[IGSREPORT-19491] Wk 1622 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Feb 24 04:30:50 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1622 (Feb 06, 2011 - Feb 12, 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:
igs1622[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1622[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1622[0-6].cls IGS GPS clock combination summary report.
igs16227.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16227.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because they either provide broadcast
clocks (NGS) or clock corrections are not provided (SIO). The clock
information not used is still compared to combination for completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | GUAT NRIL
0 | EMR | 3 6 26 3 6 26 WTZR WES2 WTZR YELL
0 | GFZ | 6 19 23 26 29 BRMU MAW1 MDVJ NYAL WSRT YELL
0 | GRG | ADIS NRC1 SANT
0 | JPL | 6 25 YELL
0 | MIT | 3 6 9 19 26 3 6 9 19 26 BRMU DAV1 MAW1 BRMU DAV1
0 | MIT | MAW1 WES2
1 | COD | WROC SANT WROC XMIS
1 | EMR | 3 6 26 3 6 26 WTZR HARB WTZR
1 | ESA | PALM
1 | GFZ | 6 17 19 23 26 29 KIRU PERT SUTM
1 | GRG | AMC2
1 | JPL | 3 25 26 GUAT
1 | MIT | 3 6 26 3 6 26 CAS1 MAW1 CAS1 DAV1 MAW1
2 | COD | 26 MDO1 MDO1
2 | EMR | 3 6 3 6 WTZR WTZR
2 | ESA | 26 UNSA
2 | GFZ | 6 17 19 22 29 32 CHAT HARB KIRU MDVJ
2 | GRG | AMC2 GLSV RAMO SANT
2 | JPL | 3 6 25 32 ADIS
2 | MIT | 3 6 32 3 6 32 CAS1 CAS1 IENG
3 | COD | YELL
3 | EMR | 26 WTZR HARB WTZR
3 | ESA | UNSA
3 | GFZ | 17 19 29 BRMU RABT
3 | GRG | AMC2 BRMU SANT
3 | JPL | 3 6 25 ADIS AREQ BRMU DAV1
3 | MIT | 3 6 26 3 6 26 BRMU DAV1 MAW1 BRMU CEDU DAV1 MAW1
3 | MIT | WES2
4 | EMR | 3 6 26 3 6 26 WTZR WTZR
4 | ESA | UNSA
4 | GFZ | 17 19 26 29 DAV1 RAMO
4 | GRG | ADIS AMC2 LPGS SANT
4 | JPL | 3 6 25 26 ADIS DAV1
4 | MIT | 3 6 26 3 6 26 DAV1 MAW1 BRMU DAV1 MAW1
5 | COD | USNO SCH2 USNO
5 | EMR | 3 6 3 6
5 | ESA | SCH2
5 | GFZ | 17 19 26 29 MAW1 MDVJ SCH2 SOFI
5 | GRG | ADIS AMC2 SANT
5 | JPL | 3 6 25 ADIS
5 | MIT | 3 6 3 6 NTUS NTUS
6 | COD | MCM4 MCM4
6 | EMR | 3 6 3 6 WTZR WTZR
6 | ESA | UNSA
6 | GFZ | 6 19 26 29 MDVJ NYAL
6 | GRG | AMC2 SANT
6 | JPL | 3 6 25 ADIS
6 | MIT | 3 6 21 26 3 6 26 DAV1 MAW1 DAV1 HARB MAW1
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 | MIT | 3
6. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products,
including the IGS combined orbits, are based on the IGS realization of the
ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447.
7. Small rotations were applied to 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 | .2 1.2 1.0 -9 -1 -10 .25
EMR | 1.6 3.3 5.8 37 -29 -12 .30
ESA | 7.8 5.6 -7.3 112 -106 -102 .30
GFZ | -.3 .9 .1 6 4 -33 .34
GRG | 5.0 8.3 -2.7 46 66 -98 .42
JPL | 3.6 4.2 9.0 38 -36 63 .17
MIT | .6 .6 -14.5 4 -8 -28 .28
NGS | 3.5 2.0 -8.0 37 -105 9 .23
SIO | 6.1 .5 2.7 -1 -93 -19 .39
8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by 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.
10. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna
model is introduced (IGSMAIL #5272). The antenna phase center offsets and
phase center variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1622.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1622.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 2.1622.[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 3.1622.[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 5.1622.0-6).
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 1622 summary. (Feb 06, 2011 - Feb 12, 2011)
Table 1.1622.a GPS week: 1622 MJD: 55598.000-55604.000
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 238| 0 0 5 63 -44 7 -.22 10 9 | -28 -570 15 75
| 0 0 1 12 21 23 .02 | 488 796
emr 88| 0 0 8 -35 -28 23 .39 19 19 | -3238 283 15 100
| 2 1 1 21 40 19 .04 | 1108 361
esa 150| 2 0 -1 -95 63 -78 .22 8 8 | 236 -1303 13 117
| 0 0 1 20 19 24 .01 | 1509 1870
gfz 189| 0 -1 -5 56 -56 48 -.14 11 11 | 320 -235 22 108
| 0 0 1 80 97 11 .03 | 223 392
grg 135| 2 0 -9 -55 -184 -33 .65 15 14 | 147 -226 42 212
| 1 1 1 27 33 19 .02 | 275 402
igr n/a| 0 0 0 47 -29 24 -.03 5 5 | 6497 192 18 65
| 0 0 0 22 50 27 .01 | 1082 335
jpl 134| 0 0 12 -42 23 25 .43 20 19 | 1192 10 18 98
| 1 1 0 16 18 38 .03 | 812 443
mit 262| -2 0 -5 64 -72 20 -.33 17 9 | 0 -19 20 141
| 0 0 0 12 31 9 .05 | 319 537
ngs 222| 0 1 -3 -5 152 24 -.23 11 8 | -81818 115361 2300 3679
| 0 0 1 39 60 14 .03 | 216646 307323
sio 260| -1 0 10 53 107 6 -.23 18 17 | --- --- --- ---
| 1 1 0 20 36 13 .02 | --- ---
Table 1.1622.b GPS week : 1622 MJD: 55598.000-55604.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 0 0 0 0 0 0 0 |
2 | 5 5 5 5 5 5 5 |
3 | 11 8 12 11 11 9 9 |
4 | 4 3 4 3 4 4 4 |
5 | 4 4 4 4 4 4 4 |
6 | 7 8 5 5 5 5 5 |
7 | 4 4 4 4 4 4 5 |
8 | 4 4 4 4 3 4 4 |
9 | 4 3 4 3 3 4 4 |
10 | 3 4 4 3 3 4 4 |
11 | 4 5 4 4 5 5 5 |
12 | 5 4 5 5 5 5 5 |
13 | 4 4 4 4 4 4 5 |
14 | 4 4 4 4 5 6 4 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 6 |
17 | 4 5 4 4 5 6 5 |
18 | 4 4 4 5 4 4 5 |
19 | 4 6 5 5 5 6 5 |
20 | 4 4 4 4 4 4 5 |
21 | 5 5 6 5 5 6 6 |
22 | 4 4 5 4 4 4 4 |
23 | 5 6 5 5 5 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 5 5 6 5 5 5 5 |
26 | 4 4 5 5 6 8 5 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 4 5 |
29 | 5 5 5 4 5 5 5 |
30 | 4 3 3 3 4 4 4 |
31 | 4 4 5 5 5 5 5 |
32 | 4 4 4 4 5 4 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 2.1622.0 GPS week: 1622 Day: 0 MJD: 55598.000
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 238| 0 0 5 40 -55 53 -.21 9 8 | -755 807 15 83
| 48 13 |
emr 88| 1 -1 8 -63 -60 -8 .42 20 20 | -5214 218 11 100
| 12 39 |
esa 150| 2 0 -2 -140 53 -121 .21 8 7 | 5 -646 13 146
| 7 17 |
gfz 189| 0 -1 -4 196 23 47 -.12 10 10 | -109 430 23 144
| -45 52 |
grg 135| 0 1 -10 -82 -221 -19 .66 16 15 | 0 -64 39 198
| 83 91 |
igr n/a| 0 0 0 22 -87 48 -.02 5 5 | 4537 301 19 82
| 0 28 |
jpl 134| 1 0 11 -43 15 96 .45 19 18 | -219 197 18 97
| 90 -171 |
mit 262| -3 0 -6 80 -33 16 -.29 17 10 | -337 463 21 161
| 12 27 |
ngs 222| 0 1 -1 -56 89 21 -.20 10 8 | -573126 812304 1962 3436
| 16 9 |
sio 260| -3 0 10 94 127 3 -.23 18 15 | --- --- --- ---
| -50 3 |
Table 2.1622.1 GPS week: 1622 Day: 1 MJD: 55599.000
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 238| 0 0 3 63 -38 -24 -.22 8 7 | 801 -1715 13 74
| 24 -24 |
emr 88| 1 -3 8 -42 11 27 .43 19 19 | -3865 162 17 108
| 3 -16 |
esa 150| 1 0 0 -89 84 -55 .22 8 8 | 2151 -3004 13 119
| 16 12 |
gfz 189| 0 -1 -5 86 -115 62 -.14 10 10 | 592 -346 23 110
| 17 40 |
grg 135| 4 0 -8 -94 -157 -30 .65 14 13 | 681 -853 46 236
| 99 -26 |
igr n/a| 0 0 0 28 -11 54 -.03 6 5 | 6020 -42 17 60
| -4 -11 |
jpl 134| 0 -1 12 -12 36 -31 .43 20 19 | 1070 -220 20 100
| -105 -4 |
mit 262| -2 0 -5 58 -87 33 -.28 20 9 | 595 -792 20 140
| 6 40 |
ngs 222| 0 2 -4 -43 183 13 -.21 12 7 | 626 -1491 2602 3812
| 13 -48 |
sio 260| -2 0 11 41 84 12 -.25 18 18 | --- --- --- ---
| -44 6 |
Table 2.1622.2 GPS week: 1622 Day: 2 MJD: 55600.000
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 238| 0 1 5 56 -26 6 -.20 9 8 | -288 -358 18 85
| 28 -25 |
emr 88| 1 0 8 -59 25 24 .41 20 20 | -3700 837 16 116
| 24 -23 |
esa 150| 1 -1 0 -92 46 -70 .21 9 9 | 2256 -2954 14 107
| 31 16 |
gfz 189| 1 0 -6 49 -179 58 -.14 12 10 | 224 -337 23 98
| -35 5 |
grg 135| 1 0 -8 -50 -154 -61 .64 15 14 | -196 256 48 234
| 46 -50 |
igr n/a| 0 0 -2 63 25 20 -.02 6 5 | 6029 629 21 69
| -46 7 |
jpl 134| 0 -3 11 -53 34 38 .48 19 19 | 841 559 18 92
| 18 32 |
mit 262| -2 0 -5 56 -66 15 -.29 16 8 | -313 378 20 133
| 4 33 |
ngs 222| 0 1 -4 7 235 10 -.22 11 9 | -292 -438 2295 3753
| -82 -71 |
sio 260| -1 0 9 33 91 -17 -.20 17 17 | --- --- --- ---
| -35 19 |
Table 2.1622.3 GPS week: 1622 Day: 3 MJD: 55601.000
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 238| 0 1 5 68 -22 8 -.21 9 8 | -285 -654 14 61
| 22 -40 |
emr 88| -2 0 6 -6 -20 46 .39 18 18 | -3041 550 17 106
| -7 21 |
esa 150| 2 0 -2 -74 65 -72 .23 8 8 | -1712 1056 15 124
| 5 28 |
gfz 189| 0 -2 -5 -21 -142 33 -.13 11 10 | 276 -550 23 99
| -47 25 |
grg 135| 2 -2 -9 -54 -140 -57 .63 15 13 | 0 -396 45 200
| 62 -70 |
igr n/a| 0 0 0 63 43 33 -.01 5 5 | 6629 517 22 68
| -68 30 |
jpl 134| 1 1 12 -52 42 14 .43 20 19 | 1372 594 19 106
| 64 10 |
mit 262| -1 0 -5 58 -83 31 -.33 16 8 | -80 -244 18 139
| 11 45 |
ngs 222| 0 0 -2 40 218 8 -.28 12 8 | -287 -695 2340 3679
| -72 -93 |
sio 260| 0 0 10 45 93 16 -.27 18 16 | --- --- --- ---
| -31 4 |
Table 2.1622.4 GPS week: 1622 Day: 4 MJD: 55602.000
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 238| 0 0 4 77 -63 13 -.20 9 8 | 38 -260 14 78
| 22 -1 |
emr 88| -2 0 10 -13 -64 4 .37 19 19 | -2076 -180 15 96
| -19 37 |
esa 150| 1 0 -2 -92 74 -52 .21 8 8 | -838 313 14 111
| 10 25 |
gfz 189| -1 -1 -5 -51 31 32 -.08 11 11 | 418 -5 21 94
| -25 43 |
grg 135| 4 0 -7 -15 -213 -31 .66 16 15 | 234 14 38 197
| 30 38 |
igr n/a| 0 0 -1 81 -48 -30 -.02 6 6 | 7591 -82 16 70
| -67 78 |
jpl 134| 0 2 13 -47 0 8 .39 21 20 | 2321 -465 18 95
| 5 78 |
mit 262| -2 0 -6 49 -54 9 -.35 16 9 | -110 503 20 127
| 8 31 |
ngs 222| 0 0 -4 45 98 31 -.26 12 9 | 129 -387 2323 3624
| -96 31 |
sio 260| -1 0 10 38 126 -3 -.21 17 19 | --- --- --- ---
| -42 -2 |
Table 2.1622.5 GPS week: 1622 Day: 5 MJD: 55603.000
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 238| 0 0 7 63 -76 0 -.22 11 10 | 237 -1240 15 73
| 35 16 |
emr 88| 2 1 9 -23 -78 45 .35 19 19 | -2271 482 15 88
| -11 52 |
esa 150| 1 0 -2 -93 34 -100 .24 8 7 | -692 -222 12 108
| 41 49 |
gfz 189| 0 -1 -6 79 71 52 -.18 12 11 | 438 -75 23 111
| -48 45 |
grg 135| 1 1 -9 -62 -212 -5 .68 16 14 | 161 69 37 219
| 83 40 |
igr n/a| 0 0 0 39 -80 15 -.03 5 5 | 7566 305 17 60
| -20 64 |
jpl 134| 0 -1 12 -57 -2 28 .39 19 18 | 1902 -157 18 102
| 41 12 |
mit 262| -3 0 -5 81 -54 12 -.39 16 10 | 98 189 21 142
| 10 31 |
ngs 222| 0 1 -1 -10 98 44 -.24 11 7 | 183 -1189 2493 3892
| -31 58 |
sio 260| 0 1 11 56 170 16 -.25 20 19 | --- --- --- ---
| -54 -19 |
Table 2.1622.6 GPS week: 1622 Day: 6 MJD: 55604.000
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 238| 0 0 5 76 -26 -4 -.25 11 10 | 50 -576 18 77
| 44 -67 |
emr 88| 2 -2 5 -37 -9 27 .33 19 19 | -2502 -82 16 88
| -7 -11 |
esa 150| 2 0 -1 -86 85 -79 .21 7 7 | 488 -3669 13 105
| 68 -8 |
gfz 189| 0 -3 -2 53 -81 50 -.18 13 12 | 404 -765 23 103
| -50 28 |
grg 135| 0 1 -8 -29 -190 -29 .64 14 14 | 151 -608 41 205
| 10 -29 |
igr n/a| 0 0 0 30 -45 27 -.05 5 5 | 7113 -282 16 46
| -10 14 |
jpl 134| -1 0 12 -29 34 21 .42 20 18 | 1057 -436 17 95
| 4 -45 |
mit 262| -1 1 -5 67 -129 27 -.42 14 10 | 142 -635 24 145
| 7 47 |
ngs 222| -1 0 -4 -24 141 38 -.21 11 8 | 36 -574 2091 3558
| -22 25 |
sio 260| -1 2 11 64 61 16 -.24 20 18 | --- --- --- ---
| -63 0 |
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 3.1622.0 GPS week: 1622 Day: 0 MJD: 55598.000
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 | 7 --- --- --- --- 27 --- --- --- --- 0 | 49 --- --- --- --- 73 --- --- --- --- 51
2 | 10 24 5 15 11 4 24 10 9 29 5 | 16 31 21 25 25 20 34 22 16 24 18
3E | 17 22 16 12 21 15 21 67 30 21 10 | 22 32 28 20 40 27 39 70 42 31 28
4 | 8 29 6 9 12 4 11 10 8 16 4 | 31 45 37 36 39 36 39 38 37 33 35
5 | 7 19 6 9 11 6 22 8 6 25 4 | 20 29 28 28 32 25 32 22 26 23 24
6E | 16 19 13 11 19 6 17 39 15 25 7 | 85 85 81 84 85 79 90 76 82 87 80
7 | 8 22 6 8 19 4 18 9 9 17 4 | 11 28 18 13 27 14 27 13 15 19 14
8 | 8 15 8 7 13 4 10 13 10 11 3 | 12 27 19 12 18 15 26 18 15 15 15
9 | 8 13 6 9 20 6 14 14 9 11 4 | 22 25 22 24 20 20 26 21 21 24 20
10 | 9 15 4 6 11 4 11 9 7 19 3 | 17 28 29 29 33 25 26 23 27 22 24
11 | 7 15 7 9 21 5 21 7 8 12 4 | 23 33 27 31 39 29 32 32 32 26 27
12 | 7 27 8 8 18 3 20 8 6 20 4 | 21 36 24 21 27 23 31 20 22 16 21
13E | 8 16 7 11 15 4 18 13 9 13 4 | 29 35 27 29 29 28 36 30 30 34 28
14E | 8 16 7 6 16 3 17 10 7 13 3 | 35 45 41 37 40 38 47 38 39 41 38
15 | 9 23 7 12 21 6 22 8 7 17 4 | 19 27 18 20 22 17 28 20 16 21 15
16 | 7 24 10 11 15 3 26 12 10 19 4 | 22 35 25 23 27 22 36 25 21 22 24
17E | 6 21 8 8 16 3 24 11 7 13 4 | 11 22 14 11 19 11 23 15 15 12 11
18 | 8 16 7 15 17 3 19 7 8 21 4 | 18 28 25 29 28 23 31 23 25 26 23
19E | 7 18 8 12 18 5 24 10 10 13 4 | 21 32 27 23 32 24 32 26 26 25 25
20 | 6 17 8 12 12 6 17 11 9 24 4 | 26 32 31 34 31 29 30 31 28 29 27
21 | 8 20 5 10 14 3 25 8 11 31 4 | 24 30 28 26 25 25 32 31 27 45 26
22 | 7 13 5 8 17 4 19 7 9 19 3 | 23 30 31 29 37 29 34 29 32 29 28
23E | 8 22 9 10 12 4 23 14 10 11 4 | 26 31 33 32 31 27 31 31 30 26 28
24 | 7 13 6 8 12 4 12 10 10 15 3 | 36 44 43 47 48 44 43 46 45 45 43
X25 | 11 16 5 8 16 5 24 12 7 --- 4 | 19 19 17 17 19 17 35 19 16 --- 15
26E | 11 18 5 9 16 5 14 10 11 18 4 | 61 68 64 60 70 63 68 67 65 71 65
X27 | 9 14 5 11 14 5 --- 11 7 27 4 | 20 26 23 25 22 20 --- 21 22 33 20
28 | 6 24 7 8 21 3 19 7 6 17 4 | 17 37 23 15 33 21 35 18 20 16 19
29E | 8 27 10 8 23 3 23 11 10 16 5 | 17 28 28 17 27 21 26 23 25 27 22
30 | 5 12 7 10 14 5 12 10 9 10 3 | 15 23 21 21 25 17 25 20 14 20 18
31 | 7 21 8 11 18 4 19 11 9 13 4 | 12 27 21 21 32 15 26 14 14 16 16
32 | 8 13 9 11 12 6 13 9 8 21 3 | 16 22 22 23 25 21 23 21 21 27 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 8 10 16 5 19 17 10 18 |T 24 33 28 27 32 28 34 29 27 29 27
WRMS | 8 20 7 10 15 5 18 10 8 15 |NE 21 30 25 24 28 25 31 23 23 25 23
MEDI | 8 18 7 9 16 4 19 10 9 17 |MD 21 30 27 25 29 23 32 23 25 26 24
Table 3.1622.1 GPS week: 1622 Day: 1 MJD: 55599.000
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 | 6 --- --- --- --- 71 --- --- --- --- 0 | 37 --- --- --- --- 116 --- --- --- --- 39
2 | 8 22 5 14 11 6 26 7 5 28 4 | 12 26 19 21 23 17 29 17 15 19 15
3E | 14 19 14 10 23 5 22 87 37 20 8 | 19 28 27 21 36 23 33 83 42 30 25
4 | 6 10 8 10 15 6 12 7 7 16 3 | 26 28 31 28 33 26 29 27 26 24 26
5 | 6 16 7 8 11 8 19 7 7 24 3 | 14 29 19 19 26 19 30 16 20 16 18
6E | 18 18 14 13 16 7 20 40 15 21 7 | 65 72 65 70 69 71 72 87 75 72 71
7 | 7 20 6 8 19 3 18 7 10 16 4 | 10 23 16 13 27 10 22 12 17 18 12
8 | 7 16 7 7 9 3 11 11 11 12 3 | 9 23 12 10 16 10 20 14 14 12 11
9 | 7 14 6 9 12 4 13 8 8 10 3 | 24 26 21 24 23 20 28 26 22 23 22
10 | 6 12 9 8 12 4 14 8 7 20 3 | 13 17 22 20 22 16 23 16 17 17 16
11 | 8 16 15 10 21 6 18 9 16 11 4 | 15 23 20 20 31 15 24 21 21 17 15
12 | 6 26 7 9 15 6 23 7 8 18 4 | 16 32 18 20 24 19 30 17 18 15 17
13E | 6 18 8 8 17 5 16 9 12 12 4 | 22 30 21 24 31 22 28 25 24 25 22
14E | 6 18 7 8 15 4 18 6 7 11 3 | 20 33 24 23 29 22 26 22 23 24 21
15 | 9 30 7 13 17 5 21 8 9 13 4 | 17 35 18 22 25 16 29 21 18 23 18
16 | 5 24 8 12 13 7 28 11 10 18 4 | 18 28 21 17 28 19 32 20 20 18 19
17E | 8 22 6 9 16 5 25 12 11 13 4 | 7 19 12 12 16 10 23 14 18 13 10
18 | 9 17 5 13 10 6 23 8 9 18 4 | 13 24 16 19 19 16 26 16 20 18 15
19E | 8 22 11 11 12 5 23 28 17 13 5 | 14 25 25 19 21 15 25 22 22 17 15
20 | 6 17 5 12 9 8 16 9 11 22 4 | 15 22 16 22 19 14 23 19 17 16 14
21 | 11 20 6 12 10 6 30 6 9 31 5 | 18 22 21 22 17 18 27 21 20 40 19
22 | 6 16 7 10 9 5 20 5 10 18 3 | 15 24 21 21 25 16 27 19 19 19 18
23E | 10 23 9 12 14 7 25 21 14 20 5 | 42 45 45 47 45 44 45 40 50 30 43
24 | 8 18 7 17 14 9 13 9 12 14 4 | 24 25 23 36 31 22 26 29 25 28 24
X25 | 15 15 6 11 16 4 25 9 9 --- 4 | 18 22 14 20 21 15 31 18 18 --- 15
26E | 10 15 8 8 19 5 16 8 13 18 4 | 50 54 53 56 58 53 47 54 54 56 51
27 | 7 16 6 11 10 5 13 7 9 27 4 | 21 27 18 22 23 18 23 22 22 32 20
28 | 6 22 10 8 19 4 20 7 8 17 4 | 13 31 23 16 30 17 29 16 20 16 17
29E | 7 25 8 9 14 5 27 9 8 15 4 | 18 28 17 22 20 18 27 21 24 21 18
30 | 5 14 4 8 10 8 13 11 9 9 3 | 8 21 14 10 18 11 19 15 13 16 12
31 | 5 21 10 9 18 7 23 10 7 12 4 | 11 26 17 11 33 13 27 12 14 14 14
32 | 8 12 8 8 12 5 17 8 10 19 3 | 13 15 15 16 16 10 20 16 12 22 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 10 14 6 20 20 12 18 |T 19 28 22 23 27 23 29 25 23 23 21
WRMS | 7 19 8 10 13 5 19 9 7 18 |NE 16 24 18 19 24 20 26 18 18 20 17
MEDI | 7 18 7 10 14 5 20 8 9 17 |MD 16 26 20 21 25 17 27 20 20 19 18
Table 3.1622.2 GPS week: 1622 Day: 2 MJD: 55600.000
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 | 5 --- --- --- --- 234 --- --- --- --- 0 | 28 --- --- --- --- 206 --- --- --- --- 31
2 | 6 24 8 11 12 4 23 8 8 27 4 | 17 31 19 23 25 22 32 18 19 19 18
3E | 22 21 14 20 19 13 22 69 33 30 11 | 18 28 23 29 33 26 31 72 40 32 23
4 | 7 13 12 11 15 5 8 7 6 18 3 | 33 37 38 37 42 36 40 35 36 29 35
5 | 7 16 9 11 14 3 20 8 8 22 4 | 20 30 25 26 31 21 29 19 19 18 22
6E | 12 18 9 14 12 6 21 17 12 14 5 | 53 61 56 60 58 58 61 62 59 58 56
7 | 6 22 6 10 18 5 17 7 11 13 4 | 13 23 17 13 25 16 25 14 17 20 15
8 | 8 15 6 7 14 5 10 9 10 11 3 | 13 24 15 15 18 14 24 17 17 15 14
9 | 9 15 8 12 11 4 12 6 8 10 3 | 19 24 19 26 22 16 21 16 18 15 16
10 | 7 15 9 14 11 4 10 8 6 18 3 | 15 19 24 27 24 22 23 20 21 19 20
11 | 7 18 5 8 23 5 18 7 12 13 4 | 18 27 25 25 38 23 29 24 27 19 22
12 | 9 27 9 11 18 7 23 8 9 17 4 | 17 34 17 22 25 22 30 18 24 15 17
13E | 7 18 6 9 17 6 17 8 10 13 3 | 26 28 22 24 31 23 31 28 26 26 23
14E | 7 14 8 9 14 3 19 7 12 14 4 | 27 34 30 28 29 27 34 29 31 31 28
15 | 10 23 8 11 19 5 22 7 12 10 4 | 16 27 20 20 24 16 25 14 16 19 16
16 | 5 24 13 12 13 5 26 12 9 17 5 | 17 27 19 18 26 18 30 16 18 16 16
17E | 7 25 6 9 18 5 21 9 12 10 4 | 13 21 17 16 18 12 22 18 17 15 12
18 | 9 17 7 13 8 4 21 7 8 19 4 | 16 22 18 24 21 18 23 18 20 18 16
19E | 8 20 9 13 13 5 25 24 11 9 5 | 18 26 22 17 28 19 29 25 20 19 19
20 | 8 16 8 14 12 6 17 6 5 21 4 | 22 27 23 26 26 22 27 25 23 21 22
21 | 15 23 7 11 14 7 29 7 12 30 5 | 24 26 23 23 23 22 28 24 29 38 21
22 | 8 16 7 25 9 4 20 10 10 15 4 | 17 23 23 37 25 19 25 22 22 21 19
23 | 9 24 12 8 20 5 26 9 7 15 4 | 37 43 41 44 44 40 40 40 38 38 38
24 | 11 18 6 9 15 4 12 8 12 16 4 | 27 31 35 36 39 33 35 33 33 31 32
X25 | 18 17 9 17 15 6 26 11 9 --- 5 | 19 20 13 26 22 15 31 20 19 --- 13
26E | 12 25 9 9 17 4 15 11 10 19 4 | 47 52 48 47 47 49 45 48 49 45 47
27 | 9 16 8 10 12 4 11 7 10 26 4 | 17 24 19 23 22 16 21 16 19 33 17
28 | 6 18 6 12 14 5 17 7 9 16 4 | 15 29 17 17 28 18 29 18 19 19 17
29E | 8 25 13 11 20 6 30 10 11 15 5 | 15 22 16 15 16 15 24 19 22 18 14
30 | 5 14 7 9 11 6 11 9 10 8 3 | 15 19 18 17 22 16 21 16 15 15 15
31 | 6 23 8 11 19 5 20 8 12 12 4 | 14 28 21 19 36 17 27 16 19 17 17
32 | 10 12 8 7 14 7 13 7 8 16 3 | 14 18 17 16 21 20 21 15 18 20 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 9 12 15 6 19 16 11 17 |T 21 28 23 25 28 28 29 25 24 23 22
WRMS | 8 20 9 10 14 5 19 8 9 17 |NE 18 25 21 23 26 28 27 19 21 20 19
MEDI | 8 18 8 11 14 5 20 8 10 15 |MD 17 27 21 24 25 20 29 19 20 19 18
Table 3.1622.3 GPS week: 1622 Day: 3 MJD: 55601.000
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 | 6 --- --- --- --- 157 --- --- --- --- 0 | 26 --- --- --- --- 138 --- --- --- --- 29
2 | 8 23 7 15 11 3 24 7 7 26 4 | 17 27 21 23 26 17 28 20 19 19 16
3E | 22 19 14 13 17 11 21 67 33 32 11 | 26 34 32 29 34 31 36 73 48 35 30
4 | 8 11 5 7 15 4 9 5 8 15 3 | 28 31 35 33 40 32 32 33 31 26 31
5 | 8 15 9 9 13 5 19 8 10 20 4 | 19 27 25 23 33 24 28 21 23 19 21
6E | 12 17 7 12 12 9 19 26 13 12 5 | 43 49 45 40 49 42 52 51 48 46 43
7 | 7 19 5 11 20 4 14 7 6 14 3 | 13 25 16 14 28 16 22 14 15 15 13
8 | 8 14 6 9 15 4 10 10 10 10 3 | 14 24 17 15 20 17 24 19 16 16 14
9 | 9 12 5 9 10 4 12 6 11 8 3 | 26 28 22 20 27 22 25 24 21 25 21
10 | 7 10 5 7 11 4 10 9 7 18 3 | 19 23 23 22 31 23 22 25 21 21 21
11 | 7 16 6 11 20 4 19 10 12 15 4 | 19 27 24 28 37 23 27 26 24 24 22
12 | 11 26 8 10 20 5 22 7 9 16 4 | 20 34 20 19 27 21 32 21 17 16 18
13E | 7 14 8 11 19 6 20 8 12 17 4 | 34 37 32 35 39 35 41 36 36 39 33
14E | 9 17 8 10 12 3 21 7 10 14 4 | 38 46 44 42 45 41 49 41 44 42 41
15 | 10 23 7 13 14 5 20 9 11 12 4 | 23 29 19 20 26 18 25 25 20 22 18
16 | 7 23 8 12 16 7 25 13 9 17 4 | 20 34 24 23 32 25 34 24 21 23 22
17E | 6 22 7 8 19 3 23 10 7 15 4 | 17 23 16 19 27 18 24 22 18 15 16
18 | 10 20 8 15 10 4 22 7 12 19 4 | 22 26 23 27 26 19 26 23 19 21 20
19E | 8 22 6 9 9 5 24 22 10 11 4 | 15 29 20 21 22 22 26 28 18 20 18
20 | 8 15 9 16 9 6 18 6 9 21 4 | 25 28 27 33 28 25 27 31 26 27 24
21 | 11 20 8 10 13 4 26 7 12 29 5 | 27 27 24 23 23 21 28 24 22 36 21
22 | 8 16 6 10 7 5 20 7 12 17 3 | 25 28 27 30 34 23 27 26 24 25 24
23 | 6 20 8 8 23 7 27 13 12 19 5 | 19 30 23 20 31 20 29 18 21 18 17
24 | 7 15 7 8 15 4 14 11 11 17 3 | 29 32 35 38 41 34 32 37 32 37 33
X25 | 16 15 8 13 18 7 24 10 9 --- 5 | 21 24 18 19 27 18 33 23 17 --- 15
26E | 11 19 7 9 15 4 15 12 14 24 4 | 57 61 59 63 63 62 63 66 61 68 61
X27 | 10 13 7 9 12 5 --- 9 10 --- 4 | 22 26 23 20 27 21 --- 24 19 --- 20
28 | 6 20 6 13 19 4 17 5 8 15 4 | 16 28 19 17 28 18 27 17 15 20 16
29E | 10 18 8 7 15 3 27 9 10 15 4 | 19 21 16 17 22 18 25 22 21 20 16
30 | 8 12 8 8 12 5 9 9 12 6 3 | 17 24 18 17 23 19 22 18 18 16 16
31 | 8 22 14 9 21 6 19 7 12 11 4 | 15 28 20 17 36 17 27 16 17 15 15
32 | 9 15 5 9 13 4 18 9 10 20 4 | 19 21 19 23 23 19 18 24 22 25 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 8 11 15 5 19 16 12 18 |T 23 30 25 25 31 28 30 28 24 25 23
WRMS | 8 18 8 10 13 5 19 8 8 16 |NE 20 27 22 22 29 26 26 23 20 22 20
MEDI | 8 17 7 10 15 4 19 9 10 16 |MD 20 28 23 23 28 21 27 24 21 22 20
Table 3.1622.4 GPS week: 1622 Day: 4 MJD: 55602.000
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 | 7 --- --- --- --- 60 --- --- --- --- 0 | 26 --- --- --- --- 49 --- --- --- --- 26
2 | 8 26 6 8 12 5 27 6 10 26 4 | 18 32 19 18 27 20 29 18 14 18 16
3E | 18 21 15 13 18 10 20 64 32 27 10 | 20 31 25 28 33 23 29 73 41 28 27
4 | 8 9 6 7 10 4 17 11 9 18 3 | 40 43 42 39 48 43 47 42 44 36 41
5 | 8 18 8 10 9 4 18 7 9 20 4 | 21 30 24 25 31 23 28 23 23 19 22
6E | 11 18 9 9 14 5 20 24 16 10 5 | 30 36 30 33 38 30 40 38 35 31 30
7 | 6 23 6 13 18 6 17 6 9 13 4 | 17 31 17 17 32 13 26 14 16 15 15
8 | 8 13 6 9 14 6 10 9 9 9 3 | 17 28 18 19 26 17 25 22 17 16 18
9 | 8 14 7 10 11 5 12 8 9 10 3 | 15 21 12 14 20 12 19 16 14 13 11
10 | 7 12 6 9 13 4 11 6 8 16 3 | 21 22 25 22 28 23 24 25 23 22 21
11 | 9 17 5 11 22 7 22 10 16 18 4 | 20 29 23 24 36 22 26 27 23 24 20
12 | 7 22 6 11 17 5 25 8 11 15 4 | 20 30 19 16 27 18 29 19 19 14 17
13E | 6 17 5 14 25 7 18 7 9 12 4 | 33 41 32 33 48 32 39 35 32 40 34
14E | 13 18 9 10 20 7 20 7 9 17 4 | 30 45 38 39 40 40 44 39 42 38 36
15 | 8 25 10 11 15 6 23 10 8 12 4 | 16 29 18 13 25 12 22 19 15 19 13
16 | 6 24 9 11 17 6 26 15 12 17 5 | 16 29 19 23 28 18 32 21 22 20 17
17E | 7 22 7 12 11 3 29 13 11 11 4 | 23 31 23 20 34 21 29 23 25 19 21
18 | 9 18 6 15 11 3 20 6 11 19 4 | 21 27 22 28 23 21 25 21 22 20 20
19E | 7 18 9 10 16 6 28 20 11 11 5 | 18 27 25 20 32 20 26 29 16 23 19
20 | 6 14 6 15 10 7 18 8 13 21 4 | 26 28 24 30 27 25 25 29 24 23 23
21 | 13 22 10 9 13 4 26 7 11 29 5 | 22 24 20 20 24 16 24 21 21 35 18
22 | 7 16 5 11 9 7 21 8 11 15 3 | 25 26 27 26 32 24 27 24 24 22 23
23 | 7 22 6 16 20 8 29 11 7 14 4 | 21 31 22 27 29 23 31 24 20 22 20
24 | 8 13 7 9 14 7 14 8 15 10 3 | 30 35 35 34 40 33 31 39 30 33 32
X25 | 12 14 7 14 17 6 22 13 9 --- 4 | 18 20 18 19 23 15 28 19 18 --- 15
26E | 15 21 11 11 16 6 17 19 9 27 5 | 62 67 66 67 63 62 62 60 66 65 63
27 | 9 16 5 8 11 5 12 8 9 24 3 | 15 23 13 14 22 13 21 16 14 27 13
28 | 7 18 6 12 20 3 16 7 7 19 4 | 21 32 20 22 36 20 29 20 19 21 20
29E | 9 22 11 11 23 3 26 12 13 13 5 | 15 20 20 23 21 14 22 19 19 20 15
30 | 8 12 7 10 15 7 14 10 15 5 3 | 18 22 18 19 27 16 22 16 18 14 15
31 | 5 23 7 10 19 7 22 11 12 15 4 | 14 29 18 18 36 15 25 15 15 15 15
32 | 7 17 8 15 12 6 16 13 9 21 4 | 16 22 16 25 24 17 17 24 15 22 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 8 11 16 6 21 16 12 17 |T 22 30 24 25 31 23 29 26 24 24 22
WRMS | 8 19 8 11 15 6 20 9 9 19 |NE 20 27 21 22 29 21 26 22 20 21 19
MEDI | 8 18 7 11 15 6 20 9 10 15 |MD 20 29 22 23 29 20 27 23 21 22 20
Table 3.1622.5 GPS week: 1622 Day: 5 MJD: 55603.000
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 | 8 --- --- --- --- 74 --- --- --- --- 0 | 23 --- --- --- --- 53 --- --- --- --- 23
2 | 10 23 8 21 12 4 24 6 9 25 5 | 15 32 18 24 25 15 29 15 17 19 15
3E | 19 18 11 13 17 5 21 49 26 33 8 | 23 33 30 25 39 29 37 62 40 35 30
4 | 10 8 3 13 11 4 9 11 7 17 3 | 19 28 27 32 29 24 26 24 23 21 24
5 | 10 11 8 7 9 5 18 10 10 22 4 | 18 27 26 22 29 21 27 20 24 16 21
6E | 12 15 9 10 15 4 20 22 14 10 5 | 27 35 27 29 40 29 39 38 31 29 29
7 | 8 18 5 7 17 5 15 8 7 13 3 | 16 25 13 13 27 12 21 11 12 12 11
8 | 12 13 8 10 15 5 11 9 6 10 3 | 18 24 20 14 22 15 21 18 13 14 15
9 | 7 13 7 8 12 3 12 9 11 18 3 | 20 25 21 22 23 19 23 19 26 18 20
10 | 9 12 4 11 11 3 9 7 7 20 3 | 15 23 21 25 26 19 21 21 21 21 19
11 | 9 18 6 13 20 4 18 9 11 18 4 | 19 29 23 25 33 19 26 24 21 24 20
12 | 10 20 9 17 16 6 22 7 11 16 4 | 19 29 18 24 27 18 27 18 22 15 18
13E | 11 13 6 11 14 5 16 5 7 10 3 | 38 38 34 33 37 34 38 37 34 35 33
14 | 24 18 8 8 23 6 17 12 11 16 5 | 64 73 71 73 79 70 73 70 74 67 69
15 | 8 28 7 10 14 3 25 10 8 16 4 | 18 33 16 17 27 15 24 19 16 20 15
16 | 7 27 7 15 16 7 27 12 6 19 5 | 17 32 23 19 28 17 33 18 14 18 18
17E | 9 18 9 10 15 6 27 22 12 23 5 | 25 29 25 22 28 21 32 28 20 27 22
18 | 8 18 7 11 11 3 20 5 9 19 4 | 20 26 22 23 25 20 24 21 19 20 20
19E | 10 19 9 9 17 5 25 23 14 15 5 | 13 26 19 16 28 14 23 28 14 20 15
20 | 8 16 6 14 10 5 16 9 7 23 4 | 21 27 23 24 27 20 27 23 20 16 20
21 | 18 22 8 10 11 6 27 7 10 32 5 | 21 25 17 19 21 18 25 23 20 40 17
22 | 8 15 8 11 8 4 21 11 10 16 4 | 20 26 25 23 28 20 28 22 19 21 21
23 | 8 25 8 15 18 3 29 14 8 17 5 | 18 28 24 28 30 21 26 24 21 25 19
24 | 7 15 7 9 15 3 12 13 11 13 3 | 21 22 24 26 29 22 24 24 23 22 22
X25 | 18 14 8 13 15 5 22 12 11 --- 5 | 18 21 16 16 26 14 30 19 18 --- 14
26E | 20 26 11 16 31 9 14 40 12 37 8 | 74 74 72 67 87 69 70 87 68 78 71
27 | 9 14 7 8 9 3 10 9 11 24 3 | 18 28 21 22 24 19 21 19 24 28 20
28 | 10 20 6 10 21 5 14 7 6 19 4 | 19 29 20 15 34 18 27 15 16 21 17
29E | 10 22 9 8 16 3 29 18 9 14 5 | 25 28 27 24 30 22 30 25 27 27 24
30 | 7 14 6 11 11 7 13 11 9 10 3 | 15 18 19 18 24 12 21 11 15 11 15
31 | 6 21 8 12 19 7 18 13 9 15 4 | 15 26 16 16 35 13 23 15 17 14 15
32 | 8 16 5 9 13 6 16 12 7 22 4 | 21 23 21 18 27 19 22 23 16 24 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 8 12 16 5 19 16 11 20 |T 22 30 25 24 32 23 29 26 24 25 22
WRMS | 10 19 7 11 14 5 18 10 7 19 |NE 18 26 20 20 27 19 25 19 18 19 18
MEDI | 9 18 8 11 15 5 18 11 9 17 |MD 19 28 22 23 28 19 26 22 20 21 20
Table 3.1622.6 GPS week: 1622 Day: 6 MJD: 55604.000
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 | 7 --- --- --- --- 153 --- --- --- --- 0 | 28 --- --- --- --- 109 --- --- --- --- 30
2 | 9 21 10 10 11 5 24 8 7 25 4 | 15 28 18 17 25 16 28 15 16 20 15
3E | 19 19 12 12 19 5 19 47 27 37 8 | 19 27 25 21 33 23 32 56 40 38 24
4 | 9 11 5 11 11 7 8 13 8 16 3 | 32 33 39 41 46 39 37 40 39 35 38
5 | 12 13 6 11 12 5 17 9 10 25 4 | 23 33 30 31 38 30 33 28 33 29 29
6E | 13 19 9 10 16 3 18 20 17 18 5 | 36 48 39 42 48 40 46 47 46 42 42
7 | 20 18 6 13 18 6 18 9 11 16 5 | 18 23 15 16 25 15 22 15 18 17 14
8 | 12 16 6 10 13 4 12 10 9 11 3 | 15 24 17 12 19 14 23 17 17 17 15
9 | 10 16 5 11 10 5 13 11 9 19 3 | 19 26 19 23 24 18 27 20 24 25 21
10 | 10 11 7 13 12 5 9 7 7 22 3 | 20 25 27 33 36 28 24 30 32 27 26
11 | 7 16 5 16 19 4 19 14 7 26 4 | 20 28 24 30 37 24 26 30 25 32 23
12 | 10 23 8 11 14 4 22 7 10 17 4 | 21 33 21 23 27 21 32 20 22 19 20
13E | 19 14 6 15 15 6 16 12 13 10 4 | 55 66 61 61 60 62 68 58 68 65 62
14 | 7 17 6 10 19 5 22 11 8 16 4 | 38 38 38 36 40 36 39 36 37 38 35
15 | 9 24 9 12 15 4 25 10 10 15 4 | 17 32 23 19 28 16 31 17 26 22 22
16 | 9 26 10 17 14 6 26 14 11 19 5 | 17 31 24 21 26 20 34 20 23 21 21
17E | 12 19 6 12 16 4 24 12 9 15 4 | 32 40 35 35 38 35 41 41 40 41 38
18 | 10 19 9 21 11 4 21 8 11 18 4 | 25 29 25 31 29 23 28 25 24 24 23
19E | 8 22 7 11 12 4 26 19 14 16 5 | 10 25 17 17 21 14 23 23 19 21 15
20 | 8 13 8 15 9 8 17 13 9 25 4 | 25 29 31 34 31 26 28 31 27 25 26
21 | 17 21 10 11 15 7 27 8 9 34 5 | 26 26 26 25 26 23 27 28 27 46 24
22 | 9 15 7 11 9 4 18 8 9 17 3 | 27 30 32 30 34 28 29 28 28 29 28
23 | 7 25 6 14 19 5 28 15 13 15 5 | 20 31 23 26 29 22 29 26 24 26 21
24 | 7 17 4 11 11 5 15 11 7 13 3 | 27 31 34 37 40 32 31 38 30 32 32
X25 | 15 14 6 13 16 6 24 11 11 --- 5 | 18 20 15 18 23 15 31 18 19 --- 14
26 | 17 19 8 14 17 5 13 14 13 27 5 | 83 93 88 93 87 88 88 90 94 91 91
27 | 11 17 6 12 10 5 12 12 10 26 4 | 16 26 19 21 27 19 23 18 24 31 20
28 | 8 27 6 12 19 3 18 9 8 20 4 | 20 36 21 19 28 22 30 21 26 30 21
29E | 12 26 9 11 13 5 31 8 7 12 5 | 22 27 26 20 21 21 24 25 28 23 24
30 | 8 16 5 12 15 7 12 12 11 10 3 | 17 22 21 24 25 18 22 19 23 18 19
31 | 5 21 9 16 18 6 18 10 6 13 4 | 13 26 18 19 32 15 24 13 17 16 15
32 | 10 14 7 12 12 6 16 15 10 22 4 | 15 21 20 20 24 17 20 17 17 24 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 7 13 14 5 20 14 11 20 |T 24 32 28 28 33 29 32 29 30 30 27
WRMS | 10 19 7 12 14 5 18 10 8 18 |NE 20 27 23 24 29 25 27 23 24 25 22
MEDI | 10 18 7 12 14 5 18 11 10 17 |MD 20 29 24 24 29 22 29 25 26 26 23
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1622 GPS week: 1622 MJD: 55598.0-55604.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 |U 8 7 23 |U 17 15 53 |U 19 7 31 |
emr | emr 2965 |U 10 10 23 |U 22 19 62 | 20 8 31 |
esa | esa 2976 | 7 7 22 |U 17 15 51 | 17 6 28 |
gfz | gfz 2963 |U 16 10 32 |U 21 20 60 |U 21 7 29 |
grg | grg 2975 | 8 8 21 |U 18 14 52 | 19 6 29 |
igr | igr 2952 | 8 8 22 | 18 18 58 | 18 7 28 |
igs | igs 2943 | 7 6 19 | 17 15 52 | 18 6 27 |
jpl | jpl 2934 | 9 9 24 |U 20 20 58 | 19 7 30 |
mit | mit 2976 |U 9 7 25 |U 23 27 81 |U 20 6 33 |
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 5.1622.0 GPS week: 1622 Day: 0 MJD: 55598.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3027 | 7 6 22 | 9 8 33 | 92 8 109 |
emr | emr 2964 | 9 8 17 | 16 13 48 | 91 6 102 |
esa | esa 2976 | 6 6 19 | 12 10 33 | 83 7 97 |
gfz | gfz 2964 | 8 6 19 | 17 17 42 | 88 5 106 |
grg | grg 2976 | 7 6 20 | 11 9 36 | 93 6 108 |
igr | igr 2962 | 6 5 19 | 11 9 30 | 86 6 99 |
igs | igs 2944 | 6 5 17 | 10 9 32 | 90 6 104 |
jpl | jpl 2867 | 8 6 19 | 10 11 35 | 85 9 95 |
mit | mit 2976 | 9 6 25 | 19 11 50 | 99 8 123 |
Table 5.1622.1 GPS week: 1622 Day: 1 MJD: 55599.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3021 | 7 8 18 | 26 16 68 | 5 5 22 |
emr | emr 2964 | 10 11 21 | 30 18 84 | 8 10 20 |
esa | esa 2976 | 6 8 16 | 26 16 61 | 6 5 15 |
gfz | gfz 2965 | 16 14 40 | 22 19 55 | 12 7 20 |
grg | grg 2976 | 7 9 16 | 27 15 75 | 6 6 20 |
igr | igr 2942 | 7 10 17 | 26 16 66 | 5 4 16 |
igs | igs 2906 | 7 9 13 | 26 16 70 | 5 6 14 |
jpl | jpl 2963 | 9 12 17 | 29 20 70 | 7 9 21 |
mit | mit 2976 | 8 10 20 | 31 72 175 | 6 6 14 |
Table 5.1622.2 GPS week: 1622 Day: 2 MJD: 55600.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 7 6 21 | 17 19 51 | 5 7 16 |
emr | emr 2964 | 12 9 24 | 31 21 50 | 6 6 18 |
esa | esa 2976 | 11 15 31 | 18 20 51 | 5 4 20 |
gfz | gfz 2959 | 17 9 33 | 22 31 63 | 7 5 17 |
grg | grg 2976 | 7 7 22 | 17 17 51 | 6 4 20 |
igr | igr 2943 | 7 6 25 | 22 22 58 | 6 4 14 |
igs | igs 2965 | 7 5 21 | 18 19 53 | 6 5 14 |
jpl | jpl 2958 | 10 9 23 | 28 20 49 | 7 6 19 |
mit | mit 2976 | 7 7 22 | 34 20 52 | 9 8 21 |
Table 5.1622.3 GPS week: 1622 Day: 3 MJD: 55601.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 10 14 29 | 18 19 75 | 10 9 18 |
emr | emr 2964 | 8 8 22 | 22 17 61 | 8 8 15 |
esa | esa 2976 | 6 4 15 | 15 20 70 | 6 6 14 |
gfz | gfz 2964 | 12 6 23 | 23 21 84 | 11 10 16 |
grg | grg 2976 | 8 8 22 | 18 20 64 | 7 7 16 |
igr | igr 2922 | 9 13 23 | 19 21 77 | 11 13 25 |
igs | igs 2967 | 6 5 17 | 17 19 70 | 8 8 14 |
jpl | jpl 2868 | 7 8 20 | 21 17 72 | 7 7 15 |
mit | mit 2976 | 8 8 26 | 18 19 80 | 7 6 17 |
Table 5.1622.4 GPS week: 1622 Day: 4 MJD: 55602.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 8 7 22 | 22 16 44 | 7 6 19 |
emr | emr 2966 | 11 11 29 | 29 35 78 | 7 7 19 |
esa | esa 2976 | 8 6 24 | 20 14 37 | 6 4 18 |
gfz | gfz 2964 | 19 11 34 | 22 21 56 | 10 7 16 |
grg | grg 2976 | 9 6 25 | 24 14 49 | 6 4 13 |
igr | igr 2958 | 8 7 24 | 24 32 73 | 5 5 15 |
igs | igs 2918 | 8 5 22 | 22 15 45 | 5 5 15 |
jpl | jpl 2964 | 9 8 28 | 22 38 80 | 8 7 20 |
mit | mit 2976 | 8 5 25 | 25 33 89 | 6 5 17 |
Table 5.1622.5 GPS week: 1622 Day: 5 MJD: 55603.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 6 5 21 | 12 12 41 | 6 5 15 |
emr | emr 2968 | 8 11 25 | 13 12 45 | 8 7 20 |
esa | esa 2976 | 6 5 22 | 13 11 49 | 6 5 17 |
gfz | gfz 2965 | 19 9 37 | 23 20 61 | 10 6 15 |
grg | grg 2976 | 6 8 22 | 13 11 38 | 7 6 18 |
igr | igr 2967 | 7 6 22 | 13 11 45 | 7 8 15 |
igs | igs 2974 | 7 6 21 | 13 11 39 | 6 6 14 |
jpl | jpl 2965 | 8 8 24 | 13 14 43 | 9 7 22 |
mit | mit 2976 | 12 5 27 | 15 12 55 | 7 6 20 |
Table 5.1622.6 GPS week: 1622 Day: 6 MJD: 55604.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 8 6 31 | 16 18 62 | 7 7 17 |
emr | emr 2968 | 11 11 24 | 16 19 69 | 9 8 20 |
esa | esa 2976 | 7 7 25 | 16 16 58 | 7 8 13 |
gfz | gfz 2965 | 24 15 36 | 18 14 60 | 7 6 13 |
grg | grg 2975 | 13 12 24 | 16 14 54 | 7 7 12 |
igr | igr 2974 | 9 8 25 | 15 16 58 | 7 8 14 |
igs | igs 2928 | 7 9 22 | 15 17 54 | 6 7 12 |
jpl | jpl 2958 | 16 16 35 | 16 22 56 | 9 7 20 |
mit | mit 2976 | 14 11 30 | 17 22 68 | 9 7 18 |
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 6.1622 GPS week: 1622 MJD: 55598.500-55604.500
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 -32 73 53 0 | 5 15
| 21 8 82 62 3 | 1
emr uuuuu | -1 1 50 -82 -15 | 24 30
| 19 15 96 32 4 | 7
esa uuuuu | -7 -25 27 -14 3 | -5 16
| 14 22 55 41 3 | 1
gfz uuuuu | -21 33 21 33 2 | 6 17
| 13 25 52 74 3 | 1
grg uuuux | 14 -59 49 -44 5 | 0 16
| 47 28 59 123 11 | 2
igr xxxxx | -17 31 40 -23 -6 | -1 20
| 19 20 97 76 12 | 6
irf xxxxx | 13 0 -56 52 1 | -4 15
| 17 10 50 46 5 | 1
jpl uuuuu | 26 -17 68 121 -16 | -2 29
| 78 64 124 78 9 | 7
mit uuuuu | -23 -8 -92 115 3 | 10 18
| 22 10 62 48 9 | 2
ngs uuuuu | 26 39 -103 -91 -2 | -3 12
| 45 36 111 99 8 | 3
sio uuuuu | 12 46 85 -22 6 | 9 17
| 27 19 56 86 5 | 3
Table 7.1622.0 GPS week: 1622 Day: 0 MJD: 55598.500
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 | 2 -38 -44 64 0 | 8 19
emr uuuuu | -24 -2 149 -110 -11 | 34 39
esa uuuuu | -2 3 60 -11 0 | -2 18
gfz uuuuu | -37 55 -16 6 5 | 8 20
grg uuuux | -76 -73 95 -281 6 | -3 17
igr xxxxx | -13 10 -7 50 -20 | 10 26
irf xxxxx | 15 10 -67 105 3 | -3 19
jpl uuuuu | 186 -80 59 120 -16 | 7 29
mit uuuuu | -12 -2 -94 185 8 | 10 22
ngs uuuuu | 6 -6 -155 -62 -1 | 1 12
sio uuuuu | 12 60 79 119 0 | 13 27
Table 7.1622.1 GPS week: 1622 Day: 1 MJD: 55599.500
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 | 28 -15 45 26 -4 | 6 17
emr uuuuu | 20 6 88 -43 -16 | 30 36
esa uuuuu | -8 -7 -27 -27 5 | -5 16
gfz uuuuu | -36 -8 -5 -21 1 | 6 18
grg uuuux | 30 -90 66 38 4 | -2 18
igr xxxxx | 15 13 -29 -22 -23 | 4 21
irf xxxxx | 4 9 -53 70 6 | -6 16
jpl uuuuu | 8 114 253 159 -20 | 4 28
mit uuuuu | -36 3 -77 133 12 | 7 17
ngs uuuuu | 52 -4 -115 -170 -7 | 0 11
sio uuuuu | -2 53 111 43 10 | 8 18
Table 7.1622.2 GPS week: 1622 Day: 2 MJD: 55600.500
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 -35 65 -61 0 | 4 15
emr uuuuu | 19 -31 125 -96 -15 | 26 31
esa uuuuu | -20 -38 -32 67 -2 | -6 15
gfz uuuuu | -9 28 92 -74 1 | 4 17
grg uuuux | 46 -53 25 -51 9 | -1 17
igr xxxxx | -11 39 -24 66 -11 | -1 18
irf xxxxx | -4 -7 -14 -33 5 | -7 16
jpl uuuuu | -36 -25 112 82 -14 | 0 28
mit uuuuu | -37 -11 -62 32 10 | 7 17
ngs uuuuu | 67 75 -184 34 -7 | -1 11
sio uuuuu | -23 28 165 -107 12 | 6 14
Table 7.1622.3 GPS week: 1622 Day: 3 MJD: 55601.500
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 | 41 -29 193 29 3 | 5 14
emr uuuuu | -20 0 10 -90 -9 | 24 31
esa uuuuu | -27 -12 57 -21 2 | -6 15
gfz uuuuu | -24 40 46 9 3 | 5 16
grg uuuux | 71 -69 -15 78 -17 | -1 17
igr xxxxx | -29 61 -77 -38 -4 | -4 20
irf xxxxx | 1 -7 -4 18 4 | -5 13
jpl uuuuu | -9 -71 -80 131 -14 | -1 29
mit uuuuu | -44 -18 3 114 7 | 10 16
ngs uuuuu | 94 65 -171 -122 -14 | -3 13
sio uuuuu | -3 24 130 -64 11 | 7 14
Table 7.1622.4 GPS week: 1622 Day: 4 MJD: 55602.500
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 | 34 -38 171 80 5 | 5 14
emr uuuuu | -4 3 -94 -100 -21 | 22 27
esa uuuuu | 8 -26 101 -12 3 | -6 15
gfz uuuuu | -10 9 77 66 6 | 5 16
grg uuuux | -5 -46 81 -95 9 | 1 16
igr xxxxx | -45 51 106 -163 5 | -5 19
irf xxxxx | 33 -16 -26 83 0 | -4 14
jpl uuuuu | -45 -21 -100 30 -30 | -4 27
mit uuuuu | 2 -24 -80 124 -1 | 11 18
ngs uuuuu | 2 80 -154 -80 2 | -5 12
sio uuuuu | 35 26 77 12 7 | 8 16
Table 7.1622.5 GPS week: 1622 Day: 5 MJD: 55603.500
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 -29 49 119 -2 | 4 14
emr uuuuu | -12 17 -54 -105 -17 | 18 25
esa uuuuu | -9 -35 59 -69 8 | -6 16
gfz uuuuu | -5 54 4 111 -2 | 6 16
grg uuuux | 0 -77 123 -59 5 | 3 15
igr xxxxx | -24 26 157 1 3 | -6 19
irf xxxxx | 40 6 -75 62 -3 | -4 13
jpl uuuuu | 28 -35 86 61 -21 | -9 29
mit uuuuu | 9 -4 -138 133 -6 | 12 18
ngs uuuuu | -18 37 -72 11 4 | -6 13
sio uuuuu | 59 60 24 -119 5 | 10 16
Table 7.1622.6 GPS week: 1622 Day: 6 MJD: 55604.500
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 | 71 -38 32 112 -2 | 4 14
emr uuuuu | 15 13 123 -28 -18 | 15 24
esa uuuuu | 12 -62 -27 -26 4 | -5 14
gfz uuuuu | -24 56 -51 134 2 | 6 16
grg uuuux | 33 -4 -35 62 19 | 3 15
igr xxxxx | -10 16 154 -52 8 | -7 19
irf xxxxx | 4 6 -151 56 -9 | -3 12
jpl uuuuu | 49 2 145 267 0 | -13 32
mit uuuuu | -43 -1 -196 82 -12 | 13 18
ngs uuuuu | -21 28 133 -248 8 | -6 13
sio uuuuu | 4 69 6 -40 -2 | 11 16
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