Encyclopedia Astronautica
SISE


Chinese manufacturer. Shanghai Institute of Satellite Engineering, Shangai, China.

AKA: CALT; CASC; SAST; 509th Research Institute.
Location: Shangai.

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SISE Chronology


1999 October 14 - . 03:15 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B-2 (58).
  • ZY-1 - . Payload: Zi Yuan 1. Mass: 1,540 kg (3,390 lb). Nation: China. Agency: SISE. Manufacturer: CAST; INP. Class: Earth. Type: Earth resources satellite. Spacecraft: ZY. USAF Sat Cat: 25940 . COSPAR: 1999-057A. Apogee: 780 km (480 mi). Perigee: 773 km (480 mi). Inclination: 98.2000 deg. Period: 100.40 min. China-Brazil Earth Resources Satellite. China's first earth resources satellite, known as ZY-1, weighed 1,540 kilograms. Chief designer was Chen Yiyuan. The satellite, a joint project of China and Brazil, was designed to gather information on the environment, agriculture and urban planning through remote sensing images and data transmitted to China, Brazil and other countries. Planned lifetime was two years. The satellite circled the Earth 14 times a day and the groundtrack repeated after 26 days. By 23 February 2000 it had taken more than 20,000 high quality images. It was formally handed over for operational use on March 2 2000. The High Resolution CCD Camera had a resolution of 20 meters in the visible spectrum. The camera could point up to 32 degrees to either side of vertical, imaging the earth's surface stereoscopically. After 177 days the Wide Field Imager failed in early May 2000. Other devices, including the high resolution CCD camera, continue to work normally.
  • SACI 1 - . Nation: Brazil. Agency: SISE. Manufacturer: INPE. Class: Technology. Type: Navigation technology satellite. Spacecraft: SACI. USAF Sat Cat: 25941 . COSPAR: 1999-057B. Apogee: 731 km (454 mi). Perigee: 719 km (446 mi). Inclination: 98.7000 deg. Period: 99.30 min. Summary: INPE experimental scientific satellite with a magnetometer, particle detectors and an atmospheric experiment. INPE reportedly lost contact with the satellite in mid-October..

2000 January 25 - . 16:45 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-4 (60).
  • Zhongxing-22 - . Mass: 2,300 kg (5,000 lb). Nation: China. Agency: SISE. Manufacturer: CAST. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: FH-1. USAF Sat Cat: 26058 . COSPAR: 2000-003A. Apogee: 35,794 km (22,241 mi). Perigee: 35,781 km (22,233 mi). Inclination: 3.2000 deg. Period: 1,436.10 min. First Chinese military communications satellite. Perhaps an update of the DFH-3 design. Stationed at 98 deg E. The first in a planned constellation of satellites to be launched through 2010. Positioned in geosynchronous orbit at 98 deg E in 2000. As of 5 September 2001 located at 98.03 deg E drifting at 0.005 deg W per day. As of 2007 Mar 10 located at 97.95E drifting at 0.009W degrees per day.

2000 September 1 - . 03:25 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B-3 (62).
  • ZY-2 - . Payload: Zi Yuan 2. Nation: China. Agency: SISE. Manufacturer: CAST. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: ZY. USAF Sat Cat: 26481 . COSPAR: 2000-050A. Apogee: 501 km (311 mi). Perigee: 489 km (303 mi). Inclination: 97.4000 deg. Period: 94.43 min. The ZY-2 (Ziyuan-2 ('Resource-2'), while disguised as a civilian earth monitoring system, was actually code-named Jianbing-3 and was China's first high-resolution military imaging satellite. The cover story of the official Xinhua news agency was that the civilian remote sensing system would be used primarily in territorial surveying, city planning, crop yield assessment, disaster monitoring and space science experimentation. However the satellite was placed at a much lower altitude than the ZY-1 satellite and US intelligence sources indicated that it was a photo-reconnaissance satellite for exclusively military purposes, such as targeting missiles at US and Taiwanese forces. The new satellite was believed to employ digital-imaging technology and to have a resolution of 2 m or less. The satellite was designed and built by the Chinese Academy of Space Technology and was developed indigenously. It was said to be more advanced than earlier sensing satellites and was expected to have an orbital life of two years. The camera provided more than three times the resolution of the ZY-1 earth resources satellite. The Zi Yuan 2 satellite may have used the CBERS Sino-Brazilian bus of the earlier ZY-1. However it was also said to be of new design and demonstrated the capability to maneuver in orbit, adjusting its orbit after launch. In October 2000 Chinese scientists denied that the ZY-2 satellite had a military mission. It was said to be a remote-sensing satellite equipped with CCD cameras and an infrared multispectral scanner that could only identify objects on the ground with a resolution of several dozen meters to 1 km.

2003 May 24 - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-7 (70).
  • Beidou 2A - . Mass: 2,200 kg (4,800 lb). Nation: China. Agency: SISE. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou. USAF Sat Cat: 27813 . COSPAR: 2003-021A. Apogee: 35,836 km (22,267 mi). Perigee: 35,760 km (22,220 mi). Inclination: 0.3000 deg. Period: 1,436.70 min. Summary: Navigation technology satellite, joined Beidou 1A and 1B launched in December 2000. This third satellite was considered a back-up element, Positioned at 110 deg E, still maintaining its position within 0.1 deg as of 2007..

2003 October 15 - . 01:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS. LV Family: CZ. Launch Vehicle: CZ-2F.
  • Shenzhou 5 Orbital Module - . Mass: 1,100 kg (2,400 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Shenzhou OM. Decay Date: 2004-05-30 . USAF Sat Cat: 28049 . COSPAR: 2003-045G. Apogee: 347 km (215 mi). Perigee: 338 km (210 mi). Inclination: 42.4000 deg. Period: 91.40 min. The Shenzhou 5 orbital module was essential an unmanned military reconnaisance satellite. It was never entered by the astronaut during the mission, and was equipped with two high resolution (1.6 m) surveillance cameras. It was expected to operate until at least spring 2004.

2003 November 14 - . 16:01 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-8 (74).
  • Zhongxing 20 - . Payload: Feng Huo 2. Mass: 2,300 kg (5,000 lb). Nation: China. Agency: SISE. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-3. USAF Sat Cat: 28082 . COSPAR: 2003-052A. Apogee: 35,811 km (22,251 mi). Perigee: 35,762 km (22,221 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Military communications satellite. As of 2007 Mar 11 located at 103.00E drifting at 0.010W degrees per day..

2003 December 29 - . 19:06 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. Launch Pad: LC1?. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C CZ2C-22 (75).
  • Tan Ce 1 - . Payload: Double Star 1, DSP-E. Mass: 350 kg (770 lb). Nation: China. Agency: SISE. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Double Star. Decay Date: 2007-10-14 . USAF Sat Cat: 28140 . COSPAR: 2003-061A. Apogee: 78,051 km (48,498 mi). Perigee: 555 km (344 mi). Inclination: 28.5000 deg. Summary: Equatorial member of a pair of Chinese-European magnetospheric research satellites carrying surplus instrumentation from the ESA Cluster program. First CZ-2C launch from Xichang..

2004 July 25 - . 07:05 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C CZ2C-24 (77).
  • Tan Ce 2 - . Payload: Double Star 2, DSP-P. Mass: 660 kg (1,450 lb). Nation: China. Agency: SISE. Manufacturer: DFH. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Double Star. USAF Sat Cat: 28382 . COSPAR: 2004-029A. Apogee: 38,574 km (23,968 mi). Perigee: 655 km (406 mi). Inclination: 90.0000 deg. Period: 695.10 min. Summary: Delayed from June, July 20.

2004 August 29 - . 07:50 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C CZ2C-25 (78).
  • FSW-3 No. 2 - . Payload: FSW-19. Mass: 2,100 kg (4,600 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 26.67 days. Decay Date: 2004-11-07 . USAF Sat Cat: 28402 . COSPAR: 2004-033A. Apogee: 547 km (339 mi). Perigee: 168 km (104 mi). Inclination: 63.0000 deg. Period: 91.70 min. Recoverable satellite officially stated to be conducting space scientific research, land surveying, mapping and other scientific experiments. Said to have improved experimental technology, with higher orientation precision and more complex on-board computers and software. Controlled from the Xian Satellite Monitoring and Control Centre. Successfully re-entered and recovered after 27 days in space at 23:55 GMT on 24 September.

2004 September 8 - . 23:14 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B-7 (79).
  • SJ-6A - . Payload: Shi Jian 6B. Nation: China. Agency: SISE. Class: Technology. Type: Navigation technology satellite. Spacecraft: SJ-6. USAF Sat Cat: 28413 . COSPAR: 2004-035A. Apogee: 593 km (368 mi). Perigee: 578 km (359 mi). Inclination: 97.7000 deg. Period: 96.40 min. It was announced that the two satellites had a design life of at least two years, and would be used to probe the space environment, radiation and its effects, record space physical environment parameters, and conduct other related space experiments. The two satellites were built by the Shanghai Academy of Space Flight Technology and Dongfanghong Satellite Company under subcontract to the China Aerospace Science and Technology Corporation. The scientific instruments aboard the satellites were mainly manufactured by the China Electronics Technology Corporation. Some Western observors believed the mission of the satellites included electronic intelligence technology tests.
  • SJ-6B - . Payload: Shi Jian 6A. Nation: China. Agency: SISE. Class: Technology. Type: Navigation technology satellite. Spacecraft: SJ-6. USAF Sat Cat: 28414 . COSPAR: 2004-035B. Apogee: 602 km (374 mi). Perigee: 593 km (368 mi). Inclination: 97.7000 deg. Period: 96.60 min. Summary: CAST968 platform. Released one minute after SJ-6A..

2004 September 27 - . 08:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS. LV Family: CZ. Launch Vehicle: CZ-2D. LV Configuration: Chang Zheng 2D CZ2D-5 (80).
  • FSW-3 No. 3 - . Payload: FSW 20. Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 17.78 days. Decay Date: 2004-11-09 . USAF Sat Cat: 28424 . COSPAR: 2004-039A. Apogee: 297 km (184 mi). Perigee: 205 km (127 mi). Inclination: 63.0000 deg. Summary: Recoverable military satellite. Returned to Earth at 02:48 GMT on October 15, falling through the roof of a house in the village of Penglai, Sichuan province..

2004 October 19 - . 01:20 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-9 (81).
  • FY-2C - . Mass: 1,380 kg (3,040 lb). Nation: China. Agency: SISE. Class: Earth. Type: Weather satellite. Spacecraft: FY-2. USAF Sat Cat: 28451 . COSPAR: 2004-042A. Apogee: 35,791 km (22,239 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.7000 deg. Period: 1,436.20 min. Third Fengyun-2 weather satellite. The apogee motor placed the satellite into a drifting geostationary orbit. As of the date of the launch, four FY-2 satellites had been launched. FY-2 01 was destroyed in a ground fire 1994. FY-2 02 / FY-2A was placed in reserve in May 2000 86 deg E; and FY-2 03 / FY-2B was operational at 123 deg E. As of 2007 Mar 11 located at 104.44E drifting at 0.026W degrees per day.

2004 November 6 - . 03:10 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B-8 (82).
  • ZY-2C - . Nation: China. Agency: SISE. Class: Earth. Type: Earth resources satellite. Spacecraft: ZY. USAF Sat Cat: 28470 . COSPAR: 2004-044A. Apogee: 504 km (313 mi). Perigee: 479 km (297 mi). Inclination: 97.3000 deg. Period: 94.40 min. Summary: Zi Yuan 2-3 was a low earth orbit digital imaging spacecraft used by the Chinese government, probably for both civilian and military reconnaissance purposes..

2004 November 18 - . 10:45 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. Launch Pad: LC1?. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C CZ2C-26 (83).
  • Shiyan Weixing 2 - . Payload: TANSUO 2. Mass: 300 kg (660 lb). Nation: China. Agency: SISE. Manufacturer: DFH. Class: Earth. Type: Earth resources satellite. Spacecraft: Shiyan Weixing. USAF Sat Cat: 28479 . COSPAR: 2004-046A. Apogee: 711 km (441 mi). Perigee: 694 km (431 mi). Inclination: 98.2000 deg. Period: 98.80 min. Summary: Remote Sensing Technology..

2005 October 12 - . 01:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS. LV Family: CZ. Launch Vehicle: CZ-2F. LV Configuration: Chang Zheng 2F CZ2F-6 (88).
  • Shenzhou 6 - . Crew: Fei Junlong; Nie Haisheng. Backup Crew: Liu Buoming; Jing Haipen. Return Crew: Zhai Zhigang; Wu Jie. Mass: 8,040 kg (17,720 lb). Nation: China. Related Persons: Fei Junlong; Nie Haisheng; Liu Buoming; Jing Haipen; Zhai Zhigang; Wu Jie. Agency: SISE. Class: Manned. Type: Manned spacecraft. Flight: Shenzhou 6. Spacecraft: Shenzhou. Duration: 4.81 days. Decay Date: 2005-10-16 . USAF Sat Cat: 28879 . COSPAR: 2005-040A. Apogee: 338 km (210 mi). Perigee: 331 km (205 mi). Inclination: 42.4000 deg. Period: 91.20 min. Moved up from October 13. Second Chinese manned space mission. The two-astronaut crew spent 5 days in space, and worked in the Shenzhou orbital module for the first time. Aside from biomedical experiments, the nature of their work was not divulged, and few images of the interior of the orbital module (with its probable military experiments) were released.

2006 October 23 - . 23:34 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B-10 (92).
  • SJ-6-2A SJ-6C - . Nation: China. Agency: SISE. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SJ-6. USAF Sat Cat: 29505 . COSPAR: 2006-046A. Apogee: 598 km (371 mi). Perigee: 594 km (369 mi). Inclination: 97.7000 deg. Period: 96.60 min. Summary: Replaced the SJ-6 Group 1 satellites A and B. Official purpose was to measure the space environment, but foreign analysts suspected a SIGINT role..
  • SJ-6-2B SJ-6D - . Nation: China. Agency: SISE. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SJ-6. USAF Sat Cat: 29506 . COSPAR: 2006-046B. Apogee: 599 km (372 mi). Perigee: 598 km (371 mi). Inclination: 97.7000 deg. Period: 96.70 min.

2006 October 28 - . 16:20 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: Chang Zheng 3B CZ3B (93).
  • Xinnuo 2 - . Payload: Sinosat-2. Mass: 5,100 kg (11,200 lb). Nation: China. Agency: SISE. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 29516 . COSPAR: 2006-048A. Apogee: 35,911 km (22,314 mi). Perigee: 35,675 km (22,167 mi). Inclination: 0.0600 deg. Period: 1,436.44 min. First DH-4 heavy Chinese communication satellite with communications equipment provided by Alcatel Alenia. Mission failed when solar panels and antennae failed to deploy in geosynchronous orbit. This was a blow to China's prestige, since the satellite was an important part of the 2008 Beijing Olympics coverage plans. As of 2007 Mar 10 located at 91.80E drifting at 0.093W degrees per day.

2006 December 8 - . 00:53 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-11 (94).
  • FY 2D - . Payload: Fengyun 2D. Nation: China. Agency: SISE. Class: Earth. Type: Weather satellite. Spacecraft: FY-2. Decay Date: 2006-12-09 . USAF Sat Cat: 29641 . COSPAR: 2006-053B. Apogee: 35,789 km (22,238 mi). Perigee: 35,781 km (22,233 mi). Inclination: 2.6000 deg. Period: 1,436.00 min. Fourth Wind and Cloud 2 geostationary weather satellite with an infrared radiometer as its primary instrument. The booster placed the spacecraft in a 226 x 36221 km x 24.9 deg geosynchronous transfer orbit. The FG-36 solid apogee motor aboard the satellite burned at 18:07 GMT and placed the FY-2D into an initial 35786 x 36478 km x 2.6 deg geosynchronous drift orbit.

2007 February 2 - . 16:28 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-12 (95).
  • Beidou G1 - . Payload: Beiduou 1D. Mass: 2,200 kg (4,800 lb). Nation: China. Agency: SISE. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou. USAF Sat Cat: 30323 . COSPAR: 2007-003A. Apogee: 36,248 km (22,523 mi). Perigee: 35,326 km (21,950 mi). Inclination: 6.2000 deg. Period: 1,436.10 min. Summary: Fourth Beidou satellite. It did not reach geostationary orbit until early April following deployment problems with its solar panels and reports of US detection of a debris cloud at the time of the original expected apogee firing..

2007 September 19 - . 03:26 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B (102).
  • CBERS-2B - . Mass: 1,452 kg (3,201 lb). Nation: China; Brazil. Agency: SISE. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft: ZY. USAF Sat Cat: 32062 . COSPAR: 2007-042A. Apogee: 775 km (481 mi). Perigee: 773 km (480 mi). Inclination: 98.5000 deg. Period: 100.30 min. Third China-Brazil joint earth resources satellite. Much higher resolution optics and multispectral sensors expected to be useful for some military applications as well. The satellite raised its orbit to its operational altitude of 773 km two days after launch.

2007 October 24 - . 10:05 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. Launch Pad: LC1?. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-15 (103).
  • Chang'e 1 - . Mass: 2,300 kg (5,000 lb). Nation: China. Agency: SISE. Class: Moon. Type: Lunar probe. Spacecraft: Chang'e. USAF Sat Cat: 32273 . COSPAR: 2007-051B. Apogee: 50,182 km (31,181 mi). Perigee: 147 km (91 mi). Inclination: 30.8000 deg. Period: 929.20 min. China's first unmanned lunar/planetary probe. The initial orbit of 221 x 50,602 km x 31.0 deg was raised to a translunar trajectory by 31 October in a serious of spacecraft engine burns. The spacecraft entered a 210 km x 8600 km lunar orbit at 03:37 GMT on 5 November.

2007 November 11 - . 22:48 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-4C. LV Configuration: Chang Zheng 4C CZ4C (104).
  • Yaogan 3 - . Mass: 2,700 kg (5,900 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Civilian surveillance radar satellite. Spacecraft: Yaogan. USAF Sat Cat: 32289 . COSPAR: 2007-055A. Apogee: 629 km (390 mi). Perigee: 628 km (390 mi). Inclination: 97.8000 deg. Period: 97.30 min. Summary: The military launch used a new version of the CZ-4 booster. The CZ-4C includes a restart capability in the upper stage and a new interstage adapter between the first and second stages..

2008 April 25 - . 15:35 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3C. LV Configuration: CZ-3C s/n CZ3C1.
  • Tian Lian 1 - . Payload: DFH 76. Mass: 3,000 kg (6,600 lb). Nation: China. Agency: SISE. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 32779 . COSPAR: 2008-019A. Apogee: 35,806 km (22,248 mi). Perigee: 35,768 km (22,225 mi). Inclination: 0.4000 deg. Period: 1,436.10 min. China's first in a series of new data relay satellites, and the first launch of the CZ-3C, a variant of the Long March with two liquid strap-ons. The satellite will relay data from Chinese manned and military satellites, beginning with the Shenzhou mission, from geostationary orbit at 77 deg E. Configuration unknown, but possibly based on the DFH-4 platform.

2008 May 27 - . 03:02 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-4C.
  • FY-3A - . Nation: China. Agency: SISE. Class: Earth. Type: Weather satellite. Spacecraft: FY-3. USAF Sat Cat: 32958 . COSPAR: 2008-026A. Apogee: 828 km (514 mi). Perigee: 826 km (513 mi). Inclination: 98.8000 deg. Period: 101.40 min. Summary: Polar orbiting weather satellite. The FY-3 series will replace the older FY-1 polar system..

2008 June 9 - . 12:15 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B.
  • Zhongxing 9 - . Nation: China. Agency: SISE. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 33051 . COSPAR: 2008-028A. Apogee: 35,804 km (22,247 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Launched to support Olympic games; 22 J-band transponders; positioned at 92.2 deg E..

2008 September 6 - . 03:25 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-2C.
  • Huan Jing-1A - . Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: HJ-1. USAF Sat Cat: 33320 . COSPAR: 2008-041A. Apogee: 662 km (411 mi). Perigee: 628 km (390 mi). Inclination: 98.0000 deg. Period: 97.60 min. Summary: 'Environment' satellites that carried visible and infrared sensors..
  • Huan Jing-1B - . Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: HJ-1. USAF Sat Cat: 33321 . COSPAR: 2008-041B. Apogee: 672 km (417 mi). Perigee: 626 km (388 mi). Inclination: 98.0000 deg. Period: 97.70 min.

2008 September 25 - . 13:10 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS. LV Family: CZ. Launch Vehicle: CZ-2F. LV Configuration: CZ-2F s/n CZ2F7.
  • Shenzhou 7 - . Crew: Zhai Zhigang; Liu Buoming; Jing Haipen. Mass: 7,840 kg (17,280 lb). Nation: China. Related Persons: Zhai Zhigang; Liu Buoming; Jing Haipen. Agency: SISE. Class: Manned. Type: Manned spacecraft. Flight: Shenzhou 7. Spacecraft: Shenzhou. Duration: 2.85 days. Decay Date: 2008-09-28 . USAF Sat Cat: 33386 . COSPAR: 2008-047A. Apogee: 336 km (208 mi). Perigee: 329 km (204 mi). Inclination: 42.4000 deg. Period: 91.20 min. Third Chinese manned space mission. The crew consisted of Zhai Zhigang, backup astronaut for China's first manned space mission; and Liu Buoming and Jing Haipeng, backups for the second mission. The astronauts demonstrated the capability of the Shenzhou spacecraft to carry its full complement of three crew for the first time. Zhai, wearing a Chinese-developed Feitian space suit, emerged from the orbital module of the Shenzhou and became China's first astronaut to conduct a spacewalk. Liu, wearing a proven Russian Orlan spacesuit, remained in the depressurized orbital module, ready to assist Zhai in an emergency. A subsatellite, weighing 40 kg, was released after the EVA, and relayed back images of Shenzhou 7 from close range to a distance of several kilometers. The crew returned safely to earth in a pinpoint landing in Outer Mongolia, carried live on television. The orbital module remained in space, conducting space network experiments with the subsatellite.
  • BX-1 - . Mass: 40 kg (88 lb). Nation: China. Agency: SISE. Class: Technology. Type: Navigation technology satellite. Flight: Shenzhou 7. Spacecraft: Ban Xing. Decay Date: 2009-10-29 . USAF Sat Cat: 33392 . COSPAR: 2008-047G. Apogee: 331 km (205 mi). Perigee: 321 km (199 mi). Inclination: 42.4000 deg. Period: 91.00 min. Summary: BanXing (companion satellite) subsatellite released by Shenzhou 7. If maneuvered away and back to the Shenzhou orbital module after the mission..

2008 October 25 - . 01:15 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-4B.
  • SJ-6-03A - . Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: SJ-6. USAF Sat Cat: 33408 . COSPAR: 2008-053A. Apogee: 603 km (374 mi). Perigee: 584 km (362 mi). Inclination: 97.7000 deg. Period: 96.50 min. Summary: Third pair in China's SJ military surveillance constellation. It has been suggested that each pair consists of two differing satellites, a smaller minisatellite built by SAST Shanghai and a larger 300-kg CAST-968 bus satellite from DFH..
  • SJ-6-03B - . Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: SJ-6. USAF Sat Cat: 33409 . COSPAR: 2008-053B. Apogee: 605 km (375 mi). Perigee: 582 km (361 mi). Inclination: 97.7000 deg. Period: 96.50 min.

2008 October 29 - . 16:54 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: CZ-3B s/n CZ3B11.
  • Simon Bolivar - . Mass: 5,100 kg (11,200 lb). Nation: Venezuela. Agency: SISE. Class: Communications. Type: Civilian communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 33414 . COSPAR: 2008-055A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.2000 deg. Period: 1,436.10 min. Summary: Venezuela's first satellite, a Chinese-built DFH-4 communications satellit with C-band and Ku-band transponders..

2008 November 5 - . 00:15 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2D.
  • Chuanxin-1-02 - . Nation: China. Agency: SISE. Class: Technology. Type: Navigation technology satellite. Spacecraft: CX-1. USAF Sat Cat: 33433 . COSPAR: 2008-056A. Apogee: 805 km (500 mi). Perigee: 785 km (487 mi). Inclination: 98.5000 deg. Period: 100.80 min. Summary: Microsat built by the Shanghai Institute of Microsystems and Information Technology) and the Shanghai Academy of Space Technology. The satellite was designed to collect and relay hydrological and meteorological data and data for disaster relief..
  • Shiyan Weixing 3 - . Nation: China. Agency: SISE. Class: Technology. Type: Navigation technology satellite. Spacecraft: Shiyan. USAF Sat Cat: 33434 . COSPAR: 2008-056B. Apogee: 806 km (500 mi). Perigee: 785 km (487 mi). Inclination: 98.5000 deg. Period: 100.80 min. Summary: Built by the Harbin Institute of Technology and the DFH Satellite Company for 'experiments on new technologies in atmospheric exploration'..

2008 December 1 - . 04:42 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2D. LV Configuration: CZ-2D s/n CZ2D10.
  • Yaogan Weixing 4 - . Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance radar satellite. Spacecraft: Yaogan. USAF Sat Cat: 33446 . COSPAR: 2008-061A. Apogee: 654 km (406 mi). Perigee: 632 km (392 mi). Inclination: 97.9000 deg. Period: 97.60 min. Summary: Fourth 'Remote Sensing Satellite'; presumed military mission..

2008 December 15 - . 03:22 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-4B. LV Configuration: CZ-4B s/n CZ417.
  • Yaogan Weixing 5 - . Mass: 2,200 kg (4,800 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Military surveillance radar satellite. Spacecraft: Yaogan. USAF Sat Cat: 33456 . COSPAR: 2008-064A. Apogee: 496 km (308 mi). Perigee: 486 km (301 mi). Inclination: 97.4000 deg. Period: 94.40 min. One of the two different series of military surveillance satellites launched under the YW designation, although YW 5 was in a lower orbit similar to the ZY-2 satellites, lower than previous YW satellites. The launch vehicle was announced as a CZ-4B, but appeared to be a CZ-4B with the CZ-4C's restartable YF-40A upper stage under the larger CZ-4C nose fairing.

2008 December 23 - . 00:54 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3A.
  • FY-2E - . Nation: China. Agency: SISE. Class: Earth. Type: Weather satellite. Spacecraft: FY-2. USAF Sat Cat: 33463 . COSPAR: 2008-066A. Apogee: 35,806 km (22,248 mi). Perigee: 35,771 km (22,227 mi). Inclination: 2.6000 deg. Period: 1,436.20 min. Summary: Member of China's geosynchronous weather satellite constellation..

2009 April 14 - . 16:16 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: CZ-2C s/n CZ3C2.
  • Beidou G2 - . Mass: 3,100 kg (6,800 lb). Nation: China. Agency: SISE. Spacecraft: Beidou. USAF Sat Cat: 34779 . COSPAR: 2009-018A. Apogee: 35,799 km (22,244 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.7000 deg. Period: 1,436.30 min. Summary: Second of second generation operational Beidou navigation satellites..

2009 April 22 - . 02:55 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: CZ-2C s/n CZ2-32.
  • Yaogan 6 - . Nation: China. Agency: SISE. Spacecraft: Yaogan. USAF Sat Cat: 34839 . COSPAR: 2009-021A. Apogee: 512 km (318 mi). Perigee: 512 km (318 mi). Inclination: 97.6000 deg. Period: 94.90 min.

2009 August 31 - . 09:28 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: CZ-3B s/n CZ3B12.
  • Palapa D - . Payload: Spacebus 4000B3. Mass: 4,100 kg (9,000 lb). Nation: China. Agency: SISE. Program: Palapa. Class: Communications. Type: Communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 35812 . COSPAR: 2009-046A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Early third stage cutoff left spacecraft in sub-geostationary transfer orbit of 217 km x 21,138 km at 22.4 deg inclination. It used its on-board system to reach an operational orbit, albeit with reduced life due to the propellant consumption..

2009 November 12 - . 02:45 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2C.
  • SJ-11-01 - . Nation: China. Agency: SISE. Spacecraft: SJ-11. USAF Sat Cat: 36088 . COSPAR: 2009-061A. Apogee: 705 km (438 mi). Perigee: 688 km (427 mi). Inclination: 98.3000 deg. Period: 98.70 min. Summary: Experimental Satellite, believed to carry infrared surveillance system sensors..

2009 December 9 - . 08:42 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2D. LV Configuration: CZ-2D s/n CZ2-34.
  • Yaogan Weixing 7 - . Nation: China. Agency: SISE. Spacecraft: Yaogan. USAF Sat Cat: 36110 . COSPAR: 2009-069A. Apogee: 659 km (409 mi). Perigee: 623 km (387 mi). Inclination: 97.8000 deg. Period: 97.50 min. Summary: Remote-Sensing Satellite, apparently a military optical surveillance satellite similar to YW-2 and YW-4..

2009 December 15 - . 02:31 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-4C. LV Configuration: CZ-4C s/n CZ4-18.
  • Yaogan Weixing 8 - . Mass: 1,040 kg (2,290 lb). Nation: China. Agency: SISE. Spacecraft: Yaogan. USAF Sat Cat: 36121 . COSPAR: 2009-072A. Apogee: 1,204 km (748 mi). Perigee: 1,193 km (741 mi). Inclination: 100.5000 deg. Period: 109.40 min. Summary: Sun-synchronous orbit low resolution imaging satellite, primarily for civilian Earth resource studies. Supplemental military missions may include weather forecasting..
  • Xi Wang 1 - . Mass: 50 kg (110 lb). Nation: China. Agency: SISE. Spacecraft: Oscar. USAF Sat Cat: 36122 . COSPAR: 2009-072B. Apogee: 1,205 km (748 mi). Perigee: 1,193 km (741 mi). Inclination: 100.5000 deg. Period: 109.40 min. Summary: Amateur radio satellite..

2010 January 16 - . 16:12 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3C. LV Configuration: CZ-3C s/n CZ3C3.
  • Beidou G3 - . Nation: China. Agency: SISE. Spacecraft: Beidou. USAF Sat Cat: 36287 . COSPAR: 2010-001A. Apogee: 35,972 km (22,351 mi). Perigee: 35,600 km (22,100 mi). Inclination: 1.8000 deg. Period: 1,436.10 min.

2010 March 5 - . 04:55 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-4C. LV Configuration: CZ-4C s/n CZ4-19.
  • Yaogan 9A - . Mass: 2,800 kg (6,100 lb). Nation: China. Agency: SISE. Class: Military. Type: Electronic intelligence satellite. Spacecraft: Yaogan. USAF Sat Cat: 36413 . COSPAR: 2010-009A. Apogee: 1,107 km (687 mi). Perigee: 1,075 km (667 mi). Inclination: 63.4000 deg. Period: 107.10 min.
  • Yaogan 9B - . Nation: China. Agency: SISE. Class: Military. Type: Electronic intelligence satellite. Spacecraft: Yaogan. USAF Sat Cat: 36414 . COSPAR: 2010-009B. Apogee: 1,107 km (687 mi). Perigee: 1,075 km (667 mi). Inclination: 63.4000 deg. Period: 107.10 min.
  • Yaogan 9C - . Nation: China. Agency: SISE. Class: Military. Type: Electronic intelligence satellite. Spacecraft: Yaogan. USAF Sat Cat: 36415 . COSPAR: 2010-009C. Apogee: 1,107 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.4000 deg. Period: 107.10 min.

2010 June 2 - . 15:53 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3C. LV Configuration: CZ-3C s/n CZ3C4.
  • Beidou G4 - . Nation: China. Agency: SISE. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou. USAF Sat Cat: 36590 . COSPAR: 2010-024A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 1.8000 deg. Period: 1,436.00 min.

2010 June 15 - . 01:39 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2D. LV Configuration: CZ-2D s/n CZ2-35.
  • SJ-12 - . Nation: China. Agency: SISE. Class: Military. Type: Anti-satellite system. Spacecraft: SJ-12. USAF Sat Cat: 36596 . COSPAR: 2010-027A. Apogee: 602 km (374 mi). Perigee: 578 km (359 mi). Inclination: 97.7000 deg. Period: 96.50 min. Summary: Satellite inspector/interceptor. Carried out a close pass or even came in contact with the SJ-6/3A satellite on 19 August 2010. By 21 September was in a 580 km x 606 km x 97.8 deg orbit..

2010 July 31 - . 21:30 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3A.
  • Beidou IGS 1 - . Payload: Beidou DW5. Nation: China. Agency: SISE. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou. USAF Sat Cat: 36828 . COSPAR: 2010-036A. Apogee: 35,901 km (22,307 mi). Perigee: 35,680 km (22,170 mi). Inclination: 55.0000 deg. Period: 1,436.30 min. Summary: Fifth Beidou navigation satellite, placed in an inclined geosynchronous orbit..

2010 August 9 - . 22:49 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-4C.
  • Yaogan 10 - . Payload: Yaogan Weixing 10. Nation: China. Agency: SISE. Class: Surveillance. Type: Civilian surveillance radar satellite. Spacecraft: Yaogan. USAF Sat Cat: 36834 . COSPAR: 2010-038A. Apogee: 630 km (390 mi). Perigee: 627 km (389 mi). Inclination: 97.8000 deg. Period: 97.30 min. Summary: Radar imaging satellite..

2010 August 24 - . 07:10 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2D.
  • Tianhui-1 Weixing - . Nation: China. Agency: SISE. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 36985 . COSPAR: 2010-040A. Apogee: 507 km (315 mi). Perigee: 484 km (300 mi). Inclination: 97.4000 deg. Period: 94.50 min. Summary: Research, mapping and land resource survey satellite..

2010 September 4 - . 16:14 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B.
  • Chinasat 6A - . Payload: Zhongxing 6A. Mass: 5,100 kg (11,200 lb). Nation: China. Agency: SISE. Program: Chinasat. Class: Communications. Type: Communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 37150 . COSPAR: 2010-042A. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: C and Ku band communications transponders..

2010 September 22 - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2D.
  • Yaogan 11 - . Payload: Zheda Pixing 1A. Nation: China. Agency: SISE. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Yaogan. USAF Sat Cat: 37165 . COSPAR: 2010-047A. Apogee: 669 km (415 mi). Perigee: 626 km (388 mi). Inclination: 98.0000 deg. Period: 97.70 min. Summary: Carried earth imaging camera..
  • Zheda Pixing 1B - . Nation: China. Agency: SISE. Spacecraft: Zheda Pixing. USAF Sat Cat: 37166 . COSPAR: 2010-047B. Apogee: 657 km (408 mi). Perigee: 622 km (386 mi). Inclination: 98.0000 deg. Period: 97.50 min.
  • Zheda Pixing 1C - . Nation: China. Agency: SISE. Spacecraft: Zheda Pixing. USAF Sat Cat: 37167 . COSPAR: 2010-047C. Apogee: 657 km (408 mi). Perigee: 623 km (387 mi). Inclination: 98.0000 deg. Period: 97.50 min.

2010 October 1 - . 11:00 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3C.
  • Chang'e 2 - . Payload: Chang'e 2. Nation: China. Agency: SISE. Class: Moon. Type: Lunar probe. Spacecraft: Chang'e. USAF Sat Cat: 37174 . COSPAR: 2010-050A. China's second lunar orbiter. Entered a 119 x 8599 km lunar orbit on 1 October at 03:14 GMT. By 9 October it had maneuvered to its operational 100-km circular lunar orbit. On 9 June 2011, its lunar mission complete, it was maneuvered out of lunar orbit, and arrived at the Sun-Earth L2 Lagrangian point on 25 August 2011.

2010 October 6 - . 00:49 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: CZ-4B.
  • SJ-6G - . Payload: SJ-6/4A. Mass: 1,000 kg (2,200 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Surveillance satellite. Spacecraft: SJ-6. USAF Sat Cat: 37179 . COSPAR: 2010-051A. Apogee: 606 km (376 mi). Perigee: 587 km (364 mi). Inclination: 97.7000 deg. Period: 96.60 min. Summary: Fourth pair of SJ-6 military surveillance satellites..
  • SJ-6H - . Payload: SJ-6/4B. Mass: 200 kg (440 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Surveillance satellite. Spacecraft: SJ-6. USAF Sat Cat: 37180 . COSPAR: 2010-051B. Apogee: 604 km (375 mi). Perigee: 588 km (365 mi). Inclination: 97.7000 deg. Period: 96.60 min.

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