[IGSREPORT-19403] Wk 1618 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jan 27 05:04:12 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1618 (Jan 09, 2011 - Jan 15, 2011)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1618[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1618[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1618[0-6].cls IGS GPS clock combination summary report.
igs16187.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16187.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 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | DGAR
0 | EMR | 26 26 WTZR WTZR
0 | ESA | UNSA
0 | GFZ | BRMU CAS1 ISPA KARR TOW2
0 | GRG | ADIS DGAR
0 | JPL | 26
0 | MIT | 26 26 MDVJ MDVJ
1 | COD | CONZ CONZ DGAR GUAT
1 | EMR | 26 HARB WTZR HARB WTZR
1 | GFZ | 4 26 CAS1 ISPA LPGS MDVJ
1 | GRG | ADIS DGAR
1 | JPL | COCO
1 | MIT | 26 26
2 | COD | 27 27 CAS1 DGAR
2 | EMR | 26 KIRU IRKT KIRU WTZR
2 | ESA | CAS1 UNSA WTZR
2 | GFZ | 26 CONZ DGAR GUAT KIRU MDVJ
2 | GRG | DGAR
2 | JPL | 26 DAV1 IRKJ
2 | MIT | 7 26 27 7 26 27 DAV1 DAV1
3 | ALL | 1 26
3 | COD | XMIS
3 | EMR | 26 3 HARB WTZR HARB IRKT WTZR
3 | ESA | 26 UNSA
3 | GFZ | 4 CAS1 DGAR KERG MDVJ RIOP
3 | GRG | ADIS DGAR
3 | JPL | HARB IRKJ
3 | MIT | 2 3 6 2 3 6 KOUC
4 | ALL | 1
4 | COD | DGAR
4 | EMR | 26 26 WTZR HARB WTZR
4 | ESA | 21 21 SUTH UNSA
4 | GFZ | 26 AUCK MDVJ
4 | GRG | AMC2 DGAR
4 | JPL | 26
4 | MIT | 26 26
5 | COD | MDVJ
5 | EMR | 26 26 WTZR WTZR YELL
5 | ESA | SUTH UNSA
5 | GFZ | 26 COCO DGAR MDVJ RAMO
5 | GRG | DGAR USN3
5 | JPL | 26 MCM4
5 | MIT | 26 26 ALGO AMC2 BJFS BRMU BRUS CHUR DAEJ DARW DAV1
5 | MIT | HARB HRAO IENG KOUR LAMA MAS1 MATE MAW1 MDVJ MEDI
5 | MIT | MIZU NICO NNOR NRC1 NTUS PDEL PERT PIE1 PTBB SCH2
5 | MIT | SPT0 STR1 SYOG TIXI TLSE TOW2 TSKB TWTF USN3 WES2
5 | MIT | WROC WSRT WTZR YELL BRMU
6 | COD | XMIS
6 | EMR | 26 26 HARB WTZR HARB WTZR
6 | ESA | DGAR SUTH UNSA
6 | GFZ | 26 WAB2 ZIMM
6 | GRG | ADIS AMC2
6 | JPL | 21 26
6 | MIT | 26 21 26
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
----+--------+--------+-------------
5 | MIT | ~16:30 | ~ 0.36 ns
6. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G15 | 2011_01_10 | 2011005
G15 | 2011_01_11 | 2011005
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 all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .6 1.8 -.3 24 -14 -18 .40
EMR | 1.4 .5 1.7 17 -61 13 .82
ESA | 7.0 3.4 6.3 47 -6 -52 .66
GFZ | -.4 1.3 -.4 -4 -2 -32 .37
GRG | 5.5 1.2 -9.8 22 88 -90 .61
JPL | 4.3 2.5 4.1 39 -48 62 .26
MIT | 1.8 -3.2 -8.2 24 -15 -19 .33
NGS | 4.0 -2.9 -4.7 -46 -110 33 .39
SIO | .0 5.1 -7.8 59 -34 -30 .46
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN. For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting 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 1.1618.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1618.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 2.1618.[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 3.1618.[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 5.1618.0-6).
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 1618 summary. (Jan 09, 2011 - Jan 15, 2011)
Table 1.1618.a GPS week: 1618 MJD: 55570.000-55576.000
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 231| 0 0 4 -23 -3 7 -.18 8 8 | -61 -936 16 69
| 0 0 0 12 24 18 .02 | 174 598
emr 87| 0 0 7 -32 110 36 .41 19 19 | -1090 -866 16 104
| 1 0 2 27 38 13 .02 | 1690 1545
esa 128| 0 0 -3 -68 -30 -45 .20 9 8 | 151 -1173 15 116
| 1 0 0 17 35 12 .03 | 1047 1357
gfz 189| 0 0 0 49 -57 15 -.20 10 11 | 258 -318 21 104
| 1 0 1 66 151 13 .02 | 286 640
grg 134| 1 1 -13 -22 -219 -19 .67 16 15 | 9285 -29887 44 210
| 0 1 2 24 29 15 .06 | 24114 77772
igr n/a| 0 0 1 20 -28 12 -.04 5 5 | -813 -546 17 113
| 0 0 0 17 41 21 .02 | 1300 1517
jpl 121| -1 0 7 -20 20 -41 .46 18 17 | 2408 -860 17 96
| 1 0 1 11 13 53 .02 | 1449 1496
mit 259| 1 0 -5 5 -46 27 -.34 13 12 | -4 -450 18 151
| 0 0 1 10 18 16 .02 | 149 564
ngs 217| 0 0 0 124 181 22 -.20 10 8 | 141017 498669 1964 3387
| 0 0 0 44 81 7 .03 | 895480 1801021
sio 260| 0 2 4 -81 8 -17 -.30 20 19 | --- --- --- ---
| 1 2 1 13 22 12 .02 | --- ---
Table 1.1618.b GPS week : 1618 MJD: 55570.000-55576.000
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 0 0 18 16 0 24 |
2 | 6 5 6 4 5 5 5 |
3 | 3 3 4 5 6 4 4 |
4 | 4 5 4 6 4 4 4 |
5 | 4 4 5 5 5 5 4 |
6 | 4 4 11 7 4 4 5 |
7 | 4 5 4 5 5 5 5 |
8 | 4 4 4 4 5 4 4 |
9 | 3 6 4 3 4 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 4 6 5 5 5 5 5 |
13 | 4 4 4 4 5 5 5 |
14 | 4 4 4 4 4 4 4 |
15 | 5 0 0 5 5 5 5 |
16 | 5 6 5 5 5 5 5 |
17 | 4 4 4 4 5 4 4 |
18 | 4 5 4 5 5 5 5 |
19 | 5 4 5 5 5 5 5 |
20 | 4 4 4 5 5 5 5 |
21 | 4 4 4 5 8 5 5 |
22 | 4 4 4 4 4 5 4 |
23 | 4 4 4 4 5 5 4 |
24 | 3 3 4 3 4 4 4 |
25 | 5 7 6 6 7 6 6 |
26 | 6 7 7 7 7 7 7 |
27 | 3 4 3 4 4 5 4 |
28 | 4 4 4 4 5 5 4 |
29 | 5 5 5 5 5 5 5 |
30 | 5 5 4 5 5 5 5 |
31 | 5 5 5 4 4 4 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 2.1618.0 GPS week: 1618 Day: 0 MJD: 55570.000
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 231| -1 -1 5 -32 -39 25 -.22 9 8 | -4 -768 14 68
| 41 19 |
emr 87| 3 0 11 -52 69 51 .39 18 18 | -621 36 16 111
| 42 -14 |
esa 128| 1 1 -3 -53 -82 -46 .24 7 7 | 1295 -2329 15 119
| -7 22 |
gfz 189| -1 -1 -2 70 233 17 -.21 11 11 | 94 -111 21 106
| -13 -47 |
grg 134| 1 3 -16 0 -238 -10 .59 16 15 | -54 228 44 188
| 20 3 |
igr n/a| 0 0 1 11 -80 -4 -.06 5 5 | -1397 513 16 115
| 43 -19 |
jpl 121| -1 0 8 -22 36 -43 .44 17 15 | 2587 385 16 93
| 15 -65 |
mit 259| 1 -2 -3 -8 -36 17 -.31 12 11 | -124 256 18 145
| 0 1 |
ngs 217| 0 0 1 108 41 21 -.24 8 7 | 21 -811 1762 3650
| -55 78 |
sio 260| 0 0 3 -87 27 -25 -.33 20 19 | --- --- --- ---
| 17 41 |
Table 2.1618.1 GPS week: 1618 Day: 1 MJD: 55571.000
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 231| 0 0 5 -33 -25 4 -.18 8 8 | -222 -628 16 67
| 42 -6 |
emr 87| -1 0 8 -70 94 37 .43 19 19 | -726 1458 19 108
| 58 -28 |
esa 128| 1 0 -4 -44 -49 -41 .20 8 8 | 434 -2314 17 115
| 19 13 |
gfz 189| -3 -1 -1 137 57 15 -.21 11 10 | -86 675 25 94
| -37 8 |
grg 134| 0 3 -15 -41 -225 -5 .60 15 15 | -41 -33 42 207
| 86 11 |
igr n/a| 0 0 0 20 -67 19 -.02 5 5 | -1161 1740 17 110
| -12 -27 |
jpl 121| -3 0 8 -10 27 18 .45 20 19 | 2687 1404 18 90
| 10 -36 |
mit 259| 2 -1 -2 3 -18 13 -.33 13 11 | -209 161 22 134
| -11 -12 |
ngs 217| -1 0 0 64 105 13 -.22 9 7 | -334 -292 1663 3285
| -20 60 |
sio 260| 1 0 6 -90 43 -23 -.28 20 19 | --- --- --- ---
| 24 38 |
Table 2.1618.2 GPS week: 1618 Day: 2 MJD: 55572.000
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 231| 0 0 4 -36 -3 -9 -.18 8 8 | 147 -1882 21 69
| 34 11 |
emr 87| -1 -1 9 -50 131 21 .43 20 19 | 777 -1669 13 90
| 28 -65 |
esa 128| 1 1 -3 -56 -24 -55 .24 9 9 | -1716 215 14 120
| 19 -26 |
gfz 189| 0 -1 0 129 -79 0 -.20 11 14 | 118 -237 22 110
| 3 -32 |
grg 134| 0 0 -16 -46 -207 -23 .65 16 15 | 63969 -206257 56 221
| 87 -37 |
igr n/a| 0 0 0 9 -30 39 -.02 5 5 | 701 -1483 18 95
| -21 -60 |
jpl 121| -1 0 7 -32 21 16 .45 19 17 | 4101 -2013 17 99
| -23 -93 |
mit 259| 1 0 -4 9 -39 31 -.31 12 10 | 260 -1369 19 145
| -21 2 |
ngs 217| -1 0 0 78 174 29 -.22 10 6 | -999999 4494749 2279 3389
| 25 43 |
sio 260| 1 3 5 -102 8 -9 -.30 18 19 | --- --- --- ---
| 19 57 |
Table 2.1618.3 GPS week: 1618 Day: 3 MJD: 55573.000
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 231| 0 1 3 -28 15 31 -.19 8 8 | -277 -308 17 66
| 35 -25 |
emr 87| 0 0 5 2 166 14 .42 20 20 | 1117 -3514 15 96
| 4 -76 |
esa 128| 0 0 -2 -66 21 -58 .20 8 8 | 1199 -1659 17 120
| 43 -44 |
gfz 189| 0 0 1 15 -171 -3 -.16 9 10 | 514 -429 21 91
| 24 -34 |
grg 134| 2 0 -15 -25 -209 -7 .70 17 15 | 556 -844 44 211
| 60 -72 |
igr n/a| 0 1 1 23 -12 -11 -.04 5 5 | 1340 -3079 17 106
| -12 -25 |
jpl 121| -2 0 7 -17 25 0 .48 19 17 | 4388 -3070 15 68
| 156 -205 |
mit 259| 1 0 -6 4 -72 4 -.34 13 12 | -43 -479 18 136
| -16 26 |
ngs 217| 0 0 0 145 237 34 -.18 10 8 | 1987591 -999999 2183 3410
| -48 -52 |
sio 260| 0 2 2 -72 -26 -29 -.32 20 21 | --- --- --- ---
| 14 73 |
Table 2.1618.4 GPS week: 1618 Day: 4 MJD: 55574.000
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 231| 0 0 5 -4 34 -16 -.14 8 8 | 153 -1621 15 72
| 45 1 |
emr 87| 2 0 4 0 152 43 .39 19 19 | -2710 -672 15 115
| 4 -31 |
esa 128| -1 0 -3 -88 -50 -22 .21 12 10 | -578 496 15 120
| 34 9 |
gfz 189| 0 0 0 -37 -182 14 -.19 10 9 | 657 -1374 21 97
| -4 -15 |
grg 134| 1 0 -12 -17 -185 -37 .76 19 15 | 163 -947 47 238
| 37 -81 |
igr n/a| 0 0 0 57 47 5 -.06 5 5 | -1779 -496 17 89
| 17 11 |
jpl 121| 1 0 6 -7 23 -88 .47 18 17 | 1140 -569 18 93
| -34 18 |
mit 259| 0 -1 -6 18 -41 52 -.34 14 13 | 69 -884 16 142
| -26 18 |
ngs 217| -1 0 0 196 270 18 -.20 12 11 | 100 -1582 2263 3755
| 18 -119 |
sio 260| 0 3 4 -60 11 0 -.27 18 18 | --- --- --- ---
| 6 69 |
Table 2.1618.5 GPS week: 1618 Day: 5 MJD: 55575.000
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 231| 0 0 4 -21 -11 18 -.18 8 8 | -39 -927 15 81
| 6 37 |
emr 87| 0 0 7 -22 79 47 .39 19 19 | -3184 -394 16 108
| 3 2 |
esa 128| 0 1 -4 -83 7 -49 .16 10 9 | 403 -2623 15 119
| 18 -16 |
gfz 189| 0 0 0 -6 -127 38 -.17 12 11 | 484 -760 21 127
| -19 -30 |
grg 134| 1 0 -10 17 -272 -43 .69 16 15 | 229 -884 42 198
| 14 -34 |
igr n/a| 0 0 2 3 -17 41 -.06 5 5 | -2055 -221 15 146
| 29 -2 |
jpl 121| 0 -1 5 -17 -5 -93 .45 17 16 | 894 -649 18 123
| 12 -2 |
mit 259| 2 0 -5 -6 -62 30 -.36 14 12 | 28 -480 18 220
| -7 22 |
ngs 217| 0 0 0 141 225 15 -.17 9 8 | -88 -848 1851 3154
| -30 -80 |
sio 260| 0 4 4 -82 -9 -28 -.28 19 18 | --- --- --- ---
| 18 72 |
Table 2.1618.6 GPS week: 1618 Day: 6 MJD: 55576.000
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 231| 0 0 5 -10 6 -1 -.18 8 8 | -191 -420 15 65
| 22 -9 |
emr 87| 0 0 6 -36 79 39 .38 19 19 | -2288 -1308 19 103
| 47 5 |
esa 128| 1 0 -4 -84 -40 -41 .17 8 8 | 23 0 13 102
| 45 23 |
gfz 189| -1 0 -2 33 -130 21 -.23 10 10 | 30 6 21 109
| -21 -31 |
grg 134| 1 1 -9 -43 -196 -5 .68 17 17 | 176 -477 39 209
| 114 -69 |
igr n/a| 0 0 1 15 -37 0 -.03 5 5 | -1340 -799 19 133
| 7 6 |
jpl 121| 0 0 7 -39 15 -99 .47 19 18 | 1064 -1509 18 106
| -4 -35 |
mit 259| 1 -1 -6 15 -58 40 -.37 16 13 | -14 -359 20 138
| -10 8 |
ngs 217| 0 0 0 136 214 25 -.15 9 8 | -166 -533 1753 3070
| -33 -55 |
sio 260| -1 5 4 -73 4 -6 -.28 21 18 | --- --- --- ---
| 17 57 |
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 3.1618.0 GPS week: 1618 Day: 0 MJD: 55570.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 5 --- --- --- --- 59 --- --- --- --- 0 | 47 --- --- --- --- 93 --- --- --- --- 47
2 | 8 11 4 34 14 5 13 11 7 30 5 | 34 37 40 50 41 38 31 38 33 32 35
3 | 8 14 6 8 12 5 11 9 8 9 3 | 28 33 31 30 38 28 35 27 24 27 28
4 | 7 10 4 11 12 4 9 12 8 25 3 | 33 36 39 38 45 36 33 39 35 33 35
5 | 7 20 6 9 15 4 20 14 7 19 4 | 23 38 26 23 38 25 35 22 23 26 23
6 | 6 16 6 10 11 3 12 9 9 23 3 | 24 31 26 28 33 24 30 25 19 32 25
7 | 6 21 5 7 19 5 20 11 6 15 4 | 27 35 28 24 33 28 33 28 27 27 25
8 | 7 12 4 7 13 4 8 11 7 29 3 | 23 30 26 24 24 23 27 24 24 36 23
9 | 8 11 4 9 12 6 10 14 7 14 3 | 26 31 29 29 28 26 28 27 28 31 27
10 | 9 11 4 7 15 5 11 12 7 29 3 | 24 27 29 28 36 26 27 26 25 35 25
11 | 8 16 5 6 15 4 13 10 6 19 3 | 42 48 46 44 61 45 44 51 45 44 45
12E | 9 22 8 10 19 5 18 14 5 15 4 | 22 30 27 25 40 25 28 24 21 22 23
13E | 6 19 7 6 17 6 17 10 5 13 3 | 19 29 19 17 26 17 24 19 16 18 16
14E | 8 19 9 8 16 4 17 14 8 12 4 | 28 34 38 29 40 31 33 33 30 31 31
15E | 9 18 6 9 21 4 22 14 8 20 4 | 8 17 8 5 14 12 18 7 5 7 8
16E | 5 23 9 14 22 3 23 13 7 17 4 | 22 30 23 24 41 23 28 25 22 23 21
17 | 8 20 5 11 18 5 17 12 5 14 4 | 23 36 29 27 41 26 33 25 23 19 24
18 | 9 20 7 8 16 4 22 8 8 14 4 | 26 41 32 27 34 28 41 24 28 28 28
19 | 6 23 9 8 16 5 22 13 8 15 4 | 25 36 27 24 34 25 34 24 23 23 23
20 | 8 19 7 14 16 5 20 12 7 20 4 | 22 33 23 27 29 22 31 23 20 26 21
21 | 8 11 7 10 13 7 12 9 9 31 4 | 30 34 35 35 40 31 28 39 31 42 33
22 | 9 19 9 6 18 6 19 10 8 21 4 | 24 38 31 26 40 25 37 22 24 22 26
23E | 8 19 6 10 17 4 24 10 8 17 4 | 25 34 23 21 37 24 30 24 21 27 23
24 | 7 10 4 7 14 3 8 10 5 20 3 | 31 31 36 34 45 34 31 38 33 29 33
X25E | 15 20 6 10 15 4 --- 16 8 --- 5 | 29 42 40 36 46 36 --- 35 35 --- 34
26E | 19 19 10 12 16 6 14 23 20 19 6 | 21 34 27 31 38 26 31 37 33 26 25
27 | 9 11 5 9 12 3 9 11 7 17 3 | 20 27 24 23 25 21 21 25 24 26 21
28E | 8 19 7 8 17 8 15 10 7 12 3 | 22 32 25 21 39 25 26 24 21 22 21
29 | 12 25 8 12 15 4 24 11 8 19 4 | 23 33 24 29 29 23 32 23 22 26 22
30 | 9 25 9 11 20 7 16 15 10 21 4 | 24 38 29 29 40 29 35 26 24 32 25
31 | 11 21 9 9 22 5 22 16 8 22 5 | 26 33 30 27 42 25 32 27 24 26 25
32 | 8 15 6 9 13 6 16 12 8 14 3 | 20 23 22 23 25 20 23 22 16 21 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 7 11 16 5 17 12 8 20 |T 25 33 28 27 36 28 30 27 25 27 26
WRMS | 8 18 7 11 15 5 15 11 7 19 |NE 26 34 30 29 36 27 31 28 26 29 26
MEDI | 8 19 6 9 16 5 16 12 8 19 |MD 24 33 28 27 38 25 31 25 24 26 25
Table 3.1618.1 GPS week: 1618 Day: 1 MJD: 55571.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 5 --- --- --- --- 53 --- --- --- --- 0 | 34 --- --- --- --- 68 --- --- --- --- 36
2 | 8 11 8 15 9 5 23 8 8 29 4 | 16 22 25 30 23 23 24 19 22 19 20
3 | 7 15 7 9 12 4 12 9 8 10 3 | 26 30 28 31 34 28 33 28 23 26 27
4 | 7 11 7 27 10 7 10 13 11 21 5 | 18 22 25 28 28 23 21 23 25 21 21
5 | 7 23 6 9 12 7 23 10 10 19 4 | 14 30 18 18 30 17 31 16 19 19 17
6 | 6 12 9 12 13 4 12 9 6 22 3 | 13 22 21 22 26 17 25 16 16 29 17
7 | 10 20 9 11 19 4 22 11 7 15 4 | 15 28 16 17 27 17 25 20 18 20 15
8 | 7 14 7 7 15 4 10 13 6 29 4 | 14 21 18 12 18 15 20 18 12 32 14
9 | 12 16 7 10 16 6 15 20 9 41 5 | 59 58 55 55 56 57 61 50 52 51 53
10 | 9 17 7 9 10 6 10 10 10 26 4 | 10 18 19 16 22 15 18 13 15 28 14
11 | 7 16 5 13 12 5 15 10 8 17 3 | 28 34 34 32 39 31 30 34 31 30 30
12E | 5 26 14 6 17 6 24 22 8 21 5 | 24 32 28 26 37 26 34 25 25 27 24
13E | 7 19 8 9 14 6 23 10 9 14 4 | 13 22 12 13 23 14 23 14 9 12 9
14E | 7 19 10 9 15 6 21 14 8 15 4 | 19 28 23 21 27 21 30 21 24 26 21
X15E | 5 --- --- --- --- 160 --- --- --- --- 0 | 31 --- --- --- --- 457 --- --- --- --- 32
16E | 8 28 10 14 23 5 25 18 9 20 5 | 17 33 20 26 32 21 34 19 25 16 20
17 | 8 21 7 11 14 4 21 10 6 13 4 | 11 27 17 15 31 16 25 15 12 12 13
18 | 7 23 7 10 13 4 30 10 6 13 4 | 12 30 15 12 23 15 35 12 13 16 13
19 | 6 21 7 9 17 4 23 12 8 13 4 | 15 26 16 19 23 16 26 17 21 15 15
20 | 8 21 9 11 12 5 24 10 9 18 4 | 13 26 12 20 19 12 25 14 14 14 11
21 | 7 14 7 9 8 5 22 8 7 29 4 | 22 19 19 22 21 21 17 26 20 32 19
22 | 6 19 6 8 14 4 26 9 7 17 4 | 11 30 17 15 28 14 32 12 13 13 14
23E | 6 19 7 9 16 4 24 10 8 14 4 | 18 28 20 21 25 19 30 18 22 17 18
24 | 6 8 8 5 10 4 11 10 6 16 3 | 21 21 27 25 25 22 22 24 24 21 22
X25 | 25 23 9 10 14 8 --- 20 10 --- 7 | 41 56 51 53 52 50 --- 51 48 --- 47
26E | 19 17 11 15 20 6 20 27 21 19 6 | 17 27 24 25 40 23 30 34 29 20 22
27 | 9 13 9 10 13 5 15 10 7 18 3 | 11 18 15 16 20 15 17 18 15 19 12
28E | 7 22 8 10 21 6 18 9 9 14 4 | 12 27 15 13 34 16 24 14 15 14 13
29 | 11 26 8 8 13 7 26 10 8 21 4 | 13 27 16 16 21 18 28 19 16 24 13
30 | 11 23 4 10 18 5 17 12 9 18 4 | 12 30 16 18 27 17 26 18 15 21 14
31 | 11 19 9 9 20 6 23 14 12 20 5 | 17 26 21 20 34 18 28 18 16 16 16
32 | 6 16 9 7 12 4 15 8 9 14 3 | 10 17 14 16 18 12 20 14 15 12 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 11 15 5 20 13 9 20 |T 18 27 21 22 28 36 27 21 20 21 20
WRMS | 8 19 8 10 15 5 19 11 7 19 |NE 17 26 21 21 26 19 26 20 19 22 18
MEDI | 7 19 8 9 14 5 21 10 8 18 |MD 15 27 19 20 27 18 26 18 18 20 17
Table 3.1618.2 GPS week: 1618 Day: 2 MJD: 55572.000
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 | 4 --- --- --- --- 67 --- --- --- --- 0 | 63 --- --- --- --- 50 --- --- --- --- 63
2 | 9 14 10 34 12 5 16 10 6 30 6 | 27 28 31 50 31 29 28 27 30 27 29
3 | 7 15 6 7 13 8 16 8 12 8 3 | 25 33 29 26 35 25 35 29 34 30 29
4 | 7 13 5 11 14 5 11 12 7 21 3 | 24 29 30 30 33 26 25 26 31 22 26
5 | 7 25 11 7 16 5 25 15 8 20 4 | 19 39 22 18 33 21 35 19 24 23 21
X6 | 14 66 --- 13 16 17 --- 10 23 --- 10 | 24 55 --- 24 32 27 --- 20 34 --- 20
7 | 10 21 6 8 18 4 22 11 5 15 4 | 17 29 18 19 27 16 27 21 21 20 18
8 | 5 12 8 5 14 3 13 14 8 29 4 | 16 21 18 19 20 15 22 19 20 34 17
9 | 9 14 6 8 12 4 12 13 10 13 3 | 31 31 29 27 25 25 27 25 32 30 28
10 | 6 12 8 3 11 5 11 14 5 28 3 | 17 20 21 18 24 19 21 20 18 29 18
11 | 6 16 5 7 13 6 16 9 10 17 3 | 34 35 36 37 46 31 35 39 34 35 34
12 | 5 25 9 7 19 5 19 14 11 17 4 | 23 32 25 21 27 23 28 20 28 26 23
13E | 6 22 9 7 15 5 24 9 5 16 4 | 19 31 22 25 27 22 29 20 20 22 20
14E | 7 16 7 8 17 6 18 10 11 11 3 | 16 23 19 17 27 15 23 16 22 21 17
X15E | 4 --- --- --- --- 32 --- --- --- --- 0 | 23 --- --- --- --- 24 --- --- --- --- 23
16E | 4 28 10 14 21 4 23 12 12 16 5 | 26 34 29 27 36 25 28 27 24 22 24
17 | 7 19 12 10 18 6 19 11 8 14 4 | 17 28 22 24 32 16 25 16 24 16 17
18 | 6 24 6 10 14 6 24 7 7 14 4 | 19 35 19 20 24 18 32 18 21 22 19
19 | 6 26 13 8 15 4 24 12 16 13 5 | 20 32 22 22 27 17 26 19 24 19 18
20 | 8 19 8 10 14 6 21 9 9 19 4 | 19 28 16 21 21 16 27 17 22 20 17
21 | 7 19 7 11 9 4 17 10 9 28 4 | 28 34 32 34 34 28 23 36 29 40 30
22 | 6 21 7 8 14 5 22 8 7 12 3 | 19 33 22 20 30 17 31 18 24 21 20
23E | 5 18 8 9 18 6 23 8 8 13 4 | 21 28 21 21 26 19 25 19 24 22 20
24 | 7 9 6 9 12 4 11 10 11 16 3 | 24 22 28 29 29 21 24 27 24 25 24
X25 | 12 25 9 8 19 8 --- 18 11 --- 5 | 28 37 28 25 33 24 --- 22 25 --- 24
26E | 19 37 12 10 24 3 18 29 20 18 7 | 17 37 23 22 38 21 31 34 29 16 21
27 | 7 13 6 9 12 3 13 8 6 15 3 | 16 22 18 22 21 17 21 18 17 22 16
28E | 11 16 9 9 18 3 15 12 7 19 4 | 16 26 21 25 28 16 21 19 23 22 17
29 | 10 26 14 8 17 6 26 12 14 18 5 | 20 31 27 20 22 18 29 22 27 28 20
30 | 11 21 7 8 17 5 16 12 8 16 4 | 17 29 21 20 29 18 26 19 22 23 18
31 | 7 21 7 8 21 5 23 13 11 17 4 | 19 30 21 21 35 17 28 21 25 19 20
32 | 5 18 7 6 13 4 16 7 9 13 3 | 15 20 17 14 20 14 21 14 17 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 9 11 16 5 19 12 10 18 |T 22 30 23 23 29 21 26 22 24 24 22
WRMS | 8 19 9 13 15 5 17 10 6 19 |NE 21 30 23 24 28 20 27 22 25 24 21
MEDI | 7 19 8 8 15 5 18 11 9 16 |MD 19 30 22 22 28 19 27 20 24 22 20
Table 3.1618.3 GPS week: 1618 Day: 3 MJD: 55573.000
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 | 16 --- --- 20 --- 138 --- --- --- --- 18 | 41 --- --- 27 --- 188 --- --- --- --- 41
2 | 7 14 7 11 12 6 15 10 7 29 4 | 26 33 32 35 38 28 27 32 31 28 29
3 | 9 14 8 10 14 6 15 28 9 25 5 | 49 58 54 61 57 53 57 61 51 55 53
4 | 9 14 10 26 16 6 13 14 11 19 5 | 25 32 28 38 39 28 29 34 30 27 26
5 | 5 22 8 6 14 7 24 16 8 21 4 | 16 31 19 18 31 17 32 20 25 22 19
X6 | 12 15 10 26 --- 7 --- 14 8 --- 7 | 20 30 27 34 --- 21 --- 21 22 --- 21
7 | 11 22 9 9 18 5 23 16 8 17 4 | 20 31 23 23 27 22 28 26 21 26 20
8 | 5 14 10 4 18 5 14 12 11 30 4 | 15 23 19 19 21 17 23 20 20 33 18
9 | 7 13 5 6 10 5 11 11 8 18 3 | 30 34 32 30 37 34 38 31 37 29 31
10 | 5 14 6 5 10 6 11 12 10 27 3 | 19 26 21 21 29 21 25 23 23 30 21
11 | 7 15 6 8 14 6 16 10 9 18 3 | 36 40 36 42 51 38 39 45 41 38 39
12 | 6 24 11 8 18 4 21 14 8 18 4 | 18 32 21 24 29 20 32 24 25 21 20
13E | 5 17 7 7 21 5 23 11 9 12 4 | 18 27 22 22 29 19 30 22 20 19 18
14E | 5 16 9 7 14 4 14 8 9 11 3 | 32 38 34 29 35 29 35 33 35 34 32
X15E | 6 22 7 8 13 5 26 17 14 --- 5 | 12 21 18 13 21 19 24 14 21 --- 12
16 | 5 28 10 11 20 6 21 14 9 21 5 | 17 28 17 20 24 17 25 19 19 21 16
17 | 7 21 9 8 18 4 18 11 7 16 4 | 16 31 25 21 36 20 31 19 19 19 19
18 | 7 26 9 7 15 3 24 9 9 18 4 | 22 36 22 18 27 22 34 22 30 22 22
19 | 8 29 8 8 16 6 21 11 10 13 4 | 20 36 26 25 28 21 32 21 23 21 21
20 | 8 18 8 11 14 5 23 11 10 22 4 | 18 29 20 23 22 18 33 20 21 23 18
21 | 6 17 10 10 9 5 17 9 13 31 4 | 29 30 36 31 32 28 26 36 30 39 30
22 | 5 22 7 5 16 4 18 9 7 12 3 | 20 34 23 16 31 20 33 21 23 20 20
23E | 6 18 11 9 19 4 22 10 11 11 4 | 16 25 20 22 25 17 25 18 20 17 17
24 | 5 9 5 7 13 6 10 10 9 18 3 | 27 29 29 30 38 29 31 31 32 25 29
X25 | 9 27 10 10 16 3 --- 17 10 --- 5 | 33 44 33 37 37 33 --- 35 37 --- 33
26E | 19 22 9 11 24 8 18 24 20 20 6 | 18 30 26 27 40 22 32 36 35 20 24
X27 | 8 12 7 7 9 5 --- 9 11 --- 3 | 20 24 20 20 23 17 --- 20 24 --- 19
28E | 9 20 8 9 24 6 16 10 7 19 4 | 18 27 21 23 35 21 25 20 19 17 19
29 | 12 23 10 7 22 6 25 15 10 20 5 | 20 31 22 24 34 23 28 24 25 29 21
30 | 10 22 8 9 14 4 19 12 10 20 4 | 17 35 20 20 24 21 30 23 20 27 20
31 | 7 19 7 8 17 4 18 14 10 14 4 | 23 31 24 23 34 21 28 24 24 22 23
32 | 8 19 7 5 17 4 16 11 8 15 3 | 16 22 19 17 21 16 23 15 18 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 8 9 17 5 19 13 10 20 |T 22 31 25 26 31 28 30 26 26 26 23
WRMS | 8 20 8 10 15 5 17 12 8 21 |NE 22 32 26 26 32 24 31 26 26 27 24
MEDI | 7 19 8 8 16 5 18 11 9 18 |MD 20 31 23 23 31 21 30 23 24 23 21
Table 3.1618.4 GPS week: 1618 Day: 4 MJD: 55574.000
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 | 14 --- --- 18 --- 257 --- --- --- --- 16 | 29 --- --- 29 --- 112 --- --- --- --- 23
2 | 7 12 11 11 13 4 13 9 13 29 4 | 24 30 34 30 34 28 28 29 30 25 26
3 | 9 19 10 12 54 7 14 11 12 13 6 | 22 27 22 17 64 23 31 21 28 24 21
4 | 7 10 6 6 16 5 9 12 11 17 3 | 22 27 28 29 34 24 28 29 25 26 24
5 | 8 23 11 8 13 6 21 17 12 17 4 | 14 29 20 17 31 16 31 20 17 18 15
6 | 6 19 10 10 13 6 13 11 11 18 4 | 17 30 21 17 30 20 29 20 19 27 19
7 | 13 21 12 10 19 5 21 16 9 16 5 | 17 26 21 23 32 17 25 20 21 18 16
8 | 8 15 10 8 18 5 9 15 10 30 4 | 15 19 14 20 19 16 20 14 16 29 14
9 | 7 13 7 10 12 3 10 11 14 15 3 | 14 16 15 18 22 12 19 14 16 12 11
10 | 6 13 6 5 13 5 9 13 9 24 3 | 14 21 20 17 24 18 23 16 15 27 16
11 | 8 16 8 10 14 6 16 14 12 18 4 | 28 33 34 35 40 28 29 35 32 29 29
12 | 6 24 12 12 17 4 19 15 10 16 4 | 15 29 18 23 28 17 25 16 20 23 16
13E | 7 19 11 8 27 4 24 14 11 12 5 | 19 29 23 24 28 20 28 19 21 20 18
14E | 6 17 8 9 19 5 19 12 10 12 4 | 24 27 24 21 28 21 29 18 23 23 22
X15E | 7 18 8 12 16 6 23 13 9 --- 4 | 17 18 16 15 19 23 21 11 16 --- 16
16 | 6 23 6 10 15 4 25 14 9 19 4 | 18 28 17 20 20 20 26 20 21 23 17
17 | 9 18 9 8 21 4 19 11 10 13 4 | 13 27 16 20 33 15 27 12 16 14 13
18 | 6 24 8 10 13 3 24 9 9 17 4 | 16 31 16 18 24 16 31 12 19 19 15
19 | 8 26 9 11 20 8 23 14 13 14 5 | 18 31 16 19 27 16 28 16 18 15 15
20 | 9 18 8 12 15 5 23 17 13 21 5 | 18 28 16 24 23 18 30 19 23 24 17
21 | 8 18 41 12 15 8 20 12 17 29 7 | 26 30 47 32 37 27 23 32 30 37 28
22 | 6 21 8 9 13 6 23 9 11 12 4 | 17 31 20 16 30 18 31 13 20 17 16
23E | 6 21 11 9 17 4 22 17 15 11 4 | 19 27 22 23 28 19 23 17 25 21 18
24 | 8 10 6 11 8 6 10 12 9 22 3 | 21 23 21 33 27 21 21 27 23 28 22
X25 | 18 25 12 12 12 6 --- 18 13 --- 6 | 28 41 29 33 38 30 --- 30 36 --- 27
26E | 15 26 13 12 28 6 17 29 25 18 7 | 15 32 22 26 45 24 29 37 33 19 21
27 | 8 11 8 11 11 5 11 9 12 19 3 | 15 20 14 19 17 15 19 15 22 24 15
28E | 8 19 8 11 19 5 16 13 10 19 4 | 14 26 15 22 24 16 23 17 17 16 16
29 | 9 24 11 9 15 7 23 13 10 19 5 | 14 26 16 18 23 14 26 16 17 23 12
30 | 10 22 8 9 13 4 16 13 10 18 4 | 12 32 15 13 21 17 28 17 18 22 14
31 | 7 18 10 6 16 5 21 14 8 14 4 | 20 27 21 15 31 20 27 19 20 17 17
32 | 8 19 7 9 15 4 13 15 13 12 4 | 10 20 12 13 17 15 17 14 20 17 10
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 12 10 19 5 18 14 12 18 |T 18 27 20 21 28 22 25 19 21 21 18
WRMS | 8 19 10 9 15 5 17 13 11 18 |NE 17 26 20 21 29 18 25 19 21 22 17
MEDI | 8 19 9 10 15 5 19 13 11 17 |MD 17 27 20 20 28 18 27 18 20 23 16
Table 3.1618.5 GPS week: 1618 Day: 5 MJD: 55575.000
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 | 4 --- --- --- --- 393 --- --- --- --- 0 | 30 --- --- --- --- 189 --- --- --- --- 31
2 | 8 11 8 20 13 7 12 10 8 30 4 | 23 30 30 37 32 26 29 28 24 24 25
3 | 9 15 13 13 10 5 12 14 8 12 4 | 24 32 30 32 26 26 32 26 23 29 25
4 | 7 9 6 13 14 5 7 11 8 18 3 | 21 28 26 25 32 22 26 27 23 22 23
5 | 7 23 12 10 14 5 21 17 11 17 5 | 15 32 22 18 32 15 31 20 17 19 17
6 | 8 14 10 13 11 4 13 16 8 18 4 | 16 26 24 26 29 17 29 18 16 28 20
7 | 10 23 10 13 21 4 23 18 7 15 5 | 15 27 18 23 28 17 25 25 16 18 15
8 | 7 14 6 9 16 4 10 12 8 28 4 | 12 17 11 16 20 12 18 14 9 29 11
9 | 8 11 10 8 10 4 10 13 13 17 4 | 22 26 26 24 27 24 26 21 31 24 24
10 | 7 14 8 10 13 4 8 15 7 23 4 | 12 19 17 17 22 14 17 17 14 27 14
11 | 7 16 8 9 16 6 16 14 10 20 4 | 26 32 26 30 37 24 30 32 29 26 26
12 | 6 24 10 11 23 6 20 15 12 15 5 | 15 25 14 16 24 13 22 13 15 18 12
13E | 7 19 8 11 18 3 21 14 8 13 4 | 15 26 16 22 29 17 25 18 15 17 15
14E | 7 19 12 7 15 6 15 8 11 11 4 | 35 38 39 36 39 33 37 32 36 32 34
X15E | 8 17 9 11 19 5 25 13 14 --- 5 | 17 20 17 13 16 16 21 12 18 --- 14
16 | 7 24 11 13 18 4 26 14 8 17 5 | 17 28 19 21 19 15 26 20 17 21 17
17 | 8 19 10 12 19 3 18 11 7 13 4 | 11 23 15 17 30 11 24 11 11 14 11
18 | 8 24 11 11 13 5 24 10 10 20 4 | 17 33 24 21 21 18 30 13 18 20 17
19 | 8 22 13 12 16 5 21 13 8 13 4 | 19 28 21 24 32 18 27 22 21 19 19
20 | 8 20 13 14 13 5 23 16 8 23 5 | 13 25 13 21 21 10 25 15 11 19 10
21 | 6 12 8 11 10 5 13 8 10 36 4 | 23 22 26 30 26 22 22 30 21 39 24
22 | 8 21 13 11 12 5 20 10 10 18 4 | 14 29 23 18 27 15 28 11 14 18 15
23E | 6 17 9 11 18 5 24 15 8 16 4 | 16 23 20 18 30 18 23 19 17 23 15
24 | 9 12 7 8 14 5 9 10 8 24 3 | 31 30 28 29 37 27 29 32 28 34 29
X25 | 12 22 9 13 19 7 --- 16 11 --- 5 | 26 33 26 28 34 26 --- 27 30 --- 26
26E | 15 24 14 12 21 5 15 30 20 20 6 | 18 35 23 24 41 20 30 39 31 18 22
X27 | 11 13 10 8 10 5 --- 11 15 19 4 | 14 21 18 19 21 13 --- 13 17 20 14
28E | 9 19 9 14 22 3 16 13 7 19 4 | 12 21 14 18 29 12 17 13 13 15 11
29 | 10 25 9 11 16 4 21 12 7 18 4 | 17 29 17 17 22 16 25 18 18 24 15
30 | 9 26 7 14 13 5 15 14 8 22 4 | 11 35 18 15 18 13 28 18 13 24 14
31 | 9 17 9 8 18 5 19 13 9 15 4 | 22 28 20 17 35 18 26 18 21 14 18
32 | 9 15 10 9 15 4 15 16 9 14 4 | 11 15 15 13 20 10 17 15 16 15 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 10 12 16 5 17 14 9 19 |T 18 26 21 22 27 23 25 20 19 22 18
WRMS | 8 19 9 11 15 5 16 12 8 18 |NE 17 26 21 22 27 17 25 20 18 23 18
MEDI | 8 19 10 11 15 5 16 13 8 18 |MD 17 28 20 21 28 17 26 18 17 21 17
Table 3.1618.6 GPS week: 1618 Day: 6 MJD: 55576.000
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 | 52 --- --- 41 --- 48 --- 48 21 --- 24 | 23 --- --- 39 --- 144 --- 3 5 --- 37
2 | 6 11 7 15 13 5 17 13 8 32 4 | 30 32 38 39 40 34 29 40 34 34 33
3 | 8 19 6 9 16 5 14 11 9 13 3 | 21 31 23 27 28 22 29 22 25 27 24
4 | 8 10 5 11 11 4 7 14 8 19 3 | 29 35 34 34 43 32 33 38 35 32 32
5 | 4 18 8 9 17 7 20 16 8 18 4 | 20 33 25 23 34 22 35 20 20 25 23
6 | 9 15 8 10 13 4 14 32 8 28 5 | 25 31 28 29 39 24 36 35 24 33 26
7 | 11 23 7 8 24 5 20 17 9 16 5 | 16 31 24 26 32 20 28 29 22 21 20
8 | 7 12 5 7 17 5 10 12 8 29 3 | 18 22 17 20 23 17 23 18 18 31 18
9 | 8 15 7 8 10 5 11 15 8 17 3 | 22 23 23 20 25 19 24 19 24 22 21
10 | 6 13 7 9 11 4 11 15 8 25 3 | 19 20 24 22 28 19 25 25 19 32 20
11 | 6 15 6 10 15 6 19 14 6 21 4 | 37 43 43 42 52 39 41 46 41 38 41
12 | 5 27 9 10 19 5 20 13 8 16 4 | 14 31 14 20 28 15 26 17 15 21 15
13E | 7 21 8 9 21 5 23 19 6 9 4 | 18 30 19 23 27 20 28 26 20 20 18
14E | 6 18 12 9 15 3 18 12 10 17 4 | 28 33 26 25 32 25 32 30 29 39 27
X15E | 9 22 7 10 22 5 26 13 11 --- 5 | 21 21 17 18 17 28 24 14 17 --- 22
16 | 6 26 8 11 19 3 26 15 8 19 4 | 15 27 19 21 29 16 27 18 18 25 16
17 | 8 16 6 7 20 4 19 13 8 13 4 | 15 26 18 18 32 16 28 17 18 20 17
18 | 6 25 9 12 12 3 26 8 10 22 4 | 20 34 19 21 26 19 36 18 21 24 19
19 | 9 25 9 9 19 5 25 16 6 14 4 | 22 33 21 21 30 19 29 19 22 19 19
20 | 6 17 9 11 10 6 29 19 9 21 4 | 21 30 21 25 24 20 37 20 25 27 21
21 | 5 17 8 9 9 4 19 15 11 40 4 | 34 34 36 37 37 33 29 43 35 48 35
22 | 8 20 7 8 13 3 24 10 8 24 4 | 18 31 21 18 30 17 33 17 20 25 18
23E | 6 19 7 11 18 6 24 12 5 12 4 | 24 27 26 28 31 22 26 24 21 25 24
24 | 6 9 4 7 13 6 14 11 8 27 3 | 30 33 34 31 39 30 37 34 33 25 32
X25 | 17 25 9 11 18 7 --- 15 7 --- 5 | 42 46 34 37 38 38 --- 37 40 --- 37
26E | 14 21 9 8 28 4 17 31 19 25 6 | 20 34 25 28 44 24 33 35 34 29 25
27 | 10 12 9 9 12 5 9 11 9 19 3 | 18 22 22 24 25 17 22 18 19 17 19
28E | 7 23 6 11 22 3 15 11 7 19 4 | 16 26 16 20 26 16 21 17 16 20 16
29 | 9 27 9 11 15 4 24 12 11 19 4 | 20 35 24 27 25 21 32 24 20 30 21
30 | 9 25 8 11 17 4 15 14 10 24 4 | 16 36 19 19 25 17 31 20 19 29 19
31 | 10 18 8 10 18 3 21 13 9 14 4 | 21 28 25 21 34 20 27 24 22 21 21
32 | 7 20 7 7 14 5 17 18 8 14 4 | 17 23 22 17 23 16 24 17 20 20 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 10 17 5 19 16 9 21 |T 22 30 24 25 31 26 29 24 23 26 23
WRMS | 8 19 8 10 17 5 18 13 8 18 |NE 22 30 25 25 31 22 30 25 24 27 23
MEDI | 7 19 8 9 16 5 19 14 8 19 |MD 20 31 23 23 30 20 29 20 21 25 21
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 4.1618 GPS week: 1618 MJD: 55570.0-55576.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 |U 7 8 18 |U 18 18 54 |U 15 14 21 |
emr | emr 2942 |U 12 10 26 | 18 19 59 | 28 14 27 |
esa | esa 2934 | 7 9 21 |U 18 18 59 | 15 13 22 |
gfz | gfz 2972 |U 9 9 21 |U 17 19 50 |U 13 13 21 |
grg | grg 2931 | 9 11 28 |U 17 19 51 | 20 13 36 |
igr | igr 2950 | 8 9 21 | 18 18 55 | 13 13 21 |
igs | igs 2921 | 7 9 20 | 18 18 51 | 24 13 33 |
jpl | jpl 2790 | 16 14 32 |U 18 19 60 |U 27 14 25 |
mit | mit 2962 |U 13 9 20 |U 18 20 51 |U 37 25 44 |
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 5.1618.0 GPS week: 1618 Day: 0 MJD: 55570.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 7 10 17 | 38 22 89 | 5 7 15 |
emr | emr 2972 | 10 8 25 | 39 24 94 | 8 6 15 |
esa | esa 2976 | 7 12 23 | 35 25 90 | 5 5 18 |
gfz | gfz 2972 | 7 9 19 | 36 25 87 | 5 6 16 |
grg | grg 2976 | 12 23 42 | 36 26 93 | 8 10 19 |
igr | igr 2972 | 7 12 20 | 37 25 92 | 4 4 16 |
igs | igs 2967 | 8 11 21 | 36 26 91 | 5 5 14 |
jpl | jpl 2876 | 35 29 33 | 38 30 95 | 8 9 16 |
mit | mit 2976 | 13 10 22 | 37 27 87 | 8 9 17 |
Table 5.1618.1 GPS week: 1618 Day: 1 MJD: 55571.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 6 8 19 | 24 25 59 | 14 16 22 |
emr | emr 2876 | 12 11 33 | 29 29 78 | 10 8 20 |
esa | esa 2880 | 8 9 25 | 27 27 76 | 6 6 14 |
gfz | gfz 2876 | 9 10 27 | 25 27 49 | 6 7 17 |
grg | grg 2880 | 12 16 36 | 24 28 46 | 23 18 34 |
igr | igr 2939 | 8 8 23 | 25 25 66 | 6 4 14 |
igs | igs 2880 | 8 8 23 | 25 27 48 | 6 7 14 |
jpl | jpl 2778 | 15 14 29 | 26 24 68 | 9 9 21 |
mit | mit 2880 | 16 8 28 | 26 26 64 | 23 22 38 |
Table 5.1618.2 GPS week: 1618 Day: 2 MJD: 55572.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3010 | 7 6 13 | 23 26 68 | 5 5 13 |
emr | emr 2860 | 23 10 24 | 18 29 57 | 9 8 13 |
esa | esa 2784 | 8 8 17 | 23 28 93 | 22 7 24 |
gfz | gfz 2851 | 12 10 19 | 19 26 55 | 7 8 12 |
grg | grg 2856 | 7 9 22 | 20 27 64 | 9 9 16 |
igr | igr 2854 | 8 7 16 | 22 29 60 | 6 6 14 |
igs | igs 2848 | 7 8 15 | 23 28 61 | 6 6 13 |
jpl | jpl 2673 | 14 7 22 | 21 33 97 | 13 7 19 |
mit | mit 2880 | 15 8 16 | 20 29 66 | 1 33 76 |
Table 5.1618.3 GPS week: 1618 Day: 3 MJD: 55573.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 9 8 21 | 11 10 48 | 22 36 36 |
emr | emr 2971 | 11 12 22 | 11 9 55 | 108 38 69 |
esa | esa 2976 | 7 9 15 | 12 9 45 | 23 37 34 |
gfz | gfz 3033 | 8 8 17 | 13 9 45 | 23 37 33 |
grg | grg 2880 | 7 8 18 | 8 9 41 | 48 20 116 |
igr | igr 2975 | 8 9 15 | 11 9 46 | 22 37 33 |
igs | igs 2880 | 7 9 18 | 11 7 46 | 94 38 126 |
jpl | jpl 2683 | 10 10 26 | 12 9 48 | 105 30 51 |
mit | mit 2976 | 14 12 22 | 14 21 36 | 159 66 97 |
Table 5.1618.4 GPS week: 1618 Day: 4 MJD: 55574.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 7 8 16 | 11 14 44 | 46 26 34 |
emr | emr 2972 | 10 12 28 | 12 15 49 | 41 24 35 |
esa | esa 2976 | 8 9 19 | 11 14 41 | 38 23 37 |
gfz | gfz 3059 | 8 10 21 | 10 15 47 | 40 24 29 |
grg | grg 2976 | 10 8 20 | 11 15 46 | 41 23 36 |
igr | igr 2974 | 8 10 18 | 11 14 46 | 33 23 42 |
igs | igs 2959 | 8 8 17 | 10 14 42 | 42 25 35 |
jpl | jpl 2870 | 15 14 39 | 12 15 44 | 37 25 34 |
mit | mit 2976 | 14 9 19 | 10 13 38 | 49 30 36 |
Table 5.1618.5 GPS week: 1618 Day: 5 MJD: 55575.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 9 7 23 | 9 11 38 | 8 8 15 |
emr | emr 2971 | 11 11 26 | 12 12 42 | 10 10 16 |
esa | esa 2976 | 8 7 27 | 8 10 37 | 7 5 14 |
gfz | gfz 2967 | 9 7 26 | 9 11 35 | 7 7 19 |
grg | grg 2976 | 9 7 32 | 9 10 36 | 7 8 15 |
igr | igr 2970 | 10 8 19 | 9 10 36 | 8 10 15 |
igs | igs 2900 | 8 8 27 | 9 11 36 | 9 7 13 |
jpl | jpl 2780 | 13 12 27 | 10 10 42 | 10 10 17 |
mit | mit 2976 | 10 8 17 | 8 11 34 | 15 12 30 |
Table 5.1618.6 GPS week: 1618 Day: 6 MJD: 55576.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 6 8 18 | 10 18 29 | 5 4 13 |
emr | emr 2972 | 10 8 27 | 9 17 37 | 9 5 19 |
esa | esa 2976 | 6 8 21 | 10 16 28 | 6 5 16 |
gfz | gfz 3049 | 8 9 19 | 10 16 30 | 6 4 17 |
grg | grg 2976 | 7 9 27 | 12 16 33 | 6 3 16 |
igr | igr 2967 | 9 13 33 | 9 15 38 | 9 6 16 |
igs | igs 3013 | 6 8 19 | 10 16 29 | 6 4 14 |
jpl | jpl 2874 | 13 11 45 | 10 15 28 | 9 5 20 |
mit | mit 3072 | 6 11 20 | 10 15 30 | 6 4 14 |
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 6.1618 GPS week: 1618 MJD: 55570.500-55576.500
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 -25 -2 144 -1 | 0 11
| 23 16 78 86 2 | 2
emr uuuuu | 17 -19 -46 243 -11 | 23 26
| 29 26 94 113 6 | 2
esa uuuuu | -10 -17 172 19 -3 | -11 17
| 18 12 78 64 3 | 2
gfz uuuuu | 13 17 12 56 2 | -2 13
| 22 17 68 40 4 | 4
grg uuuux | 27 -52 8 74 7 | -11 25
| 23 31 113 68 23 | 5
igr xxxxx | 4 0 -1 68 4 | -4 12
| 33 33 112 51 4 | 3
irf xxxxx | -12 7 -89 -9 6 | -2 15
| 20 10 34 30 6 | 6
jpl uuuuu | 47 -12 53 220 -8 | -19 23
| 67 60 64 76 10 | 3
mit uuuuu | -22 20 -270 -119 10 | 2 16
| 32 17 59 43 8 | 7
ngs uuuuu | 5 28 -73 -163 -3 | -7 11
| 65 30 74 124 10 | 0
sio uuuuu | -71 -9 109 -159 4 | 6 14
| 33 12 61 84 6 | 5
Table 7.1618.0 GPS week: 1618 Day: 0 MJD: 55570.500
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 -49 45 259 2 | -5 9
emr uuuuu | 25 -50 41 54 -3 | 19 22
esa uuuuu | -11 -1 151 -52 -1 | -15 18
gfz uuuuu | 58 5 -24 110 9 | -9 13
grg uuuux | 8 -28 -194 -5 -20 | -14 25
igr xxxxx | 30 -51 158 -16 -4 | -9 12
irf xxxxx | 11 -8 -61 10 12 | -12 16
jpl uuuuu | 76 -23 6 194 -14 | -19 24
mit uuuuu | 10 -8 -201 -70 14 | -8 13
ngs uuuuu | -67 47 -49 -32 -14 | -8 10
sio uuuuu | -30 -25 162 -117 4 | -2 9
Table 7.1618.1 GPS week: 1618 Day: 1 MJD: 55571.500
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 -33 -121 229 -1 | -2 12
emr uuuuu | 41 -49 29 221 -10 | 23 26
esa uuuuu | 0 -10 136 -21 -3 | -12 18
gfz uuuuu | 5 46 -36 17 7 | -6 16
grg uuuux | 2 -77 65 -5 -17 | -15 25
igr xxxxx | 40 21 74 58 3 | -7 13
irf xxxxx | 13 9 -52 -10 14 | -7 18
jpl uuuuu | 49 -1 121 108 -12 | -17 22
mit uuuuu | 25 20 -244 -124 20 | -5 17
ngs uuuuu | -47 29 -96 17 -11 | -7 10
sio uuuuu | -25 -15 160 -156 10 | 1 14
Table 7.1618.2 GPS week: 1618 Day: 2 MJD: 55572.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -25 -19 -89 137 -1 | 0 12
emr uuuuu | 51 -13 -61 289 -4 | 24 27
esa uuuuu | 12 -4 127 -52 -3 | -11 17
gfz uuuuu | 18 12 43 46 1 | -3 15
grg uuuux | 23 -72 33 92 4 | -15 25
igr xxxxx | 46 36 70 131 4 | -5 12
irf xxxxx | -14 15 -67 9 10 | -4 16
jpl uuuuu | 79 38 156 315 -9 | -17 22
mit uuuuu | -16 36 -265 -111 15 | -1 18
ngs uuuuu | -57 -10 -112 -128 -9 | -7 11
sio uuuuu | -71 -4 178 -150 11 | 4 14
Table 7.1618.3 GPS week: 1618 Day: 3 MJD: 55573.500
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 -14 29 46 -2 | 2 11
emr uuuuu | 32 17 -123 319 -15 | 26 28
esa uuuuu | 0 -22 264 111 -2 | -10 16
gfz uuuuu | -10 -3 -12 110 3 | 0 12
grg uuuux | 28 -39 61 182 25 | -13 24
igr xxxxx | -19 33 -143 37 4 | -4 11
irf xxxxx | -44 21 -74 -72 5 | 0 14
jpl uuuuu | 161 -135 -5 288 -17 | -16 21
mit uuuuu | -70 37 -197 -199 8 | 4 16
ngs uuuuu | 8 69 -163 -318 -1 | -8 11
sio uuuuu | -117 7 85 -342 5 | 8 14
Table 7.1618.4 GPS week: 1618 Day: 4 MJD: 55574.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -20 -40 62 163 -5 | 1 10
emr uuuuu | 12 1 -214 398 -19 | 24 26
esa uuuuu | -28 -29 232 14 1 | -11 16
gfz uuuuu | -4 9 147 32 -1 | 1 13
grg uuuux | 62 -32 -5 92 43 | -9 24
igr xxxxx | -30 -12 -116 101 4 | -3 12
irf xxxxx | -19 5 -110 7 6 | 2 14
jpl uuuuu | -37 39 32 196 -9 | -19 22
mit uuuuu | -37 31 -330 -91 12 | 6 17
ngs uuuuu | 100 -13 -120 -281 -2 | -7 11
sio uuuuu | -88 -1 98 -149 5 | 9 15
Table 7.1618.5 GPS week: 1618 Day: 5 MJD: 55575.500
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 | -57 -9 82 143 1 | 1 11
emr uuuuu | -22 -6 13 263 -12 | 23 26
esa uuuuu | -4 -21 245 75 -5 | -11 16
gfz uuuuu | 10 16 19 15 -2 | 2 11
grg uuuux | 14 -17 -69 39 17 | -4 24
igr xxxxx | -18 -32 24 113 11 | -2 11
irf xxxxx | -20 -3 -112 11 1 | 4 12
jpl uuuuu | -18 -15 -1 160 -5 | -22 25
mit uuuuu | -42 4 -326 -91 4 | 9 16
ngs uuuuu | 60 27 -31 -180 6 | -8 12
sio uuuuu | -92 -21 65 -93 1 | 10 15
Table 7.1618.6 GPS week: 1618 Day: 6 MJD: 55576.500
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 -9 -25 28 0 | 1 11
emr uuuuu | -20 -34 -5 155 -13 | 21 25
esa uuuuu | -38 -32 49 58 -8 | -10 15
gfz uuuuu | 16 34 -54 59 -2 | 2 11
grg uuuux | 54 -101 161 119 -5 | -4 24
igr xxxxx | -21 6 -74 53 6 | 0 10
irf xxxxx | -15 13 -145 -19 -4 | 5 12
jpl uuuuu | 20 17 63 277 14 | -23 26
mit uuuuu | -23 23 -325 -149 -3 | 10 16
ngs uuuuu | 40 46 62 -219 13 | -8 12
sio uuuuu | -72 -4 13 -105 -6 | 11 15
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