Long March (Chang Zheng)
by Jean-Jacques Serralisting by Gunter Krebs
After the rupture between China and USSR in June 1959 the Chinese started to develop a series a ballistic missiles powered with stockable propellant. The first of these was the CSS-1: a single stage rocket very close to the Soviet SS-3 which was 22 m in length and 1.65 m in diameter that could cover 1100 km. It was tested in the sixties and entered service in 1970. The first Chinese IRBM, the CSS-2 was also single staged. It was 23 m long, 2.23 m diameter and ranged 2500 km. The first in-flight tests were carried out on 1969 and was deployed in 1972. The CSS-3 version with 6500 km range was made by adding a second stage to the CSS-2 (with same diameter). It never entered operational service was was used as the basis of the first Chinese launcher: CZ-1.
CZ-1 launchers
The CZ-1 rocket (Chang Zheng = Long March) was derived from the CSS-3 (also called DF-4 by the Chinese, Dong Feng = East Wind) which was added a solid fuel third stage. The first stage was 17.8 m long and weighed 64.1 tons including 60 tons of propellant (Nitric Acid and UDMH). It was powered by a YF-2A motor featuring 4 chambers of 1100 kN at ground level, burning during 130 seconds (ISp = 241 s). The 5.4 m second stage weighed 15.9 tons including 13.2 tons of ergols (NTO and UDMH). It used a YF-3 motor providing 294 kN thrust in vacuum during 126 seconds (ISp = 287 s). The spin-stabilized third stage required a GF=02 powder bloc weighing 1.8 tons which provides 29 kN thrust.
The full CZ-1 launcher was 29.45 m high for 81.6 tons at takeoff and could orbit a 300 kg payload at 440 km with 70° inclination. It launched the 2 first Chinese satellites from Juiquan in April 1970 and March 1971 after a failure in November 1969.
Enhanced version of this launcher: CZ-1C and CZ-1D completly Chinese and CZ-1M featuring an Italian 3rd stage (IRIS) were announced...
Second generation launchers: FB-1 and CZ-2A/D
The first Chinese ICBM CSS-3 (or DF-5 in the Chinese jargon) was over 30 m high for 3.35 m diameter. It featured two liquid fuel stages (NTO and UDMH) and ranged 11000 km. In-flight tests were carried out in 1979 and only few exemplars (8 to 12 ?) were deployed after 1980.
Its development was carried out in the same time as two space launcher programs: FB-1 (Feng Bao = storm) and CZ-2. Very little is known on the FB-1 but it is probably similar to CZ-2 with lower performances (1.2 tons is LEO against 1.7 tons). Some sources believe the two launchers were developped by two different agencies (SBA (Shanghai Bureau of Astronautics) et la BWYIC (Beijing Wan Yuan Industry Corporation)) from the same specifications. It was launched successfully 4 times from Jiuquan between July 1975 and September 1981; 4 failures and 3 suborbital flights were also reported.
The most important launcher of the other series is the CZ-2C. The CZ-2A was indeed only fired once in November 1974 and the B designation used for the FB-1. The CZ-2C featured a L-140 first stage of 20.5 m long which weighed 151 tons including 142 tons of propellant. It was powered by 4 YF-20 motors of 696 kN thrust at ground level (ISp = 260 s) which burned during 132 seconds. The second stage (L-35) was 7.5 m long and 39 tons (35 tons for propellant). It was equipped with an YF-22 motor providing 762 kN in vacuum (ISp = 290 s) associated with 4 deployable YF-23 verniers providing a total of 44 kN. The main engine burned 110 seconds while the verniers 300 seconds.
The CZ-2C launcher is 32.6 to 35.1 m high (depending on the cap) and weighed about 191 tons. It can deliver 2 to 2.5 tons in LEO. From Juiquan it orbited 9 retrievable FSW-0 (Fanhui Shi Weixing) satellites between November 1975 and August 1987 and 5 FSW-1 since September 1987. An enhanced version named CZ-2D launched two FSW-2 satellites in August 1992 and July 1994.
Three-stage versions of the CZ-2C were announced . Only the CZ-2C/SD should be used for Iridium.
CZ-3 launchers
The CZ-3 rocket is a 3-stage launcher which makes use of modified versions of the 2 first stages of CZ-2C (same performances) and adds a cryogenic third stage. This H-8 cryogenic stage is 7.5 m long for 2.25 m diameter. It weighs 10.5 tons including 8.5 tons of propellant (LH2 and LOX). it is equipped with a 4-chamber YF-73 motor providing 44 kN thurst in vacuum (ISp = 420 s). The reignitable motor is used for two burns during 500 and 300 seconds.
This launcher is 43.2 to 43.8 m high and weighs 202 tons. It can orbit 1.4 tons in GTO. It was used from Xichang from January 1984 on to launch Chinese telecommunication satellites of foreign spacecrafts. It should still be used even after the introduction of enhanced versions designated CZ-3A and CZ-3B.
Third generation launchers: CZ-4, CZ-2E and CZ-3A/B
A new Chinese generation was introduced in the late eighties based on a streched L-180 first stage equipped with more powerful motors.
The first launcher to use those new elements was CZ-4 specialy designed for sunsynchronous orbits. The first stage is thus an L-180 with 24.7 m long carrying 138 tons propellant powered during 156 seconds by 4 YF-20 motors which unitary thrust was boosted to 735 kN. The second stage is an modified L-35 with 10.4 m long. Its main engine is a YF-25 of 766 kN assisted by 4 YF-23 verniers. The third stage (L-14) specific to the CZ-4 is 6.2 m long for 2.9 m diameter. It is equipped with a pair of YF-40 engines which burn NTO and UDMH. Their total thrust is 98 kN during 321 seconds (ISp = 303 s). This CZ-4 reaches 42 m high and 250 tons. It can deliver a 1.5 ton payload on sun-synchronous orbit at 900 km. It was used to launch 2 meteorological FY satellites from Taiyuan in Sep 1988 and Sep 1990. The CZ-4C is similar to CZ-4B, with the restart capability added.
The second launcher to use the L-180 and the enhanced motors is the CZ-2E devoted to heavy GEO payloads. The first stage is an L-180 with 23.7 m long (187 tons propellant) propulsed during 159 seconds by 4 YF-20 motors of 735 kN. It is assisted during 126 seconds by 4 LB-40 boosters of 15.6 m long and 2.25 m diameter (38 tons of propellant each) equipped with the same YF-20 engines. The second stage is an L-90 of 15.5 m long (86 tons ergols) with a YF-25 main engine of 831 kN. It is surrounded by 4 YF-23 verniers. The main engine burns during 300 seconds while the version 413 seconds.
The CZ-2E is 49.7 to 51.2 m high. It weighs 460 tons at takeoff. Its capacity reaches 8.8 tons in LEO but it is only used for geostationary satellites with a solid perigee stage. The first version with the American Thiokol Star-63F could place 3.14 tons in GTO. With the EPKM of the Chinese HCMC (Hexi Chemical & Manufacturing Corp) company used for the first time in Nov 1995 the performance reaches 3.46 tons. After a trial launch in July 1990 the CZ-2E was used to launch several telecommunications satellites from Xichang...
The third launcher based on the L-180 was the CZ-3A also devoted to heavy payloads aimed at GEO. The first stage is a 23 m long L-180 (170 tons of propellant) powered by four 735 kN YF-20 motors. The second stage is a L-35 of 11.5 m long (29.6 tons ergol) with an YF-25 main engine of 766 kN which burns during 110 seconds assited by 4 YF-23 verniers. The new H-18 cryogenic third stage is 8.8 m long and 3.0 m diameter (17.6 tons propellant). It features 2 YF-75 engines providing a total thrust of 157 kN (ISp = 425 s) during 470 seconds in 2 burns.
The CZ-3A has a total of 52.3 m high and 240 tons at takeoff. It can orbit 2.3 tons in GTO. After a trial launch in Feb 1994 to launched a 3rd generation telecommunication DFH satellite in Nov 1994.
The CZ-3B used the CZ-3A with 4 liquid boosters inherited from the CZ-2E. It then weighs 403 tons at takeoff and its capacity reaches 4.85 tons in GTO. It first launch failed in Feb 1996.
In 2015, the Yuanzheng-1 (YZ-1, "Expedition 1") restartable upper stage was introduced. It can send one or more payload into different orbits, using liquid propellant (can be restarted 20 times and carry as much as 10 satellites).
Fourth generation launchers: CZ-5, CZ-6, CZ-7, CZ-8
Chang Zheng 5 is 5m diameter and 860 tons. It can carry 25 tons in LEO. It is key to building the Chinese Space Station. The rocket is powered by a core stage equipped with two YF-77 engines running on LH2/LOX, the first high-thrust cryogenic engine developed in China. The stage is augmented by four strap-on boosters. Each of the boosters is equipped with two YF-100 engines derived from Russia's RD-120, which consume kerosene and LOX. The upper stage is propelled by a restartable YF-75D cryogenic engine.
Chang Zheng 7 is a medium-sized rocket to carry upto 13.5 tons to LEO. 600 ton, 3.35m diameter.
CZ-5 and CZ-7 are launched from the Wenchan satellite launch center, located on the Hainan island, in the South China Sea. It is only at 19° North.
For Chang Zheng 8, the core-stage will be based on CZ-7 and CZ-3A rockets, the CZ-8 is expected to have two solid-propelled boosters with a diameter of 1.95 m although these were removed from the new model. It has a total length of 50.3 meters, with a takeoff mass of 198 m tonnes. It can carry a payload of at least 4500 kg to a Sun-synchronous orbit at an altitude of 700 km.
See also Chang Zheng 6 and Chang Zheng 11
CZ-1 launches
| # | Launch id | Payload | Launch date | Type | Status/Comment (orbit in perigee x apogee x inc. x period) |
| 1, CZ-1 | n/a | R&D suborbital | 10 Jan 1970 | ||
| 2, CZ-1 | 70034 | DFH 01 | 24 Apr 1970 | ||
| 3, CZ-1 | 71018 | DFH 02 | 3 Mar 1971 |
Notes: All launches from Juiquan.
CZ-5 launches
| # | Launch id | Payload | Launch date | Type | Status/Comment (orbit in perigee x apogee x inc. x period) |
| 1 | 16065 | DFH 156 | 3 Nov 2016 at 12:43 UT | 5B |
YZ-2
upper stage Inaugural launch |
| 2, Y2 | n/a | DFH 169 | 2 Jul 2017 at 11:23 UT | 5 | Failure: payload left in low orbit, issues with first stage (turbine exhaust problem) |
| 3 | 19097 | DFH 243 (Shijian 20) | 27 Dec 2019 at 12:45 UT | 5 Y3 | |
| 4 | 20027 |
XZF-SC RCS-FC-SC | 5 May 2020 at 10:00 UT | 5B |
No upper stage the spacecraft landed safely on 10 May |
| 5 | 20049 | Tianwen 1 | 23 Jul 2020 at 04:41 UT | 5 | Mars probe |
| 6 | 20087 | Chang'e 5 | 23 Nov 2020 at 20:30 UT | 5 | |
| 7 | 21035 | Tianhe 1 | 29 Apr 2021 at 03:18 UTC | 5B | Core module for the Chinese space station. 16.6 m long x 4.2 m diameter. 22500 kg at launch |
| 8 | 22085 | Wentian | 24 Jul 2022 at 06:22 UTC | 5B | Additional module |
| 9 | 22143 | Mengtian | 31 Oct 2022 at 7:37 UTC | 5B |
3rd module of the station approx. 23000 kg |
| 10 | 23197 | Yaogan 41 | 15 Dec 2023 at 13:41 UTC | 5 | |
| 11 | 24037 | DFH 332 | 23 Feb 2024 at 11:30 UTC | 5 | |
| 12 | 24083 | Chang'e 6 | 3 May 2024 at 09:27 UTC | 5 |
Notes: All launches from Wenchang, on Hainan island.
CZ-7 launches
| # | Launch id | Payload | Launch date | Type | Status/Comment (orbit in perigee x apogee x inc. x period) |
| 1, CZ-7 | 16042 |
DFFC rentry module (2600 kg) B: DFH 148 (AX 1) F: DFH 149 (AL 1) L: DFH 150 (Tiange 1) M: DFH 151 (Tiange 2) | 25 Jun 2016 at 12:00 UT |
200
x 394 km First launch from Wenchang | |
| 2, CZ-7 | 17021 |
Tianzhou
1 F: Silkroad 1 | 20 Apr 2017 at 11:41 UT | Payload is a cargo ship measuring 10.6 m lengthx 3.35m diameter, can contain 6 tons | |
| 3, CZ-7 | n/a | XJY 6 (XinJishu Yanzheng 6) aimed to GEO | 16 Mar 2020 at 13:34 UT | 7A | Failure: second stage failure 52 seconds into flight |
| 4, CZ-7 | 21019 | DFH 268 | 11 Mar 2021 at 17:51 UT | 7A | |
| 5, CZ-7 | 21046 | Tianzhou 2 | 29 May 2021 at 12:55 UTC | cargo to Chinese space station | |
| 6, CZ-7 | 21085 | Tianzhou 3 | 20 Sep 2021 at 07:10 UT | ||
| 7, CZ-7 | 21129 |
A: DFH 294 (SY 12-01) B: DFH 295 (SY 12-02) | 23 Dec 2021 at 10:12 UTC | 7A | 210 x 35765 km x 19.46° |
| 8, CZ-7 | 22050 | Tianzhou 4 | 9 May 2022 at 17:56 UTC | ||
| 9, CZ-7 | 22112 | Chinasat 1E | 13 Sep 2022 at 13:18 UTC | 7A | |
| 10, CZ-10 | 22152 | Tianzhou 5 | 12 Nov 2022 at 02:03 UTC | ||
| 11, CZ-11 | 23002 | DFH 316 | 8 Jan 2023 at 22:00 UTC | 7A | |
| 12, CZ-7 | 23063 |
Tianzhou
6~ C: Dalian 1~ | 10 May 2023 at 13:22 UTC | 7 | |
| 13, CZ-7 | 23169 | DFH 327 | 3 Nov 2023 at 14:54 UTC | 7A | |
| 14, CZ-7 | 24013 | Tianzhou 7 | 17 Jan 2024 at 14:27 UTC | 7 | |
| 15, CZ-7 | 24122 | Chinasat 3A | 29 Jun 2024 at 11:57 UTC | 7A |
CZ-8 launches
| # | Launch id | Payload | Launch date | Type | Status/Comment (orbit in perigee x apogee x inc. x period) |
| 1, CZ-8 | 20102 |
A:
Tianqi 8 ET-SMART-RSS DFH 264 (Yuanguang) DFH 265 (Haisi 1) DFH 266 (Xinjishu Yanzheng-7) | 22 Dec 2020 at 04:37 UT | ||
| 2 | 22019 |
Chaohu 1 Chuangxing Leishen Hainan 1-01 and 1-02 Jilin 1 Gaofen 03D 10 to 18 Jilin 1 Mofang 02A 01 Qimingxing 1 Taijing 3-01 Taijing 4-01 Tianqi 19 Wenchang 1-01 and 1-02 Xidian 1 Xingshidai 17 | 27 Feb 2022 at 23:44 UTC | no side boosters | 525 x 574 km x 97.5° |
| 3 | 24051 |
A:
Queqiao
2 C: Tiandu 1 D: Tiandu 2 | 20 Mar 2024 at 00:31 UTC |
Lunar orbit Queqiao 2 is a telecom relay satellite 1276 kg payload |
CZ-2, 3 & 4 launches
| # | Launch id | Payload | Launch date | Site | Type | Status/Comment (orbit in perigee x apogee x inc. x period) | |||||||
| 1, CZ-2 | n/a | FSW 0 | 05 Nov 1974 | Ji | A? | Failure: 1st stage control system failure | |||||||
| 2, CZ-2 | 75111 | FSW 0-1 | 26 Nov 1975 | Ji | C | ||||||||
| 3, CZ-2 | 76116 | FSW 0-2 | 07 Dec 1976 | Ji | C | ||||||||
| 4, CZ-2 | 78011 | FSW 0-3 | 26 Jan 1978 | Ji | C | ||||||||
| 5, CZ-2 | 82090 | FSW 0-4 | 09 Sep 1982 | Ji | C | ||||||||
| 6, CZ-2 | 83086 | FSW 0-5 | 19 Aug 1983 | Ji | C | ||||||||
| 7, CZ-3 | 84008 | STTW-T1 | 29 Jan 1984 | Xi | Partial failure: 3rd stage failed to ignite | ||||||||
| 8, CZ-3 | 84035 | STTW-T2 | 08 Apr 1984 | Xi | |||||||||
| 9, CZ-2 | 84098 | FSW 0-6 | 12 Sep 1984 | Ji | C | ||||||||
| 10, CZ-2 | 85096 | FSW 0-7 | 21 Oct 1985 | Ji | C | ||||||||
| 11, CZ-3 | 86010 | STTW 1 | 01 Feb 1986 | Xi | |||||||||
| 12, CZ-2 | 86076 | FSW 0-8 | 06 Oct 1986 | Ji | C | ||||||||
| 13, CZ-2 | 87067 | FSW 0-9 | 05 Aug 1987 | Ji | C | ||||||||
| 14, CZ-2 | 87075 | FSW 1-1 | 09 Sep 1987 | Ji | C | ||||||||
| 15, CZ-3 | 88014 | STTW 2 | 07 Mar 1988 | Xi | |||||||||
| 16, CZ-2 | 88067 | FSW 1-2 | 05 Aug 1988 | Ji | C | ||||||||
| 17, CZ-4 | 88080 | FY 1-1 | 06 Sep 1988 | Ty | |||||||||
| 18, CZ-3 | 88111 | STTW 3 | 22 Dec 1988 | Xi | |||||||||
| 19, CZ-3 | 90011 | STTW 4 | 04 Feb 1990 | Xi | |||||||||
| 20, CZ-3 | 90030 | Asiasat 1 | 07 Apr 1990 | Xi | |||||||||
| 21, CZ-2 | 90059 | Badr A | 16 Jul 1990 | Xi | E (PKM) | Failed to place the Optus model in GTO | |||||||
| 22, CZ-4 | 90081 |
A:
FY 1-2 B: DFH 31 C: DFH 32 | 03 Sep 1990 | Ty | |||||||||
| 23, CZ-2 | 90089 | FSW 1-3 | 05 Oct 1990 | Ji | C | ||||||||
| 24, CZ-3 | 91088 | STTW 5 | 28 Dec 1991 | Xi | Partial failure: 3rd stage failed to ignite | ||||||||
| 25, CZ-2 | 92051 | FSW 2-1 | 09 Aug 1992 | Ji | D | ||||||||
| 26, CZ-2 | 92054 | Optus B1 | 13 Aug 1992 | Xi | E (Star-63F) | ||||||||
| 27, CZ-2 | 92064 |
A:
Freja B: FSW 1-4 | 06 Oct 1992 | Ji | C | ||||||||
| 28, CZ-2 | 92090 | Optus B2 | 21 Dec 1992 | Xi | E (Star-63F) | Partial failure: payload fairing collapsed | |||||||
| 29, CZ-2 | 93063 | FSW 1-5 | 08 Oct 1993 | Ji | C | ||||||||
| 30, CZ-3 | 94010 |
A:
SJ 4 B: DFH 3-0 | 08 Feb 1994 | Xi | A | ||||||||
| 31, CZ-2 | 94037 | FSW 2-2 | 3 Jul 1994 | Ji | D | ||||||||
| 32, CZ-3 | 94043 | Apstar 1 | 21 Jul 1994 | Xi | |||||||||
| 33, CZ-2 | 94055 | Optus B3 | 27 Aug 1994 | Xi | E (Star-63F) | ||||||||
| 34, CZ-3 | 94080 | DFH 3-1 | 29 Nov 1994 | Xi | A | ||||||||
| 35, CZ-2 | n/a | Apstar 2 | 25 Jan 1995 | Xi | E (Star-63F) | Failure: vehicle destroyed due to wind shear | |||||||
| 36, CZ-2 | 95064 | Asiasat 2 | 28 Nov 1995 | Xi | E (STPM-17) | ||||||||
| 37, CZ-2 | 95073 | Echostar 1 | 28 Dec 1995 | Xi | E (?) | ||||||||
| 38, CZ-3 | n/a | Intelsat 708 | 14 Feb 1996 | Xi | B | Failure: attitude control lost within seconds, due to an electrical failure | |||||||
| 39, CZ-3 | 96039 | Apstar 1A | 03 Jul 1996 | Xi | 225 x 42184 km x 26.9° | ||||||||
| 40, CZ-3 | 96048 | DFH 42 | 18 Aug 1996 at 10:27 UT | Xi | Partial failure: 3rd stage shutdown 48s early | ||||||||
| 41, CZ-2 | 96059 | FSW 2-3 | 20 Oct 1996 | Ji | D | ||||||||
| 42, CZ-3 | 97021 | DFH 44 | 11 May 1997 at 16:17 UT | Xi | A | ||||||||
| 43, CZ-3 | 97029 | DFH 45 | 10 Jun 1997 at 12:01 UT | Xi | 206 x 35987 km x 28.4° | ||||||||
| 44, CZ-3 | 97042 | Mabuhay 1 | 19 Aug 1997 at 17:30 UT | Xi | B | 170 x 44499 km x 24.6° | |||||||
| 45, CZ-2 | 97048 |
2 Iridium
MFS (Mass Frequency Simulators) 650 kg each | 1 Sep 1997 at 14:00 UT | Ty | C |
First flight from Taiyan with Smart Dispenser upper stage | |||||||
| 46, CZ-3 | 97062 | Apstar 2R | 16 Oct 1997 at 17:13 UT | Xi | B | 201 x 47922 km x 24.4° | |||||||
| 47, CZ-2 | 97077 |
A:
Iridium 42 B: Iridium 44 | 8 Dec 1997 at 07:16 UT | Ty | C-3/SD | SD = Smart Dispenser | |||||||
| 48, CZ-2 | 98018 |
A: Iridium 51 B: Iridium 61 | 25 Mar 1998 at 17:01 UT | Ty | C-3/SD | ||||||||
| 49, CZ-2 | 98026 |
A:
Iridium 69 B: Iridium 71 | 2 May 1998 | Ty | C-3/SD | ||||||||
| 50, CZ-3 | 98034 | Chinastar 1 | 30 May 1998 | Xi | B | ||||||||
| 51, CZ-3 | 98044 | Sinosat 1 | 18 Jul 1998 at 09:20 UT | Xi | B | ||||||||
| 52, CZ-2 | 98048 |
A: Iridium 78 B: Iridium 76 | 19 Aug 1998 at 23:01 UT | Ty | C-3/SD | ||||||||
| 53, CZ-2 | 98074 |
A: Iridium 88 B: Iridium 89 | 19 Dec 1998 at 11:30 UT | Ty | C-3/SD | ||||||||
| 54, CZ-4 | 99025 |
A:
FY 1C B: DFH 48 | 10 May 1999 at 01:33 UT | Ty | 4B | ||||||||
| 55, CZ-2 | 99032 |
A:
Iridium 14A B: Iridium 21A | 11 Jun 1999 at 17:15 UT | Ty | C/SD | ||||||||
| 56, CZ-4 | 99057 |
A:
CBERS 1 B: SACI 1 | 14 Oct 1999 at 03:15 UT | Ty | 4B | ||||||||
| 57, CZ-2 | 99061 | Shenzhou 1 | 19 Nov 1999 at 22:43 UT | Ji | 2F | ||||||||
| 58, CZ-3 | 00003 | DFH 48 | 25 Jan 2000 at 16:45 UT | Xi | A | ||||||||
| 59, CZ-3 | 00032 | DFH 49 | 25 Jun 2000 at 11:50 UT | Xi | |||||||||
| 60, CZ-4 | 00050 | DFH 50 | 1 Sep 2000 at 03:25 UT | Ty | 4B | ||||||||
| 61, CZ-3 | 00069 | DFH 51 | 30 Oct 2000 at 16:02 UT | Xi | 3A | ||||||||
| 62, CZ-3 | 00082 | DFH 52 | 21 Dec 2000 at 16:20 UT | Xi | 3A | ||||||||
| 63, CZ-2 | 00101 | Shenzhou 2 | 9 Jan 2001 at 17:00 UT | Ji | 2F | First mission completed in winter, with temperature -13°C | |||||||
| 64, CZ-2 | 02014 | Shenzhou 3 | 25 Mar 2002 at 14:00 UT | Ji | 2F | 197 x 326 km x 42.4° | |||||||
| 65, CZ-4 | 02024 |
A: DFH 53 B: DFH 54 | 15 May 2002 at 01:50 UT | Ty | 4B | ||||||||
| 66, CZ-4 | 02049 | DFH 55 | 27 Oct 2002 at 03:17 UT | Ty | 4B | ||||||||
| 67, CZ-2 | 02061 | Shenzhou 4 | 29 Dec 2002 at 16:40 UT | Ji | 2F | ||||||||
| 68, CZ-3 | 03021 | DFH 56 | 24 May 2003 at 16:34 UT | Xi | 3A | ||||||||
| 69, CZ-2 | 03045 | Shenzhou 5 | 15 Oct 2003 at 01:00 UT | Ji | 2F | First manned mission for China | |||||||
| 70, CZ-4 | 03049 |
A:
CBERS 2 B: Chuangxin 1 | 21 Oct 2003 at 03:16 UT | Ty | 4B | ||||||||
| 71, CZ-2 | 03051 | DFH 57 | 03 Nov 2003 at 07:20 UT | Ji | 2D | ||||||||
| 72, CZ-3 | 03052 | DFH 58 | 14 Nov 2003 at 16:01 UT | Xi | 3A | 212 x 41981 km | |||||||
| 73, CZ-2 | 03061 | Tan Ce 1 | 29 Dec 2003 at 19:06 UT | Xi | 2C/SM |
550 x 66000 km x 28.5° Had an SM upper stage derived from the smart dispenser used for Iridium. First 2C launch from Xichang. | |||||||
| 74, CZ-2 | 04012 |
A: Tansuo 1 B: Naxing 1 | 18 Apr 2004 at 15:59 UT | Xi | 2C | Polar orbit | |||||||
| 75, CZ-2 | 04029 | Tan Ce 2 | 25 Jul 2004 at 07:05 UT | Xi | 2C/SM | 666 x 38566 km x 90.1° | |||||||
| 76, CZ-2 | 04033 | DFH 59 | 29 Aug 2004 at 07:50 UT | Ji | 2C | ||||||||
| 77, CZ-4 | 04035 |
A: DFH 60 B: DFH 61 | 8 Sep 2004 at 23:14 UT | Ty | 4B | ||||||||
| 78, CZ-2 | 04039 | DFH 62 | 27 Sep 2004 | Ji | 2D | ||||||||
| 79, CZ-3 | 04042 | DFH 63 | 19 Oct 2004 at 01:20 UT | Xi | 3A | ||||||||
| 80, CZ-4 | 04044 | DFH 64 | 6 Nov 2004 at 03:10 UT | Ty | 4B | ||||||||
| 81, CZ-3 | 05012 | Apstar 6 | 12 Apr 2005 at 12:00 UT | Xi | 3B | 209 x 49991 km x 26° | |||||||
| 82, CZ-2 | 05024 | DFH 65 | 5 Jul 2005 at 22:40 UT | Ji | 2D |
547 x 570 km x 97.6° First sun-synchronous launch from Jiuquan | |||||||
| 83, CZ-2 | 05027 | DFH 66 | 2 Aug 2005 at 07:30 UT | Ji | 2C | ||||||||
| 84, CZ-2 | 05033 | DFH 67 | 29 Aug 2005 | Ji | 2D | ||||||||
| 85, CZ-2 | 05040 | Shenzhou 6 | 12 Oct 2005 at 01:00 UT | Ji | 2F |
Second manned mission 198 x 344 km x 42.4° | |||||||
| 86, CZ-4 | 06015 |
A: Yaogan 1 B: picosat | 26 Apr 2006 at 22:48 UT | Ty | 4B | a 1kg object was also launched with, microelectronics experiment | |||||||
| 87, CZ-2 | 06035 | DFH 68 | 9 Sep 2006 at 07:00 UT | Ji | 2C | ||||||||
| 88, CZ-3 | 06038 | DFH 69 | 12 Sep 2006 at 16:02 UT | Xi | 3A | ||||||||
| 89, CZ-4 | 06046 |
A: DFH 70 B: DFH 71 | 23 Oct 2006 at 23:43 UT | Ty | 4B | ||||||||
| 90, CZ-3 | 06048 | Sinosat 2 | 28 Oct 2006 at 16:20 UT | Xi | 3C | ||||||||
| 91, CZ-3 | 06053 | DFH 72 | 08 Dec 2006 at 00:53 UT | Xi | 3A | ||||||||
| 92, CZ-3 | 07003 | DFH 73 | 03 Feb 2007 at 16:28 UT | Xi | 3A | ||||||||
| 93, CZ-2 | 07010 | DFH 74 | 11 Apr 2007 at 03:27 UT | Ty | 2C | ||||||||
| 94, CZ-3 | 07011 | DFH 75 | 13 Apr 2007 at 20:11 UT | Xi | 3A | ||||||||
| 95, CZ-3 | 07018 | Nigcomsat 1 | 13 May 2007 at 16:01 UT | Xi | 3B | 200 x 41600 km x 25° | |||||||
| 96, CZ-2 | 07019 | Yaogan 2 | 25 May 2007 at 07:12 UT | Ji | 2D | ||||||||
| 97, CZ-3 | 07021 | Sinosat 3 | 31 May 2007 at 16:08 UT | Xi | 3A | ||||||||
| 98, CZ-3 | 07031 | Chinasat 6B | 5 Jul 2007 at 12:08 UT | Xi | 3B | ||||||||
| 99, CZ-4 | 07042 | CBERS 2B | 19 Sep 2007 at 03:26 UT | Xi | 4B | ||||||||
| 100, CZ-3 | 07051 | Chang'e 1 | 24 Oct 2007 at 10:05 UT | Xi | 3A | Moon probe, non-earth orbit | |||||||
| 101, CZ-4 | 07055 | Yaogan 3 | 11 Nov 2007 at 22:48 UT | Ty | 4C | ||||||||
| 102, CZ-3 | 08019 | DFH 76 | 25 Apr 2008 at 22:16 UT | Xi | 3C | ||||||||
| 103, CZ-4 | 08026 | DFH 77 | 27 May 2008 at 03:02 UT | Ty | 4C | ||||||||
| 104, CZ-3 | 08028 | Chinasat 9 | 9 Jun 2008 at 12:15 UT | Xi | 3B | ||||||||
| 105, CZ-2 | 08041 |
DFH 78 DFH 79 | 6 Sep 2008 at 03:25 UT | Ty | 2C | ||||||||
| 106, CZ-2 | 08047 |
Shenzou 7 Bx 1 (unknown sub-satellite, 40 kg) | 25 Sep 2008 at 13:10 UT | Ji | 2F |
Manned mission 200 x 344 km x 43° | |||||||
| 107, CZ-4 | 08053 |
DFH 80 DFH 81 | 25 Oct 2008 at 00:15 UT | Ty | 4B | ||||||||
| 108, CZ-3 | 08055 | Venesat 1 | 29 Oct 2008 at 16:53 UT | Xi | 3B | ||||||||
| 109, CZ-2 | 08056 |
A: DFH 82 B: Chuangxin 2 | 5 Nov 2008 at 00:15 UT | Ji | 2D | ||||||||
| 110, CZ-2 | 08061 | Yaogan 4 | 01 Dec 2008 at 04:42 UT | Ji | 2D | ||||||||
| 111, CZ-4 | 08064 | Yaogan 5 | 15 Dec 2008 at 03:22 UT | Ty | 4B | ||||||||
| 112, CZ-3 | 08066 | DFH 83 | 23 Dec 2008 at 00:54 UT | Xi | 3A | ||||||||
| 113, CZ-3 | 09018 | DFH 84 | 15 Apr 2009 at 16:16 UT | Xi | 3C | ||||||||
| 114, CZ-2 | 09021 | Yaogan 6 | 22 Apr 2009 at 02:55 UT | Ty | 2C | ||||||||
| 115, CZ-3 | 09046 | Palapa D | 31 Aug 2009 at 09:28 UT | Xi | 3B | Partial failure of the 3rd stage. Payload left in 225 x 21.160 km x 22° | |||||||
| 116, CZ-2 | 09061 | DFH 85 | 12 Nov 2009 at 02:45 UT | Ji | 2C | ||||||||
| 117, CZ-2 | 09069 | Yaogan 7 | 09 Dec 2009 at 08:42 UT | Ty | 2D | ||||||||
| 118, CZ-4 | 09072 |
A: Yaogan 8 B: XiWang 1 | 15 Dec 2009 at 02:31 UT | Ty | 4C | ||||||||
| 119, CZ-3 | 10001 | DFH 86 | 16 Jan 2010 at 16:12 UT | Xi | 3C | ||||||||
| 120, CZ-4 | 10009 |
A:
Yaogan 9 B: Yaogan 9B C: Yaogan 9C | 5 Mar 2010 at 04:55 UT | Ji | 4C | ||||||||
| 121, CZ-3 | 10024 | DFH 87 | 2 Jun 2010 at 15:53 UT | Xi | 3C | ||||||||
| 122, CZ-2 | 10027 | DFH 88 | 15 Jun 2010 at 01:39 UT | Ji | 2D | ||||||||
| 123, CZ-3 | 10036 | DFH 89 | 31 Jul 2010 at 21:30 UT | Xi | 3A | ||||||||
| 124, CZ-4 | 10038 | Yaogan 10 | 9 Aug 2010 at 22:49 UT | Ty | 4C | ||||||||
| 125, CZ-2 | 10040 | DFH 90 | 24 Aug 2010 at 07:10 UT | Ji | 2D | ||||||||
| 126, CZ-3 | 10042 | Sinosat 6 | 04 Sep 2010 at 16:14 UT | Xi | 3B | ||||||||
| 127, CZ-2 | 10047 |
A: Yaogan 11 B: Zheda Pixing 1A-1 C: Zheda Pixing 1A-2 | 22 Sep 2010 at 02:42 UT | Ji | 2D | ||||||||
| 128, CZ-3 | 10050 | Chang'e 2 | 2 Oct 2010 at 10:59 UT | Xi | 3C | Moon probe, non-earth orbit | |||||||
| 129, CZ-4 | 10051 |
A: DFH 91 B: DFH 92 | 6 Oct 2010 at 00:49 UT | Ty | 4B | ||||||||
| 130, CZ-3 | 10057 | DFH 93 | 31 Oct 2010 at 16:26 UT | Xi | 3C | ||||||||
| 131, CZ-4 | 10059 | DFH 94 | 5 Nov 2010 at 18:37 UT | Ty | 4C | ||||||||
| 132, CZ-3 | 10064 | DFH 95 | 24 Nov 2010 at 16:09 UT | Xi | 3A | ||||||||
| 133, CZ-3 | 10068 | DFH 96 | 17 Dec 2010 at 20:20 UT | Xi | 3A | ||||||||
| 134, CZ-3 | 11013 | DFH 97 | 9 Apr 2011 at 20:47 UT | Xi | 3A | ||||||||
| 135, CZ-3 | 11026 | Sinosat 5 | 20 Jun 2011 at 16:13 UT | Xi | 3B | ||||||||
| 131, CZ-2 | 11030 | DFH 98 | 6 Jul 2011 at 04:28 UT | Ji | 2C | ||||||||
| 132, CZ-3 | 11032 | DFH 99 | 11 Jul 2011 at 15:41 UT | Xi | 3C | ||||||||
| 133, CZ-3 | 11038 | DFH 100 | 26 Jul 2011 at 21:44 UT | Xi | 3A | ||||||||
| 134, CZ-2 | 11039 | DFH 101 | 29 Jul 2011 at 07:42 UT | Ji | 2C | ||||||||
| 135, CZ-3 | 11042 | Paksat 1R | 11 Aug 2011 at 16:15 UT | Xi | 3B | ||||||||
| 136, CZ-4 | 11043 | DFH 102 | 15 Aug 2011 at 22:57 UT | Ty | 4B | ||||||||
| 137, CZ-2 | n/a | DFH (Shijian 11-04) | 18 Aug 2011 at 09:28 UT | Jq | 2C | Failure: second stage did not ignite (failed connection between components) | |||||||
| 138, CZ-3 | 11047 | Chinasat 1A | 18 Sep 2011 at 16:33 UT | Xi | 3B/E | ||||||||
| 139, CZ-2 | 11052 | Tiangong 1 | 29 Sep 2011 at 13:36 UT | Ji | 2FT1 | 8500 kg, 10.4 m x 3.35 m diameter, first manned module | |||||||
| 140, CZ-3 | 11057 | Eutelsat W3C | 7 Oct 2011 at 08:20 UT | Xi | 3B/E | ||||||||
| 141, CZ-3 | 11063 | Shenzhou 8 | 31 Oct 2011 at 21:58 UT | Ji | 2F/H | To rendezvous with Tiangong 1 | |||||||
| 142, CZ-4 | 11066 |
A: DFH 103 B: Yaogan 12 | 09 Nov 2011 at 03:21 UT | Ty | 4B | ||||||||
| 143, CZ-2 | 11068 |
A:
Chuangxin 3 B: DFH 104 | 20 Nov 2011 at 00:15 UT | Ji | 2D | ||||||||
| 144, CZ-2 | 11072 | Yaogan 13 | 30 Nov 2011 at 18:50 UT | Ty | 2C | ||||||||
| 145, CZ-3 | 11073 | DFH 105 | 2 Dec 2011 at 21:07 UT | Xi | 3A | ||||||||
| 146, CZ-3 | 11077 | Nigcomsat 1R | 19 Dec 2011 at 16:41 UT | Xi | 3B | ||||||||
| 147, CZ-4 | 11079 | CBERS 2C | 22 Dec 2011 at 03:26 UT | Ty | 4B | ||||||||
| 148, CZ-4 | 12001 |
A: DFH 106 B: Vesselsat 2 | 9 Jan 2012 at 03:17 UT | Ty | 4B | ||||||||
| 149, CZ-3 | 12002 | DFH 107 | 13 Jan 2012 at 00:56 UT | Xi | 3A | ||||||||
| 150, CZ-3 | 12008 | DFH 108 | 24 Feb 2012 at 16:12 UT | Xi | 3C | ||||||||
| 151, CZ-3 | 12013 | Apstar 7 | 31 Mar 2012 at 10:27 UT | Xi | 3B/E | ||||||||
| 152, CZ-3 | 12018 |
DFH 109 DFH 110 | 29 Apr 2012 at 20:50 UT | Xi | 3B | ||||||||
| 153, CZ-2 | 12020 | DFH 111 | 6 May 2012 at 07:10 UT | Ji | 2D | ||||||||
| 154, CZ-4 | 12021 |
A:
Yaogan 14 B: DFH 112 | 10 May 2012 at 07:06 UT | Ty | 4B | ||||||||
| 155, CZ-3 | 12028 | Chinasat 2A | 26 May 2012 at 15:56 UT | Xi | 3B/E | ||||||||
| 156, CZ-4 | 12029 | Yaogan 15 | 29 May 2012 at 07:31 UT | Ty | 4C | ||||||||
| 157, CZ-2 | 12032 | Shenzhou 9 | 16 Jun 2012 at 10:37 UT | Ji | 2F | ||||||||
| 158, CZ-3 | 12040 | DFH 113 | 25 Jul 2012 at 15:43 UT | Xi | 3C | ||||||||
| 159, CZ-3 | 12050 |
DFH 114 DFH 115 | 18 Sep 2012 at 18:30 UT | Xi | 3B/E | ||||||||
| 160, CZ-2 | 12052 | VRSS 1 | 30 Sep 2012 at 04:12 UT | Ji | 2D | ||||||||
| 161, CZ-2 | 12056 |
DFH 116 DFH 117 | 13 Oct 2012 at 03:25 UT | Ty | 2C | ||||||||
| 162, CZ-3 | 12059 | DFH 118 | 25 Oct 2012 at 15:35 UT | Xi | 3C | ||||||||
| 163, CZ-2 | 12064 |
A: DFH 119 B: DFH 120 C: DFH 121 | 18 Nov 2012 at 22:53 UT | Ty | 2C | ||||||||
| 164, CZ-4 | 12066 | Yaogan 16 | 25 Nov 2012 at 04:06 UT | Ji | 4C | ||||||||
| 165, CZ-3 | 12067 | Chinasat 12 | 27 Nov 2012 at 10:13 UT | Xi | 3B/E | ||||||||
| 166, CZ-2 | 12073 | Gokturk 2 | 18 Dec 2012 at 16:12 UT | Ji | 2D | ||||||||
| 167, CZ-2 | 13018 |
A: Gaofen 1 B: Nee 01 Pegaso C: Turksat 3USat D: Cubebug 1 | 26 Apr 2013 at 04:13 UT | Ji | 2D | ||||||||
| 168, CZ-3 | 13020 | Chinasat 11 | 1 May 2013 at 16:06 UT | Xi | 3B/E | ||||||||
| 169, CZ-2 | 13029 | Shenzhou 10 | 11 Jun 2013 at 09:38 UT | Ji | 2F | ||||||||
| 170, CZ-2 | 13035 | DFH 122 | 15 Jul 2013 at 09:27 UT | Ji | 2C | ||||||||
| 171, CZ-4 | 13037 |
A:
DFH 123 B: DFH 124 C: Chuangxin 3A | 19 Jul 2013 at 23:37 UT | Ty | 4C | ||||||||
| 172, CZ-4 | 13046 | Yaogan 17 | 1 Sep 2013 at 19:16 UT | Ji | 4C | ||||||||
| 173, CZ-4 | 13052 | DFH 125 | 23 Sep 2013 at 03:07 UT | Ty | 4C | ||||||||
| 174, CZ-4 | 13058 | DFH 127 | 25 Oct 2013 at 03:50 UT | Ji | 4B | ||||||||
| 175, CZ-2 | 13059 | Yaogan 18 | 29 Oct 2013 at 02:50 UT | Ty | 2C | ||||||||
| 176, CZ-4 | 13065 | Yaogan 19 | 20 Nov 2013 at 03:31 UT | Ty | 4C | ||||||||
| 177, CZ-2 | 13068 | DFH 128 | 25 Nov 2013 at 02:12 UT | Ji | 2D | ||||||||
| 178, CZ-3 | 13070 |
Chang'e 3 Yutu rover | 1 Dec 2013 at 17:30 UT | Xi | 3B | lunar mission | |||||||
| 179, CZ-4 | n/a | CBERS 3 | 9 Dec 2013 at 03:26 UT | Ty | 4B | failure: 3rd stage failure (clogged fuel line) | |||||||
| 180, CZ-3 | 13075 | TKsat 1 | 20 Dec 2013 at 17:02 UT | Xi | 3B | ||||||||
| 181, CZ-2 | 14014 | DFH 129 | 31 Mar 2014 at 02:46 UT | Ji | 2C | ||||||||
| 182, CZ-4 | 14047 | Yaogan 20 | 9 Aug 2014 at 05:45 UT | Ji | 4C | ||||||||
| 183, CZ-4 | 14049 |
A: Gaofen 2 B: CanX 3D | 19 Aug 2014 at 03:15 UT | Ty | 4B | ||||||||
| 184, CZ-2 | 14051 |
A: DFH 130 B: Chuangxin 4 | 4 Sep 2014 at 00:15 UT | Ji | 2D | ||||||||
| 185, CZ-4 | 14053 |
A:
Yaogan 21 B: DFH 131 | 8 Sep 2014 at 03:22 UT | Ty | 4B | ||||||||
| 186, CZ-2 | 14059 | DFH 132 | 28 Sep 2014 at 05:13 UT | Ji | 2C | ||||||||
| 187, CZ-4 | 14063 | Yaogan 22 | 20 Oct 2014 at 06:31 UT | Ty | 4C | ||||||||
| 188, CZ-3 | 14065 |
A: Chang'e 5-T1 B: 4M (attached to upper-stage) | 23 Oct 2014 at 17:59 UT | Xi | 3C/G2 |
lunar return module 4M owned by LuxSpace, carries a radio amateur beacon, first private mission around the Moon | |||||||
| 189, CZ-2 | 14066 | DFH 133 | 27 Oct 2014 at 06:59 UT | Jy | 2C | ||||||||
| 190, CZ-2 | 14071 | Yaogan 23 | 14 Nov 2014 at 18:53 UT | Ty | 2C | ||||||||
| 191, CZ-2 | 14072 | Yaogan 24 | 20 Nov 2014 at 07:12 UT | Jy | 2D | ||||||||
| 192, CZ-4 | 14079 | Cbers 4 | 7 Dec 2014 at 03:26 UT | Ty | 4B | ||||||||
| 193, CZ-4 | 14080 | Yaogan 25 | 10 Dec 2014 at 19:33 UT | Ji | 4C | ||||||||
| 194, CZ-4 | 14088 | Yaogan 26 | 27 Dec 2014 at 03:22 UT | Ty | 4B | ||||||||
| 195, CZ-3 | 14090 | DFH 135 | 31 Dec 2014 at 01:02 UT | Xi | 3A | ||||||||
| 196, CZ-3 | 15019 | DFH 136 | 30 Mar 2015 at 13:52 UT | Xi | 3C/YZ1 | Carried the Yuanzheng 1 4th stage | |||||||
| 197, CZ-4 | 15030 | Gaofen 8 | 26 Jun 2015 at 06:22 UT | Ty | 4B | ||||||||
| 198, CZ-3 | 15037 |
DFH 137 DFH 138 | 25 Jul 2015 at 12:29 UT | Xi | 3B/YZ1 | ||||||||
| 199, CZ-4 | 15040 | Yaogan 27 | 27 Aug 2015 at 02:31 UT | Ty | 4C | ||||||||
| 200, CZ-3 | 15046 | DFH 139 | 12 Sep 2015 at 15:42 UT | Xi | 3B | ||||||||
| 201, CZ-2 | 15047 | Gaofen 9 | 14 Sep 2015 at 04:45 UT | Ji | 2D | ||||||||
| 202, CZ-3 | 15053 | DFH 140 | 29 Sep 2015 at 23:13 UT | Xi | 3B | ||||||||
| 203, CZ-2 | 15057 |
A: Jilin Lqsat B: Jilin Lingqiao 1-01 C: Jilin Lingqiao 1-02 D: Jilin 1 | 7 Oct 2015 at 04:13 UT | Ji | 2C | 640 x 664 km x 98° | |||||||
| 204, CZ-3 | 15059 | Apstar 9 | 16 Oct 2015 at 16:16 UT | Xi | 3B | ||||||||
| 205, CZ-2 | 15061 | DFH 141 | 26 Oct 2015 at 07:10 UT | Ji | 2D | ||||||||
| 206, CZ-3 | 15063 | Chinasat 2C | 3 Nov 2015 at 16:25 UT | Xi | 3B | ||||||||
| 207, CZ-4 | 15064 | Yaogan 28 | 8 Nov 2015 at 07:06 UT | Ty | 4B | ||||||||
| 208, CZ-3 | 15067 | Laosat 1 | 20 Nov 2015 at 16:07 UT | Xi | 3B/G2 | ||||||||
| 209, CZ-4 | 15069 | Yaogan 29 | 26 Nov 2015 at 21:24 UT | Ty | 4C | ||||||||
| 210, CZ-3 | 15073 | Chinasat 1C | 9 Dec 2015 at 16/46 UT | Xi | 3B/G2 | ||||||||
| 211, CZ-2 | 15078 | DFH 142 | 17 Dec 2015 at 00:12 UT | Ji | 2D | ||||||||
| 212, CZ-3 | 15083 | Gaofen 4 | 28 Dec 2015 at 16:05 UT | Xi | 3B | ||||||||
| 213, CZ-3 | 16001 | Belintersat 1 | 15 Jan 2016 at 16:57 UT | Xi | 3B/G2 | ||||||||
| 214, CZ-3 | 16006 | DFH 143 | 1 Feb 2016 at 07:29 UT | Xi | 3C/YZ1 | ||||||||
| 215, CZ-3 | 16021 | DFH 144 | 29 Mar 2016 at 20:11 UT | Xi | 3A | ||||||||
| 216, CZ-2 | 16023 | DFH 145 | 6 Apr 2016 at 17:38 UT | Ji | 2D | ||||||||
| 217, CZ-2 | 16029 | Yaogan 30 | 15 May 2016 at 02:43 UT | Ji | 2D | ||||||||
| 218, CZ-4 | 16033 |
A: DFH 146 B: Nusat 1 C: Nusat 2 | 30 May 2016 at 03:17 UT | Ty | 4B | ||||||||
| 219, CZ-3 | 16037 | DFH 147 | 12 Jun 2016 at 15:30 UT | Xi | 3C | ||||||||
| 220, CZ-4 | 16043 | DFH 152 | 29 Jun 2016 at 03:21 UT | Ji | 4B | ||||||||
| 221, CZ-3 | 16048 | DFH 153 | 5 Aug 2016 at 16:22 UT | Xi | 3B/G2 | ||||||||
| 222, CZ-4 | 16049 | Gaofen 3 | 9 Aug 2016 at 22:55 UT | Ty | 4C | ||||||||
| 223, CZ-2 | 16051 |
A: DFH 154 B: 3CAT 2 C: DFH 155 | 15 Aug 2016 at 17:40 UT | Ji | 2D | ||||||||
| 224, CZ-4 | n/a | Gaofen 10 | 31 Aug 2016 | Ty | 4C | Failure | |||||||
| 224, CZ-2 | 16057 | Tiangong 2 | 15 Sep 2016 at 14:00 UT | Ji | 2F |
8.6 tons mini space station 380 km altitude Released a secondary satellite | |||||||
| 225, CZ-2 | 16061 | Shenzhou 11 | 16 Oct 2016 at 23:30 UT | Ji | 2F | 2 astronauts to mini space station | |||||||
| 226, CZ-2 | 16068 | Yunhai 1 | 11 Nov 2016 at 23:14 UT | Ji | 2D | ||||||||
| 227, CZ-3 | 16072 | DFH 159 | 22 Nov 2016 at 15:24 UT | Xi | 3C/G2 | ||||||||
| 228, CZ-3 | 16077 | DFH 160 | 10 Dec 2016 at 16:11 UT | Xi | 3B | ||||||||
| 229, CZ-2 | 16081 |
A: Tansat B: DFH 163 (Yijian) C: DFH 161 (Spark 1) D: DFH 162 (Spark 2) | 21 Dec 2016 at 15:22 UT | Ji | 2D | ||||||||
| 230, CZ-2 | 16083 |
A: Superview 1-01 B: Superview 1-02 C: DFH 164 (BY70-1) | 28 Dec 2016 at 03:23 UT | Ty | 2D | Partial failure: satellites left in lower than expected orbit | |||||||
| 231, CZ-3 | 17001 | DFH 165 | 5 Jan 2017 at 15:18 UT | Xi | 3B | ||||||||
| 232, CZ-3 | 17018 | Chinasat 16 | 12 Apr 2017 at 11:04 UT | Xi | 3B/G2 | ||||||||
| 233, CZ-4 | 17034 |
A: Huiyan B: Zhuhai 1-01 C: NuSat 3 D: Zhuhai 1-02 | 15 Jun 2017 at 03:00 UT | Ji | 4B | ||||||||
| 234, CZ-3 | 17035 | Sinosat 4 | 18 Jun 2017 at 16:11 UT | Xi | 3B |
Partial
failure: satellite left in wrong orbit, probably a 3rd stage failure 193 x 16357 km x 25° | |||||||
| 235, CZ-2 | 17058 | Yaogan 30-01 (3 satellites) | 29 Sep 2017 at 04:20 UT | Xi | 2C | ||||||||
| 236, CZ-2 | 17060 | VRSS 2 | 9 Oct 2017 at 04:13 UT | Ji | 2D | ||||||||
| 237, CZ-3 | 17069 |
A: DFH 170 B: DFH 171 | 5 Nov 2017 at 11:45 UT | Xi | 3B | ||||||||
| 238, CZ-4 | 17072 |
A: DFH 172 B: DFH 173 | 14 Nov 2017 at 18:35 UT | Ty | 4C | ||||||||
| 239, CZ-2 | 17075 | Yaogan 30-02 (3 satellites) | 24 Nov 2017 at 18:10 UT | Xi | 2C | ||||||||
| 240, CZ-2 | 17077 | LKW 1 | 3 Dec 2017 at 04:11 UT | Ji | 2D | ||||||||
| 241, CZ-3 | 17078 | Alcomsat 1 | 10 Dec 2017 at 16:40 UT | Xi | 3B | 200 x 41991 km x 26.4° | |||||||
| 242, CZ-2 | 17084 | LKW 2 | 23 Dec 2017 at 04:14 UT | Ji | 2D | ||||||||
| 243, CZ-2 | 17085 | Yaogan 30-03 (3 satellites) | 25 Dec 2017 at 19:44 UT | Xi | 2C | ||||||||
| 244, CZ-2 | 18002 |
A: Superview 1-03 B: Superview 1-04 | 09 Jan 2018 at 03:24 UT | Ty | 2D | ||||||||
| 245, CZ-3 | 18003 |
A: DFH 174 B: DFH 175 | 11 Jan 2018 at 23:18 UT | Xi | 3B | ||||||||
| 246, CZ-2 | 18006 | LKW 3 | 13 Jan 2018 at 07:10 UT | Ji | 2D | ||||||||
| 247, CZ-2 | 18011 |
A:
DFH 179 BCD: Yaogan 30-04 (3 satellites) | 25 Jan 2018 at 05:39 UT | Xi | 2C | ||||||||
| 248, CZ-2 | 18015 |
A: DFH 180 C: Zhang Heng 1 D: Nusat 4 E: Gomx 4B F: Gomx 4A H: DFH 181 K: Nusat 5 | 2 Feb 2018 at 07:51 UT | Ji | 2D | ||||||||
| 249, CZ-3 | 18018 |
A:
DFH 182 B: DFH 183 | 12 Feb 2018 at 05:03 UT | Xi | 3B | ||||||||
| 250, CZ-2 | 18025 | LKW 4 | 17 Mar 2018 at 07:10 UT | Ji | 2D | ||||||||
| 251, CZ-3 | 18029 |
A:
DFH 184 B: DFH 185 | 29 Mar 2018 at 17:56 UT | Xi | 3B | ||||||||
| 252, CZ-4 | 18031 |
A: Gaofen 1-02 B: Gaofen 1-03 D: Gaofen 1-04 | 31 Mar 2018 at 03:22 UT | Ty | 4C | ||||||||
| 253, CZ-4 | 18034 |
Yaogan 31-01
(3 satellites) D: DFH 186 | 10 Apr 2018 at 04:25 UT | Ji | 4C | ||||||||
| 254, CZ-3 | 18041 | Apstar 6C | 3 May 2018 at 16:06 UT | Xi | 3B | ||||||||
| 255, CZ-4 | 18043 | Gaofen 5 | 8 May 2018 at 18:28 UT | Ty | 4C | ||||||||
| 256, CZ-4 | 18045 |
A: DFH 187 B: DFH 188 C: DFH 189 | 20 May 2018 at 21:28 UT | Xi | 4C | Earth-Moon transfer orbit | |||||||
| 257, CZ-2 | 18048 |
A: Gaofen 6 B: DFH 190 | 2 Jun 2018 at 04:13 UT | Ji | 2D | ||||||||
| 258, CZ-3 | 18050 | DFH 191 | 5 Jun 2018 at 13:07 UT | Xi | 3A | ||||||||
| 259, CZ-2 | 18054 |
A:
DFH 192 B: DFH 193 | 27 Jun 2018 at 03:30 UT | Xi | 2C | ||||||||
| 260, CZ-2 | 18056 |
A: PakTES 1A B: PRSS 1 | 9 Jul 2018 at 03:56 UT | Ji | 2C | SMA solid upper stage motor | |||||||
| 261, CZ-3 | 18057 | DFH 194 | 9 Jul 2018 at 20:58 UT | Ji | 3A | ||||||||
| 262, CZ-3 | 18062 |
A:
DFH 195 B: DFH 196 | 29 Jul 2018 at 01:40 UT | Xi | 3B | ||||||||
| 263, CZ-4 | 18063 | Gaofen 11 | 31 Jul 2018 at 03:00 UT | Ty | 4B | ||||||||
| 264, CZ-3 | 18067 |
A:
DFH 197 B: DFH 198 | 24 Aug 2018 at 23:52 UT | Xi | 3B | ||||||||
| 265, CZ-2 | 18068 | DFH 199 | 7 Sep 2018 at 03:15 UT | Ty | 2C | ||||||||
| 266, CZ-3 | 18072 |
A:
DFH 200 B: DFH 201 | 19 Sep 2018 at 14:07 UT | Xi | 3B | ||||||||
| 267, CZ-2 | 18077 | Yaogan 32-01 A B | 10 Oct 2018 at 04:43 UT | Ji | 2C | First use of the YZ-1S upper stage | |||||||
| 268, CZ-3 | 18078 |
A:
DFH 203 B: DFH 204 | 15 Oct 2018 at 04:23 UT | Xi | 3B | ||||||||
| 269, CZ-4 | 18081 | DFH 205 | 24 Oct 2018 at 22:57 UT | Ty | 4B | ||||||||
| 270, CZ-2 | 18083 |
A:
CFOsat B: Tongchuan 1 E: CubeBel 1 TY1-02 TY1-03 TY4-01 TY4-02 G: Tianqi 1 | 29 Oct 2018 at 00:43 UT | Ji | 2C | ||||||||
| 271, CZ-3 | 18085 | DFH 206 | 2 Nov 2018 at 15:57 UT | Xi | 3B/G2 | ||||||||
| 272, CZ-3 | 18093 |
A:
DFH 207 B: DFH 208 | 18 Nov 2018 | Xi | 3B | ||||||||
| 273, CZ-2 | 18094 |
A: Tianzhi 1 B: Tansuo 6 C: Tianping 1A D: DFH 209 E: Tianping 1B | 19 Nov 2018 at 23:40 UT | Ji | 2D | ||||||||
| 274, CZ-2 | 18102 |
A:
SaudiSat 5A C: SaudiSat 5B D: DFH 210 Tianyi DF-1 TFSTAR Xinjiang Jiaotong 1 Piao chong 2 Piao chong 3 Piao chong 4 Piao chong 5~ Piao chong 6 Piao chong 7~ | 7 Dec 2018 at 04:12 UT | Ji | 2D | ||||||||
| 275, CZ-3 | 18103 | Chang'e 4 | 7 Dec 2018 at 18:23 UT | Xi | 2B | Includes a lunar rover | |||||||
| 276, CZ-3 | 18110 | DFH 211 | 24 Dec 2018 at 16:53 UT | Xi | 3C | ||||||||
| 277, CZ-2 | 18112 |
A:
Yunhai 2-1 B: Yunhai 2-2 C: Yunhai 2-3 D: Yunhai 2-4 E: Yunhai 2-5 H: Hongyan 1 G: Yunhai 2-6 | 29 Dec 2018 at 08:00 UT | Ji | 2D | First use of the YZ-3 upper stage | |||||||
| 278, CZ-3 | 19001 | Chinasat 2D | 10 Jan 2019 at 17:11 UT | Xi | 3B | ||||||||
| 279, CZ-3 | 19012 | Chinasat 6C | 9 Mar 2019 at 16:28 UT | Xi | 3B | ||||||||
| 280, CZ-3 | 19017 | Tianlian 2-01 | 31 Mar 2019 at 15:51 UT | Xi | 3B/G2 | ||||||||
| 281, CZ-3 | 19023 | DFH 213 | 20 Apr 2019 at 14:41 UT | Xi | 3B/G2 | ||||||||
| 282, CZ-4 | 19024 |
A: DFH 214 B: DFH 215 | 29 Apr 2019 at 22:52 UT | Ty | 4B | ||||||||
| 283, CZ-3 | 19027 | DFH 216 | 17 May 2019 at 15:48 UT | Xi | 3C | ||||||||
| 284, CZ-4 | n/a | Yaogan 33 | 22 May 2019 | Ty | 4C | Failure: 3rd stage | |||||||
| 285, CZ-3 | 19035 | DFH 220 | 24 Jun 2019 at 18:05 UT | Xi | 3B/G2 | ||||||||
| 286, CZ-2 | 19045 | ABC: Yaogan 30-05 (3 satellites) | 26 Jul 2019 at 03:57 UT | Xi | 2C | ||||||||
| 287, CZ-3 | 19053 | Chinasat 18 | 19 Aug 2019 at 12:03 UT | Xi | 3B | ||||||||
| 288, CZ-4 | 19059 |
A:
DFH 225 (ZY-1-02D) B: DFH 226 (BNU 1) C: DFH 227 (Taurus 1) | 12 Sep 2019 at 03:26 UT | Ty | 4B | ||||||||
| 289, CZ-3 | 19061 |
A: DFH 228 B: DFH 229 | 22 Sep 2019 at 21:10 UT | Xi | 3B | ||||||||
| 290, CZ-2 | 19063 | Yunhai 1-2 | 25 Sep 2019 at 00:54 UT | Ji | 2D | ||||||||
| 291, CZ-4 | 19066 | Gaofen 10R | 4 Oct 2019 at 18:51 UT | Ty | 4C | ||||||||
| 292, CZ-3 | 19070 | DFH 230 | 17 Oct 2019 at 15:21 UT | Xi | 3B | ||||||||
| 293, CZ-4 | 19072 |
A: Gaofen 7 B: DFH 231 (SSES 1) C: DFH 232 (Huangpu 1) D: DFH 233 (TY1-08) | 03 Nov 2019 at 03:22 UT | Ty | 4B | ||||||||
| 294, CZ-3 | 19073 | DFH 234 (Beidou) | 04 Nov 2019 at 17:43 UT | Xi | 3B/G2 | ||||||||
| 295, CZ-3 | 19078 |
A: DFH 235 (Beidou) B: DFH 236 (Beidou) | 23 Nov 2019 at 00:55 UT | Xi | 3B | ||||||||
| 296, CZ-4 | 19082 | Gaofen 12 | 27 Nov 2019 at 23:52 UT | Ty | 4C | ||||||||
| 297, CZ-3 | 19090 |
A: DFH 237 (Beidou) B: DFH 238 (Beidou) | 16 Dec 2019 at 07:22 UT | Xi | 3A | ||||||||
| 298, CZ-4 | 19093 |
A: DFH 242 (Tianqin 1) E: CBERS 4A G: FloripaSat 1 ETRSS 1sat_etrss_1 DFH 239 (Weilai 1R) DFH 240 (Tianyan 1) DFH 241 (Tianyan 2) Yuheng Shuntian | 20 Dec 2019 at 03:22 UT | Ty | 4B | ||||||||
| 299, CZ-3 | 20002 | DFH 244 (TJS 5) | 7 Jan 2020 at 15:20 UT | Xi | 3B/G2 | ||||||||
| 300, CZ-2 | 20003 |
A:
Jilin 1 Kuanfu 1 C: Nusat 7 D: Nusat 8 Tianqi 5 | 15 Jan 2020 at 02:53 UT | Ty | 2D | ||||||||
| 301, CZ-2 | 20014 |
A:
DFH 245 B: DFH 246 C: DFH 247 D: DFH 248 XJS F~ | 19 Feb 2020 at 21:07 UT | Xi | 2D | 474 x 482 km x 35° | |||||||
| 302, CZ-3 | 20017 | DFH 249 | 9 Mar 2020 at 11:55 UT | Xi | 3B/G2 | ||||||||
| 303, CZ-2 | 20021 | ABC: Yaogan 30-06 (3 satellites) | 24 Mar 2020 at 03:43 UT | Xi | 2C | 591 x 602 km x 35° | |||||||
| 304, CZ-3 | n/a | Palapa N1 | 9 Apr 2020 at 11:46 UT | Xi | 3B/G2 | Failure of 3rd stage | |||||||
| 305, CZ-2 | 20034 |
A:
Head 4 B: Gaofen 9-2 | 31 May 2020 at 08:53 UT | Ji | 2D | ||||||||
| 306, CZ-2 | 20036 | DFH 252 | 10 Jun 2020 at 18:31 UT | Ty | 2C | ||||||||
| 307, CZ-2 | 20039 |
A:
Gaofen 9-3 B: Zheda Pixing 3A C: Head 5 | 17 Jun 2020 at 07:19 UT | Ji | 2D | ||||||||
| 308, CZ-3 | 20040 | DFH 253 | 23 Jun 2020 at 01:43 UT | Xi | 3B/G2 | ||||||||
| 309, CZ-4 | 20042 |
A:
Gaofen Duomo B: DFH 254 | 3 Jul 2020 at 03:10 UT | Ty | 4B | ||||||||
| 310, CZ-2 | 20043 | DFH 255 | 4 Jul 2020 at 23:44 UT | Ji | 2D | ||||||||
| 311, CZ-3 | 20045 | Apstar 6D | 9 Jul 2020 at 12:10 UT | Xi | 3B/G2 | ||||||||
| 312, CZ-4 | 20051 |
A: DFH 256 B: Tianqi 10 C: DFH 257 | 25 Jul 2020 at 03:13 UT | Ty | 4B | ||||||||
| 313, CZ-2 | 20054 |
A: Gaofen 9-4 B: DFH 258 | 6 Aug 2020 at 04:01 UT | Ji | 2D | ||||||||
| 314, CZ-2 | 20058 |
A: Gaofen 9-5 B: DGSW C: DFH 259 | 23 Aug 2020 at 02:27 UT | Ji | 2D | ||||||||
| 315, CZ-2 | 20063 | CSSHQ / Chongfu Shiyong Sh. Han.Qi / Chinese test winged vehicle | 4 Sep 2020 at 07:30 UT | Ji | 2F | landed after 2 days in orbit | |||||||
| 316, CZ-4 | 20064 | Gaofen 11-02 | 7 Sep 2020 at 05:57 UT | Ty | 4B | ||||||||
| 317, CZ-4 | 20066 | DFH 260 | 21 Sep 2020 at 05:40 UT | Ji | 4B | ||||||||
| 318, CZ-4 | 20067 |
A: DFH 261 B: DFH 262 | 27 Sep 2020 at 03:23 UT | Ty | 4B | ||||||||
| 319, CZ-4 | 20071 | Gaofen 13 | 11 Oct 2020 at 16:57 UT | Xi | 3B | ||||||||
| 320, CZ-2 | 20076 |
Yaogan 30-07
U V W Tianqi 6 | 26 Oct 2020 at 15:19 UT | Xi | 2C | ||||||||
| 321, CZ-3 | 20082 | DFH 263 | 12 Nov 2020 at 15:59 UT | Xi | 3B/G2 | ||||||||
| 322, CZ-3 | 20092 | Gaofen 14 | 6 Dec 2020 at 03:58 UT | Xi | 3B/G5 | ||||||||
| 323, CZ-4 | 20103 |
A: Yaogan 33-01 B: Weina 2 | 27 Dec 2020 at 15:44 UT | Ji | 4C | ||||||||
| 324, CZ-3 | 21003 | Tiantong 1-3 | 20 Jan 2021 at 16:25 UT | Xi | 3B/G2 | ||||||||
| 325, CZ-4 | 21007 | Yaogan 31-02 D E F | 29 Jan 2021 at 04:47 UT | Ji | 4C | ||||||||
| 326, CZ-3 | 21010 | DFH 267 | 4 Feb 2021 at 15:36 UT | Xi | 3B/G2 | ||||||||
| 327, CZ-4 | 21014 | Yaogan 31-03 G H I | 24 Feb 2021 at 02:22 UT | Ji | 4C | ||||||||
| 328, CZ-4 | 21020 | Yaogan 31-04 J K L | 13 Mar 2021 at 02:20 UT | Ji | 4C | ||||||||
| 329, CZ-4 | 21026 | Gaofen 12-02 | 30 Mar 2021 at 22:45 UT | Ji | 4C | ||||||||
| 330, CZ-4 | 21028 | DFH 269 | 8 Apr 2021 at 23:01 UT | Ty | 4B | ||||||||
| 331, CZ-4 | 21037 | Yaogan 34-01 | 30 Apr 2021 at 07:27 UTC | Ji | 4C | ||||||||
| 332, CZ-2 | 21039 |
Yaogan 30-08
X Y Z D: Tianqi 12 | 6 May 2021 at 18:11 UT | Xi | 2C | ||||||||
| 333, CZ-4 | 21043 | Haiyang 2D | 19 May 2021 at 04:03 UTC | Ji | 4B | ||||||||
| 334, CZ-4 | 21047 | DFH 270 | 2 Jun 2021 at 16:17 UTC | Xi | 3B | ||||||||
| 335, CZ-2 | 21050 |
A: Beijing 3 B: DFH 271 (Haisi 2) DFH 272 (Tianjian Space Test 1) Yangwang 1 | 11 Jun 2021 at 03:03 UTC | Ty | 2D | 488 x 502 km x 97.5° | |||||||
| 336, CZ-2 | 21053 | Shenzhou 12 | 17 Jun 2021 at 01:22 UTC | Ji | 2F | Crew to Tianhe space station | |||||||
| 337, CZ-2 | 21055 |
ABD: Yaogan 30-09
(3 satellites) E: Tianqi 14 | 18 Jun 2021 at 06:30 UTC | Xi | 2C | ||||||||
| 338, CZ-2 | 21061 |
Jilin 1 Kuanfu 1B Jilin 1 Gaofen 03L-N Xingshidai 10 | 3 Jul 2021 at 02:51 UTC | Ty | 2D | ||||||||
| 339, CZ-4 | 21062 | DFH 273 | 4 Jul 2021 at 23:28 UTC | Ji | 4C | ||||||||
| 340, CZ-3 | 21063 | Tianlian 1-5 | 6 Jul 2021 at 15:53 UTC | Xi | 3C/E | ||||||||
| 341, CZ-2 | 21065 |
Yaogan 30-10
AD AE AF B: Tianqi 15 | 19 Jul 2021 at 00:19 UTC | Xi | 2C | Tested the parachute return of the fairing to land in a controlled manner | |||||||
| 342, CZ-2 | 21067 | Tianhui 1-04 | 29 Jul 2021 at 04:01 UTC | Ji | 2D | ||||||||
| 343, CZ-3 | 21071 | Chinasat 2E | 5 Aug 2021 at 16:30 UTC | Xi | 3B/E | ||||||||
| 344, CZ-4 | 21074 | TianHui 2-02 A and B | 18 Aug 2021 at 22:32 UTC | Ty | 4B | ||||||||
| 345, CZ-2 | 21076 |
DFH 274 DFH 275 DFH 276 | 24 Aug 2021 at 11:15 UTC | Ji | 2C | new 4.2m diameter fairing | |||||||
| 346, CZ-3 | 21077 | DFH 277 | 24 Aug 2021 at 15:41 UTC | Xi | 3B | ||||||||
| 347, CZ-4 | 21079 | Gaofen 5-02 | 7 Sep 2021 at 03:01 UTC | Ty | 4C | ||||||||
| 348, CZ-3 | 21080 | Chinasat 9B | 9 Sep 2021 at 11:50 TUC | Xi | 3B | ||||||||
| 349, CZ-3 | 21087 | DFH 278 | 27 Sep 2021 at 08:30 UTC | Xi | 3B | ||||||||
| 350, CZ-2 | 21091 |
A: Xihe Head 2E & 2F DFH 279 (TianYuan 1) DFH 280 (QX 1) DFH 281 (Jiaoton SW) DFH 282 (Tianshu 1) DFH 283 (Jin Zijing 2) DFH 284 (SSS 1) DFH 285 (SSS 2A) | 14 Oct 2021 at 10:51 UTC | Ty | 2D | ||||||||
| 351, CZ-2 | 21092 | Shenzhou 13 | 15 Oct 2021 at 16:23 UTC | Ji | 2F | ||||||||
| 352, CZ-3 | 21094 | DFH 286 | 24 Oct 2021 at 01:57 UTC | Xi | 3B | ||||||||
| 353, CZ-2 | 21099 | Yaogan 32-02 | 3 Nov 2021 at 07:43 UTC | Ji | 2C | ||||||||
| 354, CZ-2 | 21101 | Yaogan 35-01 | 6 Nov 2021 at 03:00 UTC | Xi | 2D | ||||||||
| 355, CZ-4 | 21107 | Gaofen 11-03 | 20 Nov 2021 at 01:51 UTC | Ty | 4B | ||||||||
| 356, CZ-4 | 21109 | Gaofen 3-02 | 22 Nov 2021 at 23:45 UTC | Ji | 4C | ||||||||
| 357, CZ-3 | 21114 | Chinasat 1D | 26 Nov 2021 at 16:40 UTC | Xi | 3B | ||||||||
| 358, CZ-4 | 21122 |
DFH 291 DFH 292 | 10 Dec 2021 at 00:11 UTC | Ji | 4B | ||||||||
| 359, CZ-3 | 21124 | Tianlian 2-02 / 2B | 13 Dec 2021 at 16:09 UTC | Xi | 3B | ||||||||
| 360, CZ-4 | 21131 |
A: ZiYuan 1-02E B: XiWang 3 | 26 Dec 2021 at 03:11 UTC | Ty | 4C | ||||||||
| 361, CZ-2 | 21134 | TianHui 4-01 A and B | 29 Dec 2021 at 11:13 UTC | Xi | 2D | ||||||||
| 362, CZ-3 | 21135 | DFH 296 | 29 Dec 2021 at 16:43 UTC | Xi | 3B/E | ||||||||
| 363, CZ-2 | 22004 | DFH 297 (SY-13) | 17 Jan 2022 at 02:35 UTC | Ty | 2D | ||||||||
| 364, CZ-4 | 22007 | Ludi Tance 1-01A | 25 Jan 2022 at 23:44 UTC | Ji | 4C | ||||||||
| 365, CZ-4 | 22018 | Ludi Tance 1-01B | 26 Feb 2022 at 23:44 UTC | Ji | 4C | ||||||||
| 366, CZ-2 | 22023 |
Yinhe 2-01 to 2-06 G: Xingyuan 2 | 5 Mar 2022 at 06:01 UTC | Xi | 2C | ||||||||
| 367, CZ-4 | 22027 | Yaogan 34-02 | 17 Mar 2022 at 08:09 UTC | Ji | 4C | ||||||||
| 368, CZ-4 | 22035 | Gaofen 3-03 | 6 Apr 2022 at 23:47 UTC | Ji | 4C | ||||||||
| 369, CZ-3 | 22038 | Chinasat 6D | 15 Apr 2022 at 12:05 UTC | Xi | 3B/E | ||||||||
| 370, CZ-4 | 22039 | Daqi 1 | 15 Apr 2022 at 18:16 UTC | Ty | 4C | ||||||||
| 371, CZ-2 | 22043 | Superview Neo 1-01 and 1-02 | 29 Apr 2022 at 04:11 UTC | Ji | 2C | ||||||||
| 372, CZ-2 | 22048 |
A: Jilin 1 Kuanfu 1C Jilin 1 Gaofen 03D 27 to 33 | 5 May 2022 at 02:38 UTC | Ty | 2D | ||||||||
| 373, CZ-2 | 22056 |
CGSTL
LEO Test Sat 1 CGSTL LEO Test Sat 2 B: DTSW | 20 May 2022 at 10:30 UTC | Ji | 2C | 900 km x 86° | |||||||
| 374, CZ-2 | 22058 | Geesat 1-01 to 1-09 | 2 Jun 2022 at 04:00 UTC | Xi | 2C | 600 x 617 km x 50° | |||||||
| 375, CZ-2 | 22060 | Shenzhou 14 | 5 Jun 2022 at 02:44 UTC | Ji | 2F | ||||||||
| 376, CZ-2 | 22068 | Yaogan 35-02 | 23 Jun 2022 at 02:22 UTC | Xi | 2D | ||||||||
| 377, CZ-4 | 22069 | Gaofen 12-03 | 27 Jun 2022 at 15:46 UTC | Ji | 4C | ||||||||
| 378, CZ-3 | 22078 | Tianlian 2-03 | 12 Jul 2022 at 16:30 UTC | Xi | 3B | ||||||||
| 379, CZ-2 | 22082 | Superview Neo 2-01 and 2-02 | 15 Jul 2022 at 22:57 UTC | Ty | 2C | ||||||||
| 380, CZ-2 | 22088 | Yaogan 35-03 | 29 Jul 2022 at 13:28 UTC | Xi | 2D | ||||||||
| 381, CZ-4 | 22090 |
A: TECIS B: Minhang Shaonian C: Head 2G | 4 Aug 2022 at 03:08 UTC | Ty | 4B | 315, CZ-2 | 20063 | CSSHQ / Chongfu Shiyong Sh. Han.Qi / Chinese test winged vehicle | 4 Sep 2020 at 07:30 UT | Ji | 2F | landed after 2 days in orbit | |
| 382, CZ-2 | 22093 | CSSHQ 2 / Chongfu Shiyong Sh. Han.Qi / Chinese test winged vehicle | 4 Aug 2022 | Ji | 2F | 346 x 593 km x 50° | |||||||
| 383, CZ-2 | 22100 | Yaogan 35-04 | 19 Aug 2022 at 17:36 UTC | Xi | 2D | ||||||||
| 384, CZ-2 | 22103 | Beijing 3B | 24 Aug 2022 at 03:01 UTC | Ty | 2D | ||||||||
| 385, CZ-4 | 22106 | Yaogan 33-02 | 2 Sep 2022 at 23:44 UTC | Ji | 4C | ||||||||
| 386, CZ-2 | 22109 | Yaogan 35-05 | 6 Sep 2022 at 04:19 UTC | Xi | 2D | ||||||||
| 387, CZ-2 | 22115 | Yunhai 1-3 | 20 Sep 2022 at 23:15 UTC | Ji | 2D | ||||||||
| 388, CZ-2 | 22120 | Yaogan 36-01 A B C | 26 Sep 2022 at 13:38 UTC | Xi | 2D | ||||||||
| 389, CZ-2 | 22129 | ASO-S | 8 Oct 2022 at 23:43 UTC | Ji | 2D | ||||||||
| 390, CZ-2 | 22132 | Huan Jing 2E | 12 Oct 2022 at 22:53 UTC | Ty | 2C | ||||||||
| 391, CZ-2 | 22133 | Yaogan 36-02 D E F | 14 Oct 2022 at 19:12 UTC | Xi | 2D | ||||||||
| 392, CZ-2 | 22142 | DFH 309 | 29 Oct 2022 at 01:01 UTC | Ji | 2D | ||||||||
| 393, CZ-3 | 22148 | Chinasat 19 | 5 Nov 2022 at 11:50 UTC | Xi | 3B/E | 220 x 35787 km x 28.3° | |||||||
| 394, CZ-4 | 22154 | Yaogan 34-03 | 15 Nov 2022 at 01:38 UTC | Ji | 4C | ||||||||
| 395, CZ-2 | 22160 | Yaogan 36-03 | 27 Nov 2022 at 12:23 UTC | Xi | 2D | ||||||||
| 396, CZ-2 | 22162 | Shenzhou 15~ | 29 Nov 2022 at 15:08 UTC | Ji | 2F | ||||||||
| 397, CZ-2 | 22165 | Gaofen 5-01 | 8 Dec 2022 at 18:31 UTC | Ty | 2D | ||||||||
| 398, CZ-4 | 22169 |
DFH 310 (SY-20A) DFH 311 (SY-20B) | 12 Dec 2022 at 08:22 UTC | Ji | 4C | ||||||||
| 399, CZ-2 | 22171 | Yaogan 36-04 J K L | 14 Dec 2022 at 18:25 UTC | Xi | 2D | ||||||||
| 400, CZ-4 | 22176 | Gaofen 11-04 | 27 Dec 2022 at 07:37 UTC | Ty | 4B | ||||||||
| 401, CZ-3 | 22178 | DFH 315 | 29 Dec 2022 at 04:43 UTC | Xi | 3B | ||||||||
| 402, CZ-2 | 23005 | Apstar 6E | 12 Jan 2023 at 18:10 UTC | Xi | 2C | ||||||||
| 403, CZ-2 | 23006 |
Yaogan 37-01 DFH 317 (SJ-22A) DFH 318 (SJ-22B) | 13 Jan 2023 at 07:00 UTC | Ji | 2D | ||||||||
| 404, CZ-2 | 23007 |
Beiyou 1 Jilin 1 Gaofen 03D 34 Jilin 1 Hongwai A07 to A08 Jilin 1 Mofang 02A 03, 04 and 07 Jinzijing 3 and 4 Jinzijing 6 Luojia 3-01 Qilu 2 and 3 Tianzhi 2D | 15 Jan 2023 at 03:14 UTC | Ty | 2D | ||||||||
| 405, CZ-3 | 23023 | Chinasat 26 | 23 Feb 2023 at 11:49 UTC | Xi | 3B/E | ||||||||
| 406, CZ-2 | 23025 | Horus 1 | 24 Feb 2023 at 04:01 UTC | Ji | 2C | ||||||||
| 407, CZ-4 | 23030 | TianHui 6-01 A and B | 9 Mar 2023 at 22:41 UTC | Ty | 4C | ||||||||
| 408, CZ-2 | 23032 | Horus 2 | 13 Mar 2023 at 04:02 UTC | Ji | 2C | ||||||||
| 409, CZ-3 | 23036 | Gaofen 13-02 | 17 Mar 2023 at 08:33 UTC | Xi | 3B/E | ||||||||
| 410, CZ-2 | 23047 | Hongtu 1-01 A to D | 30 Mar 2023 at 10:50 UTC | Ty | 2D | ||||||||
| 411, CZ-4 | 23048 | Yaogan 34-03 | 31 Mar 2023 at 06:27 UTC | Ji | 4C | ||||||||
| 412, CZ-4 | 23055 | DFH 320 | 16 Apr 2023 at 01:36 UTC | Ji | 4B | ||||||||
| 413, CZ-3 | 23066 | DFH 321 | 17 May 2023 at 02:49 UTC | Xi | 3B/E | ||||||||
| 414, CZ-2 | 23069 |
Macao Science Satellite 1A and 1B A: Luojia 2-01 | 21 May 2023 at 08:00 UTC | Ji | 2C | ||||||||
| 415, CZ-2 | 23077 | Shenzhou 16~ | 30 May 2023 at 01:31 UTC | Ji | 2F | ||||||||
| 416, CZ-2 | 23085 |
Jilin 1 Gaofen 03D 19 to 26 Jilin 1 Gaofen 06A 01 to 30 Jilin 1 Pingtai 02A 1 and 2 DFH 324 | 15 Jun 2023 at 05:30 UTC | Ty | 2D | ||||||||
| 417, CZ-2 | 23095 | GuoWang Hulianwang Jishu Shiyan 1 | 9 Jul 2023 at 11:00 UTC | Ji | 2C | Not clear if there is a second satellite | |||||||
| 418, CZ-2 | 23104 |
Lingxi-03 Sixiang 1 to 3 | 23 Jul 2023 at 02:50 UTC | Ty | 2D | ||||||||
| 419, CZ-2 | 23106 | Yaogan 36-05 M N O | 26 Jul 2023 at 21:02 UTC | Xi | 2D | ||||||||
| 420, CZ-4 | 23111 | DFH 326 | 3 Aug 2023 at 03:47 UTC | Ji | 4C | ||||||||
| 421, CZ-2 | 23116 | Huan Jing 2F | 8 Aug 2023 at 22:53 UTC | Ty | 2C | ||||||||
| 422, CZ-3 | 23120 | Ludi Tance 4-01A | 12 Aug 2023 at 17:26 UTC | Xi | 3B/E | ||||||||
| 423, CZ-4 | 23123 | Gaofen 12-04 | 20 Aug 2023 at 17:45 UTC | Ji | 4C | ||||||||
| 424, CZ-2 | 23130 | Yaogan 39-01 A B C | 31 Aug 2023 at 07:36 UTC | Xi | 2D | ||||||||
| 425, CZ-4 | 23136 | Yaogan 33-03 | 6 Sep 2023 at 18:14 UTC | Ji | 4C | ||||||||
| 426, CZ-2 | 23145 | Yaogan 39-02 D E F | 17 Sep 2023 at 04:13 UTC | Xi | 2D | ||||||||
| 427, CZ-4 | 23149 | Yaogan 33-04 | 26 Sep 2023 at 20:15 UTC | Ji | 4C | ||||||||
| 428, CZ-2 | 23152 | Yaogan 39-03 G H I | 5 Oct 2023 at 00:24 UTC | Xi | 2D | ||||||||
| 429, CZ-2 | 23159 | Yunhai 1-4 | 15 Oct 2023 at 00:54 UTC | Ji | 2D | ||||||||
| 430, CZ-2 | 23163 | Yaogan 39-04 J K L | 23 Oct 2023 at 20:03 UTC | Xi | 2D | ||||||||
| 431, CZ-2 | 23164 | Shenzhou 17~ | 26 Oct 2023 at 03:14 UTC | Ji | 2F | ||||||||
| 432, CZ-3 | 23172 | Chinasat 6E | 9 Nov 2023 at 11:23 UTC | Xi | 3B | ||||||||
| 433, CZ-2 | 23176 | Haiyang 3A | 16 Nov 2023 at 03:55 UTC | Ji | 2C | ||||||||
| 434, CZ-2 | 23181 | GuoWang Hulianwang Jishu Shiyan 2 | 23 Nov 2023 at 10:00 UTC | Xi | 2D | ||||||||
| 435, CZ-2 | 23187 |
B: Egyptsat 2B Xingchi 1-02A and 1-02B | 04 Dec 2023 at 04:10 UTC | Ji | 2C | ||||||||
| 436, CZ-2 | 23194 | Yaogan 39-05 M N O | 10 Dec 2023 at 01:58 UTC | Xi | 2D | ||||||||
| 437, CZ-2 | 23195 | CSSHQ 3 / Chongfu Shiyong Sh. Han.Qi / Chinese test winged vehicle | 14 Dec 2023 at 14:12 UTC | Ji | 2F | ||||||||
| 438, CZ-3 | 23207 |
A: DFH 330 B: DFH 331 | 26 Dec 2023 at 03:26 UTC | Xi | 3B/YZ1 | ||||||||
| 439, CZ-2 | 23212 | GuoWang Hulianwang Jishu Shiyan 4 | 30 Dec 2023 at 00:13 UTC | Ji | 2C/YZ1 | ||||||||
| 440, CZ-2 | 24007 | Einstein probe | 9 Jan 2024 at 07:03 UTC | Xi | 2C | ||||||||
| 441, CZ-2 | 24023 | Geesat 2-01 to 2-11 | 02 Feb 2024 at 23:37 UTC | Xi | 2C | ||||||||
| 442, CZ-3 | 24040 | HWGGW 01 | 29 Feb 2024 at 13:03 UTC | Xi | 3B | ||||||||
| 443, CZ-2 | 24048 |
DRO A DRO B | 13 Mar 2024 at 12:51 UTC | Xi | 2C/YZ1 | Upper stage failure | |||||||
| 444, CZ-2 | 24052 |
Yunhai 2-7 to 2-9 Yunhai 2-10 to 2-12 | 21 Mar 2024 at 05:27 UTC | Ji | 2D/YZ3 | ||||||||
| 445, CZ-2 | 24063 | Yaogan 42-01 | 2 Apr 2024 at 22:56 UTC | Xi | 2D | ||||||||
| 446, CZ-2 | 24072 | Superview Neo 3-01 | 15 Apr 2024 at 04:12 UTC | Ji | 2D | ||||||||
| 447, CZ-2 | 24075 | Yaogan 42-02 | 20 Apr 2024 at 23:45 UTC | Xi | 2D | ||||||||
| 448, CZ-2 | 24078 | Shenzhou 18 | 25 Apr 2024 at 12:59 UTC | Ji | 2F | ||||||||
| 449, CZ-3 | 24087 | Zhihui TianWang 1-01A and 1-01B | 9 May 2024 at 01:43 UTC | Xi | 3B | ||||||||
| 450, CZ-4 | 24089 | DFH 333 | 11 May 2024 at 23:43 UTC | Ji | 4C | ||||||||
| 451, CZ-2 | 24094 | Beijing 3C 1 to 4 | 20 May 2024 at 03:06 UTC | Ty | 2D | ||||||||
| 452, CZ-3 | 24104 | Paksat MM1 | 30 May 2024 at 12:12 UTC | Xi | 3B | ||||||||
| 453, CZ-2 | 24116 | SVOM | 22 Jun 2024 at 07:00 UTC | Xi | 2C | ||||||||
| 454, CZ-4 | 24130 | Gaofen 11-05 | 19 Jul 2024 at 03:03 UTC | Ty | 4B | ||||||||
| 455, CZ-3 | 24135 | HWGGW 02 | 1 Aug 2024 at 13:14 UTC | Xi | 3B | ||||||||
| 456, CZ-4 | 24148 | Yaogan 43-01 | 16 Aug 2024 at 07:35 UTC | Xi | 4B |
Notes: Launch sites: Xi = Xichang, Ji = Jiuquan, Ty = Taiyuan, WE = Wenchang
FB-1 launches
| # | Launch id | Payload | Launch date | Type | Status/Comment (orbit in perigee x apogee x inc. x period) |
| 1, FB-1 | n/a | R&D suborbital | 10 Aug 1972 | ||
| 2, FB-1 | n/a | JSSW? | 18 Sep 1973 | Failure | |
| 3, FB-1 | n/a | JSSW? | 14 Jul 1974 | Failure: 2nd stage engine lost thrust | |
| 4, FB-1 | 75070 | JSSW 1 | 26 Jul 1975 | ||
| 5, FB-1 | 75119 | JSSW 2 | 16 Dec 1975 | ||
| 6, FB-1 | 76087 | JSSW 3 | 30 Aug 1976 | ||
| 7, FB-1 | n/a | JSSW? | 10 Nov 1976 | Failure | |
| 8, FB-1 | n/a | (suborbital) | 14 Sep 1977 | ||
| 9, FB-1 | n/a | (suborbital) | 16 Apr 1978 | ||
| 10, FB-1 | n/a | SJ? | 27 Jul 1979 | Failure: 2nd stage thrusters failure | |
| 11, FB-1 | 81093 |
A:
SJ 2 B: SJ 3A C: SJ 3B | 19 Sep 1981 |
*Notes: All launches from Juiquan.
This document is part of The Satellite Encyclopedia, © Tag's Broadcasting Services, all rights reserved, NO REPRODUCTION ALLOWED. Please notify any errors, omissions, etc.
V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly
V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly