[IGSREPORT-17312] Wk 1525 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 16 05:36:19 PDT 2009
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IGS Electronic Report 16 Apr 05:36:41 PDT 2009 Message Number 17312
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1525 (Mar 29, 2009 - Apr 04, 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:
igs1525[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1525[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1525[0-6].cls IGS GPS clock combination summary report.
igs15257.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15257.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 | EMR | MIZU
0 | GFZ | 7 29 MATE YAKT
0 | GRG | NLIB
0 | MIT | 5 19 5 19 BOR1
1 | COD | NISU NRIL ULAB
1 | EMR | HARB
1 | ESA | MAL2
1 | GFZ | 7 29 BOGT CRO1 EIL1 FAA1 GLPS GUAT IRKT SCUB SSIA
1 | GFZ | YELL
1 | GRG | NLIB
1 | MIT | BOR1
2 | COD | MATE PRE1
2 | EMR | WTZR
2 | GFZ | 7 29 CONZ HRM1 IRKT MAL2 REYK
2 | GRG | JPLM KHAJ MANA NLIB NOVM WTZR ZECK
2 | MIT | 5 5 ADE1 BUE1 EIL1
3 | COD | BOR1
3 | EMR | MIZU
3 | ESA | ALGO BHR1 CAS1 COCO DRAO HOLM KARR KERG KIT3 MAS1
3 | ESA | MDVJ NLIB PERT QAQ1 SCH2 VILL YELL
3 | GFZ | 7 29 IRKT KERG KOUR
3 | GRG | NLIB
3 | MIT | KOUR HRAO KOUR NNOR NTUS SHAO
4 | ALL | 1 1 18
4 | COD | HARB NISU THU3
4 | EMR | MIZU
4 | GFZ | 7 29 HARB IRKT THU3
4 | GRG | NLIB
4 | MIT | 5 5 HARB KERG MDVJ
5 | ALL | 1 1
5 | COD | TWTF TWTF
5 | EMR | 21 21 MIZU
5 | ESA | 4
5 | GFZ | 7 8 29 GUAT IRKT SSIA TWTF
5 | GRG | BOR1 GLSV JPLM KHAJ NLIB NOVM SYOG
5 | MIT | 5 5 MAS1 MAS1
6 | ALL | 1
6 | EMR | HARB HARB
6 | GFZ | 7 29 IRKT
6 | GRG | NLIB
6 | JPL | HARB
6 | MIT | 5 26 5 26 HOB2
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
----+------------+----------
G18 | 2009_04_02 | 2009024
G18 | 2009_04_03 | 2009024
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G01 | 4 | 4 | 2 | 2 | 1 | | |
7. 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.
8. 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 | .1 .4 .1 -24 -19 -6 -.04
EMR | 11.4 -6.1 -1.0 59 29 51 .07
ESA | 4.0 .0 .2 -8 -33 26 .04
GFZ | .8 1.1 1.6 20 -17 13 -.42
GRG | 4.7 .5 -5.1 8 -22 25 -.02
JPL | 1.7 3.3 13.2 -13 -30 -6 .22
MIT | 6.1 -8.7 1.9 -20 23 -40 -.08
NGS | 10.2 -5.0 -3.1 -61 -160 18 .16
SIO | 6.3 -1.2 10.3 -33 -69 -21 .12
9. 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.
10. 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.
11. 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 1.1525.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1525.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 2.1525.[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 3.1525.[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 5.1525.0-6).
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 1525 summary. (Mar 29, 2009 - Apr 04, 2009)
Table 1.1525.a GPS week: 1525 MJD: 54919.000-54925.000
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 241| 0 0 1 16 -19 -14 -.11 8 8 | -244 -608 15 110
| 0 0 1 8 14 23 .02 | 174 845
emr 82| 0 0 6 -147 -127 -39 .49 19 19 | 1683 565 17 168
| 1 2 1 23 23 19 .02 | 1635 954
esa 123| 0 0 0 -27 -20 -15 .34 10 10 | 369 -563 20 145
| 0 1 1 14 50 28 .04 | 884 1992
gfz 199| 0 0 -3 -54 -19 94 -.09 11 11 | -46 136 23 146
| 0 0 1 20 16 39 .04 | 424 973
grg 115| 0 1 -6 -49 4 43 1.08 34 32 | 34592 10923 207 6868
| 1 1 3 24 26 18 .04 | 101890 26825
igr n/a| 0 0 0 -30 -41 6 .05 6 5 | -902 765 21 65
| 0 0 1 14 18 29 .04 | 1809 917
jpl 134| 0 2 2 3 21 -17 .61 18 18 | 964 642 18 96
| 2 1 0 31 10 28 .02 | 3079 815
mit 266| 0 -2 -2 18 -126 -30 -.32 12 12 | -75 372 20 136
| 0 0 0 30 33 13 .03 | 345 730
ngs 220| 0 0 0 104 203 -11 -.39 11 9 | -414 -624 2245 4038
| 0 0 1 20 50 16 .03 | 480 1033
sio 262| 0 0 0 29 92 7 .07 21 20 | --- --- --- ---
| 1 1 1 28 31 26 .02 | --- ---
Table 1.1525.b GPS week : 1525 MJD: 54919.000-54925.000
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 | 0 0 0 0 18 12 11 |
2 | 5 5 5 5 5 5 6 |
3 | 4 4 4 5 4 5 4 |
4 | 4 6 4 5 5 4 4 |
5 | 7 8 8 9 12 11 8 |
6 | 4 4 4 5 5 4 4 |
7 | 5 5 5 5 5 6 5 |
8 | 4 4 4 4 4 4 5 |
9 | 4 4 5 5 4 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 6 6 6 6 6 5 5 |
12 | 5 5 6 5 5 5 5 |
13 | 5 5 5 4 4 4 4 |
14 | 5 5 5 5 4 5 5 |
15 | 5 5 6 5 5 5 5 |
16 | 5 5 6 6 5 5 5 |
17 | 5 5 6 6 5 5 6 |
18 | 6 6 6 7 7 0 6 |
19 | 5 4 5 5 5 5 5 |
20 | 6 5 6 5 5 5 6 |
21 | 6 5 5 5 5 5 5 |
22 | 5 5 5 5 4 5 6 |
23 | 5 5 6 5 5 5 5 |
24 | 4 4 5 4 4 4 5 |
25 | 4 4 5 5 5 5 5 |
26 | 4 4 5 5 4 4 4 |
27 | 4 4 4 4 4 4 4 |
28 | 5 4 6 5 4 4 5 |
29 | 5 5 6 6 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 5 5 6 5 5 5 5 |
32 | 5 6 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 2.1525.0 GPS week: 1525 Day: 0 MJD: 54919.000
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 241| 0 0 3 14 -1 0 -.12 8 8 | -237 -261 14 109
| 18 -20 |
emr 82| -1 1 7 -177 -106 -63 .51 21 21 | 923 265 20 213
| 44 -21 |
esa 123| 0 0 0 -32 -104 8 .31 8 8 | 562 -413 18 125
| 37 111 |
gfz 199| 0 0 -4 -47 -9 88 -.05 11 11 | 18 513 22 155
| 9 0 |
grg 115| 1 1 -12 -50 -21 32 1.13 34 34 | -49 503 225 299
| 82 -18 |
igr n/a| 0 1 -2 -24 -22 -15 .08 6 6 | -2300 668 25 84
| 10 -30 |
jpl 134| 2 2 2 -18 10 -44 .60 19 19 | 2659 439 20 113
| -4 -25 |
mit 266| 0 -3 -2 24 -151 -31 -.32 11 11 | -80 505 21 148
| 13 41 |
ngs 220| 0 0 -2 104 291 -5 -.36 10 9 | -261 -265 2498 4299
| -3 7 |
sio 262| 0 -1 -1 16 51 -23 .07 22 22 | --- --- --- ---
| -4 -73 |
Table 2.1525.1 GPS week: 1525 Day: 1 MJD: 54920.000
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 241| 0 0 3 10 -13 14 -.12 8 8 | -489 -162 14 134
| 40 3 |
emr 82| 1 3 8 -171 -117 -50 .47 19 19 | -103 666 14 172
| 18 25 |
esa 123| 0 -2 0 -24 6 -6 .38 9 9 | -631 2875 22 148
| 35 35 |
gfz 199| 1 1 -4 -35 -43 115 -.06 12 11 | -21 139 25 159
| 17 49 |
grg 115| -2 3 -8 -41 0 38 1.04 33 31 | -249 -172 193 283
| 83 43 |
igr n/a| -1 1 -1 -38 -72 -10 .07 5 5 | -2978 922 21 65
| 10 13 |
jpl 134| 1 4 3 -1 9 7 .65 19 19 | 1572 744 20 114
| -42 -12 |
mit 266| 0 -2 -2 29 -121 -44 -.31 10 9 | -98 -102 20 159
| 22 38 |
ngs 220| 0 0 -3 92 221 -40 -.36 10 9 | -498 -162 2486 4373
| 24 53 |
sio 262| 0 -1 0 55 81 -24 .04 23 20 | --- --- --- ---
| -30 -61 |
Table 2.1525.2 GPS week: 1525 Day: 2 MJD: 54921.000
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 241| 0 0 1 12 -18 -29 -.12 9 9 | 15 -1981 18 115
| -14 26 |
emr 82| 0 -1 4 -138 -160 -37 .51 18 18 | 521 935 15 151
| 14 66 |
esa 123| 1 0 0 -22 46 -29 .35 12 12 | 843 -1474 21 127
| 29 -15 |
gfz 199| 1 0 -3 -61 -12 151 -.10 12 12 | 6 30 23 141
| 16 47 |
grg 115| 0 3 -2 -46 52 21 1.05 34 31 | 176 5648 225 17537
| 9 76 |
igr n/a| 0 0 -1 -37 -46 -4 .07 5 5 | -2017 1139 20 56
| -4 -38 |
jpl 134| 0 0 2 15 39 -12 .61 18 18 | 2114 835 19 94
| -37 -32 |
mit 266| 1 -1 -2 -4 -96 -32 -.30 11 10 | 622 -979 20 127
| 29 33 |
ngs 220| 0 1 0 136 132 -8 -.40 12 10 | -1061 -652 2146 4676
| -47 207 |
sio 262| 0 0 1 -4 112 19 .07 20 19 | --- --- --- ---
| -14 -75 |
Table 2.1525.3 GPS week: 1525 Day: 3 MJD: 54922.000
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 241| 0 0 0 6 -27 15 -.08 7 7 | -297 -273 15 106
| 62 47 |
emr 82| -2 1 4 -161 -148 -64 .50 18 18 | 1310 775 17 155
| 37 62 |
esa 123| 1 0 2 -17 0 -70 .35 14 14 | 759 -1664 26 246
| 28 22 |
gfz 199| 0 0 -3 -22 -10 108 -.06 11 11 | -344 981 22 131
| 38 61 |
grg 115| 0 1 -5 -90 8 50 1.13 36 32 | 39 491 183 264
| 82 58 |
igr n/a| 0 0 0 -53 -42 -31 .07 5 5 | -1029 1025 21 74
| -4 -35 |
jpl 134| -1 2 3 -41 20 -18 .60 17 17 | 1500 783 19 96
| 3 42 |
mit 266| 0 -1 -2 55 -96 -48 -.28 13 12 | -341 829 21 136
| 18 25 |
ngs 220| 1 -1 -1 68 173 -4 -.43 12 10 | -503 70 1779 3583
| 9 141 |
sio 262| -1 0 1 64 115 -12 .12 20 22 | --- --- --- ---
| -7 -80 |
Table 2.1525.4 GPS week: 1525 Day: 4 MJD: 54923.000
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 241| 1 0 -1 21 -8 -40 -.11 8 8 | -67 45 16 85
| 28 -11 |
emr 82| 0 0 6 -136 -104 -17 .51 18 18 | 1419 1224 19 134
| 30 23 |
esa 123| 2 1 0 -42 -66 8 .35 9 9 | 0 -1080 19 130
| 30 69 |
gfz 199| 1 0 -1 -65 1 90 -.14 11 11 | -256 270 25 148
| 21 10 |
grg 115| 2 0 -5 -41 -4 54 1.08 36 35 | -142 -220 188 264
| 15 -36 |
igr n/a| -1 0 1 -24 -20 32 .04 5 5 | -793 1261 19 57
| -8 -45 |
jpl 134| -3 2 1 21 24 -58 .62 16 16 | 1611 1256 15 89
| -10 30 |
mit 266| 0 -1 -2 14 -190 -11 -.34 13 12 | -183 656 21 129
| 22 39 |
ngs 220| 0 0 1 110 223 -8 -.36 9 9 | -274 -144 2112 3321
| -51 61 |
sio 262| 0 2 0 21 49 34 .08 20 19 | --- --- --- ---
| 3 -79 |
Table 2.1525.5 GPS week: 1525 Day: 5 MJD: 54924.000
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 241| 0 0 0 19 -22 -31 -.15 7 7 | -389 42 15 119
| 76 64 |
emr 82| -1 0 6 -125 -106 -29 .48 19 19 | 3052 1498 21 209
| 42 40 |
esa 123| 1 0 0 -4 -25 -20 .27 8 8 | -717 1041 19 123
| -22 64 |
gfz 199| 0 0 -3 -66 -20 87 -.13 9 9 | -524 927 22 153
| 26 67 |
grg 115| 1 1 -6 -65 -23 77 1.05 34 30 | -22505 71545 253 29132
| 62 30 |
igr n/a| -1 0 1 -26 -32 50 -.03 5 5 | 535 1562 20 62
| -28 -34 |
jpl 134| 0 0 1 -6 30 -20 .58 18 18 | 3167 1472 19 95
| 14 1 |
mit 266| 0 -2 -2 43 -119 -19 -.37 14 13 | 2 1292 19 132
| 39 9 |
ngs 220| 0 0 0 102 209 -24 -.38 13 11 | -774 -301 2297 3839
| -87 90 |
sio 262| -2 1 1 53 105 15 .07 21 20 | --- --- --- ---
| 21 -70 |
Table 2.1525.6 GPS week: 1525 Day: 6 MJD: 54925.000
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 241| 0 0 2 30 -47 -29 -.10 8 8 | -246 -1667 17 107
| 13 65 |
emr 82| 0 -2 4 -119 -146 -17 .46 17 17 | 4659 -1405 16 147
| 9 78 |
esa 123| 0 0 -1 -45 -2 0 .35 11 11 | 1772 -3227 18 120
| 11 54 |
gfz 199| 0 0 -4 -83 -39 19 -.07 11 11 | 797 -1908 23 140
| 1 75 |
grg 115| 1 0 -4 -11 21 33 1.08 33 28 | 264878 -1332 183 300
| -7 49 |
igr n/a| -1 1 0 -6 -54 23 .04 7 7 | 2268 -1218 27 63
| -61 30 |
jpl 134| 0 2 2 55 18 25 .62 17 17 | -5875 -1035 16 73
| -60 51 |
mit 266| 1 -1 0 -36 -108 -24 -.32 14 12 | -451 409 24 126
| 36 2 |
ngs 220| 0 0 0 115 173 13 -.43 10 8 | 470 -2915 2397 4176
| -104 165 |
sio 262| -1 0 1 -1 128 39 .07 22 21 | --- --- --- ---
| 32 -77 |
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 3.1525.0 GPS week: 1525 Day: 0 MJD: 54919.000
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 | 2 --- --- --- --- 153 --- --- --- --- 0 | 56 --- --- --- --- 87 --- --- --- --- 56
2 | 7 22 8 12 37 4 21 9 7 21 4 | 26 42 30 24 51 27 35 23 27 21 26
3 | 9 18 7 9 29 4 11 13 9 18 4 | 21 35 25 19 35 21 30 14 23 32 21
4 | 6 18 6 6 39 4 13 12 9 16 3 | 36 46 44 36 64 39 48 40 41 47 40
X5 | 6 21 16 12 --- 11 --- 19 15 --- 6 | 19 29 15 31 --- 21 --- 23 35 --- 24
6 | 9 18 6 7 29 5 11 11 8 22 4 | 17 30 21 16 32 17 28 14 23 36 19
7 | 8 22 9 15 27 6 21 12 11 14 5 | 17 26 18 19 37 16 24 15 27 14 17
8 | 10 18 8 7 33 6 10 9 9 11 3 | 11 22 18 15 29 13 19 15 24 12 14
9 | 8 15 9 7 27 6 14 13 11 16 4 | 16 25 19 19 27 17 23 21 28 25 19
10 | 7 13 9 10 30 4 13 9 11 23 4 | 24 21 27 29 29 23 22 21 32 15 24
11E | 10 36 7 13 39 5 18 16 8 17 5 | 16 51 25 29 49 22 27 22 26 16 21
12 | 8 14 10 10 38 8 21 9 12 36 5 | 21 28 25 22 41 21 31 21 35 24 23
13 | 6 26 8 12 42 6 20 11 12 9 4 | 13 32 17 14 42 14 25 15 25 13 14
14 | 9 19 9 7 24 8 23 17 8 20 5 | 14 24 20 18 32 14 25 17 20 12 16
15 | 8 22 9 10 26 4 25 9 11 24 5 | 16 26 21 16 32 14 26 16 24 22 17
16 | 6 24 7 13 32 7 22 10 9 28 5 | 21 29 22 21 38 19 32 21 27 22 21
17 | 6 27 10 7 31 6 23 9 12 11 4 | 20 32 20 19 44 21 32 23 25 21 19
18 | 9 20 8 12 50 7 24 14 10 32 5 | 13 27 20 20 35 19 26 16 19 21 18
19 | 7 26 9 10 27 7 21 8 7 14 4 | 21 36 23 19 46 22 36 21 27 22 22
20 | 7 24 9 14 22 4 22 17 9 25 5 | 21 30 25 31 35 22 25 29 24 23 21
21 | 11 25 10 11 29 7 19 10 13 28 5 | 19 29 20 20 37 15 25 14 29 30 19
22 | 9 19 8 8 55 8 21 12 7 26 4 | 27 34 33 35 39 31 33 35 35 29 31
23 | 6 30 7 14 26 5 26 11 11 19 5 | 15 35 18 16 39 17 32 15 27 14 16
24 | 6 15 9 7 23 5 12 9 13 25 4 | 18 27 21 18 34 16 25 16 27 27 19
25 | 7 20 5 10 25 7 9 11 10 25 4 | 13 23 14 17 29 14 21 17 25 27 15
26 | 6 18 7 8 25 8 14 9 10 21 4 | 14 23 21 19 29 15 25 15 24 29 18
27 | 7 21 7 7 22 6 9 8 9 18 3 | 14 27 20 15 28 16 22 14 22 23 16
28 | 5 17 8 11 34 7 16 13 9 26 4 | 22 29 25 22 35 22 26 25 26 25 22
29 | 6 23 8 10 34 7 26 10 10 21 5 | 23 34 26 24 28 23 39 23 34 25 26
30 | 3 13 6 5 45 5 14 10 9 20 3 | 27 30 33 28 23 27 26 32 34 23 29
31 | 6 24 7 17 38 5 22 10 10 17 5 | 18 29 20 22 48 17 27 15 24 13 17
32 | 10 19 9 15 39 6 23 13 8 25 5 | 14 23 20 25 47 18 20 22 19 19 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 21 8 11 34 6 19 11 10 22 |T 20 30 22 21 37 21 27 20 27 22 21
WRMS | 8 21 8 11 34 6 19 11 9 22 |NE 20 29 22 21 36 21 27 20 27 22 21
MEDI | 7 20 8 10 30 6 20 11 10 21 |MD 18 29 21 20 35 19 26 21 26 22 19
Table 3.1525.1 GPS week: 1525 Day: 1 MJD: 54920.000
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 | 2 --- --- --- --- 84 --- --- --- --- 0 | 87 --- --- --- --- 123 --- --- --- --- 86
2 | 7 20 8 14 41 4 22 9 14 19 5 | 17 34 21 15 43 18 32 17 19 18 17
3 | 9 16 7 11 22 5 14 14 7 19 4 | 21 29 28 20 29 23 30 25 21 32 22
4 | 8 16 9 12 43 5 16 7 15 50 6 | 68 75 77 66 80 69 78 71 73 84 71
X5 | 10 26 17 16 --- 12 --- 11 23 --- 7 | 15 27 13 22 --- 17 --- 19 37 --- 17
6 | 9 15 8 10 27 5 11 12 8 23 4 | 16 28 26 18 29 19 28 20 17 33 18
7 | 8 21 10 16 27 6 21 10 13 13 5 | 12 26 17 16 37 13 22 12 19 13 12
8 | 10 16 7 10 30 5 12 9 9 10 4 | 9 24 13 15 27 13 20 14 17 14 11
9 | 8 12 6 6 19 4 14 10 11 17 3 | 13 25 18 17 26 14 23 17 21 27 15
10 | 7 12 8 10 28 7 12 6 11 20 3 | 13 24 17 18 28 18 24 11 19 13 14
11E | 7 27 9 30 44 6 17 10 7 19 6 | 15 37 20 33 48 20 25 18 16 22 16
12 | 8 15 8 10 42 6 21 8 14 33 5 | 14 26 20 20 34 17 28 18 26 22 16
13 | 6 25 10 10 51 7 20 8 10 12 4 | 12 30 18 15 37 14 22 16 18 13 13
14 | 8 18 11 10 26 6 25 11 9 15 4 | 10 20 19 13 31 13 22 16 13 16 11
15 | 10 20 12 14 23 3 23 8 10 19 5 | 11 25 18 14 31 11 25 13 12 13 11
16 | 8 19 10 14 33 5 21 11 11 27 5 | 16 26 21 16 34 17 28 18 21 16 15
17 | 6 24 11 10 35 5 25 8 9 12 4 | 17 36 18 24 37 23 34 23 23 20 20
18 | 9 21 8 16 42 4 25 10 10 28 5 | 10 29 17 19 30 16 26 14 17 17 13
19 | 8 17 11 10 26 5 21 8 8 14 4 | 19 26 23 18 40 20 29 19 22 20 19
20 | 8 22 10 13 31 5 25 13 8 20 5 | 17 29 28 23 33 19 28 23 22 21 19
21 | 11 18 11 11 30 7 21 7 13 23 5 | 15 27 19 15 34 14 27 14 24 24 16
22 | 8 20 12 12 51 7 24 9 8 27 5 | 16 29 27 24 32 21 29 23 19 25 20
23 | 7 23 9 10 30 5 24 7 10 17 4 | 11 30 17 13 32 13 24 12 16 12 11
24 | 7 14 7 8 20 4 13 8 10 24 4 | 17 28 21 17 27 18 27 19 23 29 18
25 | 9 15 7 11 24 4 10 9 10 23 4 | 12 21 16 16 32 14 20 17 21 27 14
26 | 7 19 8 8 25 3 15 9 9 20 4 | 13 26 21 16 29 13 23 15 17 28 15
27 | 8 16 7 9 17 3 11 5 11 17 3 | 11 26 16 14 27 13 23 11 15 23 13
28 | 6 19 7 7 31 5 16 5 9 27 4 | 16 29 21 21 30 20 27 18 24 18 18
29 | 8 18 8 10 27 6 25 10 12 19 4 | 16 29 23 22 29 20 32 21 31 20 20
30 | 4 12 7 6 34 5 13 11 10 19 3 | 18 23 22 18 20 16 20 25 26 20 18
31 | 8 22 9 17 34 7 17 15 12 21 5 | 19 28 19 18 38 16 26 13 19 14 15
32 | 11 20 13 11 34 6 26 19 8 30 6 | 17 24 28 20 39 19 22 26 14 23 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 9 12 33 5 19 10 10 23 |T 18 28 22 19 34 21 27 19 22 22 19
WRMS | 8 19 9 11 31 5 19 9 9 20 |NE 18 28 22 19 33 21 27 19 22 22 19
MEDI | 8 19 9 10 30 5 20 9 10 19 |MD 15 27 20 18 32 17 26 18 19 20 16
Table 3.1525.2 GPS week: 1525 Day: 2 MJD: 54921.000
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 | 2 --- --- --- --- 61 --- --- --- --- 0 | 95 --- --- --- --- 121 --- --- --- --- 95
2 | 8 17 11 10 46 4 19 7 10 17 4 | 19 31 20 16 45 19 29 18 19 19 18
3 | 8 14 8 9 29 3 10 12 11 16 4 | 21 30 25 19 30 22 27 23 22 30 21
4 | 8 18 12 7 30 5 15 10 8 11 4 | 36 42 38 34 46 39 42 37 37 42 37
X5 | 12 29 10 22 --- 18 --- 15 23 --- 8 | 13 30 13 31 --- 33 --- 23 27 --- 19
6 | 8 14 10 8 27 5 10 12 9 19 4 | 14 29 23 15 29 20 25 19 18 30 17
7 | 9 15 15 14 28 5 20 10 11 13 5 | 12 24 17 14 38 16 23 15 20 14 13
8 | 9 18 12 10 18 3 10 9 11 9 4 | 9 23 14 13 27 14 17 16 23 16 12
9 | 11 16 14 12 21 4 11 12 11 15 4 | 12 24 17 21 26 14 20 17 23 23 14
10 | 8 13 6 9 28 5 9 6 13 21 4 | 15 19 23 19 25 21 20 15 23 21 16
11E | 10 29 17 20 45 7 20 12 13 16 6 | 17 44 23 32 49 23 28 24 22 26 22
12 | 9 13 14 11 46 5 19 11 14 29 5 | 13 26 22 18 37 17 26 17 23 19 16
13 | 8 16 13 12 60 4 19 8 14 9 4 | 14 28 21 15 41 17 25 18 19 15 15
14 | 10 22 11 10 33 6 24 9 13 13 5 | 9 28 17 13 29 14 22 15 16 15 12
15 | 11 24 14 14 23 4 22 9 7 19 5 | 11 26 16 13 33 13 24 17 15 16 12
16 | 7 19 11 16 26 5 20 13 10 26 5 | 16 25 20 17 31 19 28 21 23 19 17
17 | 8 21 17 9 28 4 24 10 11 24 5 | 22 30 14 18 29 24 33 26 22 23 20
18 | 11 19 11 18 53 4 25 12 10 28 6 | 14 28 20 20 31 17 27 13 16 15 16
19 | 6 20 13 12 29 6 18 9 10 16 4 | 18 32 20 18 41 18 28 20 21 21 18
20 | 9 20 11 11 28 7 23 15 12 23 5 | 20 30 29 24 35 21 29 26 22 25 22
21 | 7 17 11 14 33 6 16 10 10 21 4 | 15 25 22 12 39 14 23 15 23 22 15
22 | 9 18 11 11 60 4 24 10 12 21 5 | 22 30 25 26 33 23 28 26 24 23 22
23 | 8 23 11 12 29 5 25 11 13 19 5 | 13 30 20 13 35 16 27 15 18 14 14
24 | 8 14 11 9 21 3 11 11 14 21 4 | 15 24 20 15 28 14 24 12 23 24 15
25 | 11 15 11 13 19 5 11 11 13 23 5 | 12 22 19 17 30 16 20 20 20 27 15
26 | 10 14 11 11 26 4 14 12 10 17 4 | 12 21 13 15 32 12 23 15 18 22 12
27 | 7 18 13 9 20 3 10 10 10 16 4 | 12 25 17 13 31 14 22 12 15 20 13
28 | 9 18 13 11 27 5 19 6 15 28 5 | 19 28 22 23 31 22 26 23 29 20 20
29 | 8 19 12 13 31 7 21 13 21 15 5 | 17 31 20 16 32 21 32 19 31 17 19
30 | 7 10 8 8 25 5 12 9 9 18 3 | 20 25 26 21 30 21 20 25 27 18 22
31 | 9 23 13 22 29 10 18 11 15 20 6 | 13 30 20 20 39 16 26 15 24 17 14
32 | 10 18 11 12 36 7 23 16 14 25 6 | 19 24 23 21 37 23 24 26 19 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 12 12 34 5 18 11 12 20 |T 18 27 20 18 33 22 25 19 22 21 19
WRMS | 9 18 12 12 31 5 18 10 10 19 |NE 18 27 20 18 33 22 25 19 22 20 19
MEDI | 8 18 11 11 28 5 19 11 11 19 |MD 15 28 20 18 32 18 25 18 22 20 16
Table 3.1525.3 GPS week: 1525 Day: 3 MJD: 54922.000
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 | 2 --- --- --- --- 98 --- --- --- --- 0 | 103 --- --- --- --- 130 --- --- --- --- 104
2 | 7 20 15 13 38 4 20 12 11 17 5 | 21 34 26 17 42 21 31 18 17 20 19
3 | 10 16 11 10 29 3 11 15 12 19 4 | 20 32 31 19 34 22 29 21 23 32 20
4 | 8 20 19 7 42 6 13 18 13 10 5 | 42 46 55 42 59 44 49 44 39 45 43
X5 | 14 21 --- 22 --- 15 --- 15 22 --- 9 | 12 28 --- 35 --- 29 --- 19 37 --- 21
6 | 8 14 12 11 31 5 9 13 14 21 4 | 15 29 25 18 30 21 23 17 25 31 17
7 | 5 18 10 16 34 5 18 13 10 14 4 | 13 25 16 18 40 13 23 13 16 15 12
8 | 8 15 9 9 21 4 11 10 12 11 3 | 8 23 16 12 27 15 18 16 18 15 11
9 | 8 22 17 6 18 4 9 17 8 17 5 | 12 29 17 15 26 15 21 18 21 23 14
10 | 5 12 14 12 24 4 10 8 11 19 4 | 13 23 21 25 24 20 20 17 22 16 16
11E | 7 20 14 24 43 5 19 11 10 20 5 | 15 30 19 28 49 19 29 17 19 18 16
12 | 6 16 15 9 49 6 16 11 10 29 4 | 17 28 28 21 39 20 27 19 22 19 18
13 | 6 15 10 10 61 4 17 9 9 11 4 | 14 25 19 13 46 16 24 15 22 17 15
14 | 8 22 17 11 32 4 24 8 11 16 5 | 10 28 20 18 37 17 26 13 19 17 13
15 | 8 23 13 11 29 5 21 11 15 18 5 | 13 29 21 14 38 17 26 15 19 19 15
16 | 8 19 16 13 42 6 23 14 13 29 6 | 18 31 30 22 43 24 33 20 29 26 20
17 | 6 19 18 10 35 5 21 13 12 25 5 | 18 31 24 22 39 24 30 25 28 25 21
X18 | 7 25 17 13 59 7 --- 12 16 30 6 | 11 32 18 17 35 15 --- 13 17 19 13
19 | 5 19 13 11 27 6 20 13 11 18 4 | 19 30 23 15 40 19 31 20 23 23 19
20 | 6 19 12 12 35 5 21 13 8 27 5 | 19 32 24 26 36 24 29 28 24 27 21
21 | 6 21 14 9 39 5 18 13 13 27 5 | 16 29 22 16 42 17 24 16 26 27 15
22 | 6 17 13 11 75 5 18 12 14 23 5 | 23 32 25 29 54 23 29 26 31 23 24
23 | 5 21 10 10 35 5 23 13 10 20 5 | 15 28 18 13 42 17 29 15 21 18 15
24 | 6 15 9 7 21 5 15 12 13 18 4 | 23 33 27 23 31 22 33 20 32 27 23
25 | 9 20 10 10 22 5 10 14 13 22 4 | 14 30 18 17 31 14 24 16 22 29 15
26 | 6 16 11 8 26 3 12 17 13 17 4 | 15 26 20 18 28 17 24 17 19 22 16
27 | 6 15 14 6 17 3 10 12 14 17 4 | 13 26 23 16 25 17 24 13 19 21 15
28 | 6 16 17 9 28 5 19 10 10 28 5 | 21 29 28 24 44 26 29 23 26 24 22
29 | 8 27 13 12 32 8 23 14 11 15 5 | 21 40 25 18 30 23 37 21 28 20 22
30 | 5 13 17 5 46 5 12 12 11 20 4 | 20 26 38 22 20 23 25 26 28 21 22
31 | 6 18 11 16 33 5 22 11 9 19 5 | 14 27 23 21 42 19 27 15 18 17 15
32 | 9 16 14 10 31 4 20 12 10 25 5 | 16 24 25 18 36 20 22 22 20 19 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 14 11 36 5 17 13 12 20 |T 19 29 24 20 36 23 27 19 23 22 20
WRMS | 7 18 14 11 32 5 17 12 10 22 |NE 19 29 24 20 36 24 27 19 23 22 21
MEDI | 6 19 13 10 32 5 18 12 11 19 |MD 15 29 23 18 37 20 27 18 22 21 17
Table 3.1525.4 GPS week: 1525 Day: 4 MJD: 54923.000
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 | 32 --- 21 --- --- 37 --- 25 43 --- 18 | 91 --- 103 --- --- 106 --- 95 110 --- 99
2 | 8 23 7 12 38 7 19 14 8 16 4 | 20 32 23 20 43 21 30 18 24 18 21
3 | 10 13 8 8 22 4 8 11 10 18 4 | 20 29 25 21 30 21 31 21 27 33 23
4 | 8 22 11 8 69 5 11 17 9 10 4 | 22 31 31 23 58 22 35 25 27 29 24
X5 | 17 18 --- 24 --- 15 --- 14 34 --- 11 | 18 34 --- 41 --- 24 --- 19 39 --- 26
6 | 10 13 10 11 30 6 9 12 11 22 4 | 16 27 21 21 31 20 27 20 27 33 19
7 | 10 17 10 15 25 5 20 17 8 13 5 | 16 23 16 17 35 12 28 17 20 14 15
8 | 10 18 6 9 17 4 10 15 10 11 4 | 10 20 11 14 21 11 20 15 21 17 11
9 | 9 15 9 10 22 5 10 15 7 18 4 | 15 28 22 23 31 16 25 21 25 27 19
10 | 5 12 9 9 20 3 10 10 10 20 3 | 14 18 20 20 23 15 20 15 23 14 15
11E | 8 23 12 18 31 6 20 11 8 20 5 | 18 36 26 28 53 23 34 22 30 21 23
12 | 8 15 7 10 56 4 16 10 10 31 4 | 21 30 27 29 41 23 29 23 29 24 24
13 | 7 15 8 11 49 4 18 10 10 9 4 | 13 24 16 15 41 15 27 17 20 18 14
14 | 6 20 9 8 29 3 19 10 6 19 4 | 13 25 17 15 30 12 24 12 24 16 14
15 | 9 21 7 12 31 5 19 10 8 17 4 | 12 26 16 13 33 12 25 13 18 18 14
16 | 6 20 6 11 29 6 19 11 11 28 5 | 18 28 22 22 32 19 31 16 25 20 19
17 | 7 19 14 12 28 5 21 13 9 26 5 | 20 27 20 21 32 20 33 26 28 25 21
X18 | 5 --- 7 --- --- 62 --- --- --- --- 6 | 12 --- 18 --- --- 114 --- --- --- --- 11
19 | 6 20 12 11 31 6 19 13 11 17 4 | 21 29 23 19 40 20 33 21 28 25 22
20 | 9 18 9 12 44 4 19 13 10 24 5 | 14 24 21 24 38 16 27 23 19 24 17
21 | 10 21 8 8 40 4 16 13 11 22 4 | 18 29 21 23 38 19 28 17 27 28 19
22 | 6 17 9 6 77 5 18 13 6 24 4 | 19 27 20 20 49 17 30 20 25 21 19
23 | 7 22 8 12 32 4 24 14 9 18 5 | 13 29 17 16 36 16 30 17 21 17 16
24 | 7 15 9 7 15 6 13 15 8 16 4 | 15 24 23 23 27 16 27 15 22 26 19
25 | 9 17 6 13 14 5 11 18 11 22 4 | 18 25 21 22 28 18 26 25 23 30 19
26 | 6 16 9 9 22 4 13 14 8 14 4 | 12 25 18 18 26 13 24 17 20 21 15
27 | 7 17 8 7 13 3 10 12 11 17 4 | 13 23 17 16 25 12 24 10 16 22 14
28 | 7 15 8 8 35 6 13 9 10 28 4 | 18 24 22 21 29 19 26 21 31 21 21
29 | 9 24 8 12 26 7 22 13 11 17 5 | 22 34 26 22 28 22 33 23 30 23 24
30 | 4 12 7 7 56 5 10 11 9 19 3 | 23 29 28 32 28 24 25 27 31 19 25
31 | 6 22 10 13 34 6 21 10 9 22 5 | 16 29 23 16 40 14 30 13 26 11 17
32 | 9 17 7 13 23 4 17 12 10 25 4 | 14 21 20 21 27 15 21 20 17 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 9 11 36 5 16 13 9 20 |T 18 27 23 21 34 23 27 21 27 21 21
WRMS | 8 18 9 11 35 5 16 12 9 19 |NE 18 26 23 20 33 23 27 21 27 21 21
MEDI | 8 17 8 11 30 5 17 13 10 19 |MD 16 27 21 21 32 18 27 20 25 21 19
Table 3.1525.5 GPS week: 1525 Day: 5 MJD: 54924.000
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 | 13 --- 19 --- --- 18 --- 26 25 --- 11 | 92 --- 82 --- --- 93 --- 74 71 --- 90
2 | 8 22 7 11 31 5 18 15 13 18 5 | 18 30 21 16 36 18 25 16 22 14 17
3 | 11 13 5 9 21 4 9 14 12 26 4 | 18 25 26 20 30 19 27 24 24 39 20
4 | 7 21 7 7 55 7 14 15 11 9 4 | 34 41 37 33 58 36 40 35 37 38 35
X5 | 12 30 --- --- --- 20 --- 15 22 --- 10 | 12 31 --- --- --- 14 --- 20 32 --- 17
6 | 9 12 8 7 26 5 10 15 10 25 4 | 13 21 21 15 27 12 22 18 18 35 15
7 | 8 20 9 21 25 7 20 17 10 13 5 | 12 24 14 22 36 10 22 11 15 13 10
8 | 9 17 6 7 28 5 10 13 11 11 3 | 10 19 13 12 24 10 15 14 18 14 9
9 | 7 17 6 5 26 3 10 14 13 20 4 | 14 24 17 15 29 13 23 16 23 29 15
10 | 7 12 8 8 27 3 10 9 13 23 4 | 13 17 17 19 26 15 19 16 24 14 13
11E | 6 22 8 10 31 4 23 16 16 25 5 | 16 29 20 17 43 18 30 23 24 22 17
12 | 7 17 10 9 43 5 19 12 14 31 5 | 18 27 22 23 31 20 29 20 33 24 21
13 | 6 18 7 9 61 7 19 10 11 12 4 | 13 28 15 10 47 14 23 17 18 18 11
14 | 9 22 6 5 30 5 24 8 14 17 4 | 15 25 17 15 37 14 23 12 24 15 13
15 | 8 24 13 8 29 3 22 10 13 19 5 | 12 27 20 13 34 14 23 13 18 16 12
16 | 7 17 10 8 26 9 19 14 11 29 5 | 17 25 20 20 29 20 27 18 23 19 16
17 | 4 17 11 10 26 5 22 19 8 19 5 | 16 24 17 17 26 15 24 24 22 17 15
X18 | 3 --- --- --- --- 19 --- --- --- --- 0 | 8 --- --- --- --- 23 --- --- --- --- 7
19 | 7 21 10 10 29 4 20 15 13 17 5 | 17 27 22 14 41 14 28 20 14 22 16
20 | 5 22 9 10 38 5 22 14 14 28 5 | 16 29 21 21 42 15 25 21 21 25 16
21 | 8 18 10 10 40 7 13 12 14 23 4 | 17 24 21 16 39 13 22 14 21 24 14
22 | 7 18 8 10 62 6 22 13 13 30 5 | 20 30 15 23 38 18 27 23 26 25 18
23 | 5 23 8 8 27 6 26 15 10 16 5 | 14 31 17 11 35 13 27 17 17 16 13
24 | 7 20 10 5 19 4 13 12 14 16 4 | 20 29 26 20 31 19 29 16 27 28 20
25 | 8 22 10 8 23 5 11 19 10 22 5 | 18 27 21 18 31 15 22 24 21 31 17
26 | 5 14 5 6 20 4 13 15 13 16 3 | 11 22 13 13 27 14 23 14 17 23 12
27 | 5 21 7 5 20 5 10 14 12 16 4 | 12 24 15 14 26 14 21 11 15 19 12
28 | 4 16 8 7 30 7 16 9 13 26 4 | 16 20 12 17 28 15 19 19 24 17 13
29 | 8 21 9 10 28 6 24 14 16 15 5 | 21 30 23 18 32 19 31 20 30 23 20
30 | 6 11 7 7 52 4 12 13 13 19 3 | 21 24 25 24 24 20 22 23 31 20 22
31 | 7 20 8 11 36 6 18 11 20 20 5 | 15 29 18 17 39 15 25 13 24 16 14
32 | 8 17 9 11 29 4 19 10 15 25 5 | 12 20 16 15 29 12 20 13 20 13 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 8 9 34 5 18 14 13 21 |T 18 26 21 17 33 18 24 19 24 21 17
WRMS | 7 19 8 9 30 5 18 13 11 20 |NE 18 26 21 17 33 18 24 19 24 21 17
MEDI | 7 18 8 8 29 5 18 14 13 19 |MD 16 25 20 17 31 15 23 18 23 20 15
Table 3.1525.6 GPS week: 1525 Day: 6 MJD: 54925.000
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 | 18 --- 21 --- --- 20 --- 20 18 --- 11 | 115 --- 66 --- --- 114 --- 64 64 --- 111
2 | 8 22 8 13 38 8 21 19 12 21 5 | 23 36 24 18 45 24 32 21 23 22 22
3 | 6 14 10 7 30 5 11 12 7 20 3 | 18 28 22 17 29 20 28 20 27 36 20
4 | 8 16 8 6 29 6 14 20 9 8 4 | 28 35 33 31 46 33 35 39 32 33 31
X5 | 15 20 --- 19 --- 18 --- 18 10 --- 8 | 16 37 --- 34 --- 27 --- 21 25 --- 21
6 | 8 12 9 7 24 5 8 16 6 27 4 | 15 23 18 15 25 17 22 22 22 38 17
7 | 7 19 12 17 32 7 20 17 8 15 5 | 17 28 20 17 39 16 27 16 22 17 16
8 | 10 16 9 9 20 4 10 22 9 16 4 | 16 24 19 14 24 15 21 21 22 23 15
9 | 9 15 11 7 22 6 12 13 10 19 4 | 16 25 19 14 28 18 25 15 22 24 15
10 | 6 10 10 6 25 6 9 14 6 21 3 | 18 21 24 25 26 21 23 24 26 19 20
11E | 9 18 10 14 45 8 22 9 5 16 4 | 26 38 29 30 60 27 36 24 26 25 26
12 | 8 15 11 8 51 6 15 13 15 33 5 | 21 30 27 23 41 25 31 26 28 23 23
13 | 7 16 9 11 56 8 15 9 7 12 4 | 18 30 25 17 52 19 29 23 24 25 20
14 | 6 20 15 10 26 8 24 10 9 24 5 | 18 26 20 18 34 17 28 20 24 22 17
15 | 10 21 7 12 30 7 19 9 14 21 5 | 17 31 23 16 36 19 28 21 24 24 19
16 | 8 20 8 12 25 6 17 12 9 28 5 | 21 29 24 25 35 21 32 22 25 26 21
17 | 7 20 15 14 29 7 25 17 10 25 5 | 26 29 21 22 37 27 35 36 32 32 25
X18 | 9 22 8 16 35 17 --- 13 10 32 6 | 7 23 3 5 19 15 --- 5 7 4 8
19 | 7 16 13 9 28 8 20 16 9 18 4 | 24 32 22 20 45 24 36 25 29 26 23
20 | 7 22 10 10 32 10 22 14 12 28 5 | 23 31 28 27 38 22 29 29 25 31 23
21 | 7 18 9 15 35 7 12 10 7 23 4 | 17 27 21 19 44 20 26 19 26 26 18
22 | 6 18 14 14 47 11 24 13 12 28 5 | 24 30 28 34 34 22 29 34 26 35 26
23 | 8 24 10 10 34 13 24 10 8 15 5 | 19 37 24 17 39 23 34 21 24 23 21
24 | 8 16 12 8 24 6 14 11 12 23 4 | 17 27 22 17 34 19 27 14 25 32 17
25 | 9 17 10 10 17 7 10 25 10 24 5 | 19 29 24 18 30 21 29 23 23 31 20
26 | 7 14 6 9 25 4 12 11 9 21 4 | 18 29 23 16 31 20 26 20 24 32 19
27 | 6 16 8 8 21 5 10 15 11 18 4 | 19 26 20 16 25 17 25 15 19 26 18
28 | 7 15 13 13 24 7 17 12 13 30 5 | 26 30 26 25 35 25 28 29 34 28 26
29 | 7 20 10 11 27 8 21 13 8 18 4 | 24 34 23 20 40 25 37 26 29 30 24
30 | 6 10 12 7 50 6 8 14 10 19 3 | 26 32 34 29 25 28 28 33 28 25 28
31 | 5 18 10 9 38 10 19 13 9 20 4 | 20 30 19 16 38 18 29 20 26 17 18
32 | 8 16 12 12 30 8 18 10 12 20 4 | 22 27 26 25 40 22 27 22 24 20 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 11 11 33 7 17 14 10 22 |T 22 29 24 20 35 24 29 24 26 25 23
WRMS | 8 17 11 11 28 7 17 12 8 21 |NE 22 29 24 20 34 24 28 24 26 25 23
MEDI | 7 17 10 10 29 7 17 13 9 21 |MD 19 29 23 18 35 21 28 22 25 25 20
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 4.1525 GPS week: 1525 MJD: 54919.0-54925.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 |U 7 6 18 |U 7 8 27 |U 7 6 14 |
emr | emr 2944 | 10 8 23 | 9 10 30 | 7 6 17 |
esa | esa 2934 | 8 7 22 |U 6 8 26 | 6 5 13 |
gfz | gfz 2930 |U 8 7 21 |U 6 8 26 | 8 6 16 |
grg | grg 2852 | 17 19 49 |U 33 44 111 | 22 24 49 |
igr | igr 2957 | 8 8 19 | 7 9 27 | 7 6 17 |
igs | igs 2948 | 7 7 21 | 6 8 26 | 6 5 13 |
jpl | jpl 2824 |U 10 8 24 |U 7 9 26 |U 7 5 18 |
mit | mit 2989 |U 9 8 25 |U 7 10 31 |U 7 6 15 |
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 5.1525.0 GPS week: 1525 Day: 0 MJD: 54919.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3027 | 5 4 16 | 7 8 22 | 9 6 13 |
emr | emr 2974 | 9 6 20 | 8 10 22 | 7 5 16 |
esa | esa 2976 | 5 4 17 | 7 8 23 | 8 6 12 |
gfz | gfz 2976 | 6 3 15 | 7 8 21 | 7 6 12 |
grg | grg 2880 | 18 18 45 | 29 48 133 | 24 21 42 |
igr | igr 2976 | 11 12 26 | 11 11 28 | 12 9 34 |
igs | igs 2976 | 5 4 16 | 7 9 21 | 7 5 11 |
jpl | jpl 2878 | 16 7 26 | 7 9 23 | 9 7 21 |
mit | mit 2976 | 21 14 52 | 7 9 22 | 9 7 13 |
Table 5.1525.1 GPS week: 1525 Day: 1 MJD: 54920.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 | 5 4 15 | 6 8 25 | 6 7 16 |
emr | emr 2957 | 7 6 17 | 9 9 27 | 7 7 14 |
esa | esa 2976 | 6 5 15 | 6 6 22 | 5 6 14 |
gfz | gfz 2969 | 5 5 14 | 6 7 22 | 10 8 16 |
grg | grg 2880 | 15 13 34 | 32 46 96 | 15 25 36 |
igr | igr 2976 | 6 5 14 | 6 7 21 | 5 6 14 |
igs | igs 2976 | 5 5 15 | 5 7 24 | 5 6 14 |
jpl | jpl 2880 | 6 6 16 | 5 7 20 | 7 5 17 |
mit | mit 2976 | 5 4 14 | 6 8 37 | 6 6 16 |
Table 5.1525.2 GPS week: 1525 Day: 2 MJD: 54921.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 6 7 18 | 6 7 31 | 5 6 13 |
emr | emr 2971 | 10 6 23 | 8 10 32 | 8 8 15 |
esa | esa 2976 | 8 8 22 | 6 8 31 | 6 6 13 |
gfz | gfz 2971 | 8 8 23 | 6 9 29 | 6 6 15 |
grg | grg 2880 | 21 19 64 | 31 33 107 | 25 31 58 |
igr | igr 2976 | 8 8 20 | 6 9 29 | 6 6 13 |
igs | igs 2976 | 7 7 20 | 6 8 30 | 6 5 13 |
jpl | jpl 2880 | 9 7 22 | 6 9 26 | 8 6 17 |
mit | mit 2976 | 7 7 20 | 7 9 36 | 7 6 14 |
Table 5.1525.3 GPS week: 1525 Day: 3 MJD: 54922.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 10 7 15 | 8 11 30 | 7 6 13 |
emr | emr 2973 | 12 9 16 | 10 14 33 | 6 6 18 |
esa | esa 2880 | 12 10 19 | 7 10 28 | 6 4 14 |
gfz | gfz 2972 | 9 8 13 | 7 9 26 | 6 5 13 |
grg | grg 2880 | 13 10 37 | 30 66 117 | 25 23 58 |
igr | igr 2976 | 10 8 13 | 6 9 28 | 6 5 14 |
igs | igs 2976 | 10 8 13 | 7 11 30 | 6 4 13 |
jpl | jpl 2784 | 9 8 16 | 8 10 30 | 8 6 20 |
mit | mit 2976 | 8 6 11 | 8 12 32 | 7 6 16 |
Table 5.1525.4 GPS week: 1525 Day: 4 MJD: 54923.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2878 | 14 13 41 | 12 10 35 | 6 5 22 |
esa | esa 2880 | 11 10 35 | 6 8 28 | 6 4 13 |
gfz | gfz 2876 | 11 10 36 | 7 9 28 | 8 7 24 |
grg | grg 2784 | 19 31 56 | 38 39 91 | 26 24 46 |
igs | igs 2880 | 11 10 36 | 6 8 28 | 4 3 14 |
jpl | jpl 2783 | 12 11 43 | 7 9 27 | 6 5 20 |
mit | mit 2976 | 12 10 38 | 8 11 33 | 7 4 16 |
Table 5.1525.5 GPS week: 1525 Day: 5 MJD: 54924.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 6 4 19 | 6 8 27 | 8 8 15 |
emr | emr 2879 | 8 6 22 | 7 9 31 | 8 6 16 |
esa | esa 2880 | 6 5 19 | 5 7 25 | 6 4 13 |
gfz | gfz 2779 | 7 6 22 | 5 7 27 | 10 5 15 |
grg | grg 2784 | 19 30 65 | 37 35 116 | 23 27 55 |
igr | igr 2880 | 6 5 18 | 5 7 27 | 6 5 10 |
igs | igs 2877 | 6 4 19 | 5 7 24 | 6 4 11 |
jpl | jpl 2784 | 7 5 19 | 6 6 25 | 7 5 15 |
mit | mit 2976 | 6 5 17 | 5 8 25 | 7 7 11 |
Table 5.1525.6 GPS week: 1525 Day: 6 MJD: 54925.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 7 10 23 | 10 8 29 | 9 6 16 |
emr | emr 2976 | 10 9 23 | 9 9 33 | 7 7 20 |
esa | esa 2976 | 8 11 27 | 8 8 27 | 7 4 15 |
gfz | gfz 2972 | 7 9 25 | 9 11 29 | 7 4 17 |
grg | grg 2880 | 13 13 41 | 32 39 118 | 17 20 50 |
igr | igr 2976 | 7 8 24 | 8 9 29 | 6 5 17 |
igs | igs 2976 | 7 9 25 | 8 8 28 | 6 5 17 |
jpl | jpl 2784 | 9 10 26 | 8 10 30 | 6 4 16 |
mit | mit 3072 | 7 9 23 | 9 11 33 | 8 7 21 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 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 6.1525 GPS week: 1525 MJD: 54919.500-54925.500
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 | 18 -26 54 74 3 | 0 16
| 25 29 67 58 7 | 5
emr uuuuu | 3 -22 134 176 3 | 57 60
| 22 13 81 115 12 | 9
esa uuuuu | -6 -16 156 -172 0 | 2 21
| 47 18 166 73 12 | 1
gfz uuuuu | -2 -13 -42 30 -2 | 12 20
| 20 11 66 43 7 | 4
grg xxxxx | 14 -41 56 93 6 | -2 40
| 35 29 86 72 47 | 3
igr xxxxx | 62 18 42 -3 -3 | 0 18
| 26 14 110 38 14 | 2
irf xxxxx | 42 6 -61 36 1 | 2 19
| 14 13 51 18 10 | 7
jpl uuuuu | 35 25 -126 -19 6 | 9 22
| 26 23 183 52 6 | 6
mit uuuuu | 16 -20 -179 112 9 | 17 26
| 28 21 150 22 10 | 9
ngs uuuuu | -61 43 10 -140 -7 | 2 13
| 60 37 78 127 8 | 3
sio uuuuu | 116 5 106 229 5 | 39 43
| 18 32 92 56 10 | 9
Table 7.1525.0 GPS week: 1525 Day: 0 MJD: 54919.500
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 | 46 -3 116 138 -2 | -7 14
emr uuuuu | 47 -29 309 358 14 | 44 46
esa uuuuu | -85 -22 -112 -194 -12 | 2 19
gfz uuuuu | 26 6 -36 33 -7 | 7 13
grg xxxxx | 44 -67 131 144 58 | -3 44
igr xxxxx | 56 5 -151 35 -29 | 0 14
irf xxxxx | 26 15 23 47 11 | -8 14
jpl uuuuu | 51 19 -174 -121 -5 | -1 15
mit uuuuu | -15 2 58 92 19 | 4 12
ngs uuuuu | 19 18 11 -24 -7 | -2 10
sio uuuuu | 99 19 201 200 15 | 26 29
Table 7.1525.1 GPS week: 1525 Day: 1 MJD: 54920.500
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 | 27 -25 6 39 -6 | -6 14
emr uuuuu | 5 -3 94 279 12 | 46 49
esa uuuuu | -5 -20 101 -191 -3 | 1 19
gfz uuuuu | -19 -2 -44 30 0 | 6 12
grg xxxxx | -13 -68 -42 128 -37 | 2 48
igr xxxxx | 17 5 -28 -9 -10 | -3 16
irf xxxxx | 30 15 -10 35 9 | -6 14
jpl uuuuu | 42 57 -408 -15 10 | 1 14
mit uuuuu | -8 -7 -11 120 17 | 7 15
ngs uuuuu | -23 -9 23 -145 -14 | -1 10
sio uuuuu | 91 45 153 212 10 | 28 32
Table 7.1525.2 GPS week: 1525 Day: 2 MJD: 54921.500
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 16 15 164 6 | -3 17
emr uuuuu | -21 -12 97 190 14 | 53 58
esa uuuuu | 60 -27 399 -243 -4 | 2 21
gfz uuuuu | -2 -14 -170 12 -1 | 10 20
grg xxxxx | -31 -7 -67 113 -38 | 3 48
igr xxxxx | 83 6 49 -70 3 | -2 17
irf xxxxx | 45 2 -59 33 11 | -1 20
jpl uuuuu | 77 39 -268 47 14 | 6 22
mit uuuuu | 12 -27 -156 145 22 | 13 26
ngs uuuuu | -162 49 30 -233 -11 | 2 13
sio uuuuu | 120 16 88 270 15 | 35 41
Table 7.1525.3 GPS week: 1525 Day: 3 MJD: 54922.500
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 | 3 -42 -44 11 11 | 1 18
emr uuuuu | -12 -17 96 100 7 | 59 64
esa uuuuu | 28 -8 235 -243 4 | 2 21
gfz uuuuu | -11 -18 -66 -11 13 | 13 22
grg xxxxx | -8 -62 145 -29 -7 | -7 40
igr xxxxx | 85 24 176 -13 12 | 0 19
irf xxxxx | 50 20 -91 42 1 | 5 21
jpl uuuuu | 8 17 160 -24 6 | 11 25
mit uuuuu | 25 2 -236 113 9 | 20 31
ngs uuuuu | -91 11 -43 -90 -12 | 3 14
sio uuuuu | 130 27 31 288 11 | 42 47
Table 7.1525.4 GPS week: 1525 Day: 4 MJD: 54923.500
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 | 45 -23 79 42 -3 | 3 18
emr uuuuu | 11 -25 131 101 -9 | 62 66
esa uuuuu | -35 -25 77 -158 -3 | 2 21
gfz uuuuu | 24 -16 -26 92 -9 | 15 23
grg xxxxx | 70 -10 23 170 -21 | -1 32
igr xxxxx | 79 13 90 35 -6 | 1 19
irf xxxxx | 34 5 -115 62 -11 | 7 21
jpl uuuuu | 4 15 -3 6 2 | 13 25
mit uuuuu | -5 -17 -297 131 -3 | 23 32
ngs uuuuu | -27 56 99 -150 6 | 3 14
sio uuuuu | 113 2 24 267 -6 | 45 49
Table 7.1525.5 GPS week: 1525 Day: 5 MJD: 54924.500
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 | -21 -75 56 89 6 | 4 18
emr uuuuu | 3 -41 146 184 -5 | 65 68
esa uuuuu | -21 23 107 -31 -5 | 2 21
gfz uuuuu | -24 -25 19 78 -5 | 16 23
grg xxxxx | 13 -61 81 18 6 | -2 33
igr xxxxx | 77 29 18 24 3 | 1 19
irf xxxxx | 43 1 -107 5 -10 | 9 20
jpl uuuuu | 42 -13 -100 2 7 | 14 26
mit uuuuu | 34 -38 -307 86 -3 | 26 33
ngs uuuuu | -47 88 81 -356 4 | 4 15
sio uuuuu | 113 -20 10 126 -5 | 47 51
Table 7.1525.6 GPS week: 1525 Day: 6 MJD: 54925.500
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 | 3 -32 148 30 11 | 5 18
emr uuuuu | -10 -28 67 20 -13 | 67 69
esa uuuuu | 14 -30 286 -144 25 | 3 21
gfz uuuuu | -7 -20 31 -24 -2 | 16 24
grg xxxxx | 19 -12 119 107 81 | -2 33
igr xxxxx | 38 42 140 -27 5 | 1 19
irf xxxxx | 68 -19 -70 28 -6 | 9 20
jpl uuuuu | 17 41 -88 -33 5 | 15 27
mit uuuuu | 66 -55 -306 96 3 | 28 34
ngs uuuuu | -97 85 -132 17 -14 | 5 16
sio uuuuu | 145 -51 237 238 -6 | 48 51
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