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{{EngvarA|date=December 2020}}
{{EngvarA|date=December 2020}}
{{Use dmy dates|date=December 2020}}
{{Use dmy dates|date=December 2020}}
{{Infobox spaceflight|auto=all
{{Infobox spaceflight
| name = CBERS-2B
| auto = all
| image =
| name = CBERS-2B
| image_caption =
| image = CBERS-2B anecoica.jpg
| insignia =CBERS-2B patch.png
| image_caption =
| insignia = CBERS-2B patch.png

| mission_type = [[Remote sensing]]
| mission_type = [[Remote sensing]]
| 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>
| 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>
| website =
| website =
| COSPAR_ID = 2007-042A
| COSPAR_ID = 2007-042A
| SATCAT = 32062
| SATCAT = 32062
| mission_duration = 2 years (planned)<br/>{{time interval|19 September 2007, 03:26:13|10 May 2010}} (achieved)
| 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|access-date=1 December 2013}}</ref>
⚫
| spacecraft_type = [[China–Brazil Earth Resources Satellite program|CBERS]]

⚫
| spacecraft_bus = [[Phoenix-Eye 1]]<ref name="gsp"/>
⚫
| spacecraft_type = [[China–Brazil Earth Resources Satellite program|CBERS]]
⚫
| manufacturer = [[China Academy of Space Technology|CAST]]
⚫
| spacecraft_bus = [[Phoenix-Eye 1]]<ref name="gsp"/>
| manufacturer = [[China Academy of Space Technology|CAST]]
| dry_mass =
| dry_mass =
| launch_mass = 1450 kg
| launch_mass = 1450 kg
| dimensions = 1.8 x 2.0 x 2.2 m
| dimensions = 1.8 x 2.0 x 2.2 m
| power = 1100 watts
⚫
| launch_date = 19 September 2007,<br/>03:26:13 UTC<ref name="launchlog">{{cite web|url=http://planet4589.org/space/log/launchlog.txt|title=Launch Log|first=Jonathan|last=McDowell|work=Jonathan's Space Page|access-date=1 December 2013}}</ref>
| power = 1100 watts
⚫
| launch_rocket = [[Long March 4B]]

⚫
| launch_site = [[Taiyuan Satellite Launch Center]], [[Taiyuan Satellite Launch Center|LC-7]]
⚫
| launch_date = 19 September 2007,<br/>03:26:13 UTC<ref name="launchlog">{{cite web|url=http://planet4589.org/space/log/launchlog.txt|title=Launch Log|first=Jonathan|last=McDowell|work=Jonathan's Space Page|access-date=1 December 2013}}</ref>
| launch_contractor = [[Shanghai Academy of Spaceflight Technology|SAST]]
⚫
| launch_rocket = [[Long March 4B]]
⚫
| last_contact = 10 May 2010
⚫
| launch_site = [[Taiyuan Satellite Launch Center]], [[Taiyuan Satellite Launch Center|LC-7]]
⚫
| decay_date =
⚫
| launch_contractor = [[Shanghai Academy of Spaceflight Technology|SAST]]
| orbit_epoch = 19 September 2007

⚫
| orbit_reference = [[Geocentric orbit]]<ref name="n2yo">{{cite web|url=http://www.n2yo.com/satellite/?s=32062|title=CBERS 2B Satellite details 2007-042A NORAD 32062|publisher=N2YO|date=25 January 2015 |access-date=25 January 2015}}</ref>
⚫
| last_contact = 10 May 2010
| decay_date =
| orbit_regime = [[Sun-synchronous orbit]]
| orbit_periapsis = 773 km

| orbit_epoch = 19 September 2007
| orbit_apoapsis = 774 km
⚫
| orbit_inclination = 98.60°
⚫
| orbit_reference = [[Geocentric orbit]]<ref name="n2yo">{{cite web|url=http://www.n2yo.com/satellite/?s=32062|title=CBERS 2B Satellite details 2007-042A NORAD 32062|publisher=N2YO|date=25 January 2015 |access-date=25 January 2015}}</ref>
| orbit_regime = [[Sun-synchronous orbit]]
| orbit_period = 100.30 minutes
| orbit_periapsis = 773 km
| apsis = gee
| orbit_apoapsis = 774 km
| instruments =
⚫
| orbit_inclination = 98.60°
| orbit_period = 100.30 minutes
| apsis = gee

⚫
| instruments =
}}
}}
'''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"/>
'''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"/>


== Spacecraft ==
== Spacecraft ==
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"/><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, [[Attitude control|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>
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>


The instrument suite aboard the CBERS-2B spacecraft consisted of three systems:
The instrument suite aboard the CBERS-2B spacecraft consisted of three systems:
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== Launch ==
== Launch ==
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>
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>


== Last contact ==
== Last contact ==
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[[Category:Satellites of China]]
[[Category:Satellites of China]]
[[Category:2007 in China]]
[[Category:2007 in China]]
[[Category:Spacecraft launched by Long March rockets]]

Latest revision as of 17:15, 13 July 2024

CBERS-2B
Mission typeRemote sensing
OperatorCNSA / INPE[1]
COSPAR ID2007-042A Edit this at Wikidata
SATCAT no.32062
Mission duration2 years (planned)
2 years, 7 months and 20 days (achieved)
Spacecraft properties
Spacecraft typeCBERS
BusPhoenix-Eye 1[1]
ManufacturerCAST
Launch mass1450 kg
Dimensions1.8 x 2.0 x 2.2 m
Power1100 watts
Start of mission
Launch date19 September 2007,
03:26:13 UTC[2]
RocketLong March 4B
Launch siteTaiyuan Satellite Launch Center, LC-7
ContractorSAST
End of mission
Last contact10 May 2010
Orbital parameters
Reference systemGeocentric orbit[3]
RegimeSun-synchronous orbit
Perigee altitude773 km
Apogee altitude774 km
Inclination98.60°
Period100.30 minutes
Epoch19 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]
  1. ^ a b c d e Krebs, Gunter. "CBERS 1, 2, 2B / ZY 1A, 1B, 1B2". Gunter's Space Page. Retrieved 1 December 2013.
  2. ^ a b c McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 1 December 2013.
  3. ^ a b "CBERS 2B Satellite details 2007-042A NORAD 32062". N2YO. 25 January 2015. Retrieved 25 January 2015.
  4. ^ "CBERS-1 (China-Brazil Earth Resources Satellite) - 1st Generation Satellite Series". Earth Observation Portal. European Space Agency. Retrieved 1 December 2013.
  5. ^ "CBERS-1, 2 and 2B Description". INPE. Archived from the original on 20 January 2014. Retrieved 1 December 2013.
  6. ^ "Display: CBERS 2B 2007-042A". NASA. 14 May 2020. Retrieved 26 July 2020. Public Domain This article incorporates text from this source, which is in the public domain.
  7. ^ "CBERS-1, 2 and 2B Cameras". INPE. Archived from the original on 20 January 2014. Retrieved 1 December 2013.
  8. ^ "UCS Satellite Database". Union of Concerned Scientists. Archived from the original on 9 September 2010. Retrieved 1 December 2013.
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