[IGSREPORT-18948] Wk 1598 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 9 09:18:31 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1598 (Aug 22, 2010 - Aug 28, 2010)
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:
igs1598[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1598[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1598[0-6].cls IGS GPS clock combination summary report.
igs15987.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15987.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 | COCO
0 | EMR | 3 WTZR WTZR
0 | ESA | IRKJ UNSA
0 | GFZ | 1 KERG KOUR MDVJ WILL
0 | GRG | DGAR IRKJ ONSA
0 | JPL | 32
0 | MIT | 25 3 25
1 | ALL | 1 1
1 | COD | DGAR
1 | EMR | 3 6 3 6 WTZR WTZR
1 | ESA | IRKJ NICO SUTH UNSA
1 | GFZ | 3 6 24 MDVJ
1 | GRG | DGAR IRKJ ONSA
1 | JPL | 26 32
1 | MIT | 3 6 25 3 6 25 DRAO NICO
2 | ALL | 1
2 | COD | 19 25 19 21 NICO DGAR MCM4
2 | EMR | 3 6 WTZR
2 | ESA | WTZR DAV1 IRKJ SUTH UNSA
2 | GFZ | 1 6 BRUS DRAO GRAS KERG MDVJ WILL
2 | GRG | DGAR IRKJ NRC1 SANT
2 | JPL | 3 32
2 | MIT | 6 21 28 3 6 21 28 SPT0 FLIN NICO SPT0
3 | COD | 1 1 MATE DGAR HOFN MATE
3 | EMR | WTZR WTZR
3 | ESA | SUTH
3 | GFZ | 1 3 6 HARB MATE MDVJ UNSA
3 | GRG | DGAR IRKJ ONSA
3 | JPL | 32 TIXI
3 | MIT | 3 6 19 25 3 6 25 DAV1 DAV1 HARB
4 | ALL | 1 1 3
4 | COD | DGAR YELL
4 | EMR | WTZR WTZR YELL
4 | ESA | SUTH UNSA
4 | GFZ | 6 YAKT
4 | GRG | DGAR IRKJ WTZR
4 | JPL | 24 32 ZWE2
4 | MIT | 6 24 6 24 MAW1 YAKT MAW1 TWTF YAKT
5 | ALL | 1
5 | COD | DGAR SOFI YELL
5 | EMR | WTZR WTZR
5 | ESA | SUTH UNSA
5 | GFZ | 6 BOR1 DAV1 MDVJ PRDS
5 | GRG | DGAR ONSA
5 | JPL | 32
5 | MIT | 6 25 26 6 25 26
6 | ALL | 1
6 | COD | DGAR
6 | EMR | 3 WTZR HARB WTZR YELL
6 | ESA | IRKJ SUTH
6 | GFZ | 21 FAA1 MDVJ UNSA
6 | GRG | DGAR IRKJ ONSA
6 | JPL | 32 YELL
6 | MIT | 3 6 10 28 3 6 10 21 28 DAEJ
5. 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
----+------------+----------
G03 | 2010_08_26 | 2010112
G03 | 2010_08_27 | 2010112
G14 | 2010_08_24 | 2010111
6. 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
----+--------+---------------
3 | EMR | 1
5 | GFZ | 26
7. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G06 | 2 | | | | | | 1 |
8. 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.
9. 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 1.3 1.7 -6 -7 -17 -.45
EMR | -2.3 7.8 -4.1 1 5 -13 -.07
ESA | -1.1 .5 3.1 13 40 -46 -.15
GFZ | .2 1.5 1.1 15 4 -50 -.24
GRG | .9 11.6 -4.7 -18 40 -23 -.18
JPL | -3.5 8.6 -11.9 -29 -7 23 -.21
MIT | 2.7 -2.8 10.1 15 3 -33 -.30
NGS | 2.8 6.6 9.6 116 -5 -13 -.27
SIO | -.9 .5 -9.6 3 -17 -19 -.09
10. 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.
11. 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.
12. 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 1.1598.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1598.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 2.1598.[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 3.1598.[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 5.1598.0-6).
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 1598 summary. (Aug 22, 2010 - Aug 28, 2010)
Table 1.1598.a GPS week: 1598 MJD: 55430.000-55436.000
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 44 27 -35 -.22 8 7 | -451 -139 16 68
| 0 0 0 10 13 21 .02 | 445 701
emr 93| -1 2 -5 11 22 17 .44 19 19 | -5145 -311 16 80
| 1 1 1 40 28 18 .03 | 807 955
esa 134| 0 0 1 4 -53 -21 .30 7 7 | -1690 1097 13 98
| 1 0 1 19 15 30 .03 | 810 623
gfz 197| 0 0 2 40 -47 15 -.21 10 10 | 133 -210 21 105
| 1 1 2 68 53 7 .05 | 377 574
grg 126| 2 0 0 64 -61 0 .59 18 16 | -54106 125278 57 215
| 1 1 0 37 31 26 .06 | 142864 331583
igr n/a| 0 0 1 39 27 7 -.03 5 5 | -7860 145 18 56
| 0 0 0 29 24 26 .04 | 1009 1048
jpl 125| 1 0 -9 105 35 65 .51 19 18 | -999 -418 19 107
| 1 1 1 17 10 49 .06 | 1000 1054
mit 263| 1 -1 0 10 2 20 -.28 11 9 | -88 52 22 172
| 0 0 2 20 22 17 .02 | 185 423
ngs 215| 0 0 2 -203 53 18 -.20 10 7 | 3888 -36590 2015 3458
| 0 0 1 29 44 15 .04 | 17123 174244
sio 259| -2 0 -1 18 48 -23 -.11 20 18 | --- --- --- ---
| 1 1 1 23 32 16 .03 | --- ---
Table 1.1598.b GPS week : 1598 MJD: 55430.000-55436.000
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 | 12 11 16 13 9 22 16 |
2 | 5 5 5 5 5 5 4 |
3 | 5 5 5 4 9 7 5 |
4 | 3 3 4 4 3 3 3 |
5 | 5 5 4 4 4 4 4 |
6 | 6 8 8 6 5 5 5 |
7 | 6 5 5 5 6 5 5 |
8 | 4 4 3 3 4 3 3 |
9 | 4 4 4 4 4 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 5 0 4 4 4 4 |
15 | 5 5 5 5 6 5 5 |
16 | 6 6 6 5 5 5 5 |
17 | 4 5 5 4 4 6 4 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 4 5 4 |
20 | 4 4 4 3 3 4 4 |
21 | 5 5 5 5 5 5 4 |
22 | 4 4 4 4 4 4 3 |
23 | 4 4 5 4 4 4 4 |
24 | 3 3 3 3 3 3 3 |
25 | 12 12 10 12 13 13 9 |
26 | 6 6 5 5 4 16 4 |
27 | 3 4 5 5 4 4 4 |
28 | 4 4 5 4 5 5 5 |
29 | 6 5 5 5 5 5 5 |
30 | 3 3 4 3 3 4 4 |
31 | 4 5 4 4 4 4 4 |
32 | 3 3 4 3 3 4 3 |
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 2.1598.0 GPS week: 1598 Day: 0 MJD: 55430.000
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 35 31 -29 -.22 9 9 | -568 -173 18 71
| 41 -2 |
emr 93| -1 5 -6 -23 -8 -12 .42 18 18 | -5372 -696 18 71
| 12 -5 |
esa 134| 0 0 1 -17 -53 -3 .30 7 7 | -2506 1580 12 81
| 23 7 |
gfz 197| 0 -1 0 93 54 3 -.24 9 9 | 179 -286 22 96
| -23 -3 |
grg 126| 1 0 0 40 -80 -23 .60 17 16 | -226 89 58 218
| 71 94 |
igr n/a| 0 0 1 49 -3 -5 -.03 4 4 | -9237 -475 17 46
| -22 -19 |
jpl 125| 2 -1 -10 99 28 147 .56 19 17 | -916 -866 18 108
| -6 63 |
mit 263| 0 0 1 41 24 -6 -.31 11 10 | -271 37 23 144
| 16 11 |
ngs 215| 0 0 4 -233 -14 5 -.26 10 7 | -399 -520 1812 2961
| 39 28 |
sio 259| -4 0 -2 61 23 -51 -.10 21 18 | --- --- --- ---
| -54 32 |
Table 2.1598.1 GPS week: 1598 Day: 1 MJD: 55431.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 -1 0 54 43 -54 -.20 8 7 | -703 -104 16 61
| 12 3 |
emr 93| 0 1 -5 -44 -1 33 .44 21 21 | -5248 237 20 91
| 14 4 |
esa 134| 0 1 0 0 -45 2 .32 9 8 | -1071 806 13 96
| 14 16 |
gfz 197| 0 1 2 108 -35 10 -.23 10 10 | 760 -858 23 113
| -51 -8 |
grg 126| 1 1 0 72 -46 -27 .54 17 15 | -320 -37 47 210
| -4 41 |
igr n/a| 0 -1 2 31 30 4 -.01 6 5 | -8968 597 18 59
| -15 -41 |
jpl 125| 1 0 -9 106 51 95 .60 19 18 | -1033 269 18 118
| -7 37 |
mit 263| 0 -1 2 -7 0 23 -.27 12 8 | -254 79 21 134
| 24 8 |
ngs 215| 0 0 1 -227 8 1 -.21 10 7 | -723 -17 2370 3953
| 38 38 |
sio 259| -3 0 0 23 28 -18 -.07 21 21 | --- --- --- ---
| -54 27 |
Table 2.1598.2 GPS week: 1598 Day: 2 MJD: 55432.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 -1 1 40 43 -1 -.19 9 8 | -116 -516 20 71
| 30 4 |
emr 93| -1 1 -4 -1 46 23 .50 18 18 | -4775 1139 18 82
| 10 -1 |
esa 134| -2 0 0 29 -59 -80 .34 9 9 | -3036 1269 16 94
| 22 22 |
gfz 197| 1 1 1 44 -92 19 -.25 10 10 | 208 -336 21 103
| -43 15 |
grg 126| 1 0 0 48 -41 25 .52 18 18 | -18 120 69 211
| 59 32 |
igr n/a| 0 0 1 35 35 -25 .03 6 5 | -8076 1753 22 65
| -21 9 |
jpl 125| 1 -1 -6 106 31 88 .56 19 18 | -458 1159 24 98
| 18 57 |
mit 263| 1 -1 1 18 12 3 -.27 12 9 | -193 333 25 163
| 18 9 |
ngs 215| 0 0 2 -197 52 24 -.25 10 7 | 41546 153930 1977 3824
| -38 6 |
sio 259| -1 0 0 25 50 -38 -.08 19 18 | --- --- --- ---
| -39 25 |
Table 2.1598.3 GPS week: 1598 Day: 3 MJD: 55433.000
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 33 20 -66 -.26 8 7 | -987 898 14 62
| 15 4 |
emr 93| -2 4 -3 42 23 9 .43 18 18 | -3924 -557 15 82
| -71 -20 |
esa 134| 1 0 2 29 -38 10 .27 6 6 | -1013 1819 13 98
| 28 -4 |
gfz 197| -1 0 4 -30 -91 18 -.28 11 11 | -442 879 20 100
| -45 1 |
grg 126| 0 0 1 39 -15 10 .53 16 15 | -189 400 62 231
| 44 -16 |
igr n/a| 0 0 1 30 22 10 -.05 5 5 | -6690 -34 20 51
| -33 -6 |
jpl 125| 1 0 -10 116 36 46 .48 19 19 | 321 -772 20 108
| -65 -65 |
mit 263| 1 0 -1 -7 -10 27 -.29 12 9 | -127 722 23 186
| 11 6 |
ngs 215| 0 1 0 -177 62 11 -.21 10 8 | -954 804 2239 3587
| 18 -13 |
sio 259| -1 1 -2 -3 33 -16 -.13 19 18 | --- --- --- ---
| -45 31 |
Table 2.1598.4 GPS week: 1598 Day: 4 MJD: 55434.000
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 57 24 -20 -.22 6 6 | -890 658 17 64
| 29 43 |
emr 93| -2 2 -6 56 62 3 .41 20 20 | -4900 -1057 15 68
| -66 -38 |
esa 134| 1 0 1 -6 -84 -19 .29 7 7 | -954 60 16 116
| 5 22 |
gfz 197| 0 0 4 -51 -87 14 -.18 10 10 | -68 -65 22 115
| -60 13 |
grg 126| 3 0 0 74 -100 -18 .68 16 15 | -168 36 47 219
| 4 97 |
igr n/a| 0 0 1 75 70 -8 -.07 5 4 | -7045 -618 18 62
| -33 -14 |
jpl 125| 0 -1 -10 109 41 2 .42 19 18 | -757 -1189 18 111
| -18 -128 |
mit 263| 0 -2 -1 -1 4 17 -.27 11 10 | -102 60 19 179
| 25 6 |
ngs 215| 0 0 3 -159 108 42 -.19 10 8 | -711 409 1995 3288
| -35 -58 |
sio 259| -3 2 -1 5 77 -15 -.13 19 16 | --- --- --- ---
| -31 24 |
Table 2.1598.5 GPS week: 1598 Day: 5 MJD: 55435.000
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 53 24 -43 -.24 7 7 | -33 -748 16 77
| -4 -20 |
emr 93| 0 0 -8 57 41 32 .42 19 19 | -5186 -1653 16 80
| -48 -18 |
esa 134| 0 0 3 9 -53 -35 .29 7 6 | -1822 1512 10 97
| 24 -21 |
gfz 197| -1 2 2 3 -60 28 -.16 10 9 | -52 -42 20 100
| -39 -41 |
grg 126| 3 2 0 141 -47 40 .62 21 18 | -378093 877239 60 205
| -43 22 |
igr n/a| 0 0 1 64 32 15 -.01 4 4 | -6928 -1263 15 60
| -20 -49 |
jpl 125| 0 -1 -9 129 42 60 .48 20 20 | -1189 -1895 17 115
| -41 -95 |
mit 263| 1 0 -2 -3 -38 39 -.29 11 9 | 218 -242 21 208
| 15 17 |
ngs 215| 0 -1 2 -193 101 10 -.14 9 7 | -11698 -409685 1623 3367
| 31 -8 |
sio 259| -1 1 -2 -8 16 0 -.16 19 18 | --- --- --- ---
| -33 22 |
Table 2.1598.6 GPS week: 1598 Day: 6 MJD: 55436.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 -1 0 34 6 -29 -.22 6 6 | 139 -991 15 74
| 48 69 |
emr 93| -3 1 -6 -4 -5 35 .45 19 19 | -6614 405 16 90
| -20 32 |
esa 134| 0 1 3 -12 -37 -25 .26 6 6 | -1434 633 11 108
| 18 28 |
gfz 197| -1 1 -1 115 -17 12 -.16 10 11 | 352 -764 21 108
| -58 -12 |
grg 126| 2 -1 0 32 -98 -8 .60 17 16 | 269 -900 58 212
| 69 144 |
igr n/a| 0 0 1 -14 4 59 -.06 6 5 | -8080 1056 16 53
| -7 28 |
jpl 125| 2 0 -7 72 17 17 .46 19 19 | -2967 362 19 97
| -11 -64 |
mit 263| 1 0 0 30 23 42 -.28 11 10 | 110 -625 26 192
| 5 8 |
ngs 215| 0 0 3 -233 55 32 -.17 10 9 | 157 -1057 2094 3228
| 87 68 |
sio 259| -1 1 0 22 106 -24 -.11 21 18 | --- --- --- ---
| -43 -6 |
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 3.1598.0 GPS week: 1598 Day: 0 MJD: 55430.000
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 | 19 --- --- 26 --- 34 --- 19 19 --- 12 | 24 --- --- 31 --- 35 --- 18 20 --- 19
2 | 8 20 8 7 17 8 23 14 6 26 4 | 13 27 20 17 26 17 27 16 16 26 16
3E | 13 14 9 11 20 4 19 19 12 24 5 | 100 97 95 98 99 101 101 83 90 101 103
4 | 5 14 8 8 8 4 14 7 6 15 3 | 23 26 31 29 31 26 26 24 26 29 26
5 | 10 18 10 12 13 3 20 10 10 25 4 | 26 30 32 32 38 30 32 27 32 29 29
6E | 14 19 10 13 20 4 18 20 14 24 5 | 101 105 104 100 104 101 107 100 100 101 102
7 | 17 21 10 9 28 6 22 9 11 22 5 | 20 30 27 23 39 20 28 18 24 17 21
8 | 9 13 5 5 15 4 11 7 11 18 3 | 13 23 18 14 21 15 24 13 20 15 15
9 | 11 13 5 7 14 3 11 8 8 22 3 | 19 23 19 15 21 17 25 19 18 20 16
10 | 7 15 7 8 14 4 12 5 9 22 3 | 29 30 32 33 37 30 26 32 31 29 30
11 | 8 14 8 7 18 4 17 9 5 15 3 | 22 31 27 21 41 23 30 23 25 21 23
12 | 6 22 9 11 20 4 25 9 10 20 4 | 17 31 20 18 27 18 32 20 22 21 18
13E | 6 19 6 11 16 3 19 9 7 20 4 | 20 27 27 23 34 23 33 23 24 24 23
14E | 8 17 7 9 15 4 17 10 7 13 3 | 7 16 11 7 12 9 14 9 11 10 9
15 | 8 24 6 11 19 5 21 13 11 13 4 | 15 27 19 15 25 15 28 19 22 22 17
16 | 10 25 10 12 16 4 26 10 8 34 5 | 20 32 18 14 26 18 36 20 21 27 17
17E | 7 17 5 10 15 4 21 16 7 12 4 | 17 27 21 20 30 18 28 15 19 16 18
18 | 10 19 8 11 14 5 21 9 13 31 4 | 24 34 32 29 34 30 34 29 37 24 29
19E | 9 16 10 10 27 5 23 12 10 14 4 | 37 45 44 35 43 37 47 37 38 38 39
20 | 4 15 6 10 14 3 16 8 8 24 3 | 30 31 36 35 37 29 29 31 29 23 30
21 | 11 24 8 9 16 5 25 16 12 21 5 | 25 40 29 22 42 26 40 27 30 20 27
22 | 10 16 6 9 14 5 19 11 8 19 4 | 28 34 34 34 38 32 33 35 37 26 32
23 | 8 20 4 8 16 4 19 8 9 21 4 | 15 26 19 15 28 16 28 15 17 22 16
24 | 7 10 6 7 15 4 10 10 5 13 3 | 25 25 28 30 30 27 24 29 29 22 26
X25 | 32 --- 13 17 --- 21 --- 22 27 --- 11 | 28 --- 27 20 --- 25 --- 22 30 --- 23
26E | 17 19 8 8 23 5 16 21 20 25 6 | 139 142 136 142 136 138 140 135 134 137 136
27 | 10 15 5 8 12 2 10 9 7 17 3 | 15 22 16 12 16 14 22 17 19 17 14
28 | 8 20 6 9 17 4 21 8 8 25 4 | 14 29 21 17 28 17 29 14 21 17 17
X29E | 13 22 11 10 15 7 28 19 15 --- 6 | 23 31 29 29 27 26 33 26 25 --- 24
30 | 7 15 7 6 10 3 12 10 6 14 3 | 20 28 24 20 30 21 27 24 26 23 22
31 | 6 23 7 9 19 3 19 8 10 13 4 | 16 28 22 19 29 18 26 16 20 18 18
32 | 4 10 5 7 13 3 14 9 11 18 3 | 19 20 19 23 27 18 17 22 22 17 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 7 9 17 4 19 11 10 21 |T 29 37 33 31 38 30 37 29 32 31 30
WRMS | 9 18 7 9 16 4 17 10 7 18 |NE 20 28 24 22 30 22 28 22 24 22 21
MEDI | 8 17 7 9 15 4 19 10 9 20 |MD 20 29 27 22 30 23 28 22 24 22 22
Table 3.1598.1 GPS week: 1598 Day: 1 MJD: 55431.000
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 | 12 --- --- 17 --- 34 --- 17 --- --- 10 | 14 --- --- 17 --- 41 --- 13 --- --- 14
2 | 6 26 8 10 21 9 22 10 10 24 4 | 11 28 17 15 26 16 28 14 14 27 13
3E | 8 16 11 12 18 5 17 13 11 22 4 | 85 83 77 88 77 89 84 75 75 79 89
4 | 4 19 5 8 10 5 12 5 6 17 3 | 19 25 24 19 25 21 25 20 20 28 20
5 | 9 24 9 14 12 5 18 9 11 24 4 | 14 27 21 22 24 17 25 17 20 18 16
6E | 14 24 12 16 20 14 21 40 23 36 8 | 111 117 114 112 121 118 122 110 121 121 113
7 | 7 20 12 11 28 6 19 8 10 20 4 | 14 31 26 22 39 18 30 16 21 19 18
8 | 6 17 7 6 15 4 11 8 9 15 3 | 12 25 20 14 20 15 23 14 16 16 14
9 | 7 20 7 7 12 4 12 12 7 15 3 | 18 24 19 18 17 19 20 23 21 25 18
10 | 7 17 12 8 13 5 13 6 9 21 3 | 16 20 26 22 24 18 19 20 19 19 18
11 | 6 18 9 10 19 4 18 6 7 13 3 | 16 29 24 15 34 17 29 18 18 17 17
12 | 5 23 8 12 24 5 23 12 10 22 4 | 17 30 19 20 31 18 31 19 17 19 16
13E | 5 25 9 9 15 4 16 10 7 13 3 | 20 32 26 23 33 22 30 25 22 28 22
X14E | 8 16 11 10 --- 4 18 10 8 20 4 | 14 20 19 11 --- 14 17 12 13 14 16
15 | 9 33 5 11 16 5 22 14 8 12 4 | 12 30 19 18 21 16 25 19 18 22 15
16 | 9 26 13 14 19 8 25 9 8 34 5 | 17 30 20 15 26 15 33 18 17 27 15
17E | 7 19 9 10 26 6 24 9 9 10 4 | 16 28 23 17 29 18 27 16 20 20 18
18 | 7 22 9 11 12 4 22 12 7 31 4 | 16 31 28 22 26 20 31 22 20 20 20
19E | 8 19 11 11 15 5 27 12 9 13 4 | 28 35 35 30 34 27 37 30 29 29 29
20 | 5 17 7 10 13 3 17 7 7 22 3 | 21 28 26 25 27 21 26 21 22 15 20
21 | 7 26 16 10 21 6 28 10 9 22 5 | 23 38 32 25 43 25 41 25 27 19 26
22 | 5 16 6 10 11 5 18 10 9 20 3 | 17 26 23 23 25 21 28 24 22 21 20
23 | 7 23 8 10 16 4 16 9 9 19 4 | 12 24 17 15 26 12 22 15 11 19 12
24 | 6 11 6 9 13 4 10 7 8 14 3 | 18 21 22 24 22 20 18 21 23 19 20
X25 | 27 --- 19 25 --- 22 --- 25 23 --- 12 | 26 --- 33 33 --- 27 --- 17 25 --- 21
26E | 18 22 7 11 20 10 14 16 15 22 5 | 138 139 134 137 133 137 133 142 139 138 137
X27 | 8 21 7 7 16 4 --- 11 6 11 3 | 14 20 17 14 17 16 --- 21 20 20 15
28 | 7 20 7 10 18 7 20 7 7 25 4 | 15 29 23 19 30 17 30 16 15 18 16
X29E | 7 21 10 9 19 6 29 11 8 --- 5 | 19 27 23 20 21 19 27 22 21 --- 19
30 | 5 18 7 6 10 4 12 12 7 11 3 | 15 21 19 16 24 16 23 20 18 21 16
31 | 4 23 9 10 23 4 21 10 10 17 4 | 14 28 15 17 31 13 28 14 14 18 13
32 | 5 12 6 10 15 3 14 6 7 17 3 | 14 20 18 21 20 15 17 19 18 15 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 21 9 10 17 6 19 12 10 21 |T 25 35 30 28 35 28 35 27 28 30 26
WRMS | 7 21 8 10 15 5 18 8 7 21 |NE 16 26 22 19 26 18 26 18 18 20 17
MEDI | 7 20 9 10 16 5 18 10 9 20 |MD 16 28 23 20 26 18 28 19 20 20 18
Table 3.1598.2 GPS week: 1598 Day: 2 MJD: 55432.000
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 --- 35 --- 20 36 --- 15 | 25 --- --- 21 --- 54 --- 16 31 --- 20
2 | 6 20 11 10 20 8 20 10 6 24 4 | 16 26 22 16 23 20 29 16 17 24 16
3E | 10 18 9 10 21 5 17 6 11 19 4 | 79 82 77 75 80 82 85 71 74 81 82
4 | 6 16 11 10 10 4 12 7 9 13 3 | 20 28 23 20 26 20 25 21 20 26 20
5 | 6 16 10 9 15 3 17 10 8 23 4 | 22 27 27 27 31 24 31 23 29 26 23
6E | 17 18 13 13 20 10 18 40 19 38 8 | 97 106 103 96 103 97 108 100 103 104 100
7 | 12 20 10 9 28 4 20 6 10 16 4 | 21 27 27 22 39 20 29 19 20 17 19
8 | 8 16 4 7 15 5 12 7 9 13 3 | 12 24 18 14 17 15 23 13 18 14 13
9 | 10 19 12 12 16 4 13 10 8 11 4 | 14 24 24 22 21 19 18 22 25 20 18
10 | 7 15 8 9 11 4 10 7 9 17 3 | 20 21 26 25 25 21 20 23 22 20 20
11 | 8 13 8 8 19 6 17 6 9 11 3 | 15 28 19 12 34 16 27 16 19 14 15
12 | 8 19 12 11 25 6 24 10 9 21 5 | 21 30 23 21 32 20 32 20 16 17 17
13E | 9 15 8 10 15 5 16 9 11 12 4 | 24 32 32 32 33 30 35 30 30 32 28
X14 | 4 --- --- --- --- 17 --- --- --- --- 0 | 16 --- --- --- --- 19 --- --- --- --- 18
15 | 9 25 8 12 16 5 23 14 10 13 4 | 12 27 19 17 23 16 25 16 23 21 15
16 | 8 26 12 12 21 9 25 9 9 34 5 | 13 31 19 16 22 16 32 16 17 28 14
17E | 9 18 8 11 22 5 23 10 9 13 4 | 15 29 20 16 23 17 28 15 20 21 16
18 | 8 17 8 13 11 6 21 12 7 26 4 | 19 32 28 26 28 24 31 24 30 19 23
19E | 8 17 8 8 20 5 29 14 9 12 4 | 24 35 31 25 33 25 39 26 27 27 26
20 | 9 14 6 11 15 4 17 7 11 18 4 | 23 26 28 27 26 23 26 22 21 17 21
21 | 6 23 8 9 17 7 26 14 8 17 4 | 22 41 27 23 42 25 40 23 30 18 25
22 | 8 15 7 11 14 3 18 8 4 18 3 | 24 32 28 28 30 26 32 28 28 25 26
23 | 9 23 7 10 17 6 18 9 13 20 4 | 14 30 21 19 25 19 30 19 23 24 17
24 | 6 10 3 6 15 4 13 6 6 11 2 | 18 19 20 19 23 19 19 20 22 18 19
X25 | 23 --- 13 20 --- 23 --- 23 22 --- 10 | 24 --- 24 18 --- 23 --- 18 22 --- 16
26E | 13 20 7 10 23 10 14 10 11 21 4 | 121 124 125 123 122 126 122 123 127 125 124
27 | 10 20 13 13 19 5 14 10 8 11 4 | 11 25 22 19 21 16 17 20 23 19 16
28 | 6 22 8 12 20 6 22 8 7 24 4 | 13 30 22 16 31 14 32 13 16 16 14
X29E | 7 20 9 13 20 9 27 14 9 --- 5 | 18 27 22 24 27 21 28 19 20 --- 18
30 | 7 13 6 9 15 6 11 8 6 17 3 | 18 23 24 22 29 20 23 22 21 22 19
31 | 4 20 8 9 24 4 21 10 9 12 4 | 14 26 17 16 34 14 26 16 15 16 13
32 | 10 13 6 6 17 6 14 6 12 13 3 | 15 16 18 17 20 13 17 17 19 13 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 9 10 18 6 19 12 10 19 |T 25 35 31 28 35 28 35 27 29 29 26
WRMS | 8 18 9 10 18 5 18 9 7 18 |NE 17 26 22 20 27 20 26 19 21 19 18
MEDI | 8 18 8 10 17 5 18 10 9 17 |MD 18 28 23 21 28 20 29 20 22 20 18
Table 3.1598.3 GPS week: 1598 Day: 3 MJD: 55433.000
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 | 15 81 --- 29 --- 37 --- 21 24 --- 12 | 30 42 --- 22 --- 34 --- 15 32 --- 22
2 | 7 24 6 9 15 9 23 9 8 23 4 | 15 28 18 17 25 17 27 15 13 26 15
3E | 9 16 6 10 17 4 17 7 11 23 4 | 84 100 92 84 103 86 102 89 88 100 88
4 | 7 12 9 10 11 6 12 12 12 16 3 | 21 26 24 25 26 20 22 21 23 27 21
5 | 6 19 3 11 10 4 19 11 10 22 4 | 21 29 27 31 31 24 28 25 23 25 23
6E | 12 17 8 12 23 5 18 27 16 30 6 | 89 96 93 88 97 92 100 93 91 96 90
7 | 6 19 9 14 24 5 22 13 12 19 5 | 21 28 24 23 40 20 28 19 19 16 20
8 | 6 13 3 9 13 4 11 10 11 13 3 | 16 20 21 19 21 16 25 19 15 15 17
9 | 7 17 7 11 15 5 14 14 11 16 4 | 21 25 20 27 24 19 23 27 19 21 20
10 | 6 15 4 11 11 6 14 11 10 17 3 | 23 26 29 31 30 24 26 28 23 25 24
11 | 7 12 5 9 21 4 18 6 8 13 3 | 19 25 17 14 35 15 24 15 15 16 16
12 | 9 20 6 13 16 5 23 13 13 20 4 | 24 31 21 25 27 21 31 25 15 21 20
13E | 5 17 6 9 15 8 18 16 13 16 4 | 29 30 30 31 30 26 33 26 30 28 27
X14 | 5 17 5 11 --- 5 20 11 9 17 4 | 16 21 20 14 --- 17 22 13 16 12 17
15 | 6 26 8 13 18 5 26 15 5 12 4 | 16 29 16 22 26 15 29 20 17 20 16
16 | 8 20 7 12 17 6 25 10 7 35 5 | 18 31 19 17 26 18 34 17 18 27 17
17E | 5 15 7 14 19 6 26 6 8 11 4 | 19 31 28 24 32 22 29 22 24 19 22
18 | 7 21 6 15 12 5 20 14 9 25 4 | 19 32 28 31 28 22 30 24 23 18 22
19E | 8 21 6 12 16 4 28 11 12 14 4 | 28 35 32 26 29 25 36 25 28 29 28
20 | 6 12 6 9 11 5 16 4 10 18 3 | 27 29 29 28 32 26 27 24 28 21 26
21 | 7 24 6 10 15 3 25 11 9 15 4 | 22 40 28 24 40 23 37 24 22 20 24
22 | 7 14 5 13 12 4 19 12 7 23 4 | 23 30 30 34 33 26 31 29 25 26 26
23 | 6 23 6 9 16 6 19 13 11 20 4 | 17 26 18 15 27 15 28 16 17 20 14
24 | 5 12 6 10 14 6 15 6 9 12 3 | 18 22 21 26 28 22 18 22 21 17 21
X25 | 28 --- 18 21 --- 17 --- 25 21 --- 11 | 32 --- 35 17 --- 25 --- 22 20 --- 22
26E | 20 16 9 12 23 5 11 10 10 20 5 | 150 150 151 156 147 146 151 150 151 150 148
27 | 6 26 7 14 16 5 14 13 13 13 4 | 18 31 16 24 22 17 22 25 19 20 18
28 | 5 21 4 11 18 4 22 8 10 25 4 | 18 28 23 22 33 19 30 18 19 17 19
X29E | 7 18 8 15 21 4 24 13 16 --- 5 | 19 25 24 25 30 18 24 19 16 --- 18
30 | 6 14 5 8 10 4 12 11 10 16 3 | 24 30 25 26 34 22 29 28 21 27 24
31 | 5 19 9 10 20 4 17 10 9 14 4 | 18 27 19 20 30 17 25 18 19 18 17
32 | 8 12 4 8 15 4 15 8 9 13 3 | 16 19 20 19 25 16 15 17 20 13 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 6 11 16 5 19 12 10 19 |T 29 36 32 31 38 28 36 29 29 30 28
WRMS | 7 18 6 11 15 5 19 9 8 18 |NE 20 28 22 23 29 20 26 21 20 20 20
MEDI | 7 17 6 11 16 5 18 11 10 17 |MD 21 29 24 24 30 21 28 22 20 21 21
Table 3.1598.4 GPS week: 1598 Day: 4 MJD: 55434.000
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 | 15 37 --- 12 --- 18 --- 12 19 --- 9 | 24 43 --- 19 --- 54 --- 22 18 --- 20
2 | 7 26 7 9 13 4 24 7 10 24 4 | 18 31 19 21 29 19 30 17 19 32 18
X3E | 6 --- --- 12 --- 130 --- --- --- --- 9 | 14 --- --- 91 --- 212 --- --- --- --- 13
4 | 3 18 7 8 10 4 11 9 12 15 3 | 22 28 23 29 28 22 27 21 22 31 22
5 | 4 20 8 11 8 4 20 10 11 22 4 | 21 30 26 31 30 24 28 27 21 27 23
6E | 9 20 7 9 25 10 18 21 14 23 5 | 106 115 109 107 116 112 118 106 105 114 107
7 | 11 26 12 12 22 5 26 13 12 19 5 | 22 35 29 24 39 21 32 23 22 23 22
8 | 6 16 9 8 17 5 11 9 9 12 3 | 14 25 20 16 18 17 24 18 15 17 15
9 | 6 22 8 11 11 3 15 15 7 13 4 | 18 29 17 20 23 18 27 23 16 19 17
10 | 5 17 5 7 11 6 10 9 11 20 3 | 23 28 27 31 31 26 24 27 25 28 24
11 | 7 17 6 11 22 3 18 6 10 12 4 | 17 28 21 19 38 20 27 18 21 20 18
12 | 7 20 8 11 22 5 21 13 8 20 4 | 19 30 19 19 33 20 29 21 15 18 17
13 | 6 19 6 8 13 4 14 13 12 12 3 | 50 51 49 57 57 53 51 53 53 53 51
14 | 5 16 5 6 18 3 19 9 7 17 3 | 16 19 14 11 22 15 20 14 14 17 16
15 | 6 32 10 12 19 6 28 17 10 16 5 | 15 28 20 21 27 17 30 21 17 20 16
16 | 6 24 7 13 14 6 24 9 9 34 5 | 20 31 18 16 24 18 32 16 19 28 17
17E | 8 14 6 9 21 5 23 9 7 9 3 | 26 32 25 24 35 25 34 25 23 26 24
18 | 5 23 7 12 9 5 23 20 11 26 5 | 23 35 32 31 36 26 34 34 30 24 27
19E | 6 21 9 11 13 4 26 11 11 13 4 | 21 32 27 26 33 25 33 23 25 25 23
20 | 5 17 6 8 13 4 14 5 10 19 3 | 26 30 27 25 29 26 28 23 24 20 23
21 | 6 27 9 7 16 4 27 9 10 15 4 | 26 41 33 26 45 29 40 27 25 24 28
22 | 6 17 5 10 11 4 19 9 7 23 3 | 25 32 27 30 34 28 32 27 29 27 27
23 | 7 22 7 7 17 4 19 12 9 19 4 | 18 28 18 17 29 19 27 19 14 24 15
24 | 6 11 6 7 12 2 13 8 9 12 3 | 19 19 21 18 25 20 21 19 19 17 18
X25 | 26 --- 17 26 --- 22 --- 25 31 --- 12 | 31 --- 27 35 --- 20 --- 20 26 --- 21
26 | 8 15 6 9 19 6 15 12 11 27 4 | 100 96 104 96 100 95 101 95 103 101 97
27 | 7 22 8 10 12 4 16 14 9 12 4 | 16 26 17 21 24 19 27 23 16 19 17
28 | 6 23 7 15 16 5 21 9 10 27 4 | 17 32 23 22 32 20 32 20 18 21 19
X29E | 8 17 8 12 15 5 24 10 10 --- 4 | 24 25 24 25 28 25 28 22 23 --- 21
30 | 5 14 7 7 9 3 11 11 7 23 3 | 22 28 27 23 30 25 28 26 24 32 23
31 | 6 19 6 8 16 3 18 10 10 13 3 | 19 28 20 21 30 19 29 18 20 18 19
32 | 7 12 4 12 13 3 14 8 5 14 3 | 17 19 19 16 22 18 20 19 17 19 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 20 7 10 16 5 19 11 10 19 |T 26 35 29 30 36 34 34 27 27 30 26
WRMS | 6 20 7 10 15 4 18 10 8 16 |NE 20 29 23 22 29 22 28 22 20 23 20
MEDI | 6 19 7 10 14 4 19 10 10 17 |MD 21 30 23 23 30 21 29 22 21 24 20
Table 3.1598.5 GPS week: 1598 Day: 5 MJD: 55435.000
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 --- --- 27 --- 152 --- --- --- --- 21 | 40 --- --- 29 --- 122 --- --- --- --- 30
2 | 7 25 8 7 17 6 24 8 7 27 4 | 13 25 18 14 26 16 24 13 18 30 14
X3E | 7 --- --- --- --- 10 --- 7 11 25 6 | 13 --- --- --- --- 44 --- 14 13 12 11
4 | 6 15 5 7 12 4 14 9 8 14 3 | 18 24 21 19 25 19 23 15 22 25 18
5 | 7 16 8 15 13 3 18 9 8 22 4 | 21 24 24 28 31 22 26 21 23 25 21
6E | 10 17 5 11 16 4 16 15 13 21 4 | 134 141 135 130 142 132 143 128 134 144 135
7 | 14 23 10 12 23 4 25 12 13 15 5 | 25 31 26 27 41 21 27 23 18 18 22
8 | 6 14 5 6 20 3 11 9 10 9 3 | 11 22 15 14 19 13 21 12 15 15 13
9 | 7 16 7 9 12 5 17 13 7 12 3 | 14 22 15 19 17 13 22 18 13 14 13
10 | 6 15 6 8 15 3 13 9 11 21 3 | 20 19 25 21 28 21 18 21 24 24 20
11 | 7 17 7 7 27 3 18 9 13 15 4 | 16 26 19 18 36 17 25 14 21 17 17
12 | 7 21 7 13 23 5 24 10 7 22 4 | 17 29 16 20 29 15 30 17 15 16 14
13 | 6 19 7 7 26 4 19 13 9 10 4 | 16 23 20 18 33 16 22 21 20 22 17
14 | 6 19 6 10 17 3 22 8 6 18 3 | 10 20 13 11 13 10 18 9 16 11 10
15 | 9 30 9 10 19 4 29 11 10 11 5 | 14 30 19 20 25 16 30 20 16 19 16
16 | 10 19 8 11 17 4 25 7 10 34 4 | 15 26 14 15 21 13 29 13 19 27 13
17E | 8 19 8 11 57 6 26 8 9 13 5 | 21 31 26 24 59 21 28 19 30 21 24
18 | 6 19 7 15 10 4 21 19 7 26 4 | 17 29 20 22 27 18 28 26 20 16 18
19E | 5 22 6 9 22 3 28 9 12 17 4 | 19 30 23 20 28 19 30 21 26 21 20
20 | 5 12 6 8 22 5 16 7 8 22 3 | 21 27 26 23 31 22 24 18 24 17 22
21 | 10 22 7 9 18 4 26 13 13 14 4 | 21 35 26 18 40 22 38 21 24 18 22
22 | 7 16 5 12 11 3 21 7 6 20 3 | 17 27 21 23 27 19 26 18 22 18 19
23 | 8 22 6 8 23 4 20 11 8 20 4 | 18 27 19 16 32 16 24 15 18 24 15
24 | 6 12 5 9 16 3 14 10 9 14 3 | 15 17 18 19 20 16 15 16 16 11 15
X25 | 36 --- 25 12 --- 17 --- 18 18 --- 12 | 27 --- 39 25 --- 24 --- 16 14 --- 19
X26 | 16 30 --- 89 34 31 --- 25 46 --- 15 | 34 37 --- 72 48 41 --- 38 70 --- 39
27 | 8 18 5 10 15 5 16 13 5 10 3 | 13 24 13 19 19 12 20 17 13 13 12
28 | 6 22 6 10 20 4 25 7 11 28 4 | 13 29 22 21 31 15 31 16 20 19 17
X29E | 8 18 7 13 15 4 22 11 12 --- 4 | 17 25 22 21 23 16 23 18 17 --- 16
30 | 7 13 5 8 9 4 11 10 5 28 3 | 15 23 18 17 22 15 22 18 16 30 16
31 | 5 18 6 9 18 4 20 9 11 13 3 | 16 25 15 15 28 14 23 16 22 13 14
32 | 8 13 8 6 20 4 15 7 10 16 3 | 16 19 21 16 23 18 16 15 23 17 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 10 21 4 20 10 9 19 |T 21 29 24 24 32 25 28 21 24 23 21
WRMS | 7 19 6 9 18 4 20 9 7 18 |NE 18 25 20 19 27 21 24 17 18 19 17
MEDI | 7 18 7 10 18 4 20 9 10 17 |MD 17 26 20 20 28 17 24 18 20 18 17
Table 3.1598.6 GPS week: 1598 Day: 6 MJD: 55436.000
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 --- --- 21 --- 158 --- --- --- --- 15 | 34 --- --- 19 --- 134 --- --- --- --- 24
2 | 6 22 5 8 15 6 25 9 8 29 4 | 14 27 17 17 27 16 28 14 19 30 16
3E | 10 21 6 11 18 6 19 8 13 28 4 | 13 15 4 6 8 29 14 15 16 16 15
4 | 5 16 4 8 8 6 14 11 9 14 3 | 22 27 26 25 28 25 26 21 26 28 23
5 | 5 19 7 11 13 7 16 10 9 23 3 | 27 30 29 36 36 30 29 31 30 31 28
6E | 9 19 6 17 14 7 16 8 15 24 4 | 79 90 82 79 89 77 89 79 80 88 79
7 | 8 24 10 13 19 7 25 13 10 14 4 | 20 33 25 25 32 22 31 22 24 21 23
8 | 6 12 5 5 16 4 13 9 10 10 3 | 18 25 23 20 22 23 27 22 24 23 23
9 | 6 18 7 8 15 3 14 14 10 13 3 | 27 32 28 31 32 33 31 38 33 32 31
10 | 6 14 4 9 13 5 14 11 8 22 3 | 28 33 35 35 36 32 28 35 34 30 31
11 | 6 14 4 7 23 6 16 9 7 14 3 | 18 23 17 17 34 17 22 19 22 18 16
12 | 7 22 7 11 24 6 24 10 14 25 4 | 24 33 24 28 35 26 33 30 27 31 26
13 | 6 19 8 7 23 6 17 12 10 10 4 | 29 31 32 33 43 29 30 32 26 29 29
14 | 4 18 5 8 20 3 22 10 10 16 3 | 15 22 14 12 17 17 21 12 16 16 17
15 | 6 29 6 11 17 4 27 13 13 14 4 | 19 34 20 23 26 23 32 24 27 29 22
16 | 7 25 8 16 15 9 23 10 12 35 5 | 18 33 18 17 21 16 32 15 20 32 17
17E | 6 22 5 8 20 6 24 8 13 16 4 | 15 27 17 16 27 16 23 16 18 21 15
18 | 6 19 8 13 12 6 21 22 9 27 5 | 25 35 34 33 33 30 32 34 33 26 29
19E | 6 22 6 9 20 5 26 9 10 15 4 | 29 35 32 30 35 27 34 29 30 30 29
20 | 4 12 5 10 16 6 14 7 8 25 3 | 31 31 32 33 35 30 27 28 33 25 30
21 | 6 23 8 7 16 6 26 13 9 16 4 | 22 37 29 24 40 25 38 29 25 22 26
22 | 4 16 4 9 13 5 19 6 7 22 3 | 29 33 32 33 36 32 31 32 31 28 31
23 | 5 22 9 8 19 6 19 10 9 21 4 | 17 29 18 17 28 17 25 19 21 28 17
24 | 5 13 5 6 14 4 12 10 8 14 3 | 23 25 25 27 27 25 22 26 24 22 25
X25 | 24 --- 10 12 --- 17 --- 18 12 --- 8 | 25 --- 20 18 --- 16 --- 18 14 --- 15
26 | 6 15 6 10 14 6 12 9 9 21 3 | 77 76 77 77 85 82 78 76 83 77 78
27 | 8 20 6 8 13 3 15 15 9 12 3 | 24 31 26 29 28 31 29 37 31 31 29
28 | 7 22 8 8 19 6 22 8 9 31 4 | 14 27 22 19 29 18 30 16 17 26 17
X29E | 7 21 9 15 16 4 20 10 12 --- 4 | 18 23 23 22 22 18 24 20 17 --- 18
30 | 5 14 6 13 9 5 11 10 9 37 4 | 24 31 27 34 32 27 29 32 27 46 28
31 | 4 25 6 11 21 4 19 9 11 15 4 | 18 28 18 21 31 18 25 16 18 17 17
32 | 5 13 6 9 15 5 13 10 8 19 3 | 19 19 21 21 26 21 16 18 23 18 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 19 6 10 17 6 19 11 10 21 |T 25 32 27 27 33 30 31 27 28 30 26
WRMS | 6 19 6 11 16 5 19 10 9 18 |NE 22 29 24 25 30 28 28 25 25 27 23
MEDI | 6 19 6 9 16 6 19 10 9 19 |MD 22 31 25 24 31 25 29 24 25 28 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 4.1598 GPS week: 1598 MJD: 55430.0-55436.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 |U 10 9 33 |U 6 6 23 |U 15 15 68 |
emr | emr 2853 | 11 10 34 |U 7 7 32 | 34 22 67 |
esa | esa 2921 | 10 9 29 |U 6 6 22 | 74 81 218 |
gfz | gfz 3014 |U 8 9 27 |U 6 7 28 |U 17 17 62 |
grg | grg 2811 | 20 17 37 |U 18 14 68 | 34 22 70 |
igr | igr 2922 | 11 9 29 | 6 7 27 | 36 22 71 |
igs | igs 2926 | 10 9 28 | 6 6 24 | 32 20 64 |
jpl | jpl 2800 |U 11 10 33 | 8 7 34 |U 76 80 207 |
mit | mit 3017 |U 11 10 31 |U 7 8 29 |U 27 29 58 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1598.0 GPS week: 1598 Day: 0 MJD: 55430.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 7 9 23 | 5 6 25 | 36 29 134 |
emr | emr 2867 | 9 10 36 | 8 8 29 | 40 29 127 |
esa | esa 2976 | 8 9 27 | 4 5 22 | 32 29 122 |
gfz | gfz 3059 | 7 9 25 | 5 7 29 | 44 30 134 |
grg | grg 2880 | 8 8 30 | 79 45 338 | 36 29 131 |
igr | igr 2959 | 7 9 25 | 5 6 26 | 35 27 128 |
igs | igs 2909 | 7 9 24 | 5 6 25 | 36 29 128 |
jpl | jpl 2859 | 9 9 31 | 7 7 31 | 45 26 133 |
mit | mit 3072 | 8 9 25 | 6 9 32 | 40 36 133 |
Table 5.1598.1 GPS week: 1598 Day: 1 MJD: 55431.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 | 10 10 38 | 5 8 25 | 9 10 23 |
emr | emr 2868 | 12 11 45 | 7 10 38 | 10 12 26 |
esa | esa 2976 | 9 12 37 | 5 7 27 | 9 11 24 |
gfz | gfz 3062 | 9 12 35 | 6 8 28 | 13 11 23 |
grg | grg 2784 | 18 14 47 | 9 9 20 | 13 14 25 |
igr | igr 2961 | 10 11 37 | 5 9 30 | 9 12 23 |
igs | igs 2927 | 10 11 38 | 5 7 30 | 9 10 21 |
jpl | jpl 2770 | 10 13 42 | 8 7 41 | 9 10 21 |
mit | mit 3072 | 16 15 47 | 7 10 31 | 11 13 24 |
Table 5.1598.2 GPS week: 1598 Day: 2 MJD: 55432.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
emr | emr 2776 | 11 8 28 | 9 7 29 | 14 18 43 |
esa | esa 2880 | 9 10 25 | 6 6 22 | 14 19 38 |
gfz | gfz 2963 | 9 10 25 | 7 6 28 | 15 17 49 |
grg | grg 2784 | 12 9 31 | 9 9 25 | 16 19 44 |
igr | igr 2875 | 10 8 25 | 6 6 24 | 13 15 38 |
igs | igs 2894 | 10 8 25 | 6 5 23 | 14 18 37 |
jpl | jpl 2774 | 10 11 28 | 7 8 31 | 14 18 39 |
mit | mit 2976 | 16 12 36 | 8 7 33 | 96 93 93 |
Table 5.1598.3 GPS week: 1598 Day: 3 MJD: 55433.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 8 10 25 | 11 7 36 | 9 5 16 |
emr | emr 2954 | 9 8 27 | 10 8 38 | 10 7 17 |
esa | esa 2976 | 9 7 26 | 10 8 30 | 12 13 111 |
gfz | gfz 3056 | 8 8 26 | 11 7 42 | 9 5 16 |
grg | grg 2784 | 12 13 39 | 12 12 29 | 13 7 22 |
igr | igr 2943 | 9 8 29 | 11 7 41 | 8 6 16 |
igs | igs 2994 | 9 8 29 | 10 7 34 | 9 5 16 |
jpl | jpl 2869 | 9 7 31 | 12 8 45 | 8 5 21 |
mit | mit 3072 | 10 8 30 | 10 7 34 | 11 8 23 |
Table 5.1598.4 GPS week: 1598 Day: 4 MJD: 55434.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3044 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
emr | emr 2863 | 9 11 25 | 6 6 29 | 11 11 28 |
esa | esa 2880 | 9 8 25 | 5 6 20 | 11 11 29 |
gfz | gfz 2972 | 7 7 20 | 6 6 21 | 11 9 27 |
grg | grg 2784 | 15 7 25 | 5 7 23 | 12 11 32 |
igr | igr 2920 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igs | igs 2879 | 8 7 21 | 5 6 20 | 9 9 27 |
jpl | jpl 2777 | 10 8 25 | 6 7 28 | 9 9 29 |
mit | mit 2976 | 7 8 20 | 7 8 23 | 12 11 29 |
Table 5.1598.5 GPS week: 1598 Day: 5 MJD: 55435.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 14 12 51 | 5 5 15 | 11 28 150 |
emr | emr 2773 | 11 13 40 | 5 6 25 | 141 68 207 |
esa | esa 2784 | 10 10 30 | 5 5 15 | 434 480 1181 |
gfz | gfz 2927 | 9 10 32 | 5 5 23 | 24 42 169 |
grg | grg 2784 | 34 41 37 | 6 7 21 | 142 70 217 |
igr | igr 2863 | 10 11 31 | 5 6 18 | 141 67 198 |
igs | igs 2915 | 9 9 27 | 4 5 16 | 141 67 202 |
jpl | jpl 2683 | 10 10 36 | 6 7 28 | 435 490 1187 |
mit | mit 2976 | 8 9 28 | 5 9 27 | 11 36 85 |
Table 5.1598.6 GPS week: 1598 Day: 6 MJD: 55436.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3050 | 9 6 28 | 5 5 17 | 7 4 20 |
emr | emr 2872 | 20 11 37 | 5 7 33 | 9 7 22 |
esa | esa 2976 | 19 9 30 | 5 5 18 | 8 6 22 |
gfz | gfz 3065 | 9 6 25 | 5 8 26 | 7 4 18 |
grg | grg 2880 | 38 27 50 | 5 8 18 | 9 5 20 |
igr | igr 2939 | 19 9 30 | 5 6 21 | 8 5 22 |
igs | igs 2967 | 19 8 31 | 6 7 23 | 7 4 20 |
jpl | jpl 2871 | 19 10 37 | 6 6 36 | 8 6 20 |
mit | mit 2976 | 12 9 29 | 6 7 22 | 8 7 20 |
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 6.1598 GPS week: 1598 MJD: 55430.500-55436.500
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 | -7 -24 -4 -20 -6 | 4 15
| 29 17 92 64 5 | 1
emr uuuuu | 14 24 290 185 -3 | 61 63
| 13 32 135 96 9 | 1
esa uuuuu | -2 -19 -59 27 1 | 14 24
| 12 9 86 83 9 | 1
gfz uuuuu | 13 46 -16 -73 0 | -1 16
| 21 12 34 51 4 | 1
grg uuuux | -51 -28 -14 -140 -14 | 1 31
| 47 39 53 69 43 | 5
igr xxxxx | 21 22 -4 129 -2 | -6 17
| 24 7 44 77 5 | 2
irf xxxxx | 8 0 -65 -9 -4 | 3 16
| 16 10 52 68 11 | 4
jpl uuuux | 36 19 -34 144 -21 | 34 40
| 68 27 77 113 24 | 5
mit uuuuu | -1 -16 -144 -63 -3 | 17 22
| 18 15 82 82 11 | 4
ngs uuuuu | -1 -20 154 6 0 | -1 15
| 30 37 108 130 7 | 2
sio uuuuu | -14 43 -80 11 -12 | 36 39
| 24 18 98 115 13 | 3
Table 7.1598.0 GPS week: 1598 Day: 0 MJD: 55430.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 22 -28 -157 57 -7 | 5 14
emr uuuuu | 25 1 300 57 4 | 60 61
esa uuuuu | 13 -10 -107 95 11 | 13 23
gfz uuuuu | 23 36 -68 -53 -5 | 1 17
grg uuuux | -74 -58 19 -127 -47 | 7 29
igr xxxxx | 39 35 57 99 -4 | -3 20
irf xxxxx | 20 13 12 73 8 | -3 14
jpl uuuux | -43 19 18 -65 14 | 36 40
mit uuuuu | 9 -3 -25 39 4 | 11 17
ngs uuuuu | -8 -26 57 -96 -7 | 3 18
sio uuuuu | -12 67 66 118 3 | 31 34
Table 7.1598.1 GPS week: 1598 Day: 1 MJD: 55431.500
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 -9 -97 31 0 | 4 14
emr uuuuu | 15 -11 559 50 1 | 60 62
esa uuuuu | 3 -11 -120 140 6 | 13 22
gfz uuuuu | 27 54 -21 -18 -7 | -1 16
grg uuuux | -22 7 -94 -110 -45 | 4 30
igr xxxxx | 60 18 26 177 -12 | -4 19
irf xxxxx | 19 3 -38 39 8 | -2 14
jpl uuuux | -18 10 98 45 4 | 37 41
mit uuuuu | 11 -21 -81 15 7 | 11 18
ngs uuuuu | -19 -35 46 -164 -3 | 1 16
sio uuuuu | -8 57 -58 64 2 | 32 35
Table 7.1598.2 GPS week: 1598 Day: 2 MJD: 55432.500
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 | 14 -33 52 45 -5 | 5 16
emr uuuuu | 19 -13 261 188 12 | 61 63
esa uuuuu | -4 -25 -171 -6 11 | 13 23
gfz uuuuu | 3 40 -28 -80 1 | -1 16
grg uuuux | -14 -62 0 -46 -67 | 3 30
igr xxxxx | 9 18 -67 169 2 | -6 17
irf xxxxx | 18 -3 -18 38 4 | 1 18
jpl uuuux | -39 -21 -62 194 -12 | 39 44
mit uuuuu | 9 -21 -76 -39 7 | 15 23
ngs uuuuu | 12 35 199 -97 -9 | 1 15
sio uuuuu | -7 36 2 144 -6 | 35 39
Table 7.1598.3 GPS week: 1598 Day: 3 MJD: 55433.500
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 -18 39 -54 -6 | 5 16
emr uuuuu | 12 68 146 229 -6 | 62 64
esa uuuuu | -4 -31 1 -21 0 | 14 24
gfz uuuuu | -9 42 4 -94 3 | -2 15
grg uuuux | 8 -47 67 -76 -18 | 1 34
igr xxxxx | -2 30 -57 156 -2 | -8 16
irf xxxxx | -8 -3 -116 -70 0 | 4 17
jpl uuuux | 57 62 -128 196 -33 | 36 41
mit uuuuu | -14 -14 -198 -156 4 | 18 24
ngs uuuuu | 5 -21 216 122 -2 | -2 14
sio uuuuu | -39 42 -197 -61 -12 | 38 41
Table 7.1598.4 GPS week: 1598 Day: 4 MJD: 55434.500
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 | -47 -47 1 -81 -7 | 5 15
emr uuuuu | 34 48 253 303 -8 | 62 64
esa uuuuu | -26 -23 29 -110 -4 | 14 24
gfz uuuuu | -17 42 25 -111 4 | -2 15
grg uuuux | -101 -22 -22 -201 39 | -6 30
igr xxxxx | 10 15 0 10 2 | -8 16
irf xxxxx | -4 -18 -111 12 -13 | 6 17
jpl uuuux | 124 0 -97 250 -50 | 34 40
mit uuuuu | -10 -43 -223 -30 -13 | 21 25
ngs uuuuu | 54 17 166 130 5 | -3 14
sio uuuuu | -28 13 -170 63 -20 | 39 41
Table 7.1598.5 GPS week: 1598 Day: 5 MJD: 55435.500
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 2 112 -100 -16 | 5 16
emr uuuuu | 3 46 178 246 -14 | 63 65
esa uuuuu | 6 -26 52 69 -9 | 15 24
gfz uuuuu | 26 37 19 -150 3 | 0 15
grg uuuux | -37 41 -64 -233 42 | -4 32
igr xxxxx | 34 18 1 59 -1 | -7 16
irf xxxxx | -15 -2 -66 -118 -19 | 8 16
jpl uuuux | 80 39 -65 172 -30 | 30 39
mit uuuuu | -32 -17 -176 -177 -19 | 22 26
ngs uuuuu | -7 -33 59 158 9 | -2 14
sio uuuuu | -37 31 -47 -154 -29 | 39 41
Table 7.1598.6 GPS week: 1598 Day: 6 MJD: 55436.500
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 | -44 -37 20 -36 -5 | 2 17
emr uuuuu | -7 31 334 225 -11 | 62 64
esa uuuuu | -3 -7 -98 20 -9 | 14 24
gfz uuuuu | 37 69 -41 -7 3 | -1 15
grg uuuux | -119 -58 -3 -185 -3 | -1 33
igr xxxxx | -3 18 12 232 1 | -8 16
irf xxxxx | 25 11 -119 -38 -15 | 5 17
jpl uuuux | 89 22 -5 219 -38 | 26 38
mit uuuuu | 17 6 -233 -96 -13 | 20 25
ngs uuuuu | -43 -76 337 -12 8 | -2 14
sio uuuuu | 31 54 -158 -98 -24 | 35 39
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