ADEOS II

ADEOS II
Illustration of ADEOS II
NamesAdvanced Earth Observing Satellite II
Midori II
ADEOS 2
Mission typeEarth observation
Environmental monitoring
OperatorNASDA
COSPAR ID2002-056A Edit this at Wikidata
SATCAT no.27597
Mission duration5 years (planned)
10 months and 9 days (achieved)
Spacecraft properties
BusADEOS
ManufacturerMitsubishi Electric Corporation
Launch mass3,680 kg (8,110 lb)
Payload mass1,300 kg (2,900 lb)
Dimensions6 × 4 × 4 m (20 × 13 × 13 ft)
Power5.3 kW
Start of mission
Launch date14 December 2002, 01:31 UTC
RocketH-IIA 202
Launch siteTanegashima Space Center, Yoshinobu 1
ContractorMitsubishi Heavy Industries
End of mission
Last contact23 October 2003, 23:55 UTC
Orbital parameters
Reference systemGeocentric orbit[1]
RegimeSun-synchronous orbit
Perigee altitude806 km (501 mi)
Apogee altitude807 km (501 mi)
Inclination98.70°
Period101.00 minutes
Instruments

ADEOS II (Advanced Earth Observing Satellite 2) was an Earth observation satellite (EOS) launched by NASDA,[2] with contributions from NASA and CNES, in December 2002.[3] and it was the successor to the 1996 mission ADEOS I. The mission ended in October 2003 after the satellite's solar panels failed.[4]

  1. ^ "ADEOS 2 2002-056A 27597". NASA. 28 October 2021. Retrieved 29 October 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  2. ^ "ADEOS-II (Advanced Earth Observing Satellite-II) / Midori-II". ESA eoPortal Directory. 2021. Retrieved 29 October 2021.
  3. ^ "ADEOS-2". NASA. Archived from the original on 27 September 2010. Retrieved 30 October 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  4. ^ "Midori I (ADEOS I)". Satellite News Digest. 2006. Archived from the original on 5 October 2011. Retrieved 18 September 2010.