[IGSREPORT-30589] Wk 2380 IGS Final Orbits
acc
acc at igs.org
Thu Sep 4 06:49:04 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2380 (Aug 17, 2025 - Aug 23, 2025)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
IGS0OPSFIN_${yyyy}${doy}0000_01D_15M_ORB.SP3 IGS GPS ephemeris files in SP3
format.
IGS0OPSFIN_${yyyy}${doy}0000_01D_05M_CLK.CLK IGS GPS satellite and station
clocks in clock RINEX format.
IGS0OPSFIN_${yyyy}${doy}0000_01D_01D_CLS.SUM IGS GPS clock combination summary
report.
IGS0OPSFIN_${yyyy}${doy}0000_07D_01D_ERP.ERP Earth Rotation Parameters (ERP)
and their rates as well as
Universal Time (UT1-UTC) and
Length Of Day (LOD) associated
with IGS ephemerides.
IGS0OPSFIN_20252290000_07D_01D_SUM.SUM Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, ESA, GFZ, GRG and JPL.
The other centres are excluded because of either poorer consistency, or they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | ABMF ADIS ALIC AREG ASCG BADG BRST BRUX BUCU CPVG
0 | COD | CRO1 DARW DUBO FLIN GANP GODE GUAM HOFN IQAL KOKV
0 | COD | KOUR LAUT MAL2 MAR6 MAS1 MCM4 MOBS NAUR NICO PARC
0 | COD | PDEL PERT POHN QUIN RESO REUN SCH2 SFER STK2 SUTM
0 | COD | THTG TID1 TLSE TRO1 ULAB URUM VNDP XMIS YEL2 ZIM2
0 | COD | POLV
0 | EMR | SUTM BADG BSHM RIGA SUTM YEL2
0 | ESA | CUSV
0 | GFZ | 21 21 BADG BSHM LAUT LAUT
0 | JPL | BADG CHTI POHN SUTM
0 | MIT | FLRS GMSD MADR MCIL MCM4 MEDI NNOR NYAL ROTH SVTL
0 | MIT | USUD VNDP WROC FLRS GMSD MADR MCIL MCM4 MEDI NNOR
0 | MIT | NYAL ROTH SVTL USUD VNDP WROC
1 | COD | 2 ASCG CCJ2 CPVG DAEJ DJIG GAMB GANP GLSV GRAC LMMF
1 | COD | MCIL MONP NLIB NYA2 NYAL PIE1 TASH YEL2 CPVG GLSV
1 | COD | GRAC MONP NYAL
1 | EMR | DAEJ DAEJ PIE1
1 | ESA | CPVG DAEJ CPVG CUSV DAEJ GLSV PIE1 TASH
1 | GFZ | 21 21 CPVG LAUT NYA2 CPVG LAUT NYA2
1 | GRG | 13 13 NRMD TASH DJIG NRMD NYA2 TASH
1 | JPL | NRMD BADG CHTI CUSV FTNA MAJU NRMD
1 | MIT | CRO1 FLRS GMSD GRAZ MADR MCM4 NNOR NOT1 NYAL PRDS
1 | MIT | ROTH WROC CRO1 FLRS GMSD GRAZ MADR MCM4 NNOR NOT1
1 | MIT | NYAL PRDS ROTH WROC
2 | COD | ASCG BADG BOGT CPVG CUSV FLRS GANP GLSV GRAC HRAO
2 | COD | LMMF MBAR MCIL NNOR NYA2 ONSA PDEL SYOG TLSE YKRO
2 | COD | ZAMB BOGT CUSV MBAR NNOR YKRO ZAMB
2 | EMR | MBAR ZAMB BADG GLSV MBAR MCM4 STHL ZAMB
2 | ESA | BADG CKSV MAW1 SCUB YEL2 POL2 POVE QUIN SCUB YEL2
2 | GFZ | 21 13 21 BADG LAUT NRMD ZAMB LAUT MONP TASH
2 | GRG | DAV1 GLSV BOGT DAV1 GLSV POL2
2 | JPL | BADG CHTI NRMD QUIN ZAMB
2 | MIT | BRST CKSV EBRE HOFN MADR MCM4 MELI MQZG NYAL REDU
2 | MIT | REYK RIGA SVTL WROC YARR YEBE BRST EBRE HOFN MADR
2 | MIT | MCM4 MELI MQZG NYAL REDU REYK RIGA SVTL WROC YARR
2 | MIT | YEBE
3 | COD | ABMF ASCG BADG BOGT BRST BUCU CEDU COCO CZTG DARW
3 | COD | DAV1 FAIR FLRS GODE HKSL KOUR LMMF MAL2 MAR6 MAW1
3 | COD | NAUR NICO PDEL PERT RESO RIGA SCH2 SCUB SFER STK2
3 | COD | SYOG TID1 WUH2 YAR2 ZIM2 CKSV CZTG GRAC
3 | EMR | DAV1 BADG DAV1 FAIR MAW1
3 | ESA | CUSV FAIR NRMD CUSV FAIR POVE TOPL TUVA
3 | GFZ | 21 21 BADG ONSA PTVL PTVL SCUB
3 | JPL | NRMD BOGT CHTI GLPS HKSL NRMD TUVA
3 | MIT | BRST EBRE GMSD GRAS JOZE LMMF MEDI MQZG NNOR ROTH
3 | MIT | SFER TRO1 USUD WROC BRST CHTI EBRE GMSD GRAS JOZE
3 | MIT | LMMF MEDI MQZG NNOR ROTH SFER TRO1 USUD WROC
4 | COD | ABMF AREG AREQ ASCG BADG CCJ2 DAEJ DUBO FALK FLIN
4 | COD | FLRS GAMB GRAC KRGG LMMF NNOR ONSA PDEL QUIN SYOG
4 | COD | TRO1 VOIM YEL2 NYA2
4 | EMR | BADG MBAR STHL YEL2
4 | ESA | BADG BAKE CUSV GMSD IISC KRGG BADG BAKE GMSD IISC
4 | ESA | MAL2 VOIM YEL2
4 | GFZ | 21 21 BADG GAMB LAUT NYA2 GAMB LAUT NYA1
4 | GRG | AREQ AREG AREQ GAMB NYA2 TRO1
4 | JPL | BADG HKSL MAJU MAL2 NRMD TUVA
4 | MIT | DARW GMSD GRAS LMMF MADR MAR6 MCM4 MEDI PIE1 REDU
4 | MIT | SFER USUD DARW GMSD GRAS LMMF MADR MAR6 MCM4 MEDI
4 | MIT | PIE1 REDU SFER USUD
5 | COD | ADIS ASCG BADG BOGT CPVG DAV1 GANP GLSV HKSL NAUR
5 | COD | NICO PDEL SCUB TLSE VNDP YEL2 BOGT DAV1 SCUB
5 | EMR | AREQ BADG NAUR YEL2
5 | ESA | BADG CUSV MAJU CUSV DJIG MAJU MAL2 SEYG
5 | GFZ | 21 13 21 BADG NYA1 NYA2
5 | GRG | 13 13 ADIS NRMD ADIS GRAC NRMD SUTM
5 | JPL | NRMD BADG HKSL NRMD PTAG SGOC
5 | MIT | 4 4 BADG DARW GANP GMSD LAUT MADR MAR6 MCM4 MEDI
5 | MIT | MELI METG NNOR SCTB TLSE BADG DARW GANP GMSD LAUT
5 | MIT | MADR MAR6 MCM4 MEDI MELI METG NNOR SCTB TLSE
6 | COD | ASCG CCJ2 CKSV CPVG CUSV GANP HKSL IISC KARR KOUR
6 | COD | LMMF MATE NLIB PDEL THTG TLSE BOGT CUSV MATE
6 | EMR | 4 4 CHUR
6 | ESA | CHUR CUSV IISC NYA2 TUVA CUSV GMSD NYA2 TUVA URUM
6 | GFZ | 5 21 5 21 IISC NYA2 PTVL AREQ NYA2 PTVL
6 | GRG | 13 13 AREQ CKSV DAV1 SSIA
6 | JPL | CHTI GUAM NRMD RIO2
6 | MIT | DARW GANP GMSD KRGG MADR MCM4 MEDI NNOR NYAL TLSE
6 | MIT | YARR DARW GANP GMSD KRGG MADR MCM4 MEDI NYAL TLSE
6 | MIT | YARR
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | ESA | ~12:00 | ~ 0.34 ns
1 | ESA | ~04:40 | ~ 0.34 ns
2 | ESA | ~08:00 | ~ 0.34 ns
3 | ESA | ~11:00 | ~ 0.33 ns
4 | ESA | ~06:00 | ~ 0.33 ns
5 | ESA | ~06:00 | ~ 0.34 ns
6 | ESA | ~18:00 | ~ 0.33 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | MIT | 4
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
Starting 28-Nov-2022, all IGS products, are based on the IGS realization of
the ITRF2020 reference frame (IGS20). Starting from the same date, the IGS
products are based on the repro3 standards, including long filename formats.
For more information see IGSMAIL #8238, #8256, #8274 and #8282.
Starting 02-Feb-2025, all IGS products, are based on the IGS realization of
the first yearly update of ITRF2020 called ITRF2020-u2023. This IGS realization
is called IGb20.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | 1.4 -1.5 1.4 6 -14 3 -.14
EMR | 0 | 3.8 -2.3 -4.6 11 -9 -5 -.06
ESA | 0 | -.4 -1.1 .0 7 5 9 -.80
GFZ | 0 | .6 -.4 .5 9 -12 5 .05
GRG | 0 | -.2 -.7 -.5 15 17 -10 -.19
JGX | 0 | 1.6 1.3 -10.2 9 -21 12 -.23
JPL | 0 | -1.6 -2.5 -7.4 8 -4 13 -.17
MIT | 0 | -1.3 -3.0 13.4 11 -5 -3 -.02
NGS | 0 | 1.1 1.6 3.6 17 -3 -18 .11
SIO | 0 | -.4 -.9 -1.8 9 -33 -13 -.03
COD | 1 | 1.3 -1.5 1.3 5 -12 4 -.09
EMR | 1 | 7.0 -3.5 -5.2 1 3 -2 -.16
ESA | 1 | -.0 -1.0 -.1 6 1 7 -.87
GFZ | 1 | .2 -.8 .6 3 4 13 .17
GRG | 1 | -.0 -.3 -.8 6 14 11 -.07
JGX | 1 | .6 2.0 -12.9 23 -3 12 -.11
JPL | 1 | .4 -5.0 -10.0 13 -5 8 -.08
MIT | 1 | -4.1 -3.5 13.8 2 8 7 .00
NGS | 1 | 1.4 -.1 10.7 7 7 -16 .02
SIO | 1 | 2.0 -3.3 -6.0 -16 -58 7 .11
COD | 2 | 1.1 -1.4 1.3 7 -7 2 -.04
EMR | 2 | 4.1 4.3 -7.0 1 3 -1 .02
ESA | 2 | .0 -1.1 -.1 1 4 12 -.82
GFZ | 2 | .1 -.7 .2 5 11 10 .18
GRG | 2 | .2 -.2 -1.3 -3 19 19 -.19
JGX | 2 | -.2 4.0 -10.7 34 6 7 -.13
JPL | 2 | .8 -.7 -7.6 6 -2 12 -.09
MIT | 2 | .2 -3.6 14.1 -5 14 3 .02
NGS | 2 | 5.4 -2.1 4.8 4 -3 -20 -.04
SIO | 2 | .3 -2.8 -5.8 -13 -71 9 .17
COD | 3 | 1.2 -1.2 1.0 11 -11 -1 -.07
EMR | 3 | 6.9 -4.3 -8.6 -2 1 -6 -.03
ESA | 3 | .0 -1.6 -.2 0 1 4 -.68
GFZ | 3 | .3 -.8 .0 -4 0 13 .23
GRG | 3 | .1 -1.2 -1.1 13 20 11 -.11
JGX | 3 | -1.6 .3 -12.3 24 -8 10 -.29
JPL | 3 | .6 -3.5 -8.5 12 0 7 -.06
MIT | 3 | -.6 -5.1 15.8 -5 10 8 -.01
NGS | 3 | 2.9 -5.1 3.0 -10 4 -22 -.02
SIO | 3 | -.8 -6.1 -3.7 -97 -17 11 .21
COD | 4 | 1.3 -1.2 1.0 7 -14 4 -.12
EMR | 4 | 4.7 -4.9 -5.2 2 2 1 -.00
ESA | 4 | -.3 -.8 -.6 -3 -1 7 -.77
GFZ | 4 | -.1 -.6 .2 -10 3 11 .09
GRG | 4 | .1 -.8 -1.2 1 31 12 .03
JGX | 4 | -2.4 .7 -11.6 18 -7 11 -.34
JPL | 4 | -5.6 -.5 -10.1 14 -1 2 -.06
MIT | 4 | -1.2 -4.7 13.3 6 13 1 -.05
NGS | 4 | 3.1 -1.6 -.6 -2 3 -8 -.04
SIO | 4 | -.3 -4.1 -2.7 -6 24 0 .12
COD | 5 | 1.2 -1.5 1.2 8 -11 -1 -.10
EMR | 5 | 7.1 -5.3 -4.3 1 3 -3 -.27
ESA | 5 | -.0 -.9 .3 -13 4 12 -.95
GFZ | 5 | .3 -.9 .0 -4 9 9 .12
GRG | 5 | -.1 -.6 -1.1 1 32 2 -.12
JGX | 5 | -.5 2.9 -13.1 10 -7 11 -.41
JPL | 5 | -3.6 .7 -7.1 6 -2 5 -.01
MIT | 5 | .2 -3.8 16.1 5 16 7 -.05
NGS | 5 | 6.3 -1.8 3.3 8 -4 -15 -.01
SIO | 5 | .0 -2.0 .5 -19 -85 18 .18
COD | 6 | 1.4 -1.4 1.0 3 -7 4 -.12
EMR | 6 | 2.3 -4.0 -8.9 10 10 0 -.25
ESA | 6 | -.2 -.5 1.1 -11 5 14 -.89
GFZ | 6 | .2 -.8 .6 4 7 4 .14
GRG | 6 | .1 -.6 -1.5 -1 17 7 -.08
JGX | 6 | .2 2.4 -11.8 39 -6 9 -.29
JPL | 6 | -1.6 -2.8 -6.5 -9 -7 10 .01
MIT | 6 | -.9 -1.2 12.6 -1 16 9 .08
NGS | 6 | 4.6 -.4 7.3 10 -3 -16 .00
SIO | 6 | -.5 -2.5 -5.8 -44 11 25 .03
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.2380.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2380.b).
The second part, Table 2, contains the complete ephemeris and clock
correction transformation parameters (includes both the apriori and a
posteriori values) for each centre and each day (Tables 2.2380.[0-6]).
The third part, Table 3, contains two types of daily RMS for each satellite
and centre, along with the computed satellite position sigmas for the
combined orbits (Tables 3.2380.[0-6]). The first type of satellite RMS is
based on orbit combination and the second RMS type is a result of the 7-day
arc evaluation of each centre ephemerides. The fourth part, Table 4, is a
weekly summary of the daily precise navigation summaries for centres
providing both orbit and clock solutions. It contains weekly station RMS
w.r.t. the initial coordinates for the Latitude, Longitude and Height
components for up to three IGS stations (Table 4.1307). The fifth part,
Table 5, is similar to Table 4 and contains daily precise navigation
statistics (Tables 5.2380.0-6). The sixth part, Table 6, is a weekly
summary of daily ERP combination statistics. The seventh part, Table 7,
contains the daily ERP statistics. But this is not the IGS official ERP
combination products (which come from the accompanying SINEX combination)
but provided to check combination consistency, etc.
In Tables 1-3, the most important statistic which is meaningful for intra
centre/satellite analysis is labeled WRMS. It is a weighted RMS where
normalized weights are based on accuracy codes given in the SP3 files, and
should not be affected by downweighted/problem satellites when acknowledged
by individual centres in their SP3 file.
Table 1: Week 2380 summary. (Aug 17, 2025 - Aug 23, 2025)
Table 1.2380.a GPS week: 2380 MJD: 60904.000-60910.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 796| 0 0 3 17 -5 23 -.02 7 6 | -680 36 6 140
| 0 0 0 6 9 15 .02 | 60 115
emr 107| 0 0 0 0 -2 25 .03 8 8 | 4233 -8535 5 95
| 0 0 1 5 7 6 .02 | 11362 22767
esa 188| 0 0 0 3 1 2 -.06 8 8 | -1168 80 6 184
| 0 0 1 11 4 12 .02 | 530 459
gfz 149| 0 0 -1 25 13 -4 .07 9 9 | -144 44 11 115
| 0 0 0 7 9 11 .02 | 70 176
grg 127| 1 0 2 -19 7 -21 .07 10 9 | -55 0 7 128
| 0 0 1 9 9 15 .02 | 44 81
igr n/a| 0 0 0 -2 -6 -2 .01 3 3 | 7770 488 8 88
| 0 0 0 7 7 9 .01 | 1032 437
jgx n/a| 0 0 -7 0 -15 1 -.03 7 7 | -46 1 23 79
| 0 0 0 3 6 5 .01 | 65 100
jpl 120| 0 0 1 0 0 21 .00 9 9 | -2835 103 8 87
| 0 0 0 9 7 9 .02 | 655 524
mit 360| 0 0 0 -7 2 -60 .02 8 7 | 7411 1224 33 103
| 0 0 0 18 17 43 .01 | 938 1758
ngs 262| 0 0 3 -8 -1 4 -.07 10 9 | -683 38 501 817
| 0 0 2 7 16 23 .02 | 60 117
sio 365| 0 0 2 -15 -2 6 .02 9 9 | --- --- --- ---
| 0 0 0 9 13 14 .02 | --- ---
Table 1.2380.b GPS week : 2380 MJD: 60904.000-60910.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 5 4 4 4 4 3 3 |
3 | 2 2 2 3 3 2 3 |
4 | --- --- --- 0 4 4 3 |
5 | 2 2 3 3 3 3 3 |
6 | 3 3 3 3 4 4 4 |
7 | 3 3 4 3 4 3 3 |
8 | 2 2 2 2 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 2 2 2 2 2 2 2 |
11 | 4 3 4 3 4 4 4 |
12 | 2 2 2 2 2 2 2 |
13 | 3 3 3 3 3 3 3 |
14 | 3 3 3 3 3 3 2 |
15 | 3 3 3 3 3 3 3 |
16 | 2 2 2 2 2 2 2 |
17 | 2 3 2 2 3 2 2 |
18 | 3 4 4 4 4 4 5 |
19 | 2 2 3 3 2 2 2 |
21 | 3 3 3 3 3 3 3 |
22 | 2 2 2 2 2 2 2 |
23 | 2 3 3 3 3 3 3 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 2 2 3 3 3 2 2 |
27 | 2 2 2 2 3 2 3 |
28 | 3 3 3 3 3 3 4 |
29 | 2 3 2 2 2 2 3 |
30 | 3 3 3 3 3 3 4 |
31 | 3 3 3 3 3 3 3 |
32 | 2 3 2 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2380.0 GPS week: 2380 Day: 0 MJD: 60904.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 802| 0 0 3 9 5 19 .01 8 7 | -613 -106 6 145
emr 109| 0 0 -1 -5 -1 32 .00 7 7 | 31 -130 5 89
esa 188| 0 0 2 15 9 -7 -.07 7 7 | -1388 -273 6 189
gfz 151| 0 1 -1 15 7 -12 .07 8 8 | -211 72 12 121
grg 128| 2 0 3 -25 18 -21 .06 10 9 | -115 4 8 130
igr n/a| 0 0 0 -6 4 -8 .01 2 2 | 6500 -78 8 80
jgx n/a| 0 0 -8 -1 -24 -2 -.04 6 6 | -84 -12 21 77
jpl 120| 0 0 0 0 0 7 -.03 8 8 | -3464 -225 8 92
mit 360| 0 0 -1 0 -21 -5 .02 8 6 | 6433 55 33 74
ngs 267| 0 0 1 -8 9 -12 -.05 9 8 | -614 -108 502 781
sio 366| 0 0 3 -5 8 -12 -.02 9 9 | --- --- --- ---
Table 2.2380.1 GPS week: 2380 Day: 1 MJD: 60905.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 805| 0 0 2 11 2 26 .01 6 6 | -791 228 6 142
emr 104| -1 0 0 -6 -3 30 .02 8 8 | 29995 -60158 6 101
esa 188| 0 0 0 16 0 2 -.07 7 8 | -1685 426 6 182
gfz 152| -1 0 -1 26 4 -3 .07 8 8 | -176 98 11 116
grg 126| 1 0 1 -18 1 -29 .04 9 9 | -119 17 7 135
igr n/a| 0 0 0 -10 -4 -14 .01 3 3 | 6356 838 8 85
jgx n/a| 0 0 -9 0 -7 1 -.03 7 6 | -121 -30 23 76
jpl 120| 0 0 2 3 0 20 -.02 9 9 | -3727 765 10 87
mit 360| 0 0 0 -5 10 -37 .02 7 6 | 6677 192 29 61
ngs 265| 0 0 5 -17 -8 -41 -.06 9 9 | -791 230 535 780
sio 367| 0 0 2 -19 -19 24 .02 9 9 | --- --- --- ---
Table 2.2380.2 GPS week: 2380 Day: 2 MJD: 60906.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 804| 0 0 3 22 -13 25 .00 7 7 | -690 21 6 144
emr 106| 0 1 0 8 -11 30 .03 8 8 | -297 548 6 97
esa 188| 0 0 0 -1 2 25 -.08 7 8 | -902 395 6 177
gfz 150| 0 0 -1 24 22 18 .08 8 8 | -27 -73 12 118
grg 130| 0 0 2 -25 7 -19 .07 10 8 | -57 90 7 126
igr n/a| 0 0 0 0 -7 1 .01 3 2 | 7415 756 8 86
jgx n/a| 0 0 -8 -2 -7 8 -.03 7 7 | -99 105 25 80
jpl 120| 0 0 0 1 3 37 .01 9 9 | -2556 550 9 84
mit 360| 0 0 0 -16 19 -121 .02 7 6 | 7661 263 36 72
ngs 265| 0 0 5 -3 -20 29 -.10 10 9 | -693 25 536 853
sio 368| 0 0 2 -5 -8 21 .02 9 9 | --- --- --- ---
Table 2.2380.3 GPS week: 2380 Day: 3 MJD: 60907.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 799| 0 0 3 18 -4 53 -.03 6 6 | -628 -92 6 128
emr 109| 0 0 -1 3 1 14 .02 7 7 | -268 463 6 95
esa 189| 0 0 -1 -7 2 -9 -.07 8 8 | -517 391 7 182
gfz 147| 0 0 -1 17 26 -9 .09 9 8 | -102 -222 11 119
grg 128| 1 0 4 -18 4 -8 .06 10 9 | -35 -60 8 141
igr n/a| 0 0 1 -8 1 -10 .02 3 3 | 8025 811 9 88
jgx n/a| 0 0 -7 2 -21 -4 -.02 7 7 | -62 150 23 77
jpl 120| 0 0 1 -12 3 15 -.00 9 9 | -2223 69 9 89
mit 360| 0 0 0 2 6 -68 .02 7 6 | 8292 275 35 72
ngs 256| 0 0 1 5 -24 9 -.09 9 9 | -631 -93 480 898
sio 363| 0 -1 2 -27 0 3 .02 11 10 | --- --- --- ---
Table 2.2380.4 GPS week: 2380 Day: 4 MJD: 60908.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 791| 0 0 3 14 -22 0 -.03 6 6 | -721 64 6 142
emr 106| 0 0 0 0 -3 22 .04 7 7 | 299 -551 5 93
esa 188| 0 0 -1 13 0 -5 -.04 8 9 | -530 -601 6 178
gfz 147| 1 0 -1 37 19 -14 .04 10 9 | -211 325 11 112
grg 128| 1 0 5 -3 23 -46 .09 11 9 | -12 67 8 124
igr n/a| 0 0 0 11 -4 6 .00 3 2 | 8737 21 9 86
jgx n/a| 0 0 -8 4 -21 -1 -.04 7 7 | 68 -94 24 82
jpl 120| -1 0 1 9 9 20 .02 9 9 | -1947 -643 9 86
mit 360| 0 0 0 -33 -18 -12 .02 7 6 | 6476 4665 32 285
ngs 256| 0 -1 0 -14 20 17 -.04 10 9 | -728 71 569 816
sio 361| 0 0 3 -25 19 1 .03 9 7 | --- --- --- ---
Table 2.2380.5 GPS week: 2380 Day: 5 MJD: 60909.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 784| 0 0 3 26 1 17 -.04 6 6 | -656 111 6 142
emr 108| 0 0 1 0 -10 25 .05 7 7 | 152 -351 6 103
esa 188| 0 0 0 -3 -6 12 -.03 8 8 | -1321 -311 6 183
gfz 150| 0 0 -3 31 0 1 .03 9 11 | -96 -42 11 104
grg 127| 0 0 2 -13 0 -22 .05 9 8 | -10 28 7 108
igr n/a| 0 0 1 4 -15 11 .01 3 3 | 8722 145 9 101
jgx n/a| 0 0 -7 -3 -16 8 -.04 7 7 | 6 18 25 92
jpl 120| -1 0 0 7 -8 29 .02 9 9 | -2728 -311 8 93
mit 360| 1 -1 0 -21 22 -94 .01 7 7 | 7491 2616 32 69
ngs 265| 0 0 2 -13 7 13 -.06 9 8 | -662 115 445 818
sio 370| 0 -1 2 -14 -11 17 .03 9 9 | --- --- --- ---
Table 2.2380.6 GPS week: 2380 Day: 6 MJD: 60910.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 793| 0 0 2 18 -8 25 -.04 6 6 | -662 27 6 141
emr 107| 0 0 -1 -2 10 22 .02 8 8 | -281 428 5 91
esa 188| 0 -1 0 -11 -1 0 -.06 8 7 | -1836 537 7 197
gfz 149| 0 0 -1 22 15 -10 .09 10 11 | -187 155 10 117
grg 128| 1 0 0 -30 0 1 .09 10 9 | -42 -149 7 134
igr n/a| 0 0 0 -6 -17 0 .02 3 3 | 8636 927 9 94
jgx n/a| 0 0 -7 -5 -11 -1 -.02 7 7 | -36 -130 25 73
jpl 120| -1 0 2 -15 -12 18 .02 9 9 | -3203 522 8 79
mit 360| 0 0 -1 23 -2 -80 .04 10 9 | 8848 503 35 88
ngs 262| 1 0 5 -6 3 13 -.06 11 10 | -667 30 444 777
sio 365| 0 0 2 -8 -6 -9 .01 9 9 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.2380.0 GPS week: 2380 Day: 0 MJD: 60904.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1E | 9 10 10 --- 14 4 --- 16 8 14 7 4 | 21 25 26 --- 28 25 --- 31 26 26 27 25
2E | 25 9 9 18 19 4 10 7 16 18 12 5 | 86 92 91 97 88 91 92 90 84 99 90 89
3 | 5 7 7 7 7 2 4 6 7 7 5 2 | 22 24 23 22 23 22 22 24 23 24 22 22
5 | 6 7 8 6 8 3 5 6 5 8 10 2 | 29 28 26 29 29 28 26 26 30 30 31 27
6E | 8 8 6 9 12 3 7 7 9 11 10 3 | 41 41 39 39 41 40 38 40 41 42 39 39
7 | 8 8 10 11 13 4 7 7 11 8 12 3 | 36 34 29 32 34 32 31 33 35 33 33 32
8 | 5 7 5 5 7 2 6 6 5 7 8 2 | 18 21 20 17 18 18 19 20 18 19 16 18
9 | 7 7 5 7 14 2 5 6 5 9 7 2 | 39 35 36 37 38 36 36 37 38 37 36 36
10 | 4 8 6 8 4 2 6 7 5 8 7 2 | 23 23 24 24 23 23 21 22 22 23 23 22
11E | 9 9 7 12 10 2 7 14 10 14 9 3 | 43 44 46 48 47 44 43 50 43 43 44 44
12 | 6 5 5 6 6 2 7 6 5 6 9 2 | 55 55 56 54 53 55 57 56 52 53 49 54
13 | 10 10 11 7 10 4 7 8 9 8 8 3 | 31 34 25 29 33 28 23 29 28 29 29 28
14 | 4 13 6 8 8 2 7 11 7 7 10 2 | 62 63 61 61 63 62 59 63 63 63 65 61
15 | 8 7 9 9 7 4 8 7 9 8 11 2 | 35 31 26 30 34 29 25 29 33 35 34 30
16 | 4 6 5 7 6 1 4 5 4 7 9 2 | 15 13 15 18 14 14 13 11 16 15 16 14
17 | 6 5 7 7 8 2 4 6 7 7 8 2 | 26 27 24 28 26 25 23 26 28 28 26 25
18E | 7 8 7 8 10 2 6 17 10 15 8 3 | 28 30 29 30 34 29 29 37 30 28 29 29
19 | 7 6 6 7 9 3 5 5 8 8 9 2 | 17 16 15 21 18 17 16 16 20 18 17 16
X21 | 7 7 8 9 10 2 --- 9 10 8 7 3 | 14 15 13 16 21 14 --- 15 17 13 18 14
22 | 6 6 7 8 8 2 5 5 6 7 9 2 | 17 20 20 19 19 18 14 19 22 18 23 18
23 | 6 6 8 7 8 1 6 8 6 10 7 2 | 11 15 11 18 20 14 15 15 18 14 16 14
24 | 7 8 6 6 22 2 8 8 7 6 11 3 | 33 33 33 33 37 32 31 33 32 34 32 32
25 | 5 9 7 6 6 2 7 11 5 10 12 2 | 19 27 24 21 19 20 17 28 20 18 17 20
26 | 4 8 6 6 6 2 6 8 8 9 7 2 | 26 31 29 26 26 26 26 31 27 26 23 26
27 | 6 6 6 7 6 2 5 7 5 8 10 2 | 19 21 22 18 19 19 18 21 18 20 17 19
28 | 10 9 7 8 10 2 8 12 5 11 9 3 | 66 66 68 68 71 67 65 70 71 68 69 68
29 | 6 5 7 7 8 3 6 7 4 8 10 2 | 36 35 33 37 36 34 35 34 36 32 32 34
30 | 8 7 7 9 14 3 5 7 9 8 8 2 | 32 30 28 28 35 29 27 29 30 28 28 28
31 | 6 5 10 10 9 1 5 7 7 10 8 2 | 25 22 18 29 26 23 23 22 23 28 25 23
32 | 6 8 6 5 6 3 6 6 5 9 8 2 | 31 32 32 30 32 31 29 33 32 32 31 31
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 7 7 8 10 2 6 8 8 9 9 |T 31 32 31 33 33 31 31 33 32 32 31 31
WRMS | 7 7 7 8 9 2 6 8 6 8 9 |NE 29 30 28 30 30 28 27 29 30 29 29 28
MEDI | 6 7 7 7 8 2 6 7 7 8 9 |MD 28 30 26 29 29 28 26 29 28 28 28 27
Table 3.2380.1 GPS week: 2380 Day: 1 MJD: 60905.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1E | 8 9 9 --- 12 4 --- 15 6 12 11 3 | 20 21 21 --- 23 21 --- 24 23 22 24 21
2E | 10 9 8 11 8 3 9 15 11 13 15 3 | 76 76 76 81 77 78 79 74 74 79 75 76
3 | 5 6 6 8 6 3 5 6 5 7 11 2 | 26 27 26 27 26 25 26 26 26 30 28 26
5 | 5 7 8 6 9 3 6 7 4 7 8 2 | 26 26 24 26 27 25 25 24 26 26 27 25
6E | 7 9 6 12 13 3 9 7 8 14 8 3 | 22 21 20 18 23 19 19 20 21 20 20 19
7 | 7 8 11 8 15 4 7 9 9 7 9 3 | 37 35 30 36 36 33 32 34 36 36 33 33
8 | 6 6 5 7 6 3 5 7 8 8 6 2 | 19 20 21 19 18 19 19 19 20 21 19 19
9 | 7 7 6 5 13 3 5 6 6 8 7 2 | 36 34 34 37 35 34 33 35 34 36 34 34
10 | 3 8 6 8 7 2 6 7 4 8 8 2 | 19 20 21 18 21 19 18 20 19 22 20 19
11E | 8 10 7 12 12 4 8 13 8 14 8 3 | 29 27 30 32 31 29 28 34 27 27 29 28
12 | 4 6 5 5 4 2 6 6 3 8 10 2 | 46 45 46 45 45 46 45 46 44 46 41 45
13 | 9 8 11 8 9 3 9 7 5 9 8 3 | 23 25 16 21 25 19 16 22 19 24 23 20
14 | 4 13 6 9 7 1 6 12 7 7 8 2 | 52 52 50 51 52 51 50 51 51 54 53 51
15 | 7 7 10 8 8 4 9 6 7 8 9 2 | 34 30 27 31 32 30 27 29 32 35 32 30
16 | 5 7 6 6 5 3 6 7 5 9 7 2 | 17 16 19 20 17 19 18 16 19 21 21 17
17 | 5 8 7 8 8 4 6 6 9 8 11 2 | 24 26 21 25 23 24 23 24 24 27 24 23
18E | 7 8 10 14 10 3 6 18 8 13 13 3 | 20 22 22 22 25 20 21 24 22 24 23 20
19 | 5 6 6 8 8 3 6 5 8 9 9 2 | 20 21 17 20 20 20 19 19 20 22 20 19
X21 | 5 7 8 9 12 3 --- 8 11 9 9 3 | 15 18 15 21 21 15 --- 17 20 16 20 16
22 | 6 6 6 8 8 2 5 5 6 10 8 2 | 18 21 20 20 18 18 17 19 18 23 22 18
23 | 6 8 8 6 7 2 6 8 6 10 8 2 | 12 17 12 16 19 15 16 16 17 16 18 14
24E | 6 9 5 8 7 3 8 9 6 10 8 2 | 44 43 43 42 41 41 39 43 41 47 40 42
25 | 5 9 8 7 6 3 7 12 5 8 12 2 | 21 27 25 20 20 21 19 28 21 21 19 21
26 | 5 7 6 4 5 3 8 7 7 8 6 2 | 17 21 22 19 18 19 19 23 17 20 17 18
27 | 7 7 7 7 5 3 4 6 7 7 10 2 | 21 22 22 20 20 20 20 21 19 21 22 20
28 | 8 8 8 13 11 2 8 14 5 9 13 3 | 38 38 38 36 43 37 36 43 41 37 42 38
29 | 6 6 7 7 7 2 6 7 6 12 8 2 | 23 21 17 21 22 21 20 21 23 22 21 20
30 | 7 8 7 7 16 2 5 8 8 4 6 2 | 29 26 25 24 31 25 23 26 25 27 25 25
31 | 6 6 11 6 8 2 5 7 6 7 9 2 | 25 22 17 25 25 22 22 21 22 25 24 22
32 | 4 10 7 6 6 2 7 6 6 8 11 2 | 32 31 32 30 32 31 30 31 31 33 32 31
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 8 7 8 9 3 7 9 7 9 9 |T 28 28 26 28 28 27 27 28 27 29 28 27
WRMS | 6 8 8 8 9 3 6 9 6 9 9 |NE 25 27 25 26 26 25 24 26 25 28 26 25
MEDI | 6 8 7 8 8 3 6 7 6 8 8 |MD 23 25 22 24 25 21 22 24 23 24 24 21
Table 3.2380.2 GPS week: 2380 Day: 2 MJD: 60906.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1E | 8 8 9 --- 10 3 --- 17 5 15 8 3 | 19 22 22 --- 22 21 --- 26 22 21 23 21
2E | 11 10 6 9 25 4 7 8 12 12 15 4 | 73 66 65 66 76 68 69 66 66 71 64 67
3 | 6 5 6 6 7 2 4 7 6 7 5 2 | 19 19 21 19 19 19 18 20 20 18 20 18
5 | 7 7 8 5 8 3 8 7 6 9 13 2 | 27 26 25 28 27 26 25 26 25 27 30 26
6E | 8 7 6 9 11 3 9 8 9 13 9 3 | 34 32 31 31 32 31 30 32 30 29 32 31
7 | 9 9 12 12 16 4 7 10 8 9 11 3 | 29 28 21 27 31 25 26 27 27 26 26 25
8 | 4 8 6 6 7 2 6 7 6 8 5 2 | 17 19 20 17 17 17 17 19 14 18 17 17
9 | 9 8 6 10 14 3 5 7 5 11 7 2 | 25 24 26 24 29 25 23 24 25 26 23 23
10 | 3 6 7 8 5 2 7 7 4 7 7 2 | 22 22 26 20 24 22 21 24 19 24 23 22
11E | 10 10 7 15 11 3 7 17 12 16 11 4 | 34 33 35 38 35 34 33 41 32 37 35 34
12 | 5 6 6 5 6 1 6 7 3 10 11 2 | 36 37 37 35 34 35 34 38 35 33 32 35
13 | 11 8 10 8 10 3 9 8 6 6 8 2 | 27 28 22 27 27 24 21 26 24 27 29 25
14 | 6 12 7 9 7 2 6 10 7 9 8 2 | 37 36 36 38 39 37 38 37 41 40 40 37
15 | 7 8 10 8 8 3 10 9 8 10 9 3 | 29 27 21 27 29 26 22 25 30 31 32 26
16 | 4 6 6 8 6 2 6 7 6 7 7 2 | 14 13 15 16 13 13 14 11 14 17 16 13
17 | 5 6 8 7 7 2 5 7 7 9 9 2 | 21 23 18 23 20 20 20 22 19 23 21 20
18E | 8 8 9 10 10 3 7 17 10 12 10 3 | 23 25 24 23 28 23 24 29 23 24 24 23
19 | 6 6 6 7 8 2 5 7 7 13 7 2 | 18 18 15 19 16 17 17 18 17 20 18 16
X21 | 7 7 7 9 9 3 --- 9 10 9 9 3 | 11 13 11 17 17 12 --- 15 15 10 19 12
22 | 7 6 7 7 7 2 4 4 6 10 6 2 | 16 21 19 17 17 17 16 20 19 18 21 17
23 | 6 7 8 8 6 2 7 7 5 10 8 2 | 15 20 18 20 23 18 20 20 18 20 21 18
24E | 7 9 6 8 10 3 6 7 5 8 9 2 | 23 25 23 22 28 23 21 24 23 25 25 23
25 | 6 9 8 5 6 2 8 12 5 11 12 2 | 15 25 23 19 16 17 14 26 16 15 17 17
26 | 5 7 6 8 6 3 7 8 8 7 8 2 | 19 23 23 17 19 19 20 25 18 18 17 19
27 | 4 6 6 7 6 2 6 8 6 8 7 2 | 18 20 21 19 18 18 18 20 16 19 17 18
28 | 10 8 8 5 8 3 8 16 6 13 12 3 | 34 36 38 37 40 37 35 42 36 41 39 36
29 | 5 5 7 8 8 3 6 7 5 9 10 2 | 29 26 26 29 28 26 27 27 26 26 26 26
30 | 9 8 7 12 18 3 6 8 6 6 6 3 | 26 24 23 22 30 22 21 23 22 20 23 22
31 | 6 5 10 9 7 2 6 7 5 10 6 2 | 22 20 16 22 23 20 20 19 20 23 22 19
32 | 5 9 6 7 6 3 7 7 5 7 11 2 | 25 26 26 27 25 25 23 26 26 26 26 24
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 8 7 8 10 3 7 9 7 10 9 |T 25 25 24 25 26 24 24 26 24 25 25 24
WRMS | 7 8 8 8 8 2 7 9 6 9 9 |NE 22 24 23 23 23 22 22 24 22 24 23 22
MEDI | 6 7 7 8 8 3 6 7 6 9 8 |MD 23 24 23 23 25 22 21 25 22 24 23 22
Table 3.2380.3 GPS week: 2380 Day: 3 MJD: 60907.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1E | 7 9 8 --- 11 4 --- 14 4 13 6 3 | 22 22 24 --- 23 21 --- 26 22 23 22 22
2E | 7 7 7 11 16 4 8 7 12 14 16 3 | 49 47 46 49 54 48 50 49 44 49 48 47
3 | 7 7 5 6 9 2 6 6 9 7 12 2 | 22 21 22 21 22 20 19 21 23 20 23 20
X4 | 3 --- --- --- --- 1062 --- --- 112 --- --- 0 | 25 --- --- --- --- 550 --- --- 69 --- --- 24
5 | 6 6 9 5 7 3 7 7 6 9 13 2 | 24 24 21 24 23 22 21 22 23 23 24 22
6E | 8 9 7 11 15 4 8 8 9 11 9 3 | 26 25 26 22 25 23 22 26 24 25 21 23
7 | 7 9 12 9 19 4 8 9 7 10 9 3 | 32 30 24 29 34 29 29 29 31 28 28 28
8 | 5 6 6 6 6 2 6 6 6 7 8 2 | 17 20 20 18 19 18 17 20 16 19 16 17
9 | 7 7 7 10 15 2 5 7 5 10 8 2 | 26 21 22 24 29 23 22 25 22 22 21 22
10 | 3 7 7 6 5 2 7 7 3 7 9 2 | 22 23 23 18 21 20 17 22 20 24 20 20
11E | 7 9 7 11 11 3 10 14 7 14 10 3 | 30 28 31 31 28 28 27 36 28 30 29 29
12 | 4 6 5 9 6 2 6 6 3 8 8 2 | 39 42 41 42 36 38 40 42 38 37 37 39
13 | 9 7 11 7 9 2 9 8 7 8 7 2 | 26 26 18 24 25 22 18 23 23 24 22 22
14 | 6 11 5 10 8 2 6 10 8 10 9 2 | 33 27 28 32 33 30 29 30 34 29 32 30
15 | 7 8 11 9 8 2 10 7 7 9 11 3 | 31 28 22 30 31 28 23 26 31 33 32 28
16 | 5 6 6 8 6 2 7 6 4 6 11 2 | 17 15 17 17 16 15 17 14 15 17 18 15
17 | 5 7 6 9 7 2 5 7 6 8 9 2 | 26 24 22 24 25 25 22 25 23 24 22 23
18E | 8 8 9 14 9 4 6 19 17 17 19 4 | 23 24 23 19 26 22 22 28 27 23 26 22
19 | 5 6 6 10 8 3 7 5 8 8 8 2 | 21 18 17 20 20 19 17 19 20 21 19 18
X21 | 9 7 8 8 9 3 --- 9 6 11 9 3 | 13 16 14 16 19 14 --- 16 17 15 19 14
22 | 5 6 5 8 7 2 5 3 7 7 7 2 | 21 21 21 20 20 20 17 22 23 20 21 20
23 | 4 5 8 5 7 2 7 9 7 12 12 2 | 17 19 14 16 21 16 17 18 19 17 21 16
24E | 5 9 6 9 9 2 8 9 4 6 10 2 | 32 32 30 30 35 30 28 32 30 32 29 30
25 | 6 8 7 7 4 3 8 11 4 9 12 2 | 19 27 24 20 17 19 18 28 18 19 18 20
26 | 5 7 6 5 6 2 8 8 6 7 13 2 | 24 25 25 24 21 22 24 28 19 21 20 22
27 | 5 7 5 6 6 3 6 6 6 7 10 2 | 18 20 21 20 19 18 18 20 17 20 19 18
28 | 8 8 9 10 11 2 10 16 6 12 12 3 | 37 37 37 36 45 38 34 43 40 40 43 38
29 | 4 5 6 5 7 3 6 7 5 9 10 2 | 28 28 25 26 27 25 26 27 28 25 26 26
30 | 8 8 7 8 20 3 7 7 7 9 9 3 | 27 23 22 23 33 23 22 23 23 20 22 22
31 | 6 6 11 7 9 1 6 7 6 7 10 2 | 24 23 15 22 24 21 20 21 21 22 24 20
32 | 4 9 8 8 6 2 8 6 4 7 10 2 | 26 27 24 24 26 23 22 25 25 25 27 24
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 7 7 9 10 3 7 9 7 9 11 |T 25 25 23 24 26 40 23 26 26 24 24 23
WRMS | 6 7 8 8 9 3 7 9 6 9 10 |NE 24 23 22 23 24 66 21 24 27 23 23 22
MEDI | 6 7 7 8 8 2 7 7 6 9 10 |MD 25 24 22 24 25 22 22 25 23 23 22 22
Table 3.2380.4 GPS week: 2380 Day: 4 MJD: 60908.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1E | 6 8 8 --- 11 4 --- 15 5 14 6 3 | 18 23 21 --- 22 20 --- 25 22 19 22 20
2E | 4 8 7 11 16 4 8 8 12 15 10 3 | 63 61 61 62 66 63 65 61 61 66 60 62
3 | 6 6 7 5 8 2 7 6 5 7 17 2 | 19 21 20 18 19 18 18 20 22 19 25 19
X4 | 10 6 11 11 13 4 --- 12 7 17 7 3 | 12 18 17 24 18 185 --- 17 31 20 19 14
5 | 7 8 10 7 8 2 8 7 6 9 8 2 | 24 23 23 26 24 23 22 24 24 23 24 23
6E | 8 7 7 23 16 3 10 9 7 12 7 3 | 30 28 30 38 30 28 27 30 29 28 30 29
7 | 7 8 14 11 20 3 7 11 11 6 8 3 | 31 31 25 29 35 28 27 29 32 29 28 28
8 | 5 6 7 7 8 2 8 8 7 9 7 2 | 15 19 21 17 18 16 16 18 17 17 15 16
9 | 9 6 8 9 15 3 6 7 8 7 8 2 | 24 22 22 20 25 23 20 23 26 21 23 21
10 | 5 7 8 9 5 3 7 8 5 8 6 2 | 22 23 25 19 23 21 21 23 21 24 23 21
11E | 8 8 8 9 11 3 9 16 10 19 9 3 | 35 33 36 35 34 33 32 39 32 37 34 33
12 | 5 5 6 6 8 2 6 6 4 9 6 2 | 38 40 43 38 38 40 40 42 42 41 37 40
13 | 10 7 12 6 11 3 9 9 7 5 6 2 | 28 26 22 25 27 23 20 25 25 23 23 23
14 | 5 10 7 7 7 1 7 9 8 7 7 2 | 37 38 36 36 39 38 37 37 42 40 40 37
15 | 6 7 12 7 9 2 8 9 9 8 9 2 | 27 26 21 26 29 24 22 22 27 25 26 24
16 | 5 6 7 10 8 3 6 9 5 7 8 2 | 11 11 14 18 11 11 11 11 14 12 14 11
17 | 5 5 8 7 9 3 6 7 9 7 7 2 | 20 22 17 20 20 19 20 22 23 19 22 19
18E | 8 8 11 15 10 3 7 18 12 14 13 4 | 22 22 21 20 24 19 20 25 20 23 21 19
19 | 6 4 6 7 9 2 6 6 7 9 7 2 | 16 18 14 18 17 16 17 18 19 18 17 16
X21 | 6 7 9 12 7 2 --- 9 9 10 8 3 | 10 14 13 17 17 11 --- 15 16 9 15 12
22 | 5 4 6 7 8 2 5 4 7 6 8 2 | 13 16 16 14 13 14 13 17 19 15 19 15
23 | 5 6 9 7 7 2 7 8 7 14 10 2 | 13 18 15 20 21 15 17 18 19 19 19 16
24E | 5 9 6 11 7 2 7 9 7 9 7 2 | 24 26 25 23 27 25 23 27 26 27 26 24
25 | 5 10 9 7 6 2 8 12 5 10 6 2 | 16 27 25 19 19 19 16 28 18 19 17 19
26 | 6 9 6 7 6 2 7 8 6 7 9 2 | 22 25 25 22 19 20 21 26 19 19 18 21
27 | 6 7 6 8 7 3 6 8 7 9 10 2 | 17 20 22 18 19 18 16 20 18 18 18 17
28 | 7 10 9 8 11 2 9 16 5 12 8 3 | 55 57 58 60 63 56 55 61 57 55 60 57
29 | 5 4 7 6 9 3 5 6 5 9 6 2 | 25 23 22 25 24 23 23 23 24 25 23 23
30 | 9 8 9 9 21 3 7 7 9 9 8 3 | 24 22 21 22 33 22 21 22 23 20 20 21
31 | 5 7 12 8 8 2 5 7 5 11 8 2 | 22 21 15 25 24 20 20 20 21 24 22 20
32 | 6 10 7 14 5 2 8 7 5 9 7 2 | 25 26 28 27 25 25 23 27 27 23 26 25
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 7 8 10 11 3 7 9 7 10 9 |T 24 25 24 26 26 29 24 26 26 25 25 24
WRMS | 6 7 9 9 9 2 7 9 6 9 7 |NE 21 23 22 22 22 35 21 23 25 22 22 21
MEDI | 6 7 8 8 8 2 7 8 7 9 8 |MD 22 23 22 22 24 22 21 23 23 23 23 21
Table 3.2380.5 GPS week: 2380 Day: 5 MJD: 60909.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1E | 6 8 8 --- 9 4 --- 15 4 12 6 3 | 19 22 20 --- 22 19 --- 25 22 20 20 20
2E | 5 9 8 7 11 3 9 7 10 12 12 3 | 66 65 66 64 66 66 68 65 62 67 64 65
3 | 7 7 5 7 7 2 5 6 6 5 9 2 | 19 21 22 19 20 20 19 21 21 18 20 19
X4 | 8 --- 9 11 12 4 --- 10 7 11 7 3 | 13 --- 10 19 19 176 --- 12 26 10 14 14
5 | 8 7 8 7 6 4 7 9 8 8 9 2 | 26 28 25 30 26 27 26 27 29 29 29 26
6E | 8 8 6 22 12 2 9 7 8 10 9 3 | 38 37 38 44 38 37 37 37 40 36 36 37
7 | 7 9 12 9 13 4 7 10 9 9 10 3 | 33 35 30 34 32 32 31 33 36 32 34 32
8 | 6 7 6 7 8 2 6 7 7 11 9 2 | 16 19 20 17 17 16 16 18 16 17 17 16
9 | 6 6 7 6 15 3 6 7 6 7 8 2 | 25 23 25 25 22 24 22 24 24 22 22 22
10 | 5 6 7 7 4 3 6 7 4 6 10 2 | 21 24 24 21 23 21 20 23 23 21 23 22
11E | 8 10 7 15 14 6 10 14 11 14 12 3 | 36 32 35 34 37 33 33 39 35 35 37 34
12 | 5 6 5 6 6 3 7 8 5 11 8 2 | 29 31 31 31 27 30 29 33 30 32 29 30
13 | 10 7 12 8 9 4 9 9 11 9 10 3 | 23 27 19 22 25 22 20 24 25 21 23 22
14 | 5 9 6 5 7 3 7 9 7 7 8 2 | 42 44 41 42 42 41 41 43 43 39 44 41
15 | 7 7 10 9 7 3 8 8 9 9 11 2 | 27 25 21 24 26 24 22 24 25 25 26 24
16 | 4 6 6 9 7 3 7 7 5 6 6 2 | 12 12 15 17 12 12 12 12 13 12 14 12
17 | 5 5 8 7 9 3 6 6 9 6 8 2 | 20 22 16 24 22 20 19 21 20 20 19 19
18E | 8 8 11 14 8 3 7 17 10 15 13 3 | 23 23 22 20 24 20 21 25 24 23 24 21
19 | 5 5 7 7 8 2 6 5 5 6 6 2 | 18 17 15 19 17 17 17 17 18 19 18 16
X21 | 11 7 7 9 7 4 --- 9 7 11 8 3 | 17 13 11 17 18 13 --- 15 16 13 19 13
22 | 3 6 7 7 6 3 5 5 8 6 7 2 | 14 19 17 17 15 16 15 18 18 17 18 16
23 | 6 8 9 9 7 3 6 8 8 14 11 2 | 18 21 17 24 23 19 20 20 25 20 24 20
24E | 7 8 6 9 7 3 8 8 5 10 9 2 | 24 22 22 20 23 22 20 24 23 26 24 22
25M | 5 9 7 9 7 4 8 12 4 9 11 2 | 18 28 25 20 18 19 15 29 19 20 19 20
26 | 4 6 6 6 6 3 7 9 7 5 7 2 | 23 28 26 24 21 22 22 28 24 21 22 23
27 | 6 8 6 6 8 2 5 8 6 7 9 2 | 17 21 21 19 19 18 16 21 17 19 18 18
28E | 9 8 8 11 8 2 10 15 6 11 12 3 | 71 72 73 73 75 72 69 75 75 73 77 73
29 | 5 6 6 8 8 3 6 8 5 7 8 2 | 25 24 23 27 26 24 24 25 26 25 26 24
30 | 9 10 7 13 11 3 6 7 6 7 9 2 | 26 26 25 26 25 25 25 24 28 22 26 24
31 | 6 5 11 9 11 3 6 8 5 8 9 2 | 24 22 15 27 22 22 20 20 22 23 24 21
32 | 6 8 6 7 5 3 8 7 5 7 11 2 | 23 25 24 24 24 23 20 25 22 21 21 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 7 8 9 9 3 7 9 7 9 9 |T 26 27 25 27 26 30 25 27 27 25 26 25
WRMS | 6 7 8 11 8 3 7 9 7 8 9 |NE 21 24 21 23 22 35 21 22 24 21 22 21
MEDI | 6 7 7 8 8 3 7 8 7 9 9 |MD 23 24 22 24 23 22 20 24 24 21 23 22
Table 3.2380.6 GPS week: 2380 Day: 6 MJD: 60910.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1E | 7 8 8 --- 10 4 --- 14 4 14 7 3 | 20 25 25 --- 26 24 --- 30 24 22 27 24
2E | 4 7 7 10 9 3 7 6 11 13 10 2 | 94 97 95 94 98 96 97 96 91 98 91 95
3M | 11 8 6 9 8 2 8 7 8 7 7 2 | 22 20 21 21 20 19 16 21 19 19 18 18
4 | 7 7 10 8 12 4 6 10 8 11 7 2 | 20 17 15 20 17 148 11 17 27 12 18 20
5M | 7 7 7 8 8 4 8 8 7 13 11 2 | 28 29 24 30 29 26 27 26 28 25 30 26
6E | 8 8 6 22 13 6 11 9 10 7 7 3 | 42 44 42 48 42 42 40 42 42 40 43 42
7E | 6 8 13 11 8 4 7 10 16 8 9 3 | 56 57 55 56 55 56 54 57 53 55 53 54
8M | 4 7 7 7 7 2 6 5 7 10 13 2 | 15 18 20 17 15 16 16 18 15 17 17 16
9 | 7 7 8 7 16 3 6 6 8 8 7 2 | 32 31 31 30 27 30 29 31 32 29 31 29
10 | 4 6 6 6 5 3 6 7 5 9 10 2 | 21 23 23 20 21 21 18 21 22 21 22 20
11E | 7 11 5 13 12 4 10 13 12 19 11 3 | 39 34 37 36 38 36 34 41 37 36 39 36
12 | 5 5 5 7 6 3 6 5 7 7 7 2 | 48 52 52 52 47 50 51 53 49 49 46 50
13 | 8 8 10 8 9 4 7 8 13 13 8 3 | 28 28 21 26 24 24 21 27 27 24 25 23
14 | 5 8 6 9 8 2 6 8 8 6 7 2 | 57 59 56 56 55 57 56 58 60 57 58 57
15M | 7 8 8 9 9 3 8 7 10 10 10 3 | 35 31 26 32 34 31 27 29 31 33 34 31
16 | 4 7 6 9 7 3 5 6 5 11 7 2 | 11 9 15 18 11 12 12 12 13 15 15 11
17 | 4 6 8 8 7 2 4 7 8 8 6 2 | 25 26 23 25 23 24 23 26 26 22 24 24
18E | 8 9 9 16 11 6 6 19 10 26 18 4 | 22 23 23 21 26 22 22 29 22 28 23 21
19 | 5 5 7 7 7 3 5 5 6 8 7 2 | 18 18 18 21 17 18 17 18 20 21 19 17
X21M | 11 6 7 10 9 3 --- 8 7 10 8 3 | 37 38 37 40 39 38 --- 38 39 39 40 37
22 | 4 6 7 9 8 3 5 4 10 8 7 2 | 16 19 18 17 15 17 16 19 21 19 20 17
23 | 5 7 8 8 7 3 7 8 8 13 13 2 | 16 18 14 20 22 17 19 18 23 17 24 18
24E | 7 8 5 10 8 3 10 10 6 10 7 2 | 26 27 26 25 29 26 26 28 26 29 26 26
25 | 7 9 7 7 8 3 9 12 9 11 11 3 | 20 29 26 21 18 21 19 31 21 19 20 22
26 | 4 7 7 7 6 2 7 6 7 8 8 2 | 27 29 30 27 26 27 27 31 26 24 25 27
27M | 4 9 6 8 8 3 6 5 10 10 9 2 | 23 24 25 24 21 21 21 24 22 22 21 22
28E | 10 9 8 9 12 2 8 17 8 11 8 3 | 61 63 65 68 64 64 63 68 66 66 66 64
29M | 6 6 7 7 8 3 6 5 11 11 10 2 | 33 31 28 34 32 30 31 32 35 28 32 31
30E | 8 10 10 22 11 4 8 10 24 9 9 4 | 33 32 32 35 33 32 30 33 34 31 31 31
31M | 6 4 10 9 22 2 5 6 5 8 5 3 | 25 22 19 27 26 23 21 23 26 28 26 23
32M | 6 8 7 9 5 3 8 7 11 10 10 2 | 29 30 30 28 28 28 24 31 29 30 30 28
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 8 8 10 10 3 7 9 10 11 9 |T 31 32 31 32 31 35 29 33 32 31 32 30
WRMS | 6 8 7 11 9 3 7 9 9 10 9 |NE 26 27 26 27 25 37 25 27 28 25 27 26
MEDI | 6 7 7 9 8 3 7 7 8 10 8 |MD 27 29 26 27 26 26 24 29 27 28 26 26
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2380 GPS week: 2380 MJD: 60904.0-60910.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2925 |U 12 11 27 |U 7 16 33 |U 9 10 37 |
emr | emr 2907 |U 13 16 30 |U 10 17 37 | 11 18 45 |
esa | esa 2921 | 10 12 28 | 9 16 32 | 10 10 33 |
gfz | gfz 2824 | 13 14 30 |U 8 16 30 | 10 12 29 |
grg | grg 2920 |U 14 13 37 |U 9 17 37 | 9 10 32 |
igr | igr 2893 | 11 11 27 | 8 16 31 | 8 11 33 |
igs | igs 2921 | 11 12 26 | 8 16 31 | 8 11 32 |
jgx | jgx 2701 |U 13 11 25 |U 8 17 33 | 11 10 34 |
jpl | jpl 2921 | 12 15 34 | 10 18 38 | 12 18 48 |
mit | mit 2934 |U 12 11 31 |U 8 16 36 |U 9 10 33 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.2380.0 GPS week: 2380 Day: 0 MJD: 60904.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 12 10 33 | 7 17 31 | 11 12 44 |
emr | emr 2880 | 12 15 34 | 9 19 29 | 10 22 50 |
esa | esa 2880 | 10 12 31 | 7 15 26 | 10 12 40 |
gfz | gfz 2784 | 11 12 33 | 6 15 24 | 12 14 36 |
grg | grg 2880 | 13 14 43 | 7 19 30 | 11 14 37 |
igr | igr 2880 | 11 11 33 | 6 17 24 | 9 14 39 |
igs | igs 2880 | 11 11 32 | 6 16 25 | 9 14 39 |
jgx | jgx 2688 | 11 10 29 | 6 18 25 | 12 12 39 |
jpl | jpl 2880 | 13 14 44 | 9 16 29 | 11 22 55 |
mit | mit 2880 | 13 11 37 | 5 17 28 | 10 14 42 |
Table 5.2380.1 GPS week: 2380 Day: 1 MJD: 60905.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 11 8 30 | 11 22 36 | 7 8 35 |
emr | emr 2880 | 12 14 29 | 17 23 57 | 11 17 43 |
esa | esa 2880 | 10 11 26 | 16 21 56 | 9 7 29 |
gfz | gfz 2784 | 11 10 26 | 14 25 39 | 9 10 29 |
grg | grg 2880 | 14 10 33 | 18 25 56 | 9 7 28 |
igr | igr 2880 | 11 9 24 | 17 23 48 | 7 9 31 |
igs | igs 2880 | 11 9 24 | 16 22 51 | 7 8 30 |
jgx | jgx 2688 | 12 8 23 | 17 27 44 | 10 8 33 |
jpl | jpl 2880 | 13 14 35 | 16 20 58 | 11 17 47 |
mit | mit 2880 | 12 8 27 | 15 21 53 | 8 8 30 |
Table 5.2380.2 GPS week: 2380 Day: 2 MJD: 60906.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 11 9 27 | 6 15 36 | 9 11 34 |
emr | emr 2880 | 13 16 28 | 8 19 37 | 11 15 41 |
esa | esa 2880 | 9 13 28 | 7 15 30 | 10 9 31 |
gfz | gfz 2781 | 13 14 28 | 7 14 35 | 8 13 24 |
grg | grg 2879 | 14 13 41 | 7 17 37 | 8 11 31 |
igr | igr 2880 | 10 11 27 | 6 15 32 | 8 10 30 |
igs | igs 2880 | 10 12 27 | 6 16 31 | 8 10 29 |
jgx | jgx 2688 | 13 11 24 | 7 16 36 | 11 11 29 |
jpl | jpl 2880 | 11 17 37 | 8 22 40 | 13 17 43 |
mit | mit 2880 | 11 12 35 | 6 14 33 | 8 8 28 |
Table 5.2380.3 GPS week: 2380 Day: 3 MJD: 60907.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2912 | 13 11 26 | 7 13 36 | ---- ---- ---- |
emr | emr 2880 | 14 16 29 | 9 17 33 | ---- ---- ---- |
esa | esa 2880 | 10 11 28 | 8 16 29 | ---- ---- ---- |
gfz | gfz 2784 | 11 12 28 | 9 15 34 | ---- ---- ---- |
grg | grg 2880 | 14 13 34 | 7 18 38 | ---- ---- ---- |
igr | igr 2880 | 12 11 26 | 7 16 33 | ---- ---- ---- |
igs | igs 2880 | 12 11 25 | 7 15 30 | ---- ---- ---- |
jgx | jgx 2688 | 14 11 25 | 8 15 36 | ---- ---- ---- |
jpl | jpl 2880 | 13 13 35 | 9 20 36 | ---- ---- ---- |
mit | mit 2976 | 13 10 31 | ---- ---- ---- | ---- ---- ---- |
Table 5.2380.4 GPS week: 2380 Day: 4 MJD: 60908.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 14 13 24 | 7 14 32 | ---- ---- ---- |
emr | emr 2976 | 12 19 27 | 8 12 34 | ---- ---- ---- |
esa | esa 2976 | 9 13 25 | 7 14 26 | ---- ---- ---- |
gfz | gfz 2880 | 14 15 26 | 8 13 30 | ---- ---- ---- |
grg | grg 2976 | 16 16 38 | 7 15 37 | ---- ---- ---- |
igr | igr 2880 | 13 14 26 | 6 14 28 | ---- ---- ---- |
igs | igs 2976 | 11 15 22 | 6 13 28 | ---- ---- ---- |
jgx | jgx 2688 | 16 13 25 | 6 15 33 | ---- ---- ---- |
jpl | jpl 2976 | 12 18 27 | 9 16 34 | ---- ---- ---- |
mit | mit 2976 | 13 13 27 | 7 14 34 | ---- ---- ---- |
Table 5.2380.5 GPS week: 2380 Day: 5 MJD: 60909.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 10 14 28 | 6 15 22 | ---- ---- ---- |
emr | emr 2880 | 13 17 35 | 9 15 28 | ---- ---- ---- |
esa | esa 2976 | 9 12 29 | 8 16 26 | ---- ---- ---- |
gfz | gfz 2879 | 19 21 36 | 8 14 22 | ---- ---- ---- |
grg | grg 2974 | 12 14 35 | 7 13 26 | ---- ---- ---- |
igr | igr 2880 | 10 11 33 | 6 14 22 | ---- ---- ---- |
igs | igs 2975 | 10 13 27 | 7 15 20 | ---- ---- ---- |
jgx | jgx 2688 | 12 12 28 | 6 14 23 | ---- ---- ---- |
jpl | jpl 2976 | 10 15 33 | 10 17 30 | ---- ---- ---- |
mit | mit 2976 | 11 14 34 | 7 14 28 | ---- ---- ---- |
Table 5.2380.6 GPS week: 2380 Day: 6 MJD: 60910.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 12 9 21 | 7 13 37 | ---- ---- ---- |
emr | emr 2976 | 14 16 30 | 9 12 43 | ---- ---- ---- |
esa | esa 2975 | 11 10 28 | 7 13 34 | ---- ---- ---- |
gfz | gfz 2880 | 13 13 31 | 8 14 30 | ---- ---- ---- |
grg | grg 2975 | 15 12 32 | 8 15 38 | ---- ---- ---- |
igr | igr 2976 | 12 10 22 | 6 13 33 | ---- ---- ---- |
igs | igs 2976 | 12 11 22 | 7 13 33 | ---- ---- ---- |
jgx | jgx 2784 | 14 10 22 | 6 13 35 | ---- ---- ---- |
jpl | jpl 2976 | 13 12 31 | 9 15 39 | ---- ---- ---- |
mit | mit 2976 | 14 10 27 | 7 13 40 | ---- ---- ---- |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.2380 GPS week: 2380 MJD: 60904.500-60910.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 -14 -1 16 -5 | 0 16
| 9 5 46 50 4 | 3
emr uuuuu | -18 1 19 -54 3 | -15 22
| 13 11 27 24 9 | 1
esa uuuuu | 2 -2 9 42 0 | -2 16
| 6 11 29 26 5 | 3
gfz uuuuu | -14 -30 -9 97 4 | 2 18
| 13 13 59 88 6 | 3
grg uuuuu | -11 20 -23 -54 -2 | 6 16
| 6 5 36 78 4 | 2
igr xxxxx | 5 4 4 13 -2 | 2 17
| 9 5 26 29 3 | 3
irf xxxxx | 1 -1 10 -7 2 | 0 16
| 3 5 9 10 3 | 2
jgx uuuuu | 25 6 -22 50 1 | 4 16
| 10 5 22 18 2 | 2
jpl uuuuu | -1 -7 50 -7 0 | 0 15
| 7 10 28 27 5 | 2
mit uuuuu | 0 8 21 -115 5 | 21 26
| 14 16 32 22 3 | 1
ngs uuuuu | -3 25 -59 60 -1 | 11 18
| 27 24 49 66 4 | 2
sio xxxxx | 29 33 -63 -10 11 | 26 31
| 54 40 71 43 7 | 2
Table 7.2380.0 GPS week: 2380 Day: 0 MJD: 60904.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 5 -13 -20 58 1 | 1 15
emr uuuuu | -16 15 13 -98 0 | -16 22
esa uuuuu | -6 -14 8 50 -3 | -1 15
gfz uuuuu | -11 -16 -63 -13 -1 | 3 19
grg uuuuu | -20 24 27 -75 4 | 6 15
igr xxxxx | -4 11 -2 -2 -1 | 4 17
irf xxxxx | 3 0 0 -11 -1 | 1 15
jgx uuuuu | 30 9 -6 69 3 | 4 15
jpl uuuuu | -12 -12 87 -60 -9 | 1 15
mit uuuuu | 25 -14 -9 -101 0 | 21 26
ngs uuuuu | -27 42 -27 182 5 | 11 18
sio xxxxx | 36 -14 -92 -44 1 | 24 29
Table 7.2380.1 GPS week: 2380 Day: 1 MJD: 60905.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 0 -6 40 -31 -2 | 4 15
emr uuuuu | -8 7 -11 -52 3 | -13 20
esa uuuuu | 0 -12 12 17 -6 | 3 13
gfz uuuuu | -9 -33 5 50 -2 | 6 19
grg uuuuu | -5 23 -34 34 1 | 10 17
igr xxxxx | -3 8 13 -25 -8 | 7 17
irf xxxxx | -1 -5 11 -22 -3 | 4 15
jgx uuuuu | 10 5 -23 53 2 | 8 16
jpl uuuuu | 1 2 90 -22 3 | 3 14
mit uuuuu | 2 -8 -11 -86 2 | 24 28
ngs uuuuu | 9 38 -83 92 4 | 15 20
sio xxxxx | 59 27 -122 -60 5 | 28 31
Table 7.2380.2 GPS week: 2380 Day: 2 MJD: 60906.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 16 -18 5 58 -3 | 1 16
emr uuuuu | -3 -8 26 -64 12 | -16 23
esa uuuuu | -4 -1 28 18 -7 | -2 15
gfz uuuuu | -32 -16 -54 44 0 | 2 19
grg uuuuu | -7 21 -5 10 -4 | 6 16
igr xxxxx | 3 3 24 3 -5 | 2 17
irf xxxxx | 1 -6 16 -12 1 | 0 16
jgx uuuuu | 12 12 -2 52 -2 | 4 15
jpl uuuuu | 5 1 16 20 7 | -1 14
mit uuuuu | -1 6 9 -100 8 | 20 25
ngs uuuuu | 8 3 -47 -15 -3 | 11 17
sio xxxxx | 78 7 -66 -24 10 | 25 29
Table 7.2380.3 GPS week: 2380 Day: 3 MJD: 60907.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 2 -14 -87 19 -8 | 0 17
emr uuuuu | -21 -8 43 -38 15 | -16 22
esa uuuuu | 1 4 33 34 -2 | -3 16
gfz uuuuu | -26 -20 -15 54 1 | 2 19
grg uuuuu | -10 15 -18 -4 -1 | 5 16
igr xxxxx | 3 4 30 59 1 | 1 18
irf xxxxx | 4 7 16 -1 2 | -1 16
jgx uuuuu | 33 -2 4 51 0 | 4 16
jpl uuuuu | -7 6 38 8 1 | -1 14
mit uuuuu | -11 34 43 -117 5 | 20 25
ngs uuuuu | 47 -21 -34 33 -4 | 11 17
sio xxxxx | -2 113 -12 -14 11 | 26 30
Table 7.2380.4 GPS week: 2380 Day: 4 MJD: 60908.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 26 -8 55 -43 -10 | 0 17
emr uuuuu | -25 14 -14 -29 -4 | -13 23
esa uuuuu | 4 -8 30 42 3 | -3 16
gfz uuuuu | -22 -53 -14 126 9 | 1 18
grg uuuuu | -7 11 -36 -27 -2 | 6 17
igr xxxxx | 5 -3 -48 35 -2 | 1 18
irf xxxxx | -1 -8 12 -13 3 | -1 16
jgx uuuuu | 38 6 -53 73 1 | 5 16
jpl uuuuu | -1 -9 33 3 2 | 1 15
mit uuuuu | -16 7 22 -128 6 | 21 26
ngs uuuuu | -12 38 -61 46 -3 | 11 18
sio xxxxx | -37 15 -174 37 17 | 27 31
Table 7.2380.5 GPS week: 2380 Day: 5 MJD: 60909.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 4 -18 2 79 -8 | -1 17
emr uuuuu | -12 -2 14 -35 8 | -14 23
esa uuuuu | 6 0 4 38 5 | -3 16
gfz uuuuu | -8 -33 -33 180 5 | 1 18
grg uuuuu | -19 21 -88 -156 -6 | 6 16
igr xxxxx | 11 -1 0 -6 1 | 0 18
irf xxxxx | 5 -2 18 4 4 | -1 16
jgx uuuuu | 27 11 -46 32 1 | 4 16
jpl uuuuu | 5 -19 38 -10 -1 | 1 15
mit uuuuu | 8 13 80 -121 6 | 22 27
ngs uuuuu | -25 29 -4 0 -3 | 11 18
sio xxxxx | 101 33 3 -27 21 | 28 33
Table 7.2380.6 GPS week: 2380 Day: 6 MJD: 60910.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 -20 -5 -29 -2 | -6 16
emr uuuuu | -43 -13 60 -63 -12 | -15 24
esa uuuuu | 14 17 -51 93 6 | -6 16
gfz uuuuu | 8 -38 114 236 14 | -2 16
grg uuuuu | -10 27 -7 -159 -6 | 3 15
igr xxxxx | 22 8 10 30 1 | -3 16
irf xxxxx | 0 5 -6 5 6 | -4 16
jgx uuuuu | 29 3 -25 23 1 | 2 15
jpl uuuuu | 5 -15 48 13 -4 | -1 15
mit uuuuu | -3 17 10 -154 6 | 19 24
ngs uuuuu | -23 44 -154 81 -4 | 8 16
sio xxxxx | -28 47 20 59 11 | 28 33
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