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lite Direct Readout Conference for the Americas, , December 9-13, 2002 Page 1 THE EUMETSAT POLAR SYSTEM (EPS) Presented by: Ken ASHWORTH EUMETSAT Representative to NOAA EUMETSAT ([email protected])

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Page 1: Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002 Page 1 THE EUMETSAT POLAR SYSTEM (EPS) Presented by: Ken ASHWORTH EUMETSAT

Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 1

THE EUMETSAT POLAR SYSTEM (EPS)

Presented by: Ken ASHWORTHEUMETSAT Representative to NOAA

EUMETSAT ([email protected])

Page 2: Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002 Page 1 THE EUMETSAT POLAR SYSTEM (EPS) Presented by: Ken ASHWORTH EUMETSAT

Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 2

Presentation Outline

The EPS Programme within IJPS

EPS Services, System Architecture

Metop Payload, EPS Mission and Products

Programmatic Status

Page 3: Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002 Page 1 THE EUMETSAT POLAR SYSTEM (EPS) Presented by: Ken ASHWORTH EUMETSAT

Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 3

The EPS Programme within IJPS

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Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 4

A Major Cooperation Between Europe and the USA

IN THE MARGINS OF THE G7, EUROPE AGREED IN PRINCIPLE TO SHARE THE BURDEN OF THE METEOROLOGICAL POLAR SERVICE WITH THE USA

INITIAL JOINT POLAR SYSTEM (IJPS) TO BE IMPLEMENTED In the context of the USA Convergence Under a NOAA-EUMETSAT cooperation agreement signed in November 1998 Through integration & coordination of the NOAA POES and the EUMETSAT EPS

(EUMETSAT POLAR SYSTEM) Programmes

SCOPE OF COOPERATION Afternoon & early morning orbits covered by the USA (POES & DMSP Satellites) Morning orbit covered by Europe (Metop Satellites) Exchange of instruments and data, coordinated development and operations

Page 5: Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002 Page 1 THE EUMETSAT POLAR SYSTEM (EPS) Presented by: Ken ASHWORTH EUMETSAT

Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 5

Initial Joint Polar System (IJPS)

Metop launches in 2005 and 2010 (9 Years of Operation)

05:30 LST 08:30 LSTUSAF - DMSP

- OLS- SSM/I- SSM/T- SSM/T-2

09:30 LSTMetop-1,2

- AVHRR/3 (US)- IASI (CNES/EUM)- HIRS/4 (US)- AMSU-A (US)- MHS (EUM) - ASCAT (ESA/EUM)- GOME-2 (ESA/EUM)- DCS (CNES)- GRAS (ESA/ EUM)

- S&R (CNES/Canada)- SEM (US)

13:30 LSTNOAA-N,N'

- AVHRR/3 (US)- HIRS/4 (US)- AMSU-A (US)- MHS (EUM)- DCS (CNES/US)- S&R (CNES/Canada)- SBUV (US)- SEM(US)

USAF (NOAA) EUMETSAT NOAA

Page 6: Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002 Page 1 THE EUMETSAT POLAR SYSTEM (EPS) Presented by: Ken ASHWORTH EUMETSAT

Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 6

EUMETSAT SATELLITE PROGRAMMES

METEOSAT

MSG

• Meteosat-5

• Meteosat-6

• Meteosat-7

• MSG-1

• MSG-2• MSG-3

EPS

• Metop-1

• Metop-2

• Metop-3

96 97 98 99 00 01 02 03 04 05 06 07 08 09 10 11 12

Over Indian Ocean since 7/98

Hot stand by at 10° W (since 6/98)

13

15

16

1714

NominaI operationestimated lifetime

Approved

Non nominal operation

Estimated fuel margin

Available for launch

IODC at 63°E

Planned

• MSG-4

JASON-2

Operational S/C at 0°(since 6/98)Cal/val phase

Page 7: Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002 Page 1 THE EUMETSAT POLAR SYSTEM (EPS) Presented by: Ken ASHWORTH EUMETSAT

Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

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• The EUMETSAT Polar System (EPS) is the European contribution to the Initial Joint Polar System (IJPS) established with NOAA;

• The IJPS will provide global meteorological and climate data from a series of European and American sun-synchronous polar orbiting satellites, comprising NOAA N&N´and Metop 1 & 2.

• EUMETSAT has established Co-operation Agreements with: ESA, for the development and procurement of the three Metop satellites;

NOAA, for the exchange of instruments, data and operation cross-support;

CNES, for the provision of IASI and ARGOS-DCS payloads;

The EPS Programme Within IJPS

Page 8: Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002 Page 1 THE EUMETSAT POLAR SYSTEM (EPS) Presented by: Ken ASHWORTH EUMETSAT

Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 8

EPS Programme Elements

Launcher

3 MetOp Satellites : MetOp-1, 2, 3

14 years of operation

Ground Segment

The EPS Programme Within IJPS

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Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 9

EPSUsers

WMO Community

through GTS/RMDCN

NOAA

NOAAsystem

EPSsystem

IJPS

The EPS Program within the IJPS

Users

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Satellite Direct Readout Conference for the Americas, Miami, December 9-13, 2002

Page 10

NOAA N & N’ p.m.METOP 1 & 2 a.m.

Global datadump

Global datadump

NOAA GS

EPS GSNOAA global dataMETOP blind orbits

METOP global dataNOAA blind orbits

Blind orbitsdata dump

CNESIASI TEC SAF

SAF

EUMETSAT POLAR SYSTEM

The EPS Programme Within IJPS

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The EPS Programme Within IJPS

EPS CDA Station (Svalbard) Coverage for Metop. Fairbanks/Wallops Stations coverage is also indicated

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EPS Services, System Architecture

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Global mission : delivery of global sounding measurements and to NMSs of Member States, NOAA within 2¼ hours of the instant of observation.

Local mission : real-time transmission of imaging and sounding data to local user stations.

DCP (data collection) mission of in-situ observational data.

Support to the space environment monitoring on behalf of NOAAPart of the IJPS program in partnership with NOAA

Search and Rescue service (S&R).

The EPS MissionsEPS Services, System Architecture

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Data set limited to

the observation of

the instantaneous

sub satellite

observation.

Data source is the

satellite for the user

point of view.

Possible means of

controlling access:

Encryption.

Direct read-out services;

HRPT and LRPT:

EPS HRPT and LRPT Services

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EPS Services, System ArchitectureProvided Service Service Characteristics / User Access

Global Data Level 0 Product Service: SEMLevel 1 Product Services: AVHRR,AMSU, HIRS, IASI, MHS, ASCAT,GOME, GRASLevel 2 Product Services: ATOVS,IASI, ASCAT, GOME, GRASLevel 3 Product Services:

Via NRT terminal (NMS, partner agencies) forcentrally-extracted products Reception of the data within 135 min from

sensing for all level 1 products, (for level 2products: 180 min);

Via RMDCN/GTS dissemination: Centrally extracted products start being put on

the GTS/RMDCN 2h15mn after sensing (level 1) 3h after sensing (level 2);

Local Data Direct Broadcast Services:HRPT Service, LRPT Service

Via a Metop-compatible High-Rate User Station(HRUS):

Via a Metop-compatible Low-Rate User Station(LRUS):.

Product retrieval U-MARF Retrieval Service Via Web-based access to the U-MARF services: The centrally-extracted archived products are

available for retrieval at the latest 7 hours aftersensing

User Services Users Information service Via Web-based access to the EUMETSAT informationservice:

Joint PolarSystem Support

NOAA Blind Orbit Support Service,NOAA TT&C Support Service,Metop Level 0 data Service

Limited to NOAA (cross-support in the frame of theIJPS)

Search andRescue MissionSupport

Search and rescue service Limited to CLS-ARGOS centre of Toulouse

Data CollectionMission Support

Data Collection Service Via U-MARF for the Level 0 A-DCS data

EPS Offers the following operational services / Data access

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Data Distribution - Timeliness

SAF (via NRT)

Other NRT User

LRPT/HRPTDownlink

Realtime

117mn

117mn

135 mn

135 mn

Global Data DumpNRT Data Circulation

Max. Data Age (up to Level 1)

GTS/RMDCN

GTS/RMDCN dissemination

7 hours U-MARF Users

U-MARF Data Access

LEGEND:

EPS Services, System Architecture

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The Metop Satellite

height: 6.3 mtransverse section:3.4 m x 3.4 m(launch configuration)

solar panel: 11.3 m

power: 2210 W (end of life, orbit average)

lifetime: 5 years

13 instruments

launch mass: 4200 kg

data flow: 3500 kbps

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IASI

HIRS-4

AVHRR-3

AMSU-A1

AMSU-A2MHS

GOME-2GRAS

ASCAT

• Customer: Single Space Segment Team at ESTEC

• EUMETSAT and ESA placed a contract with Astrium.

– Metop Prime Contractor

– ASCAT+GRAS development

– Satellite Simulator

The Metop satellites design is based on the heritage of the SPOT-5 and ENVISAT programmes;

• Status of Metop Space segment

– PDR held in June 1999

– CDR held in September 2001

• EUMETSAT and ESA placed a contract (Signed in March 2000) with Officine Galileo for the development of 3 GOME-2 instruments

• IASI CDR held April 2002

Metop Satellites

EPS Services, System Architecture

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Metop Payload, EPS Missions & Products

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MetOp-1, 2, 3 satellites embark the following sensor payload (except HIRS not planned to be flown on MetOp-3):

• Infrared / Visible Imagery:Advanced Very High Resolution Radiometer (AVHRR/3)6 channel visible / infrared cross-track scanning radiometer.

• Advanced Infrared Sounding:Infrared Atmospheric Sounding Interferometer (IASI) Michelson interferometer covering 3.4 to 15 m range with

0.25 cm-1 spectral resolution and integrated infrared imager.

• Infrared Sounding:High resolution Infra-Red Sounder (HIRS/4)

20 channel visible / infrared cross-track sounder.

Metop Payload, EPS Missions & Products

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• Microwave Sounding:Advanced Microwave Sounding Unit - A (AMSU-A)Microwave Humidity Sounder (MHS)20 channel microwave radiometer suite (cross-track scanning).

• Ozone Profiling:Global Ozone Monitoring Experiment - 2 (GOME-2)

Ultraviolet / visible, nadir-viewing grating spectrometer.

• Wind Scatterometry:Advanced Scatterometer (ASCAT)

C-band, dual swath scatterometer with three independent views.

• GPS Sounding:GNSS Receiver for Atmospheric Sounding (GRAS)

12 channel GPS receiver for navigation and occulation sounding.

Metop Payload, EPS Missions & Products

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IASI

HIRS-4

AVHRR-3

AMSU-A1

AMSU-A2MHS

GOME-2GRAS

ASCAT

Metop Payload, EPS Missions & ProductsThe Metop meteorological Payload - Accomodation

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EPS Product Services PRODUCT SERVICES AVAILABLE FROM CORE GROUND SEGMENT

& NETWORK OF SATELLITE APPLICATION FACILITIES

CGS BASELINE PRODUCTS INCLUDE: All level 1 Products from all NOAA & Metop sensors Selected Level 2 Products: Temperature/Moisture Profiles, Cloud Products...

VARIETY OF SERVICES/LEVEL 2 PRODUCTS FROM 7 SAFs: Ocean & Sea Ice Support to nowcasting & VSRF (SW Packages) Ozone Monitoring GRAS Meteorology Climate Monitoring Land Surface Analysis Numerical Weather Prediction (NWP)

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Metop Payload, EPS Missions & ProductsThe Metop System generates the following products (all in near realtime, Global coverage):

Level 0 products: SEM,

Level 1b products: AVHRR, AMSU, HIRS, IASI, MHS, ASCAT, GOME, GRAS

Level 2 Products : ATOVS, IASI, ASCAT, GOME, GRAS

Note: Level 1b products are radiometrically corrected, calibrated in physical units and geolocation information appended;

All Level 0, Level 1 and IASI/ATOVS Level 2 products are generated within the Core Ground Segment located at the EUMETSAT headquarters

Level 2 products for ASCAT, GOME,GRAS are generated by decentralised Satellite Application Facilities (SAF)

Further processing to Level 3 is entirely performed at SAFs

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EPS Data Circulation

Global data read-out through high latitude station

Exchange of global data with NOAA

Direct data read-out services: HRPT and LRPT High Resolution Picture Transmission Low Resolution Picture Transmission

Digital version of NOAA APT Level of commonality with MSG HRIT/LRIT

Coordinated with CGMS

Near Real Time delivery of CGS products (level 1 and elected level 2) to Primary NRT Terminals within Member States

Near Real Time delivery of level 2 products through GTS/RMDCN

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EPS Data Distribution and User Community

EPS Users

EPS Space Segment

EPS Overall Ground Segment (OGS)

UMARFSAFs

IASI-TEC CAL/VAL

HRPT/LRPTUsers

GTS/RMDCNNetwork

EPS System

Key

to Primary NRT User Entitiesexternal to OGS (level 1/2 products)

to off line OGS Users

to CGS NRT Users - Internal to OGS

End Users

to Space Segment Users

to EPS NRT End User (level 2 products, via GTS/RMDCN)

Primary NRT User Entity

WMOCommunity

EPS OfflineUsers

EPS NRTEnd Users

ARGOS DATA

GTSGateway

EPS CoreGround Segment

CGS

National Met.Services

ARGOS UsersCLS-ARGOS

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EPS provides global soundings at high spectral resolution with IASI

Metop Payload, EPS Missions & Products

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EPS provides global AVHRR imagery at full resolution

Multispectral image(Channels 2,3,4)

Metop Payload, EPS Missions & Products

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EPS Global AVHRR data is received & processed with 1 km sampling (nadir)

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EPS provides operational services with instruments in the heritage of European Earth Observation missions

• Global Ozone Monitoring Experiment (GOME-2)• Advanced Scatterometer (ASCAT)

Metop Payload, EPS Missions & Products

Exemple of Ozone Products from the GOME mission

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Example of ERS Wind Vector Field (500 Km Swath)

Source: ESA

Metop Payload, EPS Missions & Products

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Example Wind prototype product from ERS-2http://www.knmi.nl/onderzk/applied/scattmtr/prescat/eng/

Metop Payload, EPS Missions & Products

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GNSS Radiooccultaion Atmospheric Sounder (GRAS)

EPS provides additional sounding capabilities (for the first time in an operational environment)

Metop Payload, EPS Missions & Products

6390

6410

6430

6450

6470

6490

1.00E-08 1.00E-07 1.00E-06 1.00E-05 1.00E-04 1.00E-03 1.00E-02 1.00E-01

Total bending angle (mrad)

Imp

act

par

amet

er (

km

)

Bending Angle: from L2from L1ionospheric correction applied

From Luntama (2000)

Path of the ray perigee through the atmosphere

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Climate monitoring capabilities

Metop Payload, EPS Missions & Products

Mean Surface Temperature in K for April ,1987 Chédin et al., 1996

Mean Surface Temperature in K for April ,1988 Chédin et al., 1996

El Nino, 1986-1987, Surface Temperature Anomaly for April 1987 compared to April 1988. Chédin et al. 1996

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EPS allows sea surface monitoring at global scale

Metop Payload, EPS Missions & Products

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GOME/ERS-2 15-16-17 July 1998

NO2 total column concentration over Europe. High concentration over areas with dense population (Po valley, The Netherland and England)

GOME/ERS-2 15-16-17 July 1998

NO2 total column concentration over USA. High concentration over areas with dense population (East coast)

Source: DLR

Metop Payload, EPS Missions & Products

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Conclusions: EPS provides (1) • Continuity to the current system;

• High level sounding performances: provide enhanced data streams needed to further improve the capabilities of advanced NWP systems;

• Multi-instrument capabilities: assure service beyond operational meteorology, e.g. climate research and monitoring);

• Instruments built on the heritage of Earth observation missions (GOME, ASCAT). These are introduced into an operational environment;

• Long mission duration (14 years). This will assure that users are provided with long-term near real-time and off-line data service for meteorological and climate applications

Metop Payload, EPS Missions & Products

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Programmatic Status

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Basic Dates:• EUMETSAT EPS Programme approval in 1998

• ESA Metop-1 Programme approval in 1999;

• Metop industrial activities: Signature of the Phase C/D Contract in 12/1999

• Core Ground Segment: Contract signature with Alcatel in 12/2000;

• Launch Service: EUMETSAT signed the contract for the launch of the Metop satellites by Soyuz launchers from Baikonour with Starsem (a joint European – Russian company) in 12/2000;

• Nominal MetOp-1 launch date is between July 2005 (without margin) and • December 2005 (5 months margin included).

Programmatic Status

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Current Status of Metop activities •PFM PLM integration at Astrium ED essentially completed;

•Final system testing started in September, including TV testing planned in November;

•In parallel integration (and test) of the FM2 PLM avionics successfully completed.

•PFM SVM integrated and initial system reference testing has commenced

•SVM will undergo TV and EMC testing at Intespace prior to satellite integration (with PLM) in March 03

Programmatic Status

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Programmatic Status

Metop Satellite Integration & Test

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Ground Segment Status:• The Core Ground Segment (CGS) CDR held from late May to early July 2002

• Core Ground Segment: Factory Acceptance Testing started for the Polar Station Facility (PSF), Front End Processor (FEP), Product Generation Facility (PGF), Flight Dynamics Facility (FDF) and the Dissemination Facility (DIF).

• Polar Site Infrastructure Service in Svalbard successfully completed its Verification Review in May 2002

– Transportation, assembly and erection of both EPS antennas and radomes was completed by early August, within the available “weather window”.

– The RF, baseband and monitoring and control equipment shipped in autumn 2002

– On-site Acceptance of the PSF planned for early 2003.

• Unified Archive Facility Detailed Design Review for the EPS extension took place in October 2002;

Programmatic Status

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Final stages of mechanical assembly of the CDA-1 antenna and radome (Svalbard).

Programmatic Status