Jiuquan LA2B (original) (raw)

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Jiuquan LA2B

Part of Jiuquan

Launch Area 2 Pad 138, North Launch Site. CZ launch complex.

First Launch: 1971-09-10. Last Launch: 1996-10-20. Number: 37 . Longitude: 100.31 deg. Latitude: 41.31 deg.

Country: China. Spacecraft: JSSW, FSW, SJ, Freja. Launch Vehicles: Dong Feng 5, Feng Bao 1, Chang Zheng 2, Chang Zheng 2C, Chang Zheng 2D, Dong Feng 5A. Launch Sites: Jiuquan.

1971 September 10 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). Research and Development Suborbital Flight.

1972 August 10 - . 00:32 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.

Shiyan Peizhong - . Nation: China. Agency: PRC. Apogee: 200 km (120 mi). Research and Development Suborbital Flight.

1973 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Apogee: 1,000 km (600 mi).

1973 September 18 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1. FAILURE: Failure. Failed Stage: U.

JSSW 1 - . Payload: JSSW 1. Mass: 1,100 kg (2,400 lb). Nation: China. Agency: PRC. Spacecraft: JSSW.

1974 July 14 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1. FAILURE: Vehicle lost attitude stability and destroyed by range safety.. Failed Stage: G.

JSSW 2 - . Payload: JSSW 2. Mass: 1,100 kg (2,400 lb). Nation: China. Agency: PRC. Spacecraft: JSSW.

1974 November 5 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2. FAILURE: Cable carrying pitch rate gyro signal disconnected.. Failed Stage: G.

FSW-0 - . Payload: FSW-0 No. A. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: PRC. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Decay Date: 1974-11-05 .

1975 July 26 - . 13:28 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.

JSSW 3 - . Payload: JSSW 3. Mass: 1,107 kg (2,440 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: JSSW. Decay Date: 1975-09-14 . USAF Sat Cat: 8053 . COSPAR: 1975-070A. Apogee: 455 km (282 mi). Perigee: 190 km (110 mi). Inclination: 69.00 deg. Period: 90.90 min. Photo surveillance; radio transmission. .

1975 November 26 - . 03:29 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 1 - . Payload: FSW-0 No. 01. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 2.00 days. Decay Date: 1975-12-29 . USAF Sat Cat: 8452 . COSPAR: 1975-111A. Apogee: 483 km (300 mi). Perigee: 183 km (113 mi). Inclination: 63.00 deg. Period: 91.10 min.
First orbital test of Chinese recoverable photo surveillance satellite. The spacecraft was brought down early, after three days in orbit, due to problems with the attitude control system cold gas supply. Along the skirt of the return capsule some wires and instruments were burnt during re-entry and capsule impacted far from its planned landing point. However usable film was obtained from the capsule. The Chinese Academy of Space Technology organised a team to determine the cause, and improvements were made in the next spacecraft of the model. Additional Details: here....

1975 December 16 - . 09:19 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.

JSSW 4 - . Payload: JSSW 4. Mass: 1,110 kg (2,440 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: JSSW. Decay Date: 1976-01-27 . USAF Sat Cat: 8488 . COSPAR: 1975-119A. Apogee: 387 km (240 mi). Perigee: 186 km (115 mi). Inclination: 69.00 deg. Period: 90.30 min. Photo surveillance; radio transmission. .

1976 August 30 - . 11:53 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.

JSSW 5 - . Payload: JSSW 5. Mass: 1,108 kg (2,442 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: JSSW. Decay Date: 1978-11-25 . USAF Sat Cat: 9394 . COSPAR: 1976-087A. Apogee: 2,145 km (1,332 mi). Perigee: 195 km (121 mi). Inclination: 69.20 deg. Period: 108.80 min.

1976 November 10 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1. FAILURE: Failure. Failed Stage: U.

JSSW 6 - . Payload: JSSW 6. Mass: 1,100 kg (2,400 lb). Nation: China. Agency: PRC. Spacecraft: JSSW.

1976 December 7 - . 04:38 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 2 - . Payload: FSW-0 No. 02. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 2.00 days. Decay Date: 1977-01-02 . USAF Sat Cat: 9587 . COSPAR: 1976-117A. Apogee: 489 km (303 mi). Perigee: 172 km (106 mi). Inclination: 59.40 deg. Period: 91.10 min. Photo surveillance; film capsule recovered 9 December. First completely successful test of the FSW spy satellite. Many improvements in comparison to the first FSW orbited..

1977 September 14 - . 00:15 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.

DDDS test - . Nation: China. Agency: PRC. Apogee: 200 km (120 mi).

1978 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Agency: XPRC. Apogee: 1,000 km (600 mi).

1978 January 26 - . 04:58 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 3 - . Payload: FSW-0 No. 03. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 5.00 days. Decay Date: 1978-02-07 . USAF Sat Cat: 10611 . COSPAR: 1978-011A. Apogee: 507 km (315 mi). Perigee: 186 km (115 mi). Inclination: 57.00 deg. Period: 91.40 min. Photo surveillance; film capsule; capsule returned January 30. Second fully successful FSW mission..

1978 April 15 - . 16:39 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.

DDDS test - . Nation: China. Agency: PRC. Apogee: 200 km (120 mi).

1979 January 7 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). Other sources say launch was from Taiyuan..

1979 July 15 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). Other sources say launch was from Taiyuan..

1979 July 28 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1. FAILURE: Second stage failure.. Failed Stage: 2.

SJ-1 - . Payload: Shi Jian 1. Mass: 221 kg (487 lb). Nation: China. Agency: PRC. Spacecraft: SJ. The SJ-1 was similar in appearance to the American Telstar and conducted communications technology tests..

1979 August 21 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). Other sources say launch was from Taiyuan on 2 August..

1979 September 4 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). Other sources say launch was from Taiyuan..

1979 November 26 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). Other sources say launch was from Taiyuan on 15 October..

1980 May 18 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Test mission - . Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi).

1980 May 21 - . 02:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Test mission - . Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi).

1981 September 19 - . 21:28 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.

SJ-2A - . Payload: Shi Jian 2B. Mass: 257 kg (566 lb). Nation: China. Agency: MAI. Class: Technology. Type: Navigation technology satellite. Spacecraft: SJ. Decay Date: 1981-09-26 . USAF Sat Cat: 12842 . COSPAR: 1981-093A. Apogee: 1,598 km (992 mi). Perigee: 232 km (144 mi). Inclination: 59.50 deg. Period: 103.30 min.
SJ-2B - . Payload: Shi Jian C. Mass: 28 kg (61 lb). Nation: China. Agency: MAI. Class: Technology. Type: Navigation technology satellite. Spacecraft: SJ. Decay Date: 1982-10-06 . USAF Sat Cat: 12843 . COSPAR: 1981-093B. Apogee: 1,615 km (1,003 mi). Perigee: 233 km (144 mi). Inclination: 59.40 deg. Period: 103.50 min. Balloon for drag studies..
SJ-2 - . Payload: Shi Jian 2. Mass: 483 kg (1,064 lb). Nation: China. Agency: MAI. Class: Technology. Type: Navigation technology satellite. Spacecraft: SJ. Decay Date: 1982-08-17 . USAF Sat Cat: 12845 . COSPAR: 1981-093D. Apogee: 1,608 km (999 mi). Perigee: 232 km (144 mi). Inclination: 59.40 deg. Period: 103.40 min.

1981 December 7 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5.

Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi). Other sources say launch was from Taiyuan..

1982 September 9 - . 07:19 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 4 - . Payload: FSW-0 No. 04. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 5.00 days. Decay Date: 1982-09-21 . USAF Sat Cat: 13521 . COSPAR: 1982-090A. Apogee: 392 km (243 mi). Perigee: 172 km (106 mi). Inclination: 63.00 deg. Period: 90.20 min. Photo surveillance; film capsule recovered 14 September..

1983 August 19 - . 06:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 5 - . Payload: FSW-0 No. 05. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 5.00 days. Decay Date: 1983-09-03 . USAF Sat Cat: 14288 . COSPAR: 1983-086A. Apogee: 493 km (306 mi). Perigee: 170 km (100 mi). Inclination: 63.30 deg. Period: 91.20 min. Photo surveillance; film capsule recovered 24 August..

1984 September 12 - . 05:44 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 6 - . Payload: FSW-0 No. 06. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 5.00 days. Decay Date: 1984-09-29 . USAF Sat Cat: 15279 . COSPAR: 1984-098A. Apogee: 398 km (247 mi). Perigee: 172 km (106 mi). Inclination: 67.90 deg. Period: 90.20 min. Photo surveillance; film capsule recovered 17 September..

1985 October 21 - . 05:04 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 7 - . Payload: FSW-0 No. 07. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 5.00 days. Decay Date: 1985-11-07 . USAF Sat Cat: 16177 . COSPAR: 1985-096A. Apogee: 393 km (244 mi). Perigee: 171 km (106 mi). Inclination: 63.00 deg. Period: 90.20 min. Fanhui Shi Weixing photo surveillance satellite; film capsule recovered 26 October..

1986 October 6 - . 05:40 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 8 - . Payload: FSW-0 No. 08. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 5.00 days. Decay Date: 1986-10-23 . USAF Sat Cat: 17001 . COSPAR: 1986-076A. Apogee: 337 km (209 mi). Perigee: 169 km (105 mi). Inclination: 57.00 deg. Period: 89.60 min. Fanhui Shi Weixing recoverable satellite; capsule re-entered October 11 after five day mission..

1987 August 5 - . 06:39 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-0 No. 9 - . Payload: FSW-0 No. 09. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 5.00 days. Decay Date: 1987-08-23 . USAF Sat Cat: 18306 . COSPAR: 1987-067A. Apogee: 366 km (227 mi). Perigee: 169 km (105 mi). Inclination: 63.00 deg. Period: 89.90 min. Fanhui Shi Weixing recoverable satellite; carried microgravity experiments; return capsule recovered August 10 after five days in space..

1987 September 9 - . 07:15 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-1 No. 1 - . Payload: FSW-1 No. 01. Mass: 2,100 kg (4,600 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 8.00 days. Decay Date: 1987-10-04 . USAF Sat Cat: 18341 . COSPAR: 1987-075A. Apogee: 222 km (137 mi). Perigee: 181 km (112 mi). Inclination: 63.00 deg. Period: 88.50 min. Fanhui Shi Weixing recoverable satellite; return capsule recovered September 17 after eight days in space..

1988 August 5 - . 07:29 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-1 No. 2 - . Payload: FSW-1 No. 02. Mass: 2,100 kg (4,600 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 8.00 days. Decay Date: 1988-08-13 . USAF Sat Cat: 19368 . COSPAR: 1988-067A. Apogee: 311 km (193 mi). Perigee: 204 km (126 mi). Inclination: 63.00 deg. Period: 89.70 min. German crystal growth experiment in recoverable capsule. Results marred by hard landing..

1990 October 5 - . 06:14 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-1 No. 3 - . Payload: FSW-1 No. 03. Mass: 2,100 kg (4,600 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Decay Date: 1990-10-23 . USAF Sat Cat: 20838 . COSPAR: 1990-089A. Apogee: 312 km (193 mi). Perigee: 208 km (129 mi). Inclination: 57.00 deg. Period: 89.70 min. Fanhui Shi Weixing recoverable satellite; carried biological research experiments..

1992 August 9 - . 08:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

FSW-2 No. 1 - . Payload: FSW-2 No. 01. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 15.00 days. Decay Date: 1992-09-01 . USAF Sat Cat: 22072 . COSPAR: 1992-051A. Apogee: 332 km (206 mi). Perigee: 171 km (106 mi). Inclination: 63.10 deg. Period: 89.50 min. Fanhui Shi Weixing recoverable imaging satellite; carried microgravity experiments; capsule returned August 25 after 15 days in orbit..

1992 October 6 - . 06:20 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

Freja - . Payload: FSW-1 4 / Freja. Mass: 259 kg (570 lb). Nation: Sweden. Agency: SSC. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Freja. USAF Sat Cat: 22161 . COSPAR: 1992-064A. Apogee: 1,763 km (1,095 mi). Perigee: 590 km (360 mi). Inclination: 63.00 deg. Period: 108.90 min.
Ionospheric, auroral, amgnetospheric studies. Freja is a Swedish/German satellite designed for research into the aurora. The satellite was launched piggyback on a Long March 2C (CZ-2C) rocket and weighs 214 kg in orbit. It is a sun-pointing spinner (10 rpm) with a 2.2 m diameter. It will make high re solution measurements in the upper ionosphere and lower magnetosphere. Data will be received at Esrange, Kiruna, Sweden and at the Prince Albert Satellite Station in Canada's Saskatchewan Province. Launch time 0620 UT.
FSW-1 No. 4 - . Payload: FSW-1 No. 04. Mass: 2,100 kg (4,600 lb). Nation: China. Agency: MAI. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 6.00 days. Decay Date: 1992-10-31 . USAF Sat Cat: 22162 . COSPAR: 1992-064B. Apogee: 309 km (192 mi). Perigee: 213 km (132 mi). Inclination: 63.00 deg. Period: 89.70 min. Fanhui Shi Weixing recoverable imaging satellite; carried remote sensing, microgravity experiments; capsule recovered October 13 after 6 days in orbit..

1993 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Dong Feng 5A.

Nation: China. Agency: XPRC. Apogee: 1,000 km (600 mi).

1993 October 8 - . 08:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Chang Zheng 2C.

FSW-1 No. 5 - . Payload: Jian Bing 93. Mass: 2,099 kg (4,627 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Decay Date: 1993-10-28 . USAF Sat Cat: 22859 . COSPAR: 1993-063A. Apogee: 2,860 km (1,770 mi). Perigee: 181 km (112 mi). Inclination: 56.60 deg. Period: 116.50 min.
The only FSW-1 mission conducted during 1993-1994 was launched into an orbit of 209 km by 300 km at an inclination of 57.0 deg. In addition to an Earth observation Payload, FSW-1 5 carried microgravity research equipment and a diamond-studded medallion commemorating the 100th anniversary of Chairman Mao Tse-Tung's birth. The spacecraft operated normally until 16 October when an attempt to recover the satellite failed. An attitude control system failure aligned the spacecraft 90 deg from its desired position, causing the re-entry capsule to be pushed into a higher elliptical orbit (179 km by 3031 km) instead of returning to Earth. Natural decay did not bring the capsule back until March 12, 1996.

1994 July 3 - . 08:00 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. Launch Pad: LA2B?. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

FSW-2 No. 2 - . Payload: FSW-2 No. 02. Mass: 2,600 kg (5,700 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 15.00 days. Decay Date: 1994-09-13 . USAF Sat Cat: 23145 . COSPAR: 1994-037A. Apogee: 350 km (210 mi). Perigee: 207 km (128 mi). Inclination: 62.90 deg. Period: 90.08 min.
The second Fanhui Shi Weixing FSW-2 was launched on 3 July 1994 into an orbit of 173 km by 343 km at an inclination of 63.0 deg. The spacecraft remained in orbit for 15 days, making four small manoeuvres before successfully returning to Earth. The payload included Earth observation systems, a biological experiment, and microgravity research instruments. The retrievable capsule was recovered in China on July 18

1996 October 20 - . 07:20 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.

FSW-2 No. 3 - . Payload: FSW-2 No. 03. Mass: 2,600 kg (5,700 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 15.00 days. Decay Date: 1996-12-03 . USAF Sat Cat: 24634 . COSPAR: 1996-059A. Apogee: 133 km (82 mi). Perigee: 121 km (75 mi). Inclination: 63.00 deg. Period: 87.00 min. Final launch in the FSW series. Landed in China on November 4 after 15 days in orbit..

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