[IGSREPORT-20692] Wk 1679 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Mar 29 06:02:50 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1679 (Mar 11, 2012 - Mar 17, 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:
igs1679[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1679[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1679[0-6].cls IGS GPS clock combination summary report.
igs16797.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16797.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because of poorer consistency (GRG),
they provide broadcast clocks (NGS), or clock corrections are not provided
(SIO). The clock information not used is still compared to combination for
completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | EMR | 4 8 9 27 4 8 9 27
0 | ESA | UNSA
0 | GFZ | 1 2 5 21 30 32 ASPA BRFT DAV1 DGAR KARR KERG PDEL
0 | GFZ | RESO RIO2 YSSK
0 | GRG | UNSA USN3
0 | JPL | 4 8 9 27
0 | MIT | 4 9 11 27 4 9 11 27 CAS1 DAV1 CAS1 DAV1
1 | COD | NRIL TIXI YELL
1 | EMR | 4 8 9 27 30 4 8 9 27 30 MCM4 WHIT MCM4 WHIT
1 | ESA | NNOR TIXI UNSA
1 | GFZ | 1 2 4 21 AUCK BRFT DAV1 OHI2 RIO2 STJO TIXI YELL
1 | GRG | USN3
1 | JPL | 4 8 27
1 | MIT | 4 9 27 30 4 9 27 30 CAS1 DAV1 MAC1 CAS1 DAV1 MAC1
1 | MIT | STJO
2 | COD | BRST WES2 BRST XMIS
2 | EMR | 4 8 9 27 4 8 9 27 MCM4 MCM4
2 | ESA | NNOR
2 | GFZ | 1 2 4 21 27 RIO2 YELL
2 | GRG | KIT3 USN3
2 | JPL | 4 8 27 MCM4
2 | MIT | 4 9 27 4 9 CONZ
3 | COD | XMIS
3 | EMR | 8 9 8 9
3 | GFZ | 1 2 4 21 27 CHUR RIO2
3 | GRG | USN3
3 | JPL | 4 8 9
3 | MIT | 4 9 4 9 CAS1
4 | COD | 9 KOUC KOUC WILL
4 | EMR | 8 27 30 8 27 30 SYOG SYOG YELL
4 | ESA | 9 KIRU NNOR UNSA
4 | GFZ | 1 2 4 9 21 27 DAV1
4 | GRG | USN3
4 | JPL | 4 8 9 30
4 | MIT | 4 8 18 21 27 30 4 8 18 21 27 CAS1 SYOG CAS1 NRIL
4 | MIT | SYOG
5 | COD | KOUC KOUC YELL
5 | EMR | 9 27 9 27 MATE
5 | ESA | UNSA
5 | GFZ | 1 2 4 9 21 27 DAV1 FAIR HRAO
5 | GRG | ADIS FAIR NRC1
5 | JPL | 4 9 27 TIXI
5 | MIT | 4 9 27 4 9 27 CAS1 CAS1
6 | COD | 2 2 KOUC NTUS KOUC NTUS
6 | EMR | 4 8 9 27 4 8 9 27
6 | ESA | HYDE HYDE NNOR TIXI UNSA
6 | GFZ | 1 4 7 9 21 27 COCO FAIR KERG NTUS
6 | GRG | USN3
6 | JPL | 8
6 | MIT | 1 4 9 21 27 31 1 4 9 21 27 31 CAS1 CAS1 TIXI
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
4 | GRG | 4
4 | MIT | 4
6 | MIT | 1
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G01 | | | | | | | 2 |
PRN G04 | | | | | 4 | | |
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 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 | -.5 -.2 -1.1 -38 -3 16 .07
EMR | 5.7 -4.1 11.8 -4 7 2 .43
ESA | 1.7 -1.9 -4.8 49 -119 129 .06
GFZ | -1.5 .8 -.3 -45 33 -38 -.01
GRG | -1.8 -3.2 1.3 -42 48 -30 .08
JPL | .6 .7 15.6 -32 -7 14 .29
MIT | 5.7 -5.2 9.0 -50 39 -74 .23
NGS | 6.6 -6.6 4.4 -57 -38 51 .27
SIO | 4.4 -2.3 1.9 -76 -130 24 .25
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting 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 1.1679.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1679.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 2.1679.[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 3.1679.[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 5.1679.0-6).
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 1679 summary. (Mar 11, 2012 - Mar 17, 2012)
Table 1.1679.a GPS week: 1679 MJD: 55997.000-56003.000
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 256| 0 0 1 1 -21 24 -.30 9 8 | -541 -849 22 85
| 0 0 1 9 13 16 .06 | 933 2220
emr 99| 1 0 4 -24 -89 -46 .48 22 22 | 4126 -324 15 105
| 2 1 1 26 55 10 .07 | 1134 986
esa 127| 0 1 0 -112 130 51 .21 9 8 | -530 -19 14 127
| 0 0 1 7 18 15 .05 | 944 835
gfz 189| 0 -2 -2 32 -94 -35 -.13 14 12 | 47 -7 32 108
| 1 0 1 34 61 8 .26 | 352 716
grg 122| 0 0 0 12 -114 -31 .61 15 14 | -119 -19 49 211
| 1 1 2 11 12 12 .04 | 218 466
igr n/a| 0 0 -1 -41 -27 -16 -.03 5 5 | 17822 240 21 81
| 0 0 0 15 17 11 .06 | 2390 1134
jpl 175| 1 0 2 -3 -7 15 .53 18 18 | 2401 -291 20 85
| 0 2 2 15 25 51 .05 | 1094 942
mit 269| 0 0 -2 43 -106 -43 -.46 14 12 | -372 158 24 154
| 0 1 1 20 33 18 .03 | 235 478
ngs 223| 1 0 -1 75 35 -40 -.33 13 9 | 18573 -63620 2041 3623
| 0 1 0 16 34 18 .02 | 51100 167645
sio 232| -2 0 1 92 225 31 .03 22 21 | --- --- --- ---
| 0 0 1 18 23 15 .06 | --- ---
Table 1.1679.b GPS week : 1679 MJD: 55997.000-56003.000
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 | 6 6 5 6 6 7 19 |
2 | 5 5 5 5 5 6 5 |
3 | 4 5 5 3 4 4 4 |
4 | 6 6 7 7 16 6 6 |
5 | 5 5 5 5 5 5 5 |
6 | 4 5 4 4 4 4 4 |
7 | 4 4 4 4 4 4 5 |
8 | 6 7 6 6 7 6 7 |
9 | 7 7 7 6 6 6 6 |
10 | 4 4 4 4 4 4 4 |
11 | 5 4 4 4 4 4 6 |
12 | 5 6 5 5 5 5 5 |
13 | 5 5 4 4 5 4 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 4 5 5 5 |
18 | 6 5 5 5 5 6 5 |
19 | 5 6 5 5 5 5 5 |
20 | 5 5 5 4 5 5 6 |
21 | 4 4 4 4 5 6 5 |
22 | 5 5 5 6 5 5 6 |
23 | 5 5 4 5 5 4 5 |
24 | 0 0 0 0 0 0 0 |
25 | 5 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 7 8 8 7 6 8 6 |
28 | 5 5 5 5 5 5 5 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 3 4 3 4 |
31 | 5 5 5 5 5 5 5 |
32 | 6 6 5 4 5 5 6 |
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 2.1679.0 GPS week: 1679 Day: 0 MJD: 55997.000
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 256| 0 0 -1 -9 -22 4 -.42 9 9 | -563 -426 26 96
| 41 -29 |
emr 99| 0 3 4 16 -119 -35 .37 20 20 | 2612 819 12 112
| -64 61 |
esa 127| 0 1 0 -101 134 52 .11 9 9 | 148 -596 13 132
| 25 35 |
gfz 189| 0 -2 -1 -13 -75 -42 .45 15 14 | -455 940 34 108
| -49 13 |
grg 122| 0 0 -2 19 -109 -34 .52 17 16 | -410 918 51 210
| 1 7 |
igr n/a| 1 -1 0 -25 -36 -19 -.10 5 5 | 13961 1906 21 77
| -32 42 |
jpl 175| 0 0 4 0 17 98 .44 16 16 | 744 978 19 84
| 67 -43 |
mit 269| 0 -1 -3 37 -117 -57 -.47 14 11 | -678 697 24 166
| 3 25 |
ngs 223| 0 -1 0 75 -3 -67 -.33 14 9 | -624 -416 1925 3794
| -35 69 |
sio 232| -1 -1 3 108 214 14 -.03 22 19 | --- --- --- ---
| -113 -166 |
Table 2.1679.1 GPS week: 1679 Day: 1 MJD: 55998.000
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 256| -1 0 1 -7 -50 40 -.31 10 9 | -543 -60 21 77
| 69 36 |
emr 99| 2 -1 6 -9 -134 -37 .52 22 22 | 3000 -283 15 102
| -61 46 |
esa 127| 0 0 0 -122 129 78 .24 9 8 | -1375 695 13 113
| 2 8 |
gfz 189| 0 -1 -3 66 20 -28 -.22 15 13 | 291 -1010 34 105
| -52 -9 |
grg 122| 0 1 0 -5 -113 -45 .62 16 15 | -338 -34 62 214
| 4 8 |
igr n/a| 0 0 -1 -51 -55 0 .01 6 6 | 15644 468 27 90
| 7 39 |
jpl 175| 1 -1 3 -17 -13 -39 .50 18 18 | 1477 -359 22 78
| -10 40 |
mit 269| 0 0 -2 57 -74 -71 -.43 15 12 | -263 -22 24 131
| 14 24 |
ngs 223| 1 -2 -3 72 -19 -51 -.30 13 8 | -452 -248 2155 3565
| 11 81 |
sio 232| -2 -1 2 119 251 27 .06 23 22 | --- --- --- ---
| -94 -172 |
Table 2.1679.2 GPS week: 1679 Day: 2 MJD: 55999.000
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 256| 0 0 1 -2 -19 47 -.29 10 9 | -450 -249 18 81
| 57 -15 |
emr 99| 4 0 4 -6 -71 -35 .47 22 22 | 3532 584 17 111
| -38 12 |
esa 127| -1 2 0 -110 156 46 .19 9 9 | 331 -376 14 130
| 22 21 |
gfz 189| 0 -1 -2 72 -134 -35 -.22 14 12 | -267 637 33 108
| -62 -6 |
grg 122| 0 1 2 11 -110 -7 .63 16 15 | 56 -437 49 220
| -4 -37 |
igr n/a| 1 0 -1 -53 2 -21 -.03 5 5 | 16991 975 21 84
| -10 -4 |
jpl 175| 2 0 3 -7 13 9 .54 17 17 | 1952 280 21 104
| -11 -3 |
mit 269| 0 0 -3 31 -168 -57 -.41 14 11 | 0 -368 27 161
| 9 60 |
ngs 223| 0 -1 -1 60 76 -58 -.31 12 9 | -555 -157 1839 3809
| -51 -13 |
sio 232| -3 0 0 79 186 16 .00 21 22 | --- --- --- ---
| -89 -138 |
Table 2.1679.3 GPS week: 1679 Day: 3 MJD: 56000.000
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 256| -1 0 0 14 -22 13 -.28 9 9 | -65 -1187 20 91
| 41 4 |
emr 99| 2 -1 4 -57 1 -56 .48 21 21 | 4451 221 13 96
| 2 -22 |
esa 127| 0 0 0 -106 148 39 .24 8 8 | -1990 1001 15 147
| 14 23 |
gfz 189| -1 -2 0 4 -173 -21 -.23 13 12 | -153 -319 31 105
| -61 44 |
grg 122| 1 1 -1 30 -125 -33 .61 14 13 | 18 -453 43 203
| -33 -24 |
igr n/a| 0 0 0 -18 -32 -6 .03 5 5 | 18324 593 20 71
| -36 37 |
jpl 175| 2 0 3 15 -3 -9 .53 17 17 | 2580 137 19 85
| 1 46 |
mit 269| 0 0 -2 17 -126 -33 -.48 13 11 | -301 -92 22 130
| 7 49 |
ngs 223| 1 0 0 104 60 -23 -.34 12 9 | -134 -1250 2407 3759
| 14 -11 |
sio 232| -2 0 1 73 213 52 -.04 20 20 | --- --- --- ---
| -96 -131 |
Table 2.1679.4 GPS week: 1679 Day: 4 MJD: 56001.000
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 256| -1 0 2 14 -10 30 -.26 8 7 | -1892 1946 20 84
| 59 -33 |
emr 99| 2 -2 3 -44 -125 -56 .54 23 23 | 5634 -554 17 87
| 1 70 |
esa 127| 0 1 0 -109 107 49 .25 8 8 | 502 -321 16 125
| 20 16 |
gfz 189| -3 -2 -1 0 -76 -47 -.20 14 13 | 378 -615 32 115
| -17 4 |
grg 122| 0 0 0 11 -115 -34 .64 15 14 | -291 152 48 215
| 7 -14 |
igr n/a| 0 0 -1 -34 -28 -9 .04 5 5 | 19941 -64 19 86
| -6 26 |
jpl 175| 1 -1 1 -2 -47 -20 .59 19 19 | 3718 -352 19 71
| 34 -2 |
mit 269| 1 0 -2 49 -91 -36 -.49 14 13 | -660 796 25 182
| -17 8 |
ngs 223| 1 0 -2 66 34 -21 -.32 11 8 | -1654 1510 1940 3605
| -1 5 |
sio 232| 0 0 0 80 224 18 .02 21 21 | --- --- --- ---
| -98 -146 |
Table 2.1679.5 GPS week: 1679 Day: 5 MJD: 56002.000
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 256| -2 0 2 0 -6 6 -.25 9 8 | 1054 -5369 25 84
| 56 -12 |
emr 99| 3 0 3 -21 -140 -58 .42 25 25 | 5299 -2008 17 114
| -17 94 |
esa 127| 0 1 0 -118 110 61 .21 8 8 | -339 -1260 13 115
| 50 15 |
gfz 189| -2 0 -2 40 -97 -36 -.22 13 11 | 57 -190 30 112
| -24 -16 |
grg 122| 0 0 -1 6 -93 -40 .66 14 13 | 13 -203 40 173
| 16 -43 |
igr n/a| 0 0 -1 -49 -20 -23 -.05 5 5 | 20225 -1627 18 74
| 16 17 |
jpl 175| 2 -4 0 13 -33 -3 .56 19 19 | 3635 -2038 19 72
| 32 29 |
mit 269| 1 -2 0 33 -90 -23 -.48 14 12 | -376 -326 22 150
| 10 28 |
ngs 223| 0 1 -1 87 57 -28 -.37 13 9 | 134453 -443800 1981 3092
| -87 22 |
sio 232| -2 0 1 76 242 42 .04 23 23 | --- --- --- ---
| -105 -163 |
Table 2.1679.6 GPS week: 1679 Day: 6 MJD: 56003.000
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 256| 0 0 0 0 -17 29 -.29 10 9 | -1333 -604 24 83
| 61 20 |
emr 99| -3 0 5 -49 -35 -42 .55 23 23 | 4355 -1049 19 117
| -48 -2 |
esa 127| -2 2 1 -118 125 30 .23 9 9 | -987 718 20 130
| 41 23 |
gfz 189| 0 -3 -1 53 -124 -36 -.26 12 11 | 478 503 30 109
| -27 26 |
grg 122| 0 -1 4 16 -132 -20 .61 14 14 | 118 -81 52 244
| 13 4 |
igr n/a| 0 0 -1 -58 -21 -33 -.10 6 6 | 19671 -571 23 87
| -8 21 |
jpl 175| 2 3 -1 -28 14 74 .54 19 19 | 2703 -684 23 106
| 69 -27 |
mit 269| 1 0 -2 79 -76 -23 -.47 15 12 | -327 423 26 162
| -11 38 |
ngs 223| 2 -1 -1 57 38 -31 -.36 14 9 | -1022 -981 2042 3743
| -23 52 |
sio 232| -1 0 0 106 249 45 .15 22 21 | --- --- --- ---
| -124 -162 |
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 3.1679.0 GPS week: 1679 Day: 0 MJD: 55997.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 24 15 13 13 6 14 25 14 20 5 | 39 48 46 46 45 38 47 43 28 32 39
2E | 10 22 9 17 24 5 16 15 10 13 5 | 24 30 23 28 27 24 26 27 24 24 24
3 | 8 17 7 11 12 5 11 13 12 20 4 | 18 22 20 23 23 19 21 23 23 28 19
4E | 12 19 12 15 21 8 16 18 21 23 6 | 84 38 86 87 93 81 89 88 80 82 84
5 | 8 17 7 21 16 6 20 10 11 24 5 | 29 35 28 33 36 30 34 33 34 34 30
6 | 9 16 7 8 12 5 9 11 10 23 4 | 20 23 22 22 22 20 26 26 21 32 21
7E | 6 16 7 12 15 6 14 10 11 12 3 | 27 30 29 27 26 26 29 24 30 24 26
8E | 14 21 9 12 25 7 19 16 27 16 6 | 23 28 24 26 32 23 31 25 39 21 24
9E | 13 21 8 10 28 6 20 13 34 15 6 | 56 61 60 65 63 56 61 53 69 58 57
10 | 7 16 7 15 19 5 12 10 8 16 4 | 31 26 33 40 36 30 25 35 33 28 31
11E | 11 17 13 13 13 5 12 16 15 13 4 | 26 37 40 38 39 29 37 30 27 28 31
12 | 10 23 8 15 19 6 18 11 8 29 5 | 20 32 25 30 31 22 28 26 22 23 22
13 | 7 19 8 13 19 5 15 12 11 16 4 | 21 31 27 28 39 22 32 27 27 25 25
14 | 7 23 8 17 18 6 15 17 10 25 5 | 20 24 23 35 34 21 25 26 23 23 22
15 | 8 20 9 12 19 4 20 13 10 29 5 | 21 31 24 32 39 21 28 22 23 20 22
16 | 7 31 8 11 13 6 22 11 9 25 5 | 24 34 26 24 33 20 32 30 24 29 25
17 | 10 21 10 16 14 5 19 15 9 23 5 | 28 30 18 22 18 21 28 30 24 22 21
18 | 9 22 8 19 17 5 20 9 13 33 5 | 26 34 25 36 28 23 31 26 26 30 24
19 | 8 25 7 16 15 5 17 13 11 24 5 | 23 33 21 22 24 18 30 25 19 30 21
20 | 6 22 8 16 15 6 18 11 11 25 4 | 23 33 27 34 29 24 32 27 27 24 25
21E | 8 19 9 12 18 4 12 11 13 14 4 | 17 20 19 22 23 15 22 20 17 22 17
22 | 8 21 11 10 14 5 15 12 12 38 5 | 29 32 30 30 32 29 30 32 31 41 28
23 | 10 23 8 13 14 4 16 9 13 24 4 | 20 27 27 29 33 21 27 24 22 20 23
X24 | 6 --- --- --- --- 23 --- --- --- --- 0 | 20 --- --- --- --- 28 --- --- --- --- 20
25 | 10 19 8 16 15 6 17 11 11 19 4 | 20 27 28 27 35 23 35 27 23 27 25
26 | 10 8 6 12 12 7 12 9 7 18 3 | 20 17 18 24 27 16 16 21 19 16 18
27E | 12 20 12 14 19 5 17 33 22 15 6 | 47 46 44 49 48 42 45 61 50 44 45
28 | 10 18 6 18 18 4 18 12 6 27 5 | 21 31 25 31 32 21 27 27 21 25 23
29 | 9 26 7 14 13 6 18 11 8 24 4 | 25 33 21 19 23 22 31 29 26 26 23
30 | 8 14 8 12 12 4 12 12 9 14 3 | 15 17 16 16 20 13 22 20 18 21 16
31E | 8 20 8 16 15 4 17 11 15 14 4 | 28 29 30 29 29 27 30 26 32 29 27
32 | 10 21 9 23 14 5 20 11 12 28 5 | 24 27 29 41 32 25 30 33 28 33 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 9 15 17 5 16 14 14 22 |T 27 31 29 32 33 26 32 31 29 29 27
WRMS | 9 20 9 14 16 5 16 11 9 19 |NE 22 28 24 28 29 22 28 27 24 26 23
MEDI | 9 20 8 14 15 5 17 12 11 23 |MD 23 31 26 29 32 23 30 27 26 27 24
Table 3.1679.1 GPS week: 1679 Day: 1 MJD: 55998.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 24 14 15 13 6 14 23 15 21 5 | 36 43 35 35 40 35 38 46 26 35 34
2E | 8 26 7 12 21 6 16 12 10 17 4 | 21 31 24 22 23 20 21 19 22 21 20
3 | 10 24 8 12 13 6 15 12 11 20 4 | 16 24 18 15 20 14 17 19 13 26 13
4E | 12 22 9 17 23 7 21 24 20 18 6 | 72 36 74 73 78 74 80 73 76 72 73
5 | 10 20 6 19 13 7 23 8 9 19 4 | 25 34 26 29 32 26 30 26 27 31 25
6 | 10 20 8 11 12 6 15 14 14 25 4 | 17 25 19 15 20 15 19 21 14 31 15
7E | 6 21 8 10 17 4 13 9 7 16 4 | 20 29 20 22 26 18 24 20 22 23 20
8E | 15 26 10 13 27 7 21 19 26 20 6 | 17 29 18 16 31 16 28 21 30 21 16
9E | 15 20 11 11 24 6 20 18 28 22 6 | 52 59 54 52 55 51 59 53 59 54 52
10 | 7 18 5 15 17 4 13 14 7 16 4 | 27 28 26 33 31 26 23 26 26 24 25
11E | 6 16 7 13 15 6 12 14 11 18 4 | 24 36 28 27 32 26 30 29 29 28 26
12 | 12 22 11 13 18 7 20 16 12 35 5 | 20 34 25 25 31 23 31 22 22 21 21
13 | 7 23 8 12 17 7 17 11 9 16 4 | 20 34 23 19 35 21 31 22 23 23 21
14 | 7 26 8 15 12 5 17 16 9 24 4 | 20 30 21 24 28 21 23 23 23 21 20
15 | 8 22 11 11 16 7 21 12 8 24 4 | 23 36 26 22 35 25 32 22 26 23 24
16 | 9 32 9 10 13 4 22 13 10 26 5 | 14 30 19 20 20 17 24 19 20 19 15
17 | 9 21 9 17 13 6 20 15 11 27 5 | 26 31 19 28 17 22 27 26 25 19 21
18 | 9 23 9 15 14 7 19 9 11 31 5 | 19 29 22 24 25 21 26 19 20 21 18
19 | 8 30 11 15 13 5 20 15 14 26 5 | 17 35 16 20 20 16 25 18 21 24 15
20 | 7 22 8 19 14 5 18 10 10 25 4 | 20 33 23 28 27 22 26 24 21 26 21
21E | 5 17 6 12 14 4 14 13 10 15 4 | 19 27 20 17 24 19 24 22 22 20 19
22 | 7 24 10 9 13 5 17 15 13 37 5 | 25 27 27 23 29 25 24 25 30 33 23
23 | 8 23 7 12 15 5 16 11 10 23 4 | 23 34 26 24 31 24 30 26 26 23 24
X24 | 6 --- --- --- --- 92 --- --- --- --- 0 | 14 --- --- --- --- 52 --- --- --- --- 12
25 | 8 16 8 14 14 5 17 10 8 24 4 | 16 32 25 22 32 21 33 22 19 23 21
26 | 11 13 5 9 14 7 17 8 12 22 4 | 20 19 16 16 21 15 20 17 17 15 15
27E | 19 20 12 17 21 9 25 36 22 22 7 | 34 35 33 33 39 32 37 49 38 34 31
28 | 10 21 8 17 14 5 18 9 10 29 5 | 18 30 21 24 29 20 26 24 19 21 19
29 | 11 25 7 12 13 5 18 12 10 26 4 | 26 34 22 22 23 23 30 24 25 22 22
30 | 8 15 9 12 11 4 11 14 9 22 4 | 14 23 14 16 18 12 19 19 16 18 13
31E | 8 21 10 14 16 5 17 17 14 18 5 | 30 33 30 32 34 28 33 35 30 34 30
32 | 8 21 8 30 12 5 16 13 11 22 5 | 26 32 27 40 28 27 31 33 28 36 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 22 9 15 16 6 18 15 13 23 |T 24 32 25 26 30 25 29 27 26 27 23
WRMS | 9 22 8 13 15 6 18 12 8 22 |NE 20 30 21 23 26 22 26 22 21 23 19
MEDI | 8 22 8 13 14 6 17 13 11 22 |MD 20 32 23 24 29 22 27 23 23 23 21
Table 3.1679.2 GPS week: 1679 Day: 2 MJD: 55999.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 12 27 12 17 10 5 13 20 11 14 5 | 31 40 40 40 41 33 38 42 27 25 34
2E | 10 21 8 11 15 7 16 16 10 19 4 | 15 21 16 18 15 13 17 17 15 15 12
3 | 9 18 7 11 13 3 20 12 11 19 4 | 13 17 16 14 20 13 17 14 16 24 12
4E | 16 25 13 15 23 9 20 26 23 26 7 | 82 39 85 82 83 80 89 82 84 84 82
5 | 8 22 13 19 13 5 22 8 9 23 5 | 20 31 21 27 25 19 29 25 23 24 20
6 | 9 19 5 10 10 4 14 12 9 24 4 | 16 17 15 15 18 12 16 17 16 28 14
7E | 7 22 9 10 14 5 14 5 10 11 3 | 18 30 20 16 22 16 24 15 21 22 17
8E | 16 23 12 16 20 5 21 13 27 14 6 | 20 28 19 21 25 18 30 18 35 16 19
9E | 17 21 12 11 24 6 22 24 26 20 7 | 50 53 49 48 51 47 53 57 59 51 50
10 | 7 14 8 12 16 5 13 14 7 19 4 | 24 21 22 30 25 24 22 30 27 26 24
11E | 8 14 4 12 13 4 11 11 11 23 4 | 18 29 22 21 29 20 26 24 26 21 20
12 | 10 23 9 13 16 6 16 13 10 29 5 | 19 34 26 21 29 21 28 23 24 20 22
13 | 5 20 9 12 16 6 13 9 6 17 4 | 15 29 19 18 33 15 28 19 14 18 16
14 | 8 25 7 14 16 4 16 13 14 23 5 | 18 30 27 25 30 22 26 26 24 17 22
15 | 10 19 10 13 19 5 21 12 8 23 5 | 14 29 22 24 32 19 27 20 21 13 19
16 | 9 28 7 8 12 5 22 11 7 24 4 | 20 28 22 18 24 20 27 22 23 22 19
17 | 10 22 8 17 14 5 17 14 11 25 5 | 24 25 14 26 15 18 20 23 21 16 16
18 | 8 22 7 22 16 4 20 8 9 20 5 | 23 29 21 32 25 20 28 21 21 22 21
19 | 12 25 11 14 11 5 20 13 12 21 5 | 17 28 15 16 15 12 25 14 17 21 13
20 | 7 22 10 14 11 4 14 10 9 24 4 | 16 29 17 21 23 15 26 18 18 19 16
21E | 8 24 8 11 20 4 14 11 8 10 4 | 17 23 19 12 31 16 22 16 17 16 16
22 | 8 21 8 11 16 5 16 10 11 31 4 | 23 25 25 27 27 25 23 27 26 35 23
23 | 7 24 6 11 13 4 16 9 7 21 4 | 13 25 17 18 25 13 24 18 14 14 14
X24 | 5 --- --- --- --- 56 --- --- --- --- 0 | 19 --- --- --- --- 20 --- --- --- --- 16
25 | 9 15 6 11 15 4 14 8 11 22 4 | 23 28 27 20 33 22 32 21 25 21 22
26 | 11 13 6 11 16 6 17 8 9 17 4 | 15 19 15 18 21 12 18 16 17 16 13
27E | 14 25 12 15 18 8 24 37 20 22 7 | 22 26 23 23 24 24 27 47 25 25 21
28 | 12 21 8 15 16 5 15 8 12 24 4 | 14 29 20 24 31 17 24 20 15 19 16
29 | 8 26 5 11 13 5 19 7 11 25 4 | 23 33 19 26 21 20 26 27 20 25 20
30 | 6 14 8 7 15 4 13 10 10 17 3 | 12 19 17 11 19 10 20 16 16 17 13
31E | 7 24 6 12 14 4 16 11 8 25 4 | 19 27 27 18 29 20 29 21 16 24 21
32 | 9 20 9 22 13 5 14 10 8 20 4 | 18 21 26 26 27 20 28 20 17 20 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 22 9 14 16 5 17 14 12 21 |T 21 27 23 24 28 21 28 25 23 23 21
WRMS | 9 22 9 12 15 5 17 11 9 22 |NE 18 26 20 21 24 17 24 20 19 20 17
MEDI | 9 22 8 12 15 5 16 11 10 22 |MD 18 28 21 21 25 19 26 21 21 21 19
Table 3.1679.3 GPS week: 1679 Day: 3 MJD: 56000.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 14 28 13 22 13 4 13 23 14 16 6 | 44 46 46 49 46 41 44 54 28 39 42
2E | 8 25 5 10 20 4 18 16 10 16 4 | 18 24 19 16 21 17 20 26 23 22 18
3 | 6 15 5 6 11 4 10 10 9 20 3 | 15 21 19 18 18 16 23 21 22 28 17
X4E | 20 --- 11 14 19 8 17 24 22 23 7 | 71 --- 68 69 77 68 77 76 67 70 70
5 | 7 19 7 16 13 7 21 10 6 20 4 | 30 35 33 31 36 30 32 32 31 29 30
6 | 8 15 5 6 11 4 11 11 10 25 3 | 16 19 20 19 21 17 23 24 23 32 19
7E | 6 22 7 11 14 5 15 8 9 12 3 | 25 31 30 25 25 24 31 26 30 27 26
8E | 14 25 9 12 16 5 19 12 30 15 6 | 20 29 24 22 25 20 30 23 36 20 21
9E | 10 25 9 10 17 4 24 22 24 18 6 | 29 40 36 39 39 31 39 34 40 33 32
10 | 9 17 5 9 14 4 10 7 11 13 3 | 29 31 33 38 38 31 28 35 34 35 32
11E | 9 17 5 10 12 6 11 9 9 17 3 | 27 35 31 26 38 28 33 30 33 28 29
12 | 12 22 10 16 13 5 19 14 11 27 5 | 17 33 27 31 33 21 28 23 19 20 21
13 | 6 21 7 12 19 3 19 9 8 18 4 | 23 33 25 26 39 23 34 24 24 26 24
14 | 8 23 8 14 13 6 17 11 9 21 4 | 22 30 28 29 33 26 28 27 24 23 24
15 | 12 21 10 11 19 5 19 12 11 20 5 | 19 31 25 22 36 20 31 23 26 19 21
16 | 9 27 8 8 13 3 21 10 9 24 4 | 16 29 20 20 25 18 28 23 24 20 18
17 | 9 19 7 14 11 6 17 7 10 25 4 | 28 28 23 28 21 23 27 27 30 24 23
18 | 10 23 7 20 13 3 19 9 9 18 4 | 24 33 28 33 30 26 31 27 30 24 26
19 | 6 23 10 10 12 4 18 12 9 20 4 | 19 31 19 19 22 17 28 19 23 18 18
20 | 8 22 7 10 11 5 18 13 9 23 4 | 22 33 27 27 29 25 32 24 27 29 24
21E | 7 21 8 10 14 3 14 9 9 11 3 | 16 25 22 22 23 20 24 21 17 22 19
22 | 7 21 9 29 12 3 17 12 10 30 5 | 28 31 30 35 30 28 29 33 33 38 27
23 | 7 28 8 10 14 3 20 9 10 23 4 | 22 36 25 25 28 22 31 25 24 22 23
X24 | 4 --- --- --- --- 33 --- --- --- --- 0 | 22 --- --- --- --- 1 --- --- --- --- 22
25 | 8 19 8 13 13 4 19 10 9 18 4 | 19 32 30 29 38 24 32 25 24 23 25
26 | 11 13 4 14 13 7 13 10 9 18 4 | 21 19 18 22 23 18 19 25 24 20 19
27E | 14 28 11 14 19 7 22 34 20 22 7 | 24 32 26 28 29 25 28 48 35 28 25
28 | 10 19 6 11 14 5 16 9 13 23 4 | 21 31 26 29 29 23 29 28 30 24 24
29 | 8 22 7 13 15 6 18 9 10 25 4 | 30 37 30 34 28 29 40 31 31 32 30
30 | 6 14 5 10 11 4 9 8 8 14 3 | 17 24 21 22 21 17 24 20 22 23 19
31E | 7 22 6 12 18 3 13 12 12 25 4 | 31 38 35 35 28 32 34 31 35 37 32
32 | 11 18 6 11 12 5 14 9 8 20 4 | 24 30 29 41 34 28 30 32 30 35 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 21 8 13 14 5 17 13 12 20 |T 24 30 28 29 31 24 31 29 29 28 25
WRMS | 9 21 8 12 13 5 17 11 9 20 |NE 22 29 25 27 29 21 28 26 26 25 23
MEDI | 8 21 7 11 13 4 17 10 10 20 |MD 22 31 27 28 29 23 30 26 28 26 24
Table 3.1679.4 GPS week: 1679 Day: 4 MJD: 56001.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 14 30 13 21 21 5 17 10 9 20 5 | 45 58 50 46 53 45 52 53 26 43 45
2E | 7 24 8 8 17 5 21 19 10 15 4 | 16 26 21 19 27 17 22 25 21 20 17
3 | 7 18 7 13 11 4 13 12 9 19 4 | 15 20 19 21 20 16 20 19 13 29 16
X4E | 23 --- 20 20 92 23 48 110 63 27 16 | 94 --- 100 96 121 97 106 129 107 103 95
5 | 7 22 13 12 12 8 22 15 12 25 5 | 26 30 25 29 31 22 29 27 27 25 24
6 | 8 21 7 12 10 3 16 12 7 24 4 | 14 16 18 22 18 15 19 19 13 30 15
7E | 7 22 9 10 15 6 15 9 10 14 4 | 21 26 19 20 26 17 24 20 20 22 19
8E | 14 24 10 10 18 5 21 17 30 19 6 | 19 32 21 19 25 18 31 23 32 21 18
9E | 13 24 8 12 15 6 30 16 18 15 5 | 20 30 19 19 24 15 34 23 26 18 17
10 | 7 17 6 13 15 7 16 16 10 17 4 | 21 24 24 30 30 23 23 36 28 26 23
11E | 8 15 8 15 13 6 13 18 8 18 4 | 24 32 25 21 30 23 32 31 25 26 24
12 | 8 26 7 11 16 4 18 15 9 29 5 | 17 34 24 31 33 22 30 23 22 19 21
13 | 6 22 8 14 19 4 18 8 11 19 4 | 20 35 24 24 35 21 34 21 26 22 22
14 | 7 24 7 16 15 4 16 13 8 20 4 | 19 27 22 27 28 21 26 22 21 24 20
15 | 9 22 8 12 14 5 20 12 7 20 4 | 15 33 20 21 31 19 29 16 17 18 17
16 | 9 34 8 14 11 4 23 12 8 25 5 | 24 32 25 31 30 24 31 26 24 25 23
17 | 6 23 9 13 12 7 21 10 10 25 4 | 22 29 18 24 14 18 25 24 23 24 18
18 | 8 26 7 23 11 4 18 12 11 21 5 | 20 33 23 30 25 20 25 20 21 18 19
19 | 4 28 11 13 11 5 22 13 8 17 4 | 18 35 19 17 21 16 31 16 21 19 16
20 | 8 22 11 12 13 6 20 21 10 25 5 | 23 28 23 26 29 21 29 27 21 24 21
21E | 6 24 8 14 34 5 13 10 9 13 5 | 14 24 18 16 38 14 19 14 16 19 14
22 | 9 26 6 12 12 6 19 14 8 29 4 | 26 30 26 26 28 28 25 30 32 34 25
23 | 4 22 7 9 15 5 22 8 12 24 4 | 18 30 22 19 29 19 31 19 22 17 19
X24 | 4 --- --- --- --- --- --- --- --- --- 0 | 33 --- --- --- --- --- --- --- --- --- 35
25 | 5 24 6 10 13 5 16 11 6 17 3 | 21 30 26 26 35 25 33 26 22 22 23
26 | 7 22 5 13 11 8 13 12 7 19 3 | 15 25 19 20 23 18 18 21 17 16 16
27E | 12 20 8 15 17 7 23 27 16 21 6 | 26 32 23 32 28 23 31 39 26 29 24
28 | 8 22 6 11 15 6 18 13 12 22 4 | 21 31 21 24 30 21 27 29 27 25 22
29 | 7 27 8 14 14 4 23 14 11 27 5 | 23 34 18 24 19 22 29 27 27 24 21
30 | 7 16 6 9 11 6 16 10 9 13 3 | 11 20 14 15 17 13 20 15 18 19 12
31E | 6 26 6 12 16 5 16 9 11 26 4 | 24 33 25 22 25 23 32 26 29 34 25
32 | 8 18 9 26 13 5 18 9 11 22 5 | 22 25 25 33 27 23 30 28 25 31 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 23 8 14 15 5 19 14 11 21 |T 23 29 25 26 30 23 30 28 25 26 23
WRMS | 7 23 8 13 14 5 19 13 8 21 |NE 20 28 21 24 26 20 26 23 22 23 20
MEDI | 7 22 8 13 14 5 18 12 10 20 |MD 21 30 22 24 28 21 29 24 23 24 21
Table 3.1679.5 GPS week: 1679 Day: 5 MJD: 56002.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 19 27 14 20 21 4 20 17 12 28 6 | 55 53 56 53 56 50 51 90 55 45 50
2E | 8 21 9 10 18 5 22 21 15 16 5 | 13 21 21 17 19 12 17 21 19 17 14
3 | 10 15 6 14 15 4 14 10 9 19 4 | 12 20 18 20 22 14 21 17 17 26 15
X4E | 10 --- 11 15 17 22 20 21 21 24 6 | 84 --- 96 89 100 89 99 101 87 94 91
5 | 7 22 7 14 13 6 26 15 15 25 5 | 27 31 22 28 28 25 29 27 28 28 24
6 | 8 18 7 14 11 4 17 11 8 23 4 | 12 19 15 20 19 14 21 18 16 29 14
7E | 9 22 5 9 14 5 16 8 7 14 3 | 23 25 19 19 27 20 24 22 25 24 21
8E | 14 25 9 15 15 7 19 16 29 18 6 | 16 31 19 21 25 15 27 20 28 19 15
9E | 14 25 14 12 11 7 25 17 25 15 6 | 32 43 36 33 33 32 45 35 45 39 33
10 | 8 17 5 10 15 6 14 14 9 21 4 | 23 23 26 27 28 23 25 30 24 29 25
11E | 7 18 6 11 12 5 14 13 9 17 4 | 18 31 23 19 25 19 27 24 18 24 20
12 | 11 22 10 11 16 7 17 12 10 26 5 | 14 32 23 23 30 19 27 21 22 18 19
13 | 5 23 8 12 17 5 16 8 12 19 4 | 17 35 21 19 33 17 32 19 18 17 19
14 | 8 27 7 16 11 5 15 14 10 20 4 | 15 28 20 26 25 18 25 21 17 20 17
15 | 10 29 12 15 14 8 21 11 12 21 5 | 17 32 21 23 28 18 27 15 19 19 17
16 | 8 32 7 13 10 5 27 9 10 25 5 | 14 31 14 18 19 14 26 16 15 15 13
17 | 8 20 8 12 12 4 22 13 10 31 5 | 19 23 13 21 12 16 21 24 18 25 14
18 | 9 30 8 22 12 5 20 17 14 26 5 | 15 31 18 27 22 16 25 21 18 22 15
19 | 8 28 10 12 9 5 20 12 10 16 4 | 13 29 14 15 18 12 26 17 15 16 12
20 | 9 26 9 11 13 4 20 14 8 28 5 | 15 30 22 20 25 16 26 24 15 25 17
21E | 7 25 7 15 13 7 18 23 14 28 5 | 14 25 17 20 28 15 22 30 18 31 16
22 | 7 26 8 10 14 5 17 16 7 31 5 | 18 27 21 26 26 21 21 25 26 36 19
23 | 6 22 7 11 14 4 19 9 8 26 4 | 16 29 21 17 27 17 28 21 14 18 17
X24 | 4 --- --- --- --- --- --- --- --- --- 0 | 21 --- --- --- --- --- --- --- --- --- 22
25 | 6 18 8 9 15 5 16 11 10 19 4 | 16 27 25 20 32 20 32 21 22 17 20
26 | 8 20 4 14 10 5 15 10 9 18 4 | 10 22 14 16 17 13 15 16 16 17 12
27E | 12 53 12 14 18 8 22 27 20 19 7 | 25 53 25 30 33 25 31 43 33 33 26
28 | 10 24 7 12 14 6 19 13 8 25 4 | 19 32 21 27 28 19 26 27 20 25 20
29 | 6 24 9 13 12 6 21 11 7 29 4 | 27 35 25 27 25 26 32 28 26 27 24
30 | 6 13 6 11 12 5 12 7 6 15 3 | 9 20 14 16 15 12 18 15 14 18 11
31E | 9 24 7 8 12 4 15 10 12 31 4 | 30 34 31 32 32 30 35 32 28 37 30
32 | 12 20 7 22 14 5 15 13 9 22 5 | 23 29 25 34 29 24 29 29 25 34 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 25 8 13 14 5 19 14 13 23 |T 21 30 24 25 28 21 29 28 24 27 22
WRMS | 8 25 8 11 13 5 19 12 9 23 |NE 16 27 19 22 24 17 25 21 19 22 17
MEDI | 8 23 8 12 14 5 19 13 10 22 |MD 17 29 21 21 27 18 26 22 19 25 19
Table 3.1679.6 GPS week: 1679 Day: 6 MJD: 56003.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 73 39 27 29 51 22 37 209 --- 35 19 | 89 69 75 61 88 72 68 170 --- 55 68
2E | 9 25 10 10 13 5 23 11 10 13 4 | 18 30 26 23 23 19 20 24 22 24 20
3 | 9 16 9 7 13 5 14 9 9 20 4 | 19 25 29 22 27 22 24 25 21 32 22
4E | 17 21 12 13 12 10 21 27 16 22 6 | 107 58 109 107 120 107 119 102 103 115 108
5 | 7 19 12 10 14 8 23 14 14 30 5 | 32 38 33 39 37 31 30 33 34 35 31
6 | 8 16 11 8 12 4 14 9 7 22 4 | 19 25 30 24 29 22 23 24 21 33 22
7E | 13 18 8 11 15 8 19 20 14 11 5 | 41 39 37 38 41 32 38 32 40 39 36
8E | 15 29 10 12 21 8 20 17 33 16 7 | 25 33 26 25 34 24 33 29 34 24 23
9E | 15 21 11 14 12 10 24 17 30 16 6 | 59 65 60 64 63 57 65 68 60 63 60
10 | 9 14 7 9 10 7 16 9 6 16 3 | 27 30 33 39 35 31 26 34 33 32 31
11E | 9 37 7 10 21 5 14 17 12 25 5 | 21 50 28 21 36 22 34 26 19 32 24
12 | 9 23 7 13 16 6 18 10 10 24 4 | 21 35 32 31 36 25 30 29 27 24 27
13 | 7 19 10 9 17 5 14 14 11 18 4 | 23 37 29 26 40 25 33 26 24 25 25
14 | 10 26 6 16 14 7 15 15 10 23 5 | 23 37 33 33 36 28 32 30 30 31 28
15 | 12 19 9 10 17 5 22 8 11 25 5 | 22 32 26 26 34 24 32 23 25 23 23
16 | 6 28 8 12 12 4 24 9 9 26 5 | 22 33 29 27 34 25 28 26 20 24 24
17 | 6 20 8 12 11 5 21 12 12 27 4 | 22 29 16 26 18 20 26 25 21 27 18
18 | 9 23 9 18 14 6 21 11 12 30 5 | 27 42 32 35 35 29 34 28 33 28 29
19 | 8 30 9 12 12 8 22 15 8 20 5 | 17 36 17 18 21 16 28 21 16 23 15
20 | 9 29 10 15 12 6 18 25 7 31 6 | 23 38 31 32 34 26 31 35 27 32 27
21E | 12 22 8 14 15 5 17 12 11 11 4 | 18 27 23 23 31 20 25 24 25 25 21
22 | 7 28 7 8 15 6 20 14 14 35 5 | 30 42 36 32 38 35 34 37 40 40 32
23 | 7 23 9 10 11 4 14 17 11 29 4 | 22 32 29 28 31 23 29 27 20 25 24
X24 | 5 --- --- --- --- --- --- --- --- --- 0 | 20 --- --- --- --- --- --- --- --- --- 22
25 | 8 16 9 10 16 4 17 11 12 16 4 | 26 39 36 30 44 31 37 31 30 26 31
26 | 8 13 8 9 11 6 13 9 9 18 3 | 19 23 24 26 29 22 23 25 24 21 22
27E | 14 21 11 13 15 8 23 20 21 15 6 | 34 38 35 40 42 36 37 49 40 37 36
28 | 8 20 8 9 14 5 21 11 6 25 4 | 25 37 32 34 39 28 32 36 27 33 29
29 | 9 23 10 12 13 6 23 13 10 28 5 | 24 36 27 29 27 25 37 25 27 28 25
30 | 8 12 6 8 14 5 13 10 12 15 3 | 15 28 23 19 25 18 24 20 20 23 18
31E | 12 20 5 9 11 6 17 24 11 13 4 | 53 63 56 52 59 51 58 57 54 60 54
32 | 14 24 11 28 16 7 19 14 9 21 6 | 29 36 39 40 38 32 37 38 36 35 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 23 9 12 14 6 19 15 14 22 |T 30 38 35 34 39 31 36 38 31 34 31
WRMS | 9 23 9 11 14 6 19 12 9 21 |NE 23 33 29 29 32 25 30 28 26 28 25
MEDI | 9 21 9 11 14 6 19 14 11 22 |MD 23 36 31 30 35 25 32 29 27 31 25
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 4.1679 GPS week: 1679 MJD: 55997.0-56003.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 |U 8 10 18 |U 11 14 33 |U 7 7 33 |
emr | emr 2920 | 10 9 27 |U 13 15 37 | 15 12 41 |
esa | esa 2976 | 7 9 19 |U 11 13 34 | 14 10 60 |
gfz | gfz 2959 |U 11 15 19 |U 22 23 53 |U 17 14 40 |
grg | grg 2975 | 7 8 22 |U 11 14 38 | 16 14 44 |
igr | igr 2974 | 7 9 18 | 11 13 32 | 13 10 40 |
igs | igs 2920 | 8 9 18 | 11 13 34 | 13 9 24 |
jpl | jpl 2958 | 9 11 22 |U 12 13 39 | 15 11 40 |
mit | mit 2976 | 9 10 20 |U 13 14 40 | 16 14 40 |
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 5.1679.0 GPS week: 1679 Day: 0 MJD: 55997.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 5 3 13 | 13 10 31 | 6 8 21 |
emr | emr 2960 | 9 7 22 | 13 15 28 | 10 10 26 |
esa | esa 2976 | 5 6 16 | 11 11 31 | 7 7 19 |
gfz | gfz 2959 | 5 4 12 | 19 13 45 | 10 8 22 |
grg | grg 2975 | 8 8 25 | 10 10 33 | 9 7 21 |
igr | igr 2974 | 5 5 18 | 11 9 28 | 7 6 18 |
igs | igs 2956 | 6 6 19 | 11 11 29 | 6 7 19 |
jpl | jpl 2960 | 8 7 18 | 11 11 41 | 10 12 24 |
mit | mit 2976 | 5 5 20 | 11 10 34 | 10 12 20 |
Table 5.1679.1 GPS week: 1679 Day: 1 MJD: 55998.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 9 5 14 | 13 20 36 | 7 9 25 |
emr | emr 2959 | 10 7 24 | 14 24 39 | 12 14 26 |
esa | esa 2976 | 4 4 12 | 13 21 40 | 8 12 23 |
gfz | gfz 2960 | 7 2 15 | 34 50 72 | 13 22 18 |
grg | grg 2975 | 5 6 19 | 12 18 36 | 12 14 30 |
igr | igr 2975 | 4 4 12 | 13 20 38 | 9 12 19 |
igs | igs 2910 | 5 5 14 | 12 21 36 | 8 9 24 |
jpl | jpl 2960 | 7 7 17 | 12 20 37 | 10 12 21 |
mit | mit 2976 | 7 6 21 | 13 17 41 | 10 15 21 |
Table 5.1679.2 GPS week: 1679 Day: 2 MJD: 55999.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 4 6 17 | 9 8 23 | 8 9 16 |
emr | emr 2960 | 9 6 16 | 11 6 30 | 14 11 34 |
esa | esa 2976 | 4 3 11 | 13 8 31 | 9 12 39 |
gfz | gfz 2961 | 8 4 12 | 16 14 39 | 14 21 31 |
grg | grg 2976 | 7 10 19 | 16 11 43 | 14 15 36 |
igr | igr 2974 | 5 4 10 | 9 9 26 | 12 11 49 |
igs | igs 2939 | 4 4 8 | 9 6 25 | 10 10 28 |
jpl | jpl 2959 | 8 7 25 | 11 8 28 | 12 10 30 |
mit | mit 2976 | 5 4 10 | 17 9 52 | 15 14 45 |
Table 5.1679.3 GPS week: 1679 Day: 3 MJD: 56000.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 24 36 41 | 12 15 51 | 12 5 124 |
emr | emr 2868 | 19 28 29 | 20 17 54 | 9 8 109 |
esa | esa 2976 | 19 36 48 | 12 16 46 | 28 8 256 |
gfz | gfz 2957 | 34 83 27 | 17 21 54 | 15 8 135 |
grg | grg 2975 | 10 9 25 | 13 17 53 | 23 12 129 |
igr | igr 2975 | 23 36 41 | 11 15 47 | 12 4 125 |
igs | igs 2964 | 22 36 41 | 12 15 47 | ---- ---- ---- |
jpl | jpl 2959 | 26 39 47 | 16 15 58 | 15 7 121 |
mit | mit 2976 | 28 38 35 | 13 16 48 | 8 6 96 |
Table 5.1679.4 GPS week: 1679 Day: 4 MJD: 56001.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 7 14 | 10 10 24 | 6 5 17 |
emr | emr 2868 | 10 6 43 | 11 8 27 | 11 10 29 |
esa | esa 2976 | 5 7 17 | 9 8 26 | 10 16 29 |
gfz | gfz 2962 | 9 5 27 | 16 17 37 | 12 10 20 |
grg | grg 2976 | 7 10 26 | 9 10 29 | 10 10 29 |
igr | igr 2976 | 5 7 16 | 9 9 23 | 8 11 20 |
igs | igs 2905 | 6 7 15 | 10 8 26 | 8 6 16 |
jpl | jpl 2956 | 6 8 15 | 10 8 27 | 12 12 19 |
mit | mit 2976 | 5 6 24 | 10 10 28 | 10 10 24 |
Table 5.1679.5 GPS week: 1679 Day: 5 MJD: 56002.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 4 5 10 | 11 20 39 | 6 3 16 |
emr | emr 2868 | 9 5 37 | 14 20 47 | 27 12 27 |
esa | esa 2976 | 4 5 13 | 11 18 40 | 23 8 25 |
gfz | gfz 2960 | 9 3 23 | 28 25 54 | 28 8 29 |
grg | grg 2976 | 4 3 13 | 11 18 42 | 23 7 29 |
igr | igr 2975 | 4 4 12 | 11 20 39 | 25 6 26 |
igs | igs 2919 | 4 4 12 | 12 16 39 | 26 6 29 |
jpl | jpl 2959 | 5 6 14 | 11 19 43 | 29 9 26 |
mit | mit 2976 | 5 3 11 | 11 21 42 | 37 21 38 |
Table 5.1679.6 GPS week: 1679 Day: 6 MJD: 56003.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 | 5 6 14 | 10 16 30 | 8 9 15 |
emr | emr 2960 | 8 6 18 | 11 14 33 | 24 22 38 |
esa | esa 2976 | 5 5 14 | 10 12 25 | 13 11 26 |
gfz | gfz 2958 | 7 5 19 | 24 22 67 | 23 17 29 |
grg | grg 2976 | 9 10 24 | 10 13 30 | 23 31 36 |
igr | igr 2975 | 5 5 16 | 10 12 26 | 17 17 20 |
igs | igs 2850 | 8 4 20 | 13 11 34 | 20 14 26 |
jpl | jpl 2959 | 7 5 18 | 12 14 40 | 20 17 38 |
mit | mit 2976 | 7 6 20 | 13 15 34 | 22 19 36 |
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 6.1679 GPS week: 1679 MJD: 55997.500-56003.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 22 -64 89 68 -1 | 10 18
| 22 12 103 112 10 | 2
emr uuuuu | -19 23 78 -46 11 | 68 70
| 44 26 120 85 3 | 5
esa uuuuu | -2 -34 10 -75 8 | 6 16
| 10 14 50 87 6 | 2
gfz uuuuu | 10 33 -7 26 -12 | 25 29
| 21 14 50 106 8 | 4
grg uuuux | 32 -9 -4 -38 -25 | 33 59
| 16 15 71 92 17 | 1
igr xxxxx | -8 1 16 -11 -3 | 5 15
| 12 19 69 41 7 | 3
irf xxxxx | 18 -9 -30 20 -6 | -2 12
| 7 6 30 34 5 | 2
jpl uuuuu | 12 -35 111 64 0 | 48 50
| 35 30 68 58 10 | 1
mit uuuuu | -15 -11 -145 128 4 | 14 19
| 20 16 78 70 5 | 2
ngs uuuuu | -11 16 37 -64 -5 | 7 13
| 33 37 80 125 5 | 2
sio xuxux | 172 94 -417 99 18 | 72 74
| 21 16 118 181 12 | 9
Table 7.1679.0 GPS week: 1679 Day: 0 MJD: 55997.500
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 | 55 -50 281 96 -19 | 13 18
emr uuuuu | -35 55 -41 -100 10 | 63 65
esa uuuuu | -9 -34 -52 -153 -1 | 5 14
gfz uuuuu | 13 40 -60 204 -5 | 31 34
grg uuuux | 19 -10 77 -152 -17 | 33 59
igr xxxxx | -16 23 25 -39 -14 | 10 17
irf xxxxx | 26 -9 32 37 -4 | 2 11
jpl uuuuu | 69 -76 -7 141 -10 | 50 51
mit uuuuu | 1 -12 -60 118 8 | 14 19
ngs uuuuu | -43 26 189 -125 -3 | 10 15
sio xuxux | 192 104 -187 298 44 | 58 62
Table 7.1679.1 GPS week: 1679 Day: 1 MJD: 55998.500
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 -82 -9 120 -6 | 11 20
emr uuuuu | -19 48 28 -92 9 | 64 66
esa uuuuu | 19 -15 -5 -151 8 | 4 14
gfz uuuuu | 36 39 59 26 -17 | 30 33
grg uuuux | 19 -17 20 -165 -46 | 34 59
igr xxxxx | -12 -20 105 -18 -12 | 7 18
irf xxxxx | 27 -13 -51 65 -11 | 1 12
jpl uuuuu | -13 -3 100 152 -12 | 48 50
mit uuuuu | 3 -27 -151 235 9 | 13 18
ngs uuuuu | -54 -24 15 -122 -10 | 9 15
sio xuxux | 199 81 -517 380 20 | 64 67
Table 7.1679.2 GPS week: 1679 Day: 2 MJD: 55999.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 25 -75 18 -161 -8 | 10 18
emr uuuuu | -2 20 -27 -29 9 | 66 68
esa uuuuu | -11 -40 -19 -13 3 | 5 15
gfz uuuuu | 16 44 45 80 -12 | 28 31
grg uuuux | 47 -14 -66 -53 -22 | 33 59
igr xxxxx | 14 -8 23 -8 -2 | 5 16
irf xxxxx | 10 -18 -45 -3 -2 | -1 11
jpl uuuuu | 13 -7 206 54 3 | 48 50
mit uuuuu | -50 -27 -148 54 3 | 14 20
ngs uuuuu | 23 33 74 -92 -1 | 7 13
sio xuxux | 148 71 -468 9 11 | 69 72
Table 7.1679.3 GPS week: 1679 Day: 3 MJD: 56000.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 15 -51 125 133 1 | 7 18
emr uuuuu | 41 -12 190 104 13 | 64 67
esa uuuuu | -4 -24 24 -121 15 | 3 14
gfz uuuuu | -25 51 -33 9 -9 | 24 28
grg uuuux | 43 23 -104 53 -39 | 31 59
igr xxxxx | -18 26 -115 0 0 | 1 14
irf xxxxx | 19 -10 -34 49 -14 | -4 12
jpl uuuuu | -27 -11 73 37 1 | 45 47
mit uuuuu | -30 -17 -52 164 8 | 12 18
ngs uuuuu | 30 -24 -15 -139 -14 | 5 12
sio xuxux | 150 86 -378 149 16 | 71 74
Table 7.1679.4 GPS week: 1679 Day: 4 MJD: 56001.500
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 | 42 -61 95 133 7 | 10 19
emr uuuuu | -61 -3 208 -61 16 | 70 72
esa uuuuu | -7 -22 79 -92 10 | 7 17
gfz uuuuu | 5 15 -48 59 -26 | 25 28
grg uuuux | 23 -9 32 35 -34 | 33 59
igr xxxxx | -17 4 -1 -9 2 | 4 15
irf xxxxx | 9 -2 -36 26 -2 | -3 11
jpl uuuuu | 11 -36 114 6 13 | 48 49
mit uuuuu | 1 15 -258 159 -3 | 16 20
ngs uuuuu | 4 -1 -18 -42 -1 | 6 12
sio xuxux | 155 96 -474 -12 14 | 77 79
Table 7.1679.5 GPS week: 1679 Day: 5 MJD: 56002.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 25 -61 -11 151 5 | 8 17
emr uuuuu | -81 12 214 -157 9 | 71 73
esa uuuuu | -2 -55 -27 -82 8 | 7 16
gfz uuuuu | 29 19 -41 -96 -8 | 20 25
grg uuuux | 56 -21 69 49 -17 | 33 59
igr xxxxx | -4 -21 4 -69 0 | 2 14
irf xxxxx | 13 -5 -59 -37 -3 | -4 12
jpl uuuuu | -16 -37 167 34 11 | 47 48
mit uuuuu | -15 -15 -229 28 5 | 14 19
ngs uuuuu | -9 82 63 208 -5 | 5 12
sio xuxux | 176 100 -523 -83 10 | 79 81
Table 7.1679.6 GPS week: 1679 Day: 6 MJD: 56003.500
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 -65 125 5 11 | 10 18
emr uuuuu | 23 44 -24 13 14 | 75 76
esa uuuuu | -2 -45 70 89 12 | 10 18
gfz uuuuu | -5 23 31 -102 -4 | 20 25
grg uuuux | 17 -17 -57 -30 4 | 34 59
igr xxxxx | 0 4 69 64 2 | 3 14
irf xxxxx | 21 -4 -17 7 -2 | -4 12
jpl uuuuu | 48 -73 121 28 -9 | 48 50
mit uuuuu | -17 7 -116 138 -3 | 17 21
ngs uuuuu | -31 19 -46 -138 -4 | 5 12
sio xuxux | 183 120 -372 -48 8 | 84 85
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