Jiuquan SLS-2

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Jiuquan SLS-2

Part of Jiuquan

Pad 603, South Launch Site-2,. CZ launch complex. A second pad was built at the new launch complex for the CZ-2F manned spacecraft launcher, but used for smaller CZ-2D launch vehicles. Vehicles were processed at nearby Vertical Assembly Facility.

First Launch: 2003-11-02. Last Launch: 2014-08-09. Number: 31 . Longitude: 100.30 deg. Latitude: 40.96 deg.

Country: China. Spacecraft: Pujiang, CAST2000, SJ-11, SJ-7, Tianhui, FSW, SJ, Cubesat, JB-8. Launch Vehicles: Chang Zheng 11, Chang Zheng 2C, Chang Zheng 2D, Chang Zheng 4C. Launch Sites: Jiuquan.

2003 November 2 - . 07:20 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

FSW-3 No. 1 - . Payload: FSW-18, FSW-3.1, Jianbing 4. Mass: 3,000 kg (6,600 lb). Nation: China. Agency: SAST. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Decay Date: 2003-12-18 . USAF Sat Cat: 28078 . COSPAR: 2003-051A. Apogee: 165 km (102 mi). Perigee: 141 km (87 mi). Inclination: 63.00 deg. Period: 87.50 min. Expected to have been long-awaited 'seeds in space' mission but official announcements spoke only of photography..

2005 July 5 - . 22:40 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. Launch Pad: Pad 603. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

SJ-7 - . Payload: Shi Jian 7. Mass: 2,000 kg (4,400 lb). Nation: China. Manufacturer: CASC. Spacecraft: SJ-7. USAF Sat Cat: 28737 . COSPAR: 2005-024A. Apogee: 573 km (356 mi). Perigee: 555 km (344 mi). Inclination: 97.60 deg. Period: 95.90 min. Perhaps early test of satellite inspector/interceptor hardware; orbit similar to SJ-12 in 2010..

2012 May 6 - . 07:10 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Tianhui 1-02 - . Payload: Tianhui 1B. Mass: 2,000 kg (4,400 lb). Nation: China. Class: Surveillance. Type: Cartographic satellite. Spacecraft: Tianhui. USAF Sat Cat: 38256 . COSPAR: 2012-020A. Apogee: 506 km (314 mi). Perigee: 485 km (301 mi). Inclination: 97.40 deg. Period: 94.50 min. Mapping-1 Satellite 02; carried visible-band mapping cameras with 5 m resolution..

2013 April 26 - . 04:13 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Gaofen 1 - . Mass: 800 kg (1,760 lb). Nation: China. Class: Surveillance. Type: Surveillance satellite. Spacecraft: CAST2000. USAF Sat Cat: 39150 . COSPAR: 2013-018A. Apogee: 656 km (407 mi). Perigee: 628 km (390 mi). Inclination: 98.06 deg. Period: 97.56 min. High resolution imaging satellite with a 2 m resolution pan-chromatic camera, an 8 m resolution multi-spectral camera and a 16 m resolution wide-angle multi-spectral camera..

2013 September 1 - . 19:16 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 17A - . Mass: 2,000 kg (4,400 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39239 . COSPAR: 2013-046A. Apogee: 1,116 km (693 mi). Perigee: 1,065 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.
Triplet of naval surveillance satellites, believed to operate like the old US PARCAE/NOSS system, in which a group of loosely formation-flying spacecraft locate radio emitters using the difference in time of arrival of the radio signals at the different satellites.

Yaogan 17B - . Mass: 200 kg (440 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39240 . COSPAR: 2013-046B. Apogee: 1,116 km (693 mi). Perigee: 1,065 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.

Yaogan 17C - . Mass: 200 kg (440 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39241 . COSPAR: 2013-046C. Apogee: 1,116 km (693 mi). Perigee: 1,064 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.

2014 March 31 - . 02:58 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

SJ-11-06 - . Nation: China. Class: Surveillance. Type: Surveillance satellite. Spacecraft: SJ-11. USAF Sat Cat: 39624 . COSPAR: 2014-014A. Apogee: 704 km (437 mi). Perigee: 688 km (427 mi). Inclination: 98.25 deg. Period: 98.68 min. Sixth satellite in China's Shi Jian 11 constellation, replacing SJ11-01 in that orbital slot. The SJ11 satellites were rumoured to carry infrared sensors of some kind..

2014 August 9 - . 05:45 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 20b - . Mass: 200 kg (440 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40110 . COSPAR: 2014-047B. Apogee: 1,094 km (679 mi). Perigee: 1,087 km (675 mi). Inclination: 63.40 deg. Period: 107.05 min.

Yaogan 20c - . Mass: 200 kg (440 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40111 . COSPAR: 2014-047C. Apogee: 1,094 km (679 mi). Perigee: 1,087 km (675 mi). Inclination: 63.40 deg. Period: 107.05 min.

Yaogan 20a - . Mass: 2,000 kg (4,400 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40109 . COSPAR: 2014-047A. Apogee: 1,066 km (662 mi). Perigee: 1,054 km (654 mi). Inclination: 63.40 deg. Period: 106.41 min. Triplet satellites, the fourth in a series; previous triplet clusters were Yaogan 9, 16 and 17. They were thought to be analogous to the old US NOSS/PARCAE ocean surveillance system..

2015 September 14 - . 04:42 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. Launch Pad: Jiuquan LC603. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Gaofen 9 - . Mass: 800 kg (1,760 lb). Nation: China. Class: Surveillance. Type: Surveillance satellite. Spacecraft: CAST2000. USAF Sat Cat: 40894 . COSPAR: 2015-047A. Apogee: 666 km (413 mi). Perigee: 617 km (383 mi). Inclination: 98.01 deg. Period: 97.55 min. High resolution imaging satellite. GF-9 have replaced GF-1, launched in 2013 to a similar sun synchronous orbit (11:00 local time longitude of descending node)..

2015 September 25 - . 01:41 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. Launch Pad: Jiuquan SLS-E. LV Family: DF-31. Launch Vehicle: Chang Zheng 11.

Pujiang-1 - . Mass: 300 kg (660 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft: Pujiang. USAF Sat Cat: 40925 . COSPAR: 2015-051A. Apogee: 487 km (302 mi). Perigee: 465 km (288 mi). Inclination: 97.30 deg. Period: 94.13 min.
First launch of the CZ-11 solid-fuel, four-stage, light launch vehicle, though to be related to the DF-31 and DF-41 ICBMs. Pujiang, the Chinese Technology Experiment Satellite, was designed to promote the construction of smart cities in China, by monitoring urban weather, traffic and population density. It was the first Chinese satellite to use 3D printing for the titanium structure of its antenna. It included a Wi-Fi router providing a communication network between the three Tianwang cubesats released on the same launch.

Shangkeda-2 - . Payload: TIANWANG 1C (TW-1C). Mass: 3.00 kg (6.60 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 40926 . COSPAR: 2015-051B. Apogee: 485 km (301 mi). Perigee: 460 km (280 mi). Inclination: 97.30 deg. Period: 94.04 min.
Part of the Tianwang constallation of three CubeSats for space networking experiments. Codeveloped by the Shanghai Engineering Center for Microsatellites (SECM), the Nanjing University of Science and Technology (NJUST), GomSpace Denmark, Tekever Space Portugal and NanoSpace Sweden.

NJUST-2 - . Payload: TIANWANG 1B (TW-1B). Mass: 3.00 kg (6.60 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 40927 . COSPAR: 2015-051C. Apogee: 485 km (301 mi). Perigee: 462 km (287 mi). Inclination: 97.31 deg. Period: 94.07 min.

NJFA-1 - . Payload: TIANWANG 1A (TW-1A). Mass: 3.00 kg (6.60 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 40928 . COSPAR: 2015-051D. Apogee: 485 km (301 mi). Perigee: 463 km (287 mi). Inclination: 97.29 deg. Period: 94.08 min.

2017 June 15 - . 03:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 4B.

Huiyan - . Payload: HXMT. Nation: China. USAF Sat Cat: 42758 . COSPAR: 2017-034A. Apogee: 547 km (339 mi). Perigee: 535 km (332 mi). Inclination: 43.02 deg. Period: 95.46 min. See HXMT (Huiyan). ..

OVS-1B - . Payload: Zhuhai-1-02; ZHUHAI-1 02. Nation: China. USAF Sat Cat: 42759 . COSPAR: 2017-034B. Apogee: 544 km (338 mi). Perigee: 531 km (329 mi). Inclination: 43.02 deg. Period: 95.40 min. See OVS 1B (Zhuhai-1 01B, CAS 4B). ..

Milanesat - . Payload: Nusat-3. Nation: Argentina. USAF Sat Cat: 42760 . COSPAR: 2017-034C. Apogee: 542 km (336 mi). Perigee: 531 km (329 mi). Inclination: 43.02 deg. Period: 95.37 min. See ÑuSat 3 (Aleph-1 3, Milanesat). ..

OVS-1A - . Payload: Zhuhai-1-01; ZHUHAI-1 01. Nation: China. USAF Sat Cat: 42761 . COSPAR: 2017-034D. Apogee: 544 km (338 mi). Perigee: 531 km (329 mi). Inclination: 43.02 deg. Period: 95.39 min. See OVS 1A (Zhuhai-1 01A, CAS 4A). ..

2017 October 9 - . 04:12 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Antonio Jose de Sucre - . Payload: VRSS-2. Nation: Venezuela. USAF Sat Cat: 42954 . COSPAR: 2017-060A. Apogee: 655 km (406 mi). Perigee: 628 km (390 mi). Inclination: 97.98 deg. Period: 97.56 min. See VRSS 2 (Antonio José de Sucre). ..

2017 December 3 - . 04:10 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Ludi Kancha Weixing yi hao - . Payload: LKW-1. Nation: China. USAF Sat Cat: 43034 . COSPAR: 2017-077A. Apogee: 503 km (312 mi). Perigee: 488 km (303 mi). Inclination: 97.42 deg. Period: 94.53 min. See LKW 1. ..

2017 December 23 - . 04:13 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Ludi Kancha Weixing er hao - . Payload: LKW-2. Nation: China. USAF Sat Cat: 43080 . COSPAR: 2017-084A. Apogee: 501 km (311 mi). Perigee: 490 km (300 mi). Inclination: 97.42 deg. Period: 94.53 min. See LKW 2. ..

2018 January 13 - . 07:09 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Ludi Kancha Weixing san hao - . Payload: LKW-3. Nation: China. USAF Sat Cat: 43146 . COSPAR: 2018-006A. Apogee: 500 km (310 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.53 min. See LKW 3. ..

2018 February 2 - . 07:50 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

FengMaNiu 1 - . Payload: FMN 1; FENGMANIU-1. Nation: China. USAF Sat Cat: 43192 . COSPAR: 2018-015A. Apogee: 507 km (315 mi). Perigee: 482 km (299 mi). Inclination: 97.38 deg. Period: 94.51 min. See FengMaNiu 1 (FMN 1). ..

Zhang Heng 1 - . Payload: CSES; ZHANGZHENG-1. Nation: China. USAF Sat Cat: 43194 . COSPAR: 2018-015C. Apogee: 515 km (320 mi). Perigee: 490 km (300 mi). Inclination: 97.37 deg. Period: 94.67 min. See Zhangheng 1 (CSES 1). ..

Ada - . Payload: Nusat-4. Nation: Argentina. USAF Sat Cat: 43195 . COSPAR: 2018-015D. Apogee: 509 km (316 mi). Perigee: 482 km (299 mi). Inclination: 97.38 deg. Period: 94.52 min. See ÑuSat 4 (Aleph-1 4, Ada). ..

GOMX-4B - . Nation: Denmark. USAF Sat Cat: 43196 . COSPAR: 2018-015E. Apogee: 508 km (315 mi). Perigee: 480 km (290 mi). Inclination: 97.37 deg. Period: 94.50 min. See GOMX 4B. ..

Ulloriaq - . Payload: GOMX-4A; GOMX4-A. Nation: Denmark. USAF Sat Cat: 43197 . COSPAR: 2018-015F. Apogee: 509 km (316 mi). Perigee: 480 km (290 mi). Inclination: 97.37 deg. Period: 94.49 min. See GOMX 4A (Ulloriaq). ..

Shaonian Xing - . Nation: China. USAF Sat Cat: 43199 . COSPAR: 2018-015H. Apogee: 506 km (314 mi). Perigee: 480 km (290 mi). Inclination: 97.36 deg. Period: 94.47 min. See Shaonian Xing (MXSat 1, Juvenile 1F). ..

Maryam - . Payload: Nusat-5; NUSAT 5. Nation: Argentina. USAF Sat Cat: 43204 . COSPAR: 2018-015K. Apogee: 508 km (315 mi). Perigee: 482 km (299 mi). Inclination: 97.38 deg. Period: 94.51 min. See ÑuSat 5 (Aleph-1 5, Maryam). ..

2018 March 17 - . 07:09 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Ludi Kancha Weixing si hao - . Payload: LKW-4. Nation: China. USAF Sat Cat: 43236 . COSPAR: 2018-025A. Apogee: 501 km (311 mi). Perigee: 490 km (300 mi). Inclination: 97.36 deg. Period: 94.53 min. See LKW 4. ..

2018 June 2 - . 04:12 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

Gao Fen 6 - . Nation: China. USAF Sat Cat: 43484 . COSPAR: 2018-048A. Apogee: 647 km (402 mi). Perigee: 634 km (393 mi). Inclination: 98.03 deg. Period: 97.53 min. See Gaofen 6 (GF 6). ..

Luojia-1 KSW 01 xing - . Nation: China. USAF Sat Cat: 43485 . COSPAR: 2018-048B. Apogee: 648 km (402 mi). Perigee: 633 km (393 mi). Inclination: 98.03 deg. Period: 97.53 min. See Luojia 1-01 (LJ 1-01). ..

2018 July 9 - . 03:55 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

PRSS-1 - . Nation: Pakistan. USAF Sat Cat: 43529 . COSPAR: 2018-056A. Apogee: 625 km (388 mi). Perigee: 588 km (365 mi). Inclination: 98.03 deg. Period: 96.82 min. See PRSS 1. ..

PakTES-1a - . Payload: PakTES-1; PRSS 1. Nation: Pakistan. USAF Sat Cat: 43530 . COSPAR: 2018-056B. Apogee: 640 km (390 mi). Perigee: 638 km (396 mi). Inclination: 98.05 deg. Period: 97.51 min. See PRSS 1. ..

2018 October 8 - . 02:42 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

Yaogan 32 hao 01 zu 01 xing - . Payload: Chuangxin-5 10 xing?; YAOGAN-32 A. Nation: China. USAF Sat Cat: 43642 . COSPAR: 2018-077A. Apogee: 696 km (432 mi). Perigee: 695 km (431 mi). Inclination: 98.26 deg. Period: 98.68 min. See Yaogan 32-01-01. ..

Yaogan 32 hao 01 zu 02 xing - . Payload: Chuangxin-5 11 xing?; YAOGAN-32 B. Nation: China. USAF Sat Cat: 43643 . COSPAR: 2018-077B. Apogee: 696 km (432 mi). Perigee: 695 km (431 mi). Inclination: 98.26 deg. Period: 98.68 min. See Yaogan 32-01-02. ..

2018 October 29 - . 00:42 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

Zhongfa Haiyang Weixing - . Payload: CFOSat. Nation: China. USAF Sat Cat: 43662 . COSPAR: 2018-083A. Apogee: 518 km (321 mi). Perigee: 516 km (320 mi). Inclination: 97.52 deg. Period: 94.97 min. See CFOSAT (Zhongfa Haiyangxue Weixing). ..

Changsha gaoxin - . Payload: TY-4-01. Nation: China. USAF Sat Cat: 43663 . COSPAR: 2018-083B. Apogee: 523 km (324 mi). Perigee: 510 km (310 mi). Inclination: 97.52 deg. Period: 94.95 min. See Changshagaoxin (TY 4-01). ..

Xiaoxiang-1 02 xing - . Payload: TY-1-02. Nation: China. USAF Sat Cat: 43664 . COSPAR: 2018-083C. Apogee: 523 km (324 mi). Perigee: 508 km (315 mi). Inclination: 97.51 deg. Period: 94.94 min. See CFOSAT (Zhongfa Haiyangxue Weixing). ..

Zhaojin-1 - . Payload: TY-4-02. Nation: China. USAF Sat Cat: 43665 . COSPAR: 2018-083D. Apogee: 524 km (325 mi). Perigee: 507 km (315 mi). Inclination: 97.51 deg. Period: 94.93 min. See Tongchuan 1 (Zhaojin 1, TY 4-02). ..

Xinghe - . Payload: TY-1-03. Nation: China. USAF Sat Cat: 43666 . COSPAR: 2018-083E. Apogee: 523 km (324 mi). Perigee: 505 km (313 mi). Inclination: 97.53 deg. Period: 94.91 min. See Xinghe (Tianfuguoxing 1, TY 1-03). ..

Tianqi-1 - . Payload: Tianqi yi hao. Nation: China. USAF Sat Cat: 43668 . COSPAR: 2018-083G. Apogee: 523 km (324 mi). Perigee: 510 km (310 mi). Inclination: 97.51 deg. Period: 94.95 min. See Tiange 1. ..

CubeBel-1 - . Payload: BSUSat-1. Nation: China. USAF Sat Cat: 43669 . COSPAR: 2018-083H. Apogee: 523 km (324 mi). Perigee: 510 km (310 mi). Inclination: 97.52 deg. Period: 94.95 min. See CubeBel 1 (BSUSat 1). ..

Unknown Chinese payload - . Payload: -. Nation: China. COSPAR: 2018-083J.

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