FY-2 (original) (raw)

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FY-2

FY-2
Geosynchronous Chinese communications satellite.

Chinese earth weather satellite. The Feng Yun 2 spin-stabilized geosynchronous meteorological spacecraft was slightly more massive than China's DFH-2 communications satellite. Meteorology satellite operated by National Satellite Meteorological Centre, China. Launched 1997 - 2014.

Status: Operational 1997. First Launch: 1997-06-10. Last Launch: 2014-12-31. Number: 7 . Gross mass: 593 kg (1,307 lb). Height: 4.50 m (14.70 ft). Span: 2.10 m (6.80 ft).

The Feng Yun 2 spacecraft bus diameter was 2.1 m, and total height on-station was about 4.5 m. The major payload was a scanning radiometer with S-band and UHF data distribution. The two principal sensors were visible and infrared imaging instruments with best resolution of 1.25 km and 5.0 km respectively. A water vapor sensor was also carried.

The first Fen Yung 2 satellite was undergoing final checkout on 2 April 1994 before being mated to its launch vehicle when a fire and explosion erupted, destroying the vehicle, killing one worker and injuring 20 others. The operational satellites finally launched was stationed over 104.6E. China planned to put six meteorological satellites into orbit from 2002 to 2008 to offer comprehensive weather services for the 2008 Olympic Games. These included FY-2C in 2003 and FY-2D in 2006.

More at: FY-2.

Family: Earth, Earth weathersat, Geosynchronous orbit. Country: China. Launch Vehicles: Chang Zheng 3, Chang Zheng 3A. Launch Sites: Xichang, Xichang LC2, Xichang LC1. Agency: SARTI, China Aerospace. Bibliography: 119, 2, 4, 424, 530, 532, 552, 554, 12465.

Photo Gallery

	FY-2

	FY-2ACredit: Manufacturer Image

	FY-2BCredit: via Chen Lan

1994 April 2 - .

Chinese satellite accident. - . Nation: China. Spacecraft: FY-2. The first Fen Yung 2 geostationary weather satellite was undergoing final checkout before being mated to its launch vehicle when a fire and explosion erupted, destroying the vehicle, killing one worker and injuring 20 others..

1997 June 10 - . 12:01 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. LV Family: CZ. Launch Vehicle: Chang Zheng 3.

FY-2A - . Payload: Fengyun 2A. Mass: 1,250 kg (2,750 lb). Nation: China. Agency: CASC. Manufacturer: SARTI. Class: Earth. Type: Weather satellite. Spacecraft: FY-2. USAF Sat Cat: 24834 . COSPAR: 1997-029A. Apogee: 35,784 km (22,235 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.80 deg. Period: 1,436.10 min.
Geosynchronous weather satellite; also known as FY-2B. Operated in geosynchronous orbit at 105 deg E in 1997-2000; 85 deg E in 2000.. The FY-2A stopped transmission in April 1998 but was put back into partial operation in December 1998. Its imager then failed completely on 30 September 1998 and it was retired in April 2000. As of 4 September 2001 located at 83.55 deg E drifting at 0.074 deg W per day. As of 2007 Mar 11 located at 58.96E drifting at 0.025W degrees per day.

2000 June 25 - . 11:50 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. LV Family: CZ. Launch Vehicle: Chang Zheng 3.

FY-2 - . Mass: 1,250 kg (2,750 lb). Nation: China. Agency: CASC. Manufacturer: Shanghai Institute of Satellite Engineering. Class: Earth. Type: Weather satellite. Spacecraft: FY-2. USAF Sat Cat: 26382 . COSPAR: 2000-032A. Apogee: 35,790 km (22,230 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.80 deg. Period: 1,436.20 min.
Second Fengyun-2 weather satellite, replacing the first FY-2 (retired in April after a three year service life). The spin-stabilised FY-2 fired its solid apogee motor early on Jun 26. By July 3, it was in a 35,791 x 35,804 km x 1.1 deg orbit drifting over the Pacific. Stationed at 104 deg E. Positioned in geosynchronous orbit at 110 deg E in 2000. As of 5 September 2001 located at 104.56 deg E drifting at 0.030 deg W per day. As of 2007 Mar 11 located at 34.70W drifting at 0.629W degrees per day.

2004 October 19 - . 01:20 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: Chang Zheng 3A.

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: 0.70 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.

2006 December 8 - . 00:53 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: Chang Zheng 3A.

FY-2D - . Payload: Fengyun 2D. Mass: 1,380 kg (3,040 lb). 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: 2.60 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.

2008 December 23 - . 00:54 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: Chang Zheng 3A.

FY-2E - . Mass: 1,380 kg (3,040 lb). 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: 2.60 deg. Period: 1,436.20 min. Member of China's geosynchronous weather satellite constellation..

2012 January 13 - . 00:56 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: Chang Zheng 3A.

FY-2F - . Mass: 1,380 kg (3,040 lb). Nation: China. Class: Earth. Type: Weather satellite. Spacecraft: FY-2. USAF Sat Cat: 38049 . COSPAR: 2012-002A. Apogee: 35,811 km (22,251 mi). Perigee: 35,758 km (22,218 mi). Inclination: 2.40 deg. Period: 1,436.00 min. Replenishment of China's geosynchronous weather satellite constellation..

2014 December 31 - . 01:02 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: Chang Zheng 3A.

FY-2-08 - . Mass: 1,380 kg (3,040 lb). Nation: China. Class: Earth. Type: Weather satellite. Spacecraft: FY-2. USAF Sat Cat: 40367 . COSPAR: 2014-090A. Apogee: 35,796 km (22,242 mi). Perigee: 35,781 km (22,233 mi). Inclination: 1.63 deg. Period: 1,436.20 min. Eighth FY-2 weather satellite for China's National Satellite Monitoring Centre. The satellite was placed in GEO using a solid apogee motor which was then ejected.. Stationed in geosynchronous orbit at 100 deg east..

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