The Status of NIES GOSAT-2 Project and NIES Satellite Observation Center

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12th International Workshop on Greenhouse Gas Measurements from Space June 7 9, 2016, Kyoto, Japan The Status of NIES GOSAT-2 Project and NIES Satellite Observation Center GOSAT GOSAT-2 T. Matsunaga, S. Maksyutov, I. Morino, Y. Yoshida, M. Saito, H. Noda, Y. Terao, T. Nishizawa, H. Mukai, N. Saigusa, and T. Machida 1

GOSAT-2 Instrument and Product Related Posters JAXA GOSAT-2 Specifications Poster 6 Poster 8 Poster 9 Poster 30 Poster 42 Poster 54 Makiko Hashimoto, et al. (JAXA, Japan) Aerosol retrieval algorithm and aerosol properties retrieved from GOSAT/TANSO-CAI Yu Someya, et al. (AORI/U. Tokyo, Japan) The CO2 slicing algorithm for the TIR cloud/aerosol products of TANSO-FTS2/GOSAT-2 Yu Oishi, et al. (Tokai U., Japan) Primary verification of new cloud discrimination algorithm used with GOSAT TANSO-CAI in Borneo Island Isamu Morino, et al. (NIES, japan) Towards TCCON in the Philippines: The importance of monitoring atmospheric carbon in tropical Southeast Asia Yosuke Niwa, et al. (MRI, Japan) A 4D-Var inversion system based on the icosahedral grid model (NICAM-TM 4D-Var) Yukio Yoshida, et al. (NIES, Japan) Plan of the GOSAT-2 FTS SWIR products and its preliminary sensitivity study CAI-2 L2 Aerosol FTS-2 TIR L2 CAI-2 L2 Cloud Validation L4A FTS-2 SWIR L2 Poster 55 Ronald Glumb, et al. (Harris Space & Intell. Sys., USA) An Update on the TANSO-FTS-2 Instrument for GOSAT-2 FTS-2 Instrument 2

Major Milestones of NIES GOSAT-2 Project in FY2015 and FY2016 FY2015 Preliminary and critical designs of G2DPS (GOSAT-2 Data Processing System) Testing of a new FTS (125HR) in NIES Tsukuba Campus Completion of Two GOSAT-2 buildings for offices and computers Installation of GOSAT RCF2 (GOSAT-2 Research Computation Facility) FY2016 (April) Establishment of Satellite Observation Center at NIES (June July) CDR of G2DPS (December) Shipment of FTS to the new TCCON site in Phillipines. Procurements of computers for G2DPS 3

Role Sharing in the GOSAT and GOSAT-2 Project In GOSAT-2 Project, Satellite development, launch, and operation are added to MOE s role. 4

NIES Organizational Structure (April 2016) National Institute for Environmental Studies Research Centers Center for Global Environmental Research Deputy Manages / Obs. Mng. Group 2 Global Carbon Cycle Res. Section Satellite Remote Sensing Section Director Research Project Collaboration Division Satellite Observation Center (Director : Matsunaga) GOSAT Project GOSAT-2 Project MOE JAXA JMA Biogeochem. Cycle Modeling/Analysis Sec. Atmospheric and Oceanic Monitoring Office Integration/Analysis of Global Environmental Databases Office Center for Environmental Measurement and Analysis Advanced Remote Sensing Section GOSAT-3 Preparation Team Validation Team Ground Data System Management Team Ground Data System Operation Team Administration and Public Relations Team Committee for Future Satellite Missions Science Teams RA PIs Overseas / International Organizations 5

Organizational Structure of NIES GOSAT-2 Project (as of April 2016) NIES GOSAT Project Leaders : Matsunaga / Yokota GOSAT-2 Science Team (Leader) R. Imasu Terry Nakajima, Y. Hikosaka, Y. Honda, Takashi Nakajima, Y. Niwa, Y. Ota, N. Saito, H. Shimoda Calibration WG Shimoda, Honda, Ono, Yamada, Tsuchida, Kouyama, Moriyama GOSAT-2 RA PIs NIES GOSAT-2 Project Leader : T. Matsunaga Ground Data System Y. Yoshida and M. Saito FTS-2 SWIR L2 Algorithm Y. Yoshida L4 Algorithm M. Saito and H. Noda Terrestrial Biosphere Model H. Noda Validation I. Morino 14 C Measurement Y. Terao Aerosol lidar T. Nishizawa MOE and JAXA Other NIES Scientists H. Mukai, N. Saigusa, T. Machida Other Organizations JMA Univ. Tokyo Other Missions OCO-2/3 TanSat Sentinel 5p MERLIN Microcarb 6

Timeline of Planned Total Column CO2 Observing Satellites as of June, 2016 Mission Period (Calender year) 2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024 2025 ESA ENVISAT SCIAMACHY Japan GOSAT 2002/3-2012/4 2009/1 + 5 years Green Yellow Pink Designed life time Extended operation End of mission NASA OCO-2 China TanSat Japan GOSAT-2 NASA OCO-3 CNES MicroCarb Japan GOSAT-3 2014/7 + 2 years End of 2016 + 3 years 2018/1 + 5 years late 2018 + 3 years 2020 + 3 years 2022- ESA ENVISAT (2002-2012) Japan GOSAT (2009-) We are here. NASA OCO-2 (2014-) China TanSat (2016-) Japan GOSAT-2 (2018-) CNES MicroCarb (2020-) 7

GOSAT-2 Project Long-term Schedule FY2013 FY2014 FY2015 FY2016 FY2017 FY2018 FY2019 FY2020 FY2021 FY2022 OCO-2 launch Tansat launch GOSAT-2 launch [Public Release] L1B CAI-2 L2 Cloud SWIR L2 OCO-3 launch [Public Release] TIR L2 CAI-2 L2 Aerosol [Public Release] L4 CO2 Microcarb launch [Public Release] SWIR L2(new version) L4 CH4 End of GOSAT-2 Nominal operation GOSAT-3 launch Spacecraft and Instruments RFP System PDR System CDR System PQR GOSAT-2 Data Processing System (G2DPS) and computing facilities Requireme nt survey Preliminary design Critical design Manufacturi ng Testing Nominal operation Nominal operation Nominal operation Nominal operation Nominal operation Design of GOSAT-2 buildings Completion of GOSAT- 2 buildings Installation of GOSAT RCF2 G2DPS computer installation G2DPS computer renewal Validation and other experiments Procureme nt of a new FTS (125HR) Modification of airborne FTS Relocation of FTS to Phillipines Validation of 2018 data Validation of 2019 data Validation of 2020 data Validation of 2021 data 8

Quick Overview of GOSAT and GOSAT-2 GOSAT Specifications GOSAT-2 Requirements Launch year and life time Jan. 2009, 5 years FY2017, 5 years Satellite (Dimension, mass, power) Orbit (Type, altitude, repeat cycle, equator crossing time) 3.7 x 1.8 x 2.0 m, 1750kg, 3.8KW (EOL) Sun synchronous, 666 km, 3 days, 13:00 5.3 x 2.0 x 2.8 m, <2000kg, 5.0KW Sun synchronous, 613 km, 6 days, 13:00±15 min Target gases CO 2, CH 4, O 2, O 3, H 2 O CO 2, CH 4, O 2, O 3, H 2 O, CO Fourier Transform Spectrometer (FTS and FTS-2) Cloud and Aerosol Imager (CAI and CAI-2) Band 1 : 0.76 0.78 µm Band 2 : 1.56 1.72 µm Band 3 : 1.92 2.08 µm Band 4 : 5.6 14.3 µm IFOV = 10.5 kmφ Pointing = ±20 (AT), ±35 (CT) Polarimetry = Band 1, 2, 3 Nadir B1 = 380 nm B2 = 674 nm B3 = 870 nm B4 = 1600 nm B1-B3 = 500 m / 1000 km, B4 = 1500 m / 750 km Band 1 : 0.75 0.77 µm Band 2 : 1.56 1.69 µm Band 3 : 1.92 2.33 µm Band 4 : 5.5 8.4 µm Band 5 : 8.4 14.3 µm IFOV = 9.7 kmφ Pointing = ±40 (AT), ±35 (CT) Polarimetry = Band 1, 2, 3 B1-5: forward (+20 ), B6-10:backward(- 20 ) B1 = 343 nm B6 = 380 nm B2 = 443 nm B7 = 550 nm B3 = 674 nm B8 = 674 nm B4 = 869 nm B9 = 869 nm B5 = 1630 nm B10= 1630 nm B1-B4, B6-B9= 460 m / 920 km B5, B10 = 920 m / 920 km Other new features of GOSAT-2 FTS-2 Intelligent pointing using FTS-2 FOV camera, fully programmable (target mode) observation, and improved SNR. 9

GOSAT-2 s New Capabilities / Major Improvements FTS-2 SWIR L2 carbon monoxide FTS-2 SWIR L2 chlorophyll fluorescence (Noda et al. [ACG10-P07]) Improved FTS-2 signal to noise ratio reduces the retrieval random error (precision) about 15% for XCO 2 and 35% for XCH 4 than those of GOSAT. (Yoshida et al., JpGU Meeting, 2016) Extended FTS-2 AT pointing angle limit FTS-2 Intelligent pointing FTS-2 Fully programmable operation CAI-2 Multiple UV bands CAI-2 forward / backward looking system => More ocean sunglint data => More cloud-free FTS data => More target-mode data => Better land aerosol estimation => More non-glint ocean data 10

GOSAT-2 FTS-2 Optical Layout FTS-2 is designed based on not GOSAT FTS but CrIS(Crosstrack Infrared Sounder ) onboard NASA s Suomi NPP. Glumb et al. IWGGMS-11, 2015 11

Simulated FTS Sunglint Observation in May-July GOSAT GOSAT-2 The apparent increase of the number of sunglint paths is simply due to the difference of orbit repeat cycles between GOSAT (3 days) and GOSAT-2 (6 days). GOSAT-2 can cover the wider latitude zone than GOSAT. The FTS sunglint data will double in number. Kamei et al. (2015) 12

GOSAT-2 Data Processing Flow CAI-2 L1A CAI-2 L1B CAI-2 Surface Albedo CAI-2 L2 Cloud CAI-2 L2 Aerosol FTS-2 L1A FTS-2 L1B FTS-2 TIR L2 Cloud and Aerosol FTS-2 SWIR L2 Chlorophyll Fluorescence FTS-2 SWIR L2 XCO 2, XCH 4, XH 2 O, XCO FTS-2 L4A CO 2 and CH 4 Flux FTS-2 TIR L2 Air temperature and Gas Concentration Profiles FTS-2 L4B 3D CO 2 and CH 4 Concentration 13

GOSAT-2 Product List (At-launch version) Product Name Algorithm Processing TANSO-CAI-2 L1A Product JAXA JAXA TANSO-CAI-2 L1B Product JAXA NIES TANSO-CAI-2 L2 Cloud Discrimination Product Tokai Univ. NIES TANSO-CAI-2 L2 Aerosol Properties Product JAXA NIES TANSO-FTS-2 L1A Product JAXA JAXA TANSO-FTS-2 L1B Product JAXA JAXA TANSO-FTS-2 SWIR L2 Chlorophyll Fluorescence/Proxy Method Product NIES NIES TANSO-FTS-2 SWIR L2 Column Averaged Gas Concentration Product NIES NIES TANSO-FTS-2 TIR L2 Cloud and Aerosol Properties Product Univ. Tokyo NIES TANSO-FTS-2 TIR L2 Air Temperature and Gas Concentration Product Chiba Univ. NIES TANSO-FTS-2 L4A Product (CO 2 and CH 4 ) NIES NIES TANSO-FTS-2 L4B Product (CO 2 and CH 4 ) NIES NIES 14

Thank you for your attention matsunag@nies.go.jp 15