[IGSREPORT-17528] Wk 1535 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 25 05:41:32 PDT 2009
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IGS Electronic Report 25 Jun 05:41:55 PDT 2009 Message Number 17528
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1535 (Jun 07, 2009 - Jun 13, 2009)
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 (weights are those from the orbit combination).
Pole rate combination uses only centres providing estimated pole rates.
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:
igs1535[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1535[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1535[0-6].cls IGS GPS clock combination summary report.
igs15357.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15357.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 they either 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 1478, a new solution from CNES/GRGS (GRG) is included for
evaluation and statistics only.
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 | ALL | 5
0 | COD | 8 10 8 10
0 | EMR | 32 WTZR
0 | ESA | 8 10 RAMO UNSA WTZR
0 | GRG | HOB2 IRKJ KHAJ NLIB
0 | MIT | 5 HOB2 IRKJ KHAJ
1 | COD | 10 10 RCMN
1 | EMR | 32 32 KERG WTZR
1 | ESA | 10 32
1 | GFZ | 8 18 CHUR MIZU
1 | GRG | NLIB
1 | JPL | MDVJ POTS
1 | NGS | 1
2 | COD | 10 10 RCMN WAB2 YAR2
2 | EMR | 32 KERG MIZU WTZR
2 | ESA | 10 32 MIZU UNSA
2 | GFZ | 18 20 22 CHUR NANO
2 | GRG | NLIB TWTF
2 | MIT | HOB2 TWTF
2 | NGS | 1
3 | ALL | 1
3 | COD | 10 20 10 20 YAR2
3 | EMR | YELL CHUR WTZR YELL
3 | ESA | 10 IRKJ
3 | GFZ | 18 20 32 UNSA
3 | GRG | IRKJ NLIB ZECK
3 | JPL | 32 YELL
3 | MIT | WAB2
4 | COD | 10 10 YAR2
4 | EMR | 32 WTZR MIZU WTZR
4 | ESA | 10 MIZU UNSA
4 | GFZ | 18 32 BAN2 CHUR
4 | GRG | COCO HOB2 NLIB
4 | JPL | MDVJ
4 | MIT | MDVJ
5 | COD | 10 10 FLIN
5 | EMR | 32 32 MIZU WTZR
5 | ESA | 10 30 32 MIZU
5 | GFZ | 18 22 32 BAN2 KERG UNSA
5 | GRG | NLIB ZECK
5 | JPL | 32
5 | MIT | 30 30 FLIN HOB2 IENG
5 | NGS | 1
6 | COD | 10 18 10 18 30 RCMN
6 | EMR | KERG MIZU WTZR
6 | ESA | 10 MIZU
6 | GFZ | 32 CHUR IRKT
6 | GRG | NLIB
6 | JPL | 32
6 | MIT | 22 30 32 22 32 BAKO HOB2
6 | NGS | 1
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
3 | GFZ | ~14:15 | ~ -0.35 ns
4 | GFZ | ~09:30 | ~ -0.32 ns
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 G32 | | | | 1 | | | |
7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) 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.
8. Small rotations were applied to the all AC orbit and ERP values in order
to align them to the IGS05. These rotations were estimated in the process
of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based
on the common stations between the individual AC SINEX solutions and the
IGS05.snx SINEX. 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 | .0 .7 .2 -3 -3 -5 .12
EMR | 10.2 -12.9 -.7 68 -7 74 -.02
ESA | 4.5 -1.6 17.0 2 -28 43 .16
GFZ | .1 .7 1.7 9 7 2 -.17
GRG | 10.9 -1.8 2.1 -17 -17 -6 .03
JPL | 4.8 -4.7 -2.8 20 0 -9 .21
MIT | 4.2 -4.9 14.3 -8 11 -9 .01
NGS | 11.1 -9.9 7.9 -107 -120 14 .12
SIO | .0 -.9 -5.7 -11 -34 -28 .15
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 NRCan. 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 on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna
model is introduced (IGSMAIL #5272). The antenna phase center offsets and
phase center variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
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 1.1535.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1535.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 2.1535.[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 3.1535.[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 5.1535.0-6).
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 1535 summary. (Jun 07, 2009 - Jun 13, 2009)
Table 1.1535.a GPS week: 1535 MJD: 54989.000-54995.000
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 233| 0 0 0 -5 -47 -38 -.17 9 8 | -94 -863 16 63
| 0 0 1 13 15 24 .01 | 336 672
emr 76| 1 0 0 -127 8 -23 .27 17 17 | 4345 111 19 94
| 2 1 2 24 30 16 .03 | 1231 1056
esa 122| 0 0 0 -44 5 21 .31 8 8 | -400 -153 18 100
| 1 1 1 23 39 19 .02 | 1441 1321
gfz 190| 0 0 0 -37 -56 141 -.06 10 10 | 42 -77 21 91
| 0 0 1 15 18 87 .03 | 226 367
grg 107| 5 0 -8 -23 14 -49 1.00 36 31 | 16 6 80 225
| 2 1 2 29 15 47 .05 | 297 464
igr n/a| 0 0 0 -8 -31 -49 .05 5 5 | 21531 78 18 63
| 0 0 1 15 16 20 .02 | 1669 1198
jpl 135| 0 2 -6 -48 -46 -5 .46 18 16 | 4150 20 16 89
| 0 1 2 19 19 19 .02 | 1399 1116
mit 260| 0 -1 2 -4 -60 -25 -.20 9 8 | -13625 583 20 142
| 0 0 0 25 32 17 .01 | 5936 440
ngs 216| 0 0 0 199 197 -73 -.24 11 9 | 8347 5219 2196 3804
| 0 0 1 42 47 19 .03 | 4380 4181
sio 257| -3 1 0 15 28 -42 .06 19 18 | --- --- --- ---
| 0 0 0 20 34 7 .04 | --- ---
Table 1.1535.b GPS week : 1535 MJD: 54989.000-54995.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 0 17 16 12 12 14 14 |
2 | 5 5 5 5 5 5 5 |
3 | 3 3 4 4 3 4 3 |
4 | 3 3 4 3 3 3 3 |
5 | 9 0 --- --- --- --- --- |
6 | 4 3 3 3 3 3 3 |
7 | 6 6 4 4 4 4 4 |
8 | 6 5 6 5 5 5 4 |
9 | 4 4 4 4 5 4 4 |
10 | 5 6 5 5 6 7 7 |
11 | 5 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 4 |
13 | 5 5 5 4 4 4 4 |
14 | 5 4 5 4 5 4 4 |
15 | 5 5 4 4 5 5 4 |
16 | 5 4 5 5 5 5 5 |
17 | 5 4 5 5 5 6 6 |
18 | 4 5 5 6 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 5 4 5 6 4 4 4 |
21 | 4 5 5 5 5 5 4 |
22 | 5 5 5 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 3 4 4 3 3 3 3 |
25 | 4 4 4 5 5 4 4 |
26 | 4 3 4 4 4 3 3 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 5 5 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 5 5 5 5 5 5 4 |
32 | 6 5 7 8 8 5 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 2.1535.0 GPS week: 1535 Day: 0 MJD: 54989.000
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 233| 1 0 0 10 -54 -55 -.19 9 7 | -206 -617 15 63
| -17 24 |
emr 76| -2 0 0 -90 -15 -14 .31 17 17 | 2370 12 18 89
| -71 -31 |
esa 122| 0 0 1 -40 -16 -4 .34 9 9 | 2380 824 19 100
| 26 49 |
gfz 190| 0 0 0 -37 -52 249 -.03 11 11 | 100 -209 25 98
| 17 20 |
grg 107| 1 0 -7 -12 -5 -120 .94 33 29 | 256 -249 76 197
| 21 14 |
igr n/a| 0 0 0 -27 -41 -79 .07 5 5 | 18847 296 19 63
| 30 -25 |
jpl 135| 0 2 -4 -53 -75 3 .45 18 16 | 1853 43 15 85
| -11 32 |
mit 260| 0 -2 0 -17 -39 -36 -.23 9 9 | -175 234 24 152
| 22 -10 |
ngs 216| 0 0 1 171 236 -103 -.28 11 10 | -83 -925 2037 3586
| 24 9 |
sio 257| -2 0 0 11 36 -44 .09 18 17 | --- --- --- ---
| -24 -50 |
Table 2.1535.1 GPS week: 1535 Day: 1 MJD: 54990.000
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 233| 0 -1 1 -16 -26 -3 -.16 10 9 | -45 -825 17 77
| -7 -20 |
emr 76| 4 0 3 -109 19 -19 .30 17 17 | 3521 338 17 99
| -54 -48 |
esa 122| 0 1 -1 -77 0 3 .33 8 8 | -136 -510 19 101
| 10 38 |
gfz 190| 0 0 -2 -36 -75 115 -.09 10 10 | 139 49 21 91
| 42 -31 |
grg 107| 0 0 -8 -27 0 -61 1.00 34 30 | -118 364 73 208
| 41 -62 |
igr n/a| -1 0 0 -25 -12 -36 .04 5 4 | 20446 493 20 61
| -7 -7 |
jpl 135| 0 1 -3 -62 -34 14 .46 18 16 | 3295 -19 18 88
| -39 12 |
mit 260| 0 -2 2 26 -113 -34 -.22 8 7 | -15772 607 22 166
| 7 8 |
ngs 216| 1 0 0 173 280 -65 -.26 10 8 | 5631 9652 2283 4048
| 12 -32 |
sio 257| -4 0 0 36 -17 -38 .09 18 17 | --- --- --- ---
| -9 -40 |
Table 2.1535.2 GPS week: 1535 Day: 2 MJD: 54991.000
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 233| 1 0 0 -5 -30 -58 -.17 10 8 | -165 -857 16 68
| 1 21 |
emr 76| 4 -2 1 -117 1 -46 .29 17 17 | 3749 2091 19 88
| -29 -15 |
esa 122| 0 2 -1 -57 6 6 .31 8 8 | -376 -633 19 99
| 37 26 |
gfz 190| 0 0 2 -65 -52 262 -.07 11 11 | -75 -41 23 95
| 11 -23 |
grg 107| 6 0 -9 -9 16 -40 .98 35 32 | -316 262 77 211
| -15 49 |
igr n/a| 0 0 -1 6 -20 -67 .05 6 5 | 20859 2167 18 67
| -4 19 |
jpl 135| -1 1 -5 -54 -36 -16 .45 18 16 | 3811 2113 16 87
| -16 35 |
mit 260| 0 -2 2 -24 -70 -53 -.20 9 8 | -16262 837 18 131
| 32 -5 |
ngs 216| 0 0 -2 269 207 -76 -.25 11 9 | 11848 4535 2145 3594
| -99 19 |
sio 257| -2 0 0 8 0 -52 .10 18 18 | --- --- --- ---
| -17 -40 |
Table 2.1535.3 GPS week: 1535 Day: 3 MJD: 54992.000
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 233| 0 0 2 9 -71 -59 -.16 9 8 | -373 -296 15 59
| -1 45 |
emr 76| 1 -2 0 -122 -39 -4 .27 17 17 | 5788 -805 21 100
| -32 2 |
esa 122| 0 0 0 -33 61 40 .29 9 8 | -827 -930 18 101
| 21 2 |
gfz 190| -1 0 0 -46 -76 140 -.10 10 10 | 153 -282 21 95
| -4 35 |
grg 107| 4 2 -5 7 18 -92 .98 35 31 | -93 136 81 234
| -17 109 |
igr n/a| 0 0 -1 6 -50 -38 .03 5 5 | 23156 -438 20 64
| -27 39 |
jpl 135| 0 3 -6 -24 -70 -27 .49 18 17 | 5899 -766 18 102
| -20 75 |
mit 260| 0 -1 3 -17 -17 -11 -.18 10 8 | -16143 224 17 129
| 17 -17 |
ngs 216| 0 0 -3 225 149 -93 -.20 12 9 | 9914 7303 2174 3408
| 10 91 |
sio 257| -3 0 0 -3 65 -45 .08 19 18 | --- --- --- ---
| -5 -72 |
Table 2.1535.4 GPS week: 1535 Day: 4 MJD: 54993.000
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 233| 0 0 0 -26 -50 -15 -.16 8 7 | 595 -2325 14 54
| 66 -2 |
emr 76| 0 1 -2 -160 7 -14 .26 17 17 | 5344 390 20 96
| -6 -28 |
esa 122| 1 0 1 -5 55 30 .31 9 9 | -1879 823 18 97
| -37 14 |
gfz 190| 0 0 2 -17 -37 106 -.06 11 11 | 411 -680 22 86
| 35 -33 |
grg 107| 7 4 -14 -45 40 -49 .99 38 32 | 533 -813 89 243
| 61 18 |
igr n/a| 0 0 0 -20 -14 -28 .06 5 5 | 23214 272 18 60
| -32 -42 |
jpl 135| 0 1 -8 -72 -43 -22 .48 17 15 | 5168 530 18 92
| -11 5 |
mit 260| 0 -1 2 35 -80 -23 -.20 9 7 | -15700 258 20 135
| 15 2 |
ngs 216| 0 0 0 138 158 -56 -.23 11 9 | 12561 160 2411 4281
| 44 109 |
sio 257| -3 1 0 44 6 -51 .04 18 18 | --- --- --- ---
| -1 -55 |
Table 2.1535.5 GPS week: 1535 Day: 5 MJD: 54994.000
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 233| 0 0 -1 -5 -51 -58 -.16 9 8 | -419 -478 17 65
| -23 24 |
emr 76| 0 0 -1 -141 34 -46 .24 17 17 | 5384 -1224 21 101
| -23 -57 |
esa 122| 1 1 0 -35 -24 36 .33 9 8 | -81 -2266 18 108
| 10 48 |
gfz 190| 0 -1 0 -35 -71 106 -.04 9 9 | -216 118 20 90
| 12 22 |
grg 107| 7 0 -8 1 26 6 1.08 36 31 | 85 -212 78 261
| -1 61 |
igr n/a| 0 1 0 -2 -30 -65 .08 5 5 | 23040 -1778 16 66
| -24 13 |
jpl 135| 0 0 -7 -19 -26 -9 .45 17 16 | 5311 -1430 14 86
| -32 0 |
mit 260| 0 -1 3 -23 -36 -19 -.19 11 9 | -15502 483 18 137
| 12 -16 |
ngs 216| 0 0 1 203 163 -61 -.23 10 9 | 10397 6747 2382 3918
| -25 94 |
sio 257| -4 2 0 -11 75 -34 .02 19 18 | --- --- --- ---
| -6 -72 |
Table 2.1535.6 GPS week: 1535 Day: 6 MJD: 54995.000
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 233| 0 0 0 -5 -44 -18 -.16 7 7 | -48 -649 18 59
| -13 8 |
emr 76| 0 2 -2 -148 52 -18 .24 17 17 | 4259 -23 20 91
| -17 -55 |
esa 122| 2 0 0 -58 -39 37 .28 7 7 | -1882 1619 18 96
| -2 35 |
gfz 190| 0 -1 3 -25 -29 11 -.04 9 9 | -216 500 20 84
| 5 2 |
grg 107| 7 0 -9 -77 7 9 1.05 41 34 | -232 556 86 227
| 70 55 |
igr n/a| 0 0 0 4 -49 -33 .01 5 5 | 21156 -461 18 65
| -20 2 |
jpl 135| 0 3 -9 -53 -35 22 .45 18 17 | 3719 -328 16 85
| -20 19 |
mit 260| -1 0 3 -12 -62 -1 -.20 10 9 | -15822 1439 25 144
| 22 -16 |
ngs 216| 0 -1 -1 216 190 -53 -.26 10 8 | 8165 9065 1942 3799
| -19 114 |
sio 257| -3 2 0 21 34 -34 -.00 19 19 | --- --- --- ---
| -9 -58 |
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 3.1535.0 GPS week: 1535 Day: 0 MJD: 54989.000
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 | 5 --- --- --- --- 32 --- --- --- --- 0 | 24 --- --- --- --- 20 --- --- --- --- 21
2 | 8 21 9 9 32 5 22 11 10 22 5 | 21 30 23 23 32 19 31 20 22 21 20
3 | 6 8 7 9 17 3 10 8 9 15 3 | 19 25 26 28 26 22 24 22 24 19 22
4 | 5 11 3 7 23 6 11 6 9 9 2 | 24 27 23 24 20 22 23 26 27 28 24
X5 | 17 21 --- --- --- 49 --- 11 13 --- 9 | 30 16 --- --- --- 29 --- 6 13 --- 33
6 | 6 9 7 8 18 4 6 6 10 21 3 | 26 35 31 34 30 31 33 29 31 22 29
7E | 19 17 14 19 31 9 20 15 12 17 6 | 70 82 86 84 86 75 79 72 84 75 77
8E | 18 18 11 15 57 11 23 8 15 17 5 | 68 71 71 72 87 73 76 74 71 77 71
9 | 8 16 7 8 37 5 17 8 9 13 4 | 13 26 19 19 33 16 26 17 21 20 16
10E | 11 15 10 15 56 6 14 13 18 18 5 | 31 33 26 32 23 27 30 24 36 26 26
11 | 8 18 12 8 54 4 17 9 9 18 4 | 30 43 38 37 46 33 40 33 34 27 33
12 | 9 21 8 9 33 5 21 12 9 22 5 | 17 32 24 20 34 18 31 20 24 17 20
13 | 8 17 10 10 35 5 22 11 9 20 4 | 14 30 22 21 42 18 29 21 22 20 18
14 | 9 21 11 10 26 5 20 8 12 19 5 | 20 32 28 30 43 24 29 24 25 24 23
15 | 6 20 10 9 29 4 22 6 10 19 4 | 18 29 25 22 36 19 27 19 24 22 20
16 | 7 19 7 10 37 4 22 11 11 16 4 | 17 33 21 20 37 18 32 19 24 19 19
17 | 8 11 8 16 14 8 11 9 11 22 4 | 27 30 29 35 31 27 22 31 29 37 28
18E | 8 17 8 11 24 5 19 9 9 14 4 | 32 34 35 41 43 31 34 37 44 40 36
19 | 6 12 7 12 16 4 14 8 10 24 4 | 31 38 38 40 40 35 36 33 31 34 34
20E | 8 13 12 11 31 4 19 8 12 13 4 | 35 40 37 40 53 38 46 40 42 41 38
21 | 8 18 9 7 27 5 21 6 8 17 4 | 17 27 17 17 36 14 27 19 24 16 17
22E | 9 16 14 10 31 4 22 12 10 10 5 | 17 26 25 25 29 18 26 22 27 22 20
23 | 7 17 9 9 39 7 22 6 9 29 4 | 17 31 23 20 44 20 29 21 21 27 18
24 | 6 11 9 7 26 4 10 8 9 11 3 | 20 23 21 20 26 18 23 22 23 21 19
25 | 7 20 6 9 27 5 17 11 9 12 4 | 12 27 14 14 28 14 25 16 21 18 13
26 | 5 11 8 8 21 4 11 8 8 16 3 | 17 22 20 23 30 18 23 19 25 26 19
27 | 7 17 9 8 28 6 17 10 10 15 4 | 14 27 18 20 35 17 26 17 21 23 17
28 | 6 17 9 9 30 5 18 10 11 15 4 | 16 28 18 17 40 15 25 16 23 18 16
29 | 8 14 6 10 30 4 15 8 11 30 4 | 27 29 26 29 21 25 26 32 31 30 27
30 | 8 13 8 9 17 4 11 7 11 23 4 | 16 22 19 21 24 16 20 19 28 26 18
31E | 6 21 8 16 54 7 19 7 12 21 5 | 27 40 33 31 29 26 35 29 31 35 29
32E | 13 27 12 9 40 7 17 12 16 15 5 | 59 63 60 60 69 58 60 63 57 61 58
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 9 11 33 5 18 9 11 18 |T 25 33 29 30 38 26 33 27 30 29 27
WRMS | 7 17 9 11 29 5 16 9 10 17 |NE 20 28 23 24 33 21 27 21 24 23 21
MEDI | 8 17 9 9 30 5 17 8 10 17 |MD 20 30 25 24 34 20 29 22 25 24 21
Table 3.1535.1 GPS week: 1535 Day: 1 MJD: 54990.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 26 --- --- --- --- 47 --- 10 33 --- 17 | 19 --- --- --- --- 45 --- 17 31 --- 17
2 | 9 21 8 9 40 6 25 8 11 22 5 | 18 29 20 17 31 17 31 17 20 19 17
3 | 7 10 4 7 26 3 10 4 7 16 2 | 18 22 22 23 22 20 20 20 27 19 21
4 | 7 11 5 8 24 4 11 5 11 10 3 | 17 23 17 14 18 18 19 19 23 24 17
X5 | 3 --- --- --- --- 209 --- --- --- --- 0 | 62 --- --- --- --- 24 --- --- --- --- 60
6 | 8 8 6 7 22 3 11 5 6 18 3 | 18 21 21 14 25 18 22 17 24 15 18
7 | 26 15 9 14 37 6 18 7 8 12 5 | 48 45 42 43 46 43 45 43 44 44 42
8E | 16 21 11 10 40 10 22 8 10 24 5 | 41 51 43 39 50 47 54 39 47 44 41
9 | 9 17 6 11 24 3 18 9 9 11 4 | 13 26 20 17 30 17 29 17 22 19 17
10E | 11 17 12 13 70 6 16 14 18 16 5 | 21 23 23 24 33 20 23 15 30 13 18
11 | 11 17 11 7 58 3 18 7 7 18 4 | 21 34 28 22 44 23 34 23 24 20 22
12 | 10 20 7 7 34 5 19 10 9 20 4 | 13 28 24 18 36 18 28 17 20 15 17
13 | 8 19 7 10 33 4 25 9 7 14 4 | 12 30 20 19 43 15 29 15 18 15 15
14 | 7 17 9 9 27 6 20 6 10 16 4 | 15 29 20 18 36 21 27 14 24 17 17
15 | 8 19 9 7 24 5 20 7 9 23 4 | 15 26 20 17 36 16 27 14 23 16 16
16 | 9 18 6 10 41 5 22 8 10 15 4 | 13 28 22 16 35 18 29 13 22 15 16
17 | 7 14 8 13 20 4 10 8 13 22 4 | 21 25 24 33 21 24 21 24 27 34 23
18E | 10 16 10 9 18 4 21 11 8 22 4 | 23 31 29 24 25 23 30 24 27 27 23
19 | 10 12 7 13 24 4 16 6 5 24 4 | 18 25 27 28 31 24 25 20 24 23 22
20E | 8 14 9 8 21 4 19 6 8 17 4 | 46 53 45 42 59 48 53 46 49 49 46
21 | 8 20 8 10 35 4 24 6 8 17 4 | 13 25 18 14 36 14 28 13 23 13 14
22E | 8 17 9 10 29 4 24 9 10 11 4 | 16 24 19 16 30 16 25 18 22 18 16
23 | 8 20 10 9 36 5 25 7 6 28 5 | 13 32 23 20 43 16 29 15 18 23 15
24 | 7 16 8 8 25 4 11 8 6 12 3 | 15 22 23 15 22 18 21 16 22 17 17
25 | 8 22 8 9 30 4 20 7 5 13 4 | 15 30 19 18 33 16 29 18 20 18 16
26 | 6 13 5 5 19 4 10 6 8 17 3 | 15 21 18 17 28 17 23 16 22 25 16
27 | 8 15 8 10 28 3 17 9 9 15 4 | 12 23 21 16 31 17 27 15 26 21 17
28 | 6 16 8 9 35 5 18 6 11 14 3 | 15 24 16 15 38 18 24 15 24 19 15
29 | 8 13 7 11 33 4 13 6 10 30 4 | 22 25 22 19 21 20 25 19 25 22 20
30 | 7 15 5 7 22 4 9 5 10 19 3 | 14 24 21 16 24 16 23 14 20 23 16
31 | 8 22 10 13 37 5 16 4 10 16 4 | 21 32 23 19 44 22 27 17 26 20 19
32E | 15 22 9 9 45 5 18 12 14 19 5 | 31 45 40 41 50 38 46 38 46 43 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 8 10 34 5 18 8 10 18 |T 21 29 24 21 34 22 29 20 26 23 22
WRMS | 9 17 8 10 30 4 16 7 8 17 |NE 17 26 21 18 31 19 25 16 23 19 19
MEDI | 8 17 8 9 29 4 18 7 9 17 |MD 17 26 22 18 33 18 27 17 24 19 17
Table 3.1535.2 GPS week: 1535 Day: 2 MJD: 54991.000
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 | 24 --- --- --- --- 52 --- 12 32 --- 16 | 21 --- --- --- --- 43 --- 13 24 --- 12
2 | 8 18 7 9 41 6 24 9 7 22 4 | 19 24 17 17 28 18 25 19 19 24 16
3 | 8 12 8 10 26 6 9 5 7 16 3 | 16 23 24 27 23 19 23 19 18 19 19
4 | 6 14 7 6 26 4 9 8 14 9 3 | 18 27 20 22 16 20 19 24 22 26 19
6 | 6 10 7 10 24 5 12 5 7 18 3 | 19 25 21 21 30 19 21 20 22 16 18
7 | 7 14 9 11 36 7 18 7 14 13 4 | 30 32 30 24 40 28 30 29 34 29 27
8E | 22 21 9 9 30 6 19 12 9 16 5 | 52 54 55 54 79 54 59 61 54 60 54
9 | 10 16 6 11 20 5 17 9 10 13 4 | 13 24 18 18 35 15 25 16 19 20 15
10E | 12 19 11 12 77 8 16 10 18 14 5 | 21 26 22 23 37 20 22 18 30 19 18
11 | 8 14 7 9 58 4 19 10 9 21 4 | 25 35 29 29 43 27 35 25 24 23 25
12 | 10 23 8 8 33 6 25 9 11 20 5 | 15 30 20 15 34 18 29 15 19 14 15
13 | 7 16 10 9 33 4 23 9 11 12 4 | 11 26 18 15 42 15 28 16 16 14 13
14 | 6 20 12 12 30 3 22 7 10 17 4 | 16 26 22 18 37 18 24 16 20 17 16
15 | 7 17 7 7 27 5 21 7 10 18 4 | 14 23 19 14 37 17 24 14 20 19 14
16 | 6 18 7 10 34 5 23 6 12 19 4 | 14 27 19 16 33 16 29 13 24 14 16
17 | 10 16 7 14 14 5 11 7 11 25 4 | 24 28 26 33 19 26 21 29 26 38 25
18E | 17 16 11 13 28 4 23 7 7 13 5 | 25 25 28 26 36 23 27 24 29 25 23
19 | 7 11 7 13 32 8 11 7 9 25 4 | 23 28 29 33 28 27 27 24 25 27 25
20E | 9 15 8 11 35 7 20 9 12 16 4 | 39 45 38 34 41 38 42 44 44 43 39
21 | 7 17 10 11 34 5 24 6 11 17 4 | 15 22 13 16 35 15 26 17 21 13 14
22E | 10 16 11 15 34 3 24 7 8 11 4 | 20 24 20 23 30 23 30 22 31 22 21
23 | 8 17 11 11 37 5 23 8 11 29 5 | 12 28 21 17 45 16 26 16 16 22 13
24 | 8 16 5 7 22 5 10 8 11 10 3 | 14 19 19 14 24 15 17 19 19 17 15
25 | 8 15 7 10 31 3 17 8 10 12 4 | 13 24 14 16 36 15 27 18 20 19 14
26 | 8 10 7 13 25 5 11 8 9 18 3 | 24 26 26 25 31 25 28 24 30 31 25
27 | 9 16 8 8 17 6 15 8 10 14 4 | 12 22 19 14 32 16 23 15 20 22 15
28 | 8 19 8 11 36 7 16 5 12 12 4 | 15 26 19 18 38 18 24 17 22 18 16
29 | 6 11 4 14 28 6 16 7 12 29 4 | 25 28 25 24 24 22 25 28 26 23 24
30 | 8 13 7 11 20 6 12 7 12 19 4 | 14 20 18 16 24 14 18 15 18 22 14
31 | 9 21 8 15 47 7 18 8 13 17 4 | 18 30 18 17 39 17 25 18 17 20 16
32E | 19 29 11 12 54 10 22 21 14 26 7 | 59 71 68 61 78 64 68 72 68 74 65
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 8 11 35 6 18 9 11 18 |T 21 28 24 23 35 23 28 23 25 25 21
WRMS | 8 17 8 11 32 5 16 8 9 18 |NE 17 25 20 19 31 19 24 18 21 20 17
MEDI | 8 16 8 11 31 5 18 8 11 17 |MD 18 26 20 18 35 19 25 19 22 22 16
Table 3.1535.3 GPS week: 1535 Day: 3 MJD: 54992.000
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 | 18 --- --- --- --- 14 --- 10 21 --- 11 | 24 --- --- --- --- 21 --- 15 20 --- 16
2 | 8 19 8 7 41 5 22 11 12 22 4 | 22 28 18 20 35 20 30 21 21 23 19
3 | 6 10 8 7 31 5 11 6 11 17 3 | 28 31 30 29 31 29 32 30 33 30 29
4 | 5 11 7 7 21 5 10 6 9 10 3 | 22 25 21 21 25 20 20 24 24 25 21
6 | 7 9 8 6 38 5 10 5 10 17 3 | 18 20 21 23 18 17 19 22 24 19 20
7 | 7 14 10 12 39 8 15 6 9 11 3 | 22 25 21 24 44 21 24 20 24 23 20
8 | 14 25 9 8 28 7 18 10 7 14 5 | 74 87 75 77 82 75 84 76 76 74 76
9 | 9 15 6 9 34 5 16 8 12 14 4 | 14 23 18 16 37 16 25 15 20 19 14
10E | 8 18 10 9 58 6 17 11 24 14 5 | 24 30 21 24 36 25 27 22 37 25 22
11 | 6 16 9 7 60 4 17 5 7 18 3 | 28 38 31 34 44 30 37 32 28 29 30
12 | 10 21 10 8 30 5 23 11 11 19 5 | 18 31 20 17 34 17 30 19 20 17 17
13 | 6 16 9 8 39 5 23 9 13 13 4 | 18 28 19 19 44 18 28 19 22 18 18
14 | 8 20 8 9 22 4 22 5 9 17 4 | 17 29 23 26 35 18 26 20 25 18 19
15 | 5 17 5 11 34 6 23 7 12 18 4 | 14 24 15 17 36 14 25 13 20 18 13
16 | 7 19 9 8 32 4 24 7 13 22 4 | 16 30 23 17 34 19 31 14 25 16 17
17 | 8 15 9 16 25 6 12 6 12 25 4 | 27 29 27 36 39 25 24 28 25 36 26
18E | 18 13 9 11 37 6 25 15 14 19 5 | 58 61 62 67 53 59 62 66 70 70 63
19 | 6 10 8 7 36 5 12 7 10 24 3 | 25 31 27 29 28 26 28 28 28 30 27
20E | 11 16 12 13 28 6 22 22 13 15 6 | 41 45 40 41 58 42 51 53 47 48 43
21 | 7 18 9 9 33 4 23 7 10 18 4 | 15 25 15 19 32 15 26 19 24 17 16
22E | 8 14 9 11 33 3 22 8 10 13 4 | 17 22 16 19 33 16 24 19 28 20 17
23 | 9 19 10 9 39 6 23 6 14 29 5 | 18 30 24 20 47 18 28 18 23 26 18
24 | 7 11 4 6 22 3 11 8 10 12 3 | 22 22 21 20 31 19 22 22 23 23 20
25 | 8 21 9 10 39 4 17 10 11 11 4 | 18 30 14 18 36 15 26 17 22 20 16
26 | 6 10 4 10 21 3 10 8 10 18 3 | 23 26 25 20 32 24 27 23 31 32 23
27 | 7 15 5 9 17 4 16 8 9 16 3 | 15 22 18 17 32 16 25 14 21 23 15
28 | 9 16 9 11 29 6 16 7 8 13 4 | 16 24 18 18 33 17 24 17 19 19 15
29 | 11 14 7 9 29 3 18 7 9 30 4 | 35 31 27 28 26 28 28 31 34 26 29
30 | 9 14 8 8 23 3 12 8 9 19 4 | 19 26 21 20 26 17 21 21 18 23 17
31 | 8 25 8 10 31 4 21 5 8 17 4 | 15 35 19 19 40 16 28 14 22 18 16
32E | 17 26 12 20 61 9 20 24 20 29 7 | 125 129 124 136 137 130 130 122 131 123 126
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 9 10 35 5 18 10 12 19 |T 27 34 28 29 40 27 33 28 31 30 27
WRMS | 8 17 8 10 31 5 17 8 9 18 |NE 20 27 21 22 33 19 26 20 23 23 19
MEDI | 8 16 9 9 32 5 17 8 10 17 |MD 22 29 21 20 35 19 27 21 24 23 19
Table 3.1535.4 GPS week: 1535 Day: 4 MJD: 54993.000
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 | 18 --- --- --- --- 13 --- 14 16 --- 11 | 22 --- --- --- --- 25 --- 18 33 --- 22
2 | 8 20 9 9 44 7 22 15 10 23 5 | 19 30 23 20 33 22 34 25 27 25 21
3 | 5 9 6 7 31 6 10 7 10 17 3 | 21 24 28 23 31 22 25 25 31 22 24
4 | 6 11 6 6 30 4 8 7 11 14 3 | 20 28 25 23 22 25 25 27 30 29 24
6 | 5 10 6 7 30 6 10 5 11 17 3 | 16 23 23 20 24 19 23 19 24 17 19
7 | 8 12 8 11 53 4 12 7 9 12 3 | 20 26 20 20 51 22 25 19 22 23 19
8 | 9 23 7 7 32 5 19 13 11 13 4 | 49 59 53 52 64 52 62 54 55 52 52
9 | 8 19 9 9 31 5 18 11 13 12 4 | 15 28 20 21 34 21 31 23 25 24 19
10E | 14 16 8 10 63 7 17 13 25 16 5 | 23 33 27 25 39 29 30 26 43 26 25
11 | 7 15 7 7 61 5 15 6 11 19 3 | 26 38 37 33 44 30 40 30 30 28 30
12 | 9 21 10 8 34 5 22 9 11 18 4 | 16 33 26 20 37 22 33 22 24 21 21
13 | 6 15 9 9 41 4 18 7 10 13 4 | 17 30 23 22 43 23 32 21 19 22 20
14 | 7 20 13 9 30 5 22 8 9 17 4 | 19 29 26 23 37 21 28 21 25 20 21
15 | 5 18 11 11 37 4 22 7 11 18 4 | 18 29 25 23 36 21 29 20 22 23 20
16 | 7 22 10 7 33 5 24 7 9 20 4 | 18 34 25 19 36 21 35 21 27 23 21
17 | 9 13 8 22 28 5 10 9 9 29 5 | 24 30 28 42 34 25 26 30 29 40 28
18E | 7 12 8 6 32 5 21 5 9 11 3 | 48 53 50 50 58 49 53 52 53 53 50
19 | 6 9 7 6 28 6 11 6 8 25 3 | 26 33 37 33 29 30 31 28 27 30 29
20E | 5 15 8 9 28 7 19 8 9 11 3 | 22 29 24 22 41 23 31 25 29 25 23
21 | 7 19 9 11 30 3 23 6 10 18 4 | 16 29 19 14 35 16 30 18 26 18 17
22E | 6 17 8 7 45 3 23 9 9 10 4 | 24 31 27 24 44 24 31 26 31 25 25
23 | 8 18 9 11 35 6 22 6 7 29 4 | 19 33 23 23 44 22 31 22 19 29 20
24 | 8 11 8 6 27 2 9 8 9 11 3 | 22 29 29 22 33 25 26 25 26 24 24
25 | 9 21 10 8 41 2 17 10 13 12 4 | 15 31 21 18 35 18 29 20 20 21 17
26 | 6 13 8 8 27 5 11 6 7 19 3 | 19 26 22 20 30 23 26 21 22 28 20
27 | 7 18 7 9 27 5 16 8 8 14 4 | 15 26 20 20 37 19 29 20 26 25 18
28 | 7 20 7 12 26 4 18 9 7 13 4 | 18 30 19 21 41 18 27 22 24 23 19
29 | 9 12 9 10 37 6 14 8 8 30 4 | 33 34 31 33 25 33 32 34 34 30 31
30 | 8 14 11 9 20 4 11 8 13 17 4 | 15 23 26 18 30 17 23 19 22 24 18
31 | 7 17 10 11 32 7 18 8 12 17 4 | 14 27 23 18 40 17 27 17 20 18 17
32E | 13 22 8 36 68 10 16 17 16 18 7 | 97 102 95 98 104 101 99 102 98 91 96
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 9 11 38 5 17 9 11 18 |T 24 33 29 27 39 26 33 27 30 28 26
WRMS | 7 17 9 11 32 5 15 7 9 18 |NE 19 29 25 23 34 22 29 23 25 24 21
MEDI | 7 16 8 9 32 5 17 8 10 17 |MD 19 30 25 22 36 22 30 22 26 24 21
Table 3.1535.5 GPS week: 1535 Day: 5 MJD: 54994.000
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 | 21 --- --- --- --- 32 --- 17 19 --- 13 | 16 --- --- --- --- 28 --- 14 25 --- 13
2 | 9 19 8 6 33 5 21 12 11 21 4 | 20 26 17 19 34 15 25 21 22 20 17
3 | 6 9 7 9 30 4 7 7 10 21 3 | 21 24 27 24 25 25 25 21 29 22 23
4 | 8 10 5 5 27 4 8 9 9 13 3 | 16 18 14 15 15 13 15 18 19 19 14
6 | 6 8 6 9 30 4 7 7 8 20 3 | 19 20 19 22 26 18 21 17 23 16 18
7 | 9 14 6 8 42 6 12 9 6 11 3 | 19 25 20 18 39 18 22 21 22 21 18
8 | 12 23 9 8 25 5 19 17 10 11 5 | 29 42 31 32 44 32 40 34 35 31 31
9 | 9 18 5 9 21 3 16 11 9 14 4 | 13 25 14 13 29 12 23 11 18 16 12
10E | 12 20 13 12 61 7 18 22 25 22 6 | 23 28 18 23 23 22 26 26 36 23 20
11 | 7 13 8 5 49 5 15 7 8 18 3 | 23 34 28 26 42 26 38 27 24 22 25
12 | 13 22 11 7 34 5 18 12 7 17 4 | 17 30 18 16 37 16 26 16 20 16 16
13 | 6 17 12 7 32 5 21 9 10 13 4 | 16 27 23 19 40 17 28 16 18 15 16
14 | 6 21 12 7 26 4 19 8 8 16 4 | 18 26 20 20 36 17 25 18 20 17 17
15 | 8 17 10 9 40 5 19 8 11 18 4 | 13 24 23 19 39 12 21 16 16 16 14
16 | 10 19 11 6 34 5 21 11 11 26 5 | 16 27 24 16 32 16 28 12 21 16 16
17 | 13 14 9 19 17 7 13 14 10 32 5 | 20 21 18 37 22 20 18 25 27 43 23
18E | 7 12 8 6 14 3 22 7 8 13 3 | 30 30 29 25 28 25 30 29 28 28 26
19 | 5 8 6 6 29 4 11 6 9 25 3 | 21 27 27 25 28 26 26 21 25 23 23
20E | 6 15 7 9 32 5 18 11 8 10 3 | 26 33 25 29 37 28 35 30 30 25 26
21 | 8 20 9 8 29 3 24 7 9 18 4 | 14 24 10 13 27 10 26 13 20 11 11
22E | 6 20 8 7 32 4 22 10 6 10 4 | 19 28 20 16 34 18 25 20 23 16 17
23 | 8 17 9 7 30 5 21 7 10 30 4 | 16 28 23 20 41 19 26 16 20 25 17
24 | 9 13 7 5 37 3 11 9 8 10 3 | 17 22 19 16 28 16 19 13 19 15 15
25 | 8 22 7 8 28 4 16 11 8 14 4 | 15 27 15 15 28 13 23 14 18 16 13
26 | 7 12 8 5 27 4 11 6 7 19 3 | 19 23 19 15 32 17 22 16 20 26 16
27 | 9 18 5 11 16 3 15 9 8 15 4 | 11 22 14 16 28 11 22 11 18 19 11
28 | 9 17 7 9 29 6 18 18 10 16 4 | 13 24 11 17 35 12 21 19 17 15 12
29 | 9 13 8 11 40 5 15 10 10 30 4 | 46 45 46 41 32 42 44 50 50 38 45
30 | 9 16 9 8 20 3 12 12 8 20 4 | 13 19 13 13 28 11 17 15 19 19 11
31 | 7 24 10 9 30 3 17 5 9 16 4 | 16 29 19 20 38 16 23 15 18 19 15
32E | 11 22 9 9 94 7 15 10 13 22 5 | 80 83 81 77 94 80 84 82 78 80 79
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 9 9 36 5 17 11 10 19 |T 21 28 22 22 34 21 27 21 25 22 20
WRMS | 8 17 8 9 31 5 16 9 9 18 |NE 17 25 20 19 31 17 24 18 22 20 17
MEDI | 8 17 8 8 30 5 16 9 9 17 |MD 18 26 19 19 32 17 25 18 21 19 17
Table 3.1535.6 GPS week: 1535 Day: 6 MJD: 54995.000
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 | 21 --- --- --- --- 24 --- 14 23 --- 14 | 25 --- --- --- --- 28 --- 17 27 --- 18
2 | 8 18 6 5 31 5 23 11 11 22 4 | 29 35 25 26 32 28 36 30 34 35 28
3 | 6 9 4 9 47 4 8 5 9 18 3 | 24 28 27 29 36 25 29 25 27 24 25
4 | 7 11 5 6 23 5 10 8 11 18 3 | 29 34 29 30 20 29 30 36 37 39 31
6 | 6 9 4 8 49 3 11 4 10 18 3 | 24 26 25 28 34 24 23 27 30 23 25
7 | 6 15 7 8 45 5 16 9 8 10 3 | 19 26 21 17 37 20 25 25 26 25 20
8 | 8 23 7 7 24 3 20 11 8 12 4 | 68 73 67 68 66 66 73 69 68 69 68
9 | 7 20 4 11 24 6 16 10 10 16 4 | 19 31 19 20 32 20 29 21 26 25 19
10E | 11 18 15 9 58 11 22 16 29 14 6 | 35 39 36 32 58 34 36 38 40 38 33
11 | 6 14 4 8 48 3 16 9 7 21 3 | 34 44 40 42 43 36 44 40 36 35 37
12 | 7 20 7 9 30 6 19 6 6 17 4 | 21 32 23 20 38 20 32 24 25 22 21
13 | 8 16 6 8 41 4 21 9 9 11 3 | 20 29 24 20 43 21 30 22 24 22 20
14 | 7 18 11 9 36 5 22 9 8 16 4 | 24 30 29 28 37 25 28 25 25 24 24
15 | 5 18 6 8 34 7 21 12 13 18 4 | 25 30 27 26 35 23 30 25 28 27 24
16 | 6 17 6 9 38 3 27 10 13 24 4 | 22 31 24 18 34 22 40 22 30 22 22
17 | 11 12 8 16 34 6 13 17 12 38 5 | 35 38 36 47 47 37 31 44 42 60 38
18E | 7 14 7 7 33 6 22 7 7 13 3 | 36 37 37 38 34 37 38 35 46 37 37
19 | 7 10 5 9 42 3 14 6 7 25 3 | 32 37 34 38 36 33 33 32 33 33 33
20E | 7 15 7 8 26 4 18 17 7 13 4 | 39 43 40 38 48 40 41 47 41 37 39
21 | 6 20 8 7 38 3 23 10 8 18 4 | 22 32 18 21 39 21 31 24 29 22 21
22E | 6 16 9 5 35 4 23 15 8 11 4 | 29 31 26 29 34 29 33 33 37 27 29
23 | 6 18 8 8 33 5 21 9 8 28 4 | 19 31 23 20 41 20 30 21 22 28 19
24 | 8 11 4 5 29 5 14 9 8 11 3 | 26 28 28 25 27 24 24 27 28 24 25
25 | 7 22 5 7 22 3 19 10 10 19 4 | 18 33 20 18 30 18 30 17 22 25 18
26 | 5 13 6 6 18 3 11 6 7 18 3 | 22 26 24 22 35 22 27 21 29 29 22
27 | 6 17 5 9 18 6 16 8 7 19 3 | 19 25 20 19 32 21 27 21 25 28 19
28 | 8 21 9 10 36 5 20 18 10 15 5 | 22 31 20 22 44 22 29 26 28 24 21
29 | 9 12 7 11 29 4 16 8 8 31 4 | 41 44 43 45 41 42 39 44 43 43 41
30 | 6 18 6 7 80 4 16 9 8 21 3 | 20 25 22 19 37 19 26 23 24 26 19
31 | 9 21 6 12 31 5 20 6 10 17 4 | 21 29 21 18 34 19 29 20 21 23 18
32E | 13 23 9 8 92 5 15 13 11 21 5 | 73 74 68 74 86 71 74 71 80 79 72
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 7 9 41 5 18 10 10 19 |T 28 35 29 29 39 28 34 30 33 32 28
WRMS | 7 17 7 9 34 5 17 9 8 19 |NE 24 31 26 26 36 25 30 26 29 29 24
MEDI | 7 17 6 8 34 5 18 9 8 18 |MD 24 31 25 26 36 24 30 25 29 27 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 4.1535 GPS week: 1535 MJD: 54989.0-54995.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2978 |U 8 8 23 |U 5 9 21 |U 8 9 21 |
emr | emr 2883 | 12 10 26 | 12 11 58 |U 9 10 23 |
esa | esa 2880 | 9 9 26 |U 4 8 21 | 8 9 22 |
gfz | gfz 2856 |U 8 8 28 |U 11 13 43 | 8 9 21 |
grg | grg 2880 | 11 10 28 |U 8 9 26 | 11 9 27 |
igr | igr 2853 | 8 8 24 | 5 11 24 | 10 10 23 |
igs | igs 2890 | 8 8 23 | 6 10 31 | 8 8 20 |
jpl | jpl 2870 |U 9 8 26 |U 8 11 35 |U 8 9 21 |
mit | mit 2976 |U 8 8 23 |U 9 13 45 |U 10 11 28 |
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 5.1535.0 GPS week: 1535 Day: 0 MJD: 54989.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 7 7 23 | 5 9 24 | 6 5 19 |
emr | emr 2952 | 11 13 25 | 13 11 82 | 7 7 16 |
esa | esa 2880 | 7 7 23 | 6 10 22 | 6 7 18 |
gfz | gfz 2849 | 8 10 34 | 13 16 49 | 8 7 16 |
grg | grg 2880 | 9 7 24 | 7 12 32 | 9 6 28 |
igr | igr 2870 | 7 7 24 | 7 15 29 | 6 7 16 |
igs | igs 2909 | 7 8 23 | 7 12 32 | 7 6 15 |
jpl | jpl 2868 | 9 9 26 | 8 14 39 | 7 8 16 |
mit | mit 2976 | 7 7 22 | 11 16 46 | 7 11 23 |
Table 5.1535.1 GPS week: 1535 Day: 1 MJD: 54990.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3002 | 7 5 18 | 5 8 19 | 7 9 24 |
emr | emr 2870 | 10 7 20 | 12 11 63 | 8 9 19 |
esa | esa 2880 | 7 6 20 | 4 6 19 | 8 10 25 |
gfz | gfz 2854 | 7 6 23 | 11 13 45 | 8 8 21 |
grg | grg 2880 | 10 8 22 | 9 6 23 | 11 9 24 |
igr | igr 2871 | 7 6 20 | 5 8 21 | 20 19 33 |
igs | igs 2902 | 7 5 19 | 7 8 47 | 7 9 21 |
jpl | jpl 2870 | 9 6 20 | 7 8 38 | 9 10 17 |
mit | mit 2976 | 7 5 18 | 8 11 59 | 9 11 26 |
Table 5.1535.2 GPS week: 1535 Day: 2 MJD: 54991.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2967 | 10 12 29 | 5 10 20 | 10 12 26 |
emr | emr 2872 | 12 9 34 | 15 14 57 | 11 10 31 |
esa | esa 2880 | 11 16 35 | 5 9 22 | 10 12 28 |
gfz | gfz 2856 | 10 13 37 | 13 14 35 | 10 11 27 |
grg | grg 2880 | 10 15 36 | 7 9 22 | 11 13 32 |
igr | igr 2868 | 10 12 31 | 6 13 24 | 9 11 28 |
igs | igs 2917 | 11 12 32 | 8 12 37 | 10 11 28 |
jpl | jpl 2872 | 10 9 32 | 8 12 35 | 9 12 27 |
mit | mit 2976 | 10 12 32 | 10 13 42 | 11 13 33 |
Table 5.1535.3 GPS week: 1535 Day: 3 MJD: 54992.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 7 8 27 | 5 8 22 | 8 9 14 |
emr | emr 2872 | 13 11 33 | 12 11 52 | 9 9 20 |
esa | esa 2880 | 8 8 30 | 4 7 22 | 8 7 15 |
gfz | gfz 2856 | 8 7 30 | 12 10 27 | 8 7 16 |
grg | grg 2880 | 12 13 33 | 8 9 27 | 11 7 20 |
igr | igr 2873 | 8 7 30 | 4 8 22 | 8 7 15 |
igs | igs 2864 | 8 8 28 | 5 8 23 | 7 7 15 |
jpl | jpl 2870 | 10 10 33 | 15 11 43 | 8 8 19 |
mit | mit 2976 | 8 8 27 | 8 10 37 | 7 5 21 |
Table 5.1535.4 GPS week: 1535 Day: 4 MJD: 54993.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2958 | 10 7 23 | 5 5 18 | 8 10 25 |
emr | emr 2872 | 13 10 26 | 9 9 41 | 10 11 24 |
esa | esa 2880 | 14 12 35 | 4 6 17 | 8 10 25 |
gfz | gfz 2861 | 8 6 25 | 9 11 53 | 9 10 27 |
grg | grg 2880 | 10 6 27 | 8 6 23 | 12 12 31 |
igr | igr 2857 | 10 7 26 | 5 9 19 | 10 11 26 |
igs | igs 2870 | 10 6 24 | 5 8 21 | 9 10 24 |
jpl | jpl 2872 | 10 7 24 | 5 9 29 | 9 11 27 |
mit | mit 2976 | 10 6 23 | 10 14 44 | 10 10 28 |
Table 5.1535.5 GPS week: 1535 Day: 5 MJD: 54994.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2965 | 8 6 19 | 4 7 17 | 8 8 17 |
emr | emr 2872 | 12 13 20 | 12 11 56 | 9 9 23 |
esa | esa 2880 | 8 5 18 | 4 7 18 | 7 10 19 |
gfz | gfz 2861 | 8 7 21 | 10 15 50 | 8 9 20 |
grg | grg 2880 | 13 11 20 | 9 10 25 | 10 9 24 |
igr | igr 2780 | 9 7 16 | 6 11 27 | 8 8 19 |
igs | igs 2824 | 9 6 16 | 7 10 33 | 8 8 19 |
jpl | jpl 2869 | 9 9 20 | 6 9 28 | 8 9 20 |
mit | mit 2976 | 8 8 15 | 9 12 45 | 7 11 22 |
Table 5.1535.6 GPS week: 1535 Day: 6 MJD: 54995.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2957 | 7 10 23 | 6 14 30 | 8 9 24 |
emr | emr 2872 | 11 10 28 | 12 9 55 | 9 12 27 |
esa | esa 2880 | 8 10 24 | 5 9 29 | 7 9 23 |
gfz | gfz 2860 | 8 9 24 | 8 11 43 | 7 9 23 |
grg | grg 2880 | 10 12 30 | 7 13 29 | 9 8 28 |
igr | igr 2853 | 7 9 22 | 5 11 30 | 7 9 22 |
igs | igs 2946 | 8 9 22 | 6 12 29 | 7 8 22 |
jpl | jpl 2869 | 8 10 27 | 6 11 31 | 8 9 23 |
mit | mit 2976 | 8 9 21 | 10 18 44 | 17 14 45 |
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 6.1535 GPS week: 1535 MJD: 54989.500-54995.500
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 | -5 1 103 -134 -4 | -1 16
| 17 28 102 108 4 | 3
emr uuuuu | 42 35 -24 68 -6 | 3 19
| 24 25 72 53 10 | 2
esa uuuuu | -21 -7 12 4 -7 | -2 14
| 21 26 65 133 7 | 1
gfz uuuuu | 10 -15 92 -125 -2 | 14 22
| 22 15 54 41 7 | 2
grg xxxxx | -26 -21 116 -155 8 | 4 24
| 46 34 81 51 26 | 3
igr xxxxx | 9 14 20 -48 5 | 1 15
| 26 21 45 61 7 | 4
irf xxxxx | 9 2 16 -34 9 | -8 20
| 9 5 21 24 4 | 6
jpl uuuuu | -16 23 0 -67 1 | -10 19
| 25 11 98 76 6 | 3
mit uuuuu | 17 -16 -48 3 17 | -4 22
| 19 11 62 49 6 | 7
ngs uuuuu | -48 9 12 75 2 | 0 16
| 50 43 98 141 9 | 1
sio uuuuu | 65 12 -120 111 7 | 31 37
| 22 9 70 46 6 | 3
Table 7.1535.0 GPS week: 1535 Day: 0 MJD: 54989.500
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 | -16 24 -25 11 -3 | -4 18
emr uuuuu | 39 78 -37 101 7 | 4 22
esa uuuuu | -41 -19 -10 -191 -6 | -2 14
gfz uuuuu | -12 -10 54 -120 -1 | 14 24
grg xxxxx | -6 -14 40 -140 23 | 5 25
igr xxxxx | 33 -23 13 -72 3 | -3 14
irf xxxxx | 8 7 20 7 10 | -15 23
jpl uuuuu | -24 18 -8 -79 10 | -14 23
mit uuuuu | 18 -15 -62 37 15 | -12 22
ngs uuuuu | -1 -17 132 244 -10 | -1 16
sio uuuuu | 58 31 -145 106 3 | 30 37
Table 7.1535.1 GPS week: 1535 Day: 1 MJD: 54990.500
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 12 64 -241 0 | -5 18
emr uuuuu | 41 59 -158 131 7 | 1 18
esa uuuuu | -45 -5 -50 4 -5 | -3 14
gfz uuuuu | 24 -37 180 -100 -13 | 13 22
grg xxxxx | 55 -36 69 -84 -4 | 6 26
igr xxxxx | 0 12 -10 -78 3 | -4 14
irf xxxxx | -7 5 44 -37 11 | -15 23
jpl uuuuu | -19 44 -79 -45 4 | -14 23
mit uuuuu | -15 -2 15 -71 17 | -13 21
ngs uuuuu | 25 -7 9 142 -6 | -2 16
sio uuuuu | 33 14 -84 16 5 | 27 31
Table 7.1535.2 GPS week: 1535 Day: 2 MJD: 54991.500
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 | -19 -5 251 -298 -2 | 0 16
emr uuuuu | 17 25 -45 130 -5 | 3 19
esa uuuuu | -24 -41 46 -72 -9 | -1 15
gfz uuuuu | 25 -15 131 -143 -2 | 15 23
grg xxxxx | -47 11 119 -226 -26 | 8 27
igr xxxxx | -17 0 -45 -23 11 | -1 14
irf xxxxx | 2 -4 39 -44 14 | -11 21
jpl uuuuu | -33 12 -119 -76 -10 | -10 20
mit uuuuu | 7 -36 54 66 24 | -8 21
ngs uuuuu | -17 95 -188 40 5 | 0 16
sio uuuuu | 42 13 22 123 12 | 29 34
Table 7.1535.3 GPS week: 1535 Day: 3 MJD: 54992.500
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 5 157 -52 -7 | 3 16
emr uuuuu | 15 36 -34 23 -12 | 6 20
esa uuuuu | 15 -17 141 27 -1 | 0 15
gfz uuuuu | -18 8 50 -184 -8 | 17 25
grg xxxxx | -92 21 125 -161 -4 | 3 24
igr xxxxx | -22 31 48 -151 2 | 3 16
irf xxxxx | 17 4 -2 -68 14 | -5 20
jpl uuuuu | -58 24 -71 -217 -2 | -7 18
mit uuuuu | 34 -13 -90 48 25 | -2 22
ngs uuuuu | -74 -6 21 147 -2 | 2 18
sio uuuuu | 89 9 -144 145 17 | 32 38
Table 7.1535.4 GPS week: 1535 Day: 4 MJD: 54993.500
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 -59 -5 -142 -7 | 0 13
emr uuuuu | 37 13 70 50 -12 | 2 16
esa uuuuu | -5 44 -27 224 3 | -3 12
gfz uuuuu | 42 -28 103 -133 1 | 12 18
grg xxxxx | -9 -54 179 -158 -11 | 1 23
igr xxxxx | 51 39 52 34 9 | 2 15
irf xxxxx | 9 7 9 -42 8 | -6 19
jpl uuuuu | 4 18 116 -61 -3 | -9 17
mit uuuuu | 7 -8 -68 -12 17 | -2 22
ngs uuuuu | -100 -37 12 -190 -1 | -1 15
sio uuuuu | 64 8 -194 150 5 | 31 36
Table 7.1535.5 GPS week: 1535 Day: 5 MJD: 54994.500
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 20 194 -136 -8 | 1 13
emr uuuuu | 75 20 6 45 -9 | 2 16
esa uuuuu | -30 -13 18 100 -12 | -1 13
gfz uuuuu | -4 -15 23 -143 6 | 14 20
grg xxxxx | -43 -2 27 -106 37 | 2 23
igr xxxxx | 5 21 88 7 14 | 5 18
irf xxxxx | 18 -3 19 -14 5 | -2 19
jpl uuuuu | 18 29 29 33 1 | -7 17
mit uuuuu | 34 -15 -58 -16 13 | 4 24
ngs uuuuu | -76 22 60 0 15 | 1 16
sio uuuuu | 90 3 -156 99 4 | 35 40
Table 7.1535.6 GPS week: 1535 Day: 6 MJD: 54995.500
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 | 10 11 88 -77 0 | -1 17
emr uuuuu | 73 15 28 -2 -17 | 0 20
esa uuuuu | -17 0 -32 -62 -20 | -4 19
gfz uuuuu | 16 -7 106 -52 5 | 12 20
grg xxxxx | -37 -72 255 -210 44 | 1 23
igr xxxxx | 16 18 -9 -50 -6 | 6 16
irf xxxxx | 18 -2 -15 -43 2 | -1 18
jpl uuuuu | -1 18 134 -24 5 | -8 18
mit uuuuu | 34 -24 -129 -32 8 | 6 22
ngs uuuuu | -96 17 38 142 13 | 2 15
sio uuuuu | 76 7 -137 136 0 | 35 40
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