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¡£¡£The China Brazil Earth Resources Satellite (CBERS) was jointly developed by China and Brazil since 1988. The first CBERS (CBRES-1) was successfully launched on October 14, 1999. After finishing on-orbit tests in China, it was relegated to China Center for Resources Satellite Data and Application (CRESDA) and switched to application and routine operation stage.
¡£¡£There are 3 kind cameras on the CBERS-1. They can make optical observation for global area and transmit remotely sensed data to ground receiving stations in high speed. After processes these data, CRESDA provides their end-users various image production.


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¡£¡£Orbit: sun-synchronous recurrent and frozen orbit
¡£¡£Mean altitude: 778Km
¡£¡£Local time at descending node: 10:30 AM
¡£¡£Repeat cycle :26 day
¡£¡£Repeat cycle: 100.26 min


¡£¡£Revolution/Day: 14+9/26
¡£¡£Inter-track distance: 107.4 Km
¡£¡£Time interval between adjacent track: 3 days


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¡£¡£¡¤Three sensors:
¡£¡£¡îCharge Coupled Device Camera (CCD)
¡£¡£¡îInfrared Multi-Spectral Scanner (IPMSS)
¡£¡£¡îWide Field Imager (WFI)
¡£¡£¡¤High Density Digital Recorder (HDDR)
¡£¡£¡¤Data Collection system (DCS)
¡£¡£¡¤Space Environmental Monitor (SEM)
¡£¡£¡¤Data Transmission System (DTS)
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  ¡£¡£The CCD Camera has a nadir spatial resolution of 19.5 meters and a swath width of 113Km. It has four spectral bands in the visible and near infrared range and one panchromatic band. The maximum side-looking angle is ¡À320 .It can perform on-orbit focal length adjusting and onboard calibration using internal lamp calibration system.

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The IRMSS instrument has spatial resolution of 78 meters(for three visible to short-wave infrared spectral bands) and 156 meters(for one thermal infrared band). It has internal lamp calibration system as well as a solar calibration system. Its swath width is 119.5 Km.


CBERS-1 Sensor Characteristics
 
¡£¡£The WFI camera has a nadir spatial resolution of 256 meters in two visible to near-infrared spectral bands. It has a swath width of 890 Km. It s relatively wider swath makes it possible to achieve repeated ground coverage in a short time period. The On-board calibration system on WFI consists of a diffuse reflective window for relative radiometric calibration.
The key property parameters of these three sensors aboard the CBERS-1 given in Table 1¡£


¡£¡£Besides the above three types of sensors, the CBERS-1 is also equipped with a high density magnetic recorder for recording CCD data of the interested area. When the CBERS-1 is in the range of a receiving station, the recorded CCD data on the satellite will be play back and received by the receiving station. The key parameters of the on-board high density magnetic recorder are as follows:
¡£¡£The speed of record/playback is 53 Mb/s, the ratio of error code is less than 1x10 -6, both the lengths of recording and playback are not less than 15 minutes¡£


CCD


WFI


IRMSS
 


CBERS-1 Sensor Characteristics

Sensor Name
CCD camera
WFI
IRMSS
Sensor Type
Pushbroom
Pushbroom (split camera)
Scanner (forward and reverse)
VIS/NIR Bands
1: 0.45 to 0.52
2:0.52¡«0.59mm
3:0.63¡«0.69mm
4:0.77¡«0.89mm
5:0.51¡«0.73mm
10:0.63¡«0.69mm
11:0.77¡«0.89mm
6:0.50¡«0.90mm
SWIR Bands
None
None
7:1.55¡«1.75mm
8:2.08¡«2.35mm
Thermal Bands
None
None
9:10.4¡«12.5mm
Radiometric Quantization
8bit
8bit
8bit
Swath Width
113km
890km
119.5km
Samples/band
5812bands
3456bands
Bands 6, 7, 8: 1536;
Band 9: 768
Spatial resolution (nadir)
19.5m
258m
Bands6¡¢7¡¢8:78m
Bands9:156Ã×
Side looking ?
Yes£¨-32¡ã¡«+32¡ã£©
No
No
FOV
8.32¡ã
59.6¡ã
8.80¡ã


 
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