[IGSREPORT-17398] Wk 1529 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu May 14 05:35:42 PDT 2009
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IGS Electronic Report 14 May 05:36:04 PDT 2009 Message Number 17398
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1529 (Apr 26, 2009 - May 02, 2009)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths 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. 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, no satellite L1/L2 delay calibration should be
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. 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 (weights are those from the orbit combination).
Pole rate combination uses only centres providing estimated pole rates.
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 3 weeks (21 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:
igs1529[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1529[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1529[0-6].cls IGS GPS clock combination summary report.
igs15297.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15297.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because they either provide broadcast
clocks (NGS) or clock corrections are not provided (SIO). The clock
information not used is still compared to combination for completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1478, a new solution from CNES/GRGS (GRG) is included for
evaluation and statistics 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 | ALL | 1 1
0 | COD | 4
0 | EMR | BREW BRUS GRAZ HARB IENG KOKB KOUR MAS1 MATE ONSA
0 | EMR | PRDS PTBB SPT0 STJO SYOG TSKB TWTF USN3 WSRT WTZR
0 | EMR | YELL ALGO AREQ BREW BRUS CRO1 DAEJ GODE GRAZ HARB
0 | EMR | IENG IRKT KERG KIRU KOKB KOUR LPGS MAR6 MAS1 MATE
0 | EMR | MCM4 MIZU NISU NLIB NNOR NRC1 NYAL ONSA PERT PIE1
0 | EMR | PRDS PTBB QAQ1 SCH2 SPT0 STJO SUTM SUWN SYOG THTI
0 | EMR | TIDB TLSE TSKB TWTF USN3 VILL WES2 WILL WSRT WTZR
0 | EMR | WUHN YAR2 YELL
0 | ESA | 4 5 24
0 | GFZ | 7 24 29
0 | GRG | NLIB YELL
0 | JPL | 2 9 15 20 23 24
0 | MIT | 5 9 27
1 | ALL | 1 1
1 | COD | 4 4 MDVJ
1 | EMR | WTZR
1 | ESA | 4 AREQ
1 | GFZ | 7 29 FAA1
1 | GRG | NLIB
1 | JPL | 24 AREQ
1 | MIT | 5 22 5 22 24
2 | ALL | 1
2 | COD | 1 4 4 9 27 WTZR
2 | EMR | MIZU
2 | ESA | 4 27
2 | GFZ | 7 29
2 | GRG | NLIB NOVM ZECK
2 | MIT | 5 24 5 24 BAKO WTZR
3 | ALL | 1
3 | COD | 4 4 9 27 RCMN
3 | EMR | SUTM
3 | ESA | 1 4 9 27 LPGS SCH2
3 | GFZ | 2 4 7 9 29 MIZU ULAB
3 | GRG | 4 9 27 CHAT DGAR HOFN HYDE KERG KHAJ LHAZ LPGS MANA
3 | GRG | MBAR MONP NLIB NOVM OUS2 POTS RABT SYOG ULAB
3 | JPL | 24
3 | MIT | 5 24 5 24 WTZR
4 | ALL | 1 1
4 | COD | 4 27 4 RCMN
4 | ESA | 4 5 9 27 LPGS OUS2 RAMO
4 | GFZ | 7 29 ALIC LPGS SUTM
4 | GRG | NLIB
4 | JPL | 24
4 | MIT | 5 5
5 | ALL | 1 1
5 | COD | 4 4 9 27
5 | EMR | SUTM
5 | ESA | 5 9 27 SYDN URUM
5 | GFZ | 7 29 FAIR SUTM
5 | GRG | NLIB
5 | JPL | 24
5 | MIT | 5 5 24 NNOR OUS2
6 | COD | 4 9 27 4 27
6 | EMR | MIZU NISU SUTM
6 | ESA | 5 27 KERG RAMO SCH2
6 | GFZ | 7 29 SUTM ULAB
6 | GRG | NLIB
6 | JPL | 4 24 FAIR NISU PIMO
6 | MIT | 5 7 19 24 5 7 19 24 SANT
5. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G16 | 2009_04_29 | 2009030
G16 | 2009_04_30 | 2009030
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
----+--------+---------------
4 | EMR | 5
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 | | | | |
PRN G05 | | | | | 4 | | |
PRN G24 | | | 2 | | | | |
8. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) 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.
9. Small rotations were applied to the all AC orbit and ERP values in order
to align them to the IGS05. These rotations were estimated in the process
of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based
on the common stations between the individual AC SINEX solutions and the
IGS05.snx SINEX. 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 | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .3 .4 .4 -22 -6 -21 .01
EMR | 13.5 -13.2 -13.0 110 37 66 .25
ESA | 5.4 .4 -6.1 -7 -110 29 .28
GFZ | .7 .6 .9 28 -30 13 -.21
GRG | 5.0 -1.9 -2.7 4 -27 25 .0
JPL | 2.7 -3.9 -7.1 7 -17 -2 .53
MIT | 7.5 -11.6 -4.9 -15 24 -15 -.07
NGS | 9.5 -11.3 -1.1 -154 -151 26 .14
SIO | 5.3 -1.0 -9.7 -2 -115 8 .27
10. 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 navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
11. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by NRCan. For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
12. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna
model is introduced (IGSMAIL #5272). The antenna phase center offsets and
phase center variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five 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 1.1529.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1529.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 2.1529.[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 3.1529.[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 and final
part, Table 5, is similar to Table 4 and contains daily precise navigation
statistics (tables 5.1529.0-6).
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 1529 summary. (Apr 26, 2009 - May 02, 2009)
Table 1.1529.a GPS week: 1529 MJD: 54947.000-54953.000
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 229| 0 0 0 14 -53 -24 -.16 9 8 | -546 75 20 79
| 0 0 0 13 17 18 .03 | 654 1123
emr 93| 0 0 2 -221 -137 -33 .44 21 21 | 2356 -218 24 107
| 1 1 2 10 26 24 .04 | 1973 1830
esa 118| 0 0 0 -30 62 -10 .28 9 9 | -205 -587 20 124
| 0 0 1 20 29 14 .03 | 1113 1568
gfz 192| 1 0 1 -73 -7 138 -.08 11 11 | 151 -60 26 173
| 1 1 0 13 7 74 .04 | 377 317
grg 108| 0 0 -1 -68 20 -35 .97 37 34 | 5992 -22820 96 23826
| 2 0 1 23 27 43 .02 | 15972 60367
igr n/a| 0 1 0 -19 -57 -28 .04 6 6 | 10816 387 23 69
| 0 0 0 16 17 24 .02 | 1706 2007
jpl 122| -1 0 -2 -40 -19 -19 .50 20 19 | 579 -230 22 98
| 1 1 1 15 11 15 .03 | 2138 1859
mit 285| 0 0 -2 0 -115 -49 -.26 11 10 | -539 -2288 24 147
| 0 1 1 22 19 18 .02 | 1352 5789
ngs 222| 0 0 0 306 180 -14 -.38 17 10 | -8069 60738 2377 4136
| 0 0 1 16 28 22 .07 | 20260 152579
sio 251| -2 1 3 -15 175 -13 -.04 21 20 | --- --- --- ---
| 0 1 1 22 20 29 .01 | --- ---
Table 1.1529.b GPS week : 1529 MJD: 54947.000-54953.000
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 | 13 12 13 18 11 12 0 |
2 | 5 5 5 5 5 5 5 |
3 | 4 4 4 4 4 4 5 |
4 | 6 6 5 6 5 6 6 |
5 | 7 8 7 9 23 20 8 |
6 | 4 4 4 4 4 4 5 |
7 | 6 5 5 5 4 5 4 |
8 | 5 6 5 5 5 6 7 |
9 | 5 5 5 6 5 5 5 |
10 | 4 4 4 4 4 4 4 |
11 | 5 4 4 4 4 5 5 |
12 | 5 6 5 5 5 5 5 |
13 | 6 5 5 5 5 6 5 |
14 | 5 5 5 5 5 5 5 |
15 | 6 6 6 6 5 6 5 |
16 | 5 5 5 5 --- 5 5 |
17 | 6 5 5 6 5 6 6 |
18 | 6 5 5 5 5 5 5 |
19 | 6 6 6 6 5 5 6 |
20 | 6 5 5 5 5 6 5 |
21 | 5 4 4 4 4 4 4 |
22 | 5 5 5 5 5 5 5 |
23 | 6 5 5 6 6 5 5 |
24 | 11 10 12 8 7 8 8 |
25 | 6 6 6 7 6 7 7 |
26 | 4 4 4 4 4 4 4 |
27 | 6 5 5 5 5 5 6 |
28 | 6 6 5 6 5 6 6 |
29 | 6 5 6 5 6 6 5 |
30 | 4 3 3 4 4 4 4 |
31 | 5 4 5 5 4 5 4 |
32 | 6 5 6 5 5 5 5 |
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 2.1529.0 GPS week: 1529 Day: 0 MJD: 54947.000
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 229| 1 0 -1 37 -49 5 -.18 9 8 | -394 -7 27 88
| 28 27 |
emr 93| -2 -1 0 -236 -166 -29 .43 21 21 | 4148 247 41 170
| 50 -2 |
esa 118| 0 0 2 -47 66 -4 .25 10 9 | -1729 1815 26 135
| 49 -15 |
gfz 192| 0 0 0 -71 -1 131 -.14 12 12 | 224 -80 29 176
| 12 -4 |
grg 108| -2 0 0 -38 6 -115 .95 36 33 | -31 70 91 197
| 70 25 |
igr n/a| 0 0 0 -33 -60 7 .05 6 6 | 11611 404 27 78
| 68 -39 |
jpl 122| 0 0 -1 -36 -20 -31 .47 20 19 | 2852 177 44 145
| 2 -41 |
mit 285| 0 0 -3 1 -99 -74 -.22 13 12 | -133 23 35 127
| 1 32 |
ngs 222| 0 0 0 288 147 -18 -.34 18 10 | -624 656 1862 3677
| -35 81 |
sio 251| -4 1 2 -2 214 -43 -.03 22 21 | --- --- --- ---
| 8 -161 |
Table 2.1529.1 GPS week: 1529 Day: 1 MJD: 54948.000
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 229| 1 0 0 24 -25 -27 -.17 9 8 | -1842 2154 18 68
| 33 -3 |
emr 93| 1 -1 3 -218 -167 -49 .38 19 19 | 3550 264 25 85
| 11 30 |
esa 118| 0 1 0 -19 82 -22 .27 9 9 | 742 -778 19 111
| 66 6 |
gfz 192| 1 0 2 -50 -15 210 -.09 12 12 | -279 323 30 181
| -1 -12 |
grg 108| 0 0 0 -32 64 24 .94 35 34 | -700 1050 87 222
| 96 -16 |
igr n/a| -2 1 0 -7 -30 -40 .04 6 6 | 11191 308 22 63
| -6 -26 |
jpl 122| 0 0 -1 -45 -22 -7 .52 20 19 | 2176 -103 21 91
| 19 5 |
mit 285| -1 -1 -4 25 -102 -64 -.24 11 10 | -523 637 29 162
| 1 14 |
ngs 222| 0 0 0 279 175 -40 -.47 20 13 | -1909 2143 2352 3866
| -43 42 |
sio 251| -3 2 5 13 180 -40 -.03 21 20 | --- --- --- ---
| -3 -142 |
Table 2.1529.2 GPS week: 1529 Day: 2 MJD: 54949.000
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 229| 0 0 0 19 -35 -33 -.19 8 7 | -28 -667 14 62
| 55 2 |
emr 93| 2 0 4 -230 -152 -59 .40 20 20 | 4341 -2535 20 106
| 11 -6 |
esa 118| 0 0 -1 -51 93 -14 .24 8 8 | -136 -336 17 108
| 76 -1 |
gfz 192| 3 0 2 -64 -17 215 -.10 12 12 | 709 -440 27 172
| 5 -41 |
grg 108| 2 -1 0 -92 26 -54 .98 36 32 | 698 -720 90 206
| 38 6 |
igr n/a| 0 1 0 5 -47 -13 .03 7 6 | 12041 -2304 22 60
| -21 -3 |
jpl 122| 0 0 0 -15 -13 -33 .53 20 20 | 2450 -2728 18 86
| -15 19 |
mit 285| 0 -1 -2 29 -128 -59 -.28 13 11 | 234 -226 22 129
| 2 37 |
ngs 222| 0 0 0 323 175 7 -.38 20 12 | -23 -737 2701 4873
| -68 3 |
sio 251| -2 1 5 -6 151 -44 -.05 21 21 | --- --- --- ---
| -13 -132 |
Table 2.1529.3 GPS week: 1529 Day: 3 MJD: 54950.000
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 229| 0 0 0 9 -61 -48 -.17 8 8 | -608 348 16 73
| 61 16 |
emr 93| 0 1 3 -214 -141 -45 .45 22 22 | 2338 -2751 19 110
| 10 -20 |
esa 118| 0 0 0 -23 83 -30 .32 9 9 | 589 -2333 21 132
| 7 3 |
gfz 192| 2 0 1 -76 -2 174 -.09 10 10 | 159 275 25 165
| 29 -27 |
grg 108| -1 0 -2 -75 9 -42 .96 38 35 | 42196 -159714 128 165497
| 23 27 |
igr n/a| 0 0 0 -4 -74 -41 .05 6 6 | 10246 -2082 21 61
| -17 5 |
jpl 122| -3 3 -3 -39 -30 -25 .55 20 19 | 375 -2697 19 98
| 30 -9 |
mit 285| 0 -1 -1 1 -101 -38 -.28 10 10 | -221 311 18 136
| 22 24 |
ngs 222| 0 0 0 322 145 -8 -.48 17 11 | -53977 406442 2130 4291
| -76 65 |
sio 251| -2 2 1 -8 185 9 -.02 20 20 | --- --- --- ---
| -20 -134 |
Table 2.1529.4 GPS week: 1529 Day: 4 MJD: 54951.000
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 229| 0 0 0 4 -67 -22 -.16 8 8 | -681 292 29 79
| 58 19 |
emr 93| 0 0 2 -219 -112 -49 .46 21 21 | -1208 2340 25 97
| 3 -58 |
esa 118| 0 0 1 7 63 -17 .28 9 9 | -1642 673 20 124
| -3 -2 |
gfz 192| 0 0 0 -76 -9 160 -.09 9 9 | -366 143 28 170
| 28 -16 |
grg 108| 1 0 0 -85 38 -37 .97 37 35 | -650 394 89 224
| 76 19 |
igr n/a| 0 0 0 -38 -45 -69 .04 6 5 | 7524 3120 25 72
| -13 -56 |
jpl 122| -1 0 -3 -67 -1 -35 .47 21 20 | -3067 2246 19 93
| 18 -41 |
mit 285| 0 0 -1 -4 -110 -53 -.27 10 9 | -325 -291 27 140
| 22 29 |
ngs 222| 0 0 0 305 193 -47 -.28 16 9 | -768 366 2492 3811
| -94 -3 |
sio 251| -2 2 3 -17 168 -6 -.03 20 21 | --- --- --- ---
| -8 -133 |
Table 2.1529.5 GPS week: 1529 Day: 5 MJD: 54952.000
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 229| 0 0 -1 1 -66 -39 -.15 9 8 | -483 -70 14 82
| 37 9 |
emr 93| 0 -1 2 -206 -117 0 .46 22 22 | 911 917 22 98
| -3 -44 |
esa 118| 1 0 2 -44 42 0 .28 10 10 | 1023 -2648 19 129
| 45 42 |
gfz 192| 0 -2 1 -95 -8 58 -.02 11 11 | 447 -422 22 165
| -1 -35 |
grg 108| 2 0 -3 -67 20 -16 .95 37 34 | 192 -535 90 213
| 38 -13 |
igr n/a| -1 1 1 -28 -63 -18 .06 6 5 | 10337 1997 22 77
| 21 16 |
jpl 122| -2 0 -2 -49 -13 0 .50 20 19 | -1106 1067 17 90
| 1 -42 |
mit 285| 1 0 -3 -27 -152 -24 -.24 11 10 | -3473 -15358 17 140
| 5 23 |
ngs 222| 0 0 0 314 222 3 -.37 13 7 | 726 17458 2353 4135
| -53 23 |
sio 251| -4 1 3 -28 158 23 -.04 20 18 | --- --- --- ---
| -20 -147 |
Table 2.1529.6 GPS week: 1529 Day: 6 MJD: 54953.000
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 229| 0 0 0 5 -70 -8 -.10 10 9 | 211 -1522 22 102
| 56 14 |
emr 93| -1 -1 0 -223 -102 -2 .47 20 20 | 2416 -11 18 84
| 20 -71 |
esa 118| 1 0 0 -38 8 12 .29 11 11 | -282 -505 21 131
| 53 47 |
gfz 192| 0 -1 1 -77 3 19 -.04 10 10 | 166 -225 26 186
| 3 -34 |
grg 108| 3 -1 -2 -87 -23 -8 1.01 38 34 | 241 -289 99 225
| 46 59 |
igr n/a| 0 0 0 -24 -79 -21 .01 6 6 | 12765 1272 22 72
| 31 2 |
jpl 122| 0 2 -2 -33 -34 -2 .49 18 18 | 374 423 17 87
| -11 -13 |
mit 285| 1 0 -3 -27 -114 -29 -.26 11 10 | 666 -1115 21 196
| 0 15 |
ngs 222| 0 0 3 310 206 4 -.35 13 7 | 90 -1157 2754 4301
| -51 15 |
sio 251| -2 0 3 -57 169 9 -.05 22 19 | --- --- --- ---
| -15 -116 |
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 3.1529.0 GPS week: 1529 Day: 0 MJD: 54947.000
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 | 23 40 30 --- --- 27 --- 12 21 --- 13 | 134 41 108 --- --- 140 --- 124 125 --- 139
2E | 7 19 9 12 21 6 22 13 14 17 5 | 20 34 27 23 41 25 33 22 18 26 22
3 | 6 15 6 13 29 6 12 11 10 13 4 | 33 45 42 40 49 40 40 35 36 41 37
4E | 12 20 10 12 45 7 15 13 26 19 5 | 27 32 25 30 31 26 27 23 35 29 24
X5 | 10 24 11 --- --- 23 --- 10 18 --- 7 | 11 26 21 --- --- 19 --- 9 20 --- 12
6 | 6 15 7 13 27 6 13 9 10 17 4 | 20 28 26 28 30 26 22 19 26 31 22
7E | 9 25 10 19 31 5 20 12 14 11 5 | 29 34 29 34 43 31 32 31 39 32 31
8 | 10 21 8 13 24 6 13 13 16 23 5 | 65 73 66 67 66 64 69 62 59 66 63
9E | 12 22 9 11 59 4 18 11 17 19 5 | 24 37 34 33 40 30 36 33 37 28 30
10 | 7 14 7 9 29 3 12 14 13 20 4 | 10 17 17 14 22 14 17 13 17 20 11
11E | 7 21 10 11 40 4 15 11 13 12 4 | 22 35 28 27 43 27 32 25 29 24 25
12 | 8 18 6 13 21 7 21 10 11 30 5 | 16 29 20 24 30 19 26 17 21 34 19
13 | 11 22 12 14 47 7 25 17 9 15 5 | 12 27 21 16 43 16 27 20 14 18 13
14 | 8 20 6 12 38 6 22 12 12 20 5 | 18 32 21 24 34 20 24 22 16 23 18
15 | 9 24 9 15 29 7 23 16 13 26 6 | 14 26 21 19 34 16 23 19 15 24 14
16 | 6 19 9 13 42 3 22 10 9 25 5 | 9 21 18 16 21 14 18 12 10 13 12
17 | 8 22 11 9 34 6 23 9 13 32 5 | 27 33 23 30 36 26 36 27 27 35 25
18 | 7 24 8 13 33 4 24 13 11 23 5 | 16 33 18 21 40 17 29 17 21 21 17
19 | 7 25 12 15 33 7 25 13 14 27 6 | 22 34 22 17 42 21 37 25 19 31 20
20 | 11 20 14 12 45 7 25 13 9 23 5 | 20 35 28 26 35 24 32 24 20 26 21
21E | 11 19 7 10 36 6 22 9 11 9 4 | 10 23 10 10 39 12 22 12 15 13 8
22 | 6 20 8 12 52 7 26 13 11 25 5 | 19 29 24 25 40 20 28 24 23 27 20
23 | 9 23 8 14 38 5 25 13 9 22 5 | 14 32 19 19 38 19 30 19 15 21 15
24E | 17 29 12 13 45 15 28 20 64 30 10 | 54 61 59 55 66 55 65 59 87 63 57
25E | 13 23 15 13 22 5 14 15 22 19 6 | 31 31 33 34 43 33 33 32 42 35 31
26 | 5 19 8 7 27 7 13 9 13 16 4 | 9 21 14 12 26 11 21 12 13 11 10
27E | 11 23 10 10 55 7 18 13 25 12 5 | 17 29 24 21 39 19 26 19 30 17 18
28 | 6 19 11 11 27 5 17 13 13 36 5 | 18 25 24 27 36 20 22 22 23 27 20
29 | 8 18 11 17 29 7 24 8 8 27 5 | 22 32 29 20 35 22 35 26 27 27 24
30 | 5 13 8 11 17 7 14 11 12 18 4 | 25 25 26 30 30 28 21 23 35 30 25
31E | 9 23 7 9 31 9 21 13 13 16 5 | 25 36 24 25 32 29 29 23 34 20 25
32 | 12 19 10 10 41 6 24 19 12 25 5 | 22 35 30 28 39 27 30 33 21 36 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 21 10 12 36 6 20 13 18 22 |T 25 32 29 26 38 28 30 27 30 28 26
WRMS | 8 21 9 12 33 6 19 12 10 21 |NE 23 29 27 22 34 26 27 25 25 26 24
MEDI | 8 20 9 12 33 6 21 13 13 20 |MD 20 32 24 25 38 22 29 23 23 27 21
Table 3.1529.1 GPS week: 1529 Day: 1 MJD: 54948.000
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 | 17 46 25 --- --- 15 --- 14 22 --- 12 | 124 43 104 --- --- 130 --- 116 118 --- 129
2E | 8 15 10 11 34 4 24 13 13 17 5 | 16 27 24 17 42 18 28 17 18 25 17
3 | 7 15 10 10 42 6 9 13 15 13 4 | 45 55 49 48 68 49 51 47 48 51 48
4E | 12 21 12 11 45 7 16 11 24 19 5 | 30 32 27 25 32 27 27 25 35 32 26
X5 | 13 25 14 20 --- 14 --- 13 30 --- 8 | 14 25 22 8 --- 18 --- 10 25 --- 14
6 | 7 15 8 9 33 5 10 9 15 12 4 | 14 27 22 22 25 19 22 16 16 23 17
7E | 6 20 7 16 31 4 21 9 18 10 4 | 20 28 21 23 34 20 27 21 26 24 20
8 | 11 21 11 10 25 6 15 12 16 25 5 | 61 68 62 66 67 65 66 71 70 59 64
9E | 12 24 10 11 58 4 17 9 20 17 5 | 27 43 33 34 46 32 37 33 38 34 32
10 | 7 13 5 7 16 3 13 8 18 14 3 | 11 18 18 13 23 15 20 16 22 20 14
11E | 9 15 8 10 36 8 10 10 11 17 4 | 19 33 27 23 45 25 30 24 22 29 23
12 | 7 17 9 12 30 5 24 7 14 32 5 | 19 27 24 21 35 20 27 21 22 31 21
13 | 8 20 8 11 49 7 23 10 12 12 4 | 12 28 17 17 42 16 28 17 16 19 14
14 | 7 16 9 15 32 5 20 8 13 18 4 | 11 26 18 20 31 16 24 14 14 18 14
15 | 9 21 12 15 29 3 25 13 18 26 6 | 10 25 21 17 37 15 25 17 19 25 13
16 | 8 20 7 12 52 5 22 11 15 26 5 | 15 23 16 15 26 16 20 13 17 13 15
17 | 6 19 9 11 30 5 21 8 14 30 5 | 22 28 18 26 25 22 28 24 22 30 21
18 | 8 22 6 16 29 4 26 10 14 18 5 | 16 33 20 20 31 19 30 16 20 21 18
19 | 10 24 12 16 32 9 24 10 14 23 5 | 16 29 15 15 34 15 29 19 20 18 15
20 | 8 20 9 13 40 9 23 10 15 21 5 | 16 31 19 20 40 20 30 19 22 20 17
21E | 7 15 7 11 22 4 22 9 13 8 4 | 12 24 15 12 24 13 20 13 20 12 13
22 | 7 19 8 11 51 6 24 8 14 21 4 | 16 29 20 21 35 19 27 19 21 25 19
23 | 6 22 6 12 32 6 25 11 9 19 5 | 16 31 19 19 36 20 33 22 19 23 18
24E | 13 27 10 13 36 7 26 24 65 18 9 | 55 62 61 57 76 57 68 64 81 62 59
25E | 14 22 12 16 25 7 16 12 26 18 6 | 28 38 33 33 39 30 36 30 39 35 30
26 | 5 13 5 10 23 5 14 6 14 14 3 | 10 20 17 14 32 12 23 13 17 14 13
27E | 9 21 7 10 44 5 17 10 27 13 5 | 11 27 17 15 44 14 23 14 25 14 13
28 | 9 17 12 14 24 7 18 13 14 37 6 | 16 25 17 27 29 21 26 19 26 25 17
29 | 9 18 8 11 28 8 22 6 16 27 5 | 18 28 22 15 31 19 31 18 21 19 19
30 | 5 12 6 6 19 4 15 5 11 15 3 | 19 22 22 19 21 20 20 20 22 24 20
31E | 8 17 7 8 26 6 22 6 16 14 4 | 22 33 24 25 29 26 29 25 25 25 24
32 | 9 19 7 11 45 4 17 14 14 29 5 | 23 30 25 24 38 25 29 30 25 30 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 9 12 35 6 20 11 20 21 |T 23 31 27 23 37 26 30 26 29 26 25
WRMS | 8 19 9 12 34 6 19 10 13 20 |NE 22 28 25 20 33 25 27 24 26 23 23
MEDI | 8 19 8 11 32 5 21 10 15 18 |MD 16 28 21 20 34 20 28 19 22 24 18
Table 3.1529.2 GPS week: 1529 Day: 2 MJD: 54949.000
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 | 22 31 28 --- --- 45 --- 19 25 --- 12 | 128 22 96 --- --- 135 --- 130 129 --- 131
2E | 7 20 9 10 36 6 23 14 15 19 5 | 24 35 30 24 40 25 31 26 27 39 26
3 | 7 14 6 13 27 6 10 12 14 13 4 | 21 27 28 25 37 26 27 28 24 27 25
4E | 10 21 6 10 55 6 16 13 22 22 5 | 27 28 23 23 22 22 20 20 30 27 21
X5 | 5 28 8 --- --- 15 --- 7 25 --- 7 | 13 27 12 --- --- 18 --- 11 22 --- 12
6 | 6 18 6 11 29 6 10 9 14 13 3 | 20 26 21 27 27 23 21 18 26 24 20
7E | 6 19 8 14 35 7 21 10 12 9 4 | 18 24 22 23 38 18 23 20 27 20 19
8E | 10 19 7 10 28 5 12 10 21 19 4 | 34 35 32 35 27 33 32 40 43 32 32
9E | 11 19 7 10 64 4 17 13 18 23 5 | 19 31 27 25 40 24 32 23 32 26 23
10 | 6 15 6 8 20 5 12 9 14 19 3 | 13 11 14 13 23 10 15 13 17 19 10
11 | 9 16 10 8 51 5 13 10 12 11 4 | 21 33 25 24 48 22 29 22 25 23 22
12 | 6 19 6 12 27 5 22 11 12 30 5 | 15 29 21 25 32 19 27 16 18 26 18
13 | 7 20 8 10 48 8 25 11 9 12 4 | 11 28 16 16 47 13 27 15 14 13 12
14 | 6 18 7 13 33 6 23 9 10 16 4 | 15 24 18 22 34 18 25 12 16 17 15
15 | 9 21 10 16 31 7 23 14 13 23 5 | 15 23 18 21 39 15 22 16 17 18 12
X16 | 8 21 9 9 37 6 --- 9 13 27 5 | 13 21 13 13 30 11 --- 10 11 11 11
17 | 6 20 8 12 36 7 23 12 9 31 5 | 24 26 19 26 31 18 26 23 24 28 20
18 | 5 22 7 11 31 5 24 7 12 19 4 | 16 28 19 18 36 16 30 15 23 20 18
19 | 7 25 9 11 31 8 23 12 15 24 5 | 20 30 20 19 31 18 33 17 22 21 18
20 | 8 21 10 12 34 6 27 11 12 15 5 | 17 30 25 23 47 17 29 17 16 16 18
21E | 6 17 7 11 30 7 19 8 9 10 4 | 15 19 16 12 34 10 22 15 21 15 13
22 | 6 18 8 10 51 5 22 8 13 19 4 | 18 25 19 20 39 18 26 20 22 23 19
23 | 8 22 6 9 34 8 25 14 10 20 5 | 14 28 14 16 42 13 29 14 12 12 11
24E | 14 28 13 19 33 13 28 33 74 37 11 | 100 98 103 97 114 107 98 102 132 121 101
25E | 13 26 12 15 26 8 19 14 25 15 6 | 19 32 23 27 35 22 29 22 35 26 21
26 | 5 14 7 11 21 4 12 10 14 16 3 | 11 17 14 15 29 11 18 12 16 11 11
27E | 8 19 8 9 49 7 16 13 24 13 5 | 13 22 20 17 43 17 23 16 30 13 15
28 | 6 15 7 12 21 8 19 13 11 35 5 | 17 26 15 24 32 17 24 20 17 26 16
29 | 9 19 8 15 31 8 22 10 15 28 5 | 20 28 23 23 37 20 32 26 24 26 20
30 | 4 13 5 8 21 5 14 5 9 18 3 | 18 23 20 22 23 21 19 18 24 26 19
31E | 7 17 6 13 30 5 22 10 14 16 4 | 17 29 23 23 32 23 30 19 22 24 20
32 | 11 20 7 11 40 5 19 17 14 25 5 | 15 23 24 20 40 17 24 18 21 18 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 8 12 36 7 20 13 20 21 |T 23 28 25 23 37 24 28 24 29 24 23
WRMS | 7 20 8 12 32 6 20 11 12 21 |NE 21 24 22 20 34 22 25 22 24 20 21
MEDI | 7 19 7 11 31 6 21 11 14 19 |MD 17 27 20 23 35 18 27 18 22 23 18
Table 3.1529.3 GPS week: 1529 Day: 3 MJD: 54950.000
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 | 38 --- 27 --- --- 26 --- 25 26 --- 17 | 147 --- 113 --- --- 148 --- 142 137 --- 145
2E | 6 19 10 10 33 5 21 10 14 13 4 | 16 31 25 18 39 19 27 22 18 26 19
3 | 6 17 5 10 35 4 13 9 13 14 3 | 46 51 47 51 52 48 48 47 54 49 48
4E | 10 20 12 11 61 9 16 14 23 26 5 | 28 33 30 26 31 27 28 28 37 33 26
X5 | 21 26 16 --- --- 12 --- 11 18 --- 9 | 21 26 23 --- --- 18 --- 17 28 --- 16
6 | 7 17 4 10 29 4 13 7 9 13 3 | 17 26 23 22 23 19 19 20 26 26 19
7E | 7 20 7 11 30 5 19 9 16 8 4 | 28 33 25 25 36 26 36 30 34 29 27
8E | 12 22 9 10 26 5 12 8 18 19 5 | 69 68 70 70 64 67 66 73 71 66 68
9E | 11 21 9 8 62 5 19 9 24 21 5 | 29 39 34 31 49 31 38 32 40 26 30
10 | 6 16 7 7 15 5 12 10 15 12 3 | 14 21 17 14 23 14 21 19 19 21 14
11 | 8 21 9 9 48 6 15 8 11 16 4 | 20 36 27 20 46 21 27 23 23 24 22
12 | 7 18 9 9 29 5 19 9 14 27 5 | 19 31 25 25 39 20 27 21 25 34 22
13 | 7 25 9 8 54 6 24 12 10 15 5 | 19 32 21 19 46 18 31 23 18 25 18
14 | 7 26 10 16 36 6 24 6 10 17 5 | 16 28 19 24 32 17 24 14 19 14 15
15 | 10 23 11 12 30 5 23 18 11 20 5 | 13 26 20 17 31 15 24 24 16 21 14
X16 | 7 --- 10 9 --- 7 --- 7 --- --- 5 | 11 --- 13 14 --- 12 --- 9 --- --- 10
17 | 7 19 11 11 39 7 21 12 12 29 5 | 23 24 19 25 38 21 28 24 24 29 20
18 | 6 26 9 11 35 3 25 7 12 19 5 | 16 32 19 21 37 17 31 16 23 19 17
19 | 8 27 10 10 33 6 26 11 10 25 5 | 22 32 20 19 37 19 38 23 27 20 21
20 | 8 23 8 8 42 9 26 10 12 16 5 | 18 32 22 22 46 21 31 21 23 22 19
21E | 7 22 7 8 34 4 19 8 13 16 4 | 12 26 15 15 32 11 22 16 18 18 13
22 | 8 20 7 9 53 3 23 8 14 20 4 | 19 29 20 24 40 18 28 22 29 23 20
23 | 8 27 8 9 44 6 24 15 14 20 5 | 21 35 21 21 45 22 32 27 20 23 20
24E | 14 27 9 14 48 10 21 15 44 21 7 | 78 89 81 80 87 80 89 87 95 86 82
25E | 15 27 15 13 28 7 18 13 31 13 6 | 31 36 33 33 46 30 38 35 48 36 31
26 | 8 16 7 6 23 5 12 7 12 17 3 | 10 21 15 15 28 13 21 18 20 15 13
27E | 7 22 9 7 42 6 16 10 29 15 5 | 17 28 24 20 38 17 25 19 32 17 17
28 | 7 24 14 8 22 5 20 9 11 36 5 | 21 30 24 24 35 21 27 24 28 30 21
29 | 9 21 8 10 29 8 20 6 12 25 5 | 22 33 25 24 26 22 34 25 27 26 23
30 | 6 15 7 8 20 5 14 5 13 17 3 | 23 28 28 29 31 24 25 23 30 27 25
31E | 8 21 7 8 33 5 21 11 13 16 4 | 23 35 28 25 40 26 33 30 28 27 26
32 | 11 22 8 10 37 9 22 13 12 21 5 | 26 33 28 26 38 28 29 34 31 33 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 22 9 10 38 6 20 10 17 20 |T 27 34 29 26 39 28 32 30 34 29 28
WRMS | 8 22 9 10 35 6 19 10 11 20 |NE 25 30 26 22 35 26 28 28 31 25 26
MEDI | 8 21 9 9 34 5 20 9 13 17 |MD 21 32 24 24 38 21 28 23 27 26 20
Table 3.1529.4 GPS week: 1529 Day: 4 MJD: 54951.000
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 | 17 --- 20 --- --- 34 --- 11 24 --- 10 | 126 --- 147 --- --- 139 --- 116 118 --- 127
2E | 7 23 10 9 29 5 22 13 9 14 4 | 23 34 29 24 41 26 32 23 25 32 24
3 | 6 17 8 7 23 4 13 8 11 20 4 | 30 37 36 33 38 33 33 28 37 32 30
4E | 9 20 6 9 50 6 14 12 23 24 5 | 24 28 22 23 27 24 25 22 34 27 22
X5 | 54 87 29 --- --- 24 --- 37 23 --- 23 | 50 19 30 --- --- 29 --- 39 34 --- 31
6 | 7 19 5 6 26 5 16 9 10 15 3 | 18 30 24 24 32 23 23 22 26 27 21
7E | 6 18 8 10 37 5 23 7 7 8 4 | 18 25 19 18 33 19 27 23 26 21 20
8E | 14 22 12 10 19 7 15 8 13 19 5 | 33 41 36 36 38 38 36 38 39 36 35
9E | 10 22 7 8 50 4 20 8 18 22 5 | 18 29 26 23 41 24 31 24 32 27 23
10 | 7 14 10 7 19 4 14 9 7 10 3 | 12 21 19 15 20 19 21 17 16 25 14
11 | 8 21 6 11 36 6 16 7 12 15 4 | 19 35 26 21 44 24 29 22 29 25 22
12 | 8 22 6 9 24 6 20 7 12 27 4 | 15 28 22 20 33 19 26 18 19 25 19
13 | 8 21 7 8 55 4 24 15 13 14 4 | 14 29 19 15 46 18 28 20 19 22 14
14 | 6 22 7 9 37 5 23 7 14 16 4 | 16 28 21 21 41 20 27 16 24 16 18
15 | 10 22 11 12 47 7 28 11 7 19 5 | 11 27 20 19 45 17 25 20 17 21 15
17 | 8 19 9 6 36 6 23 7 12 31 5 | 21 26 17 22 37 21 29 22 28 32 20
18 | 6 27 9 9 39 6 26 6 10 21 5 | 14 32 16 17 35 16 28 13 20 19 15
19 | 8 22 11 8 33 8 26 10 11 25 5 | 20 31 20 20 43 21 36 20 23 26 20
20 | 8 24 6 11 46 7 29 11 15 15 5 | 17 31 20 18 47 21 31 16 24 19 16
21E | 7 22 7 8 26 3 19 8 12 12 4 | 10 26 13 7 28 10 21 12 18 12 10
22 | 5 22 9 8 54 4 25 8 9 20 4 | 17 29 20 19 41 18 27 20 21 22 17
23 | 9 26 6 9 44 5 27 15 12 19 5 | 16 32 17 15 43 19 30 20 18 19 14
24E | 15 24 9 10 45 12 21 14 42 22 7 | 43 52 48 46 59 49 51 51 67 52 47
25E | 13 24 11 10 28 5 18 14 27 12 6 | 16 26 21 21 30 18 26 24 39 21 18
26 | 7 14 8 6 27 3 14 6 13 12 3 | 10 21 14 12 36 15 21 14 19 13 12
27E | 8 21 8 8 41 5 17 12 22 11 4 | 14 28 20 16 39 20 27 18 28 18 16
28 | 7 20 10 9 28 5 21 8 8 36 5 | 17 27 21 19 40 19 23 19 25 27 17
29 | 9 21 15 10 32 8 20 8 11 28 5 | 16 28 25 17 31 19 31 21 21 23 19
30 | 5 16 4 7 33 6 14 6 12 16 3 | 19 22 23 20 44 20 18 19 24 23 21
31E | 6 16 6 13 40 8 25 9 10 13 4 | 15 22 17 13 32 15 23 20 18 19 15
32 | 11 23 6 13 37 6 22 11 17 19 5 | 19 27 19 19 32 19 24 20 24 21 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 21 9 9 37 6 21 10 16 20 |T 22 29 26 20 37 25 27 25 29 24 23
WRMS | 8 21 9 9 35 5 20 9 9 21 |NE 23 27 27 19 38 26 26 25 27 22 23
MEDI | 8 22 8 9 36 6 21 9 12 19 |MD 17 28 21 19 38 20 27 20 24 23 19
Table 3.1529.5 GPS week: 1529 Day: 5 MJD: 54952.000
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 | 11 --- --- --- --- 23 --- 17 20 --- 11 | 105 --- --- --- --- 105 --- 116 114 --- 109
2E | 7 25 12 12 29 3 20 13 13 16 5 | 23 29 28 23 40 22 25 18 29 25 22
3 | 9 17 7 7 38 6 14 9 6 18 3 | 44 49 48 47 55 49 48 48 53 53 47
4E | 12 19 11 11 43 8 14 13 18 27 5 | 33 33 27 31 38 31 31 28 42 31 30
X5 | 60 34 26 --- --- 26 --- 20 36 --- 20 | 42 23 21 --- --- 35 --- 19 28 --- 21
6 | 7 17 9 9 38 6 15 13 5 19 4 | 17 23 24 24 23 20 20 21 24 27 20
7E | 7 23 9 13 30 4 23 10 7 10 4 | 13 23 17 18 33 13 22 13 20 12 13
8E | 15 28 11 11 24 7 17 11 15 24 6 | 67 70 69 68 65 69 65 74 73 67 68
9E | 9 19 10 9 65 5 17 10 19 19 5 | 20 27 25 25 43 23 28 22 36 24 23
10 | 6 15 8 10 13 6 11 9 7 10 3 | 11 16 17 19 20 11 17 14 22 12 14
11 | 10 20 11 12 32 5 16 9 6 14 4 | 15 25 21 18 42 16 21 14 19 20 15
12 | 7 22 8 12 28 6 20 8 10 27 5 | 14 28 22 22 33 19 25 17 22 24 18
13 | 8 25 8 7 52 5 24 20 10 16 5 | 12 30 19 15 47 12 25 14 12 17 11
14 | 8 29 10 13 41 4 22 7 8 16 5 | 15 27 21 25 35 19 26 17 21 20 18
15 | 10 22 13 16 42 5 22 12 9 22 5 | 13 25 16 22 40 12 23 16 17 19 12
X16 | 10 24 8 7 33 13 --- 10 11 28 5 | 10 20 9 10 21 12 --- 6 20 7 10
17 | 9 22 13 14 34 5 23 10 9 34 6 | 25 26 18 24 28 22 24 27 30 39 22
18 | 7 25 10 11 40 4 24 8 9 18 5 | 15 30 19 20 36 18 28 15 26 20 18
19 | 6 23 11 11 27 9 25 12 8 22 5 | 17 30 21 19 34 22 34 19 24 20 19
20 | 10 27 9 13 48 6 25 10 10 17 5 | 14 28 17 19 52 15 26 12 21 18 14
21E | 7 19 8 8 28 4 18 8 9 13 4 | 12 21 16 14 26 11 19 15 19 19 13
22 | 5 21 11 7 52 7 22 10 10 16 4 | 17 25 19 17 34 17 27 21 26 21 19
23 | 10 25 10 8 40 4 25 10 10 21 5 | 16 27 21 17 40 16 27 14 16 17 14
24E | 18 22 11 15 43 6 19 15 33 21 7 | 36 49 45 42 51 40 47 44 54 45 41
25E | 14 23 14 12 22 8 20 15 29 12 6 | 25 29 27 30 37 28 32 28 47 29 27
26 | 8 16 12 10 16 3 12 8 8 14 4 | 11 19 15 18 26 12 20 13 19 10 13
27E | 9 20 9 8 46 7 17 12 23 14 5 | 14 24 17 14 36 17 24 18 31 20 14
28 | 8 22 12 13 29 4 23 8 11 36 6 | 13 23 16 17 37 13 22 14 24 25 13
29 | 10 24 8 15 32 7 20 12 10 28 5 | 14 28 16 20 27 14 26 19 23 15 15
30 | 5 17 8 9 24 5 13 8 9 19 4 | 18 18 24 22 28 21 18 17 25 21 19
31E | 7 17 8 12 29 9 23 12 11 14 4 | 19 29 24 25 34 22 29 17 27 21 21
32 | 11 24 8 12 37 4 20 6 14 17 5 | 23 30 28 27 37 24 29 26 27 30 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 22 10 11 37 6 20 11 13 20 |T 23 28 23 23 36 24 27 24 30 24 23
WRMS | 8 22 10 11 34 5 19 10 7 18 |NE 22 26 20 21 34 23 25 23 28 21 22
MEDI | 9 22 10 11 33 6 20 10 10 18 |MD 16 27 21 20 36 19 26 17 24 20 18
Table 3.1529.6 GPS week: 1529 Day: 6 MJD: 54953.000
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 | 4 --- --- --- --- 18 --- --- --- --- 0 | 119 --- --- --- --- 113 --- --- --- --- 120
2E | 7 25 14 11 24 4 19 14 9 16 5 | 26 38 28 28 35 27 34 34 29 37 28
3 | 9 13 12 11 31 4 11 10 8 27 4 | 32 35 32 35 34 33 32 34 37 45 34
4E | 10 28 11 8 62 8 16 14 19 25 5 | 39 46 40 39 20 43 37 40 53 45 40
X5 | 15 23 13 --- --- 17 --- 10 19 --- 8 | 24 29 26 --- --- 26 --- 17 20 --- 17
6 | 8 15 9 12 31 5 13 12 8 24 4 | 18 24 24 28 25 22 18 21 24 33 21
7E | 8 21 8 11 24 4 19 10 5 12 4 | 17 29 17 20 34 16 26 18 21 17 17
8E | 17 26 15 10 26 10 18 15 15 28 6 | 78 73 75 81 71 73 71 80 80 71 75
9E | 11 17 9 7 55 4 16 10 17 19 4 | 21 33 29 25 45 24 34 26 33 28 25
10 | 7 17 8 10 15 5 11 9 6 11 3 | 18 23 19 17 25 17 22 20 18 19 16
11 | 8 19 12 10 42 4 12 9 8 23 4 | 20 31 23 25 46 21 26 20 21 24 20
12 | 7 20 10 9 22 7 19 7 11 34 5 | 18 31 22 21 34 21 28 17 21 34 19
13 | 7 22 8 9 60 4 22 16 7 17 5 | 14 30 17 19 51 14 25 16 16 16 12
14 | 7 23 10 10 26 5 23 11 6 18 5 | 17 26 17 20 30 15 23 17 18 16 14
15 | 10 21 12 11 34 8 23 11 8 18 5 | 15 29 24 21 34 21 25 23 19 19 16
16 | 7 20 9 9 40 6 20 13 9 30 5 | 8 19 8 6 23 7 18 7 15 7 7
17 | 8 17 11 10 37 3 23 11 11 40 5 | 28 25 23 28 45 27 32 32 34 49 28
18 | 8 26 10 9 38 6 23 9 8 18 5 | 14 32 16 17 39 15 30 14 19 19 15
19 | 11 23 13 11 29 7 23 11 9 26 5 | 20 35 19 16 37 18 36 25 22 23 21
20 | 13 19 13 10 40 5 22 9 13 16 5 | 16 26 23 20 44 16 26 16 18 18 16
21E | 7 19 12 8 31 4 15 7 9 12 4 | 16 24 17 12 34 13 24 16 23 16 15
22 | 8 22 13 9 50 5 24 15 7 19 5 | 15 25 18 17 39 15 25 22 19 20 15
23 | 10 22 11 8 44 5 21 7 10 21 5 | 14 30 17 15 45 13 26 13 14 12 12
24E | 19 22 11 15 54 5 20 16 34 22 7 | 46 58 50 50 53 48 59 51 62 57 50
25E | 17 24 15 13 19 10 16 13 28 11 6 | 20 36 28 28 39 22 31 25 40 30 24
26 | 8 14 9 4 19 6 11 9 8 16 3 | 10 21 14 12 24 13 19 18 17 14 12
27E | 10 20 10 8 56 6 16 12 24 15 5 | 18 27 23 19 36 20 28 23 33 25 18
28 | 9 21 14 12 26 5 20 6 11 39 5 | 19 28 27 25 33 22 23 22 27 31 19
29 | 10 22 9 11 29 8 19 8 11 29 5 | 22 34 23 21 35 20 36 28 24 27 23
30 | 7 14 8 6 24 5 11 9 8 22 3 | 23 27 26 25 38 26 23 20 26 26 22
31E | 7 13 7 8 34 10 17 6 12 13 3 | 17 26 17 15 34 18 25 19 23 18 18
32 | 12 19 9 11 44 4 18 7 12 18 4 | 17 26 23 20 46 18 25 19 24 21 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 11 10 38 6 18 11 13 22 |T 24 31 24 24 37 25 29 24 27 27 25
WRMS | 9 20 11 10 34 6 18 10 7 19 |NE 22 27 20 20 35 23 25 20 21 23 22
MEDI | 8 21 11 10 31 5 19 10 9 19 |MD 18 29 23 20 35 20 26 20 23 23 19
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 4.1529 GPS week: 1529 MJD: 54947.0-54953.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3012 |U 8 8 24 |U 7 8 22 |U 8 9 16 |
emr | emr 2962 | 14 9 32 | 9 11 27 | 10 10 22 |
esa | esa 3017 | 9 9 28 |U 6 8 21 | 8 8 18 |
gfz | gfz 2826 |U 11 9 29 |U 8 13 36 | 8 8 19 |
grg | grg 2852 | 11 9 30 |U 10 10 31 | 10 10 22 |
igr | igr 2962 | 10 9 29 | 7 10 24 | 9 9 19 |
igs | igs 2901 | 10 9 28 | 7 10 23 | 8 8 18 |
jpl | jpl 2800 |U 11 8 32 |U 8 11 24 |U 9 8 23 |
mit | mit 3030 |U 9 9 29 |U 7 9 25 |U 9 8 25 |
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 5.1529.0 GPS week: 1529 Day: 0 MJD: 54947.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 | 6 7 24 | 6 7 14 | 7 12 22 |
emr | emr 3048 | 10 8 26 | 7 9 21 | 9 10 26 |
esa | esa 3072 | 6 6 26 | 5 7 17 | 9 9 22 |
gfz | gfz 2841 | 6 7 24 | 8 10 29 | 7 9 21 |
grg | grg 2880 | 7 5 21 | 9 8 22 | 9 8 21 |
igr | igr 2988 | 9 10 30 | 10 12 24 | 12 16 26 |
igs | igs 2829 | 8 11 29 | 9 14 27 | 8 12 24 |
jpl | jpl 2856 | 6 5 22 | 5 8 16 | 7 7 21 |
mit | mit 3072 | 6 6 24 | 5 7 18 | 9 10 22 |
Table 5.1529.1 GPS week: 1529 Day: 1 MJD: 54948.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 | 7 8 24 | 7 9 20 | 7 6 18 |
emr | emr 3049 | 11 8 29 | 9 12 24 | 12 11 23 |
esa | esa 3072 | 7 9 27 | 6 9 18 | 10 8 20 |
gfz | gfz 2931 | 8 9 29 | 7 12 28 | 9 9 20 |
grg | grg 2880 | 8 9 25 | 8 10 28 | 10 8 22 |
igr | igr 2966 | 8 9 29 | 6 9 18 | 9 8 19 |
igs | igs 2972 | 7 8 26 | 6 9 20 | 9 8 19 |
jpl | jpl 2855 | 7 6 31 | 6 11 20 | 12 11 24 |
mit | mit 3072 | 7 10 24 | 6 9 23 | 11 6 26 |
Table 5.1529.2 GPS week: 1529 Day: 2 MJD: 54949.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 9 6 24 | 7 8 27 | 9 10 17 |
emr | emr 3040 | 18 8 35 | 8 11 31 | 11 11 19 |
esa | esa 3072 | 11 8 29 | 7 7 24 | 10 10 17 |
gfz | gfz 2844 | 17 9 37 | 8 9 38 | 9 9 20 |
grg | grg 2880 | 17 7 45 | 10 11 35 | 12 12 22 |
igr | igr 2952 | 20 9 40 | 7 10 27 | 9 8 19 |
igs | igs 2958 | 13 8 31 | 7 8 27 | 9 9 19 |
jpl | jpl 2763 | 17 8 35 | 9 15 28 | 10 8 25 |
mit | mit 3072 | 7 7 27 | 7 8 30 | 12 16 21 |
Table 5.1529.3 GPS week: 1529 Day: 3 MJD: 54950.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2928 | 10 6 27 | 7 7 23 | 8 8 14 |
emr | emr 2859 | 16 7 39 | 9 11 31 | 10 10 23 |
esa | esa 2976 | 13 7 38 | 5 8 23 | 8 7 16 |
gfz | gfz 2745 | 12 6 33 | 8 13 40 | 8 8 19 |
grg | grg 2784 | 15 8 43 | 10 15 35 | 8 9 21 |
igr | igr 2903 | 11 6 32 | 6 11 22 | 7 7 16 |
igs | igs 2868 | 12 6 36 | 6 10 25 | 7 7 16 |
jpl | jpl 2763 | 18 7 41 | 7 11 25 | 7 6 21 |
mit | mit 2976 | 12 9 44 | 6 11 24 | 10 5 22 |
Table 5.1529.4 GPS week: 1529 Day: 4 MJD: 54951.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2929 | 10 13 25 | 5 8 21 | 8 9 15 |
emr | emr 2853 | 16 11 34 | 8 12 23 | 10 10 22 |
esa | esa 2976 | 11 15 25 | 6 7 22 | 8 8 20 |
gfz | gfz 2744 | 12 16 28 | 6 10 35 | 8 8 21 |
grg | grg 2784 | 12 12 28 | 10 9 29 | 8 7 25 |
igr | igr 2954 | 11 14 26 | 6 7 26 | 8 8 20 |
igs | igs 2824 | 12 13 28 | 6 9 19 | 7 8 19 |
jpl | jpl 2758 | 9 11 25 | 8 9 23 | 8 7 23 |
mit | mit 2976 | 9 11 30 | 7 7 25 | 7 8 23 |
Table 5.1529.5 GPS week: 1529 Day: 5 MJD: 54952.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 6 7 25 | 6 8 25 | 7 9 16 |
emr | emr 2942 | 16 9 35 | 10 10 29 | 10 10 19 |
esa | esa 2976 | 7 8 28 | 7 8 21 | 8 8 18 |
gfz | gfz 2838 | 12 8 35 | 13 28 50 | 7 8 19 |
grg | grg 2880 | 8 9 24 | 12 9 35 | 11 16 23 |
igr | igr 2990 | 7 8 26 | 7 10 25 | 7 6 18 |
igs | igs 2920 | 7 8 28 | 6 9 22 | 7 7 17 |
jpl | jpl 2757 | 14 10 49 | 7 10 32 | 8 6 20 |
mit | mit 3072 | 10 8 31 | 8 9 28 | 8 7 19 |
Table 5.1529.6 GPS week: 1529 Day: 6 MJD: 54953.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 7 8 19 | 10 10 24 | 9 9 13 |
emr | emr 2947 | 11 13 28 | 12 12 28 | 11 10 23 |
esa | esa 2976 | 8 8 20 | 8 9 20 | 7 6 13 |
gfz | gfz 2844 | 7 7 21 | 9 11 33 | 7 7 16 |
grg | grg 2880 | 8 11 25 | 11 13 35 | 10 12 19 |
igr | igr 2984 | 8 9 21 | 9 10 24 | 8 7 14 |
igs | igs 2942 | 7 9 20 | 9 11 22 | 8 6 15 |
jpl | jpl 2852 | 9 10 22 | 10 11 24 | 10 12 23 |
mit | mit 2976 | 9 10 25 | 10 11 28 | 10 7 45 |
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 : 21-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 6.1529 GPS week: 1529 MJD: 54947.500-54953.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -20 -40 56 163 -1 | 10 16
| 12 19 157 33 9 | 1
emr uuuxu | 16 -8 -32 531 10 | 53 56
| 32 14 200 148 9 | 7
esa uuuuu | -20 -35 36 -156 -3 | 13 21
| 24 26 67 78 12 | 2
gfz uuuuu | 16 -4 -1 124 3 | 25 28
| 13 17 88 56 9 | 5
grg xxxxx | -24 -48 48 156 13 | -2 35
| 27 24 116 126 32 | 3
igr xxxxx | 6 -2 -3 55 4 | 1 11
| 26 33 42 87 5 | 3
irf xxxxx | -8 7 -5 63 0 | 2 15
| 5 8 24 22 10 | 5
jpl uuuuu | 9 1 64 171 1 | 17 23
| 23 19 113 92 13 | 4
mit uuuuu | -33 -1 109 15 5 | 22 28
| 11 15 90 64 13 | 7
ngs uuuuu | -41 67 -163 -143 -6 | 9 14
| 29 18 147 122 10 | 1
sio uuuuu | 130 17 -199 120 17 | 42 47
| 16 8 67 57 15 | 9
Table 7.1529.0 GPS week: 1529 Day: 0 MJD: 54947.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -32 -13 -201 216 -13 | 8 14
emr uuuxu | -3 -35 319 309 11 | 45 46
esa uuuuu | 10 -34 50 -87 5 | 11 19
gfz uuuuu | -1 3 -147 79 -3 | 18 21
grg xxxxx | -30 -55 -165 23 51 | -7 34
igr xxxxx | 34 -53 14 18 1 | -3 8
irf xxxxx | -5 15 39 60 8 | -6 14
jpl uuuuu | 36 13 -77 125 -13 | 14 19
mit uuuuu | -37 14 267 79 10 | 13 19
ngs uuuuu | -86 50 -252 -185 -6 | 8 13
sio uuuuu | 156 7 -305 86 27 | 30 32
Table 7.1529.1 GPS week: 1529 Day: 1 MJD: 54948.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 1 -17 -77 130 -7 | 8 14
emr uuuxu | -32 5 118 388 19 | 46 48
esa uuuuu | -8 -50 44 -158 1 | 12 21
gfz uuuuu | 10 17 -34 219 11 | 19 23
grg xxxxx | 14 -80 -61 262 -19 | -1 39
igr xxxxx | 24 22 -8 124 13 | -3 9
irf xxxxx | -2 16 -15 70 10 | -4 15
jpl uuuuu | -7 -3 149 51 11 | 12 16
mit uuuuu | -16 15 123 44 17 | 15 21
ngs uuuuu | -44 59 -409 -232 -20 | 8 12
sio uuuuu | 140 19 -226 153 33 | 33 37
Table 7.1529.2 GPS week: 1529 Day: 2 MJD: 54949.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -12 -42 62 158 -9 | 11 14
emr uuuxu | -4 2 21 547 9 | 51 53
esa uuuuu | -9 -63 61 -105 -17 | 17 21
gfz uuuuu | 31 8 14 118 0 | 24 26
grg xxxxx | -16 -25 72 257 -1 | -1 39
igr xxxxx | -7 34 -35 114 5 | 1 9
irf xxxxx | -10 13 -16 65 3 | 1 12
jpl uuuuu | -29 28 -60 159 8 | 15 19
mit uuuuu | -47 11 133 33 11 | 20 25
ngs uuuuu | -13 81 -239 -145 -2 | 9 12
sio uuuuu | 122 26 -160 53 25 | 39 44
Table 7.1529.3 GPS week: 1529 Day: 3 MJD: 54950.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -22 -56 178 166 4 | 9 13
emr uuuxu | 14 -5 -115 694 25 | 52 53
esa uuuuu | -9 -2 141 -145 -4 | 14 20
gfz uuuuu | 21 -24 -60 131 15 | 24 26
grg xxxxx | -33 -18 95 148 -15 | -6 36
igr xxxxx | -11 22 -38 -86 -1 | 1 9
irf xxxxx | -6 5 -25 84 11 | 2 11
jpl uuuuu | 3 -25 -27 173 22 | 15 19
mit uuuuu | -30 -17 71 92 20 | 21 25
ngs uuuuu | -71 81 -131 -344 -17 | 9 12
sio uuuuu | 128 25 -90 103 27 | 42 46
Table 7.1529.4 GPS week: 1529 Day: 4 MJD: 54951.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -35 -59 12 140 -4 | 11 18
emr uuuxu | 42 -4 -201 593 2 | 58 62
esa uuuuu | -14 2 -53 -76 -21 | 15 23
gfz uuuuu | 0 -29 26 67 -11 | 30 34
grg xxxxx | -35 -77 143 47 -10 | 0 31
igr xxxxx | 40 12 0 134 -2 | 4 13
irf xxxxx | -16 -1 14 19 -12 | 7 17
jpl uuuuu | 25 -19 181 215 -2 | 21 29
mit uuuuu | -45 -23 143 -73 -8 | 27 34
ngs uuuuu | -13 93 -60 -35 11 | 10 14
sio uuuuu | 117 7 -178 88 4 | 48 55
Table 7.1529.5 GPS week: 1529 Day: 5 MJD: 54952.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -19 -38 183 131 4 | 11 18
emr uuuxu | 34 2 -256 699 3 | 61 64
esa uuuuu | -52 -46 -45 -285 5 | 12 20
gfz uuuuu | 25 0 105 172 3 | 30 34
grg xxxxx | 3 -39 140 325 22 | 0 31
igr xxxxx | -26 -22 -34 106 3 | 5 14
irf xxxxx | -10 -1 -4 81 -7 | 8 17
jpl uuuuu | 32 -2 151 346 -2 | 22 29
mit uuuuu | -33 -6 43 -43 -6 | 30 35
ngs uuuuu | -33 52 26 -67 -3 | 12 16
sio uuuuu | 137 19 -206 128 3 | 51 57
Table 7.1529.6 GPS week: 1529 Day: 6 MJD: 54953.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -23 -55 233 197 14 | 9 19
emr uuuxu | 62 -19 -108 484 3 | 61 64
esa uuuuu | -56 -52 56 -237 12 | 10 20
gfz uuuuu | 25 -2 88 82 5 | 29 33
grg xxxxx | -68 -45 109 32 60 | -1 31
igr xxxxx | -11 -30 79 -28 8 | 3 15
irf xxxxx | -9 1 -29 62 -9 | 6 19
jpl uuuuu | 4 12 129 130 -16 | 19 29
mit uuuuu | -24 1 -18 -31 -10 | 29 35
ngs uuuuu | -24 52 -78 4 -2 | 9 17
sio uuuuu | 107 16 -231 226 -3 | 52 57
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