CBERS-2B

Launch Success

Liftoff Time (GMT)

03:26:00

Wednesday September 19, 2007

Mission Details

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CBERS-2B

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CBERS-2B was a 1,450-kilogram (3,200 lb) spacecraft built by the China Academy of Space Technology and based on the Phoenix-Eye 1 satellite bus. The spacecraft was powered by a single solar array, which provided 1,100 watts of electricity for the satellite's systems. The instrument suite aboard the CBERS-2B spacecraft consisted of three systems: the Wide Field Imager (WFI) produced visible-light to near-infrared images with a resolution of 260 metres (850 ft) and a swath width of 890 kilometres (550 mi); a high-resolution CCD camera was used for multispectral imaging at a resolution of 20 metres (66 ft) with a swath width of 113 kilometres (70 mi); the third instrument, the High-Resolution Camera (HRC) was a panchromatic imager with a resolution of 2.7 metres (8 ft 10 in) and a swath width of 27 kilometres (17 mi). HRC replaced the lower-resolution Infrared Multispectral Scanner instrument flown on earlier CBERS satellites.

Sun-Synchronous Orbit

1 Payload

1,450 kilograms

Rocket

Active
Long March 4B

Active Since 1999

China Aerospace Science and Technology Corporation logo

Agency

CASC

Price

$64.68 million

Rocket

Height: 46.97m

Payload to Orbit

LEO: 4,200 kg

GTO: 1,500 kg

Liftoff Thrust

2,993 Kilonewtons

Fairing

Diameter: 3.8m

Height: 11.74m

Stages

3

Launch Site

LC-7

Taiyuan Satellite Launch Center, China

Fastest Turnaround

32 days 15 hours

Stats

Long March 4B


10th

Mission

1st

Mission of 2007

2007


45th

Orbital launch attempt