[IGSREPORT-19634] Wk 1628 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Apr 7 05:36:27 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1628 (Mar 20, 2011 - Mar 26, 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:
igs1628[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1628[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1628[0-6].cls IGS GPS clock combination summary report.
igs16287.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16287.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 | 4 24 4 24 WTZR WTZR
0 | GFZ | DAV1
0 | GRG | ADIS AMC2 LPGS SANT
0 | JPL | 9 25
0 | MIT | 4 9 24 27 4 9 17 24 27 CAS1 DARW HYDE MAW1 MIZU PERT
0 | MIT | CAS1 HYDE MAW1 MIZU PERT
1 | ALL | 1
1 | COD | PETS REUN
1 | EMR | 24 9 24 WTZR WTZR
1 | ESA | ALGO ALGO BRMU UNSA
1 | GFZ | 4
1 | GRG | ADIS AMC2 SANT
1 | MIT | 19 24 19 24 DAV1 DAV1 MAW1 SOFI
2 | COD | 26 26
2 | EMR | 24 4 9 24 WTZR WTZR
2 | ESA | UNSA
2 | GFZ | 2 MDVJ YELL
2 | GRG | ADIS SANT WTZR
2 | JPL | 9 YAKT
2 | MIT | 24 26 4 24 26 DAV1
3 | EMR | 4 24 4 24 WTZR WTZR
3 | ESA | UNSA
3 | GFZ | 2 21 KOUC MDVJ PIE1
3 | GRG | ADIS NRC1
3 | JPL | 25
3 | MIT | 4 6 9 10 21 22 24 27 4 6 9 10 21 22 24 27 PDEL PIE1
3 | MIT | PTBB PDEL PIE1 PTBB
4 | COD | 21 21 RAMO SOFI
4 | EMR | 4 8 19 24 4 WTZR WTZR
4 | ESA | FAA1 UNSA
4 | GFZ | 2 21 24 25 27 MDVJ YAKT
4 | GRG | LPGS
4 | JPL | 25
4 | MIT | 4 9 19 22 24 27 31 4 9 19 22 27 ALGO AMC2 BRMU BRUS
4 | MIT | CAS1 CHUR CONZ DAEJ DARW GODE HARB HOB2 HRAO IENG
4 | MIT | KOKB KOUR MAS1 MATE MAW1 MDVJ MIZU NICO NNOR NRC1
4 | MIT | NTUS ONSA PDEL PERT PTBB SPT0 SYOG TIXI TLSE TOW2
4 | MIT | TSKB TWTF USN3 USNO WROC WSRT YELL BAKO CAS1 DARW
4 | MIT | KOUC NTUS PDEL PERT SYDN
5 | EMR | 4 9 24 4 9 24 WTZR WTZR
5 | ESA | MATE
5 | GFZ | 2 21
5 | GRG | ADIS SANT
5 | JPL | 25 27 ADIS
5 | MIT | 4 9 24 27 30 4 9 24 27 30 CAS1 MAW1 MAW1
6 | COD | AREQ AREQ FAA1
6 | EMR | 4 24 4 WTZR WTZR
6 | ESA | ALRT ALRT
6 | GFZ | 2 4 21 MAW1 YAKT
6 | GRG | SANT
6 | JPL | 4 9 25 27 ADIS PIMO
6 | MIT | 4 9 24 27 4 9 27 CAS1 MAW1 BOR1 CAS1 MAW1
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
4 | MIT | ~00:00 | ~ 0.70 ns
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
----+--------+---------------
0 | GRG | 4
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 | -.3 1.0 .5 -5 4 -18 .41
EMR | -.2 5.5 1.7 -3 -8 -1 .75
ESA | 2.9 8.4 -6.7 170 -45 14 .36
GFZ | -1.2 .8 -.7 11 24 -26 .68
GRG | -1.4 10.0 9.2 9 29 -84 .46
JPL | 2.9 3.9 3.8 12 -51 2 .42
MIT | 7.3 -5.9 -6.1 -17 -9 -59 .44
NGS | 5.2 -2.3 -2.6 -28 -110 28 .41
SIO | 2.7 5.5 -5.0 134 -109 17 .77
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 5-Nov-2006 (GPS Week 1400, day 0; MJD 54044) the absolute antenna
model is introduced (IGSMAIL #5438). 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 1.1628.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1628.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 2.1628.[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 3.1628.[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 5.1628.0-6).
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 1628 summary. (Mar 20, 2011 - Mar 26, 2011)
Table 1.1628.a GPS week: 1628 MJD: 55640.000-55646.000
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 245| 0 0 3 56 -46 1 -.28 10 9 | -451 -187 21 70
| 0 0 1 10 19 16 .01 | 466 626
emr 92| 0 2 3 105 -24 9 .41 20 20 | -1031 164 19 96
| 1 3 1 24 30 10 .03 | 982 831
esa 136| 0 1 0 -176 -25 21 .21 8 8 | -1340 -60 15 104
| 0 0 1 15 16 18 .03 | 747 1233
gfz 194| 0 -1 -3 43 -80 -11 -.20 11 11 | 17 172 22 100
| 1 1 1 36 103 11 .02 | 417 663
grg 133| 0 0 2 29 -78 -21 .58 19 16 | -145 96 54 222
| 1 1 1 32 30 13 .07 | 215 236
igr n/a| 0 0 -1 65 -26 -9 -.05 5 5 | -4546 -14 19 64
| 0 0 0 22 37 31 .02 | 817 717
jpl 121| 0 -1 5 11 48 27 .45 23 22 | 1334 190 21 96
| 1 1 0 19 26 36 .04 | 1069 689
mit 258| 1 -3 -6 99 -41 -24 -.31 15 13 | -606 650 26 162
| 1 0 1 28 35 9 .05 | 1192 1574
ngs 212| -1 -1 -4 122 150 -20 -.27 12 9 | -7850 -7207 2361 4284
| 0 1 0 23 61 17 .05 | 19447 18611
sio 255| 0 1 9 -201 177 18 .03 20 21 | --- --- --- ---
| 0 1 1 37 43 18 .05 | --- ---
Table 1.1628.b GPS week : 1628 MJD: 55640.000-55646.000
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 56 0 0 0 0 0 |
2 | 5 5 5 4 5 5 6 |
3 | 4 4 4 4 4 4 4 |
4 | 6 5 5 5 5 6 7 |
5 | 5 5 4 4 5 5 5 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 6 4 4 4 5 |
8 | 5 6 6 6 6 6 6 |
9 | 7 7 7 7 7 7 7 |
10 | 4 4 4 3 4 4 5 |
11 | 5 5 5 5 5 5 5 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 5 4 5 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 6 5 5 5 5 5 5 |
18 | 6 6 6 6 6 6 6 |
19 | 5 5 6 5 6 5 5 |
20 | 5 5 5 5 5 5 6 |
21 | 5 5 4 5 5 4 5 |
22 | 6 6 6 6 6 6 6 |
23 | 6 5 5 5 5 5 5 |
24 | 7 6 6 5 5 5 5 |
25 | 5 5 11 5 5 5 5 |
26 | 4 4 4 4 4 4 4 |
27 | 6 6 7 6 7 6 7 |
28 | 5 5 5 5 5 6 6 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 3 4 |
31 | 5 5 5 4 5 4 5 |
32 | 5 5 5 5 5 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 2.1628.0 GPS week: 1628 Day: 0 MJD: 55640.000
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 245| 0 1 2 46 -20 -15 -.29 9 8 | -348 -248 18 73
| 105 4 |
emr 92| 0 6 6 64 -3 11 .43 20 20 | -1821 726 23 89
| -13 -2 |
esa 136| 0 1 1 -200 -14 44 .25 10 9 | -1757 -1244 19 115
| 63 89 |
gfz 194| 1 -2 -4 90 -217 -25 -.18 14 12 | 202 -69 24 96
| -27 60 |
grg 133| 0 -1 0 -7 -90 -35 .62 30 17 | -33 144 52 194
| 115 -41 |
igr n/a| 0 0 0 54 15 -14 -.04 7 7 | -4591 34 19 56
| -20 54 |
jpl 121| 0 0 6 -26 63 20 .45 23 22 | 747 151 22 82
| -6 19 |
mit 258| 0 -3 -8 135 -52 -17 -.27 14 11 | -114 84 37 146
| 16 17 |
ngs 212| 0 -2 -4 77 205 -4 -.26 12 8 | -348 -294 2437 4039
| -43 -103 |
sio 255| -1 0 7 -156 154 32 .08 21 20 | --- --- --- ---
| 63 -59 |
Table 2.1628.1 GPS week: 1628 Day: 1 MJD: 55641.000
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 245| 0 0 1 69 -34 29 -.29 11 10 | -180 -485 29 78
| 66 36 |
emr 92| 3 4 5 127 -23 -3 .43 20 20 | -1842 548 20 80
| -52 42 |
esa 136| 0 1 0 -161 -32 21 .17 8 8 | -923 -368 18 107
| 44 83 |
gfz 194| 0 -1 -3 -14 -90 -3 -.20 10 9 | 448 -475 22 100
| -71 41 |
grg 133| 0 0 3 36 -46 -17 .57 16 15 | -21 -164 45 179
| 39 -62 |
igr n/a| 0 -1 -1 41 -45 4 -.09 6 5 | -5207 154 20 58
| -57 96 |
jpl 121| 2 0 5 34 62 -6 .45 23 22 | 348 190 23 100
| -7 28 |
mit 258| 0 -3 -8 95 -22 -20 -.25 14 12 | 13 -215 31 149
| 17 18 |
ngs 212| -1 0 -3 137 157 -45 -.26 13 10 | -159 -686 2067 4225
| 4 -32 |
sio 255| 0 1 9 -185 204 32 .07 20 20 | --- --- --- ---
| 72 -71 |
Table 2.1628.2 GPS week: 1628 Day: 2 MJD: 55642.000
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 245| 1 0 3 52 -52 -8 -.27 10 9 | -64 -766 26 67
| 95 40 |
emr 92| 2 5 4 116 -28 12 .45 20 20 | -752 -2 18 99
| -67 32 |
esa 136| 0 2 -1 -176 -38 36 .17 8 8 | -2463 488 16 109
| 46 109 |
gfz 194| -2 -2 -5 56 -33 9 -.16 11 11 | 6 112 25 103
| -79 50 |
grg 133| 2 0 1 23 -79 -26 .49 18 17 | -59 256 49 210
| 55 -36 |
igr n/a| 0 0 -2 93 -64 -7 -.03 6 6 | -4373 -194 23 61
| -63 99 |
jpl 121| 3 0 6 11 39 17 .48 21 21 | 1207 96 19 88
| 11 -4 |
mit 258| 0 -4 -5 115 -7 -24 -.26 15 13 | -3250 4178 29 150
| 17 -1 |
ngs 212| 0 -3 -4 117 107 -38 -.33 13 10 | -51943 -49392 2294 4132
| -84 127 |
sio 255| 0 0 11 -187 224 -3 .09 20 20 | --- --- --- ---
| 96 -72 |
Table 2.1628.3 GPS week: 1628 Day: 3 MJD: 55643.000
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 245| 0 0 1 51 -56 0 -.29 10 9 | -1373 869 21 77
| 91 -7 |
emr 92| 0 4 4 95 -46 14 .41 19 19 | -2093 1023 21 106
| -34 25 |
esa 136| 0 0 0 -191 -10 -3 .25 7 7 | -709 -1607 14 103
| 62 62 |
gfz 194| 0 0 -2 62 16 -12 -.22 11 10 | -716 748 22 91
| -13 14 |
grg 133| 0 0 2 18 -69 -2 .52 17 16 | -608 43 56 225
| 70 -17 |
igr n/a| 0 0 0 78 -12 -15 -.04 5 5 | -5786 866 17 61
| -50 74 |
jpl 121| 1 -2 4 14 81 104 .48 21 21 | 105 1033 22 91
| 44 -30 |
mit 258| 1 -2 -5 133 -73 -9 -.33 14 11 | -696 315 25 138
| 9 14 |
ngs 212| 0 0 -3 139 92 -30 -.33 12 9 | -1368 814 2475 4166
| -58 100 |
sio 255| -1 3 10 -160 140 26 .04 20 21 | --- --- --- ---
| 88 -51 |
Table 2.1628.4 GPS week: 1628 Day: 4 MJD: 55644.000
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 245| 1 0 3 73 -80 19 -.26 11 10 | -431 -759 19 79
| 34 112 |
emr 92| 0 -1 2 113 -70 27 .38 21 21 | 441 -1167 19 121
| -77 48 |
esa 136| 0 0 0 -171 -53 -3 .23 8 8 | -2034 2122 13 96
| -3 100 |
gfz 194| 0 -1 -3 48 68 -14 -.20 11 11 | -285 1312 21 113
| -45 36 |
grg 133| 0 0 3 32 -110 -36 .58 18 17 | -221 470 54 297
| 16 45 |
igr n/a| 0 0 -1 92 -59 -50 -.03 5 6 | -3575 -1009 16 94
| -50 83 |
jpl 121| 0 -3 4 2 -2 39 .45 24 23 | 2414 -578 22 108
| 19 48 |
mit 258| 2 -3 -6 68 8 -32 -.35 16 14 | -210 352 22 290
| 22 -2 |
ngs 212| -1 1 -4 147 69 -20 -.24 12 8 | -343 -924 2585 4547
| -58 109 |
sio 255| 0 2 10 -244 235 12 -.00 20 29 | --- --- --- ---
| 117 -77 |
Table 2.1628.5 GPS week: 1628 Day: 5 MJD: 55645.000
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 245| 0 1 3 50 -37 -2 -.28 10 10 | -56 -401 20 61
| 67 -4 |
emr 92| -1 -2 3 134 -28 7 .36 20 20 | -1176 754 16 91
| -90 18 |
esa 136| 0 2 -2 -179 -13 29 .22 9 9 | -1041 345 15 103
| 12 72 |
gfz 194| 1 0 -1 58 -164 -18 -.23 11 10 | 461 -557 25 94
| -52 16 |
grg 133| 0 1 1 11 -36 -25 .61 15 14 | -48 -213 62 219
| 28 -117 |
igr n/a| 0 0 -1 62 28 -31 -.06 5 5 | -4758 819 18 63
| -87 44 |
jpl 121| -1 -1 4 22 43 3 .49 23 23 | 1507 1099 21 101
| 34 47 |
mit 258| 2 -3 -7 77 -87 -30 -.35 16 14 | 2 -302 20 131
| 17 5 |
ngs 212| -1 -2 -4 108 222 -1 -.25 13 9 | -99 -400 2504 4479
| -128 -58 |
sio 255| 0 2 9 -232 123 37 -.00 19 18 | --- --- --- ---
| 123 -36 |
Table 2.1628.6 GPS week: 1628 Day: 6 MJD: 55646.000
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 245| 0 0 5 52 -42 -11 -.27 11 10 | -705 478 18 59
| 52 43 |
emr 92| 0 3 0 83 26 0 .41 21 21 | 26 -732 16 91
| -13 -47 |
esa 136| 2 2 -2 -154 -17 24 .20 9 8 | -458 -157 12 96
| 33 57 |
gfz 194| 0 0 -2 4 -144 -14 -.18 11 10 | 4 135 21 103
| -68 27 |
grg 133| 0 1 4 94 -115 -3 .69 18 17 | -26 141 66 230
| -42 -6 |
igr n/a| 0 0 -2 37 -49 49 -.04 5 4 | -3538 -769 20 56
| -29 103 |
jpl 121| 0 0 4 20 51 10 .38 23 23 | 3014 -656 21 102
| 47 -5 |
mit 258| 2 -2 -6 70 -52 -36 -.38 18 14 | 8 141 19 130
| 3 11 |
ngs 212| -1 -3 -5 126 202 -4 -.20 13 9 | -691 433 2165 4401
| -65 10 |
sio 255| -1 2 9 -242 157 -6 -.05 21 19 | --- --- --- ---
| 119 -52 |
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 3.1628.0 GPS week: 1628 Day: 0 MJD: 55640.000
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 --- --- --- --- 254 --- --- --- --- 0 | 66 --- --- --- --- 206 --- --- --- --- 63
2E | 7 18 5 11 24 4 24 11 11 10 4 | 21 33 29 22 29 23 32 21 21 25 24
3 | 6 11 7 11 14 12 18 16 8 13 3 | 18 26 26 23 32 23 25 24 24 27 23
4E | 11 23 23 13 132 6 17 12 16 10 6 | 135 133 132 138 137 134 128 138 136 130 134
5 | 7 18 6 15 16 5 25 8 13 20 4 | 19 31 26 29 34 22 33 24 25 21 23
6 | 6 14 7 9 12 10 17 14 8 15 3 | 19 26 26 22 30 23 24 23 24 25 22
7E | 6 16 9 17 14 4 22 9 11 10 4 | 19 26 22 17 26 19 28 19 22 18 18
8 | 14 21 8 16 20 8 17 16 10 21 5 | 55 57 56 54 50 53 57 58 60 56 56
9E | 19 19 11 15 18 6 18 28 22 19 6 | 29 37 33 37 37 34 37 51 44 33 33
10 | 8 13 5 11 13 4 14 15 11 20 4 | 20 21 28 28 31 25 25 32 24 22 22
11E | 7 17 12 11 17 7 23 16 6 13 4 | 21 30 28 27 34 24 36 29 28 25 27
12 | 9 22 5 7 21 6 21 14 10 24 4 | 12 26 20 18 26 18 27 20 19 23 17
13 | 6 18 7 13 20 5 27 18 11 16 5 | 15 26 20 22 35 18 30 24 19 17 15
14 | 9 22 8 11 16 6 29 17 10 18 5 | 25 29 30 34 39 26 29 33 25 22 27
15 | 10 20 10 16 19 6 25 9 11 27 5 | 15 28 25 24 35 20 29 24 17 21 19
16 | 8 21 9 13 12 6 29 11 7 28 5 | 16 28 23 22 26 19 29 18 23 19 19
17 | 9 23 15 14 20 5 28 12 12 18 5 | 25 34 27 29 27 22 35 28 23 25 23
18 | 10 23 10 15 13 6 32 10 10 34 5 | 20 33 27 27 29 24 35 27 27 33 24
19 | 6 21 10 12 16 8 28 10 8 22 4 | 12 29 16 14 24 18 34 16 18 19 16
20 | 8 19 8 12 15 6 24 14 13 19 4 | 22 31 27 35 30 23 31 25 27 24 24
21E | 8 18 7 11 33 5 22 12 13 12 5 | 15 28 23 18 42 20 28 16 18 18 19
22 | 9 21 6 11 14 7 28 9 7 42 5 | 27 35 35 35 39 29 34 36 29 37 31
23 | 7 24 9 13 17 4 30 18 10 23 5 | 31 36 33 37 37 30 37 31 31 25 28
24E | 16 25 14 19 29 14 19 18 16 20 6 | 133 132 131 125 131 133 132 124 125 137 128
X25 | 10 16 3 11 17 6 25 20 11 --- 5 | 36 38 35 33 51 35 47 49 38 --- 38
26 | 7 19 6 20 11 6 15 11 6 20 4 | 14 21 22 23 26 20 25 22 20 18 18
27E | 13 19 10 15 20 6 17 25 20 19 6 | 17 27 27 28 37 25 30 39 35 31 25
28 | 6 19 9 14 16 6 23 13 10 27 5 | 22 30 28 30 33 24 29 27 28 29 26
29 | 9 23 7 9 18 5 26 15 10 21 5 | 26 38 27 30 27 27 37 36 31 36 28
30 | 7 10 7 9 14 5 18 10 7 23 3 | 21 25 27 23 31 23 23 25 27 29 23
31E | 10 20 7 11 22 7 24 10 16 14 5 | 18 30 18 10 28 21 30 20 18 19 18
32 | 9 21 8 24 17 6 16 13 13 25 5 | 19 24 25 34 33 24 24 28 25 24 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 10 14 30 7 23 14 12 21 |T 30 37 33 33 39 37 38 35 33 32 32
WRMS | 8 20 9 12 17 7 22 11 8 20 |NE 22 29 26 27 32 31 30 27 24 24 25
MEDI | 8 19 8 13 17 6 23 13 11 20 |MD 20 30 27 28 33 23 30 27 25 25 23
Table 3.1628.1 GPS week: 1628 Day: 1 MJD: 55641.000
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 | 47 --- --- --- --- 373 --- 67 --- --- 56 | 53 --- --- --- --- 334 --- 6 --- --- 65
2E | 10 17 6 8 23 4 24 11 13 9 4 | 31 33 33 26 35 29 34 30 32 31 28
3 | 9 13 5 8 13 4 16 13 10 13 3 | 21 27 25 20 32 21 27 21 21 25 21
4E | 19 19 15 8 17 7 18 12 13 11 5 | 128 122 122 128 111 124 119 127 129 118 123
5 | 9 18 6 10 17 5 23 8 16 18 4 | 24 35 27 22 39 24 37 28 28 23 24
6 | 10 13 5 7 12 5 14 10 11 12 3 | 20 27 24 20 30 18 24 19 20 22 20
7E | 9 18 7 9 14 3 20 12 17 10 4 | 27 28 23 21 29 21 27 27 34 21 21
8E | 16 25 7 10 21 5 12 16 16 22 5 | 53 55 50 52 46 49 45 61 60 51 50
9E | 18 19 11 11 16 5 17 27 26 19 6 | 25 37 30 32 31 31 34 47 45 32 31
10 | 11 12 8 5 12 4 10 13 8 15 3 | 25 25 28 24 31 24 24 32 27 28 24
11E | 7 18 6 7 20 6 24 24 14 14 5 | 21 28 21 21 32 16 28 26 23 19 19
12 | 11 22 7 6 16 8 26 13 13 23 5 | 17 29 23 20 27 20 27 22 16 22 18
13 | 6 17 5 10 19 6 24 17 10 14 4 | 20 28 21 17 37 19 31 24 21 20 18
14 | 11 20 8 7 16 4 28 14 10 19 4 | 22 28 25 26 36 23 29 26 27 21 24
15 | 10 21 9 11 18 5 26 8 8 24 5 | 21 31 25 24 36 23 31 23 27 22 23
16 | 8 22 6 11 14 5 25 11 13 28 5 | 17 24 17 19 25 17 27 14 18 16 15
17 | 9 23 8 10 17 6 24 12 12 19 5 | 28 32 23 25 27 23 32 25 23 23 22
18 | 10 20 8 12 13 6 29 12 10 36 5 | 19 29 21 24 25 21 31 22 23 31 20
19 | 9 23 10 10 17 6 29 12 15 22 5 | 17 29 17 17 26 15 29 16 23 18 15
20 | 10 24 10 13 13 6 27 12 11 18 5 | 21 35 30 26 29 22 31 25 20 22 22
21E | 10 21 6 9 21 5 23 12 10 13 4 | 30 33 30 23 35 27 36 29 28 26 25
22 | 12 20 10 10 16 5 28 8 10 42 6 | 22 33 25 26 33 24 33 26 25 33 23
23 | 9 22 5 12 14 5 28 11 9 18 4 | 27 38 29 26 38 29 38 30 29 28 27
24E | 20 19 9 14 19 10 21 18 12 21 5 | 119 116 116 116 120 115 122 114 116 125 118
X25 | 8 18 4 8 15 6 --- 16 13 --- 4 | 33 31 28 24 41 26 --- 38 33 --- 30
26 | 7 14 5 9 11 5 16 12 11 15 3 | 19 23 20 16 25 16 22 18 17 20 16
27E | 10 22 9 9 17 4 16 24 23 19 5 | 17 28 23 20 30 22 27 34 34 31 22
28 | 9 21 7 10 13 5 21 15 14 26 5 | 23 30 23 25 29 21 29 26 21 28 22
29 | 9 24 7 9 15 4 28 16 11 23 5 | 26 30 22 22 23 22 32 28 26 28 22
30 | 7 13 5 9 12 5 16 11 10 16 3 | 23 21 23 20 29 19 25 21 22 26 20
31E | 9 23 9 9 16 6 25 12 11 13 4 | 18 27 18 11 32 13 26 15 20 16 15
32 | 11 21 6 12 14 5 23 18 12 25 5 | 20 24 26 26 27 23 25 30 20 27 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 20 8 10 16 6 23 14 13 20 |T 30 36 31 29 36 38 36 32 32 31 30
WRMS | 10 20 8 9 15 5 22 12 10 20 |NE 23 29 23 22 30 35 29 23 23 24 23
MEDI | 10 20 7 9 16 5 23 12 12 18 |MD 22 29 25 24 31 22 29 26 25 25 22
Table 3.1628.2 GPS week: 1628 Day: 2 MJD: 55642.000
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 --- --- --- --- 487 --- --- --- --- 0 | 41 --- --- --- --- 419 --- --- --- --- 36
2E | 10 20 8 8 23 6 21 14 12 9 4 | 28 35 31 27 33 27 32 31 26 29 27
3 | 8 13 6 8 14 5 13 16 11 10 3 | 22 26 27 26 32 22 28 24 22 26 23
4E | 16 16 9 10 18 6 17 12 14 12 4 | 116 110 109 115 112 111 105 116 116 106 112
5 | 9 17 8 10 16 6 21 8 12 17 4 | 23 36 28 27 39 24 35 27 22 24 25
6 | 7 13 8 8 12 4 13 14 12 13 3 | 22 28 29 25 32 22 27 24 20 23 23
7E | 9 19 8 16 33 6 21 11 17 13 5 | 22 27 22 26 40 20 28 23 21 20 19
8E | 16 24 12 15 21 7 17 13 18 28 6 | 44 45 45 52 41 42 38 49 46 40 42
9E | 17 18 10 11 11 4 15 31 27 17 6 | 23 35 31 29 34 28 34 43 37 30 28
10 | 10 11 7 14 14 4 10 12 10 10 4 | 27 26 29 28 35 23 28 30 23 21 26
11E | 7 17 9 8 20 6 21 18 9 15 4 | 19 26 22 25 29 19 25 26 20 20 20
12 | 10 21 8 13 14 8 22 10 14 24 5 | 15 27 16 22 28 18 25 18 18 21 17
13 | 9 23 7 11 22 6 25 17 16 12 5 | 21 31 24 27 38 22 32 28 26 20 22
14 | 10 22 6 9 18 5 24 14 9 18 4 | 25 31 27 30 37 25 29 27 19 20 25
15 | 11 21 8 11 17 4 26 11 9 22 5 | 16 31 23 22 35 19 30 18 18 12 19
16 | 8 20 7 7 17 5 24 11 14 27 5 | 17 25 18 18 27 14 27 15 19 18 15
17 | 9 23 9 10 20 6 23 11 13 19 5 | 26 32 20 27 21 23 31 22 22 21 21
18 | 8 21 9 12 15 4 26 13 14 36 5 | 20 32 24 28 29 21 31 20 23 30 22
19 | 8 27 12 10 17 4 30 14 10 19 5 | 19 31 17 22 26 17 33 19 20 16 17
20 | 10 23 8 12 17 6 25 14 9 19 5 | 22 36 28 33 31 25 33 28 24 26 25
21E | 9 16 7 10 14 4 20 11 9 10 4 | 24 35 35 33 35 29 34 27 26 27 29
22 | 8 20 9 8 18 5 27 10 13 41 6 | 28 35 31 30 38 27 36 29 27 32 28
23 | 9 28 6 11 19 4 29 15 12 16 5 | 27 40 31 32 39 27 36 31 28 24 28
24E | 18 19 8 15 23 10 16 17 13 19 5 | 81 79 84 84 87 81 86 81 81 90 84
X25 | 12 --- --- --- 29 30 --- 21 18 --- 11 | 34 --- --- --- 49 37 --- 38 41 --- 31
26 | 9 11 6 10 16 8 14 14 9 13 3 | 16 21 18 21 29 17 22 20 18 19 16
X27E | 11 21 9 10 15 4 --- 28 25 17 6 | 17 31 24 22 33 20 --- 32 32 26 22
28 | 9 23 8 13 16 7 22 12 14 28 5 | 23 29 25 26 31 22 29 27 23 23 23
29 | 9 24 7 12 14 4 24 12 11 19 4 | 25 32 18 20 19 19 30 23 21 20 19
30 | 7 15 6 8 15 5 14 13 13 13 3 | 20 24 21 18 30 17 19 20 22 25 17
31E | 8 25 8 12 19 5 25 16 11 15 5 | 22 33 23 20 33 19 32 21 19 18 21
32 | 12 20 8 8 17 7 15 19 10 22 5 | 23 27 27 29 31 26 30 38 20 33 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 8 11 18 6 21 15 13 20 |T 28 35 30 31 37 40 34 31 29 28 28
WRMS | 9 20 8 11 17 6 21 13 10 20 |NE 23 30 24 25 32 40 29 25 22 22 22
MEDI | 9 20 8 10 17 5 21 14 12 17 |MD 23 31 25 27 33 22 31 27 22 23 23
Table 3.1628.3 GPS week: 1628 Day: 3 MJD: 55643.000
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 --- --- --- --- 287 --- --- --- --- 0 | 36 --- --- --- --- 328 --- --- --- --- 34
2E | 7 20 5 8 18 3 23 13 6 11 4 | 27 33 32 25 31 27 33 31 27 32 28
3 | 10 14 4 9 17 4 16 12 12 12 3 | 25 30 32 29 37 29 29 30 28 33 28
4E | 15 20 10 9 17 7 16 12 17 13 5 | 109 105 101 109 90 105 101 112 112 100 105
5 | 6 18 5 11 17 3 22 9 9 18 4 | 28 38 32 32 37 28 38 29 25 29 29
6 | 8 14 5 6 14 3 16 11 7 10 3 | 24 32 32 27 36 27 27 29 26 30 27
7E | 8 17 7 10 14 5 18 9 10 8 3 | 26 31 24 25 32 23 25 25 22 24 22
8E | 17 24 9 12 17 5 17 13 16 23 5 | 44 50 45 45 42 42 38 50 42 43 43
9E | 18 18 9 13 13 5 17 32 24 12 6 | 27 36 31 34 36 31 34 48 40 33 31
10 | 8 14 4 9 13 3 12 10 11 9 3 | 32 32 33 36 36 30 27 34 26 29 30
11E | 8 18 7 8 16 5 22 17 9 18 4 | 22 30 26 24 32 21 28 30 26 22 23
12 | 11 25 5 11 13 7 26 8 15 23 5 | 24 31 28 28 31 25 27 26 23 26 25
13 | 7 17 5 12 21 8 24 10 10 10 4 | 28 34 25 28 37 25 35 31 27 29 25
14 | 10 22 5 10 17 3 27 12 11 18 4 | 30 43 35 33 41 29 35 36 31 28 32
15 | 12 24 7 12 21 5 25 13 9 23 5 | 24 34 29 30 38 28 34 29 27 25 26
16 | 7 24 7 9 16 4 28 9 10 27 5 | 23 32 27 24 30 24 32 24 23 27 24
17 | 9 20 7 12 17 5 23 9 11 18 4 | 35 38 33 34 31 32 37 33 35 34 32
18 | 10 20 7 17 15 4 26 9 9 35 5 | 21 31 25 30 27 21 31 24 20 31 22
19 | 7 23 9 11 16 5 28 13 11 20 5 | 25 35 28 25 30 25 36 27 27 24 25
20 | 9 22 8 16 15 5 23 14 8 26 5 | 24 35 31 31 30 26 33 31 22 32 26
21E | 7 18 6 11 26 8 21 11 11 11 4 | 25 35 34 32 35 30 31 29 30 28 28
22 | 9 19 6 10 16 4 26 7 11 42 5 | 30 37 33 33 39 29 35 34 29 37 31
23 | 9 24 6 10 17 5 27 21 9 18 5 | 34 41 34 36 40 32 41 43 25 38 32
24E | 14 16 5 14 17 6 17 11 12 16 4 | 117 120 117 115 121 114 120 114 113 122 116
X25 | 9 30 6 10 16 5 26 9 9 --- 5 | 36 56 46 44 42 39 39 38 38 --- 38
26 | 5 9 6 6 15 5 14 13 11 18 3 | 24 24 24 25 30 22 26 29 21 26 23
27E | 11 17 10 11 19 6 14 29 20 14 5 | 24 30 31 27 36 27 32 40 31 32 27
28 | 8 23 7 14 18 5 22 12 13 28 5 | 33 39 35 37 36 34 34 39 38 35 35
29 | 8 24 5 12 13 4 24 12 11 20 4 | 38 44 37 36 36 36 40 40 39 39 36
30 | 7 12 6 9 18 4 15 8 7 12 3 | 26 29 31 28 34 26 26 27 25 32 27
31E | 8 21 6 11 21 3 20 7 11 12 4 | 24 34 27 21 35 23 31 26 23 21 23
32 | 10 18 7 10 15 5 20 17 9 21 4 | 31 33 35 30 34 28 34 39 26 36 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 7 11 17 5 21 14 12 20 |T 33 40 36 35 39 42 37 37 33 35 33
WRMS | 9 19 7 10 16 5 21 11 9 21 |NE 28 35 31 31 34 41 33 32 27 31 29
MEDI | 8 20 6 11 17 5 22 12 11 18 |MD 27 34 32 30 36 28 34 31 27 31 28
Table 3.1628.4 GPS week: 1628 Day: 4 MJD: 55644.000
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 | 8 --- --- --- --- 344 --- --- --- --- 0 | 38 --- --- --- --- 328 --- --- --- --- 39
2E | 9 22 8 12 17 6 27 20 7 11 5 | 29 37 36 25 34 31 37 29 28 33 31
3 | 9 14 3 8 15 5 16 15 9 10 3 | 26 34 31 26 37 28 31 28 26 32 28
4E | 11 24 9 12 18 6 17 17 17 17 5 | 116 114 109 112 104 110 106 118 114 104 112
5 | 7 22 6 14 13 5 29 17 15 17 5 | 33 44 37 34 42 34 45 33 33 33 34
6 | 8 16 3 7 14 6 17 16 7 8 3 | 27 35 31 26 37 29 31 30 25 31 28
7E | 8 20 7 12 11 4 23 12 9 11 4 | 24 32 23 27 34 26 33 29 27 24 24
8E | 17 24 10 14 20 5 20 15 17 23 6 | 35 42 37 34 35 35 34 41 40 32 35
9E | 17 19 11 12 24 5 18 31 22 15 6 | 25 37 34 32 36 33 35 48 44 29 31
10 | 8 11 5 10 14 4 16 14 11 13 3 | 24 27 29 27 32 27 28 29 24 24 25
11E | 10 17 8 9 19 5 24 19 9 13 4 | 18 25 22 23 30 22 30 26 23 19 20
12 | 7 24 7 9 19 6 24 16 14 25 5 | 25 35 26 23 36 29 33 28 30 28 27
13 | 9 21 6 12 19 6 26 16 7 14 4 | 26 31 31 26 41 27 36 28 24 25 26
14 | 9 23 12 10 17 4 29 16 10 21 5 | 33 40 40 35 43 36 40 38 34 30 35
15 | 10 23 9 10 19 5 29 11 6 21 5 | 28 37 33 29 41 31 36 31 27 27 28
16 | 11 24 8 10 14 7 28 11 11 27 5 | 23 32 31 25 33 26 34 24 22 26 25
17 | 11 22 12 17 16 5 24 12 10 19 5 | 35 37 36 31 31 32 37 33 33 31 31
18 | 10 22 8 12 18 5 29 11 6 33 5 | 24 34 26 27 32 26 36 26 23 33 24
19 | 9 24 10 10 16 6 34 14 15 17 5 | 24 36 25 22 33 25 39 26 30 24 24
20 | 12 22 6 17 18 5 26 12 8 23 5 | 25 37 35 34 34 30 39 31 29 34 30
21E | 10 22 8 10 21 6 29 12 8 12 4 | 28 38 33 29 42 32 42 31 28 32 30
22 | 9 21 8 10 19 7 27 16 10 40 6 | 32 41 32 32 45 33 38 35 31 37 32
23 | 11 23 6 12 18 6 27 16 8 21 5 | 34 38 37 32 43 33 46 38 30 28 33
24E | 14 13 7 10 18 6 17 15 11 15 4 | 80 84 84 79 88 80 85 76 75 84 79
X25 | 9 17 7 10 17 5 26 13 7 --- 4 | 34 41 41 36 47 36 46 37 32 --- 37
26 | 9 13 5 7 13 6 19 15 12 15 4 | 23 29 27 25 32 26 29 26 29 26 25
27E | 11 18 13 11 29 5 16 29 23 16 6 | 24 33 33 27 40 29 32 40 37 28 28
28 | 10 21 6 13 16 5 26 13 14 29 5 | 31 35 31 29 36 31 35 34 35 34 31
29 | 7 23 7 13 16 4 27 12 14 23 5 | 29 39 26 32 33 32 42 33 34 30 28
30 | 9 12 5 10 16 8 18 9 12 14 3 | 25 30 32 27 38 28 29 28 27 33 29
31E | 10 28 9 11 22 5 19 10 10 12 5 | 26 41 31 25 42 27 35 24 22 26 29
32 | 14 22 6 11 18 4 18 15 6 19 4 | 25 28 32 23 35 29 34 29 28 27 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 21 8 11 18 5 24 16 12 20 |T 32 39 35 32 40 43 39 35 33 33 33
WRMS | 10 21 8 11 17 6 23 14 8 29 |NE 28 35 31 28 37 43 36 30 28 29 29
MEDI | 9 22 7 11 18 5 24 15 10 17 |MD 26 37 32 27 36 30 36 31 29 30 29
Table 3.1628.5 GPS week: 1628 Day: 5 MJD: 55645.000
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 --- --- --- --- 250 --- --- --- --- 0 | 38 --- --- --- --- 205 --- --- --- --- 37
2E | 9 19 8 8 18 3 30 27 11 11 5 | 20 29 27 24 29 23 32 28 22 26 23
3 | 10 13 7 13 13 5 19 15 11 12 4 | 17 25 22 22 24 21 24 23 20 25 19
4E | 11 22 13 11 17 5 16 21 21 17 5 | 114 113 107 112 96 112 106 124 118 106 111
5 | 7 21 7 10 14 6 26 18 12 14 4 | 20 34 23 23 35 22 36 22 18 20 20
6 | 9 13 6 11 12 5 17 16 11 9 4 | 17 23 21 22 22 20 24 23 20 22 18
7E | 6 18 8 14 12 4 22 12 9 9 4 | 16 24 16 16 21 17 24 17 18 16 14
8E | 17 23 11 13 14 4 20 20 17 22 6 | 37 41 34 37 28 34 34 45 40 33 34
9E | 13 22 14 12 16 6 18 29 26 14 6 | 13 26 20 20 24 17 26 40 36 20 18
10 | 8 12 6 9 13 4 15 13 12 11 3 | 18 20 23 19 24 20 19 21 23 21 18
11E | 11 18 10 11 17 5 20 16 14 19 5 | 11 25 19 18 25 17 23 21 20 18 14
12 | 10 23 5 10 14 6 22 13 13 24 5 | 16 26 19 18 22 19 26 19 19 16 16
13 | 8 18 7 10 20 5 23 17 15 13 5 | 11 26 14 15 34 12 30 17 13 17 11
14 | 9 24 10 9 14 5 29 15 6 18 5 | 22 29 24 22 33 22 30 27 23 17 22
15 | 11 21 10 13 18 5 26 10 8 21 5 | 13 27 23 20 34 19 32 20 20 17 18
16 | 8 23 8 12 11 5 28 11 10 28 5 | 17 26 18 18 19 19 29 16 23 17 15
17 | 9 22 9 15 16 4 22 13 9 20 5 | 28 29 23 28 20 25 27 28 27 31 23
18 | 8 22 11 14 13 5 32 13 6 31 5 | 16 28 20 22 24 19 31 20 19 31 17
19 | 10 24 9 13 12 5 31 13 9 17 5 | 17 31 20 19 23 21 34 20 21 19 18
20 | 10 22 9 9 13 4 21 12 14 25 5 | 15 27 20 21 25 17 27 19 21 22 15
21E | 10 15 8 10 17 4 27 11 9 10 4 | 21 28 30 25 33 27 33 26 28 28 26
22 | 9 22 10 10 16 8 29 18 10 39 6 | 22 33 26 24 34 25 34 29 22 36 22
23 | 8 25 8 11 16 5 25 13 12 24 5 | 20 32 21 19 34 19 34 19 18 19 18
24E | 12 19 9 11 16 6 17 14 11 13 4 | 93 98 97 93 98 95 96 93 96 98 95
X25 | 9 17 8 9 16 6 27 12 6 --- 4 | 31 25 30 32 34 28 32 27 31 --- 28
26 | 10 13 6 9 11 5 16 14 11 12 3 | 11 19 15 13 21 14 20 16 17 19 12
27E | 11 21 12 9 18 6 17 28 21 13 6 | 14 24 20 18 28 17 27 34 30 23 19
28 | 12 20 8 15 12 6 23 15 12 28 5 | 21 26 21 24 21 19 26 25 22 24 18
29 | 9 22 6 10 15 5 26 13 8 23 4 | 27 32 28 28 19 28 34 32 32 27 26
30 | 8 11 6 8 10 5 16 10 8 12 3 | 19 22 21 21 21 20 23 20 25 23 19
31E | 9 22 10 8 17 3 20 9 9 11 4 | 14 25 16 12 25 15 24 15 15 11 13
32 | 13 22 9 9 13 6 14 10 7 16 4 | 15 21 20 19 25 19 21 20 18 20 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 9 11 15 5 23 16 13 19 |T 24 32 27 26 30 31 32 29 28 27 24
WRMS | 10 20 9 10 14 5 23 14 9 18 |NE 19 26 21 21 26 28 28 22 21 22 19
MEDI | 9 21 8 10 14 5 22 13 11 16 |MD 17 26 21 21 25 20 29 22 22 21 18
Table 3.1628.6 GPS week: 1628 Day: 6 MJD: 55646.000
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 --- --- --- --- 393 --- --- --- --- 0 | 53 --- --- --- --- 315 --- --- --- --- 52
2E | 10 23 10 10 17 4 28 30 13 13 6 | 22 32 29 25 32 23 32 32 24 27 23
3 | 8 15 4 9 19 4 15 15 10 13 4 | 28 31 32 32 37 31 27 32 33 30 29
4E | 19 20 11 9 30 7 17 34 25 22 7 | 120 118 114 120 101 120 112 135 127 113 117
5 | 10 25 7 12 16 4 27 17 10 19 5 | 28 38 32 39 39 31 37 32 28 28 30
6 | 8 18 4 9 18 4 16 17 8 11 4 | 28 32 33 32 37 31 28 32 34 29 29
7E | 8 19 8 11 21 5 23 14 12 11 4 | 25 29 23 24 30 25 30 26 27 23 22
8E | 17 28 11 9 22 4 18 19 14 24 6 | 49 49 49 48 41 47 46 57 57 46 46
9E | 13 21 12 11 17 4 19 33 24 12 6 | 26 33 34 32 33 32 34 49 42 30 31
10 | 11 15 7 13 17 3 13 15 12 16 4 | 29 29 33 44 40 32 29 35 30 32 31
11E | 9 19 6 12 24 4 21 17 15 20 5 | 26 36 26 24 36 24 29 29 28 28 23
12 | 10 24 8 11 13 6 25 10 14 28 5 | 23 30 26 30 34 26 28 25 24 29 26
13 | 9 20 9 8 20 5 24 17 12 16 5 | 25 32 29 27 38 26 33 28 28 23 24
14 | 12 23 9 11 14 4 27 9 9 16 4 | 33 36 36 38 43 31 35 36 29 27 32
15 | 12 22 10 10 20 5 27 14 9 22 5 | 25 35 31 31 39 27 33 30 24 25 25
16 | 8 24 8 9 17 4 25 14 7 28 5 | 26 30 29 30 35 26 30 25 24 27 25
17 | 10 23 10 14 13 5 26 13 12 21 5 | 34 36 30 36 27 34 33 35 33 38 31
18 | 11 22 9 13 15 7 29 14 9 31 5 | 23 32 26 28 29 24 34 27 23 36 23
19 | 9 25 9 11 19 4 27 15 13 17 5 | 21 32 21 23 28 23 34 25 27 20 21
20 | 12 23 10 12 16 5 24 11 10 31 5 | 22 31 29 31 29 25 30 27 26 32 23
21E | 9 16 6 11 25 9 25 12 11 15 4 | 15 23 21 22 29 19 27 21 20 22 17
22 | 10 22 11 9 17 5 30 15 9 38 6 | 33 36 35 39 40 33 36 38 33 45 33
23 | 9 24 8 11 13 3 30 15 10 22 5 | 30 37 32 33 38 30 40 32 30 27 29
24E | 12 18 8 13 18 4 19 18 17 15 5 | 98 103 100 104 105 102 106 97 104 104 103
X25 | 8 15 9 7 13 6 27 14 10 --- 4 | 39 35 40 40 45 37 41 36 36 --- 38
26 | 10 15 7 7 16 3 12 13 9 15 3 | 23 26 25 27 30 24 26 25 24 22 22
27E | 9 20 12 10 18 5 18 35 23 15 6 | 25 33 29 26 38 26 34 42 34 26 25
28 | 11 23 8 11 14 5 23 14 11 31 5 | 30 33 31 37 39 33 35 35 32 34 31
29 | 8 24 7 10 14 5 22 15 9 23 4 | 32 40 31 35 30 34 39 37 34 31 32
30 | 8 12 8 8 17 3 15 8 9 15 3 | 30 27 32 30 35 31 27 26 32 27 28
31E | 9 21 9 9 14 5 22 15 6 16 4 | 28 32 27 21 37 25 32 29 26 26 24
32 | 13 18 5 12 13 3 19 10 8 18 4 | 24 26 30 30 33 28 28 30 27 27 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 21 9 11 18 5 23 18 13 21 |T 33 37 35 36 39 42 37 37 35 34 33
WRMS | 10 21 8 10 17 4 23 14 9 19 |NE 29 32 30 32 35 42 32 30 29 29 29
MEDI | 10 21 8 11 17 4 23 15 10 17 |MD 28 32 31 31 37 30 33 32 29 28 28
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 4.1628 GPS week: 1628 MJD: 55640.0-55646.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 |U 10 8 23 |U 10 12 39 |U 7 7 18 |
emr | emr 2943 |U 12 11 39 |U 13 11 40 | 10 9 20 |
esa | esa 2962 | 10 9 31 |U 10 11 40 | 7 8 18 |
gfz | gfz 2943 |U 9 8 24 |U 15 13 49 |U 8 10 18 |
grg | grg 2973 | 11 9 27 |U 11 11 49 | 10 11 22 |
igr | igr 2952 | 9 8 24 | 12 10 40 | 7 7 17 |
igs | igs 2960 | 11 9 34 | 13 12 41 | 6 6 14 |
jpl | jpl 2910 |U 13 13 37 |U 12 10 38 |U 10 10 21 |
mit | mit 2989 |U 99 53 77 |U 12 16 46 |U 9 11 20 |
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 5.1628.0 GPS week: 1628 Day: 0 MJD: 55640.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 8 7 28 | 9 15 45 | 7 6 15 |
emr | emr 2962 | 7 8 30 | 9 14 41 | 7 6 18 |
esa | esa 2976 | 9 8 41 | 9 13 50 | 7 5 15 |
gfz | gfz 2961 | 5 6 20 | 12 13 53 | 7 7 14 |
grg | grg 2976 | 6 7 28 | 8 11 52 | 7 6 18 |
igr | igr 2947 | 7 6 31 | 9 13 44 | 6 5 13 |
igs | igs 2961 | 7 6 27 | 10 19 46 | 6 4 15 |
jpl | jpl 2955 | 7 7 21 | 10 11 43 | 8 5 16 |
mit | mit 2976 | 8 8 48 | 8 11 47 | 8 7 17 |
Table 5.1628.1 GPS week: 1628 Day: 1 MJD: 55641.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3006 | 7 7 14 | 9 9 29 | 11 7 20 |
emr | emr 2956 | 12 12 60 | 10 10 31 | 11 13 14 |
esa | esa 2976 | 9 10 36 | 9 7 27 | 9 12 17 |
gfz | gfz 2957 | 6 4 17 | 12 14 43 | 10 11 17 |
grg | grg 2972 | 8 7 24 | 9 8 35 | 10 14 22 |
igr | igr 2952 | 6 5 18 | 9 6 28 | 9 7 16 |
igs | igs 2972 | 17 15 86 | 9 7 29 | 8 13 15 |
jpl | jpl 2854 | 24 28 76 | 10 9 28 | 13 14 20 |
mit | mit 3072 | 6 4 15 | 10 9 33 | 7 17 18 |
Table 5.1628.2 GPS week: 1628 Day: 2 MJD: 55642.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3013 | 9 10 27 | 14 13 56 | 5 5 20 |
emr | emr 2862 | 13 12 31 | 23 15 51 | 9 6 21 |
esa | esa 2880 | 12 11 25 | 16 13 51 | 6 7 16 |
gfz | gfz 2859 | 10 11 22 | 20 13 53 | 7 7 16 |
grg | grg 2968 | 11 13 31 | 18 15 60 | 7 5 17 |
igr | igr 2956 | 9 11 25 | 18 12 52 | 6 6 16 |
igs | igs 2934 | 9 9 25 | 21 13 54 | 7 5 16 |
jpl | jpl 2768 | 13 14 41 | 19 14 53 | 10 8 19 |
mit | mit 2976 | 638 319 334 | 21 15 52 | 6 5 16 |
Table 5.1628.3 GPS week: 1628 Day: 3 MJD: 55643.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 18 13 28 | 11 12 40 | 6 8 16 |
emr | emr 2956 | 21 14 51 | 15 11 42 | 11 10 25 |
esa | esa 2976 | 20 14 38 | 12 12 43 | 7 6 17 |
gfz | gfz 2955 | 19 15 35 | 12 12 43 | 7 15 23 |
grg | grg 2975 | 20 14 29 | 12 10 55 | 11 14 19 |
igr | igr 2963 | 20 14 29 | 11 12 41 | 8 8 18 |
igs | igs 2974 | 19 13 29 | 12 10 41 | 7 7 18 |
jpl | jpl 2953 | 21 14 49 | 11 11 40 | 10 11 21 |
mit | mit 2976 | 19 20 61 | 12 16 39 | 10 15 22 |
Table 5.1628.4 GPS week: 1628 Day: 4 MJD: 55644.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 8 8 24 | 13 17 51 | 6 6 18 |
emr | emr 2956 | 11 8 20 | 16 12 62 | 10 8 17 |
esa | esa 2976 | 8 7 20 | 13 16 57 | 7 8 17 |
gfz | gfz 2956 | 7 6 17 | 21 15 63 | 8 8 17 |
grg | grg 2975 | 14 7 21 | 14 12 62 | 17 16 43 |
igr | igr 2941 | 7 6 18 | 17 13 56 | 7 6 17 |
igs | igs 2960 | 7 6 17 | 16 14 58 | 7 6 17 |
jpl | jpl 2946 | 8 7 17 | 18 14 51 | 8 6 21 |
mit | mit 2976 | 7 5 17 | 16 16 57 | 8 8 19 |
Table 5.1628.5 GPS week: 1628 Day: 5 MJD: 55645.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 8 7 27 | 7 10 24 | 8 6 14 |
emr | emr 2955 | 10 13 58 | 10 9 27 | 11 13 22 |
esa | esa 2976 | 9 9 38 | 7 10 27 | 9 8 16 |
gfz | gfz 2957 | 8 10 43 | 14 12 38 | 10 11 20 |
grg | grg 2975 | 9 10 37 | 8 9 37 | 10 9 15 |
igr | igr 2961 | 7 9 31 | 14 10 35 | 8 8 14 |
igs | igs 2968 | 8 9 36 | 15 11 37 | 9 8 17 |
jpl | jpl 2946 | 10 11 35 | 8 9 27 | 12 13 27 |
mit | mit 2976 | 8 10 45 | 9 36 64 | 12 12 22 |
Table 5.1628.6 GPS week: 1628 Day: 6 MJD: 55646.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 14 7 18 | 7 7 25 | 6 10 19 |
emr | emr 2956 | 11 10 24 | 9 8 27 | 10 8 24 |
esa | esa 2976 | 6 6 18 | 7 6 28 | 6 13 33 |
gfz | gfz 2957 | 6 5 18 | 18 10 47 | 7 10 22 |
grg | grg 2976 | 8 7 19 | 8 8 39 | 9 13 21 |
igr | igr 2947 | 7 6 15 | 7 7 29 | 3 10 27 |
igs | igs 2951 | 6 6 16 | 7 7 26 | 0 0 0 |
jpl | jpl 2950 | 8 8 20 | 7 7 24 | ---- ---- ---- |
mit | mit 2976 | 8 5 17 | 7 8 27 | 11 12 27 |
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 6.1628 GPS week: 1628 MJD: 55640.500-55646.500
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 -72 135 127 -13 | 6 19
| 31 19 127 77 6 | 3
emr uuuuu | 8 51 -44 168 0 | 52 55
| 27 23 85 101 9 | 6
esa uuuuu | -57 -35 -2 -156 0 | 4 20
| 18 15 58 63 9 | 4
gfz uuuuu | -11 52 -6 86 4 | 12 24
| 24 19 79 91 5 | 7
grg uuuux | 58 -39 35 69 -2 | 3 19
| 38 40 190 108 43 | 4
igr xxxxx | -55 52 59 -1 1 | -3 23
| 21 18 88 73 9 | 4
irf xxxxx | 24 1 -88 86 -4 | 12 25
| 20 14 61 90 25 | 8
jpl uuuuu | 10 -19 262 75 -6 | 17 28
| 38 29 140 97 10 | 4
mit uuuuu | 15 -13 -170 159 3 | 26 35
| 26 17 110 164 24 | 9
ngs uuuuu | 2 63 7 -168 -5 | -2 14
| 74 34 121 135 11 | 3
sio uuuuu | 84 -96 27 15 13 | 57 64
| 33 37 90 119 25 | 14
Table 7.1628.0 GPS week: 1628 Day: 0 MJD: 55640.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 3 -85 45 53 -8 | 4 17
emr uuuuu | 9 33 -68 262 6 | 46 47
esa uuuuu | -82 -43 30 -142 1 | 1 16
gfz uuuuu | -53 47 -135 -100 4 | 4 15
grg uuuux | 48 -95 263 170 29 | -4 23
igr xxxxx | -47 40 88 124 -14 | -5 21
irf xxxxx | 7 20 -91 88 12 | 2 14
jpl uuuuu | -12 26 335 174 -6 | 13 24
mit uuuuu | -10 4 -137 236 13 | 14 19
ngs uuuuu | 110 63 -78 -154 -13 | -3 14
sio uuuuu | 66 -43 54 -140 28 | 37 42
Table 7.1628.1 GPS week: 1628 Day: 1 MJD: 55641.500
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 | -15 -61 210 166 -16 | 5 16
emr uuuuu | -21 57 -33 44 0 | 46 48
esa uuuuu | -62 -39 39 -114 -5 | 0 16
gfz uuuuu | -20 76 -77 126 3 | 6 16
grg uuuux | 83 -34 89 107 -5 | 0 25
igr xxxxx | -75 62 -22 33 -1 | -7 21
irf xxxxx | 21 5 -23 96 17 | 4 15
jpl uuuuu | -7 12 104 23 -21 | 15 24
mit uuuuu | 3 -12 -49 222 21 | 17 21
ngs uuuuu | 53 1 -66 -285 -4 | -4 14
sio uuuuu | 92 -67 93 -10 34 | 43 47
Table 7.1628.2 GPS week: 1628 Day: 2 MJD: 55642.500
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 | 7 -99 133 238 -8 | 2 15
emr uuuuu | 15 63 -103 54 6 | 45 47
esa uuuuu | -62 -50 -42 -131 -9 | -2 13
gfz uuuuu | -3 75 47 97 15 | 6 15
grg uuuux | 83 -59 72 -34 -59 | 2 24
igr xxxxx | -52 59 70 -7 -5 | -9 20
irf xxxxx | 47 -4 -43 221 21 | 5 17
jpl uuuuu | 51 -15 217 28 5 | 11 21
mit uuuuu | 48 -21 -102 385 28 | 18 24
ngs uuuuu | -80 80 -19 -360 -18 | -6 14
sio uuuuu | 119 -100 53 179 40 | 48 53
Table 7.1628.3 GPS week: 1628 Day: 3 MJD: 55643.500
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 | 37 -70 152 34 -7 | 8 19
emr uuuuu | 5 55 -64 142 12 | 52 55
esa uuuuu | -32 -41 41 -128 17 | 3 16
gfz uuuuu | 16 34 -1 138 7 | 14 25
grg uuuux | 47 -49 -26 34 -47 | 6 17
igr xxxxx | -44 71 131 -15 9 | -4 21
irf xxxxx | 30 21 -15 96 10 | 14 27
jpl uuuuu | 60 -23 90 90 -1 | 18 28
mit uuuuu | 16 12 -51 168 21 | 28 38
ngs uuuuu | -70 79 -102 -185 -19 | -1 14
sio uuuuu | 81 -67 156 6 27 | 61 68
Table 7.1628.4 GPS week: 1628 Day: 4 MJD: 55644.500
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 | -59 -43 24 169 -21 | 10 22
emr uuuuu | 5 68 -6 135 -11 | 57 62
esa uuuuu | -47 -6 15 -121 0 | 8 25
gfz uuuuu | 17 36 93 181 1 | 18 32
grg uuuux | 8 -25 73 -96 13 | 5 16
igr xxxxx | -30 41 200 -55 9 | 0 26
irf xxxxx | 53 -9 -152 129 -16 | 20 35
jpl uuuuu | 5 -28 436 -18 -5 | 22 34
mit uuuuu | 55 -31 -293 165 -5 | 35 47
ngs uuuuu | -56 49 -38 -195 2 | 0 15
sio uuuuu | 130 -126 -113 164 1 | 68 77
Table 7.1628.5 GPS week: 1628 Day: 5 MJD: 55645.500
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 | 2 -83 11 64 -19 | 8 21
emr uuuuu | -20 74 -151 244 -6 | 57 62
esa uuuuu | -74 -28 -118 -294 0 | 8 26
gfz uuuuu | -18 36 47 109 -2 | 19 33
grg uuuux | 115 -44 124 203 -13 | 4 14
igr xxxxx | -46 71 -22 -107 12 | 1 26
irf xxxxx | -2 -16 -143 46 -34 | 19 35
jpl uuuuu | -49 -50 419 -10 4 | 22 33
mit uuuuu | -7 -33 -273 80 -28 | 36 48
ngs uuuuu | 56 112 144 -19 3 | 1 16
sio uuuuu | 34 -139 -21 -9 -16 | 70 79
Table 7.1628.6 GPS week: 1628 Day: 6 MJD: 55646.500
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 | -30 -58 370 164 -13 | 5 21
emr uuuuu | 60 7 117 297 -9 | 57 62
esa uuuuu | -44 -39 22 -160 -7 | 9 26
gfz uuuuu | -14 62 -13 53 2 | 19 33
grg uuuux | 19 36 -350 101 67 | 4 14
igr xxxxx | -90 23 -29 20 -1 | 1 26
irf xxxxx | 13 -6 -146 -76 -36 | 16 35
jpl uuuuu | 18 -53 231 237 -18 | 20 32
mit uuuuu | 2 -9 -281 -146 -29 | 34 47
ngs uuuuu | 3 59 211 20 10 | 0 15
sio uuuuu | 65 -125 -34 -86 -20 | 70 79
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