[IGSREPORT-20177] Wk 1653 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 29 09:46:29 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1653 (Sep 11, 2011 - Sep 17, 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:
igs1653[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1653[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1653[0-6].cls IGS GPS clock combination summary report.
igs16537.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16537.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because of poorer consistency (GRG),
they provide broadcast clocks (NGS), or clock corrections are not provided
(SIO). The clock information not used is still compared to combination for
completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 27 27 KOSG KOSG NRIL
0 | EMR | 9 9 KHAJ
0 | ESA | 17 29 30 30 IRKJ
0 | GFZ | 8 27 30 HOLM KOSG MDVJ
0 | GRG | IRKJ
0 | JPL | 9 IRKJ
0 | MIT | 1 9 27 1 9 27 DAV1
1 | COD | CHUR
1 | EMR | 9 9
1 | ESA | 30 30 TIXI
1 | GFZ | 30 MDVJ
1 | GRG | URUM USN3
1 | JPL | 27
1 | MIT | 9 27 30 6 9 27 30 KHAJ KHAJ MAW1
2 | ALL | 27
2 | COD | KOSG
2 | EMR | 9 9
2 | ESA | 30 30 NANO UNSA
2 | GFZ | 30 MDVJ NKLG NYAL THU3
2 | GRG | SANT
2 | MIT | 1 9 28 1 9 28 KOSG
3 | COD | 30 30
3 | EMR | HARB MATE
3 | GFZ | 27 30
3 | JPL | 27
3 | MIT | 1 27 30 1 27 30
4 | EMR | 9 9
4 | GFZ | 11 30 MDVJ
4 | GRG | AMC2
4 | MIT | 1 9 27 1 8 9 27 MAW1 MOBS KOSG MAW1 MOBS
5 | COD | 30 MCM4 NNOR MCM4 NNOR USNO WILL
5 | EMR | 9 4 9 24
5 | ESA | 30 KOSG COCO KOSG NKLG SFER UNSA
5 | GFZ | 7 11 27 30
5 | GRG | AMC2
5 | JPL | 8 27
5 | MIT | 1 8 9 27 1 4 8 9 27
6 | COD | 27 MAC1
6 | EMR | 9 9 MATE
6 | ESA | IRKJ UNSA
6 | GFZ | 7 11 27 30 MAC1 MDVJ
6 | GRG | IRKJ
6 | JPL | IRKJ
6 | MIT | 1 9 27 1 8 9 27 CAS1 MAC1 CAS1 MAC1
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | GRG | 27
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G01 | 4 | | | | | | |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
8. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .8 .5 .1 -19 -14 24 -.02
EMR | -1.3 2.9 1.7 3 -3 10 .26
ESA | 1.4 2.8 20.6 40 -13 75 -.09
GFZ | -.7 1.0 -.1 -28 11 7 -.06
GRG | -3.6 2.2 14.6 -16 8 9 -.08
JPL | -2.1 4.0 5.2 -27 -8 20 .0
MIT | .8 1.9 12.5 -20 13 -20 .17
NGS | 3.4 -.6 10.5 -43 -3 5 .10
SIO | 5.3 3.8 -5.4 61 -142 -3 .21
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1653.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1653.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 2.1653.[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 3.1653.[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 5.1653.0-6).
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 1653 summary. (Sep 11, 2011 - Sep 17, 2011)
Table 1.1653.a GPS week: 1653 MJD: 55815.000-55821.000
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 252| 0 0 2 16 4 27 -.29 9 8 | -433 164 19 101
| 0 0 0 8 7 16 .01 | 386 753
emr 91| 0 0 -2 -22 -3 11 .40 20 20 | 605 -31 18 103
| 2 2 0 23 12 11 .03 | 1189 950
esa 139| 0 0 1 -83 59 -7 .22 8 7 | -38 -301 19 189
| 0 0 1 16 21 14 .02 | 598 1187
gfz 197| 0 2 -1 50 -116 9 -.21 12 11 | 19 -79 24 107
| 0 1 1 22 31 12 .04 | 363 573
grg 128| 2 0 8 5 -30 20 .54 16 15 | 99 -189 55 237
| 0 1 3 18 13 13 .05 | 336 297
igr n/a| 0 0 0 -18 -21 -14 -.10 5 5 | 2121 82 19 84
| 0 0 0 9 13 16 .02 | 1224 903
jpl 145| -1 0 -3 44 -27 6 .57 16 15 | 446 -14 19 109
| 1 1 1 8 13 27 .01 | 1081 851
mit 278| 0 -1 -4 9 -64 -16 -.34 11 10 | -31 29 24 182
| 0 1 0 20 18 6 .02 | 473 727
ngs 221| 0 0 0 68 2 -23 -.25 10 8 | -411 96 2046 3729
| 0 1 1 14 18 6 .03 | 336 711
sio 254| 2 1 -4 -150 251 -20 .05 20 19 | --- --- --- ---
| 1 1 1 9 18 5 .02 | --- ---
Table 1.1653.b GPS week : 1653 MJD: 55815.000-55821.000
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 17 11 12 12 14 10 |
2 | 4 5 4 5 4 5 4 |
3 | 3 4 4 4 4 4 4 |
4 | 4 5 5 5 6 6 6 |
5 | 4 4 4 4 4 5 5 |
6 | 3 4 4 3 4 4 4 |
7 | 5 4 5 5 5 5 5 |
8 | 4 5 5 6 5 5 5 |
9 | 5 5 6 5 6 7 8 |
10 | 3 3 3 3 3 3 4 |
11 | 3 4 4 4 4 3 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 5 5 |
14 | 4 4 5 4 4 5 5 |
15 | 5 5 5 5 5 6 5 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 5 5 |
18 | 4 4 4 5 5 5 5 |
19 | 4 4 4 4 4 5 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 5 5 4 4 5 |
22 | 4 4 4 4 4 5 5 |
23 | 4 4 4 5 5 5 5 |
24 | 4 4 5 5 5 5 5 |
25 | 4 5 5 4 4 4 5 |
26 | 3 4 4 4 4 4 4 |
27 | 7 7 7 7 8 9 9 |
28 | 5 5 5 4 5 5 5 |
29 | 4 5 4 4 4 5 4 |
30 | 6 7 6 5 4 4 4 |
31 | 5 4 4 5 4 5 4 |
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 2.1653.0 GPS week: 1653 Day: 0 MJD: 55815.000
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 252| 0 0 1 12 8 13 -.29 8 7 | -941 823 20 90
| 29 -19 |
emr 91| -1 5 -2 -16 -5 7 .44 19 19 | 423 -912 13 84
| 0 -29 |
esa 139| 1 0 2 -55 81 -15 .22 6 6 | 520 -1911 19 198
| 20 -22 |
gfz 197| 0 0 -2 28 -129 28 -.26 10 9 | 317 -777 22 114
| -2 15 |
grg 128| 3 -1 12 9 -44 35 .59 16 15 | 216 -702 39 216
| 4 -20 |
igr n/a| 0 0 0 -20 -11 -26 -.10 4 4 | 1757 -1153 18 89
| -7 12 |
jpl 145| -2 1 -5 38 -24 42 .58 15 15 | 474 -938 17 94
| -30 29 |
mit 278| 0 -3 -4 -13 -82 -15 -.35 11 10 | 341 -424 19 157
| 7 13 |
ngs 221| -1 0 0 76 -4 -21 -.20 9 7 | -706 513 2287 3594
| -25 -13 |
sio 254| 3 0 -5 -156 245 -29 .08 20 19 | --- --- --- ---
| 32 -121 |
Table 2.1653.1 GPS week: 1653 Day: 1 MJD: 55816.000
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 252| 0 0 1 24 2 34 -.29 9 8 | -888 1195 18 97
| 9 -2 |
emr 91| 2 -1 -2 -46 -21 29 .43 19 19 | -328 -489 14 103
| 19 1 |
esa 139| 0 0 2 -83 37 -5 .25 7 7 | -104 3 18 217
| 43 2 |
gfz 197| 0 2 -1 56 -52 11 -.26 11 11 | -574 837 26 116
| 4 29 |
grg 128| 3 0 12 12 -9 26 .50 16 16 | -129 -286 62 205
| 37 -83 |
igr n/a| 0 1 0 -13 -3 -19 -.12 5 5 | 996 -501 19 85
| 4 16 |
jpl 145| -3 0 -4 52 -19 -11 .56 16 16 | -292 -512 18 117
| -28 4 |
mit 278| 0 -1 -4 -14 -69 -31 -.36 11 11 | -212 673 20 182
| 0 7 |
ngs 221| -1 -1 -1 76 -12 -22 -.26 10 8 | -862 1153 1830 3109
| -106 -11 |
sio 254| 4 0 -4 -144 253 -28 .05 20 18 | --- --- --- ---
| 26 -123 |
Table 2.1653.2 GPS week: 1653 Day: 2 MJD: 55817.000
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 252| 0 0 2 0 -3 20 -.28 9 7 | -327 417 18 102
| 25 3 |
emr 91| -5 0 0 -48 -1 -8 .40 20 20 | -1031 -27 14 90
| -19 -42 |
esa 139| 0 0 0 -99 75 -19 .24 8 8 | -703 558 16 172
| 52 -25 |
gfz 197| 0 0 0 85 -124 6 -.18 11 10 | -285 234 25 110
| -4 81 |
grg 128| 1 0 10 -24 -37 23 .54 16 15 | -400 -144 57 244
| 38 -82 |
igr n/a| 0 0 0 -28 -20 -34 -.09 5 5 | 491 115 20 78
| 8 24 |
jpl 145| -2 1 -2 31 -15 36 .57 15 15 | -1237 164 17 101
| -57 14 |
mit 278| 0 -1 -4 23 -50 -15 -.35 12 11 | 830 -1225 28 159
| -21 -8 |
ngs 221| 1 1 0 65 -18 -30 -.21 9 8 | -325 396 1944 3826
| -45 -28 |
sio 254| 3 1 -4 -138 241 -13 .06 19 18 | --- --- --- ---
| 34 -131 |
Table 2.1653.3 GPS week: 1653 Day: 3 MJD: 55818.000
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 252| 0 0 2 17 4 20 -.31 8 7 | -527 207 18 79
| 13 -25 |
emr 91| 0 -1 -3 -14 18 13 .38 21 21 | 267 1601 20 101
| -7 -56 |
esa 139| 0 0 0 -74 30 -18 .20 7 6 | 339 -388 18 163
| 38 15 |
gfz 197| 0 2 -2 41 -122 8 -.17 13 12 | -164 375 22 100
| 1 82 |
grg 128| 2 0 6 27 -12 21 .60 15 14 | 49 198 46 235
| -17 -102 |
igr n/a| 0 0 0 -12 -24 -16 -.14 6 6 | 1814 1380 20 80
| 12 43 |
jpl 145| 0 1 -3 57 -19 25 .56 15 15 | 77 1344 19 111
| -29 8 |
mit 278| 0 -2 -3 -2 -72 -9 -.32 11 10 | -582 1018 26 218
| 4 -1 |
ngs 221| 0 0 2 79 9 -21 -.24 10 7 | -569 163 1925 3658
| -104 -122 |
sio 254| 2 0 -3 -165 236 -18 .03 20 21 | --- --- --- ---
| 53 -144 |
Table 2.1653.4 GPS week: 1653 Day: 4 MJD: 55819.000
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 252| 1 0 1 19 -3 16 -.29 8 7 | 76 -1034 20 128
| 20 7 |
emr 91| 0 -2 -3 -41 2 8 .40 21 21 | 1704 874 23 112
| 17 -19 |
esa 139| 0 0 1 -77 46 7 .21 8 8 | -692 1679 20 197
| 41 10 |
gfz 197| -1 2 0 19 -102 7 -.16 12 11 | 373 -386 22 93
| -15 102 |
grg 128| 1 0 5 9 -34 -3 .58 15 14 | 505 -249 44 234
| 33 -31 |
igr n/a| 0 0 -1 -18 -38 -8 -.09 4 4 | 2985 1043 19 96
| -21 6 |
jpl 145| -1 0 -1 45 -51 -2 .56 16 15 | 1185 864 23 116
| -33 -11 |
mit 278| 0 0 -4 6 -35 -14 -.32 11 11 | -283 16 25 171
| -5 -13 |
ngs 221| 0 0 0 80 -11 -22 -.23 10 8 | 68 -1045 2096 3802
| -136 -46 |
sio 254| 3 3 -5 -158 287 -20 .04 19 17 | --- --- --- ---
| 51 -155 |
Table 2.1653.5 GPS week: 1653 Day: 5 MJD: 55820.000
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 252| 1 0 2 16 4 28 -.29 9 8 | -381 -7 19 86
| 24 -7 |
emr 91| 1 0 -3 1 -13 20 .35 21 21 | 2496 -975 14 105
| -9 -5 |
esa 139| 0 -1 0 -101 63 16 .23 9 9 | 787 -1191 19 184
| 54 1 |
gfz 197| 0 2 -2 54 -129 18 -.21 14 13 | 295 -337 22 119
| -38 57 |
grg 128| 3 1 5 -15 -34 8 .46 16 15 | 515 -267 58 278
| 41 -57 |
igr n/a| 0 -1 0 -3 -38 16 -.09 5 5 | 4037 -547 17 73
| -32 11 |
jpl 145| 0 -1 -1 39 -20 -25 .58 15 15 | 2132 -740 18 108
| -8 0 |
mit 278| -1 0 -3 29 -86 -13 -.32 12 10 | -31 84 21 199
| -14 17 |
ngs 221| 0 0 1 63 28 -33 -.29 10 8 | -429 -25 2029 3945
| -41 -151 |
sio 254| 1 2 -3 -147 256 -19 .01 21 20 | --- --- --- ---
| 36 -143 |
Table 2.1653.6 GPS week: 1653 Day: 6 MJD: 55821.000
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 252| 1 0 1 26 18 62 -.28 11 10 | -44 -448 24 125
| 29 -24 |
emr 91| 0 0 -3 10 -3 13 .37 22 22 | 709 -289 29 128
| -45 -5 |
esa 139| 0 0 3 -93 82 -20 .18 8 7 | -417 -859 27 198
| 59 1 |
gfz 197| 0 3 0 65 -152 -12 -.19 12 11 | 174 -504 29 101
| -31 60 |
grg 128| 4 -1 5 19 -38 32 .49 16 16 | -62 121 85 253
| 14 -64 |
igr n/a| 0 0 0 -33 -17 -12 -.09 5 5 | 2771 239 23 89
| -21 11 |
jpl 145| 1 -1 -3 46 -41 -16 .57 16 16 | 783 -280 25 117
| -23 8 |
mit 278| 0 -1 -4 35 -54 -14 -.34 11 9 | -284 66 33 193
| -16 1 |
ngs 221| 0 1 0 39 23 -14 -.28 11 8 | -56 -481 2217 4173
| -5 -158 |
sio 254| 1 1 -6 -145 235 -16 .07 21 18 | --- --- --- ---
| 22 -111 |
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 3.1653.0 GPS week: 1653 Day: 0 MJD: 55815.000
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 | 20 --- 17 --- --- 14 --- 21 --- 30 11 | 127 --- 139 --- --- 145 --- 142 --- 100 135
2 | 10 21 5 7 16 7 15 10 10 16 4 | 40 45 42 41 46 41 44 39 45 46 41
3 | 7 13 5 7 13 4 11 11 8 20 3 | 18 23 25 25 28 24 29 23 17 32 22
4 | 7 18 7 10 18 4 14 9 12 29 4 | 89 89 89 95 87 92 87 94 93 85 89
5 | 6 17 6 10 15 6 15 14 6 23 4 | 33 40 38 32 44 33 43 30 33 34 34
6 | 7 16 6 6 11 4 10 11 8 12 3 | 13 20 23 22 25 18 25 22 14 24 19
7E | 15 24 9 10 25 8 22 10 7 15 5 | 64 75 73 69 73 70 73 68 73 62 69
8 | 10 15 7 13 14 3 19 11 7 26 4 | 101 105 101 102 102 103 104 103 105 108 102
9E | 15 16 7 13 15 6 18 16 9 28 5 | 40 37 35 42 30 36 35 43 38 26 36
10 | 6 11 5 10 16 3 10 7 9 16 3 | 28 38 32 35 43 30 36 31 30 24 31
11E | 5 18 5 6 13 3 14 7 9 15 3 | 19 35 27 23 34 22 31 21 23 31 24
12 | 9 20 8 10 14 5 17 14 10 28 4 | 18 30 24 27 27 22 30 26 26 25 23
13 | 5 20 4 8 18 4 14 9 6 16 3 | 18 29 22 21 37 18 26 18 18 17 19
14 | 7 23 7 9 14 4 15 9 9 20 4 | 20 24 26 28 35 21 22 21 21 20 20
15 | 6 25 7 12 14 4 18 13 10 23 4 | 26 31 29 31 35 27 29 27 25 23 26
16 | 8 23 7 12 15 5 16 10 9 29 4 | 13 28 19 23 20 16 23 18 14 21 15
17 | 6 20 6 10 17 3 14 7 11 15 3 | 14 31 20 18 28 18 29 16 18 15 18
18 | 7 19 6 12 15 5 15 11 7 16 3 | 20 33 22 25 30 22 30 25 19 26 21
19 | 6 19 6 8 18 4 13 9 6 20 3 | 12 23 14 11 26 10 21 10 11 16 11
20 | 7 17 8 8 13 4 16 8 7 25 4 | 20 28 27 23 27 22 28 20 21 28 22
21 | 6 20 5 10 17 4 13 9 7 16 3 | 35 37 33 35 35 32 36 35 33 40 34
22 | 6 18 6 10 13 4 14 15 11 20 4 | 21 31 27 25 35 24 32 27 25 25 24
23 | 6 25 7 10 16 5 17 11 7 20 4 | 14 29 20 20 31 16 23 15 17 16 16
24 | 8 18 6 8 12 4 12 10 10 19 3 | 18 25 18 21 19 17 20 22 21 21 17
25 | 10 13 5 9 14 4 14 10 8 20 3 | 30 35 36 31 39 30 41 35 33 30 33
26 | 5 11 5 9 16 4 9 12 7 14 3 | 20 21 22 24 31 20 22 26 20 21 21
X27E | 12 22 16 17 372 17 16 14 --- 23 6 | 34 35 33 39 110 38 25 37 --- 31 31
28 | 9 18 7 19 15 6 15 11 8 27 4 | 24 37 34 33 34 29 38 34 27 28 29
29 | 8 25 8 11 16 4 17 8 8 18 4 | 27 34 28 25 31 25 29 28 25 32 26
X30 | 12 19 8 25 11 4 --- 13 --- 19 6 | 11 21 21 37 19 14 --- 19 --- 17 17
31E | 7 24 7 11 20 4 20 11 11 11 4 | 19 29 22 19 36 20 27 22 23 22 20
32 | 8 15 4 7 14 2 15 12 8 14 3 | 15 18 21 21 26 18 18 22 17 20 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 6 10 16 4 15 11 9 20 |T 31 36 35 33 39 33 35 34 30 33 33
WRMS | 7 19 6 9 15 4 15 10 7 19 |NE 19 28 25 25 31 21 28 23 21 23 22
MEDI | 7 19 6 10 15 4 15 11 8 20 |MD 20 31 27 25 34 22 29 26 23 25 23
Table 3.1653.1 GPS week: 1653 Day: 1 MJD: 55816.000
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 | 38 --- 19 --- --- 28 --- 26 --- 32 16 | 92 --- 97 --- --- 104 --- 100 --- 89 94
2E | 9 21 7 10 18 8 15 13 9 23 4 | 19 30 22 19 25 19 30 22 24 29 21
3 | 7 11 7 11 12 6 11 12 10 15 3 | 13 21 17 17 22 15 25 18 15 22 15
4 | 18 24 7 7 20 6 15 10 11 32 5 | 86 89 86 91 89 88 88 88 92 90 87
5 | 8 18 7 11 16 2 20 10 9 22 4 | 24 39 32 29 41 28 40 29 30 30 29
6 | 5 15 7 15 12 4 12 12 9 11 3 | 9 20 15 17 20 12 22 16 12 20 13
7E | 9 20 8 11 15 6 22 11 10 12 4 | 32 41 33 32 41 32 36 34 34 33 32
8 | 11 16 7 8 13 4 17 12 11 26 4 | 118 120 115 116 116 117 124 115 116 123 117
9E | 15 21 7 11 15 7 18 15 8 28 5 | 42 38 37 43 36 38 39 43 45 25 38
10 | 7 11 5 7 19 4 10 7 7 14 3 | 20 24 23 21 30 20 23 20 16 19 20
11E | 6 17 5 7 19 5 12 10 9 11 3 | 17 29 21 18 30 17 24 16 20 24 19
12 | 8 19 8 14 15 5 17 13 10 27 4 | 23 36 25 30 30 26 33 27 28 24 25
13 | 6 18 5 7 20 4 16 8 10 15 3 | 13 26 14 14 30 12 22 13 14 16 12
14 | 6 20 8 11 15 4 21 9 8 19 4 | 17 26 23 22 29 19 26 19 20 17 18
15 | 6 23 7 11 15 4 19 15 15 24 4 | 22 30 23 23 30 21 30 22 25 24 21
16 | 9 22 7 11 15 4 18 10 12 27 4 | 13 25 16 18 20 13 23 15 15 17 13
17 | 7 17 5 6 21 3 13 9 9 15 3 | 18 25 19 16 27 16 24 15 17 18 16
18 | 7 19 6 11 13 4 16 11 5 18 3 | 20 31 22 23 27 22 30 23 20 23 21
19 | 7 21 5 9 20 3 16 9 7 17 4 | 12 27 10 11 22 10 20 12 14 15 9
20 | 8 18 5 8 13 6 17 9 8 21 3 | 13 25 17 15 23 16 24 17 16 23 15
21 | 7 18 7 8 18 3 14 8 7 16 3 | 30 34 30 33 35 28 35 31 30 29 30
22 | 6 17 6 9 11 6 15 15 9 19 4 | 18 29 23 18 30 20 30 23 21 20 20
23 | 7 25 8 9 17 5 17 9 11 18 4 | 11 30 13 14 23 11 21 13 13 14 11
24 | 9 20 6 8 12 5 15 13 9 17 4 | 19 27 15 21 17 15 17 26 18 17 16
25 | 11 12 8 19 14 6 14 10 13 20 4 | 31 33 30 30 35 30 40 31 34 29 29
26 | 7 13 6 8 13 4 11 12 11 13 3 | 18 22 21 21 23 18 25 25 23 22 20
X27E | 16 25 18 15 --- 12 18 13 --- 20 7 | 36 37 35 35 --- 32 29 37 --- 21 32
28 | 10 21 8 18 15 5 17 12 10 27 5 | 19 36 27 31 30 24 31 26 24 24 23
29 | 6 23 9 12 16 5 19 9 10 18 4 | 35 40 34 35 34 35 39 36 34 33 33
X30 | 14 41 11 17 12 4 --- 12 --- 17 7 | 17 49 24 34 17 20 --- 22 --- 20 22
31E | 9 17 7 8 20 4 19 9 13 14 4 | 14 21 19 15 24 14 22 17 14 20 15
32 | 8 15 5 9 13 4 13 13 7 13 3 | 12 16 11 16 17 12 14 14 15 15 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 7 11 16 5 16 11 10 20 |T 27 34 29 28 32 28 32 30 27 29 28
WRMS | 8 19 7 11 16 5 16 11 8 18 |NE 18 29 20 21 26 19 27 20 20 21 18
MEDI | 8 19 7 10 15 4 16 11 9 18 |MD 19 30 23 21 29 20 26 22 20 22 20
Table 3.1653.2 GPS week: 1653 Day: 2 MJD: 55817.000
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 | 16 --- 14 --- --- 31 --- 22 --- 29 10 | 106 --- 103 --- --- 113 --- 101 --- 96 102
2E | 6 25 8 12 15 3 14 11 7 17 4 | 27 40 32 30 37 31 39 31 33 36 31
3 | 7 17 6 13 10 5 11 12 8 15 3 | 12 16 18 19 24 16 21 19 20 22 16
4E | 16 18 6 12 23 7 17 12 12 23 5 | 97 95 97 98 94 93 92 97 93 90 94
5 | 8 19 7 9 14 4 17 11 9 25 4 | 29 40 34 33 44 31 43 30 32 31 32
6 | 7 20 6 9 10 4 11 12 11 12 3 | 12 19 20 18 25 16 24 18 19 21 16
7E | 8 29 12 12 15 5 19 14 7 14 4 | 27 38 30 27 35 25 31 28 30 32 28
8E | 13 23 8 12 18 5 18 13 9 21 5 | 66 78 70 69 75 69 74 70 66 77 69
9E | 17 20 10 12 22 7 21 14 12 28 5 | 37 35 31 38 25 33 30 38 38 23 31
10 | 5 13 4 8 13 4 10 8 9 15 3 | 25 30 26 28 34 26 30 27 24 24 26
11E | 7 16 7 9 20 5 12 11 5 10 3 | 24 34 31 27 35 25 32 25 25 31 26
12 | 11 20 12 11 15 6 15 11 9 27 4 | 20 36 22 29 26 23 29 25 24 26 22
13 | 7 20 5 8 18 3 15 10 11 17 4 | 16 25 17 21 31 16 24 17 18 17 16
14 | 6 24 9 8 15 5 18 10 10 25 4 | 21 28 23 24 30 20 26 20 23 25 19
15 | 5 26 12 10 13 2 18 14 13 19 4 | 22 33 27 30 34 23 28 25 25 24 23
16 | 7 25 9 13 14 3 17 9 7 28 4 | 15 28 20 23 23 17 24 18 17 18 16
17 | 5 21 6 10 19 4 14 8 12 15 4 | 12 25 17 18 25 12 21 17 13 14 12
18 | 6 18 7 11 12 5 14 12 6 22 4 | 18 33 22 22 23 21 28 21 21 22 20
19 | 7 24 7 11 18 4 17 11 8 15 4 | 14 26 13 14 22 14 21 14 17 14 12
20 | 7 18 6 7 17 3 16 10 6 20 4 | 18 31 23 23 27 22 29 22 20 23 20
21E | 10 21 9 9 14 8 13 17 10 15 4 | 36 41 32 36 37 33 35 33 33 31 33
22 | 5 16 8 9 11 4 15 14 6 18 3 | 20 34 24 21 35 22 32 25 24 24 22
23 | 6 23 7 10 16 4 19 9 9 18 4 | 14 27 17 23 29 16 24 17 16 16 15
24 | 9 21 9 9 15 5 13 17 9 18 4 | 21 28 24 23 21 20 22 25 23 23 20
25 | 9 13 8 17 14 4 14 9 10 22 4 | 26 33 28 32 31 25 35 31 26 24 26
26 | 6 13 9 10 12 4 12 11 11 15 3 | 18 24 23 22 28 19 20 25 21 23 19
X27E | 13 28 14 16 20 17 --- 14 --- 23 7 | 26 33 23 28 66 27 --- 31 --- 29 23
28 | 9 23 9 14 15 5 16 11 9 27 4 | 27 36 33 34 36 28 33 36 33 32 29
29 | 7 22 8 9 14 5 16 10 10 17 4 | 36 43 32 36 30 33 36 39 33 36 33
X30 | 13 16 11 19 13 6 --- 12 --- 17 5 | 15 24 26 34 21 20 --- 21 --- 18 20
31E | 9 17 9 8 16 5 18 11 10 13 4 | 17 26 25 18 29 18 26 19 20 23 19
32 | 8 14 6 8 15 4 11 10 7 15 3 | 22 25 23 26 29 24 23 25 20 23 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 8 11 16 5 15 12 9 19 |T 28 34 30 29 34 29 32 30 27 30 28
WRMS | 7 20 8 10 15 5 15 11 8 18 |NE 19 29 23 25 28 21 27 23 22 22 20
MEDI | 7 20 8 10 15 5 15 11 9 18 |MD 21 33 24 27 30 23 29 25 24 24 22
Table 3.1653.3 GPS week: 1653 Day: 3 MJD: 55818.000
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 | 17 --- 11 --- --- 19 --- 21 --- --- 11 | 89 --- 95 --- --- 98 --- 94 --- --- 91
2E | 7 28 7 12 14 5 15 17 11 26 4 | 29 40 31 27 36 31 35 33 30 39 30
3 | 7 17 6 10 12 5 10 12 7 15 3 | 12 20 18 16 22 12 20 18 15 22 15
4E | 9 20 8 9 17 6 17 16 14 21 4 | 69 72 70 74 65 70 69 76 74 76 70
5 | 6 17 4 12 14 4 16 10 8 24 4 | 22 34 29 24 36 24 36 22 25 21 26
6 | 7 16 6 9 12 3 9 12 6 12 3 | 13 18 19 16 25 13 22 19 16 21 16
7E | 6 25 7 13 21 5 21 11 9 13 4 | 36 46 39 36 46 38 42 37 38 36 38
8E | 13 21 9 14 16 7 20 17 12 28 5 | 137 142 137 140 143 137 144 136 136 144 138
9E | 18 20 6 12 16 10 18 12 8 30 5 | 42 39 33 40 29 36 36 41 41 29 35
10 | 5 12 4 9 14 4 9 8 7 16 3 | 21 26 25 28 32 22 28 26 26 18 24
11E | 6 19 4 10 21 5 12 10 8 10 3 | 24 36 29 24 34 22 31 22 26 27 25
12 | 9 20 8 16 11 7 18 10 9 25 4 | 22 29 26 33 32 25 32 27 28 24 25
13 | 7 19 5 11 18 4 15 10 7 16 3 | 16 24 15 18 33 14 23 14 18 15 15
14 | 6 24 6 13 13 5 17 10 12 20 4 | 16 26 20 23 27 17 23 16 23 16 16
15 | 5 27 7 14 14 6 18 11 9 19 4 | 25 32 27 26 33 25 30 24 24 24 24
16 | 8 24 9 14 15 6 16 9 9 28 4 | 14 27 17 22 21 16 24 17 18 19 14
17 | 5 21 7 11 17 4 12 6 13 15 3 | 13 27 17 18 26 14 24 14 20 13 15
18 | 6 22 7 16 13 5 15 15 9 21 4 | 22 32 25 26 27 21 30 28 22 26 22
19 | 8 25 7 11 18 5 16 10 7 15 4 | 14 28 11 11 24 11 21 10 14 15 11
20 | 7 19 5 12 15 5 16 11 9 23 4 | 19 28 21 22 26 20 28 21 25 26 20
21E | 7 31 12 15 13 7 14 12 10 18 4 | 45 59 50 46 49 44 51 50 45 48 47
22 | 5 21 5 13 9 3 15 11 10 21 4 | 16 32 24 22 28 20 31 22 21 17 21
23 | 8 23 6 14 17 5 17 11 7 19 4 | 17 28 18 22 30 16 24 15 21 16 17
24 | 8 23 5 11 23 7 15 18 11 14 4 | 20 28 18 23 24 20 22 26 23 19 18
25 | 9 14 5 19 11 6 14 8 11 22 4 | 29 35 32 39 39 32 41 35 35 29 32
26 | 7 18 7 13 13 7 9 10 14 14 3 | 18 24 21 22 27 16 21 22 21 19 18
X27E | 13 24 17 18 26 16 19 14 --- --- 7 | 35 42 34 31 45 35 34 37 --- --- 31
28 | 8 21 8 13 14 6 17 9 8 25 4 | 21 34 30 32 30 28 32 30 29 26 26
29 | 8 23 8 14 14 5 13 8 10 18 4 | 24 31 23 26 26 23 25 27 23 27 22
X30 | 11 17 7 11 13 4 --- 11 12 --- 4 | 14 18 20 21 22 14 --- 21 14 --- 16
31E | 10 23 8 11 14 4 18 10 12 15 4 | 22 27 26 21 32 20 27 25 27 20 22
32 | 7 16 4 12 17 4 12 8 7 18 3 | 20 22 20 24 28 22 21 21 26 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 21 7 13 15 6 15 11 10 20 |T 29 35 31 30 35 29 34 32 30 29 30
WRMS | 7 21 6 12 14 6 15 10 7 21 |NE 18 27 21 23 28 19 26 21 22 20 19
MEDI | 7 21 7 12 14 5 15 11 9 19 |MD 21 29 25 24 30 22 28 24 24 22 22
Table 3.1653.4 GPS week: 1653 Day: 4 MJD: 55819.000
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 | 13 --- 13 --- --- 17 --- 22 --- --- 11 | 59 --- 55 --- --- 65 --- 67 --- --- 58
2E | 6 26 9 10 11 3 15 12 10 19 4 | 24 33 26 26 27 26 31 27 25 31 25
3 | 8 17 9 9 13 4 13 17 9 14 4 | 17 23 24 21 25 19 24 26 22 26 20
4E | 11 21 9 9 17 4 19 20 17 20 5 | 95 100 98 101 99 97 97 98 100 99 97
5 | 5 19 6 13 14 6 15 8 8 25 4 | 22 36 30 29 38 25 38 24 23 21 26
6 | 6 16 9 8 13 4 15 16 12 12 4 | 18 24 25 19 26 21 27 27 23 25 21
7E | 7 23 8 12 22 4 20 12 10 12 4 | 26 36 33 25 38 26 33 27 24 29 27
8E | 12 17 9 13 13 6 19 14 13 24 5 | 102 106 100 103 102 104 108 102 104 106 102
9E | 17 22 11 12 13 5 18 15 12 32 5 | 45 43 37 43 35 40 37 47 43 32 38
10 | 6 11 6 10 14 5 8 7 7 16 3 | 28 32 31 34 37 28 32 30 31 28 30
11E | 5 18 5 9 17 5 14 9 6 13 3 | 41 51 44 42 52 42 47 43 41 49 43
12 | 8 20 13 13 14 5 16 8 10 24 4 | 19 31 32 25 26 22 27 22 23 22 22
13 | 7 21 8 9 17 3 15 13 9 16 4 | 21 29 25 23 32 21 27 21 19 20 20
14 | 6 21 8 13 13 5 14 9 9 17 4 | 20 29 22 27 30 20 27 21 21 20 20
15 | 7 26 9 13 12 4 17 10 9 19 4 | 20 30 25 26 29 19 27 22 21 22 21
16 | 8 23 10 15 12 4 18 11 8 27 5 | 18 27 25 26 23 19 27 23 21 21 20
17 | 5 22 9 10 14 3 16 7 9 14 4 | 16 28 20 21 27 19 27 17 18 18 17
18 | 8 22 9 15 14 4 16 9 13 20 4 | 25 32 28 27 27 23 29 27 28 27 25
19 | 7 24 7 12 15 4 18 10 9 15 4 | 19 29 19 21 25 19 27 20 20 19 18
20 | 7 21 8 12 15 3 14 8 8 22 4 | 22 31 26 24 29 23 28 23 26 27 23
21E | 6 26 7 13 15 3 16 10 12 9 4 | 41 45 40 39 41 38 47 39 41 40 40
22 | 7 19 8 12 10 4 18 9 10 22 4 | 22 31 27 25 33 22 33 24 25 23 24
23 | 7 25 10 12 16 3 18 13 7 19 4 | 19 29 24 22 24 17 26 18 19 18 19
24E | 10 24 6 12 18 4 17 14 9 15 4 | 25 38 25 29 31 26 34 28 30 23 26
25 | 9 11 3 12 13 6 15 10 11 20 4 | 26 31 30 23 36 27 39 31 30 23 28
26 | 6 14 8 12 10 4 11 9 8 16 3 | 20 25 26 24 28 20 27 25 24 22 22
X27E | 16 20 16 20 --- 12 22 16 --- --- 8 | 35 42 35 38 --- 37 26 44 --- --- 33
28 | 8 20 8 16 14 4 17 8 7 26 4 | 20 31 27 33 28 25 30 27 27 27 24
29 | 7 22 10 11 13 3 15 9 9 17 4 | 25 30 27 25 20 23 25 26 23 25 23
X30 | 7 17 10 10 12 2 --- 9 10 13 4 | 16 20 22 18 18 17 --- 21 14 20 17
31E | 8 19 6 13 21 5 18 10 12 11 4 | 19 26 22 17 30 18 27 20 21 21 19
32 | 8 16 7 12 16 2 11 10 6 16 3 | 29 29 29 31 32 30 31 31 34 28 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 21 8 12 15 4 16 11 10 19 |T 29 36 33 31 34 30 35 32 30 30 30
WRMS | 7 21 8 11 14 4 15 11 8 17 |NE 21 28 25 24 28 21 28 24 23 22 22
MEDI | 7 21 8 12 14 4 16 10 9 17 |MD 22 31 27 26 29 23 28 26 24 23 24
Table 3.1653.5 GPS week: 1653 Day: 5 MJD: 55820.000
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 | 16 --- 16 --- --- 15 --- 25 --- --- 13 | 87 --- 89 --- --- 95 --- 90 --- --- 87
2E | 8 24 10 12 17 5 14 9 9 19 4 | 21 32 27 20 26 22 29 22 22 26 23
3 | 8 15 6 10 15 5 11 13 8 19 3 | 13 19 21 18 23 15 23 20 17 25 17
4E | 13 21 11 7 19 6 19 21 18 23 6 | 50 55 46 49 48 47 52 52 50 49 48
5 | 8 17 8 14 15 5 16 10 9 26 4 | 23 38 31 23 36 24 38 20 20 18 25
6 | 7 17 8 20 16 5 12 12 8 15 4 | 14 23 22 26 27 16 25 21 19 24 19
7E | 8 28 8 12 12 4 17 14 8 34 5 | 30 41 35 32 35 33 34 33 37 41 32
8E | 16 17 9 14 16 5 18 14 12 22 5 | 118 121 114 116 120 117 126 117 112 127 117
9E | 20 21 12 13 15 9 18 20 17 33 6 | 42 36 36 40 32 35 33 45 43 28 35
10 | 7 11 7 10 12 5 9 6 8 13 3 | 14 18 21 16 21 17 19 16 15 17 16
11E | 6 21 6 9 12 3 12 8 7 10 3 | 28 35 35 30 32 29 34 29 27 33 30
12 | 9 21 10 14 16 5 16 8 11 25 4 | 18 30 25 25 23 23 30 21 25 22 21
13 | 7 21 8 12 21 3 14 14 9 16 4 | 14 26 19 20 27 14 25 17 17 14 14
14 | 7 24 8 15 18 5 17 11 10 20 4 | 18 28 24 25 26 19 26 19 20 17 19
15 | 6 26 12 18 16 5 19 14 15 21 5 | 20 32 31 30 28 22 28 24 24 23 22
16 | 10 21 11 18 13 5 16 9 8 30 5 | 15 27 23 25 20 16 25 19 15 17 17
17 | 6 23 9 14 19 3 14 8 14 14 4 | 11 24 16 16 25 12 20 12 17 13 12
18 | 12 19 11 16 15 5 17 10 11 25 5 | 17 28 26 21 23 20 29 22 23 19 20
19 | 9 23 8 12 19 5 16 10 8 16 4 | 14 26 15 15 22 13 21 15 18 14 12
20 | 7 21 6 11 15 5 16 8 7 18 4 | 17 26 20 19 25 17 27 17 16 25 18
21E | 8 19 10 19 12 5 12 8 9 13 4 | 25 32 26 23 29 23 30 25 25 20 24
22 | 7 23 9 16 15 5 14 8 6 28 4 | 19 29 26 24 31 21 31 21 21 22 22
23 | 8 26 9 13 16 3 19 13 10 19 4 | 15 29 19 19 21 13 26 16 18 14 14
24E | 9 24 10 10 16 4 16 13 11 14 4 | 15 28 19 19 19 15 20 18 20 16 15
25 | 10 13 7 12 15 5 13 9 10 22 4 | 24 28 30 26 34 27 34 30 27 23 27
26 | 6 16 11 15 10 5 11 12 10 16 4 | 18 23 24 24 21 19 22 21 19 21 19
X27E | 12 23 27 12 --- 16 18 20 --- --- 9 | 36 36 41 39 --- 39 26 42 --- --- 33
28 | 9 23 13 19 14 4 17 10 7 27 5 | 17 28 27 28 25 19 26 21 20 21 19
29 | 9 22 10 13 17 5 13 11 10 20 4 | 23 28 19 24 21 21 23 28 19 29 20
X30 | 9 18 7 13 15 5 --- 8 7 15 4 | 15 18 23 23 20 18 --- 23 17 16 18
31E | 9 20 6 12 21 4 19 11 12 25 5 | 17 25 21 21 24 17 26 21 23 22 18
32 | 9 17 5 11 13 4 11 8 9 15 3 | 26 26 25 27 29 25 26 24 28 27 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 21 9 14 16 5 15 12 10 21 |T 26 32 30 27 29 26 31 28 25 26 26
WRMS | 8 21 9 13 15 5 15 10 8 20 |NE 17 26 23 22 25 18 26 20 19 20 18
MEDI | 8 21 9 13 15 5 16 10 9 19 |MD 18 28 25 24 25 20 26 21 20 22 20
Table 3.1653.6 GPS week: 1653 Day: 6 MJD: 55821.000
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 | 11 --- 13 --- --- 18 --- 21 --- 25 9 | 93 --- 94 --- --- 93 --- 86 --- 98 91
2E | 7 23 8 12 20 6 14 7 11 18 4 | 32 41 36 32 36 33 37 32 33 39 33
3 | 6 16 4 9 12 4 12 11 8 20 3 | 20 24 26 24 27 23 27 26 21 33 23
4E | 15 20 9 9 20 7 16 22 18 21 5 | 83 86 82 85 84 85 81 84 88 84 82
5 | 10 19 6 12 17 5 17 8 13 30 4 | 28 40 36 32 44 30 42 26 29 26 31
6 | 5 17 4 10 15 4 12 10 8 19 3 | 22 25 29 28 32 24 29 28 23 34 25
7E | 8 22 8 8 13 5 18 9 9 27 4 | 26 34 32 26 32 28 31 27 29 39 28
8E | 13 14 10 12 14 5 17 13 9 21 4 | 134 134 137 132 137 131 137 130 131 140 134
9E | 25 19 13 15 19 7 19 25 25 32 7 | 40 42 38 43 33 39 37 50 54 41 38
10 | 9 13 6 10 18 4 10 8 11 15 3 | 25 31 31 32 37 28 32 30 26 24 29
11E | 6 17 7 9 14 3 11 9 12 7 3 | 34 44 37 32 44 34 42 35 38 39 36
12 | 11 20 8 12 14 7 16 8 9 27 4 | 20 31 27 31 28 23 30 23 23 25 24
13 | 7 25 8 11 20 4 16 13 11 17 4 | 19 32 26 24 32 21 30 22 23 20 21
14 | 9 26 6 13 16 3 16 10 10 18 4 | 24 33 29 31 32 24 29 23 20 23 24
15 | 10 24 9 14 17 5 17 9 7 22 4 | 24 31 31 35 38 26 30 27 24 27 26
16 | 10 23 8 14 15 5 19 8 7 28 4 | 22 29 25 29 25 22 28 22 20 24 22
17 | 6 26 9 13 24 4 17 7 13 19 4 | 16 31 22 22 31 19 27 17 18 17 18
18 | 10 25 8 12 14 4 15 8 13 22 4 | 23 33 26 25 27 24 32 24 28 28 24
19 | 7 24 8 9 19 4 14 8 7 20 4 | 18 35 22 20 33 23 28 18 18 24 20
20 | 9 24 10 9 14 4 16 10 7 15 4 | 27 40 35 31 34 31 37 28 30 34 30
21E | 17 29 8 12 16 6 12 6 11 15 4 | 51 51 44 43 48 42 48 44 46 45 45
22 | 8 25 6 13 13 3 17 7 6 34 4 | 25 34 30 29 36 27 36 27 26 30 27
23 | 11 29 8 12 17 4 20 12 9 19 5 | 18 33 24 26 27 20 29 22 19 22 20
24E | 10 24 10 12 15 4 16 14 13 13 4 | 22 34 27 27 29 25 30 25 29 26 24
25 | 15 15 5 22 16 5 14 9 15 21 5 | 35 34 32 36 39 33 42 37 35 27 33
26 | 11 13 8 9 14 4 12 7 8 19 3 | 25 31 31 31 38 26 32 29 29 25 28
X27E | 17 22 20 18 --- 11 --- 21 --- 28 9 | 33 36 37 38 --- 32 --- 39 --- 26 32
28 | 12 21 7 13 18 6 18 8 9 28 4 | 22 33 33 36 31 28 31 31 29 30 27
29 | 8 22 7 14 14 4 13 7 11 21 4 | 21 27 19 24 21 20 22 23 21 28 19
X30 | 8 17 4 11 14 4 --- 9 12 15 4 | 17 21 23 25 23 19 --- 23 14 17 20
31E | 7 22 7 11 16 6 19 9 10 13 4 | 24 33 28 25 32 25 29 22 27 26 25
32 | 9 18 7 11 14 4 11 7 7 12 3 | 29 37 37 37 37 34 36 34 34 38 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 22 8 12 16 5 16 11 11 21 |T 32 38 37 35 38 34 37 34 32 36 34
WRMS | 10 22 7 11 16 5 16 9 8 18 |NE 22 31 28 28 32 25 31 25 24 26 24
MEDI | 9 22 8 12 15 4 16 9 10 20 |MD 24 33 31 31 32 26 31 27 27 27 27
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 4.1653 GPS week: 1653 MJD: 55815.0-55821.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 |U 10 8 25 |U 7 8 25 |U 10 11 39 |
emr | emr 2963 |U 12 11 35 |U 14 11 39 | 13 15 42 |
esa | esa 3072 | 10 8 25 |U 6 9 23 | 11 13 38 |
gfz | gfz 2960 |U 10 8 30 |U 12 12 37 |U 12 16 39 |
grg | grg 2907 | 11 9 28 |U 6 9 30 | 10 12 44 |
igr | igr 2999 | 10 8 26 | 7 9 27 | 10 11 40 |
igs | igs 3035 | 10 8 26 | 11 10 37 | 11 12 40 |
jpl | jpl 2835 |U 12 10 36 |U 13 11 42 | 13 17 41 |
mit | mit 3072 |U 10 9 26 |U 14 13 44 |U 11 13 41 |
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 5.1653.0 GPS week: 1653 Day: 0 MJD: 55815.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 11 8 28 | 5 7 13 | 7 6 17 |
emr | emr 2968 | 13 10 31 | 17 14 36 | 10 10 23 |
esa | esa 3072 | 10 5 25 | 6 11 20 | 8 8 19 |
gfz | gfz 2967 | 10 6 26 | 5 7 18 | 9 7 18 |
grg | grg 2880 | 11 9 28 | 7 13 38 | 9 11 19 |
igr | igr 2922 | 11 8 29 | 6 10 20 | 8 7 18 |
igs | igs 3027 | 11 7 26 | 6 9 18 | 8 7 18 |
jpl | jpl 2866 | 14 6 28 | 8 11 20 | 9 7 22 |
mit | mit 3072 | 11 9 26 | 15 12 35 | 8 10 20 |
Table 5.1653.1 GPS week: 1653 Day: 1 MJD: 55816.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 10 11 29 | 7 8 24 | 9 10 15 |
emr | emr 2968 | 13 11 33 | 16 10 39 | 11 9 23 |
esa | esa 3072 | 11 9 28 | 7 10 26 | 8 10 20 |
gfz | gfz 2968 | 10 9 29 | 18 31 51 | 9 9 17 |
grg | grg 2880 | 10 10 28 | 6 9 28 | 7 8 21 |
igr | igr 3037 | 10 9 30 | 6 9 23 | 8 8 17 |
igs | igs 3067 | 11 9 29 | 12 12 35 | 9 9 19 |
jpl | jpl 2864 | 13 8 35 | 16 10 49 | 9 9 23 |
mit | mit 3072 | 11 9 29 | 13 11 32 | 8 9 19 |
Table 5.1653.2 GPS week: 1653 Day: 2 MJD: 55817.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 12 7 28 | 6 9 19 | 8 6 18 |
emr | emr 2968 | 13 8 32 | 7 7 21 | 11 10 23 |
esa | esa 3072 | 11 8 28 | 5 8 17 | 7 9 21 |
gfz | gfz 2959 | 12 10 30 | 12 9 32 | 11 12 26 |
grg | grg 2976 | 12 11 30 | 6 8 21 | 8 11 27 |
igr | igr 2971 | 11 8 27 | 5 8 19 | 8 8 20 |
igs | igs 2959 | 12 8 28 | 13 11 37 | 9 7 20 |
jpl | jpl 2780 | 13 11 34 | 15 11 43 | 10 8 25 |
mit | mit 3072 | 12 8 29 | 13 11 33 | 11 10 24 |
Table 5.1653.3 GPS week: 1653 Day: 3 MJD: 55818.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 7 23 | 7 8 33 | 8 5 19 |
emr | emr 2964 | 11 11 30 | 17 12 46 | 8 6 17 |
esa | esa 3072 | 9 8 25 | 7 9 27 | 7 6 18 |
gfz | gfz 2960 | 9 8 35 | 13 9 45 | 6 7 20 |
grg | grg 2976 | 10 8 28 | 8 8 34 | 7 7 24 |
igr | igr 2970 | 9 7 24 | 7 8 29 | 7 6 18 |
igs | igs 3057 | 9 8 24 | 13 9 43 | 7 6 18 |
jpl | jpl 2865 | 11 9 27 | 14 10 46 | 8 8 23 |
mit | mit 3072 | 9 11 26 | 14 13 47 | 9 7 20 |
Table 5.1653.4 GPS week: 1653 Day: 4 MJD: 55819.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 10 11 26 | 7 11 26 | 10 8 15 |
emr | emr 2960 | 9 7 42 | 9 14 32 | 11 13 24 |
esa | esa 3072 | 8 6 22 | 5 12 25 | 9 9 15 |
gfz | gfz 2961 | 8 5 37 | 13 13 37 | 9 12 20 |
grg | grg 2878 | 8 8 25 | 5 11 31 | 9 7 14 |
igr | igr 3048 | 8 6 23 | 9 15 46 | 8 7 15 |
igs | igs 3057 | 7 7 21 | 13 13 39 | 13 8 19 |
jpl | jpl 2851 | 10 9 46 | 16 14 45 | 10 13 23 |
mit | mit 3072 | 6 5 20 | 13 15 44 | 10 10 20 |
Table 5.1653.5 GPS week: 1653 Day: 5 MJD: 55820.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 9 7 22 | 7 6 34 | 11 11 24 |
emr | emr 2957 | 13 11 49 | 14 9 51 | 10 13 26 |
esa | esa 3072 | 11 12 23 | 6 6 28 | 10 11 22 |
gfz | gfz 2956 | 10 9 23 | 11 7 40 | 12 12 25 |
grg | grg 2880 | 11 10 32 | 6 6 33 | 11 10 26 |
igr | igr 3053 | 10 8 22 | 5 7 27 | 10 9 22 |
igs | igs 3062 | 10 10 24 | 10 8 39 | 10 10 23 |
jpl | jpl 2855 | 14 9 43 | 10 9 37 | 14 30 32 |
mit | mit 3072 | 10 8 23 | 16 13 56 | 11 12 25 |
Table 5.1653.6 GPS week: 1653 Day: 6 MJD: 55821.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 8 9 23 | 7 6 26 | 20 33 168 |
emr | emr 2956 | 13 18 29 | 15 9 48 | 31 42 156 |
esa | esa 3072 | 8 9 26 | 6 7 22 | 25 37 153 |
gfz | gfz 2954 | 11 13 32 | 13 10 38 | 29 54 145 |
grg | grg 2880 | 12 10 28 | 6 7 26 | 20 31 178 |
igr | igr 2998 | 8 9 26 | 7 9 26 | 21 29 169 |
igs | igs 3022 | 10 9 30 | 12 10 45 | 23 37 160 |
jpl | jpl 2767 | 13 16 41 | 16 13 57 | 30 47 141 |
mit | mit 3072 | 11 14 30 | 16 15 59 | 19 37 163 |
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 6.1653 GPS week: 1653 MJD: 55815.500-55821.500
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 | -9 -24 31 39 -8 | 15 21
| 11 7 44 50 9 | 3
emr uuuuu | 3 4 34 169 -12 | 58 61
| 23 26 75 87 8 | 4
esa uuuuu | -16 -46 37 98 -5 | 15 23
| 20 13 52 46 4 | 3
gfz uuuuu | -80 10 -48 -83 0 | 9 18
| 34 20 31 82 4 | 3
grg uuuux | 44 -24 -31 2 -18 | 4 19
| 27 22 88 54 41 | 3
igr xxxxx | -37 6 -57 -20 -1 | 1 12
| 18 20 28 79 7 | 3
irf xxxxx | -19 -3 -40 -64 0 | 4 16
| 9 6 29 23 3 | 3
jpl uuuuu | -26 27 -28 -31 9 | 49 51
| 14 14 71 79 8 | 4
mit uuuuu | -21 4 -128 -108 7 | 18 24
| 16 14 35 61 5 | 4
ngs uuuuu | 57 63 159 28 0 | 10 19
| 57 43 70 111 6 | 3
sio uuuuu | 114 -39 -109 -153 2 | 52 53
| 17 18 87 85 6 | 3
Table 7.1653.0 GPS week: 1653 Day: 0 MJD: 55815.500
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 -28 30 32 -9 | 21 24
emr uuuuu | 18 1 100 67 -12 | 65 67
esa uuuuu | 11 -19 -30 74 -5 | 19 27
gfz uuuuu | -26 3 -50 30 -5 | 13 21
grg uuuux | 9 -3 69 11 6 | 6 23
igr xxxxx | -23 8 -92 56 -11 | 6 13
irf xxxxx | -11 1 -19 -30 -3 | 8 19
jpl uuuuu | -40 31 -99 13 3 | 49 51
mit uuuuu | -24 -6 -97 -70 -3 | 22 29
ngs uuuuu | 2 26 166 -94 11 | 12 23
sio uuuuu | 110 -31 -36 -74 6 | 49 51
Table 7.1653.1 GPS week: 1653 Day: 1 MJD: 55816.500
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 -11 66 116 -4 | 17 22
emr uuuuu | -10 -21 -17 29 4 | 60 63
esa uuuuu | -11 -45 81 126 3 | 15 23
gfz uuuuu | -38 -6 -50 34 -5 | 9 18
grg uuuux | 74 -39 10 48 -14 | 1 19
igr xxxxx | -25 -6 -35 62 -6 | 1 13
irf xxxxx | -9 -2 -34 -53 4 | 4 16
jpl uuuuu | -13 26 -99 10 -6 | 45 48
mit uuuuu | -16 -2 -114 -97 10 | 17 24
ngs uuuuu | 2 104 109 -114 -3 | 8 18
sio uuuuu | 114 -28 -69 -194 7 | 48 50
Table 7.1653.2 GPS week: 1653 Day: 2 MJD: 55817.500
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 -27 29 -21 -12 | 16 22
emr uuuuu | 26 17 114 253 -20 | 59 62
esa uuuuu | 9 -54 -28 124 -6 | 15 23
gfz uuuuu | -97 2 -34 -85 -1 | 8 17
grg uuuux | 66 -40 35 36 -19 | 3 17
igr xxxxx | -40 -10 -19 -15 3 | 0 12
irf xxxxx | -16 -2 -72 -99 -1 | 3 16
jpl uuuuu | -30 55 102 13 14 | 46 48
mit uuuuu | -8 19 -169 -238 4 | 16 23
ngs uuuuu | 12 43 135 52 2 | 8 18
sio uuuuu | 115 -36 -174 -167 1 | 51 53
Table 7.1653.3 GPS week: 1653 Day: 3 MJD: 55818.500
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 | -3 -22 5 63 -20 | 14 21
emr uuuuu | 28 -2 69 213 -15 | 56 59
esa uuuuu | -43 -47 22 18 -6 | 14 22
gfz uuuuu | -110 -10 11 -124 2 | 7 16
grg uuuux | 74 8 -153 -44 23 | 4 15
igr xxxxx | -71 -21 -62 6 -1 | -1 12
irf xxxxx | -28 -9 -51 -85 -4 | 1 15
jpl uuuuu | -36 20 -58 53 7 | 46 49
mit uuuuu | -27 -13 -135 -91 4 | 14 21
ngs uuuuu | 94 95 252 89 0 | 8 18
sio uuuuu | 116 -62 -221 -98 -6 | 51 53
Table 7.1653.4 GPS week: 1653 Day: 4 MJD: 55819.500
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 | -18 -33 -41 53 -15 | 12 19
emr uuuuu | 8 -30 80 181 -19 | 55 58
esa uuuuu | -21 -54 66 71 -10 | 13 22
gfz uuuuu | -113 2 -55 -162 0 | 7 17
grg uuuux | 20 -46 -97 -99 21 | 6 17
igr xxxxx | -17 8 -45 -86 -4 | -2 12
irf xxxxx | -11 -13 -57 -51 -1 | 2 15
jpl uuuuu | 0 20 -42 -181 13 | 48 51
mit uuuuu | 2 -8 -164 -84 9 | 15 22
ngs uuuuu | 35 123 220 211 1 | 9 18
sio uuuuu | 144 -64 -172 -44 -5 | 52 54
Table 7.1653.5 GPS week: 1653 Day: 5 MJD: 55820.500
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 | -24 -21 33 60 -2 | 10 19
emr uuuuu | -26 12 -81 245 -16 | 53 56
esa uuuuu | -32 -51 43 123 -6 | 12 22
gfz uuuuu | -88 41 -74 -136 3 | 7 17
grg uuuux | 26 -38 34 30 -83 | 9 19
igr xxxxx | -42 35 -53 -159 -3 | -2 12
irf xxxxx | -31 3 -58 -72 3 | 2 15
jpl uuuuu | -31 11 -9 -44 17 | 50 52
mit uuuuu | -48 17 -141 -125 12 | 16 23
ngs uuuuu | 120 44 185 47 -8 | 11 18
sio uuuuu | 112 -33 -114 -209 3 | 52 53
Table 7.1653.6 GPS week: 1653 Day: 6 MJD: 55821.500
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 | -3 -25 96 -27 5 | 15 21
emr uuuuu | -22 49 -29 194 -9 | 58 60
esa uuuuu | -28 -55 102 151 -9 | 19 23
gfz uuuuu | -87 35 -86 -139 5 | 14 19
grg uuuux | 37 -10 -117 30 -63 | 1 22
igr xxxxx | -38 25 -92 -7 12 | 2 11
irf xxxxx | -27 4 14 -60 3 | 8 14
jpl uuuuu | -35 27 8 -81 13 | 58 60
mit uuuuu | -28 20 -74 -54 12 | 25 28
ngs uuuuu | 131 9 43 4 -5 | 17 19
sio uuuuu | 84 -18 22 -284 7 | 58 59
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