[IGSREPORT-20154] Wk 1652 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 22 04:52:46 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1652 (Sep 04, 2011 - Sep 10, 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:
igs1652[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1652[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1652[0-6].cls IGS GPS clock combination summary report.
igs16527.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16527.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 | COD | 30 30 NRIL
0 | EMR | 27
0 | ESA | KOSG IRKJ KOSG NICO
0 | GFZ | 30 MDVJ
0 | GRG | IRKJ USN3
0 | JPL | IRKJ
0 | MIT | 18 27 30 18 21 27 30 MAW1
1 | COD | 30 30 WILL
1 | EMR | 9 9
1 | ESA | 17 22 29 30 30 MDVJ REUN
1 | GFZ | 30 DAV1 MDVJ
1 | GRG | SANT
1 | JPL | 9 27 28
1 | MIT | 9 11 28 9 11 27 28 MAW1 MIZU CAS1 MIZU
2 | COD | 30 SYDN WROC YELL COCO MDVJ MOBS WROC YELL
2 | EMR | 9 9 YELL YELL
2 | ESA | 30
2 | GFZ | 30 BRUS MDVJ STJO YELL
2 | JPL | 9 27
2 | MIT | 9 26 27 9 26 27 BRUS BRUS HARB
3 | COD | 27 30 27 30 DARW KOSG
3 | EMR | 9 9 HARB HARB
3 | GFZ | 9 25 27 30 KOSG MDVJ
3 | GRG | SANT
3 | JPL | 9
3 | MIT | 9 27 9 27 BRMU
4 | COD | KOSG
4 | EMR | 9 27 9 27
4 | ESA | IRKJ
4 | GFZ | 27 30
4 | GRG | IRKJ LHAZ SANT USN3
4 | JPL | 9
4 | MIT | 1 9 30 1 9 27 30 NICO BOR1 KOSG NICO
5 | ALL | 27
5 | COD | MOBS MOBS
5 | EMR | 9 9
5 | ESA | 30 30 HOFN IRKJ UNSA
5 | GFZ | 30 MDVJ
5 | GRG | IRKJ LHAZ SANT USN3
5 | JPL | 9
5 | MIT | 1 9 1 9 MAC1
6 | COD | KOSG
6 | ESA | 29 30 30 KOSG TIXI BAN2 IRKJ KOSG TIXI
6 | GFZ | 7 8 27 30 ISPA QAQ1
6 | GRG | IRKJ SANT
6 | JPL | CHUR
6 | MIT | 1 7 8 27 30 1 7 8 11 27 30 DAV1 HARB DAV1 HARB MAW1
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
----+--------+---------------
2 | GRG | 27
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 | | | 2 | 1 | | | 1 |
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 | .4 .4 .6 -19 -15 23 -.05
EMR | -2.9 6.0 -2.6 19 15 10 .16
ESA | -3.0 3.1 16.0 70 23 56 -.04
GFZ | -.7 .7 .5 -40 13 14 .03
GRG | -4.8 3.8 15.2 -3 5 13 -.13
JPL | -5.3 5.7 .4 -12 -11 18 -.05
MIT | 1.7 1.0 14.2 -17 7 -16 .04
NGS | 1.8 -.6 8.4 -29 6 6 .05
SIO | 1.2 4.7 -8.9 82 -106 -6 -.04
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 did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 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 1.1652.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1652.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 2.1652.[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 3.1652.[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 5.1652.0-6).
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 1652 summary. (Sep 04, 2011 - Sep 10, 2011)
Table 1.1652.a GPS week: 1652 MJD: 55808.000-55814.000
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 252| 0 0 3 35 9 10 -.23 7 7 | -420 63 19 88
| 0 0 0 9 11 15 .02 | 758 493
emr 95| 0 3 -2 -22 -59 8 .46 20 20 | 1367 332 15 99
| 1 1 0 14 18 11 .03 | 1250 1136
esa 142| 0 0 0 -95 12 -18 .25 7 7 | -1304 1048 19 182
| 0 0 0 9 23 14 .03 | 1811 1549
gfz 197| 0 1 -4 51 -5 3 -.21 12 11 | 188 -186 22 101
| 1 0 2 23 78 13 .02 | 138 267
grg 129| 1 0 7 -11 -17 19 .56 15 14 | 119 139 54 238
| 0 0 3 11 29 12 .04 | 212 436
igr n/a| 0 0 0 5 -14 -23 -.06 5 4 | 2051 467 19 76
| 0 0 1 14 22 10 .02 | 1527 1139
jpl 133| -1 0 -5 39 10 60 .57 15 15 | 652 363 18 107
| 1 0 0 10 6 38 .02 | 1790 1315
mit 276| 1 -1 0 27 -27 -11 -.41 11 10 | -70 280 21 176
| 0 1 0 19 14 17 .02 | 1486 1884
ngs 221| 0 0 0 58 -36 -5 -.25 9 7 | 36462 -129656 1886 3540
| 0 1 0 24 47 13 .05 | 97523 343040
sio 250| 1 1 -3 -157 220 -36 -.14 22 21 | --- --- --- ---
| 1 1 1 19 23 11 .03 | --- ---
Table 1.1652.b GPS week : 1652 MJD: 55808.000-55814.000
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 14 13 14 13 |
2 | 4 4 5 4 4 5 4 |
3 | 3 3 3 3 4 4 4 |
4 | 4 5 4 3 4 4 4 |
5 | 4 4 4 4 4 4 4 |
6 | 3 3 3 3 3 3 4 |
7 | 5 4 4 4 4 4 4 |
8 | 3 4 3 3 4 4 4 |
9 | 6 5 5 5 6 5 5 |
10 | 3 4 4 3 4 3 4 |
11 | 3 4 3 3 3 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 5 4 4 4 4 4 4 |
15 | 5 5 5 5 5 5 5 |
16 | 6 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 5 |
21 | 4 4 5 4 5 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 4 4 4 4 4 5 |
24 | 4 4 4 4 5 4 4 |
25 | 4 5 4 5 4 4 4 |
26 | 3 4 4 3 4 3 3 |
27 | 9 7 8 9 8 14 6 |
28 | 5 5 5 5 5 5 5 |
29 | 4 5 4 4 4 4 4 |
30 | 4 4 3 4 6 7 6 |
31 | 5 5 4 4 5 5 5 |
32 | 4 4 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1652.0 GPS week: 1652 Day: 0 MJD: 55808.000
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 252| 0 0 3 33 0 11 -.24 7 7 | -559 -148 18 84
| 30 11 |
emr 95| 0 4 -2 -41 -38 -8 .42 20 20 | -558 854 14 102
| -13 -9 |
esa 142| -1 0 0 -88 18 -15 .26 6 6 | -1396 1672 16 159
| 43 -3 |
gfz 197| 0 2 -3 77 -59 -5 -.19 12 11 | 177 -343 26 101
| -25 33 |
grg 129| 2 0 3 -15 -75 17 .54 15 14 | 56 -71 47 246
| 70 49 |
igr n/a| 0 0 0 -11 7 -10 -.05 5 4 | -53 606 18 60
| -4 6 |
jpl 133| 0 0 -6 57 4 71 .55 15 14 | -1649 603 19 101
| -19 0 |
mit 276| 0 0 0 24 -30 6 -.38 11 11 | -62 191 23 180
| -20 -5 |
ngs 221| 0 0 1 27 21 -10 -.29 9 8 | -550 -153 1795 3888
| 13 -63 |
sio 250| 0 0 -4 -143 214 -57 -.15 24 22 | --- --- --- ---
| 38 -107 |
Table 2.1652.1 GPS week: 1652 Day: 1 MJD: 55809.000
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 252| 0 0 3 26 0 11 -.23 8 8 | -489 312 18 81
| 32 -7 |
emr 95| 1 3 -3 -32 -52 9 .46 20 20 | 610 1501 14 106
| -27 30 |
esa 142| 0 0 1 -105 43 -31 .27 7 7 | -1033 1852 18 220
| 47 -10 |
gfz 197| -1 1 -6 93 -26 27 -.21 13 14 | 299 -383 21 106
| -42 37 |
grg 129| 1 0 4 -5 -34 20 .58 13 12 | -1 548 48 244
| 67 8 |
igr n/a| 0 0 0 -5 -16 -25 -.05 5 5 | 739 1455 23 72
| 3 32 |
jpl 133| 0 -1 -5 33 19 37 .56 15 15 | -782 1315 17 107
| 3 -11 |
mit 276| 2 0 0 40 -31 14 -.41 11 10 | -159 610 18 167
| -28 -2 |
ngs 221| 0 1 0 26 -25 -12 -.31 8 6 | -465 227 1788 3684
| 60 50 |
sio 250| 0 0 -4 -142 210 -42 -.17 22 21 | --- --- --- ---
| 32 -131 |
Table 2.1652.2 GPS week: 1652 Day: 2 MJD: 55810.000
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 252| 0 0 2 29 15 33 -.21 7 7 | -465 249 18 85
| 35 -3 |
emr 95| 0 4 -2 -6 -85 22 .47 20 20 | 1227 1499 18 108
| -27 47 |
esa 142| -1 0 0 -97 -20 -9 .25 7 7 | -825 957 20 194
| 77 23 |
gfz 197| 1 2 -8 35 75 9 -.22 12 11 | 93 -252 22 106
| -44 56 |
grg 129| 2 1 7 -26 4 20 .63 14 13 | 174 274 43 243
| 47 -10 |
igr n/a| 0 0 -2 -6 -20 -29 -.04 4 4 | 1417 1757 21 97
| -5 28 |
jpl 133| 0 -1 -3 49 10 -5 .56 16 16 | -370 2179 22 165
| -14 -49 |
mit 276| 1 -1 0 54 -14 -1 -.43 9 9 | -66 345 21 191
| -21 -16 |
ngs 221| 0 -1 -1 64 -86 -23 -.24 8 7 | 257617 -907599 2011 3755
| 36 43 |
sio 250| 0 0 -2 -140 235 -24 -.15 21 22 | --- --- --- ---
| 41 -148 |
Table 2.1652.3 GPS week: 1652 Day: 3 MJD: 55811.000
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 252| 0 0 2 39 8 5 -.22 7 7 | -172 -241 16 70
| 24 -24 |
emr 95| 0 4 0 -9 -71 3 .42 19 19 | 1587 927 15 95
| -23 14 |
esa 142| 0 0 0 -101 -11 0 .28 6 6 | 1025 -589 17 156
| 41 27 |
gfz 197| 0 1 -4 30 97 2 -.23 11 12 | -74 257 22 105
| -32 33 |
grg 129| 1 0 7 4 6 5 .57 15 14 | 94 -127 49 251
| -5 -26 |
igr n/a| 0 -1 0 23 -27 -33 -.07 4 4 | 2107 1432 18 71
| -5 20 |
jpl 133| 0 0 -5 42 13 58 .56 14 15 | 753 1221 16 115
| -15 -6 |
mit 276| 1 -1 0 22 -30 -27 -.43 9 9 | 399 -501 18 185
| 1 -15 |
ngs 221| 0 -1 0 88 -90 -2 -.28 9 8 | -128 -336 2162 3340
| -42 37 |
sio 250| 1 1 -3 -164 210 -35 -.15 21 21 | --- --- --- ---
| 58 -125 |
Table 2.1652.4 GPS week: 1652 Day: 4 MJD: 55812.000
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 252| 0 0 3 31 0 12 -.20 7 7 | 1070 -813 18 120
| 31 16 |
emr 95| -2 3 -2 -30 -78 5 .52 19 19 | 3317 -1344 15 93
| 0 12 |
esa 142| 0 1 0 -105 0 -20 .24 8 8 | 219 -1074 22 171
| 41 17 |
gfz 197| 1 1 -5 39 35 -12 -.20 12 11 | 306 -285 22 95
| -21 89 |
grg 129| 0 0 5 -25 -19 22 .52 16 15 | 568 -632 61 235
| 34 -6 |
igr n/a| 0 0 0 22 -52 -10 -.04 5 5 | 4342 -1147 18 76
| -29 24 |
jpl 133| -2 -1 -4 31 5 118 .58 16 15 | 3416 -1408 18 92
| 3 4 |
mit 276| 0 -2 0 39 -3 -30 -.39 10 9 | 2608 -3031 23 171
| -12 -16 |
ngs 221| 0 0 -1 56 -64 -14 -.16 9 7 | 1254 -1060 2067 3364
| -21 55 |
sio 250| 1 0 -2 -147 265 -35 -.12 22 21 | --- --- --- ---
| 53 -154 |
Table 2.1652.5 GPS week: 1652 Day: 5 MJD: 55813.000
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 252| 0 0 2 54 12 -18 -.28 7 7 | -1286 497 21 94
| -8 -35 |
emr 95| -1 1 -2 -7 -50 0 .45 19 19 | 2409 -483 13 96
| -43 0 |
esa 142| 0 0 0 -90 21 -9 .24 7 6 | -2709 987 20 172
| 54 13 |
gfz 197| 1 2 -2 46 -34 5 -.21 11 11 | 248 128 22 99
| -34 41 |
grg 129| 1 0 10 -1 0 7 .51 14 14 | 13 475 54 226
| 39 -53 |
igr n/a| 0 0 1 14 -13 -17 -.08 4 4 | 3512 -280 20 75
| -21 9 |
jpl 133| -1 -1 -5 34 14 82 .58 14 14 | 2432 -502 18 86
| 20 -9 |
mit 276| 0 -2 -1 -4 -39 -17 -.43 11 10 | -2358 3278 21 161
| -10 -6 |
ngs 221| -2 -1 0 84 -35 5 -.25 9 7 | -1301 517 1741 3605
| -48 -48 |
sio 250| 2 1 -5 -183 211 -23 -.12 21 21 | --- --- --- ---
| 63 -127 |
Table 2.1652.6 GPS week: 1652 Day: 6 MJD: 55814.000
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 252| 0 0 3 34 30 20 -.23 8 8 | -1045 586 25 84
| 27 -22 |
emr 95| 0 0 -2 -29 -42 25 .46 19 19 | 979 -628 16 96
| -48 -1 |
esa 142| 0 -1 0 -80 34 -44 .19 7 7 | -4413 3534 23 204
| 58 1 |
gfz 197| 0 1 -4 40 -124 -4 -.19 9 9 | 271 -427 22 97
| -43 31 |
grg 129| 2 0 14 -9 -6 44 .55 18 17 | -70 508 76 221
| 8 -99 |
igr n/a| 0 0 0 1 17 -34 -.09 4 4 | 2295 -551 20 83
| -24 -16 |
jpl 133| -2 0 -5 26 1 62 .60 14 14 | 769 -864 18 86
| -56 6 |
mit 276| 1 -1 0 14 -46 -22 -.42 13 12 | -857 1073 24 181
| -21 -11 |
ngs 221| 0 0 -1 65 24 17 -.24 9 7 | -1189 808 1639 3144
| -48 -34 |
sio 250| 3 2 -4 -184 195 -37 -.09 21 20 | --- --- --- ---
| 69 -120 |
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 3.1652.0 GPS week: 1652 Day: 0 MJD: 55808.000
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 | 5 26 6 11 16 4 13 11 7 14 3 | 19 34 19 19 25 19 26 23 19 25 20
3 | 5 14 6 13 13 4 11 8 7 17 3 | 11 17 14 16 16 12 19 13 14 15 12
4 | 9 13 6 8 10 5 12 20 11 20 4 | 14 23 16 15 12 14 19 23 14 22 14
5 | 5 18 6 8 8 4 14 15 8 20 3 | 18 25 26 21 28 22 28 27 21 22 21
6 | 6 17 5 11 12 4 10 9 6 16 3 | 10 20 16 17 18 13 20 14 14 16 13
7 | 3 21 7 8 21 5 20 11 10 24 4 | 36 42 37 33 46 38 39 35 38 41 36
8 | 9 13 7 11 10 4 11 8 9 14 3 | 17 21 16 13 21 15 21 15 16 18 14
9E | 21 22 9 14 23 11 19 11 11 32 6 | 88 88 94 87 91 94 91 85 93 101 89
10 | 6 11 5 9 9 4 8 11 8 13 3 | 22 26 23 25 28 24 28 30 28 23 24
11E | 5 16 4 7 12 3 13 10 11 13 3 | 26 36 30 26 32 29 31 27 28 31 28
12 | 7 22 8 16 15 6 14 11 9 38 4 | 15 29 23 26 27 22 29 22 20 33 21
13 | 5 24 5 9 21 4 16 10 8 21 4 | 15 31 18 16 35 17 30 16 18 17 17
14 | 6 24 8 12 18 5 17 15 9 26 4 | 17 30 21 23 25 18 26 21 16 20 17
15 | 7 30 8 13 18 5 15 10 12 21 4 | 18 29 22 23 28 19 25 21 21 19 18
16 | 8 22 8 21 15 7 16 7 10 54 5 | 15 27 20 27 22 18 27 18 16 47 16
17 | 7 27 8 8 17 5 14 16 8 16 4 | 18 37 22 15 26 18 29 23 23 23 20
18 | 6 18 4 13 9 4 14 14 7 28 4 | 16 29 22 19 25 18 26 21 19 21 18
19 | 6 22 4 10 16 3 15 9 8 19 3 | 23 37 22 21 29 22 29 20 18 30 22
20 | 8 18 5 11 12 3 17 8 6 23 3 | 21 30 28 25 30 23 29 23 22 36 24
21 | 5 23 6 10 18 4 14 10 10 22 4 | 15 31 22 16 29 16 26 19 20 23 19
22 | 6 17 6 10 13 3 14 13 7 23 3 | 20 27 24 24 31 22 26 26 19 25 21
23 | 5 28 5 10 18 5 18 11 10 23 4 | 17 36 22 18 29 18 32 18 20 17 19
24 | 7 17 6 9 14 5 13 11 11 21 3 | 14 23 21 15 18 16 24 17 18 27 16
25 | 8 13 8 18 14 3 14 9 9 23 4 | 21 31 28 30 34 24 38 28 25 20 25
26 | 5 15 7 8 11 3 8 9 11 14 3 | 14 21 17 16 20 15 20 17 14 16 14
X27E | 18 33 14 16 23 10 --- 18 --- --- 8 | 34 37 31 33 20 29 --- 35 --- --- 31
28 | 6 21 6 10 16 5 15 11 10 37 4 | 15 31 23 24 27 18 29 23 18 36 18
29 | 6 22 6 15 16 4 15 10 13 20 4 | 21 31 19 17 27 19 26 17 17 25 18
X30 | 7 12 8 13 16 4 --- 13 7 18 4 | 12 19 23 19 22 17 --- 22 6 19 17
31 | 8 23 6 12 20 5 17 16 9 19 4 | 19 33 21 24 31 20 27 20 20 21 19
32 | 8 18 4 10 14 3 16 8 9 17 3 | 22 26 25 24 30 24 27 28 25 30 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 20 6 12 15 5 15 11 9 24 |T 20 30 24 23 28 22 29 24 22 27 22
WRMS | 7 20 6 11 14 4 14 11 8 22 |NE 16 27 21 20 25 18 26 20 18 24 18
MEDI | 6 21 6 11 15 4 14 11 9 20 |MD 18 30 22 21 27 19 27 22 19 23 19
Table 3.1652.1 GPS week: 1652 Day: 1 MJD: 55809.000
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 27 7 13 14 4 15 13 8 14 4 | 17 32 18 17 15 15 21 17 19 18 15
3 | 5 17 5 10 10 4 9 8 7 16 3 | 12 19 14 13 14 12 17 13 15 11 12
4 | 10 16 8 12 11 5 14 15 13 22 4 | 14 18 11 16 7 11 14 18 15 16 10
5 | 6 16 6 12 8 3 15 14 7 21 3 | 15 26 22 18 22 19 28 18 21 19 19
6 | 6 18 4 10 10 4 10 7 6 16 3 | 11 19 12 13 16 11 17 13 14 11 11
7E | 8 19 9 12 15 9 17 10 12 16 4 | 59 62 62 64 61 57 68 63 64 61 61
8 | 11 14 6 12 8 5 14 6 8 15 3 | 16 23 15 15 19 13 21 12 15 16 13
9E | 17 22 7 12 20 11 20 9 12 24 5 | 77 69 69 70 72 72 67 70 72 74 70
10 | 9 12 6 10 13 2 10 11 7 13 3 | 18 21 21 20 20 19 19 21 22 19 19
11E | 6 20 6 10 15 3 14 9 6 12 3 | 29 37 31 33 37 27 32 31 29 28 29
12 | 7 20 6 16 12 5 16 12 12 33 4 | 13 27 17 18 23 16 26 21 18 29 15
13 | 5 24 8 10 18 4 16 8 9 21 4 | 15 32 19 17 32 15 28 14 12 16 15
14 | 6 22 7 15 13 5 20 12 6 17 4 | 16 26 20 21 23 17 24 17 15 16 15
15 | 7 28 10 12 13 4 13 10 8 23 4 | 17 28 24 19 24 17 24 19 19 18 18
16 | 8 24 7 16 13 4 15 8 9 51 5 | 12 30 17 18 20 12 25 15 13 42 13
17 | 7 22 8 10 15 4 15 12 7 14 4 | 18 30 17 11 21 16 24 21 17 20 17
18 | 7 20 7 13 9 3 16 10 8 24 4 | 12 26 20 15 20 15 26 14 17 16 15
19 | 7 24 5 14 14 3 13 10 6 20 4 | 17 30 15 16 24 15 21 15 17 21 15
20 | 8 19 6 10 9 5 18 10 6 22 3 | 15 28 23 19 24 17 26 16 15 33 18
21 | 6 25 6 13 16 4 14 7 9 16 4 | 12 27 17 12 27 11 24 13 17 18 14
22 | 6 16 6 9 8 5 14 10 7 22 3 | 13 24 19 16 19 16 23 15 16 20 14
23 | 5 27 8 12 12 3 21 10 7 21 4 | 16 33 19 19 25 17 30 15 14 15 17
24 | 7 19 7 11 12 4 15 12 6 20 3 | 13 21 16 17 17 11 20 14 14 21 12
25 | 9 15 8 34 12 4 16 8 10 18 5 | 16 28 23 28 30 19 33 18 19 18 19
26 | 8 16 8 9 9 3 9 10 7 18 3 | 17 24 21 17 19 17 24 17 16 20 18
X27E | 17 20 12 15 23 11 17 12 --- --- 6 | 27 32 25 31 27 26 16 30 --- --- 27
28 | 12 19 9 15 13 5 15 11 9 36 5 | 14 30 21 23 23 15 27 17 16 33 15
29 | 9 20 10 14 14 5 17 10 11 18 4 | 15 24 16 15 23 14 23 13 16 19 13
X30 | 8 14 9 11 9 3 --- 6 5 16 3 | 12 20 18 17 19 14 --- 16 7 14 14
31E | 10 22 9 12 16 7 18 16 9 21 4 | 27 33 34 30 36 28 34 31 30 38 29
32 | 6 17 4 11 10 4 16 13 6 16 3 | 22 26 22 22 22 21 26 23 22 24 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 7 13 13 5 15 11 8 22 |T 19 29 22 21 25 19 26 20 20 24 19
WRMS | 8 20 7 14 12 5 15 10 6 21 |NE 14 25 18 17 21 15 23 16 16 20 15
MEDI | 7 20 7 12 13 4 15 10 7 18 |MD 16 27 19 18 23 16 24 17 16 19 15
Table 3.1652.2 GPS week: 1652 Day: 2 MJD: 55810.000
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 --- --- --- --- 4679 --- --- --- --- 0 | 25 --- --- --- --- 9999 --- --- --- --- 23
2 | 8 27 8 19 16 2 13 11 9 15 4 | 17 30 18 16 15 16 22 21 21 20 16
3 | 6 13 5 12 10 4 11 7 7 15 3 | 12 16 13 15 13 11 20 14 16 14 11
4 | 10 16 6 8 10 4 13 12 9 19 3 | 15 21 16 18 12 16 18 25 22 19 15
5 | 7 19 10 11 11 3 16 13 8 20 4 | 14 24 19 17 22 15 25 22 17 15 16
6 | 5 15 5 11 10 4 12 8 8 15 3 | 12 18 14 15 14 12 22 15 17 12 12
7E | 6 17 8 12 16 4 18 8 7 16 4 | 29 36 32 27 42 30 37 30 36 32 31
8 | 9 15 7 10 9 3 11 8 8 14 3 | 15 23 19 15 20 13 22 16 16 18 14
9E | 13 19 9 14 18 8 23 12 14 24 5 | 54 52 53 53 54 55 57 50 57 65 53
10 | 7 14 7 8 15 3 9 9 10 13 3 | 17 19 17 18 23 17 22 26 23 21 18
11E | 8 17 4 9 14 4 14 8 7 10 3 | 30 31 27 32 32 28 31 30 30 27 27
12 | 7 22 10 16 10 5 16 13 11 31 4 | 15 26 18 22 24 19 27 21 24 27 17
13 | 6 23 7 9 18 5 16 9 7 20 4 | 18 31 20 17 34 18 29 20 21 20 18
14 | 7 24 6 14 15 3 18 8 7 17 4 | 16 24 18 18 24 14 24 17 15 15 14
15 | 6 27 9 14 13 7 19 12 9 20 4 | 15 26 20 21 27 17 26 21 19 18 16
16 | 8 23 9 18 12 6 16 8 7 46 5 | 14 28 18 21 21 16 26 15 17 36 14
17 | 8 23 9 11 16 4 17 10 6 13 4 | 16 31 19 15 22 16 29 24 21 22 18
18 | 5 20 9 13 8 5 17 7 6 25 3 | 15 28 19 16 25 15 27 16 14 18 16
19 | 7 22 6 10 12 3 14 9 5 20 3 | 18 32 15 14 24 14 26 18 18 24 15
20 | 7 20 5 11 11 4 18 8 8 23 4 | 18 29 27 22 26 21 28 21 21 31 21
21 | 8 24 9 13 18 5 18 10 6 16 4 | 14 29 21 20 27 15 28 17 21 20 16
22 | 4 19 5 12 9 4 16 7 10 22 3 | 16 24 15 18 23 16 24 19 17 20 16
23 | 5 27 7 10 14 5 20 7 8 21 4 | 18 34 21 18 28 18 30 20 18 21 18
24 | 9 17 5 9 13 3 14 9 10 21 3 | 13 20 14 17 14 12 18 18 18 19 12
25 | 8 14 7 13 11 4 16 7 8 15 3 | 19 29 25 26 32 23 36 26 25 21 22
26 | 6 16 6 9 10 4 11 11 11 16 3 | 15 20 15 13 19 16 22 20 20 18 15
X27E | 11 24 18 14 81 9 22 19 --- --- 7 | 17 30 27 18 62 21 17 23 --- --- 19
28 | 9 21 8 16 11 5 14 10 9 37 4 | 14 29 25 26 24 19 28 24 24 34 19
29 | 8 24 10 13 11 4 15 10 7 17 4 | 20 27 19 16 24 16 26 18 22 20 18
X30 | 7 14 6 12 12 2 --- 6 6 12 3 | 14 20 14 18 17 13 --- 16 9 22 14
31E | 6 19 7 14 24 4 20 8 8 10 4 | 19 29 26 27 35 21 30 24 25 27 24
32 | 7 17 5 9 12 3 17 9 6 16 3 | 14 17 17 17 18 13 18 19 18 16 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 20 7 12 14 4 16 9 8 21 |T 18 26 20 20 25 18 26 21 21 23 18
WRMS | 7 20 7 11 13 4 16 9 7 22 |NE 15 25 18 18 22 15 24 19 19 20 16
MEDI | 7 19 7 12 12 4 16 9 8 17 |MD 16 28 19 18 24 16 26 20 20 20 16
Table 3.1652.3 GPS week: 1652 Day: 3 MJD: 55811.000
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 | 20 --- 22 --- --- 11 --- 16 --- --- 14 | 45 --- 9999 --- --- 9999 --- 9999 --- --- 49
2 | 7 21 6 13 17 3 14 8 10 14 4 | 18 28 17 18 18 19 26 20 24 25 18
3 | 5 10 6 10 14 3 11 7 10 17 3 | 12 12 10 13 15 9 15 13 18 11 9
4 | 8 15 6 6 9 5 12 9 9 21 3 | 16 19 13 13 13 15 19 19 19 16 13
5 | 7 16 7 11 14 5 17 11 9 19 4 | 16 25 20 22 26 18 27 22 20 18 18
6 | 4 11 5 7 15 4 10 7 11 16 3 | 11 14 9 13 17 9 15 13 18 11 9
7E | 7 23 6 11 14 3 16 8 7 18 3 | 26 39 31 23 35 26 30 29 29 32 27
8 | 8 13 5 10 12 4 11 8 9 16 3 | 17 22 16 14 19 13 20 16 14 19 13
9E | 10 20 6 11 17 5 20 15 12 28 4 | 66 63 61 61 68 60 65 61 62 71 62
10 | 7 12 4 6 12 6 11 9 10 14 3 | 24 26 20 23 29 22 28 31 23 24 23
11E | 5 17 5 8 13 2 13 9 9 11 3 | 28 37 32 32 33 30 31 32 29 32 29
12 | 6 19 6 12 15 4 14 14 9 31 4 | 16 29 19 20 23 17 27 22 22 28 17
13 | 6 21 5 8 19 3 16 9 10 20 4 | 15 30 18 16 33 15 27 17 16 17 15
14 | 6 24 7 11 15 3 14 7 9 18 3 | 14 25 17 18 22 13 20 14 13 13 13
15 | 8 26 7 14 17 5 19 15 13 21 5 | 16 27 18 20 25 14 26 20 15 18 15
16 | 6 22 6 15 17 5 16 9 11 39 5 | 13 28 17 19 20 13 23 15 16 27 13
17 | 6 19 5 8 16 3 13 8 9 15 3 | 18 28 18 15 24 16 25 22 23 23 17
18 | 7 18 6 12 14 5 15 7 10 24 4 | 11 26 18 16 22 14 25 14 16 14 14
19 | 5 21 6 8 18 3 12 10 8 19 3 | 21 32 18 16 25 18 23 19 17 25 17
20 | 7 17 4 9 13 3 16 9 8 29 3 | 18 28 26 24 29 21 28 21 25 35 22
21 | 6 24 8 10 17 4 11 9 10 17 4 | 12 27 18 12 24 14 23 15 17 16 13
22 | 5 17 4 10 13 4 13 7 8 22 3 | 16 23 19 22 25 17 22 20 19 20 17
23 | 6 25 6 10 13 3 17 9 8 21 4 | 16 31 19 17 25 16 26 17 15 15 15
24 | 7 20 8 6 12 3 13 10 7 23 3 | 11 24 14 13 15 12 20 17 14 20 11
25 | 8 12 7 27 13 5 14 8 8 15 4 | 22 29 23 33 31 22 33 24 20 20 22
26 | 7 15 6 8 14 4 12 10 8 16 3 | 16 19 15 15 21 13 21 20 12 19 14
X27E | 16 30 18 19 --- 15 --- 14 --- --- 9 | 26 33 33 25 --- 26 --- 24 --- --- 28
28 | 10 20 8 11 11 5 13 10 5 39 4 | 18 31 26 27 27 20 31 25 23 36 22
29 | 8 21 8 15 13 3 15 8 6 16 4 | 19 27 21 16 25 18 24 18 20 22 17
X30 | 9 15 4 9 13 4 --- 6 --- --- 4 | 16 21 16 21 22 16 --- 22 --- --- 17
31E | 6 24 6 11 19 5 16 7 6 10 3 | 21 33 26 22 33 22 28 24 24 22 23
32 | 8 15 3 9 15 3 15 10 7 19 3 | 23 26 23 27 28 23 24 27 24 24 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 6 11 15 4 14 9 9 21 |T 19 27 21 20 25 18 25 21 20 23 19
WRMS | 7 19 6 12 14 4 15 9 8 21 |NE 17 25 18 18 23 16 23 19 18 20 17
MEDI | 7 19 6 10 14 4 14 9 9 19 |MD 16 27 18 19 25 17 25 20 19 20 17
Table 3.1652.4 GPS week: 1652 Day: 4 MJD: 55812.000
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 | 20 --- 21 --- --- 16 --- 14 --- 49 13 | 34 --- 9999 --- --- 9999 --- 9999 --- 31 28
2 | 5 21 10 12 18 4 16 8 12 15 4 | 12 24 10 13 17 12 18 14 18 15 11
3 | 5 12 8 12 13 5 12 9 6 19 3 | 11 16 12 15 15 12 17 16 10 11 9
4 | 8 17 8 7 11 3 14 11 14 22 4 | 15 24 15 15 16 17 19 20 23 14 15
5 | 7 18 8 11 12 6 19 9 11 21 4 | 18 26 23 24 25 21 27 23 23 19 20
6 | 5 15 7 11 12 5 12 9 7 16 3 | 12 19 12 15 16 12 18 15 11 9 10
7E | 6 21 8 12 16 6 21 6 8 17 4 | 17 29 20 18 29 18 27 19 20 21 18
8 | 10 18 6 14 11 6 12 8 8 16 3 | 19 29 16 19 20 18 27 20 15 23 18
9E | 11 18 9 12 17 6 19 20 17 24 5 | 30 38 37 32 39 31 41 37 31 42 32
10 | 5 15 5 9 13 6 12 9 11 16 3 | 22 29 23 23 26 24 25 27 24 22 23
11E | 7 15 7 9 12 6 13 7 8 16 3 | 20 29 18 23 24 22 25 21 20 20 19
12 | 7 21 9 12 15 4 16 17 9 31 5 | 16 32 23 20 26 20 28 26 17 26 19
13 | 6 21 5 10 20 5 14 6 8 19 4 | 15 31 18 17 34 18 28 15 17 17 16
14 | 6 19 10 11 18 6 15 7 10 20 4 | 18 25 19 20 25 16 23 18 18 15 16
15 | 8 27 10 11 17 6 21 18 8 21 5 | 17 28 19 22 25 19 28 25 19 19 18
16 | 9 23 9 14 16 5 18 7 9 33 5 | 13 29 20 21 22 18 26 16 16 21 15
17 | 6 19 8 8 16 3 15 8 10 16 3 | 17 28 15 13 21 18 26 20 22 23 17
18 | 6 19 7 10 12 6 15 8 7 23 3 | 16 28 17 17 23 18 26 18 17 17 16
19 | 6 22 8 11 20 5 14 9 7 19 4 | 20 32 21 17 26 19 25 17 20 24 18
20 | 7 19 5 12 15 5 16 7 6 29 4 | 15 28 23 22 28 19 27 18 17 32 19
X21 | 6 26 8 13 19 6 15 9 7 --- 4 | 10 24 14 12 25 9 21 10 11 --- 9
22 | 7 18 8 9 14 5 16 12 6 23 4 | 19 25 21 20 26 18 23 22 19 21 18
23 | 7 24 6 14 17 4 16 5 10 20 4 | 15 32 17 19 25 17 27 15 17 16 15
24 | 8 18 10 16 15 5 12 10 8 25 4 | 11 23 15 19 17 13 19 16 14 19 11
25 | 7 12 7 8 14 6 15 7 8 15 3 | 18 27 26 20 32 20 34 23 21 18 21
26 | 5 15 8 9 13 8 12 12 8 15 3 | 16 21 18 15 21 17 23 22 18 18 17
X27E | 17 25 17 19 --- 10 --- 17 --- 25 8 | 26 24 24 25 --- 27 --- 24 --- 16 24
28 | 9 20 8 20 13 5 17 8 10 39 5 | 17 32 23 33 28 21 30 26 25 36 22
29 | 9 20 10 14 15 6 14 9 7 17 4 | 22 30 18 18 26 19 26 22 22 26 20
X30 | 11 16 16 15 10 6 --- 8 --- --- 5 | 15 21 28 24 19 18 --- 21 --- --- 18
31E | 7 23 6 8 23 5 19 15 9 16 4 | 13 24 14 16 23 13 22 19 15 19 13
32 | 9 15 7 11 16 5 13 10 4 20 3 | 20 25 20 21 26 23 25 25 23 19 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 8 12 16 5 16 10 9 22 |T 17 26 19 19 24 18 25 20 18 20 17
WRMS | 7 19 8 11 15 5 15 9 7 21 |NE 16 26 18 19 23 17 24 19 18 20 17
MEDI | 7 19 8 11 15 5 15 9 8 20 |MD 17 28 19 19 25 18 26 20 18 19 18
Table 3.1652.5 GPS week: 1652 Day: 5 MJD: 55813.000
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 | 26 --- 24 --- --- 19 --- 17 --- 36 14 | 39 --- 9999 --- --- 9999 --- 9999 --- 25 42
2 | 9 24 9 12 17 4 12 10 11 23 4 | 17 29 19 21 16 19 21 25 22 29 18
3 | 4 11 6 11 14 6 11 13 9 15 3 | 12 16 12 14 16 11 18 17 14 13 11
4 | 10 17 7 11 9 4 15 11 12 21 4 | 15 20 16 21 12 15 19 23 22 18 14
5 | 8 16 9 10 12 3 17 8 6 21 3 | 18 27 26 27 26 22 29 26 24 23 22
6 | 5 12 5 8 13 4 11 11 7 13 3 | 12 16 13 17 17 11 17 16 14 12 11
7E | 7 19 5 12 14 3 15 10 8 18 3 | 16 28 23 19 25 18 27 21 23 27 19
8 | 9 16 6 13 11 3 14 7 6 12 3 | 19 26 21 20 22 19 23 20 20 23 18
9E | 11 14 6 9 12 5 20 21 12 24 5 | 56 53 53 51 57 54 54 53 59 62 54
10 | 7 10 4 10 13 4 8 9 9 16 3 | 21 22 21 26 25 22 22 27 25 24 22
11E | 5 17 6 7 15 4 14 9 8 13 3 | 20 28 24 22 24 19 25 23 25 22 21
12 | 9 21 9 10 15 7 16 13 8 33 4 | 19 29 28 22 26 21 30 29 23 29 23
13 | 7 21 6 10 19 3 13 6 11 21 4 | 15 31 19 19 32 15 28 15 20 17 16
14 | 6 22 5 10 17 4 13 8 12 17 4 | 15 26 17 20 23 16 22 18 18 18 15
15 | 7 22 6 15 15 3 19 16 16 21 5 | 16 26 21 24 25 17 26 23 20 19 18
16 | 8 21 8 15 17 5 17 8 13 30 4 | 12 28 21 21 21 16 26 16 19 18 15
17 | 4 20 7 11 15 3 17 8 9 17 3 | 16 25 14 18 24 17 27 19 17 22 15
18 | 6 17 7 12 11 4 13 12 8 21 3 | 13 25 16 17 21 13 25 18 15 16 14
19 | 6 21 7 12 18 3 14 9 6 19 4 | 17 29 19 16 26 18 24 17 19 24 17
20 | 10 19 7 13 13 3 14 8 9 29 4 | 17 29 25 25 28 20 27 18 24 33 21
21 | 5 20 5 12 20 5 14 8 9 13 3 | 14 24 19 17 26 15 21 18 19 20 16
22 | 6 16 5 11 12 5 13 15 7 21 3 | 15 23 17 21 24 14 23 23 18 20 16
23 | 7 24 7 11 15 3 15 7 8 21 4 | 15 32 22 20 25 16 26 16 20 17 17
24 | 7 17 6 8 14 4 12 13 9 25 4 | 14 22 16 16 19 12 17 17 19 21 13
25 | 8 12 6 14 13 3 13 10 8 15 3 | 19 25 22 20 27 18 32 23 19 19 20
26 | 6 14 5 10 11 6 11 11 10 13 3 | 14 19 18 20 19 16 21 23 17 17 15
X27E | 11 --- --- 17 --- 19 --- --- --- --- 13 | 34 --- --- 38 --- 43 --- --- --- --- 37
28 | 8 16 6 15 14 7 14 10 8 39 4 | 13 28 20 23 24 15 26 18 20 33 16
29 | 7 22 8 14 17 4 14 9 10 18 4 | 25 33 25 29 27 24 30 24 29 30 23
X30 | 12 23 14 16 15 7 --- 23 --- 21 7 | 25 29 33 31 24 25 --- 35 --- 21 27
31E | 8 30 7 10 15 4 17 12 11 11 4 | 17 33 20 19 29 18 25 26 21 22 19
32 | 10 17 6 10 13 3 11 9 8 20 3 | 18 20 19 21 21 17 17 19 18 21 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 11 14 4 14 11 9 21 |T 19 26 21 22 24 19 25 22 21 23 20
WRMS | 7 19 6 11 14 4 14 10 7 21 |NE 17 25 19 21 22 17 23 20 19 21 18
MEDI | 7 17 6 11 14 4 14 10 9 21 |MD 16 26 20 21 24 17 25 20 20 21 17
Table 3.1652.6 GPS week: 1652 Day: 6 MJD: 55814.000
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 | 20 --- 18 --- --- 12 --- 18 --- 47 13 | 31 --- 9999 --- --- 9999 --- 9999 --- 21 30
2 | 6 22 7 13 21 3 14 9 9 21 4 | 21 28 24 19 15 20 22 24 21 31 19
3 | 7 14 5 11 13 5 11 18 11 15 4 | 14 14 18 14 14 17 17 19 18 22 15
4 | 10 18 8 8 16 4 12 14 12 20 4 | 13 23 11 14 13 11 19 20 16 20 11
5 | 7 17 7 8 19 5 15 10 12 22 4 | 25 32 32 32 38 28 35 32 29 24 28
6 | 6 13 5 9 13 5 9 18 10 11 3 | 13 15 19 16 16 15 19 20 17 16 15
7E | 8 22 8 10 18 4 19 10 7 13 4 | 18 28 22 21 26 17 24 17 16 21 17
8 | 10 18 5 12 12 4 13 10 9 14 3 | 21 30 25 23 24 19 27 20 16 24 20
9E | 13 16 6 8 22 6 15 17 10 24 4 | 75 74 73 70 71 72 72 71 77 77 73
10 | 6 11 10 7 19 4 8 10 10 15 3 | 24 28 26 31 37 25 29 32 26 26 26
11E | 7 17 8 6 15 4 11 11 8 13 3 | 18 25 22 17 21 16 21 20 22 20 18
12 | 9 20 9 12 19 5 14 13 12 38 5 | 20 34 26 32 25 25 32 28 26 37 24
13 | 6 22 5 9 21 3 14 11 9 21 4 | 17 33 22 20 35 17 31 17 17 18 18
14 | 6 20 8 10 21 3 16 8 13 16 4 | 20 29 24 26 31 21 30 20 25 19 21
15 | 8 25 10 10 17 4 19 23 11 22 5 | 21 31 24 26 29 22 32 28 20 21 21
16 | 8 22 6 12 15 6 16 9 11 30 4 | 15 30 21 22 21 18 27 18 18 16 17
17 | 6 18 9 6 19 3 16 10 6 16 3 | 22 32 22 17 28 21 32 22 21 26 22
18 | 6 21 7 8 17 4 15 11 9 19 4 | 19 30 23 23 33 19 30 25 22 19 21
19 | 7 20 10 8 18 6 12 11 9 19 4 | 27 36 25 22 31 26 32 20 28 31 25
20 | 9 22 7 10 16 3 17 14 7 27 4 | 19 31 27 25 34 24 30 24 23 36 24
21 | 5 19 8 10 20 3 14 7 5 16 3 | 17 24 22 18 28 14 23 14 17 16 16
22 | 5 19 6 6 19 4 15 15 8 23 4 | 23 29 27 28 39 24 30 30 24 25 24
23 | 7 25 7 11 18 3 16 10 9 22 4 | 19 35 25 21 29 20 32 18 20 20 20
24 | 9 18 7 7 14 5 11 14 13 22 4 | 14 21 16 14 12 11 18 18 18 23 13
25 | 6 12 7 8 18 5 13 8 7 20 3 | 25 29 29 30 36 25 39 29 24 21 27
26 | 7 13 5 8 15 5 10 13 7 12 3 | 17 19 19 17 25 18 22 24 17 18 17
X27E | 11 20 11 11 --- 15 --- 13 --- 21 6 | 40 49 57 41 --- 42 --- 50 --- 13 44
28 | 11 18 8 13 15 4 14 11 7 39 5 | 18 30 27 32 30 21 31 27 21 37 22
29 | 8 23 8 10 16 4 15 13 10 19 4 | 34 42 34 29 37 31 39 27 34 35 32
X30 | 9 17 13 14 22 8 --- 14 --- 17 5 | 15 27 23 27 24 16 --- 21 --- 14 19
31E | 5 21 8 8 21 6 20 20 8 15 4 | 16 21 23 14 28 16 26 22 19 20 16
32 | 9 16 7 7 17 3 12 9 6 18 3 | 17 19 18 18 26 16 18 18 18 20 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 7 9 18 4 14 13 9 21 |T 22 29 26 24 28 22 28 25 23 24 22
WRMS | 8 19 7 9 17 4 14 12 7 20 |NE 20 28 23 22 27 20 27 22 21 23 20
MEDI | 7 19 7 9 18 4 14 11 9 19 |MD 19 29 24 22 28 20 30 22 21 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 4.1652 GPS week: 1652 MJD: 55808.0-55814.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 |U 27 16 41 |U 6 8 25 |U 13 15 22 |
emr | emr 2955 |U 25 18 44 |U 17 10 37 | 16 16 25 |
esa | esa 3017 | 27 17 41 |U 8 9 23 | 11 15 21 |
gfz | gfz 2963 |U 26 17 43 |U 7 9 33 |U 12 16 22 |
grg | grg 2920 | 26 16 41 |U 6 8 24 | 13 16 24 |
igr | igr 2998 | 26 18 38 | 6 8 27 | 12 15 21 |
igs | igs 2988 | 29 16 46 | 9 9 25 | 13 16 22 |
jpl | jpl 2805 |U 28 20 50 |U 19 15 74 | 14 15 25 |
mit | mit 3017 |U 26 18 38 |U 16 13 34 |U 18 17 27 |
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 5.1652.0 GPS week: 1652 Day: 0 MJD: 55808.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 11 10 32 | 7 7 43 | 7 7 16 |
emr | emr 2972 | 12 11 32 | 14 8 31 | 11 10 17 |
esa | esa 2976 | 11 10 31 | 23 14 28 | 7 8 17 |
gfz | gfz 2969 | 11 10 30 | 7 7 64 | 6 6 17 |
grg | grg 2976 | 11 10 32 | 7 7 25 | 8 9 21 |
igr | igr 2974 | 11 10 33 | 8 7 62 | 7 7 16 |
igs | igs 2951 | 37 11 74 | 21 13 25 | 8 7 16 |
jpl | jpl 2784 | 32 13 70 | 31 39 253 | 8 8 19 |
mit | mit 2976 | 10 10 31 | 30 18 38 | 7 8 22 |
Table 5.1652.1 GPS week: 1652 Day: 1 MJD: 55809.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 15 10 34 | 6 8 19 | 42 48 35 |
emr | emr 2970 | 16 14 38 | 17 7 32 | 41 49 42 |
esa | esa 2976 | 15 10 33 | 5 7 20 | 27 49 26 |
gfz | gfz 2968 | 14 9 30 | 5 7 19 | 39 57 36 |
grg | grg 2976 | 15 10 33 | 5 9 22 | 35 49 30 |
igr | igr 2973 | 15 10 30 | 5 9 19 | 38 49 25 |
igs | igs 2956 | 15 10 33 | 5 7 19 | 39 50 32 |
jpl | jpl 2870 | 13 9 30 | 20 11 51 | 40 46 38 |
mit | mit 2976 | 14 9 28 | 14 11 33 | 53 53 38 |
Table 5.1652.2 GPS week: 1652 Day: 2 MJD: 55810.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2990 | 61 29 89 | 5 7 20 | 10 15 22 |
emr | emr 2968 | 63 32 95 | 13 11 27 | 12 13 17 |
esa | esa 2976 | 63 31 88 | 5 7 17 | 9 13 18 |
gfz | gfz 2967 | 65 32 100 | 5 5 18 | 12 14 17 |
grg | grg 2970 | 65 33 92 | 5 8 22 | 10 14 21 |
igr | igr 2974 | 63 31 95 | 5 7 17 | 9 13 17 |
igs | igs 2938 | 61 29 91 | 5 8 19 | 12 20 24 |
jpl | jpl 2870 | 55 48 97 | 21 11 49 | 12 13 23 |
mit | mit 2976 | 63 31 88 | 14 14 32 | 11 11 20 |
Table 5.1652.3 GPS week: 1652 Day: 3 MJD: 55811.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 18 9 26 | 7 6 23 | 8 8 18 |
emr | emr 2968 | 16 9 29 | 18 11 43 | 10 9 21 |
esa | esa 3072 | 17 8 25 | 8 9 25 | 8 6 21 |
gfz | gfz 2968 | 17 9 28 | 6 8 23 | 7 7 19 |
grg | grg 2880 | 18 11 26 | 7 9 22 | 8 8 21 |
igr | igr 3065 | 17 9 27 | 7 8 24 | 8 6 19 |
igs | igs 3029 | 17 8 26 | 7 8 22 | 7 6 18 |
jpl | jpl 2776 | 19 10 31 | 19 11 50 | 9 8 18 |
mit | mit 3072 | 18 9 26 | 14 12 32 | 18 15 22 |
Table 5.1652.4 GPS week: 1652 Day: 4 MJD: 55812.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 61 38 58 | 7 8 23 | 6 9 21 |
emr | emr 2968 | 47 38 49 | 20 10 42 | 11 9 24 |
esa | esa 3072 | 62 39 59 | 6 9 23 | 8 9 20 |
gfz | gfz 2967 | 57 39 56 | 6 7 22 | 8 9 23 |
grg | grg 2880 | 49 33 49 | 7 8 26 | 8 9 23 |
igr | igr 3060 | 58 46 34 | 6 9 23 | 7 9 24 |
igs | igs 3037 | 55 38 55 | 6 8 23 | 7 7 20 |
jpl | jpl 2780 | 48 41 50 | 12 9 35 | 12 7 22 |
mit | mit 3072 | 57 47 35 | 13 12 34 | 18 13 39 |
Table 5.1652.5 GPS week: 1652 Day: 5 MJD: 55813.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 11 10 26 | 6 11 28 | 9 9 20 |
emr | emr 2876 | 13 12 30 | 19 13 43 | 13 16 36 |
esa | esa 2976 | 11 11 28 | 7 9 28 | 10 14 25 |
gfz | gfz 2937 | 11 10 28 | 6 8 27 | 9 14 23 |
grg | grg 2880 | 12 11 30 | 7 9 28 | 10 14 26 |
igr | igr 2902 | 12 10 28 | 6 9 28 | 9 12 25 |
igs | igs 2953 | 11 11 26 | 6 8 28 | 10 13 25 |
jpl | jpl 2779 | 16 13 40 | 11 13 36 | 11 15 31 |
mit | mit 2976 | 11 9 26 | 12 16 32 | 10 11 26 |
Table 5.1652.6 GPS week: 1652 Day: 6 MJD: 55814.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 9 7 22 | 6 8 20 | 8 12 21 |
emr | emr 2968 | 12 9 33 | 16 11 43 | 15 9 18 |
esa | esa 3072 | 11 8 23 | 5 9 23 | 6 9 23 |
gfz | gfz 2967 | 10 8 28 | 16 21 61 | 6 8 22 |
grg | grg 2880 | 11 8 24 | 6 7 24 | 11 12 24 |
igr | igr 3044 | 10 7 20 | 5 10 19 | 7 8 21 |
igs | igs 3054 | 10 7 22 | 14 10 41 | 7 8 19 |
jpl | jpl 2780 | 12 10 33 | 17 12 47 | 8 8 23 |
mit | mit 3072 | 10 10 29 | 12 11 33 | 8 9 24 |
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 6.1652 GPS week: 1652 MJD: 55808.500-55814.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 9 -16 28 19 6 | 16 21
| 17 16 79 52 8 | 1
emr uuuuu | -13 34 -8 62 -2 | 65 67
| 15 16 77 60 3 | 2
esa uuuuu | -10 -44 8 88 -1 | 20 27
| 14 15 39 39 7 | 2
gfz uuuuu | -46 42 -80 -22 -1 | 13 19
| 16 15 78 43 4 | 3
grg uuuux | 19 -29 6 0 9 | 5 24
| 44 20 70 95 30 | 2
igr xxxxx | -15 20 29 -13 -1 | 6 16
| 10 10 62 61 10 | 1
irf xxxxx | 0 8 -23 -44 -5 | 10 20
| 11 11 28 56 2 | 3
jpl uuuuu | 9 19 -23 65 8 | 42 45
| 24 20 109 79 8 | 2
mit uuuuu | 10 24 -65 -121 -8 | 24 31
| 15 18 70 93 4 | 4
ngs uuuuu | -6 15 74 -66 -1 | 12 21
| 41 34 61 74 7 | 3
sio uuuuu | 130 -43 114 7 17 | 38 41
| 26 24 82 124 10 | 3
Table 7.1652.0 GPS week: 1652 Day: 0 MJD: 55808.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -20 -17 -88 40 17 | 15 20
emr uuuuu | 0 26 35 111 -3 | 68 69
esa uuuuu | -6 -30 63 143 5 | 24 27
gfz uuuuu | -42 38 -141 18 2 | 17 20
grg uuuux | -58 -57 117 -126 24 | 2 24
igr xxxxx | -15 17 -34 44 12 | 8 16
irf xxxxx | -9 13 -51 -89 -3 | 15 20
jpl uuuuu | -9 32 -183 78 6 | 43 46
mit uuuuu | -4 33 -151 -179 -3 | 29 32
ngs uuuuu | 54 0 156 -73 -9 | 17 21
sio uuuuu | 98 -25 67 -152 15 | 38 41
Table 7.1652.1 GPS week: 1652 Day: 1 MJD: 55809.500
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 | 13 -10 104 -69 14 | 14 19
emr uuuuu | -24 49 59 169 4 | 66 67
esa uuuuu | 16 -25 -26 108 0 | 22 25
gfz uuuuu | -31 64 -222 -36 -1 | 15 18
grg uuuux | -2 -45 21 -6 9 | 4 25
igr xxxxx | -26 19 34 64 6 | 7 14
irf xxxxx | 6 22 11 -115 -3 | 13 17
jpl uuuuu | 17 19 -10 170 17 | 42 44
mit uuuuu | 8 50 45 -271 -6 | 27 30
ngs uuuuu | -44 -38 19 9 -6 | 14 19
sio uuuuu | 137 -10 283 -150 27 | 35 37
Table 7.1652.2 GPS week: 1652 Day: 2 MJD: 55810.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 9 -15 119 84 10 | 16 20
emr uuuuu | -41 47 29 23 -5 | 67 68
esa uuuuu | -17 -57 -5 113 -9 | 22 25
gfz uuuuu | -50 64 -84 -55 0 | 15 17
grg uuuux | 16 -27 10 76 66 | 4 25
igr xxxxx | -22 25 86 25 7 | 7 14
irf xxxxx | 6 20 2 26 -7 | 13 17
jpl uuuuu | 55 34 -131 150 13 | 42 44
mit uuuuu | 22 41 -31 -56 -11 | 27 30
ngs uuuuu | -37 -16 89 -199 0 | 13 19
sio uuuuu | 154 -21 134 117 29 | 36 39
Table 7.1652.3 GPS week: 1652 Day: 3 MJD: 55811.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 31 -25 83 23 2 | 14 21
emr uuuuu | -7 22 -68 12 -1 | 63 66
esa uuuuu | -20 -42 -14 70 8 | 17 27
gfz uuuuu | -26 31 -18 52 -7 | 11 20
grg uuuux | 33 4 34 -37 11 | 3 24
igr xxxxx | -13 4 47 -51 -1 | 5 18
irf xxxxx | 7 -1 -10 -2 -5 | 8 22
jpl uuuuu | 13 14 -10 -17 11 | 40 43
mit uuuuu | 22 -2 -44 -42 -12 | 22 31
ngs uuuuu | -30 41 56 -118 -2 | 9 22
sio uuuuu | 132 -59 129 89 24 | 34 37
Table 7.1652.4 GPS week: 1652 Day: 4 MJD: 55812.500
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 | -1 -25 38 36 -1 | 16 22
emr uuuuu | 3 6 53 67 -3 | 64 67
esa uuuuu | -2 -35 -30 26 -5 | 20 29
gfz uuuuu | -74 27 -15 -57 -5 | 11 21
grg uuuux | 21 -28 -31 -87 -20 | 8 24
igr xxxxx | -9 35 122 -45 -12 | 7 18
irf xxxxx | 15 6 -5 15 -6 | 9 22
jpl uuuuu | 11 3 134 78 -8 | 43 46
mit uuuuu | 31 18 -30 -5 -10 | 22 32
ngs uuuuu | -40 27 -22 -56 12 | 10 22
sio uuuuu | 169 -47 70 150 16 | 39 42
Table 7.1652.5 GPS week: 1652 Day: 5 MJD: 55813.500
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 14 -17 -29 -2 | 16 23
emr uuuuu | -12 49 -153 3 -4 | 63 66
esa uuuuu | -25 -48 62 97 4 | 18 27
gfz uuuuu | -53 40 -64 -61 1 | 10 20
grg uuuux | 41 -33 -115 30 -19 | 6 23
igr xxxxx | -21 27 -7 -112 -15 | 5 16
irf xxxxx | -12 6 -59 -73 -6 | 7 20
jpl uuuuu | -3 -14 70 39 10 | 42 45
mit uuuuu | -6 16 -120 -144 -8 | 20 29
ngs uuuuu | 36 54 120 -33 -3 | 11 23
sio uuuuu | 115 -57 47 31 6 | 41 45
Table 7.1652.6 GPS week: 1652 Day: 6 MJD: 55814.500
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 -37 -42 51 3 | 18 24
emr uuuuu | -13 38 -7 48 0 | 64 67
esa uuuuu | -15 -68 5 56 -9 | 20 28
gfz uuuuu | -45 33 -17 -13 4 | 12 21
grg uuuux | 85 -18 4 152 -6 | 6 23
igr xxxxx | 2 14 -47 -18 -7 | 5 16
irf xxxxx | -14 -10 -45 -71 -6 | 7 21
jpl uuuuu | -20 46 -29 -41 5 | 45 49
mit uuuuu | -3 11 -125 -150 -3 | 21 30
ngs uuuuu | 20 38 98 7 0 | 11 24
sio uuuuu | 106 -79 69 -34 6 | 44 48
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