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Satellite Altimetry Status

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users needs as seen by space agencies. One ' high accuracy ' reference mission. TOPEX/Poseidon , Jason series (including Jason ... Constellations (Iridium-NEXT? ... – PowerPoint PPT presentation

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Title: Satellite Altimetry Status


1
Satellite Altimetry Status Products Part 1
  • J. Lambin, CNES
  • G. Dibarboure, CLS

2
Satellite altimetry users needs as seen by
space agencies
  • One high accuracy reference mission
  • TOPEX/Poseidon , Jason series (including Jason-3)
    gt to be continued by Jason-CS?
  • Payload required
  • Dual-frequency altimeter,
  • Microwave radiometer,
  • Precise orbit determination suite (GPS, DORIS,
    laser)
  • Orbit
  • Minimizing tide aliasing non-sunsynchronous,
    mid-inclination
  • Suitable for POD (high altitude)
  • Data latency 3h / 2 days / 2 month
  • One at least (ideally 3) other altimetry missions
    (ERS, GFO, ENVISAT)
  • less demanding POD gt post-calibrations using
    reference mission, SSO OK
  • Mesoscale oriented gt better spatial coverage,
    but longer cycles
  • Future generation / alternatives
  • Swath altimetry SWOT
  • Constellations (Iridium-NEXT?)

3
Ocean Surface Topography Constellation Roadmap
21
Medium accuracy SSH from high-inclination
sun-synchronous orbit
ENVISAT ESA
GFO-FO NOAA
Swath altimetry from high-inclination orbit
(several orbit options)
Orbit to be assessed
High accuracy SSH from mid-inclination orbit
Jason-3 Europe/USA
Jason-1 Fr./USA
4
Current altimetry missions
  • Jason1 in extended mission, fully operational
  • Moved to interleaved orbit with Jason-2 in
    Jan/Feb 09, after 6-month formation flying
    phase
  • Vulnerable to equipments failure risk
  • Jason-2 lauched in June 2008,
  • OGDR distributed operationally since Dec 2008,
  • IGDR distributed operationally since Jan 2009
  • GDR will be released after OSTST (July 2009)
  • DUACS products already available
  • Very good product quality
  • ENVISAT
  • excellent synergy with Jason1 (T/P and ERS
    complementarity further improved)
  • S-band missing degraded quality by lack of
    ionospheric delay correction
  • Will be put on a drifting orbit in 2010

Jason-1 vs Jason-2 SSH differences
DUACS map of SLA J1J2EN
5
SARAL/AltiKa
  • Cooperative framework CNES/ISRO
  • Altimetric Gap filler between ENVISAT SENTINEL3
  • Research oriented mission
  • new, higher frequency, greater performance
  • potential new applications on ice, land, coastal
    areas
  • but with a consolidated architecture
    conventional altimeter
  • Tentative launch date mid- to end-2010
  • Payload
  • AltiKa Ka-band altimeter (higher accuracy, no
    need for a 2nd frequency)
  • Dual-frequency radiometer (sharing the same
    antenna)
  • POD DORIS/LASER
  • Orbit same as ENVISAT (sun-synchronous, 35-day
    cycle)
  • Data policy the same as JASON missions
    (through CNES/ISRO RAs)
  • Next India/France scientific workshop on 3-5
    december in Ahmedabad

6
Sentinel-3
  • ESA mission, in the frame of GMES program
  • Mission Profile
  • 7-year lifetime (consumables for 12 years)
  • SSO orbit (10h descending), 27-day repeat cycle,
    98.65
  • Satellite Payload
  • Ocean and Land Colour Instrument (OLCI)
  • Sea and Land Surface temperature (SLST)
  • Sentinel-3 Ku/C Radar Altimeter (SRAL)
  • Dual Frequency MicroWave Radiometer (MWR)
  • POD GPS/DORIS/Laser
  • Products 3h / 1-2 days / final after POD

7
HY-2A mission description
  • Chinese oceanographic mission ( French
    participation)
  • Launch planned Sept 2010
  • Payload
  • Dual-frequency altimeter Ku/C
  • nadir 3-frequency radiometer
  • 5-frequency scanning radiometer
  • Wind/wave scanning scatterometer
  • DORIS/GPS/LRA
  • Orbit (sun-synchronous 6-18, 99.35)
  • First 2 years with a 14-day cycle
  • Then one year with geodetic orbit (168-day cycle,
    5-day approx. subcycle)
  • Products availability?
  • Through DUACS multi-mission products (not
    confirmed yet)

geodetic orbit after 3 days
One day of the 14-day orbit
8
Cryosat-2
  • ESA mission, to be launched in Nov 2009
  • Objective to determine fluctuations in the mass
    of the Earths major land and marine ice fields
  • Mission description
  • Lifetime 3 years 6 month comissioning
  • Orbit
  • LEO, non sun-synchronous
  • Repeat cycle 369 days (30 d sub-cycle)
  • Mean altitude 717 km
  • Inclination 92
  • Spacecraft and Payload recurrent from lost
    CryoSat 1
  • Instruments
  • SIRAL (SAR/Interferometric Radar Altimeter)
  • Low-Resolution / SAR / SARIn modes
  • KU-band (single frequency, no radiometer)
  • POD from DORIS and laser
  • Ocean data availability not confirmed yet,
    studies under way

9
Jason-3
  • NOAA/EUMETSAT cooperation with CNES NASA
    contributions
  • CNES in-kind contribution Proteus platform ,
    system engineering, and manpower equivalent to
    JASON/OSTM (i.e. about one third of European part
    of the program)
  • Launch mid-2013
  • Mission design Jason-2 like
  • Pending approval (in December 2009)

and Jason-CS?
10
Surface Water Ocean Topography (SWOT)
  • Mission combining research needs associated to
    hydrology and oceanography
  • - mapping of water level for rivers, lakes, and
    oceans (including coasts)
  • Principle Wide-swath interferometric, Ka-band
    altimeter
  • Recommended by the US Decadal Survey
  • Submitted in the frame of the Cnes Scientific
    Prospective Seminar (march, 2009)
  • Cooperation scheme TBD (NASA/CNES/)
  • Phase 0 in 2007, pre-phase A phase A in
    2008/2009
  • Launch possible in 2016

11
Conclusions
  • There is a rich panel of missions under
    development or planning gt let us wish they will
    all succed!
  • Space agencies (NASA, CNES) tend to put as
    priority innovative missions
  • Promising in a long term perspective, but
  • Potential issues in the continuity of the
    long-term record
  • Some effort is required to secure the transition
    to operational agencies of already mature
    concepts
  • Multiple missions decided/developed by multiple
    agencies/countries
  • Coordination not guaranteed, higher programatics
    risk
  • Data availability on a case-by-case basis
  • Efforts from CEOS (through NOAA and EUMETSAT) to
    improve altimetry mission coordination
  • GODAE could (and should) be more vocal about
    their needs

12
CNES involvment in altimetry
Reference mission Ocean Large scale
Complementing mission mesoscale, ice
Earth reference system
1990
experiment
ERS-1 (ESA) Altimeter algorithm
TOPEX/POSEIDON (CNES/NASA) Launcher DORIS
POSEIDON Mission Center
ERS-2 (ESA)
ENVISAT (ESA) DORIS Altimeter Processing Archive
distrib.
2000
Jason-1 (CNES/NASA) Satellite bus DORIS
POSEIDON Control Mission Center
HY-2 (CNSA) DORIS
2005
ALTIKA/SARAL (CNES/ISRO) Altimeter, radiometer,
DORIS, Lra Process, archive distrib.
Jason-2 / OSTM (CNES/NASA/EUMETSAT/NOAA) Satellit
e bus DORIS POSEIDON Control Mission Center
PLEIADES (CNES) DORIS
2010
CRYOSAT2 (ESA) DORIS
Sentinel-3A (ESA) DORIS
SALP Altimetry and precise positioning service
operational
MERCATOR assimilation, forecast CNES / SHOM /
METEOFRANCE / IFREMER / CNRS / IRD
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