[IGSREPORT-16893] Wk 1506 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 4 04:52:16 PST 2008
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IGS Electronic Report 04 Dec 04:52:19 PST 2008 Message Number 16893
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1506 (Nov 16, 2008 - Nov 22, 2008)
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:
igs1506[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1506[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1506[0-6].cls IGS GPS clock combination summary report.
igs15067.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15067.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 | MIZU THU3
0 | ESA | 6 9 27 CHUR MKEA
0 | GFZ | 7 24
0 | JPL | 9 27
1 | COD | 9 27
1 | EMR | MIZU NRC1
1 | ESA | 4 9 25 27 DAEJ NRC1
1 | GFZ | 7 9 EIL1
1 | JPL | ZWE2
1 | MIT | KHAJ SYDN
2 | COD | 9 27
2 | EMR | HARB
2 | ESA | 8 9 25 27 ONSA SCUB
2 | GFZ | 7 9
2 | JPL | MCM4
3 | COD | 9 MCM4 NRIL
3 | EMR | MCM4 MIZU
3 | ESA | 8 9 25
3 | GFZ | 7 9
3 | MIT | 18 20 21 25 27 PTBB QUIN
4 | ALL | 27
4 | COD | 9 YELL
4 | EMR | MIZU
4 | ESA | 4 8 9
4 | GFZ | 7 9 13 ALGO HARB HOLM
4 | JPL | 25
4 | MIT | 13 ALIC
5 | COD | 9
5 | EMR | MIZU
5 | ESA | 9 QUIN
5 | GFZ | 7 9 13 29 AREQ
5 | JPL | 8 25 MCM4
5 | MIT | ALIC DARW SYDN
6 | COD | 9 DARW
6 | EMR | KERG MIZU
6 | ESA | 8 9 21 27
6 | GFZ | 7 9 21 NTUS
6 | JPL | 27 ZWE2
6 | MIT | ALIC DARW NTUS
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
----+------------+----------
G27 | 2008_11_20 | 2008140
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 G24 | 2 | | | | | | |
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 | .2 .6 .4 -7 -13 -4 .16
EMR | 6.9 -2.8 12.0 83 -9 45 .30
ESA | 3.0 4.5 4.4 37 -51 38 .13
GFZ | 1.0 .8 1.6 21 -37 15 -.14
GRG | 6.9 .3 1.1 -13 -70 43 -.02
JPL | 4.3 5.2 11.7 -1 -30 13 .26
MIT | 3.5 .2 6.7 -10 -1 9 .10
NGS | 9.4 -4.4 .7 -49 -145 58 .23
SIO | 4.7 2.2 2.8 54 -48 4 .22
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 1.1506.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1506.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 2.1506.[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 3.1506.[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 5.1506.0-6).
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 1506 summary. (Nov 16, 2008 - Nov 22, 2008)
Table 1.1506.a GPS week: 1506 MJD: 54786.000-54792.000
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 243| 0 0 0 23 -67 -36 -.21 11 10 | -283 93 28 124
| 0 0 1 14 10 8 .02 | 333 1008
emr 84| -3 0 3 -157 -84 -25 .45 17 17 | 633 560 22 198
| 1 3 1 27 40 16 .05 | 2325 1499
esa 128| 1 -1 0 -33 8 11 .25 11 11 | -754 365 23 117
| 0 1 1 15 21 11 .02 | 723 1081
gfz 200| 0 1 1 -27 -17 178 -.00 16 16 | 132 -70 24 131
| 0 0 1 35 9 54 .05 | 184 510
grg 84| 4 0 9 25 46 -33 1.14 48 45 | -271 23 111 348
| 1 1 2 27 17 82 .04 | 334 1002
igr n/a| 0 0 0 19 -69 -57 .09 6 5 | -18688 1478 25 89
| 0 0 1 8 15 14 .03 | 4034 1576
jpl 130| 0 0 0 3 -26 13 .49 15 14 | 2141 671 23 113
| 0 1 1 20 22 27 .05 | 2053 1409
mit 259| 0 0 0 53 -71 -18 -.38 13 13 | -59 -91 24 151
| 0 0 1 34 40 11 .02 | 219 459
ngs 239| 0 0 0 99 198 -61 -.25 11 9 | -284 73 2186 3704
| 1 0 0 22 43 19 .05 | 319 958
sio 109| 0 1 -5 -76 -11 -33 -.12 22 20 | --- --- --- ---
| 1 1 1 16 46 13 .03 | --- ---
Table 1.1506.b GPS week : 1506 MJD: 54786.000-54792.000
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 27 0 |
2 | 6 5 5 5 5 5 6 |
3 | 5 4 4 4 4 4 4 |
4 | 6 6 5 5 5 5 5 |
5 | 6 4 4 4 4 4 4 |
6 | 5 4 4 4 3 4 4 |
7 | 5 5 5 5 6 5 5 |
8 | 6 5 6 6 7 8 9 |
9 | 7 7 6 6 6 6 6 |
10 | 5 4 4 4 5 5 5 |
11 | 6 5 5 5 5 5 5 |
12 | 6 6 5 5 6 6 6 |
13 | 6 5 5 5 6 5 6 |
14 | 6 6 6 5 5 5 6 |
15 | 6 6 6 6 6 6 6 |
16 | 7 6 6 6 6 6 7 |
17 | 6 6 5 5 6 5 5 |
18 | 6 6 5 5 6 5 6 |
19 | 5 5 5 5 5 5 5 |
20 | 5 5 5 5 5 5 5 |
21 | 7 5 5 5 5 5 5 |
22 | 6 6 5 5 5 5 5 |
23 | 6 6 6 6 6 6 6 |
24 | 9 9 6 5 5 5 5 |
25 | 6 5 4 6 6 6 6 |
26 | 5 5 4 4 5 4 4 |
27 | 6 6 6 7 11 11 8 |
28 | 7 7 6 6 6 6 6 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 5 6 5 5 5 6 6 |
32 | 6 5 5 5 6 5 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 2.1506.0 GPS week: 1506 Day: 0 MJD: 54786.000
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 243| 0 0 0 23 -52 -30 -.21 12 10 | -466 -105 36 124
| -13 7 |
emr 84| 0 2 1 -155 -140 -1 .36 19 19 | -820 -1532 32 238
| 13 119 |
esa 128| 2 0 2 -5 32 -7 .24 11 11 | 513 -913 31 161
| 3 -8 |
gfz 200| -1 0 1 -40 -8 153 -.06 17 17 | 333 -591 27 140
| 20 -12 |
grg 84| 3 2 8 48 39 -188 1.18 49 46 | -461 -155 121 365
| 48 -24 |
igr n/a| 0 0 -2 26 -89 -88 .05 6 5 | -22412 -871 28 100
| -26 22 |
jpl 130| 0 2 0 -17 -33 24 .37 15 14 | 811 -1098 29 118
| 20 -6 |
mit 259| -1 -1 -1 45 -84 -37 -.39 14 13 | 21 -344 24 138
| 20 -8 |
ngs 239| 1 -2 -1 103 228 -49 -.17 13 11 | -456 -166 2002 3645
| 2 -17 |
sio 109| -3 0 -5 -66 -42 -38 -.17 24 18 | --- --- --- ---
| 73 -22 |
Table 2.1506.1 GPS week: 1506 Day: 1 MJD: 54787.000
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 243| 0 -1 2 -1 -68 -35 -.18 12 10 | -781 1887 33 131
| 5 64 |
emr 84| -1 1 2 -168 -110 -15 .46 18 18 | -2742 1344 27 246
| 17 87 |
esa 128| 0 -1 0 -37 6 23 .25 11 10 | -166 -458 26 134
| -3 10 |
gfz 200| 0 1 0 -6 -34 220 -.09 17 17 | 118 -112 28 149
| -16 31 |
grg 84| 2 0 10 -4 56 -33 1.19 51 47 | -757 1795 121 389
| 24 90 |
igr n/a| 1 0 -3 19 -64 -45 .12 7 6 | -23581 1893 28 89
| -31 17 |
jpl 130| 0 2 0 -30 -34 -18 .50 16 15 | -648 1122 28 123
| 19 -14 |
mit 259| -1 0 0 69 -9 -30 -.38 13 11 | -256 -25 24 161
| 8 -39 |
ngs 239| 1 0 -2 122 166 -61 -.25 11 9 | -744 1792 2395 3945
| 17 28 |
sio 109| -1 0 -7 -54 25 -44 -.09 22 20 | --- --- --- ---
| 59 -26 |
Table 2.1506.2 GPS week: 1506 Day: 2 MJD: 54788.000
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 243| 0 0 0 19 -78 -29 -.18 10 10 | -136 132 30 123
| 5 59 |
emr 84| -3 0 3 -156 -116 -35 .43 18 18 | -800 -490 28 232
| 21 113 |
esa 128| 0 -2 0 -33 11 14 .25 11 11 | -1730 1490 21 110
| 31 17 |
gfz 200| 0 1 0 -63 -7 241 .05 16 16 | 279 -457 26 128
| 14 13 |
grg 84| 3 -1 9 13 70 -45 1.12 53 47 | -108 35 108 346
| 27 66 |
igr n/a| 0 1 -1 30 -59 -51 .10 6 5 | -21017 166 24 79
| -15 17 |
jpl 130| 0 0 1 3 6 3 .50 15 14 | 1015 -748 22 97
| 19 -12 |
mit 259| 0 0 0 49 -32 -11 -.36 11 11 | 238 -640 28 157
| 30 -17 |
ngs 239| 0 0 0 111 151 -96 -.23 11 8 | -94 -3 2138 3540
| 35 22 |
sio 109| 0 1 -6 -71 35 -14 -.10 19 18 | --- --- --- ---
| 36 -45 |
Table 2.1506.3 GPS week: 1506 Day: 3 MJD: 54789.000
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 243| 1 0 0 19 -79 -54 -.22 9 9 | 304 -1534 26 119
| 6 69 |
emr 84| -6 0 3 -193 -71 -39 .51 16 16 | -12 3036 21 198
| 32 66 |
esa 128| 0 -2 0 -31 17 0 .23 11 11 | -1067 1837 23 118
| -27 -20 |
gfz 200| 0 2 1 15 -23 231 -.02 15 15 | 22 457 23 132
| -28 9 |
grg 84| 4 1 6 15 65 16 1.15 48 42 | 320 -1608 111 362
| 47 35 |
igr n/a| 0 0 0 8 -44 -58 .10 6 6 | -19676 4034 22 103
| -51 -5 |
jpl 130| 0 -1 0 6 -6 23 .53 14 13 | 1251 2999 20 108
| -6 19 |
mit 259| 0 0 0 91 -64 -13 -.36 11 11 | -49 171 22 152
| -9 -9 |
ngs 239| 1 0 0 58 177 -68 -.26 11 9 | 257 -1388 2301 4049
| 84 32 |
sio 109| 0 1 -5 -70 32 -16 -.14 21 20 | --- --- --- ---
| 81 -26 |
Table 2.1506.4 GPS week: 1506 Day: 4 MJD: 54790.000
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 243| 0 0 0 46 -73 -38 -.21 10 9 | -190 -202 28 158
| -39 29 |
emr 84| -2 -2 4 -159 -67 -9 .47 16 16 | 2347 10 17 136
| 44 29 |
esa 128| 1 -1 0 -54 14 9 .27 12 12 | -943 168 22 94
| 20 15 |
gfz 200| 0 2 3 -29 -13 106 .05 15 15 | 222 -372 24 124
| -24 -23 |
grg 84| 5 -1 5 73 23 16 1.08 44 47 | -189 -259 102 277
| 2 2 |
igr n/a| 0 0 0 13 -66 -55 .08 6 5 | -16490 1173 25 80
| -26 -5 |
jpl 130| 0 -1 -1 23 -21 64 .50 16 14 | 3431 103 21 127
| 11 15 |
mit 259| 0 0 -1 66 -71 -2 -.41 14 14 | 71 -389 31 165
| 38 -22 |
ngs 239| -1 0 0 84 163 -53 -.25 10 9 | -190 -253 2285 3675
| 51 34 |
sio 109| 1 2 -6 -78 4 -45 -.15 21 20 | --- --- --- ---
| 69 -4 |
Table 2.1506.5 GPS week: 1506 Day: 5 MJD: 54791.000
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 243| 0 0 0 28 -65 -30 -.22 10 9 | -389 429 19 100
| 16 -21 |
emr 84| -2 -4 4 -165 -68 -33 .48 16 16 | 3115 120 17 170
| 17 22 |
esa 128| 0 0 -1 -48 14 17 .27 11 11 | -822 -556 22 109
| -20 -5 |
gfz 200| 0 1 2 11 -14 121 .01 15 15 | 167 -213 22 125
| -59 -27 |
grg 84| 6 -1 13 32 40 69 1.15 47 42 | -391 364 112 298
| 20 -68 |
igr n/a| 0 0 0 25 -81 -54 .05 5 5 | -14605 1543 23 90
| -58 -5 |
jpl 130| 0 -1 0 11 -32 12 .50 14 13 | 4194 738 19 105
| -11 36 |
mit 259| 0 1 0 65 -120 -14 -.38 14 13 | -11 -180 21 144
| 25 -7 |
ngs 239| 0 0 0 96 237 -33 -.31 11 8 | -466 567 1992 3365
| -31 -42 |
sio 109| 1 2 -4 -93 -61 -46 -.12 22 21 | --- --- --- ---
| 93 24 |
Table 2.1506.6 GPS week: 1506 Day: 6 MJD: 54792.000
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 243| 0 0 0 32 -58 -38 -.21 10 10 | -324 48 27 116
| -43 -11 |
emr 84| -3 -5 4 -103 -18 -43 .47 18 18 | 3347 1436 18 172
| -15 -56 |
esa 128| 0 0 -2 -25 -35 22 .24 12 12 | -1064 989 21 93
| -6 -8 |
gfz 200| 0 1 1 -75 -21 176 .03 15 15 | -215 797 24 123
| -4 -20 |
grg 84| 8 -2 8 1 30 -66 1.11 46 43 | -315 -10 104 402
| -35 -35 |
igr n/a| 1 -1 0 10 -78 -46 .10 5 5 | -13035 2409 25 87
| -23 -6 |
jpl 130| 0 1 -1 26 -64 -11 .50 15 13 | 4935 1583 22 118
| -2 79 |
mit 259| -1 0 0 -15 -116 -22 -.36 16 15 | -429 765 22 146
| 58 -3 |
ngs 239| 0 0 0 117 262 -70 -.31 11 8 | -299 -36 2195 3713
| 3 -92 |
sio 109| 1 2 -2 -103 -74 -32 -.09 24 21 | --- --- --- ---
| 41 58 |
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 3.1506.0 GPS week: 1506 Day: 0 MJD: 54786.000
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 | 5 --- --- --- --- 29 --- --- --- --- 0 | 26 --- --- --- --- 32 --- --- --- --- 26
2 | 11 18 11 16 55 4 21 14 11 24 5 | 22 31 20 29 31 22 34 22 25 26 24
3 | 11 11 11 11 63 4 7 14 14 14 4 | 40 44 47 38 57 42 43 36 42 38 41
4 | 11 20 9 15 54 9 15 12 15 20 5 | 19 28 19 29 34 22 26 23 25 25 21
5 | 5 12 11 17 45 4 9 24 11 22 5 | 20 26 28 26 36 25 29 26 27 26 23
6 | 9 14 12 13 58 3 7 9 15 14 4 | 29 33 37 31 46 32 33 29 35 35 32
7E | 13 20 9 14 19 5 16 13 11 15 5 | 24 35 28 32 42 25 34 19 26 22 25
8E | 12 25 11 14 40 8 11 8 11 34 5 | 40 50 37 44 33 38 36 44 42 35 39
9E | 20 18 12 18 121 8 17 24 18 21 7 | 36 43 41 48 74 37 47 42 44 40 39
10 | 9 21 7 15 31 5 9 11 14 19 4 | 19 37 19 27 35 21 28 21 25 18 22
11 | 14 15 10 19 59 5 11 14 15 20 5 | 23 33 26 27 58 23 31 20 21 23 22
12 | 10 16 12 18 42 5 15 13 11 29 5 | 22 30 28 32 48 25 30 16 29 20 24
13 | 11 21 9 21 35 5 15 13 11 12 5 | 23 38 24 30 41 26 31 26 28 24 25
14 | 8 18 13 20 47 6 17 13 11 16 5 | 18 33 30 27 35 23 28 22 29 22 24
15 | 8 19 12 19 34 4 18 12 14 25 5 | 23 34 27 34 44 26 32 25 27 27 25
16 | 15 20 15 16 77 6 19 25 17 29 7 | 23 33 27 27 75 24 32 19 24 23 22
17 | 8 12 9 18 60 6 12 9 10 41 5 | 28 37 29 34 61 29 36 26 31 37 29
18 | 11 23 13 17 34 5 17 13 11 16 5 | 22 39 28 38 37 28 36 22 29 27 28
19 | 14 16 10 15 39 6 14 12 14 22 5 | 27 40 31 33 46 27 36 26 25 30 29
20 | 11 20 9 19 34 5 15 10 10 10 5 | 22 35 24 33 47 26 34 20 24 26 24
21 | 26 21 11 16 34 7 13 12 15 17 6 | 74 77 78 73 82 74 78 65 76 64 72
22 | 10 17 13 21 22 6 16 13 13 19 5 | 19 36 27 34 40 26 32 20 29 30 25
23 | 11 24 13 17 24 5 20 14 14 20 6 | 22 39 29 30 37 27 34 24 29 33 25
24E | 22 26 16 20 44 7 21 18 16 58 9 | 117 139 135 137 134 137 140 128 140 159 134
25E | 10 29 11 14 58 6 13 16 10 12 5 | 21 37 23 27 22 22 24 27 24 26 22
26 | 10 15 8 14 29 4 8 9 13 28 4 | 20 33 23 28 38 24 29 25 28 28 24
27E | 13 20 17 12 37 6 13 13 13 17 5 | 18 27 23 23 20 18 20 23 22 15 19
28 | 13 18 11 19 39 6 19 17 11 34 6 | 23 32 23 28 36 22 34 26 23 23 23
29 | 6 13 9 16 54 5 13 9 15 31 5 | 29 37 35 35 54 32 40 29 38 32 33
30 | 5 10 10 15 35 5 8 9 13 16 4 | 30 31 31 25 28 32 32 32 29 35 28
31E | 8 19 11 12 38 6 18 13 12 15 5 | 19 30 28 26 42 23 28 22 28 27 23
32 | 9 22 8 19 38 6 17 13 12 21 5 | 24 28 30 29 31 27 32 27 25 35 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 19 11 17 49 6 15 14 13 24 |T 28 39 33 35 46 31 37 30 33 33 31
WRMS | 10 19 11 17 46 5 14 13 11 18 |NE 25 36 30 32 44 28 34 26 30 29 27
MEDI | 11 19 11 16 39 5 15 13 13 20 |MD 23 35 28 30 41 26 32 25 28 27 25
Table 3.1506.1 GPS week: 1506 Day: 1 MJD: 54787.000
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 | 5 --- --- --- --- 26 --- --- --- --- 0 | 33 --- --- --- --- 25 --- --- --- --- 35
2 | 10 20 10 15 52 4 16 14 11 19 5 | 19 29 20 21 29 18 24 18 17 22 16
3 | 8 14 9 11 70 5 10 10 9 19 4 | 38 39 39 39 51 38 40 42 41 34 37
4 | 10 21 14 21 43 13 18 10 10 19 5 | 17 29 19 32 35 21 26 21 18 17 17
5 | 9 11 9 15 50 6 9 12 8 20 4 | 20 25 22 24 36 23 26 23 20 26 19
6 | 8 15 9 12 49 3 10 9 10 18 4 | 27 26 29 28 34 27 30 25 26 26 24
7E | 11 21 8 10 26 7 14 8 9 11 4 | 23 33 26 25 41 27 29 20 26 18 22
8E | 12 18 11 12 62 10 14 11 11 29 5 | 40 44 39 42 34 42 42 44 45 38 40
9E | 18 16 12 19 130 9 19 25 12 19 6 | 29 38 37 36 59 36 47 47 34 38 35
10 | 12 14 7 12 28 5 8 10 11 17 4 | 17 26 24 24 28 22 22 23 25 23 20
11 | 7 14 9 20 61 6 13 10 11 22 5 | 19 28 24 24 54 21 29 24 23 27 20
12 | 10 15 11 17 59 4 19 11 9 26 5 | 19 32 26 31 52 25 35 19 21 23 22
13 | 11 18 9 18 48 4 17 14 10 12 5 | 16 33 22 27 43 23 28 18 19 18 18
14 | 8 16 12 20 55 8 19 11 13 22 5 | 18 31 22 25 39 22 30 18 24 22 19
15 | 9 18 13 20 37 4 16 11 12 28 5 | 21 27 26 26 41 22 29 21 22 19 20
16 | 9 18 12 17 60 4 21 16 12 29 6 | 18 31 20 28 46 20 28 20 22 18 18
17 | 9 12 9 17 47 6 15 8 16 32 5 | 19 27 22 25 44 23 28 20 24 30 19
18 | 13 26 11 21 27 6 19 11 9 19 6 | 19 34 23 31 43 22 33 15 22 19 20
19 | 9 16 13 18 32 8 14 10 11 24 5 | 20 33 26 27 38 25 32 25 21 21 22
20 | 9 18 12 17 40 5 17 12 10 11 5 | 20 33 23 25 46 23 29 17 22 21 20
21 | 12 20 11 15 52 6 11 11 8 17 5 | 35 36 30 30 60 32 35 24 30 23 29
22 | 13 22 14 22 30 5 20 13 12 20 6 | 18 30 20 25 39 19 26 17 21 22 16
23 | 11 23 13 17 35 5 21 12 9 19 5 | 18 36 23 27 43 22 30 18 19 22 19
24E | 37 22 13 19 45 13 21 22 19 25 8 | 96 107 106 109 116 107 112 102 108 99 103
25E | 7 20 8 14 48 6 13 12 9 12 4 | 23 34 24 27 32 26 33 28 29 30 24
26 | 9 14 9 11 27 3 11 9 11 24 4 | 18 23 23 22 29 20 23 21 21 24 18
27E | 14 24 14 11 45 6 14 12 13 12 5 | 16 29 18 21 31 20 24 24 24 18 17
28 | 11 18 10 17 43 7 26 18 12 35 6 | 17 29 22 27 37 20 35 26 18 27 19
29 | 9 12 9 16 41 5 17 8 10 26 5 | 22 28 26 26 40 25 33 22 21 18 22
30 | 8 12 6 18 43 6 9 11 9 16 4 | 22 29 23 28 32 25 26 25 28 28 22
31E | 7 16 13 13 39 7 15 12 15 31 5 | 19 29 22 23 46 20 25 18 25 19 18
32 | 8 19 12 19 43 7 19 11 9 17 5 | 20 27 22 21 36 21 29 23 23 27 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 18 11 17 51 7 16 13 11 22 |T 24 33 27 29 43 26 32 26 27 26 24
WRMS | 10 18 10 17 47 6 15 11 9 20 |NE 21 30 24 26 40 23 29 21 22 23 21
MEDI | 9 18 11 17 45 6 16 11 11 19 |MD 19 30 23 27 40 23 29 22 23 23 20
Table 3.1506.2 GPS week: 1506 Day: 2 MJD: 54788.000
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 --- --- --- --- 57 --- --- --- --- 0 | 59 --- --- --- --- 30 --- --- --- --- 58
2 | 11 20 9 18 54 5 17 11 8 23 5 | 22 33 21 29 25 24 30 23 25 33 24
3 | 11 13 13 10 32 4 8 8 11 17 4 | 32 34 34 32 31 33 32 37 38 30 32
4 | 10 19 7 16 57 6 14 9 12 19 4 | 21 32 21 29 30 23 23 24 26 20 21
5 | 8 11 7 13 40 4 10 9 6 17 3 | 18 27 23 22 34 21 26 21 20 24 19
6 | 8 17 12 12 20 4 8 9 11 14 4 | 27 30 31 26 27 27 27 28 27 29 25
7E | 15 24 10 12 34 5 13 11 10 10 5 | 24 35 26 26 41 24 30 24 27 22 24
8E | 14 20 11 14 73 7 13 12 10 31 5 | 34 41 29 35 31 34 33 39 36 27 31
9E | 17 17 10 12 150 13 18 18 10 16 5 | 29 41 34 36 65 35 42 41 36 31 34
10 | 9 18 10 13 21 4 9 9 11 14 4 | 18 32 19 24 28 20 23 22 26 20 20
11 | 12 14 10 19 61 5 12 8 10 18 4 | 20 27 22 26 51 21 26 24 28 27 21
12 | 10 17 10 16 54 6 17 13 8 25 5 | 18 32 23 29 51 23 31 20 22 22 21
13 | 10 19 12 20 49 6 15 12 9 12 5 | 22 36 28 30 45 25 31 26 26 23 24
14 | 7 20 15 20 45 7 17 11 10 15 5 | 20 36 28 25 42 24 29 23 27 19 22
15 | 11 17 12 19 28 6 21 13 13 23 6 | 23 33 21 29 37 23 33 24 22 24 22
16 | 12 19 17 18 51 6 19 11 15 27 6 | 19 32 24 28 44 23 30 21 26 23 21
17 | 8 14 10 15 45 5 16 7 9 27 4 | 25 33 25 30 43 26 32 26 27 28 25
18 | 9 20 12 16 27 6 19 8 11 16 5 | 23 38 26 32 44 25 34 22 23 27 25
19 | 11 16 16 14 28 6 14 8 11 24 5 | 21 30 26 25 29 23 30 24 27 26 23
20 | 9 18 10 18 34 6 15 12 8 11 4 | 22 35 26 29 43 25 29 20 23 24 22
21 | 9 19 10 15 41 8 12 8 10 12 4 | 30 34 28 26 53 31 32 27 30 25 27
22 | 9 20 12 21 26 5 15 6 14 19 5 | 19 35 25 29 39 23 28 21 27 27 22
23 | 10 23 15 18 31 6 20 13 10 17 5 | 20 40 30 28 43 25 31 25 25 27 23
24 | 15 22 9 15 52 11 17 15 12 22 5 | 54 62 58 61 69 59 65 53 62 57 57
25E | 9 17 12 11 69 4 14 10 7 11 4 | 23 32 25 27 40 23 30 26 28 29 24
26 | 8 12 9 11 23 5 9 9 10 17 4 | 21 29 21 23 29 23 23 24 26 25 21
27E | 16 28 18 10 84 5 15 14 11 14 6 | 18 33 19 20 36 20 20 26 22 18 19
28 | 10 19 12 18 72 5 17 15 11 34 6 | 19 33 20 27 56 21 30 26 28 27 21
29 | 7 14 7 14 34 5 15 9 11 25 4 | 25 32 28 26 36 27 33 26 31 26 26
30 | 6 11 5 13 32 5 11 9 8 16 3 | 23 30 27 26 33 25 26 27 25 31 24
31E | 8 20 11 12 37 6 19 11 13 15 5 | 18 31 23 22 45 20 28 20 24 15 19
32 | 9 19 12 17 45 5 16 10 10 17 5 | 22 29 30 26 37 23 31 25 24 30 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 11 16 53 6 15 11 11 19 |T 24 34 26 28 40 25 30 26 27 26 25
WRMS | 10 18 11 16 47 5 14 11 8 18 |NE 23 32 25 27 38 24 29 24 26 25 24
MEDI | 9 19 11 15 41 5 15 10 10 17 |MD 22 33 26 27 40 24 30 24 26 26 23
Table 3.1506.3 GPS week: 1506 Day: 3 MJD: 54789.000
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 | 7 --- --- --- --- 45 --- --- --- --- 0 | 23 --- --- --- --- 47 --- --- --- --- 23
2 | 9 21 9 15 45 5 15 10 10 16 4 | 19 34 17 28 30 20 27 20 24 23 21
3 | 7 10 8 11 37 4 7 8 11 14 3 | 31 32 33 27 28 30 32 31 33 29 30
4 | 10 14 7 19 49 6 11 10 9 21 4 | 16 25 18 28 34 18 19 20 20 19 16
5 | 8 13 7 12 32 8 9 10 7 17 3 | 16 30 19 19 30 22 24 16 16 19 16
6 | 6 12 9 11 33 5 8 8 13 13 3 | 21 26 26 20 26 21 25 22 24 26 21
7E | 12 20 10 13 34 5 16 15 9 12 5 | 16 29 21 24 36 21 24 16 19 13 16
8E | 14 15 11 14 64 11 14 14 11 32 5 | 39 41 38 49 42 41 38 45 45 40 39
9E | 16 16 11 12 132 7 17 15 12 17 5 | 30 41 37 38 57 36 43 38 31 31 34
10 | 8 15 11 14 25 6 10 9 9 14 4 | 12 27 17 21 28 15 18 16 16 11 14
11 | 10 14 10 19 50 5 11 9 9 24 4 | 14 24 18 23 49 16 21 13 16 19 13
12 | 10 14 11 18 27 6 17 12 9 25 5 | 15 27 20 27 37 20 26 18 18 18 17
13 | 10 21 13 18 39 6 14 14 10 9 5 | 19 35 24 25 41 22 28 23 16 22 19
14 | 7 18 12 23 50 6 14 13 11 18 5 | 16 29 23 24 37 20 23 17 24 19 18
15 | 9 15 12 20 29 8 18 12 11 24 5 | 21 32 24 32 35 26 29 22 23 20 21
16 | 11 20 16 18 51 6 16 14 13 27 6 | 17 30 21 26 53 21 27 17 20 23 17
17 | 9 12 10 12 35 8 11 11 13 26 4 | 24 35 27 32 44 31 31 26 32 30 27
18 | 10 19 11 14 32 5 17 9 9 20 5 | 21 34 23 30 37 25 33 22 24 29 24
19 | 10 14 10 13 28 5 13 9 12 23 4 | 20 28 20 24 31 19 26 20 20 20 19
20 | 6 16 13 17 26 5 14 11 9 10 4 | 18 31 22 26 41 23 28 15 22 20 19
21 | 9 20 10 14 61 5 11 8 10 13 4 | 16 30 20 23 43 19 25 15 18 20 18
22 | 9 12 15 18 21 6 11 7 11 19 4 | 17 29 19 27 37 20 25 18 27 29 20
23 | 10 25 17 15 21 6 18 12 11 17 6 | 18 38 26 25 39 22 31 19 16 26 19
24 | 11 17 9 14 45 4 17 15 11 20 5 | 52 61 58 59 65 56 61 56 52 60 55
25E | 9 19 11 13 95 5 19 11 10 29 5 | 31 36 30 32 41 30 37 31 32 42 30
26 | 6 12 10 11 27 6 8 10 13 17 4 | 17 28 26 24 31 24 22 24 25 21 20
X27E | 18 24 14 15 62 8 --- 19 12 17 7 | 15 29 15 20 22 20 --- 32 26 19 19
28 | 10 16 10 17 54 7 18 15 14 35 6 | 16 28 18 28 41 20 27 22 24 21 17
29 | 7 12 8 14 27 5 13 9 11 26 4 | 25 30 25 30 40 27 31 22 29 24 25
30 | 8 9 7 13 33 7 8 8 7 16 3 | 22 28 24 20 32 23 24 25 20 30 21
31E | 8 13 12 13 34 4 18 14 11 20 5 | 17 28 16 18 42 18 25 12 18 16 14
32 | 7 15 13 19 34 5 15 13 11 19 5 | 17 21 21 22 31 18 25 17 21 26 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 11 15 48 6 14 11 11 21 |T 20 31 24 27 38 24 28 22 24 24 21
WRMS | 9 16 11 15 42 6 13 11 9 20 |NE 18 29 22 25 36 22 26 20 22 22 19
MEDI | 9 15 11 14 34 6 14 11 11 19 |MD 18 30 22 26 37 21 26 20 23 22 19
Table 3.1506.4 GPS week: 1506 Day: 4 MJD: 54790.000
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 --- --- --- --- 14 --- --- --- --- 0 | 22 --- --- --- --- 24 --- --- --- --- 23
2 | 11 21 13 14 41 3 16 11 10 15 5 | 15 27 12 23 24 16 25 20 17 20 16
3 | 7 10 8 11 39 5 8 7 9 14 3 | 18 18 19 18 23 18 20 22 23 22 17
4 | 12 15 9 19 29 4 9 13 10 22 5 | 12 22 14 27 27 17 18 23 20 22 15
5 | 7 14 8 11 26 4 9 15 8 17 4 | 14 25 20 22 30 18 25 14 14 19 16
6 | 5 8 7 11 36 5 8 9 9 13 3 | 17 21 19 23 25 19 23 20 21 24 17
7E | 14 19 11 12 30 7 17 18 14 10 5 | 15 26 15 19 37 17 22 18 20 12 13
8E | 13 18 17 13 56 6 16 23 16 32 7 | 40 38 37 40 44 36 41 42 39 36 36
9E | 17 19 10 13 134 7 18 21 10 16 6 | 23 38 33 35 46 30 43 39 28 27 29
10 | 9 13 11 13 38 5 11 11 13 11 4 | 11 24 18 18 29 13 18 15 14 13 14
11 | 10 14 13 21 59 4 14 10 8 25 5 | 11 22 12 21 47 12 22 13 12 21 9
12 | 11 17 12 18 32 6 18 19 9 27 6 | 12 25 19 28 33 18 28 15 17 15 15
13 | 10 19 14 18 35 7 16 19 9 11 5 | 15 32 19 23 39 20 28 22 15 18 16
14 | 6 16 13 20 42 6 16 15 10 16 5 | 12 27 18 23 34 18 23 17 19 16 16
15 | 10 18 12 18 29 5 19 14 10 24 5 | 14 28 24 28 36 20 25 17 19 16 16
16 | 11 18 12 16 45 5 19 12 13 27 6 | 17 28 20 29 40 21 30 22 21 25 18
17 | 9 13 15 15 38 6 17 14 9 25 5 | 24 28 20 25 44 25 31 29 26 22 23
18 | 12 23 10 15 32 6 18 15 11 17 5 | 17 35 21 28 35 23 33 19 27 22 21
19 | 10 16 8 12 30 6 15 12 10 23 4 | 15 26 16 27 27 20 26 17 20 18 17
20 | 7 15 15 16 31 5 18 11 9 11 5 | 15 26 19 25 41 19 29 15 15 17 17
21 | 8 17 9 14 29 5 10 12 9 18 4 | 16 29 22 23 42 20 24 16 19 23 18
22 | 10 12 11 17 19 7 17 11 10 18 5 | 12 25 17 25 34 19 30 17 25 26 17
23 | 11 23 15 16 23 6 20 15 11 18 6 | 14 33 22 25 36 20 30 19 15 21 16
24 | 10 14 9 16 39 6 17 15 10 20 5 | 28 41 35 37 46 33 42 29 29 39 33
25E | 9 16 12 11 63 6 20 17 10 32 5 | 33 35 35 36 53 34 41 38 37 43 34
26 | 9 13 8 14 28 4 13 11 9 20 4 | 13 23 21 22 29 17 14 20 20 21 15
X27E | 8 --- 14 --- --- 95 --- --- --- --- 11 | 50 --- 19 --- --- 144 --- --- --- --- 52
28 | 13 14 13 20 41 7 20 14 12 32 6 | 16 25 18 24 32 18 27 23 17 27 16
29 | 9 14 7 11 36 5 13 8 10 25 4 | 21 31 25 26 35 24 29 24 24 21 23
30 | 4 10 8 11 26 6 9 10 9 17 3 | 17 23 23 21 28 20 26 21 16 27 18
31E | 8 19 13 13 28 5 17 18 12 15 5 | 8 23 15 16 35 13 23 16 17 16 11
32 | 8 19 14 21 30 3 16 11 8 21 5 | 14 18 17 18 26 13 26 18 19 25 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 12 15 44 6 16 14 10 21 |T 18 27 20 25 35 24 27 21 20 22 19
WRMS | 9 16 12 15 47 5 14 13 9 20 |NE 15 25 18 23 33 18 25 19 18 20 16
MEDI | 9 16 12 14 32 6 16 13 10 18 |MD 15 26 19 24 35 19 26 19 19 21 17
Table 3.1506.5 GPS week: 1506 Day: 5 MJD: 54791.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 22 32 --- --- --- 58 --- --- --- --- 26 | 17 22 --- --- --- 54 --- --- --- --- 24
2 | 10 19 13 14 46 5 12 15 10 23 5 | 16 28 16 22 24 15 24 22 20 26 18
3 | 9 9 5 11 54 4 9 8 7 19 3 | 21 24 21 23 29 24 23 29 31 25 23
4 | 11 17 7 18 40 4 10 13 9 20 4 | 10 24 17 27 25 17 16 26 23 20 17
5 | 8 14 7 12 22 2 10 15 7 19 4 | 18 23 23 24 31 19 27 21 21 21 20
6 | 5 11 7 11 44 4 8 8 9 17 3 | 13 17 15 17 29 14 21 17 18 25 15
7E | 12 16 10 13 31 6 16 17 11 12 5 | 10 24 15 18 34 13 20 16 16 16 13
8E | 18 19 19 11 59 7 15 28 20 34 7 | 41 44 42 43 48 41 43 53 47 43 40
9E | 17 19 13 11 131 6 15 19 14 20 6 | 22 39 35 38 58 33 41 39 35 31 32
10 | 9 12 10 13 25 5 10 12 12 17 4 | 9 21 14 18 21 11 17 14 16 14 13
11 | 8 13 10 20 58 5 12 10 8 24 4 | 8 22 12 21 45 11 21 10 11 17 10
12 | 12 16 11 18 37 6 15 19 9 28 6 | 12 23 16 25 37 16 26 17 18 19 16
13 | 10 17 13 20 49 6 13 17 10 11 5 | 12 31 18 24 43 17 27 20 16 16 17
14 | 8 17 11 22 46 5 13 15 11 17 5 | 13 30 20 26 32 18 26 20 23 20 20
15 | 10 14 11 18 39 7 18 15 14 22 5 | 12 28 17 24 36 18 25 16 24 14 16
16 | 11 19 14 19 48 8 19 14 11 30 6 | 13 28 20 25 37 19 29 17 21 22 17
17 | 8 14 9 12 57 5 12 14 11 29 5 | 18 29 23 23 46 21 27 23 25 25 22
18 | 10 18 11 14 29 5 17 12 12 19 5 | 20 34 26 29 38 24 32 20 25 24 25
19 | 9 12 8 12 29 6 12 10 11 23 4 | 13 25 18 22 29 16 24 16 23 12 17
20 | 8 15 14 15 32 5 17 10 7 8 4 | 13 26 21 21 46 16 26 13 18 15 17
21 | 10 17 9 14 24 4 10 10 9 19 4 | 17 27 20 24 39 17 21 17 17 23 19
22 | 8 14 12 17 28 5 15 12 12 17 5 | 14 28 21 26 38 18 28 20 25 27 21
23 | 11 23 14 16 32 6 18 13 12 17 5 | 11 33 20 26 42 18 29 16 19 18 18
24 | 10 14 10 14 42 6 15 15 10 17 4 | 36 45 40 44 45 41 47 36 43 44 41
25E | 13 15 12 11 59 6 19 20 12 30 6 | 39 40 41 40 46 38 43 44 39 47 39
26 | 8 13 6 12 37 4 11 13 11 21 4 | 10 25 16 16 28 14 15 17 21 14 14
X27E | 23 31 --- 22 --- 17 --- 20 12 --- 11 | 32 30 --- 17 --- 29 --- 26 13 --- 28
28 | 11 16 11 19 43 7 16 17 11 34 6 | 14 25 19 22 30 15 26 23 16 23 15
29 | 9 13 7 12 48 5 11 8 13 27 4 | 18 28 23 24 41 21 27 20 21 19 21
30 | 7 18 7 12 27 5 8 11 8 19 4 | 19 26 21 19 26 19 23 20 18 26 18
31E | 10 20 13 15 37 5 19 15 9 16 5 | 12 27 17 18 43 15 24 14 19 15 15
32 | 6 17 12 19 32 3 14 12 5 21 5 | 12 18 15 19 29 12 24 15 14 28 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 11 15 47 5 14 14 11 22 |T 17 27 21 24 36 21 26 21 22 22 20
WRMS | 9 16 11 15 42 5 13 13 8 21 |NE 14 25 18 22 34 18 24 18 20 20 17
MEDI | 10 16 11 14 39 5 13 14 11 19 |MD 13 27 20 24 37 18 26 20 21 21 18
Table 3.1506.6 GPS week: 1506 Day: 6 MJD: 54792.000
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 | 5 --- --- --- --- 47 --- --- --- --- 0 | 25 --- --- --- --- 50 --- --- --- --- 27
2 | 10 21 13 14 44 5 16 20 12 25 6 | 22 32 16 27 23 20 29 33 19 35 23
3 | 9 13 8 10 37 5 7 11 11 22 4 | 26 27 30 26 28 25 25 35 28 34 26
4 | 13 18 8 16 34 6 8 19 8 26 5 | 16 29 17 29 25 17 20 32 25 23 21
5 | 8 14 7 11 34 4 8 19 6 21 4 | 16 25 20 20 37 20 24 21 20 25 19
6 | 7 12 8 12 19 5 7 9 10 20 4 | 23 27 26 25 28 24 27 27 22 36 24
7E | 11 16 11 12 31 7 16 17 9 12 5 | 16 25 18 18 34 17 24 18 19 18 16
8E | 19 19 24 16 55 7 16 32 25 32 8 | 43 46 48 45 40 43 44 56 51 43 42
9E | 17 19 16 11 134 7 16 19 12 21 6 | 29 44 42 42 53 36 46 43 37 40 37
10 | 11 15 9 13 30 5 10 15 9 14 4 | 13 21 16 21 27 14 21 21 18 16 17
11 | 9 17 9 20 60 4 12 13 8 25 5 | 16 26 17 26 55 15 23 19 19 21 17
12 | 14 17 12 17 44 6 17 18 9 32 6 | 19 27 22 31 49 22 31 22 25 25 22
13 | 10 18 14 19 56 5 15 21 9 15 5 | 15 30 20 24 44 19 29 21 21 20 18
14 | 7 18 14 20 49 5 15 17 9 19 5 | 17 30 25 24 34 20 27 24 24 21 21
15 | 10 19 11 17 28 5 18 12 12 27 5 | 19 29 21 28 35 20 28 20 22 17 21
16 | 10 22 14 21 64 5 19 17 14 36 6 | 19 33 23 30 57 21 29 22 22 33 21
17 | 6 15 10 12 43 5 12 16 13 34 5 | 28 36 31 33 54 31 34 35 32 35 30
18 | 11 23 11 15 34 7 20 11 9 22 5 | 22 35 22 33 38 25 35 21 26 28 26
19 | 9 13 8 12 36 4 12 13 11 28 4 | 23 29 23 30 38 24 30 28 25 24 24
20 | 7 18 14 13 23 6 15 12 10 15 4 | 19 30 20 26 41 21 30 18 25 22 22
21 | 10 21 14 14 29 5 12 11 10 16 5 | 24 37 27 27 39 23 28 23 27 26 26
22 | 10 16 13 19 26 5 14 15 9 21 5 | 17 27 18 29 38 20 27 22 23 30 21
23 | 9 22 16 16 21 5 20 13 10 23 6 | 14 34 23 26 37 20 31 17 19 25 19
24 | 12 17 11 14 38 5 16 13 8 21 5 | 45 51 47 48 54 48 55 45 50 47 47
25E | 12 18 13 9 45 5 16 23 11 26 6 | 50 56 50 50 64 51 56 49 59 55 50
26 | 7 12 8 13 30 3 11 9 9 25 4 | 16 22 21 23 28 17 16 20 22 19 18
X27E | 21 19 11 17 108 8 21 28 19 --- 8 | 11 21 5 18 11 17 15 28 19 --- 15
28 | 11 17 11 18 56 5 19 14 9 29 5 | 21 27 25 29 45 21 34 25 24 24 23
29 | 11 12 8 11 34 6 13 11 11 30 4 | 30 38 32 34 55 33 36 32 36 32 33
30 | 8 11 10 12 30 4 8 13 6 19 4 | 27 31 29 26 35 27 30 30 30 34 27
31E | 9 31 13 12 30 5 18 19 14 15 6 | 14 39 18 21 40 16 26 18 20 17 17
32 | 8 23 9 18 32 4 17 15 9 29 5 | 17 22 16 20 31 15 28 19 20 32 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 12 15 46 5 15 16 11 24 |T 22 31 24 28 39 24 30 27 26 28 24
WRMS | 10 18 12 15 43 5 13 15 8 21 |NE 20 29 22 26 38 22 28 24 23 26 22
MEDI | 10 18 11 14 34 5 15 15 10 22 |MD 19 30 22 27 38 21 29 23 24 25 22
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 4.1506 GPS week: 1506 MJD: 54786.0-54792.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 |U 9 11 22 |U 11 13 49 |U 9 10 18 |
emr | emr 2957 | 14 13 28 | 13 15 49 | 11 17 27 |
esa | esa 2948 | 9 11 24 |U 11 13 48 | 10 12 21 |
gfz | gfz 2937 |U 12 11 24 |U 13 15 45 | 13 16 32 |
igr | igr 2942 | 12 13 28 | 11 13 46 | 11 17 24 |
igs | igs 2950 | 12 10 26 | 11 14 45 | 10 13 22 |
jpl | jpl 2917 |U 14 14 29 |U 11 13 43 |U 11 16 25 |
mit | mit 2962 |U 15 13 28 |U 11 15 55 |U 11 12 25 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1506.0 GPS week: 1506 Day: 0 MJD: 54786.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 | 9 10 19 | 10 11 49 | 9 9 15 |
emr | emr 2958 | 12 14 28 | 13 9 46 | 9 11 23 |
esa | esa 2976 | 10 10 19 | 11 11 52 | 8 8 16 |
gfz | gfz 2944 | 13 8 23 | 13 12 57 | 11 10 30 |
igr | igr 2951 | 14 18 31 | 9 9 40 | 9 6 21 |
igs | igs 2973 | 11 9 32 | 10 10 54 | 9 9 22 |
jpl | jpl 2951 | 17 19 25 | 8 8 36 | 11 11 29 |
mit | mit 2976 | 12 7 23 | 11 9 89 | 11 11 24 |
Table 5.1506.1 GPS week: 1506 Day: 1 MJD: 54787.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 6 11 27 | 9 12 64 | 11 10 20 |
emr | emr 2960 | 16 14 30 | 11 15 50 | 12 12 23 |
esa | esa 2976 | 7 8 27 | 9 13 56 | 12 12 32 |
gfz | gfz 2949 | 13 13 26 | 11 16 43 | 13 9 27 |
igr | igr 2949 | 9 9 31 | 10 13 64 | 12 11 22 |
igs | igs 2964 | 11 9 27 | 9 14 47 | 12 11 20 |
jpl | jpl 2955 | 13 14 35 | 10 12 53 | 11 11 22 |
mit | mit 2976 | 11 10 23 | 10 16 53 | 11 11 20 |
Table 5.1506.2 GPS week: 1506 Day: 2 MJD: 54788.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 12 21 | 11 15 46 | 13 29 35 |
emr | emr 2960 | 13 12 25 | 14 19 57 | 22 54 42 |
esa | esa 2976 | 7 9 22 | 10 16 46 | 15 35 38 |
gfz | gfz 2953 | 11 10 19 | 14 18 48 | 19 48 43 |
igr | igr 2956 | 10 12 20 | 10 15 45 | 19 65 36 |
igs | igs 2965 | 16 14 23 | 11 17 45 | 16 36 37 |
jpl | jpl 2959 | 15 13 28 | 11 16 44 | 17 50 37 |
mit | mit 2976 | 13 12 19 | 11 17 49 | 15 31 46 |
Table 5.1506.3 GPS week: 1506 Day: 3 MJD: 54789.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 7 23 | 7 12 35 | 8 5 12 |
emr | emr 2960 | 13 11 26 | 9 12 39 | 8 9 24 |
esa | esa 2976 | 9 10 24 | 7 12 34 | 7 6 13 |
gfz | gfz 2951 | 13 13 24 | 8 12 35 | 11 10 30 |
igr | igr 2966 | 12 12 26 | 7 14 35 | 7 5 17 |
igs | igs 2963 | 13 6 33 | 6 12 29 | 6 7 16 |
jpl | jpl 2867 | 13 9 32 | 6 11 25 | 8 9 21 |
mit | mit 2976 | 14 14 33 | 7 13 40 | 11 8 25 |
Table 5.1506.4 GPS week: 1506 Day: 4 MJD: 54790.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2972 | 10 7 18 | 11 14 47 | 6 5 12 |
emr | emr 2868 | 11 10 28 | 12 15 47 | 7 8 22 |
esa | esa 2880 | 10 10 25 | 10 13 48 | 6 5 14 |
gfz | gfz 2860 | 12 7 23 | 12 17 37 | 12 11 30 |
igr | igr 2874 | 11 7 19 | 10 14 41 | 7 7 15 |
igs | igs 2873 | 12 9 22 | 9 15 40 | 6 6 15 |
jpl | jpl 2867 | 10 12 23 | 10 15 46 | 11 11 22 |
mit | mit 2880 | 11 9 23 | 10 18 42 | 7 6 17 |
Table 5.1506.5 GPS week: 1506 Day: 5 MJD: 54791.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 10 20 | 17 13 58 | 8 6 16 |
emr | emr 3033 | 13 12 31 | 17 19 64 | 9 10 23 |
esa | esa 2880 | 11 12 23 | 15 12 56 | 10 9 21 |
gfz | gfz 2952 | 10 10 28 | 16 16 48 | 10 10 26 |
igr | igr 2948 | 18 15 43 | 17 15 57 | 12 18 28 |
igs | igs 2948 | 11 11 26 | 16 14 58 | 9 10 20 |
jpl | jpl 2864 | 14 13 31 | 16 15 52 | 10 11 20 |
mit | mit 2976 | 17 11 31 | 16 15 65 | 11 8 21 |
Table 5.1506.6 GPS week: 1506 Day: 6 MJD: 54792.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 13 17 25 | 14 17 44 | 7 6 14 |
emr | emr 2960 | 19 20 31 | 17 18 42 | 14 13 30 |
esa | esa 2976 | 12 15 26 | 15 14 41 | 9 7 15 |
gfz | gfz 2952 | 14 16 23 | 18 15 46 | 16 18 41 |
igr | igr 2950 | 12 16 26 | 16 14 43 | 10 8 27 |
igs | igs 2968 | 13 15 21 | 16 14 41 | 11 10 24 |
jpl | jpl 2959 | 19 19 29 | 14 15 44 | 9 10 23 |
mit | mit 2976 | 25 27 43 | 16 13 47 | 10 9 25 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 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 6.1506 GPS week: 1506 MJD: 54786.500-54792.500
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 | -24 23 -17 -101 -1 | 6 19
| 29 30 76 40 10 | 2
emr uuuuu | -51 -4 -27 -187 0 | 45 52
| 54 16 120 150 9 | 3
esa uuuuu | 3 14 24 36 -2 | 14 22
| 14 14 114 90 5 | 2
gfz uuuuu | 8 28 -28 -38 5 | 11 22
| 17 22 81 71 5 | 3
grg xxxxx | -6 -5 -62 -103 -4 | -7 34
| 50 30 56 86 33 | 6
igr xxxxx | -1 47 67 -39 -1 | -5 23
| 12 11 55 80 12 | 3
irf xxxxx | 4 14 -8 39 5 | -4 20
| 10 12 53 40 6 | 2
jpl uuuuu | -13 7 23 11 -13 | 6 26
| 42 11 105 76 9 | 5
mit uuuuu | 19 -10 -36 153 1 | 13 25
| 20 24 100 111 10 | 2
ngs uuuuu | 9 -9 17 -27 3 | 12 24
| 38 31 84 119 16 | 3
sio uuxxu | 9 -50 -17 -98 4 | 23 33
| 45 29 109 80 13 | 2
Table 7.1506.0 GPS week: 1506 Day: 0 MJD: 54786.500
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 30 43 -58 12 | 6 13
emr uuuuu | -116 4 -21 -461 -17 | 51 55
esa uuuuu | 11 14 -36 137 5 | 16 20
gfz uuuuu | 15 -3 49 9 12 | 9 16
grg xxxxx | 27 -31 -67 -13 -41 | 3 32
igr xxxxx | -19 43 -33 -64 -17 | 1 16
irf xxxxx | 3 17 21 -9 -2 | -3 14
jpl uuuuu | 9 -3 -32 -10 -31 | 15 21
mit uuuuu | 11 -3 24 16 -6 | 15 22
ngs uuuuu | 20 15 27 126 35 | 13 29
sio uuxxu | 25 -56 129 -4 -14 | 27 32
Table 7.1506.1 GPS week: 1506 Day: 1 MJD: 54787.500
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 | -54 6 77 -99 12 | 3 15
emr uuuuu | -77 -6 -8 -276 -3 | 44 51
esa uuuuu | 0 14 70 16 -2 | 12 20
gfz uuuuu | -21 27 49 6 7 | 7 17
grg xxxxx | -80 -13 -76 -114 -51 | -4 40
igr xxxxx | -7 42 58 -26 -11 | -5 24
irf xxxxx | 10 11 77 19 -1 | -7 20
jpl uuuuu | 24 -8 -123 -40 -6 | 6 27
mit uuuuu | 49 3 85 96 -10 | 11 24
ngs uuuuu | -18 -6 -99 74 4 | 6 17
sio uuxxu | 36 -48 17 -68 -7 | 22 32
Table 7.1506.2 GPS week: 1506 Day: 2 MJD: 54788.500
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 | -48 22 -61 -168 0 | 6 20
emr uuuuu | -102 6 -21 -148 -2 | 45 53
esa uuuuu | -6 -4 -85 154 2 | 13 22
gfz uuuuu | -2 13 -15 -112 8 | 11 22
grg xxxxx | -55 0 -2 -201 1 | -7 41
igr xxxxx | -6 42 129 -111 -13 | -4 24
irf xxxxx | 11 27 10 3 -1 | -6 21
jpl uuuuu | 23 8 23 -127 -21 | 8 28
mit uuuuu | 28 -3 31 96 -10 | 12 25
ngs uuuuu | -11 -8 48 -6 10 | 8 20
sio uuxxu | 56 -9 -13 -170 -4 | 22 33
Table 7.1506.3 GPS week: 1506 Day: 3 MJD: 54789.500
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 | -58 8 -86 -85 -6 | 9 22
emr uuuuu | -55 -18 142 -44 15 | 46 54
esa uuuuu | 31 41 -102 -49 -4 | 16 25
gfz uuuuu | 2 42 -47 -64 3 | 14 25
grg xxxxx | -24 -33 -70 -101 42 | -14 33
igr xxxxx | 16 65 97 112 7 | -4 24
irf xxxxx | 11 14 -17 30 8 | -3 22
jpl uuuuu | -8 20 132 40 -11 | 7 27
mit uuuuu | 20 23 -53 61 9 | 14 26
ngs uuuuu | -21 -70 -11 24 -5 | 13 24
sio uuxxu | 37 -67 -120 -196 10 | 24 34
Table 7.1506.4 GPS week: 1506 Day: 4 MJD: 54790.500
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 68 -57 -121 -12 | 8 23
emr uuuuu | -20 -15 6 -234 3 | 45 53
esa uuuuu | -6 9 215 84 -8 | 14 25
gfz uuuuu | 32 53 -106 73 7 | 13 25
grg xxxxx | 7 27 -84 -86 -4 | -9 30
igr xxxxx | 14 55 108 -48 5 | -5 25
irf xxxxx | 9 29 -84 102 8 | -3 22
jpl uuuuu | -6 18 139 96 -11 | 4 28
mit uuuuu | 31 -9 -200 251 4 | 15 26
ngs uuuuu | -25 -22 -66 -224 0 | 12 24
sio uuxxu | 13 -40 -88 -58 11 | 23 34
Table 7.1506.5 GPS week: 1506 Day: 5 MJD: 54791.500
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 | 17 -23 -99 -54 -6 | 7 21
emr uuuuu | -26 -24 -25 -109 5 | 43 50
esa uuuuu | 1 13 -4 -68 -2 | 13 23
gfz uuuuu | 23 52 -157 -63 -2 | 14 25
grg xxxxx | 64 -27 16 11 27 | -9 30
igr xxxxx | 1 51 79 -8 11 | -6 24
irf xxxxx | -4 -7 -59 80 12 | -3 22
jpl uuuuu | -40 4 98 60 -9 | 2 26
mit uuuuu | 3 -32 -132 300 10 | 14 26
ngs uuuuu | 38 24 146 -99 -11 | 14 26
sio uuxxu | -28 -100 -149 -17 21 | 23 33
Table 7.1506.6 GPS week: 1506 Day: 6 MJD: 54792.500
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 51 66 -127 -9 | 4 20
emr uuuuu | 41 23 -264 -40 -1 | 40 46
esa uuuuu | -7 14 111 -26 -5 | 10 21
gfz uuuuu | 5 12 34 -120 1 | 12 24
grg xxxxx | 20 43 -154 -218 -1 | -11 28
igr xxxxx | -9 31 32 -132 10 | -9 22
irf xxxxx | -15 8 -1 44 9 | -4 21
jpl uuuuu | -94 10 -79 56 -5 | -1 25
mit uuuuu | -12 -50 -5 246 11 | 12 23
ngs uuuuu | 77 5 76 -89 -9 | 14 26
sio uuxxu | -73 -33 106 -174 13 | 22 32
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