Global Change Observation Mission

JAXA project of long-term observation of Earth

GCOM (Global Change Observation Mission), is a JAXA project of long-term observation of Earth environmental changes. As a part of Japan's contributions to GEOSS (Global Earth Observation System of Systems), GCOM will be continued for 10 to 15 years with observation and utilization of global geophysical data such as precipitation, snow, water vapor, aerosol, for climate change prediction, water management, and food security. On May 18, 2012, the first satellite "GCOM-W" (nickname "Shizuku") was launched. On December 23, 2017, the second satellite "GCOM-C1" (nickname "Shikisai") was launched.

GCOM-W

GCOM-W (Global Change Observation Mission – Water; nickname "Shizuku") is the first in the GCOM series. Its mission is to observe the water cycle. The satellite carries the AMSR2 (Advanced Microwave Scanning Radiometer 2) instrument, the successor to the AMSR-E carried by Aqua. This microwave radiometer will observe precipitation, water vapor, wind velocity above the ocean, sea water temperature, water levels on land areas, and snow depths. GCOM-W was approved in 2006, and development of the satellite started in 2007 with a mission budget of 20 billion Yen (US$200 Million). Mass of the satellite is 1990 kg. Planned lifespan is 5 years. Polar orbit (altitude 700 km) with equator crossing local time on the ascending orbit is 13:30PM +/- 00:15.

GCOM-W was launched on May 17, 2012, via a H-IIA rocket, and it flies in a Sun-synchronous orbit as part of the "A-train" satellite constellation. It successfully began collecting data on July 4, 2012. Its planned lifespan of 5 years means that the satellite is set to operate until 2017, although JAXA hopes that it will last longer.

GCOM-C1

GCOM-C1 (Global Change Observation Mission – Climate; nickname "Shikisai"), the first satellite in the GCOM-C series, will monitor global climate change by observing the surface and atmosphere of Earth over the course of 5 years. Through use of its SGLI (Second generation GLobal Imager) optical instrument, it will collect data related to the carbon cycle and radiation budget, such as measurements of clouds, aerosols, ocean color, vegetation, and snow and ice. From its Sun-synchronous orbit (altitude 798 km), SGLI will collect a complete picture of Earth every 2–3 days with a resolution of 250-1000m, across the UV, visible, and infrared spectrums. Mass of the satellite is 2020 kg. Equator crossing local time on the descending orbit is 10:30AM +/- 00:15.

GCOM-C was launched on December 23, 2017, via a H-IIA rocket.

Sensors

AMSR2

AMSR2 (Advanced Microwave Scanning Radiometer 2) is an improved version of AMSR (aperture 2.0 m) on ADEOS II and AMSR-E (aperture 1.6 m) on NASA's Aqua satellite. By rotating a disc antenna (diameter 2.0 m) in 1.5 s period, it scans the Earth surface along an arc of 1450 km length. Reliability is better than AMSR and AMSR-E. Planned lifetime has been extended from 3 years to 5 years.

A new microwave band, namely 7.3 GHz, has been added. The 7.3 GHz band is for duplication and calibration of 6.925 GHz band. AMSR2 continues the legacy of AMSR-E, which also observed as part of the A-Train constellation.

AMSR2 observation frequency
parameter / frequency (GHz)	6.925/ 7.3	10.65	18.7	23.8	36.5	89.0	comments
column vapor			○	◎	○
column precipitable water			○	○	◎
precipitation		○	◎	○	○	◎
sea surface temperature	◎	○		○	○
sea surface wind speed	○	○		○	◎
sea ice density	○		◎	○	◎	◎	89 GHz is only for cloudless area
snowpack		○	◎	○	◎	○
soil moisture	◎	◎	○	○	○	○

Note: ◎ means the most important band for that purpose.

SGLI

SGLI (Second-generation Global Imager) is a multi-band optical radiometer and the successor of GLI sensor on ADEOS-II. It consists of two sensors: SGLI-VNR (an electronic scan) and SGLI-IRS (a mechanical scan). SGLI-VNR succeeds the technology of MESSR on MOS-1, OPS/VNIR on JERS-1, AVNIR on ADEOS, and AVNIR-2 on ALOS.

The number of channels of SGLI is 19, which is much less than GLI (36 channels). This is because SGLI carefully selected the essential bands for observations.

The swath size is 1150 km for SGLI-VNR and 1400 km for SGLI-IRS. Although a little reduction from GLI (all channels were mechanical scan with 1400 km swath), it has more bands with high-resolution (250 m). Polarimetry function has been added to SGLI-VNR, which helps detection of size of aerosol particles, enabling detection of source of the aerosols.

The lesson of GLI sensor's too big and too complicated structure, SGLI is divided to two simple systems, and the number of channels have been minimized to really essential bands, aiming at better reliability and survivability.

SGLI observation channels
instruments		channel	central wavelength	bandwidth	resolution	target
SGLI- VNR	non- polarization	VN1	380 nm	10.6 nm	250 m	terrestrial aerosol, atmospheric correction, ocean color, snow and ice
		VN2	412 nm	10.3 nm		vegetation, terrestrial aerosol, atmospheric correction, oceanic aerosol, photosynthetic active radiation, snow and ice
		VN3	443 nm	10.1 nm		vegetation, oceanic aerosol, atmospheric correction, photosynthetic active radiation, ocean color, snow and ice
		VN4	490 nm	10.3 nm		ocean color (chlorophyll, suspended sediments)
		VN5	530 nm	19.1 nm		photosynthetic active radiation, ocean color (chlorophyll)
		VN6	565 nm	19.8 nm		ocean color (chlorophyll, suspended sediments, colored dissolved organic matters)
		VN7	673.5 nm	22 nm		vegetation, terrestrial aerosol, atmospheric correction, ocean color
		VN8	673.5 nm	21.9 nm
		VN9	763 nm	11.4 nm	1000 m	liquid cloud geometric thickness
		VN10	868.5 nm	20.9 nm	250 m	vegetation, terrestrial aerosol, atmospheric correction, ocean color, snow and ice
		VN11	868.5 nm	20.8 nm	250 m
	polarization	P1	673.5 nm	20.6 nm	1000 m	vegetation, terrestrial aerosol, atmospheric correction, ocean color
	polarization	P2	868.5 nm	20.3 nm	1000 m	vegetation, terrestrial aerosol, atmospheric correction, ocean color, snow and ice
SGLI- IRS	short wave infrared (SWIR)	SW1	1050 nm	21.1 nm	1000 m	liquid cloud optical thickness, particle size
		SW2	1380 nm	20.1 nm	1000 m	detection of clouds over snow and ice
		SW3	1630 nm	195 nm	250 m	detection of clouds over snow and ice
		SW4	2210 nm	50.4 nm	1000 m	liquid cloud optical thickness, particle size
	thermal infrared (TIR)	T1	10.8 μm	0.756 μm	250 m	surface temperature of land, ocean, snow & ice. Fire detection, vegetation water stress
	thermal infrared (TIR)	T2	12.0 μm	0.759 μm	250 m

References

GCOM-W1 Archived 2020-08-10 at the Wayback Machine at NSSDC
GCOM-W Archived 2014-04-26 at the Wayback Machine at JAXA
"SHIZUKU Observation Data Acquired by AMSR2". JAXA. Archived from the original on 26 April 2014. Retrieved 2 July 2014.
"JAXA: Global Change Observation Mission – Climate (GCOM-C)". Archived from the original on 9 March 2018. Retrieved 2 July 2014.

Japanese space program

Italics indicates projects in development.
Symbol indicates failed projects.
~~Strikethrough lines~~ indicate cancelled projects.

Space agencies

National space agencies	JAXA former ISAS NAL NASDA NICT JSS
Joint development partners	United States NASA ESA Italy ASI Canada CSA Russia Roscosmos Brazil AEB INPE India ISRO

Astronomical observation

Past	Akari ASCA ASTRO-E ~~Astro-G~~ CORSA Ginga Hakucho HALCA Hinotori Hitomi ~~SPICA~~ Suzaku Tenma Yohkoh
Active	Hinode Hisaki XRISM
Future	ATHENA SOLAR-C GREX-PLUS [ja] HiZ-GUNDAM [ja] LAPYUTA LiteBIRD Nancy Grace Roman Space Telescope JASMINE

Communications satellites, broadcasting satellites and satellite navigation systems

Past	BS 2X 3H 3N Kakehashi Kirari Kizuna Kodama MBSat N-STAR a b Sakura (1 2a 2b 3a 3b) Yuri 1 2a 2b 3a 3b
Active	Kirameki 1 2 Michibiki 1 2 3 4 1R MTSAT N-STAR c d JDRS
Future	DSN 3 QZS 5 6 7

Earth observation

Past	Akebono Daichi 1 3 Denpa Fuyo-1 Jikiken Kyokko Midori I II Momo 1 1b Ohozora Taiyo TRMM Ume 1 b Geotail
Active	Aqua Arase ASNARO 1 2 Daichi 2 4 EarthCARE GPM Himawari Ibuki original 2 Shikisai Shizuku
Future	GOSAT-GW PMM

Engineering tests

Past	Ayame 1 2 DASH EXPRESS IKAROS Jindai Kiku 1 2 3 4 5 6 7 8 LDREX 1 2 LRE Micro LabSat-1 Myojo Ohsumi Orizuru RAISE 2 3 ~~PETSAT~~ RAPIS-1 Ryusei SERVIS-1 SERVIS-2 SDS-1 SFU Shinsei ~~SmartSat-1~~ Tansei 1 2 3 4 Tasuki Tsubame Tsubasa USERS
Active	Ajisai Reimei SDS-4
Future	BEAK ETS-IX G-SATELLITE SERVIS-3

Human spaceflight

Past	~~Fuji crewed spacecraft~~ ~~HOPE-X~~ H-II Transfer Vehicle
Active	International Space Station (ISS) & Japanese Experiment Module (Kibō)
Future	HTV-X Japanese Space Station Module (Mitsui) Lunar Gateway

Space probes

The Moon

Past	Hakuto-R Mission 1 Hiten ~~Lunar-A~~ Kaguya (SELENE) OMOTENASHI ~~SELENE-2~~
Active	EQUULEUS Smart Lander for Investigating Moon (SLIM)
Future	Hakuto-R Mission 2 HERACLES Lunar Cruiser Lunar Polar Exploration Mission (LUPEX) Yaoki

Others

Past	Hayabusa ~~Hayabusa Mk2~~ Nozomi PROCYON Sakigake Shin'en Suisei
Active	Akatsuki BepiColombo (MMO/Mio) Hayabusa2 Jupiter Icy Moons Explorer Hera
Future	Comet Interceptor DESTINY+ Dragonfly MELOS Martian Moons eXploration Next Generation Small-Body Sample Return TEREX

Reconnaissance satellites

Past	IGS-Optical 1 2 Experimentally 3 IGS-Radar 1 2
Active	IGS-Optical 3 4 5 6 Experimentally 5 IGS-Radar 3 4 Spare 5 6
Future	IGS-Optical 7 8 IGS-Radar 7 8

Private small satellites

Past	CosMoz CUTE 1.7+APD Fuji 1 2 Hayato HIBARI HIT-SAT Kagayaki Kanta-kun (WEOS) Kūkai Maido-1 Negai☆″ Niwaka RAIKO Waseda-SAT2 WE WISH
Active	CUTE 1 1.7+APDII Fuji-3 Hitomi Hodoyoshi 1 2 3 4 Horyu 2 Kiseki PROITERES Raijin Raijin-2 SEEDS SOCRATES XI IV V
Future	DRUMS KITSUNE OPUSAT-II QSAT-EOS RSP-01 SOMESAT SpaceTuna1 SPROUT TSUBAME Wisseed Sat WNI satellite

Categories:

Misplaced Pages