Names | Ibuki-2 |
---|---|
Mission type | Environmental |
Operator | JAXA |
COSPAR ID | 2018-084B |
SATCAT no. | 43672 |
Website |
www |
Mission duration | 5 years (planned) Elapsed: 5 years, 5 months, 23 days |
Spacecraft properties | |
Manufacturer | Mitsubishi Electric [1] |
Launch mass | 1,800 kilograms (4,000 lb) [1] |
Power | 5000 W [1] |
Start of mission | |
Launch date | 29 October 2018 04:08 | UTC
Rocket | H-IIA F40 |
Launch site | Tanegashima, Yoshinobu 1 |
Contractor | Mitsubishi Heavy Industries |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Eccentricity | 0.00106 [2] |
Altitude | 612.98 km [2] |
Inclination | 97.84° [2] |
Period | 98.1 minutes [2] |
Main Instrument | |
Wavelengths | 0.75 – 0.77 µm / 1.56 – 1.69 µm / 1.92 – 2.38 µm / 5.6 – 8.4 µm / 8.4 – 14.3 µm (FTS-2) [3] |
Resolution | 0.2 cm−1 (FTS-2) |
Instruments | |
TANSO-FTS-2 - Infrared Fourier Transform Spectrometer TANSO-CAI-2 - Thermal and Near-Infrared Sensor | |
The Greenhouse Gases Observing Satellite-2 (GOSAT-2), also known as Ibuki-2 ( Japanese: いぶき2号, Hepburn: Ibuki nigō), is an Earth observation satellite dedicated to greenhouse gas monitoring. It is a successor of Greenhouse Gases Observing Satellite (GOSAT). The GOSAT-2 was developed as a joint project of the Japan Aerospace Exploration Agency ( JAXA), Ministry of the Environment, and the National Institute for Environmental Studies (NIES). It was launched on 29 October 2018 from the Tanegashima Space Center aboard the H-IIA rocket.[ citation needed]
Major changes in comparison to the previous GOSAT are: [4]
As of November 2023 [update], GOSAT-GW, the successor of GOSAT-2 and GCOM-W "Shizuku", is under development for launch in JFY2024 on the last flight of the H-IIA launch vehicle. [5]