CBERS-2B: Difference between revisions
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{{short description|Chinese-Brazilian remote sensing satellite}} |
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{{EngvarA|date=December 2020}} |
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| name = CBERS-2B |
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| mission_duration = 2 years planned<ref name="EOP">{{cite web|url=https://directory.eoportal.org/web/eoportal/satellite-missions/c-missions/cbers-1-2|title=CBERS-1 (China-Brazil Earth Resources Satellite) - 1st Generation Satellite Series|publisher=European Space Agency|work=Earth Observation Portal|accessdate=1 December 2013}}</ref> |
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| insignia = CBERS-2B patch.png |
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⚫ | | operator = [[China National Space Administration|CNSA]] / [[National Institute for Space Research|INPE]]<ref name="gsp">{{cite web|url=http://space.skyrocket.de/doc_sdat/cbers-1.htm|title=CBERS 1, 2, 2B / ZY 1A, 1B, 1B2|first=Gunter|last=Krebs|work=Gunter's Space Page|access-date=1 December 2013}}</ref> |
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| COSPAR_ID = 2007-042A |
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| SATCAT = 32062 |
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| mission_duration = 2 years (planned)<br/>{{time interval|19 September 2007, 03:26:13|10 May 2010}} (achieved) |
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| manufacturer = [[China Academy of Space Technology|CAST]] |
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| power = 1100 watts |
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| launch_contractor = [[Shanghai Academy of Spaceflight Technology|SAST]] |
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| orbit_epoch = 19 September 2007 |
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| orbit_periapsis = 773 km |
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| orbit_apoapsis = 774 km |
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⚫ | '''China–Brazil Earth Resources Satellite 2B''' ('''CBERS-2B'''), also known as '''Ziyuan 1-2B''', was a [[remote sensing]] satellite operated as part of the [[China–Brazil Earth Resources Satellite program]] between the [[People's Republic of China|Chinese]] [[Center for Resources Satellite Data and Application of People's Republic of China|Center for Resources Satellite Data and Application]] and [[Brazil]]ian [[National Institute for Space Research]].<ref name="gsp"/> The third CBERS satellite to fly, it was launched by China in 2007 to replace [[CBERS-2]].<ref name="launchlog"/> |
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== Spacecraft == |
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CBERS-2B was a {{convert|1450|kg|abbr=off|adj=on}} spacecraft built by the [[China Academy of Space Technology]] and based on the [[Phoenix-Eye 1]] [[satellite bus]].<ref name="gsp"/> The spacecraft was powered by a single solar array, which provided 1100 watts of electricity for the satellite's systems.<ref name="EOP">{{cite web|url=https://directory.eoportal.org/web/eoportal/satellite-missions/c-missions/cbers-1-2|title=CBERS-1 (China-Brazil Earth Resources Satellite) - 1st Generation Satellite Series|publisher=European Space Agency|work=Earth Observation Portal|access-date=1 December 2013}}</ref><ref name="desc">{{cite web |url=http://www.cbers.inpe.br/ingles/satellites/description_cbers1_2_2b.php|title=CBERS-1, 2 and 2B Description|publisher=INPE|access-date=1 December 2013|archive-url=https://web.archive.org/web/20140120084318/http://www.cbers.inpe.br/ingles/satellites/description_cbers1_2_2b.php#|archive-date=2014-01-20|url-status=dead}}</ref> The 1.8 m x 2.0 m x 2.2 m, [[Three-axis stabilization|triaxially-stabilized]] spacecraft carries a low 20 m resolution, and a higher 2.5 m resolution camera. The data help in [[Agriculture|crop estimation]], [[urban planning]], [[water resource management]], and [[military intelligence]].<ref name="Display">{{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=2007-042A|title=Display: CBERS 2B 2007-042A|publisher=NASA|date=14 May 2020|access-date=26 July 2020}} {{PD-notice}}</ref> |
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| manufacturer = |
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The instrument suite aboard the CBERS-2B spacecraft consisted of three systems: |
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* Wide Field Imager (WFI) produced visible-light to near-infrared images with a resolution of {{convert|260|m|abbr=off|sp=us}} and a swath width of {{convert|890|km|abbr=off|sp=us}}. |
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* High-resolution CCD camera was used for multispectral imaging at a resolution of {{convert|20|m|abbr=on}} with a swath width of {{convert|113|km|abbr=on}}. |
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* High Resolution Camera (HRC) was a panchromatic imager with a resolution of {{convert|2.5|m|abbr=on}} and a swath width of {{convert|27|km|abbr=on}}.<ref name="cameras">{{cite web |url=http://www.cbers.inpe.br/ingles/satellites/cameras_cbers1_2_2b.php|title=CBERS-1, 2 and 2B Cameras|publisher=INPE|access-date=1 December 2013|archive-url=https://web.archive.org/web/20140120084308/http://www.cbers.inpe.br/ingles/satellites/cameras_cbers1_2_2b.php#|archive-date=2014-01-20|url-status=dead}}</ref> |
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The HRC replaced the lower-resolution Infrared Multispectral Scanner instrument flown on earlier CBERS satellites.<ref name="gsp"/> |
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| orbit_reference = [[Geocentric orbit|Geocentric]] |
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| orbit_periapsis = {{convert|744|km|mi}}<ref name="n2yo"/> |
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| orbit_apoapsis = {{convert|791|km|mi}}<ref name="n2yo"/> |
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| orbit_semimajor = {{convert|7138.610|km|mi}}<ref name="n2yo"/> |
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| orbit_eccentricity = 0.0032873<ref name="n2yo"/> |
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| orbit_RAAN = 45.48 degrees<ref name="n2yo"/> |
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| orbit_arg_periapsis = 65.010 degrees<ref name="n2yo"/> |
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| orbit_mean_anomaly = 14.39 degrees<ref name="n2yo"/> |
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| orbit_mean_motion = 14.39<ref name="n2yo"/> |
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| orbit_rev_number = 37,986<ref name="n2yo"/> |
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| apsis = gee |
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== Launch == |
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⚫ | A [[Long March 4B]] [[Launch vehicle|carrier rocket]], operated by the [[China Academy of Launch Vehicle Technology]] (CALT), was used to launch CBERS-2B. The launch took place at 03:26:13 UTC on 19 September 2007, using [[Taiyuan Satellite Launch Center|Launch Complex 7]] at the [[Taiyuan Satellite Launch Center]] (TLSC).<ref name="launchlog"/> The satellite was successfully placed into a [[Sun-synchronous orbit]].<ref name="UCS">{{cite web|url=http://www.ucsusa.org/assets/documents/nwgs/UCS_Satellite_Database_7-1-10.txt|title=UCS Satellite Database|publisher=Union of Concerned Scientists|access-date=1 December 2013|url-status=dead|archiveurl=https://web.archive.org/web/20100909133456/http://www.ucsusa.org/assets/documents/nwgs/UCS_Satellite_Database_7-1-10.txt|archive-date=9 September 2010}}</ref> |
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⚫ | '''China–Brazil Earth Resources Satellite 2B''' ('''CBERS-2B'''), also known as '''Ziyuan |
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== Last contact == |
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CBERS-2B was a {{convert|1450|kg|lb|adj=on}} spacecraft built by the [[China Academy of Space Technology]] and based on the [[Phoenix-Eye 1]] [[satellite bus]].<ref name="gsp"/> The spacecraft was powered by a single solar array, which provided 1,100 watts of electricity for the satellite's systems.<ref name="EOP"/><ref name="desc">{{cite web|url=http://www.cbers.inpe.br/ingles/satellites/description_cbers1_2_2b.php|title=CBERS-1, 2 and 2B Description|publisher=INPE|accessdate=1 December 2013}}</ref> 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 {{convert|260|m}} and a swath width of {{convert|890|km}}; a high-resolution CCD camera was used for multispectral imaging at a resolution of {{convert|20|m}} with a swath width of {{convert|113|km}}; the third instrument, the High Resolution Camera (HRC) was a panchromatic imager with a resolution of {{convert|2.7|m}} and a swath width of {{convert|27|km}}.<ref name="cameras">{{cite web|url=http://www.cbers.inpe.br/ingles/satellites/cameras_cbers1_2_2b.php|title=CBERS-1, 2 and 2B Cameras|publisher=INPE|accessdate=1 December 2013}}</ref> HRC replaced the lower-resolution Infrared Multispectral Scanner instrument flown on earlier CBERS satellites.<ref name="gsp"/> |
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The CBERS-2B spacecraft suffered a power system failure on 10 May 2010, leaving it unable to continue operations. It remains in orbit.<ref name="n2yo"/> |
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⚫ | A [[Long March |
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{{Portal|Spaceflight}} |
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CBERS-2B suffered a power system failure on 10 May 2010, leaving it unable to continue operations. As of {{Orbit|epoch|14 December 2014}} it remains in orbit, with a [[apsis|perigee]] of {{convert|{{Orbit|perigee|744}}|km|mi}}, an [[apsis|apogee]] of {{convert|{{Orbit|apogee|791}}|km|mi}}, {{Orbit|inclination|98.27}} degrees inclination and a [[orbital period|period]] of {{Orbit|period|100.05}} minutes. It has a [[semimajor axis]] of {{convert|{{Orbit|semimajor axis|7138.610}}|km|mi}}, and [[Orbital eccentricity|eccentricity]] of {{orbit|eccentricity|0.0032873}}.{{orbit|ref|<ref name="n2yo"/>}} |
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{{reflist}} |
{{reflist}} |
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{{CBERS}} |
{{CBERS}} |
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{{Ziyuan}} |
{{Ziyuan}} |
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{{Use British English|date=January 2014}} |
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[[Category:Spacecraft launched in 2007]] |
[[Category:Spacecraft launched in 2007]] |
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[[Category:China–Brazil Earth Resources Satellite program]] |
[[Category:China–Brazil Earth Resources Satellite program]] |
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[[Category:Derelict satellites orbiting Earth]] |
[[Category:Derelict satellites orbiting Earth]] |
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[[Category: |
[[Category:Earth observation satellites of Brazil]] |
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[[Category:Satellites of China]] |
[[Category:Satellites of China]] |
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[[Category:2007 in China]] |
[[Category:2007 in China]] |
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[[Category:Spacecraft launched by Long March rockets]] |
Latest revision as of 17:15, 13 July 2024
Mission type | Remote sensing |
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Operator | CNSA / INPE[1] |
COSPAR ID | 2007-042A |
SATCAT no. | 32062 |
Mission duration | 2 years (planned) 2 years, 7 months and 20 days (achieved) |
Spacecraft properties | |
Spacecraft type | CBERS |
Bus | Phoenix-Eye 1[1] |
Manufacturer | CAST |
Launch mass | 1450 kg |
Dimensions | 1.8 x 2.0 x 2.2 m |
Power | 1100 watts |
Start of mission | |
Launch date | 19 September 2007, 03:26:13 UTC[2] |
Rocket | Long March 4B |
Launch site | Taiyuan Satellite Launch Center, LC-7 |
Contractor | SAST |
End of mission | |
Last contact | 10 May 2010 |
Orbital parameters | |
Reference system | Geocentric orbit[3] |
Regime | Sun-synchronous orbit |
Perigee altitude | 773 km |
Apogee altitude | 774 km |
Inclination | 98.60° |
Period | 100.30 minutes |
Epoch | 19 September 2007 |
China–Brazil Earth Resources Satellite 2B (CBERS-2B), also known as Ziyuan 1-2B, was a remote sensing satellite operated as part of the China–Brazil Earth Resources Satellite program between the Chinese Center for Resources Satellite Data and Application and Brazilian National Institute for Space Research.[1] The third CBERS satellite to fly, it was launched by China in 2007 to replace CBERS-2.[2]
Spacecraft
[edit]CBERS-2B was a 1,450-kilogram (3,200-pound) spacecraft built by the China Academy of Space Technology and based on the Phoenix-Eye 1 satellite bus.[1] The spacecraft was powered by a single solar array, which provided 1100 watts of electricity for the satellite's systems.[4][5] The 1.8 m x 2.0 m x 2.2 m, triaxially-stabilized spacecraft carries a low 20 m resolution, and a higher 2.5 m resolution camera. The data help in crop estimation, urban planning, water resource management, and military intelligence.[6]
The instrument suite aboard the CBERS-2B spacecraft consisted of three systems:
- Wide Field Imager (WFI) produced visible-light to near-infrared images with a resolution of 260 meters (850 feet) and a swath width of 890 kilometers (550 miles).
- High-resolution CCD camera was used for multispectral imaging at a resolution of 20 m (66 ft) with a swath width of 113 km (70 mi).
- High Resolution Camera (HRC) was a panchromatic imager with a resolution of 2.5 m (8 ft 2 in) and a swath width of 27 km (17 mi).[7]
The HRC replaced the lower-resolution Infrared Multispectral Scanner instrument flown on earlier CBERS satellites.[1]
Launch
[edit]A Long March 4B carrier rocket, operated by the China Academy of Launch Vehicle Technology (CALT), was used to launch CBERS-2B. The launch took place at 03:26:13 UTC on 19 September 2007, using Launch Complex 7 at the Taiyuan Satellite Launch Center (TLSC).[2] The satellite was successfully placed into a Sun-synchronous orbit.[8]
Last contact
[edit]The CBERS-2B spacecraft suffered a power system failure on 10 May 2010, leaving it unable to continue operations. It remains in orbit.[3]
References
[edit]- ^ a b c d e Krebs, Gunter. "CBERS 1, 2, 2B / ZY 1A, 1B, 1B2". Gunter's Space Page. Retrieved 1 December 2013.
- ^ a b c McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 1 December 2013.
- ^ a b "CBERS 2B Satellite details 2007-042A NORAD 32062". N2YO. 25 January 2015. Retrieved 25 January 2015.
- ^ "CBERS-1 (China-Brazil Earth Resources Satellite) - 1st Generation Satellite Series". Earth Observation Portal. European Space Agency. Retrieved 1 December 2013.
- ^ "CBERS-1, 2 and 2B Description". INPE. Archived from the original on 20 January 2014. Retrieved 1 December 2013.
- ^ "Display: CBERS 2B 2007-042A". NASA. 14 May 2020. Retrieved 26 July 2020. This article incorporates text from this source, which is in the public domain.
- ^ "CBERS-1, 2 and 2B Cameras". INPE. Archived from the original on 20 January 2014. Retrieved 1 December 2013.
- ^ "UCS Satellite Database". Union of Concerned Scientists. Archived from the original on 9 September 2010. Retrieved 1 December 2013.