[IGSREPORT-27631] Wk 2132 IGS Final Orbits
acc
acc at igs.org
Thu Dec 3 17:56:52 PST 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2132 (Nov 15, 2020 - Nov 21, 2020)
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:
igs2132[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2132[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2132[0-6].cls IGS GPS clock combination summary report.
igs21327.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21327.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, 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.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
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 | 21 21 ALIC ANKR ASCG ASPA AUCK BAKO BJFS BOR1 BRAZ
0 | COD | BRST CCJ2 CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GRAZ
0 | COD | GUAT GUUG HOFN HYDE INVK KARR KERG KRGG LHAZ MATE
0 | COD | MAYG MQZG NICO NIST NRMD NYA1 NYAL OHI3 PARC PERT
0 | COD | POVE REYK RIOP SALU SAVO SFER SSIA STK2 SUWN SYOG
0 | COD | THTI TIXI TLSE TRO1 TSKB UFPR WARK WILL WTZR XMIS
0 | COD | ALIC ANKR ASCG ASPA AUCK BAKO BJFS BOR1 BRAZ BRST
0 | COD | CCJ2 CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUAT GUUG
0 | COD | HOFN HYDE INVK KARR KERG KRGG LHAZ MATE MAYG MQZG
0 | COD | NICO NIST NRMD NYA1 NYAL OHI3 PARC PERT POVE REYK
0 | COD | RIOP SALU SAVO SFER SSIA STK2 SUWN SYOG THTI TIXI
0 | COD | TLSE TRO1 TSKB UFPR WARK WILL WTZR XMIS
0 | EMR | GRAZ GRAZ
0 | ESA | DGAR PTBB DGAR PTBB
0 | GFZ | DGAR DGAR GRAZ REUN
0 | GRG | 13 13 MCM4 WUH2 CPVG MCM4 STJO WUH2
0 | JPL | 21 21
1 | COD | ALIC ANKR ASCG ASPA AUCK BARH BJFS BOR1 BRAZ BRST
1 | COD | CCJ2 CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUUG HOFN
1 | COD | HRAO HYDE INVK KARR KERG KRGG LHAZ MAG0 MATE MAYG
1 | COD | NICO NRIL NRMD NYA1 NYAL OHI3 PARC PERT POVE REYK
1 | COD | RIOP SALU SAVO SFER SGOC SOFI SSIA STK2 SUWN SYOG
1 | COD | THTI TIXI TLSE TRO1 TSKB UFPR WARK WILL XMIS ALIC
1 | COD | ANKR ASCG ASPA AUCK BARH BJFS BOR1 BRAZ BRST CCJ2
1 | COD | CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUUG HOFN HRAO
1 | COD | HYDE INVK KARR KERG KRGG LHAZ MAG0 MATE MAYG NICO
1 | COD | NRMD NYA1 NYAL OHI3 PARC PERT POVE REYK RIOP SALU
1 | COD | SAVO SFER SOFI SSIA STK2 SUWN SYOG THTI TIXI TLSE
1 | COD | TRO1 TSKB UFPR WARK WILL XMIS
1 | EMR | GRAZ CRO1 GRAZ
1 | ESA | 21 CHUR PTBB PTBB
1 | GFZ | SGOC GRAZ SGOC
1 | GRG | 21 NRIL
2 | COD | ALIC ANKR ASCG ASPA AUCK BAKO BARH BJFS BOR1 BRAZ
2 | COD | BRST CCJ2 CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUUG
2 | COD | HOFN HYDE INVK IRKJ KARR KERG KRGG LHAZ MATE MAYG
2 | COD | NICO NRMD NYA1 NYAL OHI3 PARC PERT POVE REYK RIOP
2 | COD | SALU SAVO SFER SOFI SSIA STK2 SYOG THTI TIXI TLSE
2 | COD | TRO1 TSKB UFPR WARK WILL WTZR XMIS ALIC ANKR ASCG
2 | COD | ASPA AUCK BAKO BARH BJFS BOR1 BRAZ BRST CCJ2 CHTI
2 | COD | CKIS CPVG DAEJ GLSV GMSD GRAS GUUG HOFN HYDE INVK
2 | COD | KARR KERG KRGG LHAZ MATE MAYG NICO NRMD NYA1 NYAL
2 | COD | OHI3 PARC PERT POVE REYK RIOP SALU SAVO SFER SOFI
2 | COD | SSIA STK2 SYOG THTI TIXI TLSE TRO1 TSKB UFPR WARK
2 | COD | WILL WTZR XMIS
2 | EMR | GRAZ GRAZ IRKJ
2 | ESA | HOB2 PTBB HOB2 PTBB
2 | GRG | IRKJ MCM4 NRMD DARW IRKJ MCM4 NRMD
2 | JPL | KOUC MATE KOUC MATE
3 | COD | ALIC ANKR ASCG ASPA AUCK BAKO BARH BJFS BOR1 BRAZ
3 | COD | BRST CCJ2 CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUUG
3 | COD | HOFN HYDE INVK KARR KERG KRGG LHAZ MANA MATE MAYG
3 | COD | NICO NRMD NYA1 NYAL OHI3 PARC PERT POVE REYK RIOP
3 | COD | SALU SAVO SFER SOFI SSIA STK2 SYOG TEHN THTI TIXI
3 | COD | TLSE TRO1 TSKB UFPR WARK WILL WTZR XMIS ALIC ANKR
3 | COD | ASCG ASPA AUCK BAKO BARH BJFS BOR1 BRAZ BRST CCJ2
3 | COD | CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUUG HOFN HYDE
3 | COD | INVK KARR KERG KRGG LHAZ MANA MATE MAYG NICO NRMD
3 | COD | NYA1 NYAL OHI3 PARC PERT POVE REYK RIOP SALU SAVO
3 | COD | SFER SOFI SSIA STK2 SYOG TEHN THTI TIXI TLSE TRO1
3 | COD | TSKB UFPR WARK WILL WTZR XMIS
3 | EMR | GRAZ GRAZ
3 | ESA | PTBB PTBB
3 | GFZ | 13 13
3 | GRG | 13 13 DJIG KIT3 MCM4 SVTL DJIG KIT3 MCM4 SVTL
3 | JPL | MATE MCM4 NRMD MATE MCM4 NRMD
4 | COD | ALIC ASCG ASPA AUCK BAKO BARH BJFS BOR1 BRAZ BRST
4 | COD | CCJ2 CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUAT GUUG
4 | COD | HOFN HYDE INVK KARR KERG KIT3 KRGG LHAZ MANA MATE
4 | COD | MAYG NICO NIST NRMD NYA1 NYAL OHI3 PARC PERT POVE
4 | COD | REYK RIOP SALU SAVO SFER SOFI SSIA STK2 SUWN SYOG
4 | COD | TEHN THTI TIXI TLSE TRO1 TSKB UFPR WARK WILL WTZR
4 | COD | XMIS ALIC ASCG ASPA AUCK BAKO BARH BJFS BOR1 BRAZ
4 | COD | BRST CCJ2 CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUAT
4 | COD | GUUG HOFN HYDE INVK KARR KERG KRGG LHAZ MANA MATE
4 | COD | MAYG NICO NIST NRMD NYA1 NYAL OHI3 PARC PERT POVE
4 | COD | REYK RIOP SALU SAVO SFER SOFI SSIA STK2 SUWN SYOG
4 | COD | TEHN THTI TIXI TLSE TRO1 TSKB UFPR WARK WILL WTZR
4 | COD | XMIS
4 | EMR | GRAZ GRAZ HARB
4 | ESA | PTBB PTBB
4 | GFZ | NRMD JOG2 NRMD
4 | GRG | 13 13 KIT3 MCM4 SVTL DARW KIT3 MCM4 SVTL
4 | JPL | 21 21 BADG KOUC MATE BADG KOUC MATE
4 | MIT | 21
5 | COD | ALIC ANKR ARTU ASCG ASPA AUCK BADG BAKO BARH BJFS
5 | COD | BOR1 BRAZ BRST CCJ2 CHTI CKIS CNMR CPVG DAEJ GLSV
5 | COD | GMSD GRAS GUUG HOFN HYDE INVK KARR KERG KRGG LHAZ
5 | COD | MATE MAYG NICO NRMD NYA1 NYAL OHI3 PARC PERT POVE
5 | COD | REYK RIOP SALU SAVO SFER SOFI SSIA STK2 SUWN SYOG
5 | COD | TEHN THTI TIXI TLSE TRO1 TSKB UFPR WARK WILL WTZR
5 | COD | XMIS ALIC ANKR ARTU ASCG ASPA AUCK BADG BAKO BARH
5 | COD | BJFS BOR1 BRAZ BRST CCJ2 CHTI CKIS CNMR CPVG DAEJ
5 | COD | GLSV GMSD GRAS GUUG HOFN HYDE INVK KARR KERG KRGG
5 | COD | LHAZ MATE MAYG NICO NRMD NYA1 NYAL OHI3 PARC PERT
5 | COD | POVE REYK RIOP SALU SAVO SFER SOFI SSIA STK2 SUWN
5 | COD | SYOG TEHN THTI TIXI TLSE TRO1 TSKB UFPR WARK WILL
5 | COD | WTZR XMIS
5 | EMR | 8 8 GRAZ GRAZ HARB
5 | ESA | PTBB CHUR PTBB
5 | GFZ | NRC1 NRC1
5 | GRG | 8 13 8 13 MCM4 SVTL MCM4 SVTL
5 | JPL | SVTL NRIL SVTL
6 | COD | ALIC ANKR ASCG ASPA AUCK BAKO BARH BJFS BOR1 BRAZ
6 | COD | BRST CCJ2 CHTI CKIS CPVG DAEJ GLSV GMSD GRAS GUAT
6 | COD | GUUG HOFN HYDE INVK KARR KERG KRGG LHAZ MATE MAYG
6 | COD | NICO NIST NRMD NYA1 NYAL OHI3 PERT POVE REYK SALU
6 | COD | SAVO SFER SOFI SSIA STK2 SUWN TEHN THTI TIXI TLSE
6 | COD | TRO1 TSKB UFPR WARK WILL WTZR XMIS ALIC ANKR ASCG
6 | COD | ASPA AUCK BAKO BARH BJFS BOR1 BRAZ BRST CCJ2 CHTI
6 | COD | CKIS CPVG DAEJ GLSV GMSD GRAS GUAT GUUG HOFN HYDE
6 | COD | INVK KARR KERG KRGG LHAZ MATE MAYG NICO NIST NRMD
6 | COD | NYA1 NYAL OHI3 PERT POVE REYK SALU SAVO SFER SOFI
6 | COD | SSIA STK2 SUWN TEHN THTI TIXI TLSE TRO1 TSKB UFPR
6 | COD | WARK WILL WTZR XMIS
6 | EMR | GRAZ GRAZ
6 | ESA | PTBB PTBB
6 | GRG | 13 13 SVTL WIND
6 | JPL | MATE MATE
5. 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.
6. 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
----+--------+---------------
5 | MIT | 8
5 | NGS | 8
7. 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 G08 | | | | | | | 4 |
PRN G14 | | | 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.
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 | .4 .0 1.0 0 -1 4 -.48
EMR | 0 | 1.5 12.3 15.0 2 11 5 -.03
ESA | 0 | .2 .1 .9 -36 16 3 -.35
GFZ | 0 | .1 -.3 .5 0 -5 18 -.42
GRG | 0 | 2.0 7.9 2.8 4 -24 6 -.12
JPL | 0 | 2.3 1.1 8.7 13 6 34 -.23
MIT | 0 | 7.0 5.5 4.7 27 -14 15 -.08
NGS | 0 | -1.6 -1.1 2.4 11 -6 27 -.23
SIO | 0 | 2.2 8.0 12.1 128 -48 31 -.65
COD | 1 | .4 .0 .9 0 -1 6 -.43
EMR | 1 | 5.1 10.2 21.3 -10 13 22 -.04
ESA | 1 | .2 -.7 .3 -23 21 -10 -.43
GFZ | 1 | .2 -.2 .6 -2 -4 16 -.30
GRG | 1 | -.8 6.3 8.9 -4 -37 18 -.01
JPL | 1 | 3.9 3.6 15.7 17 -1 18 -.13
MIT | 1 | 8.2 7.1 11.7 5 -28 -37 -.12
NGS | 1 | -2.2 4.4 12.6 44 -19 35 -.15
SIO | 1 | 1.9 8.5 16.8 124 -48 11 -.46
COD | 2 | .3 -.0 .9 -1 -1 4 -.39
EMR | 2 | 5.9 9.1 20.3 -4 13 18 .0
ESA | 2 | .4 -.7 1.0 -26 12 -15 -.24
GFZ | 2 | .2 -.2 .6 -9 -3 11 -.35
GRG | 2 | -.2 6.9 19.4 -6 -26 12 -.11
JPL | 2 | 8.8 .1 14.0 15 -2 12 -.35
MIT | 2 | 8.4 6.6 17.5 8 -20 4 -.11
NGS | 2 | 5.7 2.6 3.9 8 -27 7 -.14
SIO | 2 | 3.6 8.7 24.2 144 -98 55 -.56
COD | 3 | .2 -.0 .7 -1 -2 1 -.31
EMR | 3 | 5.6 6.8 24.1 -5 22 4 -.10
ESA | 3 | .5 -.5 1.3 -41 6 -19 -.44
GFZ | 3 | .1 -.3 .7 7 -6 20 -.44
GRG | 3 | 1.5 5.6 21.6 4 -37 8 -.05
JPL | 3 | 6.3 -1.2 20.4 7 -1 40 -.13
MIT | 3 | 10.4 5.2 15.8 1 -23 -1 -.12
NGS | 3 | 3.8 2.6 2.1 5 -25 9 -.30
SIO | 3 | 4.7 6.6 30.4 211 -176 45 -.18
COD | 4 | .3 -.0 .6 -1 -1 3 -.27
EMR | 4 | 8.7 7.4 25.0 5 4 10 -.17
ESA | 4 | .0 -1.0 1.1 -18 6 -8 -.39
GFZ | 4 | .1 -.2 .8 6 -12 17 -.30
GRG | 4 | 4.0 5.7 23.1 9 -41 12 -.21
JPL | 4 | 9.9 1.2 19.1 16 4 27 -.28
MIT | 4 | 10.6 6.9 15.3 -54 -44 -71 -.14
NGS | 4 | 7.4 4.8 -2.5 9 -2 12 -.12
SIO | 4 | 4.8 6.8 22.7 122 -103 61 -.50
COD | 5 | .2 -.0 .5 0 0 5 -.19
EMR | 5 | 5.6 11.9 21.4 2 0 9 -.06
ESA | 5 | .3 -.9 1.0 -29 4 -8 -.21
GFZ | 5 | -.2 -.1 .7 7 -2 16 -.26
GRG | 5 | 4.0 6.1 19.1 -5 -32 13 .05
JPL | 5 | 7.9 .3 10.7 20 2 4 -.13
MIT | 5 | 8.7 5.4 14.3 1 -28 30 -.03
NGS | 5 | 2.5 .2 5.4 -9 -30 3 -.12
SIO | 5 | 3.4 5.1 29.6 77 -95 37 -.42
COD | 6 | .2 .0 .4 0 0 6 -.12
EMR | 6 | 8.1 11.5 25.0 -3 -2 26 -.17
ESA | 6 | .1 -.7 1.2 -39 18 -2 -.23
GFZ | 6 | .2 -.8 .0 -1 -13 33 -.18
GRG | 6 | 3.5 2.5 23.7 -11 -29 4 .05
JPL | 6 | 8.0 6.9 20.5 20 16 -6 -.24
MIT | 6 | 6.9 8.9 18.5 -20 -15 50 .02
NGS | 6 | 2.2 -3.4 4.5 -16 -11 19 .04
SIO | 6 | 4.7 8.3 28.7 133 -130 49 -.33
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://igs.org/pub/station/general/igs14.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 1.2132.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2132.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 2.2132.[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 3.2132.[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 5.2132.0-6). 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 2132 summary. (Nov 15, 2020 - Nov 21, 2020)
Table 1.2132.a GPS week: 2132 MJD: 59168.000-59174.000
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 728| 0 0 4 18 10 6 -.07 8 7 | -446 -260 6 81
| 0 0 1 16 16 11 .03 | 175 295
emr 81| 0 0 8 -13 -3 -4 .12 13 13 | 174550 227 18 95
| 0 1 1 11 9 16 .02 | 22265 926
esa 148| 0 0 4 6 8 -8 -.04 11 10 | -715 -1075 7 72
| 0 0 1 10 7 14 .01 | 384 664
gfz 214| -1 0 0 7 2 -9 .13 10 10 | -613 335 11 74
| 1 0 2 10 10 15 .03 | 372 515
grg 110| 0 0 0 3 11 -14 -.10 11 9 | -179 79 9 130
| 0 0 3 12 10 13 .01 | 164 199
igr n/a| -1 0 -3 11 1 -2 .05 4 4 | 753 176 11 100
| 0 0 1 11 4 12 .02 | 887 907
jpl 80| 0 0 4 12 9 3 .17 10 10 | 2659 223 9 80
| 1 0 0 10 5 18 .01 | 976 926
mit 362| 0 0 -3 -22 -15 -8 -.02 6 6 | -33 192 23 1300
| 0 0 0 26 11 26 .01 | 842 728
ngs 201| 0 0 -6 -3 4 -7 -.03 9 9 | -31 -48492 1044 2083
| 1 0 3 19 20 17 .02 | 1303 127541
sio 409| 1 0 -9 1 -4 39 -.05 10 9 | --- --- --- ---
| 0 0 1 51 21 24 .02 | --- ---
Table 1.2132.b GPS week : 2132 MJD: 59168.000-59174.000
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 | 6 4 3 4 4 4 3 |
3 | 3 3 3 3 3 3 3 |
4 | 3 3 3 3 4 3 4 |
5 | 3 3 3 3 4 3 3 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 4 4 3 |
8 | 3 3 3 3 3 6 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 5 4 4 4 5 4 4 |
12 | 3 3 3 3 3 3 3 |
13 | 3 3 3 3 3 3 3 |
14 | --- --- 0 0 7 8 7 |
15 | 2 3 3 3 2 2 2 |
16 | 4 3 4 4 4 3 4 |
17 | 3 3 3 3 3 3 3 |
18 | 5 5 6 5 5 6 6 |
19 | 3 3 3 4 3 4 3 |
20 | 3 4 3 3 3 3 3 |
21 | 3 3 3 0 5 4 4 |
22 | 3 3 3 3 3 3 3 |
23 | 3 3 3 3 3 3 3 |
24 | 3 4 3 4 4 3 3 |
25 | 3 3 3 4 4 3 4 |
26 | 4 9 5 4 4 3 4 |
27 | 4 3 3 3 3 3 3 |
28 | 3 3 3 3 3 3 3 |
29 | 3 3 3 3 4 3 4 |
30 | 4 4 4 4 4 4 4 |
31 | 4 4 4 4 5 4 3 |
32 | 3 3 3 3 3 2 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 2.2132.0 GPS week: 2132 Day: 0 MJD: 59168.000
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 727| 0 0 3 -13 -18 -4 -.11 9 8 | -326 -536 6 80
emr 81| 0 0 10 -8 -1 -13 .15 13 13 | 161208 922 18 103
esa 149| 0 0 6 -1 9 5 -.02 10 10 | -732 -1034 7 66
gfz 216| -2 0 0 7 6 -25 .15 10 11 | -446 47 11 74
grg 110| 1 0 -4 23 21 -14 -.12 12 10 | -275 305 11 147
igr n/a| -1 0 -2 -2 3 -22 .06 4 4 | 438 821 11 102
jpl 80| 1 0 4 1 14 18 .16 10 10 | 2251 889 9 93
mit 362| 0 0 -3 28 -6 -7 -.02 6 6 | -276 734 25 1152
ngs 206| -1 0 -2 -26 4 7 -.02 8 8 | -515 -302 829 1802
sio 431| 0 0 -7 -25 -1 12 -.04 9 9 | --- --- --- ---
Table 2.2132.1 GPS week: 2132 Day: 1 MJD: 59169.000
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 727| 0 0 4 15 -1 19 -.09 7 7 | -417 -432 7 84
emr 81| 0 0 8 -22 0 16 .12 12 12 | 161884 1115 19 103
esa 149| -1 0 4 -1 -2 0 -.03 11 11 | -430 -1741 8 116
gfz 213| 0 0 0 24 2 -9 .18 9 9 | -672 220 13 89
grg 112| 1 0 -2 10 9 13 -.12 11 10 | 30 -85 10 134
igr n/a| -1 0 -3 22 9 8 .09 4 4 | 1253 505 12 106
jpl 80| -1 0 5 8 7 25 .17 10 10 | 2833 1158 10 97
mit 362| 0 0 -3 -21 -14 -47 -.03 6 6 | 30 404 26 1293
ngs 196| 0 0 -4 22 6 0 -.03 9 8 | -436 -404 1051 2000
sio 429| 1 0 -8 -45 15 19 -.03 9 9 | --- --- --- ---
Table 2.2132.2 GPS week: 2132 Day: 2 MJD: 59170.000
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 728| 0 -1 6 41 21 -9 -.09 8 7 | -663 -85 7 78
emr 81| 0 0 9 -15 -15 4 .10 13 13 | 162218 159 21 67
esa 149| -1 0 4 20 0 -19 -.05 11 10 | -818 -1399 7 63
gfz 213| -1 0 1 11 -10 -19 .12 10 11 | -639 620 12 71
grg 113| 0 0 0 5 5 -12 -.10 10 10 | -190 24 10 113
igr n/a| 0 0 -2 14 -3 -11 .05 4 4 | 1084 -129 12 96
jpl 80| 0 0 4 29 0 -6 .20 9 9 | 3198 171 8 71
mit 362| 0 0 -3 -28 -6 -10 -.03 6 5 | 798 -170 23 1530
ngs 200| 0 -1 -10 9 19 4 -.02 10 10 | -539 -299 1139 2131
sio 425| 1 0 -7 -61 -2 85 -.05 10 9 | --- --- --- ---
Table 2.2132.3 GPS week: 2132 Day: 3 MJD: 59171.000
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 731| 0 0 4 20 19 20 -.06 7 7 | -448 -366 7 83
emr 81| 0 0 6 -29 -15 -21 .15 13 13 | 162635 385 19 96
esa 149| 0 0 4 -8 7 -25 -.04 11 11 | -1095 -131 7 63
gfz 216| -3 0 3 -3 1 -13 .10 11 10 | -215 -164 11 73
grg 112| 1 0 1 -10 16 -19 -.10 10 9 | -99 -176 8 126
igr n/a| -1 0 -4 1 0 -2 .05 4 4 | 1259 623 11 94
jpl 80| 0 0 4 0 15 -13 .17 9 9 | 3636 351 10 87
mit 362| 0 0 -4 -20 -3 9 -.02 6 6 | 722 586 22 1116
ngs 203| 0 0 -7 -10 5 -20 -.01 9 9 | -477 -335 854 2021
sio 305| 1 0 -11 63 -49 52 -.08 12 11 | --- --- --- ---
Table 2.2132.4 GPS week: 2132 Day: 4 MJD: 59172.000
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 731| 0 0 3 23 5 7 -.06 7 7 | -676 213 7 85
emr 81| 0 -1 7 -20 8 -6 .12 13 13 | 207425 -430 20 118
esa 149| -1 0 3 11 20 9 -.05 11 10 | -914 -681 8 66
gfz 215| -2 -1 4 1 22 -21 .13 11 11 | -1070 1028 12 71
grg 111| 1 0 1 10 0 -18 -.09 12 9 | -240 348 10 134
igr n/a| -1 0 -1 -3 -1 0 .03 5 5 | 1335 -175 12 106
jpl 80| 1 0 4 14 10 -5 .16 10 10 | 3305 -410 11 74
mit 362| 0 0 -2 -59 -33 -25 -.03 6 6 | 597 -359 23 1274
ngs 200| 0 0 -11 4 34 12 -.01 10 9 | -688 -161 1196 2501
sio 430| 0 0 -9 48 -7 43 -.08 10 9 | --- --- --- ---
Table 2.2132.5 GPS week: 2132 Day: 5 MJD: 59173.000
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 727| 0 0 2 26 11 4 -.03 7 7 | -187 -580 7 83
emr 81| 0 2 7 -3 7 13 .10 14 14 | 206803 -1485 18 98
esa 148| -1 0 4 11 11 -2 -.04 11 11 | 4 -1969 8 67
gfz 212| -1 0 1 14 1 17 .12 10 9 | -160 -286 11 71
grg 109| 0 0 1 -8 28 -26 -.10 11 9 | -24 -33 9 137
igr n/a| 0 0 -2 23 0 15 .03 4 4 | 1047 -1567 11 95
jpl 80| -1 0 3 21 9 21 .15 10 10 | 2696 -1496 9 76
mit 362| 0 0 -2 -31 -15 -12 .00 6 6 | -566 -979 24 1330
ngs 200| 1 -1 -5 6 -31 -28 -.03 9 8 | 2919 -337729 928 1999
sio 425| 1 0 -7 -17 8 30 -.05 9 8 | --- --- --- ---
Table 2.2132.6 GPS week: 2132 Day: 6 MJD: 59174.000
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 725| -1 0 4 17 31 4 -.05 7 7 | -405 -35 7 76
emr 81| 0 2 8 1 -9 -25 .11 14 14 | 159683 928 17 81
esa 149| 0 -1 2 12 14 -25 -.03 11 10 | -1024 -572 7 64
gfz 215| 0 0 -4 -4 -6 6 .14 10 10 | -1089 883 12 71
grg 107| 0 0 5 -4 0 -23 -.10 11 9 | -455 172 9 122
igr n/a| -1 0 -5 20 0 -6 .05 4 4 | -1141 1160 11 106
jpl 80| 0 1 6 16 10 -17 .16 10 10 | 694 898 12 62
mit 362| 0 0 -2 -27 -25 35 -.01 6 6 | -1536 1133 23 1409
ngs 203| 0 -2 -6 -28 -6 -25 -.06 9 9 | -481 -214 1312 2132
sio 420| 1 0 -10 51 6 32 -.05 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 3.2132.0 GPS week: 2132 Day: 0 MJD: 59168.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 13 20 7 12 4 10 5 9 8 3 | 40 44 44 41 43 41 44 39 43 42 41
2E | 28 18 6 7 31 5 13 8 9 9 5 | 45 29 30 27 33 29 28 32 29 32 29
3 | 7 10 9 7 12 3 12 5 4 11 3 | 35 44 39 40 30 37 42 36 37 38 37
4 | 7 12 12 7 8 5 14 7 6 7 3 | 70 68 67 72 70 69 67 73 71 72 70
5M | 7 9 8 6 10 5 9 8 8 11 3 | 105 105 107 101 103 104 106 99 103 99 102
6E | 8 9 19 16 14 4 8 6 6 10 3 | 49 54 46 56 53 50 53 50 51 50 50
7E | 10 18 6 9 9 5 13 5 10 16 3 | 25 28 29 33 31 29 27 31 29 35 29
8M | 6 12 12 8 6 6 12 4 9 5 3 | 31 34 35 32 35 33 33 93 31 37 33
9 | 6 12 7 6 7 5 9 5 7 11 2 | 22 30 25 26 24 23 32 24 23 27 25
10 | 6 10 6 9 7 2 9 6 9 12 3 | 33 39 36 36 34 34 40 31 34 33 34
X11E | 10 10 11 15 12 10 11 6 19 --- 4 | 28 30 28 31 30 27 32 30 27 --- 28
12 | 9 15 6 8 11 4 10 6 10 8 3 | 49 52 52 52 50 53 53 52 55 54 52
13M | 10 10 6 7 8 3 12 8 8 6 3 | 41 48 41 43 42 42 49 45 41 46 43
15 | 7 10 5 7 6 4 7 4 6 5 2 | 92 95 93 94 91 91 94 89 91 93 92
16M | 8 22 6 12 12 2 11 5 6 10 3 | 22 24 25 25 23 24 24 24 24 25 22
17M | 7 12 7 9 9 4 9 4 6 6 2 | 30 32 27 34 33 29 31 30 31 34 30
18E | 13 19 15 21 18 5 12 8 16 7 5 | 52 53 55 59 55 54 54 50 51 55 52
19M | 9 16 6 9 10 3 7 5 4 9 3 | 21 20 21 23 20 20 22 21 21 24 20
20 | 7 9 5 8 10 6 7 6 9 11 2 | 26 28 27 28 26 27 29 30 30 35 28
21E | 8 12 8 8 16 4 10 5 9 7 3 | 21 21 17 20 24 19 17 18 19 24 19
22M | 6 10 11 7 9 3 10 5 8 5 2 | 57 59 57 59 60 59 62 59 58 59 58
23 | 6 10 9 8 9 5 13 5 8 7 3 | 64 63 64 68 68 66 63 65 69 68 65
24M | 9 10 14 10 14 6 10 5 6 6 3 | 56 60 59 58 58 58 60 58 60 64 58
25 | 10 12 12 11 6 4 9 5 8 9 3 | 23 27 26 26 24 24 27 23 24 27 24
26 | 8 13 13 10 6 4 12 7 10 11 3 | 65 64 52 49 64 64 48 65 64 52 64
27M | 9 15 12 13 8 4 11 4 11 6 3 | 19 22 24 24 22 22 20 20 25 25 20
28M | 9 11 7 8 10 4 10 4 7 6 2 | 23 24 23 24 21 21 27 23 20 25 22
29 | 8 16 5 8 10 3 9 6 11 8 3 | 21 23 19 23 22 22 23 22 26 24 21
30E | 9 10 17 16 15 6 9 6 7 11 4 | 31 32 31 42 34 34 34 34 32 36 33
31E | 5 13 10 11 15 5 7 9 9 15 3 | 51 52 50 52 47 49 52 51 54 58 51
32 | 6 11 8 11 6 3 10 6 10 5 3 | 24 32 27 25 24 23 32 22 24 25 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 10 12 4 10 6 8 9 |T 41 43 41 42 41 41 42 43 41 43 41
WRMS | 8 13 10 11 10 4 10 6 8 9 |NE 43 47 43 44 43 44 45 44 45 45 44
MEDI | 8 12 8 8 10 4 10 5 8 8 |MD 33 34 35 36 34 34 34 34 32 36 33
Table 3.2132.1 GPS week: 2132 Day: 1 MJD: 59169.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 17 20 10 12 5 9 5 6 8 3 | 37 42 37 39 37 37 40 36 36 40 36
2E | 10 15 9 8 12 4 10 9 7 11 3 | 36 37 38 34 41 36 36 38 36 40 36
3 | 5 7 11 6 7 4 9 4 7 5 2 | 29 34 28 30 29 30 37 31 31 32 30
4 | 8 12 11 7 10 5 16 7 6 7 3 | 48 45 46 49 50 47 46 49 49 50 48
5 | 6 8 9 7 8 4 9 6 10 13 3 | 84 84 84 82 82 83 83 80 80 79 81
6E | 8 9 18 14 14 4 7 5 8 9 3 | 44 49 42 48 46 46 48 45 44 46 44
7E | 9 12 7 10 10 4 13 7 8 8 3 | 27 28 29 36 31 32 29 33 32 36 30
8 | 6 12 12 9 7 5 11 4 8 7 3 | 58 63 61 63 60 58 68 128 60 68 59
9 | 8 11 9 7 6 5 9 4 6 13 2 | 26 34 27 29 28 27 35 25 27 27 27
10 | 6 10 6 8 8 3 11 7 6 11 2 | 31 36 31 34 32 33 39 30 30 32 31
X11E | 9 11 10 11 11 7 8 5 11 --- 3 | 26 28 27 28 28 27 30 26 24 --- 26
12 | 9 15 6 7 8 4 8 7 8 8 3 | 36 38 37 38 35 37 40 38 38 40 37
13 | 7 10 8 6 8 3 10 6 6 8 2 | 42 48 42 45 42 43 44 41 40 45 41
15 | 7 10 5 7 6 3 7 7 7 6 2 | 71 69 72 73 70 72 69 67 69 73 69
16 | 7 17 6 8 12 4 10 6 8 8 3 | 23 26 25 28 25 24 25 26 27 29 24
17 | 6 9 8 8 10 3 6 4 8 8 2 | 25 28 23 30 28 28 30 27 31 30 27
18E | 13 19 17 20 17 6 11 7 15 9 5 | 44 46 50 53 46 49 49 44 44 50 45
19 | 7 14 8 8 11 4 6 4 11 9 3 | 22 25 25 26 24 25 27 25 29 25 24
20 | 7 8 6 10 11 5 10 7 12 14 3 | 24 26 27 29 24 26 30 26 26 29 25
21E | 6 10 7 8 12 5 11 6 7 12 3 | 15 14 15 14 17 15 17 15 13 21 14
22 | 6 8 9 5 9 3 8 7 8 7 2 | 44 45 43 45 46 46 48 46 45 45 44
23 | 7 9 8 7 9 5 12 6 8 10 3 | 52 53 54 56 55 55 53 54 53 57 53
24 | 7 12 14 8 16 6 12 6 10 9 3 | 49 51 52 52 53 52 53 48 48 54 49
25 | 8 11 11 10 7 5 9 7 9 8 3 | 24 30 29 29 26 27 28 26 24 30 26
X26 | 9 15 --- --- 35 14 --- 12 7 --- 8 | 76 77 --- --- 93 70 --- 71 71 --- 75
27 | 7 13 13 8 9 4 10 4 11 6 3 | 25 27 27 25 26 27 28 24 30 30 25
28 | 6 11 8 8 11 3 7 5 9 8 2 | 22 30 27 29 24 26 30 27 26 31 25
29 | 7 18 6 7 10 4 11 6 9 9 3 | 22 22 21 25 23 25 23 23 25 27 22
30E | 7 9 16 8 13 6 10 6 8 8 3 | 33 37 32 35 33 37 38 37 37 38 34
31E | 8 17 9 14 14 5 8 9 11 14 4 | 60 62 58 67 59 61 61 60 61 62 60
32 | 6 11 9 9 8 3 10 5 5 6 2 | 28 34 28 26 27 28 36 26 27 32 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 11 9 11 4 10 6 9 9 |T 38 40 37 39 40 39 40 41 39 41 38
WRMS | 7 12 11 9 10 4 10 6 8 9 |NE 38 41 36 38 41 39 39 38 39 39 39
MEDI | 7 11 9 8 10 4 10 6 8 8 |MD 33 37 31 34 33 36 37 36 36 38 34
Table 3.2132.2 GPS week: 2132 Day: 2 MJD: 59170.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 11 19 13 10 5 9 4 8 7 3 | 32 35 34 35 31 32 36 31 34 38 32
2E | 8 13 9 9 9 5 10 7 8 13 3 | 18 19 21 20 20 19 19 20 23 28 19
3 | 6 9 9 8 9 5 8 4 8 7 2 | 37 42 38 38 37 38 38 37 40 43 38
4 | 7 12 11 8 11 5 16 6 8 7 3 | 44 43 42 41 49 44 41 50 50 52 45
5 | 8 10 8 6 10 3 7 5 9 11 2 | 94 93 96 94 92 93 97 90 95 95 93
6E | 7 9 19 13 13 5 7 7 8 11 3 | 35 38 33 42 40 36 39 34 38 42 36
7E | 8 14 9 8 11 6 12 8 14 12 3 | 27 28 29 31 29 32 27 34 37 38 30
8 | 7 14 12 11 10 4 9 5 9 9 3 | 88 85 88 95 88 86 93 112 88 98 88
9 | 7 9 9 8 5 5 7 4 7 11 2 | 27 35 29 29 30 30 36 28 34 35 30
10 | 6 10 5 8 9 4 9 6 9 15 3 | 24 30 26 25 24 24 28 23 25 31 24
X11E | 8 11 11 17 12 10 10 6 9 --- 4 | 38 44 41 39 44 42 45 41 41 --- 40
12 | 9 16 6 9 8 4 7 6 8 8 3 | 30 34 30 32 29 32 33 32 33 34 31
13 | 8 12 8 7 8 3 9 5 6 7 2 | 39 45 39 42 39 42 45 40 44 47 41
X14 | 4 --- --- --- --- >>>> --- --- --- --- 0 | 174 --- --- --- --- 9999 --- --- --- --- 174
15 | 6 10 5 8 6 4 7 5 8 6 2 | 84 87 87 87 86 85 85 84 85 87 85
16 | 9 22 7 9 15 4 11 7 11 9 3 | 20 22 19 23 21 20 22 23 22 30 20
17 | 7 9 7 10 9 4 7 4 7 8 2 | 23 27 25 30 25 26 28 26 28 30 25
18E | 13 21 18 21 17 7 13 6 24 7 5 | 37 42 43 49 41 41 39 37 47 41 39
19 | 7 13 6 10 10 4 9 5 6 11 3 | 18 20 20 24 19 20 21 21 22 26 19
20 | 5 10 7 12 9 4 8 7 13 14 3 | 18 23 21 22 21 20 20 20 28 23 19
21E | 7 10 7 8 14 5 10 5 12 12 3 | 17 16 11 14 18 17 14 16 17 28 19
22 | 6 7 8 8 10 4 7 5 11 7 2 | 61 63 62 62 62 60 63 62 62 68 62
23 | 7 10 11 8 8 5 12 5 11 9 3 | 50 51 52 50 54 49 49 52 59 56 52
24 | 6 9 14 9 7 3 12 4 11 8 3 | 48 50 46 49 49 48 49 46 52 51 48
25 | 10 13 12 10 7 4 9 8 8 8 3 | 23 28 26 24 23 24 28 24 28 28 24
X26 | 9 14 14 17 10 7 --- 10 11 --- 5 | 78 80 96 97 76 80 --- 78 80 --- 78
27 | 6 14 13 10 12 4 9 4 7 8 3 | 26 27 28 27 25 26 27 26 28 32 26
28 | 8 10 7 9 11 5 9 5 12 10 3 | 23 26 25 29 21 25 31 25 26 30 24
29 | 9 16 6 6 10 4 10 7 11 9 3 | 23 24 22 27 23 24 24 26 33 28 24
30E | 7 11 17 9 13 5 8 6 11 10 3 | 38 38 38 37 36 38 39 39 41 43 38
31E | 11 14 10 9 10 6 9 7 9 13 3 | 48 45 45 45 44 44 47 44 46 43 44
32 | 5 11 7 9 8 3 8 4 6 6 2 | 22 31 24 21 20 23 30 22 24 31 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 11 10 10 4 9 6 10 10 |T 42 41 39 41 39 39 39 40 42 43 43
WRMS | 7 13 10 11 10 4 9 5 10 9 |NE 48 42 41 41 39 39 37 39 43 40 49
MEDI | 7 11 9 9 10 4 9 5 9 9 |MD 32 35 33 35 31 32 36 34 37 38 32
Table 3.2132.3 GPS week: 2132 Day: 3 MJD: 59171.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 5 12 17 12 12 4 8 6 7 10 3 | 45 50 46 49 44 46 48 44 50 50 45
2E | 10 13 8 9 8 4 12 9 9 16 3 | 46 49 46 47 47 46 49 47 48 54 47
3 | 9 8 10 10 9 5 9 4 9 10 3 | 42 48 46 46 43 44 42 43 43 45 43
4 | 5 13 12 8 7 4 16 6 7 7 3 | 59 60 58 60 63 60 58 66 64 68 61
5 | 8 9 9 7 10 4 7 5 10 10 3 | 59 59 61 59 60 57 62 56 57 57 58
6E | 8 10 20 18 12 5 6 7 8 12 4 | 48 51 46 52 51 48 52 48 47 52 48
7E | 8 16 8 8 12 7 13 7 9 14 3 | 54 54 55 55 56 57 54 59 60 63 55
8 | 6 10 11 11 7 5 9 5 5 9 2 | 143 143 144 147 144 142 151 112 137 148 143
9 | 5 9 9 10 5 5 8 6 5 11 2 | 38 44 40 40 38 40 44 39 40 41 39
10 | 7 10 6 8 8 3 8 5 5 13 2 | 44 51 48 47 47 47 52 47 47 46 47
X11E | 9 11 9 16 12 7 7 8 17 --- 4 | 40 43 43 41 44 41 47 42 55 --- 43
12 | 9 16 6 9 8 4 6 6 11 11 3 | 46 52 48 51 48 49 52 47 48 54 48
13 | 7 11 7 5 6 3 11 6 11 10 3 | 45 51 46 46 45 48 53 47 47 51 47
X14 | 3 --- --- --- --- 39 --- --- --- --- 0 | 90 --- --- --- --- 9999 --- --- --- --- 90
15 | 8 8 5 11 7 3 6 5 9 9 2 | 54 58 55 54 51 52 57 52 52 51 53
16 | 5 22 6 11 12 3 11 7 9 9 3 | 45 47 47 47 47 47 49 48 49 49 46
17 | 7 12 7 8 11 4 9 5 11 6 3 | 48 50 46 50 45 47 50 46 48 50 47
18E | 14 19 16 24 19 5 10 5 11 9 5 | 48 49 52 52 49 51 53 48 52 54 49
19 | 8 14 7 10 10 4 8 5 11 16 3 | 48 49 47 49 45 47 50 46 48 53 47
20 | 6 9 6 8 10 3 8 8 9 12 3 | 36 40 40 41 39 39 43 39 41 40 39
X21E | 3 --- --- --- --- 25 --- --- --- --- 0 | 23 --- --- --- --- 26 --- --- --- --- 22
22 | 6 7 9 8 9 5 8 4 12 9 2 | 42 45 43 44 41 45 45 43 47 46 43
23 | 6 8 10 8 9 3 10 5 8 11 3 | 48 50 50 50 53 51 52 52 53 55 51
24 | 6 12 14 8 7 4 11 6 9 17 3 | 40 44 44 43 40 43 46 40 43 47 42
25 | 10 14 13 11 8 3 8 7 10 9 3 | 45 50 49 50 46 48 50 45 48 49 47
26 | 6 11 13 12 9 4 10 9 10 12 3 | 60 61 53 45 63 59 46 60 61 46 60
27 | 6 13 13 11 9 4 9 4 9 9 3 | 66 67 67 65 66 66 68 65 67 66 66
28 | 7 10 9 7 10 3 7 6 8 8 2 | 41 44 42 40 41 42 45 43 42 44 41
29 | 7 17 7 6 8 4 8 6 8 16 3 | 39 41 40 41 39 42 42 40 42 43 40
30E | 8 12 19 8 13 3 7 5 13 15 4 | 56 58 55 54 56 57 58 56 61 58 56
31E | 9 14 11 13 15 5 10 6 12 16 4 | 93 91 92 92 92 91 92 91 89 93 91
32 | 5 11 7 10 7 5 9 5 8 8 2 | 39 45 42 41 41 41 47 39 41 43 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 11 11 10 4 9 6 9 12 |T 52 54 53 53 52 52 55 51 54 55 52
WRMS | 7 13 11 10 9 4 9 6 9 11 |NE 49 50 47 47 47 47 48 47 48 48 50
MEDI | 7 11 9 9 9 4 8 6 9 10 |MD 46 50 47 49 47 47 50 47 48 51 47
Table 3.2132.4 GPS week: 2132 Day: 4 MJD: 59172.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 13 15 9 13 6 11 8 12 10 3 | 46 52 49 45 49 47 52 46 43 51 47
2E | 7 12 9 12 10 5 10 9 12 9 3 | 40 36 41 39 41 42 38 38 44 41 39
3 | 6 9 9 9 7 3 9 4 9 7 2 | 45 51 47 47 47 46 40 44 43 48 46
4 | 5 14 12 7 9 5 17 6 8 9 3 | 55 55 54 56 57 55 53 56 62 63 56
5 | 8 10 11 10 18 5 7 7 8 11 3 | 101 99 101 104 92 99 99 96 98 98 99
6E | 7 13 19 12 9 4 7 6 7 8 3 | 54 56 51 58 57 53 55 50 54 55 54
7 | 7 16 9 10 12 7 12 9 13 14 4 | 58 56 58 57 57 60 58 60 64 63 59
8 | 7 10 11 8 8 4 9 6 9 8 3 | 147 149 149 154 147 151 154 231 139 156 149
9 | 4 9 10 9 5 5 9 6 8 10 2 | 36 44 36 36 39 37 44 35 40 41 38
10 | 4 11 7 7 7 4 9 7 6 11 2 | 43 44 42 45 42 42 45 40 41 44 42
X11E | 9 13 12 17 13 9 10 9 14 --- 4 | 37 45 39 42 44 40 42 37 37 --- 39
12 | 8 15 6 9 8 3 8 6 10 8 3 | 43 45 43 46 44 44 45 41 45 42 43
13 | 6 12 9 9 5 4 10 6 6 9 2 | 53 58 52 57 55 56 57 53 57 55 55
X14 | 15 --- 15 15 --- 11 --- 8 13 --- 6 | 53 --- 50 47 --- 9999 --- 48 40 --- 51
15 | 6 9 7 8 7 3 7 4 7 6 2 | 89 90 91 92 90 90 88 88 88 91 90
16 | 5 22 7 11 13 5 11 6 9 6 3 | 36 37 36 37 39 35 40 35 35 38 36
17 | 8 12 9 9 10 4 6 7 9 9 3 | 40 39 41 44 40 40 43 38 42 41 40
18E | 13 21 19 25 19 6 12 5 14 7 5 | 54 54 57 60 55 55 57 52 55 57 54
19 | 8 17 8 13 11 5 5 5 10 11 3 | 37 37 38 42 39 40 39 36 39 40 38
20 | 7 12 8 9 8 4 9 9 9 12 3 | 36 35 37 42 38 37 39 37 37 40 37
21E | 8 9 11 9 29 8 13 9 13 12 4 | 26 32 27 31 35 30 26 27 27 32 27
22 | 7 10 9 8 8 4 7 5 13 5 3 | 64 68 67 65 65 63 69 63 60 66 65
23 | 5 13 12 8 9 3 10 6 8 8 3 | 61 60 62 65 65 62 61 62 63 65 62
24 | 8 11 15 12 7 3 12 5 8 8 3 | 53 56 53 57 56 55 56 53 54 59 55
25 | 11 15 14 11 7 4 10 6 7 10 3 | 43 44 42 45 42 42 43 39 42 45 42
26 | 6 14 13 19 8 6 11 7 8 9 3 | 74 73 66 67 73 72 46 69 72 44 73
27 | 7 11 13 10 10 4 9 4 6 6 3 | 59 62 63 62 60 63 64 59 62 62 61
28 | 7 14 9 9 10 3 7 5 10 7 3 | 39 41 40 43 39 40 44 37 39 43 40
29 | 9 17 7 10 9 7 11 6 14 12 3 | 37 38 37 40 38 39 39 35 45 40 38
30E | 8 11 18 15 17 6 9 5 10 12 4 | 106 103 102 106 102 104 105 104 103 110 104
31E | 9 10 11 17 17 5 10 8 12 23 4 | 72 77 73 78 73 75 77 75 80 86 76
32 | 7 11 8 10 7 5 10 4 9 6 2 | 41 46 39 39 39 40 46 37 39 41 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 11 11 12 5 10 6 10 10 |T 55 57 55 57 56 56 56 56 55 58 56
WRMS | 7 13 10 11 9 5 10 6 9 9 |NE 50 52 49 51 51 50 49 48 50 50 50
MEDI | 7 12 10 10 9 5 10 6 9 9 |MD 46 52 49 47 49 47 46 46 45 48 47
Table 3.2132.5 GPS week: 2132 Day: 5 MJD: 59173.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 15 19 10 10 5 10 6 7 13 3 | 27 31 27 23 24 27 30 27 26 32 26
2E | 10 17 8 8 6 5 11 6 10 10 3 | 36 38 34 40 34 36 36 31 36 35 34
X3 | 7 11 9 10 7 4 --- 6 8 6 3 | 18 27 21 21 19 20 --- 18 20 22 19
4 | 4 13 10 9 9 5 17 6 6 9 3 | 56 55 53 54 55 54 55 56 54 56 55
5 | 7 9 11 7 8 4 7 9 6 11 3 | 69 69 70 68 69 67 70 72 69 66 69
6E | 7 10 19 12 12 6 7 5 9 9 3 | 30 32 28 32 32 29 32 27 30 30 29
7 | 9 14 7 11 13 6 13 6 11 11 3 | 34 30 29 33 32 33 34 30 33 33 31
X8 | 7 11 11 --- 8 8 --- 2849 108 --- 5 | 129 127 131 --- 131 128 --- 9999 192 --- 128
9 | 3 10 10 10 6 5 9 5 6 8 2 | 18 28 20 18 18 18 28 18 19 20 19
10 | 4 9 6 6 6 3 8 6 6 13 2 | 15 25 16 19 17 17 23 18 15 23 17
X11E | 7 9 13 12 10 8 9 7 12 --- 3 | 27 31 31 35 31 29 30 26 30 --- 28
12 | 7 17 7 13 9 5 9 8 6 7 3 | 62 64 65 69 63 66 65 60 66 64 63
13 | 6 12 8 8 8 3 11 7 8 9 3 | 18 29 16 16 18 19 28 20 18 23 18
X14 | 13 --- 18 15 --- 8 --- 9 20 --- 7 | 80 --- 50 49 --- 9999 --- 45 51 --- 78
15 | 8 9 5 8 6 2 6 5 5 7 2 | 60 59 57 59 59 57 58 59 59 62 59
16 | 6 21 5 9 12 3 10 5 8 7 3 | 39 39 38 38 40 38 42 37 41 41 38
17 | 7 14 8 14 10 4 9 7 7 7 3 | 49 50 47 50 48 47 50 48 49 51 48
18E | 15 23 17 25 17 6 12 6 17 8 5 | 31 33 37 38 34 34 35 32 34 36 32
19 | 7 15 8 13 11 3 11 4 10 13 3 | 40 41 37 42 39 38 40 37 39 44 38
20 | 6 9 6 6 8 3 9 6 7 11 2 | 20 24 21 26 22 22 23 22 20 28 22
21E | 5 10 9 10 26 5 8 7 8 11 3 | 23 22 19 19 30 23 22 18 19 24 22
22 | 7 11 11 8 8 4 7 5 11 7 2 | 34 36 33 36 34 34 35 35 39 37 34
23 | 7 9 10 7 7 4 10 5 6 7 2 | 27 25 25 29 29 25 25 28 28 31 27
24 | 8 11 15 7 7 4 12 4 9 6 3 | 26 29 32 27 28 29 30 27 29 30 27
25 | 8 16 14 9 8 4 11 5 5 8 3 | 34 37 37 36 31 35 37 31 35 34 33
26 | 7 9 11 11 7 4 9 5 7 11 3 | 22 26 27 23 23 24 24 25 24 24 24
27 | 7 12 12 8 9 5 9 4 9 8 3 | 39 40 44 40 39 39 39 42 40 42 40
28 | 7 15 7 10 13 4 10 5 9 9 3 | 29 33 30 31 30 29 35 29 32 33 30
29 | 6 17 5 8 11 5 10 6 8 7 3 | 22 25 25 27 24 25 26 22 26 25 23
30 | 6 11 17 10 11 3 9 6 10 9 3 | 74 70 71 70 75 71 75 69 76 70 72
31 | 7 15 8 10 16 4 8 5 11 12 3 | 84 85 85 84 85 83 86 84 82 89 84
32 | 4 13 5 6 5 3 9 5 7 7 2 | 22 31 23 22 21 23 29 20 22 23 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 11 10 11 4 10 6 9 9 |T 40 41 39 37 39 39 39 35 42 38 40
WRMS | 7 14 11 9 9 4 10 6 8 8 |NE 35 35 33 34 31 32 35 32 33 34 35
MEDI | 7 12 9 10 9 4 9 6 8 9 |MD 31 33 32 35 32 33 35 30 33 33 31
Table 3.2132.6 GPS week: 2132 Day: 6 MJD: 59174.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 12 18 12 9 6 8 6 7 9 3 | 28 31 26 31 27 30 31 27 30 31 27
2E | 8 12 8 7 8 3 12 8 6 12 3 | 34 38 30 33 34 34 39 34 36 34 34
X3 | 6 9 6 9 7 3 --- 4 12 7 2 | 29 33 30 35 30 30 --- 30 29 29 30
4 | 4 14 10 9 9 5 19 5 8 7 3 | 71 70 68 72 70 71 70 73 72 73 71
5 | 7 9 8 9 8 5 8 6 10 8 2 | 104 102 106 104 103 102 105 103 103 103 103
6E | 9 10 19 20 13 5 12 6 9 11 4 | 30 33 25 38 29 30 32 30 33 34 30
7 | 5 14 8 9 12 5 12 6 10 9 3 | 45 42 41 44 45 43 44 44 43 46 43
8 | 5 10 10 9 6 5 7 4 9 6 2 | 250 250 253 256 251 250 259 582 225 260 251
9 | 5 10 8 7 9 3 8 5 7 11 2 | 24 30 27 26 22 25 30 23 25 25 24
10 | 4 11 6 7 7 3 10 6 8 10 2 | 24 30 25 25 26 24 30 27 24 25 25
X11E | 7 11 10 22 11 7 10 9 11 --- 4 | 35 35 37 38 37 33 36 31 37 --- 34
12 | 9 15 6 10 10 4 10 7 7 9 3 | 67 69 67 69 68 68 71 67 69 66 67
13 | 8 12 9 9 6 3 10 6 7 10 3 | 28 36 28 30 30 31 36 33 32 36 31
X14 | 14 --- 16 21 --- 10 --- 7 17 --- 7 | 120 --- 58 55 --- 9999 --- 53 53 --- 120
15 | 6 9 5 8 5 3 6 6 4 7 2 | 92 94 93 94 93 92 93 92 93 96 93
16 | 6 23 5 13 12 3 10 6 10 9 3 | 38 39 39 38 40 38 41 38 40 40 38
17 | 8 13 7 8 9 4 8 5 11 6 3 | 53 53 50 52 51 50 53 52 50 55 51
18E | 13 28 18 22 16 7 12 7 21 9 5 | 33 38 41 41 40 39 38 36 42 38 36
19 | 7 15 8 8 8 4 10 5 10 10 3 | 45 44 40 46 45 43 45 41 43 49 43
20 | 4 12 6 9 10 4 9 5 7 11 2 | 22 23 22 27 27 24 25 25 26 27 24
21E | 7 9 9 7 21 5 9 4 8 12 3 | 19 16 15 18 22 20 16 15 17 22 18
22 | 7 9 8 11 7 4 9 6 10 7 3 | 56 59 56 58 59 57 58 59 59 62 58
23 | 5 11 10 8 8 5 9 6 8 8 2 | 48 47 46 49 53 47 46 50 51 54 49
24 | 7 12 15 5 6 3 10 5 6 7 3 | 35 36 35 36 35 34 37 35 35 37 35
25 | 9 19 13 14 14 4 12 6 6 10 4 | 37 41 38 41 39 37 39 34 37 36 36
26 | 5 14 11 12 8 5 11 5 8 14 3 | 45 45 44 42 46 46 34 46 46 34 46
27 | 6 12 12 7 8 4 8 3 9 6 2 | 81 81 79 78 81 79 81 78 81 80 79
28 | 8 12 7 9 14 5 10 5 10 7 3 | 35 33 32 35 30 34 36 32 30 33 32
29 | 7 15 7 9 13 6 11 8 14 8 3 | 32 31 29 32 33 31 32 31 35 33 31
30 | 8 14 18 7 21 3 10 5 7 10 4 | 56 54 53 54 55 53 54 54 52 55 53
31 | 7 13 9 11 9 7 7 5 5 11 3 | 75 75 77 74 77 74 76 75 72 72 75
32 | 6 12 7 5 5 4 9 6 7 7 2 | 24 29 22 23 24 23 30 24 22 20 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 11 10 11 4 10 6 9 9 |T 53 52 51 52 52 51 53 61 51 53 53
WRMS | 7 14 10 10 9 4 10 6 9 9 |NE 48 45 43 45 44 43 45 44 44 43 49
MEDI | 7 12 8 9 9 4 10 6 8 9 |MD 37 39 39 41 40 38 39 36 40 37 36
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 4.2132 GPS week: 2132 MJD: 59168.0-59174.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3000 |U 10 12 23 |U 12 16 53 |U 14 11 20 |
emr | emr 2960 |U 18 13 38 |U 18 22 54 |U 23 18 53 |
esa | esa 2989 | 15 14 25 |U 12 19 48 | 14 10 35 |
gfz | gfz 2975 |U 12 12 25 |U 11 17 47 |U 12 9 24 |
grg | grg 2958 |U 17 21 40 |U 12 17 49 | 28 18 59 |
igr | igr 2983 | 12 11 23 | 11 16 48 | 13 10 27 |
igs | igs 2999 | 12 11 22 | 11 16 49 | 14 10 25 |
jpl | jpl 2893 |U 17 14 33 | 15 20 52 |U 20 14 51 |
mit | mit 3003 |U 11 11 21 |U 12 14 48 |U 13 10 22 |
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 5.2132.0 GPS week: 2132 Day: 0 MJD: 59168.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 14 20 | 12 15 52 | 15 11 21 |
emr | emr 2976 | 22 18 43 | 17 18 52 | 20 16 54 |
esa | esa 2976 | 14 18 26 | 11 15 46 | 14 10 35 |
gfz | gfz 2976 | 10 13 22 | 10 13 46 | 12 9 26 |
grg | grg 2975 | 16 23 54 | 9 12 39 | 35 25 82 |
igr | igr 2953 | 11 13 21 | 11 14 47 | 13 10 29 |
igs | igs 2967 | 12 14 22 | 10 12 47 | 13 10 28 |
jpl | jpl 2976 | 18 16 30 | 13 17 43 | 18 12 56 |
mit | mit 2976 | 11 13 22 | 10 12 48 | 12 10 22 |
Table 5.2132.1 GPS week: 2132 Day: 1 MJD: 59169.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2965 | 12 15 29 | 10 14 55 | 12 9 16 |
emr | emr 2968 | 22 19 42 | 18 19 51 | 20 14 54 |
esa | esa 2880 | 16 16 31 | 11 19 51 | 10 9 24 |
gfz | gfz 2879 | 15 15 33 | 10 16 49 | 10 6 16 |
grg | grg 2967 | 14 17 30 | 9 14 50 | 27 17 58 |
igr | igr 2877 | 15 15 33 | 10 16 50 | 12 6 19 |
igs | igs 2965 | 14 15 28 | 10 14 50 | 12 8 21 |
jpl | jpl 2880 | 21 18 44 | 14 18 59 | 19 11 41 |
mit | mit 2976 | ---- ---- ---- | 9 13 54 | ---- ---- ---- |
Table 5.2132.2 GPS week: 2132 Day: 2 MJD: 59170.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 10 22 | 13 18 42 | 15 10 20 |
emr | emr 2976 | 16 10 42 | 20 24 44 | 22 17 64 |
esa | esa 2976 | 13 13 22 | 13 20 37 | 15 13 41 |
gfz | gfz 2976 | 8 7 17 | 11 18 33 | 12 9 25 |
grg | grg 2976 | 20 25 42 | 13 20 39 | 42 21 88 |
igr | igr 2976 | 9 9 19 | 12 18 36 | 14 12 32 |
igs | igs 2976 | 9 9 18 | 12 18 38 | 15 11 28 |
jpl | jpl 2880 | 13 14 31 | 15 21 42 | 21 15 51 |
mit | mit 2976 | 9 9 19 | 12 19 37 | 14 10 24 |
Table 5.2132.3 GPS week: 2132 Day: 3 MJD: 59171.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 11 11 27 | 13 14 67 | 16 13 22 |
emr | emr 2880 | 18 10 42 | 21 19 77 | 25 20 45 |
esa | esa 2880 | 15 11 30 | 15 15 63 | 17 11 34 |
gfz | gfz 2879 | 15 17 39 | 12 14 61 | 14 12 23 |
grg | grg 2879 | 17 23 44 | 13 15 68 | 28 18 58 |
igr | igr 2880 | 11 8 26 | 12 13 63 | 16 13 25 |
igs | igs 2880 | 12 9 26 | 13 13 62 | 16 12 24 |
jpl | jpl 2880 | 18 12 34 | 17 19 62 | 24 17 50 |
mit | mit 2880 | 11 10 27 | 13 12 63 | 14 12 18 |
Table 5.2132.4 GPS week: 2132 Day: 4 MJD: 59172.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 14 22 | 17 15 50 | 14 11 21 |
emr | emr 2976 | 22 16 30 | 22 28 51 | 31 21 58 |
esa | esa 3072 | 16 15 19 | 18 19 50 | 14 10 39 |
gfz | gfz 3072 | 14 12 20 | 17 19 51 | 12 9 28 |
grg | grg 2975 | 23 29 40 | 18 19 56 | 15 13 29 |
igr | igr 3072 | 13 13 19 | 15 15 46 | 12 11 29 |
igs | igs 3072 | 13 13 18 | 17 16 49 | 14 11 28 |
jpl | jpl 2976 | 20 20 32 | 20 21 48 | 19 14 54 |
mit | mit 3072 | 13 13 18 | 16 15 51 | 14 12 24 |
Table 5.2132.5 GPS week: 2132 Day: 5 MJD: 59173.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 8 10 19 | 8 21 63 | 12 12 18 |
emr | emr 2973 | 16 11 31 | 15 27 55 | 22 22 51 |
esa | esa 3072 | 13 10 27 | 8 24 51 | 15 9 34 |
gfz | gfz 2976 | 9 9 21 | 11 21 56 | 13 11 25 |
grg | grg 2966 | 16 20 50 | 8 22 57 | 23 14 46 |
igr | igr 3051 | 10 8 21 | 8 21 56 | 13 12 24 |
igs | igs 3066 | 10 8 20 | 7 21 57 | 13 11 21 |
jpl | jpl 2784 | 15 9 29 | 13 20 58 | 19 18 47 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
Table 5.2132.6 GPS week: 2132 Day: 6 MJD: 59174.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 11 21 | 12 15 41 | 14 10 24 |
emr | emr 2976 | 13 9 35 | 17 23 47 | 19 18 44 |
esa | esa 3072 | 15 11 23 | 12 20 40 | 13 9 41 |
gfz | gfz 3072 | 12 9 20 | 9 15 37 | 14 9 26 |
grg | grg 2971 | 13 7 22 | 13 15 37 | 24 17 54 |
igr | igr 3072 | 12 9 21 | 11 15 38 | 13 10 29 |
igs | igs 3072 | 12 8 19 | 11 16 38 | 13 8 28 |
jpl | jpl 2880 | 17 8 30 | 15 22 52 | 18 14 56 |
mit | mit 3072 | 12 8 21 | 11 16 39 | 13 9 24 |
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 6.2132 GPS week: 2132 MJD: 59168.500-59174.500
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 -20 -50 -9 5 | 8 23
| 16 18 39 74 4 | 4
emr uuuuu | -11 32 -7 214 -7 | 33 40
| 17 23 70 20 6 | 5
esa uuuuu | -31 -7 -10 -189 -3 | 20 27
| 6 7 45 47 5 | 4
gfz uuuuu | -15 -10 29 -73 -5 | 21 28
| 18 16 106 71 4 | 4
grg uuuuu | -23 -14 -53 -27 0 | -1 20
| 9 23 46 35 4 | 4
igr xxxxx | -6 -14 5 -63 2 | -3 18
| 10 11 53 49 4 | 4
irf xxxxx | 2 5 36 2 2 | -1 20
| 7 9 24 12 5 | 4
jpl uuuuu | 8 -25 50 -12 8 | 31 38
| 5 15 45 51 4 | 4
mit uuuuu | 35 36 48 45 2 | 20 28
| 11 27 48 40 2 | 4
ngs uuuuu | -7 -11 -25 50 -3 | 13 24
| 31 29 157 127 5 | 4
sio xxxxx | 61 -123 -149 -338 -10 | 51 56
| 53 27 80 49 9 | 7
Table 7.2132.0 GPS week: 2132 Day: 0 MJD: 59168.500
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 | 25 6 26 -128 0 | 8 17
emr uuuuu | -24 26 -16 220 -8 | 35 39
esa uuuuu | -23 -4 33 -89 6 | 20 23
gfz uuuuu | -35 -7 -67 -188 0 | 22 24
grg uuuuu | -30 -42 9 -62 -1 | -1 14
igr xxxxx | -10 8 -66 -68 6 | -3 12
irf xxxxx | -11 13 24 -3 3 | -2 13
jpl uuuuu | 2 -9 80 -68 3 | 30 33
mit uuuuu | 17 4 8 44 1 | 20 23
ngs uuuuu | 24 16 -70 241 -3 | 13 19
sio xxxxx | -2 -154 -119 -303 5 | 57 60
Table 7.2132.1 GPS week: 2132 Day: 1 MJD: 59169.500
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 | 12 -1 -54 -5 2 | 5 15
emr uuuuu | -31 59 -51 254 -18 | 32 37
esa uuuuu | -32 7 -5 -230 -4 | 18 20
gfz uuuuu | -28 -13 -33 -98 -2 | 20 22
grg uuuuu | -13 -2 -56 -6 3 | -4 13
igr xxxxx | -23 -18 -44 -89 2 | -6 12
irf xxxxx | 3 15 4 10 5 | -4 13
jpl uuuuu | 5 -28 87 -66 10 | 27 29
mit uuuuu | 47 36 -33 99 0 | 17 21
ngs uuuuu | -14 -60 155 33 -3 | 11 17
sio xxxxx | 1 -126 -50 -398 -23 | 55 57
Table 7.2132.2 GPS week: 2132 Day: 2 MJD: 59170.500
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 -29 -32 25 9 | 6 15
emr uuuuu | 0 48 -74 204 -7 | 33 37
esa uuuuu | -30 -7 -93 -213 -5 | 19 21
gfz uuuuu | -5 13 -128 -82 -12 | 21 24
grg uuuuu | -14 -10 0 -30 0 | -2 14
igr xxxxx | -12 -14 -1 -91 -4 | -5 12
irf xxxxx | 12 10 38 19 3 | -2 13
jpl uuuuu | 15 -40 44 -23 9 | 29 32
mit uuuuu | 43 36 50 85 3 | 18 22
ngs uuuuu | -60 -26 166 -22 -6 | 12 18
sio xxxxx | 51 -117 -245 -270 -14 | 53 56
Table 7.2132.3 GPS week: 2132 Day: 3 MJD: 59171.500
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 | -10 -38 -53 19 8 | 14 26
emr uuuuu | 8 42 -47 200 -1 | 40 45
esa uuuuu | -27 -11 -24 -174 -5 | 25 30
gfz uuuuu | -2 -26 116 -100 -6 | 27 31
grg uuuuu | -30 -13 -106 -68 -7 | 5 20
igr xxxxx | -6 -15 6 -72 4 | 3 16
irf xxxxx | 8 11 18 10 -8 | 6 21
jpl uuuuu | 3 0 -12 48 14 | 37 43
mit uuuuu | 40 48 62 54 0 | 26 33
ngs uuuuu | -17 -20 16 -3 7 | 19 26
sio xxxxx | 142 -138 -254 -325 -13 | 58 62
Table 7.2132.4 GPS week: 2132 Day: 4 MJD: 59172.500
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 -40 -93 -20 2 | 14 26
emr uuuuu | -20 27 98 192 -4 | 38 43
esa uuuuu | -42 -7 -28 -199 -9 | 24 30
gfz uuuuu | -39 -29 147 -63 -4 | 26 30
grg uuuuu | -16 -47 -38 14 6 | 4 20
igr xxxxx | 4 -13 19 9 -2 | 2 16
irf xxxxx | 4 -5 71 -3 -2 | 4 21
jpl uuuuu | 12 -33 83 -26 8 | 38 44
mit uuuuu | 44 88 84 43 4 | 24 32
ngs uuuuu | -7 -18 -243 70 -6 | 19 26
sio xxxxx | 46 -93 -186 -383 -5 | 53 55
Table 7.2132.5 GPS week: 2132 Day: 5 MJD: 59173.500
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 | -18 -28 -64 -65 4 | 8 31
emr uuuuu | -21 36 -44 211 -9 | 30 42
esa uuuuu | -36 -7 6 -205 -6 | 17 34
gfz uuuuu | -6 -17 123 -8 -3 | 19 33
grg uuuuu | -36 11 -86 16 2 | -2 28
igr xxxxx | 5 -21 20 -1 3 | -4 27
irf xxxxx | -3 -3 61 -19 7 | -3 30
jpl uuuuu | 12 -33 80 -16 1 | 31 43
mit uuuuu | 27 16 114 -15 6 | 18 34
ngs uuuuu | 36 24 -190 174 0 | 12 31
sio xxxxx | 88 -82 -80 -305 -8 | 45 52
Table 7.2132.6 GPS week: 2132 Day: 6 MJD: 59174.500
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 | -17 -10 -83 108 11 | 5 32
emr uuuuu | 11 -12 86 216 1 | 25 40
esa uuuuu | -28 -17 41 -211 0 | 13 33
gfz uuuuu | 8 9 42 31 -5 | 15 32
grg uuuuu | -23 9 -95 -51 -4 | -6 29
igr xxxxx | -1 -27 99 -126 6 | -7 29
irf xxxxx | 5 -5 32 -1 6 | -6 31
jpl uuuuu | 10 -32 -12 64 9 | 28 41
mit uuuuu | 30 22 48 7 1 | 15 33
ngs uuuuu | -9 10 -12 -141 -9 | 8 31
sio xxxxx | 105 -148 -109 -382 -9 | 39 49
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