Shijian XI-01
From Infogalactic: the planetary knowledge core
Mission type | Technology |
---|---|
Operator | CASC |
COSPAR ID | 2009-061A |
SATCAT № | 36088 |
Mission duration | 3 years planned |
Spacecraft properties | |
Manufacturer | ADSC |
Start of mission | |
Launch date | 12 November 2009, 02:45 | UTC
Rocket | Chang Zheng 2C |
Launch site | Jiuquan LA-4/SLS-2 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-Synchronous |
Perigee | 691 kilometres (429 mi)[1] |
Apogee | 708 kilometres (440 mi)[1] |
Inclination | 98.26 degrees[1] |
Period | 98.62 minutes[1] |
Epoch | 25 January 2015, 01:37:35 UTC[1] |
Shijian XI-01 (Chinese: 实践十一号01星,[2] meaning Practice 11-01)[3] is a Chinese technology demonstration satellite which was launched in November 2009.[4] It was built by the Aerospace Dongfanghong Satellite Company, and is being operated by the China Aerospace Science and Technology Corporation.[2]
Shijian XI-01 was launched from the SLS-2 pad of Launch Area 4 at the Jiuquan Satellite Launch Centre, atop a Long March 2C carrier rocket. Liftoff occurred at 02:45 GMT on 12 November 2009.[5] The satellite separated into an orbit with an apogee of 699.9 kilometres (434.9 mi), a perigee of 690.5 kilometres (429.1 mi), and 98.3° inclination.[3] It has the International Designator 2009-061A.
References
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