ERS and Envisat Precise Orbit Determination: Status
Last update: 16 Nov 2000
Status
Precise ERS-1 and ERS-2 orbits are available for the period 30 July 1991 to
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This covers the entire ERS-1 altimeter mission and ERS-2
since launch until July 2003, after the end of the global (LBR) altimetry mission.
These orbits are produced with the Delft Gravity Model DGM-E04, an ERS-tailored clone of JGM-3.
New ERS-2 orbits processed with the EIGEN-GRACE01S gravity field and other updated
force models are available from 2002 unwards, including SLR-only orbits after
June 2003.
Precise Envisat orbits processed with SLR and DORIS data and the EIGEN-GRACE01S gravity
field are available since the start of the DORIS data availability.
NEW since 27 May 2004
- ERS-2 and Envisat EIGEN-GRACE01S orbits, which have been available by ftp for some time now,
have now also been linked from this website.
NEW since 16 Nov 2000
- Changes made to getorb package for compatibility with Red Hat 7.0.
Download getorb_2.1.5 now.
NEW since 27 Oct 2000
- Extra utilities included in the getorb package (version 2.1.4).
Go for the download now.
- New on-line utilities.
Interpolate orbits and do date conversions on-line.
- Precise ERS-2 orbits are available till
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Go for the download now.
NEW since 22 Feb 2000
- Precise ERS-2 orbits are available till 14 October 1999 (end of Cycle 46).
Earlier released versions for Cycles 43 and 44 have been updated.
- Preliminary ERS-2 orbits are available till 4 February 2000 (early Cycle 50).
NEW since 22 Nov 1999
- Fast-delivery orbits for ERS-1 (since July 1999) are available.
- Precise ERS-2 orbits are available till 5 August 1999 (end of Cycle 44).
- Preliminary ERS-2 orbits are available till 31 October 1999 (mid Cycle 47).
- All orbits have been moved back to the RADS server
ftp://dutlru2.lr.tudelft.nl/pub/orbits/
NEW since 7 Sep 1999
- Precise ERS-2 orbits for Cycles 39-41 (1 January to 22 April 1999).
- All orbits are now stored on both FTP sites arc by arc. This makes
updating more easy and if you want to mirror the sites yourself, you have
short download times.
NEW since 27 Apr 1999
- Precise ERS-2 orbits for Cycles 35-38 (20 August 1998 to 7 January 1999).
- Precise ERS-1 orbits for Mission Phases A and B (30 July 1991 to 11
April 1992). Note that these orbits have a lesser precision than others
because of the limited amount of tracking.
NEW since 23 Feb 1999
- Precise ERS-2 orbits for Cycle 34 (16 July to 20 August 1998).
NEW since 3 Nov 1998
- Precise ERS-2 orbits for Cycles 31-33 (27 March to 16 July 1998).
NEW since 21 Jul 1998
- Precise ERS-2 orbits for Cycles 29-30 (20 January to 27 March 1998).
- SLR tracking to ERS-1 has commenced again.
NEW since 14 Jun 1998
- Precise ERS-2 orbits for Cycles 27-28 (11 November 1997 to 22 January 1998).
NEW since 28 Mar 1998
- Precise ERS-2 orbits for Cycles 23-26 (23 June to 13 November 1997).
NEW since 5 Dec 1997
- Precise ERS-2 orbits for Cycles 17-22 (27 November 1996 to 25 June 1997).
- Preliminary orbits now also available at a few weeks delay, based on
SLR and OPR-1 derived altimeter crossovers. Read how to
download these orbits now.
- A full FTP site has now been provided at DEOS. Read how to
download or go directly to
ftp://dutlru2.lr.tudelft.nl/pub/orbits/
- Regular updates of sea level anomalies in the Central Pacific
displaying the effect on sea level of the 1997/1998 El
Niño. These results are based on the ESA OPR-1 altimeter
data enhanced with Delft ERS-2 Preliminary orbits.
NEW since 20 May 1997
NEW since 29 April 1997
- ERS-2 orbits beyond the Tandem Mission are available till 27 Novermber 1996
(up to and including Cycle 16). This covers all available ERS-2 OPR
altimeter products to date.
Download them now.
- The Web Pages have a new layout. Hopefully this makes the information
- The tar files in which the ERS-1 and ERS-2 orbit files where
distributed before are repackaged to archives of 4 MBytes maximum. This
has, however, no impact on the orbits itself.
NEW since 1 April 1997
- Over 4 years of ERS-1 orbits (April 1992 - May 1996) are now
available, consistently produced with the DGM-E04 gravity field model.
This completes the production of all ERS-1 orbits.
Download.
- Orbits for the ERS tandem mission have been completed until the end of the
ERS-1 mission. The orbit determination for the two satellites is combined during
this period, using SLR, single and dual satellite crossovers as tracking data.
Precise orbits for ERS-2 are available for the period May 1995 - May 1996.
Download.
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