[IGSREPORT-16955] Wk 1509 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 25 06:16:09 PST 2008
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IGS Electronic Report 25 Dec 06:16:18 PST 2008 Message Number 16955
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1509 (Dec 07, 2008 - Dec 13, 2008)
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 (weights are those from the orbit combination).
Pole rate combination uses only centres providing estimated pole rates.
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:
igs1509[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1509[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1509[0-6].cls IGS GPS clock combination summary report.
igs15097.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15097.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 1478, a new solution from CNES/GRGS (GRG) is included for
evaluation and statistics only.
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.
Day | Centre | PRN/STA list
----+--------+---------------
0 | EMR | MIZU
0 | ESA | 8 SCH2
0 | GFZ | 7 13 31 CHUR
0 | JPL | 9 19 27
0 | MIT | 9 13
1 | COD | NISU TOW2
1 | EMR | 32 DAEJ MIZU
1 | ESA | 8
1 | GFZ | 7 8 31 ANKR DAEJ HARB NISU
1 | JPL | 9 27 MCM4
1 | MIT | 9
2 | COD | 8
2 | EMR | 32 MIZU
2 | ESA | 8 19
2 | GFZ | 7 8 13 19 31 KOKB
2 | JPL | 8 19
2 | MIT | HARB
3 | COD | WHIT
3 | EMR | 32 DAEJ MIZU
3 | ESA | 21 WHIT
3 | GFZ | 7 22 29 GOLD
3 | JPL | 8 21 32
3 | MIT | NRC1
4 | ALL | 13
4 | EMR | 21 32 MIZU
4 | ESA | 32
4 | GFZ | 7 21 29 31 32 DARW HYDE IRKT WHIT
4 | JPL | 8 32 BOR1 HYDE
4 | MIT | 8 BOR1 HYDE KOKB
5 | ALL | 10
5 | EMR | 32 MATE MIZU
5 | ESA | 32 KHAJ
5 | GFZ | 7 29 31
5 | JPL | 8
5 | MIT | 8 21 ALIC DARW MAW1
6 | COD | 21 FAA1
6 | EMR | 32 MIZU
6 | ESA | 21 32
6 | GFZ | 7 29 31 DAEJ DARW HARB IRKT MATE THTI
6 | JPL | 32 ZWE2
6 | MIT | CHUR DAEJ HARB
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
----+------------+----------
G13 | 2008_12_11 | 2008143
G13 | 2008_12_12 | 2008143
6. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
5 | ESA | 10
7. 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.
8. Small rotations were applied to the all AC orbit and ERP values in order
to align them to the IGS05. These rotations were estimated in the process
of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based
on the common stations between the individual AC SINEX solutions and the
IGS05.snx SINEX. 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 -21 -34 1 .19
EMR | 12.0 -.3 -1.3 139 -42 3 .34
ESA | 4.8 2.8 -7.4 15 -120 45 .15
GFZ | .9 .7 1.1 16 -32 8 -.15
GRG | 8.5 -.2 -4.4 -35 -17 7 -.04
JPL | 3.4 4.9 6.2 11 41 13 .31
MIT | 2.7 .0 -4.1 15 -11 5 -.02
NGS | 8.4 -4.2 -7.8 -50 -189 60 .16
SIO | 3.1 3.8 -3.6 63 -99 2 .36
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by NRCan. For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting 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 1.1509.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1509.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 2.1509.[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 3.1509.[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 5.1509.0-6).
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 1509 summary. (Dec 07, 2008 - Dec 13, 2008)
Table 1.1509.a GPS week: 1509 MJD: 54807.000-54813.000
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 243| 0 1 0 53 -25 -55 -.21 11 9 | -246 -173 15 129
| 0 0 1 9 13 29 .02 | 468 739
emr 72| 1 0 4 -210 -14 -53 .43 20 20 | 344 -111 19 253
| 1 1 0 32 34 15 .06 | 1932 2267
esa 137| 1 -1 -1 -13 18 -18 .30 19 11 | 361 -49 21 112
| 0 1 2 28 41 23 .04 | 1679 1100
gfz 202| 0 0 -2 -19 -38 162 -.11 10 10 | 24 -9 25 135
| 0 1 1 15 16 78 .03 | 507 934
grg 81| 3 2 11 116 -67 -106 1.13 46 45 | -264 -181 113 364
| 2 1 3 38 25 56 .06 | 464 735
igr n/a| 0 0 0 20 -84 -66 .07 6 6 | 5044 944 24 78
| 0 0 1 14 16 16 .02 | 2507 1988
jpl 130| -1 0 2 0 -167 -20 .52 18 17 | 1433 -141 22 119
| 1 1 1 17 15 26 .03 | 1767 2028
mit 277| 0 -1 0 -25 -125 -19 -.30 15 14 | -276 360 21 158
| 1 0 1 65 53 24 .03 | 461 634
ngs 236| 0 0 0 141 249 -80 -.28 13 10 | -195 -237 2375 4065
| 0 1 0 54 57 21 .04 | 453 738
sio 109| -1 2 1 -102 105 -32 .02 26 23 | --- --- --- ---
| 0 2 1 20 45 25 .02 | --- ---
Table 1.1509.b GPS week : 1509 MJD: 54807.000-54813.000
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 | 6 6 6 7 6 6 6 |
3 | 5 5 5 5 5 5 5 |
4 | 4 5 5 5 4 5 4 |
5 | 4 4 4 5 5 5 4 |
6 | 5 4 5 5 4 5 5 |
7 | 5 5 5 6 5 5 5 |
8 | 7 6 7 7 7 7 6 |
9 | 7 7 7 7 7 6 7 |
10 | 6 6 6 6 6 8 7 |
11 | 4 5 5 5 5 5 5 |
12 | 6 6 6 5 6 6 5 |
13 | 5 5 5 5 15 0 5 |
14 | 5 5 6 6 6 6 5 |
15 | 5 6 6 6 6 6 6 |
16 | 6 6 6 7 6 6 5 |
17 | 6 6 7 8 8 8 7 |
18 | 5 6 5 5 5 5 6 |
19 | 4 4 5 5 5 5 5 |
20 | 5 5 5 5 5 6 5 |
21 | 5 5 5 6 5 6 5 |
22 | 5 5 5 6 5 5 6 |
23 | 6 6 6 6 5 6 5 |
24 | 4 4 4 4 4 4 4 |
25 | 6 6 6 7 6 5 5 |
26 | 5 5 5 5 5 5 5 |
27 | 7 7 8 7 5 6 5 |
28 | 5 5 6 6 6 6 6 |
29 | 4 4 4 4 4 5 4 |
30 | 4 4 4 4 4 5 4 |
31 | 5 5 5 5 6 6 6 |
32 | 9 7 7 7 7 7 6 |
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 2.1509.0 GPS week: 1509 Day: 0 MJD: 54807.000
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 243| 0 1 1 63 -35 -5 -.18 11 9 | -373 795 19 126
| -24 -48 |
emr 72| 0 -1 6 -218 -20 -60 .49 20 20 | 3614 -3241 20 284
| -21 -54 |
esa 137| 2 0 -2 -18 51 8 .34 12 11 | -239 -515 21 109
| 30 -38 |
gfz 202| 0 1 -3 -9 -42 120 -.11 9 9 | 234 -80 22 124
| -38 -17 |
grg 81| 1 0 7 157 -75 -192 1.15 51 47 | -386 790 124 331
| -70 32 |
igr n/a| 0 0 1 22 -88 -82 .11 8 7 | 4945 -1719 27 80
| -47 -11 |
jpl 130| -2 0 0 -1 -144 -16 .51 19 17 | 4608 -2928 21 129
| -41 -116 |
mit 277| -1 -1 0 -49 -100 -34 -.32 14 12 | 285 -173 21 196
| 26 18 |
ngs 236| 0 1 1 165 237 -97 -.29 13 10 | -416 804 2317 3814
| -28 19 |
sio 109| -2 0 0 -108 65 -38 .02 26 23 | --- --- --- ---
| 84 -31 |
Table 2.1509.1 GPS week: 1509 Day: 1 MJD: 54808.000
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 243| 0 1 1 52 -42 -100 -.21 10 9 | 325 -1406 19 156
| 22 -30 |
emr 72| -1 0 3 -250 -32 -31 .48 19 19 | -250 -1558 17 253
| 26 -63 |
esa 137| 0 -2 -1 14 9 0 .26 10 9 | -56 -142 23 118
| -26 -33 |
gfz 202| -1 1 -2 -36 -38 127 -.12 10 10 | 583 -1394 27 140
| 35 -19 |
grg 81| 7 3 10 141 -94 -160 1.05 47 44 | 305 -1407 111 296
| 82 48 |
igr n/a| 0 0 0 -1 -85 -46 .06 6 6 | 2586 -391 24 83
| -6 -21 |
jpl 130| 0 1 2 2 -165 11 .52 17 16 | 1082 -1403 26 127
| 1 -37 |
mit 277| -1 -1 0 39 -103 -1 -.35 16 13 | -319 42 19 160
| 15 3 |
ngs 236| 1 1 0 75 252 -45 -.34 12 9 | 303 -1398 2590 3682
| 33 -106 |
sio 109| 0 0 0 -72 81 -8 .02 26 23 | --- --- --- ---
| 102 -12 |
Table 2.1509.2 GPS week: 1509 Day: 2 MJD: 54809.000
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 243| 0 1 1 52 -13 -62 -.21 10 9 | -187 -288 14 155
| 39 -67 |
emr 72| 0 0 4 -232 -2 -71 .52 19 19 | -1476 1655 15 246
| -1 -82 |
esa 137| 1 -1 -3 -37 -4 -56 .31 10 10 | 313 663 23 110
| 16 53 |
gfz 202| 0 0 -1 -2 -52 320 -.13 11 11 | -121 313 28 154
| 2 -34 |
grg 81| 1 1 8 69 -106 -38 1.11 46 46 | -199 -308 105 388
| 29 -88 |
igr n/a| 0 0 0 36 -56 -89 .09 7 6 | 2389 2610 24 69
| -79 -89 |
jpl 130| -3 1 4 -19 -163 -71 .48 21 20 | -149 1416 24 137
| -32 -148 |
mit 277| 0 -1 0 57 -213 -58 -.28 16 14 | -494 840 18 160
| -14 46 |
ngs 236| 0 0 0 103 303 -109 -.29 13 9 | -198 -333 2193 4229
| 6 -154 |
sio 109| -1 0 1 -99 66 -78 -.02 27 23 | --- --- --- ---
| 132 -74 |
Table 2.1509.3 GPS week: 1509 Day: 3 MJD: 54810.000
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 243| 0 1 0 53 -17 -61 -.19 12 11 | -234 -32 18 120
| -43 -39 |
emr 72| 4 0 3 -182 14 -61 .40 22 22 | -1621 1305 21 257
| -26 -84 |
esa 137| 0 -3 -4 -55 -45 -24 .34 13 12 | -1623 -1210 22 108
| 93 37 |
gfz 202| 0 -1 -2 -35 -30 194 -.06 11 11 | -237 161 29 141
| -27 -12 |
grg 81| 0 2 12 137 -48 -80 1.11 46 48 | -248 -38 122 447
| -124 -53 |
igr n/a| 0 0 0 39 -83 -54 .08 6 5 | 3417 1859 25 82
| -50 -26 |
jpl 130| -1 2 2 27 -174 -24 .50 19 19 | -288 894 22 97
| -100 -107 |
mit 277| 0 -1 0 -75 -107 -34 -.28 13 12 | -629 565 25 157
| 34 10 |
ngs 236| 0 0 0 246 302 -66 -.26 12 10 | -249 -36 2629 4364
| -152 -65 |
sio 109| -1 1 3 -136 71 -37 .02 26 23 | --- --- --- ---
| 90 -67 |
Table 2.1509.4 GPS week: 1509 Day: 4 MJD: 54811.000
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 243| 0 1 0 37 -4 -68 -.23 10 9 | -1160 577 14 112
| 5 -39 |
emr 72| 1 -1 3 -155 29 -52 .39 21 21 | -393 3288 21 262
| -96 -91 |
esa 137| 1 -1 0 -13 -1 -39 .28 11 10 | 3858 -1505 19 99
| 5 64 |
gfz 202| -1 -2 -3 -8 -25 171 -.08 10 10 | -867 1382 24 128
| -12 -5 |
grg 81| 5 1 16 76 -61 -113 1.10 44 46 | -1174 559 108 394
| 33 11 |
igr n/a| 0 -1 0 13 -81 -75 .07 6 6 | 5325 4044 24 80
| -44 -16 |
jpl 130| -1 0 2 13 -166 -10 .53 17 16 | 870 3039 21 103
| -21 37 |
mit 277| 0 0 0 -47 -143 -16 -.31 15 15 | -971 1472 21 136
| 41 25 |
ngs 236| 0 0 0 142 279 -85 -.29 14 11 | -1052 478 2397 4536
| -93 -66 |
sio 109| -1 3 1 -108 115 -35 .02 27 22 | --- --- --- ---
| 91 -122 |
Table 2.1509.5 GPS week: 1509 Day: 5 MJD: 54812.000
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 243| 0 0 0 49 -32 -41 -.19 10 9 | -220 -216 13 119
| 25 -6 |
emr 72| 1 1 4 -202 -12 -32 .39 21 21 | 2250 -757 19 232
| -46 -27 |
esa 137| 2 1 -2 -14 71 -15 .31 67 14 | 379 1317 24 134
| 62 -19 |
gfz 202| 0 0 -2 -35 -64 93 -.12 9 9 | 4 538 25 136
| -6 6 |
grg 81| 4 2 13 80 -33 -46 1.23 45 42 | -238 -228 110 311
| 76 40 |
igr n/a| 0 0 2 7 -85 -52 .07 6 6 | 8760 439 25 76
| 10 15 |
jpl 130| -1 0 3 -20 -164 -3 .57 18 16 | 3006 -662 22 115
| -22 -1 |
mit 277| 0 -1 -1 18 -162 12 -.26 17 16 | 216 91 23 163
| -19 33 |
ngs 236| 0 -2 1 130 233 -91 -.26 13 11 | 88 -458 2350 3907
| 113 45 |
sio 109| -2 3 1 -85 174 -1 .02 25 23 | --- --- --- ---
| 83 -168 |
Table 2.1509.6 GPS week: 1509 Day: 6 MJD: 54813.000
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 243| 0 1 0 67 -35 -48 -.24 11 10 | 122 -645 14 121
| -14 -3 |
emr 72| 1 0 4 -231 -76 -61 .36 19 19 | 287 -1473 20 238
| 8 -1 |
esa 137| 0 -1 2 29 51 -1 .26 9 9 | -102 1044 21 108
| -6 -15 |
gfz 202| 0 -1 -5 -6 -16 109 -.15 9 9 | 578 -986 26 127
| -35 5 |
grg 81| 0 4 14 151 -56 -114 1.14 45 43 | 88 -641 115 383
| 49 136 |
igr n/a| 0 0 1 23 -112 -66 .03 4 4 | 7890 -232 22 77
| -8 23 |
jpl 130| -1 1 4 2 -196 -31 .53 18 16 | 907 -1345 22 129
| 4 30 |
mit 277| 1 -1 -2 -122 -44 -2 -.28 16 15 | -24 -311 22 138
| 38 -17 |
ngs 236| 0 0 1 126 136 -68 -.23 13 10 | 153 -722 2155 3928
| 6 192 |
sio 109| -3 5 1 -104 159 -24 .05 25 25 | --- --- --- ---
| 68 -114 |
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 3.1509.0 GPS week: 1509 Day: 0 MJD: 54807.000
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 --- --- --- --- 20 --- --- --- --- 0 | 35 --- --- --- --- 32 --- --- --- --- 38
2 | 11 26 14 13 42 9 20 8 12 29 6 | 21 41 27 20 47 26 37 20 23 27 23
3 | 7 11 13 4 28 7 15 14 9 37 5 | 32 28 30 30 27 27 39 32 28 38 28
4 | 10 9 7 8 45 7 9 10 9 33 4 | 26 27 29 27 32 26 32 24 22 34 25
5 | 6 12 12 7 43 5 9 11 12 19 4 | 16 20 19 14 29 14 20 16 22 23 15
6 | 6 12 13 4 17 7 14 8 9 33 4 | 35 38 38 36 47 37 45 35 34 29 35
7E | 6 21 10 13 39 5 16 14 7 19 4 | 22 30 27 24 49 23 32 22 23 29 21
8E | 18 19 18 8 64 7 19 16 28 22 7 | 31 38 29 29 40 31 39 35 44 34 29
9E | 18 19 10 12 84 8 18 20 20 25 6 | 113 122 118 121 110 119 121 127 122 119 119
10E | 10 19 11 9 45 7 15 18 18 19 5 | 18 29 50 24 46 22 23 22 34 26 22
11 | 8 16 6 9 81 8 19 9 9 22 4 | 25 34 28 23 60 25 41 25 24 28 24
12 | 9 20 13 10 45 9 23 19 12 19 5 | 22 33 26 25 40 25 36 24 22 24 22
13 | 6 20 13 8 41 7 20 9 9 25 4 | 17 30 20 13 44 18 29 9 17 19 14
14 | 7 20 12 11 56 10 24 10 11 22 5 | 22 29 24 26 41 21 31 21 18 27 18
15 | 9 23 10 7 38 11 23 12 14 21 5 | 15 28 18 14 34 16 29 16 16 21 14
16 | 9 26 13 8 41 8 25 10 10 32 5 | 27 42 28 23 58 29 40 22 25 29 24
17 | 13 16 8 10 103 9 12 11 19 43 6 | 45 51 52 56 75 48 52 45 47 74 50
18E | 9 25 11 10 54 6 23 10 9 16 5 | 33 47 40 33 54 36 45 32 33 42 34
19 | 9 15 10 8 73 8 12 8 7 27 4 | 37 37 41 37 74 35 40 36 36 38 35
20E | 6 23 11 7 47 6 18 9 8 19 4 | 17 28 21 17 47 18 27 18 21 23 17
21 | 11 22 11 8 25 8 18 11 14 20 5 | 24 36 25 17 40 24 33 18 27 20 22
22E | 7 25 10 10 57 8 19 10 10 15 4 | 19 32 26 21 53 25 32 22 29 24 24
23 | 8 25 15 8 33 7 24 15 8 33 6 | 18 34 27 21 46 20 30 17 20 29 17
24 | 9 12 10 8 39 7 12 16 8 18 4 | 17 21 23 22 26 20 27 25 26 25 21
25E | 13 19 13 9 44 8 16 18 14 38 6 | 57 52 55 53 65 53 59 50 56 52 51
26 | 7 14 8 9 30 6 12 14 16 32 5 | 15 26 19 19 24 17 21 18 18 35 18
27E | 21 17 16 9 76 8 17 31 20 17 7 | 69 82 74 72 85 76 82 85 74 77 74
28 | 12 18 10 7 43 9 21 13 15 25 5 | 24 34 28 26 48 25 38 28 23 27 25
29 | 5 9 10 7 27 7 9 11 10 22 3 | 39 43 42 40 46 40 41 43 43 40 41
30 | 8 10 11 7 30 6 8 19 11 13 4 | 26 26 27 22 29 22 28 23 24 24 22
31E | 8 23 12 10 37 8 19 11 10 17 5 | 28 41 31 28 43 30 33 25 25 30 25
32E | 20 35 12 10 47 9 46 19 16 26 8 | 109 114 107 109 107 110 121 107 114 105 110
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 20 12 9 51 8 19 14 13 26 |T 32 41 37 33 50 34 42 33 35 37 33
WRMS | 9 20 11 9 47 7 17 12 10 23 |NE 25 32 28 25 43 26 34 24 25 30 25
MEDI | 9 19 11 8 43 8 18 11 11 22 |MD 25 34 28 25 46 25 36 24 25 29 24
Table 3.1509.1 GPS week: 1509 Day: 1 MJD: 54808.000
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 --- --- --- --- 46 --- --- --- --- 0 | 23 --- --- --- --- 33 --- --- --- --- 24
2 | 9 23 11 14 38 4 23 11 11 37 6 | 16 38 28 26 43 23 35 17 15 26 21
3 | 7 9 7 8 46 5 15 9 12 34 4 | 23 27 23 29 20 22 25 26 23 33 22
4 | 10 12 10 9 32 6 11 12 11 35 4 | 22 30 31 24 37 26 27 27 23 40 23
5 | 8 13 8 7 34 5 9 15 6 20 3 | 14 22 20 19 26 18 18 15 21 24 17
6 | 5 8 8 8 49 6 15 8 12 29 4 | 21 33 29 27 32 28 36 24 24 20 25
7E | 9 21 9 14 33 5 18 12 9 18 5 | 15 33 26 15 36 20 30 22 20 23 19
8E | 14 20 14 9 70 5 17 19 23 21 6 | 25 37 32 26 43 31 33 36 44 38 30
9E | 17 19 10 12 58 7 21 22 20 33 6 | 98 100 102 103 105 99 99 103 104 107 99
10E | 11 19 10 11 30 5 16 17 20 21 5 | 17 27 48 24 32 18 24 17 24 23 17
11 | 6 18 10 12 94 6 16 7 9 25 4 | 17 31 19 20 55 19 29 18 18 22 17
12 | 9 21 12 8 38 6 23 20 7 21 5 | 18 32 25 23 45 22 33 20 21 22 20
13 | 7 20 10 11 38 4 16 15 10 24 5 | 14 31 18 17 38 17 26 13 15 18 14
14 | 8 21 11 8 49 7 24 11 8 23 5 | 17 34 26 23 51 24 33 24 20 23 21
15 | 7 25 10 12 39 8 24 15 11 26 5 | 12 30 18 17 43 15 26 16 16 18 14
16 | 9 30 10 8 28 7 23 16 11 27 5 | 21 37 28 23 39 23 36 20 23 27 23
17 | 12 13 8 15 78 8 12 9 12 54 6 | 29 38 38 41 42 37 38 32 32 67 34
18E | 9 26 8 13 49 5 24 10 9 22 5 | 41 54 49 41 55 47 55 43 49 45 45
19 | 10 10 6 8 84 7 12 10 10 25 4 | 16 25 22 19 55 19 25 18 15 21 18
20E | 9 21 14 7 36 6 18 10 7 17 4 | 17 28 24 20 35 18 23 18 14 15 17
21 | 10 21 11 7 38 7 18 10 11 19 4 | 22 39 30 22 40 27 33 23 28 23 23
22E | 8 18 8 13 37 8 20 11 9 11 4 | 19 31 20 25 39 19 28 21 15 18 21
23 | 8 27 8 11 38 5 20 13 11 28 5 | 19 37 22 24 47 21 30 18 16 26 18
24 | 8 14 7 8 32 6 13 17 13 12 4 | 16 23 23 21 23 19 21 18 18 18 18
25E | 9 20 12 9 38 5 13 21 13 25 5 | 38 48 39 40 48 41 43 49 45 45 42
26 | 8 12 6 10 26 4 11 13 10 35 4 | 16 28 21 21 33 17 23 20 21 40 17
27E | 17 19 12 13 66 5 16 37 16 19 7 | 68 78 74 68 80 70 77 73 71 76 69
28 | 12 18 10 11 44 6 21 12 8 22 5 | 21 36 30 24 49 25 35 25 24 24 24
29 | 7 10 5 5 30 8 7 16 14 22 4 | 21 28 26 23 23 24 24 23 25 22 23
30 | 8 12 9 8 24 5 7 21 8 13 4 | 19 23 22 19 29 19 19 16 23 17 18
31E | 10 23 9 8 37 5 21 11 12 14 5 | 21 36 25 21 44 21 30 24 20 23 22
32E | 15 30 16 11 35 7 15 19 17 20 6 | 89 96 99 94 82 92 86 88 86 89 90
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 10 10 47 6 17 16 12 26 |T 26 38 33 30 44 29 35 29 29 33 28
WRMS | 9 19 9 10 43 6 16 13 9 23 |NE 18 31 24 23 38 22 28 20 21 26 20
MEDI | 9 19 10 9 38 6 16 13 11 22 |MD 19 33 26 23 42 22 30 22 23 23 21
Table 3.1509.2 GPS week: 1509 Day: 2 MJD: 54809.000
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 --- --- --- --- 46 --- --- --- --- 0 | 47 --- --- --- --- 40 --- --- --- --- 49
2 | 9 28 10 11 45 7 25 13 13 34 6 | 23 45 30 28 45 27 36 20 25 24 29
3 | 8 15 11 6 45 4 20 12 11 37 5 | 26 31 29 27 25 28 29 30 32 42 30
4 | 12 11 7 10 34 6 16 14 11 39 5 | 21 27 28 22 32 24 24 24 27 34 26
5 | 7 13 4 8 19 6 14 15 13 20 4 | 20 26 27 21 26 23 23 23 30 28 26
6 | 7 11 12 7 61 4 19 11 11 27 4 | 29 35 35 28 41 32 35 30 34 29 32
7E | 8 20 9 16 32 7 19 14 9 20 5 | 21 34 23 25 30 22 27 23 24 25 25
8E | 14 18 15 14 62 6 20 16 21 26 6 | 28 37 32 25 31 29 33 33 37 35 31
9E | 16 17 14 13 45 9 25 26 18 32 7 | 91 94 95 97 107 89 94 100 90 104 92
10E | 11 19 8 12 38 7 23 16 20 26 6 | 19 29 34 25 42 20 25 18 33 28 24
11 | 8 18 10 14 97 8 23 9 9 20 5 | 22 38 30 32 64 26 33 26 30 24 30
12 | 11 19 8 7 35 8 27 18 11 20 5 | 26 33 29 27 47 26 34 25 29 27 29
13 | 8 20 10 10 38 5 19 16 12 26 5 | 18 34 22 21 44 23 29 17 26 21 24
14 | 9 21 8 12 51 7 26 14 13 22 5 | 23 33 32 26 45 27 29 25 30 30 29
15 | 7 22 10 10 48 8 26 16 10 24 5 | 17 32 23 20 43 20 29 19 20 21 22
16 | 10 26 9 6 37 6 26 15 7 33 5 | 26 41 31 25 50 29 39 25 29 30 30
17 | 12 14 10 20 58 10 20 12 12 61 7 | 27 34 34 42 28 34 32 31 34 62 35
18E | 10 22 9 13 48 8 26 12 9 16 5 | 45 52 53 45 56 50 53 45 54 49 50
19 | 10 9 8 10 73 6 17 12 12 22 4 | 31 36 39 36 58 31 31 30 32 30 34
20E | 9 21 7 11 26 5 22 13 11 18 5 | 18 35 26 24 35 24 28 19 25 26 25
21 | 9 21 8 10 46 7 20 10 9 20 4 | 19 33 24 21 36 22 27 20 27 27 25
22E | 9 23 11 10 36 8 24 13 11 13 5 | 22 36 38 32 39 31 34 29 32 31 33
23 | 9 24 14 10 35 6 23 14 12 27 5 | 20 38 30 27 54 24 33 24 27 29 26
24 | 7 12 8 8 30 8 18 14 10 18 4 | 26 33 34 31 24 29 30 30 35 27 35
25E | 13 21 11 10 37 7 17 23 10 28 6 | 62 68 64 62 64 65 63 66 64 61 65
26 | 7 12 6 9 43 6 17 16 8 34 4 | 16 29 20 18 38 19 22 19 18 36 21
27E | 16 22 16 16 46 5 22 31 20 26 7 | 104 109 108 107 117 105 106 106 106 101 107
28 | 12 20 11 11 39 7 25 11 12 31 5 | 23 35 27 25 42 23 34 24 25 25 27
29 | 6 9 8 7 39 5 11 17 12 20 4 | 33 37 33 35 40 33 31 35 40 35 38
30 | 8 11 6 7 23 5 13 17 10 12 4 | 26 27 30 23 32 26 24 27 31 26 29
31E | 9 19 11 13 34 6 22 12 11 13 5 | 24 35 28 25 42 25 29 23 26 24 28
32E | 13 30 12 9 48 6 17 19 20 24 6 | 56 67 60 65 62 61 64 62 64 57 61
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 10 11 46 7 21 16 13 27 |T 31 41 37 34 46 33 37 33 36 37 36
WRMS | 9 19 10 11 46 6 20 14 9 23 |NE 24 33 29 26 40 26 30 25 29 30 29
MEDI | 9 19 10 10 39 6 20 14 11 24 |MD 24 35 30 27 42 27 31 25 30 29 29
Table 3.1509.3 GPS week: 1509 Day: 3 MJD: 54810.000
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 --- --- --- --- 56 --- --- --- --- 0 | 38 --- --- --- --- 30 --- --- --- --- 42
2 | 11 36 12 10 43 6 24 10 12 32 6 | 19 42 29 23 41 22 32 22 22 30 24
3 | 9 12 9 7 33 7 14 11 10 33 4 | 27 26 30 27 22 25 27 29 27 36 29
4 | 14 10 10 7 35 6 12 12 13 31 5 | 20 23 26 26 29 23 24 25 26 34 24
5 | 9 15 13 6 17 4 12 11 11 21 4 | 17 19 18 17 27 17 17 21 30 27 22
6 | 9 11 13 9 39 5 16 9 8 29 4 | 27 29 34 33 29 30 33 31 30 27 31
7E | 11 25 12 11 35 6 15 12 10 26 5 | 27 39 34 32 50 29 33 32 32 48 31
8E | 17 22 17 13 69 6 16 16 23 27 7 | 23 32 26 29 39 23 27 29 38 34 27
9E | 18 20 17 13 38 6 18 17 12 26 6 | 99 105 99 102 96 103 103 105 108 106 103
10E | 12 24 12 9 36 5 21 15 21 27 6 | 27 35 57 28 42 28 25 27 42 36 30
11 | 6 18 10 12 84 5 16 8 10 17 4 | 25 28 29 26 58 22 30 22 23 22 24
12 | 11 18 15 8 32 6 23 12 10 20 5 | 21 26 27 25 42 21 28 24 27 25 25
X13 | 8 23 13 10 38 5 --- 10 11 25 5 | 17 27 21 19 43 17 --- 18 23 17 18
14 | 8 22 16 11 47 4 30 12 9 23 6 | 23 34 31 29 48 22 30 24 23 32 25
15 | 10 23 10 9 35 6 24 12 12 30 5 | 22 31 24 22 38 21 29 22 29 25 24
16 | 12 33 13 7 43 5 25 15 8 34 6 | 21 37 26 23 59 22 33 23 29 31 24
17 | 15 13 14 15 69 9 20 10 11 65 7 | 40 38 44 50 41 39 39 42 42 73 43
18E | 11 21 11 11 37 7 23 7 13 15 5 | 26 35 27 31 38 27 37 27 33 32 29
19 | 10 14 8 12 76 6 13 11 13 19 4 | 29 29 33 35 62 30 30 31 30 33 30
20E | 7 23 11 11 48 3 20 8 8 17 4 | 24 29 26 28 47 24 27 21 26 26 24
21 | 13 25 15 9 49 8 21 11 12 19 5 | 27 38 30 27 37 24 30 25 29 29 28
22E | 13 29 11 12 41 5 22 10 10 13 5 | 27 36 30 31 56 28 35 31 34 31 30
23 | 7 28 13 12 33 5 20 9 13 22 5 | 26 38 34 31 48 28 33 25 27 29 27
24 | 10 16 14 9 38 5 11 12 9 12 4 | 23 22 28 26 33 24 23 25 34 21 26
25 | 24 19 16 14 57 7 17 20 12 25 7 | 80 88 96 90 79 88 92 83 93 78 87
26 | 12 13 10 8 29 3 13 9 11 33 4 | 23 27 23 23 27 21 24 25 28 40 25
27E | 15 20 16 17 31 6 15 25 12 24 7 | 117 123 114 118 115 118 122 120 117 122 118
28 | 12 23 15 13 39 5 23 9 17 28 6 | 22 31 28 27 38 22 33 24 31 25 26
29 | 7 12 12 8 25 6 10 11 9 21 4 | 36 40 38 39 43 37 35 40 39 36 39
30 | 9 15 10 8 18 3 11 13 12 14 4 | 20 22 24 18 28 22 20 22 32 21 24
31E | 9 27 12 9 36 5 20 8 7 14 5 | 26 40 28 28 42 26 32 30 33 30 29
32E | 13 27 16 11 81 5 21 16 18 21 6 | 77 78 81 81 73 78 81 78 82 84 80
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 22 13 11 46 6 19 13 12 26 |T 33 40 38 36 47 34 38 35 39 40 36
WRMS | 11 22 12 11 48 5 19 12 10 23 |NE 24 30 28 27 39 24 28 26 29 30 27
MEDI | 11 21 13 10 38 5 18 11 11 24 |MD 26 34 29 28 42 24 30 25 30 31 27
Table 3.1509.4 GPS week: 1509 Day: 4 MJD: 54811.000
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 --- --- --- --- 33 --- --- --- --- 0 | 37 --- --- --- --- 32 --- --- --- --- 36
2 | 10 29 10 9 35 6 22 10 16 26 5 | 18 39 27 23 56 24 33 20 19 16 22
3 | 9 14 11 7 52 3 9 16 13 34 5 | 20 24 22 21 36 21 24 31 23 35 21
4 | 8 13 8 9 34 7 10 14 14 23 4 | 19 23 24 24 36 23 25 21 21 27 21
5 | 9 17 8 6 20 4 13 13 15 24 4 | 17 22 20 19 27 20 23 20 28 24 19
6 | 7 13 10 6 62 3 9 11 11 33 4 | 24 28 25 27 38 26 31 26 27 28 25
7E | 8 24 10 13 34 6 15 13 11 19 5 | 15 30 21 22 36 19 23 19 24 20 17
8E | 18 21 10 16 62 6 17 17 21 25 6 | 23 32 27 34 38 25 26 29 34 32 25
9E | 18 22 13 12 33 5 14 19 16 30 6 | 63 77 68 66 79 69 70 70 73 72 68
10E | 13 24 10 8 42 5 17 17 26 27 6 | 16 27 96 24 41 20 22 19 35 29 20
11 | 8 20 9 8 86 7 15 11 16 20 4 | 16 32 20 21 56 19 28 19 19 22 17
12 | 7 17 13 8 32 5 21 16 16 24 5 | 23 27 27 24 45 23 32 24 32 25 25
X13 | 13 --- 16 --- --- 34 --- --- --- --- 14 | 22 --- 22 --- --- 53 --- --- --- --- 22
14 | 7 22 11 9 41 5 27 13 11 22 5 | 17 27 24 20 47 18 30 20 22 23 20
15 | 10 23 12 10 32 7 25 14 12 25 5 | 15 29 17 18 38 18 30 18 21 19 18
16 | 9 26 9 7 31 6 23 16 9 40 6 | 24 39 28 25 44 26 37 25 25 29 26
17 | 13 15 14 23 65 9 16 12 13 66 8 | 30 36 37 51 33 35 34 34 37 76 38
18E | 8 25 13 8 32 4 21 12 12 17 5 | 24 34 31 25 41 26 35 26 28 30 27
19 | 8 14 8 10 68 6 11 16 13 19 4 | 28 33 29 33 54 30 30 27 30 29 29
20E | 6 22 11 7 48 5 19 14 11 19 4 | 18 27 17 19 51 18 25 23 18 20 17
21 | 9 26 11 7 33 6 21 9 10 20 5 | 19 35 21 17 47 18 30 17 18 25 21
22E | 8 21 12 8 35 4 17 13 9 14 4 | 25 28 25 26 49 26 35 28 31 28 27
23 | 7 27 10 9 34 5 21 10 13 21 5 | 20 35 23 20 42 21 29 22 25 21 21
24 | 7 18 8 8 45 6 11 13 10 15 4 | 22 21 26 26 35 22 24 24 26 20 23
25 | 11 20 9 9 44 6 16 22 13 22 5 | 54 61 57 52 83 57 60 57 59 47 55
26 | 10 14 10 5 20 5 10 12 13 33 4 | 11 20 19 16 27 15 18 17 18 33 16
27E | 11 20 9 10 36 5 16 19 9 25 5 | 105 114 113 106 103 108 113 106 106 110 106
28 | 12 23 14 10 44 6 22 12 14 22 5 | 17 37 25 23 46 20 31 20 20 23 20
29 | 6 14 7 8 28 9 12 14 14 25 4 | 30 33 32 31 35 28 31 33 37 35 33
30 | 7 17 9 7 23 5 9 14 11 16 4 | 20 26 20 17 31 21 25 20 25 18 19
31E | 8 29 11 9 30 5 22 15 12 19 5 | 18 38 25 21 38 20 29 21 26 30 21
32E | 12 29 11 9 66 6 16 21 26 27 6 | 52 56 48 53 57 51 56 55 57 56 52
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 21 11 10 44 6 17 15 14 27 |T 26 36 32 30 46 29 34 29 32 33 28
WRMS | 9 21 10 10 46 6 16 15 11 22 |NE 21 29 24 24 40 24 28 23 24 27 23
MEDI | 8 21 10 8 35 6 16 14 13 23 |MD 20 32 25 24 41 23 30 23 26 28 22
Table 3.1509.5 GPS week: 1509 Day: 5 MJD: 54812.000
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 --- --- --- --- 35 --- --- --- --- 0 | 30 --- --- --- --- 30 --- --- --- --- 33
2 | 10 25 19 12 51 5 21 13 9 25 6 | 13 30 22 21 50 19 31 17 20 15 18
3 | 8 14 9 6 80 5 11 18 8 34 5 | 23 26 28 26 60 21 26 27 30 31 23
4 | 11 15 12 8 34 4 12 17 13 17 4 | 19 22 24 23 33 19 25 20 19 23 20
5 | 7 15 14 9 21 3 11 16 11 20 4 | 16 22 25 20 23 17 20 22 20 23 20
6 | 8 13 11 6 79 5 11 18 9 30 4 | 22 29 30 25 58 23 29 25 33 18 24
7E | 10 21 11 10 41 7 17 16 10 16 5 | 19 29 25 21 32 20 24 19 25 22 19
8E | 20 18 11 12 59 6 17 16 20 23 6 | 40 43 38 47 46 38 45 44 49 40 39
9E | 15 20 10 12 36 5 17 21 9 24 6 | 84 94 88 89 86 85 92 86 86 94 87
10E | 13 23 361 9 58 8 19 18 26 27 7 | 17 29 265 21 52 20 22 21 47 20 22
11 | 8 21 10 9 71 6 16 13 15 15 4 | 20 32 20 22 44 18 29 22 21 22 18
12 | 10 21 16 10 28 5 23 20 10 19 5 | 18 29 22 21 41 20 29 21 26 20 21
X13 | 5 --- --- --- --- 10 --- --- --- --- 0 | 12 --- --- --- --- 10 --- --- --- --- 12
14 | 12 23 15 9 45 9 25 14 15 20 6 | 13 28 27 22 41 15 26 22 29 20 18
15 | 8 26 18 9 23 5 23 17 11 24 6 | 17 32 24 21 42 19 30 19 26 24 20
16 | 9 26 12 7 41 7 23 17 12 32 6 | 24 37 28 21 51 24 35 22 33 26 24
17 | 13 14 14 16 50 9 17 16 18 62 8 | 29 34 39 40 29 31 33 34 29 63 33
18E | 7 26 10 10 44 5 20 15 11 15 5 | 20 31 25 21 36 21 28 19 30 25 20
19 | 6 14 9 6 60 7 12 23 13 22 4 | 20 26 24 25 28 18 25 20 27 19 20
20E | 9 22 13 9 29 4 22 19 12 15 5 | 23 28 27 25 52 23 29 25 28 23 21
21 | 9 28 16 7 27 3 22 16 10 24 6 | 23 36 29 19 35 22 31 22 28 32 24
22E | 9 23 17 8 32 7 18 20 9 13 5 | 22 35 36 27 54 23 30 29 31 27 26
23 | 8 25 17 7 22 5 22 12 10 21 5 | 20 34 31 25 37 24 31 21 25 23 21
24 | 8 18 12 5 42 3 10 11 11 11 4 | 17 22 24 18 35 18 20 19 30 19 21
25 | 11 21 12 8 47 5 14 19 12 21 5 | 25 35 25 25 35 24 28 28 27 16 24
26 | 9 15 14 7 16 5 10 15 7 33 5 | 15 25 21 17 28 16 22 19 24 38 18
27 | 13 25 8 10 38 7 16 15 13 24 5 | 129 139 132 127 128 130 136 127 130 129 129
28 | 9 24 11 11 45 13 23 13 12 22 5 | 24 37 31 26 46 24 36 24 26 26 25
29 | 8 12 12 7 27 5 13 12 15 24 4 | 31 32 38 31 41 31 29 32 40 34 33
30 | 8 19 16 6 29 5 11 15 11 12 4 | 17 25 23 18 35 17 20 16 24 16 19
31E | 10 27 14 10 41 6 23 16 17 14 6 | 14 33 19 16 42 15 25 16 26 21 15
32E | 14 26 13 12 57 7 18 21 22 25 6 | 74 77 79 76 67 77 77 77 83 78 75
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 21 67 9 45 6 18 17 13 25 |T 27 37 42 31 46 28 35 30 35 32 29
WRMS | 9 21 14 9 42 6 16 16 11 23 |NE 20 29 26 23 39 20 27 22 26 25 22
MEDI | 9 21 12 9 41 5 17 16 11 22 |MD 20 31 27 22 41 21 29 22 28 23 21
Table 3.1509.6 GPS week: 1509 Day: 6 MJD: 54813.000
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 --- --- --- --- 38 --- --- --- --- 0 | 33 --- --- --- --- 38 --- --- --- --- 32
2 | 11 22 14 7 36 5 19 13 12 24 5 | 21 35 30 22 47 23 32 23 19 22 21
3 | 9 11 5 6 46 4 12 13 10 38 4 | 26 28 29 27 37 26 28 29 32 28 27
4 | 10 14 10 5 32 4 10 12 10 14 3 | 29 32 30 30 33 30 28 30 27 27 26
5 | 10 16 8 8 22 4 12 13 9 20 4 | 15 25 22 15 31 17 24 20 21 28 16
6 | 7 11 5 7 69 3 12 14 13 34 4 | 31 36 37 35 48 32 38 37 41 22 34
7E | 11 22 9 8 38 5 16 16 11 24 5 | 23 32 23 20 37 23 30 25 25 33 21
8E | 17 19 11 11 32 5 17 17 18 22 6 | 53 58 53 57 50 52 51 60 58 59 55
9E | 26 19 5 15 50 4 16 20 8 27 6 | 95 107 103 106 122 104 107 104 101 115 101
10E | 13 20 12 10 35 5 17 19 27 19 6 | 19 26 99 25 31 22 24 22 38 23 18
11 | 10 20 10 6 83 4 17 16 10 19 4 | 27 36 26 26 66 25 33 27 22 25 23
12 | 9 19 10 8 27 4 22 16 9 22 5 | 25 36 29 28 44 27 37 31 30 28 26
X13 | 11 23 10 6 37 5 18 11 12 --- 5 | 15 25 8 7 16 17 19 8 6 --- 13
14 | 10 22 7 9 37 6 24 14 12 24 5 | 19 30 22 22 44 17 29 23 23 27 18
15 | 12 24 10 7 31 3 22 14 14 23 5 | 19 31 27 20 42 24 33 24 23 25 19
16 | 8 25 9 7 40 4 24 12 11 23 5 | 26 38 29 27 55 28 39 26 24 30 26
17 | 13 13 11 16 57 7 18 12 11 58 7 | 49 48 51 55 48 48 48 52 44 74 47
18E | 8 24 10 10 34 3 25 19 10 15 5 | 24 37 24 26 42 24 36 26 26 32 25
19 | 11 11 8 7 83 4 11 21 12 23 4 | 40 41 39 41 74 37 42 41 37 37 37
20E | 7 16 10 8 42 4 20 22 8 15 4 | 24 35 32 28 45 27 29 28 25 31 25
21 | 10 18 7 7 35 3 20 16 10 21 4 | 25 30 27 27 35 26 32 26 30 31 24
22E | 10 27 10 11 37 4 20 18 9 13 5 | 19 34 26 20 48 21 31 26 25 25 21
23 | 7 25 10 8 37 5 21 13 13 21 5 | 28 42 31 30 57 28 37 27 27 30 26
24 | 10 12 7 6 41 3 10 12 8 10 3 | 23 25 27 30 27 26 27 26 32 23 26
25 | 11 17 8 8 38 5 17 18 12 20 5 | 39 45 44 36 58 40 48 39 43 35 37
26 | 9 18 7 9 22 3 11 14 10 28 4 | 18 29 24 22 27 23 28 24 19 36 19
27 | 13 19 8 9 29 4 16 15 11 24 5 | 120 129 124 121 124 122 124 123 120 124 123
28 | 11 23 9 9 44 6 22 12 15 23 5 | 28 40 28 27 41 29 37 30 25 34 26
29 | 9 10 6 5 39 4 12 12 13 23 4 | 45 50 47 47 42 47 47 49 48 43 46
30 | 11 18 8 8 29 4 10 13 8 16 4 | 19 30 23 20 32 21 23 21 22 18 19
31E | 10 20 11 11 46 5 24 17 12 24 5 | 17 33 17 20 38 19 31 21 17 27 15
32E | 10 22 11 9 68 5 14 22 24 22 6 | 80 87 83 83 68 80 84 83 84 86 81
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 9 9 45 4 18 16 13 25 |T 33 42 39 35 48 35 40 36 35 39 33
WRMS | 10 19 9 9 43 4 16 15 10 25 |NE 26 34 29 27 42 28 33 28 27 30 26
MEDI | 10 19 9 8 37 4 17 14 11 22 |MD 25 35 29 27 44 26 33 27 27 30 26
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 4.1509 GPS week: 1509 MJD: 54807.0-54813.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 |U 7 8 21 |U 13 17 45 |U 12 13 26 |
emr | emr 2931 | 14 11 25 | 15 19 49 | 14 15 31 |
esa | esa 2948 | 10 10 25 |U 13 16 44 | 13 13 29 |
gfz | gfz 2907 |U 13 12 26 |U 14 22 64 | 21 14 42 |
igr | igr 2955 | 10 9 24 | 14 18 47 | 12 12 29 |
igs | igs 2919 | 10 8 21 | 13 17 42 | 13 13 31 |
jpl | jpl 2915 |U 17 13 26 |U 13 17 45 | 14 19 38 |
mit | mit 2948 |U 11 10 24 |U 12 15 46 |U 15 15 35 |
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 5.1509.0 GPS week: 1509 Day: 0 MJD: 54807.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 6 18 | 18 16 89 | 11 10 37 |
emr | emr 2956 | 10 12 25 | 19 17 84 | 12 14 45 |
esa | esa 2976 | 9 10 20 | 17 16 82 | 13 12 40 |
gfz | gfz 2933 | 11 11 19 | 19 17 92 | 17 16 58 |
igr | igr 2967 | 10 11 19 | 17 17 86 | 12 15 46 |
igs | igs 2974 | 10 7 18 | 18 16 83 | 13 12 41 |
jpl | jpl 2956 | 17 9 26 | 20 19 87 | 14 29 65 |
mit | mit 2976 | 10 12 28 | 18 16 89 | 12 17 46 |
Table 5.1509.1 GPS week: 1509 Day: 1 MJD: 54808.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 | 7 6 19 | 15 22 47 | 13 13 27 |
emr | emr 2954 | 9 7 23 | 16 18 41 | 14 14 31 |
esa | esa 2976 | 7 5 24 | 16 13 46 | 12 11 29 |
gfz | gfz 2930 | 8 6 23 | 16 14 58 | 20 12 40 |
igr | igr 2976 | 7 5 20 | 16 14 44 | 13 10 29 |
igs | igs 2974 | 7 6 20 | 14 18 36 | 13 12 30 |
jpl | jpl 2953 | 13 14 22 | 16 14 39 | 15 23 40 |
mit | mit 2976 | 12 10 22 | 15 18 39 | 15 22 43 |
Table 5.1509.2 GPS week: 1509 Day: 2 MJD: 54809.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 7 12 23 | 11 14 34 | 12 14 25 |
emr | emr 2956 | 12 11 21 | 15 13 53 | 16 16 34 |
esa | esa 2976 | 9 9 22 | 11 13 40 | 14 15 28 |
gfz | gfz 2934 | 14 14 24 | 12 20 51 | 21 15 39 |
igr | igr 2976 | 9 9 22 | 11 15 43 | 13 11 28 |
igs | igs 2952 | 9 9 23 | 10 13 33 | 14 14 30 |
jpl | jpl 2956 | 18 20 31 | 12 14 44 | 13 24 43 |
mit | mit 2976 | 8 10 24 | 11 10 48 | 21 15 34 |
Table 5.1509.3 GPS week: 1509 Day: 3 MJD: 54810.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 8 9 25 | 10 15 31 | 10 13 28 |
emr | emr 2959 | 16 12 24 | 10 19 38 | 12 13 27 |
esa | esa 2976 | 10 8 24 | 9 12 25 | 13 14 30 |
gfz | gfz 2931 | 15 17 41 | 10 14 47 | 21 14 41 |
igr | igr 2974 | 11 9 25 | 9 16 26 | 11 13 28 |
igs | igs 2976 | 10 8 22 | 8 14 25 | 12 13 31 |
jpl | jpl 2860 | 21 17 23 | 9 20 35 | 14 16 41 |
mit | mit 2976 | 9 7 20 | 8 12 27 | 14 13 29 |
Table 5.1509.4 GPS week: 1509 Day: 4 MJD: 54811.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 9 16 | 7 8 34 | 14 13 26 |
emr | emr 2864 | 14 10 25 | 11 10 36 | 12 13 26 |
esa | esa 2880 | 10 11 23 | 7 7 30 | 11 12 29 |
gfz | gfz 2839 | 12 9 22 | 9 11 56 | 20 14 44 |
igs | igs 2809 | 9 9 20 | 7 8 27 | 11 14 30 |
jpl | jpl 2863 | 15 10 22 | 7 9 32 | 13 15 31 |
mit | mit 2880 | 14 9 26 | 7 8 31 | 14 12 30 |
Table 5.1509.5 GPS week: 1509 Day: 5 MJD: 54812.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 6 7 20 | 18 30 41 | 14 13 18 |
emr | emr 2868 | 17 13 27 | 20 34 47 | 14 15 27 |
esa | esa 2880 | 12 14 30 | 18 30 46 | 14 16 28 |
gfz | gfz 2842 | 13 13 25 | 20 40 65 | 22 14 37 |
igr | igr 2873 | 9 10 27 | 16 31 42 | 11 12 25 |
igs | igs 2780 | 9 10 21 | 18 36 44 | 13 15 31 |
jpl | jpl 2866 | 15 12 25 | 17 26 38 | 13 14 24 |
mit | mit 2880 | 12 13 23 | 16 25 42 | 15 14 35 |
Table 5.1509.6 GPS week: 1509 Day: 6 MJD: 54813.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 10 5 28 | 12 17 40 | 13 12 18 |
emr | emr 2964 | 19 11 32 | 15 19 43 | 18 17 27 |
esa | esa 2976 | 15 10 32 | 11 17 41 | 14 12 23 |
gfz | gfz 2941 | 18 12 30 | 15 38 78 | 23 12 34 |
igr | igr 2975 | 14 9 28 | 12 14 41 | 13 11 20 |
igs | igs 2973 | 14 8 26 | 13 16 43 | 13 13 25 |
jpl | jpl 2957 | 19 10 30 | 12 15 42 | 14 12 25 |
mit | mit 2976 | 15 10 25 | 12 16 47 | 15 16 30 |
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 6.1509 GPS week: 1509 MJD: 54807.500-54813.500
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 | 17 1 92 214 0 | -4 20
| 23 21 88 100 6 | 3
emr uuuuu | 42 24 -257 11 0 | 44 47
| 36 37 180 100 14 | 5
esa uuuuu | -23 -23 135 -202 -9 | -5 18
| 37 47 136 118 12 | 4
gfz uuuuu | -5 14 49 95 5 | -3 19
| 14 20 60 65 6 | 5
grg xxxxx | -34 -9 129 172 11 | -6 13
| 72 67 153 120 17 | 3
igr xxxxx | 2 34 74 -10 5 | -4 15
| 36 26 47 73 4 | 3
irf xxxxx | -16 2 -40 1 3 | -10 19
| 13 15 56 41 3 | 4
jpl uuuuu | 33 32 76 272 5 | 7 21
| 67 29 164 190 16 | 2
mit uuuuu | -33 -15 -239 -21 4 | -1 16
| 24 38 139 74 10 | 3
ngs xuuuu | 3 19 82 -70 -7 | 0 16
| 114 72 146 69 7 | 4
sio uuxxu | 68 -91 93 226 13 | -11 24
| 64 23 111 139 15 | 5
Table 7.1509.0 GPS week: 1509 Day: 0 MJD: 54807.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 16 19 68 216 -11 | -7 19
emr uuuuu | 22 16 -113 -47 15 | 36 39
esa uuuuu | 6 -35 317 -152 1 | -4 16
gfz uuuuu | -15 33 19 68 10 | -10 19
grg xxxxx | -64 65 -149 126 15 | -10 15
igr xxxxx | -21 42 64 -70 10 | -10 15
irf xxxxx | -32 -5 0 -33 1 | -16 20
jpl uuuuu | 84 36 -27 162 -9 | 7 19
mit uuuuu | -50 -31 -125 -50 -7 | -4 13
ngs xuuuu | -51 23 -160 45 -3 | -3 17
sio uuxxu | -1 -89 10 269 15 | -17 22
Table 7.1509.1 GPS week: 1509 Day: 1 MJD: 54808.500
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 -5 -46 213 -2 | -6 19
emr uuuuu | 37 -9 -21 -98 12 | 38 41
esa uuuuu | 7 43 96 13 -20 | -4 16
gfz uuuuu | -7 -18 -35 58 14 | -9 19
grg xxxxx | -74 -65 194 18 -21 | -9 15
igr xxxxx | -5 23 118 -76 0 | -8 15
irf xxxxx | -26 17 -40 -40 5 | -15 20
jpl uuuuu | 11 16 153 134 -8 | 8 19
mit uuuuu | -29 2 -209 -43 7 | -5 12
ngs xuuuu | 80 -16 5 -81 -11 | -1 15
sio uuxxu | -14 -85 37 139 25 | -18 22
Table 7.1509.2 GPS week: 1509 Day: 2 MJD: 54809.500
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 | 49 -31 34 24 8 | -1 20
emr uuuuu | 64 9 -87 -2 11 | 46 50
esa uuuuu | -71 -8 -90 -185 -11 | 0 15
gfz uuuuu | 16 6 40 29 10 | -1 20
grg xxxxx | 70 -21 329 397 9 | -8 15
igr xxxxx | 71 87 138 -6 8 | -3 16
irf xxxxx | -18 8 -92 56 7 | -9 19
jpl uuuuu | 130 40 393 565 -13 | 11 23
mit uuuuu | -64 22 -312 12 10 | 0 17
ngs xuuuu | 136 2 189 -88 -7 | 4 16
sio uuxxu | 56 -124 88 119 26 | -12 26
Table 7.1509.3 GPS week: 1509 Day: 3 MJD: 54810.500
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 26 240 324 -4 | 0 19
emr uuuuu | 64 9 -345 38 3 | 48 51
esa uuuuu | -57 -110 70 -370 -22 | 0 15
gfz uuuuu | -8 10 119 88 7 | 1 18
grg xxxxx | 33 107 101 193 30 | -6 12
igr xxxxx | 6 33 8 -42 2 | -1 15
irf xxxxx | -20 -17 41 28 6 | -8 17
jpl uuuuu | 87 83 -47 454 3 | 9 23
mit uuuuu | -30 -51 -38 94 13 | 1 17
ngs xuuuu | 45 135 44 -178 -4 | 4 16
sio uuxxu | 47 -107 256 241 23 | -11 25
Table 7.1509.4 GPS week: 1509 Day: 4 MJD: 54811.500
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 | 46 -18 114 239 1 | -4 19
emr uuuuu | 98 83 -493 49 -7 | 47 50
esa uuuuu | -57 -18 99 -236 -14 | -6 18
gfz uuuuu | 12 -1 121 192 1 | -1 18
grg xxxxx | -4 -46 250 99 0 | -3 10
igr xxxxx | 23 31 24 -57 1 | -3 15
irf xxxxx | 7 -13 -6 13 4 | -9 18
jpl uuuuu | -30 8 -67 18 20 | 5 20
mit uuuuu | -18 -54 -190 33 13 | 0 16
ngs xuuuu | 73 80 231 -83 -19 | 2 16
sio uuxxu | 129 -104 159 388 13 | -9 25
Table 7.1509.5 GPS week: 1509 Day: 5 MJD: 54812.500
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 0 128 169 3 | -3 19
emr uuuuu | 14 71 -384 201 -18 | 48 51
esa uuuuu | 6 -37 183 -277 -12 | -7 18
gfz uuuuu | -19 31 78 49 -4 | 1 18
grg xxxxx | -53 -51 82 225 18 | -2 11
igr xxxxx | -28 15 73 112 9 | -2 16
irf xxxxx | -13 25 -117 31 1 | -7 18
jpl uuuuu | -12 47 -5 297 28 | 6 22
mit uuuuu | -46 44 -434 -62 4 | 3 18
ngs xuuuu | -58 -88 239 -89 -5 | 0 15
sio uuxxu | 155 -58 169 28 2 | -5 24
Table 7.1509.6 GPS week: 1509 Day: 6 MJD: 54813.500
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 15 103 313 5 | -6 22
emr uuuuu | -8 -7 -358 -68 -15 | 45 50
esa uuuuu | 6 7 266 -210 11 | -12 25
gfz uuuuu | -14 36 0 181 0 | -1 21
grg xxxxx | -145 -48 93 143 25 | -3 12
igr xxxxx | -32 9 95 67 6 | -2 16
irf xxxxx | -9 1 -64 -49 -2 | -9 21
jpl uuuuu | -39 -3 130 276 14 | 7 22
mit uuuuu | 8 -37 -363 -134 -11 | 2 20
ngs xuuuu | -201 -5 25 -14 3 | -5 20
sio uuxxu | 105 -67 -72 396 -14 | -5 25
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