[IGSREPORT-17021] Wk 1512 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jan 15 10:41:10 PST 2009
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IGS Electronic Report 15 Jan 10:41:13 PST 2009 Message Number 17021
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1512 (Dec 28, 2008 - Jan 03, 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:
igs1512[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1512[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1512[0-6].cls IGS GPS clock combination summary report.
igs15127.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15127.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.
Day | Centre | PRN/STA list
----+--------+---------------
0 | EMR | 32
0 | ESA | 10
0 | GFZ | 7 18 29 32 CHUR FAA1
0 | JPL | 32
0 | MIT | CHUR
1 | COD | 10 RCMN
1 | EMR | MIZU
1 | ESA | 10 UNSA
1 | GFZ | 7 18 29 32 BJFS CHUR IRKT
1 | JPL | 32
1 | MIT | 32 CHUR
2 | COD | 5 REUN
2 | EMR | MIZU
2 | ESA | 10 32
2 | GFZ | 7 21 29
2 | JPL | DUBO
2 | MIT | 32
3 | ALL | 10 19
3 | COD | 5 YELL
3 | EMR | 7 NISU
3 | ESA | 32 YELL
3 | GFZ | 7 29 IRKT NISU
3 | JPL | 5
3 | MIT | 25 32
4 | COD | 5 RCMN YELL
4 | EMR | 30 MIZU
4 | ESA | 10 YELL
4 | GFZ | 7 29 32 PETP
4 | JPL | 5 32
4 | MIT | 32 HRAO
5 | COD | 5 10 30 RCMN
5 | EMR | MIZU
5 | ESA | 30
5 | GFZ | 5 7 10 18 29 32 DAEJ IRKT
5 | JPL | 10 30 32 BOGT ZWE2
5 | MIT | 32 KHAJ
6 | COD | 5 10 30
6 | EMR | MIZU
6 | ESA | 5 10 30 32
6 | GFZ | 7 29 30 32 BJFS BOR1 ONSA SUTM
6 | JPL | 32 YELL ZWE2
6 | MIT | 13 32 AUCK BOR1 OUS2 TIXI
5. 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 G32 | | 2 | | | | | |
6. 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.
7. 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 | .0 -.1 1.3 -12 -11 8 .10
EMR | 10.9 1.8 -6.5 109 -5 43 .20
ESA | 6.6 5.7 -6.5 57 -132 25 .12
GFZ | 1.0 .7 1.5 11 -19 5 -.14
GRG | 4.8 .8 -7.0 -26 -6 14 -.16
JPL | 5.1 3.3 15.7 7 -54 4 .35
MIT | 5.0 -.8 -8.9 12 -3 3 .05
NGS | 5.9 -5.7 -4.0 -74 -118 63 .08
SIO | 4.5 6.6 6.9 99 -64 -39 .16
8. 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.
9. 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.
10. 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 1.1512.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1512.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 2.1512.[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 3.1512.[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 5.1512.0-6).
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 1512 summary. (Dec 28, 2008 - Jan 03, 2009)
Table 1.1512.a GPS week: 1512 MJD: 54828.000-54834.000
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 242| 1 0 2 37 -66 -38 -.16 10 9 | -45 -387 18 96
| 0 0 1 11 8 19 .03 | 600 894
emr 79| -1 0 4 -196 -71 -30 .42 19 19 | -3327 1031 21 145
| 2 1 1 33 23 20 .02 | 2785 1528
esa 145| 0 0 -1 -54 87 -18 .29 10 10 | 440 -1077 19 102
| 0 0 1 27 35 31 .02 | 701 1483
gfz 192| 0 0 -4 -5 -59 156 -.12 10 10 | 368 -545 23 126
| 1 0 1 17 19 87 .04 | 473 646
grg 76| 1 -1 2 93 -96 11 1.23 51 52 | -44 -432 117 344
| 3 2 2 36 36 67 .04 | 600 885
igr n/a| 0 0 0 14 -69 -50 .02 7 7 | 14458 1130 24 84
| 0 0 1 12 16 22 .10 | 3396 1587
jpl 133| -1 0 7 1 33 -11 .58 17 16 | -3341 1055 20 101
| 1 1 1 13 17 17 .06 | 2601 1562
mit 287| 0 0 -3 22 -92 -13 -.26 12 10 | 30 -275 24 111
| 0 1 1 14 16 27 .02 | 558 1001
ngs 231| 0 0 1 162 136 -52 -.25 11 9 | -17 -410 2314 3898
| 0 0 0 22 33 20 .05 | 578 860
sio 248| 0 1 1 -189 38 -57 .03 21 19 | --- --- --- ---
| 2 1 1 13 17 41 .05 | --- ---
Table 1.1512.b GPS week : 1512 MJD: 54828.000-54834.000
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 0 0 0 |
2 | 5 5 5 5 5 5 6 |
3 | 4 4 4 5 4 4 5 |
4 | 4 4 5 5 5 5 5 |
5 | 5 6 7 5 5 6 6 |
6 | 4 4 4 4 3 4 4 |
7 | 5 5 5 5 5 5 5 |
8 | 6 4 4 5 4 4 5 |
9 | 4 4 4 5 5 4 4 |
10 | 5 6 6 6 7 5 6 |
11 | 4 4 5 4 4 4 4 |
12 | 5 5 5 5 5 6 6 |
13 | 4 4 4 4 4 4 4 |
14 | 6 5 5 5 5 5 6 |
15 | 5 5 5 6 5 5 6 |
16 | 6 5 6 7 5 6 6 |
17 | 5 5 5 5 5 6 5 |
18 | 4 5 5 5 5 5 5 |
19 | 6 5 5 6 5 5 5 |
20 | 5 5 5 5 5 4 5 |
21 | 5 5 5 5 5 5 5 |
22 | 5 4 5 4 4 4 4 |
23 | 5 5 5 5 5 4 5 |
24 | 3 3 4 4 3 3 3 |
25 | 4 4 4 4 3 3 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 4 4 5 4 4 5 |
28 | 4 5 5 4 4 4 5 |
29 | 4 4 5 5 5 5 5 |
30 | 5 5 5 7 5 5 6 |
31 | 5 4 5 5 5 4 5 |
32 | 6 6 10 8 7 6 6 |
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 2.1512.0 GPS week: 1512 Day: 0 MJD: 54828.000
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 242| 1 0 1 52 -62 -17 -.20 10 9 | -86 -519 26 121
| -9 -3 |
emr 79| -1 0 2 -206 -54 -6 .42 19 19 | -4718 -1449 23 95
| 46 -41 |
esa 145| 0 1 -1 -72 51 42 .28 10 9 | 695 -43 24 105
| 51 26 |
gfz 192| -1 0 -4 5 -46 25 -.13 10 10 | 329 -440 23 114
| 17 -10 |
grg 76| 1 0 0 81 -101 -55 1.21 50 48 | -95 -547 100 366
| -21 -7 |
igr n/a| 0 0 1 28 -86 -33 .07 5 5 | 12246 -1279 24 80
| -15 -16 |
jpl 133| 0 -1 7 -4 27 -35 .61 17 15 | -4481 -1368 22 94
| 38 -49 |
mit 287| 0 0 -3 10 -112 16 -.28 11 10 | 415 -1007 24 104
| -18 2 |
ngs 231| 0 0 2 169 189 -35 -.19 10 8 | -66 -552 2114 3953
| 38 -53 |
sio 248| 0 -1 3 -194 21 -22 -.04 23 20 | --- --- --- ---
| 201 -5 |
Table 2.1512.1 GPS week: 1512 Day: 1 MJD: 54829.000
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 242| 0 0 2 47 -69 -32 -.18 10 9 | -744 625 13 61
| 2 -8 |
emr 79| 2 0 3 -166 -40 -46 .43 18 18 | -6708 1168 23 136
| 24 -60 |
esa 145| 1 0 -2 -87 98 -8 .30 9 9 | -838 -78 17 100
| 58 -7 |
gfz 192| 0 0 -5 -21 -93 134 -.20 10 10 | -408 115 20 126
| 24 10 |
grg 76| 0 0 3 117 -49 -44 1.25 50 48 | -756 591 119 313
| -8 21 |
igr n/a| 0 0 0 30 -92 -66 .02 6 6 | 10504 1306 19 70
| 13 9 |
jpl 133| 0 0 9 7 41 -23 .62 16 15 | -6301 1008 18 96
| 48 -16 |
mit 287| -1 0 -2 12 -104 -9 -.28 10 10 | -675 219 20 88
| -15 -9 |
ngs 231| 0 1 2 190 136 -29 -.20 10 7 | -721 497 2525 4148
| -31 45 |
sio 248| -3 0 3 -208 42 -35 -.02 21 20 | --- --- --- ---
| 209 -8 |
Table 2.1512.2 GPS week: 1512 Day: 2 MJD: 54830.000
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 242| 1 0 0 33 -75 -39 -.15 10 9 | 769 -1585 23 107
| 34 36 |
emr 79| 0 2 6 -168 -70 -52 .42 20 20 | -4854 -566 24 193
| 8 -46 |
esa 145| 2 0 1 -56 112 -36 .29 11 10 | 1195 -3236 22 103
| -1 -41 |
gfz 192| 0 0 -5 -9 -55 277 -.09 12 12 | 1172 -1638 28 121
| 24 -21 |
grg 76| -3 0 5 96 -75 37 1.26 52 48 | 775 -1637 115 299
| 41 70 |
igr n/a| 0 0 0 2 -75 -90 .15 7 7 | 12300 -122 24 79
| 20 -61 |
jpl 133| -2 0 6 -20 20 -8 .67 17 16 | -4731 -770 24 108
| 31 -17 |
mit 287| 0 -1 -2 40 -68 -48 -.28 13 10 | 924 -1784 24 103
| -7 -34 |
ngs 231| 0 1 0 128 96 -38 -.30 11 8 | 715 -1512 2405 3796
| 108 94 |
sio 248| -3 0 2 -191 25 -123 .04 21 19 | --- --- --- ---
| 216 23 |
Table 2.1512.3 GPS week: 1512 Day: 3 MJD: 54831.000
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 242| 1 0 2 22 -51 -77 -.14 12 9 | -360 -86 18 110
| 22 1 |
emr 79| -2 0 3 -160 -57 -37 .44 19 19 | -4905 2930 21 164
| 10 7 |
esa 145| 0 -1 0 -63 98 -46 .28 11 11 | 1136 -2252 21 102
| 7 14 |
gfz 192| 2 0 -5 2 -52 246 -.15 9 9 | 318 -999 25 138
| 25 10 |
grg 76| -1 -1 3 154 -89 133 1.27 54 60 | -354 -137 135 351
| 58 -21 |
igr n/a| 2 -2 -1 19 -70 -43 -.11 9 9 | 12834 3494 31 90
| 26 3 |
jpl 133| -2 0 7 11 49 -21 .58 17 17 | -5159 2886 22 101
| 19 -16 |
mit 287| 0 0 -3 43 -104 -49 -.26 12 10 | -513 832 33 116
| 4 5 |
ngs 231| 0 0 1 168 150 -78 -.29 13 12 | -268 -113 2349 4410
| 81 -22 |
sio 248| 0 1 2 -173 47 -110 .04 20 18 | --- --- --- ---
| 174 -6 |
Table 2.1512.4 GPS week: 1512 Day: 4 MJD: 54832.000
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 242| 1 0 3 45 -68 -30 -.17 9 8 | 804 -1594 19 95
| 15 18 |
emr 79| -3 -2 4 -222 -109 -48 .44 19 19 | -2949 1991 24 164
| 91 15 |
esa 145| 1 -1 0 -7 118 -47 .33 10 9 | 596 -2060 19 103
| -13 -39 |
gfz 192| 0 0 -5 -29 -56 193 -.09 10 10 | 623 -788 23 123
| 43 2 |
grg 76| 4 -8 6 36 -102 44 1.18 52 55 | 797 -1606 122 340
| 40 51 |
igr n/a| 0 0 0 17 -47 -54 -.10 8 8 | 15416 2572 26 83
| 1 -44 |
jpl 133| -1 2 7 19 56 19 .51 16 16 | -3117 2074 20 99
| -2 -60 |
mit 287| 0 1 -3 9 -73 -21 -.27 11 9 | 267 -877 25 108
| 21 -21 |
ngs 231| -1 0 0 162 100 -80 -.24 11 9 | 842 -1632 2437 3663
| 106 84 |
sio 248| 0 2 1 -179 62 -42 .05 19 18 | --- --- --- ---
| 130 7 |
Table 2.1512.5 GPS week: 1512 Day: 5 MJD: 54833.000
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 242| 1 0 5 22 -73 -25 -.12 11 9 | -391 360 14 101
| 27 8 |
emr 79| -2 2 3 -204 -87 -12 .40 18 18 | 140 1876 18 130
| 80 -17 |
esa 145| 0 0 -2 -61 108 -17 .32 10 9 | 95 939 19 102
| 3 -14 |
gfz 192| 1 0 -3 24 -78 110 -.08 10 10 | 213 167 23 142
| 21 30 |
grg 76| 4 0 0 81 -89 0 1.26 51 53 | -372 292 116 418
| 33 97 |
igr n/a| 0 0 0 0 -62 -26 .07 7 6 | 19080 1037 22 117
| -1 -3 |
jpl 133| -2 0 9 -3 32 -12 .58 18 17 | -99 1847 20 110
| -9 -64 |
mit 287| 0 0 -4 28 -84 1 -.22 10 9 | -247 897 23 154
| 12 -5 |
ngs 231| -1 0 1 136 122 -45 -.29 8 7 | -273 303 2130 3508
| 86 79 |
sio 248| 0 1 1 -202 52 -40 .10 20 19 | --- --- --- ---
| 141 -1 |
Table 2.1512.6 GPS week: 1512 Day: 6 MJD: 54834.000
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 242| 0 0 4 35 -62 -43 -.17 10 8 | -311 85 15 79
| 47 -7 |
emr 79| 1 -2 5 -249 -79 -8 .40 19 19 | 699 1267 17 134
| 117 -20 |
esa 145| 0 0 -3 -30 23 -12 .26 10 9 | 203 -810 16 103
| 3 61 |
gfz 192| 0 -1 -1 -10 -36 107 -.11 10 10 | 332 -234 21 124
| 48 -15 |
grg 76| 2 -1 0 84 -169 -39 1.19 52 55 | -307 16 117 326
| 42 47 |
igr n/a| 0 0 2 5 -50 -35 .05 7 6 | 18832 906 22 70
| 26 -48 |
jpl 133| -1 0 6 -2 5 -1 .51 18 18 | 499 1709 20 101
| 39 -43 |
mit 287| 0 2 -5 13 -99 16 -.26 14 13 | 40 -210 20 108
| 39 -24 |
ngs 231| -1 -1 1 180 157 -61 -.23 10 9 | -350 137 2240 3814
| 5 -49 |
sio 248| 2 3 -1 -177 14 -24 .01 22 20 | --- --- --- ---
| 109 33 |
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 3.1512.0 GPS week: 1512 Day: 0 MJD: 54828.000
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 | 6 --- --- --- --- 188 --- --- --- --- 0 | 34 --- --- --- --- 143 --- --- --- --- 36
2 | 10 20 7 7 40 7 16 13 12 26 5 | 28 40 32 27 50 30 38 29 32 31 31
3 | 7 12 11 10 71 3 14 7 10 25 4 | 27 30 30 29 47 27 30 30 33 42 30
4 | 13 12 5 7 39 5 10 7 7 30 4 | 34 28 31 28 30 31 25 29 30 39 30
5 | 13 15 9 9 36 5 16 10 10 31 5 | 125 135 129 132 132 131 134 129 124 135 130
6 | 5 12 11 13 68 3 11 12 9 22 4 | 29 30 28 34 48 28 26 35 36 41 31
7 | 9 22 9 14 29 4 17 10 10 17 4 | 22 34 23 19 41 22 31 23 23 23 22
8 | 25 20 14 11 23 6 16 14 5 18 6 | 22 24 21 17 33 18 24 24 20 23 18
9 | 7 18 8 7 42 4 14 9 8 20 4 | 19 31 23 14 41 19 28 21 20 28 20
10E | 11 22 8 14 50 3 17 12 13 15 5 | 39 52 44 45 45 44 48 46 41 44 43
11 | 6 21 7 7 87 5 14 11 12 19 4 | 37 53 41 34 69 36 47 35 34 38 38
12 | 8 22 8 8 32 4 20 8 6 25 4 | 25 36 30 27 42 28 34 29 29 33 28
13 | 6 20 11 8 28 5 17 9 10 14 4 | 21 38 28 17 49 26 33 20 20 21 21
14 | 11 26 12 8 40 4 21 7 12 25 5 | 20 34 27 21 37 21 31 22 25 23 23
15 | 10 25 11 8 35 6 22 9 11 21 5 | 20 38 26 18 43 26 31 24 24 26 22
16 | 7 23 12 11 36 9 23 9 9 35 5 | 22 36 29 21 46 21 33 19 27 41 24
17 | 9 17 7 17 90 7 17 7 11 19 4 | 26 29 26 27 73 23 28 27 27 23 25
18E | 8 16 7 11 42 5 20 7 10 16 4 | 27 32 29 28 47 26 32 23 31 30 28
19 | 8 18 11 6 60 7 16 21 12 35 5 | 24 29 28 20 44 23 30 22 30 35 24
20E | 9 17 10 12 39 6 16 14 12 19 5 | 16 28 20 21 43 21 27 21 28 28 20
21 | 9 15 10 8 62 5 19 7 10 32 4 | 25 37 33 24 51 27 40 26 28 34 28
22E | 9 15 9 9 36 8 20 9 13 13 4 | 23 33 26 22 50 27 31 23 34 23 26
23 | 8 27 11 9 28 5 20 12 10 12 5 | 22 39 30 17 48 26 32 20 22 21 22
24 | 5 11 4 5 71 5 8 9 9 17 3 | 31 34 33 32 44 32 32 34 34 39 34
25 | 5 14 9 7 29 6 14 14 10 13 4 | 17 25 21 19 31 20 28 24 20 18 19
26 | 8 17 12 4 31 4 10 10 10 14 4 | 19 28 23 16 33 22 25 23 22 22 20
27 | 16 16 12 7 25 5 15 13 6 17 4 | 20 24 21 16 32 19 22 23 21 20 18
28 | 8 20 9 9 32 4 17 6 10 17 4 | 18 28 23 14 38 20 28 20 22 23 19
29 | 7 12 8 6 45 5 14 10 7 30 4 | 25 32 27 23 44 26 31 25 27 24 26
30 | 9 17 7 8 31 3 16 14 8 29 4 | 39 54 48 41 50 46 55 50 47 47 46
31 | 9 16 10 8 32 8 17 12 10 19 4 | 19 30 23 20 37 21 31 24 20 26 22
32E | 14 28 12 12 98 7 16 14 19 23 6 | 104 106 106 107 121 106 104 107 115 108 109
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 10 10 50 5 17 11 10 23 |T 30 39 34 30 49 35 37 32 33 35 32
WRMS | 9 19 9 10 48 5 15 10 8 20 |NE 24 32 27 22 43 29 30 25 25 28 25
MEDI | 8 17 9 8 39 5 16 10 10 19 |MD 24 33 28 22 44 26 31 24 28 28 25
Table 3.1512.1 GPS week: 1512 Day: 1 MJD: 54829.000
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 | 6 --- --- --- --- 103 --- --- --- --- 0 | 59 --- --- --- --- 61 --- --- --- --- 58
2 | 6 17 9 10 43 7 19 11 10 20 4 | 12 24 14 11 36 14 28 15 16 16 14
3 | 9 11 7 8 81 6 10 10 6 24 3 | 24 24 25 27 30 27 23 23 28 36 25
4 | 8 11 8 12 43 8 9 12 8 22 4 | 21 19 20 25 24 21 16 21 24 27 20
5E | 25 18 10 11 35 9 17 10 9 29 6 | 104 120 114 111 122 114 121 110 115 121 112
6 | 8 9 8 9 78 6 10 15 8 18 4 | 24 22 26 28 29 25 19 24 26 30 24
7 | 11 20 7 12 24 4 17 11 10 19 4 | 19 32 19 20 36 19 28 17 19 19 17
8 | 12 16 10 9 17 7 12 11 9 18 4 | 18 23 15 14 28 13 20 19 15 16 12
9 | 7 15 7 7 39 5 13 9 8 15 3 | 11 23 15 12 28 14 22 13 13 18 12
10E | 16 22 8 15 63 6 18 13 15 24 5 | 29 36 29 28 50 27 37 29 35 34 28
11 | 5 20 10 9 75 5 15 8 11 20 4 | 23 41 28 22 45 25 37 22 28 27 25
12 | 8 21 11 8 25 7 21 6 6 20 4 | 21 32 26 26 46 26 29 22 27 30 23
13 | 8 19 9 7 28 3 18 8 7 11 4 | 11 31 19 15 44 14 27 10 12 14 12
14 | 8 24 10 11 38 7 20 8 8 24 5 | 11 27 18 16 36 14 25 9 18 15 13
15 | 9 26 7 9 29 4 21 9 12 24 5 | 10 28 12 14 34 10 23 15 16 16 11
16 | 11 22 8 11 36 5 20 8 10 26 5 | 13 27 17 16 41 14 23 14 18 35 15
17 | 11 15 10 19 88 6 16 9 7 23 5 | 22 23 18 20 49 17 21 23 22 22 17
18E | 9 21 8 13 49 3 19 6 9 15 4 | 18 27 21 22 46 18 28 16 23 21 20
19 | 7 13 8 7 51 3 14 16 14 33 5 | 13 18 15 14 31 14 18 20 20 26 13
20E | 8 17 11 9 26 6 16 17 13 15 5 | 17 26 21 21 33 19 25 22 23 22 17
21 | 9 16 8 7 56 5 17 7 9 30 4 | 16 28 21 14 47 16 30 13 23 21 18
22E | 9 14 9 10 50 5 18 8 9 18 4 | 14 21 17 17 53 15 23 14 24 14 16
23 | 11 24 13 9 28 5 23 11 7 14 5 | 12 32 21 14 39 15 27 11 12 16 12
24 | 5 9 6 7 67 3 9 8 6 14 3 | 16 23 21 18 35 18 20 19 23 26 20
25 | 8 17 8 8 28 4 14 10 9 13 4 | 16 26 21 18 29 16 27 20 17 16 16
26 | 8 14 7 7 26 5 10 10 8 13 3 | 12 16 12 13 21 9 17 13 15 13 10
27 | 11 16 8 9 15 6 12 10 7 17 4 | 17 22 14 14 30 13 18 19 15 14 12
28 | 9 23 11 9 35 5 18 8 11 12 4 | 13 26 17 13 37 12 23 15 17 17 12
29 | 5 16 7 8 44 7 17 9 10 28 4 | 16 25 20 15 44 15 25 15 19 19 17
30 | 9 17 9 7 36 7 19 12 8 24 4 | 38 48 43 41 50 44 52 44 43 48 43
31 | 8 20 10 9 30 8 15 11 8 16 4 | 13 27 18 16 36 17 25 15 18 17 15
32E | 16 26 12 10 106 7 17 12 16 21 5 | 91 97 96 92 98 94 97 95 88 92 91
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 9 10 50 6 16 10 10 21 |T 23 32 25 24 42 24 30 23 26 27 24
WRMS | 9 18 9 10 48 6 15 10 7 20 |NE 17 25 18 16 34 18 23 16 18 20 17
MEDI | 8 17 8 9 38 6 17 10 9 20 |MD 16 26 20 17 36 16 25 19 20 21 17
Table 3.1512.2 GPS week: 1512 Day: 2 MJD: 54830.000
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 | 6 --- --- --- --- 27 --- --- --- --- 0 | 37 --- --- --- --- 43 --- --- --- --- 37
2 | 9 19 7 13 41 7 18 14 10 21 5 | 21 32 23 19 39 25 31 24 27 25 22
3 | 8 14 10 6 95 7 12 10 7 26 4 | 24 28 26 24 54 26 22 25 24 34 24
4 | 12 15 10 12 44 6 10 14 10 23 4 | 28 27 31 29 30 29 25 26 34 32 27
5E | 16 17 13 18 42 6 21 11 13 33 6 | 111 113 109 118 121 108 112 107 112 117 111
6 | 6 13 11 5 103 6 11 14 9 22 4 | 29 29 29 27 63 29 24 31 33 35 29
7 | 8 23 9 13 27 6 17 14 10 21 5 | 22 39 27 25 36 29 33 26 24 24 23
8 | 11 14 6 13 19 5 12 8 8 17 4 | 17 27 23 22 25 22 25 23 24 21 19
9 | 7 20 7 8 42 5 16 8 9 13 4 | 16 30 19 14 37 19 25 18 18 22 17
10E | 14 26 9 15 43 9 19 16 13 28 6 | 24 35 27 24 46 26 28 30 31 37 24
11 | 9 20 11 9 90 7 15 9 11 17 4 | 25 39 26 27 57 29 35 27 29 29 26
12 | 9 21 13 9 23 7 23 7 12 20 5 | 21 36 30 24 47 25 30 24 29 23 24
13 | 8 21 11 8 27 6 17 6 6 13 4 | 19 39 25 21 44 28 32 23 19 21 21
14 | 13 24 11 9 39 6 21 9 7 22 5 | 17 35 24 21 39 22 31 19 25 25 21
15 | 7 24 9 12 30 10 22 9 10 22 5 | 18 32 20 20 40 24 31 23 21 24 19
16 | 6 29 10 7 31 12 19 14 7 37 5 | 23 43 27 21 43 27 30 25 27 43 24
17 | 8 16 12 16 114 7 16 10 10 19 4 | 24 22 20 20 82 22 24 25 28 21 20
18E | 9 21 16 16 52 7 15 8 14 10 5 | 26 38 32 33 51 33 34 29 35 29 31
19 | 7 16 10 7 35 5 14 12 10 27 4 | 19 25 22 19 32 21 22 25 25 28 19
20E | 7 21 13 18 36 5 18 11 10 14 5 | 23 37 30 30 39 27 29 31 29 36 27
21 | 10 20 10 8 56 6 17 8 12 28 5 | 21 35 29 21 52 27 37 23 30 29 25
22E | 10 15 14 18 39 5 18 8 14 14 5 | 17 27 21 23 44 22 26 23 28 23 20
23 | 9 26 9 9 21 6 17 9 9 12 4 | 19 39 26 19 39 28 29 21 23 23 20
24 | 5 13 11 7 61 5 11 7 10 16 3 | 26 31 29 29 33 27 31 28 33 33 29
25 | 6 16 10 10 31 6 12 9 11 9 4 | 17 30 24 22 30 24 29 22 20 18 19
26 | 9 16 7 11 26 7 11 9 12 9 4 | 20 27 24 26 27 26 27 27 22 26 22
27 | 10 16 5 12 17 5 13 8 6 17 4 | 17 28 24 22 24 24 25 24 23 20 19
28 | 10 22 12 12 42 7 16 9 11 12 4 | 17 29 22 17 40 21 25 19 21 22 17
29 | 6 16 11 9 45 8 16 13 16 29 5 | 18 30 22 17 34 22 30 21 25 24 20
30 | 9 14 9 8 21 7 18 14 9 20 4 | 51 59 58 56 60 56 62 53 56 54 55
31 | 7 21 11 8 37 7 19 10 12 16 4 | 17 33 22 17 42 20 30 20 25 25 20
32E | 22 23 16 17 74 16 19 46 26 27 10 | 74 78 75 77 82 75 78 64 74 79 71
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 11 12 52 7 17 13 11 21 |T 26 37 30 28 46 30 33 29 31 32 28
WRMS | 9 20 10 12 48 7 16 10 8 19 |NE 21 31 24 21 40 25 28 23 25 25 22
MEDI | 9 20 10 10 39 6 17 9 10 20 |MD 21 32 26 22 40 26 30 25 27 25 22
Table 3.1512.3 GPS week: 1512 Day: 3 MJD: 54831.000
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 | 6 --- --- --- --- 41 --- --- --- --- 0 | 40 --- --- --- --- 41 --- --- --- --- 41
2 | 9 19 10 9 37 6 18 13 8 20 4 | 22 30 22 23 43 20 34 24 22 26 23
3 | 8 14 12 7 105 7 13 12 12 29 4 | 29 28 25 28 68 27 26 30 31 42 27
4 | 11 14 10 7 42 10 9 16 15 20 4 | 24 26 30 25 23 28 23 24 28 30 25
5E | 16 18 12 8 55 11 17 9 15 22 5 | 73 79 77 70 88 72 77 70 70 77 73
6 | 7 12 12 5 96 7 12 12 9 24 4 | 30 29 22 32 55 27 26 32 34 38 28
7 | 8 24 7 10 28 9 19 7 10 21 4 | 23 35 25 26 41 27 34 24 25 22 24
8 | 9 17 11 10 22 10 12 13 12 18 4 | 15 25 15 19 34 17 23 20 14 17 15
9 | 11 17 8 7 56 11 19 10 18 12 4 | 19 28 20 13 38 11 25 14 17 17 16
10E | 16 20 14 11 37 13 17 16 16 31 6 | 30 37 36 35 47 30 35 38 37 43 34
11 | 7 20 7 8 95 7 15 8 13 20 4 | 33 43 35 32 57 28 37 30 35 29 31
12 | 13 24 10 9 42 9 21 7 14 18 5 | 27 38 35 31 64 31 34 27 32 25 30
13 | 6 20 8 7 37 7 18 6 7 12 4 | 15 29 19 19 48 16 28 15 13 16 16
14 | 10 21 9 7 41 10 20 7 10 18 4 | 20 31 23 15 35 16 28 16 25 17 20
15 | 9 23 13 10 47 10 23 9 15 23 5 | 14 29 17 18 53 18 26 19 23 19 17
16 | 8 34 17 10 50 5 18 13 12 35 6 | 14 36 19 15 45 10 23 15 20 33 14
17 | 11 14 10 14 105 6 16 9 12 21 5 | 22 26 21 24 73 21 26 22 29 22 22
18E | 8 24 11 12 47 5 19 8 8 11 4 | 25 37 23 27 48 26 35 26 29 31 28
19 | 7 17 15 6 34 15 15 14 15 29 5 | 17 21 22 20 41 23 21 19 26 20 16
20E | 8 19 11 10 38 7 18 15 13 17 5 | 21 30 21 26 50 24 28 25 27 32 23
21 | 11 16 9 9 38 7 19 9 9 26 4 | 18 32 25 19 48 17 34 17 23 24 21
22E | 10 17 9 8 39 8 15 8 13 11 4 | 21 29 21 20 46 20 31 22 29 21 23
23 | 11 24 10 7 29 8 19 9 13 10 4 | 15 31 20 17 44 14 27 14 17 16 15
24 | 9 10 7 8 42 6 10 6 10 15 3 | 21 28 28 28 31 25 24 23 31 25 26
25 | 7 13 6 7 31 7 13 10 10 15 3 | 18 21 21 20 27 17 26 20 18 14 18
26 | 11 13 8 7 31 11 10 9 15 13 4 | 16 23 15 17 31 16 21 19 21 16 16
27 | 9 16 10 10 22 9 13 12 10 18 4 | 17 25 16 20 32 19 23 22 18 17 17
28 | 9 21 10 6 60 6 16 8 12 15 4 | 15 26 21 19 50 16 22 16 21 21 17
29 | 8 16 10 8 31 8 18 8 13 28 5 | 22 28 23 24 35 21 29 21 24 20 23
30 | 34 20 9 13 48 13 19 16 13 18 7 | 67 75 68 68 91 62 77 71 64 66 66
31 | 6 24 16 7 29 8 18 8 14 17 5 | 18 35 24 16 38 18 29 18 26 17 20
32E | 20 23 8 13 80 13 25 34 23 21 8 | 66 70 64 66 92 62 71 66 61 70 64
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 19 11 9 54 9 17 12 13 20 |T 25 34 27 26 48 25 32 26 28 28 26
WRMS | 9 19 11 9 60 9 17 10 12 18 |NE 21 28 22 21 42 21 26 20 23 22 21
MEDI | 9 19 10 8 41 8 18 9 13 18 |MD 21 29 22 23 46 21 28 22 26 22 23
Table 3.1512.4 GPS week: 1512 Day: 4 MJD: 54832.000
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 | 6 --- --- --- --- 52 --- --- --- --- 0 | 19 --- --- --- --- 43 --- --- --- --- 19
2 | 9 18 12 8 68 9 18 16 14 20 5 | 15 29 20 16 51 15 29 23 17 18 18
3 | 9 13 7 8 59 9 10 8 10 23 4 | 20 25 25 21 20 17 18 21 25 32 21
4 | 9 12 12 6 44 9 10 20 16 19 5 | 24 24 20 28 28 26 20 29 24 29 23
5E | 13 17 10 10 74 12 15 10 14 26 5 | 74 80 76 76 107 75 78 74 71 81 75
6 | 7 12 6 7 73 7 9 8 7 17 3 | 24 27 27 30 28 25 23 28 30 30 26
7 | 5 20 10 10 28 7 18 8 9 21 4 | 15 30 18 17 39 17 27 17 20 21 16
8 | 9 19 8 7 22 7 12 12 9 16 4 | 14 23 14 12 32 11 19 20 16 19 12
X9 | 8 --- 8 9 37 14 14 9 14 16 4 | 8 --- 14 15 32 14 20 11 16 17 10
10E | 16 32 10 12 41 8 20 19 13 36 7 | 15 39 19 22 46 18 26 25 26 39 21
11 | 7 18 7 9 106 9 16 6 11 16 4 | 21 36 22 25 66 21 32 20 22 22 22
12 | 11 24 13 9 38 9 22 7 7 18 5 | 37 44 45 40 69 39 36 38 34 39 38
13 | 7 20 10 5 31 6 17 9 14 12 4 | 11 31 18 13 43 14 26 10 22 15 13
14 | 8 21 8 8 36 7 20 8 11 20 4 | 13 25 15 15 36 14 27 12 19 13 15
X15 | 9 --- 7 9 27 8 23 7 11 26 5 | 9 --- 16 15 39 13 23 13 17 22 12
16 | 9 26 9 10 31 11 21 11 9 24 5 | 19 31 20 20 32 22 28 18 21 29 18
17 | 8 15 11 20 79 7 14 9 12 22 5 | 24 22 17 20 59 16 23 27 21 20 18
18E | 9 26 10 15 56 8 19 8 11 16 5 | 25 38 27 28 43 26 33 26 34 27 26
19 | 8 16 7 6 39 9 17 9 12 27 4 | 15 22 18 18 27 20 20 19 23 21 15
20E | 7 20 10 14 50 6 14 13 13 13 4 | 19 28 20 20 54 20 27 26 29 24 20
21 | 9 17 7 7 52 9 18 8 12 26 4 | 17 30 18 15 50 18 30 18 20 18 17
22E | 8 16 10 6 42 8 15 9 8 12 4 | 17 27 19 18 51 20 26 19 24 20 19
23 | 8 25 10 8 28 8 21 9 10 11 4 | 11 32 20 12 41 12 24 12 21 14 12
24 | 4 11 6 7 49 7 7 7 10 9 2 | 17 20 20 23 24 21 20 19 23 21 20
25 | 6 14 8 4 27 6 14 9 8 10 3 | 10 19 16 14 28 13 23 14 16 12 12
26 | 8 15 10 7 20 6 9 8 9 11 3 | 11 20 13 15 31 9 17 13 16 16 10
27 | 9 17 8 7 21 8 12 12 6 17 4 | 13 21 13 12 26 12 17 21 15 18 12
28 | 7 22 8 7 69 8 12 7 9 11 3 | 13 25 15 15 49 14 20 17 15 18 12
29 | 5 15 10 7 59 8 17 12 10 28 4 | 14 24 17 14 53 18 25 18 14 18 15
30E | 16 23 9 13 65 12 18 11 9 19 5 | 65 67 63 62 96 60 67 61 63 59 61
31 | 5 19 11 15 32 5 18 7 13 14 4 | 15 27 16 21 37 18 25 17 25 18 16
32E | 15 21 13 11 66 12 21 24 16 15 6 | 57 65 65 61 75 62 67 68 67 70 62
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 10 10 52 8 16 11 11 19 |T 21 32 24 23 45 23 28 24 26 26 22
WRMS | 8 19 9 10 55 8 16 9 9 18 |NE 15 25 17 17 38 17 23 18 19 19 15
MEDI | 8 18 10 8 42 8 17 9 11 17 |MD 15 27 19 18 41 18 25 19 22 21 18
Table 3.1512.5 GPS week: 1512 Day: 5 MJD: 54833.000
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 | 6 --- --- --- --- 42 --- --- --- --- 0 | 30 --- --- --- --- 53 --- --- --- --- 32
2 | 8 19 9 7 46 7 19 15 9 21 4 | 16 27 20 16 38 20 30 22 22 14 18
3 | 10 13 8 7 61 4 11 8 8 23 3 | 23 27 21 25 30 24 22 26 27 36 24
4 | 14 13 9 8 43 9 11 15 11 20 4 | 17 17 18 19 26 17 14 27 27 28 18
5E | 13 17 11 13 45 6 19 14 9 31 5 | 54 64 64 61 77 57 69 57 60 53 58
6 | 8 9 7 6 62 5 11 8 9 20 3 | 22 24 21 27 22 23 20 26 26 26 23
7 | 7 20 8 12 27 4 16 8 8 22 4 | 22 34 23 26 44 25 32 24 22 24 23
8 | 8 15 6 8 17 4 13 9 8 15 3 | 18 24 19 18 29 19 25 24 18 24 18
9 | 12 17 8 8 51 6 15 10 10 16 4 | 9 25 15 13 31 12 19 13 14 17 10
10E | 17 19 11 10 41 9 20 10 9 17 5 | 31 37 36 33 45 32 34 31 33 34 31
11 | 7 18 7 7 127 6 16 7 9 16 3 | 18 33 24 21 78 20 31 19 21 21 20
12 | 21 22 12 10 40 7 23 13 7 19 5 | 50 62 60 63 82 52 62 59 55 48 54
13 | 7 19 8 7 31 6 16 5 8 13 3 | 13 28 19 18 45 18 28 14 15 15 15
14 | 8 33 11 8 40 7 18 10 5 19 5 | 13 39 19 15 36 17 23 18 23 15 18
15 | 8 19 14 9 35 7 24 10 9 29 5 | 7 22 17 9 39 9 23 10 15 17 9
16 | 14 29 9 10 42 7 26 10 7 19 5 | 26 41 28 28 44 26 35 24 29 28 26
17 | 11 17 15 24 65 8 23 8 11 26 6 | 17 22 22 22 33 15 27 19 18 23 14
18E | 12 23 12 10 51 5 20 7 10 18 5 | 28 38 28 29 39 28 33 28 32 32 28
19 | 7 13 9 8 55 6 15 9 6 32 4 | 11 18 17 16 31 13 18 15 15 18 12
20E | 9 15 7 10 32 6 17 6 9 15 4 | 21 26 21 22 41 21 28 23 28 26 20
21 | 9 16 8 7 69 6 18 9 8 29 4 | 16 29 21 18 51 18 32 17 19 20 17
22E | 10 17 12 12 36 6 16 8 5 9 4 | 16 26 19 21 45 20 25 20 26 21 19
23 | 8 23 9 7 27 7 18 5 7 12 4 | 12 29 19 16 41 17 26 14 16 13 14
24 | 6 10 5 6 60 5 11 6 6 8 2 | 17 21 19 17 26 17 20 18 20 23 18
25 | 7 12 7 7 36 5 14 10 5 12 3 | 15 23 19 19 30 17 27 20 16 16 16
26 | 9 15 9 11 41 9 12 8 7 12 3 | 13 20 14 15 30 13 21 13 16 14 11
27 | 9 14 8 7 14 4 13 11 7 16 3 | 18 22 18 17 32 19 23 25 18 24 18
28 | 8 19 11 8 36 6 19 8 7 12 4 | 15 26 18 13 43 16 23 17 16 19 15
29 | 8 16 11 7 56 8 20 15 9 29 5 | 18 27 21 21 45 19 29 21 22 19 20
30E | 17 19 11 11 57 6 20 10 9 20 5 | 55 62 59 51 39 57 60 54 53 57 56
31 | 8 19 10 5 35 6 19 7 10 15 4 | 14 29 20 19 41 18 27 18 21 15 18
32E | 15 22 8 9 66 9 20 14 14 21 5 | 64 71 71 69 87 71 73 67 68 72 67
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 10 10 51 7 18 10 8 20 |T 22 32 26 25 42 25 30 25 26 26 23
WRMS | 9 18 9 10 53 6 17 9 7 19 |NE 16 25 19 18 37 19 24 19 19 20 17
MEDI | 8 17 9 8 42 6 18 9 8 19 |MD 17 27 20 19 39 19 27 21 22 23 18
Table 3.1512.6 GPS week: 1512 Day: 6 MJD: 54834.000
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 | 6 --- --- --- --- 19 --- --- --- --- 0 | 44 --- --- --- --- 40 --- --- --- --- 46
2 | 7 21 14 9 54 9 18 21 11 20 5 | 22 34 22 20 50 24 31 32 23 24 23
3 | 12 14 6 7 64 6 16 15 11 26 4 | 23 27 25 27 42 23 22 28 27 37 25
4 | 9 13 9 7 39 7 11 24 10 20 4 | 31 30 35 32 38 32 28 35 34 37 33
5E | 13 17 10 8 59 7 19 16 8 32 5 | 50 56 57 52 67 55 58 50 55 62 54
6 | 8 13 5 6 58 7 16 12 9 24 4 | 29 32 31 35 41 30 30 33 39 36 32
7 | 6 18 8 13 25 7 16 15 12 24 5 | 21 30 22 20 45 23 29 22 24 24 20
8 | 7 17 8 6 24 5 15 16 12 18 4 | 19 23 21 19 33 17 22 21 19 21 17
9 | 8 15 9 5 40 5 13 14 10 23 4 | 15 25 18 15 33 17 19 18 20 25 18
10E | 17 23 12 14 60 10 24 20 12 19 6 | 40 47 42 45 56 43 49 50 43 45 40
11 | 7 20 8 6 113 5 16 10 7 16 4 | 27 37 27 30 78 27 33 30 24 28 27
12E | 12 20 9 18 32 7 22 13 6 19 5 | 31 40 46 48 48 39 36 39 39 44 40
13 | 6 17 8 7 44 6 14 13 11 15 4 | 18 30 20 19 53 19 27 16 21 18 18
14 | 9 26 15 11 44 5 19 13 8 18 5 | 19 31 25 24 40 19 22 21 17 21 22
15 | 7 26 14 10 45 9 27 11 14 29 6 | 15 30 19 15 41 18 27 16 24 25 18
16E | 10 26 10 11 48 7 23 17 10 28 6 | 29 38 34 40 52 31 38 37 32 33 33
17 | 10 19 9 14 75 6 18 8 10 28 5 | 30 32 27 31 67 26 32 27 25 27 27
18E | 9 24 8 15 48 6 21 10 8 16 5 | 32 44 32 28 49 29 41 30 30 35 33
19 | 8 17 7 10 45 7 17 12 12 33 5 | 19 25 20 20 36 19 24 21 22 30 19
20E | 9 18 5 17 52 5 17 12 11 18 5 | 27 38 29 33 56 28 37 30 34 33 30
21 | 9 18 8 7 60 6 19 8 9 34 5 | 27 36 26 21 63 26 39 23 25 29 26
22E | 8 18 10 7 37 5 16 14 10 9 4 | 20 31 21 19 43 22 30 23 24 24 22
23 | 9 24 8 10 35 5 15 14 11 13 4 | 17 29 19 17 44 18 22 16 20 17 17
24 | 6 11 5 5 57 4 11 10 7 11 3 | 26 25 34 27 35 28 28 31 30 33 31
25 | 7 12 6 6 37 6 13 15 12 10 3 | 14 20 18 14 28 15 22 16 19 16 15
26 | 9 13 11 7 37 6 12 10 12 18 4 | 17 20 17 16 29 17 21 17 20 25 17
27 | 7 17 7 6 26 4 15 18 12 23 4 | 20 24 20 18 32 19 20 22 22 22 18
28 | 16 17 8 8 51 6 17 10 13 13 4 | 26 27 21 24 44 21 26 23 20 24 20
29 | 6 17 10 6 41 9 20 21 6 29 5 | 22 27 29 21 47 21 31 28 25 24 25
30E | 17 21 14 9 78 9 21 16 10 30 6 | 84 82 90 84 109 80 88 89 81 71 82
31 | 8 22 11 8 33 8 19 9 10 10 4 | 20 28 24 20 49 22 29 23 22 21 22
32E | 16 24 10 10 67 10 17 16 12 26 5 | 80 84 80 82 86 78 81 82 76 90 81
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 10 10 52 7 18 14 10 22 |T 28 34 30 29 49 28 33 30 30 32 29
WRMS | 8 19 9 10 55 6 18 13 9 20 |NE 22 28 23 22 44 22 26 23 23 25 23
MEDI | 8 18 9 8 45 6 17 14 10 20 |MD 23 30 25 24 45 23 29 27 24 27 25
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 4.1512 GPS week: 1512 MJD: 54828.0-54834.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 |U 7 8 16 |U 9 13 31 |U 13 10 23 |
emr | emr 2936 | 14 12 32 | 15 17 44 | 13 11 25 |
esa | esa 2976 | 7 8 17 | 10 12 33 | 14 11 24 |
gfz | gfz 2951 |U 12 10 24 | 13 16 45 | 15 11 28 |
igr | igr 2906 | 9 8 21 | 11 14 36 | 13 10 25 |
igs | igs 2913 | 12 10 22 | 12 14 38 | 12 10 27 |
jpl | jpl 2963 |U 13 10 28 | 12 16 37 | 13 11 29 |
mit | mit 2976 |U 10 9 23 | 12 17 42 |U 17 9 36 |
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 5.1512.0 GPS week: 1512 Day: 0 MJD: 54828.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 5 6 16 | ---- ---- ---- | 13 12 26 |
emr | emr 2968 | 15 11 22 | ---- ---- ---- | 12 12 26 |
esa | esa 2976 | 6 8 18 | ---- ---- ---- | 14 12 26 |
gfz | gfz 2958 | 12 11 24 | ---- ---- ---- | 14 12 30 |
igr | igr 2958 | 6 8 17 | ---- ---- ---- | 13 11 26 |
igs | igs 2954 | 13 11 18 | ---- ---- ---- | 12 11 25 |
jpl | jpl 2967 | 12 10 24 | ---- ---- ---- | 12 13 30 |
mit | mit 2976 | 11 10 18 | ---- ---- ---- | 39 11 76 |
Table 5.1512.1 GPS week: 1512 Day: 1 MJD: 54829.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 5 8 15 | 7 8 22 | 13 11 24 |
emr | emr 2968 | 11 8 22 | 10 12 33 | 12 10 27 |
esa | esa 2976 | 6 8 16 | 7 9 27 | 14 11 23 |
gfz | gfz 2957 | 11 11 28 | 12 12 46 | 14 11 30 |
igr | igr 2968 | 6 9 21 | 9 11 27 | 12 9 22 |
igs | igs 2960 | 10 9 22 | 8 10 25 | 12 10 23 |
jpl | jpl 2968 | 10 9 22 | 10 12 28 | 13 15 31 |
mit | mit 2976 | 10 9 19 | 11 15 34 | 12 11 32 |
Table 5.1512.2 GPS week: 1512 Day: 2 MJD: 54830.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 12 12 17 | 11 13 32 | 14 11 26 |
emr | emr 2966 | 19 13 24 | 14 13 39 | 13 11 28 |
esa | esa 2976 | 11 11 15 | 12 12 32 | 13 10 26 |
gfz | gfz 2954 | 16 10 18 | 12 13 45 | 16 11 31 |
igr | igr 2965 | 15 9 18 | 12 12 35 | 12 9 27 |
igs | igs 2955 | 13 13 15 | 13 11 38 | 12 10 35 |
jpl | jpl 2964 | 16 11 20 | 13 12 41 | 12 10 26 |
mit | mit 2976 | 12 12 16 | 15 15 46 | 19 11 43 |
Table 5.1512.3 GPS week: 1512 Day: 3 MJD: 54831.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 7 8 17 | 15 26 58 | 14 9 24 |
emr | emr 2964 | 10 8 27 | 18 27 62 | 11 8 24 |
esa | esa 2976 | 8 10 17 | 14 24 50 | 15 11 26 |
gfz | gfz 2955 | 9 9 19 | 18 26 65 | 18 12 28 |
igr | igr 2816 | 8 8 19 | 16 25 57 | 15 12 33 |
igs | igs 2761 | 8 10 19 | 16 23 64 | 15 10 43 |
jpl | jpl 2964 | 8 9 27 | 20 28 58 | 12 9 32 |
mit | mit 2976 | 7 8 24 | 18 22 74 | 16 9 28 |
Table 5.1512.4 GPS week: 1512 Day: 4 MJD: 54832.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 6 18 | 9 9 25 | 14 9 21 |
emr | emr 2772 | 18 22 60 | 17 24 44 | 14 14 24 |
esa | esa 2976 | 8 7 17 | 10 8 31 | 15 11 21 |
gfz | gfz 2945 | 13 10 24 | 13 24 38 | 14 9 25 |
igr | igr 2759 | 8 9 25 | 12 12 38 | 13 11 25 |
igs | igs 2950 | 12 8 23 | 12 19 30 | 12 10 21 |
jpl | jpl 2964 | 14 7 24 | 12 16 28 | 14 9 21 |
mit | mit 2976 | 10 12 31 | 11 20 29 | 13 8 19 |
Table 5.1512.5 GPS week: 1512 Day: 5 MJD: 54833.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 | 5 6 12 | 6 7 21 | 13 10 21 |
emr | emr 2960 | 14 9 35 | 14 8 43 | 14 10 23 |
esa | esa 2976 | 7 5 15 | 8 8 26 | 13 11 19 |
gfz | gfz 2949 | 8 6 16 | 14 5 33 | 15 12 26 |
igr | igr 2918 | 5 4 15 | 7 8 21 | 13 10 19 |
igs | igs 2895 | 13 9 29 | 10 8 33 | 11 9 21 |
jpl | jpl 2959 | 13 9 34 | 6 10 31 | 14 12 31 |
mit | mit 2976 | 10 6 24 | 7 11 27 | 13 10 25 |
Table 5.1512.6 GPS week: 1512 Day: 6 MJD: 54834.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 5 7 15 | ---- ---- ---- | 12 9 22 |
emr | emr 2960 | 15 12 35 | ---- ---- ---- | 13 9 25 |
esa | esa 2976 | 6 6 19 | ---- ---- ---- | 12 10 24 |
gfz | gfz 2945 | 13 13 37 | ---- ---- ---- | 12 10 30 |
igr | igr 2964 | 14 11 32 | ---- ---- ---- | 11 8 25 |
igs | igs 2921 | 13 11 32 | ---- ---- ---- | 11 9 24 |
jpl | jpl 2959 | 14 13 42 | ---- ---- ---- | 12 7 30 |
mit | mit 2976 | 7 9 31 | ---- ---- ---- | 11 7 28 |
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 6.1512 GPS week: 1512 MJD: 54828.500-54834.500
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 | -9 17 15 -31 -5 | 1 21
| 17 17 67 70 10 | 4
emr uuuuu | 21 -17 -127 -6 -4 | 43 47
| 27 41 172 74 13 | 4
esa uuuuu | -2 21 207 71 17 | -10 31
| 40 32 136 116 19 | 9
gfz uuuuu | -3 8 28 -11 7 | -17 28
| 12 11 57 54 4 | 4
grg xxxxx | -39 10 1 -59 -2 | 2 35
| 39 27 116 109 31 | 2
igr xxxxx | 21 27 64 -3 16 | 1 25
| 25 17 132 63 16 | 9
irf xxxxx | -2 37 -8 14 3 | 2 20
| 8 6 27 45 4 | 3
jpl uuuuu | 36 13 85 -4 -7 | 20 33
| 24 26 161 78 25 | 6
mit uuuuu | 10 32 -216 6 -2 | -1 19
| 15 18 39 92 9 | 3
ngs uuuuu | -28 -19 -9 -57 -8 | 2 22
| 61 49 88 163 12 | 4
sio uuxxu | -8 -132 6 -9 -4 | 6 19
| 20 45 75 51 11 | 3
Table 7.1512.0 GPS week: 1512 Day: 0 MJD: 54828.500
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 44 -68 6 -2 | -6 21
emr uuuuu | 26 -11 -198 -73 -2 | 36 40
esa uuuuu | -41 -16 262 -96 9 | -23 31
gfz uuuuu | -5 18 2 -21 6 | -24 30
grg xxxxx | -8 56 -24 -7 -60 | 2 38
igr xxxxx | 1 50 -10 34 6 | -14 22
irf xxxxx | -15 35 -12 16 -4 | -3 19
jpl uuuuu | 34 -3 -12 97 19 | 9 24
mit uuuuu | -17 53 -240 -48 -12 | -3 20
ngs uuuuu | 38 -3 77 162 11 | -4 18
sio uuxxu | -10 -166 -118 -26 -19 | 3 19
Table 7.1512.1 GPS week: 1512 Day: 1 MJD: 54829.500
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 | 8 24 57 -49 8 | -2 23
emr uuuuu | 60 2 -162 26 9 | 40 45
esa uuuuu | 7 -32 238 -62 38 | -19 31
gfz uuuuu | -10 2 76 107 0 | -20 29
grg xxxxx | -21 34 -170 50 -4 | -1 39
igr xxxxx | -9 13 7 0 19 | -8 22
irf xxxxx | 0 26 -3 -16 -1 | 1 21
jpl uuuuu | 16 -22 -50 41 18 | 18 30
mit uuuuu | 9 41 -241 -111 -12 | 0 20
ngs uuuuu | -45 57 17 47 2 | 2 22
sio uuxxu | 8 -183 39 15 -17 | 6 20
Table 7.1512.2 GPS week: 1512 Day: 2 MJD: 54830.500
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 | -41 7 -69 53 6 | 4 23
emr uuuuu | 41 33 -328 49 8 | 46 51
esa uuuuu | 36 42 288 175 38 | -11 32
gfz uuuuu | 16 17 -32 -48 13 | -16 28
grg xxxxx | -75 0 72 -193 20 | 0 39
igr xxxxx | 56 21 139 -21 42 | -1 23
irf xxxxx | -5 41 11 -58 3 | 5 22
jpl uuuuu | 12 10 81 -85 19 | 24 36
mit uuuuu | 29 48 -228 -80 -7 | 3 20
ngs uuuuu | -99 -67 102 -7 -21 | 7 22
sio uuxxu | -28 -175 -59 6 -6 | 9 20
Table 7.1512.3 GPS week: 1512 Day: 3 MJD: 54831.500
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 | 0 12 112 -138 -9 | 7 22
emr uuuuu | -6 24 -294 -130 9 | 48 52
esa uuuuu | -13 27 258 69 30 | -5 31
gfz uuuuu | -9 9 59 -22 7 | -14 26
grg xxxxx | 22 -24 56 20 25 | 7 37
igr xxxxx | -2 8 -154 12 32 | 5 25
irf xxxxx | 1 34 24 32 6 | 6 22
jpl uuuuu | 17 15 119 -31 -14 | 28 38
mit uuuuu | -4 30 -141 53 -1 | 2 20
ngs uuuuu | 23 -47 -149 -31 -11 | 7 22
sio uuxxu | 7 -140 111 -59 -5 | 10 20
Table 7.1512.4 GPS week: 1512 Day: 4 MJD: 54832.500
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 29 15 35 -9 | 2 20
emr uuuuu | -17 -47 165 16 -21 | 45 49
esa uuuuu | 37 57 254 92 18 | -6 30
gfz uuuuu | -4 1 39 -28 8 | -17 27
grg xxxxx | -53 4 -104 -110 27 | 1 30
igr xxxxx | 42 43 73 -134 9 | 6 25
irf xxxxx | -2 44 -8 21 8 | 2 19
jpl uuuuu | 58 46 -86 86 -34 | 24 36
mit uuuuu | 19 23 -212 57 9 | -3 18
ngs uuuuu | -86 -62 -91 -212 -18 | 4 23
sio uuxxu | -9 -86 3 24 4 | 5 18
Table 7.1512.5 GPS week: 1512 Day: 5 MJD: 54833.500
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 | 4 12 3 -102 -9 | 1 19
emr uuuuu | 29 -41 -68 -19 -16 | 43 47
esa uuuuu | 26 36 251 97 4 | -3 31
gfz uuuuu | -18 18 -52 -55 8 | -15 27
grg xxxxx | -85 6 -6 32 4 | 2 32
igr xxxxx | 15 40 137 25 9 | 9 27
irf xxxxx | 12 39 -4 18 6 | 3 20
jpl uuuuu | 76 48 149 -43 -27 | 20 34
mit uuuuu | 17 27 -192 17 6 | -3 18
ngs uuuuu | -67 -47 -11 -30 -15 | 1 22
sio uuxxu | 13 -102 8 -87 8 | 4 17
Table 7.1512.6 GPS week: 1512 Day: 6 MJD: 54834.500
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 | 0 -9 56 -23 -19 | 0 19
emr uuuuu | 13 -79 -4 86 -15 | 41 45
esa uuuuu | -68 35 -100 224 -14 | -1 31
gfz uuuuu | 8 -10 101 -13 6 | -15 27
grg xxxxx | -54 -4 181 -207 -24 | 3 32
igr xxxxx | 41 12 256 62 -6 | 11 28
irf xxxxx | -7 38 -64 88 1 | 3 20
jpl uuuuu | 36 -1 392 -91 -32 | 18 33
mit uuuuu | 17 -1 -257 155 5 | -3 18
ngs uuuuu | 42 33 -7 -326 -3 | -1 21
sio uuxxu | -40 -71 55 63 8 | 4 16
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