final junkyard '', documentary film Would a Saturn - like ring system around planet Earth remain stable ? Abdul Ahad EISACT Space Debris during the international polar year Intro to mathematical modeling of space debris flux SOCRATES : A free daily service predicting close encounters on orbit between satellites and debris orbiting Earth A summary of current space debris by type and orbit Space Junk Astronomy Cast episode No. 82, includes full transcript Paul Maley 's Satellite Page -- Space debris ( with photos ) Space Debris Illustrated : The Problem in Pictures PACA : Space Debris IEEE -- The Growing Threat of Space Debris The Threat of Orbital Debris and Protecting NASA Space Assets from Satellite Collisions ( 1 ) ( 2 ) Space Age Wasteland : Debris in Orbit Is Here to Stay ; Scientific American ; 2012 United States Space Surveillance Network PATENDER : GMV 'S Trailblazing low - gravity space - debris capture system Space Junk Infographic Project West Ford an intentional placement of a large amount of small copper metallic objects in medium Earth orbit ( long lifetime ) in the 1960s by the US government, resulting in a large amount of space debris, which created international relations adverse effects. 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Question: what's the name for a chunk of space debris that is still floating in space
Answer: Space debris