[IGSREPORT-19211] Wk 1610 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Dec 2 06:21:53 PST 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1610 (Nov 14, 2010 - Nov 20, 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:
igs1610[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1610[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1610[0-6].cls IGS GPS clock combination summary report.
igs16107.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16107.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 | 22 WTZR DGAR
0 | EMR | 3 WTZR
0 | ESA | MATE WTZR
0 | GFZ | 3 17 AUCK CAS1 DGAR KERG MDVJ SCUB UNSA
0 | GRG | AMC2 DGAR POTS
0 | JPL | 22 32
0 | MIT | 3 3 22 USNO USNO
1 | ALL | 1 1
1 | COD | 22 22 ALGO
1 | EMR | 32 21 32 WTZR WTZR
1 | ESA | 21 KERG
1 | GFZ | 22 MAC1 UNSA
1 | GRG | AMC2 DGAR
1 | JPL | 21 22 32
1 | MIT | 22 21 22 ALGO DAV1 KHAJ MAW1 ALGO BRUS KHAJ MAW1
1 | MIT | SYDN
2 | ALL | 1
2 | COD | 22 22 CONZ ALBH ALRT CONZ DGAR GUAT WILL XMIS
2 | EMR | HARB WTZR HARB WTZR
2 | ESA | UNSA
2 | GFZ | CAS1 DGAR FAA1
2 | GRG | ADIS DAV1 DGAR
2 | JPL | 22 32
2 | MIT | 22 22 DAV1 ALIC
3 | ALL | 27
3 | COD | 22 22 CHUR DGAR
3 | EMR | 32 VILL WTZR VILL WTZR
3 | ESA | SUTH UNSA
3 | GFZ | BAKO CAS1 CRO1 DGAR MDVJ SCH2 SCUB SFER WHIT
3 | GRG | AMC2 DGAR
3 | JPL | 22 32 MCM4
3 | MIT | 22 31 22 31 KELY TIDB
4 | COD | 22 22 ALGO COCO DGAR
4 | EMR | 32 10 32 WTZR WTZR
4 | ESA | MCM4 SUTH
4 | GFZ | CAS1 CRO1 MDVJ SCUB
4 | GRG | ADIS DAV1 DGAR THTI
4 | JPL | 32 ALGO
4 | MIT | 22 9 22 ALGO ALGO
5 | ALL | 1
5 | COD | 22 32 22 DGAR
5 | EMR | WTZR WTZR
5 | ESA | 32 SUTH UNSA
5 | GFZ | 17 CRO1 FAA1 MATE ONSA SCUB SFER THTI
5 | GRG | ADIS DAV1 DGAR
5 | JPL | 22 32 TIDB
5 | MIT | 22 22 DAV1
6 | COD | 22 22 DAV1 DGAR HOB2
6 | EMR | 32 WTZR WTZR
6 | ESA | KERG SUTH
6 | GFZ | CAS1 DGAR HOB2 KARR MAW1 MDVJ SCUB UNSA
6 | GRG | ADIS DGAR USNO
6 | JPL | 22 32
6 | MIT | 12 22 12 22 32 DAV1 MAW1 MAW1 NKLG
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
----+------------+----------
G27 | 2010_11_16 | 2010141
G31 | 2010_11_19 | 2010142
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
----+--------+---------------
2 | GFZ | 1
5 | GFZ | 1
6 | GRG | 31
7. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G08 | 2 | | | | | | |
8. 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.
9. 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 | .6 1.3 .7 0 -21 -14 .04
EMR | 4.3 6.9 3.2 -11 -21 9 .36
ESA | 8.3 4.7 -3.9 99 -159 -23 -.12
GFZ | .6 1.0 -.4 23 -31 -21 .20
GRG | 3.0 11.0 1.1 40 45 -96 .28
JPL | -3.7 8.2 7.2 15 -46 -5 .25
MIT | -.5 -.8 -2.9 2 13 -31 .03
NGS | 2.2 2.7 -5.3 40 -75 4 -.06
SIO | 1.0 5.0 -4.9 69 -31 -61 .31
10. 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.
11. 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.
12. 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 1.1610.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1610.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 2.1610.[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 3.1610.[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 5.1610.0-6).
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 1610 summary. (Nov 14, 2010 - Nov 20, 2010)
Table 1.1610.a GPS week: 1610 MJD: 55514.000-55520.000
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 230| 0 0 2 61 -14 -12 -.24 10 9 | -457 106 15 70
| 0 0 1 14 18 5 .02 | 499 761
emr 89| 1 1 4 70 -33 22 .44 19 19 | 1723 -79 13 106
| 1 1 3 21 28 15 .02 | 912 1289
esa 143| 1 0 -1 -109 113 -28 .22 9 9 | -272 346 14 128
| 0 1 1 13 18 7 .06 | 496 1693
gfz 189| -1 0 -1 -9 18 0 -.15 12 11 | 11 81 23 110
| 0 0 1 74 28 10 .04 | 225 185
grg 128| 2 2 -3 -30 -159 -26 .68 17 16 | 19027 -14273 50 285
| 1 1 2 25 20 14 .03 | 53599 47569
igr n/a| 0 0 0 64 -20 25 -.06 6 5 | 17931 -873 18 75
| 0 0 0 32 25 19 .02 | 2391 1498
jpl 136| 0 0 2 15 47 43 .47 18 18 | 4584 96 18 122
| 0 1 2 21 12 82 .03 | 985 1319
mit 266| 0 -2 -4 61 -142 33 -.41 14 12 | -171 77 22 156
| 0 0 0 19 27 15 .03 | 257 342
ngs 215| -1 0 0 4 57 18 -.23 11 8 | -23321 21456 1995 3609
| 1 0 1 40 22 19 .03 | 60546 56897
sio 250| -1 3 3 -53 -31 -54 -.16 20 19 | --- --- --- ---
| 0 0 1 24 21 19 .04 | --- ---
Table 1.1610.b GPS week : 1610 MJD: 55514.000-55520.000
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 | 28 23 0 29 0 16 0 |
2 | 5 5 7 5 5 6 6 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 6 4 5 4 4 |
5 | 4 4 5 5 5 5 6 |
6 | 4 4 3 3 3 4 4 |
7 | 6 4 5 4 5 4 4 |
8 | 8 7 6 6 6 6 6 |
9 | 5 4 5 5 4 5 5 |
10 | 6 6 6 7 7 7 8 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 5 5 4 5 5 |
14 | 5 5 4 5 4 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 6 |
17 | 6 5 4 6 5 7 6 |
18 | 5 6 5 5 5 6 5 |
19 | 4 4 4 4 4 4 4 |
20 | 5 5 5 5 4 5 6 |
21 | 5 5 5 4 5 5 5 |
22 | 5 4 4 4 4 5 5 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 3 4 4 4 5 |
25 | 5 5 5 5 5 6 7 |
26 | 4 4 4 4 4 4 5 |
27 | 5 4 0 10 5 5 4 |
28 | 5 4 5 5 5 4 5 |
29 | 4 4 4 5 4 4 4 |
30 | 4 4 4 4 4 5 4 |
31 | 6 5 5 4 5 9 6 |
32 | 5 6 7 7 7 7 8 |
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 2.1610.0 GPS week: 1610 Day: 0 MJD: 55514.000
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 230| 0 0 3 88 -25 -18 -.23 10 8 | -895 843 15 64
| 24 -80 |
emr 89| 0 5 2 82 -16 -9 .46 20 20 | 719 2593 17 110
| -6 -60 |
esa 143| 1 0 0 -139 114 -40 .20 9 9 | -431 15 17 130
| 23 -56 |
gfz 189| 0 0 0 -61 0 -3 -.12 11 10 | 34 183 23 111
| -79 -60 |
grg 128| 0 1 0 -52 -136 -18 .67 16 15 | -412 692 50 267
| 75 -90 |
igr n/a| 0 0 0 92 -32 14 -.04 5 5 | 19020 2160 19 75
| -67 -41 |
jpl 136| 1 1 0 32 47 145 .49 19 18 | 3037 2791 20 103
| 38 -55 |
mit 266| 0 -2 -4 57 -164 14 -.44 13 12 | -572 691 24 161
| 2 37 |
ngs 215| 0 0 0 62 86 24 -.24 10 7 | -815 694 1991 3659
| -125 30 |
sio 250| 0 3 3 -76 -42 -60 -.12 23 20 | --- --- --- ---
| 49 45 |
Table 2.1610.1 GPS week: 1610 Day: 1 MJD: 55515.000
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 230| 0 0 4 63 -29 -6 -.23 10 9 | -650 391 14 67
| 73 -27 |
emr 89| 2 1 1 78 -2 23 .43 20 19 | 2295 526 13 105
| 6 -19 |
esa 143| 1 0 0 -102 108 -32 .21 9 8 | -416 -665 15 125
| 49 -27 |
gfz 189| -1 0 -1 -119 -8 -8 -.18 11 11 | -323 227 23 114
| -15 -48 |
grg 128| 4 4 -1 -8 -162 -30 .70 16 15 | 154 -215 61 302
| 35 -44 |
igr n/a| 0 0 0 88 -6 15 -.06 5 5 | 20212 -74 18 68
| -25 -45 |
jpl 136| 0 0 1 -2 40 173 .50 19 19 | 4871 688 19 121
| 108 -52 |
mit 266| 0 -3 -5 93 -93 7 -.40 12 10 | -65 22 21 172
| -9 9 |
ngs 215| -1 -1 0 38 67 -14 -.23 10 7 | -609 232 2254 3881
| -90 3 |
sio 250| 0 2 0 -20 -20 -80 -.16 21 17 | --- --- --- ---
| 8 64 |
Table 2.1610.2 GPS week: 1610 Day: 2 MJD: 55516.000
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 230| -1 0 3 62 -21 -22 -.22 10 9 | -844 320 18 72
| 29 -19 |
emr 89| 0 0 0 91 -23 37 .46 19 19 | 2852 -832 13 86
| -21 -19 |
esa 143| 1 -2 -1 -104 144 -24 .30 11 12 | -918 2987 17 126
| 20 -6 |
gfz 189| 0 0 0 -48 38 18 -.10 11 13 | -62 34 24 114
| -82 -24 |
grg 128| 2 2 -4 0 -189 -56 .62 18 19 | -6835 20225 41 288
| 12 -10 |
igr n/a| -1 0 0 103 -18 19 -.04 6 6 | 20103 -1462 17 74
| -67 -45 |
jpl 136| 0 0 2 12 44 38 .51 18 18 | 5560 -355 17 127
| 39 -68 |
mit 266| 0 -2 -4 36 -136 39 -.39 12 10 | -225 185 23 153
| 5 30 |
ngs 215| -1 1 0 7 50 7 -.28 11 9 | -660 -65 1827 3494
| -75 -34 |
sio 250| -2 2 2 -73 -8 -59 -.11 19 18 | --- --- --- ---
| 23 36 |
Table 2.1610.3 GPS week: 1610 Day: 3 MJD: 55517.000
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 230| 0 0 3 44 0 -11 -.23 9 9 | -539 413 16 85
| 74 -54 |
emr 89| 2 0 4 85 -5 23 .44 19 19 | 2654 -999 15 130
| -19 -34 |
esa 143| 2 0 0 -99 86 -28 .23 9 9 | -3 -560 12 133
| 30 -29 |
gfz 189| 0 1 -1 40 10 -15 -.12 12 11 | -84 161 23 106
| -91 -23 |
grg 128| 2 1 -3 -53 -144 -15 .69 17 15 | 140442 -120799 55 341
| 78 -46 |
igr n/a| 0 0 0 33 -20 56 -.07 6 5 | 19307 -2019 19 91
| -58 -65 |
jpl 136| 0 -1 1 -15 53 3 .51 19 19 | 5739 -880 19 126
| 37 -81 |
mit 266| 0 -2 -3 70 -121 41 -.39 12 10 | -25 67 21 142
| 4 25 |
ngs 215| -2 0 -1 -18 39 42 -.26 11 7 | -160624 150481 1798 3298
| 14 -17 |
sio 250| -1 3 4 -33 -31 -69 -.16 20 19 | --- --- --- ---
| 22 47 |
Table 2.1610.4 GPS week: 1610 Day: 4 MJD: 55518.000
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 230| 1 0 1 67 12 -10 -.26 10 9 | 423 -1047 17 73
| 17 -48 |
emr 89| 3 2 1 65 -55 22 .43 18 18 | 1799 -817 11 101
| -3 13 |
esa 143| 0 -2 -4 -109 101 -32 .27 10 10 | 577 -2097 16 128
| 39 4 |
gfz 189| -2 0 0 -23 -5 0 -.19 9 9 | 232 -50 22 108
| -47 -43 |
grg 128| 1 3 -3 -27 -143 -24 .71 17 16 | 465 -613 46 242
| 39 -90 |
igr n/a| 0 0 0 43 -21 0 -.08 6 6 | 17466 -2136 17 77
| -32 -71 |
jpl 136| 1 0 3 38 64 -17 .42 18 18 | 4995 -1049 19 127
| -19 -43 |
mit 266| 0 -1 -3 42 -152 51 -.44 14 11 | 251 -366 21 154
| -1 32 |
ngs 215| 0 0 2 18 75 35 -.23 12 10 | 307 -990 2042 3537
| -112 5 |
sio 250| -1 3 5 -72 -9 -53 -.19 20 18 | --- --- --- ---
| 29 18 |
Table 2.1610.5 GPS week: 1610 Day: 5 MJD: 55519.000
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 230| 0 0 1 46 -2 -10 -.29 9 9 | 49 -896 15 63
| 41 -64 |
emr 89| 2 0 7 25 -61 28 .43 18 18 | 682 -252 13 109
| 47 19 |
esa 143| 0 -1 0 -103 115 -15 .17 10 9 | -37 1692 12 118
| 37 -32 |
gfz 189| 0 0 -4 61 22 4 -.16 12 11 | 361 -254 23 111
| -41 -36 |
grg 128| 1 3 -6 -10 -154 -19 .67 16 17 | -179 -172 45 284
| 68 -94 |
igr n/a| -1 0 0 71 20 45 -.09 6 6 | 15100 -1175 18 61
| -76 -61 |
jpl 136| 1 -2 6 2 57 -35 .44 17 17 | 3751 -25 18 124
| 13 -61 |
mit 266| -1 -3 -4 69 -174 41 -.43 18 14 | -280 -244 22 156
| -11 24 |
ngs 215| -2 0 1 -27 63 22 -.21 13 9 | -109 -761 2043 3949
| 15 -14 |
sio 250| -1 4 2 -27 -70 -21 -.23 20 20 | --- --- --- ---
| 10 46 |
Table 2.1610.6 GPS week: 1610 Day: 6 MJD: 55520.000
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 230| 0 0 1 59 -37 -9 -.24 9 9 | -744 721 16 66
| 60 -21 |
emr 89| 2 1 11 66 -72 31 .46 20 20 | 1064 -772 15 102
| 4 11 |
esa 143| 2 0 -1 -106 123 -29 .14 9 9 | -680 1051 14 138
| 29 -42 |
gfz 189| -2 0 -3 88 69 2 -.15 13 12 | -81 271 25 111
| -61 -28 |
grg 128| 2 0 -3 -60 -184 -20 .68 19 17 | -446 968 57 276
| 96 -46 |
igr n/a| 0 0 0 19 -64 28 -.07 6 6 | 14315 -1406 18 81
| -17 -27 |
jpl 136| 1 0 4 37 26 0 .44 18 17 | 4138 -496 19 126
| -56 -73 |
mit 266| 0 -2 -5 59 -152 35 -.37 18 14 | -282 187 22 160
| -11 14 |
ngs 215| -2 0 0 -54 21 8 -.18 12 7 | -739 607 2016 3449
| -22 64 |
sio 250| -2 5 3 -66 -34 -36 -.19 19 20 | --- --- --- ---
| 27 24 |
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 3.1610.0 GPS week: 1610 Day: 0 MJD: 55514.000
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 | 25 --- --- 30 --- 135 --- --- --- --- 27 | 82 --- --- 101 --- 95 --- --- --- --- 77
2 | 11 23 10 10 12 4 24 8 9 24 4 | 23 31 21 22 32 19 33 22 16 22 19
3 | 3 13 9 7 9 6 11 11 11 22 3 | 18 23 20 21 25 18 25 23 21 19 20
4 | 13 11 7 4 9 3 10 15 9 28 4 | 23 25 29 27 31 25 30 32 22 34 24
5E | 7 21 8 9 18 6 20 10 7 10 4 | 13 26 16 12 24 14 25 14 18 17 15
6 | 4 12 8 7 10 6 11 14 11 17 3 | 23 29 25 24 30 23 28 30 25 25 24
7E | 17 15 9 14 20 6 18 19 10 17 5 | 69 74 69 74 78 71 73 65 68 61 68
8E | 20 19 15 18 17 5 21 26 19 62 8 | 123 124 130 126 126 125 125 126 122 132 124
9 | 10 18 6 8 16 8 16 19 8 14 4 | 14 25 16 20 20 17 24 22 19 16 14
10E | 17 18 10 15 25 5 16 16 14 21 5 | 33 34 31 33 32 31 32 43 33 28 31
11 | 8 13 9 11 14 5 16 9 9 17 4 | 23 31 26 24 38 22 30 27 22 20 23
12 | 8 22 12 12 16 6 25 15 9 17 5 | 18 30 23 27 27 20 31 23 22 22 19
13 | 7 18 7 7 18 5 21 10 11 15 4 | 23 34 24 25 40 22 33 21 22 16 21
14 | 6 19 10 11 14 5 23 11 9 22 4 | 18 29 26 27 32 19 28 20 22 19 21
15 | 7 27 9 6 19 6 26 13 10 18 5 | 13 26 19 14 27 12 26 17 15 16 14
16 | 6 29 8 10 16 6 26 13 10 17 5 | 22 36 25 21 32 20 32 20 22 21 20
17 | 13 13 7 30 14 6 15 9 10 31 5 | 26 31 32 42 34 31 33 31 34 37 31
18E | 10 26 9 9 12 6 24 14 9 29 5 | 23 31 23 19 33 19 29 23 20 34 19
19 | 6 14 9 10 9 6 11 9 6 24 3 | 31 31 30 30 29 29 29 33 31 28 29
20E | 8 30 7 13 15 5 21 13 6 19 5 | 15 32 20 18 30 15 24 21 12 21 15
21 | 7 23 9 7 17 4 22 10 7 24 4 | 18 30 18 16 33 17 32 14 18 16 17
22E | 8 23 13 10 15 5 22 16 6 21 5 | 16 27 23 12 34 17 30 21 20 22 18
23 | 6 25 8 11 14 4 24 11 9 16 4 | 17 33 20 22 29 16 30 20 14 15 15
24 | 9 17 6 11 12 3 13 7 9 18 3 | 19 24 17 16 19 16 22 20 15 18 14
X25 | 15 --- 8 7 17 6 --- 12 8 --- 5 | 29 --- 21 24 34 23 --- 21 23 --- 23
26 | 6 13 6 6 14 7 12 16 10 26 4 | 18 19 22 18 24 17 19 25 22 29 20
X27 | 10 22 8 8 14 8 --- 16 9 --- 4 | 9 21 13 12 13 12 --- 15 13 --- 11
28 | 12 21 9 8 19 6 21 11 6 18 4 | 17 31 25 23 35 18 31 23 20 23 20
X29 | 7 11 9 8 13 4 14 11 8 --- 3 | 30 30 31 31 32 30 30 34 33 --- 31
30 | 6 14 8 6 13 4 15 9 8 15 3 | 16 22 18 17 24 16 21 20 17 22 16
31 | 19 18 10 11 23 6 25 10 12 16 5 | 78 92 85 82 87 79 87 77 89 74 84
32E | 12 24 10 12 17 6 20 13 7 17 4 | 114 113 109 106 107 114 111 116 114 109 110
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 9 11 16 5 19 13 10 23 |T 31 38 32 33 38 31 38 32 31 32 31
WRMS | 8 20 9 10 15 5 18 12 7 20 |NE 25 31 25 28 31 25 31 25 24 24 25
MEDI | 8 18 9 10 15 6 20 12 9 18 |MD 22 30 23 23 32 19 30 23 22 22 20
Table 3.1610.1 GPS week: 1610 Day: 1 MJD: 55515.000
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 | 34 --- --- 54 --- 35 --- 31 40 --- 23 | 50 --- --- 88 --- 54 --- 24 30 --- 30
2 | 9 22 7 18 14 5 24 10 7 24 5 | 16 30 19 20 26 15 31 17 13 18 15
3 | 6 9 10 10 11 5 11 8 9 21 3 | 15 18 15 12 23 15 22 18 16 18 14
4 | 14 13 7 9 9 3 10 15 10 22 4 | 16 25 22 21 24 17 26 23 16 26 18
5E | 7 20 7 10 10 5 17 9 8 17 3 | 13 23 15 18 21 11 24 12 15 17 13
6 | 5 10 10 11 9 6 9 10 11 14 3 | 17 24 21 16 23 20 25 23 20 20 18
7 | 9 19 10 10 17 7 17 7 7 15 4 | 32 35 32 35 39 33 37 27 33 30 32
8E | 17 20 11 16 18 5 17 21 17 46 7 | 135 135 135 133 133 135 138 133 135 141 134
9 | 11 17 7 12 16 6 14 16 8 14 4 | 14 21 15 20 19 14 21 20 17 14 14
10E | 19 23 13 17 24 6 16 16 15 19 6 | 30 33 26 28 24 25 26 36 32 23 24
11 | 8 16 10 10 14 4 17 10 7 18 4 | 19 29 17 18 30 17 29 20 17 18 16
12 | 10 25 9 11 19 4 25 15 13 16 5 | 15 27 16 22 25 16 28 20 22 19 14
13 | 7 18 9 11 19 4 19 8 9 14 4 | 20 30 25 23 35 18 31 18 18 15 18
14 | 6 21 9 10 18 7 24 9 10 14 4 | 15 27 21 18 30 17 28 16 18 16 16
15 | 8 28 8 6 20 6 25 12 7 17 5 | 16 27 17 17 29 13 28 17 14 17 14
16 | 8 22 9 11 17 6 26 13 8 18 5 | 19 31 21 16 30 19 33 18 20 20 17
17 | 8 14 9 11 13 6 12 9 13 32 4 | 16 19 24 29 20 20 24 16 23 27 19
18E | 8 27 12 11 16 7 26 11 9 37 5 | 51 58 53 57 51 51 56 53 54 54 54
19 | 8 12 9 10 9 5 9 9 12 22 3 | 19 18 12 14 16 15 18 20 18 15 14
20E | 7 21 9 12 17 4 21 11 9 15 4 | 20 31 23 23 29 20 31 22 21 21 19
21 | 8 21 6 9 18 5 24 8 4 21 4 | 16 29 16 12 30 14 31 13 13 17 14
22E | 9 17 7 10 14 7 19 16 7 17 4 | 28 32 31 21 33 27 37 27 26 26 25
23 | 6 22 11 14 14 4 22 12 8 16 4 | 15 28 20 20 23 12 28 17 10 14 12
X24 | 9 15 12 8 14 5 --- 10 8 20 4 | 16 19 15 13 17 15 --- 17 18 18 12
X25 | 14 --- 5 8 16 6 --- 10 7 --- 4 | 20 --- 18 21 29 18 --- 16 20 --- 17
26 | 6 14 4 8 11 5 9 13 5 26 3 | 22 22 19 20 24 19 21 27 24 31 20
27 | 10 17 9 11 14 7 14 16 7 15 4 | 11 15 12 11 12 11 10 16 10 7 10
28 | 13 19 8 9 17 3 20 9 7 15 4 | 19 27 24 19 32 17 31 19 20 19 18
X29 | 10 12 6 12 13 4 15 10 5 --- 3 | 19 16 16 19 13 14 17 18 16 --- 15
30 | 7 13 7 10 12 4 12 9 7 14 3 | 16 21 18 15 25 13 23 17 13 20 14
31 | 16 16 10 15 19 6 21 13 9 14 5 | 31 37 33 39 40 30 35 27 32 26 31
32E | 15 33 10 13 19 5 19 15 12 17 5 | 116 122 116 123 121 119 116 121 115 117 117
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 9 11 16 5 19 12 10 21 |T 27 33 27 30 33 26 34 27 27 28 25
WRMS | 9 19 8 11 15 5 19 10 7 17 |NE 18 24 18 21 25 18 25 19 18 18 16
MEDI | 8 18 9 11 16 5 17 10 8 17 |MD 19 27 20 20 26 17 28 19 18 19 17
Table 3.1610.2 GPS week: 1610 Day: 2 MJD: 55516.000
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 --- --- 380 --- 57 --- --- --- --- 0 | 27 --- --- 314 --- 118 --- --- --- --- 26
2 | 13 26 13 25 14 7 26 15 9 26 6 | 16 31 23 24 28 16 32 23 15 17 16
3 | 7 10 9 8 15 8 9 12 6 19 3 | 14 23 19 21 25 18 21 23 18 20 18
4 | 14 13 13 26 9 6 8 18 11 22 5 | 22 26 31 32 31 24 29 32 25 31 24
5E | 9 19 10 12 17 4 19 14 14 18 5 | 10 23 16 15 21 10 24 13 12 16 9
6 | 5 11 8 7 11 7 9 11 6 11 3 | 19 29 28 27 30 23 27 28 24 24 25
7 | 10 22 15 10 25 4 17 7 8 17 5 | 21 31 26 21 32 19 23 18 23 21 20
8E | 15 17 11 11 20 6 16 22 12 33 6 | 85 88 81 87 80 87 85 96 83 93 86
9 | 12 16 10 10 15 7 16 14 14 15 4 | 12 24 22 17 17 16 22 20 23 15 15
10E | 16 20 18 11 23 6 16 17 22 19 6 | 22 23 25 22 28 19 24 31 30 15 18
11 | 6 15 6 8 15 5 19 9 9 17 4 | 23 30 20 21 30 22 27 26 23 20 19
12 | 9 21 13 12 16 4 22 11 9 14 4 | 17 28 28 25 23 18 27 21 19 20 18
13 | 7 21 11 11 28 4 18 8 9 17 4 | 18 31 22 24 36 17 28 15 15 17 17
14 | 6 22 7 11 19 5 21 8 7 14 4 | 17 28 22 23 31 18 29 19 19 16 19
15 | 9 21 13 9 21 4 22 12 13 16 5 | 13 24 21 17 29 11 25 16 14 15 12
16 | 7 28 10 11 14 5 26 13 10 16 5 | 18 31 21 17 30 17 33 19 20 21 18
17 | 8 11 11 9 16 6 12 8 9 29 4 | 23 25 25 37 29 25 26 23 26 34 25
18E | 10 20 10 8 16 5 22 9 9 13 4 | 30 38 38 34 39 34 38 30 35 42 34
19 | 5 13 7 10 13 7 11 8 8 20 3 | 22 24 21 22 23 21 22 24 23 21 20
20E | 8 26 11 8 20 4 21 10 10 17 4 | 24 37 24 21 30 25 31 26 20 26 21
21 | 8 19 11 9 17 5 21 9 8 20 4 | 20 30 21 21 27 18 31 17 13 17 16
22E | 7 19 11 8 15 5 18 9 6 15 4 | 22 32 29 23 31 22 34 25 25 25 24
23 | 7 22 12 14 24 5 22 11 7 16 5 | 14 27 21 21 27 15 27 17 11 14 13
24 | 7 11 4 5 14 6 11 9 8 17 3 | 13 17 15 13 17 16 18 16 12 19 12
X25 | 12 --- 7 7 16 6 --- 10 8 --- 4 | 23 --- 22 23 27 22 --- 19 20 --- 19
26 | 6 11 7 7 13 6 9 12 11 27 4 | 16 17 16 17 25 14 19 19 17 30 14
X27 | 6 --- --- --- --- 21 --- --- --- --- 0 | 22 --- --- --- --- 34 --- --- --- --- 21
28 | 12 19 7 9 19 6 19 11 9 16 4 | 15 29 20 25 33 18 28 25 18 22 19
X29 | 6 11 12 13 15 5 14 12 6 --- 4 | 21 25 22 27 22 21 22 25 22 --- 21
30 | 6 15 10 9 14 4 13 10 6 15 3 | 14 25 18 22 23 17 22 19 17 21 15
31 | 10 19 16 9 25 5 17 8 11 5 4 | 23 30 28 17 37 18 26 20 21 18 19
32E | 16 30 9 9 24 7 20 22 19 17 6 | 82 83 84 82 84 82 83 79 85 80 81
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 11 11 18 6 18 12 11 19 |T 23 31 26 35 31 26 30 26 24 26 22
WRMS | 9 19 12 13 19 6 18 10 9 18 |NE 18 26 22 35 27 23 25 21 18 20 18
MEDI | 8 19 10 9 16 5 18 11 9 17 |MD 20 28 22 22 29 18 27 21 20 20 19
Table 3.1610.3 GPS week: 1610 Day: 3 MJD: 55517.000
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 | 24 --- --- 35 --- 391 --- --- --- --- 29 | 23 --- --- 85 --- 286 --- --- --- --- 35
2 | 10 23 10 14 15 7 22 11 10 25 5 | 15 28 21 17 29 14 30 18 13 18 15
3 | 7 12 7 9 12 6 12 10 8 21 3 | 16 25 21 21 26 18 28 23 20 20 20
4 | 12 12 7 8 12 6 10 17 11 19 4 | 23 25 30 28 33 24 28 29 26 27 25
5E | 8 17 9 11 18 6 19 11 9 17 4 | 12 23 16 14 23 15 28 16 12 20 13
6 | 7 10 6 10 10 5 11 10 9 14 3 | 20 29 25 24 30 23 31 27 26 23 25
7 | 9 17 8 11 16 5 15 7 8 17 4 | 28 37 31 33 36 28 32 27 23 30 28
8E | 15 24 8 14 17 5 18 17 11 29 5 | 127 132 130 131 128 127 133 132 124 133 128
9 | 11 19 5 10 13 6 17 14 13 14 4 | 14 27 16 17 20 16 25 22 21 19 15
10E | 15 24 15 15 25 7 17 22 22 21 6 | 27 33 28 29 30 25 25 36 32 22 22
11 | 8 15 9 11 15 5 18 8 7 18 4 | 26 33 31 28 36 25 33 29 28 23 27
12 | 9 21 7 11 17 7 28 10 14 13 4 | 18 31 24 21 26 19 32 23 21 22 20
13 | 7 21 9 9 23 7 19 10 11 17 4 | 28 39 31 30 41 27 38 25 23 27 28
14 | 9 20 12 10 18 6 23 8 10 15 4 | 15 29 26 22 29 16 29 18 24 18 20
15 | 7 22 7 7 19 7 24 12 13 18 4 | 14 24 16 16 31 12 26 17 11 17 14
16 | 5 27 11 9 15 7 24 13 8 19 4 | 19 31 22 17 29 19 30 20 18 23 19
17 | 13 11 4 30 17 7 17 9 9 28 5 | 25 29 31 45 33 30 30 30 32 35 30
18E | 7 20 10 14 15 4 25 12 10 31 5 | 36 45 36 40 38 36 45 38 44 30 40
19 | 7 11 8 9 10 3 12 10 7 21 3 | 25 27 28 29 27 28 29 31 32 26 27
20E | 7 18 13 11 20 5 23 9 7 20 4 | 16 29 19 21 30 16 29 22 15 22 18
21 | 8 18 6 13 16 6 19 10 6 20 4 | 18 28 20 19 28 15 31 17 15 19 18
22E | 7 15 7 12 17 4 20 10 7 13 4 | 19 24 24 15 34 16 30 17 16 17 18
23 | 7 23 11 10 18 6 21 12 10 17 4 | 17 32 21 22 26 16 30 19 14 18 17
24 | 9 13 6 9 13 3 13 11 9 20 3 | 14 21 19 18 22 16 20 19 20 19 15
X25 | 14 --- 10 11 17 7 --- 10 10 --- 5 | 24 --- 21 23 27 22 --- 23 23 --- 22
26 | 7 12 9 10 11 7 8 12 12 27 4 | 17 20 21 17 23 16 21 24 16 29 18
X27 | 8 --- --- 11 --- 12 --- --- --- --- 10 | 13 --- --- 17 --- 16 --- --- --- --- 14
28 | 12 20 7 15 18 4 22 10 6 18 4 | 19 31 22 28 35 19 33 22 21 27 21
X29 | 5 12 11 25 17 13 17 10 9 --- 5 | 25 28 29 32 31 29 27 28 29 --- 26
30 | 7 14 9 8 16 5 11 9 8 19 3 | 18 22 21 19 28 17 23 20 16 24 18
31 | 8 15 13 11 21 5 21 8 7 8 4 | 17 26 26 20 33 17 27 20 20 18 19
32E | 14 29 9 13 23 6 19 27 20 17 6 | 97 99 95 97 100 98 96 101 100 96 97
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 9 12 17 6 19 12 11 20 |T 25 34 30 31 35 34 35 29 27 29 27
WRMS | 9 19 9 11 15 5 19 10 7 19 |NE 19 27 23 25 29 30 28 22 21 22 21
MEDI | 8 18 9 11 17 6 19 10 9 18 |MD 19 29 24 22 30 19 30 23 21 22 20
Table 3.1610.4 GPS week: 1610 Day: 4 MJD: 55518.000
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 --- --- --- --- 82 --- --- --- --- 0 | 27 --- --- --- --- 119 --- --- --- --- 24
2 | 10 23 12 10 14 4 22 14 11 27 5 | 12 27 21 14 29 14 28 18 13 18 13
3 | 7 10 7 8 13 6 11 9 10 21 3 | 12 21 21 16 25 15 21 18 18 18 17
4 | 13 10 8 12 11 6 10 18 13 19 4 | 24 27 32 28 32 26 28 27 23 24 25
5E | 8 17 8 9 24 6 19 15 14 16 4 | 12 22 17 12 23 12 23 14 13 15 12
6 | 7 8 7 9 14 5 12 9 10 13 3 | 17 26 26 20 31 19 27 22 23 22 22
7 | 10 16 13 9 17 5 19 8 11 20 4 | 20 28 25 18 29 17 25 16 20 14 17
8 | 14 20 6 9 18 6 17 17 16 28 5 | 76 80 79 77 81 79 82 75 77 73 76
9 | 9 18 9 8 15 7 14 16 7 15 4 | 14 24 19 17 17 16 21 19 20 14 16
10E | 20 20 12 11 27 6 17 26 27 25 7 | 23 32 21 26 28 24 26 41 34 28 23
11 | 9 14 8 8 15 4 16 10 10 15 3 | 22 32 27 24 31 22 28 24 23 18 23
12 | 11 19 9 11 16 3 23 12 7 16 4 | 17 26 20 25 26 20 29 23 23 23 20
13 | 7 17 8 7 22 8 19 10 11 16 4 | 19 30 22 23 36 22 28 16 25 13 18
14 | 8 15 9 7 16 4 20 9 9 15 4 | 16 28 26 19 31 18 27 20 21 19 20
15 | 11 22 11 7 22 5 24 15 11 20 5 | 18 25 19 14 33 14 26 20 15 20 16
16 | 8 25 13 8 17 6 28 13 6 21 5 | 18 31 23 20 30 19 32 19 18 23 19
17 | 11 10 10 14 18 6 14 9 14 29 5 | 25 30 30 40 29 29 30 28 32 32 30
18E | 9 25 11 10 14 4 22 10 10 20 5 | 28 37 32 27 38 27 36 29 29 41 29
19 | 8 10 7 6 10 4 10 10 10 24 3 | 22 22 28 27 23 22 20 28 28 21 24
20E | 8 20 8 12 15 6 20 10 7 16 4 | 15 29 20 20 27 18 28 19 16 18 17
21 | 8 18 7 8 17 5 23 10 11 21 4 | 15 29 18 12 29 15 30 12 13 18 15
22E | 8 16 11 7 16 3 19 10 9 13 4 | 17 26 23 16 33 17 30 19 22 22 20
23 | 7 20 9 10 15 8 22 11 9 18 4 | 15 29 19 20 25 17 26 15 15 13 14
24 | 10 13 10 8 13 4 9 12 10 18 4 | 14 21 22 17 20 17 17 18 17 19 15
X25 | 14 --- 9 7 14 5 --- 9 6 --- 4 | 30 --- 25 23 30 25 --- 24 26 --- 25
26 | 7 13 7 7 13 6 12 12 9 26 4 | 13 18 15 14 24 12 20 20 15 29 15
X27 | 10 17 7 8 10 8 14 18 11 --- 4 | 12 20 10 11 16 11 16 18 15 --- 13
X28 | 11 19 5 10 18 5 19 9 11 --- 4 | 17 31 23 22 35 20 30 20 22 --- 21
X29 | 7 11 11 6 13 6 14 11 9 --- 3 | 20 26 25 25 26 23 20 25 23 --- 22
30 | 9 13 7 8 12 4 13 11 8 16 3 | 16 26 19 17 25 17 24 18 20 24 18
31 | 13 17 13 8 17 5 21 9 8 9 4 | 18 30 25 19 30 14 26 15 23 20 19
32E | 18 26 12 10 21 8 23 30 23 15 7 | 64 73 66 68 66 69 69 83 72 70 68
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 10 9 17 6 18 14 12 20 |T 21 30 25 23 30 25 29 24 24 24 22
WRMS | 9 18 10 9 16 6 18 11 10 18 |NE 18 26 22 20 27 22 25 20 20 20 19
MEDI | 9 17 9 8 15 5 19 11 10 18 |MD 17 27 23 20 29 18 27 20 22 20 19
Table 3.1610.5 GPS week: 1610 Day: 5 MJD: 55519.000
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 | 18 --- --- 101 --- 39 --- 26 26 --- 16 | 31 --- --- 100 --- 61 --- 20 26 --- 25
2 | 9 21 11 12 13 4 22 19 12 27 5 | 9 27 19 15 26 12 27 15 14 17 13
3 | 6 13 4 9 13 4 10 10 8 23 3 | 13 18 13 14 22 14 17 13 16 14 14
4 | 11 11 9 8 9 4 7 20 13 16 4 | 19 22 25 18 29 21 22 22 20 20 20
5E | 10 18 10 11 17 5 19 17 12 16 4 | 7 20 18 9 23 10 20 18 12 19 12
6 | 6 12 6 8 12 5 9 11 10 18 3 | 17 23 19 18 27 18 23 17 20 16 18
7 | 6 14 14 8 15 6 14 12 13 16 4 | 21 31 27 28 33 25 24 23 21 25 23
8 | 13 23 8 11 18 4 17 18 11 26 5 | 69 72 68 71 65 70 69 73 70 79 69
9 | 9 18 10 8 14 6 15 16 13 15 4 | 11 22 16 12 20 12 21 16 16 16 13
10E | 15 22 15 16 21 6 15 34 23 22 7 | 24 30 26 26 29 23 23 43 36 22 21
11 | 5 15 9 8 14 8 16 14 11 12 4 | 23 29 27 24 32 21 25 28 22 21 22
12 | 8 20 13 11 17 5 20 14 12 14 5 | 12 24 22 15 27 14 24 17 15 14 15
13 | 9 16 13 7 21 8 18 12 12 16 4 | 22 32 24 22 35 23 31 21 22 20 21
14 | 6 16 6 9 15 4 19 18 12 15 4 | 11 27 16 13 28 14 25 20 16 16 15
15 | 5 23 10 7 18 5 23 19 12 20 5 | 12 26 16 12 27 11 24 18 11 18 12
16 | 8 25 7 10 17 8 27 13 9 23 5 | 14 30 18 13 28 14 31 15 18 19 16
17 | 12 12 9 36 16 6 14 15 7 26 6 | 19 22 23 42 25 25 23 25 21 29 23
18E | 9 21 9 14 19 6 24 13 17 38 6 | 50 54 52 55 52 49 54 48 53 53 53
19 | 6 11 4 8 11 5 12 18 10 21 3 | 18 19 18 15 18 18 17 27 20 17 17
20E | 8 18 8 9 17 6 20 15 11 14 4 | 13 26 18 12 25 13 24 18 16 19 13
21 | 9 19 9 13 17 5 21 13 11 21 5 | 13 30 16 13 28 12 29 10 12 19 14
22E | 9 20 9 9 16 5 18 17 11 14 4 | 14 26 22 17 27 16 26 18 22 15 17
23 | 8 19 12 10 17 7 21 13 11 17 4 | 12 29 20 16 25 14 26 13 14 12 12
24 | 8 12 8 10 17 5 11 14 10 17 4 | 12 18 19 16 23 14 17 16 14 18 12
X25 | 15 --- 9 14 18 7 --- 13 11 --- 6 | 24 --- 24 21 29 22 --- 20 21 --- 22
26 | 5 14 7 9 12 5 8 14 9 26 4 | 13 18 17 14 20 14 17 18 16 28 15
X27 | 8 20 9 7 13 5 --- 17 10 15 4 | 7 20 12 11 14 11 --- 17 9 14 10
28 | 11 17 6 12 18 4 17 10 7 17 4 | 19 30 23 26 34 21 29 22 22 20 21
X29 | 6 12 10 11 15 8 12 14 13 --- 4 | 20 22 23 23 24 21 21 22 24 --- 21
30 | 10 15 8 13 14 7 13 15 14 17 4 | 15 22 16 15 25 15 23 15 21 23 17
X31 | 8 --- --- 10 --- 14 --- --- --- --- 9 | 8 --- --- 26 --- 8 --- --- --- --- 10
32E | 13 20 11 13 18 6 19 41 26 16 7 | 89 95 91 92 94 93 95 105 96 93 91
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 10 12 16 6 17 18 13 20 |T 20 29 24 25 30 22 28 24 23 24 21
WRMS | 9 18 9 11 17 6 17 14 9 20 |NE 15 24 19 21 25 17 23 18 17 18 16
MEDI | 8 18 9 10 16 5 17 15 11 17 |MD 14 26 19 16 27 15 24 18 20 19 17
Table 3.1610.6 GPS week: 1610 Day: 6 MJD: 55520.000
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 --- --- --- --- 38 --- --- --- --- 0 | 29 --- --- --- --- 63 --- --- --- --- 26
2 | 9 23 12 16 16 7 21 18 12 27 5 | 11 28 23 22 27 14 28 15 16 18 15
3 | 7 16 8 11 13 5 13 12 8 21 4 | 16 23 23 17 30 17 26 21 18 18 19
4 | 12 13 4 13 16 5 9 18 11 12 4 | 27 28 32 26 36 30 33 29 28 24 27
5E | 10 20 9 12 16 4 23 22 10 28 5 | 13 25 18 14 23 15 27 28 17 32 16
6 | 6 13 6 10 14 5 11 11 9 17 3 | 22 28 30 23 37 24 30 28 23 23 26
7 | 6 16 10 11 20 6 15 11 6 15 4 | 21 31 24 26 30 22 27 21 24 24 24
8 | 14 25 7 14 21 4 17 15 11 27 5 | 77 81 77 74 70 76 79 77 73 87 76
9 | 11 20 7 12 14 7 15 16 9 14 4 | 18 26 14 20 23 16 25 20 16 20 15
10E | 16 26 15 22 28 6 17 35 27 17 8 | 26 33 25 30 31 27 29 45 40 23 24
11 | 5 14 8 12 17 6 18 16 8 12 4 | 31 33 36 32 37 30 31 39 32 27 29
12 | 8 22 9 11 17 7 23 12 9 13 4 | 19 29 25 20 30 19 32 23 19 21 19
13 | 9 16 10 8 22 6 18 10 12 15 4 | 23 29 25 23 34 22 29 17 23 16 21
14 | 8 19 10 9 19 6 21 17 7 16 4 | 16 27 24 20 31 17 27 24 21 20 19
15 | 7 22 8 9 19 7 23 17 7 20 4 | 17 27 20 16 33 18 27 24 19 25 17
16 | 6 33 10 13 19 5 27 12 12 20 5 | 21 38 21 19 33 20 35 20 19 23 19
17 | 14 15 7 31 19 6 16 12 11 27 6 | 32 34 38 50 40 38 34 40 40 38 36
18E | 8 22 12 10 16 9 24 12 10 20 5 | 24 33 24 23 30 21 34 23 24 35 23
19 | 9 13 9 7 12 5 14 17 9 24 4 | 31 31 34 32 32 32 31 37 33 30 31
20E | 7 23 12 12 31 5 20 17 12 16 5 | 14 27 16 13 27 15 26 19 16 18 12
21 | 10 21 9 10 17 5 22 13 13 22 5 | 16 30 14 17 28 15 30 17 15 21 13
22E | 7 16 14 11 16 7 22 16 8 13 4 | 15 25 21 16 29 15 29 21 15 18 16
23 | 7 22 9 11 22 6 24 13 9 19 5 | 15 29 21 19 27 17 27 13 14 13 14
24 | 10 15 8 15 16 4 9 17 8 18 4 | 16 21 22 20 23 18 20 22 16 20 16
X25 | 19 --- 10 14 20 6 --- 13 12 --- 6 | 38 --- 28 27 36 31 --- 32 28 --- 30
26 | 7 14 10 9 15 7 9 13 12 27 4 | 19 26 26 21 33 21 25 26 28 36 22
27 | 8 22 6 11 12 5 13 16 8 13 4 | 12 25 10 13 21 14 19 16 11 15 11
28 | 11 25 7 15 19 6 19 10 10 16 4 | 23 35 26 28 36 24 34 26 27 27 25
X29 | 6 14 7 11 21 6 14 11 11 --- 4 | 30 34 36 34 41 34 34 37 33 --- 34
30 | 6 13 7 11 17 5 12 16 11 17 4 | 17 22 18 18 29 19 25 19 17 27 18
X31 | 9 --- 10 --- 3216 7 21 11 9 --- 5 | 8 --- 5 --- 7 7 18 5 6 --- 8
32E | 14 24 11 14 25 6 20 40 25 16 7 | 104 109 105 107 111 110 108 113 112 107 107
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 9 13 19 6 18 18 12 19 |T 25 33 27 27 34 26 32 28 26 28 25
WRMS | 9 20 9 12 17 6 17 14 7 20 |NE 21 28 23 23 30 23 28 23 21 23 21
MEDI | 8 20 9 11 17 6 18 15 10 17 |MD 19 29 24 21 31 20 29 23 21 23 19
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 4.1610 GPS week: 1610 MJD: 55514.0-55520.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 |U 10 19 33 |U 8 9 26 |U 7 8 18 |
emr | emr 2816 |U 14 23 38 |U 9 10 30 | 10 10 24 |
esa | esa 2934 | 10 18 31 |U 8 9 25 | 8 9 21 |
gfz | gfz 2976 |U 12 19 37 |U 8 10 28 |U 8 10 22 |
grg | grg 2934 | 13 23 37 |U 9 11 31 | 10 12 26 |
igr | igr 2945 | 10 18 29 | 8 10 26 | 8 9 19 |
igs | igs 2925 | 11 20 34 | 9 10 26 | 8 9 20 |
jpl | jpl 2787 |U 14 22 35 | 11 10 31 |U 9 10 22 |
mit | mit 2962 |U 15 21 38 |U 8 10 26 |U 9 10 23 |
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 5.1610.0 GPS week: 1610 Day: 0 MJD: 55514.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 | 13 19 32 | 9 9 23 | 7 9 23 |
emr | emr 2872 | 16 14 38 | 10 10 23 | 10 11 23 |
esa | esa 2976 | 7 7 29 | 8 9 21 | 8 11 24 |
gfz | gfz 3037 | 15 18 40 | 8 11 22 | 9 13 24 |
grg | grg 2976 | 11 12 30 | 9 12 27 | 11 14 28 |
igr | igr 3010 | 13 12 22 | 8 11 25 | 8 12 22 |
igs | igs 2970 | 16 24 37 | 9 12 20 | 9 12 23 |
jpl | jpl 2775 | 23 20 43 | 10 9 25 | 9 11 23 |
mit | mit 2976 | 12 19 32 | 9 11 21 | 8 11 25 |
Table 5.1610.1 GPS week: 1610 Day: 1 MJD: 55515.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3050 | 8 6 20 | 8 12 22 | 7 10 19 |
emr | emr 2870 | 9 10 32 | 11 12 27 | 15 15 23 |
esa | esa 2976 | 8 5 21 | 8 11 20 | 8 9 22 |
gfz | gfz 3033 | 9 5 24 | 8 12 22 | 8 11 21 |
grg | grg 2976 | 26 24 36 | 8 12 25 | 10 12 25 |
igr | igr 3017 | 7 4 20 | 8 12 18 | 9 12 22 |
igs | igs 2917 | 8 6 21 | 11 14 26 | 8 10 22 |
jpl | jpl 2774 | 8 8 26 | 13 12 30 | 9 12 26 |
mit | mit 3072 | 8 6 22 | 9 11 23 | 10 15 23 |
Table 5.1610.2 GPS week: 1610 Day: 2 MJD: 55516.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 22 88 112 | 9 8 27 | 10 9 19 |
emr | emr 2776 | 25 90 94 | 10 7 36 | 13 13 28 |
esa | esa 2880 | 20 89 85 | 9 7 26 | 10 11 22 |
gfz | gfz 2938 | 21 86 94 | 10 7 25 | 11 14 27 |
grg | grg 2880 | 20 85 102 | 10 8 33 | 11 15 28 |
igr | igr 2945 | 20 89 80 | 8 7 24 | 10 13 21 |
igs | igs 2880 | 21 88 100 | 9 7 25 | 10 12 21 |
jpl | jpl 2775 | 25 87 84 | 12 8 36 | 12 13 26 |
mit | mit 2880 | 21 86 102 | 9 9 31 | 11 10 22 |
Table 5.1610.3 GPS week: 1610 Day: 3 MJD: 55517.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 | 6 8 15 | 7 8 22 | 7 7 18 |
emr | emr 2776 | 12 16 26 | 8 9 35 | 9 10 23 |
esa | esa 2880 | 8 7 19 | 7 9 24 | 7 8 19 |
gfz | gfz 3043 | 7 6 18 | 6 9 21 | 7 7 19 |
grg | grg 2880 | 8 7 18 | 7 11 29 | 9 11 24 |
igr | igr 2814 | 7 7 21 | 8 12 27 | 7 7 19 |
igs | igs 2880 | 12 7 21 | 7 9 25 | 7 7 19 |
jpl | jpl 2776 | 11 11 22 | 9 10 35 | 10 10 19 |
mit | mit 2880 | 41 17 53 | 8 10 22 | 11 10 23 |
Table 5.1610.4 GPS week: 1610 Day: 4 MJD: 55518.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 8 6 21 | 9 9 37 | 6 6 14 |
emr | emr 2871 | 9 7 26 | 9 9 36 | 9 8 23 |
esa | esa 2976 | 8 5 19 | 8 9 35 | 7 6 20 |
gfz | gfz 2964 | 9 7 21 | 8 8 39 | 7 7 19 |
grg | grg 2976 | 8 6 20 | 8 9 40 | 8 10 21 |
igr | igr 2936 | 8 5 19 | 8 11 36 | 7 6 16 |
igs | igs 2976 | 8 5 19 | 8 8 35 | 7 6 16 |
jpl | jpl 2863 | 9 6 22 | 10 10 37 | 8 8 19 |
mit | mit 2976 | 9 9 21 | 9 9 34 | 8 7 19 |
Table 5.1610.5 GPS week: 1610 Day: 5 MJD: 55519.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 6 4 13 | 8 12 29 | 7 6 20 |
emr | emr 2776 | 12 12 29 | 8 12 32 | 9 8 24 |
esa | esa 2880 | 8 8 20 | 9 12 31 | 8 8 21 |
gfz | gfz 2951 | 8 8 22 | 9 12 40 | 7 8 22 |
grg | grg 2880 | 8 8 19 | 10 15 32 | 7 8 22 |
igr | igr 2917 | 7 5 18 | 7 12 30 | 7 8 18 |
igs | igs 2879 | 9 8 19 | 7 11 29 | 7 8 21 |
jpl | jpl 2680 | 14 17 27 | 9 12 35 | 8 6 21 |
mit | mit 2976 | 8 8 20 | 6 12 28 | 9 8 27 |
Table 5.1610.6 GPS week: 1610 Day: 6 MJD: 55520.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 7 4 18 | 10 8 21 | 7 7 17 |
emr | emr 2776 | 13 10 22 | 10 7 25 | 8 7 24 |
esa | esa 2976 | 7 6 22 | 9 9 20 | 7 7 20 |
gfz | gfz 2866 | 13 4 38 | 10 10 25 | 8 9 24 |
grg | grg 2976 | 11 21 32 | 9 8 29 | 12 16 37 |
igr | igr 2976 | 8 5 20 | 9 8 23 | 7 7 17 |
igs | igs 2975 | 8 5 21 | 9 7 19 | 6 7 19 |
jpl | jpl 2872 | 9 7 22 | 10 8 22 | 8 7 21 |
mit | mit 2976 | 8 4 18 | 9 8 21 | 7 8 23 |
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 6.1610 GPS week: 1610 MJD: 55514.500-55520.500
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 | 29 -50 -21 266 -5 | -1 15
| 18 18 26 41 6 | 3
emr uuuuu | -3 -6 -18 106 -1 | 44 46
| 26 17 124 80 4 | 2
esa uuuuu | 11 -37 21 -129 -5 | -1 16
| 18 12 71 124 6 | 3
gfz uuuuu | 21 55 -53 2 8 | -3 17
| 12 25 65 58 3 | 5
grg uuuux | 44 -62 58 181 0 | 0 26
| 29 27 105 65 30 | 2
igr xxxxx | 35 44 85 81 2 | -2 15
| 15 27 64 96 4 | 3
irf xxxxx | -16 -4 -47 3 3 | 7 19
| 6 14 71 36 7 | 5
jpl uuuuu | 46 -27 -55 199 -10 | 10 19
| 15 52 63 120 6 | 5
mit uuuuu | -40 -1 -179 -35 10 | 16 24
| 13 19 118 55 6 | 7
ngs uuuuu | -21 52 83 -126 -1 | -4 14
| 32 48 61 111 9 | 3
sio uuuuu | -56 -28 199 109 1 | 20 26
| 20 25 96 66 10 | 5
Table 7.1610.0 GPS week: 1610 Day: 0 MJD: 55514.500
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 | 56 -44 -8 289 -5 | 2 15
emr uuuuu | 36 -14 -97 161 -3 | 44 47
esa uuuuu | 32 -43 -24 -323 -10 | 2 18
gfz uuuuu | 36 59 20 63 12 | -8 18
grg uuuux | 66 -95 125 134 -10 | 0 30
igr xxxxx | 17 47 63 81 6 | -3 16
irf xxxxx | -24 -20 11 -20 10 | 3 18
jpl uuuuu | 31 -58 -83 423 -15 | 17 26
mit uuuuu | -61 -22 -82 -56 11 | 9 20
ngs uuuuu | -54 105 -12 15 -7 | 0 14
sio uuuuu | -69 -69 290 47 11 | 15 23
Table 7.1610.1 GPS week: 1610 Day: 1 MJD: 55515.500
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 | 11 -71 -27 221 -13 | 0 13
emr uuuuu | 3 -4 -17 211 -5 | 43 45
esa uuuuu | 11 -47 -63 -228 -1 | -1 16
gfz uuuuu | 32 17 30 -46 7 | -8 18
grg uuuux | 28 -33 -80 173 1 | 1 30
igr xxxxx | 29 27 108 42 6 | -4 16
irf xxxxx | -16 2 9 -4 6 | 3 18
jpl uuuuu | 36 -106 -60 278 -9 | 14 23
mit uuuuu | -25 11 -125 -24 12 | 9 20
ngs uuuuu | -19 92 108 -16 -7 | -1 14
sio uuuuu | -80 -6 309 60 7 | 15 24
Table 7.1610.2 GPS week: 1610 Day: 2 MJD: 55516.500
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 -48 29 326 -7 | -4 16
emr uuuuu | 7 2 -225 167 -3 | 40 43
esa uuuuu | -6 -39 15 -149 0 | -5 16
gfz uuuuu | 12 63 -16 79 13 | -9 19
grg uuuux | -2 -31 -54 240 -45 | -1 30
igr xxxxx | 33 48 83 -105 3 | -6 16
irf xxxxx | -12 -19 11 42 10 | 2 18
jpl uuuuu | 56 -58 -40 68 -12 | 8 17
mit uuuuu | -42 -24 -76 22 18 | 9 19
ngs uuuuu | 22 56 114 -207 -12 | -5 16
sio uuuuu | -48 -42 250 104 7 | 15 24
Table 7.1610.3 GPS week: 1610 Day: 3 MJD: 55517.500
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 | 36 -68 -37 233 -6 | -1 17
emr uuuuu | 16 25 -41 31 -2 | 43 46
esa uuuuu | 11 -24 -47 -55 -4 | -1 18
gfz uuuuu | 5 97 -91 -75 9 | -3 21
grg uuuux | 28 -72 61 181 -18 | 3 26
igr xxxxx | 47 64 64 203 3 | -3 18
irf xxxxx | -18 6 -37 -11 5 | 8 22
jpl uuuuu | 63 -31 50 127 -4 | 9 18
mit uuuuu | -43 2 -147 7 17 | 15 27
ngs uuuuu | -1 -8 159 -79 -5 | -4 16
sio uuuuu | -65 -16 215 107 2 | 21 29
Table 7.1610.4 GPS week: 1610 Day: 4 MJD: 55518.500
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 | 37 -31 -43 306 -8 | 3 14
emr uuuuu | -24 -11 47 125 1 | 48 49
esa uuuuu | -15 -53 48 -122 2 | 3 15
gfz uuuuu | 32 33 -71 28 6 | 3 15
grg uuuux | 79 -53 29 227 40 | -2 23
igr xxxxx | 60 18 23 116 3 | 2 13
irf xxxxx | -11 -14 -26 25 1 | 14 19
jpl uuuuu | 32 5 -8 217 -20 | 12 18
mit uuuuu | -43 -13 -128 -10 8 | 23 28
ngs uuuuu | -16 98 29 -273 3 | -2 15
sio uuuuu | -29 -43 186 153 1 | 27 30
Table 7.1610.5 GPS week: 1610 Day: 5 MJD: 55519.500
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 | 42 -25 -16 240 3 | -1 13
emr uuuuu | -41 -31 170 34 7 | 46 47
esa uuuuu | 10 -21 129 -91 -12 | -1 13
gfz uuuuu | 14 57 -126 5 5 | 3 15
grg uuuux | 72 -52 104 245 38 | -3 21
igr xxxxx | 39 92 39 103 -2 | 0 13
irf xxxxx | -22 16 -149 42 -4 | 13 19
jpl uuuuu | 39 3 -104 130 -5 | 7 15
mit uuuuu | -46 27 -337 -38 5 | 23 28
ngs uuuuu | -8 1 54 -227 12 | -6 13
sio uuuuu | -68 6 67 234 -9 | 25 29
Table 7.1610.6 GPS week: 1610 Day: 6 MJD: 55520.500
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 -62 -43 244 3 | -4 14
emr uuuuu | -19 -6 34 12 -3 | 44 46
esa uuuuu | 34 -31 86 66 -9 | -5 16
gfz uuuuu | 20 59 -119 -39 8 | 1 15
grg uuuux | 38 -98 222 66 -9 | 0 20
igr xxxxx | 19 15 216 127 -4 | -2 14
irf xxxxx | -8 -2 -146 -55 -7 | 10 18
jpl uuuuu | 65 54 -140 153 -7 | 3 15
mit uuuuu | -22 9 -358 -145 0 | 22 27
ngs uuuuu | -72 20 127 -96 10 | -8 13
sio uuuuu | -32 -29 77 56 -15 | 22 27
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