[IGSREPORT-20219] Wk 1655 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Oct 13 09:15:00 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1655 (Sep 25, 2011 - Oct 01, 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:
igs1655[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1655[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1655[0-6].cls IGS GPS clock combination summary report.
igs16557.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16557.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 | ALL | 27
0 | EMR | 9 8 9 24
0 | ESA | 27 IRKJ
0 | GFZ | 7 8 9 11 30 31 MDVJ
0 | GRG | IRKJ USN3
0 | JPL | 8 9
0 | MIT | 1 9 24 27 1 4 8 9 24 CAS1 CAS1 KOSG
1 | COD | CHUR HNPT
1 | EMR | 9 4 9 KIRU
1 | GFZ | 7 8 11 27 30 31 MDVJ
1 | GRG | SANT USN3
1 | JPL | 4 8 9 27
1 | MIT | 9 27 9 24 CAS1 FAIR CAS1 FAIR MAW1
2 | COD | WROC WROC
2 | EMR | 4 9 4 9 YELL
2 | ESA | 27 SCH2 FLIN SCH2 UNSA
2 | GFZ | 2 4 7 8 9 21 30 31
2 | GRG | AREQ NKLG TLSE USN3
2 | JPL | 4 8 9 YELL
2 | MIT | 4 9 27 4 8 9 24 27 ALGO KOSG MAW1 TLSE
3 | COD | 4 CEDU KOSG
3 | EMR | 9 9
3 | ESA | 4 27 27 CEDU KOSG
3 | GFZ | 2 7 8 9 21 27 30 31 GODE MDVJ QAQ1 THU3
3 | JPL | 8
3 | MIT | 8 9 24 27 8 9 24 27 FAIR CEDU FAIR NYAL
4 | COD | 8 ULAB
4 | EMR | 4 9 4 9
4 | ESA | 8 CHUR
4 | GFZ | 2 4 7 8 21 30 31 KARR MDVJ NKLG
4 | GRG | AMC2
4 | JPL | 4 9 18 21
4 | MIT | 1 4 9 21 27 1 4 9 21 27 MAW1 MAW1
5 | COD | 27
5 | EMR | 4 9 4 9
5 | GFZ | 2 4 7 21 30 31 ALGO GODE MDVJ NRC1 WAB2 WES2
5 | GRG | USN3
5 | JPL | 9 BAN2
5 | MIT | 1 4 9 21 27 1 4 9 21 27 TWTF
6 | COD | 31 31
6 | EMR | 4 4 8 9 27
6 | ESA | TLSE
6 | GFZ | 2 4 21 30 ALGO MDVJ STJO
6 | GRG | AMC2
6 | JPL | 4 9 NKLG
6 | MIT | 1 8 27 28 1 4 8 9 27 28 KOSG
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
----+--------+---------------
1 | ESA | 1
2 | ESA | 1
5 | GRG | 24
5 | MIT | 24
5 | SIO | 24
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 | 1 | 4 | | | | |
PRN G08 | | | | | 4 | 4 | 4 |
PRN G24 | | | | | | 2 | |
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 | -.1 .4 -.1 -30 -5 23 -.11
EMR | -2.1 10.9 8.6 4 5 5 .13
ESA | .1 5.9 17.4 54 -6 71 -.06
GFZ | -1.3 .7 -.1 -41 21 2 -.10
GRG | -7.3 15.0 17.1 -17 22 7 .0
JPL | -2.3 9.0 17.4 -68 86 57 .03
MIT | 1.3 1.2 15.4 -21 16 -20 -.05
NGS | 1.7 -.2 9.6 -45 -8 2 .13
SIO | 6.3 6.0 .9 85 -107 21 .12
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 1.1655.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1655.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 2.1655.[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 3.1655.[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 5.1655.0-6).
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 1655 summary. (Sep 25, 2011 - Oct 01, 2011)
Table 1.1655.a GPS week: 1655 MJD: 55829.000-55835.000
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 253| 0 0 0 25 7 10 -.33 10 8 | -427 20 24 86
| 0 0 1 6 11 11 .01 | 650 882
emr 97| 1 0 1 -40 -37 7 .46 21 21 | 2001 205 20 134
| 2 1 2 25 23 14 .03 | 755 816
esa 137| 0 0 1 -106 72 -29 .17 9 8 | 44 -470 21 191
| 1 0 1 14 11 7 .03 | 1611 2043
gfz 193| 0 2 1 43 -44 15 -.23 11 10 | -180 616 25 99
| 0 1 0 40 42 9 .02 | 227 717
grg 127| 2 0 4 21 -30 6 .58 15 14 | -18 25 57 214
| 1 0 2 18 20 14 .03 | 571 800
igr n/a| 0 0 0 -10 4 -47 -.14 5 5 | 6403 5 21 80
| 0 0 0 14 10 20 .02 | 1104 673
jpl 127| 1 0 -1 108 -187 68 .57 16 16 | 1141 249 20 94
| 1 1 1 8 17 57 .02 | 811 624
mit 260| 0 -3 -2 18 -12 -33 -.38 15 13 | -210 85 25 191
| 0 0 1 21 20 22 .03 | 653 897
ngs 219| -1 0 -1 69 7 -12 -.30 11 8 | -433 51 1759 3625
| 0 0 0 25 23 24 .01 | 692 882
sio 251| 2 1 -4 -207 204 -13 .09 20 19 | --- --- --- ---
| 0 0 1 16 40 17 .04 | --- ---
Table 1.1655.b GPS week : 1655 MJD: 55829.000-55835.000
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 | 39 0 0 26 8 10 9 |
2 | 4 5 5 4 4 5 5 |
3 | 4 4 4 4 5 4 4 |
4 | 6 7 7 6 6 7 6 |
5 | 4 5 5 5 5 5 5 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 4 5 4 |
8 | 5 6 6 9 13 0 23 |
9 | 5 5 5 6 7 7 7 |
10 | 4 4 4 4 4 3 3 |
11 | 4 5 4 4 5 4 4 |
12 | 6 5 5 5 5 5 4 |
13 | 4 5 4 4 5 5 5 |
14 | 5 5 4 5 5 5 4 |
15 | 5 5 4 4 4 4 4 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 4 5 6 4 5 |
19 | 4 4 5 5 5 4 4 |
20 | 5 5 5 5 5 5 4 |
21 | 4 6 6 5 7 5 4 |
22 | 5 4 4 4 5 4 5 |
23 | 5 5 5 5 5 5 5 |
24 | 7 8 6 6 6 0 --- |
25 | 5 4 5 5 4 4 4 |
26 | 3 4 3 3 3 3 3 |
27 | 9 12 9 9 9 7 9 |
28 | 5 5 5 5 5 5 5 |
29 | 5 5 5 5 5 4 4 |
30 | 4 4 4 4 4 4 3 |
31 | 5 4 4 4 4 5 4 |
32 | 4 4 5 4 5 5 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1655.0 GPS week: 1655 Day: 0 MJD: 55829.000
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 253| 0 0 1 32 12 1 -.31 8 8 | -473 161 22 84
| 0 0 |
emr 97| 0 0 0 -9 -25 -16 .49 20 20 | 2229 842 17 126
| -24 15 |
esa 137| 0 0 2 -121 88 -18 .21 8 8 | -240 34 17 169
| 69 -10 |
gfz 193| 0 2 0 -16 -87 23 -.23 12 11 | 15 346 22 101
| 22 28 |
grg 127| 4 1 7 58 -50 28 .60 15 15 | 428 -409 52 208
| -59 -3 |
igr n/a| 0 0 0 7 4 -67 -.11 5 5 | 6918 866 18 86
| 10 35 |
jpl 127| 0 0 -3 112 -214 1 .58 16 16 | 1535 725 19 90
| -24 112 |
mit 260| -1 -3 -3 -2 -31 -1 -.38 14 11 | -230 472 21 185
| 2 -6 |
ngs 219| -1 0 -2 109 45 11 -.31 10 8 | -464 78 1987 3821
| -132 33 |
sio 251| 1 0 -5 -227 160 2 .13 18 18 | --- --- --- ---
| 58 -41 |
Table 2.1655.1 GPS week: 1655 Day: 1 MJD: 55830.000
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 253| 0 1 0 15 17 6 -.34 10 9 | -215 -465 40 93
| 68 16 |
emr 97| 0 -2 2 -21 -37 21 .46 20 20 | 2537 -37 31 139
| -31 30 |
esa 137| 1 0 3 -127 75 -27 .12 10 9 | 94 -780 35 196
| 57 -3 |
gfz 193| -1 0 0 54 -90 5 -.22 11 10 | 109 214 32 96
| -1 54 |
grg 127| 1 1 4 5 -43 24 .60 15 14 | 405 -392 65 228
| -2 -5 |
igr n/a| 0 0 -1 -14 11 -60 -.14 5 5 | 7695 -202 29 85
| 3 23 |
jpl 127| 1 -1 -1 114 -183 76 .57 16 16 | 1946 -311 24 87
| -34 115 |
mit 260| -1 -3 -4 44 -11 -36 -.38 15 13 | 110 -55 37 192
| 7 -23 |
ngs 219| -1 1 -1 61 20 -17 -.31 11 9 | -236 -460 1983 3269
| -120 8 |
sio 251| 3 1 -6 -183 186 -15 .11 18 18 | --- --- --- ---
| 54 -66 |
Table 2.1655.2 GPS week: 1655 Day: 2 MJD: 55831.000
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 253| 0 0 -1 33 18 26 -.31 9 8 | -332 467 30 92
| -1 -6 |
emr 97| -1 0 1 -18 -3 3 .44 20 20 | 2501 537 24 132
| -30 -11 |
esa 137| 1 0 3 -107 86 -35 .17 10 8 | -1657 2484 24 194
| 72 6 |
gfz 193| 0 2 0 18 -65 16 -.26 11 10 | -370 1281 25 93
| -5 72 |
grg 127| 0 0 1 23 -9 -2 .60 15 15 | -385 1122 60 229
| -13 -18 |
igr n/a| 0 0 -1 0 11 -56 -.14 5 5 | 7322 340 20 91
| -13 -4 |
jpl 127| -1 0 0 96 -178 26 .59 15 15 | 1480 459 21 84
| -9 81 |
mit 260| 0 -4 -3 -11 -47 -43 -.34 16 14 | -295 509 29 170
| 6 -5 |
ngs 219| -1 0 -1 102 17 10 -.31 11 8 | -310 507 1911 3877
| -116 -19 |
sio 251| 2 0 -4 -218 150 15 .11 20 20 | --- --- --- ---
| 36 -81 |
Table 2.1655.3 GPS week: 1655 Day: 3 MJD: 55832.000
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 253| 0 0 0 23 -14 -6 -.33 8 7 | -626 239 23 89
| 28 15 |
emr 97| 4 0 2 -62 -20 19 .41 22 22 | 2447 -814 21 148
| 25 -2 |
esa 137| 0 0 0 -95 68 -20 .18 8 7 | 2306 -2411 16 175
| 68 30 |
gfz 193| -1 1 1 68 24 1 -.21 12 11 | -297 458 25 95
| 13 92 |
grg 127| 2 1 4 33 -59 -10 .55 15 15 | 191 -182 54 202
| -13 52 |
igr n/a| 0 0 -1 -7 -18 -67 -.15 5 5 | 7035 -1061 20 77
| -29 45 |
jpl 127| 3 0 0 110 -198 142 .57 16 16 | 1355 -716 19 95
| -50 93 |
mit 260| -1 -3 -2 34 0 -47 -.36 17 14 | -675 720 22 170
| -10 -25 |
ngs 219| -1 -1 -1 50 -18 -28 -.30 13 8 | -437 124 1638 3594
| -63 52 |
sio 251| 2 1 -3 -186 203 -23 .12 20 20 | --- --- --- ---
| 42 -101 |
Table 2.1655.4 GPS week: 1655 Day: 4 MJD: 55833.000
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 253| 0 0 0 24 0 21 -.35 16 8 | -1271 1227 19 79
| 5 -4 |
emr 97| 2 2 -2 -79 -73 0 .47 20 20 | 718 844 17 133
| 5 48 |
esa 137| 0 0 1 -110 62 -37 .18 9 9 | -445 -1136 21 214
| 66 33 |
gfz 193| 0 1 2 93 -7 20 -.25 12 10 | -460 537 25 99
| -29 92 |
grg 127| 2 0 5 7 -9 0 .54 17 13 | -967 908 51 211
| 6 -15 |
igr n/a| 0 0 0 -37 3 -23 -.16 6 5 | 5068 338 23 79
| -40 6 |
jpl 127| 1 -1 -1 118 -165 148 .55 17 17 | -206 691 19 99
| -93 108 |
mit 260| 0 -3 -4 9 4 -52 -.40 15 13 | -683 106 23 202
| -20 -29 |
ngs 219| -1 0 -2 42 -22 -57 -.31 12 8 | -1086 780 1904 3697
| 10 23 |
sio 251| 2 1 -4 -215 236 -24 .06 20 19 | --- --- --- ---
| 40 -125 |
Table 2.1655.5 GPS week: 1655 Day: 5 MJD: 55834.000
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 253| 0 0 1 27 12 18 -.33 8 7 | -882 138 19 73
| 28 -13 |
emr 97| 4 3 2 -41 -54 3 .47 21 21 | 1117 1014 18 128
| 5 45 |
esa 137| 0 0 0 -91 58 -37 .20 8 8 | -1776 1669 20 184
| 49 38 |
gfz 193| -2 2 1 8 -32 11 -.19 11 10 | -296 1824 26 103
| 15 62 |
grg 127| 3 -1 3 12 -24 9 .60 15 14 | -386 288 55 208
| -4 -26 |
igr n/a| 0 0 0 -20 11 -26 -.14 5 5 | 4990 398 20 76
| -48 6 |
jpl 127| 1 0 -1 109 -200 53 .59 15 15 | 201 974 19 107
| -36 139 |
mit 260| 0 -3 0 14 12 -50 -.38 15 12 | -786 688 26 228
| -8 -12 |
ngs 219| -1 0 -1 64 0 -5 -.31 11 7 | -1329 964 1355 3437
| -69 39 |
sio 251| 1 0 -4 -219 256 -12 .03 21 18 | --- --- --- ---
| 54 -127 |
Table 2.1655.6 GPS week: 1655 Day: 6 MJD: 55835.000
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 253| 0 0 1 22 5 7 -.33 9 8 | 808 -1622 18 92
| 43 -1 |
emr 97| 3 1 0 -48 -45 20 .46 22 22 | 2458 -947 15 135
| 8 20 |
esa 137| -1 0 0 -91 67 -30 .14 6 6 | 2026 -3150 16 207
| 87 21 |
gfz 193| 0 4 0 78 -56 26 -.24 12 10 | 35 -344 23 109
| -1 44 |
grg 127| 3 0 0 11 -12 -4 .55 15 14 | 586 -1154 62 217
| 18 -61 |
igr n/a| 0 0 -1 -3 10 -27 -.12 5 4 | 5796 -644 20 69
| -65 5 |
jpl 127| 1 -1 0 96 -173 29 .56 15 15 | 1682 -77 20 100
| 0 77 |
mit 260| 0 -3 0 37 -16 0 -.44 15 12 | 1087 -1842 21 195
| -16 23 |
ngs 219| 0 0 -1 59 8 0 -.28 11 9 | 829 -1633 1537 3686
| -52 86 |
sio 251| 1 0 -3 -204 239 -35 .08 20 19 | --- --- --- ---
| 35 -128 |
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 3.1655.0 GPS week: 1655 Day: 0 MJD: 55829.000
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 | 58 --- 57 --- --- 43 --- 46 --- --- 39 | 158 --- 158 --- --- 162 --- 14 --- --- 164
2E | 8 17 9 9 19 4 15 10 11 13 4 | 30 36 35 35 42 31 35 36 32 40 33
3 | 7 12 6 12 17 4 10 10 7 16 3 | 13 22 21 23 28 16 23 23 17 25 18
4E | 16 18 12 10 21 5 19 26 15 10 6 | 77 75 73 77 67 73 71 74 75 71 72
5 | 4 20 7 9 16 5 14 11 9 20 4 | 22 33 29 25 35 25 34 24 26 22 24
6 | 6 14 7 11 14 3 10 11 9 13 3 | 15 20 21 25 27 18 21 26 18 23 19
7E | 8 20 6 8 14 4 15 16 11 16 4 | 19 30 22 25 27 22 26 27 29 19 22
8E | 12 14 10 13 18 6 14 12 13 16 4 | 33 33 34 31 26 33 30 31 30 26 30
9E | 11 17 8 17 17 6 18 14 8 26 5 | 60 64 65 65 66 63 66 61 62 70 62
10 | 8 10 6 6 16 4 9 8 11 14 3 | 32 39 36 36 40 32 39 35 34 33 35
11E | 7 11 7 12 13 5 8 16 9 14 3 | 38 42 44 42 42 41 45 40 43 35 40
12 | 7 22 12 16 16 4 18 25 8 21 5 | 19 26 25 29 20 18 25 28 22 21 20
13 | 6 21 6 11 18 3 13 8 8 18 4 | 17 30 20 23 31 17 27 15 20 16 17
14 | 7 22 10 15 14 6 16 14 8 22 4 | 17 26 20 26 26 15 25 24 14 21 17
15 | 5 28 9 10 13 5 18 13 13 17 4 | 23 32 27 26 29 24 30 22 26 22 22
16 | 8 24 10 14 13 4 20 9 9 25 4 | 15 27 21 29 24 16 25 24 17 20 19
17 | 8 21 10 15 15 4 17 10 11 26 5 | 21 39 25 23 27 23 35 20 23 24 22
18 | 8 27 10 15 13 6 18 12 9 19 4 | 20 34 25 25 27 23 31 25 24 24 21
19 | 7 20 8 12 16 4 14 11 7 23 4 | 21 36 23 17 29 21 33 20 21 26 21
20 | 8 21 7 13 15 3 19 12 8 17 4 | 19 31 24 25 28 21 27 18 24 24 20
21E | 8 20 9 11 12 5 17 11 10 14 4 | 48 48 49 50 55 48 49 53 49 53 49
22 | 8 22 8 13 16 5 19 14 9 18 4 | 16 31 25 24 31 19 32 27 22 25 21
23 | 7 24 9 13 13 4 17 11 7 20 4 | 23 34 28 28 27 24 30 21 27 21 23
X24E | 11 21 16 15 20 7 --- 28 24 15 7 | 62 57 63 55 68 64 --- 66 60 71 66
25 | 9 16 7 11 15 5 15 17 10 19 4 | 36 32 31 38 35 32 37 37 33 27 32
26 | 6 13 6 7 11 5 10 8 6 9 2 | 13 19 20 19 22 14 22 19 16 18 16
X27E | 18 22 17 24 --- 11 18 14 --- --- 8 | 35 39 32 33 --- 34 34 30 --- --- 31
28 | 10 21 12 11 13 6 18 16 8 26 5 | 21 34 32 33 32 26 31 34 26 28 26
29 | 8 24 8 13 15 5 18 12 11 20 4 | 23 36 24 22 26 22 33 25 21 19 22
X30 | 8 17 5 12 15 6 --- 12 8 15 4 | 10 16 14 19 12 10 --- 21 14 17 12
31E | 8 21 6 11 14 3 17 15 15 13 4 | 11 22 15 14 23 12 22 15 16 15 13
32 | 10 17 5 12 14 4 14 13 8 18 4 | 18 21 21 17 21 17 23 23 17 32 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 8 12 15 5 16 14 10 18 |T 30 34 34 30 33 31 33 29 28 29 32
WRMS | 8 20 8 11 15 5 16 11 8 18 |NE 19 29 24 25 27 20 29 24 22 23 21
MEDI | 8 20 8 12 15 5 17 12 9 17 |MD 21 33 25 26 28 23 31 25 24 24 22
Table 3.1655.1 GPS week: 1655 Day: 1 MJD: 55830.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 5 --- 222 --- --- 231 --- --- --- --- 0 | 126 --- 115 --- --- 116 --- --- --- --- 127
2E | 8 18 12 9 17 5 16 27 11 15 5 | 20 29 30 26 32 23 26 23 21 29 23
3 | 8 15 8 8 14 4 14 13 11 15 4 | 11 18 17 16 22 13 21 19 15 23 14
4E | 20 21 15 13 14 6 20 23 20 16 6 | 75 72 71 73 69 75 70 81 75 65 72
5 | 10 23 8 12 15 5 16 11 9 20 4 | 20 41 28 27 38 24 35 27 24 26 26
6 | 8 14 8 12 13 5 13 13 14 12 4 | 11 17 16 19 21 12 18 22 17 19 14
7E | 9 24 6 8 14 5 13 16 9 13 4 | 18 29 18 18 21 18 21 24 27 23 18
8E | 15 16 11 12 14 6 16 17 17 19 5 | 29 31 30 31 26 29 28 35 38 28 27
9E | 14 19 13 12 12 7 20 15 11 24 5 | 44 53 51 46 52 47 57 50 51 54 48
10 | 8 13 6 6 12 5 10 11 9 14 3 | 29 32 29 28 28 27 32 27 28 25 27
11E | 10 11 11 10 16 4 10 20 13 11 4 | 19 25 22 23 26 20 26 24 30 22 20
12 | 10 23 10 13 13 5 18 21 10 24 5 | 14 33 20 21 18 16 26 24 22 19 17
13 | 5 21 6 10 18 4 14 10 13 18 4 | 17 31 17 18 29 18 25 20 22 18 17
14 | 7 22 12 14 13 7 17 13 10 20 4 | 14 26 20 21 24 12 24 18 19 19 15
15 | 11 24 8 8 12 5 19 12 14 16 4 | 19 32 20 21 26 19 29 20 19 21 19
16 | 12 24 10 13 13 4 18 10 11 24 5 | 16 29 18 24 23 16 23 24 18 23 17
17 | 11 20 12 16 15 4 13 9 9 28 5 | 15 28 20 22 24 16 26 19 18 20 17
18 | 7 22 11 13 13 6 16 15 8 19 4 | 21 33 22 23 31 23 31 28 28 30 23
19 | 7 21 7 8 14 4 16 11 10 20 4 | 14 32 17 15 26 16 28 16 20 20 16
20 | 10 22 9 9 14 6 16 13 9 16 4 | 20 34 26 23 31 22 31 25 29 27 24
21E | 8 14 12 9 30 6 24 17 9 10 5 | 57 58 57 61 71 56 60 62 56 55 58
22 | 5 21 8 10 13 5 17 14 7 18 4 | 18 34 23 19 34 21 32 24 25 26 22
23 | 10 24 9 10 14 5 17 12 11 19 4 | 24 36 26 26 30 27 30 27 28 28 25
X24E | 13 20 17 12 25 6 --- 33 24 16 7 | 51 49 48 47 62 52 --- 56 44 52 53
25 | 10 20 8 8 9 6 12 15 10 19 4 | 24 25 20 22 26 19 30 25 21 22 20
26 | 9 14 8 6 13 5 12 9 10 11 3 | 15 23 23 20 22 19 25 23 26 23 19
X27E | 15 --- 32 24 --- 25 29 17 --- --- 12 | 40 --- 42 35 --- 27 36 37 --- --- 34
28 | 11 24 10 12 13 5 16 15 7 27 5 | 17 35 22 29 28 22 30 30 25 30 23
29 | 14 22 9 13 12 6 18 12 9 19 5 | 17 27 19 17 22 15 26 20 19 17 15
X30 | 11 16 7 10 10 7 --- 13 7 15 4 | 12 16 13 17 14 13 --- 20 18 18 12
31E | 6 22 9 11 11 5 16 16 8 11 4 | 13 27 18 17 25 14 24 20 23 21 17
32 | 8 21 9 10 16 6 13 12 7 18 4 | 11 15 11 10 14 8 14 10 9 21 7
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 10 11 15 5 16 15 11 18 |T 26 32 29 26 30 26 30 28 27 27 27
WRMS | 9 20 9 10 14 5 16 13 9 18 |NE 17 28 20 20 25 18 26 22 21 22 18
MEDI | 10 21 9 10 13 5 16 13 10 18 |MD 18 31 22 22 26 19 28 24 23 23 20
Table 3.1655.2 GPS week: 1655 Day: 2 MJD: 55831.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 5 --- 221 --- --- 232 --- --- --- --- 0 | 138 --- 171 --- --- 180 --- --- --- --- 143
2E | 8 20 10 9 14 4 13 23 14 15 4 | 16 25 26 20 23 18 23 22 23 19 18
3 | 8 15 7 10 8 6 12 17 11 18 4 | 13 17 20 16 23 15 22 22 16 24 15
4E | 15 21 30 11 20 10 20 13 19 22 7 | 56 57 54 54 51 59 57 60 60 46 54
5 | 5 19 9 9 15 4 16 12 16 21 4 | 18 33 27 23 35 20 32 22 22 20 22
6 | 6 17 9 9 9 4 12 17 11 17 4 | 16 17 21 17 23 16 22 25 17 23 17
7E | 7 24 6 9 14 5 16 18 8 13 4 | 16 23 16 17 21 15 18 20 17 19 14
8E | 15 16 14 11 19 7 18 22 19 26 6 | 36 36 37 36 35 36 36 42 38 33 34
9E | 12 16 12 12 16 8 19 18 11 22 5 | 27 31 32 27 38 28 37 32 31 41 28
10 | 8 10 5 6 17 6 9 13 9 15 3 | 21 22 23 22 26 21 24 20 18 17 20
11E | 6 17 6 8 16 3 10 16 10 17 4 | 31 38 34 31 34 31 38 32 35 32 32
12 | 10 19 9 13 14 7 16 17 8 22 4 | 13 24 21 20 21 15 23 22 16 17 15
13 | 7 21 7 12 19 3 16 11 5 18 4 | 12 26 17 17 29 13 24 15 13 16 13
14 | 7 18 10 13 13 5 15 10 10 21 4 | 16 26 22 23 23 16 24 20 19 19 17
15 | 7 24 7 10 12 5 15 10 9 15 4 | 15 29 18 18 24 15 27 18 17 18 16
16 | 8 23 9 12 14 3 21 13 10 26 5 | 18 27 20 21 26 16 27 21 14 19 17
17 | 7 21 9 14 15 4 15 8 9 27 4 | 20 33 24 21 25 19 31 20 20 24 21
18 | 7 22 7 11 13 5 15 17 7 19 4 | 15 31 20 19 27 16 28 23 18 24 18
19 | 7 24 7 11 15 5 15 11 11 21 4 | 17 35 18 12 30 16 31 13 17 19 17
20 | 10 24 7 12 18 4 17 14 9 21 4 | 21 33 21 21 30 18 29 19 24 24 21
21E | 9 25 10 8 23 7 13 32 11 15 5 | 48 55 54 52 59 49 50 56 49 49 50
22 | 7 20 7 10 12 3 16 13 9 22 4 | 16 32 23 19 33 18 30 21 19 22 20
23 | 7 27 9 11 13 4 16 12 7 19 4 | 19 33 21 18 25 19 28 19 19 21 18
X24E | 10 21 9 11 18 8 --- 26 23 19 6 | 48 50 48 44 54 48 --- 58 47 50 50
25 | 9 16 7 8 12 4 14 19 13 21 4 | 19 22 17 24 27 17 29 28 21 19 19
26 | 7 11 7 8 15 5 10 9 8 13 3 | 14 19 19 16 22 16 21 20 17 19 15
X27E | 21 31 16 14 --- 18 19 17 --- --- 8 | 37 53 49 37 --- 41 34 50 --- --- 41
28 | 9 22 7 9 16 5 15 14 9 28 4 | 21 32 24 26 29 21 28 30 25 24 23
29 | 8 23 7 14 13 5 18 18 11 22 5 | 17 31 21 15 20 16 30 22 16 20 16
X30 | 9 15 6 13 10 3 --- 13 11 16 4 | 13 15 15 18 14 10 --- 17 11 17 11
31E | 9 21 5 11 10 6 14 13 15 14 4 | 14 22 14 12 21 10 20 17 12 23 12
32 | 11 18 4 11 18 6 14 13 8 22 4 | 17 17 15 15 16 14 19 17 14 27 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 10 11 15 5 15 16 11 20 |T 25 30 30 23 28 26 29 26 22 24 26
WRMS | 8 20 8 10 15 5 15 14 8 20 |NE 16 26 20 19 25 16 26 20 17 20 17
MEDI | 8 21 7 11 14 5 15 14 10 19 |MD 17 31 21 20 26 17 28 22 18 21 18
Table 3.1655.3 GPS week: 1655 Day: 3 MJD: 55832.000
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 | 25 --- 25 --- --- 39 --- --- --- --- 25 | 78 --- 78 --- --- 78 --- --- --- --- 78
2E | 7 21 7 11 16 3 14 13 11 10 4 | 19 27 27 26 28 21 27 24 27 25 23
3 | 7 16 6 10 11 5 14 19 11 18 4 | 18 25 25 22 26 18 27 30 18 29 22
4E | 16 20 9 12 20 4 19 19 15 22 5 | 68 63 62 64 58 64 55 64 65 55 61
5 | 7 23 9 8 15 6 18 13 9 21 4 | 20 38 30 25 40 26 36 29 30 26 27
6 | 7 16 6 7 10 5 13 17 10 16 3 | 17 23 24 22 25 18 25 29 18 26 21
7E | 6 22 5 8 14 5 14 17 12 15 4 | 21 27 21 22 30 21 26 27 29 27 23
8E | 16 20 23 12 21 13 20 37 42 30 9 | 55 62 71 63 64 56 59 60 67 48 58
9E | 11 24 9 12 13 6 25 24 12 31 6 | 33 40 33 28 35 29 45 44 30 43 33
10 | 6 12 5 8 18 3 10 13 9 12 3 | 26 28 25 23 28 24 27 27 27 27 26
11E | 12 15 7 8 15 6 11 15 14 18 4 | 29 38 37 33 37 35 42 35 40 34 34
12 | 7 22 10 22 14 5 16 15 15 22 5 | 21 32 27 37 25 23 33 28 30 28 26
13 | 6 23 5 11 21 4 13 11 7 17 4 | 18 30 19 19 30 15 27 21 17 17 17
14 | 5 25 7 14 14 5 17 11 11 22 4 | 18 32 23 27 26 19 29 24 19 24 21
15 | 5 23 8 9 13 3 17 8 8 16 4 | 21 33 26 26 30 21 33 25 25 25 24
16 | 6 24 7 14 13 4 18 20 11 23 5 | 23 35 24 27 25 22 31 34 20 27 24
17 | 8 24 9 19 15 3 14 8 13 27 5 | 15 31 17 21 24 15 26 14 20 17 16
18 | 6 26 6 15 13 5 16 12 9 18 4 | 22 37 27 25 30 23 33 30 24 27 24
19 | 7 26 6 13 17 5 16 11 8 19 4 | 21 36 21 17 26 21 35 19 22 21 21
20 | 8 25 6 12 17 4 14 14 8 20 4 | 25 34 25 21 29 21 32 23 23 28 24
21E | 7 25 11 9 15 4 12 26 5 12 4 | 45 49 49 45 55 44 43 50 44 45 45
22 | 5 22 7 14 13 5 17 13 9 20 4 | 18 33 23 24 32 18 32 24 20 22 21
23 | 7 27 7 13 16 4 18 14 7 20 4 | 23 35 23 25 29 21 33 27 22 28 23
X24E | 8 21 11 9 18 8 --- 30 17 22 6 | 56 57 52 51 62 57 --- 55 52 64 57
25 | 9 14 5 11 13 5 18 16 14 20 4 | 29 31 27 28 32 26 39 35 28 29 28
26 | 7 11 4 7 15 4 11 11 8 14 3 | 20 25 21 22 27 19 28 26 25 26 22
X27E | 25 22 11 26 --- 16 23 18 --- --- 9 | 62 55 51 51 --- 58 38 68 --- --- 57
28 | 8 21 8 11 15 5 17 14 11 26 4 | 21 30 22 27 29 22 29 27 27 26 23
29 | 7 23 8 14 13 4 18 15 12 27 4 | 19 33 24 20 22 17 30 24 18 22 20
X30 | 9 17 4 9 15 5 --- 15 9 16 4 | 20 26 17 23 17 17 --- 27 21 27 20
31E | 6 21 4 11 12 4 17 18 9 15 4 | 14 29 17 17 23 14 24 24 15 23 17
32 | 7 20 8 11 16 4 14 14 8 23 4 | 21 24 26 19 22 21 26 24 20 35 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 22 8 12 15 5 16 17 13 20 |T 28 35 31 29 32 28 33 32 28 30 29
WRMS | 7 22 7 11 15 5 16 14 8 20 |NE 20 31 23 23 27 20 30 26 22 25 22
MEDI | 7 22 7 11 15 5 16 15 10 20 |MD 21 33 25 25 29 21 32 27 24 27 23
Table 3.1655.4 GPS week: 1655 Day: 4 MJD: 55833.000
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 | 9 --- 13 --- --- 33 --- 10 --- --- 8 | 63 --- 62 --- --- 69 --- 14 --- --- 63
2E | 9 24 9 11 13 3 9 11 12 13 4 | 12 24 20 18 21 14 19 16 19 20 15
3 | 8 14 6 11 12 5 9 19 15 22 4 | 16 24 21 20 22 15 24 28 18 28 19
4E | 15 21 13 13 16 6 17 15 14 27 5 | 46 42 44 45 38 44 44 45 47 52 43
5 | 8 22 8 12 17 5 19 11 10 20 4 | 20 35 26 21 34 21 35 21 24 20 22
6 | 7 14 6 10 11 4 7 16 13 17 4 | 18 25 21 23 23 17 22 30 20 25 21
7E | 6 18 6 9 17 4 15 15 12 11 4 | 24 31 22 22 32 23 27 26 29 27 24
8E | 69 25 14 23 19 13 22 35 33 21 12 | 80 29 39 39 31 46 31 42 48 29 76
9E | 15 20 13 12 15 5 21 29 12 29 6 | 48 50 49 46 48 49 52 65 50 53 48
10 | 6 13 8 10 11 5 11 12 7 12 3 | 16 21 17 19 21 15 21 17 15 16 16
11 | 20 17 9 9 18 6 10 13 10 23 5 | 52 64 56 55 56 56 60 54 54 54 54
12 | 7 22 11 14 14 8 19 12 13 20 5 | 20 28 22 24 21 19 28 25 20 23 20
13 | 7 21 7 12 17 6 14 12 10 17 4 | 18 32 19 21 34 18 29 19 20 17 19
14 | 8 20 10 14 12 5 19 15 9 21 4 | 14 29 23 26 25 17 31 22 17 19 18
15 | 5 21 8 10 11 6 18 10 12 16 4 | 17 26 22 25 26 19 26 22 21 21 19
16 | 9 20 10 15 12 5 17 14 11 24 5 | 18 27 19 27 21 16 24 23 17 20 18
17 | 7 18 13 13 13 4 15 8 7 26 4 | 13 24 19 17 22 14 26 16 16 16 15
18 | 6 26 10 12 14 4 36 14 13 18 6 | 20 37 26 21 28 21 43 25 24 25 22
19 | 8 23 8 9 16 6 14 12 10 21 4 | 15 34 18 13 27 15 28 16 15 18 16
20 | 9 22 8 12 14 4 12 12 11 21 4 | 19 33 22 19 28 19 26 22 22 25 20
21E | 8 18 10 9 52 6 11 18 11 16 6 | 24 30 25 28 62 26 27 31 24 31 27
22 | 5 24 9 12 13 4 19 13 8 20 4 | 18 36 26 20 32 19 36 22 22 21 22
23 | 8 24 8 11 13 6 18 13 10 20 4 | 18 33 18 22 27 17 27 21 21 21 18
X24E | 11 24 11 11 22 8 --- 21 16 21 6 | 54 58 52 50 54 53 --- 56 49 58 54
25 | 6 16 9 10 12 4 16 12 13 19 4 | 24 27 24 21 29 21 35 30 25 22 23
26 | 6 12 6 7 10 6 11 9 13 13 3 | 18 18 20 19 24 17 20 20 17 21 17
X27E | 18 23 15 16 --- 27 --- 20 --- --- 9 | 39 42 37 34 --- 34 --- 34 --- --- 34
28 | 9 18 9 13 14 6 15 14 8 25 4 | 15 27 21 25 25 18 26 23 18 21 18
29 | 8 22 9 15 13 5 17 11 11 23 4 | 13 26 18 19 17 14 25 22 15 15 16
X30 | 7 12 8 9 11 6 --- 12 10 20 4 | 14 16 16 15 15 11 --- 17 18 18 14
31E | 7 20 8 10 12 4 12 12 11 17 4 | 15 23 18 16 23 14 23 19 17 17 16
32 | 9 17 8 9 14 6 15 14 7 24 4 | 15 17 12 13 18 14 20 17 14 28 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 20 9 12 17 6 17 15 12 20 |T 25 31 26 25 29 24 29 26 24 26 26
WRMS | 8 20 9 10 13 5 17 13 8 19 |NE 17 27 20 20 24 17 27 21 19 20 18
MEDI | 8 20 9 11 13 5 15 13 11 20 |MD 18 29 22 21 26 18 27 22 20 21 19
Table 3.1655.5 GPS week: 1655 Day: 5 MJD: 55834.000
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 --- 14 --- --- 15 --- 14 --- --- 9 | 51 --- 43 --- --- 50 --- 12 --- --- 48
2E | 9 23 7 8 19 3 12 15 12 17 4 | 14 26 19 17 22 14 21 19 21 19 16
3 | 8 14 4 6 15 5 10 18 11 20 4 | 15 20 21 15 25 13 24 24 15 26 17
4E | 16 35 10 14 26 7 17 10 16 50 7 | 73 73 67 69 61 69 61 64 68 73 65
5 | 5 24 8 11 18 7 16 11 8 21 4 | 23 40 28 25 40 24 41 24 26 24 27
6 | 7 15 6 6 13 5 9 15 13 17 3 | 17 19 22 18 24 13 23 24 17 22 18
7E | 9 19 7 12 18 5 17 15 12 8 4 | 26 31 24 27 35 20 29 23 19 21 23
X8E | 5 --- --- --- --- 5125 --- --- --- --- 0 | 50 --- --- --- --- 183 --- --- --- --- 68
9E | 14 23 13 14 12 6 22 36 13 20 6 | 52 55 57 54 56 54 61 55 55 56 53
10 | 8 11 7 7 12 6 13 10 6 11 3 | 16 18 20 17 19 14 17 18 17 16 16
11 | 6 19 8 13 21 6 11 13 12 13 4 | 35 39 39 38 42 34 42 37 40 35 36
12 | 7 24 11 12 12 3 16 14 16 20 4 | 16 26 23 21 21 18 26 22 19 21 17
13 | 9 23 8 12 20 7 15 11 9 17 4 | 15 33 19 22 30 13 26 14 18 13 16
14 | 5 21 8 13 13 5 14 20 10 20 4 | 15 28 19 17 23 14 26 27 16 19 16
15 | 5 19 10 8 13 6 17 12 11 14 4 | 16 30 23 22 28 18 29 21 23 20 20
16 | 7 23 11 11 14 4 16 14 10 25 4 | 15 28 24 20 21 12 25 19 13 11 16
17 | 5 23 9 13 14 4 16 9 11 24 4 | 12 31 18 15 22 13 28 12 17 14 14
18 | 6 22 9 11 12 3 17 12 8 17 4 | 16 31 24 19 29 18 34 21 16 21 19
19 | 5 24 6 10 15 6 15 13 8 20 4 | 15 34 18 14 28 14 30 15 15 18 16
20 | 7 24 6 12 16 5 15 13 12 17 4 | 18 32 20 20 28 18 28 16 21 21 19
21E | 7 18 12 10 15 3 12 18 10 15 4 | 33 33 31 36 23 30 30 37 34 32 30
22 | 4 21 9 10 13 3 16 14 7 23 4 | 15 33 23 18 33 17 31 20 19 20 18
23 | 9 27 8 16 15 6 19 11 6 17 4 | 21 35 24 24 26 19 31 19 22 19 21
X24E | 5 --- --- --- 884 708 --- 805 --- 797 0 | 41 --- --- --- 37 40 --- 40 --- 46 42
25 | 8 14 7 8 12 4 15 13 10 17 4 | 20 27 23 21 29 22 35 26 22 21 21
26 | 6 11 6 8 13 3 11 8 7 10 3 | 13 17 18 17 21 13 18 15 18 15 15
X27E | 11 21 13 12 --- 24 --- 14 --- --- 6 | 36 36 39 33 --- 41 --- 42 --- --- 35
28 | 8 21 8 12 15 4 17 13 8 28 4 | 15 28 19 20 26 15 26 18 15 18 16
29 | 5 22 8 10 10 6 17 11 9 19 4 | 16 27 20 18 20 15 28 21 14 15 16
X30 | 6 13 6 14 13 4 --- 12 6 15 3 | 11 14 13 17 11 9 --- 14 11 15 10
31E | 6 19 8 12 12 4 12 21 13 26 4 | 17 21 15 13 20 13 24 25 18 25 15
32 | 7 21 7 12 15 5 14 17 10 20 4 | 13 18 15 13 17 11 18 15 11 24 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 21 8 11 15 5 15 15 11 21 |T 23 30 25 23 28 27 30 24 22 24 24
WRMS | 7 21 8 10 14 5 15 12 7 18 |NE 15 27 20 18 24 15 27 19 17 18 17
MEDI | 7 21 8 12 14 5 15 13 10 19 |MD 16 30 22 20 26 17 28 21 18 21 18
Table 3.1655.6 GPS week: 1655 Day: 6 MJD: 55835.000
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 | 14 --- 12 --- --- 8 --- 9 --- --- 8 | 75 --- 71 --- --- 69 --- 11 --- --- 75
2E | 7 25 6 11 20 3 12 15 16 20 4 | 15 23 21 21 21 17 24 19 23 22 17
3 | 8 14 4 10 18 5 7 13 10 23 3 | 18 23 24 23 31 18 28 26 16 33 22
4E | 19 21 6 14 16 5 19 16 16 21 5 | 75 66 70 69 62 69 61 80 73 61 68
5 | 8 24 6 10 14 5 19 12 14 22 4 | 24 41 28 27 41 26 41 24 26 25 27
6 | 7 15 3 10 17 5 7 9 11 19 3 | 21 23 26 25 34 20 28 28 20 29 24
7E | 8 22 7 8 17 6 15 14 11 17 4 | 37 47 39 35 43 38 39 44 43 42 38
X8E | 66 41 16 --- 32 28 --- 62 --- --- 23 | 67 25 21 --- 14 139 --- 27 --- --- 94
9E | 13 20 14 11 12 9 19 47 16 19 7 | 67 67 65 60 68 65 70 80 67 66 66
10 | 6 13 7 7 14 2 11 8 13 9 3 | 17 23 18 20 23 15 20 19 19 15 16
11 | 5 17 7 8 23 4 9 13 10 15 4 | 25 29 30 28 32 27 29 30 30 26 26
12 | 6 26 5 10 13 7 16 14 11 20 4 | 19 26 21 22 26 20 24 22 23 21 18
13 | 8 26 5 11 21 4 17 8 8 18 4 | 19 31 21 26 34 20 28 18 18 18 19
14 | 7 20 6 15 12 4 13 17 9 21 4 | 16 24 23 28 25 19 25 28 22 23 19
15 | 6 25 7 12 12 6 18 13 11 16 4 | 20 27 24 29 31 21 27 17 22 21 21
16 | 7 23 5 14 16 5 14 14 11 26 4 | 16 29 21 28 25 15 26 21 17 16 18
17 | 8 23 6 16 14 3 16 9 11 25 4 | 12 29 16 20 23 14 27 13 13 16 14
18 | 5 24 8 16 14 5 18 13 9 16 4 | 19 37 25 21 30 22 35 25 23 27 21
19 | 8 24 4 12 14 2 13 15 10 21 4 | 17 34 18 12 26 14 31 15 15 22 16
20 | 8 26 6 12 15 3 14 13 13 15 4 | 19 32 23 20 30 20 29 18 22 23 20
21E | 7 17 6 8 12 4 13 11 10 10 3 | 34 33 33 36 32 33 33 39 35 35 33
22 | 6 24 8 13 14 4 15 14 7 26 4 | 18 36 26 20 32 19 33 22 21 22 21
23 | 9 29 7 13 16 4 18 11 7 17 4 | 21 35 24 26 31 21 30 21 22 23 22
25 | 9 18 4 10 13 4 15 11 10 18 3 | 25 25 26 26 35 24 36 29 28 22 25
26 | 6 18 5 8 8 4 12 8 9 16 3 | 20 21 24 23 26 17 22 19 18 18 20
X27E | 17 30 13 16 --- 30 --- 19 --- --- 8 | 42 47 38 51 --- 42 --- 50 --- --- 41
28 | 9 19 5 11 16 5 16 12 10 29 4 | 20 28 24 29 32 22 29 25 23 24 23
29 | 9 25 5 9 9 4 18 14 10 18 4 | 11 28 15 11 19 11 27 16 12 14 11
X30 | 7 17 3 9 12 3 --- 11 6 14 3 | 10 15 13 15 14 9 --- 16 14 18 10
31E | 8 18 6 10 13 5 14 13 10 21 4 | 26 33 30 27 32 29 33 33 32 29 28
32 | 12 19 7 11 15 5 14 14 10 20 4 | 15 18 19 16 23 16 22 19 12 29 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 22 6 12 15 5 15 15 11 20 |T 27 31 28 27 30 29 31 27 25 26 28
WRMS | 8 22 6 10 14 4 15 12 9 19 |NE 17 27 21 22 28 18 28 21 19 21 19
MEDI | 8 22 6 11 14 5 15 13 10 19 |MD 20 29 24 26 31 20 29 22 22 23 21
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1655 GPS week: 1655 MJD: 55829.0-55835.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3027 |U 10 8 26 |U 8 11 30 |U 30 17 44 |
emr | emr 2903 |U 14 10 30 |U 16 14 42 | 32 18 47 |
esa | esa 3030 | 11 8 26 |U 7 10 29 | 31 18 37 |
gfz | gfz 2893 |U 15 11 33 |U 21 23 59 |U 35 23 49 |
grg | grg 2846 | 11 9 28 |U 9 15 42 | 31 17 40 |
igr | igr 2988 | 11 8 26 | 7 10 29 | 30 17 40 |
igs | igs 2951 | 11 8 27 | 8 11 31 | 31 16 46 |
jpl | jpl 2699 |U 19 19 50 |U 18 16 61 | 34 26 55 |
mit | mit 3003 |U 18 28 35 |U 20 18 66 |U 31 17 53 |
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 5.1655.0 GPS week: 1655 Day: 0 MJD: 55829.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3061 | 11 7 24 | 5 7 35 | 7 12 20 |
emr | emr 2955 | 13 8 26 | 9 11 34 | 11 10 19 |
esa | esa 3072 | 13 8 27 | 7 9 28 | 9 12 23 |
gfz | gfz 2950 | 14 9 32 | 16 28 50 | 12 24 31 |
grg | grg 2880 | 13 10 28 | 7 11 37 | 7 6 21 |
igr | igr 2958 | 12 10 27 | 6 10 27 | 9 11 23 |
igs | igs 2919 | 13 9 30 | 7 10 32 | 12 9 33 |
jpl | jpl 2765 | 18 10 40 | 8 13 41 | 12 7 23 |
mit | mit 3072 | 13 9 32 | 19 17 63 | 9 10 25 |
Table 5.1655.1 GPS week: 1655 Day: 1 MJD: 55830.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 | 12 8 29 | 7 15 26 | 105 32 85 |
emr | emr 2864 | 13 11 28 | 11 15 43 | 102 31 91 |
esa | esa 3072 | 11 9 29 | 5 13 33 | 106 33 57 |
gfz | gfz 2940 | 15 8 34 | 18 24 52 | 105 31 94 |
grg | grg 2880 | 12 8 29 | 6 15 32 | 106 34 65 |
igr | igr 3024 | 12 8 30 | 6 13 31 | 106 33 73 |
igs | igs 3054 | 11 9 31 | 11 16 41 | 106 33 86 |
jpl | jpl 2764 | 25 32 78 | 16 23 57 | 107 36 88 |
mit | mit 2976 | 12 8 24 | 12 19 53 | 111 37 125 |
Table 5.1655.2 GPS week: 1655 Day: 2 MJD: 55831.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 | 10 7 20 | 8 12 24 | 17 30 27 |
emr | emr 2956 | 14 8 25 | 25 12 48 | 18 24 26 |
esa | esa 3072 | 11 6 21 | 6 8 24 | 17 31 32 |
gfz | gfz 2942 | 13 9 29 | 18 19 54 | 19 27 32 |
grg | grg 2880 | 11 7 25 | 8 13 84 | 17 25 30 |
igr | igr 2968 | 9 7 23 | 7 9 25 | 17 31 27 |
igs | igs 2977 | 12 7 27 | 6 10 23 | 18 27 27 |
jpl | jpl 2760 | 18 17 40 | 19 13 43 | 14 37 26 |
mit | mit 2976 | 12 9 23 | 30 19 90 | 16 24 27 |
Table 5.1655.3 GPS week: 1655 Day: 3 MJD: 55832.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3056 | 9 8 26 | 9 9 32 | 10 13 23 |
emr | emr 2954 | 11 8 25 | 14 14 32 | 10 12 33 |
esa | esa 3072 | 10 9 29 | 8 7 28 | 10 13 26 |
gfz | gfz 2942 | 12 10 27 | 21 16 73 | 13 12 26 |
grg | grg 2879 | 10 8 23 | 8 9 29 | 12 15 26 |
igr | igr 3038 | 10 7 26 | 7 8 31 | 8 10 21 |
igs | igs 2892 | 10 7 21 | 9 8 29 | 9 12 25 |
jpl | jpl 2764 | 26 38 75 | 13 12 36 | 16 24 49 |
mit | mit 2976 | 34 67 39 | 17 23 76 | 9 10 29 |
Table 5.1655.4 GPS week: 1655 Day: 4 MJD: 55833.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 11 8 29 | 7 9 19 | 54 10 110 |
emr | emr 2956 | 17 8 30 | 13 13 30 | 57 10 113 |
esa | esa 3072 | 12 7 31 | 6 7 21 | 52 14 82 |
gfz | gfz 2945 | 14 12 32 | 27 23 47 | 64 35 107 |
grg | grg 2880 | 12 8 32 | 8 9 28 | 54 11 82 |
igr | igr 3052 | 12 8 29 | 7 7 22 | 53 9 101 |
igs | igs 3036 | 14 10 36 | 6 8 20 | 54 10 106 |
jpl | jpl 2676 | 14 11 27 | 17 20 39 | 63 42 128 |
mit | mit 3072 | 19 71 58 | 17 16 45 | 54 15 114 |
Table 5.1655.5 GPS week: 1655 Day: 5 MJD: 55834.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2939 | 9 7 26 | 10 16 37 | 8 17 25 |
emr | emr 2772 | 16 17 47 | 22 16 57 | 13 30 29 |
esa | esa 2880 | 8 7 22 | 11 19 37 | 10 13 25 |
gfz | gfz 2765 | 18 13 28 | 24 27 64 | 21 28 30 |
grg | grg 2745 | 9 8 24 | 9 16 35 | 12 20 33 |
igr | igr 2918 | 9 7 23 | 10 16 35 | 9 17 23 |
igs | igs 2829 | 8 8 22 | 10 16 34 | 9 13 27 |
jpl | jpl 2584 | 14 16 45 | 29 19 102 | 15 22 47 |
mit | mit 2976 | 12 13 36 | 27 19 69 | 11 13 29 |
Table 5.1655.6 GPS week: 1655 Day: 6 MJD: 55835.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2967 | 11 9 25 | 7 7 39 | 10 9 18 |
emr | emr 2864 | 14 9 30 | 18 17 50 | 11 11 19 |
esa | esa 2976 | 11 10 24 | 7 7 36 | 10 9 17 |
gfz | gfz 2773 | 19 13 48 | 21 22 73 | 11 6 26 |
grg | grg 2783 | 13 15 33 | 15 29 52 | 10 8 21 |
igr | igr 2963 | 11 12 25 | 8 7 35 | 8 5 15 |
igs | igs 2952 | 12 9 26 | 7 7 37 | 10 9 17 |
jpl | jpl 2584 | 15 12 44 | 22 15 106 | 13 14 27 |
mit | mit 2976 | 23 22 34 | 16 11 65 | 10 9 19 |
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 6.1655 GPS week: 1655 MJD: 55829.500-55835.500
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 | 21 -24 -7 25 -6 | 10 19
| 14 25 95 67 6 | 3
emr uuuuu | 1 6 -88 -124 12 | 58 60
| 21 16 49 96 4 | 6
esa uuuuu | 6 -67 93 106 -3 | 17 24
| 12 10 85 93 4 | 2
gfz uuuuu | -41 -2 11 17 -5 | 15 24
| 21 21 48 78 7 | 2
grg uuuux | 33 10 -96 -56 -5 | 0 25
| 32 19 43 88 17 | 5
igr xxxxx | 6 26 0 3 -12 | 1 14
| 18 37 35 43 7 | 4
irf xxxxx | 22 0 20 0 0 | 5 16
| 9 10 35 21 2 | 2
jpl uuuuu | -81 35 8 -139 -9 | 62 64
| 21 31 57 87 17 | 5
mit uuuuu | 33 6 29 43 5 | 22 27
| 22 20 87 35 2 | 2
ngs uuuuu | -10 78 40 95 2 | 12 16
| 29 44 56 52 4 | 1
sio uuuuu | 118 -45 -229 -239 -8 | 66 67
| 41 18 137 89 5 | 2
Table 7.1655.0 GPS week: 1655 Day: 0 MJD: 55829.500
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 -10 87 47 -8 | 13 22
emr uuuuu | 1 14 -60 -20 5 | 52 54
esa uuuuu | 26 -79 134 184 3 | 15 25
gfz uuuuu | -12 -32 11 45 -2 | 15 25
grg uuuux | 19 49 -67 -195 -30 | -3 32
igr xxxxx | -19 -20 -6 -43 -17 | 6 16
irf xxxxx | 16 -10 24 -4 3 | 5 18
jpl uuuuu | -96 14 -45 -182 -27 | 69 71
mit uuuuu | 22 -12 -43 17 4 | 22 30
ngs uuuuu | -17 122 -16 45 0 | 11 17
sio uuuuu | 57 -68 -101 -257 -6 | 67 69
Table 7.1655.1 GPS week: 1655 Day: 1 MJD: 55830.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -1 -77 -146 -47 -11 | 14 22
emr uuuuu | -15 22 -189 -229 12 | 54 57
esa uuuuu | 18 -66 119 255 -4 | 18 26
gfz uuuuu | -39 -8 58 18 1 | 16 26
grg uuuux | 20 -7 -156 -47 15 | -8 32
igr xxxxx | -8 -12 -50 -8 -12 | 6 15
irf xxxxx | 15 -9 -8 -14 1 | 7 19
jpl uuuuu | -100 25 79 -202 -25 | 68 70
mit uuuuu | 38 -16 -67 -2 4 | 23 31
ngs uuuuu | 7 111 129 69 1 | 12 18
sio uuuuu | 81 -63 -275 -246 -8 | 69 70
Table 7.1655.2 GPS week: 1655 Day: 2 MJD: 55831.500
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 -5 114 -69 -11 | 11 20
emr uuuuu | 21 24 -48 -54 14 | 55 57
esa uuuuu | 4 -78 123 70 -6 | 16 25
gfz uuuuu | -62 -1 -15 -2 -7 | 15 24
grg uuuux | 28 7 -143 -16 18 | -3 27
igr xxxxx | 14 7 -30 40 -14 | 4 15
irf xxxxx | 10 -6 18 -23 -1 | 5 17
jpl uuuuu | -71 3 76 -160 -9 | 63 65
mit uuuuu | 15 -12 58 6 2 | 21 27
ngs uuuuu | 29 110 -15 164 5 | 11 16
sio uuuuu | 91 -42 -303 -301 -5 | 67 68
Table 7.1655.3 GPS week: 1655 Day: 3 MJD: 55832.500
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 -22 36 37 -11 | 7 18
emr uuuuu | 36 -19 -84 -1 15 | 54 57
esa uuuuu | 4 -62 5 98 -4 | 14 24
gfz uuuuu | -58 -7 58 -98 5 | 11 22
grg uuuux | -18 19 -30 -111 -9 | 3 22
igr xxxxx | -11 35 57 -57 -21 | -1 15
irf xxxxx | 34 6 -7 40 0 | 2 16
jpl uuuuu | -59 56 37 -216 -21 | 59 62
mit uuuuu | 59 16 52 87 9 | 17 23
ngs uuuuu | -18 69 79 118 -3 | 9 15
sio uuuuu | 135 -36 -342 -70 -12 | 64 66
Table 7.1655.4 GPS week: 1655 Day: 4 MJD: 55833.500
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 | 31 -4 -24 5 -4 | 10 17
emr uuuuu | -21 -4 -71 -197 13 | 61 62
esa uuuuu | -6 -65 234 132 -5 | 19 23
gfz uuuuu | -65 30 -64 -12 -6 | 17 23
grg uuuux | 42 -5 -99 -59 -6 | 4 22
igr xxxxx | 21 41 28 55 -15 | 0 14
irf xxxxx | 27 1 1 3 -3 | 6 13
jpl uuuuu | -81 94 -13 -39 -8 | 60 62
mit uuuuu | 56 21 19 66 8 | 23 26
ngs uuuuu | 4 -9 13 29 3 | 12 15
sio uuuuu | 152 -39 -382 -194 -16 | 67 68
Table 7.1655.5 GPS week: 1655 Day: 5 MJD: 55834.500
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 | 43 -28 -105 85 3 | 9 16
emr uuuuu | -15 -5 -58 -204 16 | 63 65
esa uuuuu | -8 -49 34 -1 0 | 19 23
gfz uuuuu | -32 -15 55 162 -11 | 17 23
grg uuuux | 56 4 -90 -57 0 | 5 22
igr xxxxx | 24 48 3 -4 -1 | -3 13
irf xxxxx | 30 0 19 11 -2 | 6 13
jpl uuuuu | -109 36 -9 -181 14 | 57 59
mit uuuuu | 42 8 -11 60 4 | 23 27
ngs uuuuu | -9 69 78 154 3 | 13 16
sio uuuuu | 157 -54 -201 -255 -11 | 65 66
Table 7.1655.6 GPS week: 1655 Day: 6 MJD: 55835.500
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 -23 -14 116 1 | 9 16
emr uuuuu | 3 12 -107 -166 6 | 66 68
esa uuuuu | 2 -67 -1 5 -9 | 19 24
gfz uuuuu | -21 21 -27 2 -16 | 16 23
grg uuuux | 84 2 -89 93 -21 | 5 22
igr xxxxx | 18 85 -2 36 -4 | -4 13
irf xxxxx | 23 20 93 -11 0 | 7 13
jpl uuuuu | -54 20 -66 7 13 | 56 57
mit uuuuu | 0 36 197 65 5 | 25 28
ngs uuuuu | -63 72 12 86 9 | 13 16
sio uuuuu | 151 -15 0 -350 -1 | 64 65
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