[IGSREPORT-19315] Wk 1614 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Dec 30 04:56:24 PST 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1614 (Dec 12, 2010 - Dec 18, 2010)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1614[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1614[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1614[0-6].cls IGS GPS clock combination summary report.
igs16147.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16147.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 | ALL | 1
0 | COD | DGAR
0 | EMR | 30 32 30 32 WTZR WTZR
0 | ESA | AUCK AUCK DAV1 KERG SUTH
0 | GFZ | 10 22 25 28 30 AUCK DGAR NRIL XMIS
0 | GRG | AMC2 DGAR
0 | JPL | 32 POTS
0 | MIT | 30 32 30 32
1 | ALL | 1 1
1 | COD | DGAR FLIN XMIS YKRO
1 | EMR | 30 32 30 WTZR WTZR
1 | ESA | 21 21 KERG SUTH
1 | GFZ | 22 25 28 30 DARW DGAR HOB2 INVK MDVJ UNSA
1 | GRG | DGAR LPGS WTZR
1 | JPL | 22 30 INVK
1 | MIT | 7 13 30 7 13 30 YELL FLIN MAW1 YELL
2 | ALL | 1 1
2 | COD | 9 9 CHUR CHUR DGAR
2 | EMR | 30 30 WTZR WTZR
2 | ESA | 9 9 SUTH UNSA
2 | GFZ | 22 25 28 30 DGAR XMIS
2 | GRG | DGAR FAA1 USN3
2 | JPL | 22 ZWE2
2 | MIT | 30 4 30 HARB MAW1 TOW2 DAV1 HARB MAW1 SANT TOW2
3 | ALL | 1
3 | COD | DGAR DUBO XMIS
3 | EMR | 30 WTZR WTZR
3 | ESA | NRC1 KERG NRC1 SUTH UNSA
3 | GFZ | 16 22 25 28 30 ALGO DGAR RAMO
3 | GRG | DGAR
3 | JPL | 22 32 ALGO
3 | MIT | 30 30 YELL YELL
4 | COD | MAW1 DGAR GUAT MAW1 RCMN
4 | EMR | 30 30 WTZR WTZR
4 | ESA | 10 SUTH
4 | GFZ | 12 16 22 25 28 30 MDVJ
4 | GRG | DGAR
4 | JPL | 22 30
4 | MIT | 29 30 29 30 ASPA TIDB
5 | COD | DGAR FAA1
5 | EMR | 30 30 HARB WTZR WTZR
5 | ESA | CAS1 QIKI SUTH WTZR
5 | GFZ | 12 16 22 25 28 30 ASPA KERG RAMO STJO
5 | GRG | DGAR HOB2
5 | JPL | 22 30 MCM4 TIDB
5 | MIT | 30 30 POL2
6 | ALL | 1 1
6 | COD | DGAR RCMN
6 | EMR | 30 30 HARB WTZR HARB WTZR
6 | ESA | KERG SUTH
6 | GFZ | 3 16 22 25 28 30 ARTU DAV1 MDVJ RAMO
6 | GRG | DGAR
6 | JPL | ARTU HARB MCM4 POTS
6 | MIT | 2 30 2 30
5. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G04 | 2010_12_17 | 2010154
G32 | 2010_12_14 | 2010150
G32 | 2010_12_14 | 2010151
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 | .3 1.1 .6 -2 -9 -36 .11
EMR | 3.8 10.9 -4.2 43 -14 26 .50
ESA | 2.8 6.6 -9.6 118 -98 -3 .32
GFZ | .2 1.6 .0 28 -19 -21 .29
GRG | 1.5 5.7 -5.1 55 57 -87 .45
JPL | .1 5.2 8.7 31 -58 -28 .31
MIT | -.4 6.0 -9.0 7 -16 -31 .27
NGS | 1.5 6.8 -5.1 112 -61 -18 .06
SIO | .6 6.2 -3.3 115 -26 -12 .43
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 1.1614.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1614.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 2.1614.[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 3.1614.[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 5.1614.0-6).
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 1614 summary. (Dec 12, 2010 - Dec 18, 2010)
Table 1.1614.a GPS week: 1614 MJD: 55542.000-55548.000
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 236| 0 0 5 110 -41 -11 -.20 8 8 | -38 -566 14 76
| 0 0 0 11 19 19 .02 | 289 540
emr 93| 0 3 3 4 -30 -3 .40 18 18 | -1987 160 13 96
| 1 1 2 23 46 13 .03 | 1412 1544
esa 156| 0 0 0 -58 61 2 .26 7 7 | 258 -1331 12 105
| 1 1 1 32 50 16 .03 | 1112 2251
gfz 193| 0 -1 -5 34 13 16 -.20 10 10 | 350 -480 21 100
| 1 0 1 78 170 16 .04 | 171 330
grg 136| 1 2 -10 -18 -188 -37 .70 17 16 | -1343 4124 45 226
| 1 0 1 22 18 12 .03 | 4111 12368
igr n/a| 0 0 0 81 -32 13 -.01 5 5 | 3187 -460 15 77
| 0 0 1 32 34 21 .03 | 1487 1609
jpl 144| 0 -1 10 23 78 0 .54 18 18 | 1540 -47 17 105
| 0 1 1 13 8 105 .03 | 1117 1480
mit 262| 0 0 -3 102 -27 14 -.34 10 9 | 285 -758 21 147
| 0 0 1 24 26 9 .02 | 384 930
ngs 216| 0 0 -2 -120 44 -7 -.19 9 8 | -21 -582 1997 3855
| 0 1 1 32 79 18 .03 | 251 457
sio 255| 0 0 7 -129 -30 -1 -.16 17 16 | --- --- --- ---
| 0 2 1 20 30 12 .02 | --- ---
Table 1.1614.b GPS week : 1614 MJD: 55542.000-55548.000
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 | 15 16 13 38 24 19 17 |
2 | 4 4 4 5 4 4 5 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 4 4 4 0 4 |
5 | 4 4 4 4 5 5 5 |
6 | 3 4 3 3 4 4 4 |
7 | 4 4 4 4 5 5 5 |
8 | 4 4 4 4 4 4 4 |
9 | 3 3 3 3 4 4 4 |
10 | 5 4 4 4 5 4 4 |
11 | 4 3 4 4 4 4 4 |
12 | 5 5 4 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 4 4 5 4 |
16 | 4 5 5 5 5 5 5 |
17 | 5 4 4 5 5 5 5 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 5 5 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 3 4 4 4 4 4 4 |
22 | 4 4 4 4 4 4 3 |
23 | 4 4 4 5 5 5 5 |
24 | 3 3 4 3 4 3 4 |
25 | 4 4 5 4 5 4 5 |
26 | 3 3 3 3 4 4 4 |
27 | 3 3 4 4 4 4 4 |
28 | 3 4 4 4 4 4 5 |
29 | 4 5 5 5 5 4 5 |
30 | 5 5 6 5 5 5 6 |
31 | 4 4 4 4 5 4 5 |
32 | 7 7 0 5 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 2.1614.0 GPS week: 1614 Day: 0 MJD: 55542.000
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 236| 0 0 6 106 -30 8 -.18 8 7 | 217 -1335 12 71
| 25 22 |
emr 93| 1 1 6 45 2 24 .38 18 17 | -1412 -1905 13 76
| -34 -54 |
esa 156| 1 -1 -3 -121 101 -17 .22 7 7 | 815 -1479 14 108
| 13 3 |
gfz 193| 0 0 -5 51 -156 38 -.18 10 9 | 572 -1028 20 89
| -66 -35 |
grg 136| 0 0 -12 -12 -158 -17 .68 17 15 | 430 -1270 50 223
| 53 -78 |
igr n/a| 0 0 -1 120 4 -17 -.00 5 5 | 5787 -2823 15 71
| -52 -56 |
jpl 144| 0 0 8 48 63 -78 .54 16 15 | 2675 -2235 15 106
| -58 -42 |
mit 262| -1 0 0 112 -42 21 -.37 11 9 | 517 -1173 21 138
| -12 16 |
ngs 216| 0 1 -2 -108 113 -15 -.20 10 8 | 179 -1261 2177 4180
| -36 -63 |
sio 255| 0 -1 8 -137 -20 5 -.17 18 17 | --- --- --- ---
| 77 53 |
Table 2.1614.1 GPS week: 1614 Day: 1 MJD: 55543.000
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 236| 0 0 4 109 -19 -12 -.16 7 7 | -143 -379 14 81
| 13 8 |
emr 93| -1 4 4 17 -23 -9 .42 19 19 | -2490 -524 12 92
| -12 -34 |
esa 156| 1 1 0 -38 104 11 .23 7 7 | 1695 -5125 15 111
| -20 27 |
gfz 193| 0 0 -5 -86 -123 28 -.18 9 8 | 80 -191 22 109
| -36 -31 |
grg 136| 2 2 -11 2 -187 -37 .71 17 15 | 338 -738 43 277
| 6 -50 |
igr n/a| 0 0 1 121 0 26 -.00 5 5 | 3867 -1404 15 79
| -47 -37 |
jpl 144| -1 -3 10 31 79 -118 .55 18 18 | 1285 -674 19 112
| -30 -66 |
mit 262| -1 0 -3 92 -37 9 -.32 9 9 | 67 -332 25 179
| -5 6 |
ngs 216| -1 0 -2 -65 106 13 -.20 9 9 | -101 -559 2339 4674
| -85 -8 |
sio 255| 0 -1 6 -141 -34 8 -.17 16 15 | --- --- --- ---
| 67 57 |
Table 2.1614.2 GPS week: 1614 Day: 2 MJD: 55544.000
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 236| 0 0 4 124 -28 -23 -.19 9 8 | -248 3 14 76
| -2 32 |
emr 93| 1 1 4 -15 -58 -5 .36 17 17 | -2838 1077 14 96
| 9 13 |
esa 156| 0 1 -1 -24 -18 3 .27 7 7 | 500 244 10 86
| -14 64 |
gfz 193| 0 0 -4 -45 105 21 -.17 9 9 | 274 -328 20 95
| -48 2 |
grg 136| 1 2 -9 -6 -194 -47 .65 17 16 | -153 596 48 188
| 24 55 |
igr n/a| 0 0 0 96 -68 36 .00 6 6 | 2677 501 14 70
| -8 29 |
jpl 144| -1 -3 12 7 85 -127 .55 18 18 | 838 938 18 90
| 80 -166 |
mit 262| 0 0 -2 87 -5 29 -.33 9 8 | -74 110 18 123
| -4 -2 |
ngs 216| -1 0 -2 -106 34 10 -.20 10 8 | -337 149 2076 4541
| -41 35 |
sio 255| 0 -2 6 -131 8 3 -.18 15 14 | --- --- --- ---
| 62 42 |
Table 2.1614.3 GPS week: 1614 Day: 3 MJD: 55545.000
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 236| 0 0 6 115 -69 -31 -.19 8 8 | -352 -301 17 78
| -5 56 |
emr 93| 2 2 3 -20 -101 -19 .42 18 18 | -3048 -1551 13 100
| 12 16 |
esa 156| 0 0 0 -54 -1 32 .30 8 8 | 1255 -2878 13 92
| -10 47 |
gfz 193| 0 0 -6 98 281 -7 -.19 10 9 | 376 -781 22 100
| -35 16 |
grg 136| 2 2 -10 -20 -204 -56 .68 18 17 | 292 -1091 49 225
| 50 143 |
igr n/a| 0 0 0 36 -82 10 .02 6 6 | 1999 -1824 16 71
| -28 13 |
jpl 144| 0 -2 11 14 80 136 .52 17 17 | 542 -1458 16 96
| 52 -47 |
mit 262| 0 0 -2 101 20 8 -.33 9 8 | 254 -991 23 145
| -3 -20 |
ngs 216| -1 1 -3 -159 -84 -28 -.15 8 7 | -342 -251 1835 3494
| 45 171 |
sio 255| 0 0 6 -133 -2 -12 -.15 15 13 | --- --- --- ---
| 63 33 |
Table 2.1614.4 GPS week: 1614 Day: 4 MJD: 55546.000
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 236| 0 0 5 92 -62 14 -.23 9 9 | -133 -376 15 89
| 56 22 |
emr 93| 0 3 2 -10 -64 0 .37 18 18 | -3326 2378 13 98
| 23 16 |
esa 156| 0 -2 -1 -78 71 -13 .27 7 7 | -1399 1955 13 126
| 19 48 |
gfz 193| -1 -1 -7 137 149 23 -.22 12 12 | 321 -86 24 104
| -47 32 |
grg 136| 2 2 -9 -33 -189 -26 .70 16 15 | 66 85 38 241
| 74 101 |
igr n/a| 0 0 2 69 -22 19 -.05 5 5 | 1359 1834 15 69
| -71 15 |
jpl 144| 0 0 10 20 90 73 .52 18 18 | 331 2037 17 116
| 12 -18 |
mit 262| 0 0 -3 152 -27 13 -.35 11 10 | 1 153 21 155
| -12 -15 |
ngs 216| 0 1 0 -161 -37 -34 -.23 9 8 | 146 -750 1917 3697
| 113 110 |
sio 255| 1 2 7 -82 -27 -11 -.17 16 15 | --- --- --- ---
| 47 18 |
Table 2.1614.5 GPS week: 1614 Day: 5 MJD: 55547.000
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 236| 0 0 5 120 -53 -35 -.23 7 7 | -91 -241 15 71
| 6 13 |
emr 93| 2 3 0 0 -4 -8 .41 19 19 | -1565 874 16 98
| 3 -51 |
esa 156| -1 0 0 -43 88 1 .24 7 7 | -618 -1281 12 101
| -4 19 |
gfz 193| 0 -2 -3 26 -3 4 -.20 10 9 | 277 -518 22 100
| -94 8 |
grg 136| 0 2 -10 0 -212 -37 .72 16 17 | 278 -845 46 237
| 27 29 |
igr n/a| 0 -1 0 58 -9 30 -.04 5 5 | 2598 168 17 99
| -37 11 |
jpl 144| 0 0 11 26 80 60 .50 19 19 | 1805 461 19 116
| 46 36 |
mit 262| 0 0 -4 80 -52 19 -.34 12 11 | 1039 -2535 20 127
| 6 1 |
ngs 216| 0 0 -2 -122 54 0 -.17 8 7 | 4 -488 1738 3069
| 18 -6 |
sio 255| 0 3 7 -137 -62 13 -.16 18 16 | --- --- --- ---
| 36 50 |
Table 2.1614.6 GPS week: 1614 Day: 6 MJD: 55548.000
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 236| 0 -1 4 101 -26 2 -.20 8 8 | 484 -1336 16 71
| 34 -12 |
emr 93| 1 4 2 12 35 -6 .42 20 20 | 764 772 14 118
| -28 -88 |
esa 156| 0 -1 0 -45 84 3 .28 9 8 | -439 -758 11 115
| -20 2 |
gfz 193| -3 -1 -4 58 -155 2 -.28 11 10 | 553 -429 22 109
| -118 11 |
grg 136| 0 1 -12 -62 -170 -41 .75 17 15 | -10658 32134 45 197
| 88 -43 |
igr n/a| 0 -1 1 64 -44 -12 -.03 5 5 | 4023 326 15 84
| -49 -1 |
jpl 144| 1 0 10 14 71 51 .59 18 18 | 3306 597 17 100
| 24 53 |
mit 262| 0 1 -5 90 -44 0 -.33 12 10 | 195 -544 20 162
| 8 4 |
ngs 216| 1 0 -2 -120 121 -1 -.21 8 6 | 300 -915 1902 3333
| 24 -15 |
sio 255| 0 3 9 -141 -75 -21 -.14 20 18 | --- --- --- ---
| 56 57 |
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1614.0 GPS week: 1614 Day: 0 MJD: 55542.000
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 | 29 --- --- 18 --- 35 --- 20 31 --- 14 | 22 --- --- 21 --- 28 --- 24 40 --- 23
2 | 6 14 5 9 14 5 19 10 8 29 4 | 25 30 26 21 27 24 34 24 25 29 25
3 | 9 14 5 7 13 5 13 8 9 18 3 | 19 21 25 23 29 20 24 22 25 24 23
4 | 5 11 6 7 13 5 12 15 9 28 4 | 23 24 28 23 30 25 26 22 24 23 26
5 | 7 16 5 9 20 5 15 7 8 15 3 | 26 26 19 13 25 19 26 21 20 22 19
6 | 8 13 4 7 12 4 12 6 6 16 3 | 27 29 33 32 36 29 30 29 30 30 31
7 | 7 17 7 11 19 5 18 9 9 13 4 | 16 26 19 21 30 17 26 19 18 17 17
8 | 7 16 9 8 19 3 14 13 9 18 4 | 12 21 16 15 20 12 23 13 14 12 12
9 | 8 14 4 7 13 4 13 11 10 10 3 | 15 18 15 15 13 13 18 14 17 12 14
10 | 10 20 8 6 15 9 15 17 8 20 4 | 14 26 18 15 21 13 25 21 16 26 17
11 | 6 15 6 10 13 4 12 7 8 22 3 | 36 41 42 44 46 39 37 41 43 31 39
12E | 7 26 9 9 17 4 25 8 10 19 4 | 10 26 19 15 19 11 22 12 13 21 14
13 | 7 19 7 8 24 5 21 9 9 12 4 | 13 25 15 13 33 12 24 14 14 13 13
14 | 8 19 7 13 17 6 19 9 10 17 4 | 19 28 24 12 28 19 27 19 17 21 20
15 | 6 17 5 9 20 4 18 8 12 15 4 | 17 25 19 14 26 16 22 18 21 18 18
16E | 7 29 7 12 11 3 19 11 5 14 4 | 18 32 17 15 17 15 24 20 18 25 18
17 | 10 14 7 17 16 4 18 10 10 27 4 | 22 30 27 33 32 24 32 26 23 29 25
18 | 6 19 6 9 21 8 19 7 16 13 4 | 24 31 22 13 25 23 33 23 29 28 23
19 | 9 18 10 7 10 5 17 12 7 21 4 | 18 26 23 23 24 19 23 23 21 22 19
20 | 6 17 9 10 17 5 15 11 10 16 4 | 20 26 16 14 20 16 26 23 19 27 17
21 | 5 12 5 8 9 5 16 8 10 19 3 | 27 34 29 24 31 25 37 26 29 28 29
22 | 7 12 5 6 25 7 15 7 11 16 3 | 20 21 20 12 30 20 27 18 23 22 19
23 | 9 23 7 10 22 7 18 9 8 12 4 | 15 27 18 9 22 13 23 17 19 17 15
24 | 8 7 5 10 14 4 8 6 9 19 3 | 24 25 29 33 37 26 23 27 28 22 26
X25E | 6 20 6 7 15 4 --- 10 8 --- 3 | 14 22 20 16 27 14 --- 15 19 --- 16
26 | 6 12 7 7 9 4 11 13 9 14 3 | 20 25 21 17 17 19 24 21 24 26 21
27 | 6 15 5 8 12 4 12 8 11 10 3 | 15 21 19 15 13 17 16 16 21 16 17
28E | 7 16 6 6 18 3 15 8 6 11 3 | 12 23 17 12 19 12 23 14 14 16 14
X29 | 6 19 6 9 9 7 20 11 7 --- 3 | 22 27 24 23 19 20 24 23 25 --- 23
30E | 12 18 9 11 19 4 16 21 11 21 5 | 41 37 38 35 38 36 36 46 42 42 37
31 | 7 20 7 8 19 5 20 10 8 18 4 | 20 25 24 16 30 19 27 21 20 23 21
32E | 17 35 9 16 23 5 18 21 13 22 6 | 23 36 24 22 7 24 13 34 24 9 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 10 17 5 16 11 10 18 |T 20 26 22 19 25 19 25 22 22 22 21
WRMS | 7 17 7 9 15 5 15 9 8 17 |NE 20 26 22 19 26 19 26 21 22 22 21
MEDI | 7 17 6 9 16 5 16 9 9 17 |MD 20 26 21 16 26 19 24 21 21 22 19
Table 3.1614.1 GPS week: 1614 Day: 1 MJD: 55543.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 17 --- --- 36 --- 27 --- 18 35 --- 15 | 30 --- --- 31 --- 35 --- 27 52 --- 28
2 | 7 18 5 7 13 5 17 10 7 27 4 | 19 31 24 20 23 20 30 17 20 19 20
3 | 7 15 6 7 15 5 14 8 12 16 3 | 17 18 21 17 25 16 19 16 15 22 16
4 | 7 12 5 5 14 5 11 12 10 27 3 | 18 21 21 16 25 18 19 19 20 23 18
5 | 7 16 7 8 19 3 19 8 8 11 3 | 17 23 20 14 25 14 22 16 15 17 14
6 | 6 17 7 8 14 4 12 8 12 16 3 | 20 21 26 25 29 21 22 20 18 27 21
7 | 8 21 9 11 20 6 18 10 7 13 4 | 20 29 24 21 28 21 25 18 23 21 20
8 | 7 16 7 7 20 6 14 12 9 15 3 | 15 22 21 16 18 16 23 18 17 18 15
9 | 6 15 4 7 9 5 14 10 7 11 3 | 13 16 13 15 14 12 17 16 16 12 12
10 | 9 19 7 9 15 6 16 15 10 18 4 | 13 24 18 16 16 14 24 18 19 23 14
11 | 4 16 5 7 15 4 14 8 8 19 3 | 24 28 26 25 32 24 25 27 23 19 23
12E | 10 25 9 8 20 3 26 7 11 17 4 | 13 25 19 18 23 12 22 15 13 20 13
13 | 7 20 5 6 23 5 19 9 7 13 3 | 16 26 20 12 34 15 24 15 16 14 14
14 | 9 18 7 9 18 7 18 8 10 14 4 | 17 27 21 15 30 16 25 17 20 17 17
15 | 7 25 6 9 19 5 23 8 11 15 4 | 15 26 17 17 27 12 23 15 22 17 14
16E | 7 30 8 12 15 3 22 11 7 13 4 | 17 30 20 15 22 17 24 19 19 23 17
17 | 8 15 7 14 15 4 19 9 7 24 4 | 17 27 24 29 29 19 29 23 20 23 21
18 | 6 21 6 10 17 5 21 8 8 10 3 | 20 30 22 16 25 19 29 19 17 21 17
19 | 6 20 7 7 11 5 21 11 9 22 4 | 17 23 16 13 20 14 24 16 14 17 13
20 | 6 16 6 9 18 5 15 6 8 14 3 | 19 26 17 16 23 18 25 21 19 22 16
21 | 6 13 4 5 9 6 18 10 11 19 3 | 18 25 23 20 26 19 27 20 17 18 18
22 | 9 21 6 9 19 5 21 6 11 10 4 | 18 26 20 9 26 16 28 16 20 16 15
23 | 8 24 8 9 21 6 20 8 9 12 4 | 14 28 20 12 24 14 25 16 17 14 13
24 | 5 11 7 9 15 4 8 5 9 15 3 | 18 18 19 21 23 16 18 19 17 14 16
X25E | 7 18 8 7 15 5 --- 7 10 --- 3 | 15 22 17 17 24 11 --- 12 16 --- 11
26 | 7 12 6 7 12 3 10 10 10 13 3 | 16 19 15 17 19 15 19 19 16 17 14
27 | 6 15 6 7 10 5 11 9 8 11 3 | 14 16 16 14 17 13 13 16 16 13 12
28E | 6 15 5 6 22 4 18 7 11 9 3 | 16 25 22 19 23 18 24 18 26 20 18
X29 | 7 18 11 11 11 5 23 11 10 --- 4 | 17 23 19 22 17 16 24 17 20 --- 16
30E | 11 21 11 13 19 5 17 17 11 20 5 | 34 33 32 36 32 31 31 39 41 33 33
31 | 8 19 9 9 19 4 22 9 10 16 4 | 17 29 24 15 32 17 26 19 22 19 18
X32E | 16 33 9 14 --- 6 --- 18 11 --- 7 | 21 33 21 24 --- 21 --- 30 17 --- 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 9 17 5 18 9 9 16 |T 17 24 20 18 24 17 23 19 20 19 17
WRMS | 7 19 7 8 15 5 18 9 9 15 |NE 17 24 20 17 24 16 23 18 18 18 16
MEDI | 7 18 7 8 15 5 18 9 10 15 |MD 17 25 20 17 24 16 24 18 18 19 16
Table 3.1614.2 GPS week: 1614 Day: 2 MJD: 55544.000
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 | 19 --- --- 31 --- 38 --- 16 22 --- 13 | 31 --- --- 29 --- 31 --- 25 39 --- 27
2 | 6 13 4 11 13 5 16 11 11 26 4 | 20 29 25 21 25 22 32 20 19 20 21
3 | 9 14 6 9 12 8 13 6 12 14 3 | 12 20 19 24 23 16 23 17 21 20 17
4 | 7 10 5 9 12 6 13 13 9 24 4 | 22 24 23 20 28 25 24 23 22 20 23
5 | 7 20 5 12 19 3 21 11 8 12 4 | 17 29 19 14 28 15 31 18 17 16 15
6 | 9 14 5 11 10 6 14 6 9 12 3 | 16 22 24 30 26 21 24 21 22 24 21
7 | 11 17 9 10 25 7 17 8 10 11 4 | 14 28 19 18 27 16 25 16 20 15 14
8 | 8 14 6 5 20 5 14 10 10 12 3 | 11 19 16 15 19 12 23 17 18 16 13
9 | 7 16 5 8 10 7 13 7 8 14 3 | 15 20 15 11 16 13 21 14 17 11 12
10 | 10 24 5 9 12 7 15 11 8 14 4 | 11 29 16 16 19 13 26 16 15 18 12
11 | 9 17 7 10 13 5 17 9 10 15 3 | 27 34 32 34 32 28 29 32 31 21 28
12E | 10 17 6 10 20 5 27 7 9 16 4 | 11 22 15 17 20 11 25 14 14 17 12
13 | 9 20 7 7 26 5 18 10 7 13 4 | 13 25 13 10 34 10 28 11 12 11 10
14 | 8 19 8 6 17 4 18 8 13 14 4 | 10 23 17 15 30 12 23 14 15 15 13
15 | 9 22 6 9 23 5 20 9 6 11 4 | 19 26 22 14 35 17 29 16 18 17 18
16E | 8 29 9 12 16 6 28 9 7 13 4 | 15 32 19 22 23 16 30 15 18 18 16
17 | 11 13 5 11 13 6 19 8 7 23 4 | 19 29 27 27 31 23 31 23 21 21 23
18 | 7 18 6 10 15 4 20 5 11 10 3 | 16 29 19 16 21 17 33 16 16 20 16
19 | 9 17 7 9 9 6 20 10 9 22 4 | 14 23 17 23 20 16 26 17 18 19 15
20 | 6 16 6 8 17 5 14 7 12 11 3 | 18 26 18 14 21 18 30 21 20 24 17
21 | 6 13 7 9 13 6 19 6 10 20 3 | 16 22 19 18 21 17 29 14 18 18 16
22 | 8 14 5 7 17 5 21 4 10 9 3 | 14 22 16 14 25 15 28 12 14 15 13
23 | 8 20 7 8 22 7 19 10 9 12 4 | 12 26 15 10 27 12 26 12 13 12 10
24 | 9 11 7 6 12 6 12 7 12 14 3 | 19 25 26 25 25 23 25 22 25 18 21
X25E | 12 21 8 8 17 6 --- 8 10 --- 4 | 15 24 19 14 24 14 --- 17 18 --- 14
26 | 7 12 6 7 11 4 13 9 6 12 3 | 14 20 16 18 21 14 26 18 14 15 14
27 | 8 15 7 9 12 7 11 9 10 14 3 | 15 20 18 12 18 15 22 16 18 14 13
28E | 6 17 7 8 17 4 21 7 8 9 3 | 16 29 21 15 26 17 29 16 19 14 16
X29 | 7 17 8 12 13 6 22 13 8 --- 4 | 16 23 20 24 17 18 27 19 19 --- 17
30E | 15 19 12 13 23 6 18 16 12 19 5 | 30 28 23 32 31 24 31 31 34 23 26
31 | 10 15 10 11 21 5 17 7 10 12 4 | 15 25 22 18 34 16 28 16 15 16 16
X32E | 9 --- --- --- --- 34 --- --- --- --- 0 | 15 --- --- --- --- 17 --- --- --- --- 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 7 9 17 6 18 9 10 15 |T 16 25 19 19 24 17 27 18 19 17 16
WRMS | 8 17 7 9 16 6 18 8 8 14 |NE 15 24 19 18 24 16 26 17 18 17 16
MEDI | 8 17 6 9 15 6 18 9 10 13 |MD 15 25 19 18 25 16 27 17 18 17 16
Table 3.1614.3 GPS week: 1614 Day: 3 MJD: 55545.000
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 | 31 --- --- 44 --- 59 --- --- --- --- 37 | 32 --- --- 40 --- 44 --- --- --- --- 36
2 | 9 14 7 24 13 5 16 9 7 25 5 | 26 33 33 30 27 30 33 25 28 25 28
3 | 7 19 6 9 12 7 11 8 8 15 3 | 17 28 25 24 26 24 26 21 27 24 23
4 | 7 10 8 6 12 5 10 10 8 22 3 | 21 24 22 17 21 24 19 18 17 18 22
5 | 7 21 8 13 21 3 20 12 5 13 4 | 20 34 27 17 30 23 30 20 21 21 21
6 | 6 15 6 8 11 6 8 8 9 12 3 | 24 32 29 32 31 30 27 28 32 29 28
7 | 6 18 8 13 27 7 16 9 8 13 4 | 22 34 25 21 34 27 26 20 25 20 22
8 | 7 16 9 9 21 7 14 13 7 11 4 | 17 27 21 15 24 23 22 21 15 20 17
9 | 8 16 5 7 13 7 12 7 7 12 3 | 18 26 23 14 19 21 24 20 19 18 18
10 | 9 20 8 8 12 6 15 11 7 12 3 | 18 31 19 16 18 19 24 17 17 20 16
11 | 7 15 7 8 12 6 16 7 10 13 3 | 36 42 42 45 43 40 38 39 40 32 38
12E | 11 21 10 11 19 8 25 8 8 15 4 | 18 28 23 18 28 20 29 18 20 21 18
13 | 10 20 7 12 27 6 19 9 5 14 4 | 20 33 20 16 38 22 26 19 18 21 18
14 | 6 19 7 8 19 6 17 8 6 11 3 | 13 26 20 18 30 17 23 15 19 14 15
15 | 7 21 7 6 22 6 21 9 7 11 4 | 18 25 21 14 31 19 27 18 19 19 18
16E | 5 28 9 11 17 6 24 10 8 11 4 | 19 30 25 23 28 22 26 22 18 24 19
17 | 9 17 11 10 13 5 22 7 8 24 4 | 22 34 28 26 31 28 31 24 26 22 25
18 | 8 20 6 10 19 6 20 7 6 12 3 | 23 33 23 25 26 23 30 22 19 25 21
19 | 7 22 7 7 11 7 20 12 11 22 4 | 18 31 23 20 24 23 27 23 22 22 20
20 | 8 17 8 7 17 7 14 6 8 10 3 | 24 29 19 17 21 20 25 21 22 27 20
21 | 9 15 7 8 13 5 16 5 10 21 3 | 25 29 24 23 28 25 28 22 25 23 22
22 | 10 16 5 8 21 7 19 5 5 11 3 | 18 27 17 21 27 19 27 16 17 18 16
23 | 7 24 7 12 23 7 17 12 7 13 4 | 19 34 21 13 30 19 27 17 17 17 16
24 | 8 11 10 10 10 7 11 6 7 12 3 | 24 32 32 32 32 29 28 27 29 23 27
X25E | 8 24 6 9 15 8 --- 8 10 --- 4 | 25 32 26 16 31 24 --- 21 24 --- 23
26 | 7 12 6 7 12 5 11 10 9 10 3 | 21 29 26 19 23 24 28 23 24 22 22
27 | 8 17 7 8 15 8 10 9 8 13 3 | 16 25 22 14 18 19 20 20 19 21 18
28E | 8 14 9 7 18 7 19 9 8 9 3 | 24 36 31 25 31 26 34 27 28 27 26
X29 | 7 18 9 9 13 8 24 12 9 --- 4 | 22 29 30 25 24 25 29 25 22 --- 24
30E | 14 18 10 13 23 8 18 15 10 18 5 | 34 35 32 36 36 34 28 34 32 30 30
31 | 9 18 7 8 20 6 19 7 9 8 3 | 17 28 23 18 35 20 27 18 17 17 18
X32 | 13 19 7 14 23 8 20 11 7 --- 5 | 19 24 17 18 20 21 24 18 14 --- 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 10 18 6 17 9 8 15 |T 21 30 24 22 27 24 27 21 22 22 21
WRMS | 8 18 8 9 17 6 17 8 7 13 |NE 20 30 24 21 27 23 26 21 22 21 21
MEDI | 8 18 7 9 17 7 17 9 8 12 |MD 20 30 23 19 28 23 27 21 21 21 21
Table 3.1614.4 GPS week: 1614 Day: 4 MJD: 55546.000
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 | 33 --- --- --- --- 36 --- 33 32 --- 23 | 44 --- --- --- --- 48 --- 33 58 --- 38
2 | 7 16 9 11 12 5 19 9 10 24 4 | 23 31 31 22 27 28 31 23 29 25 27
3 | 9 19 6 8 15 5 16 9 7 22 4 | 16 25 19 20 26 19 22 18 18 22 19
4 | 9 12 8 10 12 3 11 11 10 20 4 | 14 26 28 26 29 18 22 21 22 20 18
5 | 11 22 6 11 19 3 17 14 8 14 4 | 14 27 14 13 28 15 23 22 18 19 14
6 | 8 16 5 8 14 5 13 10 7 18 3 | 20 28 25 25 32 24 24 25 22 27 24
7 | 8 18 10 10 23 6 21 9 8 14 4 | 18 29 21 17 34 19 27 18 17 17 18
8 | 9 16 7 12 17 5 14 14 12 11 4 | 13 23 15 15 19 16 19 19 19 16 15
9 | 7 16 7 12 11 5 15 10 7 16 3 | 17 25 17 15 16 17 20 16 22 15 18
10 | 11 22 10 8 15 3 17 15 9 13 4 | 15 30 22 15 18 17 24 19 19 22 17
11 | 8 17 5 11 12 5 17 8 8 13 3 | 30 36 33 39 37 32 30 36 30 28 31
12E | 12 22 7 10 18 6 26 10 14 18 5 | 21 28 22 19 27 21 24 17 28 24 23
13 | 8 18 7 10 24 3 21 7 10 12 4 | 16 26 16 14 35 13 24 15 14 14 14
14 | 5 21 5 13 18 5 17 7 7 10 3 | 17 28 23 14 33 19 26 17 19 20 20
15 | 6 22 6 11 17 5 19 14 6 11 4 | 13 23 15 12 26 12 19 15 12 15 12
16E | 5 24 9 11 14 6 22 10 14 17 4 | 16 27 20 23 26 18 27 18 18 22 18
17 | 13 14 9 15 13 5 24 9 10 26 5 | 15 28 24 28 29 22 30 21 21 23 20
18 | 7 23 5 11 18 3 23 7 6 12 4 | 15 33 21 22 26 21 31 18 19 22 20
19 | 10 21 6 9 13 5 22 12 12 23 4 | 17 26 18 19 19 17 24 23 19 20 18
20 | 8 20 8 12 17 4 16 9 9 10 4 | 19 30 21 15 20 18 25 22 21 24 18
21 | 8 14 8 16 11 5 16 5 8 22 4 | 16 24 24 26 23 19 26 20 23 19 21
22 | 6 13 6 21 21 5 19 8 7 13 4 | 12 20 19 26 29 18 23 15 15 18 15
23 | 9 25 7 11 21 6 19 16 9 14 4 | 14 28 16 15 27 12 22 18 13 14 12
24 | 11 12 4 14 13 5 13 6 6 12 3 | 21 26 21 30 24 21 19 24 18 18 21
X25E | 12 23 7 10 16 6 --- 11 13 --- 5 | 20 28 22 15 27 18 --- 17 24 --- 20
26 | 8 13 7 12 11 5 15 12 7 10 3 | 18 23 15 18 16 17 21 21 20 16 16
27 | 8 15 5 12 10 4 13 11 7 15 3 | 15 20 16 13 16 16 18 18 22 18 17
28E | 8 12 8 11 19 4 23 11 9 12 4 | 17 27 21 16 25 19 25 20 21 22 21
X29 | 8 18 8 9 12 7 23 14 13 --- 4 | 21 26 21 18 21 20 25 22 23 --- 21
30E | 13 19 7 14 18 5 17 14 11 16 4 | 25 28 22 25 26 22 23 26 26 20 21
31 | 12 19 8 12 18 4 21 9 11 10 4 | 18 27 21 20 32 20 28 18 18 16 19
32 | 12 21 7 16 18 5 17 12 10 21 4 | 11 23 15 19 14 12 18 17 9 16 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 7 12 16 5 18 11 9 16 |T 18 26 20 19 25 19 24 20 21 19 19
WRMS | 9 18 7 12 15 5 18 10 8 15 |NE 17 26 20 19 25 18 24 20 19 19 18
MEDI | 8 18 7 11 16 5 17 10 9 14 |MD 17 27 21 19 26 18 24 19 19 20 18
Table 3.1614.5 GPS week: 1614 Day: 5 MJD: 55547.000
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 | 29 --- --- 34 --- 30 --- 32 35 --- 18 | 60 --- --- 36 --- 51 --- 40 68 --- 54
2 | 6 15 6 9 13 5 20 11 7 26 4 | 18 25 25 29 26 21 29 18 20 19 20
3 | 6 17 4 12 13 5 15 12 9 29 4 | 13 19 15 11 20 14 21 16 13 27 13
X4 | 9 --- --- --- --- 22 --- --- --- --- 0 | 7 --- --- --- --- 21 --- --- --- --- 8
5 | 7 20 9 9 20 4 18 18 8 18 4 | 15 24 15 15 28 13 23 21 13 20 11
6 | 6 17 3 11 14 5 14 12 8 25 4 | 16 23 19 18 24 18 23 20 18 28 18
7 | 10 23 10 10 19 5 19 14 8 17 4 | 22 29 21 19 29 19 25 17 17 16 17
8 | 6 14 7 11 18 5 15 13 9 10 3 | 11 19 11 18 18 11 20 13 12 13 9
9 | 9 15 6 9 10 6 16 10 7 15 3 | 14 18 11 12 14 11 17 13 12 10 10
10 | 8 23 7 7 15 7 16 15 8 13 4 | 13 27 20 18 19 14 22 15 12 21 14
11 | 5 16 6 8 15 2 18 10 6 17 3 | 23 27 23 28 29 25 20 29 24 21 22
12E | 8 18 9 8 23 7 28 10 9 15 4 | 12 21 16 15 27 12 23 14 14 15 12
13 | 5 22 6 11 25 5 21 11 8 13 4 | 14 28 18 16 35 14 26 13 16 13 13
14 | 7 23 8 6 15 5 20 8 7 11 3 | 14 25 20 14 29 14 24 17 14 15 15
15 | 7 26 6 6 20 4 19 16 10 13 4 | 13 25 14 11 30 9 21 13 13 12 10
16E | 5 25 7 17 12 6 24 9 9 18 4 | 13 25 19 20 17 15 28 15 16 21 16
17 | 6 17 9 12 16 6 22 8 6 28 4 | 14 26 23 24 27 18 29 20 18 22 18
18 | 7 23 6 8 16 4 23 10 5 14 4 | 23 33 23 19 25 23 32 23 22 27 21
19 | 6 20 5 10 11 4 25 14 10 26 4 | 12 22 14 18 19 12 26 19 15 15 12
20 | 5 19 6 10 18 5 17 9 7 11 3 | 15 24 14 14 18 15 22 19 15 20 12
21 | 5 15 5 7 10 7 18 7 7 25 3 | 24 26 25 21 22 25 30 23 25 28 23
22 | 6 18 5 10 17 6 19 6 7 13 3 | 16 25 17 10 24 17 26 14 17 19 13
23 | 9 25 9 13 22 4 21 17 9 17 5 | 12 26 17 14 26 11 22 15 10 13 10
24 | 5 12 5 8 12 4 15 7 8 14 3 | 18 22 18 23 23 18 16 20 18 16 16
X25E | 5 22 8 7 11 4 --- 12 11 --- 4 | 12 24 17 14 24 12 --- 13 15 --- 12
26 | 8 11 7 9 10 5 14 17 7 13 3 | 17 22 17 20 21 15 24 20 15 13 14
27 | 8 17 5 10 10 6 15 13 6 17 3 | 14 20 12 12 15 12 19 14 12 14 11
28E | 7 15 5 9 16 4 23 10 7 13 3 | 20 27 23 19 27 17 28 19 17 20 19
X29 | 6 21 8 8 10 5 25 14 8 --- 4 | 17 27 19 22 18 18 24 21 17 --- 18
30E | 13 21 7 13 15 6 17 17 8 19 4 | 38 37 35 38 32 34 32 39 38 32 34
31 | 6 19 11 8 16 5 22 11 8 10 4 | 15 23 24 15 31 13 27 21 14 14 15
32 | 12 23 8 12 13 4 17 11 10 20 4 | 11 21 17 15 13 12 19 17 13 13 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 10 16 5 19 12 8 18 |T 17 24 18 18 23 17 24 19 18 18 16
WRMS | 7 19 7 9 17 5 19 11 7 16 |NE 15 24 18 17 23 16 23 18 15 18 14
MEDI | 6 19 6 9 15 5 19 11 8 15 |MD 14 25 18 18 24 15 24 18 15 16 14
Table 3.1614.6 GPS week: 1614 Day: 6 MJD: 55548.000
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 | 21 --- --- --- --- 54 --- 26 22 --- 16 | 52 --- --- --- --- 55 --- 25 57 --- 48
X2 | 6 14 8 --- 11 6 17 11 9 28 4 | 27 33 34 --- 32 28 38 27 31 31 30
3 | 6 16 8 8 15 5 13 8 8 34 4 | 17 24 23 21 29 19 25 22 19 31 21
X4 | 7 12 8 --- 14 8 11 12 7 18 4 | 7 11 3 --- 5 9 9 3 4 4 7
5 | 9 20 11 20 20 7 19 16 7 18 5 | 18 28 16 22 30 14 28 19 18 20 16
6 | 7 20 10 6 13 3 11 10 8 31 4 | 22 32 30 29 35 27 28 31 25 34 27
7 | 9 19 12 8 22 4 21 11 10 17 4 | 21 27 24 19 27 18 27 17 22 15 19
8 | 8 16 6 9 18 6 14 10 10 16 3 | 15 21 12 15 19 12 22 14 19 14 14
9 | 8 16 6 7 12 5 12 9 8 15 3 | 15 22 17 16 18 13 21 14 18 12 13
10 | 8 20 8 9 14 5 14 12 9 16 4 | 16 24 15 17 20 13 22 17 18 23 14
11 | 5 17 7 10 13 4 15 10 7 24 4 | 39 43 41 46 48 40 37 44 42 35 39
12E | 8 18 8 14 20 5 28 8 10 14 4 | 11 22 20 21 19 15 29 14 21 16 17
13 | 6 21 8 10 25 6 22 7 8 12 4 | 13 24 14 14 32 8 25 10 13 11 10
14 | 6 21 9 10 15 5 17 13 6 13 4 | 17 26 21 17 29 16 27 17 20 18 17
15 | 9 21 9 9 18 2 17 12 8 13 4 | 14 26 16 18 32 14 22 14 17 16 15
16E | 5 31 8 10 15 3 21 9 7 15 4 | 19 30 20 19 24 15 30 18 16 20 15
17 | 12 18 10 18 14 5 21 7 7 32 5 | 22 29 24 29 33 23 31 24 23 33 23
18 | 8 21 8 7 16 4 22 10 7 15 4 | 26 30 22 19 21 21 33 25 22 28 20
19 | 7 21 7 9 10 3 23 15 11 26 4 | 20 29 22 18 26 19 31 25 23 19 20
20 | 7 17 5 11 20 6 20 11 7 14 4 | 19 24 16 20 22 16 27 22 18 26 17
21 | 7 15 6 7 8 5 16 6 5 26 3 | 26 26 22 26 25 25 30 24 24 29 22
22 | 6 17 7 8 16 3 15 5 5 13 3 | 17 24 18 15 25 15 28 16 17 22 15
23 | 6 25 11 10 23 5 22 17 10 17 5 | 11 27 15 12 26 9 25 16 9 13 9
24 | 8 12 5 13 12 4 11 8 10 18 3 | 23 25 23 29 29 23 25 24 26 19 22
X25E | 9 23 7 6 16 6 --- 11 10 --- 4 | 20 25 21 17 24 15 --- 16 21 --- 19
26 | 9 12 8 13 9 5 12 14 8 19 4 | 16 23 19 27 23 16 24 17 17 24 16
X27 | 7 20 6 10 13 5 --- 8 9 14 3 | 14 24 16 17 19 12 --- 14 16 12 13
28E | 8 15 9 14 19 5 23 12 12 14 4 | 13 23 17 18 25 12 25 17 17 16 14
X29 | 9 20 9 10 11 3 25 10 11 --- 4 | 24 33 28 33 26 26 32 28 30 --- 28
30E | 16 22 12 15 24 4 17 21 11 18 6 | 40 37 36 38 33 33 33 35 41 33 35
31 | 11 21 9 14 20 5 17 15 6 14 4 | 18 26 22 18 32 16 27 22 14 17 16
32 | 12 24 10 12 17 4 17 13 9 21 4 | 11 22 16 18 14 11 20 17 15 17 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 9 11 17 5 18 12 8 20 |T 20 26 20 21 25 19 26 20 21 20 19
WRMS | 8 19 8 10 15 5 18 10 6 18 |NE 19 26 20 21 26 18 26 20 20 21 18
MEDI | 8 20 8 10 15 5 17 11 8 17 |MD 18 26 20 19 26 16 27 17 19 19 17
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 4.1614 GPS week: 1614 MJD: 55542.0-55548.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 |U 7 6 19 |U 13 30 51 |U 26 12 60 |
emr | emr 2943 |U 9 11 25 |U 16 30 54 | 25 10 60 |
esa | esa 2948 | 8 9 22 |U 12 28 52 | 27 11 57 |
gfz | gfz 2973 |U 9 10 25 |U 18 27 72 |U 26 11 58 |
grg | grg 2934 | 10 10 26 |U 13 29 54 | 23 17 211 |
igr | igr 2957 | 8 8 20 | 14 14 54 | 26 11 58 |
igs | igs 2911 | 8 9 20 | 38 42 146 | 25 11 61 |
jpl | jpl 2818 |U 11 13 32 | 13 31 57 |U 23 17 195 |
mit | mit 3030 |U 8 9 21 |U 12 30 58 |U 27 12 59 |
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 5.1614.0 GPS week: 1614 Day: 0 MJD: 55542.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 8 7 20 | 15 125 46 | 34 22 135 |
emr | emr 2968 | 9 11 22 | 31 137 39 | 29 18 136 |
esa | esa 2976 | 7 9 19 | 14 120 45 | 29 18 123 |
gfz | gfz 3059 | 7 9 25 | 26 93 111 | 32 23 142 |
grg | grg 2976 | 7 10 22 | 14 121 41 | 32 18 151 |
igr | igr 2988 | 7 9 21 | 28 26 53 | 27 17 125 |
igs | igs 2905 | 7 9 19 | 194 220 694 | 28 25 155 |
jpl | jpl 2871 | 10 10 21 | 18 131 46 | 31 26 118 |
mit | mit 3072 | 7 8 18 | 15 133 53 | 36 26 142 |
Table 5.1614.1 GPS week: 1614 Day: 1 MJD: 55543.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 8 7 20 | 11 16 35 | 115 20 196 |
emr | emr 2970 | 11 9 30 | 13 15 42 | 109 18 191 |
esa | esa 2976 | 8 8 24 | 11 13 35 | 122 20 200 |
gfz | gfz 3061 | 8 9 22 | 12 15 41 | 114 10 179 |
grg | grg 2880 | 12 11 28 | 12 12 39 | 88 47 1240 |
igr | igr 2972 | 8 8 25 | 13 13 40 | 121 20 207 |
igs | igs 2944 | 8 8 22 | 11 14 37 | 113 16 198 |
jpl | jpl 2779 | 12 9 28 | 13 14 50 | 83 51 1156 |
mit | mit 3072 | 7 9 21 | 13 15 58 | 116 17 192 |
Table 5.1614.2 GPS week: 1614 Day: 2 MJD: 55544.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 5 5 14 | 19 16 58 | 8 14 24 |
emr | emr 2876 | 8 8 26 | 18 13 78 | 10 9 18 |
esa | esa 2880 | 7 8 19 | 18 14 65 | 8 9 14 |
gfz | gfz 2949 | 6 8 20 | 22 13 93 | 7 9 14 |
grg | grg 2880 | 8 10 20 | 20 15 66 | 9 13 16 |
igr | igr 2912 | 7 8 16 | 18 14 68 | 7 9 12 |
igs | igs 2841 | 6 7 16 | 18 13 67 | 8 9 13 |
jpl | jpl 2779 | 8 10 21 | 16 15 79 | 10 9 17 |
mit | mit 2976 | 6 8 19 | 14 13 68 | 9 11 20 |
Table 5.1614.3 GPS week: 1614 Day: 3 MJD: 55545.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 6 6 17 | 12 7 53 | 9 6 16 |
emr | emr 2972 | 10 12 29 | 12 10 51 | 6 8 19 |
esa | esa 2976 | 7 8 19 | 11 9 52 | 9 10 16 |
gfz | gfz 3055 | 7 9 21 | 15 12 54 | 10 12 21 |
grg | grg 2976 | 8 9 21 | 11 11 57 | 10 14 20 |
igr | igr 3002 | 7 8 18 | 11 8 55 | 8 9 15 |
igs | igs 2945 | 7 8 18 | 12 9 57 | 8 8 15 |
jpl | jpl 2876 | 9 12 26 | 12 11 46 | 10 9 21 |
mit | mit 2976 | 7 8 18 | 13 8 57 | 8 11 13 |
Table 5.1614.4 GPS week: 1614 Day: 4 MJD: 55546.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3044 | 9 5 25 | 12 13 45 | 7 6 18 |
emr | emr 2972 | 11 11 24 | 13 10 44 | 7 7 16 |
esa | esa 2976 | 11 10 27 | 12 10 47 | 7 9 18 |
gfz | gfz 2972 | 12 10 27 | 17 12 63 | 6 7 16 |
grg | grg 2976 | 14 10 31 | 13 10 48 | 8 10 21 |
igr | igr 2952 | 11 8 25 | 13 10 46 | 6 8 17 |
igs | igs 2938 | 10 9 26 | 12 11 46 | 6 7 17 |
jpl | jpl 2865 | 16 19 42 | 13 11 47 | 7 6 15 |
mit | mit 3072 | 11 10 27 | 13 12 47 | 7 8 15 |
Table 5.1614.5 GPS week: 1614 Day: 5 MJD: 55547.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 7 5 19 | 10 13 41 | 7 7 21 |
emr | emr 2876 | 9 10 24 | 10 13 37 | 7 5 20 |
esa | esa 2880 | 8 9 21 | 8 12 37 | 7 7 17 |
gfz | gfz 2946 | 10 12 28 | 12 19 43 | 6 5 17 |
grg | grg 2880 | 11 12 29 | 8 13 38 | 8 9 19 |
igr | igr 2910 | 7 8 18 | 8 12 35 | 6 7 18 |
igs | igs 2876 | 8 8 19 | 7 10 35 | 7 7 19 |
jpl | jpl 2777 | 9 14 31 | 10 13 39 | 10 8 18 |
mit | mit 2976 | 8 11 24 | 9 12 35 | 6 6 14 |
Table 5.1614.6 GPS week: 1614 Day: 6 MJD: 55548.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 6 8 18 | 11 19 79 | 5 8 13 |
emr | emr 2972 | 9 14 24 | 14 16 86 | 8 5 19 |
esa | esa 2976 | 8 11 24 | 11 17 86 | 6 6 13 |
gfz | gfz 2772 | 11 17 36 | 21 27 98 | 8 9 17 |
grg | grg 2976 | 9 12 28 | 11 22 86 | 7 7 14 |
igr | igr 2967 | 7 9 20 | 11 18 83 | 5 5 13 |
igs | igs 2931 | 7 11 21 | 12 18 89 | 5 5 12 |
jpl | jpl 2779 | 13 20 57 | 12 21 89 | 8 8 17 |
mit | mit 3072 | 7 11 19 | 11 20 86 | 6 7 14 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1614 GPS week: 1614 MJD: 55542.500-55548.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -7 -19 -18 65 -1 | -1 11
| 20 22 89 107 3 | 2
emr uuuuu | 39 3 138 -60 -10 | 22 25
| 27 14 99 129 5 | 2
esa uuuuu | -17 4 68 -15 1 | -5 12
| 18 16 30 98 4 | 2
gfz uuuuu | 12 62 -6 -22 0 | -4 11
| 15 33 36 51 5 | 3
grg uuuux | -10 -47 121 34 -1 | 1 13
| 58 25 63 75 15 | 3
igr xxxxx | 17 40 58 -98 3 | -2 10
| 20 30 153 64 9 | 1
irf xxxxx | 13 -1 -38 24 3 | -4 12
| 25 17 69 45 5 | 4
jpl uuuuu | 49 -19 -39 177 -6 | 10 16
| 79 44 150 110 6 | 2
mit uuuuu | 14 2 -146 74 5 | 14 18
| 38 20 86 58 7 | 4
ngs uuuuu | -19 -7 -15 -123 3 | -11 14
| 57 50 56 87 5 | 1
sio uuuuu | -31 -60 -52 33 -1 | 13 17
| 38 26 176 80 6 | 1
Table 7.1614.0 GPS week: 1614 Day: 0 MJD: 55542.500
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 -39 -60 -22 -3 | -4 12
emr uuuuu | 33 20 -22 -110 -12 | 24 27
esa uuuuu | -24 -27 59 95 4 | -9 16
gfz uuuuu | 14 52 17 21 9 | -10 17
grg uuuux | 57 -67 138 119 -7 | 2 19
igr xxxxx | 35 38 -90 -105 -7 | -4 10
irf xxxxx | -21 -14 -53 -30 6 | -10 16
jpl uuuuu | 21 44 6 218 -12 | 13 17
mit uuuuu | -37 -2 -182 3 8 | 8 13
ngs uuuuu | 42 22 -3 -265 -3 | -13 15
sio uuuuu | -74 -91 71 -44 -6 | 13 16
Table 7.1614.1 GPS week: 1614 Day: 1 MJD: 55543.500
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 | -13 -36 88 -80 0 | -3 12
emr uuuuu | 29 -11 19 -184 -16 | 24 26
esa uuuuu | -32 -3 44 143 -1 | -7 13
gfz uuuuu | 26 13 14 -75 4 | -7 13
grg uuuux | 45 -29 55 147 -5 | -1 18
igr xxxxx | 32 24 -65 -134 -6 | -4 11
irf xxxxx | -5 -23 23 -8 6 | -9 13
jpl uuuuu | 61 7 -123 136 -5 | 11 17
mit uuuuu | -11 -18 -74 49 6 | 9 13
ngs uuuuu | 3 62 -32 -204 -2 | -12 15
sio uuuuu | -62 -90 130 -55 -2 | 11 16
Table 7.1614.2 GPS week: 1614 Day: 2 MJD: 55544.500
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 | -15 -4 101 180 0 | -1 11
emr uuuuu | 4 -15 173 -172 -15 | 24 26
esa uuuuu | -47 8 43 -21 -6 | -6 12
gfz uuuuu | 15 42 -38 -3 1 | -4 11
grg uuuux | -38 -30 18 43 -1 | -4 15
igr xxxxx | -12 2 40 -179 -3 | -3 10
irf xxxxx | 17 -6 45 79 8 | -6 12
jpl uuuuu | 183 -86 -279 49 -9 | 11 17
mit uuuuu | 19 -2 -21 125 12 | 12 15
ngs uuuuu | -18 35 -39 -125 2 | -11 14
sio uuuuu | -25 -68 133 89 6 | 11 16
Table 7.1614.3 GPS week: 1614 Day: 3 MJD: 55545.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -6 18 -17 203 1 | 0 11
emr uuuuu | 34 1 174 -169 -9 | 23 25
esa uuuuu | 3 23 104 -79 2 | -5 12
gfz uuuuu | 34 48 17 -56 -6 | -3 11
grg uuuux | -93 -37 171 -31 -5 | 1 10
igr xxxxx | 37 41 300 -162 2 | -2 10
irf xxxxx | 50 13 21 83 7 | -3 12
jpl uuuuu | 97 -39 -127 75 -8 | 11 17
mit uuuuu | 70 16 -89 175 10 | 14 19
ngs uuuuu | -121 -32 -103 -73 2 | -10 14
sio uuuuu | 17 -50 -3 153 8 | 11 16
Table 7.1614.4 GPS week: 1614 Day: 4 MJD: 55546.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 19 -27 -117 61 -1 | 1 11
emr uuuuu | 25 6 244 24 -6 | 22 25
esa uuuuu | -7 10 37 -77 1 | -3 10
gfz uuuuu | 9 76 -11 -28 0 | -2 9
grg uuuux | -60 -45 195 14 9 | 0 9
igr xxxxx | 26 100 175 -17 17 | -2 10
irf xxxxx | 41 29 -69 47 3 | -1 11
jpl uuuuu | 59 17 186 329 -7 | 10 16
mit uuuuu | 56 41 -186 71 5 | 17 21
ngs uuuuu | -69 -84 -32 -124 3 | -9 13
sio uuuuu | 23 -18 -187 93 0 | 14 18
Table 7.1614.5 GPS week: 1614 Day: 5 MJD: 55547.500
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 | -4 -9 -5 -6 -4 | 1 11
emr uuuuu | 60 -6 201 55 -12 | 21 23
esa uuuuu | -10 1 80 -45 4 | -3 10
gfz uuuuu | 1 91 29 -74 -1 | -1 8
grg uuuux | -20 -30 129 4 26 | 2 9
igr xxxxx | -2 34 138 -53 11 | -1 11
irf xxxxx | 9 -3 -110 3 -1 | 0 10
jpl uuuuu | -27 -49 29 306 -11 | 9 16
mit uuuuu | 8 -9 -261 56 -1 | 19 22
ngs uuuuu | 15 -21 32 -40 9 | -9 13
sio uuuuu | -41 -39 -254 -21 -3 | 15 18
Table 7.1614.6 GPS week: 1614 Day: 6 MJD: 55548.500
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 | 10 -40 -119 120 4 | -1 11
emr uuuuu | 86 22 177 133 0 | 18 22
esa uuuuu | -4 14 111 -124 5 | -5 10
gfz uuuuu | -13 112 -69 59 -6 | -2 9
grg uuuux | 41 -94 140 -57 -20 | 4 10
igr xxxxx | -1 43 -95 -36 7 | -1 11
irf xxxxx | -2 -6 -126 -4 -6 | -1 11
jpl uuuuu | -55 -30 35 127 7 | 6 15
mit uuuuu | -6 -14 -211 37 -7 | 18 21
ngs uuuuu | 13 -30 73 -29 8 | -10 14
sio uuuuu | -59 -62 -257 18 -9 | 13 17
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