[IGSREPORT-21063] Wk 1698 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Aug 10 08:40:18 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1698 (Jul 22, 2012 - Jul 28, 2012)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi 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:
igs1698[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1698[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1698[0-6].cls IGS GPS clock combination summary report.
igs16987.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16987.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 | ALIC KOUC ALIC KOUC
0 | EMR | 3 3 6 HERS HERS
0 | GFZ | 3 6 23 BRFT OHI2 PDEL RIO2
0 | JPL | 3 6
0 | MIT | 3 3 6 REUN
1 | COD | KOUC KOUC XMIS
1 | EMR | 3 3 6
1 | ESA | IRKJ NKLG
1 | GFZ | 3 6 23 BRFT METS WSRT
1 | GRG | IRKJ
1 | JPL | 3 6
1 | MIT | 3 19 3 6 19 RIOP NICO RIOP
2 | COD | 3 KOUC
2 | EMR | HERS HERS
2 | ESA | 3 6 6 IRKJ
2 | GFZ | 6 13 23 30 BRFT COCO NTUS PIE1
2 | GRG | IRKJ
2 | MIT | 6 6 NTUS NTUS
3 | COD | KOUC TLSE KOUC
3 | EMR | 6 3 6 TLSE TLSE
3 | ESA | IRKJ TLSE
3 | GFZ | 3 23 MDO1
3 | GRG | IRKJ
3 | JPL | 3 6
3 | MIT | 6 3 6 TLSE
4 | COD | KOUC SCH2 SOFI FLRS KOUC SOFI
4 | EMR | 3 6 3 6 THTI
4 | ESA | DAV1 IRKJ NNOR SCH2
4 | GFZ | 3 6 23 30 MDVJ
4 | GRG | IRKJ
4 | JPL | 3 6
4 | MIT | 6 3 6 GMAS SOFI
5 | COD | KOUC KOUC
5 | EMR | 3 6 3 6
5 | ESA | IRKJ
5 | GFZ | 3 6 23 ABPO
5 | GRG | IRKJ
5 | JPL | 3 6
5 | MIT | 3 6 3 6 GMAS
6 | COD | 17 KOUC FLRS KOUC
6 | EMR | 6 3 GMAS NNOR
6 | ESA | IRKJ
6 | GFZ | 3 6 23 BRAZ XMIS
6 | GRG | IRKJ
6 | JPL | 3 6
6 | MIT | 3 6 3 6 MAS1
5. 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.
6. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the current IGS reference frame. These rotations were
estimated in the IGS SINEX combination process, performed by the IGS Reference
Frame Coordinator at the Institut Geographique National (IGN). 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 | .8 .9 .5 -56 -15 5 -.34
EMR | .4 -4.9 11.8 -6 4 -11 .12
ESA | -.8 .2 20.4 -37 57 80 -.21
GFZ | -1.0 1.1 .4 -41 -4 -16 -.34
GRG | 2.5 -10.6 25.4 -59 55 -48 -.31
JPL | -.5 -1.3 7.1 -37 37 -14 -.13
MIT | 1.5 -2.0 22.4 -17 12 -42 -.23
NGS | -2.4 1.3 26.7 -81 43 -15 -.12
SIO | -1.3 -4.2 3.2 -93 7 43 -.18
7. 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.
8. 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.
9. 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 1.1698.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1698.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 2.1698.[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 3.1698.[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 5.1698.0-6).
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 1698 summary. (Jul 22, 2012 - Jul 28, 2012)
Table 1.1698.a GPS week: 1698 MJD: 56130.000-56136.000
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 261| 0 0 -3 18 50 0 -.26 8 8 | -425 -196 13 59
| 0 0 1 10 8 19 .03 | 265 720
emr 89| 1 -2 -5 -74 41 -17 .40 15 15 | 346 101 31 132
| 1 1 1 14 16 21 .03 | 709 842
esa 175| 0 0 1 -44 -28 16 .28 7 7 | -553 -292 13 124
| 0 0 0 27 13 9 .02 | 679 920
gfz 196| 0 0 1 13 14 -11 -.25 11 11 | 282 -70 33 150
| 0 0 1 51 67 12 .03 | 693 549
grg 124| 2 0 9 33 -56 -6 .55 16 14 | 138 356 58 207
| 0 0 2 13 12 20 .02 | 365 1025
igr n/a| 0 0 -1 -74 22 -22 -.07 4 4 | 15528 -312 19 67
| 0 0 0 14 12 11 .02 | 1357 888
jpl 142| 1 0 -5 -16 -34 -4 .49 13 13 | 1831 161 19 100
| 0 0 0 10 16 19 .02 | 698 864
mit 258| 0 0 -1 -42 21 -16 -.34 10 9 | -251 274 23 172
| 0 0 1 22 22 12 .03 | 348 534
ngs 257| 0 0 7 86 -47 -14 -.26 9 8 | -327 -263 2154 3806
| 0 0 1 30 38 7 .03 | 373 721
sio 246| 0 1 -9 122 47 59 -.31 18 18 | --- --- --- ---
| 1 0 1 23 25 11 .02 | --- ---
Table 1.1698.b GPS week : 1698 MJD: 56130.000-56136.000
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 | 4 4 4 4 4 3 4 |
2 | 4 4 4 4 4 4 4 |
3 | 5 6 5 6 6 5 5 |
4 | 3 3 3 3 3 3 3 |
5 | 5 4 6 4 4 5 5 |
6 | 4 5 5 5 5 5 5 |
7 | 4 4 4 4 4 4 4 |
8 | 4 3 3 3 3 3 3 |
9 | 4 4 4 4 3 4 4 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 3 4 4 4 |
12 | 6 5 5 5 5 4 5 |
13 | 4 4 4 3 3 3 4 |
14 | 4 4 4 3 4 3 4 |
15 | 5 4 5 4 4 4 4 |
16 | 5 5 4 4 5 4 4 |
17 | 4 3 3 4 3 4 4 |
18 | 4 4 4 4 4 3 3 |
19 | 4 4 3 3 3 4 3 |
20 | 4 4 4 4 4 4 4 |
21 | 4 5 4 4 4 4 5 |
22 | 4 4 3 3 3 3 3 |
23 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 3 3 3 3 |
27 | 4 4 4 4 3 3 4 |
28 | 4 4 4 4 4 4 4 |
29 | 4 5 5 4 4 4 5 |
30 | 4 4 4 4 4 4 4 |
31 | 4 5 4 4 4 4 4 |
32 | 4 4 4 3 4 3 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 2.1698.0 GPS week: 1698 Day: 0 MJD: 56130.000
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 261| -1 0 -6 10 52 7 -.26 9 9 | -393 150 13 54
| 58 -2 |
emr 89| 2 -4 -3 -77 71 -28 .42 16 16 | 525 625 31 128
| -7 -41 |
esa 175| 0 0 2 -33 -30 11 .27 6 6 | -1550 1553 12 114
| 27 10 |
gfz 196| 0 -1 0 10 16 -6 -.28 11 11 | -185 543 33 143
| -3 16 |
grg 124| 1 0 10 20 -50 -13 .52 17 15 | -183 394 58 214
| -5 -14 |
igr n/a| 0 0 -1 -70 30 -31 -.05 4 4 | 17064 -173 21 78
| 24 11 |
jpl 142| 0 0 -5 -18 -1 19 .48 14 14 | 2143 303 21 101
| 2 -29 |
mit 258| 0 0 0 -25 1 -36 -.30 11 9 | -706 944 22 166
| 11 -25 |
ngs 257| 0 1 6 89 -45 -16 -.25 10 9 | -131 -371 2407 3827
| 0 48 |
sio 246| -3 2 -10 121 27 49 -.29 18 20 | --- --- --- ---
| -75 -27 |
Table 2.1698.1 GPS week: 1698 Day: 1 MJD: 56131.000
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 261| -1 0 -6 8 55 0 -.29 9 9 | -441 -644 14 51
| 57 -2 |
emr 89| 1 -2 -4 -47 43 -42 .38 15 15 | 1484 -512 29 111
| -44 -16 |
esa 175| 1 0 2 3 -38 23 .30 7 7 | -241 142 13 114
| 4 23 |
gfz 196| 0 0 -1 -22 29 -6 -.27 10 10 | 962 -644 34 162
| -21 -1 |
grg 124| 2 0 12 27 -32 0 .56 15 14 | 107 305 57 215
| -21 -20 |
igr n/a| 0 0 -2 -68 18 -36 -.08 4 4 | 17296 -869 18 62
| -7 23 |
jpl 142| 2 1 -5 -21 -31 2 .47 14 14 | 2886 -428 18 92
| -42 33 |
mit 258| 0 -1 0 -82 31 -24 -.32 10 10 | -314 772 23 178
| 33 -26 |
ngs 257| -2 0 6 87 -58 -9 -.24 9 7 | -433 -472 2118 4314
| -41 37 |
sio 246| -1 0 -9 83 58 54 -.32 19 18 | --- --- --- ---
| -62 -23 |
Table 2.1698.2 GPS week: 1698 Day: 2 MJD: 56132.000
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 261| -1 0 -3 19 47 -15 -.29 8 8 | 127 -1449 13 65
| 62 6 |
emr 89| 0 -3 -3 -73 36 -40 .34 13 13 | 132 -313 30 136
| 11 -9 |
esa 175| 0 1 2 -31 -18 18 .28 7 7 | -347 -716 14 131
| 19 -12 |
gfz 196| 0 0 2 -53 58 2 -.30 11 10 | 253 70 33 148
| 3 -9 |
grg 124| 1 0 7 16 -58 -28 .57 15 14 | 409 -658 47 196
| -15 -5 |
igr n/a| 0 0 -1 -62 33 -33 -.08 4 4 | 15564 -593 19 62
| 4 10 |
jpl 142| 1 0 -5 -8 -41 -8 .45 13 13 | 1397 -193 18 99
| 5 31 |
mit 258| 0 0 0 -46 20 -12 -.33 11 10 | 135 -434 25 178
| 17 -23 |
ngs 257| 0 0 5 114 -80 -5 -.30 10 9 | 405 -1494 2077 3880
| -3 32 |
sio 246| -1 1 -8 118 34 48 -.31 17 18 | --- --- --- ---
| -82 -24 |
Table 2.1698.3 GPS week: 1698 Day: 3 MJD: 56133.000
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 261| 0 0 -3 15 57 6 -.25 8 7 | -704 -308 12 61
| 73 -7 |
emr 89| 4 0 -4 -88 33 -3 .41 15 15 | 900 -1324 37 139
| -4 -3 |
esa 175| 0 0 1 -58 -20 7 .29 6 6 | 505 -1082 14 130
| 29 23 |
gfz 196| 0 0 1 13 44 -13 -.27 10 10 | 1327 -427 33 144
| 15 -21 |
grg 124| 0 0 8 47 -59 -29 .54 16 14 | 838 -1076 56 210
| -24 -18 |
igr n/a| 0 0 -1 -77 27 -18 -.07 4 4 | 16077 -1856 19 63
| 8 47 |
jpl 142| 1 0 -4 -5 -37 -31 .50 13 12 | 2293 -1253 18 100
| 9 35 |
mit 258| 0 0 0 -37 10 2 -.34 10 8 | 225 -318 24 176
| 19 -26 |
ngs 257| 0 -1 5 103 -57 -20 -.29 10 8 | -729 -241 2086 3866
| -45 44 |
sio 246| 0 1 -11 122 37 75 -.31 17 17 | --- --- --- ---
| -71 -33 |
Table 2.1698.4 GPS week: 1698 Day: 4 MJD: 56134.000
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 261| 0 0 -2 41 36 -10 -.23 9 8 | -525 765 16 64
| 17 19 |
emr 89| 0 -2 -8 -67 26 4 .42 14 14 | -339 454 34 136
| 3 -6 |
esa 175| 0 0 1 -81 -44 23 .29 7 7 | -410 -442 13 131
| 54 10 |
gfz 196| -1 0 1 -17 69 -9 -.20 11 11 | 515 -478 33 148
| 28 10 |
grg 124| 3 0 9 54 -61 -8 .55 15 13 | -112 304 59 193
| -18 3 |
igr n/a| 0 0 -1 -61 17 -13 -.06 4 4 | 14412 54 20 71
| 10 23 |
jpl 142| 1 0 -7 -6 -52 -15 .53 13 13 | 1086 497 20 100
| 6 54 |
mit 258| 0 0 -1 -57 64 -5 -.35 8 8 | -164 293 22 175
| 10 -35 |
ngs 257| 0 0 9 114 -84 -20 -.25 9 7 | -510 845 2189 3591
| -25 53 |
sio 246| 0 1 -10 114 87 73 -.28 17 17 | --- --- --- ---
| -97 -44 |
Table 2.1698.5 GPS week: 1698 Day: 5 MJD: 56135.000
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 261| 0 0 -2 14 42 33 -.21 7 7 | -445 -228 13 58
| 48 2 |
emr 89| 0 0 -6 -75 52 -22 .44 14 14 | -589 746 30 138
| -30 -37 |
esa 175| 0 -1 1 -58 -37 4 .30 7 7 | -1260 -399 14 123
| 42 28 |
gfz 196| 0 0 2 84 15 -7 -.22 10 10 | -427 -336 33 152
| 1 41 |
grg 124| 3 0 12 31 -74 31 .57 16 14 | -91 1436 75 231
| -3 -18 |
igr n/a| 0 0 0 -103 -1 -4 -.05 5 4 | 13838 460 19 59
| 37 27 |
jpl 142| 1 0 -6 -27 -46 -20 .52 13 13 | 981 865 19 107
| -6 37 |
mit 258| 0 1 -3 -29 25 -19 -.35 8 8 | -329 50 25 164
| 10 -30 |
ngs 257| 0 0 7 27 -39 -24 -.23 9 7 | -327 -405 1895 3211
| 26 0 |
sio 246| 0 2 -10 141 70 64 -.29 18 16 | --- --- --- ---
| -104 -47 |
Table 2.1698.6 GPS week: 1698 Day: 6 MJD: 56136.000
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 261| 0 0 -1 22 61 -26 -.25 8 7 | -595 339 15 62
| 35 -13 |
emr 89| 1 -3 -4 -92 25 9 .37 14 14 | 312 1031 30 137
| 13 6 |
esa 175| -1 0 0 -54 -6 29 .25 7 6 | -568 -1101 14 129
| 33 23 |
gfz 196| -1 0 1 79 -131 -36 -.24 14 14 | -465 778 35 158
| -32 42 |
grg 124| 3 0 6 35 -59 2 .53 15 14 | 2 1789 59 192
| 7 -44 |
igr n/a| 0 0 0 -77 28 -17 -.10 5 4 | 14450 791 20 75
| 12 16 |
jpl 142| 0 0 -6 -29 -28 20 .49 12 12 | 2033 1338 20 105
| 13 15 |
mit 258| 0 0 -1 -18 -2 -20 -.41 10 8 | -608 614 25 172
| 20 -21 |
ngs 257| 0 0 7 68 30 -5 -.23 10 8 | -564 291 2306 3956
| -7 -51 |
sio 246| 1 1 -6 157 14 51 -.33 20 16 | --- --- --- ---
| -98 -23 |
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 3.1698.0 GPS week: 1698 Day: 0 MJD: 56130.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 15 5 12 13 4 13 10 8 13 3 | 25 32 35 32 45 33 44 32 34 26 32
2 | 8 17 9 8 16 4 17 10 8 22 4 | 31 40 35 32 39 32 40 31 30 30 32
3E | 9 22 6 14 20 7 18 11 15 14 4 | 107 110 108 106 107 108 108 112 113 110 109
4 | 9 10 5 7 15 3 13 7 11 11 3 | 24 30 34 31 39 30 28 28 35 25 30
5 | 11 14 5 8 12 5 15 8 10 34 4 | 22 29 30 29 35 27 31 26 30 29 27
6E | 11 17 5 13 19 4 15 12 12 13 4 | 74 77 73 76 80 72 76 70 71 69 72
7 | 8 19 5 11 19 3 13 7 9 12 3 | 13 28 18 22 26 14 23 19 15 18 15
8 | 8 14 7 7 16 4 11 14 11 13 3 | 9 24 15 14 14 11 18 18 13 15 12
9 | 7 11 5 11 14 4 10 15 10 17 3 | 20 25 22 24 22 22 25 28 24 35 22
10 | 8 11 5 9 11 4 8 8 11 15 3 | 23 27 29 29 35 26 27 28 34 23 28
11 | 8 11 5 12 20 4 11 9 10 13 3 | 18 29 24 23 40 21 29 21 22 18 21
12 | 17 20 11 12 21 4 18 17 9 22 5 | 23 29 22 25 24 20 27 27 18 25 20
13 | 8 13 4 9 24 4 10 10 9 11 3 | 12 20 15 15 30 13 18 14 12 16 12
14 | 7 14 6 9 16 4 14 11 8 10 3 | 10 17 14 10 25 10 17 13 10 14 10
15 | 11 27 9 13 18 5 20 10 9 19 5 | 11 32 22 25 30 17 27 21 17 20 18
16 | 9 18 6 17 20 2 16 7 9 23 4 | 15 26 19 12 26 14 25 13 16 19 15
17E | 7 13 5 8 21 3 17 7 12 15 3 | 22 29 28 25 32 24 28 23 25 22 24
18 | 7 13 5 13 11 4 16 15 9 21 4 | 21 26 22 30 25 23 25 28 27 24 22
19E | 6 16 5 11 17 4 10 11 10 13 3 | 18 27 23 19 25 19 25 22 20 21 20
20 | 7 13 5 11 14 3 12 8 10 27 3 | 20 21 19 26 26 19 21 22 23 18 20
21 | 8 16 6 13 14 3 17 8 11 28 4 | 18 27 19 17 25 16 29 19 16 22 17
22 | 5 13 4 10 13 4 15 15 10 21 4 | 18 26 21 22 27 20 23 27 20 27 20
23 | 8 16 5 12 16 3 14 12 11 12 3 | 12 22 14 16 23 14 22 19 12 14 13
25 | 7 28 5 7 20 4 14 10 8 12 4 | 13 27 16 18 26 14 24 20 15 21 15
26 | 10 13 6 9 12 7 17 11 7 19 3 | 16 33 22 22 28 19 34 27 17 32 22
27 | 7 12 4 10 18 4 11 13 10 15 3 | 17 23 19 20 21 19 22 28 21 32 20
28 | 7 15 5 10 17 5 11 7 8 19 3 | 10 27 18 13 28 13 24 14 15 19 15
29E | 9 19 8 10 15 5 20 9 12 12 4 | 15 24 22 17 23 18 26 19 19 20 18
30 | 9 10 5 10 19 3 12 9 8 23 3 | 12 18 15 14 18 11 23 13 11 28 13
31 | 10 15 5 13 21 5 13 10 8 15 4 | 15 25 18 15 30 14 23 17 16 22 15
32 | 8 14 7 10 13 2 9 9 10 20 3 | 12 18 20 18 23 16 19 17 18 24 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 6 11 17 4 14 11 10 18 |T 21 30 26 25 32 23 30 26 24 27 24
WRMS | 9 16 6 11 15 4 14 9 9 20 |NE 16 26 21 21 28 18 25 21 20 22 19
MEDI | 8 14 5 10 16 4 14 10 10 15 |MD 18 27 22 22 26 19 25 22 19 22 20
Table 3.1698.1 GPS week: 1698 Day: 1 MJD: 56131.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 13 8 11 13 4 15 10 8 13 3 | 24 37 34 24 41 28 44 26 29 23 30
2 | 8 15 9 7 13 5 16 10 10 22 4 | 25 33 29 22 37 25 37 23 27 18 27
3E | 10 39 11 11 16 6 18 11 15 16 6 | 112 122 114 113 113 111 114 113 116 115 113
4 | 9 10 8 9 9 4 11 7 9 10 3 | 21 23 29 25 29 21 23 23 24 21 25
5 | 9 12 4 8 10 4 15 9 8 35 4 | 17 23 24 19 27 16 24 17 19 24 20
6E | 12 20 7 9 19 6 16 11 13 17 4 | 79 72 76 77 81 77 73 74 74 72 75
7 | 6 15 6 12 16 5 14 10 8 12 3 | 15 19 13 16 25 13 22 15 15 16 13
8 | 8 11 6 7 11 4 12 11 9 13 3 | 13 18 13 13 15 10 19 18 13 17 13
9 | 10 10 5 12 11 4 13 12 8 19 3 | 15 18 16 14 19 12 20 18 12 20 15
10 | 7 12 7 8 12 5 9 8 7 15 3 | 21 24 23 19 25 19 20 22 23 18 22
11 | 8 10 10 7 16 5 12 11 8 14 3 | 18 31 26 18 38 22 31 19 23 20 22
12 | 15 19 11 13 22 4 17 14 9 18 5 | 18 23 19 17 28 12 23 20 16 17 15
13 | 7 11 7 12 18 5 10 9 10 11 3 | 12 17 14 13 30 11 18 11 14 12 12
14 | 6 12 5 9 16 3 14 9 9 13 3 | 13 18 14 12 25 10 19 11 13 13 12
15 | 10 16 7 12 15 4 17 10 11 14 4 | 14 21 18 16 26 10 21 13 15 13 15
16 | 10 15 10 15 19 5 17 8 10 23 4 | 14 23 20 16 30 14 25 10 15 10 15
17E | 7 10 6 6 13 3 15 6 11 11 3 | 17 23 22 19 27 19 25 15 23 15 19
18 | 7 13 4 14 10 5 13 16 5 22 4 | 15 18 11 25 16 14 18 20 16 17 14
19E | 5 17 8 12 16 5 10 9 8 12 3 | 23 35 27 24 32 25 31 19 22 21 23
20 | 7 12 4 9 13 4 11 9 9 27 3 | 21 22 23 23 26 20 22 21 22 18 22
21 | 8 15 7 8 15 4 16 12 8 30 4 | 17 22 17 13 24 14 26 15 15 16 14
22 | 6 11 4 11 10 3 13 13 6 21 3 | 14 19 14 13 20 12 21 18 13 19 13
23 | 9 14 8 11 15 3 12 12 10 13 4 | 17 21 20 14 26 14 20 14 19 14 17
25 | 7 16 6 8 16 2 15 9 7 15 3 | 12 14 15 11 24 8 23 12 12 16 11
26 | 10 12 6 10 12 4 11 11 9 24 4 | 13 22 17 15 25 12 28 17 17 24 17
27 | 11 10 4 12 15 5 12 12 8 16 3 | 11 16 13 12 19 10 18 18 14 19 13
28 | 7 12 5 10 15 5 12 7 7 18 3 | 11 22 15 17 27 13 21 14 15 17 14
29E | 12 21 7 6 16 5 20 8 10 19 4 | 14 20 20 14 20 12 23 15 16 20 15
30 | 8 10 9 11 16 3 11 10 8 25 4 | 16 19 22 17 20 14 23 12 12 26 16
31 | 13 15 10 12 19 3 16 9 10 16 4 | 15 24 20 16 30 12 24 10 12 16 14
32 | 8 13 6 8 14 3 12 8 6 21 3 | 15 21 19 18 25 17 23 16 20 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 7 10 15 4 14 10 9 19 |T 21 27 24 22 30 20 28 21 22 22 22
WRMS | 9 15 7 10 14 4 14 10 7 18 |NE 16 21 19 16 26 14 23 16 17 17 16
MEDI | 8 13 7 10 15 4 13 10 9 16 |MD 15 22 20 17 26 14 23 17 16 18 15
Table 3.1698.2 GPS week: 1698 Day: 2 MJD: 56132.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 13 6 10 11 5 14 10 10 16 3 | 27 33 39 32 43 31 46 29 36 25 34
2 | 7 15 7 7 13 4 15 11 9 21 4 | 31 40 38 30 40 33 43 31 33 27 34
3E | 13 18 7 12 15 5 16 11 16 17 4 | 81 86 85 89 88 85 86 89 87 88 85
4 | 7 9 6 9 8 3 11 8 7 8 2 | 21 23 25 24 23 21 22 25 28 21 23
5 | 10 13 24 11 10 4 14 17 11 33 6 | 19 26 38 21 26 20 27 23 22 26 23
6E | 14 21 8 17 18 4 19 10 12 15 5 | 44 40 41 35 44 40 40 41 43 43 40
7 | 7 13 7 12 16 4 13 10 7 11 3 | 16 21 14 20 24 12 20 17 18 16 15
8 | 8 8 5 8 9 3 10 6 8 10 2 | 14 16 12 12 12 10 16 16 18 14 13
9 | 8 12 7 11 14 4 11 12 10 14 3 | 15 18 19 18 16 14 22 18 19 22 17
10 | 7 9 5 10 12 5 9 10 7 13 3 | 20 23 21 22 24 19 22 22 26 20 22
11 | 6 10 4 10 17 4 11 10 12 14 3 | 19 31 27 25 42 22 34 20 26 19 25
12 | 13 15 8 14 23 6 17 12 10 15 4 | 22 25 22 23 25 16 25 22 17 21 20
13 | 6 11 5 10 20 6 9 12 10 10 3 | 17 18 16 13 31 13 18 15 17 17 15
14 | 5 13 6 10 17 2 13 8 11 9 3 | 11 19 14 11 25 11 20 14 16 14 13
15 | 12 19 7 11 15 4 18 11 11 12 4 | 19 26 18 18 29 16 25 18 19 17 18
16 | 7 16 8 15 18 5 15 9 9 21 4 | 16 24 19 15 26 14 24 13 18 15 16
17E | 6 12 7 9 12 5 14 8 7 11 3 | 20 25 24 25 26 21 26 18 21 17 21
18 | 6 13 5 14 12 4 14 15 8 18 4 | 19 19 18 25 17 17 21 24 22 19 18
19E | 5 10 4 11 15 5 10 9 6 13 3 | 25 32 28 27 37 25 32 25 26 23 26
20 | 8 10 5 15 13 4 11 8 15 26 4 | 21 19 21 25 19 17 21 20 25 17 21
21 | 7 13 6 7 13 5 17 10 11 28 4 | 17 24 19 14 27 16 28 19 17 18 18
22 | 5 11 5 9 10 3 11 12 6 18 3 | 14 20 18 18 20 15 21 23 16 22 16
23 | 9 11 7 11 14 3 12 12 11 13 3 | 18 21 20 15 25 14 23 17 19 15 18
25 | 6 17 5 6 22 5 14 9 9 14 3 | 17 20 18 15 26 14 26 20 19 20 17
26 | 7 13 9 9 12 3 9 13 11 17 3 | 18 30 21 20 27 17 28 23 19 25 21
27 | 8 12 6 12 16 5 9 12 8 15 3 | 14 18 18 19 18 13 19 19 21 23 17
28 | 5 13 8 14 16 5 12 8 9 17 3 | 13 22 17 14 24 13 21 16 17 19 15
29E | 11 18 5 10 14 5 19 11 14 11 4 | 18 25 24 18 30 19 27 24 24 25 22
30 | 7 10 7 9 15 4 10 8 9 24 3 | 15 21 19 14 18 14 21 18 21 30 18
31 | 12 15 7 11 20 6 14 8 8 14 4 | 17 25 20 16 30 16 25 18 20 20 18
32 | 8 12 4 12 11 3 9 10 11 20 3 | 18 24 25 24 24 20 24 21 22 27 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 7 11 15 4 13 11 10 17 |T 21 26 24 22 28 20 27 23 24 23 22
WRMS | 8 13 7 10 14 4 13 10 9 18 |NE 18 23 21 19 25 16 24 20 21 20 19
MEDI | 7 13 6 11 14 4 13 10 10 15 |MD 18 24 20 20 26 16 24 20 21 20 18
Table 3.1698.3 GPS week: 1698 Day: 3 MJD: 56133.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 14 5 13 11 3 11 9 8 11 3 | 23 29 32 31 41 27 40 24 27 17 27
2 | 6 18 7 7 15 4 16 8 8 20 3 | 28 39 33 25 35 28 37 24 25 24 28
3E | 15 24 9 14 15 7 19 18 22 31 6 | 134 137 133 129 136 131 135 136 137 133 134
4 | 8 10 5 7 12 4 12 8 7 8 3 | 23 27 30 28 31 24 31 25 27 23 26
5 | 8 12 6 8 11 4 13 10 9 32 4 | 22 28 23 26 29 23 29 23 24 29 23
6E | 12 28 8 12 21 5 21 12 12 19 5 | 78 80 83 85 84 81 80 80 80 82 80
7 | 8 16 5 7 19 4 15 8 12 10 3 | 17 23 17 19 26 16 24 19 22 18 17
8 | 8 10 5 11 10 4 8 7 8 10 3 | 15 17 15 17 17 12 18 17 18 16 14
9 | 9 16 8 8 14 5 10 11 10 14 3 | 11 25 20 17 17 17 21 20 16 24 16
10 | 6 9 6 10 12 4 7 8 8 13 3 | 27 27 27 29 32 26 29 26 33 26 27
11 | 6 10 3 11 18 3 11 10 10 12 3 | 15 27 20 19 38 17 29 14 15 14 18
12 | 12 20 8 16 20 3 14 11 12 16 4 | 17 26 17 20 25 14 22 21 16 20 16
13 | 6 14 3 8 19 3 9 8 7 9 3 | 12 19 14 13 29 11 19 13 14 14 12
14 | 6 15 6 13 15 3 13 6 7 8 3 | 15 25 22 19 27 19 23 19 20 19 18
15 | 8 18 8 10 15 6 17 12 10 13 4 | 11 25 18 15 25 14 22 19 12 19 14
16 | 6 15 6 12 18 4 15 7 11 21 4 | 15 26 20 16 27 16 26 15 16 15 16
17E | 7 13 5 14 17 4 14 8 7 9 3 | 20 29 28 25 28 23 28 22 22 20 23
18 | 6 12 6 14 10 4 12 15 7 17 3 | 18 23 22 28 22 19 22 25 19 21 19
19E | 6 14 4 9 16 3 11 9 10 10 3 | 18 25 22 20 28 18 27 16 17 18 19
20 | 7 12 5 11 14 4 10 6 7 25 3 | 18 19 19 23 23 16 18 18 18 14 17
21 | 7 15 5 7 13 3 18 9 9 30 4 | 18 25 20 18 26 18 27 19 16 17 17
22 | 6 12 4 7 11 4 10 8 8 18 3 | 19 28 24 22 26 23 27 26 22 28 22
23 | 7 16 4 10 14 3 12 10 11 11 3 | 11 21 15 13 24 11 19 14 11 11 12
25 | 4 17 7 9 25 4 12 8 9 14 3 | 16 19 17 17 28 16 24 20 17 20 16
26 | 7 12 5 8 13 4 11 10 8 16 3 | 15 25 19 16 23 16 27 22 16 24 18
27 | 10 14 5 9 15 4 10 11 9 13 3 | 11 20 17 17 17 15 19 19 13 22 14
28 | 7 16 7 10 17 5 13 8 7 18 3 | 16 24 21 21 30 16 24 17 17 21 18
29E | 11 20 7 8 20 3 18 9 12 9 4 | 19 25 23 23 26 19 23 22 21 23 20
30 | 7 10 6 8 16 4 9 6 10 24 3 | 20 26 24 21 24 20 25 21 20 30 21
31 | 8 14 6 11 21 3 12 7 7 14 3 | 21 30 25 23 33 22 29 19 21 22 22
32 | 6 13 5 9 14 4 9 9 9 20 3 | 13 23 21 17 24 15 22 17 13 23 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 15 6 10 16 4 13 10 10 17 |T 23 30 27 26 32 23 30 25 24 26 24
WRMS | 7 15 6 10 14 4 12 8 8 17 |NE 17 24 21 20 26 18 25 19 18 20 18
MEDI | 7 14 6 10 15 4 12 9 9 14 |MD 18 25 21 20 27 18 25 20 18 21 18
Table 3.1698.4 GPS week: 1698 Day: 4 MJD: 56134.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 17 6 13 11 5 15 8 8 14 3 | 23 28 33 25 40 27 40 24 30 21 28
2 | 6 15 7 7 13 5 18 10 5 20 3 | 24 36 30 24 36 24 37 22 24 19 26
3E | 16 21 6 18 17 7 17 13 17 26 5 | 67 72 70 68 69 68 73 71 69 76 70
4 | 6 10 5 9 9 3 12 7 8 10 3 | 31 31 34 35 36 32 31 34 36 29 33
5 | 7 11 6 10 10 5 13 7 8 34 4 | 21 26 25 21 28 22 27 18 25 26 23
6E | 14 25 9 15 21 6 18 12 13 14 5 | 42 48 45 51 52 47 45 44 47 44 44
7 | 9 16 6 11 19 3 14 6 7 12 3 | 22 25 19 19 30 17 23 20 20 19 19
8 | 8 10 6 11 10 5 10 6 7 8 3 | 15 16 13 14 17 11 15 15 15 15 13
9 | 7 12 5 9 13 3 10 8 7 10 3 | 11 21 13 12 19 9 17 11 13 12 12
10 | 6 9 4 9 10 4 10 7 6 15 2 | 27 26 30 27 32 28 27 27 33 23 29
11 | 6 12 6 13 19 4 11 8 11 15 3 | 16 28 25 21 40 19 28 17 20 15 20
12 | 15 16 8 13 20 3 15 9 11 17 4 | 16 24 19 17 28 14 23 16 19 17 17
13 | 5 14 5 8 19 3 12 7 8 11 3 | 17 21 17 16 30 14 21 14 18 15 17
14 | 8 11 11 13 15 3 12 8 9 11 3 | 14 18 15 19 27 14 21 14 14 15 15
15 | 9 16 7 11 15 7 17 10 7 12 4 | 16 23 16 12 24 12 24 17 15 18 15
16 | 14 16 9 13 18 4 15 6 9 20 4 | 15 26 22 22 31 18 26 14 23 14 19
17E | 8 12 7 8 10 3 13 8 5 7 3 | 23 27 25 24 30 22 28 25 23 19 23
18 | 5 13 5 12 10 5 14 11 5 15 3 | 19 21 18 26 19 18 21 22 21 22 19
19E | 7 11 6 10 16 3 14 7 6 13 3 | 18 27 25 19 32 20 28 16 20 17 21
20 | 6 12 8 15 11 2 11 8 6 26 3 | 21 21 25 27 26 22 21 21 25 16 22
21 | 6 15 7 9 11 3 17 8 10 32 4 | 16 26 18 14 23 15 27 15 15 19 15
22 | 6 13 5 8 9 4 11 5 8 19 3 | 19 23 20 19 26 18 23 20 24 23 20
23 | 8 13 7 8 16 2 14 10 9 11 3 | 18 20 16 14 24 13 20 13 18 14 16
25 | 6 16 7 11 23 4 13 7 7 12 3 | 14 21 19 16 30 13 24 16 16 15 15
26 | 7 12 7 13 10 3 11 10 7 13 3 | 17 30 20 17 25 18 27 19 21 22 20
27 | 9 10 6 12 16 4 9 6 9 10 3 | 13 21 14 12 22 11 17 12 14 14 13
28 | 8 14 7 11 18 5 11 6 8 19 3 | 13 25 23 20 29 17 23 20 22 18 19
29E | 7 19 9 8 14 4 18 8 10 11 4 | 15 28 24 15 22 17 23 18 20 19 19
30 | 8 11 9 9 14 3 11 6 6 25 3 | 15 24 25 20 28 19 27 15 20 29 20
31 | 7 14 10 9 22 3 12 10 12 14 4 | 16 23 23 17 35 14 24 17 16 15 18
32 | 8 12 7 11 11 3 8 7 7 22 3 | 15 21 24 22 25 17 22 16 19 26 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 7 11 15 4 13 8 9 17 |T 20 26 24 22 30 20 26 20 23 21 21
WRMS | 8 14 7 11 13 4 13 8 7 17 |NE 17 24 21 19 28 17 24 18 20 18 19
MEDI | 7 13 7 11 14 4 13 8 8 14 |MD 17 25 23 19 28 18 24 17 20 19 19
Table 3.1698.5 GPS week: 1698 Day: 5 MJD: 56135.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 10 6 10 12 6 13 8 10 13 3 | 24 32 34 26 43 29 44 23 28 22 28
2 | 7 15 8 7 15 5 16 13 6 19 4 | 25 40 35 26 38 29 39 28 27 20 29
3E | 12 18 6 20 13 6 16 9 12 17 4 | 122 129 127 128 125 124 129 128 127 125 126
4 | 5 12 7 6 12 4 14 5 7 10 3 | 16 20 19 21 23 18 18 16 19 18 16
5 | 6 14 8 10 13 4 14 6 7 39 4 | 16 26 23 21 26 18 25 14 19 26 18
6E | 14 24 7 17 15 7 19 14 13 19 5 | 79 76 75 80 81 79 73 73 79 77 75
7 | 6 16 5 10 19 3 16 7 11 15 3 | 16 24 15 17 26 15 24 15 19 21 15
8 | 7 10 6 11 11 4 11 5 5 8 2 | 16 20 16 13 17 15 18 13 16 14 14
9 | 9 12 6 8 15 3 12 7 12 10 3 | 14 25 19 16 19 18 22 18 22 18 17
10 | 5 9 6 8 13 5 9 5 6 15 2 | 18 22 16 23 25 20 21 18 24 22 19
11 | 7 13 7 8 20 4 11 8 11 15 3 | 14 29 23 17 41 19 29 14 19 17 19
12 | 9 18 8 12 22 4 16 9 9 18 4 | 16 24 18 19 25 17 24 17 18 20 16
13 | 6 14 6 10 20 4 11 7 5 11 3 | 13 25 15 12 30 13 20 12 13 16 13
14 | 4 14 6 8 18 5 10 9 10 10 3 | 16 25 17 15 30 17 20 15 20 18 15
15 | 10 20 9 9 18 5 20 10 7 14 4 | 14 26 19 16 28 15 25 20 17 22 16
16 | 7 17 9 10 17 5 15 8 8 22 4 | 12 26 17 12 25 14 25 11 13 14 12
17E | 6 13 4 10 24 4 14 11 10 8 3 | 19 25 23 22 41 21 27 23 19 18 21
18 | 7 13 5 13 11 5 11 9 6 13 3 | 16 23 18 25 18 19 23 20 19 21 17
19E | 7 16 9 9 18 4 10 5 9 12 3 | 13 29 23 14 32 16 24 14 16 15 17
20 | 6 13 8 11 12 4 11 9 8 26 3 | 19 23 21 17 21 20 22 22 22 21 19
21 | 6 18 7 9 13 4 16 8 7 32 4 | 12 24 17 14 26 15 24 14 16 17 13
22 | 7 11 7 8 12 3 9 5 10 20 3 | 15 23 22 19 23 19 21 17 22 25 17
23 | 8 15 7 10 16 3 13 10 8 15 3 | 14 25 18 11 26 15 21 19 17 20 15
25 | 7 15 6 9 23 6 14 8 10 12 3 | 17 17 17 19 25 19 24 18 22 16 16
26 | 5 11 7 9 12 5 10 8 8 14 3 | 16 27 19 16 25 17 27 20 21 20 18
27 | 9 9 5 9 15 3 13 7 11 9 3 | 14 24 17 15 20 18 21 17 20 19 16
28 | 7 13 7 11 16 6 12 6 7 21 3 | 16 24 19 16 27 17 21 17 16 21 15
29E | 9 17 8 8 15 4 19 10 8 9 4 | 24 26 30 26 28 26 27 27 21 30 25
30 | 5 10 6 8 14 5 9 7 9 27 3 | 19 27 22 20 22 21 26 18 21 30 19
31 | 6 13 6 10 21 5 13 11 9 13 3 | 20 29 22 21 32 20 27 17 24 20 20
32 | 4 12 6 9 9 4 10 6 7 22 3 | 13 23 20 14 21 17 22 14 17 26 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 7 10 16 5 13 8 9 18 |T 21 30 25 23 31 23 29 22 24 25 22
WRMS | 7 14 7 10 14 4 13 8 7 16 |NE 16 25 19 17 26 18 24 17 19 20 17
MEDI | 7 13 7 9 15 4 13 8 8 15 |MD 16 25 19 17 26 18 24 17 19 20 17
Table 3.1698.6 GPS week: 1698 Day: 6 MJD: 56136.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 13 4 16 12 4 15 8 12 12 3 | 31 37 43 36 54 37 52 32 37 28 38
2 | 7 17 7 15 13 4 17 12 7 20 4 | 28 41 33 27 41 30 41 28 27 23 30
3E | 9 20 8 19 13 7 16 14 15 30 5 | 133 141 136 128 137 134 137 136 132 142 134
4 | 6 11 4 12 11 3 10 7 6 14 2 | 28 30 32 33 37 29 30 31 31 26 29
5 | 10 13 7 15 13 4 13 5 11 43 4 | 23 28 29 29 30 25 29 21 27 34 24
6E | 14 21 10 18 13 7 15 13 16 23 5 | 83 80 80 89 86 83 82 79 86 81 82
7 | 4 15 6 17 18 3 14 7 12 14 4 | 16 24 17 18 26 15 23 16 22 17 16
8 | 9 10 6 15 10 3 11 6 11 9 3 | 10 19 14 15 11 10 16 11 15 12 9
9 | 9 13 7 13 15 4 10 11 9 13 3 | 14 19 17 13 21 14 23 14 13 16 13
10 | 4 11 6 11 13 5 7 7 10 18 3 | 26 29 27 28 34 24 26 26 29 30 26
11 | 6 12 4 13 18 4 8 8 11 15 3 | 19 32 28 23 46 23 32 19 26 20 24
12 | 11 16 10 16 17 5 15 10 11 17 4 | 17 25 18 16 28 15 24 11 18 13 13
13 | 7 14 7 14 21 5 10 8 7 11 3 | 11 20 15 16 32 12 19 14 14 15 12
14 | 6 12 8 11 13 4 12 9 11 11 3 | 13 22 19 13 22 15 22 17 22 20 15
15 | 9 20 8 13 15 4 16 11 8 15 4 | 12 24 17 17 25 12 22 17 14 21 13
16 | 8 16 9 16 16 6 12 7 9 24 4 | 15 27 20 16 27 14 27 14 16 16 16
17E | 8 10 7 18 17 5 13 17 11 11 4 | 52 54 54 49 57 50 54 54 49 47 51
18 | 6 12 5 15 11 5 11 6 8 14 3 | 21 26 24 27 23 22 25 24 23 28 22
19E | 5 14 4 13 15 4 12 9 7 11 3 | 17 30 26 20 34 21 27 18 19 20 21
20 | 5 12 5 14 12 4 11 11 9 29 3 | 24 26 26 33 30 26 25 24 27 22 24
21 | 8 19 5 12 13 4 17 10 8 34 4 | 19 31 21 15 25 17 29 16 15 21 16
22 | 6 13 4 13 8 4 11 5 7 23 3 | 20 28 26 24 26 23 25 24 24 32 23
23 | 7 15 7 13 17 5 14 11 8 18 4 | 15 24 19 16 24 14 24 18 14 17 15
25 | 6 17 6 14 23 5 13 9 10 13 4 | 15 19 18 13 30 13 24 14 13 10 12
26 | 7 12 6 15 8 5 10 8 10 13 3 | 14 28 19 18 20 16 24 16 17 19 15
27 | 9 12 6 14 17 4 10 11 8 9 3 | 10 17 16 12 21 12 21 11 13 11 10
28 | 7 13 6 17 16 5 11 6 13 25 4 | 12 25 19 18 24 14 23 14 18 23 14
29E | 13 16 10 13 19 7 16 20 9 24 5 | 47 42 41 32 40 36 42 46 32 32 38
30 | 8 10 6 14 13 5 11 5 9 26 3 | 13 21 18 18 17 14 24 14 17 26 15
31 | 8 16 7 13 20 3 12 8 12 17 4 | 15 26 18 17 29 16 22 15 17 20 15
32 | 5 11 5 11 11 4 8 6 7 25 3 | 15 24 21 24 28 19 24 16 20 30 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 7 14 15 5 12 10 10 20 |T 25 32 29 27 35 25 32 26 27 28 25
WRMS | 7 14 6 14 14 4 12 8 8 16 |NE 17 25 22 20 28 18 26 18 20 21 18
MEDI | 7 13 6 14 13 4 12 8 9 17 |MD 17 26 21 18 28 17 25 17 20 21 16
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 4.1698 GPS week: 1698 MJD: 56130.0-56136.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 |U 7 9 21 |U 5 6 19 | ---- ---- ---- |
emr | emr 2968 | 9 10 23 |U 6 10 30 | ---- ---- ---- |
esa | esa 2976 | 7 8 20 |U 4 6 19 | ---- ---- ---- |
gfz | gfz 2967 |U 8 9 20 |U 6 7 25 | ---- ---- ---- |
grg | grg 2975 |U 12 15 32 |U 11 17 47 | ---- ---- ---- |
igr | igr 2974 | 7 8 20 | 4 5 18 | ---- ---- ---- |
igs | igs 2913 | 7 8 20 | 4 6 19 | ---- ---- ---- |
jpl | jpl 2967 | 8 8 22 |U 5 6 21 | ---- ---- ---- |
mit | mit 2976 | 7 8 20 |U 7 9 32 | ---- ---- ---- |
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 5.1698.0 GPS week: 1698 Day: 0 MJD: 56130.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 10 32 | 5 5 20 | ---- ---- ---- |
emr | emr 2968 | 9 10 32 | 6 7 24 | ---- ---- ---- |
esa | esa 2976 | 8 10 30 | 5 6 20 | ---- ---- ---- |
gfz | gfz 2966 | 9 12 31 | 6 6 17 | ---- ---- ---- |
grg | grg 2976 | 13 18 41 | 12 14 54 | ---- ---- ---- |
igr | igr 2974 | 8 10 30 | 5 6 18 | ---- ---- ---- |
igs | igs 2888 | 7 9 29 | 5 5 17 | ---- ---- ---- |
jpl | jpl 2967 | 7 9 33 | 5 6 17 | ---- ---- ---- |
mit | mit 2976 | 7 7 29 | 6 8 22 | ---- ---- ---- |
Table 5.1698.1 GPS week: 1698 Day: 1 MJD: 56131.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 8 17 | 4 6 19 | ---- ---- ---- |
emr | emr 2968 | 7 6 19 | 6 11 32 | ---- ---- ---- |
esa | esa 2976 | 6 7 14 | 4 6 18 | ---- ---- ---- |
gfz | gfz 2969 | 6 7 16 | 5 6 20 | ---- ---- ---- |
grg | grg 2975 | 8 14 29 | 8 18 28 | ---- ---- ---- |
igr | igr 2975 | 6 7 16 | 4 5 16 | ---- ---- ---- |
igs | igs 2911 | 6 6 15 | 4 6 19 | ---- ---- ---- |
jpl | jpl 2968 | 7 7 18 | 5 6 22 | ---- ---- ---- |
mit | mit 2976 | 6 7 15 | 5 7 27 | ---- ---- ---- |
Table 5.1698.2 GPS week: 1698 Day: 2 MJD: 56132.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 15 | 4 6 17 | ---- ---- ---- |
emr | emr 2968 | 7 7 16 | 6 13 30 | ---- ---- ---- |
esa | esa 2976 | 6 7 14 | 4 6 16 | ---- ---- ---- |
gfz | gfz 2964 | 6 8 17 | 6 9 36 | ---- ---- ---- |
grg | grg 2975 | 10 12 29 | 15 18 74 | ---- ---- ---- |
igr | igr 2970 | 6 7 17 | 4 6 16 | ---- ---- ---- |
igs | igs 2875 | 5 7 13 | 4 6 17 | ---- ---- ---- |
jpl | jpl 2968 | 6 7 15 | 5 6 23 | ---- ---- ---- |
mit | mit 2976 | 6 8 13 | 9 11 42 | ---- ---- ---- |
Table 5.1698.3 GPS week: 1698 Day: 3 MJD: 56133.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 9 16 | 4 7 19 | ---- ---- ---- |
emr | emr 2968 | 11 12 16 | 6 11 28 | ---- ---- ---- |
esa | esa 2976 | 8 9 15 | 4 7 18 | ---- ---- ---- |
gfz | gfz 2967 | 8 8 15 | 4 8 21 | ---- ---- ---- |
grg | grg 2976 | 13 14 32 | 11 26 51 | ---- ---- ---- |
igr | igr 2976 | 7 8 15 | 4 6 19 | ---- ---- ---- |
igs | igs 2959 | 8 8 14 | 4 6 19 | ---- ---- ---- |
jpl | jpl 2968 | 8 7 17 | 4 6 20 | ---- ---- ---- |
mit | mit 2976 | 7 8 12 | 9 11 39 | ---- ---- ---- |
Table 5.1698.4 GPS week: 1698 Day: 4 MJD: 56134.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 7 16 | 4 5 19 | ---- ---- ---- |
emr | emr 2968 | 9 10 21 | 7 13 44 | ---- ---- ---- |
esa | esa 2976 | 5 6 15 | 4 5 19 | ---- ---- ---- |
gfz | gfz 2968 | 6 6 15 | 5 7 26 | ---- ---- ---- |
grg | grg 2976 | 11 12 32 | 9 12 53 | ---- ---- ---- |
igr | igr 2976 | 6 7 15 | 4 5 18 | ---- ---- ---- |
igs | igs 2884 | 6 8 16 | 4 6 21 | ---- ---- ---- |
jpl | jpl 2968 | 6 7 18 | 5 6 22 | ---- ---- ---- |
mit | mit 2976 | 5 9 16 | 7 9 35 | ---- ---- ---- |
Table 5.1698.5 GPS week: 1698 Day: 5 MJD: 56135.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 10 22 | 6 6 26 | ---- ---- ---- |
emr | emr 2968 | 12 12 29 | 7 6 27 | ---- ---- ---- |
esa | esa 2976 | 9 9 22 | 6 6 23 | ---- ---- ---- |
gfz | gfz 2969 | 8 10 21 | 8 6 24 | ---- ---- ---- |
grg | grg 2974 | 13 15 34 | 11 13 40 | ---- ---- ---- |
igr | igr 2975 | 9 9 22 | 6 6 23 | ---- ---- ---- |
igs | igs 2939 | 9 9 23 | 7 5 26 | ---- ---- ---- |
jpl | jpl 2967 | 9 9 23 | 6 5 23 | ---- ---- ---- |
mit | mit 2976 | 9 9 25 | 7 7 32 | ---- ---- ---- |
Table 5.1698.6 GPS week: 1698 Day: 6 MJD: 56136.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 11 28 | 3 4 18 | ---- ---- ---- |
emr | emr 2968 | 12 13 29 | 7 7 22 | ---- ---- ---- |
esa | esa 2976 | 11 11 28 | 4 5 18 | ---- ---- ---- |
gfz | gfz 2968 | 11 11 27 | 6 7 29 | ---- ---- ---- |
grg | grg 2976 | 14 17 28 | 7 14 30 | ---- ---- ---- |
igr | igr 2975 | 11 12 28 | 4 4 20 | ---- ---- ---- |
igs | igs 2936 | 11 11 27 | 4 4 17 | ---- ---- ---- |
jpl | jpl 2967 | 11 13 31 | 3 4 17 | ---- ---- ---- |
mit | mit 2976 | 10 12 27 | 7 8 29 | ---- ---- ---- |
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 : 10-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 6.1698 GPS week: 1698 MJD: 56130.500-56136.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 2 -48 -4 -58 3 | 7 27
| 9 23 74 90 4 | 3
emr uuuuu | 17 10 21 48 5 | 22 34
| 18 17 139 118 6 | 4
esa uuuuu | -13 -28 38 16 4 | 19 32
| 13 10 45 67 6 | 4
gfz uuuuu | -9 3 65 -90 -2 | 8 27
| 26 19 96 87 2 | 3
grg uuuux | 19 13 -62 -88 -23 | 15 37
| 13 10 48 61 17 | 6
igr xxxxx | -20 -11 17 -29 0 | 5 25
| 10 11 31 34 6 | 3
irf xxxxx | 2 2 -6 -12 0 | 9 26
| 5 8 28 25 3 | 3
jpl uuuuu | -23 3 61 48 1 | 20 31
| 24 12 48 49 6 | 3
mit uuuuu | 29 -16 -118 -21 1 | 21 33
| 9 16 47 47 6 | 3
ngs uuuuu | -21 15 -40 12 -6 | 16 25
| 34 21 95 130 6 | 2
sio uuuuu | 34 86 76 79 2 | 46 51
| 13 23 60 51 4 | 4
Table 7.1698.0 GPS week: 1698 Day: 0 MJD: 56130.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 2 -54 16 -51 -1 | 5 28
emr uuuuu | 41 11 84 189 12 | 14 35
esa uuuuu | -10 -23 20 -43 8 | 12 31
gfz uuuuu | -16 7 121 -26 2 | 3 30
grg uuuux | 14 9 20 -162 -35 | 15 45
igr xxxxx | -11 -20 -17 15 8 | 0 28
irf xxxxx | 0 4 -3 -29 1 | 4 28
jpl uuuuu | 29 2 77 118 -5 | 17 33
mit uuuuu | 25 -7 -126 -50 3 | 17 32
ngs uuuuu | -48 4 -147 39 -12 | 16 26
sio uuuuu | 27 79 59 20 0 | 39 48
Table 7.1698.1 GPS week: 1698 Day: 1 MJD: 56131.500
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 -74 31 -161 -3 | 10 28
emr uuuuu | 22 27 -180 134 -7 | 24 35
esa uuuuu | -17 -21 34 -106 11 | 20 32
gfz uuuuu | 7 4 39 -14 -3 | 10 27
grg uuuux | 26 4 -98 -121 -1 | 23 38
igr xxxxx | -17 -10 -30 -73 -3 | 8 25
irf xxxxx | 6 -17 28 -8 1 | 11 26
jpl uuuuu | -27 25 50 92 -2 | 24 33
mit uuuuu | 32 -50 -34 11 3 | 22 34
ngs uuuuu | -31 24 -1 33 -2 | 20 26
sio uuuuu | 29 45 206 126 3 | 46 51
Table 7.1698.2 GPS week: 1698 Day: 2 MJD: 56132.500
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 -60 61 40 3 | 7 27
emr uuuuu | 7 -9 143 121 4 | 19 33
esa uuuuu | 10 -17 41 63 6 | 18 31
gfz uuuuu | 7 -1 146 -13 -3 | 8 27
grg uuuux | 3 17 -122 -118 -18 | 21 37
igr xxxxx | -12 -2 48 -46 -4 | 4 25
irf xxxxx | -2 2 -26 -4 5 | 8 26
jpl uuuuu | -33 -3 109 69 0 | 20 30
mit uuuuu | 21 -15 -155 -29 10 | 20 33
ngs uuuuu | -34 5 -180 -184 -12 | 17 25
sio uuuuu | 22 84 43 80 8 | 45 50
Table 7.1698.3 GPS week: 1698 Day: 3 MJD: 56133.500
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 -72 25 -126 10 | 6 26
emr uuuuu | 9 5 38 -46 9 | 21 33
esa uuuuu | -17 -28 -30 54 7 | 18 31
gfz uuuuu | 27 -14 170 -50 -2 | 8 27
grg uuuux | 24 25 -74 -93 -25 | 15 31
igr xxxxx | -41 -7 29 -40 6 | 3 24
irf xxxxx | 6 1 -13 23 1 | 8 26
jpl uuuuu | -29 -8 31 -8 4 | 19 30
mit uuuuu | 32 -18 -132 55 3 | 20 33
ngs uuuuu | -38 46 12 -109 -12 | 15 24
sio uuuuu | 39 72 65 152 1 | 47 52
Table 7.1698.4 GPS week: 1698 Day: 4 MJD: 56134.500
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 | -11 -10 56 3 3 | 11 26
emr uuuuu | 14 4 -43 -34 8 | 26 36
esa uuuuu | -2 -47 123 53 -1 | 24 33
gfz uuuuu | -2 -21 25 -131 -5 | 12 26
grg uuuux | 5 25 -20 -73 -51 | 15 30
igr xxxxx | -15 -3 45 -18 2 | 8 24
irf xxxxx | 8 7 28 -16 0 | 13 25
jpl uuuuu | -46 1 -19 49 1 | 23 32
mit uuuuu | 43 -3 -88 3 1 | 26 34
ngs uuuuu | -45 32 -69 31 -1 | 18 25
sio uuuuu | 52 104 80 17 3 | 51 55
Table 7.1698.5 GPS week: 1698 Day: 5 MJD: 56135.500
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 -42 -99 43 8 | 8 28
emr uuuuu | 39 36 -106 105 3 | 25 36
esa uuuuu | -26 -36 36 20 -1 | 22 33
gfz uuuuu | -39 5 67 -164 1 | 9 28
grg uuuux | 20 9 -59 33 -26 | 8 39
igr xxxxx | -25 -31 36 14 3 | 6 26
irf xxxxx | 2 6 -4 1 -1 | 10 27
jpl uuuuu | -35 12 121 30 -1 | 20 32
mit uuuuu | 32 -4 -110 -57 -4 | 23 34
ngs uuuuu | 2 -20 19 45 1 | 15 26
sio uuuuu | 49 110 37 97 2 | 48 54
Table 7.1698.6 GPS week: 1698 Day: 6 MJD: 56136.500
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 -28 -120 -156 3 | 5 23
emr uuuuu | -10 -6 212 -130 4 | 23 32
esa uuuuu | -27 -26 39 73 -3 | 19 29
gfz uuuuu | -46 39 -116 -235 -1 | 5 22
grg uuuux | 40 0 -83 -85 -8 | 6 39
igr xxxxx | -20 -5 10 -57 -8 | 3 21
irf xxxxx | -4 7 -51 -54 -5 | 7 22
jpl uuuuu | -19 -6 54 -12 13 | 17 26
mit uuuuu | 17 -13 -180 -83 -11 | 20 29
ngs uuuuu | 47 14 82 226 -1 | 12 21
sio uuuuu | 19 105 38 61 -5 | 45 49
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