[IGSREPORT-27898] Wk 2153 IGS Final Orbits
acc
acc at igs.org
Fri Apr 30 04:10:05 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2153 (Apr 11, 2021 - Apr 17, 2021)
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:
igs2153[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2153[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2153[0-6].cls IGS GPS clock combination summary report.
igs21537.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21537.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 | ANKR LPGS TIXI LPGS TIXI
0 | EMR | 10 YELL
0 | ESA | IQAL LPGS PTBB IQAL LPGS PTBB
0 | GFZ | 10 10
0 | GRG | HOB2 SVTL HOB2 SVTL
1 | COD | CEDU CHTI FAA1 IQAL KARR KERG LPGS MAJU NIST NKLG
1 | COD | POVE SCUB SEYG SGOC STK2 SYOG THTI TIXI TOW2 YKRO
1 | COD | TIXI
1 | EMR | 24 NIST
1 | ESA | PTBB LPGS PTBB
1 | GFZ | ANKR HERS MAYG ANKR HERS MAYG
1 | GRG | 13 13 HOB2 SVTL SYOG HOB2 SYOG
1 | JPL | NRIL SVTL ZECK NRIL ZECK
1 | MIT | 24 24
2 | COD | BOGT BRAZ CRO1 DGAR FAA1 HOB2 KOUR LPGS NIST NKLG
2 | COD | POVE SALU SAVO SCUB SYOG THTI TIXI UFPR USUD DGAR
2 | COD | GODE LPGS TIXI
2 | EMR | USUD
2 | ESA | IRKJ LPGS PTBB SYOG GODE IRKJ LPGS PTBB SYOG
2 | GFZ | DGAR GODE SYOG DGAR GODE IRKJ
2 | GRG | CCJ2 IRKJ CCJ2 DGAR IRKJ SYOG
2 | JPL | BADG IQAL BADG IQAL MCM4 SVTL SYOG
2 | MIT | GODE
3 | COD | ASPA BOGT FLIN GMSD IRKJ JOG2 LPGS NYA2 SCUB SGOC
3 | COD | TIXI FLIN TIXI
3 | EMR | 21 LPGS
3 | ESA | 21 21 PTBB RAMO PTBB
3 | GFZ | MDVJ SCH2 IRKJ JOG2 SCH2
3 | GRG | 21 21 FLIN HOB2 IRKJ TRO1 FLIN IRKJ TRO1
3 | JPL | RAMO
4 | COD | ASPA AUCK CPVG DARW DAV1 DRAO MAJU MDVJ MKEA NIST
4 | COD | PIMO SAVO SCUB TIXI WARK IRKJ MDVJ MKEA TIXI
4 | EMR | NIST
4 | ESA | DAV1 DRAO FAIR PTBB ANKR DAV1 DRAO FAIR PTBB
4 | GFZ | AREQ DRAO IRKJ
4 | GRG | CCJ2 JOG2 LHAZ SVTL JOG2 LHAZ SVTL
4 | JPL | POLV AREQ CPVG POLV
5 | COD | SUWN TIXI WTZR WTZR
5 | EMR | TLSE HOB2 IRKJ TLSE
5 | ESA | HOB2 KIT3 HOB2 KIT3
5 | GFZ | HOB2 HOB2 JOG2 SUWN
5 | GRG | 13 13 CCJ2 HOB2 IRKJ MAW1 SVTL SYOG CCJ2 IRKJ KIT3
5 | GRG | SVTL TLSE
5 | JPL | MCM4 NRMD CHUR DAV1 MAG0 MCM4 NRIL NRMD NYA2
5 | MIT | WTZR
6 | COD | DAV1 TIXI TRO1 DAV1 TIXI
6 | EMR | TLSE CHUR FAIR NIST TLSE WHIT
6 | ESA | DAV1 FAIR FLIN HOFN KIRU PTBB DAV1 FAIR FLIN HOFN
6 | ESA | KIRU PTBB
6 | GFZ | DAV1 MDVJ DAV1 KOUR MDVJ
6 | GRG | 13 13 IRKJ SVTL
6 | JPL | POLV ASPA MCM4 POLV TRO1 WHIT
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
----+--------+---------------
3 | GFZ | 24
4 | COD | 6
4 | JPL | 6
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 G01 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G06 | 4 | 4 | 4 | 4 | 4 | 4 | 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 | .3 .0 .4 4 1 -2 -.22
EMR | 0 | -3.1 3.9 -6.5 -3 -6 2 .20
ESA | 0 | .4 -1.2 -.3 -26 22 6 -.06
GFZ | 0 | -.4 -.6 .0 6 8 24 -.07
GRG | 0 | 4.3 .4 1.6 16 -9 -6 .08
JPL | 0 | 1.0 .8 2.2 5 -10 -11 .03
MIT | 0 | -.7 8.6 -6.0 3 20 -6 .26
NGS | 0 | -4.7 3.6 -9.6 3 68 17 .16
SIO | 0 | -.6 6.4 6.9 154 -3 0 -.04
COD | 1 | .2 -.1 .3 2 3 1 -.15
EMR | 1 | -.9 -.7 -3.0 -1 2 18 .18
ESA | 1 | -.2 -.7 .5 -39 17 18 -.11
GFZ | 1 | -.4 -.7 .4 6 14 31 .0
GRG | 1 | 5.2 -2.1 6.2 6 -11 -5 .01
JPL | 1 | 1.7 -4.2 2.4 -6 -3 -13 -.39
MIT | 1 | 3.3 3.7 -1.8 -12 20 3 .31
NGS | 1 | 1.4 -2.9 -2.1 4 29 -7 .06
SIO | 1 | 4.1 1.4 2.6 47 -70 22 .05
COD | 2 | .1 .1 .4 3 1 0 -.07
EMR | 2 | -.0 -5.4 -5.7 2 -5 12 .22
ESA | 2 | .3 -.7 .2 -38 12 17 .04
GFZ | 2 | -.3 .0 -.2 7 -1 19 .20
GRG | 2 | 4.9 -2.1 5.8 -13 -22 -3 .22
JPL | 2 | 11.9 -6.8 9.9 0 -6 -5 -.26
MIT | 2 | 3.8 2.4 .4 -13 13 5 .39
NGS | 2 | 8.6 -6.0 2.7 -15 -24 -51 .27
SIO | 2 | 6.0 2.1 9.5 78 -100 43 .05
COD | 3 | .1 .1 .3 8 0 4 -.09
EMR | 3 | -3.2 -1.2 -4.5 -11 1 3 .34
ESA | 3 | .3 -.6 -.1 -45 17 16 .11
GFZ | 3 | -.5 .0 -.6 8 4 19 .28
GRG | 3 | 4.0 -4.4 -.5 2 -21 2 .16
JPL | 3 | 4.6 -11.3 6.4 2 9 -7 .03
MIT | 3 | 1.3 .6 -1.6 -13 28 11 .41
NGS | 3 | 4.1 -3.7 -.0 -6 8 -23 .27
SIO | 3 | 1.4 1.4 8.6 61 -36 64 .22
COD | 4 | .2 -.0 .1 3 0 2 -.17
EMR | 4 | -5.9 -9.4 -5.0 -28 -4 0 .07
ESA | 4 | .2 -.7 1.5 -27 10 18 -.05
GFZ | 4 | -.2 -.5 .3 -5 7 8 .04
GRG | 4 | .2 -7.7 -9.6 -6 -22 -2 .14
JPL | 4 | -2.1 -11.6 1.0 1 1 3 .23
MIT | 4 | .1 -2.1 -2.3 -21 36 -1 .29
NGS | 4 | -.9 -5.2 -2.5 -31 24 -26 .21
SIO | 4 | -1.4 -3.0 12.3 -30 15 40 .14
COD | 5 | .2 -.1 .4 3 1 -2 -.23
EMR | 5 | -4.1 -7.6 -9.8 -18 10 -12 .23
ESA | 5 | .2 -.8 1.3 -28 17 9 .10
GFZ | 5 | -.2 -.0 .4 -3 3 12 .16
GRG | 5 | 1.6 -7.2 -4.6 0 -24 -4 .10
JPL | 5 | -5.6 -16.6 2.6 -1 -4 -5 .16
MIT | 5 | -.5 -2.3 1.0 -18 30 8 .25
NGS | 5 | -1.3 -6.5 -5.4 -63 30 6 .51
SIO | 5 | -2.2 .4 10.8 24 22 69 .15
COD | 6 | .3 .0 .3 4 2 3 -.19
EMR | 6 | -.1 -7.7 -2.9 0 -6 1 .27
ESA | 6 | -.1 -.6 1.0 -17 5 17 -.13
GFZ | 6 | -.3 -.1 .2 4 7 15 -.02
GRG | 6 | 1.5 -6.2 -3.5 5 -30 6 .01
JPL | 6 | -.3 -10.3 4.1 12 0 6 .08
MIT | 6 | 1.7 2.3 -3.7 -16 14 14 .23
NGS | 6 | 4.0 -4.4 8.5 -14 -28 -3 .22
SIO | 6 | 5.4 1.1 12.0 37 -126 89 .12
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 1.2153.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2153.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 2.2153.[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 3.2153.[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 5.2153.0-6). 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 2153 summary. (Apr 11, 2021 - Apr 17, 2021)
Table 1.2153.a GPS week: 2153 MJD: 59315.000-59321.000
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 731| 0 0 2 -5 -6 -8 -.55 7 7 | -745 326 6 88
| 0 0 0 22 13 8 .03 | 168 400
emr 80| -4 1 -1 0 4 -3 .13 12 12 | 180233 -107 13 92
| 1 1 1 21 19 13 .02 | 9446 870
esa 150| -1 0 -1 6 3 2 .07 7 7 | -949 475 6 86
| 0 0 1 21 10 8 .02 | 139 399
gfz 240| 0 1 3 -1 4 -8 .16 10 10 | 54 -138 10 75
| 0 0 1 28 18 5 .03 | 189 328
grg 108| 1 -1 0 -6 -8 3 -.04 10 9 | 36 -71 8 115
| 0 0 3 19 20 11 .01 | 156 219
igr n/a| 0 0 0 2 -12 -17 .10 4 4 | 3157 -229 10 75
| 0 0 0 13 19 13 .01 | 708 904
jpl 80| 0 0 2 3 -12 -1 .22 8 8 | 525 -104 8 87
| 1 1 1 24 17 18 .02 | 697 875
mit 354| 0 0 -2 -20 4 0 .07 6 6 | 5292 -4111 27 1503
| 0 0 1 30 30 12 .02 | 5052 7102
ngs 210| 0 0 1 11 22 -16 .04 9 9 | -934 138 818 1673
| 1 0 2 30 12 15 .03 | 727 750
sio 418| 1 0 -1 27 -20 32 .05 8 8 | --- --- --- ---
| 0 0 2 78 30 28 .01 | --- ---
Table 1.2153.b GPS week : 2153 MJD: 59315.000-59321.000
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 | 3 3 3 3 5 4 3 |
2 | 3 3 3 3 4 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 4 3 3 3 3 3 3 |
5 | 3 3 3 3 3 3 3 |
6 | 3 3 3 3 15 3 3 |
7 | 3 3 3 4 3 3 4 |
8 | 4 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 2 3 3 3 |
12 | 3 3 3 3 3 3 4 |
13 | 3 3 3 3 3 3 3 |
14 | 3 3 3 3 3 3 3 |
15 | 3 3 4 3 3 3 3 |
16 | 3 3 3 3 3 3 3 |
17 | 2 2 3 2 3 3 3 |
18 | 5 5 5 5 5 5 5 |
19 | 3 3 3 3 3 3 3 |
20 | 3 3 3 3 3 3 3 |
21 | 4 4 3 3 4 4 3 |
22 | 3 3 2 3 3 3 3 |
23 | 4 4 4 4 4 4 4 |
24 | 3 5 9 4 5 5 5 |
25 | 3 3 3 3 3 3 3 |
26 | 3 2 3 3 3 3 2 |
27 | 3 3 3 3 3 3 3 |
28 | 2 3 2 3 3 3 3 |
29 | 4 4 4 4 4 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 4 |
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 2.2153.0 GPS week: 2153 Day: 0 MJD: 59315.000
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 10 18 -5 -.52 6 6 | -641 364 6 85
emr 80| -5 1 0 18 20 20 .13 12 12 | 176690 -411 12 75
esa 150| -1 0 -1 23 5 -9 .07 7 7 | -884 142 7 89
gfz 243| 0 0 2 -1 -13 -3 .16 8 8 | 6 -309 12 76
grg 108| 2 0 1 19 3 0 -.03 11 10 | 87 -353 8 104
igr n/a| 0 0 0 0 1 -6 .10 4 4 | 3031 -430 9 73
jpl 80| 0 0 1 8 -10 30 .24 8 8 | 418 -562 8 82
mit 354| 0 0 -2 -34 -29 -6 .09 6 6 | 2706 -348 27 2132
ngs 214| -1 1 -1 -2 25 0 .02 8 8 | -754 405 826 1864
sio 414| 0 0 0 -18 -2 -13 .03 8 8 | --- --- --- ---
Table 2.2153.1 GPS week: 2153 Day: 1 MJD: 59316.000
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 729| 0 -1 2 21 -11 -7 -.51 6 6 | -645 -214 7 89
emr 80| -5 0 -2 11 21 -1 .08 12 12 | 201580 -1035 13 88
esa 150| -1 0 -2 8 -1 13 .09 7 7 | -952 49 7 93
gfz 241| 0 1 3 2 -11 -16 .16 9 9 | 67 11 10 70
grg 105| 1 0 4 7 6 18 -.05 11 10 | 241 -178 9 119
igr n/a| -1 0 -1 9 -11 -29 .12 5 5 | 3419 -1337 11 82
jpl 80| -1 0 1 5 -1 -7 .23 9 9 | 600 -988 9 128
mit 354| 0 0 -2 -8 13 19 .07 6 5 | 6620 -13397 26 1167
ngs 207| 1 0 0 6 8 -27 .07 8 8 | -750 8 790 1521
sio 419| 1 0 -4 -66 -22 4 .05 8 7 | --- --- --- ---
Table 2.2153.2 GPS week: 2153 Day: 2 MJD: 59317.000
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 726| 0 0 1 4 -5 -3 -.54 6 6 | -940 767 6 86
emr 80| -2 1 -2 4 -13 -4 .14 12 12 | 175507 249 13 92
esa 150| -2 0 -2 9 -7 2 .07 8 8 | -1177 335 6 83
gfz 241| -1 0 5 40 -12 -11 .13 10 10 | -176 201 11 81
grg 110| 1 0 1 -13 -3 2 -.03 9 8 | -221 171 8 123
igr n/a| -1 0 -1 1 -15 -38 .12 5 5 | 2104 356 10 67
jpl 80| 1 -1 2 -2 -24 -3 .22 8 8 | -466 482 9 79
mit 354| 0 0 -3 -32 25 2 .09 6 5 | 16196 -15427 34 1330
ngs 208| 1 0 2 22 11 -23 .05 9 9 | -962 715 710 1640
sio 417| 1 0 -2 6 -5 38 .06 8 8 | --- --- --- ---
Table 2.2153.3 GPS week: 2153 Day: 3 MJD: 59318.000
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 726| 0 0 1 5 -25 -26 -.56 8 8 | -605 528 7 89
emr 80| -5 2 0 -31 21 -2 .13 12 12 | 175837 1187 14 82
esa 150| -1 0 -2 -17 13 14 .04 7 7 | -1018 1047 7 100
gfz 243| -1 1 3 -12 31 -10 .14 9 9 | -167 3 10 71
grg 111| 1 -1 -1 -14 15 2 -.04 9 9 | -88 145 8 104
igr n/a| 0 0 0 -17 1 -12 .08 4 4 | 2561 954 9 77
jpl 80| 0 0 3 -33 12 9 .21 8 8 | 49 955 9 77
mit 354| 0 0 -2 -4 -39 0 .06 7 7 | 1675 1253 33 1364
ngs 212| 0 1 0 -5 33 -17 -.01 8 8 | -2518 -1276 749 1641
sio 414| 1 0 -1 134 -63 38 .05 10 9 | --- --- --- ---
Table 2.2153.4 GPS week: 2153 Day: 4 MJD: 59319.000
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 733| 0 0 1 -8 -5 0 -.54 7 7 | -1031 685 7 85
emr 80| -4 0 -1 18 -22 -12 .11 12 12 | 177562 -549 13 104
esa 150| -1 1 0 35 -8 -1 .07 8 8 | -855 752 8 74
gfz 240| 0 2 3 24 -2 0 .20 10 10 | 316 -344 10 70
grg 108| 2 -2 -7 -3 -43 1 -.07 10 10 | 67 -27 9 127
igr n/a| 0 0 0 24 -38 -19 .12 5 5 | 4071 -971 12 76
jpl 80| 0 -2 2 26 -26 8 .19 8 8 | 1465 -1091 8 80
mit 354| 0 0 0 -78 44 0 .05 6 5 | 3534 -780 25 1301
ngs 210| 0 1 0 -31 30 -41 .05 10 10 | -549 1001 924 1696
sio 423| 0 0 2 86 -18 34 .04 9 9 | --- --- --- ---
Table 2.2153.5 GPS week: 2153 Day: 5 MJD: 59320.000
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 735| 0 0 2 -35 -12 -10 -.57 8 8 | -705 -225 7 88
emr 80| -5 3 0 -32 -9 -2 .15 11 11 | 176801 796 15 101
esa 150| -1 0 0 -25 1 0 .09 7 8 | -1017 846 7 76
gfz 242| 0 1 3 -49 15 -10 .16 10 11 | 71 173 10 75
grg 109| 1 -1 -2 -41 -25 13 -.05 11 11 | -3 77 8 111
igr n/a| 0 0 0 -9 -35 0 .10 4 4 | 2985 718 10 78
jpl 80| 0 -2 4 -16 -37 -27 .20 8 8 | 235 923 9 74
mit 354| 1 0 -3 2 -3 -19 .05 6 6 | 2626 731 22 1550
ngs 210| 0 1 0 64 38 2 .02 9 9 | -308 -258 693 1524
sio 421| 1 0 -3 96 24 69 .05 8 8 | --- --- --- ---
Table 2.2153.6 GPS week: 2153 Day: 6 MJD: 59321.000
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 740| 0 -1 2 -33 -7 -1 -.58 8 7 | -652 379 7 95
emr 80| -4 1 -2 3 15 -23 .15 12 12 | 177660 -988 14 103
esa 150| -1 0 0 12 18 -1 .06 7 7 | -743 155 5 93
gfz 233| 0 2 2 -13 19 -4 .18 11 11 | 261 -704 11 84
grg 110| 1 -1 -4 -3 -15 -18 -.03 9 10 | 174 -334 9 118
igr n/a| -1 0 0 9 13 -19 .10 5 5 | 3931 -899 10 74
jpl 80| 0 0 2 37 3 -16 .25 9 9 | 1378 -448 9 89
mit 354| 0 0 -4 11 17 10 .06 6 6 | 3691 -811 24 1679
ngs 214| 0 0 6 26 8 -10 .05 8 8 | -698 374 1035 1827
sio 424| 1 0 -3 -48 -54 53 .04 8 7 | --- --- --- ---
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 3.2153.0 GPS week: 2153 Day: 0 MJD: 59315.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 12 8 10 10 3 7 6 6 7 2 | 361 363 361 361 267 361 361 362 360 363 361
2 | 6 9 8 9 10 5 9 6 7 9 2 | 32 34 29 34 36 33 34 37 35 37 33
3 | 6 12 7 7 11 4 9 5 4 7 2 | 21 34 29 26 24 27 33 24 23 26 25
4 | 8 17 8 9 14 5 9 7 12 6 3 | 71 68 69 75 73 68 69 67 75 68 70
5 | 5 8 8 9 6 4 6 7 9 10 2 | 24 30 27 33 28 30 31 30 30 33 28
6 | 8 10 7 8 9 5 8 7 7 7 2 | 772 543 772 770 545 770 771 774 772 772 773
7 | 8 14 7 7 16 3 8 5 8 8 3 | 31 39 36 38 36 36 38 36 38 36 35
8 | 8 14 8 9 11 4 10 9 9 9 3 | 30 37 35 33 35 34 38 33 33 35 32
9 | 6 11 8 9 12 4 8 5 7 6 2 | 26 32 33 31 29 31 32 31 30 30 29
10 | 5 16 7 10 7 4 8 5 4 9 2 | 25 40 31 29 29 30 35 29 28 29 29
12 | 6 14 6 7 8 3 8 4 9 13 3 | 32 41 33 36 36 35 39 34 35 40 34
13 | 7 9 5 8 12 5 9 6 9 7 2 | 24 32 29 31 28 30 34 29 27 29 27
14 | 5 7 7 6 7 6 8 9 9 8 2 | 46 49 45 50 49 47 47 52 47 54 48
15 | 7 12 7 9 10 4 7 5 5 8 2 | 56 62 58 59 52 58 60 55 55 56 56
16 | 7 19 4 6 8 5 7 7 9 7 3 | 18 22 22 24 21 23 24 23 22 26 21
17 | 5 12 5 5 9 3 4 6 6 8 2 | 42 47 45 47 45 47 47 46 44 49 45
X18 | 11 16 14 10 17 5 10 5 10 --- 4 | 93 87 87 90 95 89 93 91 92 --- 90
19 | 7 14 4 7 11 4 7 6 9 10 3 | 42 53 47 50 48 48 50 48 45 50 47
20 | 7 8 8 8 7 4 6 10 7 13 3 | 85 83 83 83 82 84 84 81 83 82 83
21 | 6 12 7 11 23 4 8 10 7 8 3 | 22 25 23 20 24 23 25 30 23 30 23
22 | 5 7 7 8 12 4 6 4 6 6 2 | 24 31 30 29 25 28 31 26 26 29 27
23 | 8 14 7 10 9 4 16 5 6 10 3 | 34 33 37 37 39 36 34 37 35 39 35
24E | 7 11 8 12 11 4 7 4 8 6 3 | 31 36 34 125 34 37 35 35 38 14 35
25 | 4 8 8 8 10 3 5 3 8 10 2 | 19 29 25 26 26 25 28 24 23 30 23
26 | 6 8 8 6 6 4 8 6 7 7 2 | 24 29 29 31 27 31 32 27 27 28 27
27 | 6 12 7 6 10 4 9 7 10 10 3 | 26 31 33 31 32 31 34 30 30 29 29
28 | 5 8 4 6 6 3 7 7 7 6 2 | 20 31 26 27 25 27 32 26 28 27 25
29 | 8 20 8 10 12 4 10 6 12 9 3 | 49 54 51 54 53 53 52 53 53 53 51
30 | 5 12 8 12 9 4 11 6 8 8 3 | 51 57 54 54 55 55 57 56 54 58 54
31 | 7 13 6 8 13 4 7 4 11 7 3 | 40 39 41 39 43 41 40 39 42 37 39
32 | 5 10 6 11 7 3 7 4 5 9 2 | 20 28 30 31 27 29 30 28 25 28 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 12 7 8 11 4 8 6 8 8 |T 70 68 73 77 63 74 75 73 73 73 72
WRMS | 6 12 7 8 10 4 8 6 8 8 |NE 77 73 80 81 68 80 82 80 80 81 79
MEDI | 6 12 7 8 10 4 8 6 8 8 |MD 31 37 34 36 36 35 35 35 35 35 34
Table 3.2153.1 GPS week: 2153 Day: 1 MJD: 59316.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 12 6 9 12 4 7 6 6 8 2 | 267 269 268 265 211 268 268 268 266 269 268
2 | 6 9 8 13 11 5 9 6 7 12 3 | 16 20 17 23 20 18 19 20 22 27 18
3 | 7 9 7 7 10 2 8 5 5 7 2 | 15 28 24 21 19 21 28 19 19 22 20
4 | 9 15 8 10 11 6 9 6 9 5 3 | 50 50 50 55 53 49 49 50 51 50 50
5 | 5 10 9 8 8 4 8 7 8 7 2 | 18 25 20 26 21 23 25 21 21 25 20
6 | 6 9 8 9 10 5 8 6 9 8 2 | 602 468 601 598 470 599 601 603 604 603 602
7E | 7 14 8 10 9 5 9 5 10 6 3 | 21 30 26 30 21 26 29 28 28 28 25
8 | 6 12 7 10 11 3 9 7 9 8 3 | 18 25 26 25 26 24 26 23 23 27 23
9 | 7 10 8 6 10 4 8 6 7 6 2 | 18 25 26 24 22 23 25 24 21 22 21
10 | 6 9 7 8 6 5 8 5 6 6 2 | 16 26 23 20 17 21 28 20 22 23 20
12 | 3 15 5 9 6 5 9 5 6 11 2 | 16 24 20 23 22 22 25 24 24 28 22
13 | 6 10 7 8 13 5 9 6 6 8 2 | 12 21 18 20 18 19 24 17 19 17 16
14 | 5 10 9 7 8 7 12 7 8 10 3 | 22 27 26 26 27 25 26 28 25 33 26
15 | 7 10 7 8 12 6 8 6 6 9 2 | 46 50 48 52 44 50 50 46 50 46 47
16 | 6 18 6 7 9 4 7 5 7 6 2 | 15 22 21 24 19 22 23 20 25 21 19
17 | 4 11 5 7 9 4 6 5 8 7 2 | 19 27 24 28 26 26 26 24 28 27 24
X18 | 9 18 16 14 17 6 10 6 15 --- 5 | 53 53 51 55 58 51 52 53 54 --- 52
19 | 6 13 5 12 9 3 7 5 7 8 2 | 18 28 25 31 28 25 26 26 26 26 24
20 | 7 8 8 9 8 6 7 10 7 11 3 | 84 84 84 84 82 85 85 83 87 83 83
21 | 7 16 7 13 22 4 7 9 10 10 4 | 19 24 21 21 21 21 23 25 21 29 20
22 | 6 7 7 8 12 4 7 4 6 7 2 | 19 25 24 24 19 23 26 21 23 25 21
23 | 8 14 6 12 9 5 18 6 8 8 3 | 15 17 18 21 21 16 18 19 17 21 16
X24E | 9 14 --- --- 10 15 --- 11 8 --- 5 | 46 44 --- --- 44 50 --- 47 41 --- 44
25 | 5 8 6 13 8 4 7 5 6 7 2 | 10 20 19 18 17 18 22 19 18 20 16
26 | 6 7 8 7 8 4 7 3 8 5 2 | 10 20 21 19 17 18 22 17 20 19 17
27 | 6 11 8 7 10 4 9 6 7 7 2 | 14 22 26 23 24 22 24 21 24 24 21
28 | 6 11 5 8 7 3 9 6 9 6 2 | 10 23 20 20 18 20 24 17 23 22 18
29 | 5 17 8 11 14 3 9 5 13 8 3 | 24 29 29 35 32 29 30 31 33 32 29
30 | 7 13 8 10 17 5 10 5 9 5 3 | 76 83 79 76 78 78 82 80 79 81 79
31M | 9 11 7 8 15 5 8 6 7 7 3 | 30 37 33 36 34 34 35 32 33 36 32
32M | 8 11 6 11 8 3 5 4 6 7 2 | 23 29 31 32 28 29 31 28 28 26 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 12 7 9 11 5 9 6 8 8 |T 52 54 57 58 50 56 59 56 57 59 55
WRMS | 6 12 7 9 10 5 9 5 8 7 |NE 54 55 59 60 52 59 61 59 60 61 58
MEDI | 6 11 7 9 10 4 8 6 7 7 |MD 19 27 25 25 24 24 26 24 25 27 23
Table 3.2153.2 GPS week: 2153 Day: 2 MJD: 59317.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 11 7 9 10 5 8 5 10 6 2 | 397 397 397 400 261 395 397 395 394 396 396
2 | 6 9 8 10 9 4 8 6 9 9 3 | 20 24 21 23 24 22 21 24 24 28 22
3 | 6 10 9 8 8 3 9 5 11 8 3 | 10 27 23 16 14 18 26 15 20 17 16
4 | 8 14 8 10 9 6 8 6 14 7 3 | 61 59 57 64 60 57 59 57 66 60 59
5 | 5 9 9 9 6 5 7 6 6 5 2 | 12 21 16 24 15 19 20 19 19 19 17
6 | 6 8 8 11 9 6 7 7 10 7 2 | 832 508 831 834 507 833 833 838 835 837 835
7E | 8 17 8 9 8 5 9 5 11 8 3 | 23 28 27 32 29 29 27 30 28 31 27
8 | 6 15 8 9 10 5 8 6 12 7 3 | 15 23 25 23 24 22 25 20 23 25 20
9 | 5 8 8 9 9 4 8 6 9 7 2 | 24 28 31 26 26 27 30 27 27 30 26
10 | 5 9 10 8 6 4 7 5 6 8 2 | 15 26 24 24 18 22 28 21 22 19 20
12 | 4 14 5 8 7 5 7 3 8 10 2 | 23 30 25 29 27 27 29 28 29 29 26
13 | 6 11 5 9 10 5 9 6 5 8 2 | 11 22 18 20 17 18 21 18 18 18 16
14 | 5 10 9 9 8 6 10 7 7 6 2 | 34 36 34 32 37 34 34 39 34 40 35
15 | 8 14 9 11 9 4 8 6 9 14 3 | 35 44 38 38 37 41 42 39 41 46 38
16 | 6 19 5 6 9 4 5 6 9 7 2 | 8 15 16 17 14 15 16 16 17 20 13
17 | 7 10 6 19 9 4 6 4 8 5 3 | 28 32 30 35 34 30 31 31 31 30 29
X18 | 9 19 17 11 16 5 10 6 11 --- 4 | 45 47 40 48 53 44 49 46 50 --- 46
19 | 8 12 5 11 8 3 8 5 10 8 3 | 26 31 29 33 32 29 29 31 35 31 29
20 | 6 10 11 10 5 6 5 10 9 11 3 | 61 59 58 62 59 61 61 65 57 64 61
21 | 7 15 7 13 11 4 6 8 11 6 3 | 14 18 18 17 19 18 20 23 20 24 17
22 | 5 6 7 8 9 2 6 4 9 5 2 | 11 20 19 15 14 17 22 17 19 19 16
23 | 9 16 8 14 7 5 18 5 6 11 3 | 16 19 19 23 21 16 17 20 20 19 17
X24E | 13 --- --- --- 14 23 13 19 --- --- 9 | 23 --- --- --- 29 35 34 34 --- --- 27
25 | 6 7 7 9 9 4 6 4 5 10 2 | 11 20 19 17 17 18 21 18 19 20 16
26 | 6 8 9 10 7 4 6 5 8 9 2 | 19 24 23 24 21 22 25 20 22 22 20
27 | 5 13 8 10 10 4 9 6 7 12 3 | 11 22 23 24 22 21 22 19 20 23 18
28 | 6 11 5 8 6 4 8 6 5 4 2 | 14 24 21 19 20 21 24 21 20 22 19
29 | 6 18 9 11 14 4 11 5 12 8 3 | 16 21 21 25 25 21 22 23 26 25 21
30E | 5 14 7 13 10 6 8 7 7 6 3 | 38 44 42 38 36 40 42 41 41 42 39
31E | 8 10 6 11 16 6 8 5 8 9 3 | 63 62 62 61 62 61 63 61 65 61 61
32 | 6 7 7 7 9 3 7 4 7 8 2 | 27 32 33 33 32 31 34 30 34 30 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 12 8 10 9 5 8 6 9 8 |T 62 58 68 69 51 66 68 67 69 70 65
WRMS | 6 12 8 10 8 5 8 5 9 8 |NE 68 61 72 73 54 71 74 72 73 75 71
MEDI | 6 11 8 9 9 4 8 6 9 8 |MD 23 27 25 25 26 27 28 27 26 28 26
Table 3.2153.3 GPS week: 2153 Day: 3 MJD: 59318.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 10 5 10 9 3 7 7 8 10 3 | 224 225 227 227 203 227 226 227 229 227 227
2 | 7 8 9 11 10 4 8 8 10 11 3 | 16 22 18 18 22 20 21 23 24 25 19
3 | 9 10 8 9 8 4 8 8 8 13 3 | 14 27 23 17 15 19 27 17 19 19 18
4 | 11 15 7 7 9 5 7 8 8 9 3 | 43 42 35 42 41 39 41 40 43 40 40
5 | 7 10 8 7 7 4 6 8 7 8 2 | 13 22 18 21 17 19 23 21 21 21 19
6 | 8 8 8 10 8 4 8 8 8 8 3 | 393 443 393 397 441 396 397 395 394 394 395
7E | 9 16 9 10 11 4 9 6 13 9 3 | 21 28 25 29 26 26 26 29 31 31 25
8 | 9 15 6 7 11 3 9 7 9 9 3 | 13 23 22 21 22 19 23 19 20 20 18
9 | 8 9 9 8 8 6 8 9 9 11 3 | 16 23 25 22 22 23 24 25 23 25 22
10 | 4 8 6 6 7 3 6 6 6 8 2 | 19 29 24 23 19 22 28 21 20 23 21
12 | 8 14 6 9 9 2 8 6 10 12 3 | 20 32 25 27 27 26 30 28 25 29 26
13 | 8 12 7 8 9 5 10 8 7 13 3 | 13 24 17 20 16 19 24 20 17 20 17
14 | 6 11 8 9 7 7 7 7 7 8 2 | 33 38 35 38 39 36 35 40 36 40 36
15 | 9 16 7 10 9 6 7 7 8 12 3 | 35 42 38 39 35 37 37 35 36 37 36
16 | 8 19 4 6 9 4 6 8 7 9 3 | 12 18 19 20 18 18 20 19 19 20 17
17 | 6 9 5 8 9 2 4 6 7 4 2 | 20 27 24 25 25 25 26 28 26 28 24
X18 | 9 18 15 12 19 5 9 8 9 --- 4 | 49 48 45 56 56 48 52 51 49 --- 50
19 | 7 11 5 8 9 4 5 6 7 7 2 | 19 24 23 25 24 23 24 25 23 26 22
20 | 6 8 9 7 8 4 6 6 9 13 3 | 34 37 34 36 35 36 37 38 34 40 35
21 | 7 10 7 12 10 4 7 9 6 10 3 | 16 20 18 18 21 18 20 23 19 23 18
22 | 8 8 7 7 8 4 5 6 9 11 2 | 14 22 20 17 16 17 21 18 17 16 16
23 | 10 15 6 11 9 3 16 6 7 10 3 | 12 18 15 22 15 13 15 16 12 17 13
X24E | 8 14 12 751 12 6 7 10 9 --- 4 | 35 42 27 628 35 38 33 42 41 --- 38
25 | 8 11 7 10 12 4 7 6 9 9 3 | 13 26 22 22 20 21 24 21 17 20 19
26 | 9 9 7 5 6 2 5 6 7 8 2 | 17 23 24 25 20 23 25 21 20 20 20
27 | 8 13 7 6 10 3 6 7 8 11 3 | 11 19 23 21 22 20 21 19 20 19 18
28 | 7 11 5 9 7 4 8 6 6 7 2 | 14 26 21 22 19 21 26 22 21 23 20
29 | 8 21 9 11 14 4 8 7 12 8 3 | 11 22 19 23 22 19 20 22 22 21 18
30E | 8 12 7 9 10 4 8 7 13 11 3 | 50 57 56 57 52 56 55 54 52 56 53
31E | 9 12 7 9 14 6 6 7 7 9 3 | 34 40 36 38 40 38 39 40 38 41 37
32 | 8 9 6 8 8 3 6 7 5 7 2 | 16 28 25 24 23 24 25 25 25 26 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 7 9 9 4 8 7 8 10 |T 40 48 44 65 45 44 46 45 44 46 43
WRMS | 8 12 7 9 9 4 8 7 8 9 |NE 42 50 46 47 47 46 48 47 46 47 45
MEDI | 8 11 7 9 9 4 7 7 8 9 |MD 17 27 24 24 22 23 26 25 23 25 22
Table 3.2153.4 GPS week: 2153 Day: 4 MJD: 59319.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 10 19 7 12 --- 5 15 8 12 10 4 | 625 628 628 628 --- 626 628 626 624 628 627
2 | 8 11 11 11 11 6 8 9 10 14 3 | 30 34 33 34 35 33 32 36 38 39 33
3 | 7 11 8 14 9 3 9 5 8 5 3 | 24 33 32 26 24 28 33 25 28 31 27
4 | 9 12 10 9 9 5 7 7 10 9 3 | 61 63 66 68 63 64 64 64 68 67 65
5 | 6 10 10 10 6 5 8 6 11 10 3 | 22 27 28 30 26 28 27 29 29 29 27
X6 | 61 --- 27 31 --- 23 75 28 33 33 15 | 9999 --- 9999 9999 --- 9999 9999 9999 9999 9999 9999
7E | 7 15 10 9 10 4 9 5 10 8 3 | 23 31 28 26 27 28 28 28 29 33 26
8 | 8 11 8 9 9 3 9 8 12 7 3 | 26 34 35 33 31 33 34 30 33 32 31
9 | 6 6 10 9 9 4 8 6 9 9 3 | 32 37 38 36 36 35 36 36 40 35 35
10 | 6 11 9 8 5 5 9 4 8 10 2 | 27 36 31 31 28 31 35 29 31 26 30
12 | 7 13 7 10 8 4 6 4 6 11 2 | 33 41 36 36 35 36 38 35 38 37 35
13 | 9 10 7 10 11 5 9 6 10 11 3 | 23 33 30 30 29 29 31 27 33 29 27
14 | 8 9 11 8 11 6 8 7 9 12 3 | 45 47 47 50 50 47 45 49 50 51 48
15 | 8 11 8 8 9 6 8 6 11 7 3 | 38 49 44 43 46 44 46 43 42 43 43
16 | 5 20 6 10 10 5 7 5 10 7 3 | 23 26 27 28 26 28 27 25 26 27 25
17 | 6 10 7 8 10 4 5 6 8 7 2 | 39 43 44 44 44 44 43 42 45 43 42
X18 | 9 19 15 15 18 7 10 6 17 --- 5 | 59 59 57 63 60 58 61 61 62 --- 60
19 | 7 15 8 8 10 7 7 6 8 11 3 | 37 44 45 42 44 43 43 41 44 42 41
20 | 7 9 8 10 7 5 7 5 9 9 2 | 54 55 56 59 56 57 56 55 55 56 55
21 | 8 11 8 16 12 5 6 9 6 9 3 | 24 29 28 30 29 28 28 32 27 32 27
22 | 7 9 6 9 9 4 6 6 9 8 2 | 24 31 28 28 25 27 29 26 27 29 26
23 | 10 15 6 11 7 5 17 4 8 7 3 | 31 34 34 38 34 33 32 34 36 32 33
X24E | 14 13 12 16 17 7 8 8 13 --- 4 | 38 36 36 177 34 37 34 36 39 --- 34
25 | 8 8 8 9 12 4 6 3 9 8 2 | 27 35 35 31 29 32 32 30 32 31 30
26 | 7 10 8 9 8 3 7 4 13 6 2 | 30 35 34 30 31 33 35 30 33 33 31
27 | 6 10 9 7 9 4 8 6 13 10 3 | 26 32 33 32 30 31 31 28 32 30 29
28 | 7 9 6 9 8 4 7 6 7 10 2 | 30 36 36 35 33 34 35 32 38 36 33
29 | 8 19 6 8 14 5 10 4 12 9 3 | 31 36 36 36 36 35 35 37 36 40 35
30E | 8 8 11 7 13 6 7 6 6 12 3 | 33 37 36 38 37 37 39 40 38 40 37
31E | 9 12 8 10 13 5 7 3 14 9 3 | 23 30 25 26 26 27 26 26 29 28 25
32 | 8 7 8 10 7 3 6 4 9 7 2 | 28 34 34 32 32 33 33 33 34 33 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 8 10 10 5 8 6 10 9 |T 52 57 56 61 35 55 56 55 57 57 54
WRMS | 7 12 8 10 10 5 8 5 10 9 |NE 56 62 61 61 36 60 61 60 61 61 59
MEDI | 8 11 8 9 9 5 8 6 10 9 |MD 30 35 35 34 33 33 34 33 36 33 33
Table 3.2153.5 GPS week: 2153 Day: 5 MJD: 59320.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 7 12 21 4 9 6 8 9 3 | 365 369 370 371 494 369 369 368 362 367 368
2 | 7 8 8 10 11 4 9 8 9 8 3 | 12 19 17 19 20 18 20 23 23 25 18
3 | 9 10 9 12 8 3 9 8 8 9 3 | 19 29 28 20 19 23 29 20 23 24 21
4 | 11 14 7 8 9 6 9 7 10 7 3 | 54 53 52 54 53 52 52 55 56 56 53
5 | 7 9 10 8 9 4 8 7 8 7 3 | 19 25 20 22 20 23 26 22 25 24 21
6 | 8 10 8 9 9 6 9 8 9 8 3 | 550 860 549 545 860 546 546 546 550 553 548
7E | 11 14 8 7 8 3 10 5 9 7 3 | 26 31 29 29 32 29 29 29 32 30 28
8 | 10 12 8 9 11 5 9 7 8 9 3 | 17 26 25 26 22 25 25 22 22 23 21
9 | 7 8 8 9 10 4 8 8 5 6 2 | 13 20 22 18 21 19 22 20 22 22 18
10 | 8 9 7 10 5 4 9 5 7 9 2 | 12 25 19 20 15 18 25 15 19 15 17
12 | 6 14 7 9 9 4 8 6 11 9 3 | 15 24 20 21 20 22 25 21 24 24 19
13 | 7 11 6 10 11 4 8 6 9 11 3 | 14 25 20 22 18 20 25 19 22 20 18
14 | 7 9 9 7 10 5 9 6 12 7 3 | 22 23 22 29 25 22 23 25 23 28 23
15 | 6 10 8 9 11 5 8 6 9 7 2 | 38 42 40 43 36 41 41 37 38 40 39
16 | 7 20 6 8 10 5 6 6 7 6 3 | 14 20 17 21 17 19 18 17 18 18 16
17 | 7 8 7 7 11 3 7 5 9 7 2 | 19 26 23 27 23 25 27 26 25 25 23
X18 | 9 18 15 11 21 7 9 8 15 --- 5 | 50 56 52 52 50 51 54 53 58 --- 52
19 | 9 12 8 6 10 4 7 6 11 7 3 | 22 30 28 27 29 26 30 28 27 27 26
20 | 6 9 8 8 7 5 4 6 9 9 2 | 49 51 48 51 47 50 50 47 50 48 48
21 | 6 10 8 17 12 5 7 8 7 9 3 | 20 27 21 24 23 23 25 25 26 26 22
22 | 9 7 7 11 10 4 8 8 10 8 3 | 20 28 26 25 24 26 27 25 27 28 24
23 | 10 15 6 10 9 5 16 6 7 8 3 | 15 20 16 20 19 15 17 17 17 19 15
X24E | 10 15 13 14 13 7 9 10 15 --- 4 | 25 30 26 82 22 27 27 29 33 --- 25
25 | 6 8 7 13 13 3 7 6 7 6 3 | 13 28 24 22 17 22 26 20 21 23 20
26 | 7 9 7 8 8 4 6 4 8 5 2 | 9 19 19 18 14 17 19 15 19 16 15
27 | 8 10 8 11 13 4 9 6 10 11 3 | 14 21 23 25 20 22 22 20 21 21 19
28 | 7 9 5 6 7 3 8 7 12 6 2 | 10 23 19 20 16 18 22 18 22 21 17
29 | 6 20 5 13 17 5 8 5 12 7 3 | 28 34 31 33 29 31 32 33 37 36 31
30E | 8 12 8 12 13 5 8 7 9 6 3 | 31 36 34 39 32 36 38 36 35 38 34
31E | 8 11 5 9 12 3 7 6 10 6 2 | 38 41 39 38 41 40 40 40 41 40 39
32 | 8 9 7 12 9 4 6 5 8 6 2 | 13 22 21 25 19 21 22 19 21 18 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 11 7 10 11 4 8 6 9 8 |T 50 67 54 57 67 54 56 54 56 57 53
WRMS | 8 11 8 11 11 4 8 6 9 8 |NE 55 73 59 60 75 59 61 59 60 61 58
MEDI | 7 10 8 9 10 4 8 6 9 7 |MD 19 27 24 25 22 23 26 25 25 25 22
Table 3.2153.6 GPS week: 2153 Day: 6 MJD: 59321.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 14 6 8 11 3 8 6 6 8 2 | 353 355 356 357 288 355 355 356 355 355 355
2 | 9 10 9 12 8 6 10 7 7 8 3 | 14 23 20 24 24 21 22 25 27 27 21
3 | 8 12 7 11 6 4 9 6 6 8 2 | 20 30 24 23 21 24 30 23 26 24 22
4 | 10 13 7 9 8 6 9 5 6 8 3 | 80 75 77 79 77 76 75 79 79 78 78
5 | 6 8 10 10 5 7 10 6 9 7 2 | 24 30 27 26 26 27 31 27 28 29 26
6 | 8 10 8 12 7 5 8 7 7 7 3 | 675 534 674 673 535 674 674 675 673 676 674
7E | 10 15 8 6 15 5 9 7 10 8 3 | 29 34 27 30 32 29 31 33 32 33 30
8 | 8 12 8 11 9 5 11 6 7 8 3 | 14 23 22 23 21 20 25 18 19 20 18
9 | 7 9 8 10 6 4 7 7 8 7 2 | 23 26 28 25 27 27 29 29 27 27 26
10 | 7 9 7 10 8 4 7 5 5 8 2 | 19 28 22 25 19 21 26 21 22 21 21
12 | 6 17 8 10 10 4 10 5 10 12 3 | 30 40 33 35 31 31 36 31 31 31 32
13 | 9 9 6 8 9 4 11 5 12 10 3 | 17 25 20 24 20 21 27 22 22 24 20
14 | 7 11 9 9 10 6 9 6 10 8 3 | 51 52 49 54 54 50 50 56 50 55 52
15 | 6 10 7 10 9 5 7 6 8 8 2 | 52 58 55 57 52 55 54 54 53 58 54
16 | 6 21 4 10 10 5 9 5 7 7 3 | 18 20 21 25 21 22 23 21 20 23 20
17 | 7 11 5 9 9 4 8 7 8 6 2 | 25 30 27 32 29 28 30 29 29 30 27
X18 | 10 19 14 13 20 8 11 8 14 --- 5 | 82 79 76 83 81 79 82 83 80 --- 80
19 | 9 12 6 10 8 4 9 7 10 12 3 | 24 31 30 34 30 29 31 28 29 35 29
20 | 6 8 8 10 7 4 6 6 7 10 2 | 63 64 63 64 61 65 65 63 64 64 63
21 | 8 8 8 12 11 4 7 6 6 8 3 | 20 27 25 30 24 26 27 24 22 26 23
22 | 7 8 7 7 9 3 6 6 4 7 2 | 26 31 29 31 25 29 31 30 30 28 28
23 | 8 15 7 15 8 5 18 5 7 8 3 | 23 25 25 30 23 24 24 23 23 24 22
X24E | 7 13 13 18 16 7 11 11 11 --- 4 | 23 31 25 74 23 30 29 32 31 --- 27
25 | 7 8 6 15 10 3 7 4 6 8 2 | 21 27 26 28 23 24 27 24 23 23 24
26 | 5 8 6 8 8 3 7 4 6 6 2 | 21 25 26 24 22 24 26 23 23 23 23
27 | 8 10 7 11 11 4 10 7 8 10 3 | 12 19 21 21 21 18 19 18 18 19 16
28 | 6 12 5 10 6 4 8 6 10 5 2 | 22 27 25 28 23 25 28 27 28 23 24
29 | 7 22 5 13 15 5 10 6 8 11 3 | 29 35 32 36 31 32 33 33 33 33 31
30E | 8 11 9 9 12 7 8 7 9 6 3 | 35 40 39 39 36 38 41 38 40 37 37
31E | 8 10 9 15 14 5 8 7 12 7 3 | 46 48 44 50 43 46 47 47 45 48 45
32 | 7 8 6 13 6 4 7 5 7 5 2 | 26 30 29 32 29 30 31 29 29 27 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 7 11 9 5 9 6 8 8 |T 61 62 64 68 57 64 66 65 64 66 63
WRMS | 7 12 7 11 10 5 9 6 8 7 |NE 67 66 70 72 61 70 72 70 70 71 69
MEDI | 7 11 7 10 9 4 9 6 8 8 |MD 24 30 27 31 27 29 31 29 29 28 27
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 4.2153 GPS week: 2153 MJD: 59315.0-59321.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 |U 8 7 19 |U 9 13 35 |U 7 8 19 |
emr | emr 2947 |U 17 21 36 |U 12 20 49 |U 11 19 33 |
esa | esa 2948 | 12 12 22 |U 10 16 45 | 10 15 30 |
gfz | gfz 2942 |U 11 10 22 |U 9 13 35 |U 14 13 40 |
grg | grg 2946 |U 10 13 21 |U 11 15 37 | 10 9 25 |
igr | igr 2957 | 10 8 18 | 10 15 37 | 10 11 24 |
igs | igs 2957 | 9 8 16 | 9 14 34 | 8 10 22 |
jpl | jpl 2962 |U 15 16 31 |U 11 18 47 | 13 19 33 |
mit | mit 2976 |U 9 9 21 |U 9 14 34 |U 10 9 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 5.2153.0 GPS week: 2153 Day: 0 MJD: 59315.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 13 7 14 | 8 10 29 | 5 7 14 |
emr | emr 2976 | 18 16 42 | 11 16 42 | 8 25 34 |
esa | esa 2976 | 14 10 26 | 8 13 43 | 9 17 27 |
gfz | gfz 2976 | 13 8 19 | 9 12 37 | 27 39 138 |
grg | grg 2973 | 13 12 21 | 9 12 37 | 11 11 29 |
igr | igr 2976 | 12 7 19 | 8 11 35 | 8 13 25 |
igs | igs 2976 | 12 6 17 | 8 11 34 | 7 11 22 |
jpl | jpl 2976 | 16 11 26 | 10 14 44 | 8 18 32 |
mit | mit 2976 | 13 9 20 | 8 13 39 | 10 13 24 |
Table 5.2153.1 GPS week: 2153 Day: 1 MJD: 59316.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2948 | 9 7 15 | 11 16 42 | 7 8 23 |
emr | emr 2968 | 16 21 30 | 15 20 51 | 12 15 34 |
esa | esa 2880 | 13 11 20 | 13 18 49 | 10 12 28 |
gfz | gfz 2880 | 13 12 15 | 12 16 48 | 12 8 24 |
grg | grg 2964 | 12 14 23 | 13 14 53 | 12 8 28 |
igr | igr 2948 | 11 8 17 | 12 17 44 | 10 8 24 |
igs | igs 2940 | 11 9 13 | 12 16 42 | 9 7 23 |
jpl | jpl 2880 | 15 17 27 | 14 19 46 | 12 14 30 |
mit | mit 2976 | ---- ---- ---- | 12 14 34 | 1 2 7 |
Table 5.2153.2 GPS week: 2153 Day: 2 MJD: 59317.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 11 | 13 14 36 | 7 7 16 |
emr | emr 2880 | 17 16 29 | 13 22 57 | 10 19 32 |
esa | esa 2880 | 11 11 19 | 12 18 60 | 11 14 30 |
gfz | gfz 2880 | 10 12 22 | 13 14 45 | 11 9 22 |
grg | grg 2976 | 10 16 17 | 13 18 44 | 9 9 26 |
igr | igr 2878 | 8 9 17 | 11 14 48 | 11 11 22 |
igs | igs 2976 | 8 9 13 | 12 15 45 | 9 10 21 |
jpl | jpl 2976 | 11 15 18 | 11 18 54 | 11 20 31 |
mit | mit 2976 | 7 11 17 | 11 15 47 | ---- ---- ---- |
Table 5.2153.3 GPS week: 2153 Day: 3 MJD: 59318.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 14 | 8 10 24 | 5 9 19 |
emr | emr 2976 | 16 18 35 | 12 20 59 | 12 22 40 |
esa | esa 2976 | 11 11 21 | 8 15 43 | 9 15 33 |
gfz | gfz 2935 | 10 7 24 | 7 11 26 | 10 9 26 |
grg | grg 2976 | 8 11 20 | 7 13 32 | 9 7 25 |
igr | igr 2976 | 8 8 16 | 8 13 30 | 9 10 29 |
igs | igs 2976 | 8 7 14 | 7 12 29 | 7 10 25 |
jpl | jpl 2976 | 13 14 20 | 8 17 36 | 11 17 35 |
mit | mit 2976 | 9 8 21 | 8 13 28 | 14 11 35 |
Table 5.2153.4 GPS week: 2153 Day: 4 MJD: 59319.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 15 12 46 | 9 16 61 | 6 6 17 |
emr | emr 2880 | 18 24 42 | 9 22 44 | 14 19 26 |
esa | esa 2976 | 11 15 23 | 8 17 33 | 7 12 25 |
gfz | gfz 2976 | 11 9 23 | 9 14 27 | 11 8 20 |
grg | grg 2784 | 11 16 23 | 15 18 36 | 10 7 21 |
igr | igr 2976 | 10 9 20 | 7 16 24 | 9 9 18 |
igs | igs 2976 | 9 9 19 | 7 15 24 | 8 9 18 |
jpl | jpl 2976 | 26 23 73 | 12 21 61 | 11 19 37 |
mit | mit 2976 | 8 9 22 | 9 14 29 | 11 8 21 |
Table 5.2153.5 GPS week: 2153 Day: 5 MJD: 59320.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 5 6 15 | 8 10 29 | 12 14 26 |
emr | emr 2976 | 16 25 38 | 12 21 44 | 13 16 33 |
esa | esa 2976 | 12 11 23 | 9 17 39 | 14 19 36 |
gfz | gfz 2976 | 11 11 23 | 7 13 27 | 12 9 24 |
grg | grg 2974 | 8 12 18 | 10 15 26 | 10 11 22 |
igr | igr 2969 | 10 7 19 | 13 16 44 | 17 16 31 |
igs | igs 2880 | 8 8 16 | 9 14 31 | 11 12 23 |
jpl | jpl 2976 | 13 19 27 | 10 17 38 | 24 28 37 |
mit | mit 2976 | 9 9 21 | 8 14 27 | 12 10 26 |
Table 5.2153.6 GPS week: 2153 Day: 6 MJD: 59321.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 6 18 | 9 13 25 | 7 8 18 |
emr | emr 2976 | 15 26 36 | 13 20 47 | 11 18 34 |
esa | esa 2976 | 11 12 24 | 10 18 47 | 9 15 29 |
gfz | gfz 2976 | 9 10 25 | 7 14 32 | 13 9 23 |
grg | grg 2976 | 7 12 22 | 10 15 30 | 12 13 26 |
igr | igr 2976 | 8 8 20 | 9 16 35 | 10 11 22 |
igs | igs 2976 | 7 7 17 | 9 15 33 | 10 10 21 |
jpl | jpl 2976 | 12 15 26 | 10 21 50 | 12 19 33 |
mit | mit 2976 | 8 9 24 | 9 14 32 | 12 9 21 |
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 6.2153 GPS week: 2153 MJD: 59315.500-59321.500
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 -2 47 6 -4 | 10 17
| 17 26 88 63 6 | 3
emr uuuuu | -24 -9 37 138 1 | 14 23
| 19 15 131 67 12 | 2
esa uuuuu | 16 -12 74 116 -1 | 39 41
| 7 13 52 73 4 | 2
gfz uuuuu | 8 -1 -7 109 4 | 24 28
| 15 31 59 157 4 | 3
grg uuuuu | 6 6 2 -79 -4 | 10 17
| 17 9 40 51 4 | 3
igr xxxxx | 16 -9 58 -16 -2 | 4 13
| 12 9 27 43 3 | 2
irf xxxxx | 21 6 -30 -17 0 | 3 16
| 13 13 15 6 5 | 3
jpl uuuuu | 31 -3 2 56 3 | 32 35
| 13 9 97 46 6 | 2
mit uuuuu | 3 28 -91 -150 5 | 26 30
| 20 13 28 44 4 | 2
ngs uuuuu | -70 -22 -29 -88 4 | 18 22
| 37 58 47 78 3 | 2
sio xxxxx | 59 -34 -219 -156 5 | 31 35
| 53 68 102 167 11 | 2
Table 7.2153.0 GPS week: 2153 Day: 0 MJD: 59315.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 -20 94 29 3 | 6 12
emr uuuuu | -12 3 -222 144 -3 | 14 21
esa uuuuu | 7 -21 -33 29 -1 | 37 38
gfz uuuuu | 8 16 14 -32 -2 | 21 24
grg uuuuu | 1 -3 31 -79 1 | 8 12
igr xxxxx | -1 4 11 -11 -2 | 2 7
irf xxxxx | 9 6 -28 -19 -6 | 4 14
jpl uuuuu | 38 -15 87 69 -8 | 30 33
mit uuuuu | 1 18 -60 -128 -1 | 24 27
ngs uuuuu | -38 27 6 52 -2 | 14 17
sio xxxxx | 10 -161 -241 -114 -9 | 33 37
Table 7.2153.1 GPS week: 2153 Day: 1 MJD: 59316.500
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 -19 73 32 4 | 9 17
emr uuuuu | -28 -17 66 187 -24 | 16 23
esa uuuuu | 14 -11 110 102 2 | 39 41
gfz uuuuu | -8 -6 -45 -114 8 | 22 26
grg uuuuu | -12 9 29 -120 0 | 11 17
igr xxxxx | 12 -5 64 3 -2 | 4 12
irf xxxxx | 18 3 -25 -13 -4 | 6 16
jpl uuuuu | 36 1 2 91 1 | 31 34
mit uuuuu | 11 25 -138 -87 0 | 27 30
ngs uuuuu | -67 10 -37 -46 7 | 17 21
sio xxxxx | 82 -47 -112 -142 -3 | 33 37
Table 7.2153.2 GPS week: 2153 Day: 2 MJD: 59317.500
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 0 18 65 -4 | 11 16
emr uuuuu | -12 -32 209 82 0 | 14 24
esa uuuuu | 21 -17 99 89 -5 | 39 41
gfz uuuuu | 11 -42 21 205 9 | 23 26
grg uuuuu | -15 15 -31 -100 -4 | 11 17
igr xxxxx | 16 -9 83 -11 -1 | 4 12
irf xxxxx | 21 15 -44 -9 -2 | 5 16
jpl uuuuu | 50 15 -1 90 9 | 31 34
mit uuuuu | 9 44 -118 -137 5 | 26 30
ngs uuuuu | -97 -36 -52 -181 2 | 18 21
sio xxxxx | 115 -60 -123 -41 1 | 30 34
Table 7.2153.3 GPS week: 2153 Day: 3 MJD: 59318.500
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 | 39 -35 18 -110 -2 | 12 17
emr uuuuu | -19 6 73 198 12 | 13 23
esa uuuuu | 11 -7 81 48 -2 | 39 41
gfz uuuuu | 4 -13 -70 251 2 | 25 29
grg uuuuu | 8 -9 43 -50 -10 | 12 18
igr xxxxx | 18 -6 49 41 -2 | 5 13
irf xxxxx | 15 24 -33 -16 -1 | 4 15
jpl uuuuu | 35 -1 55 30 8 | 32 35
mit uuuuu | -10 41 -76 -150 5 | 27 31
ngs uuuuu | -80 3 -101 -97 1 | 19 23
sio xxxxx | 58 -27 -282 -203 9 | 29 32
Table 7.2153.4 GPS week: 2153 Day: 4 MJD: 59319.500
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 15 188 67 -5 | 15 19
emr uuuuu | -2 -23 5 161 7 | 16 26
esa uuuuu | 28 -30 55 236 0 | 42 44
gfz uuuuu | -2 -30 -27 -16 5 | 29 32
grg uuuuu | 16 17 -41 -113 -6 | 14 19
igr xxxxx | 26 -23 84 -69 -1 | 7 14
irf xxxxx | 42 -16 -18 -22 0 | 6 16
jpl uuuuu | 16 -4 -64 103 1 | 35 39
mit uuuuu | 24 8 -69 -189 6 | 29 33
ngs uuuuu | -112 38 -38 -131 5 | 21 25
sio xxxxx | -9 52 -189 -507 6 | 32 35
Table 7.2153.5 GPS week: 2153 Day: 5 MJD: 59320.500
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 5 -101 -11 -8 | 11 20
emr uuuuu | -41 3 89 13 4 | 12 25
esa uuuuu | 14 11 86 128 4 | 38 41
gfz uuuuu | 5 44 -48 255 5 | 25 30
grg uuuuu | 13 4 29 -112 -4 | 9 19
igr xxxxx | 33 -17 76 -78 1 | 4 17
irf xxxxx | 36 14 -9 -26 7 | 0 17
jpl uuuuu | 30 -7 107 -27 0 | 32 37
mit uuuuu | 22 36 -78 -134 11 | 25 31
ngs uuuuu | -92 -119 -33 -63 4 | 18 24
sio xxxxx | 27 1 -183 -78 26 | 28 33
Table 7.2153.6 GPS week: 2153 Day: 6 MJD: 59321.500
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 42 36 -30 -15 | 9 19
emr uuuuu | -56 -6 37 184 9 | 9 22
esa uuuuu | 14 -10 123 178 -6 | 36 39
gfz uuuuu | 39 22 103 214 2 | 24 29
grg uuuuu | 33 6 -49 24 -2 | 7 18
igr xxxxx | 5 -7 36 12 -8 | 2 16
irf xxxxx | 7 -1 -52 -15 6 | -1 17
jpl uuuuu | 10 -7 -175 37 10 | 30 35
mit uuuuu | -33 22 -96 -223 9 | 24 30
ngs uuuuu | -7 -77 49 -150 7 | 17 23
sio xxxxx | 130 6 -406 -9 6 | 29 35
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