boundary="_000_a942fe53021d4dcba6259eb2d2cfdc65cnesfr_" ****************************************************************************** dorismail 18-Mar-2026 11:26:19 Message No 1476 ****************************************************************************** Author: Couhert Alexandre Subject: Ocean Surface Topography Science Team Meeting 2026, Session Precision --_000_a942fe53021d4dcba6259eb2d2cfdc65cnesfr_ Dear Colleagues, Please consider submitting an abstract to this dedicated Precision Orbit De= termination session organized at the 2026 OSTST, to be held i= n Wiesbaden, Germany, 22-26 June 2026. The deadline for abstract submission= is April 3, 2026. Our splinter's description: Precision orbit determination underpins the accuracy and quality of the dat= a for all altimeter missions. With a thirty-year long altimeter record from= six missions on the reference orbit (TOPEX/Poseidon, Jason-1, Jason-2/OSTM= , Jason-3, Sentinel-6A/B) and from several others on lower orbits (ERS, Env= isat, CryoSat-2, HY-2A/-2B/-2C/-2D, SARAL/AltiKa, Sentinel-3A/B, SWOT), the= focus is now on the long-term stability of the orbit solutions and on the = impact of geographically correlated errors on both the global and regional = Mean Sea Level estimates. The most critical issues concern the stability of the reference frame for c= omputing the orbits, the accuracy and fidelity of the force models that und= erpin the POD computations and the overall quality of the available trackin= g data. We monitor closely the performance of the tracking systems onboard = the current flight missions (especially Jason-3 and Sentinel-6) but we are = also interested in the general performance of the SLR, DORIS, and GNSS netw= orks used for orbit determination. The stability of the reference frame and= the tracking systems, and the consistency between the orbits produced by t= he different geodetic techniques contributes to the error budget for the al= timetric data and the science products. The new reference frames realizatio= ns for ITRF2020 show improvement with respect to ITRF2014, and we are espec= ially interested in their application to satellite altimetry POD for each o= f the techniques. Each of the geodetic techniques has systematic errors tha= t impact the measurements which affect the POD stability and accuracy on bo= th the short- and the long-term. With the stringent radial orbit accuracy r= equirements, the refinement of the satellite force and measurement modellin= g continues to be essential. We encourage papers that discuss the latest models that are applicable for = satellite altimetry POD given the operational constraints of latency and th= e timely delivery of GDR products. The POD splinter brings together POD spe= cialists with altimetry users so that the two communities can interact. POD= specialists gather during the splinter to discuss their latest results but= they are also there to answer questions from the community. The goal of th= e POD splinter is to ensure that spurious orbit-related signals do not cont= aminate the altimetric products on medium-term or long-term time scales, an= d to help ensure that altimetric data across different missions from differ= ent orbits can be compared and combined in a seamless fashion. We are looking forward to discussing with you in Wiesbaden! On behalf of the co-chairs of the session, Alex Conrad, Alexandre Couhert, Frank Lemoine and Carlos Fern=E1ndez Mart= =EDn --_000_a942fe53021d4dcba6259eb2d2cfdc65cnesfr_

Dear Colleagues,

 

Please consider submitting an a= bstract to this dedicated Precision Orbit Determination session organized a= t the 2026 OSTST<= /a>, to be held in Wiesbaden, Germany, 22-26 June 2026= . The deadline for abstract submission is April 3, 2026.

 

Our splinter’s descriptio= n:

 

Precision orbit determination u= nderpins the accuracy and quality of the data for all altimeter missions. W= ith a thirty-year long altimeter record from six missions on the reference = orbit (TOPEX/Poseidon, Jason-1, Jason-2/OSTM, Jason-3, Sentinel-6A/B) and from several others on lower orbits (ERS, Envi= sat, CryoSat-2, HY-2A/-2B/-2C/-2D, SARAL/AltiKa, Sentinel-3A/B, SWOT), the = focus is now on the long-term stability of the orbit solutions and on the i= mpact of geographically correlated errors on both the global and regional Mean Sea Level estimates.

 

The most critical issues concer= n the stability of the reference frame for computing the orbits, the accura= cy and fidelity of the force models that underpin the POD computations and = the overall quality of the available tracking data. We monitor closely the performance of the tracking systems = onboard the current flight missions (especially Jason-3 and Sentinel-6) but= we are also interested in the general performance of the SLR, DORIS, and G= NSS networks used for orbit determination. The stability of the reference frame and the tracking systems, and the con= sistency between the orbits produced by the different geodetic techniques c= ontributes to the error budget for the altimetric data and the science prod= ucts. The new reference frames realizations for ITRF2020 show improvement with respect to ITRF2014, and we are especia= lly interested in their application to satellite altimetry POD for each of = the techniques. Each of the geodetic techniques has systematic errors that = impact the measurements which affect the POD stability and accuracy on both the short- and the long-term. With = the stringent radial orbit accuracy requirements, the refinement of the sat= ellite force and measurement modelling continues to be essential.

 

We encourage papers that discus= s the latest models that are applicable for satellite altimetry POD given t= he operational constraints of latency and the timely delivery of GDR produc= ts. The POD splinter brings together POD specialists with altimetry users so that the two communities can inter= act. POD specialists gather during the splinter to discuss their latest res= ults but they are also there to answer questions from the community. The go= al of the POD splinter is to ensure that spurious orbit-related signals do not contaminate the altimetric prod= ucts on medium-term or long-term time scales, and to help ensure that altim= etric data across different missions from different orbits can be compared = and combined in a seamless fashion.

 

We are looking forward to discu= ssing with you in Wiesbaden!

 

On behalf of the co-chairs of t= he session,

Alex Conrad, Alexandre Couhert,= Frank Lemoine and Carlos Fern=E1ndez Mart=EDn

 

 

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