[IGSREPORT-20028] Wk 1646 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 11 04:50:58 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1646 (Jul 24, 2011 - Jul 30, 2011)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1646[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1646[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1646[0-6].cls IGS GPS clock combination summary report.
igs16467.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16467.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 | 6 3 6 26
0 | ESA | 6 30 6 UNSA
0 | GFZ | 19
0 | GRG | NKLG SANT
0 | JPL | 15 19 25 26 GUAT
0 | MIT | 16 19 26 30 3 16 19 26 30 CAS1 CAS1 CEDU MDVJ
1 | COD | MCM4 MCM4
1 | EMR | 26
1 | ESA | UNSA
1 | GFZ | MDVJ
1 | GRG | IRKJ SANT
1 | JPL | 6 25 26
1 | MIT | 5 26 30 3 26 30 DAV1 MDVJ DAV1 MDVJ
2 | EMR | 3 6
2 | ESA | NTUS UNSA
2 | GFZ | 22 BOGT HOLM MDVJ NKLG RIOP
2 | GRG | SANT
2 | JPL | 15 25 26 PRDS
2 | MIT | 1 11 26 30 1 3 6 11 26 30
3 | COD | IISC
3 | EMR | 3 6 3 6
3 | ESA | 3 IRKJ UNSA
3 | GFZ | 31 DAV1 MAS1 MDVJ NTUS
3 | GRG | IRKJ
3 | JPL | 25 26
3 | MIT | 1 6 26 30 1 6 26 30 DAV1 NTUS USNO DAV1 NTUS USNO
4 | COD | ALGO
4 | EMR | 3 6 3 6
4 | ESA | UNSA
4 | GFZ | MDVJ
4 | GRG | SANT
4 | JPL | 3 18 25 26
4 | MIT | 1 3 6 15 26 30 1 3 6 15 26 30 DAV1 MDVJ NNOR MDVJ
4 | MIT | NNOR
5 | EMR | 3 6 3 6
5 | ESA | BJFS UNSA
5 | GFZ | MDVJ
5 | GRG | CEDU
5 | JPL | 3 15 25 26 CEDU
5 | MIT | 1 26 30 31 1 3 6 26 30 MDVJ USNO
6 | EMR | 3 6 3 6 MATE MATE
6 | ESA | UNSA
6 | GFZ | MATE MDVJ
6 | JPL | 25
6 | MIT | 1 3 6 25 26 30 1 3 6 25 26 30 MAW1 BOR1 MAW1
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
1 | GRG | 30
3 | GRG | 30
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G01 | 4 | 2 | 2 | 1 | | | 1 |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
8. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .2 .4 .3 -9 -6 14 .0
EMR | -1.9 -4.2 -.2 1 11 10 .37
ESA | -.3 -9.1 11.9 -66 -4 95 .10
GFZ | -1.3 .2 -.1 -24 19 5 .04
GRG | 4.3 -5.0 13.5 -7 -6 -8 .0
JPL | -2.4 2.2 -10.1 -42 88 57 -1.22
MIT | 3.9 -11.0 22.1 -8 6 -18 .0
NGS | 1.7 -.5 13.9 -37 22 -6 .04
SIO | 5.8 -5.1 -4.8 -97 -131 19 -.03
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution does not yet use IGS08/igs08.atx, which causes their RMS
clock residuals to be higher than for the other centres; for the same
reason, the JPL solution is excluded from the weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1646.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1646.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 2.1646.[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 3.1646.[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 5.1646.0-6).
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 1646 summary. (Jul 24, 2011 - Jul 30, 2011)
Table 1.1646.a GPS week: 1646 MJD: 55766.000-55772.000
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 253| 0 0 -2 -25 5 19 -.21 8 7 | -252 51 16 76
| 0 0 0 17 6 20 .03 | 600 712
emr 95| 0 0 -7 -79 10 -13 .38 18 18 | 2781 349 18 117
| 1 2 1 35 19 11 .02 | 1068 1200
esa 124| 1 0 0 -2 61 24 .26 8 8 | -408 -620 19 162
| 1 0 0 15 12 17 .03 | 1198 2134
gfz 197| 0 0 3 -5 -65 -25 -.28 13 12 | -77 219 24 135
| 1 1 1 116 73 21 .02 | 162 251
grg 131| 1 1 10 -32 31 -4 .72 16 14 | 1685 317 46 227
| 0 1 1 28 30 14 .08 | 962 1107
igr n/a| 0 0 1 -30 -2 -61 -.09 5 5 | 6019 533 21 98
| 0 0 0 15 25 5 .03 | 1363 1190
jpl 137| -1 0 -12 9 -181 -4 .54 18 18 | 1281 322 22 303
| 0 0 1 15 12 29 .04 | 954 1092
mit 268| 0 -1 2 -16 -48 -29 -.36 13 10 | 751 -497 24 197
| 0 0 1 32 22 15 .04 | 1551 2272
ngs 225| 0 0 2 43 -44 -15 -.18 10 7 | -6438 90283 2022 3723
| 1 0 1 58 36 23 .04 | 123283 578438
sio 252| 0 2 -2 160 252 10 -.29 19 19 | --- --- --- ---
| 1 1 1 27 16 8 .02 | --- ---
Table 1.1646.b GPS week : 1646 MJD: 55766.000-55772.000
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 | 46 33 25 25 25 17 19 |
2 | 4 5 4 5 5 4 4 |
3 | 6 6 5 6 6 5 6 |
4 | 3 3 3 4 4 4 4 |
5 | 4 5 4 5 5 5 5 |
6 | 5 6 6 6 6 6 6 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 4 4 4 4 |
9 | 4 4 4 4 4 4 4 |
10 | 3 3 3 4 3 3 4 |
11 | 3 3 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 5 4 4 4 5 |
14 | 5 4 4 4 4 4 4 |
15 | 4 4 4 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 4 5 4 5 4 5 4 |
19 | 4 4 4 4 4 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 4 5 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 4 4 5 |
24 | 3 3 3 3 3 4 4 |
25 | 5 5 6 5 5 5 5 |
26 | 6 7 6 6 6 6 6 |
27 | 4 4 5 4 4 4 4 |
28 | 4 4 4 5 4 5 4 |
29 | 5 5 5 5 5 5 5 |
30 | 7 10 8 10 10 9 10 |
31 | 6 4 4 5 5 5 5 |
32 | 3 4 4 3 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1646.0 GPS week: 1646 Day: 0 MJD: 55766.000
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 253| 0 0 -2 -21 1 33 -.23 7 6 | -61 111 19 85
| 30 2 |
emr 95| 0 -1 -7 -43 24 -32 .38 18 18 | 703 2216 15 116
| -3 -81 |
esa 124| 1 0 0 -16 60 11 .25 7 7 | 138 -744 16 147
| 35 -24 |
gfz 197| 0 2 2 -35 -43 -25 -.26 13 13 | -8 367 23 132
| -16 6 |
grg 131| 1 1 11 -60 -26 -11 .66 15 13 | -41 1912 50 212
| 17 31 |
igr n/a| 0 0 2 -32 14 -53 -.09 5 5 | 3518 2350 21 88
| 26 -6 |
jpl 137| -2 0 -11 14 -192 20 .48 18 17 | -428 1908 24 319
| -73 -39 |
mit 281| 0 -1 1 -21 -51 -41 -.41 15 10 | 952 -374 26 171
| -3 37 |
ngs 225| 0 0 3 55 -31 -24 -.20 9 6 | 205411 -900425 2228 4098
| -45 -16 |
sio 252| -1 1 -2 164 249 5 -.30 19 17 | --- --- --- ---
| -78 -130 |
Table 2.1646.1 GPS week: 1646 Day: 1 MJD: 55767.000
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 253| 0 1 -3 -28 6 -13 -.22 8 7 | 116 -1184 17 65
| 45 -24 |
emr 95| 0 -1 -8 -67 45 -11 .39 18 18 | 3301 -1368 21 90
| 9 -88 |
esa 124| 0 0 1 4 58 46 .27 7 7 | 933 -2890 21 167
| 25 -21 |
gfz 197| 0 0 2 -74 -188 -15 -.29 13 12 | -84 269 24 136
| -31 45 |
grg 131| 0 0 12 -18 64 1 .63 16 14 | 2244 -1465 43 201
| -35 -119 |
igr n/a| 0 0 1 -31 7 -61 -.11 5 5 | 6229 -1232 21 103
| 35 16 |
jpl 137| -2 -1 -10 1 -172 31 .49 18 17 | 1754 -1413 23 310
| 74 8 |
mit 281| 0 0 0 -32 -79 -19 -.42 13 10 | 1674 -3318 24 220
| 0 41 |
ngs 225| 1 0 2 70 6 -39 -.23 10 7 | -219939 963078 1710 3891
| -31 -40 |
sio 252| 0 1 -4 163 228 4 -.29 19 17 | --- --- --- ---
| -79 -125 |
Table 2.1646.2 GPS week: 1646 Day: 2 MJD: 55768.000
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 253| 0 0 -1 10 8 32 -.16 7 7 | -1539 1206 14 77
| 2 -25 |
emr 95| 0 3 -10 -29 10 4 .40 18 18 | 1964 1133 17 117
| 0 -53 |
esa 124| 0 0 -1 23 53 10 .29 8 8 | 693 -2852 19 173
| 28 -14 |
gfz 197| 0 0 1 -191 -61 -44 -.25 11 11 | -229 343 26 145
| -31 35 |
grg 131| 1 2 9 10 44 24 .65 17 16 | 834 1101 44 249
| -76 -96 |
igr n/a| 0 0 1 -14 -23 -61 -.06 5 5 | 4826 1468 20 112
| 25 45 |
jpl 137| -2 0 -11 30 -179 -30 .56 19 18 | 371 1101 21 308
| -13 76 |
mit 281| 0 -1 3 -80 -58 -19 -.37 12 9 | -1991 2307 23 189
| 7 35 |
ngs 225| 1 0 4 144 -26 -7 -.18 10 8 | -30276 571242 2184 3994
| -90 54 |
sio 252| -2 2 -2 106 256 23 -.29 20 19 | --- --- --- ---
| -58 -136 |
Table 2.1646.3 GPS week: 1646 Day: 3 MJD: 55769.000
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 253| 0 0 -2 -25 5 -1 -.18 8 7 | -146 -142 18 84
| 74 -11 |
emr 95| 1 -3 -7 -82 -4 -20 .36 19 19 | 3657 -840 22 123
| 34 -42 |
esa 124| 0 0 0 -20 52 50 .28 9 9 | 301 -2418 22 168
| 33 -11 |
gfz 197| -2 1 5 -31 42 -2 -.30 14 12 | 106 70 26 135
| -12 31 |
grg 131| 1 3 11 -26 18 -3 .75 17 16 | 2483 -527 49 271
| -11 -17 |
igr n/a| 0 0 1 -56 -47 -66 -.05 5 5 | 6852 -346 24 95
| 51 14 |
jpl 137| -1 0 -12 -8 -175 6 .57 18 18 | 2024 -539 26 306
| 109 -34 |
mit 281| 0 0 1 2 -19 -11 -.35 11 8 | 1242 -1369 31 207
| -15 14 |
ngs 225| 0 0 2 48 -101 -30 -.11 9 8 | -160 -141 1784 3271
| 21 43 |
sio 252| 2 3 -4 174 281 9 -.25 18 19 | --- --- --- ---
| -94 -153 |
Table 2.1646.4 GPS week: 1646 Day: 4 MJD: 55770.000
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 253| 0 0 -2 -33 -1 39 -.21 7 7 | -142 384 17 73
| 23 16 |
emr 95| -2 0 -5 -103 -12 -6 .38 18 18 | 3144 728 19 128
| 67 -42 |
esa 124| 1 0 0 -8 48 9 .24 7 7 | -1527 1266 18 164
| 56 5 |
gfz 197| 1 0 4 135 -47 -33 -.31 15 14 | -359 454 27 137
| -43 39 |
grg 131| 0 0 11 -74 34 -9 .83 15 14 | 2107 804 48 211
| 70 -60 |
igr n/a| 0 0 1 -42 -8 -64 -.13 5 5 | 6584 1005 21 81
| 38 -5 |
jpl 137| -1 0 -12 26 -174 9 .55 18 18 | 1598 753 21 279
| -17 -5 |
mit 281| 0 0 3 11 -51 -22 -.36 12 10 | -387 2722 22 203
| -31 26 |
ngs 225| -1 0 2 -19 -65 -36 -.19 9 7 | -86 -1704 2303 3230
| 31 -6 |
sio 252| 1 4 -2 195 258 1 -.30 17 18 | --- --- --- ---
| -99 -149 |
Table 2.1646.5 GPS week: 1646 Day: 5 MJD: 55771.000
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 253| 0 0 -3 -41 18 16 -.22 8 7 | 306 -133 14 68
| 25 -30 |
emr 95| -1 -2 -7 -131 5 -16 .39 18 18 | 3508 170 20 130
| 94 -26 |
esa 124| 2 0 0 6 84 17 .26 9 9 | -1370 1416 20 161
| 44 1 |
gfz 197| 0 1 4 132 -126 1 -.28 11 12 | 33 315 22 145
| -37 -2 |
grg 131| 0 1 9 -34 31 -15 .82 15 13 | 2539 37 48 230
| 36 -25 |
igr n/a| 0 0 1 -10 27 -66 -.08 5 5 | 7403 76 21 113
| 0 -16 |
jpl 137| -1 -1 -14 12 -172 -50 .60 19 19 | 2177 14 19 291
| -16 178 |
mit 281| 0 -2 1 -12 -60 -36 -.34 13 11 | 2867 -2437 19 188
| -33 22 |
ngs 225| 0 0 1 -28 -21 13 -.17 10 8 | 293 -147 1892 3520
| 47 13 |
sio 252| 1 3 -1 150 241 22 -.28 19 18 | --- --- --- ---
| -100 -145 |
Table 2.1646.6 GPS week: 1646 Day: 6 MJD: 55772.000
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 253| 0 0 -2 -37 2 32 -.24 8 8 | -302 120 15 81
| 48 10 |
emr 95| -1 -1 -6 -97 4 -8 .36 17 17 | 3193 407 18 118
| 60 -34 |
esa 124| 1 0 1 -8 72 26 .22 8 8 | -2028 1882 17 160
| 50 -17 |
gfz 197| 0 0 2 28 -34 -55 -.27 10 11 | -3 -285 23 117
| 3 22 |
grg 131| 1 1 8 -21 56 -16 .74 15 14 | 1631 359 41 215
| 15 -29 |
igr n/a| 0 0 0 -27 11 -55 -.08 5 5 | 6726 416 20 97
| 38 11 |
jpl 137| -2 0 -11 -8 -206 -16 .50 18 18 | 1471 436 26 311
| 217 -48 |
mit 281| 0 -2 4 14 -17 -53 -.31 14 12 | 905 -1012 25 201
| -24 7 |
ngs 225| 0 0 1 31 -74 16 -.17 9 7 | -313 82 2054 4060
| -34 82 |
sio 252| 2 3 -1 171 252 9 -.32 22 22 | --- --- --- ---
| -96 -140 |
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 3.1646.0 GPS week: 1646 Day: 0 MJD: 55766.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 47 --- 45 --- --- 110 --- --- --- --- 46 | 42 --- 32 --- --- 77 --- --- --- --- 35
2 | 6 16 8 13 9 2 18 14 5 23 4 | 22 33 27 24 31 22 36 21 24 28 23
3E | 13 20 10 14 20 7 18 24 20 13 6 | 35 38 38 36 48 37 47 47 46 41 38
4 | 6 12 4 8 11 4 11 9 8 17 3 | 34 33 36 41 41 38 37 39 41 34 35
5 | 6 15 6 11 9 7 22 11 8 30 4 | 20 24 21 22 27 19 30 22 24 28 20
6E | 13 20 9 13 18 8 15 18 13 20 5 | 44 53 46 47 50 44 47 51 50 47 46
7 | 5 19 5 9 19 5 17 8 5 12 3 | 17 28 19 18 25 15 28 19 18 17 17
8 | 6 12 5 7 15 3 9 10 7 13 3 | 16 22 14 17 14 14 25 19 15 17 15
9 | 8 15 8 8 11 5 12 19 11 21 4 | 15 24 18 15 19 13 25 19 12 21 14
10 | 6 10 5 11 14 2 8 11 10 14 3 | 22 25 23 30 30 24 25 29 26 25 24
11 | 6 13 4 10 12 4 18 8 7 13 3 | 39 50 44 45 59 42 52 38 43 34 43
12 | 6 20 10 20 16 6 23 13 8 16 4 | 23 35 24 20 34 22 38 23 25 24 22
13E | 6 16 6 12 15 4 20 11 9 23 4 | 24 34 28 24 38 23 38 22 27 23 25
14E | 5 13 7 12 28 3 23 11 7 12 4 | 18 24 21 19 23 16 31 16 16 16 17
15E | 7 26 7 11 13 6 20 13 9 11 4 | 18 34 22 18 28 16 32 19 21 16 19
16 | 7 22 6 14 14 6 24 15 9 18 4 | 29 38 30 26 38 29 42 26 31 23 29
17 | 6 15 5 13 20 3 14 9 5 17 3 | 27 29 22 28 25 24 31 27 23 30 23
18 | 7 23 7 10 10 4 20 12 6 22 4 | 22 34 22 27 24 21 37 22 21 29 21
19 | 6 20 7 11 16 4 17 11 5 12 3 | 24 34 24 27 38 24 34 22 26 24 25
20 | 6 17 6 11 11 4 17 10 6 26 4 | 21 31 22 23 27 22 35 20 23 22 22
21 | 6 18 6 7 12 3 20 11 9 27 4 | 18 28 23 20 27 21 28 20 24 23 20
22 | 6 18 5 8 14 5 20 10 8 24 4 | 20 26 19 24 24 19 29 25 21 31 20
23E | 7 23 6 16 12 4 19 11 9 14 4 | 21 35 23 20 25 19 35 18 21 21 21
24 | 4 12 4 10 13 5 12 8 5 14 2 | 38 39 40 42 47 39 45 37 40 38 39
25 | 7 15 8 10 19 4 25 17 6 18 4 | 21 32 28 28 38 26 45 27 26 28 25
26E | 12 16 11 12 16 4 15 41 16 13 6 | 38 27 39 35 43 35 40 41 35 36 35
27 | 8 15 8 7 11 5 13 21 11 22 4 | 16 24 19 15 21 14 26 19 15 20 15
28 | 5 16 5 9 18 4 16 8 8 24 4 | 21 30 22 21 32 20 36 21 21 27 21
29 | 5 24 6 12 21 4 21 13 8 20 4 | 19 30 19 24 23 21 27 25 25 27 20
X30 | 8 19 12 --- --- 10 --- 14 --- --- 7 | 19 25 22 --- --- 17 --- 17 --- --- 18
31 | 8 19 6 32 17 4 19 17 8 18 5 | 16 26 18 29 29 13 25 19 14 18 15
32 | 6 14 3 11 12 5 12 10 6 16 3 | 19 23 22 20 26 19 30 17 21 26 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 13 15 5 18 15 9 19 |T 24 31 25 26 31 25 34 25 25 26 24
WRMS | 6 18 7 13 13 5 17 10 6 17 |NE 21 28 22 21 26 22 31 21 20 23 20
MEDI | 6 16 6 11 14 4 18 11 8 17 |MD 21 30 22 24 28 21 34 22 24 25 21
Table 3.1646.1 GPS week: 1646 Day: 1 MJD: 55767.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 34 --- 31 --- --- 56 --- --- --- --- 32 | 74 --- 85 --- --- 85 --- --- --- --- 79
2 | 6 19 9 19 12 5 23 13 7 24 4 | 21 33 28 31 29 24 36 27 24 26 25
3E | 13 16 9 12 17 6 17 23 21 14 5 | 31 37 37 34 41 35 44 40 38 38 34
4 | 6 12 6 10 10 4 12 8 9 19 3 | 24 24 28 32 27 26 24 30 26 24 25
5 | 5 17 6 15 20 6 24 11 10 27 4 | 17 21 19 22 26 18 25 22 21 24 18
6E | 15 21 9 14 20 8 19 23 19 21 6 | 30 38 31 32 39 29 38 31 37 30 30
7 | 7 19 5 12 17 5 18 8 6 13 3 | 12 24 16 16 24 13 24 12 13 13 12
8 | 7 14 5 10 10 4 9 7 6 12 3 | 12 17 15 18 15 12 19 17 14 14 13
9 | 9 16 7 13 10 8 13 15 8 20 4 | 20 25 22 24 25 19 27 27 24 25 21
10 | 5 14 7 13 11 6 10 10 5 13 3 | 19 20 21 24 21 20 17 26 20 23 20
11 | 7 12 4 10 15 3 16 6 7 15 3 | 31 45 37 36 51 35 50 31 35 29 36
12 | 8 21 7 19 20 3 24 10 9 15 4 | 16 33 24 24 33 20 32 21 18 19 19
13E | 6 17 5 12 14 4 18 10 8 26 4 | 21 30 24 22 29 22 31 21 21 28 21
14E | 7 12 7 11 16 5 21 9 9 14 3 | 22 25 26 24 28 21 29 20 23 19 22
15E | 6 25 6 15 10 6 20 12 10 13 4 | 16 27 22 21 25 16 26 17 19 14 17
16 | 8 22 6 15 16 5 21 13 12 19 4 | 27 35 31 25 33 28 38 25 26 25 27
17 | 14 17 5 12 15 7 16 8 9 19 4 | 31 37 34 34 32 32 38 36 33 34 32
18 | 6 20 10 14 11 4 23 12 8 22 4 | 18 29 21 27 22 18 31 16 16 22 17
19 | 6 20 5 12 13 4 14 10 9 10 3 | 23 30 25 27 32 24 28 20 25 22 23
20 | 8 15 8 15 12 5 14 7 10 26 4 | 14 25 24 23 21 18 28 14 19 16 18
21 | 6 14 7 10 12 3 20 8 5 28 4 | 19 29 23 22 28 19 30 18 20 22 20
22 | 5 17 9 9 9 5 18 11 10 23 4 | 18 24 21 23 21 18 24 22 19 29 18
23E | 5 21 5 14 16 4 19 9 7 20 4 | 20 32 27 18 24 20 30 20 20 24 21
24 | 5 10 4 10 13 5 10 6 8 15 3 | 31 35 36 34 37 34 38 29 33 33 33
25 | 7 18 7 15 19 4 24 14 7 18 4 | 16 32 24 22 35 19 39 21 20 21 20
26E | 12 17 10 14 27 8 14 38 13 15 6 | 43 29 41 43 52 42 46 61 47 45 44
X27 | 9 14 6 14 12 8 --- 15 10 17 4 | 18 23 21 23 25 18 --- 25 23 22 20
28 | 6 19 5 11 22 5 18 8 9 21 4 | 16 26 16 18 29 14 27 17 15 26 15
29 | 8 23 7 15 15 4 21 9 8 25 4 | 28 32 27 27 27 26 31 26 25 26 26
X30 | 13 20 18 --- 112 16 --- 15 --- --- 9 | 17 29 35 --- 9999 28 --- 15 --- --- 24
31 | 6 16 7 13 19 5 15 9 7 17 4 | 17 27 21 28 28 17 26 18 17 18 18
32 | 7 14 5 13 13 5 10 9 8 14 3 | 17 21 24 19 22 18 25 17 19 21 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 13 16 5 18 13 10 19 |T 23 28 27 25 29 24 31 23 23 24 24
WRMS | 7 18 7 12 14 5 17 10 7 17 |NE 21 26 27 22 26 23 28 19 19 21 23
MEDI | 7 17 7 13 15 5 18 10 8 18 |MD 19 29 24 24 28 20 30 21 21 24 21
Table 3.1646.2 GPS week: 1646 Day: 2 MJD: 55768.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 34 --- 40 --- --- 78 --- 28 --- --- 24 | 32 --- 44 --- --- 60 --- 730 --- --- 34
2 | 7 19 8 13 11 3 21 7 6 26 4 | 16 26 22 27 19 20 30 18 19 19 18
3E | 12 18 9 8 18 6 16 21 19 15 5 | 26 33 32 24 37 28 36 32 37 29 29
4 | 6 12 6 8 9 4 12 6 8 21 3 | 30 27 30 35 32 31 31 34 32 28 31
5 | 5 17 7 10 12 4 18 11 8 26 4 | 20 23 21 24 23 20 27 22 22 27 20
6E | 14 21 8 11 20 7 19 21 18 21 5 | 20 28 23 29 31 21 30 31 27 27 21
7 | 5 19 6 7 20 3 17 8 8 13 3 | 14 30 19 19 26 16 27 16 18 16 17
8 | 5 12 5 8 17 3 8 7 9 13 3 | 18 22 19 22 21 19 23 23 19 19 19
9 | 9 17 13 9 7 5 12 13 10 20 4 | 15 24 26 22 23 17 23 23 17 24 19
10 | 4 12 7 13 14 4 9 7 9 16 3 | 24 21 21 29 28 23 23 28 23 25 24
11 | 7 15 5 8 21 4 20 7 10 15 3 | 35 44 38 32 53 38 47 31 39 29 36
12 | 7 20 9 21 19 4 27 8 10 16 5 | 20 31 24 26 30 19 35 23 24 22 21
13E | 6 18 5 10 19 4 22 9 10 36 4 | 22 29 25 19 31 25 33 22 26 35 24
14E | 6 14 8 9 15 7 22 8 10 12 3 | 19 25 21 25 23 21 27 21 21 17 19
15E | 5 26 7 9 13 6 20 13 8 11 4 | 15 28 21 22 23 18 29 19 18 17 17
16 | 7 23 5 13 17 6 23 12 11 22 4 | 23 33 25 22 30 23 33 23 29 21 23
17E | 10 16 5 10 17 7 15 7 5 17 3 | 31 36 29 31 32 28 31 31 33 31 30
18 | 7 20 8 12 13 4 23 8 10 22 4 | 21 29 24 27 23 21 32 21 22 26 21
19 | 6 20 7 8 13 4 22 9 9 11 3 | 26 33 26 21 29 26 32 23 27 23 25
20 | 5 15 9 11 13 3 16 8 9 24 3 | 22 31 24 24 26 23 32 21 23 20 23
21 | 6 18 6 8 14 3 22 8 7 29 4 | 19 29 23 21 27 19 31 17 21 24 20
22 | 6 17 8 8 12 5 22 9 10 23 4 | 22 25 24 27 23 22 28 25 22 31 22
23E | 4 26 6 13 21 3 17 8 10 17 4 | 17 32 22 20 22 19 28 19 20 18 19
24 | 4 12 4 10 13 4 11 5 9 15 3 | 32 33 33 28 38 33 34 29 35 32 32
25 | 7 17 8 26 19 5 29 15 9 19 5 | 18 30 24 34 33 19 43 22 20 22 21
26E | 13 14 11 10 27 6 16 28 16 17 6 | 28 29 31 37 32 30 29 49 39 35 31
27 | 9 19 13 8 11 6 14 13 13 19 4 | 16 26 26 23 23 18 23 25 19 26 19
28 | 6 18 4 8 20 3 18 8 7 20 3 | 25 29 24 21 30 24 32 25 26 29 24
29E | 7 27 8 10 22 5 23 8 6 15 4 | 27 37 30 37 30 28 34 29 28 30 28
X30 | 13 23 13 --- --- 20 --- 8 --- --- 8 | 23 31 25 --- --- 25 --- 16 --- --- 21
31 | 8 17 9 11 21 5 16 14 7 21 4 | 22 29 23 21 31 19 28 22 23 21 21
32 | 6 14 7 10 12 5 15 6 9 18 3 | 18 25 22 22 24 20 28 18 20 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 8 11 17 5 19 12 10 20 |T 22 29 25 25 28 24 30 46 24 24 23
WRMS | 7 18 8 11 16 5 18 9 8 19 |NE 20 27 24 24 26 22 29 72 21 23 21
MEDI | 6 18 7 10 15 4 18 8 9 18 |MD 22 29 24 24 28 21 30 23 23 24 21
Table 3.1646.3 GPS week: 1646 Day: 3 MJD: 55769.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 36 --- 42 --- --- 34 --- 25 --- --- 25 | 93 --- 122 --- --- 112 --- 707 --- --- 104
2 | 7 19 10 14 12 4 23 7 8 23 4 | 23 30 23 26 26 22 36 22 27 23 21
3E | 12 17 10 11 19 7 18 21 15 17 5 | 29 34 32 29 36 32 38 39 38 36 31
4 | 5 14 10 9 16 5 14 4 7 20 3 | 37 34 34 41 39 37 33 36 36 32 35
5 | 6 18 9 15 16 4 22 9 10 26 4 | 19 26 16 22 25 21 30 22 22 29 19
6E | 15 25 12 14 17 7 18 21 15 22 6 | 39 47 47 42 44 39 55 44 50 48 42
7 | 8 18 7 10 16 7 16 6 6 16 3 | 19 30 23 19 28 21 31 20 21 21 19
8 | 7 14 9 11 20 4 9 8 6 13 3 | 19 26 20 19 21 20 26 21 20 19 18
9 | 9 12 9 10 11 4 13 12 9 15 3 | 19 21 16 18 21 17 28 22 23 22 18
10 | 4 13 9 10 20 4 12 8 8 15 3 | 24 26 21 26 28 25 25 29 26 26 24
11 | 7 15 6 13 19 4 20 7 7 15 4 | 34 48 44 45 55 40 50 35 41 33 39
12 | 7 19 12 20 20 4 24 8 9 13 4 | 22 34 25 21 34 23 39 23 28 23 23
13E | 5 18 6 10 19 5 20 9 9 16 4 | 26 35 30 25 37 29 40 23 30 24 27
14E | 7 14 9 13 23 4 18 7 7 11 4 | 21 24 23 22 29 21 31 22 23 21 20
15E | 7 31 8 10 15 7 22 11 5 10 4 | 19 32 20 17 29 17 31 19 21 18 19
16 | 7 21 9 12 15 6 22 12 10 20 4 | 27 34 24 22 27 24 36 24 25 25 24
17E | 5 25 8 11 16 7 16 6 9 18 4 | 27 40 27 27 27 27 34 31 25 30 26
18 | 7 21 9 14 15 4 20 9 8 22 4 | 22 30 20 26 28 22 33 22 22 28 21
19 | 5 21 6 14 18 4 16 9 7 12 4 | 22 33 24 31 33 23 28 19 27 23 23
20 | 7 17 7 13 11 6 18 7 7 23 4 | 22 28 21 25 26 22 33 20 22 17 21
21 | 7 17 6 11 15 5 20 9 7 28 4 | 22 30 21 19 30 21 30 19 20 24 20
22 | 7 18 8 9 15 4 17 7 7 24 4 | 23 26 19 25 26 23 27 25 25 33 21
23E | 5 23 7 16 17 5 20 8 8 19 4 | 23 32 25 19 27 24 36 19 25 23 22
24 | 4 11 5 11 16 6 13 6 8 16 3 | 36 37 39 41 42 37 38 34 35 36 36
25 | 7 18 9 27 15 7 25 13 9 16 5 | 23 35 25 38 34 26 44 24 31 27 26
26E | 14 16 10 16 22 6 20 25 15 16 6 | 58 41 56 57 63 56 61 66 60 58 57
27 | 10 16 8 8 14 4 12 13 9 16 4 | 19 25 16 18 23 17 27 21 20 22 17
28 | 7 20 9 11 20 7 19 10 9 21 4 | 23 34 19 23 28 24 34 24 29 30 22
29E | 8 25 14 17 16 6 21 12 11 12 5 | 33 39 33 33 34 31 35 33 34 32 32
X30 | 12 29 22 --- >>>> 15 --- 9 --- --- 10 | 20 30 29 --- 9999 22 --- 16 --- --- 17
31 | 7 17 6 26 15 4 15 11 8 19 4 | 17 28 19 35 27 16 26 16 14 16 16
32 | 5 13 5 12 13 8 14 6 5 16 3 | 19 22 20 24 25 19 29 17 20 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 9 14 17 5 18 11 9 18 |T 27 31 29 27 31 28 34 47 28 27 27
WRMS | 7 19 9 12 16 5 18 8 8 19 |NE 26 28 28 23 27 27 31 70 22 24 25
MEDI | 7 18 9 12 16 5 18 9 8 16 |MD 23 32 23 25 28 23 33 22 25 24 22
Table 3.1646.4 GPS week: 1646 Day: 4 MJD: 55770.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 35 --- 37 --- --- 29 --- 29 --- --- 24 | 82 --- 103 --- --- 95 --- 720 --- --- 90
2 | 5 18 8 16 11 4 22 9 10 24 4 | 17 25 19 19 22 15 25 18 20 19 16
3E | 13 16 9 11 15 6 19 23 19 14 5 | 26 33 31 26 36 29 38 39 36 32 29
4 | 7 12 6 13 13 3 15 7 10 20 3 | 26 28 31 33 33 28 24 30 32 26 27
5 | 6 19 8 16 15 4 22 12 10 31 5 | 17 25 20 23 23 17 29 20 21 28 17
X6E | 13 22 9 13 15 7 --- 23 17 --- 6 | 26 37 28 33 28 29 --- 37 33 --- 28
7 | 6 17 7 10 13 5 17 6 7 15 3 | 19 29 22 16 26 15 31 19 19 20 19
8 | 6 14 6 10 22 4 10 7 7 12 3 | 21 26 22 19 23 19 30 23 21 21 21
9 | 8 13 6 9 15 5 14 12 7 11 3 | 16 23 19 15 22 16 26 21 19 17 16
10 | 6 10 6 12 13 5 11 9 8 15 3 | 20 22 22 26 26 20 22 27 24 24 20
11 | 7 13 3 14 17 6 18 8 4 12 3 | 31 43 36 38 57 34 44 33 34 29 34
12 | 7 21 9 26 15 6 26 10 8 14 5 | 21 36 23 20 29 19 35 25 23 21 21
13E | 5 17 6 15 17 5 19 10 7 14 4 | 22 32 26 17 36 22 31 20 28 21 24
14E | 7 17 8 15 20 5 18 10 8 9 4 | 19 27 25 21 23 20 29 19 25 19 20
15E | 7 27 8 11 17 5 20 13 9 11 4 | 16 29 24 14 28 15 29 16 21 16 17
16 | 8 21 8 20 13 9 22 12 9 19 4 | 24 35 29 21 32 24 39 24 27 21 25
17E | 5 13 5 11 17 4 20 12 11 17 4 | 23 25 20 23 25 24 30 27 25 27 23
18 | 6 20 7 15 13 6 18 11 10 22 4 | 19 28 20 25 24 19 33 20 20 26 18
19E | 8 23 8 16 20 4 19 10 8 9 4 | 41 48 42 47 48 42 44 38 45 41 41
20 | 5 15 6 17 11 4 17 8 5 21 3 | 17 26 21 24 28 18 28 19 19 20 19
21 | 6 19 7 12 15 6 21 12 8 27 4 | 15 31 23 16 30 17 29 20 18 22 18
22 | 5 18 6 15 12 6 17 10 11 23 4 | 18 23 18 25 22 21 25 26 22 33 18
23E | 6 20 5 19 16 4 19 9 10 13 4 | 22 32 28 21 31 24 31 23 29 23 25
24 | 6 12 5 12 14 6 13 8 7 12 3 | 30 35 32 35 40 32 37 29 33 30 31
25 | 6 15 6 22 11 5 22 19 11 15 4 | 20 32 24 26 31 24 41 26 26 25 23
26E | 11 17 10 12 21 6 14 23 15 18 5 | 17 32 20 19 23 14 23 25 21 20 13
27 | 9 17 6 7 15 5 14 12 11 10 3 | 19 28 22 14 23 18 28 22 25 19 19
28 | 6 19 5 6 17 6 19 13 8 22 4 | 20 30 19 19 25 20 31 24 21 27 19
29E | 7 23 6 19 12 6 22 14 9 13 4 | 18 32 21 27 19 18 26 26 21 27 19
X30 | 15 23 21 --- --- 17 --- 9 --- --- 10 | 17 23 33 --- --- 21 --- 17 --- --- 17
31 | 6 18 7 20 13 5 22 15 9 17 4 | 16 27 21 21 24 15 27 18 18 17 16
32 | 6 13 6 16 15 3 11 8 8 13 3 | 13 21 20 17 26 14 24 14 18 21 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 15 15 5 18 12 9 17 |T 22 29 27 23 28 23 30 45 24 23 23
WRMS | 7 18 7 14 14 5 18 10 7 18 |NE 23 28 28 20 25 24 31 71 21 22 24
MEDI | 6 17 6 14 15 5 19 10 9 15 |MD 19 29 22 21 26 20 29 23 22 22 19
Table 3.1646.5 GPS week: 1646 Day: 5 MJD: 55771.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 23 --- 27 --- --- 35 --- 22 --- --- 17 | 72 --- 84 --- --- 80 --- 712 --- --- 74
2 | 6 19 10 9 13 7 22 10 8 25 4 | 15 27 23 24 23 16 26 17 18 17 16
3E | 9 18 9 8 18 6 17 21 16 16 5 | 28 34 30 28 38 30 37 37 35 30 29
4 | 5 13 7 7 13 5 11 9 9 24 3 | 32 33 34 39 38 34 31 39 35 34 33
5 | 6 17 11 12 11 4 19 12 10 35 5 | 17 23 20 18 19 15 24 20 16 30 15
6E | 11 19 8 11 23 5 17 21 13 21 5 | 40 49 48 46 52 43 50 49 44 42 44
7 | 5 19 11 10 12 5 19 8 8 14 3 | 11 25 22 18 26 14 30 14 11 13 13
8 | 6 15 9 10 12 6 10 9 9 10 3 | 12 21 17 17 15 14 20 18 15 16 13
9 | 10 13 11 7 14 5 14 13 9 13 4 | 16 21 20 18 24 14 28 18 18 17 15
10 | 4 10 7 10 13 4 12 8 9 16 3 | 21 22 23 23 23 20 19 28 22 25 21
11 | 7 14 5 11 15 4 18 10 7 13 3 | 32 42 36 33 53 32 43 30 33 27 33
12 | 6 21 13 16 16 5 25 8 7 15 4 | 16 33 22 20 28 16 31 21 18 20 17
13E | 5 17 11 13 11 5 19 9 7 11 3 | 16 24 20 16 30 15 32 14 14 15 16
14E | 9 15 11 9 19 5 20 11 11 9 4 | 21 27 30 20 27 21 31 22 24 21 21
15E | 5 29 11 10 16 5 23 14 11 12 4 | 20 27 23 20 31 17 30 20 18 20 18
16 | 7 20 10 15 13 9 21 14 12 19 4 | 23 30 24 16 26 20 32 22 23 19 20
17E | 7 17 6 8 11 6 18 15 10 24 4 | 19 21 17 23 18 19 22 23 22 28 18
18 | 5 19 9 11 14 4 25 11 9 22 4 | 21 27 20 21 23 19 43 19 19 26 18
19E | 6 18 10 14 13 6 21 12 7 22 4 | 25 31 28 30 33 27 34 25 30 27 26
20 | 5 16 10 14 11 5 18 9 9 23 4 | 16 23 23 21 22 17 26 17 20 18 17
21 | 7 21 7 9 15 4 24 14 11 27 5 | 20 33 23 18 31 20 40 23 22 28 20
22 | 7 15 7 7 10 4 17 11 10 27 4 | 17 21 18 21 19 16 29 22 21 32 16
23E | 6 22 7 15 16 5 18 9 8 12 4 | 24 33 29 25 28 27 34 25 31 28 26
24 | 6 16 5 12 14 5 13 8 9 16 3 | 36 35 36 39 40 35 35 34 38 35 35
25 | 9 14 12 22 14 6 25 16 10 18 5 | 17 29 24 32 28 22 43 21 20 24 20
26E | 16 17 8 8 22 8 18 22 20 19 5 | 44 41 43 46 51 42 46 48 46 45 43
27 | 11 15 10 6 13 6 12 13 8 14 4 | 16 23 21 19 24 16 26 20 21 22 17
28 | 7 20 7 8 14 6 22 15 8 21 4 | 16 29 18 17 26 15 33 21 18 27 16
29E | 10 22 9 15 19 6 24 19 9 18 5 | 21 30 25 23 22 21 30 27 23 28 21
X30 | 10 28 13 --- --- 14 --- 13 --- --- 8 | 19 30 23 --- --- 16 --- 15 --- --- 16
31 | 5 19 11 12 16 5 19 10 14 19 4 | 16 26 22 18 27 17 28 17 29 16 16
32 | 8 13 7 12 10 5 17 12 10 14 3 | 14 20 22 17 23 17 25 18 20 22 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 9 11 15 5 19 13 10 19 |T 22 28 27 24 28 23 31 45 24 25 23
WRMS | 7 18 9 12 13 5 19 11 8 18 |NE 20 26 25 19 24 21 31 68 19 21 20
MEDI | 7 17 9 10 14 5 18 12 9 18 |MD 19 27 23 21 26 19 31 21 21 25 18
Table 3.1646.6 GPS week: 1646 Day: 6 MJD: 55772.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 28 --- 26 --- --- 25 --- 26 --- --- 19 | 96 --- 106 --- --- 101 --- 741 --- --- 96
2M | 7 15 7 8 12 5 22 9 7 25 4 | 19 25 25 26 25 22 32 26 21 25 21
3E | 10 16 12 10 14 9 17 25 22 15 5 | 34 37 34 29 38 33 47 37 37 36 32
4M | 9 9 7 7 13 6 13 11 8 27 3 | 40 41 40 47 46 42 36 48 43 41 41
5 | 9 15 7 12 10 5 21 10 6 38 4 | 21 23 23 27 24 22 30 24 24 37 21
6E | 11 21 10 12 17 6 17 25 16 24 5 | 43 52 46 50 50 45 45 52 50 44 46
7 | 7 19 6 9 14 4 17 11 9 16 4 | 19 29 23 21 27 20 33 21 20 21 20
8 | 7 12 8 11 15 4 10 11 7 16 3 | 22 27 23 25 24 23 35 24 22 21 23
9 | 9 14 6 7 15 4 13 15 9 16 3 | 23 28 24 26 28 24 39 30 23 26 24
10M | 7 11 9 9 15 3 8 10 7 21 3 | 23 28 25 32 32 25 30 33 28 32 26
11M | 6 14 5 12 15 4 16 16 8 18 4 | 46 57 49 55 66 49 58 46 49 44 50
12 | 8 20 9 17 18 5 26 11 8 17 5 | 27 40 28 25 31 26 47 29 28 27 27
13E | 7 18 7 12 22 6 18 12 10 29 4 | 21 30 23 18 32 20 35 18 24 32 21
14E | 8 17 10 8 19 3 17 9 9 9 4 | 30 34 30 29 30 28 37 30 31 29 28
15E | 8 32 11 8 12 4 21 16 9 12 5 | 24 37 28 24 31 23 34 21 24 24 24
16 | 9 18 8 11 13 4 21 13 11 20 4 | 33 37 32 24 32 29 43 27 29 29 29
17E | 8 14 7 9 14 6 14 16 7 27 4 | 31 35 29 30 29 30 38 36 28 40 30
18 | 6 18 8 11 10 4 22 11 6 22 4 | 26 32 25 27 25 24 40 26 26 30 24
19E | 5 20 8 16 13 5 15 13 11 20 4 | 35 38 37 39 38 36 40 36 37 37 35
20M | 7 17 10 10 14 5 13 9 8 28 4 | 27 34 28 28 32 27 36 29 29 40 28
21 | 7 20 6 8 12 6 25 19 8 28 4 | 21 35 22 21 35 22 33 23 23 29 22
22 | 7 16 8 7 12 2 19 13 6 28 4 | 21 25 21 24 23 21 33 27 21 34 20
23E | 7 20 7 15 19 4 15 12 8 13 4 | 29 37 31 22 31 28 38 27 32 30 28
24M | 10 11 4 10 13 5 10 17 6 19 3 | 35 39 39 41 45 37 37 38 37 32 37
25 | 7 17 8 6 16 3 24 16 8 21 4 | 24 34 30 28 34 26 47 24 28 28 26
X26E | 15 --- 10 10 16 5 15 20 12 23 5 | 46 --- 41 46 43 41 43 53 46 44 43
27 | 9 17 7 9 13 5 12 12 7 13 3 | 20 27 22 21 26 20 34 22 21 20 20
28M | 8 21 8 8 14 5 19 14 7 23 4 | 25 36 24 24 29 23 41 27 23 33 24
29E | 8 21 10 11 24 6 23 17 6 22 5 | 21 31 21 22 24 19 31 27 24 34 21
X30 | 14 30 14 --- --- 20 --- 16 --- --- 10 | 20 31 24 --- --- 13 --- 14 --- --- 16
31 | 9 16 9 12 15 6 17 9 13 16 4 | 19 25 21 23 26 19 27 18 23 20 18
32M | 9 15 6 11 12 5 11 10 7 22 3 | 16 21 19 14 23 15 24 17 18 26 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 8 10 15 5 18 14 9 22 |T 29 33 31 28 32 29 37 51 28 31 29
WRMS | 8 17 8 10 14 5 18 12 7 22 |NE 28 30 30 24 27 27 36 75 24 26 27
MEDI | 8 17 8 10 14 5 17 13 8 21 |MD 24 34 25 26 31 24 36 27 26 30 24
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 4.1646 GPS week: 1646 MJD: 55766.0-55772.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 |U 8 10 23 |U 5 7 23 |U 12 10 30 |
emr | emr 2948 |U 12 10 25 |U 9 12 32 | 12 15 37 |
esa | esa 3072 | 8 10 22 |U 5 6 21 | 8 11 25 |
gfz | gfz 2866 |U 14 11 31 |U 5 7 21 |U 9 9 30 |
grg | grg 2879 | 15 12 32 |U 5 7 22 | 9 10 23 |
igr | igr 3017 | 8 10 21 | 5 7 22 | 13 12 46 |
igs | igs 3045 | 9 10 21 | 4 7 21 | 12 10 29 |
jpl | jpl 2838 | 15 12 31 |U 6 14 29 |U 13 13 43 |
mit | mit 3044 |U 9 10 22 |U 8 18 33 |U 21 16 48 |
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 5.1646.0 GPS week: 1646 Day: 0 MJD: 55766.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 9 14 23 | 5 7 19 | ---- ---- ---- |
emr | emr 2963 | 11 12 24 | 7 12 31 | ---- ---- ---- |
esa | esa 3072 | 10 14 22 | 4 5 19 | 3 6 21 |
gfz | gfz 2868 | 18 14 37 | 4 5 17 | ---- ---- ---- |
grg | grg 2880 | 19 14 35 | 5 7 21 | ---- ---- ---- |
igr | igr 2974 | 9 13 23 | 5 5 19 | 30 23 154 |
igs | igs 3029 | 12 13 23 | 4 5 19 | ---- ---- ---- |
jpl | jpl 2858 | 18 15 35 | 6 13 28 | 26 19 97 |
mit | mit 2976 | 8 11 22 | 7 19 34 | 31 23 153 |
Table 5.1646.1 GPS week: 1646 Day: 1 MJD: 55767.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 8 9 23 | 5 6 29 | 13 11 42 |
emr | emr 2963 | 11 11 22 | 10 16 36 | 11 10 39 |
esa | esa 3072 | 9 10 24 | 5 5 27 | 9 14 35 |
gfz | gfz 2869 | 14 11 32 | 5 5 29 | 6 10 36 |
grg | grg 2880 | 16 10 37 | 7 9 31 | 7 11 21 |
igr | igr 2955 | 9 11 25 | 6 6 29 | 8 11 33 |
igs | igs 3058 | 9 9 22 | 5 5 27 | 14 9 38 |
jpl | jpl 2772 | 13 13 27 | 7 15 43 | 10 11 35 |
mit | mit 2976 | 8 11 23 | 9 21 43 | 25 24 35 |
Table 5.1646.2 GPS week: 1646 Day: 2 MJD: 55768.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 7 7 19 | 6 7 27 | 8 9 16 |
emr | emr 2961 | 9 7 19 | 9 13 36 | 10 12 22 |
esa | esa 3072 | 7 8 18 | 5 7 25 | 8 8 17 |
gfz | gfz 2869 | 14 9 31 | 5 9 26 | 7 8 18 |
grg | grg 2880 | 11 10 24 | 6 6 28 | 8 8 21 |
igr | igr 3035 | 7 7 18 | 6 8 25 | 7 9 19 |
igs | igs 3046 | 7 7 16 | 5 7 27 | 7 8 17 |
jpl | jpl 2868 | 12 9 26 | 8 22 33 | 8 9 22 |
mit | mit 3072 | 11 9 17 | 8 19 32 | 8 9 23 |
Table 5.1646.3 GPS week: 1646 Day: 3 MJD: 55769.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 8 9 21 | 5 10 21 | 9 6 19 |
emr | emr 2961 | 24 10 30 | 10 12 27 | 9 6 14 |
esa | esa 3072 | 7 9 20 | 4 8 19 | 8 5 16 |
gfz | gfz 2869 | 16 10 26 | 5 8 21 | 8 5 15 |
grg | grg 2880 | 16 11 28 | 5 7 20 | 9 6 18 |
igr | igr 3051 | 8 8 19 | 5 8 19 | 8 5 15 |
igs | igs 3040 | 8 9 21 | 4 9 19 | 8 6 17 |
jpl | jpl 2863 | 16 13 30 | 6 14 21 | 9 5 19 |
mit | mit 3072 | 8 8 20 | 7 16 26 | 9 5 20 |
Table 5.1646.4 GPS week: 1646 Day: 4 MJD: 55770.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 10 12 30 | 5 8 24 | 8 10 23 |
emr | emr 2962 | 12 11 28 | 10 11 40 | 11 12 27 |
esa | esa 3072 | 9 10 27 | 5 7 19 | 8 9 20 |
gfz | gfz 2853 | 14 14 30 | 5 9 16 | 7 7 24 |
grg | grg 2879 | 14 15 28 | 5 7 19 | 8 9 24 |
igr | igr 3060 | 8 9 24 | 6 9 22 | 8 9 20 |
igs | igs 3043 | 9 9 27 | 5 8 19 | 8 10 21 |
jpl | jpl 2776 | 16 14 27 | 8 14 28 | 9 10 31 |
mit | mit 3072 | 13 11 32 | 9 17 31 | 11 12 32 |
Table 5.1646.5 GPS week: 1646 Day: 5 MJD: 55771.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 8 9 19 | 4 6 20 | 11 8 29 |
emr | emr 2956 | 8 10 22 | 8 7 26 | 14 10 34 |
esa | esa 3072 | 8 10 19 | 5 5 17 | 11 7 29 |
gfz | gfz 2868 | 13 9 30 | 4 5 17 | 12 9 28 |
grg | grg 2879 | 15 11 35 | 5 6 17 | 12 8 26 |
igr | igr 3000 | 8 8 17 | 5 6 18 | 11 7 31 |
igs | igs 3045 | 8 9 17 | 3 5 15 | 11 8 28 |
jpl | jpl 2862 | 14 11 37 | 5 11 25 | 13 9 35 |
mit | mit 3072 | 7 7 17 | 7 15 31 | 11 8 31 |
Table 5.1646.6 GPS week: 1646 Day: 6 MJD: 55772.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 9 11 23 | 5 7 20 | 25 18 52 |
emr | emr 2872 | 9 10 32 | 10 9 27 | 15 43 86 |
esa | esa 3072 | 9 13 25 | 4 7 20 | 8 29 36 |
gfz | gfz 2869 | 11 12 32 | 4 7 19 | 16 17 61 |
grg | grg 2880 | 13 13 35 | 4 7 19 | 12 19 27 |
igr | igr 3050 | 9 12 22 | 4 7 19 | 17 19 50 |
igs | igs 3059 | 9 11 24 | 4 7 18 | 20 19 52 |
jpl | jpl 2868 | 12 10 35 | 5 10 27 | 15 31 63 |
mit | mit 3072 | 8 11 23 | 7 18 33 | 51 35 41 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1646 GPS week: 1646 MJD: 55766.500-55772.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 0 -36 -33 -65 -1 | 3 16
| 24 23 92 102 7 | 2
emr uuuuu | 43 -38 39 153 3 | 27 31
| 15 26 88 19 5 | 2
esa uuuuu | 3 -39 92 -2 -2 | 11 18
| 12 8 60 50 4 | 3
gfz uuuuu | -34 24 -94 16 -1 | -5 17
| 24 23 81 79 5 | 4
grg uuuux | 36 -3 -31 -236 56 | -7 54
| 51 35 137 80 41 | 31
igr xxxxx | -17 -31 5 2 -6 | 0 17
| 22 22 66 92 5 | 5
irf xxxxx | -9 0 -54 -13 1 | 1 14
| 12 14 64 45 2 | 3
jpl uxuuu | -28 -40 79 -28 0 | 25 30
| 76 99 78 129 7 | 2
mit uuuuu | -35 14 -208 -106 -1 | 18 22
| 22 30 88 64 3 | 3
ngs uuuuu | -27 14 -7 59 0 | 11 15
| 34 37 109 72 7 | 2
sio uuuuu | 131 86 190 164 9 | 29 33
| 20 29 113 46 4 | 1
Table 7.1646.0 GPS week: 1646 Day: 0 MJD: 55766.500
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 -36 -128 -13 -3 | 4 13
emr uuuuu | 61 -3 -38 163 10 | 26 30
esa uuuuu | 4 -41 98 2 -1 | 13 18
gfz uuuuu | -26 10 -38 -5 -7 | 1 15
grg uuuux | -51 -23 161 -304 88 | -59 115
igr xxxxx | -14 -32 13 30 -7 | 6 16
irf xxxxx | -20 -6 -118 -12 -1 | 4 13
jpl uxuuu | 19 67 149 85 -12 | 29 33
mit uuuuu | -57 -3 -320 -93 -3 | 21 24
ngs uuuuu | -4 39 -74 20 9 | 13 17
sio uuuuu | 110 72 69 185 10 | 29 32
Table 7.1646.1 GPS week: 1646 Day: 1 MJD: 55767.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -4 -56 1 -222 11 | 2 14
emr uuuuu | 60 -20 -59 154 4 | 27 31
esa uuuuu | -7 -36 117 -40 2 | 11 18
gfz uuuuu | -73 20 -90 -110 0 | -3 17
grg uuuux | 91 24 -40 -91 23 | -34 85
igr xxxxx | -44 -46 -43 -63 -6 | 2 17
irf xxxxx | -28 -11 -71 -84 3 | 1 14
jpl uxuuu | -36 -85 141 120 -2 | 25 31
mit uuuuu | -69 -11 -222 -170 -1 | 19 24
ngs uuuuu | 12 20 -33 113 -6 | 11 16
sio uuuuu | 97 68 187 137 16 | 28 30
Table 7.1646.2 GPS week: 1646 Day: 2 MJD: 55768.500
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 | 28 -25 76 -68 3 | 5 17
emr uuuuu | 56 -23 -38 166 2 | 30 34
esa uuuuu | 17 -51 184 -76 1 | 13 20
gfz uuuuu | -32 8 -75 -45 -5 | -2 18
grg uuuux | 99 53 -163 -285 14 | -13 56
igr xxxxx | -42 -48 -59 -137 2 | 3 17
irf xxxxx | 3 -23 43 -13 0 | 3 15
jpl uxuuu | -73 -10 -82 -35 8 | 25 31
mit uuuuu | -32 -30 -69 -59 -3 | 21 26
ngs uuuuu | -51 67 -132 180 -1 | 12 17
sio uuuuu | 139 35 357 221 12 | 30 35
Table 7.1646.3 GPS week: 1646 Day: 3 MJD: 55769.500
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 | 6 -71 0 1 -6 | 4 16
emr uuuuu | 37 -31 135 165 -6 | 29 32
esa uuuuu | 6 -30 31 61 -9 | 13 19
gfz uuuuu | -36 15 19 21 -2 | -5 15
grg uuuux | 12 14 -19 -318 25 | 4 18
igr xxxxx | -19 -48 102 -37 -9 | 1 16
irf xxxxx | -5 3 23 10 -3 | 2 14
jpl uxuuu | 29 -106 76 -216 2 | 25 31
mit uuuuu | -19 18 -131 -45 -6 | 19 23
ngs uuuuu | -48 -18 -118 30 10 | 11 16
sio uuuuu | 148 97 334 188 7 | 30 35
Table 7.1646.4 GPS week: 1646 Day: 4 MJD: 55770.500
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 | -29 -5 -185 -10 2 | 1 16
emr uuuuu | 29 -49 55 113 5 | 25 29
esa uuuuu | -18 -38 12 -4 2 | 9 18
gfz uuuuu | -52 61 -168 119 1 | -8 16
grg uuuux | 47 -52 92 -216 104 | 6 18
igr xxxxx | -8 -20 48 9 -8 | -3 16
irf xxxxx | -13 18 -117 66 1 | -1 14
jpl uxuuu | -8 35 120 -184 4 | 22 28
mit uuuuu | -39 49 -298 -31 -2 | 15 20
ngs uuuuu | -7 -13 142 -2 -5 | 10 15
sio uuuuu | 136 117 93 203 7 | 28 32
Table 7.1646.5 GPS week: 1646 Day: 5 MJD: 55771.500
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 | 33 -12 -32 -187 -10 | 2 16
emr uuuuu | 29 -81 161 143 -1 | 26 29
esa uuuuu | 2 -31 71 -17 -6 | 9 18
gfz uuuuu | 5 50 -225 93 1 | -9 17
grg uuuux | 28 -23 -12 -257 105 | 19 36
igr xxxxx | 19 13 -76 146 -11 | -4 16
irf xxxxx | 3 13 -76 -36 1 | -1 14
jpl uxuuu | -175 29 88 43 6 | 25 29
mit uuuuu | -19 46 -196 -188 1 | 15 20
ngs uuuuu | -10 -34 96 92 0 | 11 14
sio uuuuu | 148 113 143 107 7 | 29 33
Table 7.1646.6 GPS week: 1646 Day: 6 MJD: 55772.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -11 -44 34 46 -4 | -1 16
emr uuuuu | 33 -56 58 165 3 | 25 28
esa uuuuu | 16 -46 131 58 -3 | 6 15
gfz uuuuu | -23 1 -83 41 9 | -12 17
grg uuuux | 28 -11 -239 -184 34 | 28 51
igr xxxxx | -12 -34 51 68 0 | -8 17
irf xxxxx | -1 4 -59 -19 4 | -3 13
jpl uxuuu | 47 -213 62 -12 -6 | 24 28
mit uuuuu | -8 28 -220 -154 4 | 13 18
ngs uuuuu | -83 38 69 -23 -4 | 8 11
sio uuuuu | 139 100 145 109 3 | 28 32
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