[IGSREPORT-21000] Wk 1695 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Jul 19 14:29:17 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1695 (Jul 01, 2012 - Jul 07, 2012)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi 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:
igs1695[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1695[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1695[0-6].cls IGS GPS clock combination summary report.
igs16957.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16957.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 | KOUC KOUC
0 | ESA | IRKJ
0 | GFZ | 26 ASPA BRFT COCO DGAR FLIN PETS RIO2 SEY1
0 | GRG | IRKJ
0 | JPL | 26 YELL
0 | MIT | 1 6 10 26 1 6 10 26 FLIN MDVJ BOR1 FLIN MDVJ
1 | COD | KOUC KOUC MDVJ
1 | ESA | IRKJ
1 | GFZ | BRFT GRAS
1 | JPL | 26 WHIT YELL
1 | MIT | 3 6 13 26 3 6 13 26 GRAZ
2 | COD | BRMU
2 | ESA | IRKJ
2 | GFZ | ASPA AUCK BRFT CAS1 COCO DGAR FLRS GMSD PDEL PETS
2 | GFZ | RIO2 SEY1 TWTF XMIS
2 | JPL | 26 31 QAQ1
2 | MIT | 26 26 JOZ2
3 | COD | TLSE
3 | ESA | DAV1 PALM TLSE
3 | GFZ | BOGT BRFT CHUR COCO GMSD HARV HOLB PDEL RIO2 SCH2
3 | GFZ | SEY1 STHL TWTF
3 | MIT | 3 16 26 3 16 26 DAV1 TLSE
4 | ESA | 1 2 3 4 5 6 8 9 10 11 12 13 14 15 16 17 18 19 20
4 | ESA | 21 22 23 25 26 27 28 29 30 31 32 1 2 3 4 5 6 8 9
4 | ESA | 10 11 12 13 14 15 16 17 18 19 20 21 22 23 25 26 27
4 | ESA | 28 29 30 31 32 AREQ AREQ
4 | GFZ | 25 BRFT COCO DGAR
4 | GRG | MATE
4 | JPL | 26 MAS1
4 | MIT | TLSE
5 | COD | FLRS KOUC
5 | ESA | MDVJ
5 | GFZ | AUCK BRFT DGAR MAG0 MIZU NICO ONSA PDEL REUN RIO2
5 | GFZ | SCH2 YIBL
5 | JPL | 26
5 | MIT | 26 26 DAV1 MAW1 MDVJ
6 | COD | KOUC TLSE KOUC
6 | EMR | MATE
6 | GFZ | 30 BRFT OHI2 RIO2
6 | GRG | MATE
6 | JPL | 26 30
6 | MIT | 26 26 MDVJ GMSD MDVJ 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
----+------------+----------
G07 | 2012_07_05 | 2012046
G07 | 2012_07_06 | 2012046
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 G26 | | | | 2 | | | |
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 | .9 .2 -.5 -33 -14 11 -.18
EMR | -2.4 -2.7 3.1 -2 2 -35 .13
ESA | .3 -4.1 2.1 -51 -64 114 -.13
GFZ | -.9 .4 -.9 -24 1 -6 -.16
GRG | 4.3 -7.2 19.5 -16 39 -4 -.13
JPL | 2.9 -.4 8.6 14 -4 -12 .10
MIT | 2.8 -2.7 14.5 -115 -109 -18 -.03
NGS | 1.0 .2 19.8 -50 17 2 -.04
SIO | -1.0 -1.9 6.2 -39 28 29 -.09
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 1.1695.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1695.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 2.1695.[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 3.1695.[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 5.1695.0-6).
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 1695 summary. (Jul 01, 2012 - Jul 07, 2012)
Table 1.1695.a GPS week: 1695 MJD: 56109.000-56115.000
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 256| 0 1 -5 -17 -17 5 -.27 10 9 | -385 -331 14 64
| 0 0 0 9 12 13 .02 | 412 920
emr 104| 0 -2 0 -42 11 -45 .42 15 15 | 389589 3130 58 137
| 1 0 1 14 11 13 .03 | 1020682 9604
esa 186| 1 0 1 -24 17 26 .21 7 7 | -381 -563 29 128
| 0 0 0 17 24 14 .02 | 577 1220
gfz 196| 0 -1 0 -1 -27 -22 -.37 12 12 | 88 201 33 118
| 0 0 1 49 59 5 .04 | 451 934
grg 123| 1 0 6 -65 -79 17 .60 15 14 | 102 -110 50 217
| 0 1 2 13 9 12 .03 | 352 795
igr n/a| 0 0 0 -58 -55 -30 -.08 5 5 | 11660 104 22 72
| 0 0 0 18 16 24 .03 | 1036 1163
jpl 173| 0 0 -4 -96 -3 0 .49 14 13 | 4729 -584 21 103
| 1 0 1 14 17 13 .04 | 798 1138
mit 260| 0 0 -1 152 172 -3 -.40 11 10 | -95 190 19 149
| 1 0 1 24 30 8 .04 | 365 565
ngs 253| 0 0 6 37 -100 -28 -.20 12 8 | -442 -305 1971 3853
| 0 1 2 23 33 19 .05 | 321 759
sio 246| 0 1 0 15 -63 14 -.24 19 19 | --- --- --- ---
| 1 0 1 25 24 5 .04 | --- ---
Table 1.1695.b GPS week : 1695 MJD: 56109.000-56115.000
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 5 5 5 5 5 5 |
3 | 4 4 4 4 4 6 6 |
4 | 4 4 4 4 4 4 4 |
5 | 5 5 5 5 5 5 5 |
6 | 4 4 4 4 4 4 5 |
7 | 4 4 4 4 0 6 4 |
8 | 4 4 4 4 4 4 4 |
9 | 4 3 3 4 4 3 4 |
10 | 4 3 3 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 3 5 4 3 4 3 4 |
14 | 4 4 3 5 4 5 4 |
15 | 5 5 5 5 5 5 5 |
16 | 4 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 5 |
18 | 5 4 4 4 4 4 4 |
19 | 4 4 5 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 3 4 4 4 4 |
23 | 4 4 4 4 4 4 4 |
25 | 4 5 4 4 4 4 4 |
26 | 7 10 10 11 8 6 6 |
27 | 4 3 4 4 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 3 4 3 4 4 4 4 |
31 | 4 4 4 4 4 4 4 |
32 | 4 3 3 3 3 4 4 |
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 2.1695.0 GPS week: 1695 Day: 0 MJD: 56109.000
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 256| 0 1 -5 -7 -22 -14 -.26 9 9 | 325 -1374 14 84
| 56 -35 |
emr 104| 1 -2 0 -51 -4 -46 .38 15 15 | 4848 -1365 59 145
| -47 -40 |
esa 186| 0 0 1 -52 -1 32 .19 6 6 | 350 -1158 11 118
| 18 7 |
gfz 196| 0 0 -1 33 -33 -16 -.33 12 13 | 643 -642 31 122
| -39 38 |
grg 123| 2 1 2 -50 -96 0 .66 14 13 | 534 -738 43 233
| 13 -3 |
igr n/a| 0 0 1 -86 -70 9 -.14 6 6 | 10687 -928 28 93
| -23 -24 |
jpl 173| 0 0 -5 -107 8 -18 .54 14 13 | 5943 -1564 18 111
| -30 -81 |
mit 260| 0 -1 0 185 193 -4 -.47 10 9 | 264 -194 21 183
| -96 -151 |
ngs 253| -2 -1 5 -1 -102 7 -.24 11 9 | 133 -1051 1761 4114
| -15 38 |
sio 246| 0 2 -1 39 -36 20 -.23 19 16 | --- --- --- ---
| -68 -13 |
Table 2.1695.1 GPS week: 1695 Day: 1 MJD: 56110.000
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 256| 0 1 -6 -9 -6 18 -.24 10 9 | -695 126 15 57
| 20 -26 |
emr 104| 0 -1 -2 -56 10 -35 .44 15 15 | 3873 -227 61 134
| -30 -48 |
esa 186| 0 0 1 -26 16 13 .24 8 8 | -682 -1125 18 127
| 38 18 |
gfz 196| -1 -2 0 -46 -82 -20 -.34 13 12 | 43 -126 37 127
| -25 10 |
grg 123| 1 -1 4 -68 -85 11 .62 16 14 | 186 -465 58 288
| 12 -26 |
igr n/a| 0 0 0 -61 -55 -6 -.08 5 5 | 10127 504 21 81
| -38 -8 |
jpl 173| -3 0 -3 -77 -17 7 .54 15 14 | 4713 -233 25 112
| 11 -55 |
mit 260| 1 0 -2 134 162 11 -.41 11 9 | 24 -132 22 142
| -96 -150 |
ngs 253| 0 0 9 50 -80 -25 -.20 12 8 | -634 -162 1567 3795
| -29 60 |
sio 246| 1 1 -1 10 -54 13 -.18 19 18 | --- --- --- ---
| -88 -10 |
Table 2.1695.2 GPS week: 1695 Day: 2 MJD: 56111.000
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 256| -1 1 -4 -21 -9 6 -.29 10 9 | -467 -85 13 56
| 70 -8 |
emr 104| 0 -1 0 -39 29 -51 .42 15 15 | 4143 -243 58 115
| -61 -54 |
esa 186| 0 0 0 -33 0 50 .19 7 6 | 434 -2267 13 112
| 7 11 |
gfz 196| -1 -1 -3 -17 -56 -29 -.39 12 11 | 358 -117 33 104
| 26 17 |
grg 123| 1 0 5 -52 -73 15 .59 15 13 | 184 -411 49 235
| 34 -49 |
igr n/a| 0 0 0 -72 -42 -53 -.06 5 4 | 11313 644 22 69
| -44 -5 |
jpl 173| 0 -1 -3 -107 0 6 .50 13 12 | 5097 -201 18 84
| 29 -69 |
mit 260| 1 0 -1 184 167 -5 -.42 12 10 | -67 80 19 140
| -100 -139 |
ngs 253| -1 0 9 44 -71 -49 -.20 14 8 | -485 -98 1874 3723
| -12 40 |
sio 246| 1 0 1 58 -51 10 -.26 19 19 | --- --- --- ---
| -79 -7 |
Table 2.1695.3 GPS week: 1695 Day: 3 MJD: 56112.000
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 256| 0 1 -5 -29 0 -8 -.28 11 10 | -42 -993 16 60
| 44 -66 |
emr 104| -1 -2 0 -37 14 -37 .47 16 16 | 3684 573 63 160
| -55 -58 |
esa 186| 0 0 1 -12 17 32 .22 7 6 | -1125 872 14 118
| -4 9 |
gfz 196| -1 -2 0 -52 -36 -22 -.41 11 11 | -576 1261 35 130
| 18 11 |
grg 123| 2 1 5 -60 -69 21 .59 16 14 | -560 1173 53 179
| 15 -41 |
igr n/a| -1 0 0 -37 -37 -25 -.08 5 4 | 11761 1455 20 57
| -39 3 |
jpl 173| 0 0 -4 -99 9 9 .51 15 14 | 4753 679 22 105
| 18 -55 |
mit 260| 1 0 -1 143 125 -3 -.38 10 9 | -864 1397 20 168
| -96 -133 |
ngs 253| -1 0 4 65 -90 -45 -.11 15 9 | -258 -715 2302 3873
| -86 31 |
sio 246| 1 2 1 -9 -104 20 -.22 18 19 | --- --- --- ---
| -51 -6 |
Table 2.1695.4 GPS week: 1695 Day: 4 MJD: 56113.000
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 256| -1 1 -4 -15 -36 10 -.27 8 8 | -553 622 14 73
| 55 7 |
emr 104| 1 -2 -1 -31 5 -42 .44 15 15 | 4007 -2327 57 144
| -57 -70 |
esa 186| 1 0 2 -31 -10 9 .20 7 7 | -650 -1133 117 165
| 7 26 |
gfz 196| 0 0 2 19 96 -29 -.36 14 14 | -9 -379 36 112
| -1 22 |
grg 123| 2 1 8 -70 -80 29 .58 17 17 | 312 -766 52 234
| 40 -8 |
igr n/a| 0 0 0 -44 -82 -42 -.07 5 4 | 12970 -1601 26 77
| -33 23 |
jpl 173| 0 0 -3 -108 -36 15 .48 14 13 | 5157 -2191 24 98
| 39 -37 |
mit 260| 0 0 -3 148 212 -18 -.35 11 9 | 135 -79 19 105
| -102 -163 |
ngs 253| 0 0 3 50 -161 -21 -.15 12 10 | -564 542 2104 3244
| -94 92 |
sio 246| 0 2 -1 14 -47 6 -.23 19 19 | --- --- --- ---
| -53 -18 |
Table 2.1695.5 GPS week: 1695 Day: 5 MJD: 56114.000
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 256| -1 1 -5 -30 -20 3 -.29 10 9 | -363 -1399 15 67
| 56 -48 |
emr 104| 1 -3 0 -62 19 -31 .43 15 15 | 2295 724 56 116
| -45 -57 |
esa 186| 2 0 0 -12 50 28 .20 7 7 | -670 1138 15 141
| 11 20 |
gfz 196| 0 -1 0 83 -12 -25 -.43 13 13 | -361 1792 33 128
| -30 22 |
grg 123| 1 0 9 -89 -74 8 .56 15 14 | -132 886 50 173
| 35 -24 |
igr n/a| 0 0 0 -67 -62 -54 -.08 5 5 | 12031 1267 20 60
| -31 14 |
jpl 173| 0 -2 -6 -102 8 4 .48 14 14 | 3672 756 20 99
| -17 -63 |
mit 260| -1 0 -2 151 149 1 -.36 13 11 | -161 377 18 146
| -119 -144 |
ngs 253| -1 1 5 11 -126 -39 -.25 11 8 | -398 -1317 2228 4551
| 30 23 |
sio 246| -2 0 0 11 -87 14 -.24 20 18 | --- --- --- ---
| -61 -21 |
Table 2.1695.6 GPS week: 1695 Day: 6 MJD: 56115.000
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 256| 0 1 -5 -11 -28 23 -.29 9 9 | -900 783 14 53
| 31 2 |
emr 104| 0 -1 0 -21 5 -71 .39 15 15 | 2704279 24776 56 146
| -69 -42 |
esa 186| 1 -1 0 0 51 18 .20 7 6 | -326 -268 16 121
| -3 26 |
gfz 196| -1 -1 1 -32 -67 -16 -.35 12 12 | 523 -376 32 108
| 9 29 |
grg 123| 1 0 10 -61 -79 37 .59 14 12 | 192 -453 45 178
| -2 -40 |
igr n/a| 0 0 0 -39 -41 -39 -.08 5 5 | 12737 -613 21 68
| -26 24 |
jpl 173| 0 1 -4 -73 1 -18 .42 15 14 | 3770 -1340 20 115
| -3 -59 |
mit 260| -1 0 -1 117 196 -4 -.40 14 13 | 3 -117 19 160
| -101 -149 |
ngs 253| 0 0 3 43 -67 -22 -.22 10 7 | -889 662 1961 3671
| -7 30 |
sio 246| -2 1 0 -14 -62 11 -.30 21 20 | --- --- --- ---
| -58 -6 |
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 3.1695.0 GPS week: 1695 Day: 0 MJD: 56109.000
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 14 7 16 8 7 15 11 10 12 4 | 49 67 64 58 67 63 75 60 65 55 61
2 | 7 12 7 16 10 5 12 10 11 31 4 | 23 26 23 29 24 24 27 26 25 29 21
3 | 9 15 5 11 13 6 15 6 12 16 3 | 54 60 57 51 55 53 59 54 56 59 54
4 | 8 7 7 14 9 5 9 10 7 23 3 | 26 32 33 30 33 32 33 32 30 35 28
5 | 9 16 7 13 12 8 19 9 14 25 4 | 23 25 20 24 20 22 23 23 25 27 18
6 | 9 12 5 10 11 7 14 9 9 18 3 | 19 16 17 21 20 15 18 20 19 17 16
7 | 10 17 10 12 14 4 14 6 14 16 4 | 15 28 22 14 27 17 26 16 16 15 17
X8 | 6 8 --- 12 15 4 9 4 11 23 4 | 14 22 --- 18 20 18 24 18 17 26 15
9 | 8 14 5 12 13 5 11 12 9 24 3 | 17 17 13 18 19 15 17 16 15 14 14
10 | 8 9 5 11 11 6 8 8 14 17 3 | 26 29 31 31 31 31 31 33 31 30 28
11 | 11 15 6 13 11 9 11 11 11 11 3 | 33 44 39 40 47 41 47 40 44 38 40
12 | 11 21 8 18 17 6 22 10 10 16 5 | 15 29 16 20 28 18 29 13 19 17 12
13E | 6 10 4 10 11 5 11 9 8 13 3 | 38 40 39 35 42 38 45 39 38 40 37
14E | 6 13 5 9 20 5 11 9 7 11 3 | 25 30 26 27 27 24 29 27 29 28 24
15E | 6 16 7 8 18 6 20 11 13 19 4 | 19 23 18 19 23 17 23 18 17 21 17
16 | 7 17 5 12 13 7 13 9 13 22 4 | 14 21 16 14 24 16 23 14 18 20 15
17 | 7 13 6 14 15 5 15 8 6 14 3 | 25 27 21 23 35 23 32 24 21 25 22
18 | 7 19 8 11 15 8 19 8 10 30 4 | 15 27 18 17 25 16 27 16 17 23 14
19 | 7 13 6 10 15 6 12 10 8 25 3 | 30 33 32 25 34 31 36 34 30 37 30
20 | 6 13 5 16 9 9 11 8 10 22 3 | 19 26 19 20 22 21 25 19 19 17 18
21 | 4 13 5 11 11 6 10 8 12 28 3 | 27 37 33 28 37 31 39 31 34 31 31
22 | 4 12 6 9 12 5 14 8 11 19 3 | 20 25 22 21 25 19 25 21 17 17 18
23E | 7 13 6 14 20 5 11 8 9 12 3 | 23 23 20 24 23 21 24 20 21 19 19
25 | 7 18 5 9 14 5 14 17 9 12 4 | 10 17 19 16 30 16 26 15 15 14 13
26E | 23 23 10 13 22 7 20 20 24 19 6 | 55 60 54 53 60 53 61 53 54 51 53
27 | 8 14 4 13 15 5 9 11 10 21 4 | 15 19 12 17 21 14 16 17 13 15 14
28 | 10 14 6 13 16 7 10 8 10 13 3 | 11 22 19 12 28 15 21 14 16 17 13
29 | 11 17 8 15 18 6 18 14 10 17 4 | 22 35 27 28 40 28 37 26 24 28 26
30 | 7 12 5 9 12 7 10 7 13 15 3 | 19 21 17 21 19 17 24 17 14 18 18
31 | 11 13 4 12 14 6 13 7 8 18 3 | 25 26 22 24 32 22 26 23 22 23 21
32 | 7 17 6 13 10 5 10 9 6 15 3 | 16 19 16 17 23 16 22 18 18 19 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 6 12 14 6 14 10 11 19 |T 23 29 26 25 31 25 31 25 25 26 23
WRMS | 9 15 6 13 13 6 13 9 9 16 |NE 21 27 23 23 29 23 29 23 23 24 21
MEDI | 7 14 6 12 13 6 12 9 10 18 |MD 22 26 21 23 27 21 26 21 21 23 18
Table 3.1695.1 GPS week: 1695 Day: 1 MJD: 56110.000
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 | 14 12 5 16 9 4 14 8 10 11 4 | 32 48 43 36 43 39 54 39 45 37 42
2 | 7 12 10 24 11 6 14 9 11 31 5 | 15 19 17 33 16 16 20 18 16 25 15
3 | 12 16 4 11 17 5 15 7 7 14 3 | 43 50 44 42 39 42 45 41 40 46 42
4 | 7 12 7 16 12 5 10 10 6 24 3 | 18 24 24 25 24 23 26 22 21 30 21
5 | 12 16 6 10 12 4 18 11 13 23 4 | 15 19 15 18 14 17 20 22 20 22 15
6 | 8 12 6 12 16 5 15 9 10 16 3 | 19 22 18 22 24 16 21 20 22 19 19
7 | 10 16 6 11 16 5 13 9 9 16 4 | 15 26 19 16 26 14 22 17 18 14 17
8 | 8 11 9 9 15 5 11 5 8 21 3 | 16 19 20 20 19 16 19 17 19 25 17
9 | 7 10 5 11 13 3 11 8 6 13 3 | 19 21 18 24 20 19 20 21 20 19 19
10 | 7 10 3 11 12 4 9 8 7 17 3 | 19 23 24 25 28 23 26 23 24 22 21
11 | 8 14 8 10 11 6 13 13 6 14 3 | 26 36 30 24 33 27 36 32 29 30 30
12 | 10 23 12 16 20 6 23 9 9 17 5 | 19 26 18 22 29 14 27 16 12 18 16
13E | 10 12 6 9 14 4 12 19 12 19 4 | 39 41 41 38 44 37 44 39 39 42 40
14E | 6 10 8 10 19 4 13 9 10 11 3 | 22 27 26 22 29 21 28 23 24 26 24
15E | 7 19 8 8 20 5 22 10 9 14 4 | 14 23 18 22 20 18 24 19 19 20 16
16 | 9 16 5 15 18 6 15 10 11 22 4 | 15 22 19 15 26 15 23 16 21 18 18
17 | 9 12 7 15 17 4 15 7 8 13 3 | 24 26 23 20 32 18 28 20 18 21 22
18 | 7 16 9 10 15 5 17 6 9 26 4 | 13 24 20 16 23 14 24 14 16 18 14
19 | 9 12 7 12 16 4 16 10 6 25 4 | 29 30 25 22 32 23 31 27 25 28 26
20 | 6 12 8 18 11 6 12 10 9 21 4 | 14 21 17 20 14 14 23 16 15 14 16
21 | 7 13 8 11 13 6 14 9 9 28 4 | 24 33 31 23 31 27 35 22 28 28 27
22 | 7 13 9 9 15 4 17 6 10 15 3 | 14 23 19 14 22 13 22 14 17 14 16
23E | 7 14 6 11 17 6 12 13 10 15 4 | 26 27 26 24 22 25 29 23 27 22 25
25 | 6 19 11 9 20 6 13 14 9 13 4 | 13 19 20 16 33 15 23 17 14 16 16
26E | 28 27 13 14 20 11 26 28 45 24 9 | 75 77 72 73 72 71 74 71 90 71 71
27 | 7 12 6 10 15 3 12 9 6 12 3 | 18 21 18 22 20 18 17 21 20 18 18
28 | 10 11 11 13 22 5 17 7 8 15 4 | 14 21 22 19 33 14 23 14 16 16 17
29 | 12 19 6 13 16 4 18 15 12 16 4 | 21 31 23 25 31 22 33 22 22 23 23
30 | 7 10 6 15 14 6 12 7 15 15 3 | 20 24 23 22 22 19 27 19 25 20 22
31 | 8 13 6 10 20 3 12 8 8 18 3 | 23 28 21 22 33 21 26 22 21 22 22
32 | 9 14 6 11 12 4 9 6 7 13 3 | 15 23 18 18 19 17 23 19 20 19 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 8 13 16 5 15 11 12 19 |T 22 28 24 24 28 22 28 23 24 24 23
WRMS | 9 15 8 12 14 5 14 9 8 18 |NE 18 25 21 21 25 18 25 20 20 21 20
MEDI | 8 13 7 11 15 5 14 9 9 16 |MD 19 24 21 22 26 18 26 21 21 22 20
Table 3.1695.2 GPS week: 1695 Day: 2 MJD: 56111.000
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 12 4 11 12 6 14 9 16 11 3 | 34 46 42 40 51 43 53 41 50 40 43
2 | 7 12 6 21 10 3 9 9 9 32 4 | 17 22 20 33 16 18 19 22 24 24 18
3 | 11 14 6 12 20 4 10 7 14 21 4 | 42 47 42 45 36 40 46 44 50 55 44
4 | 8 9 5 17 10 2 7 8 11 24 3 | 19 27 25 29 28 22 26 25 25 32 24
5 | 9 16 7 16 12 6 16 10 9 23 4 | 20 25 17 27 17 21 24 25 24 26 19
6 | 9 14 5 13 10 4 10 7 12 17 3 | 18 20 16 24 16 15 17 20 16 18 16
7 | 11 15 6 10 14 5 12 9 12 16 4 | 18 27 20 19 26 19 25 17 16 15 18
8 | 9 11 7 9 17 4 8 7 12 22 3 | 15 22 21 25 20 19 22 21 19 28 18
9 | 8 11 4 8 13 4 9 9 8 14 3 | 18 23 18 23 19 19 22 22 22 21 18
10 | 6 10 5 10 13 2 9 10 10 16 3 | 18 25 24 24 28 22 27 26 24 25 22
11 | 8 13 6 11 13 4 9 17 13 19 4 | 27 34 27 28 36 27 32 31 35 30 29
12 | 10 22 7 15 18 5 21 9 12 16 5 | 19 30 16 21 24 13 28 15 17 16 15
13E | 7 10 7 11 13 5 9 19 9 18 4 | 26 26 25 29 32 24 28 27 28 30 26
14E | 6 11 7 9 15 4 9 7 8 13 3 | 19 25 20 19 26 19 22 18 21 23 20
15E | 8 20 8 12 12 4 21 15 8 14 4 | 21 29 23 23 20 21 29 25 25 20 21
16 | 8 18 7 18 16 7 14 11 11 20 4 | 11 22 14 19 21 13 18 13 16 15 13
17 | 8 14 6 8 17 3 17 9 10 12 3 | 21 27 21 21 35 20 29 20 21 22 21
18 | 7 18 7 9 11 4 14 8 6 22 3 | 14 27 14 18 20 16 24 16 14 18 14
19 | 6 12 6 10 21 4 13 16 13 25 4 | 26 27 25 23 32 23 28 26 22 26 23
20 | 9 12 6 13 8 4 10 9 10 21 3 | 17 20 16 18 18 15 21 16 19 15 17
21 | 6 13 6 11 11 3 12 11 10 30 4 | 22 31 28 22 31 25 31 23 31 27 25
22 | 6 13 6 9 12 4 13 7 10 14 3 | 15 23 16 18 21 16 22 16 18 14 16
23E | 8 13 6 13 15 3 10 10 10 12 3 | 22 25 24 30 21 24 23 19 29 19 22
25 | 7 20 5 9 19 5 13 14 10 10 4 | 15 17 18 16 30 16 24 18 17 18 15
26E | 28 29 14 17 24 11 22 33 55 26 10 | 70 76 69 71 73 68 74 68 91 63 68
27 | 8 18 5 8 14 4 9 11 9 15 3 | 18 26 19 22 18 20 22 24 23 22 18
28 | 9 13 5 11 17 2 10 8 9 15 3 | 11 22 16 18 28 11 20 13 15 16 14
29 | 12 19 9 14 15 5 22 13 7 15 5 | 18 30 19 27 29 21 32 23 18 24 21
30 | 8 13 6 14 11 5 10 7 6 14 3 | 20 26 21 27 21 20 21 21 21 20 21
31 | 12 15 6 9 16 4 13 8 9 16 4 | 23 25 21 22 30 20 24 20 22 22 20
32 | 6 17 5 8 9 3 8 7 9 11 3 | 17 21 17 22 19 18 22 20 21 18 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 7 12 15 5 13 12 14 19 |T 21 28 23 25 27 22 27 23 25 24 22
WRMS | 9 15 6 11 13 4 12 10 8 19 |NE 18 25 20 23 25 19 25 21 22 22 19
MEDI | 8 13 6 11 13 4 10 9 10 16 |MD 19 26 20 23 26 20 24 21 22 22 20
Table 3.1695.3 GPS week: 1695 Day: 3 MJD: 56112.000
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 15 5 14 8 3 16 7 8 10 3 | 41 54 46 47 53 46 57 46 41 46 47
2 | 7 14 4 22 15 3 11 7 11 32 4 | 19 21 19 34 22 18 21 22 21 25 19
3 | 15 14 5 11 16 7 15 7 9 15 4 | 59 65 61 59 60 60 68 59 57 64 61
4 | 9 10 7 11 14 4 8 7 9 26 3 | 26 28 31 29 24 25 28 30 31 34 29
5 | 13 17 8 12 11 5 18 10 15 24 4 | 22 23 16 21 20 18 22 25 28 26 18
6 | 9 13 5 9 12 4 13 9 7 17 3 | 22 21 22 22 23 18 18 24 22 21 21
7 | 8 15 6 8 15 4 13 7 6 14 3 | 16 30 20 19 28 16 26 21 17 18 19
8 | 10 14 5 6 16 4 10 9 8 21 3 | 23 25 21 22 21 20 23 25 24 30 21
9 | 9 20 6 7 11 4 10 9 9 13 3 | 26 25 24 21 25 21 21 22 18 19 22
10 | 7 9 6 11 11 2 9 11 9 18 3 | 28 31 32 29 33 29 32 33 29 30 30
11 | 8 14 7 11 12 3 13 13 16 12 4 | 27 35 26 32 35 27 35 29 29 29 29
12 | 11 23 8 15 22 3 24 8 11 15 5 | 24 30 19 20 26 17 28 20 16 16 17
13E | 7 8 7 10 13 4 10 10 10 13 3 | 35 34 38 34 38 34 37 33 34 36 35
14E | 11 12 6 11 30 4 11 11 11 16 4 | 21 27 25 24 37 21 27 23 22 31 23
15E | 10 20 9 14 23 5 24 8 12 11 5 | 23 28 25 29 30 25 28 26 28 24 24
16 | 8 17 8 16 17 5 17 10 6 20 4 | 12 20 16 17 24 13 18 17 14 16 14
17 | 10 15 5 7 15 4 15 8 9 13 3 | 27 28 23 25 33 25 33 27 27 26 27
18 | 8 17 6 10 13 6 16 8 11 23 4 | 15 24 15 19 22 14 23 17 18 18 14
19 | 9 14 4 10 17 3 14 9 10 19 4 | 32 36 34 27 36 29 35 33 35 33 32
20 | 8 12 5 11 10 4 13 7 10 22 3 | 18 24 22 22 22 20 25 20 20 18 22
21 | 8 14 5 12 14 7 13 9 8 30 4 | 24 32 27 25 30 25 32 26 26 27 26
22 | 10 14 6 8 13 5 14 7 12 16 3 | 15 23 15 19 24 14 20 16 17 14 16
23E | 6 10 6 13 17 4 11 11 10 12 3 | 23 26 25 29 26 25 27 26 27 24 25
25 | 9 19 7 7 21 3 13 13 8 10 4 | 18 17 19 12 31 13 23 16 13 14 15
26E | 29 34 14 13 24 15 28 24 64 19 10 | 134 127 130 131 132 136 127 127 160 129 130
27 | 8 24 6 7 14 5 10 10 9 14 3 | 24 29 22 21 25 21 20 23 19 21 21
28 | 7 13 8 12 21 3 11 9 11 17 4 | 19 23 18 25 31 15 21 19 20 22 19
29 | 14 20 7 11 16 4 23 9 11 16 4 | 27 37 31 30 37 30 40 30 28 32 31
30 | 12 12 4 11 11 4 12 8 8 13 3 | 22 25 24 29 26 23 25 21 19 19 24
31 | 11 13 5 10 19 4 14 7 10 15 3 | 25 28 23 26 33 21 27 23 25 22 24
32 | 14 15 5 9 9 3 8 5 8 12 3 | 18 26 27 29 26 23 27 24 26 20 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 7 11 16 5 15 10 15 18 |T 27 32 28 29 33 27 32 29 29 29 28
WRMS | 10 16 6 11 14 4 14 9 9 19 |NE 22 27 23 24 28 21 27 24 23 23 23
MEDI | 9 14 6 11 15 4 13 9 10 16 |MD 23 28 24 25 28 21 27 24 25 24 24
Table 3.1695.4 GPS week: 1695 Day: 4 MJD: 56113.000
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 15 8 17 13 5 17 7 12 11 4 | 33 48 39 42 42 37 54 37 36 37 38
2 | 6 14 5 25 13 4 11 9 8 32 4 | 27 27 25 34 29 25 28 30 26 29 24
3E | 10 12 7 13 13 4 13 7 11 22 4 | 54 54 50 54 55 50 53 53 51 52 52
4 | 8 9 6 15 15 4 8 11 9 25 3 | 28 32 29 27 37 29 33 30 29 35 27
5 | 9 17 8 14 15 5 15 10 8 26 4 | 27 32 26 25 31 28 29 29 28 32 25
6 | 9 12 7 14 12 4 11 10 9 17 3 | 31 28 27 31 31 28 28 31 29 28 27
X7 | 5 --- --- --- --- 166 --- --- --- --- 0 | 28 --- --- --- --- 338 --- --- --- --- 30
8 | 7 12 7 6 17 4 12 11 10 22 4 | 27 31 32 24 28 29 31 32 31 36 27
9 | 9 10 7 9 15 2 10 13 11 15 3 | 23 25 25 22 23 26 26 27 26 29 22
10 | 5 9 5 13 13 3 7 10 14 20 3 | 30 34 33 36 40 33 36 36 40 35 33
11 | 8 12 7 16 14 4 13 11 14 13 4 | 22 32 24 29 32 25 36 23 32 25 24
12 | 9 25 7 16 23 4 21 10 9 14 5 | 24 34 26 24 29 24 29 23 28 21 22
13E | 7 10 6 13 20 6 11 6 14 14 3 | 27 33 31 32 39 30 32 30 37 30 29
14E | 7 11 7 14 13 3 12 13 12 15 3 | 28 35 32 27 34 28 35 31 29 34 29
15E | 7 24 7 13 24 5 22 14 9 11 5 | 27 34 25 25 33 29 33 30 32 29 25
16 | 7 17 6 19 15 5 15 9 12 21 4 | 21 26 22 25 30 22 25 24 23 25 21
17 | 12 13 6 9 21 5 16 13 11 16 4 | 26 31 30 27 38 27 35 31 30 31 27
18 | 7 18 7 9 14 5 13 9 9 25 4 | 22 29 26 19 29 23 28 23 25 25 21
19 | 7 13 6 15 17 3 11 9 10 14 3 | 41 40 37 30 40 37 41 39 35 37 36
20 | 8 12 6 15 13 5 13 7 9 20 3 | 22 28 23 24 25 22 30 23 20 26 22
21 | 5 14 5 17 13 3 12 8 9 28 4 | 24 33 30 26 34 28 35 28 30 31 26
22 | 5 15 7 8 14 4 13 9 9 19 3 | 23 28 25 22 27 23 27 23 23 24 21
23E | 6 10 6 14 15 5 12 9 10 14 3 | 28 29 27 32 31 26 29 29 31 27 27
25 | 7 20 7 9 23 4 13 11 13 13 4 | 24 25 25 16 34 24 30 26 28 22 22
26E | 16 24 10 11 27 11 28 21 33 18 7 | 144 148 144 142 141 146 149 146 156 147 143
27 | 7 11 8 7 17 4 9 13 9 17 3 | 23 23 26 20 23 25 24 28 26 30 22
28 | 10 12 7 11 18 4 11 14 13 21 4 | 23 29 28 24 35 24 28 27 24 30 23
29 | 14 23 6 18 18 4 18 7 15 16 5 | 23 35 25 29 35 27 36 28 29 31 26
30 | 6 11 7 14 14 4 11 17 9 18 4 | 48 47 45 46 47 46 50 52 48 53 47
31 | 8 12 5 12 18 4 13 9 12 17 3 | 29 32 26 27 34 26 32 26 29 26 26
32 | 7 13 4 14 10 3 10 5 11 15 3 | 25 30 26 31 31 25 31 28 26 28 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 15 7 14 17 5 14 11 12 19 |T 31 36 32 32 37 42 37 34 34 34 31
WRMS | 8 15 7 14 17 4 13 9 10 19 |NE 26 31 28 27 32 40 32 29 29 30 26
MEDI | 7 12 7 14 15 4 12 10 10 17 |MD 27 32 26 27 33 27 31 29 29 30 26
Table 3.1695.5 GPS week: 1695 Day: 5 MJD: 56114.000
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 | 8 16 8 14 6 4 17 7 8 13 3 | 28 44 29 30 41 30 49 32 36 29 32
2 | 7 15 4 20 12 4 13 14 11 32 4 | 20 22 20 38 19 20 24 26 25 31 20
3E | 23 14 7 13 16 7 19 13 14 19 5 | 54 58 54 47 59 52 61 49 47 55 51
4 | 8 10 3 12 14 4 11 17 11 26 4 | 20 29 23 29 26 24 27 29 23 33 22
5 | 11 20 6 11 12 6 19 15 10 31 5 | 20 25 18 26 24 21 26 34 27 39 21
6 | 11 12 6 12 16 6 15 18 10 15 4 | 18 17 19 24 16 17 19 26 19 23 17
X7 | 10 16 --- 12 --- 15 --- 8 11 --- 5 | 13 20 --- 13 --- 47 --- 10 13 --- 13
8 | 7 12 6 10 16 5 11 11 9 22 3 | 21 27 22 21 21 22 25 29 20 34 20
9 | 8 10 5 9 13 4 9 11 9 15 3 | 17 21 17 20 19 19 19 25 22 25 17
10 | 11 10 6 12 12 5 10 11 12 23 4 | 27 31 29 33 32 27 31 34 32 34 28
11 | 7 13 7 12 11 4 12 8 16 10 3 | 18 28 17 22 31 17 29 20 27 17 19
12 | 10 21 7 17 21 5 20 11 8 15 5 | 20 28 17 25 26 18 26 22 18 21 17
13E | 5 11 7 10 11 6 10 9 8 12 3 | 28 34 31 28 34 28 33 30 28 34 29
14E | 10 13 7 8 20 5 11 18 15 19 4 | 18 22 21 19 23 18 23 24 25 31 19
15E | 11 19 8 15 14 6 22 15 15 18 5 | 11 25 18 21 20 17 23 28 21 30 16
16 | 7 20 10 19 17 6 15 13 12 20 5 | 13 23 18 15 24 15 21 17 17 20 14
17 | 11 15 6 9 17 5 19 13 10 12 4 | 27 35 32 29 35 30 38 31 31 33 29
18 | 9 15 7 11 17 5 16 10 8 25 4 | 15 28 19 22 24 20 28 22 20 28 17
19 | 16 13 7 11 17 5 13 9 9 16 4 | 28 28 27 22 27 23 30 27 25 24 24
20 | 6 13 8 15 11 5 12 10 11 23 4 | 16 23 21 20 16 16 22 18 20 17 16
21 | 7 13 7 13 15 7 13 9 8 31 4 | 22 34 29 24 36 27 35 27 26 29 26
22 | 7 15 6 7 14 4 14 11 7 21 3 | 19 28 19 21 25 20 26 26 22 30 19
23E | 7 12 8 15 13 4 12 13 6 16 3 | 20 26 23 22 28 22 24 26 20 25 20
25 | 11 20 5 9 20 4 15 11 9 12 4 | 16 21 19 19 30 18 27 23 21 20 17
26E | 18 18 8 12 17 7 17 20 27 18 6 | 82 92 87 91 91 87 92 87 99 87 88
27 | 7 10 7 9 16 4 11 13 10 19 3 | 19 22 18 21 21 21 22 30 25 31 19
28 | 7 12 7 11 22 5 11 12 11 19 4 | 20 28 23 22 33 20 28 24 20 26 20
29 | 11 21 8 14 13 2 20 11 10 16 4 | 20 30 23 26 28 21 32 26 22 28 22
30 | 8 11 6 12 12 4 13 12 8 13 3 | 36 35 33 38 34 34 40 39 37 37 35
31 | 8 11 8 10 18 4 11 9 10 18 3 | 25 29 26 23 31 23 27 23 24 28 23
32 | 9 14 6 12 12 4 8 10 8 12 3 | 16 23 21 21 23 20 21 21 20 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 7 13 15 5 14 13 11 20 |T 23 30 25 26 29 25 30 28 26 30 24
WRMS | 9 15 7 13 14 5 14 11 8 18 |NE 20 27 22 24 26 22 28 25 23 27 21
MEDI | 8 13 7 12 14 5 13 11 10 18 |MD 20 28 21 22 26 21 27 26 23 29 20
Table 3.1695.6 GPS week: 1695 Day: 6 MJD: 56115.000
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 | 9 15 10 12 9 5 16 10 9 11 4 | 41 57 48 50 58 48 63 48 51 45 49
2 | 9 13 4 18 11 6 14 16 8 33 4 | 23 25 23 35 27 23 25 28 23 31 23
3E | 16 13 10 14 15 6 18 17 17 27 5 | 80 79 78 82 82 78 78 78 83 87 80
4 | 10 9 5 9 10 3 11 18 11 27 4 | 21 26 30 30 30 27 26 33 27 34 26
5 | 12 15 7 11 11 5 20 16 7 37 5 | 26 30 24 29 28 24 26 30 28 37 24
6 | 11 17 7 11 19 5 16 17 11 17 4 | 30 31 32 34 31 29 32 33 32 29 30
7 | 11 16 6 11 12 5 13 11 9 19 4 | 9 22 6 13 5 32 14 11 16 6 15
8 | 8 10 6 9 12 5 9 12 10 23 3 | 20 23 21 24 23 20 23 25 23 31 21
9 | 8 13 6 9 16 6 12 16 7 15 3 | 22 20 22 26 21 23 23 27 23 25 21
10 | 8 9 5 10 12 3 9 14 9 21 3 | 38 41 40 44 47 40 43 45 43 38 41
11 | 6 15 5 11 12 6 12 10 9 10 3 | 22 36 26 31 39 26 35 23 30 21 27
12 | 9 19 7 17 15 5 18 12 7 18 4 | 26 25 21 27 26 20 26 20 19 20 21
13E | 6 15 4 12 13 4 10 14 5 18 3 | 38 43 42 39 48 39 43 37 40 36 40
14E | 7 11 5 8 11 4 13 22 8 18 4 | 30 36 33 31 36 30 35 33 35 41 32
15E | 8 20 8 14 12 4 18 14 11 22 4 | 23 31 25 30 31 24 32 30 26 33 25
16 | 7 19 6 17 13 6 15 13 10 21 4 | 17 26 22 24 28 22 24 23 23 22 21
17 | 12 15 6 6 20 4 19 14 9 13 4 | 33 39 34 30 47 33 43 33 31 35 34
18 | 6 15 6 11 10 4 16 11 9 27 4 | 17 29 24 20 29 19 28 19 20 24 19
19 | 6 14 6 10 16 5 13 10 9 20 3 | 40 41 41 36 43 39 44 42 39 37 39
20 | 8 13 6 17 10 6 13 11 7 23 4 | 18 25 22 26 24 20 25 18 21 19 20
21 | 7 13 5 12 8 5 16 11 8 32 4 | 29 39 34 32 40 32 40 34 31 33 33
22 | 5 13 7 9 11 4 15 11 7 22 3 | 23 32 27 27 35 25 29 24 26 28 25
23E | 7 14 6 16 14 3 13 20 6 21 4 | 27 29 29 35 31 28 29 31 28 29 28
25 | 6 20 6 8 19 4 13 16 10 17 4 | 19 21 22 16 31 17 28 20 21 17 19
26E | 15 20 12 11 14 6 17 16 29 17 6 | 97 109 101 104 107 105 108 107 115 110 104
27 | 9 11 5 9 15 5 12 17 6 22 3 | 22 17 20 24 20 21 19 30 21 33 20
28 | 9 13 4 7 17 5 12 10 10 20 3 | 18 27 24 23 34 20 27 21 21 23 22
29 | 10 23 6 11 15 5 23 13 11 16 4 | 31 41 34 37 44 36 46 37 36 39 36
30 | 9 12 5 10 10 6 14 13 8 13 3 | 36 42 41 45 41 42 44 37 43 32 41
31 | 6 15 7 9 14 4 15 11 8 19 3 | 28 33 32 31 36 28 34 26 31 25 29
32 | 6 15 7 12 12 4 9 11 7 12 3 | 22 34 30 35 37 28 34 28 27 29 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 7 12 14 5 15 14 10 21 |T 29 35 32 34 37 32 36 33 33 33 32
WRMS | 9 15 6 12 12 5 14 13 7 20 |NE 25 31 28 29 32 27 32 28 28 28 27
MEDI | 8 15 6 11 12 5 14 13 9 20 |MD 26 31 29 31 34 28 32 30 28 31 27
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 4.1695 GPS week: 1695 MJD: 56109.0-56115.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 |U 7 7 18 |U 5 8 21 |U 17 22 35 |
emr | emr 2537 | 8 7 21 |U 9 11 26 | 15 21 34 |
esa | esa 2934 | 7 7 19 |U 6 8 24 | 19 18 36 |
gfz | gfz 2956 |U 7 7 20 |U 6 9 24 |U 18 22 39 |
grg | grg 2948 |U 18 18 44 |U 16 25 72 | 25 29 48 |
igr | igr 2957 | 7 7 19 | 5 7 21 | 17 21 34 |
igs | igs 2956 | 7 7 19 | 5 7 21 | 18 21 35 |
jpl | jpl 2943 | 9 9 23 |U 9 16 33 | 20 24 36 |
mit | mit 2962 | 7 7 20 |U 9 21 38 |U 21 25 36 |
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 5.1695.0 GPS week: 1695 Day: 0 MJD: 56109.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 8 14 | 4 6 21 | 12 16 21 |
emr | emr 31 | 0 0 0 | 0 0 0 | 0 0 0 |
esa | esa 2880 | 7 8 15 | 4 7 20 | 14 18 26 |
gfz | gfz 2971 | 6 7 16 | 6 18 28 | 16 18 24 |
grg | grg 2976 | 33 34 76 | 28 42 110 | 17 37 54 |
igr | igr 2945 | 7 8 16 | 4 6 17 | 13 15 23 |
igs | igs 2954 | 6 7 15 | 4 6 17 | 16 16 26 |
jpl | jpl 2972 | 8 7 20 | 8 22 34 | 13 15 22 |
mit | mit 2976 | 7 7 15 | 12 32 51 | 15 26 27 |
Table 5.1695.1 GPS week: 1695 Day: 1 MJD: 56110.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 6 11 | 4 8 23 | 11 20 20 |
emr | emr 2972 | 9 7 19 | 8 10 24 | 13 20 28 |
esa | esa 2976 | 5 6 13 | 5 7 21 | 10 16 20 |
gfz | gfz 2973 | 5 5 13 | 4 5 21 | 12 20 22 |
grg | grg 2976 | 22 32 54 | 20 35 90 | 24 23 43 |
igr | igr 2974 | 5 6 13 | 4 7 19 | 11 17 22 |
igs | igs 2965 | 4 6 11 | 4 6 20 | 10 18 20 |
jpl | jpl 2972 | 8 8 18 | 7 19 31 | 10 18 23 |
mit | mit 2976 | 4 7 14 | 7 20 30 | 13 16 22 |
Table 5.1695.2 GPS week: 1695 Day: 2 MJD: 56111.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 4 13 | 7 8 29 | 30 58 102 |
emr | emr 2972 | 9 7 20 | 18 12 58 | 34 60 86 |
esa | esa 2976 | 4 4 13 | 9 8 39 | 38 36 93 |
gfz | gfz 2973 | 4 4 13 | 7 7 36 | 31 58 107 |
grg | grg 2975 | 15 13 34 | 21 20 92 | 49 57 82 |
igr | igr 2976 | 4 4 13 | 7 8 31 | 31 53 92 |
igs | igs 2976 | 4 4 13 | 7 7 32 | 32 52 91 |
jpl | jpl 2972 | 8 11 22 | 18 11 62 | 35 59 87 |
mit | mit 2976 | 4 4 14 | 18 14 64 | 41 55 72 |
Table 5.1695.3 GPS week: 1695 Day: 3 MJD: 56112.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 8 21 | 4 7 16 | 27 15 28 |
emr | emr 2972 | 12 9 24 | 7 6 21 | 24 27 39 |
esa | esa 2976 | 9 8 24 | 4 6 21 | 21 18 29 |
gfz | gfz 2970 | 9 8 24 | 5 5 17 | 22 21 33 |
grg | grg 2976 | 16 16 46 | 10 17 45 | 30 23 36 |
igr | igr 2976 | 9 8 23 | 3 5 16 | 24 20 29 |
igs | igs 2976 | 8 8 23 | 3 5 19 | 25 17 26 |
jpl | jpl 2972 | 8 9 26 | 4 8 20 | 28 30 36 |
mit | mit 2976 | 8 8 22 | 6 16 31 | 31 24 30 |
Table 5.1695.4 GPS week: 1695 Day: 4 MJD: 56113.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 10 11 28 | 6 9 18 | 15 13 28 |
emr | emr 2876 | 13 14 30 | 9 10 20 | 14 12 24 |
esa | esa 2880 | 10 10 28 | 6 7 21 | 14 12 26 |
gfz | gfz 2872 | 9 11 28 | 5 9 19 | 14 11 26 |
grg | grg 2880 | 17 13 33 | 10 17 40 | 21 23 41 |
igr | igr 2880 | 10 11 29 | 5 7 19 | 13 11 24 |
igs | igs 2876 | 9 11 29 | 5 7 16 | 15 12 27 |
jpl | jpl 2876 | 11 12 31 | 6 15 26 | 12 10 22 |
mit | mit 2880 | 10 11 31 | 8 21 31 | 19 18 34 |
Table 5.1695.5 GPS week: 1695 Day: 5 MJD: 56114.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 5 22 | 6 8 16 | 16 25 31 |
emr | emr 2968 | 9 8 26 | 10 16 28 | 17 22 43 |
esa | esa 2880 | 7 6 23 | 6 10 20 | 27 22 41 |
gfz | gfz 2967 | 7 5 23 | 7 11 20 | 28 22 42 |
grg | grg 2880 | 12 8 32 | 8 23 38 | 27 25 58 |
igr | igr 2976 | 7 5 23 | 6 9 19 | 18 25 34 |
igs | igs 2975 | 7 5 24 | 6 8 19 | 19 25 38 |
jpl | jpl 2872 | 9 6 24 | 8 19 31 | 33 27 44 |
mit | mit 2976 | 8 5 25 | 7 22 25 | 19 27 44 |
Table 5.1695.6 GPS week: 1695 Day: 6 MJD: 56115.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 8 19 | 8 9 24 | 6 7 18 |
emr | emr 2968 | 9 9 25 | 13 22 29 | 6 5 21 |
esa | esa 2976 | 7 8 19 | 8 9 26 | 6 6 18 |
gfz | gfz 2967 | 7 8 21 | 7 10 25 | 6 6 18 |
grg | grg 2976 | 13 10 30 | 13 23 89 | 8 12 19 |
igr | igr 2976 | 7 8 19 | 7 8 24 | 6 7 18 |
igs | igs 2975 | 7 8 20 | 7 8 25 | 6 6 18 |
jpl | jpl 2968 | 8 8 23 | 9 21 31 | 6 8 21 |
mit | mit 2976 | 7 9 21 | 9 21 33 | 9 6 21 |
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 : 10-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 6.1695 GPS week: 1695 MJD: 56109.500-56115.500
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 -57 14 -77 -2 | 3 22
| 23 17 119 99 4 | 3
emr uuuuu | 52 43 -187 110 8 | 17 29
| 14 13 43 64 7 | 4
esa uuuuu | -18 -20 17 58 -2 | 10 24
| 5 13 52 23 4 | 2
gfz uuuuu | -22 -3 -71 -66 -4 | 3 22
| 11 27 84 86 6 | 2
grg uuuux | 26 -30 72 -247 -5 | -5 27
| 14 15 77 90 21 | 7
igr xxxxx | -5 24 27 -28 6 | -6 23
| 16 11 56 60 6 | 3
irf xxxxx | -1 -9 -32 -36 0 | 4 22
| 7 6 27 24 2 | 2
jpl uuuuu | 59 -16 -13 21 -4 | 20 29
| 11 26 84 97 8 | 2
mit xxxxu | 146 92 -152 -31 0 | 19 29
| 16 12 37 65 5 | 3
ngs uuuuu | -46 21 6 -33 3 | 10 21
| 19 40 102 147 5 | 3
sio uuuuu | 10 56 247 61 1 | 37 42
| 10 19 59 67 4 | 3
Table 7.1695.0 GPS week: 1695 Day: 0 MJD: 56109.500
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 | 33 -69 -142 -205 3 | 4 24
emr uuuuu | 38 34 -220 56 2 | 16 29
esa uuuuu | -9 -31 37 22 -5 | 12 25
gfz uuuuu | -40 26 -171 -219 5 | 5 25
grg uuuux | 1 -26 15 -309 25 | -18 42
igr xxxxx | 22 10 22 -134 5 | -7 24
irf xxxxx | -2 -13 -45 -29 3 | 4 23
jpl uuuuu | 79 17 -36 40 5 | 22 31
mit xxxxu | 149 83 -139 46 -2 | 20 30
ngs uuuuu | -40 2 161 213 -5 | 11 22
sio uuuuu | 11 55 159 88 6 | 36 42
Table 7.1695.1 GPS week: 1695 Day: 1 MJD: 56110.500
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 | 28 -26 -67 -95 4 | 3 24
emr uuuuu | 50 24 -131 103 9 | 15 28
esa uuuuu | -16 -44 67 64 0 | 10 25
gfz uuuuu | -8 19 -201 -76 0 | 4 25
grg uuuux | 28 -18 -13 -315 -9 | -11 35
igr xxxxx | 10 32 -63 -32 11 | -8 24
irf xxxxx | 2 -6 -44 -71 0 | 3 23
jpl uuuuu | 57 -17 -80 -78 -2 | 21 30
mit xxxxu | 152 90 -162 -42 -4 | 19 30
ngs uuuuu | -58 23 84 113 -3 | 9 21
sio uuuuu | 12 82 242 -50 4 | 36 42
Table 7.1695.2 GPS week: 1695 Day: 2 MJD: 56111.500
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 | -1 -71 -80 -28 -7 | 4 25
emr uuuuu | 45 60 -176 191 13 | 16 29
esa uuuuu | -20 -8 66 78 -3 | 10 25
gfz uuuuu | -26 -27 13 -119 -11 | 5 25
grg uuuux | 40 -35 0 -231 -3 | -4 23
igr xxxxx | -4 43 3 17 3 | -6 24
irf xxxxx | -9 -1 -41 -18 -4 | 4 23
jpl uuuuu | 60 -30 -97 28 0 | 21 30
mit xxxxu | 130 99 -146 38 -8 | 20 30
ngs uuuuu | -49 11 -32 -103 7 | 8 21
sio uuuuu | -2 78 209 29 -3 | 37 43
Table 7.1695.3 GPS week: 1695 Day: 3 MJD: 56112.500
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 | 59 -61 180 -153 -5 | 1 21
emr uuuuu | 51 38 -186 123 6 | 15 27
esa uuuuu | -16 -13 52 40 -5 | 8 22
gfz uuuuu | -18 -35 -8 43 -11 | 1 20
grg uuuux | 34 -32 67 -258 -15 | 1 21
igr xxxxx | -10 22 -8 -56 -6 | -7 22
irf xxxxx | -7 -17 3 -58 0 | 2 20
jpl uuuuu | 48 -35 -72 25 -2 | 19 27
mit xxxxu | 126 79 -89 -41 3 | 17 26
ngs uuuuu | -38 69 -134 -91 9 | 8 19
sio uuuuu | -1 34 320 25 4 | 35 40
Table 7.1695.4 GPS week: 1695 Day: 4 MJD: 56113.500
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 -69 94 55 -3 | 0 21
emr uuuuu | 80 43 -137 196 13 | 14 27
esa uuuuu | -16 -21 -14 47 -3 | 7 22
gfz uuuuu | -12 -13 -26 -24 -2 | 0 21
grg uuuux | 18 -54 168 -342 -29 | -1 22
igr xxxxx | -13 19 67 -41 6 | -8 23
irf xxxxx | 10 -14 8 -22 2 | 1 20
jpl uuuuu | 47 -53 12 -105 -19 | 17 26
mit xxxxu | 173 88 -134 4 7 | 16 26
ngs uuuuu | -82 80 -89 -20 4 | 7 19
sio uuuuu | 28 39 319 136 -1 | 34 40
Table 7.1695.5 GPS week: 1695 Day: 5 MJD: 56114.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 43 -59 -3 -145 -5 | 3 19
emr uuuuu | 52 42 -209 73 17 | 18 27
esa uuuuu | -25 -14 -71 89 -5 | 9 21
gfz uuuuu | -27 27 -78 1 -6 | 2 19
grg uuuux | 19 -38 176 -189 -24 | -4 24
igr xxxxx | -19 28 62 50 10 | -5 20
irf xxxxx | -5 -3 -64 -45 -2 | 4 18
jpl uuuuu | 58 14 137 40 2 | 18 25
mit xxxxu | 139 116 -202 -129 1 | 19 26
ngs uuuuu | -28 -33 48 -158 1 | 10 18
sio uuuuu | 16 58 216 64 -3 | 37 41
Table 7.1695.6 GPS week: 1695 Day: 6 MJD: 56115.500
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 | 0 -43 115 29 1 | 8 23
emr uuuuu | 44 57 -247 29 -5 | 26 37
esa uuuuu | -24 -9 -13 66 6 | 14 25
gfz uuuuu | -27 -21 -21 -66 -4 | 6 22
grg uuuux | 42 -10 91 -82 22 | -1 24
igr xxxxx | -22 14 105 3 10 | 1 24
irf xxxxx | 2 -12 -42 -6 0 | 9 23
jpl uuuuu | 61 -9 49 194 -11 | 23 32
mit xxxxu | 151 89 -187 -90 6 | 24 33
ngs uuuuu | -28 -5 6 -187 5 | 15 25
sio uuuuu | 8 46 266 135 -3 | 42 47
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