[IGSREPORT-20431] Wk 1666 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Dec 29 04:58:26 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1666 (Dec 11, 2011 - Dec 17, 2011)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1666[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1666[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1666[0-6].cls IGS GPS clock combination summary report.
igs16667.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16667.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because of poorer consistency (GRG),
they provide broadcast clocks (NGS), or clock corrections are not provided
(SIO). The clock information not used is still compared to combination for
completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | EMR | IRKT
0 | ESA | NNOR POTS TIXI UNSA
0 | GFZ | 12 16 28 GMSD GUUG KOUC MDVJ OHI2 TLSE
0 | GRG | BRST USN3
0 | JPL | 25 30 AREQ KARR
0 | MIT | 7 21 27 29 30 7 21 27 29 30 DAV1 NNOR NNOR
1 | COD | 12 12
1 | ESA | UNSA
1 | GFZ | 12 16 28 BRFT BRUS GMSD KOUR NRIL OHI2 STHL TWTF
1 | GFZ | WILL
1 | GRG | AMC2
1 | JPL | 30 AREQ BRUS
1 | MIT | 27 30 27 30 BRUS DAV1 BRUS
2 | COD | 16 27 16 27 HNPT XMIS
2 | EMR | GRAZ WTZR
2 | ESA | KOUR UNSA
2 | GFZ | 28 BRFT CAS1 COCO KARR MDVJ TSKB
2 | GRG | KOUR SANT USN3 USNO
2 | JPL | 30 AREQ KARR
2 | MIT | 16 21 27 30 16 21 27 30 DAV1 NICO SPT0 DAV1 IRKT
2 | MIT | NICO SPT0
3 | COD | BRUS NICO BRUS NICO WROC
3 | EMR | 30 WTZR WTZR WUHN
3 | ESA | WUHN CONZ KOUR MATE
3 | GFZ | BOGT BRFT BRUS DGAR KARR MANA NICO OHI2
3 | GRG | AMC2 KOUR NOVM SANT
3 | JPL | AREQ KARR POL2
3 | MIT | 27 30 27 30 CAS1 WTZR
4 | COD | WROC WROC
4 | EMR | 30 30
4 | ESA | KOUR UNSA
4 | GFZ | MANA WUHN
4 | GRG | AMC2 KOUR
4 | JPL | AREQ
4 | MIT | 27 27
5 | ESA | NICO KOUR NICO UNSA
5 | GFZ | 30 ARTU KARR KELY KIRU MDVJ NYAL WUHN
5 | GRG | AMC2 KOUR
5 | JPL | AREQ
5 | MIT | 3 6 27 30 31 3 6 27 30 31 DAV1 MAW1 WUHN DAV1 MAW1
5 | MIT | SYOG WTZR WUHN
6 | COD | KARR POTS XMIS
6 | EMR | 30 30 WTZR WUHN
6 | ESA | KOUR UNSA
6 | GFZ | 30 BRFT KIRU MDVJ
6 | GRG | AMC2 KOUR
6 | JPL | 27 AREQ KOUR
6 | MIT | 2 30 2 30 CAS1 MAW1 WTZR CAS1 CONZ HYDE MAW1
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
----+------------+----------
G25 | 2011_12_15 | 2011104
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
7. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the current IGS reference frame. These rotations were
estimated in the IGS SINEX combination process, performed by the IGS Reference
Frame Coordinator at the Institut Geographique National (IGN). 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 | .4 .6 .0 -55 -9 32 .07
EMR | 3.6 5.1 11.9 4 13 8 .34
ESA | 6.8 5.1 -1.7 86 -183 108 .08
GFZ | -.7 1.4 -.8 -54 18 -1 .29
GRG | 7.5 1.4 -4.9 -38 17 3 -.01
JPL | -1.7 7.1 15.4 14 -45 73 .22
MIT | 8.4 4.8 1.2 -23 12 -25 .19
NGS | 7.6 1.0 -.7 5 -60 47 .25
SIO | 2.1 4.6 8.7 37 -16 -2 .16
8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1666.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1666.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 2.1666.[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 3.1666.[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 5.1666.0-6).
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 1666 summary. (Dec 11, 2011 - Dec 17, 2011)
Table 1.1666.a GPS week: 1666 MJD: 55906.000-55912.000
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 255| 0 0 3 96 -54 -13 -.33 9 8 | -49 -523 19 70
| 0 0 0 8 20 13 .04 | 372 923
emr 94| -1 1 8 -29 -90 -29 .36 19 19 | 2761 255 15 89
| 1 1 1 44 27 16 .07 | 825 882
esa 132| 0 0 0 -97 170 30 .12 7 7 | 563 -377 14 131
| 0 0 0 13 21 20 .05 | 655 918
gfz 194| 0 -1 -5 105 -115 -19 .27 12 12 | 16 -74 33 110
| 1 0 1 48 46 7 .25 | 221 448
grg 124| 2 0 -8 52 -102 4 .62 16 15 | 278 -189 49 217
| 1 0 1 20 24 9 .03 | 346 556
igr n/a| 0 0 0 -14 -70 -31 -.18 5 5 | -2211 78 20 77
| 0 0 0 12 21 21 .08 | 810 829
jpl 125| -2 0 5 -42 10 42 .51 14 14 | 3265 350 17 81
| 1 0 2 9 25 36 .05 | 1333 820
mit 266| 2 0 -4 26 -117 -25 -.45 12 11 | 3 -256 22 151
| 0 0 0 14 37 11 .06 | 267 448
ngs 214| 0 0 -1 -22 58 -7 -.34 10 8 | -18201 23336 1641 3283
| 0 0 1 35 27 18 .10 | 47728 62592
sio 247| 0 1 2 -90 -26 -7 -.19 17 16 | --- --- --- ---
| 0 1 0 18 44 14 .02 | --- ---
Table 1.1666.b GPS week : 1666 MJD: 55906.000-55912.000
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 | 6 5 6 5 5 6 6 |
2 | 4 4 4 4 5 4 4 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 4 4 4 4 4 4 4 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 5 4 4 4 4 |
8 | 4 4 5 4 5 4 4 |
9 | 4 4 4 4 4 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 4 4 4 4 5 6 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 5 4 5 5 |
16 | 5 5 5 4 4 4 4 |
17 | 5 4 4 4 5 4 4 |
18 | 4 4 4 5 4 4 4 |
19 | 4 4 4 4 4 4 5 |
20 | 4 4 5 4 4 4 5 |
21 | 4 3 4 4 4 4 4 |
22 | 4 3 3 4 4 4 4 |
23 | 4 5 5 4 5 6 5 |
25 | 6 5 5 5 0 7 5 |
26 | 4 4 5 4 4 5 5 |
27 | 8 7 8 9 8 7 4 |
28 | 4 4 6 4 4 4 4 |
29 | 5 5 5 5 5 6 5 |
30 | 8 8 8 8 7 7 8 |
31 | 4 4 4 4 5 4 4 |
32 | 5 4 5 4 4 4 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1666.0 GPS week: 1666 Day: 0 MJD: 55906.000
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 255| 0 0 3 95 -64 -24 -.25 8 8 | 408 -1313 21 91
| 24 20 |
emr 94| 0 1 11 -6 -111 -43 .47 18 18 | 2609 -1128 16 113
| -14 -8 |
esa 132| 0 0 -1 -91 138 46 .20 7 7 | 624 -1557 12 160
| 20 13 |
gfz 194| 0 -1 -4 39 -79 -18 -.30 11 11 | 401 -784 33 118
| -13 34 |
grg 124| 1 -1 -8 58 -76 6 .65 17 16 | 796 -1088 42 208
| 3 -14 |
igr n/a| 0 0 0 -16 -82 -51 -.06 5 5 | -2041 -1301 22 66
| 31 64 |
jpl 125| -4 -1 4 -47 -23 64 .61 14 14 | 2374 -943 20 96
| 62 -12 |
mit 266| 1 0 -3 8 -48 -27 -.35 13 11 | 263 -754 22 154
| 1 10 |
ngs 214| 0 0 0 30 34 -15 -.20 10 8 | -126438 165271 1600 3389
| -116 17 |
sio 247| 0 0 1 -118 63 0 -.17 19 18 | --- --- --- ---
| 44 -33 |
Table 2.1666.1 GPS week: 1666 Day: 1 MJD: 55907.000
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 255| 0 0 4 99 -30 -8 -.35 8 8 | -497 -22 18 75
| 9 -49 |
emr 94| 0 1 9 -24 -44 1 .38 19 19 | 1525 657 18 94
| -27 -68 |
esa 132| 0 0 0 -116 188 5 .11 7 7 | 1212 -1089 16 191
| 38 -20 |
gfz 194| -2 -1 -4 137 -205 -23 .37 11 11 | -214 -63 35 110
| -36 22 |
grg 124| 0 -1 -9 54 -103 -1 .67 16 15 | 224 -650 39 201
| 14 -44 |
igr n/a| -1 0 0 -5 -63 -59 -.15 4 4 | -3332 399 20 72
| -34 33 |
jpl 125| 0 0 5 -43 38 84 .51 14 14 | 1430 696 19 75
| 32 -46 |
mit 266| 2 0 -5 27 -141 -32 -.44 11 9 | 0 -258 22 159
| -24 39 |
ngs 214| 0 1 -1 -31 101 25 -.25 10 8 | -486 -97 1454 2703
| -106 -44 |
sio 247| 0 0 1 -106 -52 -28 -.19 17 15 | --- --- --- ---
| 52 15 |
Table 2.1666.2 GPS week: 1666 Day: 2 MJD: 55908.000
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 255| 0 0 3 98 -25 -29 -.32 8 8 | -130 -378 17 50
| 22 -41 |
emr 94| 0 3 6 49 -75 -23 .34 24 23 | 2162 806 16 80
| -94 -11 |
esa 132| 0 0 1 -111 178 60 .11 7 7 | 895 -402 16 106
| 30 -21 |
gfz 194| -1 -2 -5 54 -149 -27 .35 13 13 | 216 -399 33 101
| -25 3 |
grg 124| 1 0 -10 44 -79 -12 .61 16 15 | 230 -172 61 203
| 26 -52 |
igr n/a| 0 0 0 -13 -63 -21 -.16 5 5 | -2899 799 19 81
| 1 43 |
jpl 125| -1 0 1 -38 32 22 .54 14 14 | 2150 964 17 76
| 1 -41 |
mit 266| 1 0 -3 14 -152 -7 -.42 11 11 | 53 -335 19 115
| -20 51 |
ngs 214| 0 0 1 12 88 -14 -.27 11 9 | -145 -260 1399 3036
| -78 -92 |
sio 247| -1 0 1 -92 -56 -5 -.18 17 16 | --- --- --- ---
| 9 20 |
Table 2.1666.3 GPS week: 1666 Day: 3 MJD: 55909.000
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 255| -1 0 4 100 -66 1 -.32 8 8 | 3 -939 17 61
| 25 -20 |
emr 94| -2 0 6 -36 -90 -46 .40 19 19 | 3112 472 16 85
| 24 -38 |
esa 132| 1 0 0 -77 143 26 .14 6 6 | -514 -510 13 109
| 16 -11 |
gfz 194| 0 -1 -8 76 -83 -12 .37 13 14 | 53 -14 34 111
| -35 13 |
grg 124| 1 0 -9 39 -93 17 .59 16 15 | 312 -104 55 225
| 36 -50 |
igr n/a| 0 0 -1 -11 -98 -17 -.14 5 5 | -1785 459 18 72
| 2 52 |
jpl 125| -1 0 5 -48 1 2 .49 14 14 | 3548 759 16 87
| 67 -17 |
mit 266| 2 0 -3 44 -113 -28 -.44 12 11 | 25 -502 22 150
| -24 30 |
ngs 214| 0 0 -2 -5 37 0 -.36 11 8 | -9 -899 1459 3236
| 14 38 |
sio 247| 0 1 2 -78 -26 -11 -.18 14 15 | --- --- --- ---
| 35 6 |
Table 2.1666.4 GPS week: 1666 Day: 4 MJD: 55910.000
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 255| 0 0 1 102 -54 -17 -.31 9 9 | -401 960 26 78
| 20 3 |
emr 94| -1 1 9 -71 -89 -38 .36 18 18 | 4066 -894 15 84
| 24 -16 |
esa 132| 1 0 0 -86 178 42 .14 6 6 | -159 1047 19 127
| -16 -28 |
gfz 194| -1 0 -4 149 -101 -21 .36 13 12 | -83 682 37 114
| 7 -5 |
grg 124| 1 0 -7 58 -102 10 .60 16 17 | 601 -176 54 251
| 14 -37 |
igr n/a| 0 0 0 -39 -66 -40 -.19 5 5 | -805 -922 23 85
| 12 15 |
jpl 125| -3 0 7 -24 2 -6 .50 14 13 | 5212 -738 17 72
| 43 -6 |
mit 266| 2 0 -4 25 -124 -22 -.46 11 11 | 337 -446 26 176
| -7 47 |
ngs 214| 0 0 -1 -55 40 0 -.42 11 8 | -437 1066 1615 3435
| -40 0 |
sio 247| 0 1 3 -84 -46 -12 -.19 15 14 | --- --- --- ---
| 60 29 |
Table 2.1666.5 GPS week: 1666 Day: 5 MJD: 55911.000
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 255| 0 0 3 77 -54 -24 -.36 9 9 | 467 -1829 18 73
| 34 -22 |
emr 94| 0 1 6 -85 -87 -31 .32 19 19 | 2545 940 17 103
| 25 -6 |
esa 132| 0 0 0 -101 192 21 .06 7 7 | 1140 615 15 115
| 42 -21 |
gfz 194| 0 0 -5 164 -104 -8 .37 10 10 | -143 40 32 105
| -41 -15 |
grg 124| 3 0 -8 25 -108 9 .65 16 14 | 45 260 49 236
| 19 -9 |
igr n/a| 0 0 -1 1 -32 1 -.30 6 6 | -2367 546 20 86
| -8 12 |
jpl 125| -2 -1 7 -41 37 52 .47 14 14 | 3867 804 16 76
| 10 -34 |
mit 266| 3 0 -5 47 -150 -15 -.49 14 13 | -202 -163 29 156
| -37 40 |
ngs 214| 0 0 0 -65 67 -29 -.44 10 8 | 316 -1614 1730 3218
| 27 -73 |
sio 247| -1 2 2 -62 -61 18 -.20 17 18 | --- --- --- ---
| 26 11 |
Table 2.1666.6 GPS week: 1666 Day: 6 MJD: 55912.000
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 255| 0 -2 4 103 -84 6 -.36 9 9 | -198 -142 16 66
| 28 27 |
emr 94| -3 0 10 -33 -133 -24 .26 19 19 | 3312 933 12 69
| -4 9 |
esa 132| 1 0 0 -96 173 11 .07 6 6 | 743 -744 12 110
| 16 -41 |
gfz 194| 0 -1 -2 118 -81 -27 .37 10 10 | -115 15 28 115
| -53 -23 |
grg 124| 3 0 -7 89 -149 -1 .58 15 14 | -256 604 45 201
| -15 3 |
igr n/a| 0 0 -1 -14 -90 -30 -.24 5 5 | -2248 567 20 77
| -5 12 |
jpl 125| -1 1 6 -54 -14 77 .46 14 14 | 4280 914 15 88
| 24 -65 |
mit 266| 1 1 -4 16 -89 -44 -.55 15 14 | -451 665 19 147
| -5 32 |
ngs 214| 0 0 -3 -39 39 -22 -.42 10 8 | -212 -110 2235 3964
| -3 -43 |
sio 247| -2 4 2 -87 -2 -17 -.24 21 18 | --- --- --- ---
| 58 35 |
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 3.1666.0 GPS week: 1666 Day: 0 MJD: 55906.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 15 5 19 15 6 23 9 11 37 5 | 61 68 65 68 74 67 74 68 69 52 64
2 | 7 14 6 10 16 5 12 11 9 28 4 | 43 45 43 43 46 42 43 44 42 44 42
3 | 10 14 4 10 15 4 10 21 6 12 4 | 19 20 16 21 24 16 20 21 18 15 15
4 | 7 11 5 9 14 5 9 12 10 33 4 | 45 45 46 46 53 46 46 46 44 46 44
5 | 8 23 5 11 18 5 11 9 8 14 3 | 23 37 23 19 26 22 28 24 21 23 19
6 | 4 14 5 12 12 5 9 14 10 13 3 | 25 25 24 29 31 24 27 27 25 24 23
7 | 5 17 9 10 23 4 13 18 5 11 4 | 20 29 22 20 32 19 26 24 20 21 18
8 | 9 14 7 9 17 5 10 9 7 26 3 | 15 23 16 17 20 15 23 18 16 31 14
9 | 6 17 6 7 14 4 13 8 9 17 3 | 22 27 22 18 27 19 29 22 20 21 19
10 | 7 14 8 8 16 4 14 10 9 19 3 | 25 27 20 17 24 21 27 22 21 24 19
11 | 7 16 6 14 11 4 12 9 10 25 4 | 50 57 58 58 66 56 58 57 58 45 55
12E | 8 19 9 10 12 4 16 14 8 12 4 | 46 47 44 44 45 41 43 39 46 40 42
13 | 6 19 5 9 26 3 11 8 10 8 3 | 22 29 25 25 41 22 31 19 27 20 22
14 | 6 19 7 8 17 6 11 8 9 12 3 | 22 27 22 20 35 22 28 21 20 20 21
15 | 9 18 5 9 21 7 18 10 12 11 4 | 31 36 34 36 41 29 39 33 30 29 30
16E | 7 20 10 12 15 3 13 22 12 14 4 | 20 26 20 21 22 21 21 28 23 23 19
17 | 9 22 8 11 12 5 17 19 8 28 5 | 59 62 58 54 53 55 58 54 57 57 54
18 | 8 23 6 10 17 3 12 13 10 15 4 | 20 38 25 13 30 20 28 20 19 21 20
19 | 8 21 7 11 12 4 17 10 6 21 4 | 21 29 23 24 25 21 26 25 21 25 20
20 | 8 16 7 14 18 4 12 13 11 19 4 | 21 28 20 18 25 16 24 17 15 24 15
21 | 6 13 3 9 12 4 10 8 12 21 3 | 41 50 47 44 47 43 48 45 41 41 43
22 | 8 21 6 10 17 5 8 13 10 16 4 | 25 34 22 16 32 21 27 21 21 23 20
23 | 6 21 6 9 24 6 19 9 9 12 4 | 30 39 29 29 40 31 37 29 28 31 28
X25E | 10 27 8 20 15 9 19 12 16 --- 5 | 12 28 14 23 17 12 17 11 20 --- 10
26 | 14 16 6 14 14 5 12 9 13 15 4 | 25 26 22 28 27 21 23 26 24 23 20
X27 | 16 27 12 28 --- 13 16 16 --- --- 8 | 20 35 26 30 --- 21 25 19 --- --- 17
28E | 7 14 7 7 17 4 12 16 8 14 3 | 21 23 20 17 25 18 22 19 16 19 16
29 | 10 28 9 11 14 6 15 10 13 23 4 | 22 34 24 25 26 20 26 19 23 19 19
X30E | 17 --- 13 --- 16 10 19 14 --- --- 7 | 19 --- 20 --- 24 20 22 17 --- --- 16
31 | 6 19 7 8 21 4 13 12 9 12 4 | 20 31 23 22 34 21 30 19 25 20 21
32 | 11 22 9 9 16 4 19 10 9 16 4 | 18 24 14 16 16 15 24 20 15 16 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 11 17 5 14 13 10 19 |T 27 34 28 28 34 27 32 28 28 28 25
WRMS | 8 18 7 11 16 5 14 11 8 18 |NE 28 35 29 28 35 27 33 29 28 28 26
MEDI | 8 18 7 10 16 5 13 11 9 15 |MD 22 29 23 23 30 21 27 22 23 23 20
Table 3.1666.1 GPS week: 1666 Day: 1 MJD: 55907.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 14 6 18 13 6 22 6 9 25 4 | 32 40 37 40 46 36 49 37 35 28 35
2 | 6 13 6 9 13 4 13 10 11 26 4 | 23 23 23 24 24 25 22 26 28 22 22
3 | 8 11 5 10 18 4 9 22 10 10 4 | 12 16 11 18 18 13 13 19 19 12 11
4 | 7 12 5 8 12 6 12 12 12 24 3 | 26 31 34 36 35 33 32 30 37 28 31
5 | 5 21 8 12 15 3 13 9 10 13 3 | 15 25 18 19 24 16 21 20 18 17 14
6 | 4 11 6 13 16 4 8 14 10 11 3 | 16 17 15 22 22 17 17 20 20 15 16
7 | 6 17 5 9 21 3 12 13 10 12 3 | 17 29 19 28 33 18 25 22 19 20 18
8 | 10 15 7 10 17 5 13 7 13 26 4 | 20 23 19 29 26 19 25 21 24 35 19
9 | 8 20 4 10 14 3 14 9 9 17 3 | 13 23 11 18 16 13 20 16 14 16 11
10 | 10 16 8 10 13 5 12 8 8 15 3 | 22 27 27 28 23 24 24 25 26 25 23
11 | 6 16 3 17 13 5 11 8 9 18 3 | 28 34 29 32 40 30 33 30 30 22 28
12E | 5 19 7 9 10 4 16 13 10 14 3 | 37 41 37 40 44 36 36 35 37 34 35
13 | 6 21 5 10 23 4 11 7 6 9 3 | 14 23 17 25 41 16 23 13 15 13 15
14 | 6 19 8 10 16 6 12 8 9 11 3 | 21 26 28 25 35 21 23 19 26 19 23
15 | 8 17 10 9 18 4 22 9 8 11 4 | 20 23 14 25 30 18 29 21 17 20 16
16E | 5 22 8 11 17 3 13 23 12 12 4 | 21 28 20 19 20 21 20 26 24 21 19
17 | 8 19 7 9 16 5 17 10 11 19 4 | 26 30 30 33 27 27 29 26 27 24 26
18 | 6 24 5 12 15 4 11 10 10 15 3 | 14 31 20 21 29 17 25 16 21 17 18
19 | 5 23 8 11 14 4 17 9 10 19 4 | 14 28 16 20 17 13 21 16 15 19 12
20 | 8 17 6 15 14 3 12 10 13 19 4 | 13 25 16 21 22 9 19 10 19 17 12
21 | 5 14 5 9 10 4 11 8 9 18 3 | 24 35 32 31 32 27 33 28 32 24 28
22 | 6 17 5 12 15 4 8 9 8 12 3 | 17 27 21 21 28 19 24 19 21 21 19
23 | 9 24 7 11 21 4 16 9 15 11 4 | 23 31 24 30 36 22 27 23 28 23 23
25E | 9 29 8 10 13 5 16 14 15 22 5 | 11 27 19 19 20 17 18 20 29 19 15
26 | 12 19 8 13 16 4 13 11 9 11 4 | 20 26 20 26 24 19 21 27 27 24 19
X27 | 14 27 13 24 --- 12 15 9 --- --- 7 | 14 26 13 21 --- 14 18 15 --- --- 9
28E | 8 18 6 11 16 4 14 14 7 12 4 | 16 24 14 16 21 14 15 14 16 14 11
29 | 8 25 7 15 14 4 14 8 12 22 4 | 13 31 19 26 23 17 23 18 24 17 16
X30E | 16 --- 15 --- 17 17 20 13 --- --- 8 | 17 --- 24 --- 20 20 19 15 --- --- 16
31 | 8 21 6 11 18 6 12 8 12 12 3 | 18 30 25 23 31 21 25 18 22 19 20
32 | 11 22 6 11 18 3 16 10 11 16 4 | 11 20 13 17 10 10 19 17 14 12 10
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 7 11 16 4 14 11 10 17 |T 18 27 21 25 27 20 24 21 23 20 19
WRMS | 8 19 7 11 15 4 14 9 8 15 |NE 18 26 21 25 27 19 24 21 23 20 18
MEDI | 8 19 6 11 15 4 13 9 10 15 |MD 17 27 20 24 24 19 23 20 24 20 18
Table 3.1666.2 GPS week: 1666 Day: 2 MJD: 55908.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 23 8 20 15 5 25 8 13 20 5 | 52 61 54 51 63 51 69 55 54 44 54
2 | 7 14 8 8 12 5 11 7 11 27 4 | 27 28 31 30 28 29 30 27 32 30 28
3 | 8 16 6 12 15 4 10 16 13 10 4 | 16 19 17 20 21 18 21 22 16 19 17
4 | 7 15 7 7 13 7 8 12 9 24 3 | 33 36 35 40 41 35 37 31 36 28 34
5 | 7 26 7 15 14 4 13 9 11 13 4 | 19 31 19 25 25 18 25 20 25 19 18
6 | 5 15 5 15 13 5 9 12 15 10 3 | 21 24 22 23 27 23 26 26 22 23 22
7 | 7 29 8 13 21 4 14 9 11 14 4 | 17 36 24 27 32 20 26 25 24 21 20
8 | 12 20 9 11 18 7 10 9 9 29 4 | 19 25 22 29 26 18 26 23 26 36 20
9 | 8 18 5 8 13 3 12 9 10 17 3 | 18 22 19 19 19 17 23 20 18 19 18
10 | 9 17 9 13 12 7 10 12 11 16 4 | 20 27 27 30 23 21 26 20 22 25 22
11 | 9 23 10 16 15 4 15 7 9 16 4 | 38 46 45 42 51 41 51 44 41 35 42
12E | 5 20 6 11 11 5 14 10 9 19 3 | 31 32 31 35 35 33 35 31 37 28 30
13 | 7 22 7 13 24 5 10 9 9 10 4 | 19 27 21 26 42 20 28 21 18 20 20
14 | 6 21 8 8 15 4 12 9 14 12 3 | 18 27 25 25 33 21 25 19 22 19 21
15 | 8 22 6 11 14 5 23 9 13 12 4 | 43 46 43 43 46 42 49 44 40 43 42
16E | 7 22 8 15 16 4 16 16 10 17 4 | 18 25 22 22 23 19 22 26 23 25 20
17 | 9 23 6 10 13 5 16 11 8 19 4 | 25 32 30 30 30 27 33 25 26 26 26
18 | 6 27 7 15 15 5 13 13 9 15 4 | 20 35 27 25 33 23 29 20 23 21 23
19 | 6 26 7 13 11 5 14 10 12 18 4 | 19 29 19 17 23 19 23 21 22 22 18
20 | 8 23 8 15 17 3 15 11 11 16 4 | 19 28 24 23 26 17 23 18 17 19 18
21 | 7 15 9 13 10 7 13 11 14 18 4 | 30 39 39 37 37 33 39 34 34 31 34
22 | 6 19 5 11 18 4 8 7 10 10 3 | 18 25 22 23 33 20 25 18 16 19 19
23 | 11 29 10 16 19 6 13 8 6 9 4 | 27 35 31 32 36 28 33 26 24 27 27
25E | 7 32 8 14 25 5 13 12 13 18 5 | 9 26 17 21 23 14 18 14 22 19 13
26 | 12 24 8 14 11 6 14 11 16 12 4 | 18 28 20 27 20 17 26 24 22 22 18
X27 | 19 16 16 28 --- 10 11 11 --- --- 8 | 15 19 23 24 --- 22 21 17 --- --- 15
28E | 11 49 5 13 20 5 13 19 11 17 5 | 24 61 28 30 29 25 29 31 26 31 26
29 | 8 27 7 12 12 6 16 11 11 22 4 | 16 31 23 27 27 19 28 20 24 16 19
X30E | 17 --- 14 --- 18 15 19 13 --- --- 8 | 14 --- 17 --- 21 18 22 16 --- --- 14
31 | 7 22 10 11 19 4 11 13 8 13 4 | 14 28 24 22 32 18 24 18 20 18 19
32 | 10 26 8 14 17 5 18 9 13 16 4 | 16 22 21 19 19 17 25 21 19 17 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 24 7 13 16 5 14 11 11 17 |T 22 31 26 28 30 23 29 25 25 24 23
WRMS | 8 23 7 13 15 5 14 11 9 16 |NE 21 30 26 27 30 23 29 24 25 23 23
MEDI | 8 22 8 13 15 5 13 11 11 16 |MD 19 28 24 26 28 20 26 22 23 22 20
Table 3.1666.3 GPS week: 1666 Day: 3 MJD: 55909.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 16 6 22 15 7 26 11 10 15 5 | 55 66 60 64 67 63 73 64 60 58 59
2 | 8 12 5 12 11 6 11 12 10 23 3 | 35 36 34 36 39 35 33 36 37 32 33
3 | 9 14 4 9 18 3 9 19 14 12 4 | 17 21 15 19 24 15 17 18 19 14 14
4 | 7 11 4 10 12 5 9 14 9 18 3 | 37 41 39 46 47 40 40 40 40 33 38
5 | 7 22 5 10 13 3 11 8 11 11 3 | 18 30 19 18 27 16 22 19 15 18 16
6 | 5 14 4 13 14 4 8 14 12 10 3 | 20 25 20 25 27 21 22 20 19 19 19
7 | 6 17 7 10 21 5 13 7 10 12 3 | 21 29 24 27 36 19 25 21 18 17 19
8 | 10 15 5 12 16 6 10 10 10 23 4 | 16 24 20 24 23 17 22 20 18 32 16
9 | 8 15 6 14 16 4 13 15 10 14 4 | 20 26 23 22 23 18 25 25 17 18 18
10 | 10 14 4 10 14 5 12 14 12 12 3 | 23 27 21 26 26 21 27 21 21 24 20
11 | 7 16 6 15 11 3 13 12 12 13 3 | 43 50 46 50 56 47 49 47 46 41 45
12E | 6 20 6 13 14 5 16 13 7 14 4 | 25 29 23 31 33 25 24 24 26 25 23
13 | 6 18 4 12 25 6 10 11 9 10 3 | 17 25 18 26 42 18 25 18 17 16 17
14 | 8 21 4 10 18 6 12 9 14 11 4 | 21 27 20 27 35 20 25 18 18 20 20
15E | 8 21 7 22 15 7 23 14 10 12 5 | 28 35 28 28 37 26 35 33 22 35 26
16E | 6 17 5 12 23 4 15 9 11 11 4 | 26 28 26 28 25 26 27 25 31 26 24
17 | 9 18 7 13 13 5 18 12 11 16 4 | 23 28 23 30 28 24 27 27 24 20 21
18 | 7 25 6 16 16 5 11 16 9 14 4 | 18 34 21 24 30 18 28 19 17 20 19
19 | 7 25 8 10 10 4 16 9 10 19 4 | 20 31 19 17 23 16 24 19 19 20 16
20 | 10 19 6 14 17 4 14 11 7 13 4 | 18 27 19 21 22 15 22 12 15 20 14
21 | 7 15 6 11 13 4 9 10 6 17 3 | 39 46 42 45 46 40 44 39 36 35 39
22 | 6 19 5 11 18 4 10 11 12 12 3 | 22 33 21 23 33 20 28 19 23 24 21
23 | 10 19 5 13 23 6 14 10 11 10 4 | 23 31 22 25 37 21 29 22 24 22 21
25E | 6 29 8 15 20 6 16 12 9 15 4 | 10 25 14 16 17 11 18 12 10 17 10
26 | 13 20 7 12 12 5 12 12 12 8 4 | 24 33 23 25 28 21 26 25 22 24 21
X27 | 14 25 11 30 --- 16 --- 19 --- --- 9 | 22 25 30 33 --- 18 --- 19 --- --- 19
28E | 9 15 4 13 14 3 12 10 9 9 3 | 26 28 24 30 30 22 25 25 26 24 23
29 | 9 26 8 11 13 3 17 15 12 21 4 | 19 32 23 27 25 18 26 17 18 18 18
X30E | 16 34 9 --- 17 7 --- 15 28 --- 8 | 20 34 19 --- 25 18 --- 15 34 --- 17
31 | 7 20 6 19 20 6 11 11 9 12 4 | 19 31 18 29 34 20 28 17 23 17 19
32 | 10 18 6 11 18 4 17 11 12 12 4 | 16 20 17 18 16 15 23 16 20 15 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 6 13 16 5 14 12 11 14 |T 23 31 24 28 32 23 28 24 24 24 22
WRMS | 8 19 6 14 15 5 14 11 8 15 |NE 24 31 25 29 32 23 29 24 24 24 23
MEDI | 8 18 6 12 15 5 12 12 10 12 |MD 21 29 22 26 28 20 26 20 21 20 19
Table 3.1666.4 GPS week: 1666 Day: 4 MJD: 55910.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 15 4 20 13 4 25 8 9 17 4 | 49 61 55 59 65 55 70 56 52 52 54
2 | 7 12 5 24 13 5 12 13 12 23 4 | 28 29 27 40 29 28 28 31 31 29 28
3 | 9 12 6 13 14 6 8 19 12 17 4 | 17 18 15 21 19 15 17 19 16 17 13
4 | 9 12 6 8 12 6 8 11 8 18 3 | 32 34 37 40 39 35 35 36 33 26 34
5 | 9 19 8 10 18 3 13 10 12 12 4 | 12 25 14 20 24 11 21 14 16 14 10
6 | 4 12 6 15 13 5 10 15 13 13 4 | 17 23 21 25 26 20 24 21 18 21 18
7 | 9 16 6 8 18 4 14 7 7 12 3 | 18 30 22 26 34 21 27 22 20 18 19
8 | 11 17 7 10 17 5 11 9 13 23 4 | 15 27 20 26 24 19 26 22 26 34 19
9 | 8 15 5 13 10 3 15 11 7 14 3 | 17 25 19 19 21 17 26 22 19 18 16
10 | 13 14 5 7 13 5 10 11 11 12 3 | 16 19 15 20 18 11 22 12 17 17 13
11 | 7 16 6 14 15 3 12 9 14 14 4 | 37 45 40 44 50 40 45 42 46 36 40
12E | 8 19 5 14 28 5 18 13 9 19 5 | 19 25 21 23 33 19 22 21 25 23 19
13 | 8 17 7 10 20 3 12 9 8 10 3 | 17 28 21 27 41 20 25 20 19 17 19
14 | 6 16 9 13 15 8 11 12 10 11 3 | 17 24 22 24 32 16 22 17 19 20 19
15E | 8 24 7 11 13 4 18 10 12 10 4 | 29 38 27 32 32 27 36 32 34 29 29
16E | 6 17 7 12 12 4 13 10 10 9 3 | 19 26 18 22 22 20 25 23 25 23 20
17 | 9 22 8 14 13 5 19 11 9 14 4 | 15 29 20 24 25 17 25 21 21 17 17
18 | 7 25 7 10 18 4 12 12 10 15 4 | 13 31 22 22 30 17 29 16 19 19 18
19 | 7 24 6 14 12 5 16 9 12 19 4 | 13 28 15 19 18 15 23 19 19 20 13
20 | 11 19 6 10 19 3 12 8 9 16 4 | 15 26 16 21 26 12 22 9 13 18 13
21 | 5 19 5 8 16 5 10 10 8 19 3 | 33 46 38 40 41 36 38 35 32 29 35
22 | 7 15 4 10 17 4 11 10 11 11 3 | 14 27 16 23 29 14 25 15 16 20 16
23 | 14 24 7 13 20 4 18 7 10 11 4 | 36 49 45 49 46 45 48 47 47 48 43
X25E | 8 --- --- --- --- 479 --- --- --- --- 0 | 6 --- --- --- --- 773 --- --- --- --- 7
26 | 13 17 6 15 11 5 11 10 13 10 4 | 13 23 14 21 19 13 19 19 24 14 13
X27 | 11 25 12 32 --- 29 14 10 --- --- 7 | 15 32 22 21 --- 17 28 19 --- --- 13
28E | 10 17 3 11 17 4 13 11 13 10 3 | 18 28 19 18 21 18 19 19 19 20 16
29 | 10 28 7 10 14 7 16 16 13 23 5 | 15 34 20 26 28 17 24 20 22 17 18
X30E | 18 23 9 13 15 7 --- 16 27 --- 7 | 19 26 15 14 23 21 --- 16 35 --- 17
31 | 8 22 8 17 17 5 11 9 14 14 4 | 11 28 18 24 28 17 25 16 19 18 16
32 | 11 16 9 8 21 4 16 8 11 14 4 | 11 20 13 16 17 9 21 14 12 13 10
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 6 13 16 5 14 11 11 15 |T 19 30 22 26 29 45 28 23 24 23 20
WRMS | 9 18 6 12 17 5 13 11 8 14 |NE 19 29 22 27 29 20 27 22 23 21 20
MEDI | 9 17 6 12 15 5 12 10 11 14 |MD 17 28 20 23 28 18 25 20 20 20 18
Table 3.1666.5 GPS week: 1666 Day: 5 MJD: 55911.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 17 7 16 13 7 26 10 13 29 5 | 37 51 45 39 55 41 59 44 44 35 42
2 | 6 11 4 15 12 7 10 14 7 23 4 | 21 21 20 28 17 18 19 24 21 19 19
3 | 11 15 7 8 14 8 8 12 11 14 3 | 13 21 15 12 16 13 15 15 20 14 13
4 | 7 9 5 9 13 7 8 13 7 19 3 | 29 33 34 38 35 29 31 33 28 21 31
5 | 7 20 7 9 16 4 14 10 14 15 4 | 14 25 17 20 26 16 23 16 22 15 15
6 | 6 15 9 8 11 5 9 10 12 13 3 | 15 22 16 13 20 15 16 15 19 17 15
7 | 6 19 8 8 15 6 11 10 9 17 3 | 15 29 21 23 28 15 23 20 17 16 17
8 | 10 15 6 10 18 7 10 12 10 25 4 | 12 22 16 20 21 12 21 21 19 31 14
9 | 9 19 6 10 14 6 13 14 8 14 4 | 21 26 23 22 22 18 27 24 21 20 21
10 | 13 14 6 8 14 6 10 18 9 16 4 | 20 26 23 25 23 19 26 23 21 29 21
11 | 8 15 7 11 14 5 13 14 12 19 4 | 29 37 32 31 42 32 34 36 39 27 32
12E | 11 23 8 12 40 7 20 14 10 17 5 | 21 31 27 29 45 22 29 28 24 22 24
13 | 5 17 5 9 19 7 13 13 8 11 3 | 15 26 18 23 37 16 23 21 17 17 18
14 | 8 19 6 9 13 4 12 12 10 15 3 | 18 26 22 23 28 17 26 16 23 20 21
15E | 6 23 9 11 13 6 20 11 13 13 4 | 16 25 19 19 22 19 27 20 18 17 16
16E | 7 23 8 11 13 4 15 13 7 11 4 | 18 26 18 23 16 14 20 21 18 18 16
17 | 7 18 7 10 14 5 15 13 10 14 4 | 20 28 22 25 28 17 25 22 18 18 19
18 | 8 24 7 9 19 5 13 11 9 17 4 | 17 32 24 22 32 17 28 18 20 21 21
19 | 4 22 8 10 11 6 18 13 10 20 4 | 13 26 15 14 17 14 21 16 18 18 13
20 | 10 19 8 11 16 4 14 11 7 19 4 | 13 22 14 18 23 8 21 11 11 18 11
21 | 7 15 7 7 12 4 10 12 8 21 3 | 26 33 33 32 34 24 34 30 23 23 29
22 | 8 17 6 9 21 6 13 15 7 15 4 | 17 28 18 22 32 15 26 18 20 22 19
23E | 20 24 9 14 17 6 19 20 9 17 5 | 62 68 65 70 69 60 65 49 63 51 60
X25E | 13 --- --- 13 17 15 --- 15 15 --- 7 | 6 --- --- 14 15 114 --- 15 16 --- 11
26 | 15 18 9 12 12 7 12 14 15 12 4 | 20 28 22 23 20 18 23 24 26 18 19
X27 | 11 21 9 14 --- 11 --- 13 --- --- 6 | 24 23 22 21 --- 20 --- 20 --- --- 18
28E | 10 16 7 7 13 6 12 16 11 12 4 | 17 28 22 23 26 15 22 22 17 20 18
29 | 11 28 10 8 15 4 18 22 15 24 5 | 13 28 19 22 27 15 25 22 22 19 16
X30E | 18 25 11 11 16 7 --- 21 24 --- 7 | 18 27 15 14 21 15 --- 15 28 --- 14
31 | 8 19 8 10 16 4 12 15 8 12 4 | 16 26 22 21 31 14 25 17 17 17 18
32 | 11 16 6 7 15 4 15 12 8 15 4 | 10 16 11 13 14 9 16 16 12 14 10
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 7 10 16 6 14 14 10 17 |T 19 28 23 23 28 22 26 22 22 21 20
WRMS | 9 19 7 10 14 6 14 13 8 18 |NE 18 27 21 22 27 18 25 21 21 20 19
MEDI | 8 18 7 10 14 6 13 13 10 15 |MD 17 26 21 22 26 17 25 21 20 19 18
Table 3.1666.6 GPS week: 1666 Day: 6 MJD: 55912.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 15 6 9 12 5 23 11 10 45 5 | 61 72 69 70 79 69 79 72 68 64 67
2 | 7 13 4 8 11 5 10 16 8 26 3 | 41 41 43 43 43 41 41 44 41 42 41
3 | 10 14 5 11 15 7 11 13 9 13 3 | 17 20 11 19 25 14 19 19 17 16 13
4 | 10 12 3 10 8 7 7 15 11 28 4 | 43 48 49 54 54 48 47 47 49 39 47
5 | 5 23 6 8 14 4 14 14 10 14 4 | 12 28 12 16 25 11 24 15 14 14 11
6 | 6 14 4 12 14 6 9 14 11 14 3 | 17 23 16 23 30 18 23 21 19 19 18
7 | 7 16 7 10 15 4 12 10 8 17 3 | 15 27 22 25 30 18 25 18 18 17 18
8 | 12 14 5 9 15 4 10 12 10 26 4 | 12 25 19 23 26 17 26 21 20 32 17
9 | 7 18 4 8 12 4 13 14 13 15 3 | 17 23 18 19 20 17 23 25 19 16 16
10 | 10 15 4 10 11 6 11 19 11 20 4 | 18 26 21 30 23 22 28 25 22 33 22
11 | 8 18 7 10 12 4 13 12 10 25 4 | 49 56 52 56 63 56 54 58 58 49 53
12E | 9 22 6 13 17 4 20 14 7 16 4 | 30 36 27 34 39 29 36 32 31 28 29
13 | 7 15 5 9 20 3 11 14 7 13 3 | 19 23 19 24 39 18 23 24 16 20 19
14 | 8 20 5 10 22 5 14 12 10 13 4 | 17 24 21 26 39 18 26 21 19 20 20
15E | 8 22 8 14 12 4 21 12 12 14 4 | 34 42 33 36 39 34 41 37 31 36 33
16E | 7 25 6 12 16 6 13 13 9 13 4 | 19 32 24 23 28 19 26 27 20 24 19
17 | 9 20 7 11 14 5 16 14 8 13 4 | 20 31 25 29 30 23 29 26 22 23 22
18 | 7 21 6 12 18 4 14 13 7 20 4 | 17 32 19 24 29 17 30 18 16 22 18
19 | 9 25 9 10 13 6 15 10 10 22 4 | 18 31 20 20 21 18 24 25 22 26 17
20 | 11 16 8 10 16 4 14 13 9 26 4 | 16 23 14 19 22 11 25 13 15 30 12
21 | 7 15 5 8 9 5 9 14 10 23 3 | 42 48 43 47 48 43 46 45 41 38 42
22 | 7 18 5 7 18 5 9 16 8 15 3 | 13 27 17 22 30 13 25 19 15 22 16
23E | 11 21 7 13 17 6 15 21 10 23 5 | 39 42 39 41 43 37 40 44 37 45 38
X25E | 6 31 6 9 11 4 16 13 7 --- 4 | 7 21 4 14 18 90 15 15 14 --- 10
26 | 14 25 10 10 15 6 13 15 10 17 4 | 18 28 18 26 21 18 25 25 23 26 18
X27 | 7 18 5 9 11 5 11 13 10 --- 3 | 14 18 17 19 6 13 16 20 6 --- 13
28E | 8 13 4 9 12 4 11 16 10 12 3 | 17 30 23 25 29 20 29 24 23 22 20
29 | 9 27 7 9 12 7 17 26 9 24 5 | 18 32 20 22 26 19 26 24 23 22 18
X30E | 17 28 10 16 16 8 --- 25 23 --- 7 | 18 30 18 14 26 17 --- 20 30 --- 15
31 | 8 25 7 11 19 6 13 16 7 16 4 | 16 30 21 23 39 20 28 22 20 23 19
32 | 11 18 6 8 15 5 17 19 12 18 4 | 12 18 10 15 16 11 20 20 12 16 8
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 6 10 15 5 14 15 10 21 |T 22 31 24 28 32 26 30 27 25 28 23
WRMS | 9 19 6 10 14 5 14 14 8 18 |NE 22 31 24 28 32 23 30 27 24 27 23
MEDI | 8 18 6 10 14 5 13 14 10 17 |MD 18 30 20 24 29 18 26 24 20 23 18
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 4.1666 GPS week: 1666 MJD: 55906.0-55912.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2956 |U 21 27 42 |U 12 14 41 |U 12 13 21 |
emr | emr 2905 |U 24 26 59 |U 14 15 46 | 16 17 34 |
esa | esa 2948 | 22 28 46 |U 12 15 45 | 12 13 21 |
gfz | gfz 2904 |U 28 27 77 |U 14 15 50 |U 16 18 32 |
grg | grg 2879 | 24 32 62 |U 12 15 45 | 12 13 23 |
igr | igr 2955 | 19 25 41 | 12 14 41 | 12 13 21 |
igs | igs 2959 | 19 26 43 | 12 14 42 | 13 14 22 |
jpl | jpl 2860 |U 21 27 58 |U 12 15 42 | 15 18 35 |
mit | mit 2962 |U 17 21 47 |U 13 16 45 |U 17 18 32 |
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 5.1666.0 GPS week: 1666 Day: 0 MJD: 55906.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 9 8 22 | 9 9 29 | 8 10 16 |
emr | emr 2880 | 15 16 45 | 12 7 35 | 10 10 16 |
esa | esa 2976 | 7 7 19 | 9 9 32 | 8 8 12 |
gfz | gfz 2880 | 21 11 26 | 17 10 58 | 14 18 34 |
grg | grg 2880 | 17 14 49 | 10 11 35 | 8 10 15 |
igr | igr 2975 | 7 7 20 | 10 8 31 | 8 9 12 |
igs | igs 2975 | 8 8 30 | 9 8 31 | 8 10 13 |
jpl | jpl 2969 | 9 9 31 | 9 10 31 | 13 18 29 |
mit | mit 2976 | 8 8 25 | 18 17 37 | 9 8 15 |
Table 5.1666.1 GPS week: 1666 Day: 1 MJD: 55907.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 12 50 26 | 12 16 42 | 6 11 17 |
emr | emr 2879 | 14 20 42 | 14 15 42 | 9 7 22 |
esa | esa 2976 | 13 52 27 | 11 16 46 | 7 9 16 |
gfz | gfz 2880 | 32 22 66 | 19 20 68 | 18 18 29 |
grg | grg 2880 | 22 49 95 | 11 15 46 | 6 11 24 |
igr | igr 2954 | 13 50 25 | 11 16 41 | 6 9 17 |
igs | igs 2965 | 13 50 26 | 12 16 44 | 7 10 18 |
jpl | jpl 2968 | 29 29 85 | 12 19 43 | 12 17 42 |
mit | mit 2976 | 11 14 30 | 12 18 46 | 11 15 28 |
Table 5.1666.2 GPS week: 1666 Day: 2 MJD: 55908.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2967 | 8 6 21 | 12 16 32 | 5 5 12 |
emr | emr 2880 | 24 15 50 | 14 14 37 | 10 8 14 |
esa | esa 2976 | 14 12 30 | 11 17 35 | 8 6 15 |
gfz | gfz 2880 | 13 15 36 | 16 18 43 | 10 12 21 |
grg | grg 2880 | 17 25 39 | 11 19 36 | 9 10 17 |
igr | igr 2952 | 11 8 24 | 11 18 33 | 6 5 11 |
igs | igs 2967 | 14 14 32 | 12 17 33 | 7 6 12 |
jpl | jpl 2966 | 14 14 33 | 11 16 30 | 16 18 37 |
mit | mit 2976 | 18 17 43 | 11 16 34 | 9 10 21 |
Table 5.1666.3 GPS week: 1666 Day: 3 MJD: 55909.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2969 | 44 49 106 | 20 21 69 | 7 7 10 |
emr | emr 2972 | 44 51 104 | 22 22 66 | 17 26 41 |
esa | esa 2976 | 39 43 102 | 19 21 72 | 8 9 11 |
gfz | gfz 2880 | 39 46 100 | 19 20 66 | 6 7 12 |
grg | grg 2880 | 41 45 108 | 19 21 74 | 10 10 18 |
igr | igr 2975 | 23 34 86 | 19 21 67 | 7 7 14 |
igs | igs 2976 | 24 34 88 | 20 21 69 | 8 8 12 |
jpl | jpl 2784 | 28 45 83 | 19 21 68 | 8 10 13 |
mit | mit 2976 | 22 31 84 | 18 23 69 | 8 14 15 |
Table 5.1666.4 GPS week: 1666 Day: 4 MJD: 55910.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2871 | 14 9 27 | 17 17 60 | 44 46 62 |
emr | emr 2876 | 24 20 57 | 18 21 75 | 39 44 70 |
esa | esa 2880 | 19 15 40 | 17 17 73 | 39 35 55 |
gfz | gfz 2875 | 21 18 50 | 17 15 57 | 43 47 80 |
grg | grg 2780 | 20 16 44 | 18 17 65 | 32 29 43 |
igr | igr 2880 | 18 13 39 | 16 16 65 | 40 42 56 |
igs | igs 2880 | 17 13 29 | 17 17 70 | 44 44 64 |
jpl | jpl 2765 | 21 20 48 | 17 16 60 | 40 45 80 |
mit | mit 2880 | 19 15 47 | 17 19 65 | 58 55 80 |
Table 5.1666.5 GPS week: 1666 Day: 5 MJD: 55911.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 17 32 55 | 9 9 30 | 5 4 13 |
emr | emr 2876 | 24 29 70 | 11 13 33 | 8 10 34 |
esa | esa 2880 | 22 33 74 | 8 10 37 | 7 8 18 |
gfz | gfz 2969 | 48 39 226 | 7 9 36 | 11 11 23 |
grg | grg 2879 | 19 38 57 | 9 11 29 | 10 10 17 |
igr | igr 2975 | 17 30 62 | 8 9 29 | 7 7 18 |
igs | igs 2976 | 16 30 64 | 8 9 28 | 7 7 16 |
jpl | jpl 2688 | 22 43 80 | 8 11 32 | 10 10 23 |
mit | mit 2976 | 17 30 64 | 8 11 37 | 10 9 29 |
Table 5.1666.6 GPS week: 1666 Day: 6 MJD: 55912.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 44 32 35 | 7 12 23 | 5 10 16 |
emr | emr 2972 | 26 32 41 | 7 14 31 | 16 15 41 |
esa | esa 2976 | 43 34 33 | 7 12 21 | 8 12 20 |
gfz | gfz 2969 | 25 35 36 | 7 13 23 | 9 13 22 |
grg | grg 2976 | 29 35 39 | 7 11 27 | 9 12 26 |
igr | igr 2976 | 43 30 33 | 6 11 22 | 8 13 22 |
igs | igs 2976 | 44 33 35 | 6 12 23 | 8 11 21 |
jpl | jpl 2880 | 25 33 48 | 8 15 30 | 9 8 22 |
mit | mit 2976 | 26 34 35 | 8 11 26 | 13 15 32 |
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 6.1666 GPS week: 1666 MJD: 55906.500-55912.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 2 -23 3 97 1 | 3 17
| 29 8 80 53 5 | 1
emr uuxxu | 10 10 -16 347 10 | 13 22
| 30 35 240 112 8 | 2
esa uuuuu | 9 -20 94 43 1 | -5 18
| 10 23 40 82 8 | 2
gfz uuuuu | -14 28 2 121 3 | 6 16
| 14 24 91 55 3 | 1
grg uuuux | 19 -13 51 70 20 | -3 20
| 27 16 60 86 25 | 3
igr xxxxx | -43 1 21 74 0 | -1 14
| 15 22 61 89 7 | 2
irf xxxxx | -10 0 -4 15 -1 | -1 16
| 11 9 18 29 6 | 2
jpl uuuuu | 22 -34 -22 48 7 | 15 20
| 12 24 45 66 7 | 2
mit uuuuu | -45 17 -176 -205 -4 | 7 17
| 22 19 39 69 3 | 2
ngs uuuuu | 18 44 -23 -25 -7 | 2 12
| 39 50 86 63 8 | 2
sio uuuuu | -22 -40 16 -75 2 | 14 23
| 32 20 56 124 16 | 4
Table 7.1666.0 GPS week: 1666 Day: 0 MJD: 55906.500
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 -30 34 84 -1 | 3 15
emr uuxxu | 15 8 -46 267 21 | 12 19
esa uuuuu | -6 -26 125 57 -6 | -3 16
gfz uuuuu | -27 7 67 68 -3 | 5 15
grg uuuux | 21 -9 45 -55 -11 | 0 22
igr xxxxx | -57 -37 70 -60 -6 | 2 12
irf xxxxx | 7 -6 10 -25 -9 | 1 14
jpl uuuuu | 19 -68 -13 7 16 | 11 15
mit uuuuu | -3 -7 -197 -132 -4 | 8 16
ngs uuuuu | -10 110 -92 65 -5 | 2 11
sio uuuuu | 40 -50 2 -198 -24 | 20 26
Table 7.1666.1 GPS week: 1666 Day: 1 MJD: 55907.500
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 | 35 -16 -109 75 -6 | 5 16
emr uuxxu | 54 20 -156 399 14 | 13 22
esa uuuuu | 6 -45 34 57 -10 | -2 16
gfz uuuuu | -36 29 61 95 4 | 7 16
grg uuuux | 30 -21 69 76 13 | -1 21
igr xxxxx | -47 27 -60 62 -10 | 2 11
irf xxxxx | -14 -7 2 46 -7 | 1 14
jpl uuuuu | 32 -39 45 -27 -6 | 14 20
mit uuuuu | -53 17 -133 -129 -4 | 10 17
ngs uuuuu | 30 99 -67 -3 6 | 4 11
sio uuuuu | -29 -59 72 -121 -14 | 18 25
Table 7.1666.2 GPS week: 1666 Day: 2 MJD: 55908.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 24 -33 83 23 -5 | 4 16
emr uuxxu | -6 83 -464 560 12 | 13 22
esa uuuuu | 4 -41 139 204 -4 | -5 18
gfz uuuuu | -20 14 108 151 0 | 6 15
grg uuuux | 35 -37 75 176 6 | -6 17
igr xxxxx | -60 -12 -43 85 -3 | -2 13
irf xxxxx | -17 -11 21 24 -4 | -1 15
jpl uuuuu | 24 -12 -65 -27 10 | 14 20
mit uuuuu | -68 9 -185 -297 -2 | 9 17
ngs uuuuu | 75 67 -137 -97 -3 | 4 11
sio uuuuu | -37 -20 73 -222 -4 | 14 23
Table 7.1666.3 GPS week: 1666 Day: 3 MJD: 55909.500
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 | 20 -11 45 176 6 | 2 18
emr uuxxu | 38 -10 30 321 11 | 12 21
esa uuuuu | 11 -2 64 12 7 | -7 19
gfz uuuuu | -13 49 44 128 8 | 5 16
grg uuuux | 50 -22 56 135 2 | -6 17
igr xxxxx | -52 12 1 134 6 | -3 14
irf xxxxx | 0 14 -11 30 4 | -3 17
jpl uuuuu | 17 -53 -80 77 9 | 13 19
mit uuuuu | -30 38 -192 -216 0 | 6 17
ngs uuuuu | -38 0 41 35 -18 | 3 12
sio uuuuu | -6 -21 -9 -128 12 | 11 22
Table 7.1666.4 GPS week: 1666 Day: 4 MJD: 55910.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -6 -18 -111 151 3 | 3 18
emr uuxxu | 13 -22 85 226 13 | 13 22
esa uuuuu | 25 18 78 -68 13 | -6 20
gfz uuuuu | 2 -5 -58 207 3 | 6 17
grg uuuux | 34 -12 -46 138 37 | -6 17
igr xxxxx | -18 -10 8 159 8 | -2 15
irf xxxxx | -3 2 -14 48 4 | -2 17
jpl uuuuu | 3 -41 -34 53 9 | 15 21
mit uuuuu | -50 9 -111 -147 -3 | 7 18
ngs uuuuu | -3 42 21 -17 -15 | 3 12
sio uuuuu | -32 -58 72 36 15 | 11 22
Table 7.1666.5 GPS week: 1666 Day: 5 MJD: 55911.500
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 | 3 -24 66 107 3 | 4 18
emr uuxxu | -13 -15 207 282 0 | 16 24
esa uuuuu | 2 -32 133 14 7 | -4 20
gfz uuuuu | -4 51 -66 147 4 | 8 18
grg uuuux | -10 -9 146 -16 61 | -2 21
igr xxxxx | -31 18 72 166 7 | -1 15
irf xxxxx | -19 10 -1 -10 3 | -1 17
jpl uuuuu | 15 0 -29 130 11 | 18 23
mit uuuuu | -59 47 -191 -269 -4 | 8 18
ngs uuuuu | 54 -17 -37 -66 -10 | 3 12
sio uuuuu | -30 -16 -35 4 18 | 12 24
Table 7.1666.6 GPS week: 1666 Day: 6 MJD: 55912.500
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 | -51 -28 10 60 5 | 2 18
emr uuxxu | -33 4 233 376 0 | 15 24
esa uuuuu | 17 -16 84 27 2 | -5 20
gfz uuuuu | -1 53 -142 47 2 | 6 17
grg uuuux | -27 15 9 35 33 | 1 24
igr xxxxx | -36 5 99 -26 -1 | -2 15
irf xxxxx | -24 0 -34 -6 -1 | -4 18
jpl uuuuu | 41 -24 23 123 1 | 18 23
mit uuuuu | -56 5 -224 -245 -9 | 5 18
ngs uuuuu | 19 3 112 -95 -2 | -1 14
sio uuuuu | -59 -58 -60 105 12 | 11 23
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