[IGSREPORT-19519] Wk 1623 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Mar 3 04:58:13 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1623 (Feb 13, 2011 - Feb 19, 2011)
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 (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 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:
igs1623[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1623[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1623[0-6].cls IGS GPS clock combination summary report.
igs16237.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16237.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 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | EMR | 3 3 6 WTZR WTZR
0 | ESA | UNSA
0 | GFZ | 19 BRUS GOLD HARB MAW1
0 | GRG | AMC2 SANT
0 | JPL | 3 6 25
0 | MIT | 3 6 3 6 HARB
1 | COD | 19
1 | EMR | 3 6 WTZR WTZR
1 | ESA | UNSA
1 | GFZ | ALIC FAA1 MDVJ WTZR
1 | GRG | ADIS AMC2 SANT
1 | JPL | 3 6 25
1 | MIT | 3 9 3 6 9 19 27 HARB
2 | EMR | WTZR HARB SUTM WTZR
2 | GFZ | 9 FAA1 MAC1 THU3
2 | GRG | ADIS AMC2 MDVJ SANT
2 | JPL | 3 6 25 HARB
2 | MIT | 3 4 6 3 4 6 DAV1 PTBB CAS1 DAV1 MDVJ PTBB
3 | COD | 32
3 | EMR | 3 3 WTZR WTZR
3 | ESA | 32 ALIC UNSA
3 | GFZ | MDVJ
3 | GRG | ADIS AMC2 SANT
3 | JPL | 6 25 32
3 | MIT | 6 21 6 21 28 CAS1 HARB CAS1 HARB SFER
4 | COD | SOFI
4 | EMR | 3 6 WTZR WTZR
4 | GFZ | ALIC ALRT BRMU BRUS KIRU MDVJ RAMO
4 | GRG | ADIS AMC2 SANT
4 | JPL | 6 25
4 | MIT | 6 21 6 21 DAV1
5 | COD | RAMO SOFI WROC
5 | EMR | WTZR YELL WTZR YELL
5 | ESA | UNSA
5 | GFZ | 6 21 DAV1 LAMA
5 | GRG | ADIS SANT
5 | JPL | 25 BAKE DAV1
5 | MIT | DAV1 DAV1
6 | COD | HARB
6 | EMR | WTZR WTZR
6 | ESA | RAMO UNSA
6 | GFZ | 32 DAV1 LAMA ONSA
6 | GRG | ADIS NRC1 SANT
6 | JPL | 6 25 32
6 | MIT | 6 32 6 32 DAV1 BOR1 DAV1 HARB
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
----+------------+----------
G21 | 2011_02_15 | 2011015
6. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | GRG | 21
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 all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .1 .3 1.3 0 5 -14 .04
EMR | 2.5 6.5 .8 50 -6 6 .08
ESA | 3.4 5.0 -1.8 145 20 -113 .03
GFZ | -.5 .5 .9 -6 28 -52 .20
GRG | 1.7 7.4 2.4 33 76 -100 .35
JPL | .5 7.9 8.3 31 -10 50 -.03
MIT | 2.2 .2 -5.8 0 -5 -22 .04
NGS | 4.9 -1.2 -1.1 -14 -93 20 .01
SIO | 8.5 1.1 -1.2 25 -167 20 .25
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 IGN. 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 1.1623.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1623.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 2.1623.[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 3.1623.[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 5.1623.0-6).
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 1623 summary. (Feb 13, 2011 - Feb 19, 2011)
Table 1.1623.a GPS week: 1623 MJD: 55605.000-55611.000
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 234| 0 0 3 47 -17 24 -.23 9 9 | 13 -1042 17 87
| 0 0 1 21 13 19 .03 | 516 927
emr 87| 0 0 4 -74 43 29 .40 19 19 | -1564 40 18 105
| 1 1 1 30 41 13 .04 | 813 1181
esa 148| 2 0 -4 -157 -93 -95 .23 8 7 | 230 -1371 14 126
| 0 0 1 29 30 28 .04 | 951 1757
gfz 190| 0 -1 -2 53 -74 27 -.19 11 11 | 149 -167 21 103
| 1 0 0 73 54 13 .03 | 277 562
grg 133| 2 0 -8 -21 -137 -27 .65 16 15 | -20 36 50 225
| 0 1 2 25 20 12 .05 | 294 526
igr n/a| 0 0 0 51 9 3 -.03 5 5 | 7933 -271 18 76
| 0 0 1 16 29 17 .04 | 588 1161
jpl 147| -1 0 7 -12 19 11 .48 20 19 | 2278 97 18 97
| 1 1 1 22 22 33 .05 | 989 1177
mit 261| 0 0 -1 71 -22 26 -.35 11 9 | -258 239 20 144
| 0 0 0 31 22 14 .05 | 279 538
ngs 225| -1 0 0 103 161 10 -.20 11 9 | -285816 601476 2247 3696
| 0 0 1 38 34 13 .04 | 487879 1119021
sio 261| 0 1 8 2 339 83 -.21 19 18 | --- --- --- ---
| 0 0 0 33 26 11 .03 | --- ---
Table 1.1623.b GPS week : 1623 MJD: 55605.000-55611.000
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 5 |
3 | 8 8 7 7 6 6 6 |
4 | 3 3 4 3 4 4 4 |
5 | 4 4 4 4 4 5 4 |
6 | 5 5 5 5 5 6 6 |
7 | 4 4 4 5 4 4 4 |
8 | 4 4 4 4 4 4 4 |
9 | 4 3 4 4 4 5 4 |
10 | 3 3 4 3 4 4 4 |
11 | 5 5 4 5 5 5 5 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 5 5 4 4 5 |
14 | 5 4 4 4 5 5 4 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 5 4 5 4 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 5 5 4 |
20 | 5 5 5 5 5 5 5 |
21 | 5 4 0 6 5 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 5 5 4 4 4 4 5 |
25 | 5 5 5 5 5 5 5 |
26 | 4 4 5 5 5 5 5 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 4 3 3 4 3 3 4 |
31 | 5 5 4 5 4 5 5 |
32 | 5 5 4 9 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1623.0 GPS week: 1623 Day: 0 MJD: 55605.000
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 234| 0 0 5 59 2 12 -.20 9 9 | -287 -167 18 83
| 5 -27 |
emr 87| 0 2 4 -67 51 28 .38 19 19 | -1326 -647 16 100
| 68 -31 |
esa 148| 2 0 -3 -118 -92 -102 .26 8 8 | 946 -3642 13 116
| 58 61 |
gfz 190| 0 -1 -2 11 -79 7 -.15 11 11 | 526 -697 21 92
| -57 37 |
grg 133| 2 -1 -10 -45 -137 -33 .64 16 15 | 64 -185 44 216
| 132 -30 |
igr n/a| 0 0 -2 42 41 4 -.00 6 5 | 8003 -405 16 69
| -26 22 |
jpl 147| -2 0 9 3 29 58 .47 20 19 | 1665 -444 16 100
| 21 9 |
mit 261| -1 0 -1 53 -50 29 -.42 12 9 | 37 -94 23 155
| -2 42 |
ngs 225| 0 0 -2 103 174 31 -.24 11 8 | -317 -133 2332 3735
| 21 -10 |
sio 261| -1 0 8 -28 315 78 -.17 21 18 | --- --- --- ---
| 4 -101 |
Table 2.1623.1 GPS week: 1623 Day: 1 MJD: 55606.000
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 234| 0 -1 6 29 -11 55 -.21 10 10 | 627 -2138 15 92
| 55 -11 |
emr 87| -3 1 4 -99 0 8 .37 20 20 | -1727 -733 19 108
| 86 14 |
esa 148| 1 1 -3 -137 -102 -63 .22 7 6 | -228 -1956 11 132
| 48 57 |
gfz 190| 0 -1 -2 119 28 17 -.18 9 9 | 207 -741 20 119
| -34 31 |
grg 133| 2 1 -11 -22 -100 -23 .60 15 13 | 27 -569 56 218
| 94 -57 |
igr n/a| 0 0 -1 51 -24 -11 -.04 4 4 | 8257 -792 15 66
| -17 4 |
jpl 147| 0 0 8 -41 18 -26 .42 21 19 | 1864 -587 18 88
| 5 -82 |
mit 261| -1 0 -1 94 -32 30 -.41 13 9 | -297 -591 17 127
| -12 30 |
ngs 225| 0 0 -1 52 110 -9 -.20 11 7 | -999999 1343181 2238 3911
| 81 33 |
sio 261| 0 0 9 5 328 76 -.22 19 17 | --- --- --- ---
| 10 -101 |
Table 2.1623.2 GPS week: 1623 Day: 2 MJD: 55607.000
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 234| 0 0 4 34 -24 25 -.22 8 8 | -666 267 15 82
| 45 18 |
emr 87| -1 0 2 -117 -19 43 .36 18 18 | -2440 1017 19 110
| 102 54 |
esa 148| 2 -1 -3 -195 -54 -122 .31 7 7 | -1 -1806 16 138
| 31 86 |
gfz 190| 0 -1 -2 161 -48 31 -.15 10 9 | -326 852 23 113
| 14 71 |
grg 133| 1 0 -9 -53 -144 -9 .58 16 16 | -663 1086 42 258
| 131 -37 |
igr n/a| 0 1 -1 22 9 27 -.02 5 5 | 7490 735 25 109
| -1 57 |
jpl 147| 0 2 6 -21 -13 -26 .41 19 18 | 1357 1006 18 91
| -27 46 |
mit 261| 0 0 -1 102 -2 43 -.39 12 9 | -832 1175 19 114
| -10 19 |
ngs 225| -1 0 0 80 119 21 -.23 13 10 | -747 356 1962 3447
| 9 85 |
sio 261| 0 0 8 29 368 103 -.25 18 16 | --- --- --- ---
| 0 -112 |
Table 2.1623.3 GPS week: 1623 Day: 3 MJD: 55608.000
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 234| 0 0 3 14 -7 26 -.20 9 8 | -210 -1139 21 83
| 45 7 |
emr 87| 0 1 3 -74 37 15 .39 19 19 | -1431 -1428 20 111
| 19 12 |
esa 148| 2 0 -5 -179 -71 -140 .24 13 10 | -1020 1782 18 131
| 37 81 |
gfz 190| 1 0 0 72 -119 22 -.22 10 11 | 40 76 24 106
| -33 54 |
grg 133| 0 1 -8 -36 -129 -13 .70 17 15 | 192 -326 58 204
| 79 -74 |
igr n/a| 0 0 -1 51 -7 -21 .03 6 5 | 8162 -1598 22 92
| -37 36 |
jpl 147| -1 0 6 -32 -1 25 .49 19 18 | 2356 -1257 22 120
| -67 44 |
mit 261| 0 0 -1 55 -37 8 -.33 11 9 | -56 105 17 146
| -2 25 |
ngs 225| -2 -1 0 109 162 4 -.16 12 10 | -159 -1279 2261 3233
| -108 82 |
sio 261| 0 2 8 -10 329 83 -.18 18 16 | --- --- --- ---
| 12 -105 |
Table 2.1623.4 GPS week: 1623 Day: 4 MJD: 55609.000
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 234| 0 0 2 62 -33 -7 -.21 9 9 | 763 -2026 19 94
| -14 -5 |
emr 87| -1 0 4 -21 73 33 .42 20 20 | -2742 2086 18 115
| -19 -51 |
esa 148| 1 0 -5 -137 -70 -83 .22 7 7 | -614 -176 16 119
| 36 87 |
gfz 190| -2 -1 -1 -62 -111 49 -.17 12 11 | 346 -396 21 93
| -52 91 |
grg 133| 3 1 -6 -2 -152 -26 .65 16 15 | -12 96 55 225
| 10 -72 |
igr n/a| 0 0 0 68 47 18 -.05 5 4 | 6859 1821 15 71
| -33 36 |
jpl 147| -1 -1 6 25 14 -12 .52 22 21 | 1420 2280 19 94
| 14 -85 |
mit 261| 0 0 0 18 -36 44 -.34 10 9 | -200 387 22 145
| 8 10 |
ngs 225| 0 -1 2 178 174 15 -.24 10 8 | 746 -2034 2134 3519
| -114 5 |
sio 261| 1 1 8 -45 305 94 -.20 17 17 | --- --- --- ---
| 12 -93 |
Table 2.1623.5 GPS week: 1623 Day: 5 MJD: 55610.000
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 234| -2 0 1 59 -30 35 -.27 10 9 | -225 -546 17 99
| 54 27 |
emr 87| 1 0 5 -63 101 40 .38 20 20 | -725 56 18 90
| 40 -64 |
esa 148| 2 0 -3 -147 -117 -83 .18 7 7 | 1609 -1232 13 116
| 29 74 |
gfz 190| 0 -2 -1 38 -130 23 -.24 15 14 | -10 131 22 106
| -54 131 |
grg 133| 2 0 -4 -11 -134 -34 .66 16 15 | 46 128 58 247
| 60 -85 |
igr n/a| 0 0 1 54 -22 0 -.08 5 5 | 8671 -720 16 61
| 12 36 |
jpl 147| -1 -1 8 -3 50 37 .53 20 19 | 3659 -132 20 95
| 26 -1 |
mit 261| 0 0 -1 77 -12 20 -.32 10 9 | -187 327 24 161
| 3 19 |
ngs 225| -1 -1 0 106 188 7 -.17 11 8 | -243 -564 2157 3763
| -26 22 |
sio 261| 0 2 7 16 349 75 -.22 19 18 | --- --- --- ---
| 4 -115 |
Table 2.1623.6 GPS week: 1623 Day: 6 MJD: 55611.000
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 234| -1 0 2 71 -13 23 -.27 9 8 | 90 -1549 18 80
| 39 9 |
emr 87| 0 1 8 -73 58 38 .48 20 20 | -558 -69 16 105
| 80 -9 |
esa 148| 3 0 -3 -188 -143 -69 .21 7 7 | 922 -2573 16 134
| 42 112 |
gfz 190| 0 -3 -3 34 -62 37 -.22 12 11 | 266 -394 22 97
| -51 98 |
grg 133| 3 3 -6 19 -164 -47 .72 18 15 | 203 22 43 212
| 15 10 |
igr n/a| 0 0 0 71 21 8 -.06 5 4 | 8089 -942 18 70
| -21 24 |
jpl 147| 0 0 7 -18 40 23 .52 21 19 | 3631 -185 18 96
| 13 5 |
mit 261| 0 0 -1 101 13 8 -.27 10 9 | -272 369 21 161
| 9 19 |
ngs 225| -1 0 -1 93 203 2 -.17 12 10 | -999999 2870805 2648 4264
| -47 10 |
sio 261| 0 1 9 49 377 71 -.22 20 23 | --- --- --- ---
| -10 -116 |
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1623.0 GPS week: 1623 Day: 0 MJD: 55605.000
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 --- --- --- --- 82 --- --- --- --- 0 | 44 --- --- --- --- 85 --- --- --- --- 44
2 | 9 22 6 12 13 9 24 7 14 23 4 | 20 27 16 19 21 17 27 21 27 20 16
3E | 19 19 12 15 23 9 19 38 21 28 8 | 84 90 89 94 95 91 91 107 63 89 92
4 | 7 11 7 9 14 6 10 8 8 14 3 | 23 26 26 26 37 27 28 30 29 24 25
5 | 8 13 7 11 10 6 15 9 11 27 4 | 28 33 33 33 37 31 30 32 33 31 30
6E | 12 18 7 13 20 8 19 18 12 16 5 | 37 38 33 34 30 33 32 44 41 30 33
7 | 7 22 7 8 21 6 18 9 8 17 4 | 12 23 19 14 31 15 23 13 18 20 13
8 | 8 13 7 10 11 4 10 14 7 19 3 | 19 27 23 22 25 22 28 21 23 28 20
9 | 11 15 5 10 11 4 14 6 6 16 3 | 16 22 18 15 22 12 19 14 16 18 13
10 | 8 11 5 10 9 5 9 9 7 23 3 | 28 31 31 28 36 28 31 35 32 30 28
11 | 10 15 8 11 20 5 16 13 9 24 4 | 22 33 33 22 46 25 35 25 25 21 24
12 | 9 24 6 11 18 4 24 9 9 24 4 | 18 33 17 18 24 18 32 15 17 16 15
13 | 9 18 6 13 18 5 23 6 10 16 4 | 17 26 16 16 31 15 29 13 16 16 15
14 | 8 20 8 10 17 6 25 6 10 18 4 | 16 29 19 16 27 17 30 17 20 17 15
15 | 9 30 9 13 19 5 27 11 10 20 5 | 19 39 21 18 28 17 36 16 19 22 18
16 | 7 23 6 13 15 6 24 11 11 30 5 | 17 29 17 17 23 17 33 20 22 29 16
17E | 7 18 5 8 14 5 24 9 8 8 3 | 24 29 24 25 25 22 30 26 25 22 24
18 | 12 19 8 15 14 5 22 9 10 27 5 | 28 33 31 35 37 28 34 29 31 30 29
19E | 7 18 9 12 14 5 27 16 15 16 5 | 33 29 29 35 28 32 34 35 38 36 30
20 | 7 14 9 14 13 4 18 13 7 30 4 | 29 34 36 29 37 30 31 35 32 43 30
21 | 11 21 8 8 12 10 27 9 11 23 4 | 9 22 12 9 11 11 23 8 12 9 7
22 | 9 15 9 8 13 6 24 8 9 17 4 | 33 35 35 37 42 31 34 33 33 35 33
23 | 7 22 7 13 17 5 30 10 13 14 5 | 20 34 20 21 32 21 38 16 26 22 20
24 | 9 16 11 9 11 4 14 18 9 34 5 | 27 31 33 28 38 29 37 34 28 34 28
X25 | 12 16 7 9 17 5 24 12 11 --- 5 | 17 25 21 16 33 16 38 21 18 --- 17
26 | 9 19 7 13 10 4 14 8 11 22 4 | 18 24 16 21 21 18 24 19 23 21 17
27 | 12 18 9 10 13 4 11 13 8 17 4 | 14 25 19 17 22 13 19 16 18 19 14
28 | 8 19 6 10 21 6 17 6 8 20 4 | 20 31 22 25 30 21 31 21 19 22 20
29E | 11 26 10 9 16 6 30 11 13 13 5 | 16 22 21 20 19 17 24 19 18 20 15
30 | 7 13 8 9 17 6 9 7 10 8 3 | 19 18 18 18 23 16 18 21 20 21 16
31 | 8 22 9 14 18 4 20 10 9 17 4 | 21 28 20 19 33 19 29 19 25 19 17
32 | 9 14 8 13 14 7 19 11 9 28 4 | 17 23 26 21 26 18 22 20 22 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 8 11 16 6 20 12 11 21 |T 23 30 25 24 31 25 31 25 25 26 23
WRMS | 9 19 8 11 15 5 19 9 8 18 |NE 21 28 23 21 29 22 29 21 23 23 20
MEDI | 9 18 7 11 14 5 19 9 10 19 |MD 20 29 21 21 30 19 30 21 23 22 19
Table 3.1623.1 GPS week: 1623 Day: 1 MJD: 55606.000
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 --- --- --- --- 49 --- --- --- --- 0 | 32 --- --- --- --- 56 --- --- --- --- 32
2 | 12 24 5 15 11 4 25 6 8 21 4 | 20 27 18 20 20 20 28 20 22 20 18
3E | 18 29 11 10 15 4 18 34 22 32 7 | 77 90 80 78 85 80 86 84 53 88 79
4 | 8 12 3 8 14 3 13 9 5 13 3 | 20 20 22 22 25 21 25 23 21 19 21
5 | 12 15 4 9 10 4 17 7 9 23 4 | 18 24 23 21 31 23 26 22 21 19 20
6E | 12 23 7 9 12 4 18 20 15 15 5 | 32 30 26 31 25 28 28 41 32 22 28
7 | 9 19 7 7 20 5 17 8 4 17 4 | 17 26 21 11 35 15 25 13 13 19 16
8 | 10 15 5 6 11 4 12 8 9 20 3 | 21 31 27 22 29 23 31 26 23 31 25
9 | 10 17 4 4 12 4 13 9 12 10 3 | 13 24 16 15 20 15 23 17 14 14 15
10 | 11 11 3 8 11 4 11 6 7 21 3 | 21 22 22 24 29 23 24 23 23 20 22
11 | 13 16 7 9 23 5 23 14 10 23 5 | 19 29 26 22 42 19 29 23 21 20 21
12 | 11 24 6 9 19 4 26 8 11 20 4 | 18 32 18 15 26 18 32 18 17 16 17
13 | 8 17 5 8 25 4 23 8 9 14 4 | 19 29 20 13 39 18 28 19 15 18 18
14 | 10 18 7 5 16 5 24 8 12 16 4 | 13 26 19 13 26 16 27 16 17 16 17
15 | 11 27 6 9 17 3 25 9 9 16 4 | 17 32 21 19 28 17 27 19 15 20 16
16 | 6 27 7 10 14 6 26 11 9 26 4 | 16 25 18 12 24 14 28 14 20 25 14
17E | 6 14 7 8 19 3 27 13 11 6 4 | 21 25 24 21 26 22 30 26 25 19 22
18 | 12 17 6 17 12 3 20 8 11 27 4 | 18 30 29 34 28 26 32 24 23 23 26
19E | 9 19 6 8 15 4 28 25 13 9 5 | 25 22 23 25 24 21 28 32 24 24 21
20 | 8 17 7 7 9 4 20 16 10 30 4 | 19 25 23 18 27 19 27 26 19 34 19
21 | 10 18 9 8 13 3 23 8 10 21 4 | 9 21 13 7 14 10 23 11 9 10 10
22 | 12 12 7 7 9 4 21 8 8 19 3 | 18 27 26 21 29 24 29 23 24 24 24
23 | 8 24 8 10 21 3 31 10 9 13 4 | 25 32 28 21 35 21 34 22 20 21 21
24 | 5 18 7 8 14 4 17 17 9 29 4 | 21 24 28 25 29 22 26 31 23 33 24
X25 | 9 15 5 8 14 5 25 12 14 --- 4 | 13 22 17 16 30 14 37 20 12 --- 15
26 | 14 16 5 8 12 5 13 7 9 22 4 | 25 23 22 26 21 21 24 23 25 20 20
27 | 11 22 6 5 11 4 13 9 12 17 4 | 16 27 21 15 24 17 26 17 14 17 16
28 | 8 22 6 6 19 3 20 6 6 16 4 | 23 33 27 18 36 23 35 22 21 23 23
29E | 12 31 9 10 17 6 27 9 15 12 5 | 17 27 22 19 20 18 24 18 18 16 16
30 | 5 15 5 8 14 4 11 8 7 9 3 | 18 17 18 16 24 17 20 17 17 18 17
31 | 9 25 6 13 18 4 20 8 10 14 4 | 15 30 22 19 36 17 28 17 19 17 20
32 | 14 19 7 8 11 5 19 12 9 23 4 | 28 27 33 24 28 23 29 28 23 29 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 7 9 15 4 21 13 11 19 |T 21 28 24 21 29 22 29 23 20 23 21
WRMS | 10 20 6 9 13 4 19 9 7 17 |NE 18 26 22 18 28 20 27 20 18 21 19
MEDI | 10 18 6 8 14 4 20 9 9 17 |MD 19 27 22 20 28 20 28 22 21 20 20
Table 3.1623.2 GPS week: 1623 Day: 2 MJD: 55607.000
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 --- --- --- --- 69 --- --- --- --- 0 | 19 --- --- --- --- 62 --- --- --- --- 22
2 | 11 20 6 12 14 4 25 8 12 19 4 | 18 23 15 20 18 13 25 17 16 17 16
3E | 17 19 8 12 19 7 20 33 21 38 7 | 68 74 72 69 78 68 75 72 59 81 69
4 | 8 12 6 8 10 3 12 8 15 14 3 | 20 21 22 21 25 19 22 22 16 19 20
5 | 8 13 7 8 8 4 17 11 17 20 4 | 19 26 26 22 27 22 26 23 21 22 22
6E | 10 21 9 10 16 5 18 21 15 15 5 | 35 36 33 34 29 36 36 46 40 29 35
7 | 8 20 7 9 21 5 18 9 11 16 4 | 13 27 18 14 35 16 24 16 17 23 16
8 | 7 15 5 9 9 5 10 7 11 20 3 | 26 31 30 24 34 23 31 21 19 32 28
9 | 8 13 5 12 15 5 11 7 12 17 3 | 16 21 17 20 23 14 23 15 15 17 16
10 | 8 11 6 9 10 4 9 6 13 18 3 | 19 24 25 25 29 24 25 23 20 22 22
11 | 7 16 7 10 23 4 20 7 9 15 4 | 17 26 23 21 38 18 29 20 17 19 21
12 | 7 22 9 10 17 5 22 10 9 19 4 | 16 27 19 15 25 15 28 17 16 18 17
13 | 7 15 6 13 22 4 22 8 13 12 4 | 15 23 18 17 35 15 27 16 19 17 17
14 | 6 16 6 7 18 4 19 8 15 13 4 | 12 25 20 14 26 16 27 15 15 19 17
15 | 8 23 6 7 16 3 23 8 13 16 4 | 16 30 20 15 27 14 30 17 12 21 17
16 | 6 23 10 11 18 8 25 10 11 21 4 | 13 25 22 12 23 16 31 15 16 22 15
17E | 6 15 7 9 14 4 19 10 10 8 3 | 16 21 18 16 21 15 25 20 15 16 18
18 | 9 16 8 15 13 5 20 12 21 25 5 | 22 34 29 32 33 28 33 26 30 23 28
19E | 6 21 8 9 15 10 26 17 11 13 4 | 22 27 22 24 24 23 31 24 25 26 22
20 | 6 12 9 10 11 7 18 14 10 30 4 | 21 29 28 25 33 24 31 28 25 38 25
X21 | 5 --- --- --- --- 42 --- --- --- --- 0 | 14 --- --- --- --- 53 --- --- --- --- 18
22 | 8 15 9 8 11 5 21 13 13 17 4 | 25 29 27 24 35 25 32 25 27 26 27
23 | 7 23 9 13 16 6 29 11 10 11 4 | 17 29 17 20 28 15 34 16 21 18 16
24 | 6 15 7 7 16 4 14 8 10 16 3 | 21 27 25 25 31 23 31 29 22 28 25
X25 | 7 15 8 10 15 6 22 12 16 --- 4 | 14 25 19 14 29 13 35 17 15 --- 16
26 | 11 23 9 8 11 3 13 9 13 25 4 | 20 28 22 21 17 17 22 21 19 18 18
27 | 10 16 8 7 14 4 13 10 12 20 4 | 16 25 18 22 24 17 27 22 20 26 18
28 | 6 20 6 9 18 5 20 7 8 15 4 | 16 28 21 15 31 16 31 16 14 17 19
29E | 9 21 8 12 19 6 28 12 13 9 5 | 15 23 23 22 21 19 25 21 22 22 20
30 | 5 12 8 7 14 6 12 8 12 8 3 | 13 17 19 13 22 13 18 16 15 18 15
31 | 6 20 7 10 23 5 22 7 11 12 4 | 14 28 22 14 35 18 27 14 16 13 18
32 | 8 17 8 8 15 8 15 9 9 19 4 | 15 22 21 21 29 16 21 23 17 25 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 10 16 5 19 12 13 18 |T 19 27 23 21 29 22 29 22 20 23 21
WRMS | 8 18 7 9 16 5 18 9 10 16 |NE 17 26 21 19 28 20 27 19 18 21 19
MEDI | 7 16 7 9 15 5 19 9 12 16 |MD 16 26 22 21 28 17 27 20 17 22 18
Table 3.1623.3 GPS week: 1623 Day: 3 MJD: 55608.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 4 --- --- --- --- 240 --- --- --- --- 0 | 36 --- --- --- --- 249 --- --- --- --- 37
2 | 9 25 11 14 14 5 22 8 9 20 5 | 20 31 23 18 17 18 29 20 24 19 17
3E | 20 19 11 11 25 10 18 25 19 32 7 | 93 100 98 95 104 96 100 98 55 97 96
4 | 5 13 8 10 13 4 11 8 9 12 3 | 19 20 25 19 26 21 22 21 20 20 19
5 | 6 16 6 9 7 5 19 9 10 21 3 | 22 29 28 29 31 27 27 28 28 25 25
6E | 12 21 8 11 23 9 15 17 13 20 5 | 32 35 31 35 28 32 32 39 36 25 30
7 | 7 23 9 9 17 5 19 11 11 18 4 | 11 25 21 14 31 14 23 13 18 20 12
8 | 6 14 7 8 11 3 11 10 11 20 3 | 20 27 23 21 26 21 28 21 26 30 22
9 | 8 19 7 11 13 6 18 8 13 11 4 | 15 23 17 17 21 15 25 15 20 11 14
10 | 8 13 6 8 9 4 10 7 8 18 3 | 23 26 30 28 31 28 27 27 29 25 26
11 | 6 17 9 7 23 4 18 8 14 17 4 | 17 26 25 19 40 19 25 17 25 15 18
12 | 7 23 9 11 18 6 22 9 11 19 4 | 14 27 18 17 25 15 30 18 22 14 15
13 | 7 17 9 9 25 5 19 7 13 12 4 | 15 28 24 18 36 17 23 17 19 17 16
14 | 6 19 11 6 19 6 21 10 11 15 4 | 17 27 19 16 30 16 28 19 24 21 18
15 | 9 26 11 10 19 6 28 11 13 16 5 | 15 30 20 17 26 15 29 17 22 18 15
16 | 6 24 12 11 22 5 25 9 11 24 5 | 14 27 18 17 25 15 31 15 19 21 14
17E | 6 20 8 12 14 4 24 11 11 9 4 | 22 26 20 23 27 20 29 21 19 19 20
18 | 9 18 8 14 13 6 22 9 11 22 4 | 21 32 29 35 35 26 31 30 27 26 27
19E | 9 20 10 11 14 4 23 13 16 14 5 | 22 24 21 24 22 20 25 23 24 24 18
20 | 7 16 10 14 12 5 16 10 13 32 5 | 25 31 33 29 35 26 30 27 29 39 26
X21 | 9 --- 10 --- 682 13 --- 8 13 --- 5 | 11 --- 18 --- 304 15 --- 10 18 --- 13
22 | 7 16 9 11 13 6 22 10 10 17 4 | 27 34 32 35 39 27 31 33 33 29 31
23 | 9 21 10 10 21 3 27 9 12 13 5 | 20 30 24 19 31 21 31 19 24 20 18
24 | 6 16 8 7 16 4 12 9 12 13 3 | 24 24 30 25 33 23 26 23 27 20 23
X25 | 8 15 6 9 21 6 23 10 14 --- 4 | 18 27 21 19 36 18 37 23 20 --- 20
26 | 10 19 9 8 12 3 14 10 15 24 4 | 23 28 30 26 21 24 26 25 32 24 23
27 | 11 19 8 10 13 6 14 9 11 12 4 | 27 35 31 27 31 29 31 27 33 26 26
28 | 5 22 7 9 15 4 22 8 10 16 4 | 17 32 23 21 31 18 31 18 15 18 18
29E | 8 17 9 11 19 5 26 11 15 11 4 | 10 17 16 17 18 13 24 18 24 17 13
30 | 6 11 9 7 20 4 11 8 12 11 3 | 18 22 19 22 29 19 22 19 21 17 19
31 | 8 19 14 10 21 5 18 8 12 16 4 | 17 28 22 21 37 17 24 14 22 17 18
32 | 11 12 54 14 14 10 16 13 17 19 8 | 29 31 74 32 35 29 32 33 32 33 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 13 10 17 6 19 11 12 18 |T 22 30 27 25 40 30 30 24 25 24 23
WRMS | 8 19 10 11 15 5 18 9 10 16 |NE 19 28 26 22 40 28 27 21 24 21 20
MEDI | 7 19 9 10 16 5 19 9 12 17 |MD 20 27 23 21 31 20 28 21 24 20 19
Table 3.1623.4 GPS week: 1623 Day: 4 MJD: 55609.000
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 --- --- --- --- 222 --- --- --- --- 0 | 26 --- --- --- --- 231 --- --- --- --- 28
2 | 10 26 6 12 14 4 27 9 6 19 4 | 21 30 16 21 22 18 31 22 21 21 18
3E | 22 21 7 17 21 8 18 17 17 23 6 | 54 66 62 66 70 63 66 69 63 67 63
4 | 9 15 7 10 13 3 13 7 9 14 3 | 18 20 17 21 24 17 24 20 19 19 17
5 | 8 15 7 9 9 3 21 9 11 19 4 | 20 27 25 27 29 23 26 23 27 23 22
6E | 14 20 7 14 21 3 18 16 12 24 5 | 43 38 38 40 38 39 38 49 43 32 39
7 | 8 22 7 9 19 4 20 8 9 14 4 | 15 26 19 13 35 16 27 14 20 20 15
8 | 9 19 9 10 10 3 16 10 9 20 4 | 17 24 22 14 26 18 27 17 21 29 17
9 | 9 18 6 10 10 4 22 9 13 13 4 | 15 23 17 14 22 13 27 16 16 16 14
10 | 7 11 5 7 11 3 9 8 10 20 3 | 21 22 25 22 28 22 26 26 21 23 22
11 | 10 18 7 11 22 4 23 10 6 16 4 | 17 31 23 21 42 19 27 19 19 17 18
12 | 10 26 8 13 18 5 26 9 7 18 4 | 15 28 19 15 25 15 30 16 15 11 12
13 | 6 15 6 10 24 5 20 6 7 12 4 | 15 24 18 17 36 17 30 17 17 17 15
14 | 8 20 7 13 15 5 29 10 9 14 4 | 17 29 20 17 30 17 30 20 20 24 16
15 | 9 29 6 13 16 4 31 9 9 14 4 | 17 30 19 18 27 14 29 18 15 20 15
16 | 5 22 7 15 16 5 25 8 9 22 4 | 17 28 17 20 22 19 31 20 20 23 16
17E | 5 19 5 12 16 5 23 11 9 9 4 | 21 26 21 20 25 17 27 26 22 21 20
18 | 11 20 4 15 11 4 25 11 6 21 4 | 26 28 32 33 38 26 31 29 28 26 27
19E | 9 21 8 16 18 4 28 10 10 16 4 | 26 32 24 31 30 27 33 28 24 34 26
20 | 9 16 7 15 9 6 17 10 10 32 4 | 29 35 35 28 34 29 33 31 30 42 30
X21 | 7 23 7 10 17 8 32 8 7 --- 4 | 15 25 17 9 137 16 25 10 14 --- 13
22 | 9 16 5 13 10 6 26 11 8 15 4 | 33 36 39 37 44 32 32 33 35 32 34
23 | 7 21 9 11 19 5 29 10 10 12 4 | 17 26 22 18 29 19 32 15 22 16 15
24 | 8 16 8 11 12 4 19 8 8 11 3 | 24 26 28 24 34 24 31 24 22 23 24
X25 | 9 17 7 12 20 4 26 11 12 --- 4 | 15 23 20 14 32 14 35 17 17 --- 15
26 | 11 21 10 8 10 3 13 14 16 23 4 | 21 26 23 26 20 19 21 24 24 21 19
27 | 10 19 5 10 10 4 21 9 13 11 4 | 13 22 13 15 25 11 29 14 14 14 12
28 | 6 23 10 10 16 3 22 7 7 16 4 | 16 30 21 18 29 16 31 19 19 19 17
29E | 8 25 7 8 22 8 27 8 10 11 4 | 19 25 17 15 20 19 23 18 21 18 16
30 | 5 13 5 11 16 5 15 6 7 9 3 | 16 20 19 22 22 19 18 19 22 19 17
31 | 8 19 7 11 19 6 22 8 11 16 4 | 14 28 19 17 31 18 25 21 23 26 16
32 | 10 16 5 12 8 5 18 9 11 16 3 | 19 23 28 24 26 21 23 22 25 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 7 12 16 5 22 10 10 17 |T 21 28 23 22 33 27 29 23 23 23 20
WRMS | 9 20 7 11 15 4 21 9 8 17 |NE 18 26 22 20 33 26 28 20 21 21 18
MEDI | 9 19 7 11 16 4 22 9 9 16 |MD 17 26 21 20 29 19 29 20 21 21 17
Table 3.1623.5 GPS week: 1623 Day: 5 MJD: 55610.000
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 --- --- --- --- 57 --- --- --- --- 31
2 | 10 26 7 15 16 5 28 10 11 18 5 | 17 29 18 21 21 19 29 21 20 18 17
3E | 21 21 9 23 17 11 16 16 13 23 6 | 88 94 92 91 97 90 95 89 74 98 91
4 | 7 13 6 11 14 6 10 8 12 15 3 | 14 21 21 21 26 18 21 19 15 18 18
5 | 8 17 8 13 13 4 20 9 12 24 4 | 22 25 28 30 33 23 28 25 22 22 24
6E | 15 21 8 20 16 4 17 19 16 24 5 | 40 38 35 38 31 35 34 47 39 32 37
7 | 8 23 6 13 18 4 21 7 9 14 4 | 14 30 19 18 34 15 26 14 15 18 15
8 | 7 17 7 13 10 4 15 13 10 20 4 | 19 27 26 21 30 22 32 23 22 32 23
9 | 9 18 7 17 11 6 18 14 9 21 4 | 13 26 22 22 20 16 24 23 18 26 19
10 | 8 15 4 11 11 4 13 12 9 21 3 | 19 22 25 27 27 22 23 26 21 25 22
11 | 9 17 8 10 24 6 17 14 10 18 4 | 15 27 23 20 40 19 28 22 19 19 19
12 | 12 23 5 12 18 4 27 12 8 19 4 | 13 28 19 19 27 17 31 23 16 16 17
13 | 6 17 8 11 25 6 19 7 8 11 4 | 14 28 17 15 37 14 23 19 16 16 15
14 | 11 18 7 15 17 5 24 9 10 14 4 | 17 26 22 23 31 19 23 23 20 23 19
15 | 9 28 8 15 16 5 30 11 9 15 5 | 12 31 18 21 26 15 29 21 15 22 17
16 | 7 22 6 19 16 4 23 6 7 24 4 | 15 26 17 21 24 16 30 18 15 22 16
17E | 8 18 6 14 23 3 20 10 15 8 4 | 26 31 28 27 36 26 30 28 23 25 28
18 | 13 19 8 18 12 5 23 11 12 21 5 | 23 33 33 36 33 29 34 33 32 27 29
19E | 7 21 9 18 21 8 28 10 13 18 5 | 21 27 25 26 31 20 32 23 22 30 24
20 | 7 17 6 15 8 8 16 10 10 33 4 | 23 29 26 24 31 22 28 23 23 39 24
21 | 8 26 8 15 16 6 28 6 10 22 5 | 13 24 19 16 115 15 23 13 16 7 16
22 | 11 16 5 15 9 5 21 9 9 16 4 | 27 33 34 32 37 29 34 33 29 28 30
23 | 7 21 10 12 17 5 24 11 6 14 4 | 21 30 24 20 30 20 28 23 20 22 19
24 | 6 17 7 10 23 6 13 10 12 13 4 | 21 24 24 20 34 20 24 21 22 21 22
X25 | 11 19 5 12 16 5 27 13 9 --- 5 | 16 27 25 22 35 22 39 24 22 --- 22
26 | 10 21 7 11 13 2 16 11 12 24 4 | 16 25 18 22 16 16 18 22 17 18 14
27 | 9 19 7 13 10 5 14 10 9 14 3 | 24 29 26 25 28 22 27 22 24 23 24
28 | 6 21 6 14 14 4 20 6 7 16 4 | 18 32 27 25 36 22 34 20 22 20 23
29E | 12 22 7 12 20 5 28 7 11 14 4 | 25 26 26 24 29 26 31 25 27 24 23
30 | 6 11 5 16 14 4 11 9 8 11 3 | 18 21 21 24 28 19 21 20 20 19 19
31 | 10 22 5 15 20 4 17 8 12 16 4 | 18 30 20 25 37 19 24 19 22 23 20
32 | 9 17 7 11 12 6 16 9 8 17 3 | 22 25 31 23 27 21 23 22 20 22 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 7 15 16 5 20 10 11 19 |T 21 29 26 25 35 23 29 25 22 25 23
WRMS | 9 20 7 14 15 5 19 9 8 18 |NE 18 27 23 22 33 21 27 22 20 21 20
MEDI | 8 19 7 14 16 5 20 10 10 17 |MD 18 27 24 23 31 20 28 23 21 22 22
Table 3.1623.6 GPS week: 1623 Day: 6 MJD: 55611.000
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 --- --- --- --- 59 --- --- --- --- 0 | 32 --- --- --- --- 49 --- --- --- --- 32
2 | 10 25 7 13 16 4 26 9 12 18 4 | 23 31 21 23 19 20 32 25 25 22 21
X3E | 19 20 8 15 21 11 17 9 --- 30 6 | 95 108 102 102 117 100 108 101 --- 105 100
4 | 8 15 7 11 14 4 10 7 12 16 3 | 22 25 27 29 29 25 25 26 22 24 24
5 | 6 17 8 10 12 3 19 9 13 27 4 | 31 32 36 38 38 33 31 35 35 31 33
6E | 14 20 7 14 23 5 19 18 20 25 6 | 48 47 44 45 41 45 43 51 48 40 45
7 | 7 22 8 10 17 3 20 6 11 14 4 | 17 26 20 18 31 15 25 15 18 19 15
8 | 9 19 5 10 14 5 13 12 6 22 4 | 20 28 24 22 28 20 25 20 19 30 22
9 | 9 15 5 13 15 4 17 9 10 24 4 | 18 25 20 20 22 18 28 19 22 21 17
10 | 7 17 6 9 15 3 13 7 10 24 3 | 27 26 34 34 34 29 28 33 30 31 29
11 | 12 15 7 10 21 5 19 13 8 18 4 | 20 28 27 25 38 21 26 24 22 23 22
12 | 8 23 6 12 20 4 22 9 11 20 4 | 18 29 20 18 25 18 31 19 19 17 17
13 | 6 18 9 11 25 5 22 12 14 12 4 | 20 26 23 23 37 20 30 23 20 20 19
14 | 7 16 6 12 18 3 22 9 11 13 4 | 19 30 22 22 30 21 31 23 26 24 21
15 | 8 29 8 13 16 6 27 8 8 16 4 | 20 32 21 23 26 18 30 21 18 23 18
16 | 7 24 6 17 18 4 26 9 10 28 5 | 19 28 18 20 25 16 33 19 15 25 18
17E | 8 19 8 10 18 4 22 10 11 10 4 | 33 36 33 31 40 30 38 30 27 29 30
18 | 12 18 8 15 12 5 21 12 13 21 4 | 30 36 36 41 40 33 34 38 35 37 34
19E | 7 23 7 12 13 5 24 12 11 11 4 | 32 33 28 32 30 28 33 32 28 31 29
20 | 9 17 7 15 8 8 18 12 16 37 5 | 33 39 43 41 41 34 33 38 35 49 36
21 | 8 25 8 9 18 5 26 7 11 22 4 | 10 23 13 13 109 12 21 11 13 8 13
22 | 10 17 7 9 12 6 22 8 11 16 4 | 39 42 46 44 46 40 38 44 43 42 42
23 | 7 26 11 12 17 4 27 12 13 15 5 | 22 31 23 22 30 20 34 21 21 23 18
24 | 10 16 6 10 37 7 14 10 9 12 4 | 31 29 33 34 38 28 33 33 29 31 32
X25 | 8 18 8 12 17 4 25 11 8 --- 4 | 18 24 25 21 34 17 37 22 18 --- 20
26 | 7 18 6 8 19 5 15 12 13 25 4 | 17 21 19 24 13 18 22 23 24 21 17
27 | 9 17 6 13 10 4 15 10 11 14 3 | 24 30 22 23 26 24 30 24 26 22 21
28 | 6 21 7 11 13 5 22 6 11 18 4 | 21 34 27 22 35 22 35 19 19 17 22
29E | 10 28 8 9 18 4 24 8 9 13 4 | 20 28 24 25 28 22 26 23 22 26 22
30 | 7 13 4 11 14 4 14 9 12 16 3 | 21 23 20 26 30 19 23 21 23 19 20
31 | 9 25 7 14 21 6 24 10 17 18 5 | 20 32 26 26 39 21 32 19 23 24 23
32 | 10 15 6 9 9 5 18 11 10 21 4 | 29 26 36 33 34 26 25 34 24 35 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 7 12 18 5 21 10 12 20 |T 26 32 29 29 37 26 32 28 24 28 26
WRMS | 8 20 7 11 15 4 19 9 10 23 |NE 23 29 26 26 34 23 29 24 24 25 23
MEDI | 8 18 7 11 17 5 21 9 11 18 |MD 21 29 25 25 34 21 31 23 23 24 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 4.1623 GPS week: 1623 MJD: 55605.0-55611.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 |U 7 9 24 |U 21 19 51 |U 7 7 14 |
emr | emr 2941 |U 10 9 24 | 21 20 44 | 10 8 21 |
esa | esa 2962 | 8 8 23 |U 18 17 48 | 7 6 14 |
gfz | gfz 2939 |U 8 9 25 |U 18 18 40 |U 7 6 14 |
grg | grg 2962 | 8 11 26 |U 19 18 54 | 9 7 20 |
igr | igr 2953 | 9 8 25 | 19 17 55 | 7 7 15 |
igs | igs 2954 | 7 7 21 | 18 18 49 | 6 6 13 |
jpl | jpl 2936 |U 10 9 27 |U 19 19 46 | 9 9 20 |
mit | mit 2962 |U 7 7 20 |U 19 20 52 |U 7 6 16 |
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 5.1623.0 GPS week: 1623 Day: 0 MJD: 55605.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3021 | 7 6 24 | 15 16 51 | 8 17 19 |
emr | emr 2968 | 11 7 28 | 17 17 36 | 11 13 30 |
esa | esa 2976 | 8 7 23 | 14 15 46 | 9 11 20 |
gfz | gfz 2968 | 8 7 24 | 15 15 54 | 7 11 23 |
grg | grg 2976 | 9 9 27 | 13 14 45 | 11 14 24 |
igr | igr 2970 | 8 5 24 | 12 14 44 | 7 12 22 |
igs | igs 2964 | 7 6 22 | 13 15 43 | 8 11 20 |
jpl | jpl 2961 | 9 7 28 | 14 17 38 | 9 17 28 |
mit | mit 2976 | 7 6 22 | 16 16 43 | 9 9 21 |
Table 5.1623.1 GPS week: 1623 Day: 1 MJD: 55606.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 8 12 25 | 19 24 57 | 6 4 15 |
emr | emr 2968 | 11 10 23 | 23 26 54 | 11 8 21 |
esa | esa 2976 | 9 13 27 | 17 23 50 | 6 6 12 |
gfz | gfz 2968 | 9 12 30 | 18 23 50 | 7 7 15 |
grg | grg 2976 | 9 16 27 | 17 23 52 | 8 6 19 |
igr | igr 2966 | 9 9 23 | 17 22 51 | 6 5 14 |
igs | igs 2961 | 9 9 21 | 17 23 50 | 6 6 12 |
jpl | jpl 2964 | 11 11 33 | 20 23 53 | 9 7 17 |
mit | mit 2976 | 10 11 26 | 20 26 63 | 7 7 17 |
Table 5.1623.2 GPS week: 1623 Day: 2 MJD: 55607.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 7 7 18 | 21 20 48 | 8 7 14 |
emr | emr 2872 | 11 13 18 | 27 20 55 | 12 11 22 |
esa | esa 2880 | 8 10 22 | 20 20 39 | 9 7 15 |
gfz | gfz 2872 | 9 9 24 | 21 20 37 | 9 7 16 |
grg | grg 2880 | 7 11 25 | 22 22 52 | 10 9 21 |
igr | igr 2870 | 16 13 42 | 27 22 69 | 12 8 27 |
igs | igs 2879 | 8 8 21 | 21 20 43 | 8 7 16 |
jpl | jpl 2868 | 10 12 23 | 26 20 48 | 13 10 23 |
mit | mit 2880 | 9 8 18 | 23 20 39 | 7 6 18 |
Table 5.1623.3 GPS week: 1623 Day: 3 MJD: 55608.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 7 7 28 | 30 22 44 | 8 7 16 |
emr | emr 2872 | 10 8 25 | 19 26 45 | 9 10 23 |
esa | esa 2976 | 8 8 21 | 16 19 48 | 7 7 13 |
gfz | gfz 2862 | 9 12 29 | 19 20 33 | 6 5 13 |
grg | grg 2976 | 8 8 25 | 23 21 65 | 8 5 17 |
igr | igr 2942 | 10 10 26 | 17 19 50 | 6 7 13 |
igs | igs 2967 | 7 7 22 | 17 19 48 | 7 7 11 |
jpl | jpl 2864 | 13 12 33 | 20 21 58 | 9 9 19 |
mit | mit 2976 | 6 5 16 | 22 28 76 | 6 9 21 |
Table 5.1623.4 GPS week: 1623 Day: 4 MJD: 55609.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 6 8 23 | 23 11 57 | 6 5 8 |
emr | emr 2968 | 8 9 28 | 18 12 30 | 12 7 18 |
esa | esa 2976 | 6 5 22 | 22 11 59 | 7 5 11 |
gfz | gfz 2968 | 6 6 23 | 16 10 28 | 6 4 12 |
grg | grg 2976 | 9 11 26 | 20 12 55 | 8 6 15 |
igr | igr 2974 | 6 5 21 | 21 11 58 | 7 5 10 |
igs | igs 2973 | 6 5 20 | 22 11 60 | 6 5 9 |
jpl | jpl 2963 | 7 6 27 | 16 12 33 | 9 6 18 |
mit | mit 2976 | 6 5 23 | 14 11 37 | 6 5 9 |
Table 5.1623.5 GPS week: 1623 Day: 5 MJD: 55610.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 7 12 25 | ---- ---- ---- | 7 5 11 |
emr | emr 2968 | 9 6 23 | ---- ---- ---- | 7 6 18 |
esa | esa 2976 | 7 6 22 | ---- ---- ---- | 7 5 11 |
gfz | gfz 2968 | 7 7 24 | ---- ---- ---- | 7 5 10 |
grg | grg 2976 | 8 11 26 | ---- ---- ---- | 9 6 26 |
igr | igr 2976 | 7 7 20 | ---- ---- ---- | 6 5 11 |
igs | igs 2975 | 7 6 20 | ---- ---- ---- | 6 3 11 |
jpl | jpl 2968 | 9 6 24 | ---- ---- ---- | 8 5 23 |
mit | mit 2976 | 7 6 21 | ---- ---- ---- | 7 4 12 |
Table 5.1623.6 GPS week: 1623 Day: 6 MJD: 55611.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 7 9 23 | ---- ---- ---- | 5 5 12 |
emr | emr 2971 | 9 10 23 | ---- ---- ---- | 6 4 16 |
esa | esa 2976 | 7 8 21 | ---- ---- ---- | 6 5 13 |
gfz | gfz 2968 | 7 8 22 | ---- ---- ---- | 6 6 12 |
grg | grg 2975 | 8 11 26 | ---- ---- ---- | 7 6 19 |
igr | igr 2975 | 6 7 19 | ---- ---- ---- | 5 6 10 |
igs | igs 2963 | 7 7 20 | ---- ---- ---- | 5 4 12 |
jpl | jpl 2965 | 7 8 21 | ---- ---- ---- | 7 6 16 |
mit | mit 2976 | 5 7 18 | ---- ---- ---- | 6 6 14 |
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 6.1623 GPS week: 1623 MJD: 55605.500-55611.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 22 -21 68 137 2 | 2 15
| 15 27 56 58 7 | 1
emr uuuuu | 35 -42 152 203 4 | 4 18
| 35 28 110 157 13 | 5
esa uuuuu | -55 -29 -17 -49 -1 | -6 15
| 13 16 48 87 10 | 2
gfz uuuuu | -49 50 -36 -50 -4 | 3 16
| 35 26 102 137 10 | 2
grg uuuux | 74 -63 5 81 10 | -1 12
| 28 38 161 77 29 | 4
igr xxxxx | -6 29 30 8 7 | -8 17
| 14 19 70 55 9 | 2
irf xxxxx | 24 11 -74 11 3 | -9 17
| 12 18 32 52 6 | 3
jpl uuuxu | 34 14 5 177 12 | -21 29
| 47 33 110 219 14 | 3
mit uuuuu | 1 12 -113 1 0 | 6 17
| 18 25 42 50 6 | 4
ngs uuuuu | -8 38 24 -97 3 | -9 14
| 32 53 141 140 7 | 2
sio uuuuu | 131 7 163 57 -8 | 6 16
| 19 22 72 66 3 | 4
Table 7.1623.0 GPS week: 1623 Day: 0 MJD: 55605.500
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 23 96 153 5 | 3 15
emr uuuuu | 45 -40 200 98 -4 | 12 25
esa uuuuu | -47 -30 -41 17 6 | -5 15
gfz uuuuu | -23 85 -194 -53 11 | 5 17
grg uuuux | 44 -104 244 59 -16 | 3 14
igr xxxxx | -8 54 -109 -12 7 | -8 20
irf xxxxx | 14 28 -104 18 -4 | -4 15
jpl uuuxu | 5 7 -56 -61 8 | -17 33
mit uuuuu | -28 30 -80 34 -4 | 11 19
ngs uuuuu | 24 7 48 -96 -5 | -6 13
sio uuuuu | 115 24 117 0 -8 | 11 17
Table 7.1623.1 GPS week: 1623 Day: 1 MJD: 55606.500
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 | 25 -24 85 219 9 | 2 14
emr uuuuu | 0 -55 186 39 -12 | 8 21
esa uuuuu | -43 -17 -44 30 4 | -6 14
gfz uuuuu | -17 65 -19 11 7 | 4 16
grg uuuux | 71 -63 34 27 -13 | 3 14
igr xxxxx | 10 48 111 -30 14 | -10 20
irf xxxxx | 14 31 -63 -1 -3 | -7 15
jpl uuuxu | 96 26 28 -90 9 | -22 31
mit uuuuu | -16 43 -96 -14 -7 | 9 17
ngs uuuuu | -19 -50 12 -94 7 | -8 14
sio uuuuu | 115 21 158 9 -11 | 9 16
Table 7.1623.2 GPS week: 1623 Day: 2 MJD: 55607.500
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 -18 -43 52 8 | 1 13
emr uuuuu | -12 -75 -56 34 -11 | 4 16
esa uuuuu | -44 -4 17 14 14 | -7 14
gfz uuuuu | -29 13 53 93 -1 | 4 15
grg uuuux | 79 -104 118 45 -22 | -1 7
igr xxxxx | -15 28 65 31 19 | -12 18
irf xxxxx | 42 27 -119 61 2 | -9 15
jpl uuuxu | -4 54 155 9 -7 | -24 30
mit uuuuu | 23 37 -172 63 -4 | 7 15
ngs uuuuu | -43 18 -28 -321 8 | -9 13
sio uuuuu | 154 27 25 18 -9 | 8 14
Table 7.1623.3 GPS week: 1623 Day: 3 MJD: 55608.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 21 -55 30 89 2 | 4 13
emr uuuuu | 16 -29 103 289 5 | 3 16
esa uuuuu | -53 -47 73 -201 -3 | -3 11
gfz uuuuu | -26 23 53 90 -8 | 6 13
grg uuuux | 102 -89 46 240 18 | -4 10
igr xxxxx | -8 27 43 66 14 | -7 14
irf xxxxx | 28 -10 -23 34 3 | -8 14
jpl uuuxu | -16 57 -80 276 17 | -21 25
mit uuuuu | 3 -8 -54 0 -1 | 7 16
ngs uuuuu | -54 98 -258 -240 9 | -7 11
sio uuuuu | 133 -22 218 61 -8 | 8 14
Table 7.1623.4 GPS week: 1623 Day: 4 MJD: 55609.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 19 1 110 121 1 | 0 15
emr uuuuu | 65 6 173 417 12 | -2 16
esa uuuuu | -73 -49 -47 -59 -7 | -7 17
gfz uuuuu | -77 39 66 -170 -8 | 1 16
grg uuuux | 86 -23 -143 56 13 | -6 11
igr xxxxx | -22 20 -3 20 -2 | -9 16
irf xxxxx | 14 -13 -56 -39 9 | -12 18
jpl uuuxu | 99 -27 -112 452 18 | -24 27
mit uuuuu | 4 -21 -127 -48 5 | 3 16
ngs uuuuu | 9 101 109 26 -5 | -11 15
sio uuuuu | 107 -25 184 64 -4 | 3 17
Table 7.1623.5 GPS week: 1623 Day: 5 MJD: 55610.500
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 -44 91 195 2 | 2 16
emr uuuuu | 83 -30 155 368 18 | 0 18
esa uuuuu | -55 -19 -65 -13 -14 | -7 17
gfz uuuuu | -112 64 -86 -282 -15 | 2 17
grg uuuux | 104 -50 -25 20 45 | -4 15
igr xxxxx | -17 -2 35 -87 1 | -6 15
irf xxxxx | 19 10 -67 -69 3 | -10 19
jpl uuuxu | 20 -16 -54 298 37 | -21 28
mit uuuuu | 0 7 -103 -72 0 | 3 17
ngs uuuuu | -3 36 153 68 9 | -10 15
sio uuuuu | 134 6 209 48 -13 | 3 17
Table 7.1623.6 GPS week: 1623 Day: 6 MJD: 55611.500
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 | 31 -32 109 131 -13 | 1 17
emr uuuuu | 49 -73 304 175 21 | 0 18
esa uuuuu | -72 -35 -14 -129 -11 | -9 20
gfz uuuuu | -58 58 -125 -38 -16 | -1 20
grg uuuux | 30 -8 -239 119 47 | -1 16
igr xxxxx | 16 28 66 65 -4 | -6 15
irf xxxxx | 40 7 -88 75 12 | -11 20
jpl uuuxu | 35 -6 152 354 5 | -19 26
mit uuuuu | 21 -2 -156 46 9 | 2 18
ngs uuuuu | 30 54 131 -24 -4 | -9 15
sio uuuuu | 156 17 229 196 -5 | 0 20
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