Major contributors to space debris include the explosion of upper stages and satellite collisions.
There were 190 known satellite breakups between 1961 and 2006.[1] By 2015, the total had grown to 250 on-orbit fragmentation events.[2]
there were an estimated 500,000 pieces of debris in orbit,[3] with 300,000 pieces below 2000 km (LEO). Of the total, about 20,000 are tracked.[4] Also, about sixteen old Soviet nuclear space reactors are known to have released an estimated 100,000 NaK liquid metal coolant droplets 800–900 km up,[5] which range in size from 1 – 6 cm.[5]
The greatest risk to space missions is from untracked debris between 1 and 10 cm in size.[4] Large pieces can be tracked and avoided, and impact from smaller pieces are usually survivable.[4]
2007 | 3,549 | Intentional collision (ASAT) | ||
2009 | 1,716 | Accidental collision with Iridium 33 | ||
2021 | 1,562 | Intentional collision (ASAT) | ||
Long March 6A upper stage | 2024 | 700–900+ | Unknown; but may be related to upper stage passivization or insulation.[7] | |
Long March 6A upper stage | 2022 | 781[8] | Unknown; but may be related to upper stage passivization or insulation with later debris cloud expansion.[9] | |
STEP 2 Rocket Body | 1996 | 756 | Residual propellant explosion | |
Iridium 33 | 2009 | 659 | Accidental collision with Kosmos 2251 | |
2008 | 511 | Disintegrated | ||
SPOT 1 Rocket Body | 1986 | 506 | Residual propellant explosion | |
1981 | 482 | Battery explosion | ||
OV2-1 Rocket Body | 1965 | 473 | Engine explosion | |
Nimbus 4 Rocket Body | 1970 | 465 | Residual propellant explosion | |
2015 | 458 | Battery explosion | ||
TES Rocket Body | 2001 | 373 | Residual propellant explosion | |
CBERS-1 Rocket Body | 2000 | 344 | Residual propellant explosion | |
Fregat tank | 2020 | 338 | Residual propellant explosion | |
1961 | 320 | Residual propellant explosion | ||
1975 | 313 | Residual propellant explosion | ||
1985 | 289 | Intentional collision (ASAT) [10] |
Date | Object | International Designation | Cause | Total Pieces | Pieces in Orbit | Reentered Pieces as of Dec 2022 | |
---|---|---|---|---|---|---|---|
August 31, 2018 | Centaur V upper stage[11] | 2014-055B | Unknown | 107 | 107 | 0 | |
December 22, 2018 | ORBCOMM FM-16 | 1998-046E | Energetic fragmentation; Probably caused by left over propellent | 13 | 5 | 8 | |
January 24, 2019 | Microsat-R[12] | 2019-006A | ASAT (Anti-Satellite) weapon system test | 129 | 0 | 129 | |
February 6, 2019 | H2-A 202 Rocket Body | 2018-084L | Unknown; Third known breakup of an H-2A Rocket Body | 6 | 0 | 6 | |
February 6, 2019 | H2-A 202 Payload Adapter | 2018-084E | Energetic fragmentation event; Cause Unknown | 3 | 0 | 3 | |
April 2019 | Centaur V Rocket Body | 2018-079B | Energetic fragmentation event; Cause Unknown | 193 | 192 | 1 | |
May 7, 2019 | Titan IIIC Transtage rocket body[13] | 1976-023F | Energetic fragmentation event by caused the overheating of leftover anhydrous hydrazine(N2H4) Mono Propellant | ? | ? | ? | |
August 19, 2019 | SOZ (Sistema Obespecheniya Zapuska) ullage motor from a Proton Block DM fourth stage | 2010-041H | Energetic fragmentation event; caused by left over fuel in the ullage motor. 30th fragmentation event of a SOZ unit. 34 intact units remain in orbit | 23 | 23 | 0 | |
August 13, 2019 | Ariane 42P third stage rocket body | 1992-052D | Unknown | 10 | 10 | 0 | |
December 23, 2019 | 2013-076E | Unknown[14] [15] | ~20 | ~20 | 0 | ||
May 8, 2020 | Fregat tank[16] | 2011-037B | Unknown, possibly explosion | 346 | 280 | 66 | |
July 12, 2020 | H2-A 202 Fairing | 2018-084C | Collision with untracked debris | 123 | 5 | 118 | |
March 18, 2021 | Yunhai-1 02 | 2019-063A | Accidental collision with a fragment from the Zenit-2 rocket body that launched Tselina-2 in 1996.[17] | 39 | 20 | 19 | |
November 15, 2021 | 1982-092A | ASAT (Anti-Satellite) weapon system test | 1787 | 394 | 1393 | ||
November 12, 2022 | Long March 6A upper stage | 2022-151B | Unknown; but may be related to upper stage passivization or insulation.[18] [19] [20] | 781 | 722 | 59 | |
November 17, 2022 | H2-A 202 Payload fairing | 2012-025F | Energetic fragmentation event; Cause unknown[21] | 50+ | 50+ | 0 | |
January 4, 2023 | 2014-028E | Unknown | 85 | 85 | 0 | ||
March 11, 2023 | Orbcomm F36 | 1999-065E | Unknown; likely energetic fragmentation event caused by a malfunction in the hydrazine orbit adjust system[22] [23] | 7 | 7 | 0 | |
August 21, 2023 | Vega VV02 VESPA adapter | 2013-021D | Unknown; likely debris impact[24] [25] | 7 | 7 | 0 | |
March 26, 2024 | Long March 6A upper stage | 2024-058B | Unknown; but may be related to upper stage passivization or insulation. | ~60 | ~60 | 0 | |
June 26, 2024 | 2013-030A | Unknown; but may be related to improper spacecraft passivization[26] [27] | 100+ | 100+ | 0 | ||
July 4, 2024 | Long March 6A upper stage | 2024-126C | Unknown; but may be related to upper stage passivization or insulation.[28] | ? | ? | 0 | |
August 6, 2024 | Long March 6A upper stage | 2024-140U | Unknown; but may be related to upper stage passivization or insulation. | 700–900+ | 700–900+ | 0 | |
September 6, 2024 | Atlas V Centaur upper stage | 2018-022B | Unknown; | 40+ | 40+ | 0 | |
October 19, 2024 | 2016-053B | Unknown; potential threat to all spacecraft in geostationary orbit, including the Russian satellites, Ekspress-AT1, Yamal-402, Ekspress-AM6 and Elektro-L;[29] | ~500 | ~500 | 0 |