View source for Engineering:Long March 2C

{{Short description|Version of the Long March 2}}
<!--{{Launching/Long March|type=rocket}}-->
{{Infobox Rocket
| name           = Long March 2C
| image          = CZ-2C rendering.jpg
| caption        = Rendering of Long March 2C

| function       = [[Engineering:Launch vehicle|Launch vehicle]]
| manufacturer   = [[Organization:China Academy of Launch Vehicle Technology|CALT]]
| country-origin = {{wipe|China}}
| height         = {{cvt|42|m}} <ref name="cgwic.com">{{cite web|url=http://cgwic.com/Launchservice/LM2C.html|title=LM-2C|publisher=China Great Wall Industry Corporation|access-date=9 August 2015}}</ref>
| diameter       = {{cvt|3.35|m}} <ref name="cgwic.com"/>
| mass           = {{cvt|233000|kg}}
| stages         = 2

| capacities     = {{Infobox Rocket/Payload
  | location     = [[Astronomy:Low Earth orbit|Low Earth orbit]]
  | kilos        = {{cvt|3850|kg}}
  }}

{{Infobox Rocket/Payload
  | location     = [[Astronomy:Sun-synchronous orbit|Sun-synchronous orbit]]
  | kilos        = '''2C:''' {{cvt|1400|kg}}<br/>'''2C/SMA:''' {{cvt|1900|kg}}
  }}

{{Infobox Rocket/Payload
  | location     = [[Astronomy:Geostationary transfer orbit|GTO]]
  | kilos        = '''2C/SM:''' {{cvt|1250|kg}}
  }}

| family         = [[Engineering:Long March (rocket family)|Long March]]
| derivatives    = 
| status         = Active
| sites          = LA-2/138 and<br/>LA-4/SLS-2, JSLC<br/>LA-7 and LA-9, TSLC<br/>LA-3, XSLC
| launches       = 75
| success        = 74
| fail           = 1
| partial        = 
| first          = 9 September 1982
| last           = 9 January 2024

| stagedata      = {{Infobox rocket/Stage
  | type         = stage
  | stageno      = First
  | name         = 
  | length       = 25.72 m
  | diameter     = 3.35 m
  | empty        = 
  | gross        = 
  | propmass     = {{cvt|162706|kg}}
  | engines      = 4 YF-21C
  | thrust       = {{cvt|2961.6|kN}}
  | burntime     = 
  | SI           = {{cvt|2556.5|m/s}}
  | fuel         = [[Chemistry:Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] / UDMH
  }}

  {{Infobox rocket/Stage
  | type         = stage
  | stageno      = Second
  | name         = 
  | length       = 7.757 m
  | diameter     = 3.35 m
  | empty        = 
  | gross        = 
  | propmass     = {{cvt|54667|kg}}
  | engines      = 1 YF-24E<br/>(1 x YF-22E (Main))<br/>(4 x YF-23C (Vernier))
  | thrust       = {{cvt|741.4|kN}} (Main)<br/>{{cvt|47.1|kN}} (Vernier)
  | burntime     = 
  | SI           = {{cvt|2922.37|m/s}} (Main)<br/>{{cvt|2834.11|m/s}} (Vernier)
  | fuel         = [[Chemistry:Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] / UDMH
  }}

{{Infobox rocket/Stage
  | type         = stage
  | stageno      = Third
  | name         = (optional)
  | length       = 1.5 m
  | diameter     = 2.7 m
  | empty        = 
  | gross        = 
  | propmass     = {{cvt|125|kg}}
  | engines      = 1 solid
  | thrust       = {{cvt|10.78|kN}}
  | burntime     = 
  | SI           = {{cvt|2804|m/s}}
  | fuel         = HTPB
  }}
}}

The '''Long March 2C''' (LM-2C), also known as the '''Chang Zheng 2C''' (CZ-2C), is a Chinese [[Physics:Orbit|orbit]]al [[Engineering:Launch vehicle|launch vehicle]], part of the Long March 2 rocket family. Developed and manufactured by the [[Organization:China Academy of Launch Vehicle Technology|China Academy of Launch Vehicle Technology]] (CALT),<ref name="bryce-2020">{{cite web|url=https://docs.google.com/gview?url=https://brycetech.com/reports/report-documents/China_Orbital_Launch_Activity_2020.pdf|title=China's Orbital Launch Activity 2020|publisher=Bryce Space and Technology|date=27 May 2020|access-date=22 June 2020}}</ref> the Long March 2C made its first launch on 9 September 1982. It is a two-stage launch vehicle with storable propellants, consisting of Nitrogen Tetroxide and [[Chemistry:Unsymmetrical dimethylhydrazine|Unsymmetrical Dimethylhydrazine]]. The launch vehicle was derived from the DF-5 ICBM.<ref name="bryce-2020"/>

Several variants of this launch vehicle have been built, all using an optional third solid motor stage:<ref>{{cite web|title=Chang Zheng-2C (Long March-2C)|url=http://sinodefence.com/rocketry/cz2c/ |publisher=SinoDefence|access-date=9 August 2015|url-status=dead|archive-url=https://web.archive.org/web/20150706002847/http://sinodefence.com/rocketry/cz2c/|archive-date=6 July 2015}}</ref>

* 2C/SD: Commercial satellite launcher with a multi-satellite smart dispenser allowing delivery of two satellites simultaneously
* 2C/SM: Version for delivery of small satellites to high orbits
* 2C/SMA: Improved version of the 2C/SM

According to the website ''Gunter's Space Page'',<ref name=Gunters>{{cite web|url=http://space.skyrocket.de/doc_lau/cz-2.htm|title=CZ-2 (Chang Zheng-2)|publisher=Gunter's Space Page|author=Gunter Dirk Krebs|access-date=17 February 2020}}</ref> in addition to the launches listed in the following table, there may have been six additional CZ-2C launches during 2014 and 2015. These possible launches apparently were conducted at the Taiyuan Satellite Launch Center on the following dates: 9 January 2014, 7 August 2014, 2 December 2014, 7 June 2015, 20 August 2015, and 23 November 2015; five of these six launches were apparently successful, while the launch on 7 August 2014 appears to have failed. However, due to the lack of additional sources for these six launches, they are not currently included in the following launch list.

Aerodynamic [[Engineering:Grid fin|grid fin]]s were added on the Long March 2C in 2019 to help guide falling stages away from populated areas. China is studying using reusable rocket technology in the future.<ref name=sfn-20200610>{{cite news|url=https://spaceflightnow.com/2020/06/10/china-launches-ocean-monitoring-satellite/|title=China launches ocean monitoring satellite|last=Clark|first=Stephen|publisher=Spaceflight Now|date=10 June 2020|access-date=12 June 2020}}</ref> A fairing recovery system through parachutes has been tested during the Yaogan 30-09 and Yaogan 30-10 launches in order to improve control of debris landing inland on potentially populated areas.<ref name="Yaogan3010">{{cite web|last=Navin|first=Joseph|url=https://www.nasaspaceflight.com/2021/07/china-fairing-recovery-long-march-2c/|title=China tests fairing recovery technologies on Long March 2C launch with four satellites|publisher=NASASpaceFlight.com|date=18 July 2021|access-date=19 July 2021}}</ref>

== List of launches ==
{{main|Engineering:List of Long March launches}}

{| class="wikitable" <!--border="2" cellpadding="4" cellspacing="0" style="margin: 0.5em 0em 0.5em 0; background: #f9f9f9; border: 1px #aaa solid; border-collapse: collapse; font-size: 95%;"-->
|----- style="background:#FFDEAD;"
! Flight number
! Serial number
! Date (UTC)
! Launch site
! Upper stage (if used)
! Payload
! Orbit
! Result
|-

| 1
| Y1
| 9 September 1982<br/>07:19
| LA-2/138, JSLC
| 
| [[Engineering:Fanhui Shi Weixing-0|FSW-0 No.4]]
| [[Astronomy:Low Earth orbit|LEO]]
| {{Success}}
|-

|2
|Y2
|19 August 1983<br/>06:00
|LA-2/138, JSLC
|
|FSW-0 No.5
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|3
|Y3
|12 September 1984<br/>05:44
|LA-2/138, JSLC
|
|[[Engineering:Fanhui Shi Weixing-0|FSW-0 No.6]]
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|4
|Y4
|21 October 1985<br/>05:04
|LA-2/138, JSLC
|
|[[Engineering:Fanhui Shi Weixing-0|FSW-0 No.7]]
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|5
|Y5
|6 October 1986<br/>05:40
|LA-2/138, JSLC
|
|[[Engineering:Fanhui Shi Weixing-0|FSW-0 No.8]]
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|6
|Y6
|5 August 1987<br/>06:39
|LA-2/138, JSLC
|
|[[Engineering:Fanhui Shi Weixing-0|FSW-0 No.9]]
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|7
|Y7
|9 September 1987<br/>07:15
|LA-2/138, JSLC
|
|FSW-1 No.1
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|8
|Y8
|5 August 1988<br/>07:29
|LA-2/138, JSLC
|
|FSW-1 No.2
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|9
|Y9
|5 October 1990<br/>06:14
|LA-2/138, JSLC
|
|FSW-1 No.3
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|10
|Y10
|6 October 1992<br/>06:20
|LA-2/138, JSLC
|
|FSW-1 No.4<br/>[[Engineering:Freja (satellite)|Freja]]
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|11
|Y11
|8 October 1993<br/>08:00
|LA-2/138, JSLC
|
|FSW-1 No.5
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|12
|2CFP-Y1
|1 September 1997<br/>14:00
|LA-7, TSLC
|2C/SD
|Iridium mass simulator A<br />Iridium mass simulator B
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|13
|2CFP-Y2
|8 December 1997<br/>07:16
|LA-7, TSLC
|2C/SD
|Iridium 42<br/>Iridium 44
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|14
|2CFP-Y3
|25 March 1998<br/>17:01
|LA-7, TSLC
|2C/SD
|Iridium 51<br/>Iridium 61
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|15
|2CFP-Y4
|2 May 1998<br/>09:16
|LA-7, TSLC
|2C/SD
|Iridium 69<br/>Iridium 71
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|16
|2CFP-Y5
|19 August 1998<br/>23:01
|LA-7, TSLC
|2C/SD
|Iridium 76<br/>Iridium 78
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|17
|2CFP-Y6
|19 December 1998<br/>11:39
|LA-7, TSLC
|2C/SD
|Iridium 88<br/>Iridium 89
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|18
|2CFP-Y7
|11 June 1999<br/>17:15
|LA-7, TSLC
|2C/SD
|Iridium 92<br/>Iridium 93
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|19
|2CSM-Y1
|29 December 2003<br/>19:06
|LA-3, XSLC
|2C/SM
|[[Engineering:Double Star (satellite)|Double Star 1]]
|[[Astronomy:High Earth orbit|HEO]]
|{{Success}}
|-
|20
|Y14
|18 April 2004<br/>15:59
|LA-3, XSLC
|
|[[Engineering:Shiyan (satellite)|Shiyan 1]]<br/>Nano Satellite 1
|SSO
|{{Success}}
|-
|21
|2CSM-Y2
|25 July 2004<br/>07:05
|LA-7, TSLC
|2C/SM
|[[Engineering:Double Star (satellite)|Double Star 2]]
|[[Astronomy:High Earth orbit|HEO]]
|{{Success}}
|-
|22
|Y12
|29 August 2004<br/>07:50
|LA-4/SLS-2, JSLC
|
|FSW-4 No.1
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|23
|Y15
|18 November 2004<br/>10:45
|LA-3, XSLC
|
|[[Engineering:Shiyan (satellite)|Shiyan 2]]
|SSO
|{{Success}}
|-
|24
|Y13
|2 August 2005<br/>07:30
|LA-4/SLS-2, JSLC
|
|FSW-4 No.2
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|25
|Y16
|9 September 2006<br/>07:00
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 8]]
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|26
|Y18
|11 April 2007<br/>03:27
|LA-7, TSLC
|
|[[Earth:HY (satellite)|HaiYang-1B]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|27
|2CSMA-Y1
|6 September 2008<br/>03:25
|LA-7, TSLC
|2C/SMA
|Huanjing-1A<br/>Huanjing-1B
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|28
|Y19
|22 April 2009<br/>02:55
|LA-7, TSLC
|
|[[Engineering:Yaogan|Yaogan 6]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|29
|Y21
|12 November 2009<br/>02:45
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 11-01]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|30
|Y25
|6 July 2011<br/>04:28
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 11-03]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|31
|Y24
|29 July 2011<br/>07:42
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 11-02]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|32
|Y26
|18 August 2011<br/>09:28
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 11-04]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Failure|Failure}}
|-
|33
|Y20
|29 November 2011<br/>18:50
|LA-9, TSLC
|
|[[Engineering:Yaogan|Yaogan 13]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|34
|2CSMA-Y2
|14 October 2012<br/>03:25
|LA-9, TSLC
|2C/SMA
|[[Engineering:Shijian|Shijian 9A]]<br/>[[Engineering:Shijian|Shijian 9B]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|35
|Y17
|18 November 2012<br/>22:53
|LA-9, TSLC
|
|Huanjing-1C<br/>Xinyan 1<br/>Fengniao 1
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|36
|Y23
|15 July 2013<br/>09:27
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 11-05]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|37
|Y28
|29 October 2013<br/>02:50
|LA-9, TSLC
|
|[[Engineering:Yaogan|Yaogan 18]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|38
|Y27
|31 March 2014<br/>02:46
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 11-06]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|39
|Y31
|28 September 2014<br/>05:13
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 11-07]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|40
|Y32
|27 October 2014<br/>06:59
|LA-4/SLS-2, JSLC
|
|[[Engineering:Shijian|Shijian 11-08]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|41
|Y35
|14 November 2014<br/>18:53
|LA-9, TSLC
|
|[[Engineering:Yaogan|Yaogan 23]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|42
|Y29
|29 September 2017<br/>04:21
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-01]] A/B/C
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|43
|Y33
|24 November 2017<br/>18:10
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-02]] A/B/C
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|44
|Y34
|25 December 2017<br/>19:44
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-03]] A/B/C
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|45
|Y36
|25 January 2018<br/>05:39
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-04]] A/B/C
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|46
|Y44
|27 June 2018<br/>03:30
|LC-3, XSLC
|
|XJSS A/B
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|47
|2CSMA-Y3
|9 July 2018<br/>03:56
|LA-4/SLS-2, JSLC
|2C/SMA
|[[Engineering:Pakistan Remote Sensing Satellite|PRSS-1]]<br/>PakTES-1A
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|48
|Y39
|7 September 2018<br/>03:15
|LA-9, TSLC
|
|[[Earth:HY (satellite)|HaiYang-1C]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|49
|Y38
|9 October 2018<br/>02:43
|LA-4/SLS-2, JSLC
|2C/YZ-1S
|[[Engineering:Yaogan|Yaogan]] 32A, 32B
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|50
|Y22
|29 October 2018<br/>00:43
|LA-4/SLS-2, JSLC
|
|CFOSAT
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|51
|Y37
|26 July 2019<br/>03:57
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-05]] A/B/C
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|52
|Y42
|24 March 2020<br/>03:43
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-06]] A/B/C
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|53
|Y40
|10 June 2020<br/>18:31 <ref name=sfn-20200610/>
|LA-9, TSLC
|
|[[Earth:HY (satellite)|HaiYang 1D]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|54
|Y43
|26 October 2020<br />15:19 <ref name="SFN20201023">{{cite web|url=https://spaceflightnow.com/launch-schedule/|title=Launch Schedule|publisher=Spaceflight Now|date=23 October 2020|access-date=25 October 2020}}</ref>
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-07]] A/B/C
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|55
|Y47
|6 May 2021<br/>18:11<ref>{{cite web |url=https://mp.weixin.qq.com/s/Ftr52RWO0izA9GNqvfNaEg |title=成功！老将长二丙2021首战！还有7发！|trans-title=success! Veteran Chang Er C first match in 2021! There are 7 more shots! |date=6 May 2021 |access-date=6 May 2021 |language=zh}}</ref>
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-08]] A/B/C<br/>Tianqi-12
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|56
|Y48
|18 June 2021<br/>06:30<ref>{{cite web |last=Cong |first=Zhao |url=https://mp.weixin.qq.com/s/9YKfNysp7Ko_5nPzQkD8bQ |title=两天两连胜！长二丙火箭成功发射遥感三十号09组卫星 |trans-title=Two consecutive victories in two days! Long March 2C rocket successfully launched Yaogan 30-09 satellites |date=18 June 2021 |access-date=18 June 2021 |publisher=[[Company:China Aerospace Science and Technology Corporation|CASC]] |language=zh}}</ref>
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-09]] A/B/C<br/>Tianqi-14
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|57
|Y49
|19 July 2021<br/>00:19<ref name="Yaogan3010"/>
|LA-3, XSLC
|
|[[Engineering:Yaogan|Yaogan 30-10]] A/B/C<br/>Tianqi-15
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|58
|Y51
|24 August 2021<br/>11:15<ref>{{cite web |url=https://mp.weixin.qq.com/s/G8Otm2dJBFZ-KHUPkzcC2A |title=又在整流罩上“搞事情”，长二丙送3颗通信卫星飞天
 |trans-title="Doing things" on the fairing again, Long March 2C sends 3 communication satellites to the sky |date=24 August 2021 |access-date=24 August 2021 |work=China Space News |language=zh}}</ref>
|LA-4/SLS-2, JSLC
|2C/YZ-1S
|RSW-01<br/>RSW-02<br/>''Undisclosed payload''
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-

| 59
| Y41
| 3 November 2021<br/>07:43
| LA-4/SLS-2, JSLC
| 2C/YZ-1S
| [[Engineering:Yaogan|Yaogan]] 32-02 A/B
| [[Astronomy:Sun-synchronous orbit|SSO]]
| {{Success}}
|-

| 60
| Y62
| 5 March 2022<br/>06:01
| LA-3, XSLC
| 
| Yinhe Hangtian-2 01/.../06<br/>Xuanming Xingyuan
| [[Astronomy:Low Earth orbit|LEO]]
| {{Success}}
|-

| 61
| Y70
| 29 April 2022<br/>04:11
| LA-4/SLS-2, JSLC
| 
| SuperView Neo 1-01/02 (Siwei Gaojing 1-01/02)
| [[Astronomy:Sun-synchronous orbit|SSO]]
| {{Success}}
|-

| 62
| Y53
| 20 May 2022<br/>10:30
| LA-4/SLS-2, JSLC
| 2C/YZ-1S
| LEO Test Sat 1/2<br />Digui Tongxin Weixing
| [[Astronomy:Low Earth orbit|LEO]]
| {{Success}}
|-

| 63
| Y65
| 2 June 2022<br/>04:00
| LA-3, XSLC
| 
| GeeSAT-1 01/.../09
| [[Astronomy:Low Earth orbit|LEO]]
| {{Success}}
|-

| 64
| Y71
| 15 July 2022<br/>22:57
| LA-9, TSLC
| 
| SuperView Neo 2-01/02 (Siwei-03/04)
| [[Astronomy:Sun-synchronous orbit|SSO]]
| {{Success}}
|-
| 65
| Y66
| 12 October 2022<br/ >22:53
| LA-9, TSLC
| 
| S-SAR 01 ([[Engineering:Huanjing (satellite)|Huanjing-2E]])
| [[Astronomy:Sun-synchronous orbit|SSO]]
| {{Success}}
|-
|66
|Y61 
|12 January 2023<br/ >18:10
|LA-3, XSLC
|
|Apstar 6E +(independent propulsion module)
|[[Astronomy:Geostationary transfer orbit|GTO]]
|{{Success}}
|-
|67
|Y63
|24 February 2023<br/>04:01
|LA-4/SLS-2, JSLC
|
|Horus-1
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|68
|Y64
|13 March 2023<br/>04:02
|LA-4/SLS-2, JSLC
|
|Horus-2
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|69
|Y60
|21 May 2023<br>08:00
|LA-4/SLS-2, JSLC
|
|MSS-1 A/B<br>Luojia-2 01
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|70
|Y52
|9 July 2023<br>11:00
|LA-4/SLS-2, JSLC
|2C/YZ-1S
|Hulianwang Jishu Shiyan A, B
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|71
|Y46
|8 August 2023<br/ >22:53
|LA-9, TSLC
| 
|S-SAR 02 ([[Engineering:Huanjing (satellite)|Huanjing-2F]])
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|72
|Y56
|16 November 2023<br>03:55
|LA-4/SLS-2, JSLC
|2C/YZ-1S
|[[Engineering:Haiyang (satellite)|Haiyang-3A]]
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|73
|Y54
|4 December 2023<br>04:10
|LA-4/SLS-2, JSLC
|
|MisrSat-2<br>Xingchi-2A/2B
|[[Astronomy:Sun-synchronous orbit|SSO]]
|{{Success}}
|-
|74
|Y73
|30 December 2023<br>00:13
|LA-4/SLS-2, JSLC
|2C/YZ-1S
|Hulianwang Jishu Shiyan 4A, 4B, 4C
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|75
|Y30
|9 January 2024<br>07:03
|LA-3, XSLC
|
|[[Astronomy:Einstein Probe|Einstein Probe]] 
|[[Astronomy:Low Earth orbit|LEO]]
|{{Success}}
|-
|76
|Y
|2 February 2024<br/>23:45
|LA-3, XSLC
| 
|Geely Constellation Group 02 (?)
|[[Astronomy:Low Earth orbit|LEO]]
|{{Planned}}
|-
|77
| Y?
| March 2024
| TBA 
| 
| TBA
| TBA 
| {{Planned}}
|-
|78
| Y?
| 24 June 2024
| LA-3, XSLC 
| 
| SVOM
| [[Astronomy:Low Earth orbit|LEO]]
| {{Planned}}
|}

== Launch failures ==
=== Shijian 11-04 launch failure ===
On 18 August 2011, a Long March 2C rocket failed during the launch of the [[Engineering:Shijian|Shijian]] 11-04 satellite. During the powered flight phase of the second stage, the connecting mechanism between vernier engine no.3 and the servo-control mechanism of the second stage failed, which led to the loss of attitude control on the second stage.<ref>{{cite web|title=Malfunction at devices connection blamed for orbiter launch failure |url=http://news.xinhuanet.com/english2010/sci/2011-09/06/c_131100892.htm|archive-url=https://web.archive.org/web/20160304073250/http://news.xinhuanet.com/english2010/sci/2011-09/06/c_131100892.htm|url-status=dead|archive-date=4 March 2016|publisher=Xinhua News Agency|date=6 September 2011|access-date=9 August 2015}}</ref>

==Launch statistics==
{{#invoke:Chart | bar chart
| height = 300
| width = 800
| stack = 1
| group 1 =  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  1:  0:  0:  0:    0:  0:  0:  0:  0:    0: 0: 0: 0: 0
| group 2 =  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0: 0: 0: 0: 0
| group 3 =  1:  1:  1:    1:  1:  2:  1:  0:    1:  0:  1:  1:  0:    0:  0:  2:  4:  1:    0:  0:  0:  1:  4:    1:  1:  1:  1:  2:    0:  3:  2:  2:  4:    0:  0:  3:  6:  1:    3: 5: 6: 9: 1
| group 4 =  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0:  0:  0:  0:  0:    0: 0: 0: 0: 2

| colors = FireBrick : Orange : ForestGreen : LightBlue
| group names = Failure : Partial failure : Success : Planned
| units suffix = _launches
| x legends = 1982 ::: 1985 ::::: 1990 ::::: 1995 ::::: 2000 ::::: 2005 ::::: 2010 ::::: 2015 ::::: 2020 ::::
}}

== References ==
{{Reflist}}

== External links ==
* {{cite web|url=https://fas.org/spp/guide/china/launch/lm2c/index.html|title=LM-2C USER'S MANUAL|publisher=CALT|year=1999|url-status=dead|archive-url=https://web.archive.org/web/20160116010401/http://fas.org/spp/guide/china/launch/lm2c/index.html|archive-date=2016-01-16}}
* {{cite web|url=http://space.skyrocket.de/doc_lau/cz-2.htm|title=CZ-2 (Chang Zheng-2)|publisher=Gunter's Space Page|author=Gunter Dirk Krebs|access-date=9 August 2015}}

{{Long March rockets}}
{{Chinese space program}}
{{Expendable launch systems}}

[[Category:Long March (rocket family)]]

{{Sourceattribution|Long March 2C}}