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Formosat-1

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Formosat-1
ROCSAT-1
福爾摩沙衛星一號
Mission type Science
Operator National Space Organization
COSPAR ID 1999-002A Edit this at Wikidata
SATCAT no. 25616 Edit this on Wikidata
Website Formosat-1
Mission duration 5.5 years
Spacecraft properties
BOL mass 401 kg
Start of mission
Launch date Jan 27, 1999
Rocket ATHENA-1/LMLV1
End of mission
Decay date 22 May 2023 [1]
Orbital parameters
Reference system Geocentric
Inclination 35°
Period 96.7 mins
 

Formosat-1 (福爾摩沙衛星一號, formerly known as ROCSAT-1 ) was an Earth observation satellite operated by the National Space Program Office (NSPO, now the National Space Organization ) of the Republic of China ( Taiwan ) to conduct observations of the ionosphere and oceans . The spacecraft and its instrumentation were developed jointly by NSPO and TRW using TRW's Lightsat bus, and was launched from Cape Canaveral Air Force Station , US , by Lockheed Martin on January 27, 1999. [2] FormoSat-1 provided 5½ years of operational service. The spacecraft ended its mission on June 17, 2004 and was decommissioned on July 16, 2004. [3] [4]

Technical details [ edit ]

Spacecraft [ edit ]

  • Weight: 401 kg
  • Shape: Hexagonal
  • Dimensions
    • Height: 2.1 m
    • Diameter: 1.1 m
  • Solar arrays: Two, 1.16 x 2.46 m
  • Electrical power: 450 watts

Instrumentation [ edit ]

  • Experimental Communication Payload (ECP)
  • Ionosphere Plasma Electrodynamics Instrument (IPEI)
  • Ocean Color Imager (OCI)

Orbit [ edit ]

  • Altitude: 600 km
  • Type: Circular
  • Inclination: 35 degrees

See also [ edit ]

References [ edit ]

  1. ^ "ROCSAT 1" . N2YO.com . 22 May 2023 . Retrieved 4 July 2023 .
  2. ^ "FORMOSAT-1: Low-earth-orbit scientific experimental satellite" . Taiwan National Space Organization . Retrieved November 24, 2022 .
  3. ^ "FormoSat-1" . eoPortal.org . Retrieved November 24, 2022 .
  4. ^ Wu, L.; Chen, S.-S.; Yaung, J. Ju-Chen (November 26, 2004). "Space Program in Taiwan". Proceedings of ASC (Asian Space Conference), Chiang Mai, Thailand .

External links [ edit ]