[IGSREPORT-20377] Wk 1663 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Dec 8 06:12:14 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1663 (Nov 20, 2011 - Nov 26, 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:
igs1663[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1663[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1663[0-6].cls IGS GPS clock combination summary report.
igs16637.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16637.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 | COD | XMIS
0 | EMR | MATE
0 | ESA | NICO KOUR NNOR
0 | GFZ | 5 10 18 20 22 30 32
0 | GRG | KOUR
0 | JPL | 32 AREQ
0 | MIT | 30 32 10 30 32
1 | COD | USNO WHIT USNO WHIT
1 | EMR | 32 32
1 | ESA | REUN KOUR NANO REUN TIXI
1 | GFZ | 5 10 18 20 22 32 MDVJ STJO
1 | GRG | KOUR
1 | JPL | 32
1 | MIT | 8 10 13 27 29 30 32 8 10 13 27 29 30 32 DAV1 GUAT
2 | COD | USNO USNO
2 | EMR | 10 30 32 10 32
2 | ESA | KOUR THTI UNSA
2 | GFZ | 5 10 18 20 22 30 32 CAS1 MDVJ
2 | GRG | KOUR
2 | JPL | 10 30 32
2 | MIT | 10 21 27 30 32 10 21 27 30 32 CAS1 DAV1 CAS1 DAV1
2 | MIT | TLSE
3 | COD | WUHN
3 | EMR | 30 32 10 30 32
3 | GFZ | 2 5 10 18 22 30 32
3 | JPL | 2 10 32
3 | MIT | 2 5 10 12 22 23 27 29 30 32 2 5 10 12 22 23 27 29
3 | MIT | 30 32 NICO NICO PRDS
4 | COD | WROC STHL WROC
4 | EMR | 30 10 30 WUHN
4 | ESA | WUHN
4 | GFZ | 5 10 22 30 32 GUAT MDVJ WILL
4 | GRG | AMC2
4 | JPL | 32 AREQ BOGT
4 | MIT | 27 30 32 7 10 27 30 32 DAV1 ALRT DAV1 WUHN
5 | COD | STHL
5 | EMR | 30 32 30 32
5 | ESA | KOUR MATE KOUR MATE
5 | GFZ | 10 28 30 32 KERG MATE
5 | GRG | KOUR
5 | JPL | 30 32 KOUR
5 | MIT | 10 27 30 32 10 27 29 30 32 NICO ALRT KOUR NICO
6 | COD | WROC WROC
6 | EMR | 30 30 PRDS
6 | ESA | KOUR UNSA
6 | GFZ | 10 30 CRO1 IRKT MDVJ PRDS
6 | GRG | AMC2 KOUR
6 | JPL | 30 AREQ KOUR
6 | MIT | 10 27 30 32 10 27 30 32 TWTF
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
----+------------+----------
G31 | 2011_11_23 | 2011094
6. 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 G32 | | | | | | | 1 |
7. 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.
8. 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 | .1 -.2 -.3 -57 -11 38 .08
EMR | 6.6 3.3 9.2 -1 21 13 .38
ESA | 6.3 1.3 -13.7 84 -236 116 .17
GFZ | -.7 .8 -.6 -50 -8 6 .17
GRG | 4.9 .6 -4.1 -20 11 15 .20
JPL | 1.6 6.4 5.8 -2 -25 -9 .50
MIT | 7.1 3.6 -1.9 -33 7 -36 .21
NGS | 9.6 3.7 -3.9 29 -66 49 .50
SIO | 5.0 3.7 -.5 52 -126 31 .34
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by 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.
11. 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 1.1663.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1663.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 2.1663.[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 3.1663.[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 5.1663.0-6).
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 1663 summary. (Nov 20, 2011 - Nov 26, 2011)
Table 1.1663.a GPS week: 1663 MJD: 55885.000-55891.000
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 258| 0 0 4 106 -72 -3 -.25 9 8 | -140 -301 21 104
| 0 0 1 6 22 16 .02 | 295 186
emr 95| -1 0 9 -29 -130 -9 .36 19 19 | 674 412 20 121
| 1 2 2 39 40 17 .04 | 639 682
esa 137| 0 1 -1 -94 173 41 .19 7 7 | -422 955 16 174
| 0 0 1 19 20 11 .03 | 950 1978
gfz 202| -1 0 -3 85 -82 -17 -.27 11 11 | 65 88 24 106
| 0 1 1 84 75 12 .03 | 300 468
grg 128| 1 1 -4 28 -128 -14 .59 16 15 | 67 57 48 264
| 1 1 2 15 21 7 .06 | 356 426
igr n/a| 0 0 0 -15 -85 -25 -.09 5 5 | -1271 444 19 83
| 0 0 0 20 18 11 .02 | 1023 732
jpl 147| -1 -1 1 -9 -41 -7 .51 14 14 | 1019 352 20 100
| 0 0 1 10 26 42 .03 | 650 633
mit 261| 0 -1 -3 49 -98 -38 -.39 13 12 | -286 7 26 213
| 1 0 1 28 46 12 .04 | 265 520
ngs 219| 1 0 -3 -62 39 -20 -.18 11 9 | -77 -324 1812 3428
| 0 1 1 50 56 12 .05 | 302 196
sio 254| 0 0 1 -125 157 -6 -.24 18 17 | --- --- --- ---
| 1 0 1 36 54 9 .01 | --- ---
Table 1.1663.b GPS week : 1663 MJD: 55885.000-55891.000
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 | 4 4 4 4 4 4 4 |
2 | 4 4 4 5 4 4 5 |
3 | 4 4 4 4 4 4 5 |
4 | 5 4 4 4 3 4 4 |
5 | 4 4 5 5 4 4 4 |
6 | 3 3 3 4 4 4 4 |
7 | 4 5 4 4 5 5 5 |
8 | 5 4 4 4 5 4 4 |
9 | 4 4 4 4 4 4 4 |
10 | 5 4 5 5 5 5 6 |
11 | 4 4 4 4 4 5 4 |
12 | 5 5 5 5 6 5 5 |
13 | 4 4 4 5 6 5 5 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 5 4 5 5 |
16 | 4 4 4 5 5 5 4 |
17 | 4 4 4 5 5 5 5 |
18 | 4 5 4 4 4 4 4 |
19 | 4 4 4 5 5 4 4 |
20 | 4 4 4 4 3 4 6 |
21 | 4 4 4 4 4 5 5 |
22 | 4 3 3 4 4 4 4 |
23 | 5 5 5 5 5 6 5 |
25 | 4 5 5 4 4 5 4 |
26 | 4 4 4 4 4 4 4 |
27 | 9 8 7 8 6 8 10 |
28 | 4 4 4 4 4 5 5 |
29 | 5 5 5 5 5 4 5 |
30 | 6 6 5 6 6 6 6 |
31 | 4 4 5 0 5 4 5 |
32 | 7 6 6 8 7 6 6 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1663.0 GPS week: 1663 Day: 0 MJD: 55885.000
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 258| 0 0 3 105 -68 -16 -.23 8 7 | -41 -196 23 101
| 39 18 |
emr 95| -2 3 12 -58 -133 12 .35 19 19 | -191 623 23 156
| 42 -18 |
esa 137| 0 1 0 -87 185 22 .16 6 6 | 239 -904 16 165
| 44 0 |
gfz 202| -1 -1 -3 64 -145 -5 -.24 10 11 | -37 438 25 96
| -15 29 |
grg 128| 3 2 -6 34 -165 -15 .63 15 13 | -55 371 39 284
| 20 -9 |
igr n/a| 0 0 0 -41 -67 -30 -.10 4 4 | -2410 626 19 91
| 8 26 |
jpl 147| -1 -1 0 -14 -51 32 .57 15 14 | 61 818 21 93
| 23 12 |
mit 261| 0 -1 -4 75 -113 -42 -.45 15 13 | -297 214 30 208
| -37 -5 |
ngs 219| 1 0 -5 -80 75 -24 -.27 11 10 | -16 -182 1779 2940
| 62 -86 |
sio 254| -1 0 0 -112 178 -1 -.25 20 19 | --- --- --- ---
| 85 -45 |
Table 2.1663.1 GPS week: 1663 Day: 1 MJD: 55886.000
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 258| 0 0 3 110 -55 -7 -.22 9 8 | 53 -490 22 105
| 13 -11 |
emr 95| -4 -3 11 14 -110 5 .30 19 19 | 231 886 23 133
| -19 -33 |
esa 137| 1 2 0 -86 196 41 .20 6 6 | -2120 3171 19 173
| 55 11 |
gfz 202| -1 0 -2 37 -154 -25 -.27 9 9 | 180 156 24 110
| -17 6 |
grg 128| 2 3 -2 40 -124 -8 .61 15 14 | 15 565 48 244
| 3 -23 |
igr n/a| 0 0 0 17 -74 -24 -.09 5 5 | -1810 547 19 78
| -17 24 |
jpl 147| -2 0 2 5 -23 -20 .50 14 13 | 744 687 22 107
| 34 -58 |
mit 261| 0 -1 -4 17 -127 -26 -.44 14 12 | -527 973 25 217
| 1 6 |
ngs 219| 1 0 -4 -8 65 -30 -.22 11 8 | 160 -617 1738 3787
| -139 -74 |
sio 254| 0 -1 0 -164 129 -1 -.25 19 16 | --- --- --- ---
| 111 -34 |
Table 2.1663.2 GPS week: 1663 Day: 2 MJD: 55887.000
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 258| 0 0 6 101 -56 7 -.22 9 7 | -582 -164 20 94
| 35 -2 |
emr 95| -1 0 8 0 -101 -29 .34 18 18 | 251 -242 22 130
| -18 -48 |
esa 137| 1 1 -1 -106 174 34 .19 8 7 | -478 -199 19 174
| 45 3 |
gfz 202| 0 0 -3 23 -87 -5 -.22 10 10 | -287 462 23 92
| 9 13 |
grg 128| 1 1 -7 37 -129 -7 .65 14 13 | -25 -453 55 255
| 4 -7 |
igr n/a| 0 0 0 -21 -79 -32 -.07 5 5 | -2089 -536 19 89
| 9 20 |
jpl 147| -1 -1 1 -22 -19 -16 .52 14 13 | 721 -538 21 98
| 57 -91 |
mit 261| 0 -1 -2 78 -98 -33 -.40 13 11 | -523 -303 26 215
| -28 10 |
ngs 219| 0 2 -2 -37 60 -21 -.21 9 8 | -618 -138 1898 3430
| 16 -123 |
sio 254| -1 0 2 -100 145 0 -.21 17 15 | --- --- --- ---
| 66 -47 |
Table 2.1663.3 GPS week: 1663 Day: 3 MJD: 55888.000
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 258| 0 0 5 117 -61 -20 -.26 8 8 | 96 -591 19 119
| -1 -31 |
emr 95| 0 1 5 15 -77 2 .31 20 20 | 452 980 14 102
| -30 -83 |
esa 137| 0 0 -1 -73 197 37 .22 8 8 | 988 1316 16 182
| 33 36 |
gfz 202| 0 -1 -3 13 -87 -28 -.28 13 13 | -179 432 24 119
| 12 16 |
grg 128| 3 0 -7 40 -101 -19 .62 14 14 | 93 -49 49 294
| 3 -50 |
igr n/a| 0 -1 -1 -9 -77 -16 -.07 5 5 | -1964 1512 20 112
| 6 26 |
jpl 147| -1 0 3 -13 -20 66 .49 14 13 | 615 911 19 101
| 24 -93 |
mit 261| 0 0 -3 19 -136 -28 -.42 12 11 | 21 -405 25 218
| -9 9 |
ngs 219| 2 -1 -5 -17 69 -25 -.15 11 10 | 203 -568 2170 4128
| -86 -81 |
sio 254| -2 0 2 -174 90 -3 -.25 17 17 | --- --- --- ---
| 89 -38 |
Table 2.1663.4 GPS week: 1663 Day: 4 MJD: 55889.000
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 258| 0 0 5 110 -56 22 -.27 9 8 | -528 -119 18 97
| 28 -34 |
emr 95| 0 2 9 -38 -123 -30 .41 17 17 | 1373 25 14 95
| 36 -19 |
esa 137| 0 1 -2 -84 154 53 .16 7 7 | -549 3068 14 162
| 63 18 |
gfz 202| -2 1 -3 61 -143 -35 -.31 13 12 | 51 -262 23 103
| -31 42 |
grg 128| 0 -1 -1 28 -113 -22 .54 17 16 | -526 483 54 245
| 59 -46 |
igr n/a| 0 0 0 -13 -76 -44 -.08 6 5 | -537 373 17 62
| -13 49 |
jpl 147| -2 -2 2 2 -22 -15 .46 14 14 | 1533 246 17 95
| 54 -55 |
mit 261| 2 -1 -3 54 -137 -63 -.34 13 12 | -260 -104 24 202
| -30 -8 |
ngs 219| 2 0 -4 -46 81 -33 -.16 11 8 | -372 -263 1456 3205
| -34 -61 |
sio 254| 0 0 1 -94 119 -17 -.24 18 18 | --- --- --- ---
| 38 -68 |
Table 2.1663.5 GPS week: 1663 Day: 5 MJD: 55890.000
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 258| 0 0 4 105 -101 -16 -.26 10 9 | 131 -388 24 107
| 32 5 |
emr 95| -1 0 9 -65 -167 -23 .41 19 19 | 1353 -589 22 132
| 67 17 |
esa 137| 1 1 -2 -94 166 55 .22 8 8 | -333 -1856 15 181
| 45 27 |
gfz 202| -2 -1 0 145 23 -4 -.26 10 10 | 87 200 25 109
| -40 4 |
grg 128| 1 0 -4 19 -120 -23 .54 17 16 | 618 -462 47 278
| 62 1 |
igr n/a| 1 0 1 -3 -115 -9 -.10 6 6 | -37 -422 21 79
| -31 61 |
jpl 147| 0 0 0 -8 -65 -53 .52 15 14 | 1834 -498 20 98
| 81 -28 |
mit 261| 1 -1 -1 23 -67 -35 -.35 13 12 | 109 -560 23 224
| -25 -41 |
ngs 219| 1 1 -2 -92 -7 -1 -.14 10 8 | 71 -159 1760 3010
| -19 6 |
sio 254| 0 0 3 -145 179 2 -.24 19 18 | --- --- --- ---
| 47 -94 |
Table 2.1663.6 GPS week: 1663 Day: 6 MJD: 55891.000
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 258| 0 0 4 98 -107 9 -.25 11 9 | -115 -163 23 110
| 21 31 |
emr 95| 0 0 11 -75 -195 -5 .37 19 19 | 1252 1201 22 104
| 52 39 |
esa 137| 0 0 0 -132 142 43 .22 8 7 | -706 2091 18 183
| 41 59 |
gfz 202| -1 0 -4 250 16 -20 -.31 9 9 | 644 -804 24 115
| -49 31 |
grg 128| 1 0 -1 -2 -144 -5 .51 16 16 | 352 -52 48 252
| 80 26 |
igr n/a| 1 0 0 -37 -110 -21 -.12 7 6 | -52 1009 21 73
| 0 51 |
jpl 147| -2 -1 1 -14 -85 -45 .50 15 14 | 1626 844 26 109
| 18 56 |
mit 261| 1 0 -1 78 -9 -36 -.36 14 13 | -527 237 31 209
| -25 -53 |
ngs 219| 0 1 -1 -154 -70 -3 -.11 12 9 | 27 -341 1886 3496
| -12 81 |
sio 254| 1 0 2 -83 258 -22 -.24 19 17 | --- --- --- ---
| 20 -119 |
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 3.1663.0 GPS week: 1663 Day: 0 MJD: 55885.000
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 | 9 13 6 7 --- 4 14 15 14 15 4 | 33 42 42 37 --- 36 52 39 31 37 38
2 | 6 19 7 12 10 5 16 15 7 27 4 | 23 37 25 29 32 25 37 25 21 23 26
3 | 9 13 4 8 13 4 9 14 13 17 3 | 29 32 32 31 39 32 37 30 37 34 33
4 | 7 12 5 20 10 5 12 16 11 36 5 | 23 25 27 33 28 25 31 27 24 35 26
5E | 7 19 6 10 13 4 22 15 9 14 4 | 23 35 26 25 31 23 31 25 22 28 24
6 | 7 13 5 7 11 3 7 12 13 14 3 | 35 34 36 35 41 36 39 35 41 39 37
7 | 7 20 6 13 18 3 19 10 10 14 4 | 19 27 20 19 24 19 26 22 18 20 18
8 | 9 23 4 11 16 4 16 19 9 17 4 | 15 23 16 20 14 15 24 22 17 21 14
9 | 6 20 5 8 9 3 12 13 14 17 3 | 12 24 14 17 16 15 22 16 17 19 15
10E | 13 21 5 12 19 5 20 16 9 16 4 | 56 61 58 59 67 57 65 54 55 59 57
11 | 8 16 7 8 14 5 15 12 14 27 4 | 23 34 28 28 38 26 35 30 24 29 27
12 | 7 23 8 7 15 4 23 14 10 16 4 | 46 49 47 51 57 48 52 50 48 49 47
13 | 6 19 7 8 21 4 16 13 12 16 4 | 12 26 16 17 32 14 23 13 14 16 15
14 | 4 20 5 8 12 4 11 14 8 13 3 | 17 26 20 20 32 17 26 22 18 26 19
15 | 6 25 7 8 18 6 16 12 12 14 4 | 12 27 17 14 30 15 24 13 14 14 15
16 | 4 26 7 11 18 4 12 13 9 23 4 | 16 29 20 18 32 18 25 20 22 30 20
17 | 7 13 7 12 10 3 17 12 11 30 4 | 27 30 34 34 30 31 34 34 32 33 31
18E | 7 18 8 11 17 4 13 15 10 13 4 | 22 30 23 19 27 20 28 27 19 25 22
19 | 7 16 4 10 9 4 13 14 13 25 4 | 17 21 20 25 23 21 22 25 25 26 20
20E | 6 14 8 9 11 4 11 16 12 19 4 | 33 37 35 33 35 33 37 36 31 42 34
21 | 7 20 5 11 12 3 11 13 10 24 4 | 18 32 20 17 23 19 27 21 21 22 20
22E | 6 15 6 9 15 6 13 18 7 15 3 | 22 28 24 23 29 21 28 25 25 25 23
23 | 7 22 6 12 18 4 17 17 11 16 4 | 11 28 15 14 23 12 23 18 15 19 13
25 | 6 17 7 9 15 4 19 13 12 12 4 | 22 32 32 30 42 29 43 32 31 33 29
26 | 10 14 5 9 7 4 10 10 11 18 3 | 19 25 19 19 25 16 26 17 14 20 18
X27 | 18 24 17 20 --- 14 20 22 --- --- 8 | 13 24 22 28 --- 19 23 20 --- --- 15
28 | 6 17 5 9 19 3 10 11 8 15 3 | 15 25 19 23 34 18 24 20 19 22 19
29 | 4 18 7 6 16 6 19 27 13 24 5 | 22 26 24 26 27 25 27 28 24 26 23
30E | 17 27 7 13 16 10 16 17 16 31 5 | 50 55 44 36 50 40 55 41 46 43 44
31 | 5 16 5 9 16 4 14 15 9 15 3 | 11 22 13 9 9 10 21 17 12 14 12
X32E | 15 --- 9 11 --- 6 16 23 15 --- 6 | 71 --- 66 69 --- 68 64 76 72 --- 67
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 6 10 15 4 15 15 11 20 |T 24 31 27 27 31 25 33 28 26 28 26
WRMS | 7 19 6 11 13 4 14 13 10 19 |NE 18 27 21 22 26 20 27 22 22 24 21
MEDI | 7 18 6 9 15 4 15 14 11 16 |MD 22 28 24 25 30 21 28 25 22 26 23
Table 3.1663.1 GPS week: 1663 Day: 1 MJD: 55886.000
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 | 9 14 6 7 --- 4 15 15 13 16 4 | 28 40 33 27 --- 27 45 29 26 32 31
2 | 8 22 5 11 10 5 14 14 9 25 4 | 18 32 24 21 27 18 29 21 18 17 21
3 | 11 13 4 7 11 4 10 10 11 17 3 | 26 30 28 26 31 27 28 28 23 26 26
4 | 7 11 8 7 11 5 8 14 7 32 4 | 18 17 15 17 16 15 16 21 17 30 14
5E | 8 17 5 11 10 4 19 20 10 15 4 | 20 26 22 21 28 18 25 23 20 23 19
6 | 6 16 4 6 9 3 7 10 10 14 3 | 29 37 32 30 35 32 32 35 28 32 31
7 | 8 21 8 14 19 4 16 10 12 13 4 | 17 29 19 17 22 15 23 18 15 16 16
8 | 12 18 5 11 16 5 13 14 10 16 4 | 16 18 15 16 12 12 19 24 13 22 13
9 | 9 17 6 8 11 4 12 9 13 17 3 | 13 25 15 16 15 13 25 15 20 18 14
10E | 14 17 7 7 17 6 20 12 7 14 4 | 50 54 54 51 55 49 54 48 44 51 49
11 | 8 19 5 11 14 4 13 10 14 26 4 | 20 30 22 22 32 19 29 22 18 21 21
12 | 8 23 6 7 17 4 21 11 16 15 4 | 36 42 39 38 49 38 41 35 48 36 38
13 | 7 17 8 7 20 3 15 15 12 14 4 | 12 25 17 16 31 12 23 12 15 14 14
14 | 6 19 5 6 14 4 14 8 6 15 3 | 22 28 23 19 26 21 25 22 21 22 22
15 | 7 21 9 8 16 4 14 12 10 16 4 | 11 24 17 15 29 12 23 12 16 14 14
16 | 5 31 7 5 18 5 12 9 11 17 4 | 16 33 20 18 30 18 22 19 17 23 18
17 | 7 14 5 11 11 4 15 9 10 27 4 | 18 19 19 20 20 16 22 21 22 23 17
18E | 8 21 7 9 26 4 11 18 10 14 4 | 27 32 26 22 29 22 28 24 22 24 24
19 | 8 18 4 10 8 6 13 15 9 22 4 | 17 21 20 14 21 18 19 21 16 23 17
20E | 6 14 6 8 17 5 12 13 11 20 3 | 35 34 35 32 40 31 37 34 34 36 34
21 | 7 21 7 7 10 5 13 14 8 27 4 | 17 25 16 15 17 14 22 15 16 17 14
22E | 7 16 6 6 14 3 9 10 10 11 3 | 21 22 19 19 21 17 22 19 19 22 18
23 | 10 20 7 11 18 4 15 15 10 14 4 | 14 27 18 12 23 12 22 15 11 16 13
25 | 10 26 6 8 20 4 18 16 11 14 4 | 20 33 27 24 34 23 33 30 29 26 25
26 | 13 13 6 9 9 6 9 10 8 14 3 | 27 29 24 27 29 22 32 24 24 29 24
X27 | 12 20 16 25 --- 15 16 16 --- --- 8 | 14 21 27 21 --- 15 23 20 --- --- 14
28 | 6 20 3 8 19 3 10 9 11 12 3 | 13 23 16 17 32 12 20 15 15 17 14
29 | 5 17 7 7 10 5 17 27 14 23 5 | 20 23 18 18 17 17 24 24 19 21 16
X30E | 13 18 7 11 19 6 --- 21 11 --- 5 | 30 40 35 36 40 33 --- 30 37 --- 33
31 | 9 23 5 10 16 5 17 11 12 13 4 | 14 25 17 11 12 12 24 16 17 13 16
32E | 16 25 6 8 16 11 15 25 17 19 5 | 65 70 59 64 11 57 56 74 57 73 61
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 6 9 15 5 14 14 11 19 |T 22 30 24 23 27 21 28 24 23 25 22
WRMS | 8 19 6 9 14 5 13 11 8 16 |NE 18 25 20 18 22 17 24 20 18 21 18
MEDI | 8 18 6 8 16 4 14 13 10 16 |MD 20 28 22 20 28 18 24 22 19 23 18
Table 3.1663.2 GPS week: 1663 Day: 2 MJD: 55887.000
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 | 9 12 6 9 --- 5 15 14 6 9 3 | 30 45 41 30 --- 36 50 38 31 33 36
2 | 6 16 5 10 11 4 12 14 9 23 4 | 19 30 22 19 26 19 29 24 24 21 19
3 | 8 11 5 11 12 7 9 9 11 17 3 | 20 25 21 23 28 19 25 21 19 23 18
4 | 5 12 3 8 10 6 9 13 7 25 3 | 21 23 22 22 27 22 24 27 25 30 21
5E | 7 19 6 14 12 4 18 17 9 15 4 | 21 28 22 21 26 19 28 26 23 26 20
6 | 5 12 7 11 10 5 7 7 11 15 3 | 19 28 22 26 29 22 27 24 23 25 21
7 | 5 17 9 10 16 3 14 9 6 11 3 | 16 26 22 20 23 19 23 22 22 17 18
8 | 10 18 7 8 15 5 15 11 11 14 4 | 17 24 17 22 18 18 26 24 21 21 16
9 | 8 16 7 8 8 4 12 10 9 16 3 | 13 24 14 18 21 15 25 18 21 21 15
10E | 16 15 8 13 15 5 19 12 8 13 4 | 31 37 33 30 35 31 41 32 31 33 31
11 | 8 17 6 8 12 5 13 11 12 17 3 | 19 31 25 24 32 22 31 25 22 22 22
12 | 8 26 9 9 18 4 21 11 9 12 4 | 32 40 39 38 49 37 40 32 36 33 36
13 | 6 18 6 8 22 5 13 13 7 12 4 | 14 26 14 14 34 13 25 15 12 14 12
14 | 6 25 10 6 15 4 16 12 10 16 4 | 15 28 19 15 25 16 24 17 19 18 16
15 | 7 22 10 9 16 4 17 11 8 16 4 | 17 31 19 22 34 18 29 19 19 16 17
16 | 6 22 10 9 16 6 12 11 11 18 4 | 17 31 21 22 32 19 25 23 21 24 19
17 | 6 13 7 13 10 3 16 9 8 25 4 | 23 25 28 25 25 24 27 27 27 27 24
18E | 9 19 7 8 15 3 11 10 10 9 3 | 21 29 21 19 24 19 24 25 22 22 20
19 | 7 15 5 10 7 4 12 17 11 25 4 | 13 22 18 18 21 16 21 24 17 23 15
20E | 6 13 7 9 16 5 11 10 9 14 3 | 33 37 35 33 37 32 36 34 32 38 33
21 | 6 18 8 8 9 3 15 7 9 24 4 | 17 24 16 13 15 14 25 17 18 18 15
22E | 8 15 7 8 14 4 11 8 6 10 3 | 28 29 22 23 23 22 27 25 30 24 24
23 | 8 22 8 14 16 4 14 14 8 13 4 | 14 29 16 12 26 12 26 16 10 15 11
25 | 16 18 10 12 17 5 18 11 13 16 5 | 36 48 45 46 48 43 53 45 38 42 42
26 | 12 13 7 9 8 5 9 8 8 14 3 | 16 21 15 17 20 14 21 15 16 17 15
X27 | 13 19 17 16 --- 9 15 17 --- --- 7 | 18 22 17 25 --- 20 25 21 --- --- 14
28 | 7 14 7 7 17 3 11 10 6 14 3 | 16 24 18 18 31 17 22 21 18 21 16
29 | 5 18 8 10 13 6 16 18 12 23 4 | 16 20 17 20 19 16 22 19 20 18 16
30E | 13 20 8 16 16 7 16 19 10 18 5 | 26 41 28 32 38 29 35 26 31 30 28
X31 | 4 20 7 10 --- 5 18 10 8 --- 4 | 12 29 19 12 --- 16 31 16 15 --- 15
32E | 18 27 12 10 17 6 15 25 13 18 6 | 90 70 82 82 9 83 82 93 85 79 84
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 8 10 14 5 14 13 9 17 |T 22 30 24 24 27 23 30 26 24 25 22
WRMS | 7 18 7 10 13 5 13 11 8 15 |NE 16 25 18 19 24 17 25 20 18 20 16
MEDI | 7 18 7 9 15 5 14 11 9 16 |MD 19 28 21 22 26 19 26 24 22 23 19
Table 3.1663.3 GPS week: 1663 Day: 3 MJD: 55888.000
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 | 9 18 4 7 --- 4 14 16 9 13 4 | 31 46 40 36 --- 37 47 40 35 35 36
2 | 9 22 8 17 11 4 15 12 15 24 5 | 20 35 22 23 26 19 30 23 24 23 21
3 | 7 14 7 13 9 7 10 7 12 17 3 | 26 26 25 23 29 25 25 22 24 20 23
4 | 5 14 5 10 10 5 7 13 11 22 3 | 21 23 23 28 25 23 20 26 28 24 22
5E | 6 20 6 18 12 5 20 10 12 22 4 | 28 32 28 26 30 22 30 27 23 37 26
6 | 6 14 8 12 9 6 8 7 13 16 3 | 29 31 29 29 33 31 28 29 28 28 29
7 | 7 19 10 14 17 5 12 9 8 10 4 | 20 27 18 19 28 21 24 24 23 18 18
8 | 11 17 7 10 15 5 12 13 9 15 4 | 15 24 15 20 19 15 22 23 21 21 14
9 | 7 17 7 14 9 4 10 8 9 14 3 | 15 22 16 19 18 14 23 19 18 20 14
10E | 18 15 9 12 16 5 17 13 11 15 5 | 46 49 50 48 50 44 49 46 46 47 46
11 | 7 20 8 8 11 5 13 14 14 15 4 | 25 33 26 25 36 24 30 29 24 23 25
12 | 8 27 8 14 16 6 22 10 9 11 4 | 63 69 69 73 77 68 68 66 69 67 67
13 | 7 22 11 12 21 6 13 14 10 11 4 | 14 30 17 20 36 14 25 14 17 14 14
14 | 7 23 6 12 13 6 12 15 10 15 4 | 15 25 18 16 26 15 20 18 17 16 15
15 | 5 22 8 9 17 5 17 12 12 17 4 | 11 24 15 14 30 13 24 15 16 15 13
16 | 6 21 9 10 14 6 14 14 14 17 4 | 16 24 16 15 26 16 21 19 21 16 15
17 | 7 17 6 18 12 4 17 9 11 26 4 | 21 25 27 30 25 24 26 28 31 27 24
18E | 8 22 7 11 21 5 12 9 10 10 4 | 23 29 24 22 27 21 26 24 25 22 23
19 | 8 19 10 10 10 4 15 17 12 27 5 | 15 22 17 16 21 18 23 25 21 20 17
20E | 6 13 7 10 16 5 9 9 10 10 3 | 42 43 42 43 46 40 44 48 44 46 42
21 | 8 20 6 12 9 5 12 11 9 26 4 | 17 25 15 16 16 14 24 17 15 20 15
22E | 8 17 6 11 16 4 9 7 8 9 3 | 24 22 24 24 25 21 23 23 24 22 22
23 | 9 27 9 14 17 5 17 20 11 14 5 | 19 35 19 19 29 17 27 19 19 16 16
25E | 9 21 8 12 13 5 15 11 8 12 4 | 24 28 23 27 26 23 32 31 25 29 22
26 | 13 14 5 13 11 3 11 7 14 13 4 | 26 24 22 24 30 19 28 22 20 24 22
X27 | 15 18 20 23 --- 12 12 19 --- --- 8 | 17 23 26 24 --- 16 22 19 --- --- 16
28 | 8 19 6 10 18 3 10 11 13 11 4 | 15 26 16 20 26 15 21 19 22 16 15
29 | 5 22 9 11 12 6 17 15 11 22 4 | 21 29 25 26 27 23 29 24 29 21 22
30E | 11 20 11 20 15 6 17 18 16 16 5 | 26 34 32 28 34 25 30 26 30 24 27
X31 | 9 --- --- --- --- 28 --- --- --- --- 0 | 9 --- --- --- --- 10 --- --- --- --- 10
X32E | 25 33 11 12 --- 7 18 23 17 20 7 | 90 101 92 94 --- 92 91 97 99 89 91
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 8 13 14 5 14 12 11 17 |T 25 32 27 28 30 25 31 28 28 27 25
WRMS | 8 20 8 13 14 5 13 11 10 17 |NE 18 26 21 21 25 18 25 21 22 21 18
MEDI | 8 19 8 12 13 5 13 12 11 15 |MD 21 27 23 24 27 21 26 24 24 22 22
Table 3.1663.4 GPS week: 1663 Day: 4 MJD: 55889.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1M | 6 14 8 10 --- 4 17 16 11 11 4 | 31 45 38 31 --- 34 49 40 32 37 35
2 | 7 18 6 15 13 5 14 10 10 24 4 | 18 31 21 23 25 19 29 21 21 16 20
3 | 9 13 5 12 16 6 10 12 12 22 4 | 18 21 21 21 21 18 23 19 21 18 18
4 | 5 11 5 13 13 5 7 9 7 17 3 | 17 18 21 25 23 21 21 22 22 22 20
5E | 9 18 6 14 16 4 18 9 10 12 4 | 25 30 25 30 29 25 29 25 25 27 24
6 | 5 13 7 14 15 5 8 12 14 20 4 | 21 23 22 23 25 21 26 23 28 22 22
7 | 8 17 10 13 22 5 15 11 12 11 4 | 26 31 28 28 34 27 30 29 28 26 25
8 | 14 19 8 9 17 6 14 13 11 14 4 | 18 23 20 22 19 17 24 22 22 21 17
9 | 6 18 5 13 10 4 11 12 7 16 3 | 12 21 12 16 18 11 18 14 15 16 12
10E | 17 18 9 11 23 6 19 13 8 18 5 | 25 33 27 32 38 28 38 29 28 28 27
11M | 5 17 7 11 13 5 15 16 16 16 4 | 19 29 21 24 30 18 28 27 21 22 19
12 | 18 22 8 11 20 14 21 14 19 14 5 | 86 94 91 94 93 85 95 92 81 91 86
13M | 7 16 7 32 26 7 12 13 10 11 5 | 15 25 16 31 34 13 23 14 12 12 14
14 | 7 17 7 6 18 4 11 14 11 16 4 | 16 26 15 15 29 15 20 19 22 18 17
15 | 5 20 6 10 23 4 18 12 8 16 4 | 9 22 14 16 34 11 21 12 15 13 12
16 | 6 23 7 10 22 4 17 11 12 19 4 | 21 31 26 25 36 23 26 23 21 21 22
17 | 7 16 6 18 15 4 17 12 13 25 4 | 19 22 19 25 20 21 22 26 24 33 19
18E | 8 20 6 12 13 6 11 11 9 14 3 | 28 32 25 26 30 24 27 26 26 25 27
19 | 6 14 6 10 11 5 13 20 10 25 4 | 11 19 14 17 15 12 20 22 13 16 12
20E | 5 12 5 9 12 4 9 11 9 10 3 | 55 55 57 51 62 52 56 53 53 57 54
21 | 7 18 5 10 9 3 13 10 10 30 4 | 16 25 15 13 18 14 24 15 14 19 15
22E | 9 13 9 13 16 4 10 10 7 14 3 | 23 24 22 24 22 20 25 23 21 25 22
23 | 11 23 8 14 24 6 16 20 11 15 5 | 17 28 18 11 27 11 22 19 13 15 12
25E | 8 18 8 8 17 5 19 13 13 10 4 | 19 28 22 26 33 24 32 30 22 28 22
26 | 12 14 4 12 14 5 10 9 11 15 3 | 22 24 17 24 27 13 24 19 16 12 16
X27 | 15 19 11 16 --- 20 11 15 --- --- 6 | 19 22 18 16 --- 16 19 15 --- --- 10
28 | 8 16 5 8 19 7 11 11 13 11 3 | 20 24 21 24 30 19 24 22 24 22 20
29 | 5 18 9 13 13 4 17 14 13 24 4 | 18 24 23 25 23 21 27 20 26 22 20
30E | 11 14 7 17 20 7 15 21 16 26 5 | 16 25 19 20 27 14 26 17 20 17 16
X31 | 6 18 6 8 23 4 15 15 7 --- 4 | 12 25 12 13 22 12 21 9 12 --- 13
X32E | 15 --- 13 13 --- 8 19 27 16 19 7 | 92 --- 89 90 --- 88 89 102 90 87 91
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 7 13 17 6 14 13 11 18 |T 24 29 26 27 30 24 30 27 26 27 24
WRMS | 8 17 7 12 16 5 14 12 8 18 |NE 16 23 17 18 23 15 22 17 18 17 15
MEDI | 7 17 7 12 16 5 14 12 11 16 |MD 19 25 21 24 27 19 25 22 22 22 20
Table 3.1663.5 GPS week: 1663 Day: 5 MJD: 55890.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 8 17 6 10 --- 5 16 14 10 15 4 | 30 44 38 36 --- 34 50 34 33 32 35
2 | 7 20 6 12 13 4 14 8 7 22 4 | 20 34 22 23 25 24 27 23 27 22 21
3 | 12 18 5 8 15 5 12 13 8 21 4 | 23 26 22 21 24 21 26 23 26 24 21
4 | 5 13 5 8 15 4 7 13 10 20 3 | 24 23 20 20 21 24 21 27 26 25 19
5E | 8 18 8 12 15 3 17 8 10 16 4 | 32 39 31 30 33 32 32 35 32 40 30
6 | 7 18 6 12 14 6 10 14 9 18 4 | 22 27 26 25 28 23 27 27 27 26 24
7M | 7 20 9 12 24 5 18 10 7 12 4 | 27 35 30 28 28 28 30 35 30 25 26
8M | 10 19 7 8 15 5 17 10 10 10 4 | 26 27 25 26 24 22 27 30 28 24 21
9 | 6 17 8 8 10 5 11 10 12 17 3 | 14 24 15 16 20 16 23 19 19 20 13
10E | 18 20 9 9 21 8 21 10 12 17 5 | 50 51 49 47 50 47 53 48 48 52 46
11M | 9 18 8 19 16 8 13 17 11 16 5 | 21 33 23 31 33 21 32 27 24 22 22
12E | 20 26 9 8 18 5 20 10 11 14 5 | 47 53 47 46 51 49 50 51 46 50 45
13 | 6 19 9 6 28 6 15 16 8 12 4 | 21 34 23 17 36 20 30 18 20 17 16
14M | 9 21 7 5 20 5 13 13 10 15 4 | 20 29 25 22 34 21 28 26 24 24 20
15 | 6 23 9 9 22 4 19 11 11 19 4 | 16 29 17 14 35 13 27 16 17 14 12
16E | 7 27 7 9 17 8 13 18 10 20 4 | 29 41 33 27 37 30 36 34 32 28 30
17M | 10 18 9 18 12 4 18 12 12 24 5 | 19 25 23 24 15 20 26 25 24 25 18
18E | 7 17 8 7 18 5 10 10 8 11 3 | 22 27 21 24 24 20 22 27 25 25 22
19 | 7 20 7 7 9 6 15 17 9 24 4 | 16 24 18 15 20 15 23 21 18 15 15
20E | 9 15 7 10 19 7 12 14 7 16 4 | 57 58 58 58 56 56 58 58 53 58 55
21 | 7 19 5 6 12 4 14 15 14 29 4 | 16 26 12 13 17 13 22 20 18 19 12
22E | 10 15 7 8 15 5 9 9 8 11 3 | 28 28 26 28 26 24 25 26 28 26 24
23 | 10 28 9 9 25 6 19 23 9 16 5 | 19 35 21 14 30 15 28 25 16 16 15
25E | 7 18 11 11 10 7 21 13 16 26 5 | 23 28 29 26 26 27 33 29 30 36 25
26 | 15 16 9 10 11 4 12 9 12 14 4 | 34 33 26 26 33 26 32 27 25 25 24
X27 | 16 24 21 18 --- 9 12 16 --- --- 8 | 16 27 27 26 --- 25 26 20 --- --- 16
28 | 17 18 5 11 20 5 14 11 10 11 4 | 21 31 25 18 35 20 27 25 29 24 21
29 | 6 14 8 6 13 5 15 10 11 29 4 | 20 26 23 20 23 21 26 23 22 27 19
30E | 13 15 8 14 21 6 19 20 12 24 5 | 26 34 31 30 35 27 33 30 31 25 28
31 | 10 21 7 7 22 4 17 11 7 15 4 | 12 25 17 13 21 15 25 13 14 8 12
X32E | 22 28 9 10 --- 11 18 19 14 17 6 | 99 69 97 97 --- 98 93 105 102 90 98
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 8 10 17 6 15 13 10 19 |T 27 33 29 27 30 27 32 30 29 28 25
WRMS | 9 19 8 10 16 6 14 12 8 18 |NE 19 27 20 18 24 19 25 21 21 20 17
MEDI | 9 18 8 9 15 5 15 13 10 16 |MD 22 29 25 25 28 23 27 27 26 25 21
Table 3.1663.6 GPS week: 1663 Day: 6 MJD: 55891.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 8 17 6 11 --- 5 16 13 12 11 4 | 37 53 47 43 --- 42 58 44 42 40 43
2 | 11 20 7 12 10 4 15 10 14 23 4 | 28 40 30 22 31 30 36 31 34 27 28
3 | 10 16 7 10 15 8 8 17 8 27 4 | 32 38 34 32 37 34 35 32 36 30 32
4 | 10 14 7 10 11 5 11 13 13 18 4 | 29 32 34 34 32 32 30 33 39 28 30
5E | 8 16 8 10 12 8 15 13 14 14 4 | 38 44 36 37 42 39 38 42 39 43 36
6 | 7 18 7 8 13 6 9 15 12 21 4 | 33 42 38 33 40 37 39 40 38 36 35
7 | 6 18 9 9 20 6 15 16 10 13 4 | 32 40 34 31 41 35 35 33 33 28 29
8 | 10 18 7 10 14 8 14 13 13 12 4 | 22 31 22 22 25 25 29 27 26 24 20
9 | 9 19 6 9 13 5 13 10 9 12 3 | 20 34 26 20 27 22 29 20 29 24 21
10E | 18 23 11 8 21 6 22 16 13 21 5 | 52 57 48 51 58 47 53 51 48 47 48
11 | 6 18 6 11 16 5 13 15 13 18 4 | 27 40 31 28 41 29 37 32 34 27 29
12E | 11 25 10 9 15 7 19 9 12 15 4 | 43 47 45 42 47 45 47 44 50 45 44
13 | 7 17 8 7 26 5 13 17 9 11 4 | 20 31 19 16 38 20 29 19 24 16 17
14 | 11 17 8 6 20 5 13 9 12 11 4 | 15 23 18 14 29 15 20 19 18 17 15
15 | 9 22 9 9 23 6 19 10 14 13 4 | 20 32 24 17 38 20 28 19 28 18 20
16E | 8 20 7 8 16 6 12 13 8 17 4 | 31 36 37 33 39 35 35 38 37 27 33
17 | 12 15 8 15 13 5 18 13 9 25 4 | 28 31 32 31 28 31 32 35 33 34 28
18E | 10 20 6 9 18 5 8 9 14 12 4 | 25 39 29 27 33 26 30 29 31 30 28
19 | 7 18 5 7 9 6 14 13 8 30 4 | 18 27 21 19 24 22 25 26 25 23 19
20 | 21 18 8 12 19 16 16 23 13 14 5 | 133 134 133 126 131 124 133 117 125 124 127
21 | 9 17 6 7 12 7 14 14 15 28 4 | 19 30 19 16 24 20 27 23 28 25 19
22E | 9 15 8 7 16 5 8 8 12 12 3 | 24 31 25 26 26 23 25 26 31 27 23
23 | 9 22 9 7 21 7 17 21 9 14 5 | 26 37 26 18 35 26 33 24 30 24 23
25E | 11 17 7 8 14 8 18 12 16 13 4 | 22 30 22 19 26 20 31 25 27 24 20
26 | 11 17 7 11 12 7 10 10 13 12 4 | 26 29 22 23 27 23 27 23 22 18 20
X27 | 23 21 29 15 --- 21 19 22 --- --- 10 | 18 29 29 23 --- 25 25 17 --- --- 17
28E | 13 23 5 12 15 6 11 13 14 9 4 | 38 44 47 55 48 40 46 43 38 44 43
29 | 7 18 9 9 10 8 16 9 8 32 4 | 25 31 32 26 31 28 31 27 32 30 27
30E | 13 20 8 11 17 5 18 22 13 28 5 | 35 39 36 33 39 32 37 33 41 29 34
31 | 12 18 6 8 22 5 16 14 10 12 4 | 15 31 18 14 31 18 28 16 20 10 15
X32E | 19 --- 9 12 --- 9 19 13 15 18 6 | 85 --- 83 85 --- 81 77 89 86 77 84
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 8 9 16 7 15 14 12 19 |T 32 39 35 32 38 33 38 34 37 33 32
WRMS | 9 19 7 9 16 6 14 13 9 17 |NE 23 33 27 22 31 25 30 25 30 24 23
MEDI | 10 18 7 9 15 6 15 13 12 14 |MD 27 34 31 27 33 29 32 31 33 27 28
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 4.1663 GPS week: 1663 MJD: 55885.0-55891.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2956 |U 8 7 18 |U 11 11 34 |U 8 9 19 |
emr | emr 2910 |U 17 18 32 |U 12 11 41 | 11 12 24 |
esa | esa 2962 | 8 8 20 |U 10 11 34 | 9 10 19 |
gfz | gfz 2950 |U 18 19 30 |U 14 19 60 |U 12 14 24 |
grg | grg 2687 | 23 25 39 |U 16 15 58 | 15 14 29 |
igr | igr 2956 | 8 8 19 | 11 11 35 | 9 9 19 |
igs | igs 2922 | 12 12 24 | 11 10 36 | 9 10 21 |
jpl | jpl 2929 |U 16 18 30 |U 11 12 36 | 10 12 25 |
mit | mit 2962 |U 25 22 29 |U 11 11 34 |U 11 17 22 |
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 5.1663.0 GPS week: 1663 Day: 0 MJD: 55885.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 9 7 15 | 9 8 24 | 9 9 23 |
emr | emr 2872 | 13 17 33 | 10 10 34 | 10 17 22 |
esa | esa 2976 | 8 8 19 | 9 9 26 | 8 11 21 |
gfz | gfz 2964 | 13 15 27 | 15 19 72 | 13 15 29 |
grg | grg 2687 | 22 28 37 | 17 23 76 | 22 17 40 |
igr | igr 2976 | 8 6 16 | 9 8 27 | 8 10 21 |
igs | igs 2961 | 15 18 32 | 9 8 27 | 8 14 26 |
jpl | jpl 2956 | 15 17 34 | 9 9 25 | 10 17 29 |
mit | mit 2976 | 52 29 56 | 9 8 24 | 8 16 22 |
Table 5.1663.1 GPS week: 1663 Day: 1 MJD: 55886.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2973 | 5 6 15 | 10 13 34 | 8 10 25 |
emr | emr 2962 | 16 17 26 | 10 13 43 | 10 13 26 |
esa | esa 2976 | 6 7 18 | 10 14 36 | 10 11 23 |
gfz | gfz 2965 | 14 17 23 | 17 30 45 | 9 12 24 |
grg | grg 2784 | 29 26 21 | 32 19 73 | 13 17 30 |
igr | igr 2958 | 6 8 18 | 10 13 36 | 10 13 27 |
igs | igs 2953 | 19 22 26 | 10 12 37 | 8 11 22 |
jpl | jpl 2872 | 16 19 32 | 10 14 37 | 10 11 27 |
mit | mit 2976 | 21 24 18 | 11 15 35 | 10 12 29 |
Table 5.1663.2 GPS week: 1663 Day: 2 MJD: 55887.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 8 8 24 | 10 13 40 | 8 7 18 |
emr | emr 2962 | 16 23 34 | 10 13 52 | 8 10 22 |
esa | esa 2976 | 8 10 23 | 9 11 40 | 7 9 19 |
gfz | gfz 2963 | 17 24 30 | 15 18 79 | 9 12 23 |
grg | grg 2687 | 22 22 31 | 11 13 61 | 13 14 30 |
igr | igr 2974 | 8 8 25 | 9 13 40 | 8 9 17 |
igs | igs 2963 | 7 9 22 | 9 11 48 | 7 8 21 |
jpl | jpl 2956 | 18 25 26 | 10 13 48 | 10 9 26 |
mit | mit 2976 | 22 24 23 | 10 12 49 | 9 14 24 |
Table 5.1663.3 GPS week: 1663 Day: 3 MJD: 55888.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2871 | 12 7 20 | 9 11 25 | 7 9 15 |
emr | emr 2868 | 20 20 39 | 11 8 27 | 17 14 29 |
esa | esa 2880 | 11 7 18 | 8 10 25 | 9 9 17 |
gfz | gfz 2868 | 22 22 34 | 13 25 103 | 18 23 30 |
grg | grg 2591 | 26 23 44 | 11 14 45 | 20 16 31 |
igr | igr 2873 | 11 7 20 | 10 11 25 | 9 9 15 |
igs | igs 2816 | 11 7 21 | 10 10 25 | 9 9 16 |
jpl | jpl 2860 | 21 20 35 | 11 14 30 | 14 18 23 |
mit | mit 2880 | 24 23 24 | 9 11 27 | 15 15 20 |
Table 5.1663.4 GPS week: 1663 Day: 4 MJD: 55889.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 | 6 8 12 | 17 14 51 | 8 8 17 |
emr | emr 2872 | 16 11 30 | 19 14 55 | 9 9 20 |
esa | esa 2976 | 7 7 17 | 17 14 50 | 9 7 18 |
gfz | gfz 2963 | 21 15 35 | 17 16 41 | 14 11 17 |
grg | grg 2688 | 18 18 38 | 18 16 58 | 11 10 20 |
igr | igr 2976 | 6 8 15 | 18 12 52 | 9 8 18 |
igs | igs 2919 | 7 6 16 | 18 13 50 | 10 8 19 |
jpl | jpl 2954 | 10 8 22 | 18 13 51 | 8 5 21 |
mit | mit 2976 | 18 14 29 | 18 17 44 | 10 12 23 |
Table 5.1663.5 GPS week: 1663 Day: 5 MJD: 55890.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 | 9 10 27 | 9 10 29 | 8 10 15 |
emr | emr 2963 | 19 19 34 | 11 8 29 | ---- ---- ---- |
esa | esa 2976 | 9 10 28 | 9 8 27 | 10 13 20 |
gfz | gfz 2963 | 19 22 34 | 11 12 37 | 10 14 21 |
grg | grg 2687 | 19 25 42 | 10 10 34 | ---- ---- ---- |
igr | igr 2976 | 9 9 27 | 9 9 28 | ---- ---- ---- |
igs | igs 2908 | 10 10 28 | 10 7 29 | ---- ---- ---- |
jpl | jpl 2955 | 18 20 36 | 9 7 27 | 8 11 23 |
mit | mit 2976 | 22 23 31 | 9 8 26 | 15 37 20 |
Table 5.1663.6 GPS week: 1663 Day: 6 MJD: 55891.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 7 7 13 | 10 11 37 | 10 9 21 |
emr | emr 2872 | 18 16 30 | 13 11 44 | 10 11 26 |
esa | esa 2976 | 9 9 14 | 9 10 36 | 10 9 17 |
gfz | gfz 2965 | 18 18 25 | 10 11 40 | 11 9 22 |
grg | grg 2685 | 24 32 59 | 13 10 56 | 15 13 24 |
igr | igr 2960 | 9 9 13 | 10 10 38 | 9 9 18 |
igs | igs 2939 | 15 13 22 | 13 12 39 | 10 11 22 |
jpl | jpl 2956 | 18 16 27 | 10 11 36 | 11 11 26 |
mit | mit 2976 | 18 18 23 | 10 11 36 | 10 9 18 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1663 GPS week: 1663 MJD: 55885.500-55891.500
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 | -8 -9 -65 122 0 | 2 10
| 18 7 125 74 8 | 2
emr uuuuu | 9 -4 56 75 -11 | 36 41
| 26 36 163 192 10 | 6
esa uuuuu | -34 -32 56 -94 -3 | -4 12
| 15 11 46 84 7 | 2
gfz uuuuu | -32 34 -2 25 -4 | -4 13
| 20 26 101 56 2 | 3
grg uuuux | 4 -18 86 -8 -2 | -8 17
| 19 32 99 101 29 | 2
igr xxxxx | -49 20 60 42 2 | -1 9
| 15 17 75 61 8 | 1
irf xxxxx | -12 15 9 11 -2 | -1 11
| 19 9 30 46 3 | 2
jpl uuuuu | 25 -27 -36 -86 -1 | 17 21
| 38 22 78 54 8 | 6
mit uuuuu | 0 37 -180 90 -3 | 8 14
| 43 22 86 95 6 | 3
ngs uuuuu | 36 45 108 52 5 | 2 7
| 51 58 46 102 3 | 1
sio uuuuu | 52 -50 -169 66 -10 | 18 22
| 49 36 108 90 5 | 3
Table 7.1663.0 GPS week: 1663 Day: 0 MJD: 55885.500
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 | -30 -11 -238 38 9 | 4 15
emr uuuuu | 6 -14 171 -106 -17 | 44 48
esa uuuuu | -12 -16 47 -38 1 | -3 17
gfz uuuuu | -41 43 -51 13 -4 | 1 16
grg uuuux | -3 8 133 -73 15 | -8 17
igr xxxxx | -38 20 -17 74 6 | 0 15
irf xxxxx | -12 28 -35 51 0 | 2 14
jpl uuuuu | -24 5 -68 -62 1 | 25 30
mit uuuuu | -7 65 -275 231 -3 | 12 17
ngs uuuuu | 74 -34 127 -48 5 | 4 11
sio uuuuu | 33 -57 -200 197 -4 | 22 27
Table 7.1663.1 GPS week: 1663 Day: 1 MJD: 55886.500
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 -9 31 80 12 | 2 12
emr uuuuu | 16 23 1 -90 -19 | 40 44
esa uuuuu | -28 -51 61 -44 12 | -5 16
gfz uuuuu | -23 21 -72 57 -4 | -3 12
grg uuuux | 6 1 -17 -130 14 | -10 15
igr xxxxx | -41 21 -30 -9 8 | -2 12
irf xxxxx | -17 4 29 -30 1 | -1 12
jpl uuuuu | 41 -30 -26 -59 -10 | 22 27
mit uuuuu | -23 3 -105 151 -4 | 9 15
ngs uuuuu | 57 143 83 16 1 | 1 7
sio uuuuu | 17 -107 27 82 -5 | 19 23
Table 7.1663.2 GPS week: 1663 Day: 2 MJD: 55887.500
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 | -32 -15 -71 154 1 | 4 10
emr uuuuu | 14 38 -122 220 -19 | 39 44
esa uuuuu | -37 -25 102 -177 -5 | -2 9
gfz uuuuu | -47 11 53 -31 1 | -2 12
grg uuuux | -27 16 -34 -105 35 | -9 14
igr xxxxx | -54 11 15 -43 14 | 0 8
irf xxxxx | -34 20 23 5 -6 | 1 9
jpl uuuuu | 57 -37 -19 -37 -10 | 21 26
mit uuuuu | -44 48 -158 120 -13 | 10 14
ngs uuuuu | 89 4 67 92 7 | 2 6
sio uuuuu | 13 -46 -94 144 -11 | 20 23
Table 7.1663.3 GPS week: 1663 Day: 3 MJD: 55888.500
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 5 -83 109 -7 | 3 9
emr uuuuu | 58 34 -163 408 -20 | 36 41
esa uuuuu | -61 -29 -25 -222 -5 | -4 10
gfz uuuuu | -41 -8 135 -56 -6 | -5 12
grg uuuux | 25 1 23 2 17 | -6 15
igr xxxxx | -51 -2 100 5 2 | -1 7
irf xxxxx | -25 4 39 -41 -4 | -1 10
jpl uuuuu | 68 -20 -23 -26 -5 | 16 22
mit uuuuu | -34 13 -59 81 -8 | 7 14
ngs uuuuu | 56 90 158 143 7 | 1 6
sio uuuuu | 13 -85 -157 19 -8 | 18 22
Table 7.1663.4 GPS week: 1663 Day: 4 MJD: 55889.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 19 -7 23 74 -2 | 2 8
emr uuuuu | 4 -15 58 148 -5 | 34 39
esa uuuuu | -33 -42 27 -142 -7 | -4 10
gfz uuuuu | -57 52 115 44 -6 | -6 12
grg uuuux | 31 -38 218 132 -21 | -5 16
igr xxxxx | -64 34 53 121 -2 | 0 7
irf xxxxx | -15 21 22 53 -3 | -2 9
jpl uuuuu | 40 -33 -80 -128 -4 | 13 16
mit uuuuu | -7 51 -189 74 -2 | 6 12
ngs uuuuu | 46 55 71 83 8 | 1 7
sio uuuuu | 53 -17 -244 65 -12 | 18 22
Table 7.1663.5 GPS week: 1663 Day: 5 MJD: 55890.500
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 -14 93 136 -11 | 1 9
emr uuuuu | -23 -49 162 16 -2 | 31 37
esa uuuuu | -33 -27 74 -17 -5 | -5 11
gfz uuuuu | -10 58 -96 39 -7 | -7 13
grg uuuux | -7 -44 189 22 -40 | -7 19
igr xxxxx | -67 49 138 46 -12 | -1 8
irf xxxxx | -6 18 20 -30 -2 | -3 10
jpl uuuuu | 22 -63 -144 -172 8 | 11 15
mit uuuuu | 35 43 -173 -75 6 | 5 12
ngs uuuuu | -12 37 178 179 2 | 2 6
sio uuuuu | 88 -29 -212 -84 -15 | 16 21
Table 7.1663.6 GPS week: 1663 Day: 6 MJD: 55891.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -4 -11 -212 264 0 | -1 8
emr uuuuu | -12 -42 284 -70 3 | 28 31
esa uuuuu | -32 -31 109 -21 -10 | -6 11
gfz uuuuu | -4 59 -99 110 -4 | -9 13
grg uuuux | 1 -70 92 99 -34 | -11 23
igr xxxxx | -24 10 161 101 -2 | -2 8
irf xxxxx | 27 10 -34 68 -4 | -4 10
jpl uuuuu | -29 -8 110 -121 11 | 11 14
mit uuuuu | 80 35 -300 51 3 | 4 12
ngs uuuuu | -54 22 73 -103 4 | 2 7
sio uuuuu | 146 -10 -302 42 -18 | 14 19
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