NOAA-B

NOAA-B
NamesNOAA-B
Mission typeWeather
OperatorNOAA
COSPAR ID1980-043A Edit this at Wikidata
SATCAT no.11819
Mission duration2 years (planned)
339 days (achieved)
Spacecraft properties
Spacecraft typeTIROS
BusTIROS-N[1]
ManufacturerRCA Astro Electronics[2]
Launch mass1,418 kg (3,126 lb) [3]
Dry mass735 kg (1,620 lb)
Start of mission
Launch date29 May 1980, 10:53:00 UTC[4]
RocketAtlas F-Star-37S-ISS
(Atlas S/N 19F) [2]
Launch siteVandenberg, SLC-3W
ContractorConvair
End of mission
DisposalOrbital decay
Decay date3 May 1981 [4]
Orbital parameters
Reference systemGeocentric orbit[4]
RegimeSun-synchronous orbit
Perigee altitude273 km (170 mi)
Apogee altitude1,453 km (903 mi)
Inclination92.3°
Period102.2 minutes
← NOAA-6
NOAA-7 →

NOAA B was an American operational weather satellite for use in the National Operational Environmental Satellite System (NOESS) and for the support of the Global Atmospheric Research Program (GARP) during 1978-1984. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.[5]

  1. ^ "Tiros N". Encyclopedia Astronautica. Archived from the original on 28 December 2016. Retrieved 15 January 2017.
  2. ^ a b Krebs, Gunter. "TIROS-N, NOAA 6, B, 7". Gunter's Space Page. Retrieved 15 January 2017.
  3. ^ "NOAA-6". World Meteorological Organisation (WMO). Retrieved 28 December 2020.
  4. ^ a b c "Trajectory: NOAA-B 1980-043A". NASA. 14 May 2020. Retrieved 28 December 2020. Public Domain This article incorporates text from this source, which is in the public domain.
  5. ^ "Display: NOAA-B 1980-043A". NASA GSFC. 14 May 2020. Retrieved 31 December 2020. Public Domain This article incorporates text from this source, which is in the public domain.