[IGSREPORT-21654] Wk 1729 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Mar 15 08:40:00 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1729 (Feb 24, 2013 - Mar 02, 2013)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
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:
igs1729[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1729[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1729[0-6].cls IGS GPS clock combination summary report.
igs17297.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17297.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 | 4 9 4 9
0 | EMR | 8 8 HERS
0 | ESA | 4 9 4 9 UNSA
0 | GFZ | 4 8 9 BOGT NRMD TLSE
0 | GRG | WROC BRAZ WROC
0 | JPL | 8 9 FAA1
0 | MIT | 1 1 MDVJ
1 | COD | 4 9 31 4 9 31 MOBS NTUS SCH2 CHPI MOBS NTUS
1 | EMR | 8 8 STJO HERS STJO
1 | ESA | 4 9 4 9 NOVM
1 | GFZ | 4 8 9 BOGT NRMD STJO
1 | GRG | NICO SCH2 USNO LHAZ MDVJ NICO USNO
1 | JPL | 8 9 FAA1 UNSA
1 | MIT | NTUS TLSE MDVJ NTUS TLSE
2 | COD | 4 9 4 9
2 | EMR | 8 8
2 | ESA | 4 9 4 9 ARTU
2 | GFZ | 4 8 9 ARTU BOGT TWTF
2 | GRG | ARTU KOUC SCH2 KOUC LHAZ NRMD POLV SCH2 UNSA
2 | JPL | 8 9 ARTU
2 | MIT | 18 8 18 KOUR KOUR
3 | COD | 4 9 4 9 KOUC KOUC
3 | EMR | 8 8
3 | ESA | 4 9 4 9 SCH2 LHAZ SCH2 UNSA
3 | GFZ | 4 8 9 BOGT HYDE MKEA NKLG NRMD NTUS SCH2 TIDB TLSE
3 | GRG | HARB KOUC NKLG TLSE ADIS HARB KOUC NKLG POLV TLSE
3 | JPL | 8 9 FAA1
3 | MIT | 5 22 5 22 MDVJ SCH2 TLSE GODE NTUS REUN SCH2
4 | COD | 4 9 4 9 FLRS
4 | EMR | 8 8
4 | ESA | 4 9 4 9 NTUS KELY NTUS UNSA
4 | GFZ | 4 8 9 BOGT CGGN LHAZ TLSE
4 | GRG | 21 21 NICO ADIS HARB
4 | JPL | 8 9
4 | MIT | 1 NTUS GMAS NTUS
5 | COD | 4 4 FLRS KOUC
5 | EMR | 8 8 9 CHUR
5 | ESA | 4 4 NTUS NTUS
5 | GFZ | 4 8 9 BOGT ISPA LHAZ
5 | GRG | 9 9 AREQ HARB MAS1 WROC ADIS AREQ CHPI HARB KIT3
5 | GRG | KOUC NRMD TRO1 WROC
5 | JPL | 8 9
5 | MIT | 10 9 10 NTUS
6 | COD | 4 4 ZAMB
6 | EMR | 8 9 8 9 YEBE YELL HERS SCH2 YEBE YELL
6 | ESA | 4 4 MATE MATE UNSA
6 | GFZ | 4 8 9 BOGT MATE
6 | GRG | 9 9 IRKT THU3 ADIS HOB2 IRKT KIT3 THU3 TLSE ZAMB
6 | JPL | 8
6 | MIT | 9 19 9 19 MAW1 KOSG MAW1 NTUS
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. 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.
7. 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 | -.7 .5 -.8 -63 9 5 -.06
EMR | 0 | 9.0 -1.4 9.2 11 13 0 -.12
ESA | 0 | -.9 3.2 -7.9 47 -165 134 .21
GFZ | 0 | -.4 .7 -.4 -30 -28 -12 -.10
GRG | 0 | 1.5 -6.9 3.7 -29 26 -7 .48
JPL | 0 | 5.7 3.7 7.5 -94 7 -15 -.17
MIT | 0 | -.7 -.6 9.6 -4 -5 -11 -.18
NGS | 0 | -2.2 .8 1.6 -15 7 23 .27
SIO | 0 | -.5 -.4 -4.5 71 -71 331 .10
COD | 1 | -1.2 -.1 -1.4 -73 19 23 -.01
EMR | 1 | 10.2 1.6 15.1 16 3 1 -.41
ESA | 1 | .9 5.8 -4.1 101 -164 139 -.06
GFZ | 1 | -.3 .8 -.7 -13 -37 -2 -.22
GRG | 1 | 3.0 -.9 11.3 -24 36 -8 .18
JPL | 1 | .3 5.1 13.7 -136 -9 -37 -.28
MIT | 1 | -6.8 2.8 5.8 -6 0 -16 -.11
NGS | 1 | .9 1.9 4.9 -27 -8 29 .42
SIO | 1 | -2.7 5.0 8.6 167 -17 285 -.20
COD | 2 | -1.5 .1 -1.3 -62 12 7 -.01
EMR | 2 | 11.6 .4 8.2 11 13 -5 -.20
ESA | 2 | -.6 3.9 -5.4 77 -133 144 .01
GFZ | 2 | -.2 .7 -.6 -24 -33 -7 -.10
GRG | 2 | -.7 -3.1 5.5 -29 56 -6 .26
JPL | 2 | 3.0 3.2 15.2 -82 51 26 .19
MIT | 2 | -.1 .7 6.5 -7 1 -15 -.02
NGS | 2 | 8.3 -2.0 10.9 -64 -55 62 .41
SIO | 2 | 3.6 .8 .8 63 -131 90 .03
COD | 3 | -.3 .9 -1.4 -57 10 11 .01
EMR | 3 | 10.5 -2.1 18.1 4 20 1 -.14
ESA | 3 | 6.2 .8 -7.7 38 -238 132 .16
GFZ | 3 | .6 .6 -.5 -24 -38 -4 -.06
GRG | 3 | 4.4 -6.3 11.6 -25 37 -5 .44
JPL | 3 | 6.8 4.0 16.7 -60 25 28 .29
MIT | 3 | .4 -1.3 7.8 -4 3 -10 .01
NGS | 3 | 8.2 1.3 9.9 -38 -56 72 .52
SIO | 3 | 4.2 2.2 10.1 92 -100 94 -.02
COD | 4 | .3 .6 -.7 -47 -5 30 .08
EMR | 4 | 11.6 -2.4 7.9 2 7 2 .06
ESA | 4 | .4 3.6 -11.3 66 -186 152 .21
GFZ | 4 | .4 .5 -.5 -15 -32 -2 .05
GRG | 4 | 1.3 -4.5 -.8 -16 33 -8 .41
JPL | 4 | 6.1 .8 21.0 -77 22 -19 .15
MIT | 4 | -1.7 .1 5.4 -6 3 -10 .17
NGS | 4 | 2.0 -4.8 9.5 -70 -10 21 .39
SIO | 4 | 1.5 .4 2.9 30 -77 74 .19
COD | 5 | .1 .5 -.3 -58 8 -1 -.03
EMR | 5 | 1.1 -2.6 8.8 -1 4 4 -.22
ESA | 5 | -.2 2.8 -8.6 54 -150 149 .13
GFZ | 5 | .5 .4 -.3 -30 -32 -10 -.08
GRG | 5 | -5.5 -4.8 3.6 -7 35 9 .34
JPL | 5 | -.6 -2.9 18.2 -56 1 -15 .09
MIT | 5 | -1.4 2.1 10.2 0 -2 -15 .01
NGS | 5 | 6.7 .9 5.7 -38 -38 65 .39
SIO | 5 | 2.9 2.6 18.3 46 -18 -88 .08
COD | 6 | .0 .6 -1.3 -35 0 7 -.02
EMR | 6 | 10.8 -8.4 15.9 0 13 -2 -.15
ESA | 6 | 1.1 4.4 -10.8 82 -195 130 .19
GFZ | 6 | .2 .5 -.1 -23 -22 -7 .04
GRG | 6 | 3.6 -8.0 6.6 4 27 1 .41
JPL | 6 | 3.6 -2.4 15.6 -82 35 -32 -.16
MIT | 6 | 4.2 .9 13.0 -2 3 -13 .05
NGS | 6 | .0 -2.8 8.2 -69 1 6 .50
SIO | 6 | 4.0 .8 -.7 54 -123 -18 .11
8. 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.
9. 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.
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 1.1729.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1729.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 2.1729.[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 3.1729.[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 5.1729.0-6). 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 1729 summary. (Feb 24, 2013 - Mar 02, 2013)
Table 1.1729.a GPS week: 1729 MJD: 56347.000-56353.000
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 263| -1 1 0 -14 32 3 -.41 11 10 | -1060 145 19 85
| 0 0 1 24 27 12 .02 | 456 792
emr 79| 1 -2 4 -7 2 8 .24 18 18 | 1241 -153 15 107
| 1 0 1 29 33 13 .04 | 1167 961
esa 172| 1 0 0 42 -67 6 .11 6 6 | -995 141 9 102
| 0 0 1 26 45 13 .02 | 931 1777
gfz 201| 0 -1 -3 19 2 -19 -.41 11 10 | 214 -249 20 125
| 0 1 0 70 84 11 .03 | 324 369
grg 140| 0 -1 -1 -5 42 -2 .59 17 16 | -89 18 18 142
| 1 0 2 13 18 20 .05 | 261 427
igr n/a| 0 0 -1 -35 77 -42 -.13 4 4 | -1009 -568 16 91
| 0 0 0 17 29 7 .05 | 1771 883
jpl 80| 0 -1 2 -33 34 -8 .36 17 17 | 2414 -402 18 112
| 1 1 0 23 41 9 .03 | 1228 859
mit 239| 0 0 0 16 20 10 -.54 14 11 | -172 233 22 187
| 1 0 1 28 24 30 .02 | 275 478
ngs 245| 0 0 0 -71 53 -1 .40 12 10 | 99537 37172 1789 3382
| 0 1 2 50 55 16 .05 | 265949 98239
sio 253| 0 -1 1 21 -59 57 -.06 19 17 | --- --- --- ---
| 0 1 1 39 61 155 .05 | --- ---
Table 1.1729.b GPS week : 1729 MJD: 56347.000-56353.000
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 | 5 5 5 5 5 5 5 |
2 | 5 4 4 4 4 4 4 |
3 | 3 4 4 4 4 4 4 |
4 | 5 5 5 6 6 7 9 |
5 | 5 4 5 5 4 5 5 |
6 | 4 4 4 4 4 4 4 |
7 | 5 6 5 5 5 4 4 |
8 | 6 6 6 7 6 6 6 |
9 | 8 7 7 6 6 6 5 |
10 | 4 4 4 4 4 4 5 |
11 | 3 4 4 4 4 4 4 |
12 | 5 5 5 6 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 5 5 4 |
15 | 6 5 5 5 5 6 5 |
16 | 4 4 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 4 4 5 5 5 4 4 |
20 | 4 5 5 5 4 5 5 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 4 4 5 4 5 |
23 | 4 4 4 4 4 4 4 |
24 | 8 5 5 5 5 6 5 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 0 0 0 0 0 0 0 |
28 | 5 5 5 5 5 5 5 |
29 | 5 5 5 4 5 5 4 |
30 | 3 3 4 3 4 4 4 |
31 | 4 6 5 5 5 5 5 |
32 | 3 3 4 4 4 4 4 |
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
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1729.0 GPS week: 1729 Day: 0 MJD: 56347.000
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 263| -1 1 -2 13 73 7 -.42 10 10 | -569 -146 18 74
emr 80| 4 -3 5 49 72 29 .29 18 18 | 1906 857 13 79
esa 172| 1 0 0 85 -10 5 .09 6 6 | -1306 340 10 97
gfz 196| 0 1 -3 -101 -115 -18 -.44 10 10 | 657 -494 21 121
grg 138| 0 0 -1 1 21 -26 .67 16 15 | -245 468 23 145
igr n/a| 0 0 0 -13 114 -49 -.08 4 4 | 861 279 15 87
jpl 80| 1 -1 3 -13 94 -4 .35 17 17 | 3387 559 15 105
mit 239| 0 -1 0 12 14 44 -.55 14 11 | -96 158 24 169
ngs 243| -2 0 0 -135 -52 -35 .44 11 10 | -565 -215 1923 3550
sio 251| 0 -2 3 25 -21 287 .04 20 18 | --- --- --- ---
Table 2.1729.1 GPS week: 1729 Day: 1 MJD: 56348.000
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 262| -1 1 -2 -11 -1 14 -.41 10 10 | -773 -376 20 94
emr 80| 2 -2 5 -18 -9 -5 .25 18 18 | 2839 -887 14 106
esa 172| 1 0 0 74 -68 -15 .10 6 6 | 301 -3188 10 91
gfz 200| 0 -2 -2 5 31 -11 -.40 10 10 | 615 -888 19 127
grg 140| 0 -1 2 -25 38 0 .63 16 15 | 384 -761 16 129
igr n/a| -1 0 -2 -44 42 -41 -.11 5 5 | 1285 -1409 18 95
jpl 80| 1 -3 3 -63 13 2 .37 17 17 | 3994 -1015 20 123
mit 240| -1 0 -1 -5 29 44 -.55 15 12 | 113 -198 23 179
ngs 244| 0 0 -1 -53 62 4 .45 11 10 | -767 -427 1672 3517
sio 255| -1 -2 0 99 7 236 -.04 18 17 | --- --- --- ---
Table 2.1729.2 GPS week: 1729 Day: 2 MJD: 56349.000
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 264| -1 1 -1 -29 0 -11 -.43 11 10 | -1261 188 19 89
emr 79| 3 -1 2 -45 -28 14 .23 17 17 | 2391 -1603 14 103
esa 172| 1 0 0 36 -55 0 .09 6 6 | -1738 -41 10 109
gfz 204| 0 -1 -2 103 90 -33 -.37 12 11 | -53 -25 22 133
grg 141| 0 0 0 -18 74 26 .60 17 16 | -41 34 15 160
igr n/a| 0 0 -1 -47 32 -35 -.14 4 4 | 327 -1825 15 102
jpl 80| 0 -1 2 -65 -28 0 .37 17 17 | 3634 -1532 18 118
mit 240| -1 0 -2 38 -17 27 -.53 14 11 | -88 198 24 200
ngs 245| 0 -1 1 -91 63 12 .46 12 10 | -1227 87 1980 3494
sio 252| 0 -1 0 34 -148 46 -.07 17 18 | --- --- --- ---
Table 2.1729.3 GPS week: 1729 Day: 3 MJD: 56350.000
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 265| -1 2 -1 -32 21 5 -.44 10 10 | -1285 -31 19 85
emr 79| 2 -1 4 -4 0 16 .20 18 18 | 386 -526 15 99
esa 172| 1 0 0 24 -155 3 .12 6 6 | -2294 2578 10 109
gfz 204| 1 -2 -4 29 117 -16 -.43 13 12 | -17 130 19 122
grg 141| 1 -2 0 -9 61 -13 .50 18 17 | -171 258 20 133
igr n/a| 0 1 -1 -49 84 -37 -.23 4 4 | -1782 -932 15 83
jpl 80| -1 -2 0 -33 42 -12 .33 16 16 | 1794 -742 19 118
mit 240| 0 0 -1 -9 57 20 -.55 14 11 | -359 333 19 191
ngs 246| 0 0 2 5 117 -5 .38 11 9 | 702654 259954 1883 3485
sio 251| 0 -1 1 13 -59 54 -.11 18 17 | --- --- --- ---
Table 2.1729.4 GPS week: 1729 Day: 4 MJD: 56351.000
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 265| 0 0 0 -46 40 23 -.41 11 10 | -1882 1883 19 84
emr 80| 1 0 4 -16 10 1 .19 19 19 | -290 1051 16 133
esa 172| 1 1 -2 27 -46 12 .13 6 6 | -946 -111 9 102
gfz 200| 1 0 -3 102 -53 -12 -.45 12 12 | 366 -139 21 133
grg 143| 0 -1 -4 -8 39 24 .56 17 17 | -441 382 16 134
igr n/a| 0 0 -1 -51 96 -51 -.17 5 5 | -2826 484 16 99
jpl 80| 0 0 2 -22 73 -26 .32 17 17 | 922 745 17 109
mit 240| 0 -1 0 66 7 -20 -.57 14 11 | -693 1240 22 199
ngs 245| -1 -1 3 -124 21 -9 .37 11 10 | -1726 1352 1810 3231
sio 254| 0 -2 2 0 -72 0 -.11 18 18 | --- --- --- ---
Table 2.1729.5 GPS week: 1729 Day: 5 MJD: 56352.000
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 262| -2 2 1 20 55 -4 -.39 12 11 | -984 -97 18 84
emr 77| 0 -2 3 3 -24 11 .23 20 20 | 367 360 14 110
esa 172| 0 1 1 24 -49 25 .11 6 6 | 94 -55 10 115
gfz 202| 1 -1 -4 -3 -59 -35 -.40 10 9 | -10 -419 20 129
grg 142| 2 -1 -3 9 32 -20 .60 17 16 | -169 45 21 144
igr n/a| 0 0 -1 -8 82 -48 -.10 4 4 | -2721 85 16 91
jpl 80| 1 -1 2 -2 8 -13 .40 18 17 | 1329 46 18 108
mit 240| 0 -1 0 -8 39 -11 -.53 15 12 | -145 -21 24 184
ngs 247| 0 0 0 -67 74 12 .36 12 9 | -978 -99 1628 2855
sio 254| 1 0 1 -26 3 -134 -.07 19 18 | --- --- --- ---
Table 2.1729.6 GPS week: 1729 Day: 6 MJD: 56353.000
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 263| -1 1 1 -12 40 -7 -.38 11 10 | -669 -401 22 86
emr 80| 0 -2 4 -22 -2 -7 .27 18 18 | 1089 -323 20 120
esa 172| 1 1 0 23 -86 16 .11 6 5 | -1079 1470 10 94
gfz 201| 1 -1 -2 -2 4 -7 -.39 10 9 | -60 90 19 111
grg 141| 2 0 -3 10 29 -9 .58 17 16 | 59 -294 21 150
igr n/a| 0 0 -1 -34 87 -35 -.10 4 4 | -2213 -658 17 81
jpl 80| -1 0 1 -30 36 -7 .40 17 17 | 1839 -878 21 106
mit 240| 1 0 1 22 12 -30 -.51 15 11 | 61 -73 22 191
ngs 246| -1 -2 -2 -31 91 7 .32 12 10 | -629 -448 1631 3547
sio 257| 0 0 1 0 -126 -86 -.06 19 16 | --- --- --- ---
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 3.1729.0 GPS week: 1729 Day: 0 MJD: 56347.000
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 | 12 24 6 11 12 4 16 9 13 20 4 | 19 17 25 19 28 21 32 14 29 22 19
2E | 8 20 4 8 20 3 18 11 11 12 4 | 31 36 35 29 35 31 35 28 38 36 31
3 | 8 12 4 11 10 4 11 10 10 13 3 | 20 22 19 23 26 19 21 20 27 19 18
4E | 14 16 7 12 18 5 18 12 14 16 5 | 126 115 122 129 109 123 113 128 119 114 121
5 | 10 21 7 11 15 4 20 6 10 18 4 | 32 32 31 32 38 27 31 26 31 27 28
6 | 6 13 5 11 10 4 12 12 10 15 3 | 16 23 21 22 28 19 24 22 28 20 20
7E | 13 21 7 7 14 5 14 14 11 20 4 | 24 34 31 34 35 30 33 42 34 39 31
8E | 16 21 6 8 25 6 20 12 14 15 5 | 22 37 24 17 35 21 37 19 27 25 21
9E | 10 32 10 12 16 5 25 37 15 14 7 | 33 52 36 37 40 34 47 42 44 37 35
10 | 9 14 6 9 15 5 17 10 12 11 4 | 41 45 50 43 48 45 45 43 42 41 43
11E | 7 12 3 9 9 5 11 9 13 14 3 | 15 21 18 17 26 18 22 18 24 21 16
12 | 10 18 5 11 19 5 17 14 12 21 4 | 30 28 26 24 37 23 28 29 27 25 25
13 | 8 17 6 8 16 5 17 11 11 22 4 | 26 34 28 24 36 25 36 29 24 24 24
14 | 7 18 5 13 13 6 17 14 8 25 4 | 34 33 34 37 40 33 34 34 33 32 33
15 | 17 21 9 10 18 6 24 11 13 25 5 | 31 35 35 36 43 32 34 28 32 35 31
16 | 9 19 6 11 13 4 19 7 11 29 4 | 20 26 26 29 36 24 28 21 30 20 23
17 | 12 19 6 14 20 5 20 13 12 24 5 | 25 37 26 22 38 20 34 19 30 22 23
18 | 12 17 6 16 16 5 19 14 14 22 5 | 27 25 27 34 31 26 27 29 20 24 25
19 | 8 16 6 10 12 4 17 11 12 23 4 | 17 29 20 18 27 19 30 17 26 23 17
20 | 8 17 8 12 10 4 17 15 8 30 4 | 28 25 26 30 24 22 26 25 19 26 22
21E | 8 13 3 10 13 3 15 9 9 16 3 | 38 43 43 36 52 38 45 37 40 42 39
22 | 8 17 4 9 14 6 19 16 10 25 4 | 33 29 33 37 39 31 31 35 27 28 30
23 | 8 18 7 11 13 4 17 13 8 27 4 | 30 32 31 28 32 28 33 28 25 22 26
24E | 13 24 8 11 32 5 19 34 19 --- 7 | 47 51 41 43 47 41 46 38 48 --- 41
25 | 5 13 4 11 17 3 14 13 10 13 4 | 23 25 24 21 37 21 30 30 25 21 23
26 | 8 13 6 9 14 2 17 7 9 16 3 | 26 27 30 27 34 25 27 25 26 28 25
X27 | 8 --- --- --- --- 76 --- --- --- --- 0 | 92 --- --- --- --- 33 --- --- --- --- 94
28 | 14 18 5 11 13 3 21 14 13 20 4 | 24 35 34 38 43 29 32 30 38 29 31
29 | 17 21 5 10 17 4 19 12 11 20 5 | 22 29 23 20 23 20 30 21 25 25 19
30 | 7 10 5 8 12 3 12 8 7 15 3 | 22 25 25 22 27 23 26 23 25 23 21
31E | 10 15 4 8 13 3 18 14 11 14 4 | 72 67 68 74 72 69 67 73 78 69 71
32 | 8 12 5 8 12 3 9 5 9 20 3 | 24 28 30 27 36 26 31 28 26 29 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 10 16 4 17 14 11 20 |T 33 35 33 33 38 31 35 32 34 31 32
WRMS | 10 18 6 10 15 4 17 11 10 18 |NE 29 29 28 28 34 25 30 26 27 25 28
MEDI | 8 17 6 11 14 4 17 12 11 20 |MD 26 32 30 29 36 26 32 28 28 25 25
Table 3.1729.1 GPS week: 1729 Day: 1 MJD: 56348.000
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 | 13 25 6 10 13 6 19 10 11 16 4 | 21 21 23 15 30 23 35 18 25 22 20
2E | 9 17 5 9 17 5 19 10 8 11 4 | 32 35 33 27 37 31 34 27 38 35 32
3 | 7 10 6 9 15 3 10 7 12 13 3 | 19 24 20 19 27 21 21 20 30 23 21
4E | 13 17 8 18 13 6 18 14 11 15 5 | 125 114 120 126 113 119 112 124 115 112 119
5 | 9 18 6 8 12 4 20 7 9 17 4 | 25 28 21 22 32 22 29 20 28 23 23
6 | 5 12 8 9 16 3 13 11 12 16 3 | 19 23 21 18 28 20 25 20 26 24 21
7E | 12 22 9 8 16 6 17 31 12 14 6 | 25 28 21 20 28 20 26 28 26 20 20
8E | 16 23 6 9 27 6 18 17 19 17 6 | 21 33 17 17 29 15 28 16 30 22 18
9E | 11 27 8 9 16 4 25 32 12 14 6 | 21 38 21 20 30 21 37 37 28 26 22
10 | 13 13 5 7 14 5 13 8 8 9 3 | 36 33 36 33 39 35 34 35 37 35 35
11E | 7 12 4 9 13 5 12 9 12 15 3 | 17 23 18 19 29 20 27 22 23 21 19
12 | 9 16 7 11 21 4 18 15 11 19 4 | 18 26 15 17 30 15 26 17 23 19 17
13 | 5 19 8 9 15 6 19 13 10 16 4 | 20 29 19 18 31 18 30 20 22 17 19
14 | 6 18 4 11 17 4 18 12 8 21 4 | 22 26 21 24 30 22 26 24 27 26 23
15 | 16 22 7 9 15 5 19 9 8 25 4 | 21 29 21 21 32 21 29 19 28 24 21
16 | 8 20 7 8 13 5 19 6 13 28 4 | 18 28 23 19 30 20 29 18 24 18 21
17 | 9 20 8 14 19 5 22 9 8 23 5 | 22 30 18 14 34 18 29 18 26 18 19
18 | 13 19 5 13 15 4 19 14 9 23 4 | 28 26 21 23 19 21 23 22 23 22 22
19 | 10 16 6 9 17 4 15 12 10 22 4 | 20 27 17 17 29 18 28 20 26 21 20
20 | 9 20 8 14 11 4 17 13 12 25 4 | 22 25 17 26 19 17 25 20 19 20 18
21E | 8 14 6 9 14 4 15 10 11 14 3 | 33 41 38 38 43 34 42 35 45 39 37
22 | 6 17 4 8 13 4 18 15 11 24 4 | 25 26 23 22 25 23 25 24 23 23 22
23 | 7 18 7 11 12 5 17 12 13 22 4 | 23 28 22 24 26 22 28 21 25 19 21
24E | 9 19 7 10 22 4 16 23 11 --- 5 | 29 33 22 22 28 25 28 37 26 --- 24
25 | 9 14 4 8 17 4 15 12 11 13 4 | 16 21 16 16 27 13 28 17 21 17 17
26 | 6 13 5 8 14 2 15 9 9 13 3 | 20 25 23 19 28 20 25 18 25 23 20
X27 | 6 --- --- --- --- 16 --- --- --- --- 0 | 31 --- --- --- --- 31 --- --- --- --- 31
28 | 10 20 6 9 16 4 19 12 15 15 4 | 22 30 27 24 40 24 30 24 32 25 25
29 | 17 21 6 8 16 4 22 14 11 20 5 | 17 28 16 16 18 17 28 17 19 20 16
30 | 6 10 4 7 13 4 9 11 12 13 3 | 22 29 27 26 29 24 25 28 29 28 26
31E | 10 15 9 8 16 8 16 36 12 12 6 | 37 38 36 36 44 37 39 31 41 33 34
32 | 10 13 4 10 11 4 10 6 8 19 3 | 17 23 21 20 24 18 26 20 24 25 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 10 16 5 17 15 11 18 |T 26 31 25 25 32 25 31 26 30 26 25
WRMS | 10 18 6 10 15 5 17 12 10 17 |NE 21 26 21 20 28 20 27 21 25 22 21
MEDI | 9 18 6 9 15 4 18 12 11 16 |MD 22 28 21 20 29 21 28 20 26 23 21
Table 3.1729.2 GPS week: 1729 Day: 2 MJD: 56349.000
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 | 15 26 6 12 15 5 16 11 10 11 5 | 25 23 28 22 37 25 34 24 29 26 25
2E | 9 16 5 9 17 4 18 10 9 12 4 | 36 41 39 34 40 36 39 34 42 41 37
3 | 11 9 3 12 20 3 11 8 12 14 4 | 29 28 22 23 30 22 31 22 24 24 25
4E | 14 17 7 16 20 4 17 12 8 15 5 | 107 95 100 109 94 102 96 108 96 95 101
5 | 10 17 6 11 15 3 20 9 13 16 4 | 25 32 26 26 34 25 34 25 30 27 26
6 | 5 11 4 12 19 3 11 9 11 17 3 | 23 29 24 23 32 24 32 24 27 26 25
7E | 13 19 7 11 14 4 16 24 11 13 5 | 22 31 27 20 32 24 30 35 30 25 25
8E | 17 26 6 11 30 6 20 15 20 18 6 | 22 39 22 18 34 19 33 23 31 28 22
9E | 15 27 9 9 18 5 26 34 13 15 7 | 25 45 26 24 33 24 43 32 28 31 25
10 | 10 12 4 9 12 2 14 9 9 8 3 | 31 29 29 27 33 29 33 31 26 30 29
11E | 13 11 4 11 19 4 10 15 12 13 4 | 22 26 20 20 30 20 31 25 23 22 21
12 | 10 16 6 11 21 4 18 14 13 17 4 | 27 32 25 24 37 27 32 29 31 29 27
13 | 6 16 6 11 16 4 17 13 12 15 4 | 23 32 23 22 33 22 31 28 24 24 23
14 | 7 18 4 12 19 4 14 11 7 21 4 | 27 31 27 30 36 28 34 30 29 29 28
15 | 13 19 9 15 15 6 21 8 13 24 5 | 29 35 31 32 38 30 35 28 30 36 29
16 | 9 20 7 14 15 3 21 9 16 28 4 | 24 29 26 26 33 23 29 22 24 22 24
17 | 12 20 6 15 19 3 25 10 11 23 5 | 21 34 22 18 33 22 37 23 25 26 22
18 | 12 20 6 16 15 5 16 11 8 22 4 | 26 27 20 24 21 22 28 23 19 22 21
19 | 11 14 6 13 18 4 15 9 13 18 4 | 25 31 19 19 27 18 32 19 26 24 22
20 | 7 18 6 15 13 4 18 11 11 22 4 | 22 27 20 24 22 19 27 24 18 23 19
21E | 6 15 4 10 15 5 15 11 10 16 3 | 20 29 22 17 30 21 29 17 24 24 22
22 | 8 18 4 12 15 5 15 14 10 24 4 | 26 29 25 28 30 27 30 26 21 23 25
23 | 5 18 6 13 12 3 16 9 13 20 4 | 23 30 24 25 30 23 29 26 25 21 23
24E | 10 21 9 10 18 3 14 21 14 15 5 | 37 40 37 34 43 34 38 33 38 31 35
25 | 10 15 5 9 18 4 16 11 11 12 4 | 25 29 25 21 35 25 36 31 27 30 26
26 | 8 12 5 12 14 3 15 8 14 16 4 | 21 30 26 24 31 23 27 22 29 31 24
X27 | 7 --- --- --- --- 61 --- --- --- --- 0 | 41 --- --- --- --- 38 --- --- --- --- 42
28 | 13 18 7 12 17 3 19 14 12 13 5 | 18 30 24 25 35 22 30 23 25 22 23
29 | 14 16 6 8 16 3 20 10 8 21 4 | 22 29 19 21 22 20 31 24 22 30 21
30 | 7 11 4 11 17 2 12 8 16 14 3 | 23 30 23 22 31 25 32 26 27 22 25
31E | 7 17 7 10 16 5 17 23 11 10 5 | 35 38 33 28 38 32 37 41 40 35 34
32 | 7 12 4 12 16 3 10 6 10 19 3 | 22 31 25 24 32 25 31 25 23 29 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 6 12 17 4 17 14 12 17 |T 28 33 27 26 34 27 34 29 29 29 28
WRMS | 10 17 6 11 16 4 17 11 10 18 |NE 25 30 24 24 31 24 31 25 25 26 25
MEDI | 10 17 6 12 16 4 16 11 11 16 |MD 25 30 25 24 33 24 32 25 27 26 25
Table 3.1729.3 GPS week: 1729 Day: 3 MJD: 56350.000
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 | 13 24 6 11 10 4 14 15 10 9 4 | 22 25 27 22 32 23 32 25 29 26 26
2E | 7 17 5 12 17 3 19 13 7 16 4 | 34 38 34 31 35 31 35 27 35 33 34
3 | 8 10 3 13 17 5 9 8 10 15 3 | 26 30 26 25 31 24 29 24 27 27 27
4E | 15 18 8 17 30 7 17 21 13 18 6 | 111 101 103 110 97 105 98 112 100 96 104
5 | 11 20 6 16 31 5 19 8 7 19 5 | 27 32 25 31 40 24 33 27 26 26 28
6 | 9 12 4 15 13 4 9 10 7 16 3 | 22 29 23 23 29 21 28 22 25 23 24
7E | 9 20 8 12 15 5 15 21 12 18 5 | 26 33 26 23 32 24 32 30 30 25 28
8E | 20 24 8 13 29 5 19 16 22 18 6 | 23 36 21 22 31 17 33 21 32 25 23
9E | 15 25 7 12 17 4 23 22 11 12 5 | 24 42 22 19 31 21 39 27 25 25 24
10 | 10 14 5 12 13 3 10 11 8 16 3 | 38 36 39 39 42 37 39 36 36 36 38
11E | 8 10 5 13 17 3 13 13 8 15 3 | 23 27 25 22 29 22 30 27 26 22 25
12 | 14 20 8 11 24 4 19 17 12 18 5 | 31 31 22 20 38 22 26 28 28 26 26
13 | 8 18 6 11 16 5 15 12 9 16 4 | 30 35 27 27 37 26 35 28 25 25 28
14 | 7 19 5 16 20 4 14 12 7 18 4 | 27 33 28 36 38 27 31 28 28 29 30
15 | 11 22 7 16 17 4 22 10 10 24 5 | 27 36 30 36 39 30 35 27 34 32 31
16 | 10 21 7 14 16 3 21 10 11 27 4 | 22 27 25 26 33 21 29 22 22 22 24
17 | 11 19 8 15 18 4 22 12 9 25 5 | 22 34 20 19 34 20 34 20 25 25 23
18 | 9 20 5 18 17 4 17 10 8 21 4 | 24 28 22 29 25 21 25 22 19 21 23
19 | 7 17 6 13 19 4 17 10 13 20 4 | 22 32 24 21 30 21 32 19 26 25 24
20 | 10 18 7 13 12 4 18 12 10 22 4 | 31 33 27 33 28 26 30 28 24 30 29
21E | 6 16 4 12 12 4 13 11 10 15 3 | 31 40 35 33 38 30 40 30 35 34 34
22 | 5 19 5 12 14 4 16 14 11 23 4 | 28 30 28 33 35 26 28 26 21 24 28
23 | 10 18 6 13 12 5 16 8 12 21 4 | 36 36 30 33 37 29 36 30 27 27 32
24E | 11 21 6 12 18 4 13 18 10 16 4 | 27 33 30 25 43 27 33 28 33 27 30
25 | 9 14 4 11 18 3 15 10 8 13 4 | 23 29 25 17 36 24 34 26 25 26 26
26 | 9 14 5 13 14 3 13 7 8 14 3 | 27 31 28 28 34 25 32 27 27 28 29
X27 | 7 --- --- --- --- 43 --- --- --- --- 0 | 38 --- --- --- --- 31 --- --- --- --- 40
28 | 13 19 7 12 21 3 16 14 13 15 5 | 18 29 25 26 40 22 29 27 27 23 25
29 | 10 19 5 10 17 4 18 10 6 19 4 | 20 31 22 24 26 19 30 22 21 27 23
30 | 5 13 5 10 14 4 12 9 8 14 3 | 29 33 31 31 36 29 31 29 30 27 31
31E | 8 21 6 8 12 5 16 25 11 12 5 | 27 30 22 21 34 21 28 31 31 27 26
32 | 8 12 5 12 15 3 12 7 12 20 3 | 29 33 32 30 37 27 33 29 24 34 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 13 18 4 16 14 11 18 |T 29 34 29 29 36 27 34 29 29 29 30
WRMS | 10 18 6 12 17 4 16 11 9 17 |NE 27 31 26 27 34 25 31 26 26 26 28
MEDI | 9 19 6 12 17 4 16 12 10 18 |MD 27 33 26 26 35 24 32 27 27 26 28
Table 3.1729.4 GPS week: 1729 Day: 4 MJD: 56351.000
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 | 9 25 7 9 18 5 16 11 11 11 4 | 22 23 31 23 33 26 31 26 34 30 26
2E | 9 18 5 8 13 5 18 12 9 17 4 | 41 47 45 40 46 41 42 39 48 47 43
3 | 12 13 3 11 19 3 11 6 12 14 4 | 16 20 18 17 24 16 19 15 19 16 16
4E | 15 23 9 15 20 5 18 23 13 21 6 | 109 93 102 111 95 104 95 113 103 95 103
5 | 8 18 5 13 13 4 21 9 10 20 4 | 23 33 29 32 40 25 31 28 28 32 27
6 | 4 13 3 12 16 5 11 8 9 13 3 | 17 23 21 21 26 18 24 20 23 18 20
7E | 11 16 6 11 16 6 16 15 10 15 4 | 15 17 16 14 17 11 18 18 20 12 12
8E | 21 25 5 14 28 5 19 16 17 18 6 | 22 35 23 20 30 19 30 21 32 26 20
9E | 18 24 7 8 16 3 22 23 12 11 6 | 23 39 23 20 32 21 35 26 25 25 22
10 | 9 15 5 12 16 3 13 17 7 16 4 | 30 34 36 33 39 34 33 39 35 36 34
11E | 7 12 5 11 18 4 11 12 13 14 4 | 15 24 22 17 25 19 23 19 26 21 18
12 | 11 19 6 8 22 5 20 17 12 20 5 | 28 30 25 20 35 26 28 31 38 27 26
13 | 7 19 5 10 16 4 17 10 11 16 4 | 20 30 24 24 36 22 31 27 22 22 23
14 | 8 23 6 14 14 6 15 14 13 25 4 | 28 32 33 35 36 29 30 30 36 33 30
15 | 17 23 7 12 16 3 24 11 9 23 5 | 27 34 27 29 36 27 31 24 33 31 25
16 | 6 23 5 14 16 4 19 9 12 28 4 | 19 28 25 24 34 23 28 21 27 23 23
17 | 14 21 7 13 17 4 21 9 7 25 4 | 20 32 23 18 32 20 32 19 27 27 22
18 | 12 21 7 18 14 7 18 13 12 20 5 | 19 22 20 24 21 17 23 21 17 18 17
19 | 9 19 7 16 20 3 18 9 13 18 4 | 18 31 24 23 26 19 30 15 24 22 20
20 | 9 19 5 12 17 5 17 8 10 25 4 | 22 25 22 25 25 20 24 21 19 24 20
21E | 7 17 4 12 17 5 15 12 13 13 4 | 28 36 34 33 41 29 34 29 37 32 32
22 | 7 19 5 13 14 5 16 21 12 23 4 | 22 23 25 26 31 23 25 27 22 20 22
23 | 7 19 5 10 14 4 16 4 14 23 4 | 24 29 26 28 32 24 29 26 25 20 24
24E | 13 17 7 8 14 3 12 18 12 16 4 | 32 33 28 25 30 29 31 31 33 33 28
25 | 8 14 4 9 18 5 16 15 13 13 4 | 20 23 22 17 31 21 29 26 29 24 21
26 | 11 13 3 13 14 3 13 7 8 17 3 | 22 24 24 24 27 21 22 22 26 29 22
X27 | 7 --- --- --- --- 48 --- --- --- --- 0 | 44 --- --- --- --- 40 --- --- --- --- 45
28 | 14 21 6 13 17 5 18 14 11 16 5 | 20 36 29 28 38 25 31 28 31 28 27
29 | 13 18 6 8 16 4 21 10 11 18 4 | 17 25 19 20 22 17 28 20 22 24 18
30 | 5 14 4 11 17 3 9 9 9 13 3 | 14 20 21 20 22 17 19 16 21 15 16
31E | 8 17 6 6 18 5 15 24 11 12 5 | 26 28 29 24 37 24 28 34 31 30 27
32 | 6 13 5 12 17 6 10 7 13 20 3 | 18 27 28 23 33 23 26 23 25 25 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 6 12 17 5 17 14 11 18 |T 25 30 28 27 33 25 30 27 30 27 26
WRMS | 10 19 6 12 17 5 17 11 10 18 |NE 22 27 24 24 30 23 27 23 26 24 23
MEDI | 9 19 5 12 16 5 16 12 12 17 |MD 22 29 25 24 32 23 29 26 27 25 23
Table 3.1729.5 GPS week: 1729 Day: 5 MJD: 56352.000
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 | 13 26 7 9 13 4 13 24 11 15 5 | 19 21 24 16 30 19 30 24 29 23 20
2E | 9 18 4 7 20 3 18 8 12 10 4 | 36 41 38 34 43 36 40 35 41 40 37
3 | 11 15 6 13 17 4 10 8 11 14 4 | 22 19 20 20 27 18 24 15 22 16 18
4E | 21 23 9 12 30 4 22 30 16 17 7 | 109 93 99 105 89 101 92 115 101 94 101
5 | 15 24 6 11 16 4 21 5 12 17 5 | 26 29 24 27 36 23 29 21 27 23 23
6 | 5 15 6 9 14 2 11 8 11 12 3 | 20 24 22 18 26 18 27 17 24 16 20
7E | 11 17 6 8 14 4 15 10 12 10 4 | 21 22 20 16 22 18 24 17 28 14 18
8E | 19 27 8 8 21 5 21 16 24 19 6 | 21 35 20 17 27 18 31 21 31 26 19
9E | 12 25 7 6 17 4 23 25 13 14 5 | 26 38 23 19 28 20 36 30 26 25 22
10 | 12 17 4 6 15 2 14 16 5 14 4 | 28 30 34 30 35 31 30 35 33 32 31
11E | 10 10 5 10 17 5 10 15 11 13 4 | 14 22 17 16 26 17 22 21 22 17 15
12 | 9 21 7 10 18 4 20 21 13 20 5 | 20 27 21 22 31 20 26 31 29 19 21
13 | 8 21 6 10 15 4 19 10 8 23 4 | 23 33 23 24 34 22 31 23 23 19 23
14 | 7 20 6 15 15 4 18 11 13 22 4 | 20 26 23 30 30 20 26 22 22 26 22
15 | 21 23 7 10 17 5 21 12 13 23 5 | 18 32 24 24 34 22 29 22 34 27 22
16 | 7 24 5 12 15 2 20 9 14 27 4 | 20 29 24 24 30 21 30 22 22 23 22
17 | 14 19 6 11 18 3 20 11 11 31 4 | 25 31 22 20 33 20 32 17 27 28 21
18 | 12 22 6 15 16 5 21 13 9 19 5 | 20 23 18 21 19 17 22 20 15 17 16
19 | 9 20 6 11 15 5 18 8 11 18 4 | 16 26 16 14 25 13 25 11 20 14 15
20 | 14 21 6 11 14 3 18 10 12 30 4 | 26 25 17 23 17 17 23 19 15 24 17
21E | 8 16 4 8 15 4 16 8 11 14 3 | 40 42 42 40 47 40 45 41 44 43 41
22 | 6 20 6 11 17 3 17 15 9 21 4 | 22 23 22 27 30 22 25 26 23 22 21
23 | 7 20 5 12 17 4 19 10 9 26 4 | 25 31 24 28 27 22 30 24 24 21 24
24E | 11 20 10 9 19 3 14 24 11 20 5 | 28 35 27 30 37 26 32 30 30 33 28
25 | 7 19 4 10 17 6 16 17 9 15 4 | 22 25 20 19 29 18 28 28 22 18 20
26 | 11 15 5 8 13 3 12 11 8 14 3 | 21 26 24 22 28 20 26 21 28 24 22
X27 | 7 --- --- --- --- 37 --- --- --- --- 0 | 64 --- --- --- --- 38 --- --- --- --- 64
28 | 15 23 7 9 18 4 21 11 13 18 5 | 21 29 24 24 34 20 29 23 31 22 23
29 | 13 18 4 8 16 3 24 10 12 18 4 | 20 24 15 17 20 15 28 19 23 19 16
30 | 6 15 5 7 15 4 13 9 13 13 3 | 16 22 19 21 22 16 24 17 22 14 17
31E | 9 20 6 7 15 4 18 20 18 13 5 | 28 29 27 28 33 25 29 28 37 30 26
32 | 7 13 4 13 14 3 11 8 14 20 4 | 22 28 23 25 27 21 28 22 23 24 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 20 6 10 17 4 18 15 12 19 |T 26 30 25 25 31 24 30 26 28 25 25
WRMS | 11 20 6 9 16 4 17 12 9 18 |NE 23 26 21 22 28 20 27 21 24 21 22
MEDI | 10 20 6 10 16 4 18 11 12 18 |MD 22 28 23 23 30 20 29 22 26 23 22
Table 3.1729.6 GPS week: 1729 Day: 6 MJD: 56353.000
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 | 12 23 6 7 15 4 16 17 13 16 4 | 18 17 25 19 28 21 32 21 29 27 21
2E | 7 15 5 8 16 3 19 14 10 12 4 | 34 40 38 35 39 35 40 32 42 39 37
3 | 8 13 4 8 18 3 12 8 9 13 3 | 27 33 29 24 37 24 34 27 25 24 28
4E | 20 22 16 16 22 7 21 37 24 18 8 | 104 91 97 101 93 101 92 120 101 93 99
5 | 14 18 7 13 15 3 22 12 10 25 5 | 34 32 29 36 41 27 31 30 28 32 30
6 | 9 13 4 9 15 4 11 12 7 12 3 | 23 32 28 24 36 22 34 30 27 23 28
7E | 9 15 5 7 14 2 17 8 11 10 3 | 18 24 20 16 28 18 24 18 25 14 19
8E | 16 27 5 11 19 5 24 15 21 19 6 | 24 36 21 19 23 19 33 24 27 26 20
9E | 11 21 7 8 13 4 21 18 10 11 4 | 24 37 23 22 27 21 37 26 27 28 23
10 | 11 14 5 9 16 4 17 19 10 16 4 | 43 41 43 48 47 43 42 41 42 40 43
11E | 7 18 4 7 23 5 13 12 11 15 4 | 16 29 17 16 29 17 29 21 22 20 19
12 | 13 18 6 9 19 4 20 17 13 21 5 | 29 28 24 26 38 23 27 34 30 26 26
13 | 8 20 5 8 19 3 16 13 11 24 4 | 24 35 25 28 40 25 35 30 28 23 27
14 | 5 19 6 13 14 5 19 10 8 25 4 | 29 33 31 38 40 30 34 32 31 35 32
15 | 20 19 7 11 15 4 21 11 13 22 5 | 26 34 31 34 41 29 34 28 35 35 30
16 | 9 21 6 15 18 3 20 9 13 28 4 | 19 30 25 25 35 19 29 25 21 26 23
17 | 13 19 6 13 19 3 19 11 10 34 4 | 20 31 18 19 31 18 32 16 22 34 19
18 | 10 19 5 15 14 4 18 11 11 18 4 | 21 26 22 28 26 20 25 25 18 23 22
19 | 8 19 6 8 18 4 19 11 10 17 4 | 16 34 21 17 30 18 35 23 24 23 21
20 | 9 19 8 9 12 4 20 12 12 32 4 | 23 26 23 29 25 20 26 25 20 37 22
21E | 7 15 5 8 11 4 14 11 10 14 3 | 24 30 29 26 31 24 31 22 30 29 27
22 | 6 22 6 12 15 5 19 19 12 21 5 | 26 27 29 34 37 27 27 33 26 26 28
23 | 8 19 5 9 16 4 15 13 10 29 4 | 27 32 27 30 38 27 33 29 30 23 28
24E | 8 20 5 9 13 5 11 18 17 13 4 | 32 32 30 29 35 29 33 30 40 23 30
25 | 9 15 5 9 18 4 15 14 9 12 4 | 22 25 22 18 36 20 32 31 23 25 23
26 | 10 13 4 10 14 4 15 6 9 16 3 | 23 28 28 29 35 25 26 26 26 29 26
X27 | 6 --- --- --- --- 60 --- --- --- --- 0 | 41 --- --- --- --- 37 --- --- --- --- 42
28 | 14 19 6 11 18 4 18 11 12 19 4 | 23 29 27 32 38 23 28 29 26 26 26
29 | 8 19 5 8 19 3 18 10 11 19 4 | 18 32 21 23 28 21 32 23 29 29 23
30 | 7 13 4 17 18 5 13 10 8 10 4 | 22 34 28 22 36 23 33 31 25 29 27
31E | 12 18 7 9 17 5 14 19 12 11 4 | 27 30 27 26 37 24 31 31 32 29 27
32 | 11 10 4 7 18 4 11 8 8 19 3 | 19 28 24 26 34 22 29 23 22 28 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 6 10 17 4 17 15 12 19 |T 27 32 28 29 36 26 33 30 30 29 28
WRMS | 10 18 5 9 16 4 17 11 10 16 |NE 25 30 26 28 35 24 31 28 26 28 27
MEDI | 9 19 5 9 16 4 18 12 11 18 |MD 24 32 27 26 36 23 32 28 27 27 26
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1729 GPS week: 1729 MJD: 56347.0-56353.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 |U 6 5 13 |U 12 16 33 |U 6 5 18 |
emr | emr 2964 | 8 7 15 |U 12 17 39 | 10 10 21 |
esa | esa 2976 | 6 6 12 |U 11 15 35 | 7 6 18 |
gfz | gfz 2964 |U 7 6 12 |U 11 16 36 |U 9 6 20 |
grg | grg 2976 |U 9 8 20 |U 12 17 38 | 11 10 24 |
igr | igr 2974 | 6 6 12 | 11 15 34 | 6 6 18 |
igs | igs 2958 | 7 6 12 | 11 16 34 | 8 7 19 |
jpl | jpl 2963 | 8 7 14 |U 12 15 37 | 10 10 21 |
mit | mit 2976 | 7 6 14 |U 12 16 38 |U 11 12 26 |
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 5.1729.0 GPS week: 1729 Day: 0 MJD: 56347.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 4 5 13 | 6 6 19 | 5 4 20 |
emr | emr 2964 | 8 7 15 | 7 9 26 | 10 6 22 |
esa | esa 2976 | 5 5 10 | 6 7 19 | 5 5 17 |
gfz | gfz 2965 | 5 5 9 | 6 8 21 | 7 5 21 |
grg | grg 2976 | 6 6 17 | 10 10 22 | 9 8 20 |
igr | igr 2975 | 4 4 9 | 7 7 20 | 5 5 18 |
igs | igs 2968 | 4 5 10 | 6 7 21 | 8 6 18 |
jpl | jpl 2964 | 7 7 12 | 6 8 27 | 10 7 16 |
mit | mit 2976 | 4 3 9 | 7 9 28 | 9 7 21 |
Table 5.1729.1 GPS week: 1729 Day: 1 MJD: 56348.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 4 4 8 | 12 18 45 | 6 4 19 |
emr | emr 2964 | 6 6 14 | 11 17 40 | 10 10 22 |
esa | esa 2976 | 4 5 9 | 9 16 38 | 6 5 18 |
gfz | gfz 2966 | 6 6 11 | 9 15 36 | 7 4 19 |
grg | grg 2976 | 7 5 15 | 12 15 42 | 9 7 23 |
igr | igr 2975 | 5 5 9 | 10 15 37 | 6 5 19 |
igs | igs 2967 | 5 5 10 | 10 15 38 | 9 8 20 |
jpl | jpl 2964 | 6 6 13 | 9 14 39 | 11 10 27 |
mit | mit 2976 | 6 5 11 | 10 14 44 | 10 9 24 |
Table 5.1729.2 GPS week: 1729 Day: 2 MJD: 56349.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3021 | 4 3 11 | 9 20 26 | 6 7 18 |
emr | emr 2964 | 5 4 14 | 10 17 33 | 8 8 19 |
esa | esa 2976 | 5 5 10 | 8 17 28 | 6 8 19 |
gfz | gfz 2964 | 5 4 10 | 9 16 32 | 7 6 19 |
grg | grg 2976 | 7 7 17 | 9 16 32 | 9 8 22 |
igr | igr 2975 | 5 4 10 | 9 17 27 | 6 6 17 |
igs | igs 2961 | 5 4 11 | 9 17 28 | 8 7 17 |
jpl | jpl 2963 | 6 5 11 | 9 16 31 | 9 9 19 |
mit | mit 2976 | 5 5 10 | 9 15 29 | 10 8 19 |
Table 5.1729.3 GPS week: 1729 Day: 3 MJD: 56350.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 9 6 15 | 12 17 42 | 6 4 15 |
emr | emr 2964 | 11 10 15 | 12 18 44 | 12 8 19 |
esa | esa 2976 | 10 9 17 | 12 16 42 | 6 5 14 |
gfz | gfz 2964 | 11 9 18 | 12 17 44 | 12 5 17 |
grg | grg 2976 | 11 9 24 | 12 17 46 | 10 6 25 |
igr | igr 2970 | 10 8 17 | 11 16 41 | 6 5 16 |
igs | igs 2933 | 10 8 15 | 12 16 43 | 7 6 15 |
jpl | jpl 2964 | 11 9 16 | 11 15 43 | 10 10 19 |
mit | mit 2976 | 12 9 19 | 13 19 47 | 13 21 39 |
Table 5.1729.4 GPS week: 1729 Day: 4 MJD: 56351.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 9 5 18 | 11 12 28 | 5 5 19 |
emr | emr 2964 | 11 7 17 | 11 19 39 | 10 9 26 |
esa | esa 2976 | 10 7 18 | 11 15 34 | 6 7 23 |
gfz | gfz 2963 | 9 6 16 | 11 15 39 | 13 7 28 |
grg | grg 2976 | 13 10 28 | 11 19 40 | 11 13 26 |
igr | igr 2976 | 10 6 17 | 12 13 31 | 6 7 23 |
igs | igs 2944 | 10 8 18 | 10 17 35 | 8 6 26 |
jpl | jpl 2963 | 11 8 18 | 11 17 34 | 9 10 25 |
mit | mit 2976 | 11 8 20 | 12 14 31 | 10 10 27 |
Table 5.1729.5 GPS week: 1729 Day: 5 MJD: 56352.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 7 9 13 | 10 13 24 | 7 6 14 |
emr | emr 2964 | 9 10 17 | 10 13 27 | 10 12 22 |
esa | esa 2976 | 7 9 11 | 10 13 29 | 8 6 19 |
gfz | gfz 2963 | 7 9 11 | 9 15 31 | 10 6 21 |
grg | grg 2976 | 12 8 20 | 10 12 30 | 12 11 26 |
igr | igr 2974 | 7 10 11 | 10 15 28 | 8 8 16 |
igs | igs 2964 | 7 9 11 | 10 13 27 | 8 7 23 |
jpl | jpl 2964 | 8 10 16 | 9 11 30 | 10 10 22 |
mit | mit 2976 | 7 9 13 | 10 14 29 | 12 13 26 |
Table 5.1729.6 GPS week: 1729 Day: 6 MJD: 56353.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 4 3 11 | 23 24 48 | 8 7 18 |
emr | emr 2964 | 8 6 13 | 24 23 63 | 12 15 20 |
esa | esa 2976 | 5 4 12 | 23 25 54 | 9 9 17 |
gfz | gfz 2964 | 5 4 10 | 24 25 50 | 8 7 17 |
grg | grg 2976 | 8 8 22 | 23 28 57 | 14 15 27 |
igr | igr 2975 | 5 4 11 | 23 25 52 | 8 7 17 |
igs | igs 2970 | 4 4 10 | 23 24 51 | 10 10 18 |
jpl | jpl 2964 | 6 5 12 | 26 22 53 | 13 14 22 |
mit | mit 2976 | 4 4 13 | 24 25 59 | 15 15 25 |
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 6.1729 GPS week: 1729 MJD: 56347.500-56353.500
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 1 9 -148 -2 | 4 13
| 15 20 88 48 5 | 1
emr uuuuu | 52 12 -114 64 20 | 12 22
| 25 25 95 51 5 | 8
esa uuuuu | -26 -3 -30 -69 -1 | 11 17
| 37 24 86 35 5 | 1
gfz uuuuu | 39 -7 5 -74 -8 | 12 17
| 14 20 40 80 3 | 1
grg uuuux | 7 -15 -38 28 -35 | 14 39
| 17 25 49 71 24 | 5
igr xxxxx | -42 14 -28 -4 -12 | 5 13
| 23 13 69 54 3 | 3
irf xxxxx | 15 -14 -8 47 -2 | 6 14
| 15 15 26 20 5 | 1
jpl uuuux | 7 1 74 50 -15 | 53 55
| 29 18 50 66 19 | 7
mit uuuuu | 48 -19 -25 248 0 | 11 18
| 23 30 79 75 9 | 1
ngs uuuuu | -30 33 108 85 -2 | 6 13
| 83 78 112 109 7 | 2
sio xxxxx | 96 -25 -369 -137 -2 | 65 67
| 54 36 62 58 7 | 2
Table 7.1729.0 GPS week: 1729 Day: 0 MJD: 56347.500
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 | -40 -22 86 -74 -6 | 5 11
emr uuuuu | 13 -34 -236 131 24 | 1 13
esa uuuuu | -60 -15 99 -101 -7 | 10 14
gfz uuuuu | 29 -44 20 -38 -12 | 12 16
grg uuuux | 24 -9 -35 134 -2 | 4 46
igr xxxxx | -75 19 -73 -105 -11 | 7 12
irf xxxxx | -5 -37 -28 47 -8 | 7 12
jpl uuuux | -24 -2 -5 16 -45 | 63 65
mit uuuuu | 17 -48 -130 190 -7 | 12 16
ngs uuuuu | 124 182 -60 3 1 | 5 10
sio xxxxx | 55 -45 -410 -159 0 | 62 63
Table 7.1729.1 GPS week: 1729 Day: 1 MJD: 56348.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 1 -10 -97 -7 | 4 11
emr uuuuu | 49 1 -66 83 24 | 3 14
esa uuuuu | -25 -40 15 -2 -6 | 9 13
gfz uuuuu | 52 -17 -4 -187 -13 | 11 16
grg uuuux | -3 30 -75 48 -30 | 12 40
igr xxxxx | -38 28 12 -29 -12 | 6 12
irf xxxxx | 15 -2 23 79 -9 | 5 11
jpl uuuux | 6 22 48 33 -35 | 58 61
mit uuuuu | 45 5 22 306 -11 | 11 16
ngs uuuuu | -68 61 18 -29 4 | 3 8
sio xxxxx | 32 -91 -269 -133 -10 | 63 65
Table 7.1729.2 GPS week: 1729 Day: 2 MJD: 56349.500
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 6 -30 -146 -7 | 4 12
emr uuuuu | 88 26 -135 45 15 | 8 22
esa uuuuu | -56 -24 53 -95 -3 | 11 16
gfz uuuuu | 41 1 -17 -73 -4 | 13 18
grg uuuux | -11 1 -11 -85 -14 | 17 37
igr xxxxx | -9 -4 20 64 -9 | 7 13
irf xxxxx | 33 1 -11 33 -3 | 6 13
jpl uuuux | 58 -10 65 -17 -6 | 55 58
mit uuuuu | 85 20 -84 251 0 | 12 17
ngs uuuuu | -64 22 52 249 7 | 6 13
sio xxxxx | 181 16 -451 -174 -4 | 66 68
Table 7.1729.3 GPS week: 1729 Day: 3 MJD: 56350.500
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 18 96 -194 -5 | 3 14
emr uuuuu | 76 40 -186 111 12 | 10 21
esa uuuuu | 48 21 -123 -87 6 | 9 16
gfz uuuuu | 18 15 -44 -117 -7 | 12 18
grg uuuux | -15 -34 34 3 -53 | 18 37
igr xxxxx | -69 30 -22 -11 -19 | 5 14
irf xxxxx | 10 -7 -43 51 3 | 4 13
jpl uuuux | 6 30 136 181 -18 | 51 54
mit uuuuu | 47 -20 -87 291 4 | 10 16
ngs uuuuu | -127 -72 223 66 -3 | 6 13
sio xxxxx | 132 -35 -405 -101 -2 | 66 68
Table 7.1729.4 GPS week: 1729 Day: 4 MJD: 56351.500
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 | -20 20 37 -204 2 | 4 15
emr uuuuu | 45 9 -117 68 21 | 17 26
esa uuuuu | -36 0 -106 -87 6 | 12 20
gfz uuuuu | 37 9 38 -141 -8 | 13 20
grg uuuux | 5 -39 -114 63 -34 | 17 37
igr xxxxx | -34 7 50 37 -13 | 4 14
irf xxxxx | -2 -15 -21 40 -3 | 6 17
jpl uuuux | -27 -7 135 1 -12 | 50 53
mit uuuuu | 31 -39 -18 285 -4 | 12 20
ngs uuuuu | 33 22 222 216 -6 | 8 16
sio xxxxx | 98 5 -384 -162 -9 | 68 70
Table 7.1729.5 GPS week: 1729 Day: 5 MJD: 56352.500
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 | -36 -30 46 -171 1 | 4 15
emr uuuuu | 62 35 -120 -15 22 | 19 28
esa uuuuu | -46 25 -93 -58 0 | 12 20
gfz uuuuu | 60 -7 -28 20 -9 | 12 18
grg uuuux | 23 -16 -59 -30 -43 | 16 37
igr xxxxx | -33 10 -156 20 -10 | 2 13
irf xxxxx | 32 -33 -5 62 2 | 5 16
jpl uuuux | 23 -4 83 64 4 | 46 48
mit uuuuu | 70 -57 32 305 8 | 10 18
ngs uuuuu | -47 30 207 0 -7 | 8 16
sio xxxxx | 46 -23 -322 -28 4 | 66 67
Table 7.1729.6 GPS week: 1729 Day: 6 MJD: 56353.500
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 | -31 12 -163 -150 5 | 4 15
emr uuuuu | 32 4 61 22 26 | 23 33
esa uuuuu | -6 11 -56 -56 -1 | 12 20
gfz uuuuu | 34 -3 70 20 -8 | 10 16
grg uuuux | 22 -40 -9 60 -73 | 15 37
igr xxxxx | -38 5 -29 -2 -9 | 1 12
irf xxxxx | 22 -7 26 19 2 | 6 16
jpl uuuux | 6 -19 52 73 7 | 45 47
mit uuuuu | 40 3 91 105 13 | 12 20
ngs uuuuu | -61 -12 92 93 -12 | 9 16
sio xxxxx | 124 -3 -344 -202 9 | 66 68
More information about the IGSREPORT
mailing list