[IGSREPORT-20091] Wk 1649 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 1 06:10:54 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1649 (Aug 14, 2011 - Aug 20, 2011)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1649[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1649[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1649[0-6].cls IGS GPS clock combination summary report.
igs16497.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16497.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 | ALL | 30 30
0 | COD | NKLG
0 | ESA | NRIL IRKJ PALM UNSA
0 | GFZ | 3 6 19 29 MDVJ NKLG
0 | GRG | IRKJ USN3
0 | JPL | IRKJ
0 | MIT | 3 6 27 3 6 27
1 | COD | MCM4 BRMU MCM4
1 | ESA | UNSA
1 | GFZ | 6 19 29 KOSG MATE
1 | GRG | BRMU USN3
1 | MIT | 3 4 6 27 30 3 4 6 27 30 DAV1 BRMU
2 | COD | 30 30
2 | EMR | BAN2
2 | ESA | CONZ IRKJ
2 | GFZ | 6 19 29 BAN2 BRFT MDVJ PERT
2 | GRG | IRKJ NKLG
2 | MIT | 3 6 15 27 3 6 15 27 KHAJ KHAJ MAW1 TIDB
3 | COD | NICO NICO NNOR WROC
3 | EMR | 3 3
3 | ESA | NNOR BAN2 DRAG IRKJ NNOR
3 | GFZ | 6 19 29 DGAR KOSG MATE MDVJ
3 | GRG | IRKJ
3 | JPL | 3
3 | MIT | 6 19 26 27 30 6 19 26 27 30 SYDN USNO WROC DAV1 USNO
4 | ALL | 30
4 | COD | NICO NICO
4 | ESA | BAN2 IRKJ
4 | GFZ | 6 29 KOSG KOUR
4 | GRG | IRKJ
4 | MIT | 7 8 26 27 28 6 7 8 26 27 28 DAV1 KOSG KOSG MDVJ TWTF
5 | ALL | 30
5 | COD | WROC WROC
5 | ESA | IRKJ KOSG
5 | GFZ | 6 9 29 CONZ MDVJ
5 | GRG | IRKJ
5 | JPL | 27
5 | MIT | 1 6 22 27 1 6 22 26 27 CONZ KOSG
6 | EMR | MATE MATE
6 | ESA | 17 19 29 IRKJ
6 | GFZ | 6 7 HOLM MDVJ OPMT QAQ1
6 | GRG | IRKJ SANT
6 | MIT | 1 7 19 27 1 6 27 CAS1
5. 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 G01 | 2 | | | | | | |
PRN G03 | | | | 1 | | | |
PRN G06 | 2 | | | | | | |
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
7. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .5 .4 .4 -13 -11 17 -.03
EMR | .0 7.8 -2.9 4 -5 3 .32
ESA | 1.3 .5 16.1 29 4 65 -.08
GFZ | -.2 .9 .3 -17 -5 -7 -.08
GRG | .9 -.2 6.5 -17 -5 2 -.01
JPL | -4.5 .4 .0 -19 11 60 .01
MIT | 1.9 -2.1 10.5 -15 6 -15 .0
NGS | 2.0 1.5 11.4 -24 13 -3 .20
SIO | -2.8 -.4 -10.9 -24 -48 -14 -.07
8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1649.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1649.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 2.1649.[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 3.1649.[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 5.1649.0-6).
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 1649 summary. (Aug 14, 2011 - Aug 20, 2011)
Table 1.1649.a GPS week: 1649 MJD: 55787.000-55793.000
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 248| 0 0 1 6 -3 8 -.28 7 7 | -482 1 18 86
| 0 0 0 11 8 15 .02 | 693 1199
emr 94| 0 3 -3 -14 21 1 .39 18 18 | 2316 -62 17 105
| 1 1 1 10 20 11 .03 | 1376 961
esa 136| 0 0 2 -56 38 -3 .26 8 8 | 795 -1375 19 184
| 0 0 2 13 14 11 .03 | 941 1258
gfz 190| -1 0 0 7 -23 -9 -.19 11 11 | 283 -275 24 100
| 0 0 1 51 43 12 .01 | 433 753
grg 128| 2 0 4 4 -8 7 .72 16 15 | -35 -128 44 233
| 1 0 1 18 21 48 .15 | 492 849
igr n/a| 0 0 1 -11 7 -45 -.08 5 5 | 3643 -319 19 78
| 0 0 0 13 14 12 .03 | 1809 942
jpl 113| 1 0 -7 16 -41 50 .58 14 13 | 370 -52 18 101
| 1 0 2 11 17 27 .03 | 1287 958
mit 264| 0 -1 0 -3 -25 -23 -.31 11 10 | -90 -269 22 184
| 0 0 0 24 24 15 .01 | 460 725
ngs 222| 0 0 2 45 -14 -11 -.23 9 7 | -522 123 1964 3648
| 1 0 1 24 30 24 .05 | 758 1152
sio 243| -2 0 -6 11 122 -30 -.25 20 19 | --- --- --- ---
| 0 1 1 18 25 9 .02 | --- ---
Table 1.1649.b GPS week : 1649 MJD: 55787.000-55793.000
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 | 0 0 0 0 0 15 14 |
2 | 4 4 4 4 4 4 4 |
3 | 4 4 4 6 5 4 4 |
4 | 6 3 4 4 4 3 4 |
5 | 4 4 4 4 4 4 4 |
6 | 6 5 4 5 5 5 5 |
7 | 4 4 5 4 4 4 5 |
8 | 4 4 4 4 4 3 4 |
9 | 4 5 4 4 4 4 4 |
10 | 3 3 3 4 3 3 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 4 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 5 4 5 5 4 4 4 |
16 | 5 5 4 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 5 5 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 4 3 3 3 3 4 4 |
21 | 5 4 4 4 4 4 5 |
22 | 4 4 4 3 3 3 3 |
23 | 5 4 4 4 5 4 4 |
24 | 3 4 3 4 4 3 4 |
25 | 4 4 4 5 4 4 4 |
26 | 4 4 4 4 4 6 4 |
27 | 6 10 7 8 6 5 5 |
28 | 4 4 4 4 4 4 4 |
29 | 4 4 5 4 5 4 4 |
30 | 8 12 10 6 4 5 4 |
31 | 4 4 4 4 4 4 4 |
32 | 3 3 3 3 3 3 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 2.1649.0 GPS week: 1649 Day: 0 MJD: 55787.000
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 248| 0 0 2 5 -15 15 -.29 9 7 | -427 -617 20 103
| 56 32 |
emr 94| -2 4 -6 -9 9 -5 .39 18 18 | 3929 42 17 101
| -39 -19 |
esa 136| 1 0 0 -70 32 12 .22 7 7 | 2082 -3023 19 181
| 35 15 |
gfz 190| -1 0 1 -23 58 -25 -.21 11 11 | 201 -45 25 97
| 5 46 |
grg 128| 2 0 6 22 -21 13 .57 14 14 | 291 -573 37 236
| 0 26 |
igr n/a| 0 0 0 -5 -13 -56 -.08 5 5 | 6090 -599 20 138
| -4 29 |
jpl 113| 1 0 -5 37 -41 57 .52 13 13 | 1996 -448 19 107
| -29 5 |
mit 264| 1 -1 0 22 -2 -4 -.32 11 10 | 19 -505 22 174
| 7 -7 |
ngs 222| 0 0 2 73 -77 -50 -.24 10 8 | -491 -540 1684 3750
| -56 22 |
sio 243| -3 -1 -5 29 143 -37 -.26 22 20 | --- --- --- ---
| -36 -88 |
Table 2.1649.1 GPS week: 1649 Day: 1 MJD: 55788.000
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 248| 0 0 1 -7 5 -20 -.30 7 6 | -1668 1429 20 94
| 30 -11 |
emr 94| 1 4 -3 -8 45 0 .35 18 18 | 3064 749 22 108
| -37 -53 |
esa 136| 0 0 2 -70 30 9 .26 7 7 | 494 190 20 181
| -11 6 |
gfz 190| -1 0 0 75 -17 4 -.19 11 11 | -506 1083 26 93
| 10 54 |
grg 128| 4 0 3 -6 18 -7 .58 13 12 | -866 1544 35 204
| 52 -22 |
igr n/a| 0 0 0 -1 -6 -39 -.09 4 4 | 4855 377 19 72
| -23 29 |
jpl 113| 0 0 -7 16 -9 64 .56 14 14 | 793 734 19 98
| -38 -3 |
mit 264| 0 0 0 0 -73 -44 -.30 11 10 | -664 893 22 182
| 15 0 |
ngs 222| 0 0 0 41 -13 2 -.19 9 7 | -1908 1713 1954 3560
| 2 30 |
sio 243| -2 0 -7 13 78 -36 -.27 20 20 | --- --- --- ---
| -37 -81 |
Table 2.1649.2 GPS week: 1649 Day: 2 MJD: 55789.000
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 248| 0 0 0 2 -8 24 -.28 8 8 | -882 609 19 94
| -2 21 |
emr 94| 2 4 -1 -18 43 22 .40 18 18 | 3859 -2067 16 87
| -29 -48 |
esa 136| 0 0 2 -66 26 -7 .25 7 7 | -22 -773 19 185
| 56 -8 |
gfz 190| -2 0 0 48 -11 5 -.19 10 9 | 200 134 22 101
| -18 59 |
grg 128| 2 0 5 10 1 18 .59 15 14 | 411 -498 45 259
| -1 0 |
igr n/a| 0 0 2 -11 7 -23 -.13 5 5 | 5359 -2227 20 60
| -11 11 |
jpl 113| 2 0 -8 21 -41 6 .57 13 13 | 1767 -2002 18 99
| -40 -9 |
mit 264| 1 -1 0 -9 -36 -33 -.31 10 9 | 219 -501 25 178
| 2 -7 |
ngs 222| -1 0 2 24 -4 3 -.32 9 7 | -886 590 1922 3856
| -14 46 |
sio 243| -2 0 -6 9 104 -25 -.26 18 18 | --- --- --- ---
| -48 -76 |
Table 2.1649.3 GPS week: 1649 Day: 3 MJD: 55790.000
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 248| 0 0 0 -5 6 15 -.27 7 6 | -622 1249 17 111
| 35 8 |
emr 94| 0 5 -2 -20 27 -5 .38 18 18 | 1382 -123 17 104
| -33 -14 |
esa 136| 0 0 0 -50 36 -13 .26 8 8 | 331 -2669 21 206
| 12 7 |
gfz 190| -1 1 0 37 -61 -14 -.21 10 11 | 345 -345 24 101
| -22 60 |
grg 128| 1 0 4 -30 8 67 .90 17 16 | -327 97 50 228
| 53 -9 |
igr n/a| 1 0 1 -16 15 -53 -.08 5 5 | 2774 -528 19 80
| 10 40 |
jpl 113| 3 0 -5 10 -29 82 .59 13 13 | -486 -92 19 105
| -33 30 |
mit 264| 0 -2 -1 10 -27 -23 -.29 12 11 | -445 230 19 162
| 6 -15 |
ngs 222| 0 0 5 24 -5 -43 -.27 9 9 | -641 1251 2071 3475
| -9 -15 |
sio 243| -3 0 -6 14 111 -31 -.25 19 20 | --- --- --- ---
| -33 -77 |
Table 2.1649.4 GPS week: 1649 Day: 4 MJD: 55791.000
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 248| 0 0 1 24 -7 -1 -.29 7 7 | 300 -1721 17 66
| -15 31 |
emr 94| -2 2 -2 -2 24 2 .37 17 17 | 805 801 18 103
| -36 -15 |
esa 136| 0 0 2 -47 34 -19 .30 8 8 | 1329 -696 20 177
| 21 -3 |
gfz 190| -2 0 0 -28 -48 -9 -.17 10 11 | 494 -1079 24 102
| -19 49 |
grg 128| 0 -2 5 23 -35 -31 .92 19 17 | -357 209 63 254
| 26 51 |
igr n/a| 0 0 1 7 10 -38 -.04 4 4 | 1901 386 17 73
| -14 39 |
jpl 113| 2 1 -5 22 -53 77 .57 14 13 | -950 566 18 100
| -10 52 |
mit 264| 1 -1 0 -39 -6 -7 -.29 10 9 | -563 16 22 202
| 16 -8 |
ngs 222| 1 0 1 61 12 -3 -.22 8 7 | 210 -1200 2121 3715
| -36 -33 |
sio 243| -2 0 -5 -16 138 -14 -.23 19 19 | --- --- --- ---
| -34 -69 |
Table 2.1649.5 GPS week: 1649 Day: 5 MJD: 55792.000
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 248| 0 0 2 12 1 18 -.28 7 7 | -421 195 20 67
| 52 17 |
emr 94| -1 1 -5 -33 10 -14 .42 19 19 | 689 272 13 106
| -5 15 |
esa 136| 0 0 4 -56 40 -7 .26 7 7 | 1767 -2285 19 168
| 22 29 |
gfz 190| -1 0 -2 16 -70 -2 -.19 11 12 | 302 -669 24 92
| -11 32 |
grg 128| 2 0 2 12 3 -68 .69 15 14 | 147 -950 40 232
| 30 0 |
igr n/a| 1 0 0 -28 30 -58 -.07 5 5 | 1355 397 20 66
| 4 29 |
jpl 113| 0 1 -9 6 -57 34 .60 15 14 | -1237 618 15 93
| 21 92 |
mit 264| 0 -1 0 24 -17 -14 -.32 11 10 | 453 -1382 25 184
| 0 -12 |
ngs 222| 0 0 1 19 12 11 -.18 8 7 | -315 248 2242 3789
| -10 6 |
sio 243| -1 0 -6 35 133 -42 -.27 20 18 | --- --- --- ---
| -44 -77 |
Table 2.1649.6 GPS week: 1649 Day: 6 MJD: 55793.000
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 248| 0 0 0 11 -9 9 -.25 7 7 | 343 -1131 18 67
| 9 17 |
emr 94| -1 4 -3 -5 -11 7 .42 19 19 | 2489 -114 16 130
| -31 11 |
esa 136| -1 0 6 -35 71 0 .30 10 10 | -415 -371 21 194
| 10 -4 |
gfz 190| -1 0 0 -71 -12 -22 -.18 10 11 | 947 -1009 26 120
| -17 30 |
grg 128| 1 0 4 4 -35 63 .76 18 18 | 453 -731 40 223
| 48 70 |
igr n/a| 1 -1 0 -25 10 -46 -.05 5 5 | 3172 -41 19 63
| 36 15 |
jpl 113| 0 1 -10 3 -60 29 .62 15 14 | 710 260 18 110
| -3 75 |
mit 264| 1 -1 -1 -29 -12 -34 -.31 10 8 | 350 -634 23 207
| 9 -10 |
ngs 222| 1 0 2 74 -25 1 -.18 8 7 | 376 -1197 1755 3394
| -55 10 |
sio 243| 0 2 -8 -7 148 -27 -.25 19 18 | --- --- --- ---
| -49 -77 |
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 3.1649.0 GPS week: 1649 Day: 0 MJD: 55787.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 4 --- --- --- --- --- --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- 1
2 | 5 21 7 8 16 5 14 7 8 20 3 | 24 39 28 24 39 25 36 25 25 27 27
3E | 9 18 6 10 14 5 15 12 11 23 4 | 23 27 21 22 22 21 25 24 20 27 21
4 | 27 17 10 10 11 6 13 10 9 13 5 | 43 35 31 29 39 31 38 31 32 30 33
5 | 7 11 6 9 12 5 15 10 11 27 3 | 28 27 31 30 35 29 32 28 32 27 28
6E | 14 17 6 12 13 7 19 23 14 45 6 | 139 142 141 139 143 138 145 139 137 148 140
7 | 9 18 8 14 16 5 12 7 6 18 4 | 21 30 23 20 29 21 27 22 21 21 21
8 | 7 14 7 11 13 4 10 10 8 17 3 | 16 23 17 16 16 15 24 14 15 17 15
9 | 8 24 6 13 9 4 12 14 10 17 4 | 21 35 20 25 20 21 29 22 26 28 22
10 | 4 11 4 8 14 4 8 7 11 22 3 | 28 31 33 31 39 30 33 32 32 26 30
11 | 7 14 6 10 19 6 8 10 6 16 3 | 18 23 15 20 28 16 20 18 16 16 15
12 | 9 22 7 17 16 6 17 18 9 25 5 | 19 30 19 23 23 18 25 22 19 20 18
13 | 5 17 7 9 23 4 11 11 11 15 4 | 19 24 18 16 35 16 24 19 19 18 17
14 | 7 16 7 9 17 4 14 10 11 15 4 | 15 27 20 19 27 16 23 20 23 17 17
15 | 9 24 6 9 16 5 17 14 14 21 4 | 15 30 18 18 24 17 26 16 27 18 16
16 | 8 21 7 16 16 7 15 9 10 23 4 | 20 28 18 14 23 17 25 18 20 17 17
17E | 6 16 8 7 14 4 18 7 5 14 3 | 22 33 27 28 31 26 30 26 25 27 25
18 | 5 17 7 15 8 6 12 8 9 27 4 | 24 28 25 28 28 24 28 27 26 23 24
19E | 5 21 8 7 12 5 12 15 10 22 4 | 23 27 23 21 24 21 24 25 21 22 21
20 | 5 15 6 12 12 4 11 7 7 25 3 | 26 25 28 32 30 26 25 25 28 20 25
21 | 8 24 6 10 17 5 17 12 10 19 4 | 22 38 23 20 40 21 34 21 23 19 23
22 | 7 16 6 12 6 4 11 13 9 21 3 | 28 33 32 32 35 29 32 34 33 29 30
23 | 6 24 8 14 18 5 12 12 10 20 4 | 17 26 17 18 25 15 22 17 16 26 14
24 | 4 14 5 8 12 4 9 11 6 20 3 | 21 22 20 24 22 21 19 23 21 22 19
25 | 4 12 3 15 14 6 12 11 10 16 3 | 19 26 21 25 31 20 31 22 23 19 21
26 | 8 15 6 8 13 7 8 9 9 28 3 | 21 30 26 24 28 23 29 27 26 34 24
X27 | 12 26 11 13 --- 12 12 15 --- --- 6 | 18 36 26 25 --- 24 28 28 --- --- 23
28 | 7 19 8 7 14 5 12 8 7 32 4 | 22 33 28 23 29 23 30 25 27 30 25
29E | 8 20 8 13 15 6 16 10 10 12 4 | 17 26 18 22 23 19 22 23 22 23 19
X30 | 12 --- 12 --- 20 11 --- 14 --- --- 8 | 18 --- 24 --- 29 24 --- 19 --- --- 19
31 | 6 20 6 11 18 4 15 9 13 12 4 | 18 30 20 19 30 18 26 21 24 23 20
32 | 5 11 5 12 10 7 10 8 8 13 3 | 18 20 17 24 24 16 19 20 17 15 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 7 11 14 5 13 11 10 22 |T 24 32 26 27 32 25 31 26 27 27 24
WRMS | 7 18 7 11 14 5 13 10 8 20 |NE 20 29 23 23 29 21 27 22 23 22 20
MEDI | 7 17 7 10 14 5 12 10 10 20 |MD 21 28 23 23 28 21 26 23 23 23 21
Table 3.1649.1 GPS week: 1649 Day: 1 MJD: 55788.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 5 --- --- --- --- 21 --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- 1
2 | 4 19 8 15 14 4 13 9 8 23 4 | 32 42 40 41 50 34 43 31 37 32 36
3E | 9 16 8 10 11 4 17 11 11 22 4 | 25 26 23 26 24 24 29 27 27 26 23
4 | 5 13 7 10 10 3 14 8 8 13 3 | 33 39 41 39 40 38 41 32 38 37 36
5 | 6 13 8 8 11 6 18 9 7 24 3 | 25 31 35 30 33 25 35 23 27 27 28
6E | 9 17 6 10 13 5 17 15 10 23 4 | 142 145 143 138 147 140 149 137 138 140 141
7 | 6 21 6 17 14 5 17 9 7 17 4 | 27 38 32 35 37 30 37 29 29 29 30
8 | 7 14 5 12 13 3 11 9 8 16 3 | 24 30 28 29 26 25 32 24 24 27 25
9 | 10 14 15 6 9 6 13 18 7 24 4 | 29 34 36 31 33 30 39 34 32 41 31
10 | 4 12 6 10 10 4 9 8 7 19 3 | 28 33 34 34 33 30 34 30 31 26 31
11 | 7 15 6 10 19 5 10 9 6 15 3 | 22 29 26 22 34 22 32 22 23 25 23
12 | 7 22 7 15 14 5 18 13 9 20 4 | 23 34 26 28 31 23 29 26 27 27 24
13 | 5 16 5 9 21 3 12 13 12 12 4 | 25 30 29 30 39 26 34 28 29 26 27
14 | 7 19 12 8 17 3 12 10 10 14 4 | 21 29 30 22 32 22 28 22 25 21 22
15 | 6 25 7 7 14 4 16 12 8 18 4 | 21 30 28 28 32 24 32 21 27 24 24
16 | 9 24 7 13 15 6 16 9 10 23 4 | 25 35 28 23 29 25 33 24 29 23 25
17E | 6 17 8 12 12 5 16 7 8 17 3 | 31 40 38 40 40 35 37 34 36 35 35
18 | 7 20 7 11 9 5 14 9 9 27 4 | 26 34 27 30 31 26 36 28 28 29 27
19E | 7 20 7 12 13 4 16 13 7 16 4 | 25 32 29 30 29 27 30 27 29 28 27
20 | 5 12 5 9 11 4 11 7 5 25 3 | 25 28 30 31 27 27 30 24 29 22 26
21 | 8 25 7 8 12 5 14 9 8 18 4 | 25 43 29 26 42 26 40 25 26 22 28
22 | 7 16 6 10 9 3 11 14 8 22 3 | 29 34 32 27 33 28 37 30 27 31 29
23 | 6 24 6 7 15 4 14 13 10 20 4 | 24 33 25 24 31 23 30 24 24 29 23
24 | 5 16 6 7 12 4 12 10 10 21 3 | 22 27 26 24 27 24 27 23 26 26 23
25 | 8 12 7 18 12 4 14 8 11 15 4 | 22 31 28 28 35 23 36 24 25 25 25
26 | 6 19 7 10 8 5 11 10 9 29 4 | 33 44 42 40 41 37 43 37 40 48 38
X27 | 16 16 21 17 --- 14 45 15 --- --- 10 | 19 26 33 31 --- 26 52 24 --- --- 24
28 | 6 21 6 12 13 5 13 5 9 28 4 | 25 41 35 34 36 31 38 30 32 31 30
29E | 8 19 9 13 17 4 16 11 10 15 4 | 20 28 25 28 26 22 26 27 28 25 23
X30 | 18 --- 26 --- 26 27 --- 8 --- --- 12 | 22 --- 41 --- 29 30 --- 24 --- --- 25
31 | 5 21 10 11 18 3 17 10 9 15 4 | 23 31 29 27 35 24 34 20 26 21 24
32 | 5 11 7 9 9 6 10 7 7 12 2 | 22 26 24 24 25 22 27 23 24 22 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 11 13 4 14 11 9 20 |T 28 36 34 33 36 30 38 30 32 31 29
WRMS | 6 18 7 11 12 4 14 10 7 20 |NE 24 33 31 29 33 26 35 26 28 27 26
MEDI | 6 17 7 10 13 4 14 9 8 19 |MD 25 32 29 29 33 26 34 26 28 27 25
Table 3.1649.2 GPS week: 1649 Day: 2 MJD: 55789.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 4 --- --- --- --- 75 --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- 1
2 | 4 20 8 9 13 4 17 9 11 19 4 | 28 38 34 31 38 30 38 27 30 28 30
3E | 10 18 8 8 14 8 16 11 12 18 4 | 44 51 49 47 49 47 54 52 45 48 47
4 | 7 13 8 10 11 4 11 10 11 10 3 | 24 30 29 27 33 27 33 27 26 28 26
5 | 6 16 8 10 11 5 14 9 8 24 3 | 28 32 30 36 36 31 34 29 31 26 29
6E | 11 16 6 8 14 3 16 13 9 15 4 | 90 97 91 89 92 90 100 92 86 89 91
7 | 11 21 7 10 19 5 18 12 10 14 4 | 25 34 24 27 32 22 32 23 26 20 24
8 | 8 17 7 12 10 3 10 8 9 9 3 | 22 29 23 24 23 20 23 20 19 20 20
9 | 10 16 8 9 14 5 10 12 8 15 3 | 22 30 28 32 26 28 29 29 28 33 27
10 | 4 11 8 8 11 3 11 8 5 17 3 | 28 33 32 32 36 30 32 30 29 23 29
11 | 8 16 7 9 19 4 9 8 9 14 3 | 19 30 19 21 33 18 21 17 17 17 18
12 | 13 20 8 15 18 5 15 13 9 21 4 | 25 33 25 31 25 24 29 24 22 24 23
13 | 6 18 7 7 22 4 11 13 8 10 3 | 19 24 19 20 38 18 23 19 15 15 17
14 | 13 17 5 8 17 3 15 8 9 13 4 | 22 33 27 24 36 23 31 25 22 25 24
15 | 7 28 9 9 20 5 18 14 7 17 4 | 18 31 24 23 31 22 29 21 24 22 21
16 | 8 22 6 11 13 5 16 9 9 22 4 | 23 34 21 21 29 19 27 20 21 23 21
17E | 7 18 10 8 14 4 15 8 8 14 3 | 24 32 27 26 33 24 29 25 24 25 25
18 | 7 17 6 16 8 6 13 16 6 27 4 | 23 32 27 35 27 26 29 22 29 21 24
19E | 9 22 5 8 11 2 11 12 8 17 3 | 21 27 18 20 21 17 19 18 15 24 17
20 | 6 12 5 10 10 5 11 7 8 21 3 | 21 27 26 28 28 24 24 22 25 24 23
21 | 7 23 6 9 17 5 15 6 7 19 4 | 27 39 31 32 40 27 35 26 28 23 28
22 | 10 14 3 9 11 2 12 10 11 20 3 | 25 35 30 31 33 29 33 30 32 30 29
23 | 7 24 9 8 16 5 14 13 8 19 4 | 18 29 20 21 31 19 24 21 18 22 18
24 | 6 13 8 6 10 4 9 7 9 18 3 | 21 28 24 21 23 21 21 21 19 22 21
25 | 7 13 4 17 16 5 13 8 13 15 4 | 24 33 28 34 34 26 35 27 32 27 27
26 | 7 17 5 11 11 6 9 11 8 28 4 | 32 34 30 33 35 30 34 34 28 41 30
X27 | 15 20 11 14 --- 14 --- 14 --- --- 7 | 19 31 27 32 --- 26 --- 33 --- --- 24
28 | 8 18 7 9 14 5 12 8 9 28 4 | 22 32 25 22 33 22 31 21 21 24 22
29E | 10 20 9 14 22 3 16 12 8 11 4 | 21 32 26 31 25 24 27 23 24 26 23
X30 | 13 --- 5 --- 41 15 --- 14 --- --- 10 | 19 --- 30 --- 51 26 --- 21 --- --- 26
31 | 11 20 7 8 18 5 13 7 12 11 4 | 22 34 26 22 36 23 32 25 25 28 24
32 | 7 11 4 8 10 5 9 9 6 12 2 | 19 23 20 20 26 18 21 21 18 18 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 10 15 5 13 10 9 18 |T 24 34 28 29 34 26 32 27 26 27 25
WRMS | 8 18 7 9 14 5 13 9 7 18 |NE 22 31 26 27 32 24 29 24 24 24 23
MEDI | 7 17 7 9 14 5 13 10 9 17 |MD 22 32 27 27 33 24 29 24 25 24 24
Table 3.1649.3 GPS week: 1649 Day: 3 MJD: 55790.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 4 --- --- --- --- 102 --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- 1
2 | 7 21 9 9 17 4 16 11 7 20 4 | 31 41 36 34 43 33 40 31 31 33 33
3E | 12 20 8 8 13 7 18 33 11 25 5 | 110 116 114 111 119 114 115 100 117 113 112
4 | 6 12 8 10 14 5 11 9 9 11 3 | 27 33 36 33 39 31 32 30 35 32 31
5 | 6 15 13 9 11 6 14 11 11 25 4 | 27 34 38 35 37 32 36 33 35 31 31
6E | 9 21 5 7 10 3 17 15 9 28 4 | 132 136 132 134 134 132 136 130 130 129 131
7 | 8 19 10 11 14 6 15 10 11 15 4 | 31 39 32 36 38 33 36 32 37 30 32
8 | 7 14 7 11 18 4 10 9 11 12 3 | 26 32 27 29 31 28 30 28 32 26 27
9 | 7 18 7 8 25 3 12 12 7 15 4 | 28 34 30 31 36 29 34 34 33 35 30
10 | 6 11 7 9 14 5 10 9 10 18 3 | 31 34 37 33 39 34 35 34 36 28 33
11 | 7 21 7 8 21 6 9 9 6 15 3 | 21 35 24 20 36 21 24 21 21 21 21
12 | 7 22 9 10 17 8 14 11 12 19 4 | 26 35 26 29 27 25 29 28 30 29 26
13 | 8 18 8 10 27 4 12 11 9 12 4 | 27 33 29 30 47 28 32 30 31 27 28
14 | 5 14 7 8 21 4 13 11 7 16 3 | 21 31 27 24 40 24 30 24 28 26 25
15 | 5 24 9 12 22 4 16 14 8 17 4 | 20 29 25 26 36 22 28 25 23 26 22
16 | 7 23 8 13 13 5 16 10 9 23 4 | 22 33 24 23 27 22 29 23 25 25 22
17E | 6 15 8 8 17 4 14 8 9 12 3 | 40 42 41 42 48 42 39 42 43 42 40
18 | 6 20 6 12 10 4 14 18 9 26 4 | 28 35 31 34 33 29 35 33 33 31 29
19E | 7 19 8 10 12 4 12 12 9 16 3 | 21 25 22 21 25 20 20 20 18 24 18
20 | 5 12 7 7 13 5 11 7 7 21 3 | 26 29 28 31 29 29 27 28 29 25 27
21 | 5 19 10 9 16 3 12 9 9 20 4 | 25 38 28 28 42 26 35 27 30 24 27
22 | 6 16 5 8 11 3 12 11 7 20 3 | 28 37 33 32 39 34 39 34 35 33 32
23 | 6 24 8 8 22 5 14 12 7 20 4 | 22 32 27 25 37 23 27 27 26 29 23
24 | 4 16 10 8 14 7 9 9 8 19 3 | 20 25 24 21 23 21 21 22 21 22 20
25 | 7 15 5 20 21 5 14 8 9 16 4 | 27 34 30 35 36 27 36 29 30 28 28
26 | 6 16 10 11 15 5 12 10 8 27 4 | 40 45 46 44 46 42 47 47 45 52 43
X27 | 15 19 13 26 --- 5 17 18 --- --- 8 | 17 29 33 36 --- 25 28 32 --- --- 25
28 | 7 21 10 9 13 5 13 9 7 27 4 | 27 38 34 30 36 30 35 32 32 31 29
29E | 8 18 10 14 17 4 13 11 10 15 4 | 23 32 27 32 28 26 26 24 29 28 24
X30 | 10 --- 9 --- 22 4 --- 11 10 17 5 | 28 --- 32 --- 36 27 --- 28 18 12 28
31 | 5 17 5 8 18 4 15 8 11 12 3 | 25 31 27 29 38 24 31 24 25 25 25
32 | 6 11 7 4 12 4 10 11 5 11 2 | 22 22 23 23 25 23 23 24 21 20 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 8 10 17 5 13 12 9 19 |T 31 39 36 36 41 34 37 34 35 34 32
WRMS | 6 18 8 11 16 5 13 11 9 20 |NE 24 33 30 30 35 27 31 29 29 28 26
MEDI | 6 18 8 9 15 4 13 11 9 17 |MD 26 34 30 31 36 28 32 29 30 28 27
Table 3.1649.4 GPS week: 1649 Day: 4 MJD: 55791.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 4 --- --- --- --- 66 --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- 1
2 | 8 20 10 8 18 5 17 9 6 21 4 | 20 32 24 22 44 20 33 17 19 20 21
3 | 12 15 8 10 20 6 16 12 9 21 4 | 77 76 75 77 76 77 76 73 78 69 75
4 | 7 13 9 8 17 3 13 9 10 9 3 | 25 33 32 27 44 27 34 23 25 26 27
5 | 5 12 7 8 15 3 14 9 8 24 3 | 21 27 28 26 36 24 30 23 24 21 23
6E | 7 16 6 9 18 4 18 10 7 32 4 | 89 91 94 87 100 88 97 88 90 100 90
7 | 6 18 7 8 17 3 17 9 8 14 3 | 23 31 27 25 40 23 31 24 25 22 24
8 | 6 11 9 9 24 3 10 9 8 12 3 | 18 23 20 22 33 17 24 17 18 17 18
9 | 10 15 7 10 26 3 11 11 6 15 4 | 17 23 21 17 31 15 22 19 16 19 16
10 | 5 9 7 5 15 3 9 7 9 19 3 | 32 35 37 33 40 31 35 33 33 25 32
11 | 6 15 7 10 24 3 9 11 6 18 3 | 17 27 18 19 39 16 22 16 17 19 16
12 | 10 21 10 12 14 6 16 9 10 17 4 | 20 30 21 25 28 19 26 22 22 21 20
13 | 5 21 7 6 28 5 14 9 9 10 4 | 21 30 23 19 47 22 28 18 24 20 21
14 | 5 16 10 8 26 3 15 9 7 14 4 | 18 26 27 20 44 17 24 18 16 19 19
15 | 7 22 7 9 21 4 14 11 11 16 4 | 16 24 18 16 33 14 22 17 17 18 15
16 | 9 22 10 15 16 5 18 10 10 25 5 | 23 36 28 23 35 22 32 20 24 23 23
17E | 6 19 9 7 16 3 16 11 5 10 3 | 31 40 35 33 42 33 37 33 33 33 32
18 | 6 15 8 15 9 4 14 12 10 26 4 | 20 27 25 25 31 20 28 24 23 21 21
19E | 5 25 6 11 13 4 12 11 8 17 4 | 16 27 15 16 27 15 18 16 17 18 15
20 | 7 11 5 8 13 3 10 8 4 20 3 | 23 26 25 24 31 23 25 20 24 18 23
21 | 6 21 7 8 21 3 18 11 7 21 4 | 21 32 25 20 46 21 32 22 19 17 22
22 | 5 13 9 8 10 2 11 10 7 19 3 | 27 33 32 27 39 25 32 26 27 27 28
23 | 7 25 8 8 23 3 15 11 9 20 4 | 20 33 23 17 38 20 26 17 21 25 19
24 | 5 11 8 9 15 4 9 10 8 19 3 | 19 20 20 17 25 18 19 19 20 18 17
25 | 7 11 7 20 17 3 11 7 11 16 4 | 17 24 24 25 32 18 30 20 22 16 20
26 | 9 18 8 8 16 3 12 10 10 27 4 | 31 38 35 30 42 31 36 38 32 41 33
X27 | 12 19 15 11 24 8 16 13 --- --- 6 | 17 24 26 18 22 23 22 26 --- --- 17
28 | 7 22 10 10 15 4 14 8 8 26 4 | 19 34 29 25 35 23 32 22 22 26 23
29E | 7 21 8 13 23 4 17 11 8 17 4 | 25 32 28 29 34 24 29 25 25 26 25
X30 | 9 --- 6 9 18 5 --- 10 8 14 4 | 17 --- 23 20 26 17 --- 19 18 14 19
31 | 7 18 7 10 19 4 14 9 10 12 3 | 20 30 24 21 40 18 27 18 18 18 20
32 | 7 11 5 8 13 3 9 8 5 11 2 | 20 22 22 20 30 19 23 22 20 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 8 10 19 4 14 10 8 19 |T 24 32 29 26 39 25 31 25 26 25 24
WRMS | 7 17 8 11 17 4 13 9 7 19 |NE 20 28 25 22 35 20 27 21 21 21 20
MEDI | 7 16 8 9 17 3 14 10 8 17 |MD 20 30 25 23 36 21 28 22 22 21 21
Table 3.1649.5 GPS week: 1649 Day: 5 MJD: 55792.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 19 --- 24 --- --- 18 --- 17 --- --- 14 | 1 --- 19 --- --- --- --- 22 --- --- 1
2 | 6 23 9 10 15 4 15 8 5 23 4 | 18 28 24 21 32 21 27 17 20 24 19
3 | 8 18 7 9 20 8 17 7 10 24 4 | 62 63 60 60 71 64 65 57 60 63 61
4 | 6 16 7 7 11 5 12 9 8 11 3 | 24 27 31 26 31 26 29 21 24 25 24
5 | 6 14 7 12 13 3 17 10 9 25 4 | 18 22 27 23 26 22 28 21 22 18 20
6E | 9 20 7 9 19 5 22 10 9 34 5 | 130 133 133 133 136 133 136 132 132 139 132
7 | 4 21 5 8 15 4 14 9 5 15 3 | 27 34 29 29 35 27 34 28 29 27 27
8 | 7 14 8 8 11 4 11 10 9 11 3 | 20 27 23 23 24 20 25 22 25 22 21
9 | 8 17 7 9 17 5 11 15 11 15 4 | 22 28 23 23 28 23 26 28 29 26 22
10 | 6 12 7 9 13 5 11 8 7 20 3 | 30 32 35 30 34 31 31 30 27 28 30
11 | 7 16 4 12 18 4 11 9 8 13 3 | 19 24 19 23 27 18 22 17 18 20 16
12 | 9 22 7 14 13 6 14 10 11 22 4 | 18 29 16 20 26 18 25 17 24 19 17
13 | 6 20 6 8 21 4 15 8 8 11 3 | 21 30 23 20 35 20 30 21 23 22 21
14 | 5 19 8 10 18 3 15 9 8 12 3 | 16 28 23 22 31 18 26 17 19 19 18
15 | 7 26 8 13 16 5 17 10 9 17 4 | 17 27 22 20 26 18 25 19 15 21 16
16 | 9 23 7 18 14 7 17 9 6 29 4 | 19 34 23 24 25 22 29 20 19 26 19
17E | 6 19 9 7 13 4 19 8 10 13 4 | 40 47 44 44 44 45 47 46 48 46 43
18 | 5 15 8 12 10 4 14 14 11 27 4 | 20 24 23 23 21 19 24 23 23 18 19
19E | 5 25 7 14 11 5 11 10 8 14 3 | 13 26 14 18 19 15 17 15 17 18 13
20 | 6 12 7 11 11 3 13 9 5 21 3 | 23 24 27 26 23 22 23 20 23 17 22
21 | 5 22 8 8 15 4 16 15 9 21 4 | 19 32 23 18 32 20 29 21 18 18 19
22 | 5 15 6 10 9 4 11 6 9 19 3 | 22 29 25 24 26 21 29 21 25 20 22
23 | 6 24 7 9 16 4 21 10 7 21 4 | 18 31 22 16 26 17 28 18 19 27 17
24 | 4 11 6 8 12 6 11 11 8 18 3 | 18 19 18 17 17 17 17 19 18 15 16
25 | 10 10 6 17 14 5 13 6 9 17 3 | 18 21 19 28 29 16 29 17 18 17 17
26 | 11 17 10 11 17 6 14 31 9 36 6 | 55 60 59 56 52 55 60 65 54 60 55
X27 | 6 18 13 9 17 9 11 17 --- --- 5 | 14 21 22 22 16 19 18 23 --- --- 15
28 | 8 22 7 11 10 4 13 9 6 27 4 | 18 38 25 27 31 23 32 26 25 32 23
29E | 8 21 7 14 17 4 15 11 8 13 4 | 21 27 16 23 27 19 22 22 20 21 18
X30 | 8 --- 7 20 16 9 --- 9 7 17 4 | 22 --- 21 23 31 19 --- 19 12 8 21
31 | 7 19 12 12 17 4 16 7 12 14 4 | 19 27 27 21 31 18 26 18 16 18 18
32 | 5 11 6 9 12 4 12 10 6 12 3 | 18 20 20 22 21 18 18 19 17 17 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 11 15 5 15 11 8 20 |T 25 33 29 29 33 27 32 27 27 28 25
WRMS | 7 19 7 12 14 5 14 10 7 18 |NE 20 28 24 24 28 21 27 22 22 22 20
MEDI | 6 18 7 10 15 4 14 9 8 17 |MD 19 28 23 23 28 20 27 21 22 21 19
Table 3.1649.6 GPS week: 1649 Day: 6 MJD: 55793.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 20 --- 22 --- --- 56 --- 16 --- --- 14 | 1 --- 30 --- --- --- --- 29 --- --- 1
2 | 6 28 10 6 17 4 17 6 8 23 4 | 21 36 24 22 34 21 34 18 20 28 22
3 | 6 18 8 7 17 4 14 7 7 22 3 | 54 54 59 59 53 56 56 55 54 54 54
4 | 13 12 17 7 13 4 11 10 10 12 4 | 21 27 32 23 34 23 28 22 25 20 22
5 | 6 16 11 9 13 8 15 7 10 25 4 | 27 30 36 32 39 30 32 29 32 24 29
6E | 9 20 9 8 22 6 20 12 8 14 4 | 147 146 141 139 149 140 147 143 141 143 144
7 | 7 23 13 16 16 4 14 8 7 15 4 | 26 31 24 29 33 25 29 25 27 26 24
8 | 6 14 9 13 15 5 10 8 8 11 3 | 22 24 19 28 25 21 22 20 19 21 20
9 | 8 15 9 8 19 4 10 14 7 15 3 | 20 28 26 27 27 21 26 28 22 23 22
10 | 5 14 11 8 17 4 9 4 14 20 3 | 34 32 37 35 40 32 34 33 31 32 33
11 | 6 14 9 9 25 4 17 11 7 19 4 | 18 20 16 14 32 14 20 21 18 22 15
12 | 8 22 10 12 17 7 14 8 9 24 4 | 21 31 23 27 25 19 26 21 22 23 20
13 | 5 20 9 9 25 5 11 8 8 12 3 | 21 26 20 20 38 19 27 21 18 20 19
14 | 4 15 16 10 19 4 16 11 9 13 4 | 19 31 27 25 35 20 30 19 20 24 21
15 | 7 24 12 12 20 6 17 8 6 16 4 | 16 28 24 24 31 18 27 21 20 24 19
16 | 9 23 13 14 15 5 14 8 10 29 4 | 20 30 22 18 27 17 27 16 19 23 17
17E | 8 22 7 6 16 6 19 9 8 10 4 | 32 34 28 28 33 31 32 27 29 31 28
18 | 5 18 9 9 11 6 14 15 7 27 4 | 25 30 34 35 32 28 31 30 29 26 28
19E | 7 28 8 10 16 3 12 9 5 17 4 | 13 28 14 12 20 10 17 9 11 18 9
20 | 6 12 9 15 14 3 14 10 6 21 4 | 26 24 27 32 31 25 24 26 24 18 25
21 | 5 24 7 8 27 5 15 17 8 21 4 | 25 37 27 24 41 24 33 23 28 25 25
22 | 5 14 6 8 11 6 14 5 9 18 3 | 29 36 35 36 39 34 36 34 32 32 32
23 | 5 24 9 9 19 6 16 9 6 21 4 | 17 31 21 17 30 17 28 22 17 24 17
24 | 4 11 9 8 16 8 17 12 6 18 3 | 23 20 21 20 27 20 21 26 23 18 20
25 | 7 12 6 7 17 5 15 6 7 20 3 | 23 28 26 25 31 21 32 24 25 17 23
26 | 6 14 9 7 16 5 10 10 7 27 3 | 27 30 31 29 34 26 31 29 26 35 27
X27 | 8 16 14 10 21 9 11 16 --- --- 5 | 13 26 25 20 23 20 24 23 --- --- 17
28 | 8 21 9 10 16 7 15 8 5 29 4 | 19 31 22 23 35 20 29 20 21 29 20
29E | 7 17 8 16 15 6 13 13 7 18 4 | 34 35 34 35 35 30 32 33 34 37 33
X30 | 8 --- 8 8 15 3 --- 5 8 19 3 | 22 --- 24 15 25 20 --- 24 15 8 22
31 | 7 22 8 11 17 6 14 13 12 13 4 | 20 29 22 21 34 17 27 16 17 19 18
32 | 7 11 10 13 16 4 16 9 8 12 3 | 18 16 18 20 24 16 19 19 15 16 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 10 10 18 5 15 10 8 19 |T 26 33 30 29 36 26 32 28 27 28 26
WRMS | 7 19 10 11 18 5 14 8 7 18 |NE 21 28 25 24 31 21 27 23 22 23 21
MEDI | 7 17 9 9 16 5 14 9 8 18 |MD 21 30 25 25 33 21 28 23 22 24 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 4.1649 GPS week: 1649 MJD: 55787.0-55793.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3008 |U 14 10 32 |U 5 6 26 |U 12 10 19 |
emr | emr 2874 |U 16 13 39 |U 6 8 25 | 12 9 20 |
esa | esa 3003 | 14 13 36 |U 5 5 25 | 14 12 23 |
gfz | gfz 2914 |U 15 14 38 |U 6 7 34 |U 14 12 27 |
grg | grg 2921 | 14 13 36 |U 5 7 27 | 15 12 21 |
igr | igr 2917 | 15 13 38 | 5 5 24 | 11 10 19 |
igs | igs 2928 | 14 12 35 | 4 6 24 | 11 10 18 |
jpl | jpl 2857 |U 15 10 36 |U 5 7 26 | 11 10 22 |
mit | mit 3003 |U 94 29 242 |U 7 10 44 |U 18 14 22 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1649.0 GPS week: 1649 Day: 0 MJD: 55787.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 13 12 35 | 6 6 26 | 12 17 25 |
emr | emr 2872 | 15 10 41 | 8 8 30 | 16 13 23 |
esa | esa 2976 | 13 11 36 | 5 5 29 | 12 16 27 |
gfz | gfz 2873 | 13 11 38 | 13 12 76 | 15 17 34 |
grg | grg 2880 | 12 10 34 | 6 6 29 | 13 16 27 |
igr | igr 2880 | 14 9 39 | 5 5 26 | 11 14 24 |
igs | igs 2873 | 13 9 40 | 5 6 27 | 12 15 25 |
jpl | jpl 2867 | 14 9 46 | 5 6 30 | 12 16 30 |
mit | mit 2976 | 12 10 34 | 6 5 30 | 12 15 27 |
Table 5.1649.1 GPS week: 1649 Day: 1 MJD: 55788.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 14 10 30 | 5 8 26 | 12 11 22 |
emr | emr 2872 | 21 11 48 | 7 9 20 | 8 10 18 |
esa | esa 2976 | 14 9 28 | 5 6 20 | 10 10 21 |
gfz | gfz 2873 | 14 11 33 | 5 8 27 | 14 9 21 |
grg | grg 2880 | 14 9 26 | 5 8 23 | 10 13 22 |
igr | igr 2879 | 16 11 37 | 5 6 18 | 9 12 21 |
igs | igs 2936 | 14 9 28 | 5 7 19 | 10 10 18 |
jpl | jpl 2870 | 19 11 47 | 5 8 23 | 7 9 20 |
mit | mit 2976 | 14 9 26 | 6 9 24 | 11 10 20 |
Table 5.1649.2 GPS week: 1649 Day: 2 MJD: 55789.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3046 | 12 7 23 | 6 7 27 | 11 10 17 |
emr | emr 2871 | 14 10 26 | 6 10 31 | 9 5 17 |
esa | esa 2976 | 14 10 30 | 5 7 27 | 9 9 16 |
gfz | gfz 2872 | 13 11 34 | 5 5 33 | 9 9 16 |
grg | grg 2880 | 13 11 29 | 4 7 29 | 12 10 18 |
igr | igr 2879 | 13 10 31 | 5 6 28 | 13 12 17 |
igs | igs 2937 | 13 9 28 | 5 6 27 | 9 8 15 |
jpl | jpl 2776 | 14 8 28 | 5 8 30 | 10 8 20 |
mit | mit 2976 | 13 9 29 | 7 9 42 | 9 8 18 |
Table 5.1649.3 GPS week: 1649 Day: 3 MJD: 55790.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 11 6 23 | 6 7 27 | 12 9 18 |
emr | emr 2875 | 13 8 32 | 5 8 29 | 12 8 19 |
esa | esa 2976 | 11 7 26 | 5 6 28 | 11 9 17 |
gfz | gfz 2871 | 11 7 28 | 6 6 29 | 12 8 17 |
grg | grg 2880 | 11 8 28 | 5 8 29 | 13 8 17 |
igr | igr 2880 | 11 7 26 | 5 5 25 | 12 9 17 |
igs | igs 2975 | 11 6 25 | 5 7 28 | 13 9 18 |
jpl | jpl 2872 | 12 7 26 | 5 7 28 | 10 7 19 |
mit | mit 2976 | 10 7 31 | 6 8 37 | 14 12 18 |
Table 5.1649.4 GPS week: 1649 Day: 4 MJD: 55791.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 21 15 50 | 5 7 30 | 10 9 15 |
emr | emr 2876 | 16 14 44 | 5 7 20 | 11 9 20 |
esa | esa 2976 | 16 13 42 | 4 6 24 | 9 9 17 |
gfz | gfz 2968 | 18 16 37 | 4 5 24 | 16 11 43 |
grg | grg 2976 | 16 14 45 | 4 5 30 | 9 8 18 |
igr | igr 2904 | 18 14 45 | 4 5 23 | 9 9 17 |
igs | igs 2872 | 15 14 40 | 4 6 24 | 9 9 16 |
jpl | jpl 2870 | 15 15 41 | 5 6 24 | 10 9 20 |
mit | mit 2976 | 15 14 42 | 5 6 25 | 9 10 18 |
Table 5.1649.5 GPS week: 1649 Day: 5 MJD: 55792.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 11 9 31 | 5 5 17 | 8 9 15 |
emr | emr 2876 | 13 9 26 | 5 7 19 | 9 8 21 |
esa | esa 3072 | 13 10 34 | 4 5 19 | 8 9 15 |
gfz | gfz 2972 | 13 10 39 | 4 5 22 | 8 8 16 |
grg | grg 2976 | 12 11 35 | 5 5 25 | 8 10 17 |
igr | igr 2981 | 13 9 34 | 5 5 19 | 9 9 16 |
igs | igs 2938 | 11 9 31 | 3 4 18 | 9 9 16 |
jpl | jpl 2874 | 13 8 29 | 4 6 21 | 9 9 21 |
mit | mit 3072 | 18 14 36 | 15 31 122 | 8 8 21 |
Table 5.1649.6 GPS week: 1649 Day: 6 MJD: 55793.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 | 14 9 29 | 5 5 27 | 19 8 20 |
emr | emr 2878 | 21 28 56 | 5 7 28 | 16 11 24 |
esa | esa 3072 | 21 29 57 | 4 4 26 | 40 22 45 |
gfz | gfz 2973 | 21 30 58 | 5 7 29 | 27 20 42 |
grg | grg 2976 | 20 28 57 | 4 8 26 | 38 19 30 |
igr | igr 3016 | 21 30 57 | 5 5 26 | 16 8 20 |
igs | igs 2965 | 21 30 55 | 4 5 27 | 16 7 19 |
jpl | jpl 2872 | 16 11 37 | 5 7 28 | 17 10 26 |
mit | mit 3072 | 578 144 1495 | 5 6 32 | 64 36 35 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1649 GPS week: 1649 MJD: 55787.500-55793.500
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 -28 -1 -80 -5 | 4 29
| 14 26 70 101 7 | 4
emr uuuuu | 25 25 159 68 5 | 40 51
| 22 9 87 55 7 | 6
esa uuuuu | 2 -25 72 81 -5 | 10 32
| 11 21 47 105 5 | 4
gfz uuuuu | -40 6 -21 -78 1 | 2 30
| 17 13 65 94 5 | 5
grg uuuux | -9 -34 -53 -181 14 | 74 111
| 32 25 82 67 111 | 20
igr xxxxx | -20 -4 -10 -6 -1 | -1 27
| 14 23 44 53 6 | 5
irf xxxxx | 8 -5 -31 -5 -3 | 0 27
| 5 5 32 58 3 | 4
jpl uuuuu | -27 14 20 -85 15 | 30 41
| 36 23 58 73 8 | 6
mit uuuuu | 16 -13 -166 -33 0 | 11 30
| 8 10 71 75 4 | 5
ngs uuuuu | -2 21 45 83 -1 | 3 24
| 27 20 78 77 9 | 4
sio uuuuu | 85 35 -80 85 -14 | 39 48
| 9 9 94 129 3 | 3
Table 7.1649.0 GPS week: 1649 Day: 0 MJD: 55787.500
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 | -23 -62 -113 99 -13 | 9 27
emr uuuuu | 28 33 133 19 4 | 42 52
esa uuuuu | -6 -41 47 -31 -6 | 14 33
gfz uuuuu | -37 -11 86 78 6 | 4 30
grg uuuux | -17 -6 -214 -234 -79 | 75 100
igr xxxxx | -20 -2 15 -29 -7 | 5 25
irf xxxxx | 9 -6 -3 120 -4 | 3 26
jpl uuuuu | 4 23 -42 -56 -1 | 29 39
mit uuuuu | 16 -13 -73 99 -5 | 15 30
ngs uuuuu | -13 50 59 -46 5 | 8 24
sio uuuuu | 97 30 -144 319 -15 | 43 49
Table 7.1649.1 GPS week: 1649 Day: 1 MJD: 55788.500
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 -32 -38 -105 -11 | 7 28
emr uuuuu | 56 35 121 87 2 | 40 51
esa uuuuu | -3 9 47 91 -5 | 12 33
gfz uuuuu | -51 -12 11 -129 -2 | 3 30
grg uuuux | 25 -54 32 -105 -27 | 66 98
igr xxxxx | -26 21 -3 40 -8 | 2 26
irf xxxxx | 3 -2 -15 -2 -2 | 2 27
jpl uuuuu | 6 36 77 -131 11 | 28 39
mit uuuuu | 3 -17 -85 -15 1 | 12 31
ngs uuuuu | -27 -4 -66 45 2 | 6 24
sio uuuuu | 84 35 -123 142 -14 | 43 49
Table 7.1649.2 GPS week: 1649 Day: 2 MJD: 55789.500
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 | -16 1 -34 19 -3 | -1 31
emr uuuuu | 53 28 254 175 21 | 32 46
esa uuuuu | 13 -57 134 14 1 | 3 32
gfz uuuuu | -54 17 -6 -110 8 | -5 31
grg uuuux | 5 0 6 -224 -33 | 52 90
igr xxxxx | -6 10 16 81 0 | -7 29
irf xxxxx | 5 -1 -63 -8 3 | -6 29
jpl uuuuu | 14 39 45 -14 13 | 23 36
mit uuuuu | 12 -3 -225 -44 7 | 4 29
ngs uuuuu | -41 13 -47 126 -19 | -1 25
sio uuuuu | 81 47 -187 95 -11 | 36 47
Table 7.1649.3 GPS week: 1649 Day: 3 MJD: 55790.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -4 -41 74 -141 -4 | -2 30
emr uuuuu | 18 27 220 68 0 | 34 48
esa uuuuu | -3 -18 -3 23 -3 | 3 32
gfz uuuuu | -56 16 -2 -105 5 | -4 32
grg uuuux | 13 -59 -9 -95 134 | 53 90
igr xxxxx | -36 -16 43 7 7 | -8 29
irf xxxxx | 4 -6 -83 -32 -5 | -6 29
jpl uuuuu | -26 27 19 -21 22 | 23 36
mit uuuuu | 19 -12 -273 -40 -3 | 4 30
ngs uuuuu | 19 3 157 105 -4 | -3 25
sio uuuuu | 81 27 -146 52 -17 | 36 47
Table 7.1649.4 GPS week: 1649 Day: 4 MJD: 55791.500
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 8 42 -104 -9 | 4 29
emr uuuuu | 18 29 -4 47 3 | 42 52
esa uuuuu | 6 -28 70 143 -5 | 10 32
gfz uuuuu | -46 12 -37 -218 1 | 4 29
grg uuuux | -48 -33 -86 -207 205 | 74 113
igr xxxxx | -36 7 -16 -62 5 | -1 28
irf xxxxx | 3 -7 -32 -19 -5 | 1 27
jpl uuuuu | -49 3 100 -224 16 | 31 44
mit uuuuu | 11 -23 -169 4 0 | 11 30
ngs uuuuu | 36 29 89 178 1 | 3 23
sio uuuuu | 72 27 -43 61 -19 | 40 49
Table 7.1649.5 GPS week: 1649 Day: 5 MJD: 55792.500
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 -49 -16 -158 -2 | 5 29
emr uuuuu | 1 8 165 69 -1 | 46 54
esa uuuuu | -13 -19 97 41 -13 | 13 31
gfz uuuuu | -16 14 -99 -54 -6 | 7 28
grg uuuux | 16 -27 -60 -137 -82 | 102 144
igr xxxxx | -13 -1 -96 -19 -6 | 1 27
irf xxxxx | 16 3 -30 -34 -5 | 3 26
jpl uuuuu | -76 -18 -6 -85 18 | 36 46
mit uuuuu | 28 3 -181 -111 1 | 14 30
ngs uuuuu | 10 13 51 142 10 | 5 23
sio uuuuu | 93 47 62 37 -14 | 39 49
Table 7.1649.6 GPS week: 1649 Day: 6 MJD: 55793.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -4 -22 81 -170 6 | 4 29
emr uuuuu | 2 18 223 8 6 | 47 54
esa uuuuu | 17 -23 114 282 -1 | 11 30
gfz uuuuu | -17 4 -97 -10 -2 | 7 28
grg uuuux | -57 -61 -40 -264 -23 | 99 143
igr xxxxx | -2 -49 -26 -63 5 | 1 27
irf xxxxx | 13 -13 6 -58 -2 | 2 26
jpl uuuuu | -62 -10 -54 -63 25 | 39 49
mit uuuuu | 23 -22 -155 -124 -1 | 14 30
ngs uuuuu | 3 42 70 31 -1 | 6 24
sio uuuuu | 90 36 18 -110 -10 | 35 45
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