[IGSREPORT-20742] Wk 1680 IGS Final Orbits Resubmission
IGS ACC
igs.acc at noaa.gov
Mon Apr 16 08:49:28 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1680 (Mar 18, 2012 - Mar 24, 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:
igs1680[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1680[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1680[0-6].cls IGS GPS clock combination summary report.
igs16807.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16807.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 | 4 9 27 4 9 27 KOUC YELL
0 | EMR | 8 8
0 | ESA | AREQ
0 | GFZ | 7 9 27 31 SUTM
0 | GRG | YELL
0 | JPL | 4 8
0 | MIT | 21 21
1 | COD | 4 9 4 9 SOFI
1 | EMR | 8 8
1 | ESA | AREQ AREQ
1 | GFZ | 4 7 9 27 30 31 ALRT BRFT
1 | GRG | YELL
1 | JPL | 8
1 | MIT | CAS1
2 | COD | 4 9 27 4 9 27 GRAZ WILL
2 | EMR | 8 MCM4
2 | ESA | AREQ AREQ
2 | GFZ | 4 7 9 27 30 31 BRFT TWTF
2 | GRG | YELL
2 | JPL | QAQ1
2 | MIT | DAV1
3 | COD | 4 9 27 4 9 GRAZ
3 | EMR | 8 8
3 | ESA | AREQ AREQ
3 | GFZ | 4 7 9 27 31 BRFT
3 | GRG | USN3
3 | JPL | 8 9 27
3 | MIT | 17 17 CAS1 DAV1 MAW1
4 | COD | 4 9 27 4 9 27
4 | GFZ | 4 7 9 31 BRFT THTI
4 | GRG | KIT3 WSRT
4 | MIT | CAS1 MAW1
5 | COD | 4 4
5 | EMR | 8 8
5 | ESA | AREQ AREQ MATE
5 | GFZ | 4 7 9 27 31 MCM4
5 | GRG | WSRT
5 | JPL | 8 30
5 | MIT | 9 27 27 DAV1
6 | ALL | 8
6 | COD | 9 9 30 KOUC
6 | ESA | AREQ AREQ
6 | GFZ | 4 7 9 30 31
6 | GRG | AMC2
6 | JPL | 4 30 CAS1 PALM
6 | MIT | 22 30 22 CAS1
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 .3 -1.8 -55 -4 -8 .12
EMR | -.3 -1.5 11.5 -2 8 11 .59
ESA | -.8 -.5 4.2 34 -79 119 .28
GFZ | -2.1 .4 -.8 -55 46 -32 .19
GRG | -2.8 -2.8 6.0 -45 54 -18 .10
JPL | -2.5 -.9 11.7 -21 -28 -2 .45
MIT | 2.7 -3.5 12.6 -48 37 -69 .34
NGS | 4.2 1.8 8.6 -35 -7 19 .38
SIO | -.1 -2.8 7.1 -54 -42 53 .65
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 1.1680.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1680.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 2.1680.[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 3.1680.[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 5.1680.0-6).
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 1680 summary. (Mar 18, 2012 - Mar 24, 2012)
Table 1.1680.a GPS week: 1680 MJD: 56004.000-56010.000
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 259| 0 0 0 39 -10 -10 -.28 9 8 | -511 -519 20 85
| 0 0 0 12 16 16 .02 | 734 925
emr 91| 0 0 4 -59 0 -29 .48 22 22 | 92430 469 17 100
| 1 3 1 44 21 10 .02 | 234605 799
esa 165| 0 0 0 -101 95 26 .23 9 9 | -438 222 41 767
| 0 0 1 11 18 17 .02 | 796 1353
gfz 186| 0 -1 -2 37 -67 -24 -.23 14 13 | 93 74 33 114
| 0 1 1 51 62 14 .02 | 582 722
grg 118| 0 0 -1 9 -109 -17 .59 18 16 | 332 309 49 218
| 0 0 2 14 11 14 .03 | 537 730
igr n/a| 0 0 -2 -45 -25 -17 -.11 6 5 | 17652 -380 22 115
| 0 0 1 14 18 16 .04 | 667 787
jpl 145| 0 -1 0 -29 44 41 .56 17 17 | 2122 254 23 93
| 1 2 1 14 9 27 .02 | 1086 798
mit 276| 0 0 0 43 -61 -12 -.37 13 11 | -189 159 23 128
| 0 1 1 25 29 21 .05 | 156 141
ngs 225| 0 1 0 16 -6 -14 -.21 13 9 | -2756 7979 1921 3513
| 0 0 1 33 35 15 .06 | 5703 22302
sio 222| -1 0 1 50 85 60 -.10 21 20 | --- --- --- ---
| 1 2 0 12 25 28 .03 | --- ---
Table 1.1680.b GPS week : 1680 MJD: 56004.000-56010.000
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 5 6 5 4 5 4 |
2 | 5 5 4 4 5 5 5 |
3 | 4 4 4 4 4 5 4 |
4 | 6 5 6 5 5 5 6 |
5 | 5 5 5 5 5 5 6 |
6 | 4 4 4 4 3 4 4 |
7 | 5 4 5 5 4 5 4 |
8 | 7 7 7 6 6 7 6 |
9 | 7 7 6 7 6 7 6 |
10 | 4 4 4 3 4 4 4 |
11 | 4 5 5 5 4 4 4 |
12 | 5 5 6 5 5 5 5 |
13 | 5 4 5 5 4 5 5 |
14 | 5 5 5 5 5 6 5 |
15 | 5 5 5 5 5 6 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 5 5 6 7 |
18 | 5 5 5 5 5 6 6 |
19 | 5 5 5 5 5 5 4 |
20 | 6 5 6 5 5 5 5 |
21 | 6 5 4 4 4 4 5 |
22 | 5 5 5 5 5 6 5 |
23 | 5 5 5 5 4 5 5 |
24 | 0 0 0 0 0 0 0 |
25 | 4 4 4 4 5 4 4 |
26 | 4 4 4 4 4 5 5 |
27 | 6 8 6 8 7 7 6 |
28 | 5 5 5 5 5 6 5 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 5 5 5 5 5 5 5 |
32 | 5 5 4 5 5 4 5 |
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 2.1680.0 GPS week: 1680 Day: 0 MJD: 56004.000
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 259| -1 0 1 51 -25 -42 -.31 10 9 | -555 -614 16 81
| 6 2 |
emr 91| 2 4 4 -4 -11 -17 .45 22 22 | 2985 -505 17 99
| -30 -37 |
esa 165| 0 0 1 -88 74 28 .19 8 8 | -1165 363 32 195
| 36 24 |
gfz 186| 0 -3 -4 -59 -87 -47 -.25 15 13 | 154 -70 33 106
| -18 71 |
grg 118| 1 0 2 14 -115 -27 .57 16 15 | 35 256 49 218
| -22 -11 |
igr n/a| 1 0 -3 -28 -33 -47 -.12 5 5 | 18764 -593 23 90
| -9 37 |
jpl 145| -2 1 -3 -18 39 53 .56 17 17 | 1717 -407 20 76
| 54 -43 |
mit 276| 0 -2 1 30 -28 31 -.44 14 12 | -111 133 23 129
| -10 -2 |
ngs 225| 0 1 -3 72 -11 -44 -.25 13 10 | -348 -1042 1821 3298
| -78 34 |
sio 222| 0 -2 1 50 104 108 -.06 23 21 | --- --- --- ---
| -19 -86 |
Table 2.1680.1 GPS week: 1680 Day: 1 MJD: 56005.000
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 259| 0 0 1 39 -19 -7 -.30 8 7 | 908 -2451 15 71
| 36 10 |
emr 91| -2 3 4 -13 -5 -29 .47 23 21 | 2205 609 18 111
| -55 -48 |
esa 165| 0 0 0 -90 102 31 .22 9 9 | -1115 759 31 250
| 23 18 |
gfz 186| -1 -2 -1 18 -10 -12 -.21 15 14 | 53 505 33 124
| -59 34 |
grg 118| 0 0 2 13 -115 -24 .64 16 15 | 113 61 40 231
| -11 -10 |
igr n/a| 0 0 -2 -55 -44 -20 -.07 6 5 | 18029 58 20 113
| 22 18 |
jpl 145| 0 0 0 -36 35 16 .53 17 17 | 1145 533 21 96
| 37 -36 |
mit 276| 0 -3 -3 5 -73 -18 -.40 14 11 | -97 129 22 127
| 20 27 |
ngs 225| 0 2 -1 45 -13 -4 -.26 13 8 | -15670 58550 1871 3518
| -97 -13 |
sio 222| 0 -2 0 41 76 81 -.11 21 21 | --- --- --- ---
| -34 -67 |
Table 2.1680.2 GPS week: 1680 Day: 2 MJD: 56006.000
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 259| -1 -1 0 35 1 -21 -.26 8 7 | -1425 322 16 86
| 16 13 |
emr 91| 0 -1 7 -27 18 -18 .48 22 21 | 2652 -402 15 96
| -34 -49 |
esa 165| 1 2 0 -102 77 30 .26 10 10 | 639 -1792 35 471
| 8 16 |
gfz 186| 0 0 0 52 -83 -30 -.24 15 14 | 73 -499 32 112
| -28 85 |
grg 118| 0 0 0 11 -102 -14 .60 16 14 | 440 -993 41 204
| 17 -4 |
igr n/a| 0 0 -1 -58 -25 4 -.09 5 5 | 17933 -1263 19 118
| 7 27 |
jpl 145| 0 0 1 -22 42 81 .55 17 18 | 1680 -732 22 99
| 25 -39 |
mit 276| -1 -1 -2 45 -55 -18 -.39 13 11 | -402 173 17 115
| -6 10 |
ngs 225| 2 2 -1 -12 16 -17 -.26 12 9 | -1150 -45 2101 3581
| 15 3 |
sio 222| -3 0 0 53 104 58 -.16 21 20 | --- --- --- ---
| -52 -87 |
Table 2.1680.3 GPS week: 1680 Day: 3 MJD: 56007.000
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 259| 0 0 1 21 1 -4 -.26 8 7 | -378 -429 22 95
| 48 -15 |
emr 91| 0 0 5 -96 30 -47 .51 23 23 | 624457 1578 16 111
| 36 -63 |
esa 165| 1 1 0 -114 97 9 .24 10 9 | -598 -256 44 1173
| 10 18 |
gfz 186| 1 -2 -2 92 -73 -34 -.21 15 15 | -966 1422 34 126
| -65 43 |
grg 118| -1 -1 -2 -9 -117 -20 .62 17 16 | -244 391 50 216
| 42 -11 |
igr n/a| 0 0 0 -37 -13 -23 -.10 6 5 | 16754 759 23 152
| -9 26 |
jpl 145| 0 -1 -1 -37 60 73 .54 17 17 | 1002 1405 23 102
| 82 -48 |
mit 276| 0 -1 0 78 -96 -10 -.36 13 10 | -346 419 22 157
| -18 21 |
ngs 225| 0 1 1 -7 1 -6 -.14 13 8 | -391 -371 1718 3200
| -16 40 |
sio 222| -3 1 1 67 54 72 -.12 20 21 | --- --- --- ---
| -57 -56 |
Table 2.1680.4 GPS week: 1680 Day: 4 MJD: 56008.000
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 259| -1 0 0 50 -36 -4 -.27 8 7 | -412 13 18 83
| 6 34 |
emr 91| 0 0 4 -102 -35 -34 .50 21 21 | 3500 1375 22 123
| 58 -40 |
esa 165| 1 0 0 -89 98 56 .22 9 9 | -544 2132 60 876
| 39 -4 |
gfz 186| 0 -2 -2 19 23 -6 -.20 13 13 | -123 175 34 108
| -88 29 |
grg 118| 1 0 -2 9 -112 -37 .57 18 18 | 657 1267 54 235
| 1 5 |
igr n/a| 0 0 -2 -44 -49 -9 -.07 6 6 | 17110 314 23 143
| -4 54 |
jpl 145| 0 -4 1 -7 36 20 .59 17 17 | 2099 1060 22 90
| -17 4 |
mit 276| 0 0 0 30 -35 -31 -.34 12 10 | -96 94 22 112
| -14 11 |
ngs 225| 0 2 0 13 -59 -23 -.21 12 8 | -306 -450 1879 3650
| -25 93 |
sio 222| -1 1 2 29 114 43 -.11 20 20 | --- --- --- ---
| -48 -67 |
Table 2.1680.5 GPS week: 1680 Day: 5 MJD: 56009.000
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 259| 0 0 2 23 4 6 -.26 9 8 | -1101 -588 30 100
| 54 10 |
emr 91| 2 -3 4 -111 2 -29 .51 23 23 | 5280 390 18 90
| 60 -48 |
esa 165| 0 0 0 -108 86 26 .26 12 11 | 707 -996 37 1163
| 28 34 |
gfz 186| 0 0 -3 88 -65 -11 -.23 12 12 | 584 -727 35 112
| -74 45 |
grg 118| 1 1 -4 -7 -116 -8 .57 21 19 | 1344 1016 60 214
| 2 -7 |
igr n/a| 0 0 -3 -66 -19 -9 -.13 6 6 | 17665 -634 23 96
| -3 -12 |
jpl 145| -1 -4 0 -50 45 17 .57 19 19 | 3366 271 28 92
| 23 -10 |
mit 276| 0 0 0 71 -37 -27 -.31 13 11 | -293 219 26 126
| -21 -7 |
ngs 225| 0 2 -1 -20 -32 0 -.12 13 10 | -953 -749 2193 3879
| -7 59 |
sio 222| 0 3 2 62 94 25 -.08 21 20 | --- --- --- ---
| -56 -57 |
Table 2.1680.6 GPS week: 1680 Day: 6 MJD: 56010.000
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 259| 0 0 0 51 3 0 -.29 9 8 | -616 111 24 82
| 11 -17 |
emr 91| -1 -3 3 -61 -1 -29 .46 22 22 | 5932 238 18 76
| 35 -2 |
esa 165| -1 0 -1 -114 129 2 .24 9 8 | -996 1348 53 1247
| 19 20 |
gfz 186| 0 -1 -1 50 -173 -25 -.24 13 12 | 879 -284 34 111
| -40 35 |
grg 118| 1 0 -3 34 -87 8 .56 18 17 | -21 168 49 213
| -13 -45 |
igr n/a| 1 0 -2 -28 5 -14 -.18 6 5 | 17312 -1306 24 93
| -25 8 |
jpl 145| 0 -1 1 -31 52 25 .55 18 17 | 3845 -351 26 96
| 23 23 |
mit 276| 1 1 0 45 -101 -16 -.33 12 11 | 18 -50 29 134
| -5 23 |
ngs 225| 0 0 2 25 50 -3 -.19 13 9 | -475 -37 1866 3469
| -42 -61 |
sio 222| 0 2 2 51 50 37 -.09 23 21 | --- --- --- ---
| -58 -33 |
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 3.1680.0 GPS week: 1680 Day: 0 MJD: 56004.000
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 32 11 22 14 7 15 19 11 16 5 | 36 44 40 35 32 32 32 44 34 37 35
2E | 9 23 5 14 25 6 18 9 13 22 5 | 24 28 24 22 25 23 24 20 21 30 21
3 | 10 12 7 12 12 6 13 11 6 14 3 | 15 26 23 22 26 19 23 21 21 16 19
4E | 11 28 11 14 14 7 20 14 17 22 5 | 32 44 32 28 34 31 40 25 33 29 29
5 | 8 20 8 15 14 6 18 18 15 20 5 | 26 37 30 33 33 26 36 32 26 30 28
6 | 10 13 7 14 11 6 13 11 4 17 3 | 19 27 26 26 26 22 24 25 23 27 23
7E | 6 20 8 9 16 6 15 17 12 17 4 | 24 27 23 18 25 21 27 29 24 21 22
8E | 15 21 7 17 25 6 18 12 32 19 6 | 32 35 33 29 36 32 37 30 49 38 32
9E | 17 22 12 18 18 7 21 16 24 22 6 | 47 45 43 50 49 47 45 46 56 43 45
10 | 7 15 5 11 11 5 13 7 10 15 3 | 21 21 23 26 25 23 22 20 23 21 22
11E | 8 18 5 12 11 5 11 16 16 19 4 | 21 28 20 24 22 22 24 27 26 26 21
12 | 10 24 9 14 16 6 18 13 9 26 5 | 21 31 27 27 30 21 27 25 24 26 23
13 | 7 24 9 12 15 6 17 14 8 19 4 | 22 35 28 26 38 24 34 29 26 22 25
14 | 10 25 6 16 14 5 15 13 7 24 4 | 24 34 30 34 38 28 33 32 27 25 28
15 | 9 23 8 18 18 5 18 15 11 24 5 | 22 32 26 35 37 25 32 26 27 24 25
16 | 7 25 9 16 12 5 22 16 9 23 5 | 22 30 25 26 28 21 30 22 20 19 21
17 | 6 22 10 15 14 5 21 10 10 36 5 | 15 29 17 18 22 14 28 14 16 26 14
18 | 10 23 6 20 15 3 18 12 11 31 5 | 23 40 27 30 30 25 36 25 22 31 25
19 | 8 26 8 13 13 5 22 10 12 24 5 | 18 29 17 22 19 20 26 20 19 22 16
20 | 9 29 13 20 13 6 17 15 13 26 5 | 31 44 32 31 35 30 37 37 31 32 31
21E | 10 21 7 14 37 6 14 11 9 24 5 | 19 31 25 24 38 24 29 24 26 27 24
22 | 9 25 6 16 15 3 18 12 9 29 5 | 26 41 30 31 37 28 39 31 26 32 28
23 | 8 26 8 15 13 5 15 12 10 25 4 | 22 34 27 27 30 24 29 29 30 23 24
X24 | 6 --- --- --- --- --- --- --- --- --- 0 | 23 --- --- --- --- --- --- --- --- --- 24
25 | 8 17 5 11 15 3 16 12 10 18 4 | 24 31 30 23 38 25 35 31 21 28 27
26 | 6 13 6 17 14 5 11 12 10 19 4 | 21 19 22 26 27 21 25 21 22 19 21
27E | 14 19 10 17 20 6 17 20 18 23 6 | 50 45 48 49 51 45 46 54 49 45 46
28 | 8 27 8 11 17 3 21 10 9 23 5 | 21 33 25 25 37 22 32 25 25 26 24
29 | 9 21 6 16 16 5 16 10 11 31 4 | 14 26 13 11 15 12 24 17 15 25 12
30 | 9 13 7 13 10 3 10 10 11 18 3 | 16 25 20 17 20 16 24 17 21 17 17
31E | 11 23 7 10 12 6 15 26 11 22 5 | 28 33 29 26 33 28 33 29 31 22 27
32 | 10 25 7 15 12 6 16 11 14 18 4 | 21 26 24 27 22 19 23 27 22 20 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 22 8 15 16 5 17 14 13 23 |T 24 32 27 27 30 24 30 27 26 26 25
WRMS | 9 22 8 13 15 5 17 12 10 21 |NE 21 30 24 25 29 22 29 25 23 24 22
MEDI | 9 23 7 15 14 6 17 12 11 22 |MD 22 31 26 26 30 24 30 26 25 26 24
Table 3.1680.1 GPS week: 1680 Day: 1 MJD: 56005.000
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 30 9 24 13 10 11 17 10 14 5 | 26 35 28 31 28 25 25 28 27 26 24
2E | 6 22 6 11 21 6 18 10 15 19 4 | 25 32 27 24 29 26 27 21 26 30 24
3 | 7 12 8 11 12 4 10 11 8 14 3 | 19 30 23 24 27 22 26 20 17 21 21
4E | 9 20 10 11 14 5 17 9 20 22 5 | 26 36 30 28 31 28 35 26 33 33 28
5 | 7 20 11 12 15 7 19 12 7 22 4 | 27 36 28 33 34 29 33 29 28 30 27
6 | 6 14 8 11 11 3 11 10 8 16 3 | 21 32 24 26 28 25 28 23 21 28 23
7E | 5 17 7 11 16 4 13 18 12 14 4 | 24 26 29 26 30 23 25 33 28 24 25
8E | 13 23 10 11 24 5 19 13 30 18 6 | 34 38 37 30 38 33 38 35 49 39 35
9E | 16 19 13 17 20 9 22 16 26 24 6 | 60 61 56 63 62 59 57 58 66 56 57
10 | 5 15 8 9 13 5 13 8 9 17 3 | 25 25 25 24 26 22 24 21 25 24 24
11E | 10 18 6 11 13 7 11 17 12 18 4 | 24 38 29 30 34 28 30 34 31 29 28
12 | 8 24 10 14 17 5 17 13 12 23 5 | 21 34 25 28 32 25 29 24 28 24 23
13 | 5 22 8 13 15 6 16 15 9 16 4 | 26 36 31 28 38 27 36 32 28 28 28
14 | 9 23 5 19 14 5 15 15 7 20 4 | 28 39 31 37 37 31 35 34 28 28 30
15 | 7 20 10 16 17 6 19 11 8 24 4 | 28 37 33 34 35 30 34 30 29 30 29
16 | 7 23 6 12 14 4 20 14 9 23 4 | 21 33 23 24 32 22 32 22 20 18 21
17 | 8 20 9 14 15 6 17 8 14 32 5 | 29 33 27 25 31 27 33 26 28 28 25
18 | 8 24 7 17 15 5 19 12 12 22 5 | 23 38 29 33 32 25 34 29 25 29 27
19 | 6 25 9 14 14 4 21 8 10 23 4 | 21 33 22 22 26 22 32 23 24 30 22
20 | 6 25 8 20 13 7 16 19 7 21 5 | 35 45 34 38 36 32 37 40 34 36 34
21E | 8 22 21 12 21 7 15 12 10 14 5 | 23 32 26 24 29 22 27 22 24 21 22
22 | 8 25 5 18 12 4 17 10 8 25 4 | 31 43 33 35 42 30 39 33 30 34 32
23 | 6 21 9 14 14 6 16 15 10 22 4 | 27 35 28 27 31 28 32 32 32 27 27
X24 | 5 --- --- --- --- 65 --- --- --- --- 0 | 23 --- --- --- --- 62 --- --- --- --- 23
25 | 7 15 12 12 17 5 15 12 10 15 4 | 25 31 32 28 38 28 34 29 25 25 27
26 | 5 17 8 12 16 5 13 10 8 26 4 | 24 28 26 27 28 25 24 23 27 26 24
27E | 12 63 10 15 25 7 21 19 16 23 7 | 57 93 55 59 50 54 55 60 55 52 56
28 | 7 23 7 11 15 6 17 10 8 22 4 | 22 37 24 19 37 24 34 22 22 26 23
29 | 10 22 8 17 16 5 19 10 10 29 5 | 16 28 22 23 22 18 27 21 22 26 18
30 | 9 11 6 7 11 4 12 14 10 16 3 | 21 31 24 21 28 23 29 27 25 23 23
31E | 8 20 8 12 10 5 17 27 12 18 5 | 21 32 27 28 32 22 29 35 23 23 24
32 | 9 22 7 30 13 5 15 12 10 16 5 | 22 27 23 36 21 18 22 24 21 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 23 9 15 16 6 17 14 13 21 |T 26 36 29 30 33 28 32 29 29 28 27
WRMS | 7 21 9 14 15 5 17 11 8 21 |NE 24 33 27 28 31 27 31 26 25 26 25
MEDI | 7 22 8 12 15 5 17 12 10 21 |MD 24 34 28 28 32 25 32 28 27 28 24
Table 3.1680.2 GPS week: 1680 Day: 2 MJD: 56006.000
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 35 11 21 20 5 11 14 11 20 5 | 25 37 24 29 28 24 24 25 25 31 23
2E | 6 22 6 13 19 6 15 8 12 18 4 | 21 29 26 21 22 23 29 21 19 24 22
3 | 6 13 9 11 13 3 9 10 11 13 3 | 18 23 22 22 24 18 23 16 20 15 18
4E | 11 21 8 12 12 10 17 16 21 25 5 | 21 31 25 21 26 26 33 24 36 27 23
5 | 7 19 12 16 14 6 21 9 12 20 4 | 27 35 27 29 31 25 34 27 29 26 26
6 | 6 15 8 11 11 3 12 10 9 15 3 | 18 25 21 21 24 19 23 17 20 22 19
7E | 6 17 8 13 19 4 15 20 10 14 4 | 21 27 20 20 24 21 26 22 17 19 19
8E | 14 26 10 16 23 6 22 14 29 20 6 | 31 34 33 30 34 27 37 30 36 33 29
9E | 14 21 12 19 17 7 18 18 20 23 6 | 47 46 37 48 43 44 45 47 48 41 43
10 | 4 15 5 11 16 4 14 8 7 18 3 | 22 21 26 27 30 23 24 23 25 26 24
11E | 13 17 11 15 15 4 10 9 15 21 4 | 34 48 42 44 46 38 44 39 38 38 38
12 | 9 25 13 23 16 5 19 14 7 24 5 | 18 30 23 25 27 18 27 20 15 20 18
13 | 7 21 12 13 15 5 18 14 9 19 4 | 24 34 29 25 37 25 37 25 20 25 24
14 | 8 23 8 17 16 5 14 18 7 22 5 | 28 33 32 33 39 28 34 28 26 32 29
15 | 8 24 13 16 16 6 21 11 13 21 5 | 23 32 25 26 30 21 30 26 24 25 22
16 | 6 29 10 16 16 5 23 9 9 23 5 | 16 29 22 21 28 18 27 15 13 16 17
17 | 8 23 12 18 13 5 18 11 8 31 5 | 16 33 21 21 29 18 31 19 16 20 18
18 | 8 26 7 20 16 5 23 11 10 21 5 | 21 38 27 27 30 24 34 23 23 23 23
19 | 6 26 11 15 16 5 20 9 9 20 4 | 15 31 18 20 24 15 27 13 15 14 15
20 | 8 23 15 19 12 7 18 21 9 21 5 | 31 41 31 34 29 29 38 32 30 34 29
21E | 5 16 14 14 15 3 15 9 12 12 4 | 24 30 34 23 30 26 30 23 26 24 25
22 | 6 24 9 14 15 4 16 14 15 23 5 | 30 37 32 31 39 29 34 27 29 27 28
23 | 6 22 8 16 13 4 16 12 7 23 4 | 24 32 24 27 26 25 33 27 25 23 24
X24 | 4 --- --- --- --- 26 --- --- --- --- 0 | 27 --- --- --- --- 31 --- --- --- --- 27
25 | 9 16 8 13 16 4 15 13 8 19 4 | 23 31 28 26 35 24 35 25 21 22 25
26 | 6 14 10 12 12 4 18 7 13 19 4 | 20 24 23 21 25 19 25 22 20 17 20
27E | 14 22 13 17 24 6 19 20 17 24 6 | 61 57 69 66 64 66 60 71 71 65 63
28 | 6 23 9 13 17 3 19 10 11 23 4 | 21 36 28 24 38 25 33 27 29 27 25
29 | 8 21 8 18 11 7 18 10 10 29 4 | 17 28 15 17 19 15 28 16 17 23 15
30 | 8 13 9 12 13 5 10 12 8 18 3 | 16 24 19 15 23 17 25 19 19 19 18
31E | 7 21 12 14 12 6 12 20 10 18 4 | 22 30 27 24 29 23 28 21 22 18 21
32 | 9 20 9 15 12 5 14 11 9 16 4 | 23 26 25 30 25 23 27 29 22 28 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 22 10 15 16 5 17 13 12 21 |T 24 32 27 27 30 25 31 25 25 25 24
WRMS | 7 21 10 14 14 5 17 11 9 20 |NE 21 30 24 24 29 22 29 22 21 23 22
MEDI | 7 21 10 15 15 5 17 11 10 20 |MD 22 31 26 25 29 24 30 24 23 24 23
Table 3.1680.3 GPS week: 1680 Day: 3 MJD: 56007.000
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 | 8 31 10 20 16 7 12 13 9 16 5 | 23 32 28 26 29 24 23 31 23 27 24
2E | 6 22 6 12 17 6 19 9 13 14 4 | 16 26 25 24 23 21 22 18 21 20 19
3 | 9 15 11 15 13 4 17 9 6 15 4 | 16 25 25 20 26 19 26 17 16 17 18
4E | 8 17 7 10 16 12 17 14 23 20 5 | 14 26 15 16 21 13 26 19 23 19 14
5 | 6 26 11 11 15 5 22 8 14 18 4 | 31 42 36 39 34 33 39 34 32 32 32
6 | 6 15 7 10 13 3 16 7 5 14 3 | 19 25 25 21 28 21 26 24 20 22 21
7E | 7 20 12 12 15 4 15 15 12 9 4 | 20 25 25 23 27 21 22 29 21 24 21
8E | 12 22 12 16 24 5 19 15 28 18 6 | 33 37 38 32 40 33 39 40 46 40 35
9E | 15 20 14 18 26 8 21 16 27 24 6 | 65 68 60 67 64 65 61 65 71 60 62
10 | 4 15 7 9 13 8 14 6 12 12 3 | 22 23 28 28 32 21 23 23 21 19 23
11 | 6 17 13 15 25 5 12 10 12 20 4 | 20 28 23 23 30 22 23 26 22 24 20
12 | 8 25 8 15 18 6 21 15 10 24 5 | 19 34 27 24 30 22 28 22 24 20 21
13 | 6 23 9 12 18 6 16 13 8 19 4 | 23 38 30 30 42 27 33 32 27 26 27
14 | 9 25 7 13 17 4 12 17 11 20 4 | 29 40 38 37 41 34 36 41 38 32 34
15 | 5 26 10 18 13 5 20 9 9 19 4 | 32 43 37 42 41 35 38 30 36 30 33
16 | 6 26 9 16 15 4 21 5 6 22 4 | 16 27 22 19 28 15 24 14 16 15 16
17 | 7 21 13 17 14 5 20 15 10 30 5 | 19 31 18 18 25 17 31 22 18 25 17
18 | 8 27 7 15 16 5 22 10 9 20 4 | 24 39 28 32 31 26 36 27 28 26 26
19 | 9 28 14 15 16 5 19 9 9 20 5 | 17 32 20 18 22 17 28 20 20 21 17
20 | 8 23 11 9 15 7 18 21 10 21 5 | 32 41 33 35 36 31 36 39 27 35 31
21E | 6 18 7 13 20 6 13 5 7 13 3 | 22 29 25 26 32 24 29 25 23 28 24
22 | 7 25 13 14 14 4 16 11 13 20 4 | 32 42 37 33 41 32 38 34 35 32 33
23 | 6 24 8 14 17 5 17 11 8 23 4 | 23 35 30 31 34 28 30 32 28 27 27
X24 | 4 --- --- --- --- 53 --- --- --- --- 0 | 25 --- --- --- --- 43 --- --- --- --- 26
25 | 5 17 6 11 16 5 15 11 9 16 3 | 22 29 25 23 33 24 32 26 27 24 23
26 | 4 17 6 10 8 6 15 8 6 22 3 | 26 31 30 33 31 27 25 26 26 29 26
27E | 14 20 15 21 28 6 21 31 28 27 8 | 110 113 114 111 114 108 111 108 108 114 109
28 | 8 30 9 16 19 4 21 8 7 23 5 | 15 37 22 21 33 17 29 21 17 22 18
29 | 8 23 6 18 16 4 18 8 9 29 4 | 17 28 18 21 19 16 27 20 25 29 18
30 | 7 16 6 12 16 3 10 8 9 17 3 | 16 28 20 14 23 16 25 21 19 21 18
31E | 6 28 7 13 16 5 11 13 10 24 4 | 18 30 22 22 28 18 23 24 21 19 19
32 | 9 26 6 27 15 4 17 8 10 17 5 | 16 25 19 37 24 20 19 23 23 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 23 10 15 17 6 17 13 13 20 |T 26 35 30 30 34 27 32 30 29 28 27
WRMS | 7 23 9 15 16 5 17 10 8 21 |NE 22 33 27 27 31 24 29 26 24 24 23
MEDI | 7 23 9 14 16 5 17 10 10 20 |MD 22 31 25 26 31 22 28 26 23 25 23
Table 3.1680.4 GPS week: 1680 Day: 4 MJD: 56008.000
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 8 14 18 7 12 9 8 17 4 | 15 27 19 20 25 16 21 20 17 21 16
2E | 6 24 7 11 20 6 21 9 11 14 4 | 20 29 23 15 27 23 28 19 22 22 21
3 | 8 12 8 10 17 7 9 8 11 14 3 | 14 22 23 15 25 17 22 13 20 12 16
4E | 10 21 8 10 16 7 16 13 22 21 5 | 14 26 17 13 19 16 25 17 27 19 16
5 | 8 24 8 12 18 5 23 8 10 18 4 | 21 31 24 27 27 20 29 20 21 22 21
6 | 6 13 10 9 13 4 10 8 6 13 3 | 15 22 26 17 25 19 22 19 17 17 19
7E | 4 16 8 12 19 7 17 12 12 9 4 | 14 21 14 14 17 15 19 18 16 14 13
8E | 12 23 9 13 26 4 21 12 24 18 6 | 19 29 25 23 33 22 32 26 34 32 23
9E | 17 20 14 17 26 8 21 15 16 21 6 | 46 51 49 58 54 50 52 52 50 50 48
10 | 6 13 7 11 19 4 13 10 9 13 3 | 18 17 21 20 25 17 18 17 21 19 18
11 | 4 16 9 15 23 7 8 7 7 20 4 | 14 27 18 14 21 13 20 16 13 17 13
12 | 7 24 10 14 18 4 21 15 7 23 5 | 13 29 24 20 28 17 25 19 15 15 17
13 | 7 19 7 9 20 4 15 10 8 17 4 | 16 29 17 17 34 15 28 17 16 14 16
14 | 9 23 8 14 17 6 15 16 12 19 4 | 16 29 26 30 31 23 27 28 25 20 23
15 | 8 25 11 12 20 7 18 9 10 19 4 | 19 29 29 29 32 23 25 19 20 18 20
16 | 6 27 9 11 17 4 20 7 7 24 4 | 15 27 19 16 26 13 25 12 13 12 14
17 | 5 19 9 15 16 7 20 12 9 32 5 | 17 30 16 15 25 18 29 18 19 24 16
18 | 10 29 8 12 19 5 19 12 7 23 5 | 15 37 26 21 29 17 30 22 19 16 20
19 | 7 19 9 13 17 8 19 8 11 21 4 | 13 26 12 16 18 13 25 15 16 16 13
20 | 9 22 11 12 16 5 16 17 10 19 5 | 19 28 19 24 23 18 25 26 21 21 18
21E | 7 15 14 12 23 6 11 7 13 12 4 | 20 27 26 19 28 18 25 22 22 20 22
22 | 8 25 11 12 17 5 19 12 9 17 4 | 15 34 28 21 31 19 30 24 19 16 20
23 | 7 23 6 13 19 5 17 8 9 21 4 | 12 26 14 17 26 14 21 15 13 9 13
X24 | 5 --- --- --- --- 26 --- --- --- --- 0 | 21 --- --- --- --- 19 --- --- --- --- 22
25 | 5 17 8 16 17 5 16 14 8 18 4 | 15 25 19 18 33 16 29 21 18 19 17
26 | 6 15 10 13 13 7 15 11 8 19 4 | 12 16 23 27 23 17 20 15 14 21 16
27E | 15 18 12 18 22 6 20 26 17 27 6 | 85 83 84 77 87 80 75 88 88 77 82
28 | 6 22 8 14 18 4 23 11 11 22 5 | 13 34 19 19 34 15 28 20 20 20 18
29 | 9 23 7 14 17 4 19 10 11 28 5 | 14 29 19 14 23 17 29 22 16 24 17
30 | 8 13 7 12 13 3 10 9 11 15 3 | 14 24 18 15 22 13 24 16 16 19 16
31E | 6 20 9 12 13 4 13 14 9 28 4 | 14 25 16 15 27 14 24 18 19 23 16
X32 | 7 21 8 27 --- 5 17 9 11 17 5 | 14 15 16 31 --- 12 15 18 12 16 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 21 9 13 18 6 17 12 12 20 |T 18 29 23 22 29 19 27 22 21 21 20
WRMS | 7 21 9 13 17 5 17 10 8 20 |NE 15 26 20 20 27 16 25 18 17 17 17
MEDI | 7 21 8 12 18 5 17 10 10 19 |MD 15 27 19 19 26 17 25 19 19 19 17
Table 3.1680.5 GPS week: 1680 Day: 5 MJD: 56009.000
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 | 8 26 10 11 17 6 13 9 14 16 4 | 16 29 20 24 23 19 24 20 20 23 17
2E | 7 22 9 11 30 5 22 10 8 17 5 | 13 25 17 11 22 13 20 11 14 16 12
3 | 14 15 9 10 17 5 15 11 12 16 4 | 11 21 16 12 20 13 19 12 13 11 11
4E | 10 22 10 11 15 10 17 11 23 16 5 | 9 27 15 14 19 17 25 16 27 18 13
5 | 7 23 8 9 21 6 22 9 12 22 4 | 24 30 25 20 25 20 27 21 22 20 20
6 | 9 16 9 11 13 5 17 11 11 15 4 | 10 22 17 16 20 11 16 17 16 15 13
7E | 6 18 11 13 19 9 17 13 13 11 4 | 11 18 14 15 14 11 17 14 10 13 9
8E | 13 24 7 13 22 10 24 15 31 21 6 | 47 51 49 44 50 44 51 52 53 53 46
9E | 17 23 22 14 23 10 24 15 25 25 7 | 80 78 71 78 79 77 79 75 76 75 74
10 | 5 14 10 11 23 5 14 13 9 14 4 | 13 15 15 18 23 13 15 15 19 17 14
11 | 6 16 10 12 24 7 12 9 8 21 4 | 17 29 19 19 27 20 25 18 19 18 16
12 | 7 27 10 13 20 6 22 14 8 23 5 | 13 30 22 19 24 15 27 16 14 13 14
13 | 6 21 8 12 21 7 16 11 9 20 4 | 18 31 21 22 36 21 29 19 21 15 18
14 | 9 25 12 16 17 8 18 18 15 20 5 | 21 31 32 29 34 26 29 28 25 22 24
15 | 7 28 16 18 18 6 23 10 12 20 5 | 17 29 27 25 29 18 26 15 20 16 18
16 | 9 30 9 14 18 4 26 8 10 24 5 | 12 26 19 16 27 14 27 11 19 12 13
17 | 7 21 12 12 18 4 21 18 11 45 6 | 11 27 17 14 21 14 29 20 17 32 12
18 | 9 30 16 15 20 5 25 14 12 22 6 | 17 34 23 19 27 16 28 20 17 19 16
19 | 7 24 12 10 17 5 21 7 7 23 4 | 14 28 14 12 20 14 25 12 16 19 12
20 | 7 26 8 8 20 5 15 12 8 19 4 | 23 37 26 25 26 24 28 27 25 27 23
21E | 8 24 10 12 18 5 14 6 13 10 4 | 15 27 17 17 28 17 22 14 18 17 15
22 | 9 31 17 13 21 7 24 16 9 19 6 | 22 35 31 24 36 23 29 27 23 22 22
23 | 7 23 7 13 19 4 15 7 10 24 4 | 21 30 21 23 27 21 24 19 25 16 19
X24 | 4 --- --- --- --- 52 --- --- --- --- 0 | 41 --- --- --- --- 25 --- --- --- --- 39
25 | 4 21 9 14 15 4 17 12 9 16 4 | 15 26 21 20 28 16 29 19 20 18 16
26 | 8 18 11 9 14 6 18 12 11 24 4 | 20 19 20 18 23 18 21 23 17 20 17
27E | 14 21 20 12 36 6 20 25 14 28 7 | 103 106 110 105 106 104 105 112 109 104 106
28 | 9 24 12 13 39 7 21 14 12 24 6 | 13 33 25 21 40 16 29 20 17 20 17
29 | 8 27 10 9 18 5 20 8 5 30 5 | 12 31 17 13 18 13 27 14 12 23 14
30 | 8 17 7 11 19 5 15 10 11 12 4 | 10 22 19 16 21 14 22 16 20 20 14
31E | 7 19 14 10 18 4 17 18 13 20 5 | 12 23 21 19 20 15 22 20 17 14 14
32 | 9 19 8 7 17 4 14 7 10 15 3 | 17 23 23 22 23 20 21 23 22 22 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 23 12 12 21 6 19 13 13 21 |T 21 32 25 24 30 22 29 24 24 24 22
WRMS | 8 23 11 12 19 6 19 11 10 20 |NE 17 27 21 19 26 17 25 18 19 19 17
MEDI | 8 23 10 12 19 5 18 11 11 20 |MD 15 29 21 19 25 17 26 19 19 19 16
Table 3.1680.6 GPS week: 1680 Day: 6 MJD: 56010.000
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 | 9 24 6 10 16 5 11 8 10 16 4 | 17 28 24 23 24 18 23 22 21 25 19
2E | 8 28 10 11 19 5 21 13 13 14 5 | 16 29 24 17 22 17 24 17 18 20 17
3 | 11 12 8 9 13 5 10 14 8 13 3 | 13 21 22 19 21 15 24 19 17 12 16
4E | 13 27 8 11 20 9 17 16 26 19 6 | 14 36 22 16 25 19 27 23 31 19 18
5 | 8 24 9 13 21 7 23 11 17 24 5 | 21 31 24 22 27 19 28 20 22 21 20
6 | 8 13 10 8 11 5 11 13 6 12 3 | 16 22 25 23 23 19 23 24 19 19 20
7E | 8 17 9 11 15 5 18 9 6 10 4 | 16 22 19 18 15 14 21 16 15 15 16
8E | 16 24 12 13 17 9 26 14 23 21 6 | 35 45 43 36 39 35 43 39 46 45 38
9E | 15 20 9 14 19 8 20 15 25 24 6 | 70 70 66 71 67 71 66 71 77 61 68
10 | 7 15 8 9 21 5 12 13 12 15 4 | 18 17 24 25 31 19 19 22 23 21 20
11 | 6 13 7 13 21 4 10 9 7 23 4 | 19 28 25 24 26 20 24 22 23 23 20
12 | 8 26 7 12 19 6 20 12 10 24 5 | 12 30 23 20 25 16 25 21 15 15 15
13 | 8 22 7 14 20 4 17 10 10 22 4 | 18 33 23 30 36 22 30 25 24 25 22
14 | 10 21 6 12 18 6 17 15 10 21 4 | 21 28 28 31 36 25 28 28 25 24 24
15 | 7 27 7 15 20 6 22 8 14 19 5 | 17 29 26 30 34 20 25 16 23 17 20
16 | 9 29 10 13 15 6 23 10 9 23 5 | 16 29 21 22 26 15 27 14 15 15 16
17 | 9 23 11 13 15 4 20 18 9 56 6 | 16 29 21 14 23 16 30 21 18 49 16
18 | 8 26 6 15 20 4 22 10 16 28 5 | 17 32 23 22 28 21 30 20 25 30 19
19 | 8 23 8 9 13 7 17 8 8 25 4 | 14 29 15 16 18 14 27 16 18 22 15
20 | 8 26 11 11 31 5 18 12 6 20 5 | 24 43 27 33 37 25 31 29 28 38 26
21E | 10 22 8 11 17 6 17 6 14 14 4 | 25 36 29 27 26 21 33 23 22 23 25
22 | 7 22 10 10 20 5 17 14 11 20 4 | 19 29 28 26 34 20 28 25 23 24 21
23 | 7 25 8 14 19 4 14 9 12 23 4 | 15 30 22 29 26 20 24 23 21 18 18
X24 | 5 --- --- --- --- 92 --- --- --- --- 0 | 26 --- --- --- --- 68 --- --- --- --- 26
25 | 7 20 6 13 13 4 15 12 13 13 4 | 20 26 25 22 28 19 31 25 18 20 20
26 | 12 18 8 12 13 5 18 13 12 24 4 | 16 20 23 25 26 16 20 21 22 18 18
27E | 12 17 13 15 25 9 19 21 15 28 6 | 110 114 120 115 108 113 113 110 114 120 112
28 | 10 25 10 15 21 6 20 11 8 24 5 | 16 34 28 30 35 19 29 24 23 25 23
29 | 8 24 5 11 14 6 19 9 8 30 4 | 19 32 20 15 18 18 32 18 20 26 19
30 | 9 14 5 12 15 6 13 10 7 15 3 | 16 23 17 19 19 15 25 19 19 17 17
31E | 9 19 8 15 18 4 18 15 8 16 4 | 15 22 24 21 20 14 23 16 15 15 16
32 | 9 20 7 22 20 6 14 12 8 16 4 | 14 25 23 35 23 18 20 27 20 25 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 22 9 13 18 6 18 12 13 23 |T 22 32 28 28 30 25 30 26 26 27 24
WRMS | 8 22 8 12 17 5 17 11 9 21 |NE 17 28 23 24 27 20 26 21 20 22 19
MEDI | 8 22 8 12 19 5 18 12 10 21 |MD 17 29 24 23 26 19 27 22 22 22 19
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 4.1680 GPS week: 1680 MJD: 56004.0-56010.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 |U 5 4 10 |U 10 13 32 |U 13 28 47 |
emr | emr 2960 | 7 8 19 |U 12 13 35 | 17 40 54 |
esa | esa 2976 | 5 5 13 |U 10 12 32 | 18 28 52 |
gfz | gfz 2959 |U 8 7 17 |U 18 17 48 |U 15 33 55 |
grg | grg 2962 | 9 12 24 |U 12 21 43 | 22 46 57 |
igr | igr 2971 | 5 5 12 | 10 12 31 | 13 28 49 |
igs | igs 2930 | 5 6 14 | 10 13 31 | 14 39 54 |
jpl | jpl 2960 | 7 7 18 |U 10 13 33 |U 18 41 56 |
mit | mit 2976 | 8 7 18 |U 10 13 33 | 19 40 58 |
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 5.1680.0 GPS week: 1680 Day: 0 MJD: 56004.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 | 5 4 12 | 9 11 33 | 7 11 18 |
emr | emr 2960 | 6 10 16 | 16 13 47 | 12 12 21 |
esa | esa 2976 | 5 6 12 | 10 11 33 | 8 14 17 |
gfz | gfz 2959 | 8 7 15 | 20 15 46 | 9 16 24 |
grg | grg 2976 | 7 8 17 | 10 11 37 | 10 16 24 |
igr | igr 2975 | 5 6 10 | 11 10 37 | 7 11 20 |
igs | igs 2915 | 5 6 18 | 10 10 34 | 8 10 20 |
jpl | jpl 2960 | 6 9 17 | 10 13 36 | 13 12 28 |
mit | mit 2976 | 19 19 29 | 10 12 35 | 17 12 52 |
Table 5.1680.1 GPS week: 1680 Day: 1 MJD: 56005.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 7 5 12 | 12 11 35 | 6 9 18 |
emr | emr 2960 | 7 8 18 | 13 12 35 | 15 12 19 |
esa | esa 2976 | 6 6 15 | 11 11 34 | 7 12 19 |
gfz | gfz 2960 | 9 7 24 | 19 16 53 | 13 15 18 |
grg | grg 2976 | 6 7 23 | 11 12 39 | 10 12 26 |
igr | igr 2976 | 5 6 15 | 11 11 31 | 7 14 18 |
igs | igs 2934 | 5 5 11 | 11 13 33 | 10 9 22 |
jpl | jpl 2960 | 13 8 21 | 11 13 34 | 12 7 16 |
mit | mit 2976 | 6 5 20 | 12 12 36 | 10 9 21 |
Table 5.1680.2 GPS week: 1680 Day: 2 MJD: 56006.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 4 5 11 | 9 13 36 | 11 33 21 |
emr | emr 2960 | 7 8 17 | 9 12 37 | 19 46 34 |
esa | esa 2976 | 5 6 16 | 9 12 40 | 12 26 24 |
gfz | gfz 2959 | 7 7 19 | 20 18 51 | 18 37 36 |
grg | grg 2976 | 6 7 23 | 10 14 42 | 21 47 44 |
igr | igr 2976 | 5 5 15 | 9 13 36 | 11 38 22 |
igs | igs 2961 | 5 6 15 | 9 12 36 | 18 39 30 |
jpl | jpl 2960 | 7 7 20 | 9 15 40 | 22 43 35 |
mit | mit 2976 | 5 5 16 | 9 13 38 | 19 39 33 |
Table 5.1680.3 GPS week: 1680 Day: 3 MJD: 56007.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 | 5 7 11 | 15 18 50 | 13 30 28 |
emr | emr 2960 | 7 12 21 | 16 20 49 | 15 44 60 |
esa | esa 2976 | 6 8 14 | 15 18 51 | 14 36 30 |
gfz | gfz 2957 | 6 8 13 | 23 21 61 | 17 47 55 |
grg | grg 2976 | 7 10 17 | 17 20 57 | 16 37 49 |
igr | igr 2976 | 6 8 12 | 14 19 47 | 12 31 26 |
igs | igs 2954 | 6 9 16 | 16 19 46 | 16 44 58 |
jpl | jpl 2960 | 8 10 19 | 15 19 51 | 14 40 60 |
mit | mit 2976 | 6 8 15 | 17 20 60 | 17 47 49 |
Table 5.1680.4 GPS week: 1680 Day: 4 MJD: 56008.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 4 2 10 | 10 20 28 | 27 36 114 |
emr | emr 2960 | 7 7 22 | 11 16 29 | 24 82 106 |
esa | esa 2976 | 5 4 13 | 10 14 23 | 57 44 199 |
gfz | gfz 2959 | 8 4 15 | 12 25 39 | 18 26 125 |
grg | grg 2880 | 14 18 33 | 14 38 50 | 59 103 136 |
igr | igr 2976 | 5 3 12 | 9 16 24 | 20 25 127 |
igs | igs 2963 | 5 5 15 | 9 17 26 | 21 87 113 |
jpl | jpl 2960 | 7 6 20 | 11 14 28 | 38 100 125 |
mit | mit 2976 | 6 5 15 | 9 17 26 | 36 93 108 |
Table 5.1680.5 GPS week: 1680 Day: 5 MJD: 56009.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 4 4 7 | 9 11 22 | 21 70 110 |
emr | emr 2960 | 7 7 19 | 10 11 23 | 25 76 119 |
esa | esa 2976 | 5 5 10 | 10 8 23 | 20 54 57 |
gfz | gfz 2960 | 9 8 17 | 16 14 41 | 17 76 109 |
grg | grg 2976 | 18 28 43 | 14 48 52 | 22 94 99 |
igr | igr 2961 | 4 5 9 | 7 9 20 | 24 68 116 |
igs | igs 2964 | 6 5 14 | 9 10 19 | 15 73 112 |
jpl | jpl 2960 | 7 7 16 | 9 9 22 | 17 76 112 |
mit | mit 2976 | 6 5 17 | 7 10 21 | 23 69 118 |
Table 5.1680.6 GPS week: 1680 Day: 6 MJD: 56010.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 4 3 9 | 6 7 19 | 7 8 19 |
emr | emr 2960 | 5 6 21 | 7 7 24 | 10 9 23 |
esa | esa 2976 | 4 3 9 | 6 7 18 | 8 10 19 |
gfz | gfz 2961 | 8 8 14 | 16 13 44 | 12 15 19 |
grg | grg 2976 | 6 5 14 | 6 8 25 | 13 15 21 |
igr | igr 2961 | 4 3 8 | 6 7 20 | 7 7 17 |
igs | igs 2823 | 4 3 9 | 7 8 21 | 10 10 21 |
jpl | jpl 2960 | 5 5 11 | 7 7 21 | 9 7 19 |
mit | mit 2976 | 6 5 15 | 7 7 20 | 12 12 25 |
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 6.1680 GPS week: 1680 MJD: 56004.500-56010.500
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 -33 7 6 0 | 9 27
| 16 21 76 64 6 | 2
emr uuuuu | 46 -17 -104 129 -8 | 74 79
| 21 48 161 107 4 | 3
esa uuuuu | -13 -31 -41 -97 0 | 11 29
| 14 16 120 46 5 | 2
gfz uuuuu | -44 46 39 -184 -8 | 10 29
| 23 24 53 143 5 | 6
grg uuuux | 17 -10 11 -100 -40 | 11 44
| 14 19 65 39 27 | 17
igr xxxxx | -18 -4 0 -41 -7 | -1 25
| 21 18 55 48 8 | 3
irf xxxxx | 5 -7 -9 -15 8 | -5 20
| 6 6 20 17 4 | 2
jpl uuuuu | 26 -40 140 18 2 | 49 54
| 26 28 105 48 14 | 2
mit uuuuu | -7 0 -29 62 -3 | 13 28
| 18 18 67 69 6 | 4
ngs uuuuu | -17 28 2 165 6 | 3 19
| 45 36 66 92 5 | 2
sio uuxuu | 69 39 -475 62 -12 | 82 86
| 20 17 88 67 4 | 5
Table 7.1680.0 GPS week: 1680 Day: 0 MJD: 56004.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 3 -11 74 -50 1 | 13 22
emr uuuuu | 42 25 -356 78 -9 | 80 82
esa uuuuu | -19 -41 89 -71 -8 | 14 22
gfz uuuuu | -66 13 -1 -313 -19 | 21 26
grg uuuux | 16 17 -47 -150 -16 | 37 61
igr xxxxx | -32 4 -23 -72 -11 | 6 16
irf xxxxx | 5 -5 -29 -10 12 | -3 12
jpl uuuuu | 48 -59 1 48 28 | 50 51
mit uuuuu | 7 5 -73 105 -9 | 20 23
ngs uuuuu | -29 73 115 206 9 | 6 13
sio uuxuu | 91 14 -584 162 -8 | 89 90
Table 7.1680.1 GPS week: 1680 Day: 1 MJD: 56005.500
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 -53 27 57 2 | 9 24
emr uuuuu | 45 38 -205 223 -3 | 75 78
esa uuuuu | -21 -40 -95 -56 -1 | 11 25
gfz uuuuu | -37 42 81 -242 -5 | 14 27
grg uuuux | 7 -6 45 -115 -17 | 27 56
igr xxxxx | -21 -39 117 -50 2 | 0 22
irf xxxxx | -3 -17 21 -26 9 | -5 16
jpl uuuuu | 33 -54 206 -19 3 | 48 49
mit uuuuu | -30 -37 39 49 -11 | 15 25
ngs uuuuu | 10 80 -43 172 6 | 3 16
sio uuxuu | 64 17 -408 50 -13 | 85 88
Table 7.1680.2 GPS week: 1680 Day: 2 MJD: 56006.500
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 -17 -33 55 6 | 6 25
emr uuuuu | 49 33 -210 217 -2 | 73 77
esa uuuuu | -16 -9 95 -150 9 | 9 26
gfz uuuuu | -85 27 50 -262 -5 | 10 28
grg uuuux | 4 -18 -79 -113 -29 | 18 53
igr xxxxx | -27 -8 -5 5 4 | -2 24
irf xxxxx | 0 -1 -29 -28 1 | -8 19
jpl uuuuu | 39 -26 178 -74 12 | 46 49
mit uuuuu | -10 5 -147 96 -3 | 12 27
ngs uuuuu | -3 -16 33 252 -2 | 1 17
sio uuxuu | 87 51 -587 74 -7 | 82 86
Table 7.1680.3 GPS week: 1680 Day: 3 MJD: 56007.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 20 -48 16 -13 1 | 9 30
emr uuuuu | 68 -36 84 274 -13 | 76 81
esa uuuuu | -13 -10 -55 -167 -1 | 13 33
gfz uuuuu | -38 65 -34 -265 -9 | 11 30
grg uuuux | 16 -42 94 -87 -18 | 7 27
igr xxxxx | -21 9 -11 -54 -1 | 0 28
irf xxxxx | 5 0 -22 -8 14 | -5 23
jpl uuuuu | 53 -82 147 34 -14 | 51 57
mit uuuuu | -16 18 -54 70 -5 | 15 31
ngs uuuuu | -35 16 -23 195 13 | 3 22
sio uuxuu | 61 57 -499 95 -17 | 85 89
Table 7.1680.4 GPS week: 1680 Day: 4 MJD: 56008.500
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 | -21 -16 52 -59 1 | 10 30
emr uuuuu | 53 -68 12 77 -8 | 74 80
esa uuuuu | 17 -49 38 -99 -3 | 12 33
gfz uuuuu | -16 78 9 -228 -4 | 7 31
grg uuuux | 8 -11 -11 -121 -71 | 4 29
igr xxxxx | -41 -6 -50 -117 -14 | -1 29
irf xxxxx | 13 -10 -13 -12 6 | -5 23
jpl uuuuu | 9 7 -14 40 0 | 50 57
mit uuuuu | 2 4 14 84 2 | 12 32
ngs uuuuu | -80 15 -64 213 4 | 3 22
sio uuxuu | 80 38 -426 30 -13 | 81 86
Table 7.1680.5 GPS week: 1680 Day: 5 MJD: 56009.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 3 -63 -145 103 -2 | 8 29
emr uuuuu | 61 -69 41 -3 -13 | 72 78
esa uuuuu | -21 -37 -216 -47 2 | 10 32
gfz uuuuu | -32 65 123 -70 -5 | 5 30
grg uuuux | 20 -11 83 -84 -82 | -4 38
igr xxxxx | 25 -6 -34 -28 -16 | -3 30
irf xxxxx | 13 -9 3 17 4 | -6 23
jpl uuuuu | 23 -32 224 64 -9 | 50 56
mit uuuuu | 20 12 -8 114 4 | 10 30
ngs uuuuu | -46 -2 -52 -31 3 | 2 22
sio uuxuu | 70 47 -469 79 -9 | 77 83
Table 7.1680.6 GPS week: 1680 Day: 6 MJD: 56010.500
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 | 17 -19 58 -47 -12 | 9 29
emr uuuuu | 2 -43 -92 36 -8 | 71 77
esa uuuuu | -20 -27 -144 -89 1 | 11 33
gfz uuuuu | -35 32 45 91 -10 | 3 30
grg uuuux | 45 5 -4 -28 -50 | -13 47
igr xxxxx | -8 17 8 27 -13 | -5 30
irf xxxxx | 0 -8 7 -35 8 | -5 23
jpl uuuuu | -23 -31 242 32 -3 | 49 56
mit uuuuu | -23 -3 29 -86 3 | 10 30
ngs uuuuu | 61 34 51 150 6 | 2 22
sio uuxuu | 33 50 -354 -58 -14 | 76 82
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