Highlights from spaceflight in 2016.[a] | |
Orbital launches | |
---|---|
First | 15 January |
Last | 28 December |
Total | 85 |
Successes | 82 |
Failures | 2 |
Partial failures | 1 |
Catalogued | 83 |
Rockets | |
Maiden flights | |
Retirements | |
Crewed flights | |
Orbital | 5 |
Total travellers | 14 |
EVAs | 4 |
Several new rockets and spaceports began operations in 2016.
Russia inaugurated the far-EasternVostochny Cosmodrome on 28 April 2016 with a traditionalSoyuz-2.1a flight,[1] before expanding it for theAngara rocket family in the following years. The ChineseLong March 7 flew itsmaiden flight from the newWenchang Satellite Launch Center onHainan Island on 25 June, and the maiden flight of theLong March 5 took place on 3 November. Two years after its2014 accident, theAntares rocket returned to flight on 17 October with its upgraded230 version featuring the RussianRD-181 engine.
Aftermany failed attempts,SpaceX began landing itsFalcon 9 first stages onautonomous spaceport drone ships, edging closer to their long-stated goal ofdeveloping reusable launch vehicles. The company indicated that the recovered engines and structures did not suffer significant damage.[2] One of the landed boosters,B1021, launched in April 2016, was flown again in March 2017;[3] two others were converted to side boosters for the maiden flight ofFalcon Heavy.[4]
TheExoMars mission, a collaboration between the European and Russian space agencies, was launched on 14 March and reached Mars on 19 October.[5] Dedicated toastrobiology investigations, this flight carried theExoMars Trace Gas Orbiter, which reached Mars orbit, and theSchiaparelli EDM lander, which crashed upon landing. A subsequent flight scheduled for 2020 will carry the ExoMarsRosalind Franklin rover along withfour static surface instruments.[6] Meanwhile, the Japanese space probeAkatsuki started its observations ofVenus in May[7] after spending five months gradually adjusting its orbit. Planetary exploration activities took center stage with the orbit insertion of NASA'sJuno probe atJupiter on 4 July, followed by the launch of NASA'sOSIRIS-REx mission to asteroid101955 Bennu on 8 September. Finally, on 30 September, theRosetta probe executed a slow crash-landing on comet67P/Churyumov–Gerasimenko.[8][9]
Human spaceflights included the return ofScott Kelly andMikhail Kornienko in March after ayearlong mission on theISS, the longest-ever continuous stay by astronauts at the station. Kelly also set the record for the longest-duration stay of an American in orbit. Four ISS Expeditions numbered47 to50 were launched in 2016, the first one using the lastSoyuz TMA-M spacecraft and the next three inaugurating the modernizedSoyuz MS. Expedition 50 will continue into 2017. SeveralEVAs were performed to maintain the exterior of the ISS. The experimentalBEAM inflatable habitat was attached to the ISS on 16 April and expanded on 28 May to begin two years of on-orbit tests. Meanwhile, China launched its newTiangong-2 space laboratory in September, which was firstvisited by two astronauts for a month between 19 October and 17 November.
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload (⚀ =CubeSat) | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
15 January 03:00:00 | ![]() | ![]() | ![]() | ||||
![]() | TPU /Tohoku University /Tokai University /KU /JAXA | Suborbital | Ionospheric research | 15 January | Successful | ||
Apogee: 161 kilometres (100 mi)[80] | |||||||
22 January | ![]() | ![]() | ![]() | ||||
![]() | Blue Origin | Suborbital | Test flight | 22 January | Successful | ||
Apogee: 101.7 kilometres (63.2 mi)[81] | |||||||
23 January 08:30 | ![]() | ![]() | ![]() | ||||
![]() ![]() | DLR /ESA | Suborbital | Microgravity | 23 January | Successful | ||
Apogee: 252 kilometres (157 mi) | |||||||
28 January | ![]() | ![]() | ![]() | ||||
MDA | Suborbital | ABM target | 28 January | Successful | |||
Apogee: 300 kilometres (190 mi), CTV-02+ target | |||||||
28 January | ![]() | ![]() | ![]() | ||||
MDA | Suborbital | ABM test | 28 January | Successful | |||
CTV-02+, successful test flight, the CE-II kill vehicle performed scripted maneuvers to demonstrate performance of alternate divert thrusters. Upon entering terminal phase, the kill vehicle initiated a planned burn sequence to evaluate the alternate divert thrusters until fuel was exhausted, intentionally precluding an intercept. | |||||||
2 February 21:09 | ![]() | ![]() | ![]() | ||||
![]() | SSC | Suborbital | Technology | 2 February | Successful | ||
Apogee: 138 kilometres (86 mi) | |||||||
21 February 07:34 | ![]() | ![]() | ![]() | ||||
US Air Force | Suborbital | Test flight | 21 February | Successful | |||
GT217GM, Apogee: ~1,300 kilometres (810 mi) ? | |||||||
22 February 04:15 | ![]() | ![]() | ![]() | ||||
![]() | LASP | Suborbital | Astronomy | 22 February | Successful | ||
Apogee: 309 kilometres (192 mi) | |||||||
26 February 07:01 | ![]() | ![]() | ![]() | ||||
US Air Force | Suborbital | Test flight | 26 February | Successful | |||
GT218GM, Apogee: ~1,300 kilometres (810 mi) ? | |||||||
1 March 14:50 | ![]() | ![]() | ![]() | ||||
![]() | West Virginia University | Suborbital | Technology experiments | 1 March | Successful | ||
Apogee: ~185 kilometers (115 mi)[82] | |||||||
7 March 12:05 | ![]() | ![]() | ![]() | ||||
![]() | NASAAmes | Suborbital | Technology experiment | 7 March | Successful | ||
![]() | Montana State University | Suborbital | Technology experiment | 7 March | Successful | ||
![]() | Controlled Dynamics | Suborbital | Technology experiment | 7 March | Successful | ||
Apogee: ~159 kilometers (99 mi) | |||||||
7 March | ![]() | ![]() | ![]() | ||||
Indian Navy | Suborbital | Missile test | 7 March | Successful | |||
Apogee: 500 km? | |||||||
8 March | ![]() | ![]() | ![]() | ||||
IRGC | Suborbital | Missile test | 8 March | Successful | |||
Apogee: ~150 kilometres (93 mi) | |||||||
14 March | ![]() | ![]() | ![]() | ||||
IDRDL | Suborbital | Missile test | 14 March | Successful | |||
Apogee: ~500 kilometres (310 mi)? | |||||||
14 March | ![]() | ![]() | ![]() | ||||
US Navy | Suborbital | Missile test | 14 March | Successful | |||
Follow-on Commander's Evaluation Test 52 | |||||||
15 March | ![]() | ![]() | ![]() | ||||
US Navy | Suborbital | Missile test | 15 March | Successful | |||
Follow-on Commander's Evaluation Test 52 | |||||||
16 March | ![]() | ![]() | ![]() | ||||
US Navy | Suborbital | Missile test | 16 March | Successful | |||
Follow-on Commander's Evaluation Test 52 | |||||||
31 March | ![]() | ![]() | ![]() | ||||
Indian Navy | Suborbital | Missile test | 31 March | Successful | |||
First K-4 launch from a submarine[83] | |||||||
2 April 15:18 | ![]() | ![]() | ![]() | ||||
![]() | Blue Origin | Suborbital | Test flight | 2 April | Successful | ||
![]() | Southwest Research Institute | Suborbital | Microgravity experiment | 2 April | Successful | ||
![]() | University of Central Florida | Suborbital | Microgravity experiment | 2 April | Successful | ||
Apogee: 103.8 kilometers (64.5 mi). Third successful booster landing of the same rocket.[84] | |||||||
19 April 06:41 | ![]() | ![]() | ![]() | ||||
RVSN | Suborbital | Missile test | 19 April | Successful | |||
Yu-71 Hypersonic Vehicle Test, Apogee: 1,000 kilometres (620 mi)? | |||||||
26 April 17:00 | ![]() | ![]() | ![]() | ||||
![]() | CSSAR | Suborbital | Environment monitoring | 26 April | Successful | ||
Apogee: 316 kilometres (196 mi) | |||||||
18 May 00:45 | ![]() ![]() | ![]() | ![]() | ||||
![]() | DSTO | Suborbital | Technology | 18 May | Successful | ||
Apogee: 278 kilometres (173 mi) | |||||||
18 May 07:02 | ![]() | ![]() | ![]() | ||||
MDA | Suborbital | Radar target | 18 May | Successful | |||
Medium Range Ballistic Missile Target, Aegis radar target FTX-21, apogee: 300 kilometres (190 mi)? | |||||||
25 May | ![]() | ![]() | ![]() | ||||
US Navy | Suborbital | Test flight | 25 May | Successful | |||
Apogee: 100 kilometres (62 mi)? | |||||||
26 May | ![]() | ![]() | ![]() | ||||
US Navy | Suborbital | Test flight | 26 May | Successful | |||
Apogee: 100 kilometres (62 mi)? | |||||||
1 June 19:00 | ![]() | ![]() | ![]() | ||||
![]() | CU Boulder | Suborbital | SDO calibration | 1 June | Successful | ||
Apogee: 290 kilometres (180 mi) | |||||||
19 June 14:35 | ![]() | ![]() | ![]() | ||||
![]() | Blue Origin | Suborbital | Test flight | 19 June | Successful | ||
![]() | Purdue University School of Aeronautics and Astronautics | Suborbital | Microgravity experiment | 19 June | Successful | ||
![]() | Louisiana State University | Suborbital | Microgravity experiment | 19 June | Successful | ||
![]() | Braunschweig University of Technology | Suborbital | Microgravity experiment | 19 June | Successful | ||
Apogee: 101 kilometers (62.8 mi). Fourth successful booster landing of the same rocket. | |||||||
21 June[85] 23:03 | ![]() | ![]() | ![]() | ||||
![]() | Korean People's Army Strategic Force | Suborbital | Missile test | 21 June | Successful | ||
Apogee: 1,400 kilometres (870 mi). | |||||||
24 June 10:06 | ![]() | ![]() | ![]() | ||||
![]() | CU Boulder | Suborbital | Student experiments | 24 June | Successful | ||
Apogee: ~119 kilometres (74 mi) | |||||||
30 June 09:43 | ![]() | ![]() | ![]() | ||||
![]() | Oslo/Andøya | Suborbital | Atmospheric Science | 30 June | Successful | ||
Apogee: 115 kilometres (71 mi) | |||||||
? June | ![]() | ![]() | ![]() | ||||
Royal Navy | Suborbital | Missile test | ? June | Launch failure | |||
– | |||||||
1 July 07:18 | ![]() | ![]() | ![]() | ||||
DGA/Marine nationale | Suborbital | Test flight | 1 July | Successful | |||
Apogee: 1,000 kilometres (620 mi)? | |||||||
8 July 13:01 | ![]() | ![]() | ![]() | ||||
![]() | Oslo/Andøya | Suborbital | Atmospheric Science | 8 July | Successful | ||
Apogee: 117 kilometres (73 mi) | |||||||
11 July | ![]() | ![]() | ![]() | ||||
AFIRI | Suborbital | Missile test | 11 July | Launch failure | |||
19 July 04:05 | ![]() | ![]() | ![]() | ||||
![]() | DLR | Suborbital | Technology | 19 July | Successful | ||
Apogee: 182 kilometres (113 mi) | |||||||
27 July 18:26 | ![]() | ![]() | ![]() | ||||
![]() | NASA/MSFC | Suborbital | Solar research | 27 July | Spacecraft failure | ||
Apogee: 250 kilometres (160 mi) | |||||||
17 August 11:33 | ![]() | ![]() | ![]() | ||||
![]() | University of Colorado Boulder | Suborbital | Student Research | 17 August | Successful | ||
Apogee: ~153 kilometres (95 mi) | |||||||
23 August[85] 20:29 | ![]() | ![]() | ![]() | ||||
![]() | Korean People's Army Strategic Force | Suborbital | Missile test | 23 August | Successful | ||
Apogee: about 550 kilometres (340 mi), according to South Korean military. | |||||||
25 August | ![]() | ![]() | ![]() | ||||
RVSN | Suborbital | Missile test | 25 August | Launch failure | |||
31 August | ![]() | ![]() | ![]() | ||||
US Navy | Suborbital | Missile test | 31 August | Successful | |||
5 September[85] 03:13 | ![]() | ![]() | ![]() | ||||
![]() | Korean People's Army Strategic Force | Suborbital | Missile test | 5 September | Successful | ||
Apogee: about 200 kilometres (120 mi).[86] 1 of 3. | |||||||
5 September[85] 03:13 | ![]() | ![]() | ![]() | ||||
![]() | Korean People's Army Strategic Force | Suborbital | Missile test | 5 September | Successful | ||
Apogee: about 200 kilometres (120 mi).[86] 2 of 3. | |||||||
5 September[85] 03:13 | ![]() | ![]() | ![]() | ||||
![]() | Korean People's Army Strategic Force | Suborbital | Missile test | 5 September | Successful | ||
Apogee: about 200 kilometres (120 mi).[86] 3 of 3. | |||||||
5 September 09:10 | ![]() | ![]() | ![]() | ||||
US Air Force | Suborbital | Test flight | 5 September | Successful | |||
GT219GM, Apogee: ~1,300 kilometres (810 mi) ? | |||||||
9 September | ![]() | ![]() | ![]() | ||||
RVSN | Suborbital | Missile test | 9 September | Successful | |||
27 September | ![]() | ![]() | ![]() | ||||
VMF | Suborbital | Missile test | 27 September | Successful | |||
27 September | ![]() | ![]() | ![]() | ||||
VMF | Suborbital | Missile test | 27 September | Launch failure? | |||
The second missile self destroyed "after completing the first phase of the flight", maybe intentional. It appears to be a normal practice in salvo launches. The missile probably carried mockups instead of working upper stages and warheads to save money. | |||||||
5 October 15:37 | ![]() | ![]() | ![]() | ||||
![]() | Blue Origin | Suborbital | Test flight | 5 October | Successful | ||
In-flight escape test 45 seconds after launch. Booster unexpectedly survived and reached an apogee of 93.7 kilometres (58.2 mi) before completing its fifth successful landing. | |||||||
12 October | ![]() | ![]() | ![]() | ||||
VMF | Suborbital | Missile test | 12 October | Successful | |||
12 October | ![]() | ![]() | ![]() | ||||
VMF | Suborbital | Missile test | 12 October | Successful | |||
12 October | ![]() | ![]() | ![]() | ||||
RVSN | Suborbital | Missile test | 12 October | Successful | |||
25 October 08:58 | ![]() | ![]() | ![]() | ||||
RVSN | Suborbital | Missile test | 25 October | Successful | |||
Yu-71 Hypersonic Vehicle Test, Apogee: 1,000 kilometres (620 mi)? | |||||||
22 November | ![]() | ![]() | ![]() | ||||
IDRDL | Suborbital | Missile test | 22 November | Successful | |||
Apogee: ~500 kilometres (310 mi)? | |||||||
6 December | ![]() | ![]() | ![]() | ||||
IRGC | Suborbital | Missile test | 6 December | Successful | |||
Apogee: ~150 kilometres (93 mi) | |||||||
8 December | ![]() | ![]() | ![]() | ||||
PLA | Suborbital | ABM target | 8 December | Successful | |||
Target | |||||||
8 December | ![]() | ![]() | ![]() | ||||
PLA | Suborbital | ABM test | 8 December | Successful | |||
Interceptor | |||||||
15 December | ![]() | FTM-27 | ![]() | ![]() | |||
MDA | Suborbital | ABM target | 15 December | Successful | |||
FTM-27 target, successfully intercepted by two SM-6 missiles in low altitude | |||||||
15 December 16:15 | ![]() | Zombie Pathfinder | ![]() | ![]() | |||
US Army | Suborbital | Test flight | 15 December | Successful | |||
Apogee: 80 kilometres (50 mi)? | |||||||
26 December 05:35 | ![]() | ![]() | ![]() | ||||
DRDO | Suborbital | Missile test | 26 December | Successful | |||
Apogee: ~800 kilometres (500 mi) |
Date (UTC) | Spacecraft | Event | Remarks |
---|---|---|---|
14 January | Mars Express | Flyby ofPhobos | Closest approach: 53 kilometres (33 mi).[87] |
15 January[88] | Cassini | 116th flyby ofTitan | Closest approach: 3,817 kilometres (2,372 mi). |
31 January | Cassini | 117th flyby of Titan | Closest approach: 1,400 kilometres (870 mi). |
16 February | Cassini | 118th flyby of Titan | Closest approach: 1,018 kilometres (633 mi). |
4 April | Cassini | 119th flyby of Titan | Closest approach: 990 kilometres (615 mi). |
6 May | Cassini | 120th flyby of Titan | Closest approach: 971 kilometres (603 mi). |
7 June | Cassini | 121st flyby of Titan | Closest approach: 975 kilometres (606 mi). |
4 July[89] | Juno | Orbit injection aroundJupiter (jovicentric) | First solar-powered Jovian probe, second orbiter. |
4 July | Mars Express | Flyby of Phobos | Closest approach: 350 kilometres (220 mi). |
25 July | Cassini | 122nd flyby of Titan | Closest approach: 976 kilometres (606 mi). |
10 August | Cassini | 123rd flyby of Titan | Closest approach: 1,599 kilometres (994 mi). |
27 August | Juno | 1stperijove of Jupiter | Closest approach: 2,600 kilometres (1,600 mi).[90] |
26 September | Cassini | 124th flyby of Titan | Closest approach: 1,737 kilometres (1,079 mi). |
30 September | Rosetta | Landing on67P/Churyumov–Gerasimenko | Probe was programmed to deactivate its thrusters and radio transmissions after landing. |
19 October | Trace Gas Orbiter (ExoMars 2016) | Orbit injection aroundMars (areocentric) | |
19 October | Schiaparelli (ExoMars 2016) | Landing onMars,Meridiani Planum | Probe entered Martian atmosphere intact, but contact was lost 50 seconds before expected landing.[91] NASA'sMRO later identified the Schiaparelli crash site at coordinates2°03′S6°14′W / 2.05°S 6.24°W /-2.05; -6.24, confirming the loss of the lander.[92] |
19 October | Juno | 2nd perijove | Period Reduction Maneuver[93] originally planned, but delayed due to valve issues.[94] The maneuver was later cancelled entirely in favor of remaining in a 53-day orbit.[95] |
13 November | Cassini | 125th flyby of Titan | Closest approach: 1,582 kilometres (983 mi). |
16 November | Mars Express | Flyby of Phobos | Closest approach: 127 kilometres (79 mi). |
29 November | Cassini | 126th flyby of Titan | Closest approach: 3,223 kilometres (2,003 mi). |
11 December | Juno | 3rd perijove |
Start date/time | Duration | End time | Spacecraft | Crew | Remarks |
---|---|---|---|---|---|
15 January 13:48 | 4 hours43 minutes | 18:31 | Expedition 46 ISSQuest | Replaced a failed voltage regulator responsible for shutting down one of the station's eight power channels in November 2015, and routed cables in support of the installation of theInternational Docking Adaptor. EVA terminated two hours early due to water leakage in Kopra's helmet, but the primary task was accomplished.[96] | |
3 February 12:55 | 4 hours45 minutes | 17:40 | Expedition 46 ISSPirs | Deployed a commemorative flash drive, took samples of module exteriors, installed handrails for use in future EVAs, retrieved an astrobiology experiment, deployed a materials science experiment, and tested a tool for applying coatings to module exteriors.[97] | |
19 August 12:04 | 5 hours58 minutes | 18:02 | Expedition 48 ISSQuest | The astronauts installed theInternational Docking Adapter (IDA) which was delivered byDragon CRS-9, allowing futurecommercial crew spacecraft to dock with the station. This first IDA was attached toHarmony's forward port, over the existingPressurized Mating Adapter (PMA).[98][99] The EVA terminated after completing the primary objective, without completing the secondary objectives, due to a malfunction of the right earphone of Jeff Williams. | |
1 September 11:53 | 6 hours48 minutes | 18:41 | Expedition 48 ISSQuest | The crew retracted a thermal radiator which is a backup, and then installed the first pair of several high-definition cameras to monitor the traffic around the station. Then they have performed some maintenance operations.[100] |
Date/Time (UTC) | Source object | Event type | Pieces tracked | Remarks |
---|---|---|---|---|
26 March 01:42[101] | Hitomi | Satellite breakup | 10[102] | JAXA lost communications with the freshly launched telescope during its early commissioning phase. Meanwhile,JspOC observed 5 then 10 pieces of debris diverging from the satellite, one of them comparably sized to the main spacecraft by radar signature.[103] Hitomi itself went into a tumble and sent short intermittent communications. The tumble was caused by a failure of the inertial reference unit mistakenly reporting the spacecraft to be spinning. As the attitude control system attempted to correct the non-existent spin, the unnecessary correction itself is believed to have caused the subsuqent failures, ultimately leading to the loss of the spacecraft, 28 April.[104][105][16] In a twist of fate, one of the secondary payloads traveling with Hitomi wasChubuSat-3, a microsatellite dedicated to monitoring global warming effects and space debris.[106] |
1 June 09:20[107] | SL-12 R/B (#33473) | Booster breakup | 20+[107] | Anullage motor, part of a RussianProton-M rocket that was launched in December 2008, exploded for unknown reasons.[108] |
For the purposes of this section, the yearly tally of orbital launches by country assigns each flight to the country of origin of the rocket, not to the launch services provider or the spaceport. For example,Soyuz launches by Arianespace in Kourou are counted under Russia becauseSoyuz-2 is a Russian rocket.
Country | Launches | Successes | Failures | Partial failures | Remarks | |
---|---|---|---|---|---|---|
![]() | 22 | 20 | 1 | 1 | ||
![]() | 7 | 7 | 0 | 0 | ||
![]() | 2 | 2 | 0 | 0 | ||
![]() | 7 | 7 | 0 | 0 | ||
![]() | 1 | 1 | 0 | 0 | ||
![]() | 4 | 4 | 0 | 0 | ||
![]() | 1 | 1 | 0 | 0 | ||
![]() | 19 | 18 | 1 | 0 | Includes twoEuropean Soyuz launches fromKourou,French Guiana byArianespace | |
![]() | 22 | 22 | 0 | 0 | +1 pre-launch failure (AMOS 6 / Falcon 9) | |
World | 85 | 82 | 2 | 1 |
Family | Country | Launches | Successes | Failures | Partial failures | Remarks |
---|---|---|---|---|---|---|
Antares | ![]() | 1 | 1 | 0 | 0 | |
Ariane | ![]() | 7 | 7 | 0 | 0 | |
Atlas | ![]() | 8 | 8 | 0 | 0 | |
Delta | ![]() | 4 | 4 | 0 | 0 | |
Epsilon | ![]() | 1 | 1 | 0 | 0 | |
Falcon | ![]() | 8 | 8 | 0 | 0 | 1 Pre-launch failure |
GSLV | ![]() | 1 | 1 | 0 | 0 | |
H-II | ![]() | 3 | 3 | 0 | 0 | |
Long March | ![]() | 22 | 20 | 1 | 1 | |
Pegasus | ![]() | 1 | 1 | 0 | 0 | |
PSLV | ![]() | 6 | 6 | 0 | 0 | |
R-7 | ![]() | 14 | 13 | 1 | 0 | |
Shavit | ![]() | 1 | 1 | 0 | 0 | |
Unha | ![]() | 1 | 1 | 0 | 0 | |
Universal Rocket | ![]() | 5 | 5 | 0 | 0 | |
Vega | ![]() | 2 | 2 | 0 | 0 |
Rocket | Country | Family | Launches | Successes | Failures | Partial failures | Remarks |
---|---|---|---|---|---|---|---|
Antares 200 | ![]() | Antares | 1 | 1 | 0 | 0 | Maiden Flight |
Ariane 5 | ![]() | Ariane | 7 | 7 | 0 | 0 | |
Atlas V | ![]() | Atlas | 8 | 8 | 0 | 0 | |
Delta IV | ![]() | Delta | 4 | 4 | 0 | 0 | |
Epsilon | ![]() | Epsilon | 1 | 1 | 0 | 0 | |
Falcon 9 | ![]() | Falcon | 8 | 8 | 0 | 0 | 1 Pre-launch failure |
GSLV | ![]() | GSLV | 1 | 1 | 0 | 0 | |
H-IIA | ![]() | H-II | 2 | 2 | 0 | 0 | |
H-IIB | ![]() | H-II | 1 | 1 | 0 | 0 | |
Long March 2 | ![]() | Long March | 8 | 7 | 0 | 1 | |
Long March 3 | ![]() | Long March | 7 | 7 | 0 | 0 | |
Long March 4 | ![]() | Long March | 4 | 3 | 1 | 0 | |
Long March 5 | ![]() | Long March | 1 | 1 | 0 | 0 | Maiden flight |
Long March 7 | ![]() | Long March | 1 | 1 | 0 | 0 | Maiden flight |
Long March 11 | ![]() | Long March | 1 | 1 | 0 | 0 | |
Pegasus XL | ![]() | Pegasus | 1 | 1 | 0 | 0 | |
Proton | ![]() | Universal Rocket | 3 | 3 | 0 | 0 | |
PSLV | ![]() | PSLV | 6 | 6 | 0 | 0 | |
Shavit | ![]() | Shavit | 1 | 1 | 0 | 0 | |
Soyuz | ![]() | R-7 | 6 | 5 | 1 | 0 | |
Soyuz-2 | ![]() | R-7 | 8 | 8 | 0 | 0 | |
Unha | ![]() | Unha | 1 | 1 | 0 | 0 | |
UR-100 | ![]() | Universal Rocket | 2 | 2 | 0 | 0 | |
Vega | ![]() | Vega | 2 | 2 | 0 | 0 |
Rocket | Country | Type | Launches | Successes | Failures | Partial failures | Remarks |
---|---|---|---|---|---|---|---|
Antares 230 | ![]() | Antares 200 | 1 | 1 | 0 | 0 | Maiden Flight |
Ariane 5 ECA | ![]() | Ariane 5 | 6 | 6 | 0 | 0 | |
Ariane 5 ES | ![]() | Ariane 5 | 1 | 1 | 0 | 0 | |
Atlas V 401 | ![]() | Atlas V | 3 | 3 | 0 | 0 | |
Atlas V 411 | ![]() | Atlas V | 1 | 1 | 0 | 0 | |
Atlas V 421 | ![]() | Atlas V | 1 | 1 | 0 | 0 | |
Atlas V 431 | ![]() | Atlas V | 1 | 1 | 0 | 0 | Final flight |
Atlas V 541 | ![]() | Atlas V | 1 | 1 | 0 | 0 | |
Atlas V 551 | ![]() | Atlas V | 1 | 1 | 0 | 0 | |
Delta IV Medium+ (4,2) | ![]() | Delta IV | 1 | 1 | 0 | 0 | |
Delta IV Medium+ (5,2) | ![]() | Delta IV | 1 | 1 | 0 | 0 | |
Delta IV Medium+ (5,4) | ![]() | Delta IV | 1 | 1 | 0 | 0 | |
Delta IV Heavy | ![]() | Delta IV | 1 | 1 | 0 | 0 | |
Epsilon | ![]() | Epsilon | 1 | 1 | 0 | 0 | |
Falcon 9 v1.1 | ![]() | Falcon 9 | 1 | 1 | 0 | 0 | Final flight |
Falcon 9 Full Thrust | ![]() | Falcon 9 | 7 | 7 | 0 | 0 | 1 Pre-launch failure |
GSLV Mk II | ![]() | GSLV | 1 | 1 | 0 | 0 | |
H-IIA 202 | ![]() | H-IIA | 2 | 2 | 0 | 0 | |
H-IIB | ![]() | H-IIB | 1 | 1 | 0 | 0 | |
Long March 2D | ![]() | Long March 2 | 6 | 5 | 0 | 1 | |
Long March 2F/G | ![]() | Long March 2 | 2 | 2 | 0 | 0 | |
Long March 3A | ![]() | Long March 3 | 1 | 1 | 0 | 0 | |
Long March 3B/E | ![]() | Long March 3 | 3 | 3 | 0 | 0 | |
Long March 3C/E | ![]() | Long March 3 | 2 | 2 | 0 | 0 | |
Long March 3C/E /YZ-1 | ![]() | Long March 3 | 1 | 1 | 0 | 0 | |
Long March 4B | ![]() | Long March 4 | 2 | 2 | 0 | 0 | |
Long March 4C | ![]() | Long March 4 | 2 | 1 | 1 | 0 | |
Long March 5 /YZ-2 | ![]() | Long March 5 | 1 | 1 | 0 | 0 | Maiden flight |
Long March 7 /YZ-1A | ![]() | Long March 7 | 1 | 1 | 0 | 0 | Maiden flight |
Long March 11 | ![]() | Long March 11 | 1 | 1 | 0 | 0 | |
Pegasus XL | ![]() | Pegasus XL | 1 | 1 | 0 | 0 | |
Proton-M /Briz-M | ![]() | Proton | 3 | 3 | 0 | 0 | |
PSLV-G | ![]() | PSLV | 1 | 1 | 0 | 0 | |
PSLV-XL | ![]() | PSLV | 5 | 5 | 0 | 0 | |
Rokot /Briz-KM | ![]() | UR-100 | 2 | 2 | 0 | 0 | |
Shavit-2 | ![]() | Shavit | 1 | 1 | 0 | 0 | |
Soyuz-2.1a or ST-A | ![]() | Soyuz-2 | 2 | 2 | 0 | 0 | |
Soyuz-2.1a or ST-A /Fregat-M | ![]() | Soyuz-2 | 1 | 1 | 0 | 0 | |
Soyuz-2.1a /Volga | ![]() | Soyuz-2 | 1 | 1 | 0 | 0 | Maiden flight |
Soyuz-2.1b or ST-B | ![]() | Soyuz-2 | 1 | 1 | 0 | 0 | |
Soyuz-2.1b or ST-B /Fregat-M | ![]() | Soyuz-2 | 2 | 2 | 0 | 0 | |
Soyuz-2.1b or ST-B /Fregat-MT | ![]() | Soyuz-2 | 1 | 1 | 0 | 0 | |
Soyuz-FG | ![]() | Soyuz | 4 | 4 | 0 | 0 | |
Soyuz-U | ![]() | Soyuz | 2 | 1 | 1 | 0 | |
Unha-3 | ![]() | Unha | 1 | 1 | 0 | 0 | |
Vega | ![]() | Vega | 2 | 2 | 0 | 0 |
Site | Country | Launches | Successes | Failures | Partial failures | Remarks |
---|---|---|---|---|---|---|
Baikonur | ![]() | 11 | 10 | 1 | 0 | |
Cape Canaveral | ![]() | 18 | 18 | 0 | 0 | 1 Pre-launch failure |
Jiuquan | ![]() | 9 | 9 | 0 | 0 | |
Kourou | ![]() | 11 | 11 | 0 | 0 | |
MARS | ![]() | 1 | 1 | 0 | 0 | |
Palmachim | ![]() | 1 | 1 | 0 | 0 | |
Plesetsk | ![]() | 5 | 5 | 0 | 0 | |
Satish Dhawan | ![]() | 7 | 7 | 0 | 0 | |
Sohae | ![]() | 1 | 1 | 0 | 0 | |
Taiyuan | ![]() | 4 | 2 | 1 | 1 | |
Tanegashima | ![]() | 3 | 3 | 0 | 0 | |
Uchinoura | ![]() | 1 | 1 | 0 | 0 | |
Vandenberg | ![]() | 3 | 3 | 0 | 0 | |
Vostochny | ![]() | 1 | 1 | 0 | 0 | First launch |
Wenchang | ![]() | 2 | 2 | 0 | 0 | First launch |
Xichang | ![]() | 7 | 7 | 0 | 0 | |
Total | 85 | 82 | 2 | 1 |
Orbital regime | Launches | Achieved | Not achieved | Accidentally achieved | Remarks |
---|---|---|---|---|---|
Transatmospheric | 0 | 0 | 0 | 0 | |
Low Earth | 43 | 42 | 2 | 0 | Including 11 to ISS (+1 failed), 1 to Tiangong-2 |
Geosynchronous /transfer | 32 | 32 | 0 | 0 | |
Medium Earth | 8 | 8 | 0 | 0 | |
High Earth | 0 | 0 | 0 | 0 | |
Heliocentric orbit | 2 | 2 | 0 | 0 | Including planetarytransfer orbits |
Total | 85 | 83 | 2 | 0 |
Notes
Citations