[IGSREPORT-17759] Wk 1545 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Sep 3 08:48:25 PDT 2009
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IGS Electronic Report 03 Sep 08:48:50 PDT 2009 Message Number 17759
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1545 (Aug 16, 2009 - Aug 22, 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:
igs1545[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1545[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1545[0-6].cls IGS GPS clock combination summary report.
igs15457.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15457.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 | 1
0 | COD | 26 26
0 | EMR | TWTF TLSE WTZR
0 | ESA | 26
0 | GFZ | 3 13 23 26 AREQ BUE1 IRKT KERG SHAO ZIMM
0 | GRG | ONSA
0 | JPL | 3 32
0 | MIT | 3 3 BAKO
1 | ALL | 1 1
1 | COD | 3 26 3 26
1 | EMR | WTZR WTZR
1 | ESA | 26
1 | GFZ | 13 14 26 31 FLIN KERG TOW2 UNSA
1 | GRG | LPGS ONSA
1 | JPL | 32
1 | MIT | GRAZ GRAZ
2 | ALL | 1
2 | COD | 3 26 3 26 DAV1
2 | EMR | WTZR
2 | ESA | 3 26 UNSA
2 | GFZ | 1 3 13 FAA1 KIRU
2 | GRG | DAV1 ONSA
2 | JPL | 32
2 | MIT | IRKJ
2 | NGS | 1
3 | ALL | 1
3 | COD | 26 3 26 ADE1 DAEJ
3 | EMR | WTZR
3 | ESA | 26
3 | GFZ | 13 26 BOR1 FAA1 KIRU MAS1 UNSA YELL
3 | GRG | DAV1 ONSA
3 | JPL | 32
3 | MIT | 6 6
4 | ALL | 1
4 | COD | 26 26 WTZR MATE
4 | EMR | YELL WTZR YELL
4 | ESA | 3 26 ALGO
4 | GFZ | 3 14 ALGO ANKR CHUR FAA1 HOFN KIRU SUWN TOW2 UNSA
4 | GFZ | WSRT
4 | GRG | ONSA
4 | JPL | 32 AREQ VESL YELL
4 | MIT | IRKT
5 | ALL | 1
5 | COD | 26 26 WTZR YELL
5 | EMR | WTZR
5 | ESA | 3 26 UNSA
5 | GFZ | CHUR FAA1 VESL
5 | GRG | ONSA
5 | JPL | 26 32
5 | MIT | DAV1
6 | COD | 3 6 26 3 6 26 WTZR
6 | EMR | MIZU WTZR
6 | ESA | 3 6 26 MDVJ UNSA
6 | GFZ | 1 3 6 14 FAA1 TOW2 TSKB
6 | GRG | NLIB TWTF
6 | JPL | 26 32
6 | NGS | 1
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
----+--------+---------------
6 | ESA | 5
6. 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.
7. 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 | .1 .3 1.4 -14 2 -11 -.48
EMR | 3.7 .6 -9.6 86 4 60 -.25
ESA | 2.8 4.2 3.1 77 -29 63 -.17
GFZ | .0 .4 1.1 7 -13 3 -.42
GRG | 2.5 2.5 9.8 -1 11 13 .07
JPL | -1.6 4.0 -3.4 -9 -13 8 -.07
MIT | 5.2 -.1 4.8 5 -2 -10 -.42
NGS | 5.6 .1 5.6 13 -38 -16 -.29
SIO | 1.4 .2 -14.9 -9 -86 10 -.02
8. 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.
9. 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.
10. 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 1.1545.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1545.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 2.1545.[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 3.1545.[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 5.1545.0-6).
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 1545 summary. (Aug 16, 2009 - Aug 22, 2009)
Table 1.1545.a GPS week: 1545 MJD: 55059.000-55065.000
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 59 -35 -18 -.19 8 7 | -569 133 17 71
| 0 0 1 13 15 16 .03 | 427 520
emr 89| 0 -1 -5 -165 -49 -25 .40 18 18 | 2657 -546 18 95
| 2 1 2 7 46 10 .04 | 909 1159
esa 131| 1 0 3 -67 27 70 .32 10 9 | -1762 1352 18 127
| 0 0 1 12 29 12 .03 | 1264 2025
gfz 188| 0 1 1 19 -24 -16 -.16 11 11 | -8 -44 28 122
| 1 1 1 27 74 10 .03 | 313 490
grg 112| 2 0 0 5 -26 23 1.04 42 40 | 78634 -36059 88 227
| 2 2 2 32 22 62 .05 | 208243 95504
igr n/a| 0 0 0 28 -18 -88 .05 5 5 | 7160 -1763 20 66
| 0 0 1 7 13 48 .02 | 2617 1015
jpl 123| 0 -1 -7 20 -3 16 .58 18 17 | 2209 -640 18 85
| 1 0 1 10 12 30 .03 | 848 1017
mit 265| 0 0 0 22 -34 -6 -.24 11 10 | -15662 -27 19 134
| 0 0 0 16 26 14 .07 | 678 1093
ngs 219| 0 0 1 14 43 -9 -.31 13 9 | -68704 44590 2218 3757
| 0 1 1 27 51 23 .05 | 216845 115375
sio 254| -2 1 4 40 121 -16 -.00 17 17 | --- --- --- ---
| 1 0 1 24 22 11 .07 | --- ---
Table 1.1545.b GPS week : 1545 MJD: 55059.000-55065.000
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 | 13 8 12 14 12 11 14 |
2 | 5 5 5 5 5 5 6 |
3 | 7 6 6 6 6 5 6 |
4 | 4 4 4 4 4 4 4 |
5 | --- --- --- --- --- 0 0 |
6 | 6 6 6 7 6 6 6 |
7 | 5 4 4 5 6 4 4 |
8 | 3 3 3 3 4 4 3 |
9 | 3 4 4 4 4 5 4 |
10 | 3 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 5 4 5 5 5 |
14 | 5 5 6 6 5 4 5 |
15 | 6 5 5 5 5 6 5 |
16 | 5 5 6 6 6 6 6 |
17 | 4 4 4 4 4 4 5 |
18 | 5 5 5 6 6 6 5 |
19 | 5 5 5 5 4 5 5 |
20 | 5 4 5 4 4 5 5 |
21 | 5 5 5 6 6 6 5 |
22 | 5 5 5 5 5 5 5 |
23 | 6 5 5 4 4 5 4 |
24 | 4 3 4 4 4 4 4 |
25 | 3 3 3 4 5 8 9 |
26 | 5 6 6 6 8 10 7 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 5 5 5 5 |
29 | 6 6 6 5 6 6 6 |
30 | 4 4 4 4 4 4 4 |
31 | 5 5 5 5 6 5 5 |
32 | 4 4 4 4 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 2.1545.0 GPS week: 1545 Day: 0 MJD: 55059.000
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 84 -20 -30 -.14 8 7 | -472 189 12 59
| -39 -15 |
emr 89| 0 -3 -7 -160 -29 -12 .44 17 17 | 1157 881 17 87
| 1 -7 |
esa 131| 0 0 3 -65 -11 72 .34 10 10 | -3254 3330 18 129
| 15 22 |
gfz 188| 0 0 1 -1 -68 -19 -.14 10 10 | 180 -421 23 112
| -32 -44 |
grg 112| 2 0 -2 39 -3 123 1.10 41 39 | -27 -263 77 235
| 3 -61 |
igr n/a| 0 0 0 32 -1 -39 .04 5 4 | 9526 -427 17 67
| -14 -47 |
jpl 123| 0 0 -8 21 -1 -7 .57 17 16 | 1152 868 16 93
| -9 8 |
mit 265| 0 0 0 14 -9 -3 -.33 11 10 | -15879 -125 19 127
| -16 -3 |
ngs 219| 1 2 2 -14 84 17 -.37 12 9 | 15849 -276 2145 3845
| 43 -18 |
sio 254| -2 1 2 36 139 -5 .07 17 17 | --- --- --- ---
| -33 -74 |
Table 2.1545.1 GPS week: 1545 Day: 1 MJD: 55060.000
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 57 -29 -6 -.16 8 7 | 196 -746 13 61
| 11 -17 |
emr 89| -1 0 -9 -177 -74 -31 .39 18 18 | 2360 -183 19 103
| 14 30 |
esa 131| 0 0 3 -84 19 69 .36 8 8 | 357 -1644 16 117
| 34 5 |
gfz 188| 2 0 3 31 -41 -3 -.12 10 10 | 418 -834 27 119
| -32 -40 |
grg 112| 0 0 0 17 -11 20 1.07 44 42 | 283 -382 87 208
| 32 -1 |
igr n/a| 0 0 0 21 -23 -50 .04 4 4 | 9524 -1520 19 65
| -27 3 |
jpl 123| 0 -3 -8 19 4 -22 .54 18 16 | 2407 -392 18 89
| -24 -40 |
mit 265| 0 0 -1 46 -33 -6 -.33 11 10 | -14368 -1858 17 139
| -20 1 |
ngs 219| 0 0 0 -28 61 -21 -.36 11 8 | 16148 -2251 2377 3652
| 4 -52 |
sio 254| -3 1 2 80 127 -16 .02 17 18 | --- --- --- ---
| -42 -64 |
Table 2.1545.2 GPS week: 1545 Day: 2 MJD: 55061.000
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 67 -32 -1 -.17 8 7 | -1156 988 17 69
| -28 5 |
emr 89| 0 -2 -6 -169 -110 -12 .39 18 18 | 3012 529 19 94
| 33 45 |
esa 131| 1 0 5 -58 25 48 .31 10 9 | -2474 1995 18 130
| 61 -4 |
gfz 188| 0 1 2 -24 -26 -28 -.19 11 11 | -201 194 26 115
| -32 -21 |
grg 112| 3 3 3 43 -20 24 1.03 43 42 | -161 204 87 211
| -5 13 |
igr n/a| 0 0 0 28 -28 -162 .07 5 4 | 8774 -821 19 57
| -16 6 |
jpl 123| 0 -1 -9 18 -8 53 .63 17 15 | 2736 233 20 77
| 9 -24 |
mit 265| 0 0 0 23 4 -3 -.27 10 9 | -16279 291 18 130
| -21 -34 |
ngs 219| 2 0 1 21 35 -38 -.31 13 10 | 9095 5972 2092 3525
| -51 81 |
sio 254| -3 0 4 56 141 -10 .06 18 18 | --- --- --- ---
| -32 -76 |
Table 2.1545.3 GPS week: 1545 Day: 3 MJD: 55062.000
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 49 -59 -21 -.18 8 7 | -612 399 16 59
| 18 26 |
emr 89| 0 0 -3 -163 -91 -32 .44 17 17 | 3828 -707 17 113
| 22 29 |
esa 131| 1 0 3 -84 82 79 .36 11 10 | -2145 3019 21 135
| 27 -65 |
gfz 188| 0 2 2 15 108 -3 -.15 11 11 | -113 268 27 111
| -31 -38 |
grg 112| 0 0 -2 -10 -54 7 1.11 42 42 | -113 327 98 225
| 70 41 |
igr n/a| 0 0 0 19 -35 -141 .06 6 6 | 8270 -1988 18 60
| 15 -13 |
jpl 123| 0 -1 -7 18 -16 29 .60 18 17 | 3329 -869 18 77
| 15 -37 |
mit 265| 0 -1 0 33 -31 -7 -.22 10 10 | -15891 206 17 128
| -8 -6 |
ngs 219| 1 -1 0 33 -44 2 -.30 13 11 | 16634 -5808 2144 3936
| -61 64 |
sio 254| -3 1 5 38 87 -12 .04 17 18 | --- --- --- ---
| -11 -60 |
Table 2.1545.4 GPS week: 1545 Day: 4 MJD: 55063.000
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 50 -55 -17 -.24 8 8 | -698 141 25 80
| -3 21 |
emr 89| 0 -2 -3 -173 -56 -21 .39 17 17 | 3511 -361 20 98
| 12 3 |
esa 131| 1 0 2 -55 27 87 .30 9 8 | -1054 -272 18 126
| 23 -14 |
gfz 188| 0 1 0 64 37 -21 -.20 10 10 | -318 632 28 137
| -73 14 |
grg 112| 6 1 0 -41 -60 -28 .95 44 37 | -131 280 114 232
| 27 19 |
igr n/a| 0 0 2 36 -27 -108 .01 6 5 | 6686 -1646 20 63
| -22 -35 |
jpl 123| -2 -1 -5 40 -22 32 .56 17 16 | 2896 -767 18 90
| -19 58 |
mit 265| 1 -1 0 12 -37 -34 -.22 12 11 | -15258 684 22 134
| -4 -12 |
ngs 219| 1 0 5 18 -6 -11 -.34 15 11 | 9273 7010 2243 3876
| -103 70 |
sio 254| -1 2 5 3 146 -34 -.02 19 15 | --- --- --- ---
| -8 -96 |
Table 2.1545.5 GPS week: 1545 Day: 5 MJD: 55064.000
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 48 -24 -7 -.21 10 9 | -880 6 26 97
| 22 -15 |
emr 89| 3 -1 -4 -157 -4 -39 .33 17 17 | 2703 -1494 24 101
| 17 -44 |
esa 131| 0 0 5 -60 6 73 .31 11 9 | -967 -189 23 135
| 46 27 |
gfz 188| 0 2 0 26 -72 -26 -.17 11 11 | -351 104 37 134
| -32 -39 |
grg 112| 2 -2 -2 -28 -15 76 1.02 42 39 | -295 60 81 258
| 45 -58 |
igr n/a| 0 0 2 38 -2 -65 .06 6 5 | 4547 -2481 28 88
| -13 -28 |
jpl 123| -3 -2 -7 22 10 -13 .56 19 18 | 1667 -1302 19 78
| -23 -8 |
mit 265| 0 0 -1 31 -66 15 -.17 12 11 | -15635 -903 21 135
| -12 -9 |
ngs 219| 0 -1 1 24 91 -32 -.28 12 8 | 12479 1446 2221 3450
| -31 -23 |
sio 254| -1 0 3 46 103 -5 -.07 16 15 | --- --- --- ---
| -44 -73 |
Table 2.1545.6 GPS week: 1545 Day: 6 MJD: 55065.000
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 -1 0 56 -23 -47 -.22 8 8 | -361 -40 14 72
| 8 -7 |
emr 89| 5 -4 -3 -157 18 -24 .39 18 18 | 2029 -2491 16 69
| 11 -65 |
esa 131| 1 0 1 -65 43 63 .28 9 9 | -2803 3226 18 120
| 43 5 |
gfz 188| 0 3 2 21 -109 -11 -.16 11 11 | 325 -255 29 131
| -67 -18 |
grg 112| 2 0 0 15 -19 -61 1.03 40 38 | 550885 -252643 74 224
| 17 -50 |
igr n/a| 0 0 0 20 -11 -56 .09 5 5 | 2796 -3458 20 64
| 43 0 |
jpl 123| 0 -1 -5 4 9 42 .61 18 17 | 1279 -2255 19 95
| 30 32 |
mit 265| 0 0 0 -3 -66 -3 -.16 12 11 | -16325 1515 22 149
| 2 5 |
ngs 219| 0 0 0 48 81 17 -.21 12 9 | -560412 306043 2304 4016
| -58 -31 |
sio 254| -2 0 4 23 104 -29 -.12 18 17 | --- --- --- ---
| -38 -69 |
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 3.1545.0 GPS week: 1545 Day: 0 MJD: 55059.000
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 --- --- 31 --- 16 --- 17 23 --- 13 | 18 --- --- 19 --- 20 --- 21 32 --- 17
2 | 5 18 9 10 49 4 16 8 7 26 4 | 22 32 26 29 46 24 29 25 23 29 23
3E | 16 19 13 13 48 8 17 15 25 18 6 | 30 39 34 31 54 29 39 36 41 37 32
4 | 6 13 9 9 29 5 10 10 7 20 3 | 30 34 36 39 28 32 28 37 33 37 33
6E | 12 20 11 14 24 8 15 20 16 21 6 | 129 130 128 128 132 126 129 122 130 121 126
7 | 8 15 12 8 37 3 16 11 15 12 4 | 19 31 23 23 37 19 28 21 19 15 19
8 | 4 8 10 6 22 3 9 9 11 10 3 | 24 26 24 28 25 23 26 23 23 22 22
9 | 5 10 6 8 32 5 10 9 10 15 3 | 17 20 20 19 25 17 20 18 21 20 17
10 | 6 12 7 7 33 5 7 10 8 9 3 | 24 22 29 28 19 25 22 28 25 29 25
11 | 6 13 7 8 68 5 15 7 10 12 3 | 27 38 34 32 55 30 40 26 32 29 30
12 | 5 16 11 15 29 4 18 11 10 20 4 | 16 27 22 15 39 16 28 19 14 20 16
13E | 7 15 9 9 29 3 17 15 12 11 4 | 21 26 26 30 37 22 28 20 24 20 21
14E | 8 14 7 8 24 5 17 17 16 20 5 | 43 44 43 41 50 43 45 51 44 50 44
15E | 11 29 11 9 28 5 23 10 12 17 5 | 18 35 18 23 29 18 28 21 17 27 19
16 | 9 22 12 10 26 6 21 12 12 21 5 | 23 29 19 13 35 20 31 18 24 22 19
17 | 6 15 7 6 44 4 16 8 10 16 3 | 32 32 27 30 28 28 29 36 35 38 31
18 | 8 18 13 12 67 5 24 8 13 18 5 | 25 36 26 31 61 24 39 26 29 22 27
19 | 9 21 8 11 31 5 20 12 11 14 4 | 18 31 17 19 26 18 28 24 21 24 19
20 | 8 21 10 11 27 5 19 7 9 16 4 | 14 25 20 20 30 16 24 15 20 14 15
21 | 5 16 9 11 24 4 21 9 13 22 4 | 29 40 34 30 43 30 40 29 33 36 31
22 | 7 17 11 9 60 3 21 9 12 14 4 | 18 25 20 23 45 18 26 24 25 21 20
23E | 10 18 14 10 25 5 26 19 12 14 5 | 32 39 39 36 43 34 42 35 37 33 34
24 | 5 14 7 11 42 3 10 9 8 15 3 | 24 29 31 33 33 26 24 26 23 27 26
25 | 5 11 8 5 --- 3 9 7 12 11 3 | 13 18 18 16 --- 13 13 11 14 10 12
26E | 13 19 10 11 99 6 17 9 14 24 5 | 43 48 47 42 67 44 49 47 44 54 44
27 | 6 10 6 10 38 5 10 10 9 15 3 | 15 19 17 17 27 15 19 17 17 18 15
28 | 5 18 8 6 28 3 16 10 12 21 4 | 21 26 19 19 37 20 27 21 16 22 17
29 | 9 25 12 16 32 7 27 9 12 15 5 | 25 38 24 32 30 23 33 29 31 29 26
30 | 7 13 9 7 28 4 11 11 8 13 3 | 13 23 21 17 27 16 27 18 16 16 16
31 | 7 21 10 11 37 5 19 11 12 20 5 | 18 29 25 25 37 18 29 20 22 16 19
32 | 7 16 9 12 21 4 15 7 7 12 3 | 13 18 21 19 25 15 21 15 18 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 10 10 41 5 17 11 12 17 |T 26 33 29 29 40 26 33 28 29 29 26
WRMS | 7 17 10 10 39 4 16 10 9 17 |NE 20 27 26 25 34 22 27 23 23 25 21
MEDI | 7 16 9 10 31 5 16 10 12 15 |MD 22 29 24 28 37 22 28 24 24 22 21
Table 3.1545.1 GPS week: 1545 Day: 1 MJD: 55060.000
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 | 11 --- --- 16 --- 10 --- 12 14 --- 7 | 20 --- --- 18 --- 17 --- 18 18 --- 16
2 | 7 18 9 10 66 4 17 10 9 27 4 | 15 27 16 21 45 17 23 17 22 20 16
3E | 13 21 8 14 49 6 16 18 23 20 6 | 18 30 25 21 43 24 30 33 36 37 24
4 | 8 12 6 9 52 4 10 12 8 18 3 | 26 33 29 34 33 29 29 29 36 32 29
6E | 12 21 8 11 27 7 16 19 13 22 5 | 126 132 129 130 130 128 130 126 130 128 128
7 | 6 15 7 13 40 2 18 9 14 14 4 | 12 27 21 16 42 17 28 17 17 13 15
8 | 6 8 8 9 16 3 8 7 9 9 3 | 16 21 22 16 25 15 23 18 18 18 17
9 | 8 11 7 10 35 3 11 8 12 16 3 | 12 16 15 16 24 11 18 14 15 20 12
10 | 5 13 9 9 35 5 7 12 13 9 3 | 18 21 18 19 20 18 17 19 22 18 17
11 | 7 16 5 7 71 3 16 8 10 11 3 | 21 35 29 25 52 25 35 22 25 25 24
12 | 6 19 13 16 29 5 19 10 11 19 5 | 14 28 17 14 36 15 25 18 17 18 13
13E | 7 15 9 10 18 4 19 14 10 14 4 | 14 24 17 19 29 12 24 16 14 17 13
14E | 8 14 7 7 35 4 19 17 14 22 5 | 42 47 43 42 52 44 46 48 45 49 44
15E | 8 22 12 13 39 3 25 9 13 16 5 | 14 25 20 20 34 15 22 17 22 19 15
16 | 10 25 8 10 26 6 20 11 10 20 5 | 19 30 19 17 34 18 27 18 21 18 17
17 | 6 17 8 6 21 5 16 6 9 8 3 | 18 26 19 21 23 18 24 22 23 24 20
18 | 6 22 11 11 72 4 24 8 10 18 5 | 19 33 22 22 57 21 35 22 23 20 21
19 | 8 22 5 14 39 4 20 12 7 14 4 | 17 26 13 17 26 12 19 18 19 18 14
20 | 7 19 9 9 31 5 17 8 12 16 4 | 14 25 17 18 31 15 25 16 18 17 14
21 | 6 19 6 10 45 5 21 8 9 24 4 | 21 35 26 23 42 23 34 18 20 28 23
22 | 6 18 10 10 62 3 21 10 11 15 4 | 16 23 18 19 39 16 25 21 21 19 17
23E | 9 20 9 8 26 4 26 17 6 12 5 | 23 32 21 19 36 20 35 25 23 24 21
24 | 8 13 7 9 35 4 10 7 7 13 3 | 16 22 24 21 25 19 20 16 15 20 18
25 | 6 13 7 7 --- 3 8 8 10 14 3 | 11 22 15 15 --- 11 15 11 16 11 11
26E | 13 21 8 14 99 6 18 12 15 27 5 | 27 37 33 33 40 29 34 35 31 38 31
27 | 8 13 8 11 41 4 13 8 11 16 4 | 12 17 13 15 28 10 17 14 15 18 10
28 | 7 17 8 12 23 4 18 8 8 17 4 | 19 28 23 16 39 17 28 20 19 23 19
29 | 8 30 10 10 48 6 27 8 10 14 5 | 16 32 18 17 33 17 26 18 17 18 16
30 | 6 16 6 8 21 2 11 11 9 14 3 | 10 25 18 16 27 13 23 11 12 12 13
31 | 10 20 7 11 37 4 20 14 8 17 4 | 12 30 20 20 40 16 28 21 17 18 17
32 | 5 13 8 7 24 5 12 8 9 12 3 | 10 16 13 12 21 9 17 11 12 14 9
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 10 44 4 18 11 11 17 |T 20 30 24 23 38 21 29 23 24 25 21
WRMS | 7 18 8 10 42 4 16 10 8 18 |NE 16 26 20 19 33 17 24 18 19 20 17
MEDI | 7 17 8 10 35 4 17 10 10 16 |MD 16 27 19 19 34 17 25 18 19 19 17
Table 3.1545.2 GPS week: 1545 Day: 2 MJD: 55061.000
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 | 22 --- --- 23 --- 18 --- 14 20 --- 11 | 21 --- --- 18 --- 21 --- 17 28 --- 15
2 | 7 18 10 10 63 3 15 8 10 30 5 | 18 28 20 25 44 18 23 21 20 24 18
3E | 12 18 13 15 52 7 15 13 24 18 6 | 22 30 26 22 36 22 30 29 29 33 23
4 | 7 14 7 9 50 3 8 6 7 21 3 | 21 28 26 28 26 22 21 23 24 24 22
6E | 13 19 15 15 22 8 15 17 19 19 6 | 71 69 71 67 77 67 71 72 64 70 68
7 | 6 18 7 10 40 4 16 10 12 15 4 | 17 33 23 23 38 19 31 22 18 16 19
8 | 5 10 7 7 24 4 9 7 12 10 3 | 13 22 19 17 27 14 23 16 14 12 14
9 | 7 11 7 12 32 3 9 7 13 15 3 | 11 17 19 22 23 16 21 16 16 20 14
10 | 6 12 10 7 43 4 8 11 12 12 3 | 19 23 24 24 21 21 18 24 23 27 21
11 | 6 15 7 8 66 3 17 7 10 11 3 | 22 35 31 24 48 26 38 25 21 25 25
12 | 6 19 14 14 34 4 20 8 13 19 5 | 14 30 14 13 37 13 28 17 18 18 13
13E | 6 19 9 9 38 5 18 10 10 15 4 | 11 27 18 18 40 14 24 13 15 18 13
14E | 10 14 12 9 37 7 19 16 15 25 5 | 21 31 31 30 53 25 32 30 27 32 26
15E | 7 23 12 17 35 5 23 10 8 14 5 | 11 25 13 23 27 14 21 16 15 19 13
16 | 9 24 8 18 21 7 19 8 14 21 5 | 17 29 17 12 35 16 28 16 20 20 15
17 | 12 16 8 7 21 5 14 7 11 11 4 | 18 28 23 26 29 25 22 27 30 28 23
18 | 9 22 10 12 49 4 22 8 13 19 5 | 19 34 26 23 43 23 37 26 24 20 23
19 | 9 22 12 11 42 5 20 8 10 15 5 | 19 29 21 19 23 18 24 21 26 21 18
20 | 8 20 11 11 28 5 19 6 12 17 4 | 12 21 23 17 29 15 26 14 17 14 13
21 | 8 19 9 12 43 4 20 9 15 25 5 | 23 36 27 25 39 23 36 22 28 33 25
22 | 9 18 9 10 41 4 19 9 12 16 4 | 21 25 24 26 28 20 24 23 21 21 20
23E | 8 17 9 8 19 3 22 12 10 12 4 | 15 22 21 14 32 14 27 16 16 16 14
24 | 7 13 8 12 29 4 10 8 10 16 3 | 18 22 24 27 33 20 22 19 19 23 20
25 | 7 14 6 5 --- 3 8 6 9 14 3 | 9 24 15 13 --- 13 13 12 16 13 11
26E | 14 24 10 13 108 7 19 12 15 28 6 | 37 45 43 43 46 38 42 43 42 49 40
27 | 7 12 8 13 39 4 9 8 14 13 3 | 10 18 17 18 26 13 19 15 18 16 12
28 | 5 17 10 13 28 6 16 8 9 17 4 | 15 27 18 13 41 15 27 14 14 17 13
29 | 12 27 9 16 37 5 24 9 10 15 5 | 24 37 29 34 34 29 31 29 32 27 27
30 | 6 14 9 7 29 4 11 8 8 16 3 | 11 25 21 16 25 14 26 14 13 12 14
31 | 8 23 6 11 40 5 18 12 12 19 5 | 16 30 17 19 41 16 28 20 15 20 17
32 | 5 15 8 9 30 3 15 7 14 13 4 | 12 14 18 16 24 13 18 13 16 14 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 10 11 43 5 17 10 13 18 |T 18 28 23 23 35 20 27 22 22 23 20
WRMS | 7 18 9 11 42 4 15 9 10 18 |NE 17 25 21 20 33 18 24 18 19 20 17
MEDI | 7 18 9 11 37 4 16 8 12 16 |MD 18 28 21 22 34 18 26 20 20 20 18
Table 3.1545.3 GPS week: 1545 Day: 3 MJD: 55062.000
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 | 25 --- --- 21 --- 29 --- 15 35 --- 13 | 33 --- --- 32 --- 28 --- 22 21 --- 22
2 | 6 16 8 10 46 6 18 8 16 30 5 | 19 29 24 24 38 21 26 22 26 26 20
3E | 16 25 13 14 61 8 17 12 24 14 6 | 18 38 27 27 33 20 30 26 28 29 22
4 | 6 9 8 10 41 8 11 5 12 20 3 | 28 34 33 32 30 30 29 30 35 31 30
6E | 16 19 14 15 46 9 18 17 22 17 6 | 108 113 111 112 110 109 112 104 113 107 108
7 | 7 17 11 16 36 6 20 9 13 15 5 | 22 36 30 28 39 27 34 25 24 22 24
8 | 6 10 10 7 24 4 11 7 11 12 3 | 23 32 27 24 24 26 31 26 31 26 25
9 | 7 11 6 11 41 5 12 6 15 13 3 | 17 20 19 19 32 16 21 17 19 18 16
10 | 6 12 11 10 39 7 10 11 14 13 4 | 20 23 31 24 19 26 21 26 27 27 23
11 | 7 13 9 9 62 5 17 7 9 10 3 | 22 36 28 26 48 26 37 25 24 27 25
12 | 6 18 11 12 41 4 23 8 15 19 5 | 16 31 18 16 42 18 33 17 22 19 16
13E | 7 16 9 8 30 5 20 10 9 16 4 | 15 27 20 19 38 17 27 16 20 21 17
14E | 11 15 12 8 42 7 21 18 15 21 5 | 57 62 60 58 65 60 64 63 59 66 60
15E | 6 23 12 10 28 5 24 8 12 15 5 | 14 28 18 19 26 14 26 16 19 21 16
16 | 7 26 10 14 21 8 21 10 13 19 5 | 20 35 24 23 36 21 32 21 26 23 21
17E | 8 12 12 9 34 7 15 6 13 10 4 | 29 31 27 28 46 26 29 30 33 29 28
18 | 7 23 12 12 44 5 26 8 14 20 5 | 25 37 27 31 49 25 37 29 23 25 26
19 | 7 20 10 11 51 6 21 11 12 14 4 | 17 27 17 19 28 16 25 22 23 23 18
20 | 7 17 12 9 34 6 18 7 9 16 4 | 15 23 20 18 35 16 25 16 15 15 14
21 | 8 20 9 10 34 5 23 13 13 27 5 | 22 37 28 28 42 27 38 26 26 33 26
22 | 7 15 9 11 36 7 20 10 12 16 4 | 17 24 18 22 30 18 24 19 20 18 17
23E | 7 16 12 10 24 4 22 9 6 14 4 | 25 32 29 30 38 27 34 26 27 27 26
24 | 7 10 6 9 27 5 10 6 12 16 3 | 17 25 25 23 26 19 20 19 23 21 20
X25 | 7 12 7 7 --- 4 --- 5 8 15 3 | 11 25 19 15 --- 16 --- 14 16 13 14
26E | 16 20 13 9 96 6 18 11 18 25 6 | 47 50 46 44 52 47 50 49 46 54 45
27 | 7 12 8 12 49 5 12 6 13 12 3 | 14 22 20 18 39 14 21 18 18 17 15
28 | 6 17 11 13 26 5 21 9 10 18 4 | 19 31 20 16 38 21 33 21 24 26 19
29E | 9 23 13 17 32 7 21 6 12 16 5 | 41 47 35 37 56 33 43 42 39 42 39
30 | 4 13 9 9 25 5 11 8 10 14 3 | 15 25 23 18 30 15 25 18 19 15 17
31 | 11 22 9 10 40 5 17 10 11 16 4 | 19 31 22 25 40 21 29 23 25 20 20
32 | 5 15 10 8 24 5 17 6 12 12 3 | 10 15 17 13 24 12 19 11 20 15 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 11 11 42 6 18 10 13 17 |T 25 34 28 28 39 26 33 27 28 28 25
WRMS | 7 17 10 11 42 6 17 10 11 18 |NE 19 27 24 22 32 21 27 21 24 23 20
MEDI | 7 16 10 10 36 5 18 8 12 16 |MD 19 31 24 24 38 21 29 22 24 23 21
Table 3.1545.4 GPS week: 1545 Day: 4 MJD: 55063.000
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 | 13 --- --- 26 --- 32 --- 13 29 --- 11 | 20 --- --- 23 --- 40 --- 15 38 --- 16
2 | 7 16 8 10 52 4 15 7 10 27 4 | 18 27 23 26 41 21 26 20 22 27 20
3E | 14 15 11 11 73 6 12 12 26 13 5 | 15 30 27 25 47 21 29 26 28 30 22
4 | 7 12 7 9 36 5 9 11 13 17 3 | 20 29 25 31 23 26 24 28 28 29 24
6E | 16 17 12 12 67 5 15 17 23 15 6 | 73 77 72 79 71 75 75 69 80 68 73
7M | 13 18 9 11 39 4 17 19 13 26 5 | 22 31 25 24 40 21 32 26 22 25 21
8M | 6 12 7 7 32 3 10 10 12 14 3 | 15 25 23 18 25 19 22 22 20 17 17
9M | 8 13 6 12 48 4 11 10 12 18 4 | 23 29 27 31 30 26 29 26 30 38 26
10 | 6 12 8 5 36 5 7 8 18 11 3 | 18 24 19 22 19 22 20 21 31 21 19
11 | 7 15 7 11 45 4 17 9 10 8 3 | 20 35 31 26 45 26 38 22 23 24 25
12 | 7 17 10 14 34 4 20 10 14 18 5 | 19 28 20 20 38 18 31 16 22 20 17
13E | 4 15 8 10 28 5 18 15 13 13 4 | 13 25 18 15 38 15 24 15 22 17 14
14E | 9 13 9 7 47 8 21 11 15 16 4 | 40 42 38 40 43 42 44 40 35 40 38
15E | 5 24 11 11 30 4 21 15 12 13 5 | 14 30 18 22 22 17 24 17 23 25 17
16M | 7 27 8 15 22 6 21 10 15 16 5 | 16 34 20 16 34 16 31 15 22 20 17
17E | 8 14 8 10 31 4 15 8 16 12 4 | 26 29 31 27 30 25 31 28 25 31 26
18M | 7 23 11 14 48 5 23 17 14 31 6 | 38 47 40 43 53 37 47 38 37 28 37
19 | 7 22 8 9 53 5 18 9 8 9 4 | 19 29 16 20 38 16 23 19 20 17 17
20M | 6 17 9 9 31 4 16 10 14 15 4 | 12 22 20 19 32 15 24 14 14 11 13
21M | 10 17 8 9 28 7 21 15 16 28 5 | 23 36 30 29 46 28 37 29 30 36 27
22M | 10 17 7 10 39 9 20 18 12 21 5 | 48 49 47 47 49 48 53 53 50 54 47
23E | 5 15 9 9 25 4 21 11 13 9 4 | 19 28 27 21 32 22 26 19 26 19 21
24 | 8 13 7 8 28 4 9 7 12 13 3 | 15 21 24 23 25 20 20 17 23 21 19
X25M | 7 12 10 12 --- 5 --- 13 12 --- 4 | 13 21 23 16 --- 15 --- 16 18 --- 14
26E | 13 23 13 12 97 13 20 20 27 43 7 | 80 85 87 82 81 86 87 88 88 85 83
27M | 9 14 7 12 57 4 11 11 13 11 4 | 15 24 21 26 39 20 24 21 25 26 19
28 | 6 19 8 10 41 4 17 9 16 21 4 | 19 29 23 17 39 21 30 19 22 26 18
29E | 8 25 8 15 28 5 25 16 13 15 5 | 38 45 40 43 44 37 45 40 36 38 38
30 | 5 13 6 7 20 4 10 9 15 15 3 | 13 23 18 21 27 17 23 14 24 14 15
31M | 11 22 8 11 39 6 22 14 17 15 5 | 13 30 19 23 41 16 29 19 19 16 16
32 | 5 13 7 6 25 5 13 9 13 10 3 | 11 15 18 17 25 12 20 13 16 13 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 9 10 44 6 17 12 15 19 |T 24 33 29 28 38 27 33 26 29 28 25
WRMS | 8 17 8 10 36 5 16 11 11 15 |NE 17 25 22 22 31 22 25 18 24 21 18
MEDI | 7 15 8 10 36 5 17 11 13 15 |MD 19 29 23 23 38 21 29 21 24 25 19
Table 3.1545.5 GPS week: 1545 Day: 5 MJD: 55064.000
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 --- --- 22 --- 19 --- 14 16 --- 11 | 16 --- --- 24 --- 32 --- 20 24 --- 18
2 | 8 13 6 7 62 6 18 9 9 28 4 | 20 27 25 22 38 23 29 21 27 27 22
3E | 12 16 8 10 64 7 16 13 21 16 5 | 15 29 27 20 42 21 30 26 29 29 23
4 | 10 12 6 7 37 7 14 15 12 16 4 | 28 34 35 30 36 30 33 32 32 35 31
X5 | 4 --- --- --- --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
6E | 14 18 9 12 64 6 16 18 21 15 5 | 79 90 82 84 84 83 89 85 87 84 83
7 | 9 16 7 11 33 5 15 10 8 13 4 | 23 34 25 24 39 23 32 25 26 22 23
8 | 6 11 8 10 23 5 12 9 8 11 3 | 23 30 29 29 28 26 33 27 23 26 25
9 | 10 13 11 10 41 4 9 16 13 14 4 | 25 32 30 32 34 29 32 29 33 31 28
10 | 9 8 5 8 48 4 11 10 12 11 3 | 20 27 26 27 22 23 28 24 31 27 25
11 | 8 14 6 9 48 5 19 6 8 9 3 | 19 36 27 24 45 23 39 20 23 22 24
12 | 7 17 10 16 35 6 22 9 9 18 5 | 17 30 23 21 38 20 33 17 19 21 18
13E | 6 19 11 13 27 6 23 17 13 14 5 | 19 32 25 24 38 21 31 24 22 25 22
14E | 9 13 8 7 29 4 24 11 8 13 4 | 53 57 54 52 57 52 56 55 50 57 54
15E | 9 21 11 13 29 6 26 12 12 17 5 | 15 29 20 23 26 19 28 21 28 26 20
16 | 8 23 11 14 19 8 23 10 15 16 5 | 21 34 26 19 34 19 35 19 25 17 21
17E | 8 12 5 8 28 6 22 10 12 8 4 | 23 27 25 19 40 22 31 24 26 26 23
18 | 10 21 9 15 46 6 24 9 11 22 5 | 20 36 26 23 44 21 39 22 23 21 22
19E | 7 23 11 9 40 5 23 9 5 10 4 | 24 33 27 22 37 23 32 27 27 26 25
20 | 7 16 11 11 33 5 18 10 9 15 4 | 14 24 23 23 34 17 27 18 19 16 18
21 | 9 16 6 12 43 6 23 13 15 26 5 | 20 35 29 26 36 26 37 25 27 33 26
22 | 12 17 8 9 48 6 21 10 10 16 4 | 41 51 46 47 48 44 50 48 50 48 47
23E | 8 19 8 11 24 7 22 10 13 9 4 | 21 32 27 27 38 24 36 20 28 23 24
24 | 9 11 5 8 31 4 14 6 10 13 3 | 19 29 29 23 27 24 28 21 26 25 24
X25 | 13 27 16 12 --- 10 --- 10 25 --- 7 | 15 41 24 25 --- 24 --- 20 35 --- 21
26E | 23 25 43 16 85 14 22 18 21 16 9 | 54 63 82 65 59 64 61 60 65 61 62
27 | 9 11 9 9 46 4 10 13 12 10 4 | 22 28 25 29 32 25 29 26 29 26 24
28 | 8 17 7 12 29 6 20 11 12 23 5 | 16 27 24 20 36 17 32 18 11 27 17
29E | 11 20 10 17 26 5 25 11 12 13 5 | 24 34 29 31 32 30 35 33 35 33 29
30 | 8 15 6 8 23 4 12 10 12 15 4 | 14 28 22 21 28 19 28 16 24 20 19
31 | 6 20 8 10 42 5 25 11 10 13 4 | 16 30 22 23 39 19 32 17 21 17 19
32 | 6 15 8 7 33 2 14 11 10 9 3 | 12 20 18 17 30 14 23 15 19 16 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 11 11 42 6 19 12 12 16 |T 24 35 31 28 38 27 36 27 30 29 27
WRMS | 9 17 9 11 39 5 18 11 8 15 |NE 18 28 25 22 33 22 30 20 23 24 21
MEDI | 9 16 8 10 35 6 20 10 12 14 |MD 20 32 26 24 37 23 32 24 27 26 23
Table 3.1545.6 GPS week: 1545 Day: 6 MJD: 55065.000
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 | 22 --- --- 25 --- 32 --- 14 32 --- 13 | 24 --- --- 18 --- 29 --- 17 36 --- 15
2 | 7 17 8 10 65 6 21 15 9 32 5 | 24 27 23 24 55 22 28 27 27 31 22
3E | 11 15 8 11 58 7 15 14 25 16 5 | 19 29 24 23 38 23 28 26 38 27 22
4 | 9 12 7 9 37 5 11 17 10 18 4 | 29 31 32 33 29 30 29 36 32 34 30
X5 | 5 --- 203 --- --- 154 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
6E | 12 18 9 12 54 7 16 18 20 14 5 | 113 119 114 116 101 115 114 115 121 112 115
7 | 7 18 9 10 31 5 18 9 10 14 4 | 22 33 24 26 37 22 31 26 24 22 23
8 | 5 11 5 5 22 4 10 7 9 12 3 | 16 22 21 21 26 18 24 18 19 17 18
9 | 8 13 8 10 29 4 9 14 10 17 4 | 20 20 23 20 30 18 25 20 23 19 18
10 | 7 9 5 10 37 5 10 11 12 16 3 | 22 23 26 24 23 24 23 26 29 29 23
11 | 7 16 8 10 43 5 16 4 10 11 3 | 25 35 33 28 50 31 38 24 31 27 28
12 | 8 18 11 14 34 5 19 9 11 21 5 | 21 32 20 17 40 21 33 23 21 29 19
13E | 7 19 11 9 28 7 22 12 10 17 4 | 20 33 23 23 41 21 33 24 25 27 23
14E | 6 11 8 8 33 4 24 14 13 15 4 | 42 43 43 45 44 40 42 45 42 43 43
15E | 8 23 14 12 36 6 22 8 9 16 5 | 18 28 19 26 33 20 25 23 26 30 20
16 | 9 24 11 14 25 4 22 13 12 17 5 | 24 35 21 15 37 21 34 21 24 20 21
17E | 9 20 9 9 33 5 15 13 10 17 4 | 32 33 31 32 37 32 36 34 34 35 31
18 | 8 23 11 13 38 5 24 10 7 22 5 | 25 38 27 31 44 26 40 25 26 19 26
19E | 8 24 7 11 35 7 19 12 12 13 4 | 24 34 27 27 37 24 27 31 29 28 25
20 | 6 17 14 9 31 5 15 10 11 18 4 | 17 26 25 21 34 21 28 21 19 20 19
21 | 10 17 7 12 54 4 23 11 7 24 5 | 26 39 32 28 47 29 43 28 28 36 29
22 | 9 17 11 9 37 4 23 9 8 18 4 | 41 46 40 39 56 40 48 39 43 44 39
23E | 6 22 8 8 23 6 18 10 11 12 4 | 25 34 26 25 38 28 34 22 28 24 24
24 | 8 12 8 12 34 4 11 6 12 13 3 | 23 25 29 26 28 24 25 23 27 23 24
X25 | 11 28 21 11 --- 14 --- 12 28 --- 8 | 21 29 27 22 --- 28 --- 16 31 --- 20
26E | 10 27 10 13 91 8 19 18 19 25 6 | 67 74 62 62 81 66 69 67 68 70 64
27 | 8 14 9 11 33 4 9 10 11 16 4 | 16 19 21 19 31 16 21 17 21 18 15
28 | 6 19 13 9 27 4 20 11 9 29 5 | 18 33 25 21 43 21 34 19 19 30 20
29E | 10 23 10 14 28 3 23 15 11 16 5 | 28 35 27 28 31 28 36 33 30 35 28
30 | 6 13 6 10 29 4 11 8 12 16 3 | 16 22 18 21 27 19 25 16 22 18 16
31 | 6 23 7 11 45 6 23 8 9 14 4 | 18 34 21 27 37 21 30 19 21 15 20
32 | 6 14 8 8 30 5 14 10 13 12 3 | 14 17 17 16 27 14 20 15 18 16 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 9 11 40 5 18 12 12 18 |T 27 34 30 29 40 28 35 28 31 30 27
WRMS | 8 18 9 11 38 5 17 11 9 17 |NE 21 27 24 22 35 23 28 22 26 26 21
MEDI | 8 17 9 10 34 5 18 11 11 16 |MD 23 33 25 25 37 24 31 24 27 27 23
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 4.1545 GPS week: 1545 MJD: 55059.0-55065.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2977 |U 15 12 96 |U 5 7 22 |U 9 8 19 |
emr | emr 2867 | 17 15 101 |U 7 8 23 |U 10 11 24 |
esa | esa 2893 | 14 14 84 |U 5 6 21 | 8 8 20 |
gfz | gfz 2944 |U 15 15 87 |U 9 10 31 | 8 8 20 |
grg | grg 2784 | 11 12 38 |U 7 7 25 | 10 11 23 |
igr | igr 2841 | 15 12 75 | 6 8 26 | 9 8 20 |
igs | igs 2880 | 14 12 61 | 5 7 21 | 8 8 20 |
jpl | jpl 2812 | 15 14 68 |U 5 7 21 |U 9 9 22 |
mit | mit 2976 |U 17 18 95 |U 6 7 24 |U 9 9 21 |
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 5.1545.0 GPS week: 1545 Day: 0 MJD: 55059.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 7 6 21 | 5 6 20 | 7 6 13 |
emr | emr 2872 | 9 8 28 | 8 8 28 | 10 9 16 |
esa | esa 2880 | 7 6 20 | 4 7 22 | 7 7 15 |
gfz | gfz 2950 | 8 7 22 | 10 13 23 | 7 7 13 |
grg | grg 2784 | 8 8 31 | 6 10 24 | 10 11 18 |
igr | igr 2877 | 7 6 20 | 5 6 20 | 7 5 13 |
igs | igs 2876 | 7 6 21 | 5 6 22 | 7 6 13 |
jpl | jpl 2872 | 9 8 25 | 5 7 22 | 7 7 15 |
mit | mit 2976 | 8 8 22 | 5 7 23 | 8 7 15 |
Table 5.1545.1 GPS week: 1545 Day: 1 MJD: 55060.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2970 | 8 14 28 | 5 9 24 | 7 7 23 |
emr | emr 2868 | 10 20 50 | 6 8 22 | 8 10 25 |
esa | esa 2880 | 8 15 32 | 5 7 22 | 7 6 22 |
gfz | gfz 2949 | 8 18 46 | 8 9 21 | 7 7 24 |
grg | grg 2784 | 8 14 27 | 8 8 34 | 8 9 24 |
igr | igr 2859 | 8 14 36 | 5 7 23 | 8 7 23 |
igs | igs 2870 | 8 16 37 | 4 8 22 | 7 6 22 |
jpl | jpl 2868 | 8 13 33 | 5 6 25 | 8 10 24 |
mit | mit 2976 | 17 55 181 | 5 9 27 | 7 7 21 |
Table 5.1545.2 GPS week: 1545 Day: 2 MJD: 55061.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2955 | 7 7 23 | 6 7 26 | 13 11 17 |
emr | emr 2868 | 11 10 33 | 7 7 27 | 12 10 19 |
esa | esa 2880 | 8 9 29 | 6 4 21 | 10 8 18 |
gfz | gfz 2950 | 8 9 33 | 8 6 29 | 10 10 23 |
grg | grg 2784 | 8 12 34 | 7 7 26 | 13 13 23 |
igr | igr 2864 | 7 9 28 | 6 5 26 | 11 9 15 |
igs | igs 2902 | 8 8 29 | 5 7 25 | 11 9 17 |
jpl | jpl 2867 | 8 11 31 | 6 6 25 | 10 9 20 |
mit | mit 2976 | 8 8 27 | 6 6 26 | 11 9 19 |
Table 5.1545.3 GPS week: 1545 Day: 3 MJD: 55062.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2964 | 8 13 28 | 4 6 25 | 6 5 14 |
emr | emr 2868 | 13 17 34 | 9 8 22 | 8 9 23 |
esa | esa 2880 | 8 13 29 | 4 6 20 | 8 7 14 |
gfz | gfz 2944 | 10 15 32 | 6 9 28 | 7 6 15 |
grg | grg 2784 | 9 14 35 | 6 7 25 | 9 11 20 |
igr | igr 2784 | 9 13 30 | 5 6 23 | 8 6 16 |
igs | igs 2874 | 9 12 28 | 5 6 21 | 7 6 15 |
jpl | jpl 2772 | 9 14 32 | 4 7 20 | 9 9 21 |
mit | mit 2976 | 9 12 29 | 6 7 23 | 10 9 21 |
Table 5.1545.4 GPS week: 1545 Day: 4 MJD: 55063.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2959 | 54 32 519 | 5 7 21 | 10 8 19 |
emr | emr 2868 | 51 31 490 | 8 7 21 | 12 14 28 |
esa | esa 2880 | 46 32 417 | 5 7 21 | 10 7 21 |
gfz | gfz 2941 | 47 27 398 | 9 9 30 | 9 9 21 |
grg | grg 2784 | 16 13 74 | 8 8 22 | 9 10 23 |
igr | igr 2870 | 46 24 342 | 6 7 22 | 9 8 19 |
igs | igs 2874 | 45 27 253 | 6 7 20 | 10 10 21 |
jpl | jpl 2771 | 43 29 290 | 6 6 19 | 10 11 22 |
mit | mit 2976 | 56 25 350 | 6 8 23 | 10 9 25 |
Table 5.1545.5 GPS week: 1545 Day: 5 MJD: 55064.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2981 | 12 8 32 | 5 5 17 | 10 11 27 |
emr | emr 2865 | 14 11 42 | 7 8 19 | 11 11 29 |
esa | esa 2880 | 15 15 40 | 4 5 16 | 9 9 26 |
gfz | gfz 2942 | 16 18 50 | 11 7 35 | 10 11 26 |
grg | grg 2784 | 17 12 39 | 6 4 19 | 11 11 27 |
igr | igr 2774 | 23 14 50 | 7 20 41 | 12 12 31 |
igs | igs 2875 | 14 12 38 | 4 5 17 | 10 10 26 |
jpl | jpl 2769 | 15 15 41 | 5 5 17 | 9 10 25 |
mit | mit 2976 | 12 12 35 | 5 7 22 | 12 10 27 |
Table 5.1545.6 GPS week: 1545 Day: 6 MJD: 55065.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 7 6 18 | 5 8 23 | 9 9 23 |
emr | emr 2866 | 10 7 32 | 7 10 24 | 10 12 30 |
esa | esa 2976 | 9 7 20 | 6 8 24 | 8 11 24 |
gfz | gfz 2935 | 8 9 26 | 11 14 55 | 8 6 21 |
grg | grg 2784 | 8 8 25 | 6 6 23 | 10 11 28 |
igr | igr 2865 | 8 7 22 | 5 9 23 | 8 7 22 |
igs | igs 2892 | 8 6 21 | 6 9 22 | 7 7 22 |
jpl | jpl 2769 | 9 7 26 | 6 9 21 | 9 9 29 |
mit | mit 2976 | 8 6 22 | 6 8 26 | 7 9 22 |
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 6.1545 GPS week: 1545 MJD: 55059.500-55065.500
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 | -12 -7 -64 -74 -15 | 2 17
| 15 26 55 46 10 | 1
emr uuuuu | -11 -24 182 -29 -3 | 22 29
| 39 11 91 38 11 | 3
esa uuuuu | -9 -44 120 -66 1 | 19 30
| 33 15 104 85 10 | 2
gfz uuuuu | 14 34 3 -37 -4 | 15 21
| 14 14 54 67 7 | 2
grg xxxxx | 1 -35 -68 -32 -6 | -5 17
| 39 27 61 88 19 | 3
igr xxxxx | 4 -3 4 -5 -8 | 6 16
| 24 26 41 46 10 | 1
irf xxxxx | -13 -8 -42 -19 -3 | -1 16
| 8 6 23 11 5 | 2
jpl uuuuu | -11 -5 -12 -30 8 | 18 26
| 32 21 173 89 13 | 8
mit uuuuu | -4 3 -174 -6 -4 | 7 18
| 19 13 92 54 6 | 2
ngs uuuuu | -26 28 -135 99 0 | 5 18
| 50 43 132 55 11 | 1
sio uuuuu | 60 21 123 119 1 | 31 35
| 19 19 114 93 8 | 4
Table 7.1545.0 GPS week: 1545 Day: 0 MJD: 55059.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 1 36 -65 12 1 | 3 20
emr uuuuu | -7 -4 224 -41 -11 | 28 37
esa uuuuu | -36 -18 128 -196 -1 | 23 34
gfz uuuuu | 30 29 -49 65 7 | 14 23
grg xxxxx | 47 -6 -127 41 -46 | 1 15
igr xxxxx | 33 11 -9 33 0 | 7 19
irf xxxxx | -14 -3 -56 -8 1 | 0 19
jpl uuuuu | -22 6 14 -78 14 | 11 23
mit uuuuu | -11 13 -187 -18 -10 | 10 21
ngs uuuuu | 4 -46 -104 179 -6 | 6 20
sio uuuuu | 60 30 115 139 10 | 28 34
Table 7.1545.1 GPS week: 1545 Day: 1 MJD: 55060.500
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 -16 -90 -127 -3 | 1 18
emr uuuuu | -51 -19 288 34 -10 | 21 26
esa uuuuu | -26 -39 43 15 13 | 20 30
gfz uuuuu | 19 27 -4 -58 5 | 12 20
grg xxxxx | -20 -37 -76 -59 3 | -5 18
igr xxxxx | -24 22 -26 38 4 | 4 14
irf xxxxx | -21 -5 -24 -38 1 | -3 15
jpl uuuuu | 19 19 -122 15 13 | 9 19
mit uuuuu | -22 15 -78 -110 -8 | 5 15
ngs uuuuu | 31 -9 -179 111 -4 | 4 18
sio uuuuu | 43 37 210 28 6 | 26 31
Table 7.1545.2 GPS week: 1545 Day: 2 MJD: 55061.500
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 24 -93 -107 -16 | 2 17
emr uuuuu | -50 -37 283 -31 3 | 18 24
esa uuuuu | -1 -65 51 -133 -19 | 20 31
gfz uuuuu | 16 28 42 -11 -5 | 14 19
grg xxxxx | -18 1 -78 -133 -4 | -5 18
igr xxxxx | -11 12 -13 -19 -7 | 5 14
irf xxxxx | -5 -4 0 -19 -3 | -3 15
jpl uuuuu | 19 -13 -154 -72 23 | 10 20
mit uuuuu | 29 17 -101 -5 -6 | 4 15
ngs uuuuu | -86 47 -157 128 -2 | 4 18
sio uuuuu | 71 28 217 243 3 | 28 32
Table 7.1545.3 GPS week: 1545 Day: 3 MJD: 55062.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -42 -25 -66 -70 -19 | 3 16
emr uuuuu | -45 -29 123 -65 11 | 19 25
esa uuuuu | 49 -34 329 -23 -4 | 18 29
gfz uuuuu | 22 24 -46 -86 -14 | 16 20
grg xxxxx | -57 -77 -95 -57 2 | -8 15
igr xxxxx | -3 -22 55 -101 -15 | 6 14
irf xxxxx | -16 -7 -36 -20 -1 | -1 15
jpl uuuuu | 21 -22 -227 -133 20 | 17 23
mit uuuuu | -10 1 -70 48 2 | 5 16
ngs uuuuu | -80 54 -400 55 -9 | 6 18
sio uuuuu | 44 4 276 200 2 | 31 34
Table 7.1545.4 GPS week: 1545 Day: 4 MJD: 55063.500
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 -17 -133 -100 -21 | 2 16
emr uuuuu | -1 -32 200 -71 8 | 21 27
esa uuuuu | 16 -43 106 45 9 | 15 24
gfz uuuuu | -12 53 -16 -142 -5 | 15 20
grg xxxxx | -17 -47 25 -94 -8 | -7 15
igr xxxxx | 37 2 -9 4 -8 | 5 14
irf xxxxx | 2 -20 -68 -28 0 | -1 15
jpl uuuuu | -56 -1 80 -82 -1 | 22 28
mit uuuuu | 14 -16 -254 28 5 | 5 16
ngs uuuuu | -68 83 -55 123 -9 | 5 17
sio uuuuu | 98 -12 -15 116 2 | 32 35
Table 7.1545.5 GPS week: 1545 Day: 5 MJD: 55064.500
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 -30 -46 -74 -23 | 1 15
emr uuuuu | 24 -25 60 -42 -5 | 24 32
esa uuuuu | -47 -54 29 -69 5 | 18 29
gfz uuuuu | 19 24 104 -32 -7 | 17 23
grg xxxxx | 38 -53 6 -50 12 | -6 17
igr xxxxx | 8 5 68 8 -4 | 6 16
irf xxxxx | -20 -8 -53 -6 -6 | 1 18
jpl uuuuu | -12 15 287 10 -10 | 26 33
mit uuuuu | -11 4 -292 40 -1 | 8 21
ngs uuuuu | 3 23 -17 11 8 | 5 18
sio uuuuu | 53 36 8 133 -7 | 35 39
Table 7.1545.6 GPS week: 1545 Day: 6 MJD: 55065.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -8 -18 44 -54 -23 | 1 15
emr uuuuu | 50 -21 93 10 -19 | 26 34
esa uuuuu | -20 -53 157 -102 4 | 21 31
gfz uuuuu | 3 57 -12 7 -10 | 19 24
grg xxxxx | 35 -27 -130 127 0 | -4 18
igr xxxxx | -15 -53 -36 1 -25 | 7 17
irf xxxxx | -15 -10 -55 -17 -11 | 3 18
jpl uuuuu | -47 -40 39 132 -4 | 29 35
mit uuuuu | -20 -12 -239 -24 -6 | 10 22
ngs uuuuu | 16 48 -31 86 20 | 7 19
sio uuuuu | 54 28 52 -27 -13 | 37 41
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