[IGSREPORT-20007] Wk 1645 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 4 06:06:04 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1645 (Jul 17, 2011 - Jul 23, 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:
igs1645[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1645[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1645[0-6].cls IGS GPS clock combination summary report.
igs16457.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16457.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 of poorer consistency (GRG),
they 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 | 26 26
0 | ESA | 21 21 BJFS DRAG UNSA
0 | GFZ | 7 13 21 26 FAA1 YAKT
0 | JPL | 25 26
0 | MIT | 26 30 21 26 30 SYOG
1 | COD | KOSG
1 | EMR | 26 30 26 30
1 | ESA | 21 21
1 | GFZ | 7 13 MDVJ
1 | GRG | NKLG SANT
1 | JPL | 25 26
1 | MIT | 26 30 26 30 IENG MAW1 IENG MAW1
2 | COD | WROC WROC
2 | EMR | 26 26
2 | ESA | IRKJ UNSA
2 | GFZ | MDVJ
2 | GRG | LHAZ SANT
2 | JPL | 25 26
2 | MIT | 26 26 MDVJ MDVJ
3 | COD | NTUS CHUR
3 | EMR | 21 26 21 26 USNO
3 | ESA | YELL NTUS UNSA
3 | GFZ | KERG MDVJ
3 | GRG | CEDU
3 | JPL | 3 21 25 26
3 | MIT | 3 26 30 3 21 26 30 DAV1 BAKO MAW1 NTUS USNO
4 | COD | MDVJ MDVJ
4 | EMR | 26 26
4 | ESA | UNSA
4 | GFZ | HARB MATE MDVJ
4 | GRG | CONZ IRKJ
4 | JPL | 3 15 25 26
4 | MIT | 3 6 24 26 30 3 6 24 26 30 NTUS NTUS
5 | EMR | 26 YELL YELL
5 | ESA | DARW UNSA
5 | GFZ | ISPA
5 | GRG | CONZ IRKJ
5 | JPL | 15 25 26
5 | MIT | 26 30 26 30 MDVJ SCH2 MDVJ SCH2
6 | COD | TIXI
6 | EMR | 3 3 26 CHUR CHUR
6 | ESA | CEDU IRKJ UNSA
6 | GFZ | CAS1 MDVJ YAKT
6 | GRG | IRKJ NKLG SANT
6 | JPL | 3 25 26 CAS1
6 | MIT | 3 26 3 26 CAS1 NTUS CAS1 MDVJ
5. 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
----+--------+---------------
4 | COD | 1
5 | COD | 1
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G01 | | | | 4 | 4 | 4 | 4 |
PRN G17 | 2 | 2 | | | | | |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) 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. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
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 | 1.0 .7 .8 -16 -9 7 .0
EMR | -2.1 -1.3 -2.4 6 5 3 .32
ESA | .8 -4.4 9.6 -31 -32 67 .13
GFZ | -1.7 .0 .8 -16 38 11 .01
GRG | 6.1 -1.7 16.0 2 2 4 -.14
JPL | .3 4.4 -8.0 -10 -9 74 -1.21
MIT | 3.8 -5.2 15.2 -6 7 -12 -.06
NGS | 2.0 1.3 14.3 -38 7 -5 .10
SIO | 3.5 -2.9 -11.9 -47 -128 -3 -.03
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) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution does not yet use IGS08/igs08.atx, which causes their RMS
clock residuals to be higher than for the other centres; for the same
reason, the JPL solution is excluded from the weekly SINEX combination.
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 1.1645.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1645.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 2.1645.[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 3.1645.[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 5.1645.0-6).
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 1645 summary. (Jul 17, 2011 - Jul 23, 2011)
Table 1.1645.a GPS week: 1645 MJD: 55759.000-55765.000
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 254| 0 0 -2 4 -9 11 -.22 8 7 | -535 807 14 82
| 0 0 0 11 13 19 .03 | 784 1123
emr 97| 0 -2 -8 -45 10 7 .34 17 17 | 337 -472 16 113
| 1 0 1 33 11 17 .04 | 1051 741
esa 126| 1 0 2 -13 60 1 .27 7 7 | -344 -1151 14 153
| 0 0 0 9 12 7 .03 | 574 1421
gfz 198| 0 0 1 -21 -118 -17 -.23 10 10 | 18 8 23 136
| 0 0 2 74 50 13 .03 | 206 459
grg 130| 3 0 10 -38 39 3 .64 17 16 | 165 -519 46 235
| 2 0 2 30 74 9 .03 | 986 653
igr n/a| 0 0 0 -25 -17 -41 -.08 5 5 | 3077 -503 19 105
| 0 0 1 21 14 15 .02 | 811 724
jpl 144| -1 -2 -8 -12 2 4 .56 18 17 | -132 -667 20 319
| 1 1 2 12 10 78 .04 | 1009 651
mit 271| 0 0 0 -32 -71 -18 -.34 14 11 | 730 -399 24 186
| 1 1 1 17 15 9 .03 | 1024 1559
ngs 230| 0 0 2 69 -29 -15 -.19 9 8 | 1429 -36747 2132 3583
| 0 0 1 37 32 14 .03 | 5321 99441
sio 251| 0 2 -3 44 231 20 -.23 17 16 | --- --- --- ---
| 0 1 1 21 14 8 .03 | --- ---
Table 1.1645.b GPS week : 1645 MJD: 55759.000-55765.000
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 48 |
2 | 4 5 5 5 5 5 5 |
3 | 4 5 4 5 6 6 6 |
4 | 4 4 4 4 4 4 4 |
5 | 4 5 4 5 4 5 5 |
6 | 4 4 4 4 6 6 5 |
7 | 5 5 4 4 4 4 4 |
8 | 4 4 4 3 3 3 3 |
9 | 3 3 4 3 5 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 3 |
12 | 4 5 4 4 5 5 4 |
13 | 4 6 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 5 4 5 5 5 |
16 | 4 5 5 5 5 5 4 |
17 | 4 6 5 4 4 5 4 |
18 | 5 5 4 4 5 5 5 |
19 | 4 4 4 4 5 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 4 4 5 4 4 |
23 | 4 4 4 4 4 5 4 |
24 | 3 4 4 4 3 4 3 |
25 | 4 5 4 4 5 5 4 |
26 | 6 6 5 8 7 7 6 |
27 | 3 4 4 4 5 5 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 4 4 4 5 5 4 |
30 | 6 6 5 5 6 10 10 |
31 | 4 5 4 5 4 5 4 |
32 | 3 4 4 3 4 4 3 |
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 2.1645.0 GPS week: 1645 Day: 0 MJD: 55759.000
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 254| 0 1 -3 0 9 18 -.23 7 7 | 84 -155 11 78
| 19 -19 |
emr 97| -1 -1 -6 2 22 34 .40 18 18 | 2010 -667 17 120
| -45 -48 |
esa 126| 0 0 1 -18 52 9 .23 7 7 | -1305 1585 13 140
| 51 -3 |
gfz 198| 0 -1 1 -19 -148 -9 -.25 11 11 | 103 193 23 142
| 16 96 |
grg 130| 3 0 8 -78 15 9 .62 14 13 | 1514 -426 54 199
| 50 -33 |
igr n/a| 0 0 0 9 0 -31 -.10 5 5 | 4130 -434 19 136
| 7 19 |
jpl 144| -1 -3 -4 1 20 -79 .61 17 16 | 1214 -501 18 313
| -50 -3 |
mit 284| 1 -1 0 -34 -77 -15 -.32 12 11 | 1100 -870 29 229
| 2 22 |
ngs 230| 0 0 2 92 -22 -18 -.21 9 7 | 13369 -262247 1914 3242
| -127 9 |
sio 251| 0 0 -2 55 218 5 -.20 18 17 | --- --- --- ---
| -41 -134 |
Table 2.1645.1 GPS week: 1645 Day: 1 MJD: 55760.000
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 254| 0 1 -3 18 -14 7 -.24 10 8 | -1074 110 14 74
| -10 3 |
emr 97| 0 -1 -8 -7 -1 0 .37 18 18 | 1650 -2020 15 125
| -12 -56 |
esa 126| 1 0 1 -21 44 0 .27 8 8 | 361 -2282 16 157
| 17 -9 |
gfz 198| 0 -1 2 -100 -70 -33 -.21 11 11 | -189 148 24 136
| 29 90 |
grg 130| 2 0 10 -23 -16 -10 .62 15 13 | 1581 -1908 44 220
| -21 -24 |
igr n/a| 0 0 1 -1 -10 -48 -.09 5 5 | 4277 -1891 21 96
| 3 8 |
jpl 144| -2 -1 -7 2 9 103 .54 18 17 | 1324 -1944 19 307
| 16 69 |
mit 284| 0 -1 1 -36 -61 -17 -.32 12 11 | -17 -134 22 164
| -2 18 |
ngs 230| 0 1 1 85 -23 -20 -.20 9 9 | -1091 88 2458 3875
| -8 13 |
sio 251| -1 1 -2 55 242 27 -.21 17 16 | --- --- --- ---
| -39 -129 |
Table 2.1645.2 GPS week: 1645 Day: 2 MJD: 55761.000
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 254| 0 1 -2 0 -17 21 -.26 8 7 | -674 573 15 90
| 37 -10 |
emr 97| 0 -2 -7 -55 -1 -21 .28 18 18 | -667 -97 15 133
| 5 -64 |
esa 126| 1 0 2 -11 61 0 .25 7 7 | 177 -2164 12 142
| 22 -24 |
gfz 198| 0 0 0 44 -56 -7 -.25 11 10 | 70 102 25 132
| -22 102 |
grg 130| 1 0 9 -65 -2 8 .66 13 12 | -331 -122 42 312
| 35 -64 |
igr n/a| 0 0 -1 -24 -34 -33 -.10 5 5 | 2401 -231 19 127
| 14 44 |
jpl 144| -3 0 -5 -22 -8 -71 .51 18 17 | -590 -547 19 321
| 8 3 |
mit 284| 0 0 0 -21 -74 -24 -.33 13 12 | 661 -950 25 176
| 2 23 |
ngs 230| 0 0 0 33 -55 3 -.20 8 6 | -696 577 1933 3492
| -49 42 |
sio 251| -1 1 -2 63 219 18 -.27 17 18 | --- --- --- ---
| -23 -126 |
Table 2.1645.3 GPS week: 1645 Day: 3 MJD: 55762.000
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 254| 0 0 -2 7 -28 -20 -.22 7 7 | -1774 2813 15 83
| 19 1 |
emr 97| 0 -2 -7 -68 22 20 .35 17 17 | -321 -141 17 108
| 14 -75 |
esa 126| 1 -1 2 0 59 -6 .27 8 7 | -298 -1875 14 148
| 29 -15 |
gfz 198| -1 0 1 1 -99 -3 -.22 9 8 | 271 -337 22 137
| -1 93 |
grg 130| 5 0 10 -63 24 -7 .64 15 14 | -129 -518 38 250
| 32 -134 |
igr n/a| 0 0 0 -49 -36 -37 -.08 5 5 | 2819 -455 19 98
| 14 31 |
jpl 144| 1 -1 -8 -7 -4 62 .55 19 18 | -436 -567 22 339
| 57 -56 |
mit 284| 0 0 0 -24 -70 -20 -.34 15 11 | -455 1171 22 205
| -7 28 |
ngs 230| 0 0 1 40 -57 2 -.13 10 8 | -1790 2816 2409 3499
| -64 -1 |
sio 251| 0 2 -3 52 239 34 -.20 15 14 | --- --- --- ---
| -33 -142 |
Table 2.1645.4 GPS week: 1645 Day: 4 MJD: 55763.000
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 254| 0 0 -2 -13 -7 44 -.17 9 8 | 668 -405 19 99
| 21 41 |
emr 97| -1 -4 -10 -91 -3 3 .32 16 16 | -40 -487 17 95
| 29 -45 |
esa 126| 1 0 3 -20 52 -7 .32 8 8 | -148 -2107 16 161
| 37 1 |
gfz 198| 0 0 5 71 -128 -14 -.17 10 9 | 115 -769 26 141
| -9 60 |
grg 130| 7 -1 5 -25 199 15 .68 28 25 | -231 -526 57 220
| 6 -336 |
igr n/a| 0 1 1 -47 -5 -61 -.04 5 5 | 2916 -772 19 90
| -9 27 |
jpl 144| 0 -3 -9 -31 4 -16 .59 20 19 | -434 -966 22 329
| -26 100 |
mit 284| -1 1 0 -18 -48 -29 -.34 14 10 | 2378 -2792 25 190
| -20 41 |
ngs 230| 0 0 2 27 -51 -19 -.17 9 7 | 658 -410 2255 3778
| -17 -56 |
sio 251| -2 3 -4 31 244 20 -.22 17 15 | --- --- --- ---
| -34 -123 |
Table 2.1645.5 GPS week: 1645 Day: 5 MJD: 55764.000
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 254| 0 0 -3 0 7 4 -.24 9 8 | -561 1419 14 79
| 16 -18 |
emr 97| -2 -2 -11 -62 16 11 .34 16 16 | 63 -124 17 103
| 22 -34 |
esa 126| 1 0 2 -20 73 3 .25 8 8 | -363 -1005 18 161
| 19 -1 |
gfz 198| 0 0 3 -13 -205 -39 -.25 11 10 | -334 702 25 131
| 18 20 |
grg 130| 2 0 12 -21 52 2 .58 16 16 | -245 -241 48 223
| 7 -159 |
igr n/a| 0 0 2 -27 -9 -19 -.08 5 5 | 2806 -240 21 98
| 8 29 |
jpl 144| -2 -3 -9 -15 3 87 .60 17 16 | -629 -257 22 323
| 76 -125 |
mit 284| 0 0 -2 -23 -99 -21 -.38 16 12 | -135 1899 23 144
| -17 52 |
ngs 230| -1 0 3 78 37 -36 -.22 11 9 | -97 782 1797 3274
| -28 -77 |
sio 251| -1 2 -5 51 211 16 -.27 19 16 | --- --- --- ---
| -42 -121 |
Table 2.1645.6 GPS week: 1645 Day: 6 MJD: 55765.000
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 254| 0 0 -3 19 -12 6 -.22 7 7 | -416 1295 13 71
| 7 -9 |
emr 97| 1 -1 -7 -34 15 5 .33 18 18 | -334 231 14 110
| 6 -59 |
esa 126| 1 0 1 0 79 11 .28 6 6 | -838 -213 15 162
| 13 -9 |
gfz 198| 0 0 -1 -136 -124 -13 -.25 10 9 | 90 22 22 137
| 11 24 |
grg 130| 1 0 13 6 1 7 .67 16 15 | -998 104 42 224
| -54 -20 |
igr n/a| 0 0 2 -34 -24 -56 -.09 5 5 | 2194 496 20 96
| 35 11 |
jpl 144| -2 0 -11 -13 -5 -51 .55 18 17 | -1374 111 20 307
| -16 -47 |
mit 284| -1 0 0 -69 -68 0 -.38 14 10 | 1582 -1121 24 195
| -4 32 |
ngs 230| 0 0 2 129 -35 -21 -.18 9 6 | -350 1162 2164 3923
| -96 7 |
sio 251| 0 2 -3 1 245 20 -.24 19 16 | --- --- --- ---
| -14 -124 |
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 3.1645.0 GPS week: 1645 Day: 0 MJD: 55759.000
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
------+--------------------------------------------------------+---------------------------------------------------------
2 | 8 13 8 11 10 6 15 12 9 29 4 | 20 24 20 27 19 20 22 25 24 21 19
3 | 8 18 5 9 11 5 14 6 10 26 4 | 104 104 101 105 99 101 101 104 103 98 102
4 | 9 11 6 10 11 6 9 11 9 19 3 | 28 37 37 33 40 33 34 38 31 32 33
5 | 7 20 8 13 11 6 20 8 10 23 4 | 18 27 20 23 25 19 27 23 23 22 19
6 | 8 18 6 10 9 4 16 6 11 26 4 | 29 37 33 31 35 32 41 33 33 42 32
7 | 7 19 9 22 18 5 19 10 6 15 4 | 14 30 22 25 28 17 27 19 13 16 17
8 | 6 15 9 8 14 4 10 12 5 14 3 | 17 27 24 18 23 19 25 21 17 19 18
9 | 8 14 5 11 11 4 9 10 9 11 3 | 17 22 22 17 21 18 21 21 22 19 18
10 | 8 13 5 10 11 6 9 17 9 24 4 | 27 34 33 36 39 29 31 43 28 34 31
11 | 8 14 5 11 11 4 15 14 9 16 3 | 35 38 39 37 41 37 37 39 34 36 36
12 | 7 19 8 15 19 4 21 11 6 10 4 | 16 28 16 16 27 15 29 21 16 19 15
13E | 5 15 6 9 16 5 20 12 10 11 3 | 29 33 30 31 38 29 35 35 31 34 30
14E | 5 13 6 9 13 3 24 8 7 16 3 | 18 23 21 19 20 18 25 21 22 22 18
15E | 5 24 8 10 11 4 19 12 11 10 4 | 13 25 19 16 14 15 21 19 19 15 14
16 | 8 24 6 13 15 4 20 11 9 16 4 | 20 31 22 14 26 18 29 15 17 18 18
17 | 8 15 8 7 19 4 16 9 9 13 3 | 60 71 76 75 71 75 72 76 74 77 71
18 | 7 25 8 9 13 4 22 10 8 28 4 | 18 33 21 19 23 19 33 22 20 24 18
19 | 6 19 4 8 15 6 20 11 10 17 4 | 21 29 20 16 23 17 28 22 18 23 19
20 | 9 17 6 12 9 3 16 9 9 17 3 | 24 25 24 25 22 23 25 22 22 21 22
21 | 6 19 7 9 12 7 15 13 6 21 4 | 20 28 24 27 27 23 25 23 22 20 22
22 | 6 22 8 9 12 5 20 12 6 20 4 | 16 29 21 21 26 18 30 22 18 19 18
23E | 5 16 5 13 12 4 18 9 9 15 3 | 16 25 19 19 21 18 23 13 17 21 16
24 | 6 14 5 9 11 4 8 11 9 15 3 | 26 28 27 28 28 26 24 31 22 27 26
25 | 7 18 6 7 20 5 24 12 9 14 4 | 15 27 20 18 32 18 38 20 21 22 18
26E | 12 15 9 16 17 8 19 28 13 15 5 | 33 31 29 30 31 32 34 26 34 32 28
27 | 8 13 5 12 12 4 10 9 10 9 3 | 15 21 19 16 20 16 23 20 19 17 17
28 | 6 17 7 10 22 4 18 9 8 14 4 | 14 25 18 12 33 14 27 17 15 17 15
29 | 6 26 10 8 16 3 22 9 11 12 4 | 18 33 17 16 20 17 26 20 17 24 16
X30 | 11 22 15 10 12 10 --- 16 --- --- 6 | 14 25 18 19 19 16 --- 19 --- --- 14
31 | 6 20 7 9 16 4 17 7 10 16 4 | 17 28 20 20 30 16 26 20 17 19 17
32 | 6 17 4 8 9 4 15 7 11 12 3 | 16 20 22 23 23 18 20 20 19 18 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 11 14 5 17 12 9 18 |T 24 32 27 26 30 25 31 28 26 27 25
WRMS | 7 18 7 11 13 5 16 11 7 17 |NE 21 30 25 24 28 22 29 25 23 24 22
MEDI | 7 17 6 10 12 4 17 11 9 15 |MD 18 28 22 21 26 18 27 22 21 21 18
Table 3.1645.1 GPS week: 1645 Day: 1 MJD: 55760.000
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
------+--------------------------------------------------------+---------------------------------------------------------
2 | 7 18 11 18 10 4 17 12 10 28 5 | 17 24 18 33 15 19 22 22 19 17 17
3 | 15 18 6 8 14 6 16 7 8 25 4 | 91 95 91 92 86 94 92 92 96 93 92
4 | 8 12 6 11 9 4 11 14 9 19 3 | 24 29 30 27 31 26 29 28 25 27 25
5 | 9 20 6 10 12 6 22 11 15 20 4 | 18 24 16 21 18 20 23 23 28 19 18
6 | 7 18 4 9 9 4 16 8 9 24 3 | 27 33 31 30 36 27 34 31 27 37 29
7 | 6 19 7 23 17 4 19 8 12 15 5 | 14 26 19 25 24 14 22 19 16 16 15
8 | 7 14 7 8 13 4 10 13 8 13 3 | 20 27 22 24 20 19 26 26 23 25 21
9 | 10 11 7 7 10 4 11 11 7 11 3 | 18 23 19 22 20 18 22 25 23 24 20
10 | 6 14 6 8 11 5 10 14 9 21 3 | 22 24 25 20 27 24 19 31 25 28 22
11 | 8 16 7 8 11 4 16 12 6 13 3 | 25 28 24 26 28 25 27 29 24 26 24
12 | 6 22 10 16 22 4 24 12 8 12 5 | 17 32 21 19 27 16 29 22 20 19 17
13E | 10 17 9 11 22 6 21 28 10 23 5 | 38 40 36 33 37 38 42 47 37 45 37
14E | 5 12 6 6 16 5 24 8 6 12 3 | 23 25 26 23 28 24 28 23 28 23 23
15E | 8 17 8 11 8 8 24 13 6 13 4 | 20 29 22 22 21 24 24 24 24 20 21
16 | 7 26 7 15 17 7 23 12 8 16 4 | 15 28 19 20 23 15 27 13 16 15 15
17 | 33 18 8 11 22 8 17 8 10 15 6 | 53 73 71 73 76 74 70 71 75 71 69
18 | 8 20 9 13 14 5 23 8 10 26 4 | 16 27 19 21 21 16 28 19 18 18 15
19 | 7 19 8 8 18 5 20 9 5 14 4 | 19 28 19 16 25 15 26 19 17 21 17
20 | 8 18 7 9 11 5 17 10 8 17 3 | 21 20 16 18 18 17 20 17 18 14 16
21 | 5 17 9 7 12 4 19 8 6 22 4 | 24 25 26 25 22 23 25 28 26 23 23
22 | 7 18 7 9 12 4 20 11 6 18 4 | 12 25 15 15 20 13 26 18 14 13 13
23E | 6 18 6 13 22 6 17 9 8 13 4 | 14 21 15 20 19 15 20 16 18 16 14
24 | 6 15 5 6 15 4 11 12 10 13 3 | 41 41 40 45 40 42 37 44 41 40 41
25 | 8 20 8 12 18 4 20 12 9 13 4 | 18 30 22 21 30 21 38 26 22 26 21
26E | 16 16 10 15 17 7 19 27 16 21 6 | 34 39 32 42 34 38 38 57 46 47 38
27 | 11 12 7 9 11 5 12 12 6 10 3 | 15 22 18 21 17 16 23 25 22 23 18
28 | 6 15 8 6 21 4 19 10 5 14 3 | 15 27 20 13 29 18 24 19 20 17 17
29 | 8 26 7 8 16 6 22 9 9 11 4 | 19 33 19 16 22 19 27 23 21 24 19
X30 | 7 29 12 11 14 12 --- 15 --- --- 6 | 12 34 18 20 16 20 --- 18 --- --- 16
31 | 7 19 12 8 18 3 20 7 12 16 4 | 19 28 27 22 31 20 27 20 26 21 21
32 | 10 16 5 8 12 3 13 9 9 12 3 | 15 17 16 20 19 16 17 18 21 15 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 8 11 15 5 18 12 9 17 |T 23 31 26 27 28 25 30 28 27 27 24
WRMS | 8 18 8 11 13 5 17 11 9 16 |NE 20 28 23 24 25 21 27 25 24 23 21
MEDI | 7 18 7 9 14 5 19 11 8 15 |MD 19 28 21 22 24 20 26 23 23 23 20
Table 3.1645.2 GPS week: 1645 Day: 2 MJD: 55761.000
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
------+--------------------------------------------------------+---------------------------------------------------------
2 | 8 18 7 14 9 3 16 12 6 29 4 | 19 22 15 28 15 17 22 22 18 17 16
3E | 9 15 8 8 11 6 14 8 10 22 4 | 106 111 106 113 102 107 109 111 112 104 108
4 | 9 15 6 13 9 6 12 16 11 22 4 | 28 34 35 34 39 33 36 35 34 33 32
5 | 6 17 7 13 11 5 21 14 8 19 4 | 18 22 16 21 18 16 23 24 21 23 16
6 | 7 18 5 7 10 4 15 10 11 25 4 | 29 35 31 31 36 28 36 28 34 37 31
7 | 7 22 8 12 14 5 19 9 5 13 4 | 16 30 20 23 24 16 26 18 14 18 16
8 | 6 10 5 26 14 4 9 14 6 14 4 | 22 27 23 28 24 22 24 30 20 28 21
9 | 8 12 8 6 8 3 13 15 6 14 3 | 17 24 18 20 18 18 23 29 20 25 18
10 | 6 13 7 9 14 5 5 16 9 21 3 | 22 28 23 26 30 21 26 31 25 29 23
11 | 6 13 7 11 11 5 16 12 7 15 3 | 32 33 32 31 39 31 37 33 30 30 31
12 | 6 22 9 13 14 6 23 12 6 11 4 | 15 29 17 14 26 14 28 22 17 19 14
13E | 7 19 7 9 14 4 21 16 8 15 4 | 24 29 23 22 31 20 31 25 20 27 22
14E | 7 14 7 8 13 4 23 11 8 10 3 | 15 23 20 16 25 15 26 15 17 16 16
15E | 6 25 8 13 11 6 25 12 9 13 4 | 18 26 17 17 20 15 26 15 15 15 14
16 | 7 26 6 13 13 7 24 15 12 16 4 | 17 32 21 13 25 17 34 15 19 16 18
17 | 21 15 7 10 17 14 15 13 13 18 5 | 47 57 59 58 61 60 56 60 60 63 55
18 | 7 22 7 9 12 5 23 10 7 22 4 | 18 29 18 17 25 17 31 19 19 19 16
19 | 7 21 6 8 17 3 18 9 6 14 3 | 18 31 20 17 25 17 26 21 18 22 17
20 | 5 21 5 11 9 5 16 11 7 17 3 | 21 26 19 23 22 20 26 19 23 21 19
21 | 6 17 5 8 11 4 22 11 8 20 4 | 21 26 24 21 24 20 28 19 22 19 20
22 | 7 20 6 8 12 5 20 12 9 16 4 | 16 27 18 18 26 17 29 21 18 15 16
23E | 5 20 5 13 17 3 17 10 6 9 3 | 18 29 20 22 27 20 28 22 22 22 20
24 | 8 12 5 11 9 6 8 10 9 18 3 | 39 39 32 37 37 35 41 33 36 29 34
25 | 4 18 5 6 17 4 22 13 8 9 3 | 16 26 21 17 29 15 36 21 19 20 17
26E | 13 19 7 13 13 6 17 28 12 17 5 | 40 46 37 37 42 38 44 56 44 44 39
27 | 8 12 7 6 10 5 14 19 7 14 3 | 16 23 16 19 18 17 27 31 17 28 17
28 | 5 19 5 9 18 4 17 11 7 13 3 | 15 27 17 12 30 14 27 15 19 18 15
29 | 7 23 7 10 15 4 20 11 5 11 4 | 18 29 14 17 22 17 29 21 18 24 16
X30 | 7 18 10 15 9 10 --- 14 --- --- 5 | 10 22 17 20 15 13 --- 14 --- --- 11
31 | 6 18 6 9 16 3 17 7 7 15 3 | 15 28 22 21 30 19 30 19 19 18 18
32 | 7 18 5 9 11 5 14 10 10 11 3 | 16 22 20 22 25 16 22 19 20 18 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 11 13 5 18 13 8 17 |T 23 32 25 26 30 24 32 27 26 27 24
WRMS | 7 18 7 10 12 5 17 12 6 18 |NE 20 28 22 23 26 20 29 24 22 24 20
MEDI | 7 18 7 10 12 5 17 12 8 15 |MD 18 28 20 21 25 17 28 22 20 22 18
Table 3.1645.3 GPS week: 1645 Day: 3 MJD: 55762.000
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 --- --- --- --- 6433 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
2 | 6 18 11 14 13 4 19 15 8 28 5 | 18 23 19 27 22 17 23 21 20 20 17
3E | 11 16 9 6 16 7 18 12 12 20 4 | 92 92 87 90 79 88 82 92 93 85 88
4 | 6 12 9 7 12 4 11 14 8 19 3 | 22 26 30 22 29 23 26 27 25 24 23
5 | 7 17 9 10 12 5 21 14 14 19 4 | 17 24 20 20 24 21 29 23 26 25 18
6 | 9 20 5 7 15 6 18 11 10 22 4 | 39 44 42 39 50 42 50 41 38 47 40
7 | 6 18 5 9 21 3 26 10 10 13 4 | 15 29 21 21 30 17 31 19 20 19 17
8 | 5 11 7 7 14 4 12 9 8 10 3 | 35 36 34 29 33 33 37 35 34 33 32
9 | 7 13 8 4 9 3 12 13 6 11 3 | 18 21 18 20 27 18 22 27 20 21 18
10 | 5 11 6 5 10 6 14 14 14 20 3 | 25 31 31 30 34 26 28 33 27 31 27
11 | 7 14 5 6 19 5 17 9 11 13 3 | 33 34 33 34 37 32 36 30 33 29 32
12 | 5 19 9 10 16 4 23 12 9 11 4 | 19 30 20 19 33 19 30 23 24 21 19
13E | 4 18 4 7 13 5 24 13 13 10 4 | 19 34 24 22 35 23 36 22 31 23 24
14E | 8 12 8 9 16 5 21 12 9 11 3 | 24 29 28 27 30 27 37 28 29 30 26
15E | 7 22 9 9 16 5 20 11 8 11 4 | 20 30 22 23 23 22 31 27 25 21 21
16 | 8 24 7 11 13 7 24 13 10 16 4 | 21 35 25 20 33 23 37 17 24 20 22
17 | 6 20 7 6 18 7 15 10 10 11 3 | 33 41 37 38 42 34 39 37 37 35 35
18 | 6 18 6 9 13 4 21 9 9 21 4 | 19 26 17 19 26 17 31 16 18 17 16
19 | 6 22 8 7 16 4 20 12 10 14 4 | 21 37 21 24 28 22 32 26 22 25 21
20 | 8 18 8 11 11 4 17 9 11 17 4 | 21 24 23 24 23 22 26 21 25 23 21
21 | 7 13 6 7 12 5 18 12 9 21 3 | 22 27 24 23 28 21 31 25 23 21 22
22 | 7 19 8 7 14 4 19 10 7 17 4 | 16 27 16 18 27 16 27 17 17 14 15
23E | 5 20 5 10 10 4 21 11 11 9 3 | 13 24 16 17 24 13 28 13 14 15 13
24 | 7 11 4 5 21 4 11 9 10 13 3 | 29 29 29 31 33 28 28 30 29 27 29
25 | 7 16 8 7 22 4 23 15 10 11 4 | 22 30 24 25 37 22 40 23 27 25 23
26E | 14 15 12 13 18 7 17 52 20 12 7 | 29 37 32 33 37 32 38 56 36 33 30
27 | 9 15 9 7 12 5 12 16 7 10 3 | 20 25 20 22 28 20 26 31 24 27 20
28 | 6 18 8 7 22 3 18 10 7 13 4 | 15 27 18 15 33 15 27 16 21 17 16
29 | 7 23 8 8 15 6 18 13 9 11 4 | 18 31 17 18 24 17 26 20 21 22 17
X30 | 7 21 10 8 16 7 --- 12 --- --- 5 | 16 25 20 17 19 10 --- 17 --- --- 15
31 | 8 18 11 19 17 4 16 8 13 15 4 | 21 34 28 32 32 24 36 25 20 25 24
32 | 7 16 5 9 13 3 17 9 7 8 3 | 21 23 27 28 28 22 27 23 24 24 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 8 9 15 5 19 15 10 15 |T 24 31 26 26 31 24 33 27 27 26 24
WRMS | 7 17 7 8 14 5 18 11 8 14 |NE 21 28 23 24 29 21 30 24 24 23 21
MEDI | 7 18 8 7 15 4 18 12 10 13 |MD 21 29 24 23 30 22 31 25 24 24 22
Table 3.1645.4 GPS week: 1645 Day: 4 MJD: 55763.000
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 | 157 --- 6 --- --- 87 --- --- --- --- 0 | 9999 --- 9999 --- --- 9999 --- --- --- --- 9999
2 | 6 15 9 11 19 4 24 13 8 28 4 | 21 23 19 27 25 21 25 23 22 22 18
3E | 15 16 13 8 27 6 17 16 18 25 5 | 77 78 71 75 79 75 73 82 79 79 75
4 | 5 11 8 8 18 4 13 9 9 18 3 | 25 34 33 30 40 31 36 29 30 29 29
5 | 8 15 8 10 18 3 25 9 5 22 4 | 16 22 17 23 25 17 25 22 21 25 16
6 | 18 20 8 8 37 6 16 11 15 26 5 | 44 58 57 53 55 53 61 51 50 59 51
7 | 6 19 6 8 29 4 21 9 9 11 4 | 12 27 17 17 36 12 28 18 19 17 14
8 | 6 10 7 6 18 4 12 8 7 10 3 | 18 21 21 19 33 19 26 20 17 17 18
9 | 8 13 9 6 32 4 13 21 7 13 4 | 16 22 20 19 31 17 24 29 21 21 17
10 | 6 8 6 10 18 5 12 13 8 22 3 | 21 27 27 28 35 24 28 29 26 29 24
11 | 6 14 6 8 19 4 18 6 8 14 3 | 26 25 28 32 29 25 25 25 25 20 24
12 | 7 17 11 13 25 3 25 10 7 12 4 | 17 27 19 18 36 16 29 20 21 18 16
13E | 6 19 8 9 15 3 21 10 9 14 4 | 20 29 23 23 31 20 30 19 25 20 20
14E | 8 13 6 8 26 5 22 12 9 16 4 | 20 26 23 19 27 22 28 19 23 22 19
15E | 7 20 9 11 26 4 25 10 7 12 4 | 19 29 23 25 37 22 26 29 22 27 21
16 | 8 20 7 12 28 6 24 10 12 17 4 | 17 25 18 12 36 13 31 13 17 13 14
17 | 6 19 10 11 18 4 16 9 8 9 3 | 29 38 33 34 36 34 36 35 34 35 32
18 | 7 18 8 7 50 5 23 11 7 23 5 | 14 27 19 16 54 16 35 15 19 15 15
19 | 7 22 9 8 28 4 16 9 12 12 4 | 20 33 17 15 37 17 29 23 17 22 17
X20 | 8 18 7 11 --- 4 16 10 6 18 4 | 17 25 17 19 --- 16 23 16 20 16 15
X21 | 5 15 5 8 --- 7 17 9 8 19 3 | 18 25 21 16 --- 23 30 20 22 19 18
22 | 9 20 7 7 54 5 19 11 7 17 5 | 15 27 16 18 60 16 28 16 21 15 16
23E | 7 19 6 13 17 4 17 10 9 13 4 | 15 24 14 20 21 12 19 15 17 16 13
24 | 8 10 6 6 17 5 13 8 7 15 3 | 20 19 20 25 25 19 18 20 21 15 18
25 | 8 14 7 16 26 5 27 10 9 11 4 | 17 25 18 28 40 20 34 22 24 22 18
26E | 15 14 12 12 29 6 19 42 17 14 7 | 24 30 27 25 41 26 26 57 36 31 27
27 | 13 12 8 10 29 7 13 24 6 16 4 | 15 20 17 16 27 16 23 28 19 22 14
X28 | 7 14 8 8 --- 3 19 9 12 13 4 | 13 24 18 15 --- 15 27 15 20 15 14
29 | 7 24 7 9 31 6 27 12 6 11 4 | 19 35 21 19 30 17 36 20 16 21 18
X30 | 11 17 9 13 33 10 --- 11 --- --- 6 | 16 22 22 22 34 14 --- 19 --- --- 17
31 | 7 15 7 10 34 4 19 9 10 17 4 | 19 29 23 26 45 20 29 20 28 21 21
32 | 9 13 6 11 17 4 15 9 5 10 3 | 17 18 20 22 21 16 19 17 20 15 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 8 10 28 5 20 14 9 17 |T 21 28 23 24 36 22 30 25 25 23 21
WRMS | 8 16 8 9 25 5 19 10 7 15 |NE 18 25 20 21 35 18 28 21 21 20 18
MEDI | 7 15 7 9 26 4 18 10 8 14 |MD 18 26 20 22 35 19 28 20 21 21 18
Table 3.1645.5 GPS week: 1645 Day: 5 MJD: 55764.000
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 | 158 --- 6 --- --- 54 --- --- --- --- 0 | 9999 --- 9999 --- --- 9999 --- --- --- --- 9999
2 | 8 15 10 17 12 5 18 16 10 29 5 | 14 19 17 30 13 17 22 22 17 18 15
3E | 15 15 10 13 20 7 17 21 22 29 6 | 70 69 64 71 63 68 67 71 73 66 67
4 | 7 9 6 8 13 5 14 11 9 20 3 | 20 27 29 24 33 25 28 20 22 19 22
5 | 10 16 10 10 16 4 20 14 11 26 5 | 15 22 21 20 15 17 26 26 22 33 18
6E | 22 19 8 13 21 6 17 11 10 31 6 | 96 103 102 97 99 94 102 96 97 96 97
7 | 8 15 7 9 20 4 21 8 9 13 4 | 10 27 20 21 28 14 27 14 14 15 15
8 | 6 10 6 9 12 5 10 9 8 9 3 | 26 29 32 23 27 27 34 27 26 28 27
9 | 8 11 8 6 14 5 12 25 9 14 4 | 11 16 18 17 17 14 19 30 15 17 14
10 | 8 9 6 12 11 5 10 16 16 25 4 | 21 24 27 33 30 23 23 28 23 29 24
11 | 8 13 5 7 13 5 17 11 13 15 3 | 22 26 26 25 33 24 30 22 25 19 23
12 | 9 16 9 14 21 3 16 15 11 17 4 | 15 26 17 20 27 14 26 18 16 18 14
13E | 7 18 7 9 12 5 20 12 13 11 4 | 16 30 20 22 27 17 31 18 20 20 19
14E | 8 13 7 11 20 4 21 12 8 15 4 | 18 23 24 22 31 18 30 18 17 21 19
15E | 8 23 11 11 14 4 17 19 10 16 5 | 17 30 24 21 27 17 22 30 22 26 19
16 | 7 19 7 15 24 7 20 12 10 22 5 | 21 26 22 12 38 20 27 17 21 18 19
17 | 6 22 8 8 15 5 17 12 17 11 4 | 32 40 37 31 39 37 35 33 41 34 34
18 | 8 19 8 9 16 4 19 15 10 25 4 | 14 28 17 13 22 14 28 16 13 21 13
19 | 6 22 7 10 18 5 18 12 7 11 4 | 19 35 21 17 27 19 25 22 20 21 20
20 | 10 16 9 10 13 5 14 12 11 19 4 | 16 21 15 17 18 12 21 13 15 14 13
21 | 8 14 8 8 12 5 19 10 9 20 4 | 17 26 25 21 26 22 23 21 23 20 20
22 | 8 17 7 9 13 5 17 11 7 19 4 | 12 25 19 19 22 15 24 15 15 20 15
23E | 7 20 7 13 19 4 16 12 11 14 4 | 10 22 14 16 14 12 21 16 16 16 11
24 | 6 11 5 6 14 5 12 11 11 17 3 | 15 16 14 17 22 15 14 20 18 14 14
25 | 9 13 8 12 23 5 23 11 6 15 4 | 16 25 22 20 35 16 38 17 16 18 17
26E | 14 13 9 10 14 5 17 41 20 15 6 | 21 27 19 26 22 22 26 49 32 26 22
27 | 9 12 8 9 17 7 14 26 9 18 4 | 12 15 17 18 18 14 22 31 17 23 14
28 | 6 18 5 7 19 4 18 9 11 13 4 | 11 25 17 14 31 13 27 12 14 15 13
29 | 9 21 9 9 15 4 21 11 8 12 4 | 15 28 16 16 18 14 26 19 14 17 15
X30 | 14 23 20 --- --- 22 --- 11 --- --- 10 | 20 25 30 --- --- 22 --- 18 --- --- 20
31 | 6 15 10 21 19 6 14 13 9 16 4 | 17 27 21 24 36 18 29 18 19 15 17
32 | 8 11 7 8 12 4 16 11 8 12 3 | 12 15 14 17 19 12 20 15 15 11 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 8 11 16 5 17 16 11 19 |T 21 28 25 24 29 22 29 25 23 24 22
WRMS | 8 16 8 10 16 5 16 12 9 16 |NE 16 24 21 20 25 18 25 20 19 19 17
MEDI | 8 15 8 9 15 5 17 12 10 16 |MD 16 26 21 20 27 17 26 20 18 19 18
Table 3.1645.6 GPS week: 1645 Day: 6 MJD: 55765.000
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 | 52 --- 44 --- --- 98 --- --- --- --- 48 | 9999 --- 9999 --- --- 9999 --- --- --- --- 9999
2 | 7 18 7 17 9 3 21 14 10 31 4 | 21 25 17 32 17 19 25 25 22 22 19
3E | 15 18 8 11 17 6 19 23 19 25 5 | 70 72 67 73 61 69 66 77 78 73 70
4 | 6 13 5 7 12 5 12 8 11 21 3 | 25 26 34 26 35 29 28 29 30 26 28
5 | 8 19 7 9 16 7 22 13 11 26 4 | 18 23 18 24 25 18 26 24 18 30 17
6E | 11 22 6 12 13 7 15 13 8 29 4 | 48 55 52 48 54 50 55 45 49 56 49
7 | 6 18 5 9 18 6 18 7 6 19 3 | 14 25 19 20 24 16 25 18 17 22 16
8 | 6 12 5 7 14 5 10 8 7 9 2 | 23 25 25 25 24 23 25 25 22 21 22
9 | 7 14 5 6 11 4 12 21 7 13 3 | 18 16 20 14 19 14 18 26 14 16 17
10 | 5 10 5 6 16 5 9 15 10 27 3 | 32 34 36 35 44 33 33 40 35 34 34
11 | 4 12 5 8 13 6 21 8 6 15 3 | 32 31 33 36 42 33 37 32 35 28 33
12 | 7 19 7 13 16 5 20 12 7 17 4 | 15 27 16 17 25 14 28 19 18 19 15
13E | 4 19 6 8 16 5 21 9 9 17 3 | 23 32 25 22 33 23 38 22 25 24 24
14E | 5 13 6 8 18 5 21 17 9 14 4 | 13 21 19 17 21 15 25 16 17 20 15
15E | 7 22 6 11 29 5 23 13 6 10 4 | 29 32 27 27 36 27 30 30 28 30 27
16 | 6 23 5 13 13 9 23 10 9 21 4 | 19 33 24 16 30 20 39 15 22 17 21
17 | 6 20 6 7 18 3 20 6 5 11 3 | 26 32 28 28 38 30 33 28 28 26 27
18 | 6 20 8 12 13 4 20 14 9 31 4 | 16 27 19 18 25 15 31 17 17 24 15
19 | 6 23 6 10 17 5 18 9 6 12 3 | 20 39 23 21 31 20 33 25 18 23 21
20 | 8 17 7 11 13 6 19 8 7 21 3 | 21 22 18 22 23 20 27 19 18 20 19
21 | 6 17 6 7 12 3 21 10 10 21 3 | 20 28 22 22 28 20 29 21 22 20 20
22 | 5 18 6 10 12 5 17 11 7 23 3 | 15 25 18 20 29 17 27 15 20 20 17
23E | 5 20 5 10 20 5 18 11 9 18 4 | 19 26 19 17 26 19 30 18 20 19 19
24 | 5 12 4 8 12 8 13 8 5 15 2 | 18 17 18 22 24 17 21 22 20 15 18
25 | 8 14 6 11 20 3 24 11 8 15 4 | 14 25 19 24 31 18 38 18 20 21 18
26E | 12 16 9 9 17 5 17 39 15 15 6 | 29 30 27 29 34 29 32 48 35 28 28
27 | 8 12 6 7 11 5 11 23 5 12 3 | 17 13 16 15 18 13 19 27 14 16 16
28 | 6 21 6 10 14 6 26 10 5 18 4 | 15 27 15 14 27 15 30 16 16 21 14
29 | 7 24 5 10 19 4 18 13 5 12 4 | 23 37 20 19 26 19 31 22 18 23 21
X30 | 16 23 17 --- --- 33 --- 9 --- --- 9 | 17 30 31 --- --- 29 --- 21 --- --- 22
31 | 6 17 5 11 16 5 17 17 6 16 4 | 20 29 24 21 35 22 32 24 24 17 22
32 | 8 17 3 9 15 4 14 10 5 13 3 | 19 20 20 26 30 18 27 20 20 16 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 6 10 16 5 18 14 9 19 |T 22 29 24 25 30 23 31 25 24 24 23
WRMS | 7 18 6 9 15 5 17 10 6 16 |NE 19 26 22 22 28 20 28 22 21 21 20
MEDI | 6 18 6 9 15 5 18 11 7 17 |MD 20 27 20 22 28 20 30 22 20 21 20
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1645 GPS week: 1645 MJD: 55759.0-55765.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 |U 8 8 19 |U 6 9 25 |U 8 8 18 |
emr | emr 2967 |U 10 9 27 |U 8 15 28 | 10 10 20 |
esa | esa 3017 | 8 8 21 |U 5 7 22 | 8 7 16 |
gfz | gfz 2938 |U 9 8 24 |U 6 12 29 |U 9 7 19 |
grg | grg 2907 | 11 9 24 |U 6 8 26 | 12 11 22 |
igr | igr 2967 | 8 8 20 | 5 7 21 | 8 7 18 |
igs | igs 2995 | 8 8 21 | 5 8 23 | 7 7 17 |
jpl | jpl 2870 | 11 10 32 |U 9 21 36 |U 9 8 22 |
mit | mit 2976 |U 8 8 21 |U 8 21 35 |U 8 10 19 |
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 5.1645.0 GPS week: 1645 Day: 0 MJD: 55759.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 9 21 | 4 6 21 | 8 11 16 |
emr | emr 2972 | 11 8 29 | 10 19 40 | 9 6 26 |
esa | esa 2976 | 8 8 22 | 3 5 20 | 8 7 17 |
gfz | gfz 2966 | 8 9 21 | 10 18 43 | 14 10 20 |
grg | grg 2976 | 9 9 22 | 5 6 28 | 8 9 16 |
igr | igr 2976 | 7 10 23 | 4 6 20 | 7 8 17 |
igs | igs 2952 | 8 9 22 | 3 5 18 | 8 9 17 |
jpl | jpl 2867 | 10 9 26 | 9 26 40 | 8 7 22 |
mit | mit 2976 | 10 9 28 | 12 36 49 | 8 11 21 |
Table 5.1645.1 GPS week: 1645 Day: 1 MJD: 55760.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 19 | 4 5 20 | 7 5 17 |
emr | emr 2966 | 11 9 28 | 8 18 38 | 11 8 24 |
esa | esa 2976 | 7 6 19 | 4 5 20 | 7 6 17 |
gfz | gfz 2964 | 8 7 19 | 5 16 30 | 6 5 16 |
grg | grg 2976 | 9 6 21 | 5 5 25 | 8 6 17 |
igr | igr 2976 | 8 6 18 | 5 6 21 | 7 6 17 |
igs | igs 2970 | 8 6 21 | 4 4 18 | 7 6 18 |
jpl | jpl 2875 | 16 10 46 | 12 30 57 | 8 6 22 |
mit | mit 2976 | 8 6 19 | 5 16 39 | 7 8 18 |
Table 5.1645.2 GPS week: 1645 Day: 2 MJD: 55761.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 18 | 12 17 42 | 8 6 15 |
emr | emr 2972 | 9 8 27 | 9 17 22 | 11 11 19 |
esa | esa 2976 | 6 6 20 | 10 17 27 | 8 7 15 |
gfz | gfz 2967 | 6 7 21 | 15 21 52 | 9 7 15 |
grg | grg 2976 | 7 6 20 | 10 14 27 | 11 8 17 |
igr | igr 2976 | 7 6 20 | 10 14 26 | 8 7 15 |
igs | igs 2973 | 7 5 19 | 15 21 49 | 9 7 15 |
jpl | jpl 2870 | 8 8 26 | 15 30 48 | 9 10 20 |
mit | mit 2976 | 6 6 20 | 9 21 29 | 10 8 16 |
Table 5.1645.3 GPS week: 1645 Day: 3 MJD: 55762.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2992 | 7 6 18 | 5 11 24 | 6 4 20 |
emr | emr 2968 | 9 9 25 | 8 10 24 | 6 5 19 |
esa | esa 2976 | 7 8 21 | 5 8 24 | 6 5 18 |
gfz | gfz 2967 | 7 8 18 | 4 8 24 | 5 5 18 |
grg | grg 2976 | 7 7 19 | 5 8 27 | 7 9 23 |
igr | igr 2971 | 7 8 20 | 5 9 24 | 5 4 17 |
igs | igs 2967 | 7 7 19 | 5 8 23 | 6 4 17 |
jpl | jpl 2871 | 11 10 36 | 6 15 28 | 4 4 18 |
mit | mit 2976 | 7 7 18 | 8 17 40 | 7 7 19 |
Table 5.1645.4 GPS week: 1645 Day: 4 MJD: 55763.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 7 8 19 | 4 6 24 | 9 15 27 |
emr | emr 2968 | 9 10 32 | 7 14 25 | 16 19 15 |
esa | esa 3072 | 12 9 28 | 3 7 24 | 8 11 18 |
gfz | gfz 2967 | 12 10 35 | 4 8 19 | 11 10 29 |
grg | grg 2688 | 18 12 27 | 6 7 33 | 28 27 39 |
igr | igr 2976 | 8 9 26 | 4 7 22 | 13 12 30 |
igs | igs 3061 | 9 9 28 | 3 6 21 | 8 13 20 |
jpl | jpl 2867 | 9 11 33 | 6 17 29 | 20 14 26 |
mit | mit 2976 | 9 11 25 | 6 20 36 | 8 19 23 |
Table 5.1645.5 GPS week: 1645 Day: 5 MJD: 55764.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 11 7 18 | 6 8 21 | 7 9 15 |
emr | emr 2968 | 11 8 30 | 8 16 28 | 10 8 21 |
esa | esa 3072 | 10 6 19 | 4 6 18 | 8 6 14 |
gfz | gfz 2872 | 14 8 33 | 4 6 16 | 7 7 14 |
grg | grg 2880 | 18 11 40 | 5 8 22 | 11 9 20 |
igr | igr 2975 | 11 6 18 | 5 6 17 | 7 6 15 |
igs | igs 3035 | 11 6 20 | 4 6 15 | 7 6 15 |
jpl | jpl 2871 | 13 11 43 | 6 11 23 | 8 7 19 |
mit | mit 2976 | 11 6 19 | 6 19 30 | 8 7 16 |
Table 5.1645.6 GPS week: 1645 Day: 6 MJD: 55765.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 9 13 19 | 6 8 21 | 8 8 17 |
emr | emr 2960 | 10 10 19 | 6 9 24 | 8 9 18 |
esa | esa 3072 | 8 10 17 | 3 4 19 | 9 8 14 |
gfz | gfz 2868 | 10 8 19 | 4 6 22 | ---- ---- ---- |
grg | grg 2880 | 11 9 18 | 4 6 22 | 10 10 22 |
igr | igr 2923 | 10 9 17 | 4 5 20 | 8 9 17 |
igs | igs 3013 | 9 10 15 | 4 5 20 | ---- ---- ---- |
jpl | jpl 2869 | 11 11 16 | 6 16 28 | 8 10 24 |
mit | mit 2976 | 8 10 16 | 6 16 25 | 10 8 18 |
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 6.1645 GPS week: 1645 MJD: 55759.500-55765.500
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 -19 24 -56 -1 | 4 16
| 22 17 118 78 7 | 2
emr uuuuu | 50 -7 72 153 7 | 21 29
| 22 22 73 130 8 | 3
esa uuuuu | 4 -31 1 -60 2 | 11 19
| 18 17 16 50 4 | 2
gfz uuuuu | -74 -10 -28 -58 -8 | 4 17
| 26 19 37 98 4 | 2
grg xuuux | 106 -12 43 -174 90 | -87 130
| 110 35 153 97 23 | 15
igr xxxxx | -29 -14 31 -24 -3 | 5 17
| 18 20 52 70 5 | 2
irf xxxxx | -4 -4 -50 -50 -1 | 3 16
| 12 9 32 34 2 | 2
jpl uuuuu | 4 -13 -25 104 5 | 21 28
| 68 39 129 26 11 | 5
mit uuuuu | -35 3 -160 -108 2 | 18 24
| 24 15 66 62 2 | 2
ngs uuuuu | 5 52 30 134 2 | 10 15
| 33 37 85 76 6 | 2
sio uuuuu | 124 28 123 59 -6 | 32 35
| 16 17 130 85 3 | 2
Table 7.1645.0 GPS week: 1645 Day: 0 MJD: 55759.500
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 | 23 -32 132 -148 -12 | 5 15
emr uuuuu | 52 32 -63 265 12 | 19 25
esa uuuuu | 7 -64 -18 -101 1 | 10 16
gfz uuuuu | -92 -29 15 -39 -6 | 4 15
grg xuuux | 37 -63 211 -126 81 | -107 142
igr xxxxx | -15 -20 87 -37 5 | 4 14
irf xxxxx | 4 -13 -21 -13 1 | 2 13
jpl uuuuu | 7 37 -139 152 11 | 15 23
mit uuuuu | -18 -15 -54 -52 5 | 16 21
ngs uuuuu | -5 114 21 80 -4 | 8 13
sio uuuuu | 138 28 49 56 -2 | 32 35
Table 7.1645.1 GPS week: 1645 Day: 1 MJD: 55760.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 4 12 78 -74 -5 | 6 16
emr uuuuu | 63 14 84 321 8 | 22 29
esa uuuuu | 16 -15 16 -79 4 | 11 18
gfz uuuuu | -83 -27 -9 -174 -1 | 6 17
grg xuuux | 31 23 81 -254 90 | -103 141
igr xxxxx | -1 -1 95 -114 -6 | 7 17
irf xxxxx | 7 2 -23 -41 1 | 4 15
jpl uuuuu | -62 -14 -122 94 -11 | 19 28
mit uuuuu | -11 4 -102 -113 5 | 18 24
ngs uuuuu | -6 10 24 217 -2 | 9 14
sio uuuuu | 136 41 46 70 -4 | 35 38
Table 7.1645.2 GPS week: 1645 Day: 2 MJD: 55761.500
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 -41 -76 -47 -6 | 7 16
emr uuuuu | 69 -9 91 205 -5 | 24 31
esa uuuuu | 29 -26 -2 -50 6 | 13 20
gfz uuuuu | -97 18 -96 -162 -7 | 8 18
grg xuuux | 69 -39 74 -138 120 | -96 140
igr xxxxx | -39 -18 57 -64 0 | 8 18
irf xxxxx | 5 -4 -85 -59 -2 | 6 17
jpl uuuuu | 2 -12 27 83 -5 | 21 29
mit uuuuu | -18 -6 -218 -119 2 | 20 26
ngs uuuuu | -37 45 101 167 5 | 11 16
sio uuuuu | 131 19 40 110 -8 | 36 39
Table 7.1645.3 GPS week: 1645 Day: 3 MJD: 55762.500
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 -19 -10 -63 -3 | 3 15
emr uuuuu | 69 -14 16 188 0 | 19 28
esa uuuuu | 9 -29 -17 -54 -4 | 10 18
gfz uuuuu | -99 1 -37 -104 -12 | 4 17
grg xuuux | 128 -32 248 -179 100 | -74 121
igr xxxxx | -37 -14 -19 -78 -11 | 4 17
irf xxxxx | -6 0 -94 -64 -3 | 2 16
jpl uuuuu | 50 -57 -141 97 12 | 18 27
mit uuuuu | -34 7 -247 -118 2 | 17 24
ngs uuuuu | -5 64 179 192 8 | 9 15
sio uuuuu | 136 33 -22 81 -5 | 31 34
Table 7.1645.4 GPS week: 1645 Day: 4 MJD: 55763.500
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 | -44 -22 -139 79 5 | 0 17
emr uuuuu | 42 -30 104 9 6 | 17 27
esa uuuuu | -4 -38 13 -96 3 | 8 19
gfz uuuuu | -63 8 -1 12 -8 | 1 20
grg xuuux | 333 -7 -141 -297 47 | -77 121
igr xxxxx | -30 8 32 69 -5 | 2 19
irf xxxxx | -3 -1 -56 -11 -3 | 1 18
jpl uuuuu | -103 25 197 83 8 | 19 27
mit uuuuu | -44 19 -180 -20 0 | 16 24
ngs uuuuu | 53 16 -69 78 0 | 8 15
sio uuuuu | 120 33 199 145 -9 | 29 34
Table 7.1645.5 GPS week: 1645 Day: 5 MJD: 55764.500
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 | -10 -9 -11 -136 5 | 4 16
emr uuuuu | 6 -15 156 -35 21 | 21 29
esa uuuuu | -27 -12 -7 -86 4 | 12 19
gfz uuuuu | -48 -11 -48 103 -12 | 4 18
grg xuuux | 131 0 -62 -4 91 | -77 121
igr xxxxx | -57 -1 -43 64 2 | 6 17
irf xxxxx | -28 7 -53 -111 -2 | 4 16
jpl uuuuu | 97 -69 75 127 21 | 25 29
mit uuuuu | -80 24 -157 -219 2 | 20 25
ngs uuuuu | 49 35 -39 190 -6 | 12 16
sio uuuuu | 93 49 206 -123 -5 | 32 35
Table 7.1645.6 GPS week: 1645 Day: 6 MJD: 55765.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 0 -25 196 -4 5 | 4 16
emr uuuuu | 50 -24 116 120 4 | 25 33
esa uuuuu | 0 -31 20 45 0 | 13 19
gfz uuuuu | -33 -29 -17 -43 -9 | 2 17
grg xuuux | 11 36 -109 -222 103 | -74 121
igr xxxxx | -20 -53 7 -9 -3 | 6 17
irf xxxxx | -9 -18 -14 -50 -2 | 4 15
jpl uuuuu | 38 -2 -68 92 0 | 28 33
mit uuuuu | -41 -14 -164 -111 -2 | 21 26
ngs uuuuu | -16 78 -9 17 10 | 11 16
sio uuuuu | 115 -4 347 72 -8 | 30 34
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