Towards eenvironment Prague, March GMES Space Component. Josef Aschbacher Head, ESA GMES Space Office

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Towards eenvironment Prague, 25-27 March 2009 GMES Space Component Josef Aschbacher Head, ESA GMES Space Office

Prague from Space Segment 2 05 Nov 2003 CNES 2003 GISAT 2007 ESA GSELAND

GMES is an EU led initiative Services Component led by EC GMES components Produces information services in response to European policy priorities in environment and security Relies on data from in-situ and space component In-situ component led by EEA Observations mostly within national responsibility, with coordination at European level Space Component led by ESA Sentinels - EO missions developed specifically for GMES: Contributing Missions - EO missions built for purposes other than GMES but offering part of their capacity to GMES (EU/ESA MSs, EUMETSAT, commercial, international)

Role of ESA in GMES: Space Council Resolution Coordinator of the overall GMES Space Component Definition of overall GSC architecture; plan for future evolutions; organisation of data access; ensuring operation of Sentinels Development and procurement Agency for dedicated space infrastructure Development of first spacecraft and ground segment; procurement of recurrent elements Interim operator of Sentinel-1, -2 and Sentinel-3 (land) Note: EUMETSAT is proposed operator of Sentinel-3 (Marine), Sentinel -4 and -5

Content of ESA GSC programme (after CM-08) Sentinel-1 A: Phase B2/C/D/E1. Sentinel-1B: up to flight readiness Sentinel-2 A: Phase B2/C/D/E1. Sentinel-2B: up to flight readiness Sentinel-3 A: Phase B2/C/D/E1. Sentinel-3B: up to flight readiness Sentinel-4 (MTG-S): Phase Segment B/C/D/E1 2 (2 units) Sentinel-5 (post-eps): Phase B1 & pre-development Sentinel-5 pre-cursor: Phase A/B/C/D/E1 (UV-NIR instrument provided by NL) Ground Segment Development for Sentinel-1, -2, -3 A & B Data Access (data procurement & management) GSC Evolution Studies, incl. low-inclination altimetry

GMES dedicated missions: Sentinels Sentinel 1 SAR imaging All weather, day/night applications, interferometry Sentinel 2 Multispectral imaging Land applications: urban, forest, agriculture,.. Continuity of Landsat, SPOT Sentinel 3 Ocean and global land monitoring Wide-swath ocean color, vegetation, sea/land surface temperature, altimetry Sentinel 4 Geostationary atmospheric Atmospheric composition monitoring, transboundary pollution Sentinel 5 Low-orbit atmospheric Atmospheric composition monitoring (S5 Precursor launch in 2014) 2019+ 2012 2011 2012 2017+

Sentinel-1 Sentinel-1: C-band SAR mission Applications: monitoring sea ice zones and the arctic environment surveillance of marine environment monitoring land surface motion risks mapping in support of humanitarian aid in crisis situations 4 nominal operation modes: strip map (80 km swath, 5X5 m res.) interferometric wide swath (250 km swath, 20X5 m res.) extra wide swath (400 km swath, 25X100 m res.) Wave (5X20 m res.) 2300 Kg spacecraft mass Sun synchronous orbit at 693 Km mean altitude 12 days repeat cycle 7 years design life time, consumables for 12 years

Sentinel-2 Sentinel-2: Superspectral imaging mission Applications: Generic land cover maps risk mapping and fast images for disaster relief generation of leaf coverage, leaf chlorophyll content and leaf water content Pushbroom filter based multi spectral imager with 13 spectral bands (VNIR & SWIR) Spatial resolution: 10, 20 and 60 m Field of view: 290 km 1098 kg spacecraft mass 10 days repeat cycle Sun synchronous orbit at 786 km mean altitude 7 years design life time, consumables for 12 years

Sentinel-3 Sentinel-3: ocean & global land mission Applications: Sea/land colour data and surface temperature sea surface and land ice topography coastal zones, inland water and sea ice topography vegetation products 1198 kg spacecraft mass Sun synchronous orbit at 814.5 km mean altitude over geoid 27 days repeat cycle 7 years design life time, consumables for 12 years

Sentinel-3 Instruments: Ocean and Land Colour Instrument (OLCI) with 5 cameras, 8 bands (only VIS) for open ocean (low res), 15 bands (only VIS) for coastal zones (high res). Spatial sampling: 300m @ SSP Sea and Land Surface Temperature (SLST) with 9 spectral bands, 0.5 (VIS, SWIR) to 1 km res (MWIR, TIR). Swath: 180rpm dual view scan, nadir & backwards RA package SRAL Ku-C altimeter (LRM and SAR measurement modes), MWR, POD (with Laser Retro Reflector, GPS and DORIS)

Sentinel-4 Sentinel-4: GEO atmospheric mission Applications: monitoring changes in the atmospheric composition (e.g. ozone, NO 2, SO 2, BrO, formaldehyde and aerosol) at high temporal resolution tropospheric variability Narrow field spectrometer covering UV (290-400 nm), visible (400-500 nm) and near-ir (750-775 nm) bands Spatial sampling 5-50 km and spectral resolution between 0.06 nm and 1 nm (depending on band) Geostationary orbit, at 0 o longitude Embarked on MTG-S and operated by EUMETSAT

Sentinel-5 Sentinel-5: LEO atmospheric mission Applications: monitoring changes in the atmospheric composition (e.g. ozone, NO 2, SO 2, BrO, formaldehyde and aerosol) at high temporal (daily) resolution tropospheric variability Wide-swath pushbroom spectrometer suite, covering UV (270-400 nm), visible (400-500 & 710-750 nm), NIR (750-775 nm) and SWIR (2305-2385 nm) bands. Spatial sampling 5-50 km and spectral resolution between 0.05 nm and 1 nm (depending on band) Low Earth orbit (reference altitude of about 817 km) Sentinel-5 precursor to fill data gaps (2013-2019). Sentinel-5 embarked on post-eps and operated by EUMETSAT

Potential Contributing Missions to GSC National, Eumetsat and Third Party Missions for GMES (list not exhaustive that will evolve based on services requirements) Jason SPOT Pléiades CosmoSkymed Radarsat Terrasar-X Rapideye DMCs METOP MSG + Seosat, Tandem-X, Enmap, Venμs, Altika, etc

Example: Optical HR and VHR missions

GMES Ground Segment and Data Access Sentinel-3

GMES Space Component Phasing ESA Prep. Programme ESA Segment 1 ESA Segment 2 EU Init-Ops EU Operational programme 2004 2006 2009 2011 2013 2014 2017 2023 16

GSC build-up GSC funding approach GSC build-up is co-funded by ESA and EC Total funding available: 2.25 billion 1621 M (2008 e.c.) by ESA MSs 626 M (2008 e.c.) by EC Completion of build-up (2011, TBC) GSC operations programme (2014 onwards) Expected to be fully funded by the EC ESA funding only for R&D elements, TBC Initial operations (2011-13)

GSC Long-Term Scenario

Further information For further information please visit ESA GMES web site (GSC) http://www.esa.int/gmes Segment 2 EC GMES web site (GMES) http://ec.europa.eu/gmes