[IGSREPORT-30785] Wk 2402 IGS Final Orbits
acc
acc at igs.org
Fri Feb 6 01:01:32 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2402 (Jan 18, 2026 - Jan 24, 2026)
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_20260180000_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 | ZIM2 MATE ZIM2
0 | EMR | DAV1 IQAL NRMD BSHM DAV1 NRMD SYOG
0 | ESA | BOGT NYA2
0 | GFZ | 21 21 AJAC ALGO ARHT ASCG BRAZ CCJ2 CHPI CHUR CKIS
0 | GFZ | COCO CPVG CRO1 CZTG DAEJ DAV1 DGAR DJIG DUMG FAIR
0 | GFZ | FALK GAMB GMSD GODE GUAM HOB2 HOFN HRAO IISC INVK
0 | GFZ | IRKJ ISPA JOG2 KAT1 KERG KIRI KOKB LAUT LPGS MAC1
0 | GFZ | MAJU MATE MAW1 MBAR MIZU MKEA NIUM NKLG NLIB NRC1
0 | GFZ | NRMD NYA2 ONSA OUS2 PDEL PGEN PIE1 POHN REUN SANT
0 | GFZ | SCOR SGOC SGPO STHL STJO SUTH SYOG TASH THU2 TONG
0 | GFZ | TOW2 TUVA TWTF UNSA VOIM WARK WHIT WTZR WUH2 YELL
0 | GFZ | ZAMB ZECK NYA2 ONSA POHN
0 | GRG | CKSV HOLB MCM4
0 | JPL | 18 BADG HKSL HOLB BADG CHTI HKSL HOLB THU2
0 | MIT | ABMF HRAO IRKJ KOUR MCM4 MEDI STJO TLSE TRO1 VACS
0 | MIT | ABMF HRAO IRKJ KOUR MCM4 MEDI STJO TLSE TRO1 VACS
1 | COD | ABMF ALIC AREQ BADG BREW BRST BRUX BSHM BUCU CAS1
1 | COD | CHPI CKIS CKSV CMUM COCO CPVG CRO1 CUSV DAEJ DARW
1 | COD | DGAR DUBO DUMG DYNG FAA1 FLIN GAMB GANP GRAC GUAM
1 | COD | HOFN HOLB HRAO IQAL IRKJ KERG KIRU KITG KOUG KOUR
1 | COD | KRGG LMMF LPGS MAC1 MAJU MAL2 MAS1 MATE MAW1 MCM4
1 | COD | MELI METG MGUE MOBS NANO NICO NKLG PARC PERT PIE1
1 | COD | POL2 RESO REUN REYK RIGA SALU SCOR SFER SSIA STJ3
1 | COD | STK2 SUTM TASH THU2 TID1 TLSE TOW2 TRO1 ULAB VILL
1 | COD | VNDP XMIS YAR2 ZIM2 CKSV MATE
1 | EMR | AJAC REUN THU2
1 | ESA | BAKE CMUM CPVG QAQ1 SCOR BAKE CHUR CMUM CPVG DAEJ
1 | ESA | FAIR FLIN NRMD UNSA
1 | GFZ | 21 21 KIT3 ONSA POHN THU2 KIT3 NRMD POHN
1 | GRG | DAEJ DAEJ IRKJ NRMD
1 | JPL | BADG BADG CAS1 CHTI CMUM DAEJ NRMD THU2
1 | MIT | DARW FLRS GANP IRKJ KITG PARC PRDS SVTL VACS YARR
1 | MIT | ZECK DARW FLRS GANP IRKJ KITG PARC PRDS SVTL VACS
1 | MIT | YARR ZECK
2 | COD | ABMF BRST CCJ2 DARW HRAO IRKJ MATE NRMD PARC PDEL
2 | COD | STK2 TASH YELL SALU WHIT
2 | EMR | HRAO MCM4 HRAO MAR6 MCM4 NRMD PDEL SCOR THU2
2 | ESA | 32 AJAC ALGO ALIC AREG ARHT ASCG BADG BAKE BOAV BOGT
2 | ESA | BRAZ BRST BSHM BUCU CAS1 CCJ2 CEDU CHPI CHUR CKIS
2 | ESA | CKSV CMUM COCO CPVG CRO1 CUSV CZTG DAEJ DARW DAV1
2 | ESA | DGAR DJIG DRAO DUBO DYNG FAA1 FAIR FALK FLIN GAMB
2 | ESA | GANP GMSD GODN GRAC GUAM HERS HKSL HOB2 HOFN HOLB
2 | ESA | HRAO IISC ISPA JOG2 KAT1 KIRI KIRU KITG KOUR KRGG
2 | ESA | LAUT LCK4 LMMF LPAL LPGS MAC1 MAJU MAL2 MAR6 MAS1
2 | ESA | MATE MAW1 MBAR MDO1 MELI METG MGUE MIZU MKEA MOBS
2 | ESA | NANO NAUR NICO NIUM NKLG NLIB NNOR NRMD NTUS NYA2
2 | ESA | PARC PERT PGEN PIE1 PNGM POAL POHN POL2 POVE QAQ1
2 | ESA | RESO REUN RIGA RIO2 SALU SANT SCOR SGOC SGPO SHLG
2 | ESA | SOLO STHL STJ3 STK2 SYOG TASH THU2 TID1 TONG TOW2
2 | ESA | TUVA ULAB UNSA URUM VILL VNDP VOIM WARK WHIT WIND
2 | ESA | WTZR XMIS YEL2 YKRO ZIM2 BAKE BSHM CMUM CPVG DUBO
2 | ESA | FAIR JOG2 KIRU MAC1 MAW1 QAQ1 RESO TASH YEL2
2 | GFZ | 6 21 21 NRMD ONSA PDEL POHN TASH BHR4 IRKJ MATE ONSA
2 | GFZ | PDEL POHN QAQ1 TASH
2 | GRG | 6 6 FAIR BHR4 CCJ2 DUBO FAIR FLIN NRMD TASH YELL
2 | JGX | CCJ2
2 | JPL | BADG BADG CCJ2 CHTI CUSV GLPS NRMD NYAL SALU SYOG
2 | MIT | KRGG STJO SVTL TLSE KRGG MEDI MQZG STJO SVTL TLSE
2 | MIT | VACS WGTN WILL
3 | COD | BADG BRST CRO1 DAV1 DUBO FAA1 FAIR MAC1 MAW1 MCM4
3 | COD | MOBS NICO NRMD PARC SFER TASH VNDP WTZR CRO1 WTZR
3 | EMR | MAW1 FAIR MAC1 MAW1 WHIT
3 | ESA | 32 AJAC ALGO ALIC ARHT ASCG BADG BAKE BJFS BOGT BRAZ
3 | ESA | BRST BSHM CAS1 CCJ2 CEDU CHPI CHUR CKIS CMUM COCO
3 | ESA | CPVG CRO1 CUSV CZTG DAEJ DAV1 DGAR DJIG DRAO DYNG
3 | ESA | FAA1 FAIR FALK FLIN GAMB GANP GMSD GODN GUAM HERS
3 | ESA | HKSL HOB2 HOFN HOLB HRAO IISC IQAL ISPA JOG2 KAT1
3 | ESA | KIRI KIRU KOKB KOUR LAUT LPGS MAC1 MAJU MAL2 MAR6
3 | ESA | MAS1 MATE MAW1 MBAR MDO1 METG MIZU MKEA MOBS NAUR
3 | ESA | NICO NIUM NKLG NLIB NRMD NTUS NYA2 PERT PIE1 PNGM
3 | ESA | POAL POHN POL2 POVE PRDS QAQ1 QUIN REUN RIGA RIO2
3 | ESA | SALU SANT SCOR SGOC SGPO SHLG SOLO STHL STJ3 STK2
3 | ESA | SYOG TASH THU2 TID1 TONG TOW2 TUVA UNSA URUM VNDP
3 | ESA | VOIM WARK WHIT WIND WTZR XMIS YEL2 YKRO ZAMB ZECK
3 | ESA | ZIM2 BAKE CHUR CRO1 CUSV FAIR FLIN IQAL KIRU MAW1
3 | ESA | QAQ1 WHIT YEL2
3 | GFZ | 21 22 21 22 NRMD ONSA POHN CMUM POHN
3 | GRG | DAV1 DAV1 DUBO FAA1 TASH YELL
3 | JGX | BADG
3 | JPL | BADG CHTI FAIR GLPS MAC1
3 | MIT | IQAL IRKJ MCM4 PARC STJO TLSE TRO1 IQAL IRKJ MCM4
3 | MIT | MEDI PARC STJO TLSE TRO1 VACS YARR
4 | COD | CMUM DAV1 MATE
4 | EMR | CHTI DAV1 NRMD DAV1 FAA1 FAIR MOBS NRMD
4 | ESA | CPVG NNOR SCOR BOGT CPVG FLRS IQAL KOUR NNOR NRMD
4 | ESA | SCOR
4 | GFZ | 21 21 ACRG AJAC ALGO AREQ ARHT ASCG BADG BAKE BHR4
4 | GFZ | BRAZ BSHM CCJ2 CHAN CHPI CHTI CHUR CKIS COCO CPVG
4 | GFZ | CRO1 CZTG DAEJ DAV1 DGAR DJIG DRAO DUMG FAIR FALK
4 | GFZ | GAMB GMSD GODE GUAM HERS HOB2 HOFN HRAO IISC INVK
4 | GFZ | IRKJ ISPA JOG2 KAT1 KERG KIRI KOKB LAUT LPGS MAC1
4 | GFZ | MAJU MATE MAW1 MBAR MIZU MKEA MONP NIUM NKLG NLIB
4 | GFZ | NRC1 NRMD NYA2 ONSA OUS2 PIE1 POHN POL2 POVE REUN
4 | GFZ | RIO2 SANT SCOR SGOC SGPO STHL STJO SUTH SYOG TASH
4 | GFZ | THU2 TONG TOW2 TUVA TWTF UNSA VOIM WARK WHIT WSRT
4 | GFZ | WTZR WUH2 YELL ZAMB ZECK CZTG ONSA POHN
4 | GRG | CHTI DAV1 GRAC NRMD DAV1 NRMD
4 | JPL | 1 4 11 18 CHTI HOLB HKSL HOLB MONP NRMD
4 | MIT | BADG MEDI PARC SCTB SFER STJO TLSE VACS YARR ZECK
4 | MIT | BADG MEDI PARC SCTB SFER STJO TLSE VACS YARR ZECK
5 | COD | ABMF ASCG BELE CASC CMUM CZTG DARW FAIR GAMB LMMF
5 | COD | MAC1 MATE NRMD PDEL STK2 TLSE TRO1 YELL ZIM2 BELE
5 | COD | CZTG MATE NICO TASH
5 | EMR | HOFN MAC1 NRMD CAS1 FAIR MAC1 RIGA TRO1 UNSA WHIT
5 | ESA | BOGT CHUR CPVG CUSV FAIR MAW1 NRMD WHIT YEL2 BAKE
5 | ESA | BOGT CHUR CPVG CUSV FAIR NRMD POVE UNSA WHIT YEL2
5 | GFZ | 21 21 ONSA POHN POVE GLPS GMSD ONSA POHN POVE TASH
5 | GRG | TRO1 YAR2 CAS1 GLPS YELL
5 | JPL | CHTI CHTI FAIR GLPS HKSL NRMD THU2 TRO1
5 | MIT | BAKE DARW IRKJ MEDI PARC SFER VACS BAKE DARW GANP
5 | MIT | MEDI PARC SFER VACS
6 | COD | BUCU FLRS ZAMB BUCU CMUM CUSV CZTG FLRS ZAMB
6 | EMR | BRST CAS1 CHTI DAV1 FAIR RIGA BRST CAS1 DAV1 FAIR
6 | EMR | NRMD RIGA SCH2 YEL2
6 | ESA | CHUR CPVG CUSV SCOR CHUR CPVG CUSV NRMD RIO2 SYOG
6 | GFZ | 21 22 21 22 AJAC ALGO ASCG BAKE BRAZ CCJ2 CHPI CHTI
6 | GFZ | CHUR CKIS CMUM COCO CRO1 CZTG DAEJ DGAR DJIG DRAO
6 | GFZ | DUMG FAIR FALK GAMB GMSD GODE GUAM HOB2 HOFN HRAO
6 | GFZ | IISC INVK IRKJ ISPA JOG2 KAT1 KERG KIRI KOKB LAUT
6 | GFZ | LPGS MAC1 MAJU MATE MAW1 MBAR MIZU MKEA NIUM NKLG
6 | GFZ | NRMD NYA2 ONSA OUS2 PIE1 POHN POVE REUN RIO2 SANT
6 | GFZ | SCOR SGOC SGPO SUTH SYOG TASH THU2 TONG TOW2 TUVA
6 | GFZ | TWTF UNSA VOIM WARK WHIT WTZR WUH2 ZAMB NRMD POHN
6 | GRG | CHTI MCM4 NRMD CAS1 MCM4
6 | JPL | 1 11 18 CAS1 CHTI HKSL CHTI HKSL NRMD NYA1 THU2
6 | MIT | BAKE DARW GANP IRKJ MCM4 MEDI PARC STJO TRO1 VACS
6 | MIT | VNDP YARR YEL2 BAKE DARW GANP IRKJ MCM4 MEDI PARC
6 | MIT | STJO TRO1 VACS VNDP YARR YEL2
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 | COD | ~00:45 | ~ -0.15 ns
0 | ESA | ~04:25 | ~ -0.34 ns
1 | ESA | ~22:25 | ~ -0.36 ns
2 | ESA | ~00:35 | ~ -0.52 ns
3 | ESA | ~01:30 | ~ 0.30 ns
4 | COD | ~12:35 | ~ 0.16 ns
4 | ESA | ~22:40 | ~ 0.30 ns
5 | ESA | ~08:45 | ~ -0.33 ns
6 | COD | ~08:05 | ~ -0.17 ns
6 | ESA | ~23:55 | ~ -0.30 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
----+--------+---------------
2 | GRG | 6
2 | JGX | 6
2 | SIO | 6
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G06 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G12 | | | | 4 | 4 | 4 | 4 |
PRN G30 | | | | | 4 | 4 | 4 |
9. 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 27-Nov-2022 (GPS Week 2238, day 0, MJD 59910), 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 lomg filename formats.
For more information see IGSMAIL #8238, #8256, #8274 and #8282.
Starting 02-Feb-2025 (GPS Week 2352, day 0, MJD 60708), 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.
For more information see IGSMAIL #8543.
Starting 11-Jan-2026 (GPS Week 2401, day 0, MJD 61051), all IGS products
are based on the IGS realization of the second yearly update of ITRF2020
called ITRF2020-u2024. This IGS realization is called IGc20.
For more information see IGSMAIL #8634.
10. 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 | -.0 -.8 -1.2 -5 -8 11 -.16
EMR | 0 | 8.7 4.0 13.1 0 0 0 -.05
ESA | 0 | -.2 .6 -.9 1 10 10 -.90
GFZ | 0 | -.4 -.1 -.2 -21 -10 3 .03
GRG | 0 | .3 .2 .5 0 3 -3 .13
JGX | 0 | 4.1 6.9 9.1 3 -7 18 -.43
JPL | 0 | 3.9 1.4 5.2 -15 16 8 -.08
MIT | 0 | 3.3 -.8 17.5 6 -14 1 -.18
NGS | 0 | 7.5 2.8 21.5 35 -17 18 .03
SIO | 0 | 4.1 -.1 4.6 4 -43 44 -.33
COD | 1 | .3 -.9 -1.0 -9 -8 5 -.17
EMR | 1 | 10.8 .7 9.1 2 -1 -1 -.23
ESA | 1 | -.1 .6 -.7 -18 22 15 -1.00
GFZ | 1 | -.2 -.5 -.3 -21 -1 -2 .07
GRG | 1 | .3 -.7 .4 7 4 -15 -.06
JGX | 1 | 6.8 3.7 11.3 -8 -11 18 -.51
JPL | 1 | 9.8 .8 9.5 -25 9 -2 -.19
MIT | 1 | 8.0 -2.3 17.5 1 -11 -5 -.07
NGS | 1 | 9.7 .1 27.2 -5 -28 7 -.07
SIO | 1 | 6.3 3.1 10.3 -69 -59 34 .04
COD | 2 | .7 -.9 -.6 -2 -9 10 -.22
EMR | 2 | 6.8 -1.7 15.8 -8 5 -17 -.09
ESA | 2 | -.1 .1 -.9 -9 12 -4 -.89
GFZ | 2 | -.2 -.4 -.0 -21 -1 -1 .32
GRG | 2 | .8 -.9 -.3 -11 -3 -21 -.05
JGX | 2 | 5.8 .0 13.0 12 -14 13 -.12
JPL | 2 | 5.6 2.2 12.2 -8 21 8 -.01
MIT | 2 | 6.4 -4.8 12.6 -15 -15 -7 -.03
NGS | 2 | 8.1 -.6 36.4 54 -7 -28 .04
SIO | 2 | 2.9 -7.7 14.7 -42 -35 46 .03
COD | 3 | .7 -.5 -.3 0 -18 4 -.12
EMR | 3 | 8.8 -7.7 15.5 0 0 0 -.04
ESA | 3 | -.4 .3 -.8 -6 15 14 -.73
GFZ | 3 | -.4 -.6 -.2 -24 -4 5 .25
GRG | 3 | .6 -.6 .2 -7 9 -2 -.07
JGX | 3 | 3.8 5.2 13.4 -1 -13 19 -.32
JPL | 3 | 2.3 -3.1 13.1 -24 23 12 -.03
MIT | 3 | 3.1 -3.6 12.9 0 -12 5 -.08
NGS | 3 | 7.2 -5.9 24.6 12 -12 -11 .23
SIO | 3 | -.4 -4.3 4.0 -90 -19 36 -.19
COD | 4 | 1.1 -.5 -.0 -2 -17 13 -.07
EMR | 4 | 8.9 -1.7 6.0 -2 -2 -7 .23
ESA | 4 | -1.2 -.2 -1.0 -4 4 15 -.76
GFZ | 4 | .1 .2 -.5 -23 5 14 .53
GRG | 4 | .4 .1 -.1 2 3 -8 .17
JGX | 4 | .8 9.8 6.8 -1 1 -2 -.20
JPL | 4 | 2.3 2.4 5.3 -10 22 10 .07
MIT | 4 | 5.7 .8 9.4 -7 -3 -3 -.00
NGS | 4 | 7.3 -.0 25.4 25 -11 0 .21
SIO | 4 | 3.9 -1.1 -2.6 -12 -91 53 .09
COD | 5 | 1.0 -.3 -.3 -6 -16 20 -.03
EMR | 5 | 6.3 2.1 8.7 -9 -5 -6 -.00
ESA | 5 | -.1 .3 -1.6 -14 10 2 -.88
GFZ | 5 | .1 .0 -.3 -21 -8 5 .33
GRG | 5 | .7 .0 .3 -18 -5 -13 .07
JGX | 5 | 2.3 6.2 11.6 5 -18 22 -.13
JPL | 5 | 5.2 -2.0 7.7 -3 22 6 .06
MIT | 5 | 4.4 .1 9.8 -16 -12 2 -.04
NGS | 5 | 7.2 2.9 22.2 11 -7 -24 .17
SIO | 5 | 3.8 .5 -1.2 -66 -65 9 .06
COD | 6 | .7 -.2 -.6 -2 -16 8 -.05
EMR | 6 | 11.4 3.3 10.4 -7 12 -8 -.08
ESA | 6 | .1 -.2 -1.3 -13 6 -6 -.84
GFZ | 6 | -.1 -.4 -.5 -13 9 4 .24
GRG | 6 | .9 -.2 .2 -24 0 -48 .24
JGX | 6 | .8 6.0 8.4 -22 -12 14 -.13
JPL | 6 | 3.3 3.3 6.0 -8 20 4 .06
MIT | 6 | 4.4 -2.6 12.8 -19 -13 -16 .09
NGS | 6 | 6.4 2.2 26.3 12 -12 -21 .24
SIO | 6 | 4.3 2.5 2.2 -52 36 -23 .05
11. 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.
12. 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 1.2402.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2402.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 2.2402.[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 3.2402.[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 5.2402.0-6). 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 2402 summary. (Jan 18, 2026 - Jan 24, 2026)
Table 1.2402.a GPS week: 2402 MJD: 61058.000-61064.000
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 929| 0 0 0 5 -2 10 .02 7 6 | -723 196 5 155
| 0 0 0 11 10 29 .04 | 160 254
emr 95| 0 0 5 -13 2 -15 -.00 11 11 | -57 41 6 110
| 1 1 2 10 7 16 .01 | 364 589
esa 186| 0 0 -3 -6 0 -19 -.11 8 8 | 2093 288 6 228
| 1 0 0 12 9 16 .02 | 946 582
gfz 147| 0 0 0 2 3 -18 .08 10 9 | -220 82 10 112
| 0 1 2 9 14 17 .05 | 86 146
grg 124| 1 0 -2 0 7 -5 .01 15 8 | -50 72 6 127
| 0 0 2 11 10 12 .02 | 127 222
igr n/a| 0 0 -2 0 8 -12 .03 4 3 | 7857 -127 9 93
| 0 0 1 7 2 14 .01 | 579 759
jgx n/a| 0 0 5 11 -5 2 .02 9 8 | -29 47 29 94
| 0 0 1 10 7 15 .02 | 154 256
jpl 120| 0 1 3 -12 0 -4 .02 11 11 | 39 128 6 77
| 0 0 0 11 8 23 .01 | 659 451
mit 359| 0 0 -7 2 7 13 .00 8 7 | 7808 -29 38 69
| 0 0 1 35 19 83 .01 | 557 479
ngs 257| 0 0 9 -7 -27 17 -.06 11 10 | -722 198 485 793
| 0 1 3 16 17 22 .02 | 169 265
sio 359| 0 0 -4 8 2 10 .02 12 9 | --- --- --- ---
| 0 0 2 9 21 33 .03 | --- ---
Table 1.2402.b GPS week : 2402 MJD: 61058.000-61064.000
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 | 3 4 3 3 3 3 3 |
3 | 3 3 3 3 2 2 2 |
4 | 3 4 4 3 4 4 4 |
5 | 3 3 3 3 2 3 3 |
6 | 3 4 19 4 3 4 3 |
7 | 3 3 3 3 3 3 3 |
8 | 4 3 3 3 2 3 2 |
9 | 4 3 3 3 3 3 3 |
10 | 3 3 2 2 2 2 2 |
11 | 3 3 3 3 3 14 4 |
12 | 3 2 3 2 2 2 2 |
13 | 4 5 4 3 3 3 3 |
14 | 3 4 4 3 3 4 3 |
15 | 3 3 4 4 3 3 3 |
16 | 3 3 2 3 3 3 3 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 3 4 4 4 4 |
19 | 3 3 5 3 3 3 3 |
21 | 3 3 3 3 3 3 3 |
22 | 3 3 3 3 2 2 3 |
23 | 3 3 3 3 3 3 3 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 3 3 3 |
27 | 3 3 3 3 2 2 2 |
28 | 3 3 3 3 3 3 3 |
29 | 3 3 3 3 3 3 3 |
30 | 3 3 3 3 2 3 2 |
31 | 3 3 3 2 3 2 2 |
32 | 3 3 3 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 2.2402.0 GPS week: 2402 Day: 0 MJD: 61058.000
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 932| 0 -1 0 -9 -1 51 -.02 7 7 | -734 100 6 164
emr 90| 1 0 7 -20 5 -14 -.02 10 10 | 17 50 7 108
esa 186| 0 0 -4 1 -5 -35 -.12 8 8 | 901 224 6 229
gfz 147| 0 0 -2 9 12 -23 .13 10 10 | -175 -108 11 110
grg 124| 2 0 0 0 0 4 .06 10 9 | 44 3 7 136
igr n/a| 0 0 -3 5 10 -25 .02 3 3 | 7284 420 9 84
jgx n/a| 0 0 4 15 -3 -3 .04 8 8 | 101 -57 29 90
jpl 120| 0 0 4 -9 3 -8 .03 10 10 | -591 31 7 80
mit 359| 0 0 -5 -3 2 -38 -.01 8 7 | 7420 147 31 63
ngs 258| -1 0 5 14 -6 45 -.08 10 10 | -735 101 534 947
sio 362| 0 0 -8 0 -4 24 .00 10 9 | --- --- --- ---
Table 2.2402.1 GPS week: 2402 Day: 1 MJD: 61059.000
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 931| 0 0 0 -3 -21 -43 .03 7 7 | -754 244 6 156
emr 103| 1 3 7 -24 3 -28 .00 10 10 | -46 -85 7 110
esa 186| 0 0 -4 -23 13 -26 -.11 8 8 | 1786 265 7 224
gfz 146| -1 -2 -1 -11 18 -30 .03 11 11 | -237 -65 12 127
grg 123| 0 0 -2 -12 20 -26 .02 9 8 | 88 -279 6 143
igr n/a| 0 0 -3 0 10 -23 .03 3 3 | 7452 -71 10 93
jgx n/a| 0 0 4 1 -2 3 .04 8 8 | 127 -331 32 99
jpl 120| 0 1 4 -28 -8 -35 .04 10 10 | -760 134 7 83
mit 359| 0 0 -5 56 -5 109 -.01 8 7 | 7437 -39 36 72
ngs 261| 0 -2 8 10 -6 -6 -.02 10 10 | -756 252 446 958
sio 363| 0 0 -5 14 3 52 -.01 12 9 | --- --- --- ---
Table 2.2402.2 GPS week: 2402 Day: 2 MJD: 61060.000
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 927| 0 0 0 -2 -1 23 -.04 10 7 | -606 47 6 173
emr 105| 1 0 9 5 -6 -33 -.01 15 15 | -390 481 7 101
esa 186| -2 1 -3 14 -5 -21 -.08 11 9 | 1037 713 6 238
gfz 146| 0 0 -4 10 -8 -36 .14 13 9 | -255 176 12 112
grg 124| 2 -1 -5 19 0 8 -.02 53 8 | -103 -48 6 126
igr n/a| 0 0 -4 7 10 -2 .02 12 4 | 7532 440 11 93
jgx n/a| 0 0 6 28 -18 -9 .04 22 17 | -40 -115 30 97
jpl 120| 1 2 2 2 -6 -4 .02 15 15 | -506 804 6 72
mit 359| 1 -1 -7 -45 26 42 -.02 10 8 | 7627 249 38 61
ngs 255| 0 0 16 -30 -23 4 -.05 14 14 | -618 62 589 815
sio 356| 0 0 -2 4 32 24 .01 20 8 | --- --- --- ---
Table 2.2402.3 GPS week: 2402 Day: 3 MJD: 61061.000
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 930| 0 0 0 20 -6 3 .02 7 7 | -1063 750 5 147
emr 87| -1 0 5 -15 13 -19 .01 11 11 | -639 966 7 120
esa 186| 0 0 -3 -11 9 -32 -.08 7 7 | 1924 1216 6 232
gfz 146| 0 0 1 -8 -19 -29 .06 10 9 | -395 262 10 112
grg 124| 1 0 -4 -12 23 -2 .01 10 8 | -289 444 8 143
igr n/a| 0 0 -2 -13 5 -25 .04 3 3 | 8131 702 9 92
jgx n/a| 0 0 6 0 6 -11 .04 7 7 | -335 487 32 97
jpl 120| 0 1 2 -25 16 -10 .00 10 10 | 290 478 6 81
mit 359| 0 0 -7 37 -24 82 .00 7 7 | 8141 681 39 70
ngs 256| 0 -1 7 -18 -24 20 -.07 10 10 | -1082 780 496 822
sio 357| 0 1 -4 7 8 -22 .06 11 9 | --- --- --- ---
Table 2.2402.4 GPS week: 2402 Day: 4 MJD: 61062.000
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 929| -1 0 0 5 8 -1 .04 7 6 | -651 148 5 147
emr 90| 0 0 5 -8 8 -26 .01 10 10 | -23 186 5 119
esa 186| 0 -1 -4 0 -13 -13 -.13 7 8 | 3003 417 6 224
gfz 148| 0 0 0 11 8 -17 .09 8 8 | -146 80 10 105
grg 123| 1 0 -1 3 0 -10 .02 9 8 | -17 87 6 110
igr n/a| 0 0 -1 5 6 -17 .02 3 2 | 8712 -100 9 90
jgx n/a| 0 0 4 17 -6 1 .01 6 6 | -63 170 27 90
jpl 120| 0 1 3 0 -4 -4 .04 10 10 | 563 298 6 76
mit 359| 0 0 -7 -19 29 25 .02 7 6 | 8649 28 34 66
ngs 254| 0 0 11 -13 -44 0 -.06 10 10 | -616 103 411 621
sio 356| 0 0 -4 -3 -3 38 .02 8 7 | --- --- --- ---
Table 2.2402.5 GPS week: 2402 Day: 5 MJD: 61063.000
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 931| 0 0 -1 10 10 8 .05 6 6 | -611 41 5 149
emr 91| 1 0 3 -21 -1 7 .00 10 10 | 450 -538 7 117
esa 186| 0 0 -2 -8 0 -23 -.14 7 7 | 3350 -356 6 233
gfz 149| -1 -1 1 -3 -2 0 .03 9 9 | -168 235 10 113
grg 124| 0 0 -1 -5 0 -14 -.00 8 7 | 27 103 7 108
igr n/a| 0 0 0 -4 5 -11 .03 3 3 | 8491 -941 9 105
jgx n/a| 0 0 5 11 -6 5 -.01 6 6 | 53 59 29 98
jpl 120| 0 1 3 -12 1 -12 .02 10 10 | 970 -442 6 81
mit 359| 0 0 -9 14 6 16 .02 7 7 | 8283 -525 42 82
ngs 260| 0 0 6 -13 -53 8 -.06 10 10 | -610 46 473 706
sio 364| 1 0 -3 17 18 -7 .06 12 9 | --- --- --- ---
Table 2.2402.6 GPS week: 2402 Day: 6 MJD: 61064.000
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 923| 0 0 0 20 -4 29 .08 7 6 | -643 44 5 150
emr 105| 0 1 3 -10 -5 7 -.00 9 9 | 232 -772 5 100
esa 186| 0 0 -3 -13 2 12 -.13 7 7 | 2651 -461 6 220
gfz 148| 0 0 2 9 17 9 .07 9 9 | -170 0 10 111
grg 126| 1 0 -1 7 9 1 .01 8 8 | -104 197 6 125
igr n/a| 0 0 -1 -3 10 15 .02 3 2 | 7398 -1345 9 98
jgx n/a| 0 0 4 7 -5 33 -.00 6 6 | -51 119 27 91
jpl 120| -1 0 3 -11 2 41 .01 9 9 | 313 -402 7 71
mit 359| 0 0 -9 -21 18 -140 .01 7 6 | 7101 -749 47 74
ngs 259| 0 1 8 -5 -30 49 -.07 10 9 | -641 47 449 683
sio 359| 0 0 -3 22 -34 -36 .02 11 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 3.2402.0 GPS week: 2402 Day: 0 MJD: 61058.000
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
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 8 12 7 --- 9 3 9 14 8 13 11 3 | 82 82 80 --- 81 82 81 84 79 85 81 81
2E | 11 9 9 9 8 3 7 9 11 13 12 3 | 50 48 47 49 49 49 48 48 45 50 45 47
3 | 5 7 7 10 8 2 8 9 7 9 14 2 | 20 21 22 21 20 20 20 22 19 19 20 19
4E | 8 8 8 12 11 3 8 15 6 13 11 3 | 42 42 38 51 45 43 43 43 46 44 47 44
X5 | 7 8 --- 8 6 5 7 9 7 10 6 2 | 33 30 --- 35 33 30 32 32 33 29 31 31
6 | 8 10 8 15 11 3 9 9 7 10 9 3 | 429 428 427 430 437 429 424 428 429 428 434 428
7M | 5 9 7 9 8 4 7 9 5 15 11 2 | 44 48 41 42 42 42 45 46 39 43 39 42
X8 | 6 9 --- 9 7 4 6 7 6 10 23 3 | 24 23 --- 24 22 22 23 23 20 23 29 21
9E | 7 12 8 10 10 5 10 10 12 8 16 3 | 35 31 33 35 31 32 32 29 31 31 30 31
10 | 5 8 6 10 7 2 7 7 6 10 6 2 | 26 24 25 25 26 24 21 25 25 24 23 24
11 | 7 10 6 9 9 4 7 15 8 10 9 3 | 55 54 53 56 54 54 54 55 51 51 54 56
12M | 7 6 7 7 8 3 7 6 6 8 8 2 | 23 20 25 24 19 22 21 20 22 27 24 22
13E | 8 9 9 18 7 4 9 7 11 9 13 3 | 32 33 30 36 31 31 28 35 34 33 34 31
14M | 7 17 4 8 8 2 8 16 7 7 12 3 | 18 23 16 20 19 17 21 22 18 21 23 17
15E | 10 11 12 8 12 3 10 11 7 9 8 3 | 64 61 55 64 66 62 62 63 63 60 63 62
16M | 6 8 8 6 8 2 6 8 8 9 8 2 | 22 20 23 23 23 21 21 20 20 23 22 21
17M | 7 7 10 14 9 4 8 8 12 8 11 3 | 22 25 21 31 22 23 24 23 21 22 26 22
18 | 7 11 7 10 15 3 5 18 9 12 10 3 | 59 65 59 62 67 60 62 61 60 61 59 61
19M | 6 7 10 11 8 4 8 9 8 7 11 2 | 33 31 27 36 30 31 32 31 28 30 36 31
21 | 8 9 9 8 10 5 7 9 9 12 9 3 | 48 48 48 48 53 46 49 50 49 48 48 48
22 | 6 6 8 10 8 4 7 6 5 8 14 2 | 19 21 23 20 19 20 19 22 16 22 19 19
23 | 6 9 6 11 7 2 7 8 7 13 6 2 | 38 43 39 45 42 40 40 39 39 39 40 40
24 | 6 9 7 11 11 4 8 9 7 8 9 2 | 32 33 29 28 34 28 29 32 30 33 30 30
25M | 6 17 9 9 8 3 10 15 6 9 7 3 | 20 35 26 22 22 22 18 35 21 25 22 23
26M | 5 17 6 6 9 2 6 15 9 7 11 3 | 19 33 20 20 22 20 18 31 12 18 14 19
27 | 6 7 8 8 9 3 6 6 5 10 9 2 | 22 22 22 23 21 20 20 22 18 21 20 20
28M | 7 9 7 8 9 3 8 8 10 12 8 2 | 27 25 28 32 31 29 27 29 29 26 31 27
29 | 8 7 10 9 16 4 6 8 8 8 6 3 | 33 30 26 31 33 28 30 29 26 30 29 29
30M | 8 8 6 8 5 4 6 7 6 9 9 2 | 30 29 26 25 25 24 26 29 22 26 21 25
31M | 5 9 7 7 9 3 5 8 6 7 9 2 | 39 43 38 40 38 39 39 42 39 44 37 39
32E | 6 10 8 9 9 3 10 9 7 10 9 3 | 24 22 22 20 25 22 22 24 23 26 24 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 10 8 10 10 3 8 10 8 10 10 |T 47 48 47 47 47 46 46 48 45 47 46 46
WRMS | 7 10 8 10 9 3 8 10 7 10 9 |NE 30 30 30 31 31 28 29 30 28 29 30 29
MEDI | 7 9 8 9 9 3 7 9 7 9 9 |MD 32 31 28 31 31 29 29 31 29 30 30 30
Table 3.2402.1 GPS week: 2402 Day: 1 MJD: 61059.000
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
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 8 11 8 --- 12 3 10 15 7 13 11 3 | 48 52 50 --- 50 51 52 55 54 50 53 51
2E | 8 10 9 14 11 3 9 10 8 12 12 3 | 54 54 52 57 52 53 52 52 54 52 51 52
3 | 5 9 6 9 7 3 5 8 6 9 12 2 | 19 20 20 17 17 18 19 21 19 19 18 18
4E | 8 9 10 8 14 4 8 16 13 13 16 4 | 36 38 32 36 42 35 36 38 35 37 39 36
5 | 7 9 9 8 6 3 8 8 5 12 8 2 | 28 27 18 27 26 26 27 26 29 25 30 26
6 | 14 12 8 19 8 2 9 9 6 10 9 3 | 440 439 438 439 434 438 433 440 434 440 440 438
7 | 7 7 7 6 7 2 7 6 8 9 11 2 | 29 30 25 29 24 27 29 29 31 29 26 27
X8 | 5 8 --- 11 8 3 7 6 8 14 16 3 | 24 24 --- 22 18 21 19 23 24 22 30 21
9E | 6 11 6 10 8 2 8 9 8 14 15 3 | 33 30 28 31 32 29 31 30 27 33 27 29
10 | 5 7 7 9 8 2 7 6 7 10 9 2 | 27 25 26 24 23 24 23 25 25 26 26 24
11 | 8 11 7 9 8 3 10 14 9 13 11 3 | 25 28 28 31 29 27 27 31 35 31 34 28
12 | 6 8 7 8 4 2 6 6 7 8 5 2 | 44 45 44 41 42 42 42 42 44 44 42 43
13E | 6 13 7 22 7 4 10 10 16 12 22 4 | 28 31 26 33 30 27 27 30 28 30 30 27
14 | 5 17 5 12 8 3 12 16 8 8 12 3 | 19 26 20 23 19 17 18 24 24 18 23 19
15E | 9 10 13 7 12 3 9 11 6 9 9 3 | 70 68 60 66 69 67 68 69 69 67 71 68
16 | 6 7 10 7 6 2 6 7 7 9 8 2 | 18 17 18 20 16 17 16 18 18 20 19 17
17 | 5 7 10 11 7 4 8 8 6 8 18 3 | 21 23 18 24 20 22 21 22 23 22 35 21
18 | 7 11 7 14 15 5 7 19 7 15 9 3 | 43 45 43 44 48 43 44 43 48 43 45 44
19 | 6 7 10 11 6 3 8 8 6 9 10 2 | 26 25 23 26 25 25 25 23 27 23 34 24
21 | 8 10 10 9 12 4 8 8 8 14 12 3 | 36 38 37 37 39 36 37 37 38 39 38 37
22M | 5 7 11 9 5 4 9 8 11 10 18 3 | 22 21 27 24 20 21 18 22 28 23 31 22
23 | 6 8 8 12 7 3 7 9 5 12 8 2 | 28 30 27 33 29 29 29 28 31 27 32 28
24 | 6 13 7 10 12 3 9 6 6 10 12 3 | 31 35 32 28 27 30 31 33 30 28 29 29
25 | 7 15 8 9 5 3 10 15 6 9 5 3 | 15 32 23 18 17 19 16 31 21 17 19 19
26 | 7 15 8 8 6 4 7 14 10 6 11 3 | 16 29 21 16 16 17 17 29 19 17 17 18
27 | 5 8 6 9 7 2 6 6 7 12 14 2 | 23 22 21 20 19 20 18 22 20 23 21 19
28 | 7 9 6 7 12 1 7 9 6 10 8 2 | 22 24 24 26 30 25 23 26 26 26 27 24
29 | 8 6 10 12 15 4 6 8 6 8 8 3 | 27 23 21 24 26 22 24 22 26 24 26 23
30 | 7 9 7 7 7 2 7 7 7 9 11 2 | 34 37 35 34 33 33 34 36 35 33 34 34
31 | 6 9 7 5 8 2 6 9 4 10 8 2 | 30 33 29 31 28 29 30 34 26 35 28 29
32E | 7 11 7 8 9 3 9 11 7 9 10 3 | 25 25 23 22 21 22 23 26 23 27 24 23
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 10 8 11 9 3 8 10 8 10 12 |T 43 45 42 43 42 42 42 44 44 43 45 42
WRMS | 7 10 8 11 8 3 8 10 7 10 9 |NE 27 27 25 25 24 25 25 26 26 25 27 25
MEDI | 7 9 7 9 8 3 8 9 7 10 11 |MD 28 30 26 27 27 27 27 29 28 27 30 27
Table 3.2402.2 GPS week: 2402 Day: 2 MJD: 61060.000
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
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 9 11 10 --- 11 3 8 15 9 19 11 4 | 34 34 36 --- 35 33 34 39 33 40 33 34
2E | 9 9 9 8 7 3 7 8 9 15 12 3 | 49 50 49 51 49 49 49 48 47 51 51 48
3 | 9 11 9 11 8 3 5 8 7 9 7 2 | 18 22 22 17 17 20 19 22 19 22 25 19
4E | 8 10 9 8 12 3 9 17 8 13 10 3 | 22 26 24 27 26 24 27 29 28 24 26 25
X5 | 7 10 --- 8 7 3 8 9 7 11 9 3 | 37 34 --- 38 35 35 34 34 34 38 34 34
6 | 42 56 34 51 279 60 111 57 36 44 85 18 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
7 | 4 9 10 9 8 3 6 7 9 10 8 2 | 34 33 33 32 30 31 36 32 30 33 33 31
X8 | 6 7 --- 11 6 4 5 5 7 9 8 2 | 27 28 --- 28 26 26 27 26 27 29 27 26
9E | 7 14 8 8 9 2 7 10 8 10 13 3 | 25 25 24 26 23 23 24 23 22 26 25 23
10 | 6 9 7 7 5 2 6 7 7 11 8 2 | 20 20 21 18 18 19 17 19 20 22 21 18
11 | 7 11 9 11 10 4 9 15 7 14 8 3 | 37 37 36 35 36 36 36 39 32 40 37 37
12 | 5 8 9 11 8 2 6 7 7 9 8 2 | 122 121 126 123 121 123 122 125 123 126 126 123
13E | 10 10 8 11 7 4 8 10 10 19 14 3 | 24 23 21 24 21 20 20 23 23 28 24 22
14 | 6 19 6 8 9 4 8 17 9 11 9 3 | 19 25 19 23 21 19 22 23 25 22 21 20
15 | 9 10 12 10 12 3 8 14 6 17 15 3 | 41 40 35 42 39 39 38 41 41 46 46 39
16 | 5 8 7 7 6 3 6 7 8 9 8 2 | 30 31 31 30 30 29 32 30 32 32 31 31
17 | 6 7 12 12 8 6 7 10 8 12 16 3 | 24 24 24 30 24 26 24 24 24 25 27 23
18 | 7 11 7 12 9 5 7 18 7 14 8 3 | 67 71 67 68 65 66 69 72 73 71 69 69
19 | 9 11 11 12 9 5 8 10 8 14 39 5 | 32 30 29 36 29 32 32 29 33 30 51 31
21 | 8 13 8 8 8 4 8 8 8 13 10 3 | 24 22 20 25 22 22 21 22 24 24 28 22
22 | 6 6 13 7 8 4 6 7 6 11 7 2 | 28 31 35 34 32 31 32 31 33 30 32 31
23 | 6 8 7 10 7 3 7 8 8 13 5 2 | 20 19 19 24 21 21 19 20 20 22 23 19
24 | 7 9 7 12 8 3 7 8 10 10 14 3 | 26 29 25 22 22 23 23 28 25 27 28 23
25 | 6 15 7 9 7 2 10 14 7 10 6 3 | 20 35 27 31 22 24 21 35 23 26 25 25
26 | 6 16 6 7 7 3 6 15 11 7 10 3 | 19 31 23 23 21 21 21 31 19 23 18 21
27 | 6 10 6 11 6 2 6 5 5 10 7 2 | 23 27 23 25 24 23 22 24 23 25 20 23
28 | 6 9 10 9 13 3 7 8 6 13 8 3 | 22 21 22 28 28 23 21 23 26 17 25 22
29 | 8 8 9 9 15 4 5 9 7 10 6 3 | 30 29 25 29 28 28 28 26 29 30 31 27
30 | 7 10 8 9 6 3 6 6 6 10 9 2 | 66 62 67 64 63 65 64 65 62 66 66 64
31 | 5 9 8 8 7 4 7 8 6 9 6 2 | 31 38 31 30 32 32 33 35 31 40 39 32
32E | 10 11 8 9 7 2 7 9 8 13 10 3 | 22 21 21 22 21 20 19 22 21 26 24 20
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 15 11 13 53 12 22 15 10 14 20 |T 33 34 33 34 32 32 32 34 33 35 35 32
WRMS | 7 15 9 9 8 4 17 15 8 14 8 |NE 25 25 22 25 23 24 23 24 24 26 26 23
MEDI | 7 10 8 9 8 3 7 9 8 11 9 |MD 26 29 25 29 26 26 27 29 27 28 28 25
Table 3.2402.3 GPS week: 2402 Day: 3 MJD: 61061.000
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
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 9 13 8 --- 19 3 8 15 8 12 13 4 | 28 32 29 --- 31 29 31 35 28 30 34 29
2E | 9 9 9 5 9 3 6 7 7 12 9 2 | 33 30 33 31 36 32 29 33 35 35 37 32
3 | 6 7 7 8 6 3 6 8 9 10 8 2 | 24 26 28 24 24 24 25 26 25 25 23 24
4E | 9 10 7 8 11 2 9 15 8 12 11 3 | 18 24 22 25 24 21 22 27 22 18 25 21
5 | 7 11 8 9 7 2 8 8 7 11 7 2 | 28 26 22 31 27 28 27 27 27 32 28 27
6 | 8 10 8 19 12 3 9 8 6 9 10 3 | 502 497 500 499 501 499 494 499 501 497 502 499
7 | 7 8 8 13 9 2 7 9 10 10 10 3 | 38 40 38 44 34 38 40 43 37 39 36 38
X8 | 6 11 --- 9 7 3 4 7 7 9 8 2 | 22 25 --- 23 23 23 22 24 22 23 22 22
9E | 6 10 6 9 8 2 7 10 7 7 8 2 | 21 22 22 22 22 21 20 21 20 22 21 20
10 | 4 9 7 10 7 2 6 7 7 8 6 2 | 27 29 29 28 26 27 26 27 26 27 29 26
11 | 7 12 6 8 11 4 10 16 6 13 8 3 | 67 61 64 68 63 65 62 66 60 62 64 66
12 | 5 9 7 6 7 2 8 6 5 7 6 2 | 173 177 174 175 176 175 176 173 176 175 174 175
13E | 6 8 7 10 16 3 8 10 10 9 12 3 | 28 25 23 31 29 26 26 27 25 26 27 25
14 | 6 18 7 8 9 2 7 16 7 7 8 3 | 15 23 16 17 18 15 18 19 15 14 18 14
X15 | 10 11 --- 11 15 3 8 12 7 11 13 3 | 42 42 --- 42 39 40 41 41 42 40 40 40
16 | 8 11 8 7 6 2 6 8 9 9 15 3 | 19 19 21 17 17 18 19 15 15 19 16 16
X17 | 4 7 --- 11 9 3 6 9 5 8 12 2 | 25 27 --- 26 27 27 25 28 24 24 30 24
18E | 8 10 8 14 14 4 6 19 12 10 9 3 | 30 33 29 35 34 31 30 33 35 33 33 31
19 | 7 6 9 11 8 2 7 8 6 10 15 3 | 31 28 27 25 28 28 27 26 25 25 32 26
21 | 7 12 9 13 9 3 7 9 6 15 12 3 | 27 27 27 31 31 27 28 28 28 33 30 28
22 | 6 7 8 6 7 2 7 6 5 7 19 2 | 18 21 22 18 20 20 20 21 16 19 23 18
23 | 6 10 7 12 8 2 7 8 5 10 7 2 | 27 30 29 33 31 30 31 31 30 31 32 29
24 | 5 10 8 10 9 3 8 7 5 7 8 2 | 31 35 32 34 29 32 32 34 30 31 31 31
25 | 7 16 8 8 6 3 10 15 4 8 9 3 | 17 32 25 20 18 20 16 32 17 16 25 20
26 | 8 17 6 7 6 1 5 15 9 6 15 3 | 20 32 23 19 18 19 20 31 14 18 19 19
27 | 5 13 8 8 9 2 5 6 7 7 17 2 | 22 25 27 21 21 23 21 24 22 22 28 22
28 | 7 9 6 5 11 3 6 8 4 8 6 2 | 19 17 16 20 26 20 20 20 22 16 21 18
29 | 9 10 9 11 18 4 6 9 7 9 5 3 | 23 20 18 21 27 21 21 20 23 23 25 20
30 | 6 8 6 8 5 4 5 6 6 10 13 2 | 127 129 126 128 127 126 128 128 127 126 127 127
31 | 6 9 7 6 7 4 6 8 4 6 8 2 | 59 61 57 60 57 58 59 60 57 60 59 58
32E | 9 11 6 8 10 3 9 10 7 14 9 3 | 21 22 22 22 22 21 21 25 22 26 25 21
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 11 7 10 10 3 7 10 7 10 11 |T 51 52 53 53 51 51 50 53 50 51 52 50
WRMS | 7 11 7 9 8 3 7 10 7 10 9 |NE 25 27 26 27 26 26 25 26 25 27 27 25
MEDI | 7 10 7 8 9 3 7 8 7 9 9 |MD 27 28 27 26 27 27 26 28 25 26 29 26
Table 3.2402.4 GPS week: 2402 Day: 4 MJD: 61062.000
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
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 9 11 8 --- 14 2 8 16 7 15 9 3 | 35 40 40 --- 39 38 39 45 38 46 41 39
2E | 11 7 8 8 11 3 7 8 8 15 13 3 | 35 31 30 35 29 32 31 33 34 32 35 32
3 | 7 10 6 5 7 2 5 8 5 10 7 2 | 25 25 27 25 25 25 25 28 25 27 26 25
4E | 8 8 8 12 11 3 8 18 8 16 9 3 | 28 30 36 30 34 29 32 34 31 28 31 30
5 | 7 8 7 9 5 2 7 8 4 7 4 2 | 35 33 19 36 33 34 34 34 35 33 33 33
6E | 8 11 8 11 10 3 7 9 7 9 8 3 | 737 738 738 738 721 741 723 739 736 740 742 738
7 | 4 7 8 9 9 2 6 8 6 9 7 2 | 39 42 38 40 36 39 39 43 41 45 38 39
8 | 4 6 7 9 8 2 4 6 6 8 8 2 | 29 31 16 31 28 30 29 29 28 27 30 29
9E | 6 11 6 13 8 3 5 9 7 11 7 2 | 26 25 26 24 28 25 26 24 24 26 25 24
10 | 6 6 8 7 6 1 5 7 6 10 5 2 | 26 26 26 26 24 24 23 26 25 26 24 25
11E | 8 9 7 6 11 4 8 16 6 10 5 3 | 80 82 80 80 80 78 79 82 77 81 81 79
12 | 6 8 6 6 6 2 5 6 5 6 6 2 | 211 210 210 211 210 210 208 209 211 210 208 210
13E | 6 7 8 9 5 3 8 9 10 11 6 2 | 36 35 32 37 35 34 33 35 34 35 36 34
14 | 6 18 6 8 10 2 6 17 7 10 11 3 | 31 32 29 31 30 28 30 32 31 27 33 29
15 | 7 11 10 10 14 3 8 14 6 11 6 3 | 39 41 44 44 41 39 37 41 39 41 39 38
16 | 6 7 9 7 9 3 3 6 13 9 11 2 | 31 31 31 29 30 30 31 30 31 32 31 30
17 | 7 8 10 8 7 3 7 7 6 11 16 3 | 26 27 25 31 25 26 26 26 26 23 36 26
18E | 6 11 7 9 13 4 8 17 8 15 9 3 | 30 34 28 29 32 28 31 32 31 28 29 29
X19 | 5 7 --- 8 5 4 6 9 6 11 12 2 | 40 38 --- 39 37 38 39 38 37 34 46 39
21 | 8 11 9 9 7 4 6 8 6 10 6 2 | 31 27 28 33 31 28 29 29 28 27 30 28
22 | 5 6 7 5 6 2 5 7 7 8 6 2 | 27 27 29 30 27 26 26 28 27 25 28 27
23 | 7 10 6 8 6 2 8 7 4 16 8 2 | 24 29 24 30 27 25 27 26 26 27 25 25
24 | 8 13 7 8 7 2 6 6 6 12 14 3 | 34 37 33 34 34 33 33 35 31 36 31 33
25 | 9 14 7 7 6 3 9 13 6 8 6 3 | 18 32 24 25 19 20 16 32 18 17 21 20
26 | 5 15 6 7 6 2 5 13 11 7 10 3 | 22 32 25 22 22 23 21 32 19 25 21 22
27 | 3 7 7 10 8 2 4 6 6 7 8 2 | 27 27 29 31 27 28 26 28 28 28 28 27
28 | 7 10 5 7 10 3 6 8 7 9 8 2 | 20 21 18 25 27 21 22 23 25 19 26 21
29 | 9 6 8 8 16 3 5 9 6 8 4 2 | 27 22 23 25 28 24 26 24 26 27 27 24
30 | 5 7 6 8 5 2 5 6 5 10 6 2 | 183 180 181 180 180 180 182 180 179 179 180 181
31 | 4 8 7 7 6 2 6 8 6 9 10 2 | 77 79 75 77 75 76 76 79 75 79 76 76
X32E | 9 12 --- 6 9 3 6 11 6 12 6 3 | 25 26 --- 25 25 24 23 25 25 27 26 24
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 10 7 8 9 3 6 10 7 10 8 |T 66 67 67 68 65 65 65 67 65 66 67 65
WRMS | 6 10 8 8 8 2 6 10 6 10 7 |NE 28 28 25 30 28 27 28 28 28 28 28 27
MEDI | 7 8 7 8 8 3 6 8 6 10 8 |MD 31 32 29 31 30 29 31 32 31 28 31 29
Table 3.2402.5 GPS week: 2402 Day: 5 MJD: 61063.000
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 | 11 10 9 --- 10 5 10 15 7 10 18 4 | 60 63 62 --- 62 61 62 66 63 61 67 62
2E | 6 7 9 10 6 2 6 8 10 10 14 2 | 32 33 32 33 34 33 34 31 34 34 35 32
3 | 4 9 6 8 5 3 5 9 6 7 10 2 | 24 25 26 23 23 24 23 26 25 24 24 24
X4E | 7 7 --- 7 8 3 7 18 9 12 10 3 | 39 41 --- 42 41 40 41 42 42 41 44 40
X5 | 4 8 --- 6 6 2 6 8 7 10 5 2 | 23 21 --- 22 18 21 21 22 22 23 22 21
6E | 8 10 8 17 11 3 8 10 6 14 14 3 | 529 531 531 527 520 531 525 531 528 533 524 529
7 | 4 7 8 9 7 3 5 8 10 13 9 2 | 29 33 27 28 30 30 31 32 27 30 34 29
X8 | 8 8 --- 9 5 2 3 6 7 7 11 2 | 26 30 --- 30 28 29 28 29 30 31 32 28
9E | 7 11 5 9 7 3 5 9 8 11 10 2 | 30 27 26 29 29 28 26 27 29 29 29 27
10 | 7 8 7 9 4 3 5 7 6 7 7 2 | 26 25 25 27 24 24 23 24 26 23 25 24
X11E | 10 --- --- 18 --- 9 --- --- --- --- --- 14 | 69 --- --- 67 --- 66 --- --- --- --- --- 67
12 | 4 8 7 11 6 3 5 6 6 9 8 2 | 268 264 267 267 273 267 267 266 269 268 271 268
13E | 8 7 8 8 6 4 7 8 10 11 9 2 | 27 29 26 28 27 26 25 27 29 31 30 27
14 | 5 17 5 7 10 2 7 17 8 10 18 3 | 34 40 36 37 35 36 35 38 40 39 38 36
15 | 7 13 10 11 10 3 8 12 5 8 12 3 | 30 27 27 31 30 27 28 28 28 28 27 27
16 | 4 9 8 5 6 3 4 8 12 8 8 2 | 25 24 27 25 25 25 26 26 31 22 26 25
17 | 6 8 9 10 8 4 6 8 5 7 24 3 | 21 25 19 26 20 23 21 24 24 23 34 21
18E | 7 11 6 7 14 3 6 19 9 11 10 3 | 29 32 28 32 34 29 31 32 32 28 32 30
19 | 5 7 8 8 7 3 6 8 7 15 16 3 | 40 41 46 42 38 41 38 39 40 45 47 40
21 | 6 9 7 11 8 3 9 8 6 12 13 3 | 33 35 34 35 33 33 33 33 36 34 40 34
22 | 4 5 8 7 6 2 6 6 7 11 6 2 | 25 28 26 28 24 26 25 26 29 28 25 26
23 | 7 9 6 10 6 2 6 8 5 9 9 2 | 22 25 21 28 25 23 24 21 23 20 24 22
24 | 6 10 7 7 7 3 5 7 6 9 11 2 | 29 32 28 29 29 28 28 30 25 28 29 27
25 | 6 14 7 5 7 3 8 15 6 8 5 2 | 16 32 24 18 18 19 17 31 20 17 24 20
26 | 4 17 6 8 5 2 6 13 9 7 10 3 | 20 30 22 18 18 19 18 29 18 16 20 19
27 | 6 8 6 8 6 2 4 5 7 5 8 2 | 26 27 27 28 26 26 25 26 27 24 27 26
28 | 6 10 5 8 10 3 6 8 7 10 7 2 | 25 26 23 29 28 26 25 25 28 25 29 25
29 | 8 8 9 8 15 4 5 9 6 8 5 2 | 28 25 22 27 26 25 25 23 27 24 29 25
30 | 4 7 7 6 5 3 4 7 7 9 20 2 | 227 227 225 226 224 226 225 225 228 227 225 226
31 | 5 9 7 6 6 3 6 8 5 8 11 2 | 77 77 76 78 75 76 76 77 78 78 75 76
32E | 9 13 6 14 7 3 6 9 6 17 9 3 | 24 24 25 23 25 23 24 23 24 30 27 23
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 10 7 9 8 3 6 10 7 10 12 |T 61 63 65 62 61 61 61 62 62 62 63 61
WRMS | 6 10 7 9 7 3 6 10 7 10 9 |NE 26 27 26 27 25 25 25 26 26 25 28 25
MEDI | 6 9 7 8 7 3 6 8 7 9 10 |MD 29 30 27 29 28 28 26 29 29 28 29 27
Table 3.2402.6 GPS week: 2402 Day: 6 MJD: 61064.000
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 10 10 --- 11 4 6 15 8 11 10 3 | 101 103 101 --- 103 103 102 105 106 104 102 103
2E | 6 7 7 7 6 3 6 7 9 17 9 2 | 39 38 39 41 38 38 37 38 44 38 41 39
3 | 5 7 7 7 4 3 4 9 6 6 12 2 | 29 30 31 28 28 29 28 30 31 30 28 29
4E | 10 8 6 9 8 3 9 15 7 14 15 3 | 38 39 42 45 42 39 39 42 37 38 44 39
5 | 6 6 7 10 7 2 6 7 5 11 6 2 | 25 22 16 27 24 22 23 22 25 25 25 23
6E | 10 12 7 9 12 4 8 9 6 11 6 3 | 683 684 683 683 671 685 674 684 684 684 683 683
7 | 6 7 8 9 8 2 5 7 6 7 9 2 | 58 58 54 56 56 56 58 59 58 58 57 57
X8 | 3 8 --- 7 6 2 3 5 6 7 10 2 | 32 35 --- 34 33 34 33 34 36 33 37 33
9E | 12 13 4 10 6 3 5 10 9 8 14 3 | 29 24 23 22 23 24 24 23 24 25 26 23
10 | 5 7 8 7 6 2 5 5 7 9 8 2 | 30 29 28 30 27 27 27 27 30 29 29 28
X11E | 9 10 6 --- 14 2 9 15 6 15 10 3 | 6 10 6 --- 15 8 10 14 10 6 12 8
12 | 4 9 6 8 6 2 6 8 5 7 6 2 | 355 357 357 356 355 356 355 355 358 356 356 356
13E | 6 8 7 12 8 3 7 10 10 12 12 3 | 33 35 30 39 35 33 33 34 30 37 33 33
14 | 5 16 6 10 8 2 6 15 8 6 7 3 | 17 22 18 19 17 15 18 20 21 17 23 17
15 | 7 11 10 9 11 3 8 11 5 13 11 3 | 46 44 43 46 46 44 46 43 47 46 46 44
16 | 6 9 8 8 6 2 4 8 10 9 9 2 | 31 29 31 29 29 29 30 29 33 28 31 30
17 | 5 7 9 10 10 3 6 7 6 7 18 3 | 29 32 28 36 31 32 29 32 32 28 37 30
18E | 8 10 5 10 15 3 8 17 8 12 13 3 | 49 55 50 54 56 52 53 49 57 53 53 52
19 | 4 6 7 9 9 3 6 7 6 7 19 2 | 37 36 34 37 39 37 35 35 42 34 48 37
21 | 8 9 8 11 9 2 7 8 5 12 11 3 | 49 48 48 46 50 47 48 49 47 51 49 48
22 | 4 5 7 8 7 2 6 7 4 7 23 3 | 27 29 28 30 27 27 26 28 30 27 39 28
23 | 7 7 6 8 7 2 5 7 5 11 8 2 | 38 40 39 41 40 39 39 39 40 43 40 39
24 | 5 10 7 6 9 3 5 6 6 11 8 2 | 40 41 38 40 42 38 41 40 37 39 37 39
25 | 7 14 6 8 6 3 10 13 6 6 5 2 | 21 34 26 28 21 23 19 33 24 22 25 24
26 | 5 14 7 8 6 2 7 13 9 8 12 3 | 23 31 25 20 19 21 21 31 20 22 21 22
27 | 5 8 7 8 5 1 4 6 7 5 14 2 | 30 30 32 31 31 30 29 31 34 28 33 30
28 | 7 9 6 6 12 3 5 7 6 11 6 2 | 28 28 28 29 33 29 29 29 32 26 30 28
29 | 9 5 10 10 15 3 6 9 7 8 5 3 | 36 33 32 33 34 33 34 33 39 35 37 34
30 | 5 8 6 8 4 3 4 6 5 8 8 2 | 255 255 255 255 256 255 256 256 254 257 255 255
31 | 5 8 7 7 7 3 5 7 6 8 9 2 | 89 92 91 90 90 89 91 92 87 94 90 90
32E | 9 10 5 8 8 2 5 9 7 9 9 2 | 24 24 21 27 26 24 23 23 24 25 25 23
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 9 7 9 8 3 6 9 7 10 11 |T 75 76 75 77 75 74 74 76 76 75 77 74
WRMS | 6 9 7 9 8 2 6 9 6 9 9 |NE 34 34 33 34 34 33 33 33 35 34 35 33
MEDI | 6 8 7 8 8 3 6 8 6 9 9 |MD 33 35 32 36 34 33 33 34 36 34 37 33
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 4.2402 GPS week: 2402 MJD: 61058.0-61064.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 |U 11 12 28 |U 12 14 55 |U 31 26 54 |
emr | emr 2962 |U 11 15 34 |U 13 14 63 | 30 29 65 |
esa | esa 2770 | 9 13 28 | 13 18 56 | 39 28 69 |
gfz | gfz 2852 | 8 13 24 | 12 14 57 | 21 22 50 |
grg | grg 2962 |U 9 15 20 |U 13 15 56 | 25 24 52 |
igr | igr 2962 | 7 12 21 | 12 14 53 | 26 23 54 |
igs | igs 2962 | 7 12 20 | 12 13 51 | 30 24 54 |
jgx | jgx 2962 |U 7 12 19 |U 12 13 52 |U 30 24 57 |
jpl | jpl 2962 | 15 19 45 | 14 17 62 | 31 29 72 |
mit | mit 2962 |U 9 11 21 |U 12 14 52 |U 26 27 55 |
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 5.2402.0 GPS week: 2402 Day: 0 MJD: 61058.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 10 21 | 15 16 59 | 10 9 24 |
emr | emr 2976 | 6 8 24 | 13 18 71 | 12 7 30 |
esa | esa 2784 | 8 10 22 | 16 18 71 | 14 11 39 |
gfz | gfz 2880 | 8 12 20 | 14 20 59 | 8 9 25 |
grg | grg 2976 | 7 15 20 | 14 18 58 | 8 8 17 |
igr | igr 2976 | 5 11 17 | 14 17 63 | 9 9 23 |
igs | igs 2976 | 5 10 16 | 13 16 59 | 9 8 22 |
jgx | jgx 2976 | 6 12 19 | 16 16 60 | 10 9 24 |
jpl | jpl 2976 | 11 16 31 | 14 21 73 | 14 8 43 |
mit | mit 2976 | 8 10 18 | 13 18 58 | 10 10 18 |
Table 5.2402.1 GPS week: 2402 Day: 1 MJD: 61059.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 8 20 | 17 16 99 | 44 13 26 |
emr | emr 2974 | 7 14 23 | 19 17 111 | 37 45 58 |
esa | esa 2880 | 8 13 22 | 15 23 85 | 47 22 35 |
gfz | gfz 2880 | 10 15 31 | 13 16 102 | 18 8 20 |
grg | grg 2976 | 8 14 19 | 18 15 94 | 45 26 36 |
igr | igr 2976 | 6 9 15 | 16 15 92 | 46 23 34 |
igs | igs 2976 | 6 10 16 | 16 15 90 | 45 13 24 |
jgx | jgx 2976 | 6 10 18 | 17 14 89 | 33 26 46 |
jpl | jpl 2976 | 13 19 29 | 19 21 106 | 33 42 61 |
mit | mit 2976 | 8 9 23 | 14 16 92 | 41 37 57 |
Table 5.2402.2 GPS week: 2402 Day: 2 MJD: 61060.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 21 22 58 | 10 16 51 | 120 108 205 |
emr | emr 2976 | 30 32 72 | 14 13 68 | 89 96 169 |
esa | esa 2784 | 10 16 26 | 11 20 52 | 130 83 185 |
gfz | gfz 2880 | 10 18 26 | 12 14 48 | 86 100 198 |
grg | grg 2976 | 10 17 18 | 11 14 47 | 88 96 198 |
igr | igr 2974 | 10 17 29 | 10 13 45 | 90 91 196 |
igs | igs 2976 | 11 19 25 | 10 12 46 | 116 104 212 |
jgx | jgx 2976 | 7 15 23 | 10 12 45 | 125 94 208 |
jpl | jpl 2976 | 34 30 96 | 14 15 64 | 99 103 191 |
mit | mit 2976 | 11 12 26 | 12 12 47 | 91 93 184 |
Table 5.2402.3 GPS week: 2402 Day: 3 MJD: 61061.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 12 22 | 9 11 41 | 12 12 30 |
emr | emr 2976 | 6 10 29 | 9 10 47 | 27 18 83 |
esa | esa 2688 | 8 14 30 | 9 13 37 | 30 25 88 |
gfz | gfz 2880 | 7 14 23 | 9 9 44 | 10 8 29 |
grg | grg 2975 | 7 15 17 | 9 10 46 | 10 9 28 |
igr | igr 2976 | 5 11 20 | 8 9 40 | 11 10 31 |
igs | igs 2976 | 5 11 21 | 8 9 38 | 11 10 31 |
jgx | jgx 2976 | 5 12 16 | 8 8 38 | 11 11 31 |
jpl | jpl 2976 | 10 16 41 | 10 13 48 | 17 12 55 |
mit | mit 2976 | 6 9 20 | 8 9 38 | 11 12 31 |
Table 5.2402.4 GPS week: 2402 Day: 4 MJD: 61062.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 9 26 | 9 13 37 | 12 14 36 |
emr | emr 2976 | 7 10 29 | 11 12 45 | 17 14 41 |
esa | esa 2784 | 8 11 28 | 12 15 45 | 26 22 54 |
gfz | gfz 2880 | 9 11 23 | 10 12 36 | 11 14 35 |
grg | grg 2976 | 11 11 23 | 10 15 37 | 10 13 36 |
igr | igr 2976 | 7 10 23 | 9 13 37 | 11 12 35 |
igs | igs 2976 | 7 10 23 | 10 12 35 | 12 13 35 |
jgx | jgx 2976 | 7 11 22 | 10 11 36 | 12 13 36 |
jpl | jpl 2976 | 10 14 38 | 12 16 46 | 18 13 56 |
mit | mit 2976 | 9 10 22 | 11 13 39 | 11 15 38 |
Table 5.2402.5 GPS week: 2402 Day: 5 MJD: 61063.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 11 12 23 | 13 18 44 | 10 12 29 |
emr | emr 2880 | 9 14 29 | 14 15 44 | 15 13 39 |
esa | esa 2592 | 13 17 32 | 16 24 49 | 12 12 40 |
gfz | gfz 2784 | 8 14 22 | 14 16 46 | 8 8 23 |
grg | grg 2880 | 10 17 22 | 14 21 50 | 8 8 26 |
igr | igr 2880 | 8 12 20 | 13 17 43 | 9 9 28 |
igs | igs 2880 | 9 12 20 | 13 16 43 | 10 9 28 |
jgx | jgx 2880 | 8 11 16 | 13 16 45 | 9 11 28 |
jpl | jpl 2880 | 14 18 39 | 14 20 49 | 16 11 50 |
mit | mit 2880 | 10 12 21 | 13 17 42 | 9 11 32 |
Table 5.2402.6 GPS week: 2402 Day: 6 MJD: 61064.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 14 23 | 12 13 51 | 9 12 26 |
emr | emr 2976 | 10 14 30 | 14 12 54 | 16 13 33 |
esa | esa 2880 | 12 9 37 | 13 14 51 | 17 19 43 |
gfz | gfz 2784 | 7 11 21 | 14 12 62 | 9 7 22 |
grg | grg 2975 | 10 16 19 | 13 16 58 | 9 8 26 |
igr | igr 2976 | 8 15 21 | 12 12 48 | 10 8 27 |
igs | igs 2976 | 9 14 22 | 12 12 48 | 10 9 27 |
jgx | jgx 2976 | 8 14 19 | 12 13 50 | 10 8 26 |
jpl | jpl 2976 | 15 18 41 | 15 16 53 | 17 12 48 |
mit | mit 2976 | 9 15 18 | 11 11 51 | 10 10 26 |
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 6.2402 GPS week: 2402 MJD: 61058.500-61064.500
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 | 7 -17 92 -4 6 | -8 18
| 15 17 49 31 3 | 2
emr uuuuu | 33 15 -56 87 -7 | -19 26
| 13 13 61 39 8 | 5
esa uuuuu | -9 3 -20 -3 1 | -4 15
| 7 8 37 43 2 | 4
gfz uuuuu | -29 -5 -39 -18 -4 | 10 17
| 18 9 105 84 4 | 4
grg uuuuu | -11 6 -27 -21 5 | 3 14
| 8 9 58 33 2 | 2
igr xxxxx | -14 -4 3 -22 5 | -1 15
| 6 6 49 47 6 | 2
irf xxxxx | -3 5 -17 -13 0 | 0 15
| 2 5 6 9 5 | 4
jgx uuuuu | -1 -17 41 -93 0 | 3 16
| 7 7 14 15 3 | 4
jpl uuuuu | 4 15 17 -47 -8 | 5 19
| 8 9 51 30 7 | 6
mit uuuuu | -6 12 -35 27 -5 | 16 22
| 16 10 27 47 4 | 5
ngs uuuuu | 23 5 -40 137 5 | 12 18
| 19 35 88 87 6 | 2
sio xxxxx | 34 67 -4 -45 -7 | 30 35
| 54 26 86 96 8 | 5
Table 7.2402.0 GPS week: 2402 Day: 0 MJD: 61058.500
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 | 8 8 159 14 3 | -6 18
emr uuuuu | 25 25 -5 45 -1 | -15 23
esa uuuuu | -4 -2 -89 59 -2 | 0 16
gfz uuuuu | -37 -14 -116 -111 1 | 13 21
grg uuuuu | -3 8 -121 15 6 | 5 16
igr xxxxx | -17 1 -84 -1 9 | 0 17
irf xxxxx | -4 4 -24 -9 -5 | 4 16
jgx uuuuu | 10 -21 42 -104 -2 | 7 18
jpl uuuuu | 6 21 69 -49 -11 | 11 26
mit uuuuu | -27 10 -13 -17 -4 | 20 26
ngs uuuuu | 28 -36 -1 161 0 | 13 21
sio xxxxx | 25 43 -123 -65 0 | 35 40
Table 7.2402.1 GPS week: 2402 Day: 1 MJD: 61059.500
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 | 30 -23 31 -23 0 | -4 18
emr uuuuu | 44 28 55 93 2 | -13 21
esa uuuuu | -19 12 -30 30 -1 | 2 16
gfz uuuuu | -55 6 -65 -38 -3 | 16 22
grg uuuuu | -4 4 -47 -4 4 | 7 17
igr xxxxx | -14 -9 -13 20 1 | 3 18
irf xxxxx | -4 8 -23 1 -7 | 6 16
jgx uuuuu | -6 -18 29 -93 -5 | 9 18
jpl uuuuu | 16 28 66 -84 1 | 13 26
mit uuuuu | -18 19 -37 -30 -6 | 22 27
ngs uuuuu | 13 -50 10 221 8 | 16 22
sio xxxxx | 80 105 45 -34 -4 | 37 42
Table 7.2402.2 GPS week: 2402 Day: 2 MJD: 61060.500
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 | -1 -3 140 30 11 | -9 18
emr uuuuu | 50 14 -108 83 -20 | -15 23
esa uuuuu | -11 -5 -34 -49 3 | -3 15
gfz uuuuu | -44 -16 -1 -133 -7 | 12 20
grg uuuuu | -18 -5 28 22 3 | 4 15
igr xxxxx | -23 -11 69 -47 12 | -1 17
irf xxxxx | -4 2 -17 -12 -3 | 1 16
jgx uuuuu | -1 -18 55 -109 1 | 5 17
jpl uuuuu | 12 23 -3 4 -20 | 10 25
mit uuuuu | 16 5 -54 20 -10 | 18 24
ngs uuuuu | 7 34 -177 252 17 | 13 19
sio xxxxx | -10 43 61 -152 -22 | 34 39
Table 7.2402.3 GPS week: 2402 Day: 3 MJD: 61061.500
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 | 23 -42 84 -9 5 | -10 18
emr uuuuu | 33 8 -96 48 -12 | -21 25
esa uuuuu | -15 -1 -23 -26 1 | -6 14
gfz uuuuu | -5 -7 116 42 -1 | 8 15
grg uuuuu | -23 23 -81 -32 4 | 1 13
igr xxxxx | -7 5 -16 31 10 | -3 15
irf xxxxx | -5 14 -16 -9 1 | -2 14
jgx uuuuu | -11 -18 28 -65 -3 | 2 14
jpl uuuuu | 3 17 54 -45 0 | 2 14
mit uuuuu | -5 23 -29 -7 -9 | 15 20
ngs uuuuu | 14 23 -97 162 2 | 11 16
sio xxxxx | 41 102 24 147 0 | 27 32
Table 7.2402.4 GPS week: 2402 Day: 4 MJD: 61062.500
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 | -6 -11 119 30 7 | -10 18
emr uuuuu | 43 29 -64 155 -2 | -22 28
esa uuuuu | 3 -5 -4 -44 1 | -6 14
gfz uuuuu | -30 -8 -4 -22 -2 | 8 15
grg uuuuu | -11 9 -8 -37 5 | 2 12
igr xxxxx | -18 -3 23 -99 5 | -1 13
irf xxxxx | -1 -1 -18 -16 3 | -2 14
jgx uuuuu | -5 -20 31 -103 1 | 1 15
jpl uuuuu | 6 6 -30 -27 -13 | 1 14
mit uuuuu | 7 -6 -59 57 -1 | 14 21
ngs uuuuu | 6 41 -39 58 5 | 11 16
sio xxxxx | 112 54 -123 -108 -2 | 27 32
Table 7.2402.5 GPS week: 2402 Day: 5 MJD: 61063.500
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 | -11 -20 36 -13 8 | -10 18
emr uuuuu | 20 6 -114 115 -14 | -24 29
esa uuuuu | -9 8 11 -26 3 | -7 15
gfz uuuuu | -12 -3 14 43 -10 | 7 15
grg uuuuu | -17 5 37 -41 7 | 1 12
igr xxxxx | -6 -6 41 -56 0 | -1 13
irf xxxxx | -2 0 -13 -25 3 | -4 14
jgx uuuuu | 0 -21 36 -86 5 | 0 15
jpl uuuuu | -6 7 -61 -80 -8 | -2 16
mit uuuuu | 8 18 10 77 -7 | 12 20
ngs uuuuu | 44 17 -72 91 2 | 11 16
sio xxxxx | 39 71 -3 -88 -9 | 26 31
Table 7.2402.6 GPS week: 2402 Day: 6 MJD: 61064.500
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 | 3 -29 77 -54 6 | -10 18
emr uuuuu | 16 -6 -58 71 -2 | -26 30
esa uuuuu | -10 13 26 35 3 | -8 14
gfz uuuuu | -22 6 -214 95 -6 | 5 12
grg uuuuu | -3 0 0 -69 4 | 1 12
igr xxxxx | -11 -4 4 -3 -3 | -2 13
irf xxxxx | -2 6 -7 -21 7 | -4 13
jgx uuuuu | 5 -2 64 -91 2 | -1 13
jpl uuuuu | -7 4 27 -47 -9 | -3 15
mit uuuuu | -20 12 -65 86 3 | 10 17
ngs uuuuu | 52 4 99 12 1 | 11 16
sio xxxxx | -51 54 88 -18 -10 | 24 28
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