Model of Fengyun-2 meteorological satellite in Shanghai Science & Technology Museum. | |
Mission type | Weather |
---|---|
Operator | National Satellite Meteorological Centre |
COSPAR ID | 2012-002A |
SATCAT no. | 38049 |
Spacecraft properties | |
Launch mass | 1,369 kilograms (3,018 lb) |
Start of mission | |
Launch date | 13 January 2012, 00:56 (2012-01-13UTC00:56Z) UTC |
Rocket | Chang Zheng 3A Y22 |
Launch site | Xichang LA-3 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 86.5° East |
Perigee altitude | 35,784 kilometres (22,235 mi) |
Apogee altitude | 35,796 kilometres (22,243 mi) |
Inclination | 1.00 degrees |
Period | 1,435.98 minutes |
Epoch | 31 October 2013, 22:00:50 UTC |
Fengyun 2-07 or FY-2-07 (Chinese: 风云二号07 meaning Wind Cloud 2-07), also known as Fengyun-2F or FY-2F, is a Chinese weather satellite operated by China's National Satellite Meteorological Centre. Part of the Fengyun programme, it was the sixth Fengyun 2 geostationary satellite to be launched.
Fengyun 2-07 was launched by a Long March 3A carrier rocket, with the serial number Y22, flying from Launch Area 3 at the Xichang Satellite Launch Centre. The launch took place on 13 January 2012 at 00:56 UTC, and resulted in the successful deployment of the satellite into a geosynchronous transfer orbit. After raising itself into its operational geostationary orbit, by means of an FG-36 apogee motor, the satellite will be positioned at a longitude of 86.5 degrees East.
At launch, Fengyun 2-07 had a mass of 1,369 kilograms (3,018 lb), however by the time it reaches its operational orbit, this will have decreased to 536 kilograms (1,182 lb), partly through jettisoning the FG-36. The spacecraft is cylindrical, with a diameter of 2.1 metres (6 ft 11 in), and a length of 4.5 metres (15 ft) fully deployed. It is spin-stabilised at a rate of 100 rpm, and carries a five-channel Stretched Visible and Infrared Spin Scan Radiometer, or S-VISSR, capable of producing visible light and infrared images of the Earth. The S-VISSR will return visible-light images with a resolution of 1.25 kilometres (0.78 mi), and infrared images with a resolution of 5 kilometres (3.1 mi). It will produce a full-disc image every thirty minutes, as well as imaging smaller areas of interest. In addition to S-VISSR, Fengyun 2-07 also carries an x-ray detector to monitor the Sun, and detect solar flares.
References
- "FENGYUN 2F Satellite details 2012-002A NORAD 38049". N2YO. 31 October 2013. Retrieved 31 October 2013.
- 长三甲遥二十二火箭将发射风云二号卫星 (in Chinese). China Academy of Launch Vehicle Technology. 15 December 2011. Archived from the original on 7 April 2014. Retrieved 13 January 2012.
- "Feng-Yun-2". AllMetSat. Archived from the original on 3 January 2012. Retrieved 13 January 2012.
- ^ Krebs, Gunter. "FY 2A, 2B, 2C, 2D, 2E, 2F, 2G, 2H". Gunter's Space Page. Archived from the original on 22 February 2012. Retrieved 13 January 2012.
- ^ Barbosa, Rui C. (12 January 2012). "China launch again – Long March 3A launches FengYun-2F". NASASpaceflight.com. Archived from the original on 16 January 2012. Retrieved 13 January 2012.
- "Status of current and future CGMS Members' satellites". World Meteorological Organization. 15 December 2011. Archived from the original on 26 June 2012. Retrieved 13 January 2012.
- "Stretched Visible and Infrared Spin Scan Radiometer (S-VISSR)". World Meteorological Organization. June 2008. Archived from the original on 25 May 2024. Retrieved 13 January 2012.
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