Greenhouse Gases Observing Satellite

Greenhouse Gases Observing Satellite

Ibuki
Mission type Environmental
Operator JAXA
COSPAR ID 2009-002A
SATCAT № 33492
Website .html_e/index/gosat/sat/projects.jp.jaxawww
.html_e/index.jp.go.nies.gosatwww
//en.jp.go.envwww
Mission duration 5 years
Spacecraft properties
Manufacturer Mitsubishi Electric
Launch mass 1,750 kilograms (3,860 lb)[1]
Power 3.8 kilowatts[1]
Start of mission
Launch date January 23, 2009, 03:54 (2009-01-23T03:54Z) UTC
Rocket H-IIA 202
Launch site Tanegashima Yoshinobu 1
Contractor Mitsubishi
Orbital parameters
Reference system Geocentric
Regime Low Earth[2]
Perigee 674 kilometres (419 mi)[3]
Apogee 676 kilometres (420 mi)[3]
Inclination 98.06 degrees[3]
Period 98.12 minutes[3]
Mean motion 14.68[3]
Epoch 25 January 2015, 03:12:11 UTC[3]
Main Instrument
Wavelengths 12900 - 13200 cm−1 / 5800 - 6400 cm−1 / 4800 - 5200 cm−1 / 700 - 1800 cm−1 (FTS)[1]
Resolution 0.2 cm−1 (FTS)
Instruments
TANSO-FTS - Infrared Fourier Transform Spectrometer
TANSO-CAI - Thermal and Near-Infrared Sensor

The Greenhouse Gases Observing Satellite or GOSAT, also known as Ibuki (いぶき Ibuki, meaning "breath"[4] or "Vitality"[5] in

  • Greenhouse gases Observing SATellite "IBUKI" (GOSAT) – JAXA
  • Earth "Breathing" as Observed from Outer Space -IBUKI promotion movie- – JAXA Official YouTube Channel
  • GOSAT Project - Global Greenhouse Gases Observation Satellite Website – National Institute for Environmental Studies
  • NIES GOSAT PROJECT NEWSLETTER

External links

  1. ^ a b c
  2. ^
  3. ^ a b c d e f
  4. ^
  5. ^ a b c d
  6. ^ a b c
  7. ^ http://www.nies.go.jp/
  8. ^ a b
  9. ^

References

See also

According to JAXA, the Ibuki satellite is equipped with a greenhouse gas observation sensor (TANSO-FTS) and a cloud/aerosol sensor (TANSO-CAI) that supplements TANSO-FTS. The greenhouse gas observation sensor of Ibuki observes a wide range of wavelengths (near-infrared region–thermal infrared region) within the infrared band to enhance observation accuracy.[8] The satellite uses a spectrometer to measure different elements and compounds based on their response to certain types of light. This technology allows the satellite to measure "the concentration of greenhouse gases in the atmosphere at a super-high resolution."[9]

Instruments

GOSAT was launched along with seven other piggyback probes using the H-IIA, Japan's primary large-scale expendable launch system, at 3:54 am on January 23, 2009 UTC on Tanegashima, a small island in southern Japan, after a two-day delay due to unfavourable weather.[5][6] At approximately 16 minutes after liftoff, the separation of Ibuki from the launch rocket was confirmed.[8]

Launch

Contents

  • Launch 1
  • Instruments 2
  • See also 3
  • References 4
  • External links 5

[6]