[IGSREPORT-20821] Wk 1685 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu May 10 07:18:31 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1685 (Apr 22, 2012 - Apr 28, 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:
igs1685[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1685[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1685[0-6].cls IGS GPS clock combination summary report.
igs16857.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16857.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 | FLRS SCH2
0 | EMR | 30 30
0 | ESA | NNOR
0 | GFZ | BRFT DAV1 OHI2 STHL
0 | GRG | ADIS
0 | JPL | 30
0 | MIT | 14 14 CAS1
1 | COD | 4 POTS
1 | EMR | 10 4 10
1 | ESA | HYDE MATE UNSA
1 | GFZ | BRFT CHAN
1 | JPL | 8 10
1 | MIT | 10 10 CAS1 DAV1 MAW1 CAS1 DAV1 HYDE MAW1
2 | EMR | 10 10 SCH2 SPT0 SFER SPT0
2 | ESA | AREQ COCO INVK NNOR PALM SFER THTI
2 | GFZ | ARTU BRFT RIO2 SCH2
2 | JPL | 10 ARTU
2 | MIT | 10 10 MAW1 CAS1 MAW1
3 | COD | MAW1 ONSA ONSA
3 | EMR | 10 30 MCM4
3 | ESA | SFER MAW1 NNOR SFER UNSA
3 | GFZ | 30 CRO1 KARR ONSA PIMO SCUB SUTM
3 | GRG | HYDE KIT3
3 | JPL | 10
3 | MIT | 22 30 10 21 22 30 DAV1 CAS1 DAV1 DRAG
4 | COD | XMIS
4 | EMR | 10 10 30 32 HERS MATE
4 | ESA | HOFN NNOR UNSA
4 | GFZ | 30 DAV1
4 | JPL | 10 32
4 | MIT | 10 32 10 32 DAV1 CAS1 DAV1 MAW1 TWTF
5 | EMR | 10 10
5 | ESA | AREQ
5 | GFZ | DAV1
5 | JPL | 10
5 | MIT | 1 2 3 4 5 6 7 8 9 10 11 13 14 15 16 17 18 19 20 21
5 | MIT | 22 23 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7 8 9 10
5 | MIT | 11 13 14 15 16 17 18 19 20 21 22 23 25 26 27 28 29
5 | MIT | 30 31 32 HOB2
6 | ALL | 24
6 | COD | XMIS
6 | EMR | 10 10 30 HERS
6 | ESA | CHUR NNOR
6 | GFZ | CHUR SCUB WUHN
6 | GRG | NTUS
6 | JPL | 10
6 | MIT | 10 32 10 31 32 CAS1 DAV1 MAW1 CAS1 MAW1 NTUS
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
----+------------+----------
G12 | 2012_04_27 | 2012028
G28 | 2012_04_24 | 2012027
G28 | 2012_04_25 | 2012027
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 G24 | | | | 2 | | | |
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 | .6 -.2 -.9 -39 -26 33 .07
EMR | 3.4 -8.7 12.6 2 23 3 .51
ESA | 1.3 -3.2 22.0 -62 40 103 .29
GFZ | -.1 .8 .1 -36 7 -15 .04
GRG | 2.6 -7.3 19.2 -35 35 -34 .04
JPL | .7 -.5 6.2 -17 3 40 .29
MIT | 5.2 -6.8 16.2 -62 41 -78 .22
NGS | 7.1 -4.3 16.6 -72 -17 34 .18
SIO | -.6 -5.9 .1 -117 -68 48 .63
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 1.1685.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1685.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 2.1685.[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 3.1685.[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 5.1685.0-6).
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 1685 summary. (Apr 22, 2012 - Apr 28, 2012)
Table 1.1685.a GPS week: 1685 MJD: 56039.000-56045.000
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 264| 0 0 0 -7 43 9 -.29 9 9 | -625 -37 21 73
| 0 0 1 11 13 18 .02 | 435 591
emr 91| 1 0 3 -67 -37 -35 .36 18 18 | 6094 -861 17 115
| 1 1 3 21 26 12 .04 | 1247 801
esa 179| 0 0 0 -19 0 40 .24 7 7 | -998 513 14 110
| 0 0 1 9 23 12 .03 | 888 873
gfz 191| -1 0 -4 -49 -21 -19 -.21 13 13 | 179 -274 30 119
| 1 1 2 36 46 7 .03 | 298 421
grg 123| 1 0 8 -38 -54 -17 .55 15 14 | -151 11 47 194
| 1 0 1 12 11 13 .03 | 409 636
igr n/a| 0 0 -4 -61 -10 -28 -.08 5 5 | 4078 -699 19 80
| 0 0 0 10 21 15 .02 | 727 731
jpl 150| 0 0 -5 -42 -18 26 .51 15 15 | 3571 -753 20 94
| 0 0 2 12 5 51 .04 | 731 825
mit 286| 0 -2 -1 30 -64 -46 -.37 11 10 | -217 -46 35 230
| 1 1 1 14 25 13 .02 | 408 682
ngs 223| 0 0 3 74 35 -14 -.25 11 9 | -605 -118 2052 3616
| 0 1 1 17 35 15 .06 | 387 476
sio 239| -1 1 0 170 131 29 -.16 20 20 | --- --- --- ---
| 1 0 1 18 25 11 .03 | --- ---
Table 1.1685.b GPS week : 1685 MJD: 56039.000-56045.000
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 | 5 4 4 5 4 4 4 |
2 | 5 5 5 5 5 5 5 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 5 4 5 4 4 4 5 |
6 | 4 4 4 4 3 3 4 |
7 | 5 5 4 4 4 5 4 |
8 | 5 4 4 4 4 4 4 |
9 | 4 4 4 4 4 4 4 |
10 | 6 6 5 5 5 5 5 |
11 | 5 4 4 4 4 4 4 |
12 | 5 5 5 5 5 0 5 |
13 | 5 5 4 4 4 4 4 |
14 | 5 5 5 5 5 5 5 |
15 | 6 5 5 5 5 5 5 |
16 | 4 4 4 6 6 5 6 |
17 | 4 4 5 5 5 5 5 |
18 | 5 4 4 5 4 4 5 |
19 | 4 4 5 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 4 4 4 5 |
22 | 4 4 4 4 4 5 4 |
23 | 5 5 5 5 5 5 6 |
24 | 0 0 0 0 0 0 13 |
25 | 4 4 4 4 4 4 5 |
26 | 4 3 4 4 4 3 4 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 7 --- 4 4 4 |
29 | 5 5 4 5 5 5 5 |
30 | 5 5 4 5 5 4 5 |
31 | 5 4 5 5 4 5 5 |
32 | 5 4 5 6 5 5 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 2.1685.0 GPS week: 1685 Day: 0 MJD: 56039.000
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 264| 0 0 -1 -19 52 7 -.34 10 10 | -905 171 27 69
| 36 3 |
emr 91| 2 0 6 -77 -78 -31 .34 19 19 | 7725 -1104 15 91
| -53 28 |
esa 179| 0 0 -1 -19 8 53 .18 7 7 | -1757 989 14 105
| -17 -20 |
gfz 191| -3 2 -5 11 -26 -4 -.27 14 15 | 153 -712 34 110
| 15 -9 |
grg 123| 0 0 7 -47 -46 -12 .59 15 14 | -95 -540 43 178
| 21 -9 |
igr n/a| 0 0 -3 -67 8 -48 -.09 5 5 | 4866 -1133 20 77
| -31 25 |
jpl 150| -1 0 -2 -60 -11 -28 .45 15 14 | 4343 -1333 20 87
| -15 56 |
mit 286| 1 -3 0 50 -62 -53 -.37 12 11 | -454 136 20 160
| -4 0 |
ngs 223| 0 -2 2 42 17 -19 -.18 10 9 | -717 -199 2218 3665
| -15 44 |
sio 239| 1 1 0 202 143 46 -.13 21 20 | --- --- --- ---
| -169 -118 |
Table 2.1685.1 GPS week: 1685 Day: 1 MJD: 56040.000
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 264| 0 0 0 -11 52 0 -.30 9 9 | -1049 295 24 69
| 11 2 |
emr 91| 1 0 5 -53 -40 -27 .41 19 19 | 7155 -352 18 151
| -77 0 |
esa 179| 0 0 0 -9 30 32 .24 7 7 | -2483 1168 13 116
| -17 -34 |
gfz 191| -1 0 -5 -78 -72 -19 -.22 12 12 | -322 44 34 119
| 49 -22 |
grg 123| 1 0 7 -26 -57 -16 .55 15 15 | -461 272 50 205
| -11 -2 |
igr n/a| 0 0 -4 -65 0 -37 -.07 5 5 | 4318 -122 21 74
| 18 31 |
jpl 150| -1 1 -8 -28 -14 65 .51 17 16 | 3630 -225 22 102
| -6 -33 |
mit 286| 0 -3 -2 5 -93 -53 -.36 10 9 | -547 528 19 133
| 4 21 |
ngs 223| 0 0 5 77 56 -6 -.20 9 8 | -1100 323 2430 3824
| -60 30 |
sio 239| 0 1 -2 151 109 22 -.12 19 17 | --- --- --- ---
| -150 -90 |
Table 2.1685.2 GPS week: 1685 Day: 2 MJD: 56041.000
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 264| 0 0 1 -25 60 39 -.28 10 9 | -49 -585 22 77
| 50 -27 |
emr 91| 1 0 7 -33 -18 -51 .42 20 20 | 7127 -1794 15 132
| -95 -16 |
esa 179| -1 1 0 -25 6 23 .26 7 7 | -402 106 14 127
| -30 -5 |
gfz 191| 0 1 -7 -51 -17 -27 -.21 13 13 | 25 -553 30 133
| 20 7 |
grg 123| 0 0 7 -49 -57 -15 .57 16 16 | 115 -351 58 202
| 13 -4 |
igr n/a| 0 0 -5 -68 -2 -38 -.07 5 5 | 4869 -1430 20 85
| 7 29 |
jpl 150| 0 0 -7 -42 -24 72 .51 16 16 | 4371 -1504 20 125
| 8 2 |
mit 286| 0 -2 -1 23 -75 -63 -.34 9 8 | 507 -600 16 130
| 11 -5 |
ngs 223| 0 -1 1 70 29 0 -.19 12 10 | -60 -609 1994 3299
| -160 31 |
sio 239| 0 1 0 173 110 20 -.17 19 18 | --- --- --- ---
| -129 -112 |
Table 2.1685.3 GPS week: 1685 Day: 3 MJD: 56042.000
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 264| 0 0 1 0 32 -2 -.27 10 9 | -56 -832 20 76
| 16 3 |
emr 91| 2 -1 3 -54 -52 -42 .38 18 18 | 5565 -730 17 94
| -54 -12 |
esa 179| 0 0 -1 -3 -16 41 .22 8 7 | -778 29 17 110
| -6 9 |
gfz 191| -1 -1 -5 -102 44 -23 -.23 13 12 | 396 -387 32 147
| 44 26 |
grg 123| 1 1 7 -36 -43 -34 .56 15 15 | 40 -103 42 206
| 5 7 |
igr n/a| 0 0 -5 -40 -53 -1 -.11 5 5 | 3741 -459 21 84
| 2 41 |
jpl 150| 0 2 -5 -26 -13 81 .54 15 14 | 3409 -578 22 79
| 15 -13 |
mit 286| 0 -1 0 28 -34 -53 -.35 10 9 | 5 -215 21 153
| -1 -19 |
ngs 223| -2 0 3 84 -32 -6 -.22 13 10 | -184 -619 1811 3391
| -206 87 |
sio 239| -1 2 1 152 150 13 -.20 20 19 | --- --- --- ---
| -136 -134 |
Table 2.1685.4 GPS week: 1685 Day: 4 MJD: 56043.000
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 264| 1 0 0 0 41 30 -.27 9 9 | -453 -465 17 62
| 38 27 |
emr 91| 0 -2 0 -80 -52 -19 .33 18 18 | 5639 -1634 17 90
| -43 2 |
esa 179| 0 0 -1 -27 -25 30 .27 7 7 | -344 362 15 97
| -8 2 |
gfz 191| 0 0 -4 -26 24 -19 -.20 10 11 | 532 -236 27 98
| 29 20 |
grg 123| 2 0 9 -51 -41 -8 .52 15 14 | 471 -577 43 200
| -6 4 |
igr n/a| 1 0 -4 -59 -2 -16 -.07 5 5 | 4297 -1457 18 82
| 3 23 |
jpl 150| 0 0 -3 -51 -18 -28 .54 14 14 | 3838 -1550 18 84
| 32 23 |
mit 286| 0 -1 0 45 -62 -39 -.37 11 10 | 35 -146 23 150
| -9 9 |
ngs 223| 0 1 2 69 47 -3 -.34 12 10 | -436 -483 2023 3657
| -138 -38 |
sio 239| -2 0 1 176 146 31 -.15 20 22 | --- --- --- ---
| -146 -117 |
Table 2.1685.5 GPS week: 1685 Day: 5 MJD: 56044.000
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 264| 1 0 -1 2 43 -4 -.29 9 9 | -879 388 20 90
| 43 4 |
emr 91| -1 1 0 -99 -16 -49 .31 19 19 | 4372 567 19 137
| -34 -23 |
esa 179| 0 0 -1 -17 21 58 .25 7 7 | -1254 1793 14 126
| 16 -17 |
gfz 191| 0 -1 0 -48 -81 -23 -.19 12 12 | 34 496 28 121
| 29 21 |
grg 123| 3 -1 8 -16 -63 0 .51 14 14 | -386 119 51 187
| -10 -19 |
igr n/a| 0 0 -3 -67 2 -31 -.09 4 4 | 2866 529 20 86
| 9 34 |
jpl 150| -1 0 -6 -42 -19 -24 .48 15 14 | 2277 742 20 100
| 41 49 |
mit 286| -1 0 -2 30 -93 -21 -.41 12 10 | -519 -1036 128 728
| -18 -7 |
ngs 223| 0 0 7 73 70 -43 -.27 10 8 | -862 236 1990 3683
| -114 25 |
sio 239| -3 1 -1 157 98 39 -.18 21 22 | --- --- --- ---
| -132 -117 |
Table 2.1685.6 GPS week: 1685 Day: 6 MJD: 56045.000
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 264| 0 0 0 2 20 -2 -.29 9 9 | -988 768 19 73
| 25 23 |
emr 91| 2 0 -1 -75 -2 -30 .33 16 16 | 5080 -985 19 114
| -49 -60 |
esa 179| 0 0 0 -31 -29 44 .24 9 9 | 32 -850 11 91
| 14 23 |
gfz 191| 0 0 -2 -51 -18 -16 -.17 14 14 | 440 -571 28 111
| 41 46 |
grg 123| 0 0 12 -40 -73 -37 .56 15 14 | -747 1258 44 182
| -4 3 |
igr n/a| 0 0 -5 -58 -26 -28 -.08 6 6 | 3589 -824 19 73
| 9 27 |
jpl 150| 0 0 -5 -47 -25 45 .54 13 13 | 3129 -824 19 86
| -1 -10 |
mit 286| 0 -1 -2 30 -28 -37 -.36 12 11 | -549 1006 22 157
| -23 -18 |
ngs 223| 0 -1 3 101 59 -22 -.32 12 10 | -877 525 1904 3797
| -116 19 |
sio 239| -3 0 -3 179 163 32 -.16 22 22 | --- --- --- ---
| -150 -121 |
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 3.1685.0 GPS week: 1685 Day: 0 MJD: 56039.000
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 10 12 14 6 18 17 12 17 4 | 15 20 15 16 21 11 25 21 14 19 13
2 | 12 21 7 16 12 5 19 7 9 22 4 | 21 27 16 24 15 16 23 18 18 23 16
3 | 7 12 7 10 13 4 11 9 12 22 3 | 25 22 26 27 27 22 22 21 20 19 23
4 | 12 11 4 14 11 7 14 13 8 22 4 | 36 37 35 37 41 32 35 39 38 36 35
5E | 9 18 7 19 18 5 17 9 14 12 4 | 20 34 24 23 29 21 31 22 27 29 22
6 | 6 9 7 9 11 4 9 8 9 29 3 | 35 37 37 37 40 33 35 32 32 27 35
7 | 12 16 8 12 21 5 14 17 9 14 4 | 14 18 15 17 29 13 23 16 11 12 13
8 | 13 23 5 13 17 6 13 14 8 19 4 | 26 32 25 30 26 25 33 29 27 27 26
9 | 8 19 5 13 14 6 17 12 9 16 4 | 28 35 33 35 39 32 37 32 29 29 32
10E | 22 24 8 15 18 8 20 18 10 20 6 | 58 65 59 59 63 56 64 60 53 68 58
11 | 6 15 9 11 19 4 15 14 13 14 4 | 28 37 32 32 44 28 37 28 32 30 31
12 | 15 23 6 15 15 6 19 17 8 19 5 | 16 27 19 18 24 17 23 20 15 16 17
13 | 6 21 8 13 19 5 14 11 9 23 4 | 23 36 28 31 35 25 38 28 25 24 27
14 | 7 21 8 16 12 6 15 17 13 28 5 | 25 31 30 30 32 28 30 32 26 32 27
15 | 11 29 10 15 15 4 20 10 12 24 5 | 23 34 22 26 29 21 26 21 20 26 21
16 | 6 20 7 11 13 4 16 6 11 28 4 | 26 35 28 28 31 27 37 27 28 25 27
17 | 10 12 5 14 10 5 14 11 8 27 4 | 27 31 32 34 30 29 29 34 29 33 28
18E | 9 25 7 16 17 4 16 11 7 16 4 | 25 40 27 24 36 25 32 24 28 28 26
19 | 7 14 7 13 12 5 12 6 11 28 4 | 15 23 24 22 21 17 23 18 19 14 19
20E | 9 19 8 15 18 6 11 12 11 9 4 | 20 27 23 23 25 19 23 18 20 19 19
21 | 10 22 7 14 11 4 14 9 10 19 4 | 13 25 12 17 19 12 20 15 14 17 11
22E | 8 23 7 16 12 5 12 12 12 13 4 | 22 34 23 24 30 22 29 21 21 25 22
23 | 8 21 7 15 16 4 13 9 10 38 5 | 23 35 27 29 31 25 33 29 24 36 25
X24 | 6 --- --- --- --- 31 --- --- --- --- 0 | 17 --- --- --- --- 30 --- --- --- --- 17
25 | 8 21 5 18 14 2 13 11 11 16 4 | 42 54 43 40 51 42 53 37 44 38 42
26 | 12 11 6 13 12 4 15 12 9 14 4 | 22 20 20 22 27 20 24 20 22 18 19
27 | 10 15 5 14 14 4 15 10 11 14 4 | 25 30 29 31 37 28 34 28 28 26 28
28 | 12 15 7 16 15 6 13 11 9 18 4 | 16 18 11 16 6 11 16 15 11 13 11
29 | 8 14 6 13 14 5 17 12 9 32 4 | 18 25 25 20 24 20 28 25 24 29 21
30 | 10 18 6 14 10 5 15 13 11 25 4 | 29 37 33 38 29 32 37 34 31 39 32
31 | 7 22 8 16 19 5 13 11 11 18 4 | 20 29 24 22 35 19 27 21 17 18 19
32 | 9 20 7 16 15 7 17 10 10 16 4 | 30 37 30 32 32 30 38 32 33 35 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 7 14 15 5 15 12 10 21 |T 24 32 26 27 30 24 31 26 25 26 24
WRMS | 10 19 7 15 14 5 14 11 9 20 |NE 23 30 25 27 29 23 29 25 23 25 23
MEDI | 9 19 7 14 14 5 15 11 10 19 |MD 23 32 26 27 30 25 30 25 25 26 23
Table 3.1685.1 GPS week: 1685 Day: 1 MJD: 56040.000
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 | 6 16 8 13 14 3 14 12 7 12 3 | 10 19 15 20 18 12 26 18 13 18 13
2 | 10 21 8 14 12 4 24 8 8 20 4 | 17 23 14 19 13 11 23 15 13 20 12
3 | 14 12 5 10 12 4 10 6 8 17 3 | 19 18 20 21 18 17 18 14 19 16 17
4 | 10 14 6 11 14 7 14 11 7 18 3 | 24 28 26 23 30 21 28 28 24 28 23
5E | 8 16 7 13 15 6 23 11 7 9 4 | 20 28 22 18 28 18 28 19 19 22 20
6 | 12 10 5 12 11 5 9 6 9 23 3 | 34 36 37 38 36 35 37 34 37 36 36
7 | 10 16 10 11 20 4 15 12 11 11 4 | 12 23 15 19 30 15 25 13 13 12 14
8 | 9 17 5 9 16 4 18 12 12 15 4 | 16 25 18 19 21 19 30 20 25 19 19
9 | 8 17 6 10 15 5 15 11 12 10 3 | 17 27 21 26 27 20 29 21 21 19 21
10E | 13 21 10 18 17 7 27 19 13 17 5 | 86 86 85 80 85 81 88 80 82 86 82
11 | 8 14 8 9 18 4 12 9 13 12 4 | 20 34 27 24 38 22 33 20 24 22 24
12 | 13 22 6 14 16 3 21 11 9 18 4 | 12 26 17 16 22 13 24 14 13 12 13
13 | 6 21 9 13 19 4 20 8 9 17 4 | 16 35 22 24 35 19 32 19 22 18 20
14 | 5 28 6 11 12 4 14 14 10 23 4 | 21 30 26 26 27 24 29 25 25 27 22
15 | 10 24 8 11 16 4 20 11 11 22 4 | 21 30 22 21 29 20 26 20 19 21 20
16 | 6 23 6 9 15 3 16 7 6 23 4 | 21 30 22 22 30 22 30 19 24 23 21
17 | 8 13 5 15 10 4 16 12 11 26 4 | 18 22 19 24 18 18 20 23 20 28 17
18E | 9 25 5 11 14 5 13 10 6 13 4 | 28 41 33 36 36 29 35 31 32 34 32
19 | 11 14 7 10 13 4 13 8 8 28 4 | 12 24 27 22 22 19 25 17 22 16 20
20E | 6 20 6 12 15 5 13 8 7 9 3 | 19 29 22 23 25 17 25 17 15 20 19
21 | 8 21 8 13 13 5 19 7 8 16 4 | 10 23 12 16 20 8 21 11 11 12 10
22E | 7 20 6 9 13 5 12 11 8 13 3 | 16 30 24 23 27 21 26 22 21 25 22
23 | 6 23 5 13 17 5 14 9 10 36 4 | 16 32 21 23 29 19 29 19 22 30 19
X24 | 5 --- --- --- --- 31 --- --- --- --- 0 | 20 --- --- --- --- 17 --- --- --- --- 21
25 | 4 20 4 13 14 3 12 10 8 15 3 | 29 39 29 30 36 28 38 28 30 28 30
26 | 9 11 5 9 10 7 12 8 11 13 3 | 18 19 18 21 22 17 23 17 19 20 18
27 | 10 16 4 10 19 4 16 11 12 10 4 | 17 24 21 27 29 19 29 20 23 20 21
28 | 10 16 7 11 17 3 17 9 9 17 4 | 12 19 16 15 8 14 18 14 15 16 16
29 | 9 14 9 14 13 5 22 12 8 28 4 | 15 26 28 23 20 18 27 18 17 24 19
30 | 8 17 6 17 10 4 13 15 8 23 4 | 21 32 25 31 27 22 30 24 19 35 23
31 | 8 20 5 10 22 4 13 11 9 14 4 | 16 22 15 16 33 13 22 13 17 11 13
32 | 9 24 4 11 17 6 18 7 6 17 4 | 23 37 25 28 27 25 34 24 25 31 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 7 12 15 5 17 10 9 19 |T 20 29 24 24 27 21 29 21 22 24 21
WRMS | 9 19 7 12 15 5 16 9 8 17 |NE 17 26 21 22 25 18 26 19 20 21 19
MEDI | 8 17 6 11 15 4 15 11 9 17 |MD 18 28 22 23 27 19 28 19 21 21 20
Table 3.1685.2 GPS week: 1685 Day: 2 MJD: 56041.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 15 9 11 13 4 15 12 10 14 4 | 12 20 15 11 19 10 24 17 14 19 13
2 | 9 24 8 16 14 3 24 7 8 19 4 | 18 28 17 20 14 14 23 16 16 21 13
3 | 13 12 7 12 15 4 10 5 13 18 4 | 19 18 18 18 20 16 19 16 19 17 17
4 | 9 14 4 12 13 6 14 10 12 19 4 | 31 33 33 29 34 27 30 34 30 34 30
5E | 7 23 8 16 17 5 22 8 12 8 4 | 17 32 25 18 25 16 28 19 25 24 20
6 | 13 11 6 12 13 4 10 5 13 21 4 | 29 32 26 29 28 28 31 28 30 29 28
7 | 9 18 9 14 20 4 15 9 10 10 4 | 13 22 15 19 27 13 24 17 13 13 15
8 | 10 19 5 13 16 5 12 8 7 14 3 | 21 29 21 28 26 22 31 24 21 22 22
9 | 9 15 7 11 14 4 17 10 12 12 4 | 22 29 28 29 31 26 30 27 26 26 26
10E | 16 18 9 15 17 7 20 12 18 16 5 | 51 55 56 55 56 52 56 52 56 64 51
11 | 9 17 7 9 16 5 12 6 10 12 3 | 24 39 28 27 39 24 35 23 26 26 27
12 | 10 22 7 15 20 4 20 8 11 18 4 | 15 26 17 17 21 15 21 16 14 14 15
13 | 8 21 5 12 20 5 17 7 13 14 4 | 17 36 23 24 35 19 33 20 24 19 21
14 | 6 26 9 15 11 7 17 11 12 23 4 | 21 27 28 26 28 23 26 25 24 24 22
15 | 9 23 7 14 15 3 18 9 14 20 4 | 22 31 24 26 29 20 26 18 23 22 20
16 | 6 21 6 13 17 2 19 5 10 25 4 | 23 31 25 25 30 24 34 24 24 25 23
17 | 8 17 6 14 10 6 20 13 16 28 5 | 16 27 24 20 19 18 20 25 21 28 18
18E | 10 24 6 15 18 4 15 8 10 12 4 | 19 35 23 21 29 20 29 19 20 23 22
19 | 9 22 5 12 15 5 14 7 11 28 4 | 16 32 23 17 20 16 24 15 16 15 17
20E | 7 18 7 15 21 7 13 6 10 9 4 | 21 31 24 26 30 24 27 24 23 25 23
21 | 7 22 8 12 14 4 19 7 10 17 4 | 11 24 10 15 21 9 22 14 11 14 11
22E | 8 22 8 14 19 5 14 9 9 13 4 | 17 31 20 22 25 16 25 19 19 23 19
23 | 9 22 7 14 18 4 15 6 9 35 5 | 20 35 24 25 29 20 29 22 23 32 21
X24 | 6 --- --- --- --- 22 --- --- --- --- 0 | 15 --- --- --- --- 26 --- --- --- --- 15
25 | 9 18 6 13 16 4 12 9 14 12 4 | 34 40 33 31 40 33 41 28 35 30 31
26 | 9 14 4 12 13 3 13 7 14 9 3 | 18 21 20 21 23 17 22 19 25 19 18
27 | 11 14 6 11 16 3 15 8 11 14 4 | 21 26 26 28 32 24 28 25 26 24 25
X28 | 10 --- 8 --- --- 6 --- 8 --- --- 6 | 14 --- 12 --- --- 11 --- 16 --- --- 14
29 | 11 12 6 12 15 5 17 9 9 26 4 | 18 24 23 16 20 16 22 18 19 24 18
30 | 9 18 6 16 11 5 12 8 8 26 4 | 28 37 31 33 30 29 37 30 26 38 29
31 | 8 27 8 14 20 5 16 9 14 14 4 | 14 28 20 18 31 16 23 17 17 13 15
32 | 17 23 9 17 18 9 17 11 11 18 5 | 57 66 63 60 62 61 67 64 62 64 63
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 7 13 16 5 16 9 12 19 |T 21 31 25 25 29 22 29 23 24 25 22
WRMS | 9 20 7 13 16 5 16 8 10 18 |NE 19 28 22 23 26 19 27 21 21 22 20
MEDI | 9 18 7 13 16 5 15 8 11 16 |MD 19 31 24 24 28 20 27 20 23 24 20
Table 3.1685.3 GPS week: 1685 Day: 3 MJD: 56042.000
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 17 10 12 13 4 15 11 10 13 4 | 18 25 18 18 25 19 31 21 21 22 18
2 | 9 23 11 14 15 4 20 9 10 20 5 | 23 30 19 21 19 20 26 23 20 24 20
3 | 10 11 5 13 14 4 10 7 16 20 4 | 22 20 19 18 23 19 23 16 21 17 19
4 | 8 12 6 12 10 8 13 9 14 20 3 | 33 32 31 33 35 29 29 35 39 36 32
5E | 8 14 9 13 12 4 19 9 11 11 4 | 25 31 28 22 29 24 32 25 27 29 26
6 | 7 10 4 11 11 5 8 7 16 20 3 | 33 32 33 32 37 31 37 29 33 28 33
7 | 10 17 6 10 20 5 13 8 9 11 4 | 16 27 20 22 30 22 28 20 15 17 19
8 | 11 18 7 10 16 4 14 11 9 17 4 | 25 35 27 26 27 28 34 31 26 31 27
9 | 12 14 9 7 12 5 14 11 11 12 4 | 19 29 30 28 32 28 29 28 22 25 26
10E | 12 15 8 13 15 9 18 12 16 15 4 | 78 79 78 77 80 77 80 76 77 82 77
11 | 10 15 8 9 15 5 11 5 17 12 4 | 26 40 32 30 43 33 41 28 34 31 32
12 | 11 22 8 13 15 5 20 9 8 19 4 | 14 25 17 17 24 16 23 17 15 14 16
13 | 6 18 7 9 19 4 15 9 10 17 4 | 23 38 30 29 36 27 37 28 26 28 27
14 | 8 24 9 13 14 5 16 12 17 21 5 | 24 32 31 29 32 26 31 28 30 28 26
15 | 8 22 6 16 17 6 21 11 13 17 5 | 20 32 22 27 30 22 29 22 22 23 22
16 | 7 22 8 16 13 4 18 15 17 33 5 | 27 37 29 30 32 28 40 27 32 27 28
17 | 11 14 7 14 9 5 19 11 13 27 4 | 29 34 28 31 29 29 35 33 31 36 29
18E | 10 21 6 12 19 4 17 8 10 14 4 | 31 43 36 33 40 32 37 31 35 37 34
19 | 9 14 5 10 12 3 13 7 14 29 4 | 16 26 23 18 22 19 28 17 20 20 20
20E | 7 15 8 12 12 6 12 7 10 10 3 | 24 30 27 24 26 23 30 21 19 25 24
21 | 8 19 11 10 16 3 13 9 9 18 4 | 13 27 22 21 23 18 27 18 16 19 19
22E | 8 26 9 11 19 5 9 10 8 14 4 | 18 35 25 18 31 21 29 23 22 28 23
23 | 7 19 7 14 18 4 14 8 8 35 4 | 23 36 28 29 36 26 34 27 26 32 26
X24 | 4 --- --- --- --- 517 --- --- --- --- 0 | 16 --- --- --- --- 13 --- --- --- --- 16
25 | 9 18 5 14 15 4 12 14 12 16 4 | 34 43 33 32 43 33 43 27 36 29 33
26 | 8 13 5 13 14 6 11 10 16 10 3 | 19 23 20 24 24 22 24 20 23 24 20
27 | 12 15 5 8 13 5 13 10 8 14 3 | 19 25 25 26 30 24 28 26 22 21 24
29 | 10 12 8 12 14 5 15 15 14 28 4 | 24 27 27 26 28 23 28 25 20 29 24
30 | 8 16 5 18 11 5 10 8 16 28 4 | 30 40 33 33 32 35 41 34 37 40 34
31 | 10 20 7 14 21 3 19 8 17 15 5 | 20 26 18 21 33 17 25 18 20 12 18
32E | 15 24 7 16 15 10 25 10 16 29 5 | 88 95 96 90 98 89 109 90 91 103 95
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 8 12 15 5 15 10 13 20 |T 26 35 30 29 34 28 35 28 29 30 28
WRMS | 9 18 7 12 15 5 14 9 10 19 |NE 22 30 25 25 30 24 31 24 25 25 24
MEDI | 9 17 7 12 14 5 14 9 12 17 |MD 23 32 27 26 30 24 30 26 23 28 26
Table 3.1685.4 GPS week: 1685 Day: 4 MJD: 56043.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 16 6 9 12 3 16 10 14 9 4 | 13 23 17 18 23 13 30 20 15 21 16
2 | 8 20 8 12 13 4 21 8 8 21 4 | 17 26 15 21 15 13 24 17 13 23 15
3 | 5 12 6 9 12 4 9 9 16 23 3 | 14 16 17 17 18 12 18 12 17 13 14
4 | 7 12 6 8 12 5 13 13 8 23 3 | 25 30 30 31 32 25 30 31 25 34 27
5E | 7 18 6 11 15 4 20 9 15 13 4 | 24 35 28 24 31 25 33 24 33 30 26
6 | 5 10 5 9 13 5 8 8 13 18 3 | 16 22 21 20 25 16 24 17 16 14 19
7 | 11 16 10 10 19 5 13 10 11 13 4 | 13 26 25 22 30 19 26 18 17 18 18
8 | 9 19 6 8 13 5 15 10 8 15 3 | 17 30 21 21 23 18 31 25 24 23 21
9 | 10 18 7 6 13 4 13 11 13 18 4 | 16 27 24 27 26 21 27 23 25 24 22
10E | 14 16 7 11 18 4 17 18 15 17 5 | 35 40 38 36 45 35 43 37 33 42 37
11 | 8 15 8 9 16 4 11 7 18 11 4 | 20 36 28 26 41 23 38 25 19 25 26
X12 | 8 26 7 8 --- 4 --- 9 8 19 4 | 16 32 20 19 --- 18 --- 18 17 16 17
13 | 6 14 8 8 19 4 12 8 9 17 3 | 18 36 26 22 35 22 34 23 24 26 23
14 | 9 24 9 13 12 4 14 11 11 20 4 | 21 31 26 27 27 21 26 28 19 27 22
15 | 11 23 7 10 17 4 18 12 14 20 4 | 22 33 25 26 26 21 31 22 23 23 21
16 | 7 23 9 15 19 6 19 14 10 35 5 | 21 35 26 27 29 26 33 25 26 27 24
17 | 11 13 8 13 8 5 14 11 14 29 4 | 19 25 24 31 20 22 26 30 21 35 23
18E | 10 25 7 13 12 4 12 12 10 13 4 | 22 33 27 19 28 22 30 22 25 27 22
19 | 5 13 4 8 11 5 13 10 14 30 4 | 15 21 24 18 22 19 27 18 18 15 18
20E | 5 14 7 11 13 5 10 7 13 8 3 | 22 26 23 23 25 20 24 23 22 23 22
21 | 8 18 7 11 15 5 13 10 7 19 4 | 11 24 15 17 21 12 21 14 15 17 12
22E | 8 19 7 9 16 4 13 10 6 13 3 | 17 29 23 16 26 17 27 19 19 25 19
23 | 8 17 8 12 19 4 10 11 8 35 4 | 22 37 30 25 31 25 33 26 25 35 25
X24 | 5 --- --- --- --- 89 --- --- --- --- 0 | 54 --- --- --- --- 49 --- --- --- --- 56
25 | 10 18 5 9 18 4 12 12 10 16 4 | 26 37 29 29 36 27 37 21 24 23 26
26 | 8 11 5 12 13 3 10 10 13 13 3 | 18 20 22 25 20 19 24 19 22 22 20
27 | 11 15 6 7 15 4 13 9 13 19 4 | 15 23 22 25 26 19 26 20 23 22 20
28 | 6 20 7 9 16 5 15 10 10 17 4 | 14 29 15 13 21 12 23 18 11 18 14
29 | 10 14 6 10 15 5 17 10 13 27 4 | 20 26 24 17 25 19 25 23 26 26 20
30 | 9 17 8 8 17 7 12 11 12 29 4 | 53 58 55 52 48 55 60 56 54 62 56
31 | 7 21 8 9 20 3 14 6 11 17 4 | 15 28 18 17 30 15 24 15 16 15 15
32E | 12 25 8 11 13 10 14 14 11 17 4 | 60 67 62 57 64 63 58 59 65 68 59
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 7 10 15 5 14 11 12 20 |T 22 31 25 24 28 23 30 24 23 26 24
WRMS | 9 18 7 11 14 5 14 10 10 22 |NE 20 29 23 23 27 21 29 22 21 24 22
MEDI | 8 17 7 9 15 4 13 10 11 18 |MD 18 29 24 23 26 20 27 22 22 23 21
Table 3.1685.5 GPS week: 1685 Day: 5 MJD: 56044.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 17 6 9 12 4 13 9 8 9 3 | 15 20 21 16 23 14 31 16 20 16 18
2 | 8 19 9 14 13 5 21 8 9 24 4 | 20 26 19 23 16 15 22 19 21 25 17
3 | 7 11 6 11 10 3 10 10 9 21 3 | 17 17 18 20 19 15 22 12 18 13 17
4 | 8 15 5 14 13 6 13 14 6 25 4 | 26 28 28 33 29 27 27 31 32 31 28
5E | 10 16 10 14 13 3 18 8 8 12 4 | 19 27 20 18 24 18 26 20 19 26 17
6 | 6 10 6 9 8 3 9 11 7 18 3 | 28 29 28 30 30 26 30 25 25 24 27
7 | 10 16 8 12 16 4 14 12 15 15 4 | 13 26 15 18 26 14 25 18 16 17 14
8 | 11 21 5 13 13 2 13 11 9 16 4 | 17 30 18 21 20 18 27 20 21 20 18
9 | 11 19 5 10 10 3 16 10 12 16 4 | 20 28 23 25 25 22 32 23 21 23 22
10E | 12 14 5 14 17 5 15 19 13 17 4 | 63 62 66 67 67 63 63 62 70 66 64
11 | 10 17 8 9 13 6 13 8 9 10 3 | 23 36 31 30 38 24 41 23 27 22 29
X12 | 5 --- --- --- --- 38 --- --- --- --- 0 | 8 --- --- --- --- 13 --- --- --- --- 9
X13 | 6 17 4 13 --- 5 12 9 9 17 3 | 22 36 24 27 --- 24 36 25 24 22 24
14 | 9 22 9 11 12 4 13 15 11 23 4 | 19 29 27 23 27 23 28 24 27 23 22
15 | 11 24 7 13 13 4 19 11 10 21 4 | 20 32 20 23 25 19 26 20 22 18 19
16 | 7 23 10 14 17 4 17 14 6 39 5 | 19 34 24 21 30 21 29 21 23 25 21
17 | 10 15 7 12 9 6 17 13 13 32 4 | 26 27 26 26 24 25 27 28 27 31 24
18E | 10 23 6 14 14 4 13 10 10 13 4 | 22 31 28 23 30 23 31 22 21 28 24
19 | 7 16 5 11 12 4 12 9 12 27 4 | 17 25 26 24 22 19 28 18 19 18 22
20E | 7 22 8 12 12 4 13 10 9 10 3 | 21 29 24 21 26 21 26 29 26 28 22
21 | 8 22 6 10 16 4 16 10 8 21 4 | 13 26 15 14 23 12 24 15 15 17 12
22E | 10 22 8 12 19 5 14 11 10 13 4 | 16 29 22 14 25 18 27 17 22 21 18
23 | 8 20 6 15 19 4 13 12 9 35 5 | 22 34 24 25 33 22 30 23 22 30 22
X24 | 5 --- --- --- --- 118 --- --- --- --- 0 | 72 --- --- --- --- 87 --- --- --- --- 72
25 | 8 17 6 10 14 3 13 17 9 19 4 | 28 33 29 25 36 25 36 23 25 23 26
26 | 9 12 5 11 9 4 11 9 6 12 3 | 17 22 21 18 23 18 23 17 18 17 17
27 | 12 19 4 8 13 4 14 9 11 15 4 | 22 30 23 23 27 22 30 23 21 22 22
28 | 9 19 6 13 17 4 14 12 6 17 4 | 11 20 17 15 17 13 20 16 15 18 15
29 | 7 14 8 13 13 5 18 14 9 25 4 | 21 27 27 23 20 22 26 21 27 25 22
30 | 9 15 7 13 8 3 13 10 6 33 4 | 47 56 50 49 52 47 51 44 47 52 47
31 | 8 25 7 14 16 4 16 9 9 22 4 | 17 26 18 18 27 15 24 14 22 15 16
32E | 10 23 8 12 15 7 16 18 19 18 5 | 60 64 60 61 67 58 66 59 62 66 61
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 7 12 14 4 15 12 10 21 |T 24 31 26 25 29 25 31 24 25 26 25
WRMS | 9 19 7 12 14 4 14 10 8 22 |NE 22 29 23 23 26 23 28 21 23 22 23
MEDI | 9 17 6 12 13 4 13 10 9 18 |MD 20 29 24 23 26 21 27 21 22 23 22
Table 3.1685.6 GPS week: 1685 Day: 6 MJD: 56045.000
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 17 8 11 12 6 14 11 12 14 4 | 17 20 19 16 23 14 26 18 22 15 16
2 | 8 22 11 18 14 7 18 10 14 28 5 | 21 27 17 26 14 17 22 23 22 33 17
3 | 7 11 9 13 11 5 9 10 11 24 4 | 16 19 21 20 24 16 17 17 19 19 18
4 | 9 11 6 13 13 8 8 15 12 25 4 | 31 30 30 35 37 27 30 35 36 34 31
5E | 8 16 10 16 19 6 19 9 14 11 4 | 23 33 26 23 32 25 33 26 31 32 26
6 | 6 9 9 14 10 5 9 8 10 19 3 | 31 29 33 31 32 28 28 30 29 30 30
7 | 9 14 10 12 17 5 14 9 13 13 4 | 12 23 20 17 27 16 22 19 17 14 17
8 | 11 17 7 12 15 4 12 10 9 19 4 | 16 24 16 19 18 17 24 21 18 20 18
9 | 10 16 8 13 10 7 13 12 12 15 4 | 19 30 24 23 30 23 31 23 25 25 24
10E | 14 14 11 13 21 7 15 11 11 14 4 | 67 74 72 70 73 69 74 69 73 77 69
11 | 9 14 7 11 13 5 9 11 8 14 3 | 28 36 38 34 46 30 40 31 35 30 34
12 | 10 25 10 14 19 11 18 11 12 19 5 | 9 24 5 6 6 12 19 6 6 5 11
13 | 7 15 8 13 18 7 11 10 12 17 4 | 20 32 24 25 40 21 33 24 20 20 23
14 | 8 18 9 17 12 5 13 13 9 23 4 | 22 30 30 30 29 26 29 33 22 29 24
15 | 10 21 8 12 15 7 16 13 13 22 5 | 22 32 23 23 28 19 27 24 22 24 20
16 | 6 18 11 16 18 5 16 11 11 38 5 | 24 34 28 25 33 26 34 24 25 29 25
17 | 9 12 8 16 9 6 15 13 15 30 4 | 21 29 26 26 28 24 28 29 27 30 24
18E | 14 18 12 16 14 5 11 11 9 14 4 | 21 32 31 22 31 22 31 21 23 27 24
19 | 7 13 8 11 10 5 10 10 8 28 4 | 17 22 26 19 23 17 24 19 19 19 21
20E | 7 13 8 12 10 5 11 11 11 12 3 | 21 26 22 19 24 19 25 21 18 21 21
21 | 8 19 10 14 15 6 13 13 9 27 4 | 10 23 12 15 23 9 20 15 12 20 10
22E | 10 16 10 15 17 4 13 9 9 15 4 | 18 28 24 17 27 19 27 18 16 21 19
23 | 9 18 10 17 17 7 11 16 11 36 5 | 22 32 25 24 33 22 29 25 20 33 22
X24 | 10 --- --- --- --- 61 15 --- --- --- 13 | 26 --- --- --- --- 47 8 --- --- --- 28
25 | 10 17 7 14 18 6 12 14 9 18 4 | 29 38 30 29 41 28 40 28 28 30 30
26 | 9 9 8 12 13 5 10 9 13 9 3 | 19 23 23 23 24 19 24 22 20 22 19
27 | 10 13 8 13 12 6 13 8 14 16 4 | 20 30 27 27 28 23 32 26 23 27 25
28 | 7 14 7 13 17 7 12 12 11 18 4 | 12 21 10 14 19 12 17 15 13 12 12
29 | 8 13 10 15 14 4 16 12 9 26 4 | 19 26 28 23 30 22 27 25 23 27 22
30 | 9 15 10 15 10 5 12 9 14 28 4 | 53 51 49 52 48 50 51 51 48 52 52
31 | 7 23 10 18 17 6 14 6 12 22 4 | 16 24 20 21 29 16 23 17 15 21 15
32E | 12 22 12 15 13 6 16 22 17 19 5 | 42 49 46 43 50 45 50 52 46 54 47
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 9 14 15 6 13 12 12 22 |T 23 30 26 25 30 24 29 26 24 27 24
WRMS | 9 16 9 14 14 6 13 11 10 22 |NE 21 28 24 24 28 22 27 24 22 24 22
MEDI | 9 16 9 14 14 6 13 11 11 19 |MD 21 29 25 23 29 22 27 24 22 27 22
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 4.1685 GPS week: 1685 MJD: 56039.0-56045.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2980 |U 6 6 18 |U 8 9 31 |U 16 11 31 |
emr | emr 2929 | 10 8 22 |U 11 17 35 | 16 12 35 |
esa | esa 2934 | 6 7 18 |U 8 9 31 | 15 12 31 |
gfz | gfz 2842 |U 6 7 19 |U 8 10 31 |U 18 11 33 |
grg | grg 2907 | 9 11 27 |U 11 18 54 | 20 16 36 |
igr | igr 2934 | 6 7 18 | 7 9 29 | 17 11 33 |
igs | igs 2926 | 6 7 18 | 8 9 30 | 15 11 31 |
jpl | jpl 2928 | 7 7 20 |U 9 21 36 | 19 14 40 |
mit | mit 2934 | 6 7 19 |U 12 24 41 | 45 18 39 |
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 5.1685.0 GPS week: 1685 Day: 0 MJD: 56039.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 4 5 15 | 5 5 19 | 6 10 13 |
emr | emr 2974 | 9 6 23 | 7 5 20 | 8 13 17 |
esa | esa 2976 | 4 5 14 | 4 5 21 | 6 9 13 |
gfz | gfz 2972 | 5 4 15 | 5 6 26 | 6 10 12 |
grg | grg 2976 | 6 5 20 | 6 5 28 | 9 13 13 |
igr | igr 2976 | 5 4 16 | 4 5 19 | 6 9 13 |
igs | igs 2976 | 5 4 16 | 4 5 20 | 6 11 13 |
jpl | jpl 2974 | 5 5 19 | 5 6 21 | 7 17 22 |
mit | mit 2976 | 5 5 16 | 6 8 24 | 7 12 13 |
Table 5.1685.1 GPS week: 1685 Day: 1 MJD: 56040.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 | 5 5 14 | 4 7 22 | 13 14 52 |
emr | emr 2972 | 11 9 22 | 8 9 22 | 10 16 62 |
esa | esa 2976 | 7 7 16 | 5 7 21 | 15 14 47 |
gfz | gfz 2971 | 7 7 18 | 5 8 21 | 13 13 56 |
grg | grg 2976 | 11 13 25 | 9 15 33 | 21 14 55 |
igr | igr 2976 | 7 7 18 | 5 7 19 | 12 14 50 |
igs | igs 2953 | 7 8 18 | 5 9 20 | 13 14 55 |
jpl | jpl 2972 | 7 7 19 | 9 25 46 | 14 27 66 |
mit | mit 2976 | 7 8 20 | 10 21 32 | 11 17 54 |
Table 5.1685.2 GPS week: 1685 Day: 2 MJD: 56041.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2956 | 5 4 14 | 6 6 25 | 13 11 18 |
emr | emr 2876 | 10 7 15 | 8 36 25 | 12 13 22 |
esa | esa 2880 | 5 4 12 | 5 6 21 | 15 16 20 |
gfz | gfz 2396 | 6 4 16 | 7 5 22 | 15 14 20 |
grg | grg 2880 | 9 9 22 | 8 22 29 | 22 20 29 |
igr | igr 2880 | 5 5 13 | 5 6 20 | 15 14 19 |
igs | igs 2868 | 5 4 14 | 5 5 21 | 15 15 19 |
jpl | jpl 2876 | 6 5 16 | 8 42 25 | 13 14 23 |
mit | mit 2880 | 6 5 16 | 8 25 23 | 15 15 20 |
Table 5.1685.3 GPS week: 1685 Day: 3 MJD: 56042.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2784 | 7 7 22 | 9 14 55 | 12 11 21 |
emr | emr 2876 | 10 8 23 | 14 29 52 | 15 11 25 |
esa | esa 2880 | 7 6 21 | 10 15 49 | 12 14 22 |
gfz | gfz 2751 | 6 6 21 | 10 17 44 | 11 10 20 |
grg | grg 2880 | 6 6 26 | 12 22 64 | 12 17 26 |
igr | igr 2880 | 7 6 20 | 9 13 43 | 12 12 21 |
igs | igs 2857 | 7 7 18 | 10 15 47 | 12 10 20 |
jpl | jpl 2874 | 7 6 20 | 11 28 42 | 17 16 30 |
mit | mit 2880 | 7 8 21 | 13 26 50 | 11 8 22 |
Table 5.1685.4 GPS week: 1685 Day: 4 MJD: 56043.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 10 25 | 8 12 29 | 9 9 17 |
emr | emr 2968 | 13 11 29 | 13 16 36 | 11 10 19 |
esa | esa 2976 | 9 10 25 | 8 12 30 | 10 10 18 |
gfz | gfz 2967 | 10 12 25 | 8 14 31 | 14 13 23 |
grg | grg 2880 | 13 16 39 | 15 22 43 | 11 14 29 |
igr | igr 2976 | 9 11 25 | 8 12 29 | 9 9 17 |
igs | igs 2974 | 9 10 25 | 8 13 27 | 9 9 18 |
jpl | jpl 2871 | 11 10 28 | 9 16 32 | 10 8 21 |
mit | mit 2976 | 8 12 26 | 15 25 38 | 8 9 18 |
Table 5.1685.5 GPS week: 1685 Day: 5 MJD: 56044.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 7 9 19 | 17 13 47 | 51 9 81 |
emr | emr 2871 | 11 9 25 | 17 13 46 | 48 10 74 |
esa | esa 2880 | 6 8 18 | 16 13 45 | 39 10 86 |
gfz | gfz 2871 | 6 8 18 | 16 13 47 | 59 8 90 |
grg | grg 2783 | 11 12 33 | 16 15 79 | 44 15 68 |
igr | igr 2879 | 6 8 19 | 14 10 42 | 58 6 94 |
igs | igs 2879 | 7 8 19 | 14 10 42 | 49 7 79 |
jpl | jpl 2871 | 7 8 17 | 15 11 51 | 62 10 101 |
mit | mit 2880 | 5 7 16 | 19 40 69 | 257 59 131 |
Table 5.1685.6 GPS week: 1685 Day: 6 MJD: 56045.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 6 5 16 | 7 7 24 | 6 12 15 |
emr | emr 2968 | 8 6 19 | 12 9 43 | 10 11 23 |
esa | esa 2976 | 5 6 19 | 7 7 27 | 6 12 15 |
gfz | gfz 2966 | 5 7 19 | 7 8 28 | 11 11 13 |
grg | grg 2976 | 10 16 28 | 15 22 100 | 24 15 29 |
igr | igr 2976 | 6 6 17 | 7 8 28 | 7 11 15 |
igs | igs 2975 | 5 7 18 | 8 7 30 | 5 9 15 |
jpl | jpl 3064 | 6 6 18 | 9 15 32 | 7 8 19 |
mit | mit 2976 | 5 8 17 | 13 20 51 | 9 7 15 |
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 6.1685 GPS week: 1685 MJD: 56039.500-56045.500
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 | -9 -58 114 -37 -3 | 1 17
| 17 16 114 70 6 | 2
emr uuuuu | 8 31 53 98 -6 | 53 56
| 27 17 71 138 7 | 2
esa uuuuu | 2 -20 84 -8 2 | 7 19
| 18 15 62 51 5 | 4
gfz uuuuu | -16 -59 149 -90 -2 | 9 18
| 21 15 75 120 4 | 2
grg uuuux | -1 -28 103 -101 11 | -13 38
| 10 15 63 47 13 | 6
igr xxxxx | -34 -29 54 -77 -5 | -1 15
| 7 19 54 55 5 | 2
irf xxxxx | -4 -26 50 -18 -5 | 3 13
| 5 7 28 28 7 | 1
jpl uuuuu | -14 -37 -30 -1 13 | 24 31
| 31 21 57 60 6 | 5
mit uuuuu | -1 -21 -126 75 -1 | 14 21
| 18 16 67 41 4 | 2
ngs uuuuu | -32 89 -87 -62 -2 | 9 15
| 35 58 108 79 7 | 1
sio uuuuu | 112 118 -234 167 -1 | 43 46
| 18 18 76 85 5 | 2
Table 7.1685.0 GPS week: 1685 Day: 0 MJD: 56039.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -2 -55 -22 -107 -8 | 2 14
emr uuuuu | -27 34 33 -141 -7 | 57 59
esa uuuuu | 21 -2 73 47 -5 | 7 19
gfz uuuuu | 10 -34 65 -3 -7 | 11 17
grg uuuux | 10 -40 47 -182 25 | -3 44
igr xxxxx | -24 12 46 -70 -7 | 2 14
irf xxxxx | 1 -19 -3 -38 4 | 4 12
jpl uuuuu | -55 -4 49 61 7 | 22 28
mit uuuuu | 1 -15 -145 151 -1 | 15 20
ngs uuuuu | -43 -4 39 -137 7 | 9 14
sio uuuuu | 119 150 -383 128 3 | 44 47
Table 7.1685.1 GPS week: 1685 Day: 1 MJD: 56040.500
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 | -14 -35 124 -14 0 | -1 17
emr uuuuu | -12 53 -13 50 1 | 53 56
esa uuuuu | 22 -7 55 22 -2 | 4 19
gfz uuuuu | 10 -73 88 35 -4 | 8 18
grg uuuux | -10 -13 23 -80 -3 | -8 42
igr xxxxx | -43 -42 -38 -13 -13 | -2 17
irf xxxxx | -12 -24 47 -44 -2 | 2 13
jpl uuuuu | 21 -18 -40 -29 11 | 19 26
mit uuuuu | -33 -28 -26 55 0 | 12 20
ngs uuuuu | -42 36 -48 -91 0 | 7 14
sio uuuuu | 78 126 -157 40 3 | 42 45
Table 7.1685.2 GPS week: 1685 Day: 2 MJD: 56041.500
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 | 21 -88 193 -113 -11 | 0 18
emr uuuuu | 10 57 -47 103 1 | 52 55
esa uuuuu | -1 -8 62 43 4 | 3 19
gfz uuuuu | -13 -58 186 4 -7 | 8 18
grg uuuux | -2 -51 174 -137 7 | -13 37
igr xxxxx | -35 -45 73 -103 -7 | -3 16
irf xxxxx | -6 -38 67 -47 0 | 3 14
jpl uuuuu | -8 -46 -91 -110 6 | 20 28
mit uuuuu | -1 -49 -75 41 -4 | 12 20
ngs uuuuu | -37 122 -60 -129 3 | 8 16
sio uuuuu | 106 91 -191 165 -5 | 42 45
Table 7.1685.3 GPS week: 1685 Day: 3 MJD: 56042.500
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 -48 187 68 -2 | -1 18
emr uuuuu | 14 22 131 32 -3 | 52 54
esa uuuuu | -7 -26 -11 -61 -2 | 3 19
gfz uuuuu | -24 -76 161 -87 -1 | 7 18
grg uuuux | -5 -37 129 -55 10 | -17 35
igr xxxxx | -39 -34 120 -111 -5 | -4 16
irf xxxxx | 2 -32 39 8 -8 | 2 14
jpl uuuuu | 15 -47 -65 -11 13 | 21 28
mit uuuuu | 21 -31 -78 92 5 | 11 20
ngs uuuuu | -85 174 -23 -8 -6 | 8 16
sio uuuuu | 136 104 -242 210 2 | 41 44
Table 7.1685.4 GPS week: 1685 Day: 4 MJD: 56043.500
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 -63 -66 -24 4 | 0 18
emr uuuuu | -5 18 119 166 -7 | 53 55
esa uuuuu | -5 -17 143 -21 10 | 6 19
gfz uuuuu | -23 -54 88 -89 2 | 8 18
grg uuuux | -7 -19 73 -103 -7 | -17 35
igr xxxxx | -26 -28 60 -67 -1 | -3 16
irf xxxxx | -3 -25 48 -1 -18 | 3 14
jpl uuuuu | -26 -57 -79 49 24 | 24 31
mit uuuuu | -12 -16 -195 78 0 | 14 21
ngs uuuuu | 35 113 -65 -111 -16 | 10 16
sio uuuuu | 114 121 -269 177 1 | 43 45
Table 7.1685.5 GPS week: 1685 Day: 5 MJD: 56044.500
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 -63 147 -93 -7 | 5 18
emr uuuuu | 19 14 119 296 -18 | 55 58
esa uuuuu | 13 -36 88 -5 2 | 12 19
gfz uuuuu | -25 -49 175 -187 2 | 12 20
grg uuuux | 15 -10 86 -49 29 | -18 35
igr xxxxx | -38 -29 15 -12 -4 | 1 15
irf xxxxx | -4 -20 68 -29 -3 | 5 13
jpl uuuuu | -53 -61 47 46 10 | 31 37
mit uuuuu | 3 -2 -194 25 -7 | 18 23
ngs uuuuu | -29 94 -157 -42 1 | 11 17
sio uuuuu | 113 112 -214 129 -10 | 47 49
Table 7.1685.6 GPS week: 1685 Day: 6 MJD: 56045.500
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 | -27 -53 235 22 3 | 2 15
emr uuuuu | 56 21 27 177 -10 | 51 53
esa uuuuu | -27 -42 181 -84 5 | 11 18
gfz uuuuu | -50 -69 282 -302 3 | 11 18
grg uuuux | -7 -24 191 -103 16 | -18 35
igr xxxxx | -31 -37 104 -166 2 | -2 12
irf xxxxx | -4 -28 85 24 -9 | 3 11
jpl uuuuu | 6 -27 -31 -13 18 | 32 37
mit uuuuu | 14 -5 -168 80 -3 | 16 21
ngs uuuuu | -23 88 -291 83 -6 | 10 15
sio uuuuu | 117 122 -181 316 1 | 44 46
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