[IGSREPORT-21164] Wk 1703 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Sep 14 10:53:42 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1703 (Aug 26, 2012 - Sep 01, 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:
igs1703[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1703[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1703[0-6].cls IGS GPS clock combination summary report.
igs17037.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17037.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. Starting 12-Aug-2012 (GPS Week 1701, day 0, MJD 56151), GRG clocks
are included after changing their procedures to generate estimates in the
center-of-figure frame instead of the center-of-mass frame.
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 | 9 9 KARR KOUC XMIS KARR KOUC XMIS
0 | ESA | 9 9
0 | GFZ | 9 23 27 30 SUTM
0 | GRG | 27 27 BRUX
0 | JPL | 8 9 27
0 | MIT | 8 27 8 27
1 | COD | 8 9 27 8 9 27 HOB2 KOUC HOB2 KOUC
1 | EMR | 8
1 | ESA | 8 9 27 8 9 27 MATE RAMO
1 | GFZ | 8 9 23 27 LHAZ
1 | GRG | ANKR USNO ANKR KOUC MATE NRMD SANT USNO WIND
1 | JPL | NKLG
1 | MIT | KARR
2 | EMR | 9 27 9 27
2 | ESA | CHUR DRAG NNOR
2 | GFZ | 9 23 27 IRKJ REUN
2 | GRG | 9 13 CHUR DUBO
2 | JPL | 9 REUN
2 | MIT | 9 IRKJ WROC IRKJ WROC
3 | EMR | 9 27 9 27
3 | ESA | PRDS AREQ IRKJ NNOR PRDS REUN
3 | GFZ | 9 27 PRDS UNSA
3 | GRG | BRUX IRKJ
3 | JPL | 9 27
3 | MIT | IENG IRKJ IENG KARR
4 | COD | 9 9 KOUC ONSA KOUC
4 | EMR | 27 27 ONSA ONSA
4 | ESA | 9 9 PALM PALM
4 | GFZ | 9 23 27 INVK NKLG
4 | GRG | SOFI SOFI
4 | JPL | 27
4 | MIT | 21 22 19 21 22 ONSA BOR1 ONSA
5 | COD | 9 9 KOUC KOUC SCH2
5 | EMR | 27 27 THTI
5 | ESA | 9 9 AREQ
5 | GFZ | 8 9 23 27 30 IRKJ MDVJ SCH2
5 | GRG | 27 ARTU CEDU KIT3 SCH2
5 | MIT | 27 27 IRKJ SANT BOR1 IRKJ
6 | COD | 9 9 KOUC KOUC
6 | EMR | 11 27 11 27
6 | ESA | 9 9 PALM AREQ BJFS MATE NNOR PALM
6 | GFZ | 9 23 27 AREQ ASPA GOLD LHAZ MATE
6 | GRG | AREQ MATE
6 | MIT | 27 27
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
----+------------+----------
G21 | 2012_08_28 | 2012052
G21 | 2012_08_29 | 2012052
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
7. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the current IGS reference frame. These rotations were
estimated in the IGS SINEX combination process, performed by the IGS Reference
Frame Coordinator at the Institut Geographique National (IGN). Starting on
19-Aug-2012 (GPS Week 1702; mjd=56158), ACs began contributing products based
on 1d SINEX integrations. As a result, the SINEX combinations are now done
daily instead of weekly, and the associated daily rotations are applied here
to the orbits and ERPs. 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 | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
EMR | 0 | 3.9 -5.5 4.7 -1 2 6 -.16
ESA | 0 | .6 1.8 20.4 47 20 100 -.37
GFZ | 0 | -1.0 1.2 .5 -60 -6 -17 -.52
GRG | 0 | .6 -10.9 17.3 -18 17 -1 -.14
JPL | 0 | -1.8 3.3 -.1 12 7 -39 -.25
MIT | 0 | 2.5 1.8 11.9 -14 19 -39 -.26
NGS | 0 | 10.3 -7.9 14.3 -118 -86 22 -.15
EMR | 1 | -4.0 -2.0 2.5 -3 -2 -2 -.08
ESA | 1 | -2.1 4.5 20.2 70 64 86 -.49
GFZ | 1 | -.8 1.1 .8 -77 -13 -15 -.58
GRG | 1 | -.5 -9.2 25.3 -60 -7 14 -.28
JPL | 1 | -6.5 1.9 3.9 9 -6 -43 -.12
MIT | 1 | -.3 3.5 12.9 -14 14 -31 -.40
NGS | 1 | 1.1 .8 9.5 -43 -15 -12 -.26
EMR | 2 | -.1 -6.2 4.0 1 4 -5 -.23
ESA | 2 | 1.0 1.6 20.5 42 11 105 -.36
GFZ | 2 | -.7 1.0 -.4 -67 -10 -28 -.38
GRG | 2 | 3.2 -5.6 25.3 -22 20 -45 -.40
JPL | 2 | -5.5 6.9 4.3 3 -19 12 -.29
MIT | 2 | 6.1 2.1 10.2 -15 20 -29 -.34
NGS | 2 | -.7 -4.5 16.8 -89 0 -11 -.09
EMR | 3 | -5.1 -7.0 10.8 -15 6 -10 -.17
ESA | 3 | .7 3.9 23.4 73 35 79 -.55
GFZ | 3 | -1.2 1.3 -.6 -50 -10 -30 -.43
GRG | 3 | .0 -8.9 36.9 -26 24 -29 -.48
JPL | 3 | .0 11.5 8.2 -72 13 -10 -.12
MIT | 3 | 1.5 3.4 11.2 -6 9 -36 -.34
NGS | 3 | 2.2 -1.2 18.8 -68 -27 2 -.09
EMR | 4 | 1.8 -6.4 1.7 -1 16 -10 -.09
ESA | 4 | .1 3.6 15.8 79 12 92 -.32
GFZ | 4 | -1.7 .5 -.5 -60 -1 -16 -.37
GRG | 4 | 4.8 -10.0 21.4 -25 41 -41 -.20
JPL | 4 | -3.3 7.7 1.4 -52 -52 -50 -.12
MIT | 4 | 1.5 5.9 10.8 -17 7 -44 -.24
NGS | 4 | 4.8 .5 8.7 -19 -46 13 .04
EMR | 5 | 6.5 2.1 4.3 -7 15 -2 .01
ESA | 5 | -2.2 4.3 23.8 81 103 82 -.55
GFZ | 5 | -.4 1.0 .2 -64 9 -32 -.35
GRG | 5 | 1.9 -4.8 10.2 -35 44 -32 -.16
JPL | 5 | -.7 8.8 2.2 -45 -6 -103 .17
MIT | 5 | 5.5 5.7 11.2 -12 14 -35 -.27
NGS | 5 | 7.4 3.4 16.3 -2 -68 24 .09
EMR | 6 | .6 2.2 3.0 -8 12 -5 -.11
ESA | 6 | -2.7 2.6 20.4 75 67 109 -.64
GFZ | 6 | -.9 1.2 .3 -63 -8 -16 -.57
GRG | 6 | -4.7 3.4 21.6 -47 40 -10 -.17
JPL | 6 | -1.3 1.5 .8 -52 16 -41 -.01
MIT | 6 | 2.8 3.7 11.9 -18 12 -49 -.17
NGS | 6 | -.8 .4 18.6 -30 -5 -7 -.02
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 daily X- and Y-rotations, i.e. RX_sp3(ac) and
RY_sp3(ac), used to align each daily AC orbit to the combined SINEX prior to
the orbit combination. These a-priori rotations are derived from three sources:
the daily AC polar motion estimates, XPO(ac) and YPO(ac), provided in their ERP
files; the combined polar motion values, XPO(cmb) and YPO(cmb), from the SINEX
combination; along with the AC TRF rotations, RX_snx(ac) and RY(ac), also from
the SINEX combination:
RX_sp3(ac) = YPO(ac) - YPO(cmb) + RX_snx(ac)
RY_sp3(ac) = XPO(ac) - XPO(cmb) + RY_snx(ac)
Thus, 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.
Starting on 19-Aug-2012 (GPS Week 1702; mjd=56158), the AC TRF rotations are
daily values, instead of weekly ones, based on the combination of daily AC
SINEX files.
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 1.1703.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1703.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 2.1703.[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 3.1703.[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 5.1703.0-6).
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 1703 summary. (Aug 26, 2012 - Sep 01, 2012)
Table 1.1703.a GPS week: 1703 MJD: 56165.000-56171.000
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 259| 0 0 2 -33 14 24 -.53 12 11 | -441 15 26 72
| 0 0 1 20 33 31 .03 | 327 389
emr 78| -1 -2 -1 -10 -32 -10 .12 17 17 | 1033 1209 18 107
| 2 2 1 19 34 11 .04 | 1538 1011
esa 177| 0 0 0 -144 -18 7 .01 9 8 | -12 227 24 144
| 1 1 1 39 59 14 .04 | 1525 1661
gfz 187| -1 2 -3 94 -11 -9 -.44 11 10 | 81 314 24 134
| 0 0 1 42 38 10 .03 | 347 807
grg 117| 2 0 10 27 -21 15 .32 15 15 | -17 197 25 158
| 0 0 1 31 22 33 .03 | 213 316
igr n/a| 0 0 0 -16 4 -19 -.18 5 5 | 6623 1077 23 87
| 0 0 1 6 24 12 .01 | 1411 990
jpl 80| 0 0 -1 43 9 7 .34 15 14 | 2446 1309 22 124
| 0 1 1 69 45 9 .04 | 1692 978
mit 239| 0 0 -1 -11 -22 -8 -.21 9 8 | -124 176 29 172
| 0 0 1 33 35 16 .03 | 148 315
ngs 235| -1 0 0 93 94 -7 .25 11 9 | -430 -42 2016 3729
| 0 0 3 91 79 26 .05 | 315 339
sio 269| 1 0 1 -43 12 -24 -.19 22 20 | --- --- --- ---
| 0 1 0 23 28 17 .01 | --- ---
Table 1.1703.b GPS week : 1703 MJD: 56165.000-56171.000
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 5 5 5 5 5 5 |
2 | 5 5 5 5 5 4 5 |
3 | 3 4 4 5 4 4 4 |
4 | 4 5 4 5 5 5 6 |
5 | 5 4 5 4 4 5 4 |
6 | 4 4 4 4 4 4 4 |
7 | 5 5 6 6 5 5 5 |
8 | 5 5 5 5 5 5 4 |
9 | 6 6 6 7 6 6 6 |
10 | 4 4 4 4 4 4 4 |
11 | 4 5 4 5 5 5 5 |
12 | 5 5 6 5 6 6 6 |
13 | 5 5 5 5 5 5 5 |
14 | 5 5 5 5 6 5 5 |
15 | 6 5 6 6 6 5 5 |
16 | 5 5 5 7 6 7 6 |
17 | 5 4 5 5 5 4 5 |
18 | 4 4 5 5 5 5 5 |
19 | 5 4 5 6 6 6 5 |
20 | 4 4 5 5 5 5 4 |
21 | 5 5 7 --- 4 5 5 |
22 | 4 4 5 5 5 5 5 |
23 | 5 5 5 5 5 6 5 |
25 | 5 5 5 5 5 6 5 |
26 | 5 4 4 5 4 4 4 |
27 | 6 7 7 7 6 6 6 |
28 | 5 5 4 5 5 5 5 |
29 | 5 5 6 5 6 6 6 |
30 | 4 4 4 5 5 4 4 |
31 | 5 5 6 6 6 6 6 |
32 | 4 4 4 5 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1703.0 GPS week: 1703 Day: 0 MJD: 56165.000
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 259| 0 0 3 -20 0 11 -.50 12 11 | -586 160 23 72
| 51 -31 |
emr 78| -2 -1 -3 -12 -51 -13 .15 16 16 | 494 -526 21 117
| 31 -5 |
esa 177| 1 0 0 -78 30 -14 .03 8 8 | 757 -1260 19 120
| 43 -53 |
gfz 191| -1 1 -3 32 -17 -7 -.39 11 11 | 733 -422 23 137
| -50 -3 |
grg 122| 1 0 8 1 -35 37 .31 15 14 | 349 -227 23 172
| -1 -38 |
igr n/a| 0 0 0 -11 3 -39 -.17 5 4 | 6260 -706 21 107
| 14 9 |
jpl 80| 1 0 -1 -23 -35 -1 .40 15 14 | 1577 -538 20 117
| 21 -2 |
mit 240| 0 1 0 -68 -79 17 -.24 7 6 | 73 25 21 171
| 9 22 |
ngs 238| 0 -1 0 256 223 -6 .23 12 9 | -412 -222 2067 3563
| -99 -37 |
sio 279| 2 0 1 -75 -21 -1 -.18 22 20 | --- --- --- ---
| 35 -33 |
Table 2.1703.1 GPS week: 1703 Day: 1 MJD: 56166.000
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 259| 0 0 2 -35 6 43 -.51 12 11 | 154 -666 17 73
| 129 -14 |
emr 78| -3 0 -1 -46 -27 -14 .12 16 16 | -797 2169 18 124
| 43 1 |
esa 177| 0 -2 -1 -161 -64 0 .03 10 9 | 2805 -1010 19 128
| 43 13 |
gfz 189| -1 2 -3 113 3 -20 -.43 11 10 | -341 1782 22 138
| -24 5 |
grg 121| 1 1 12 65 17 70 .35 14 14 | -142 653 19 165
| -1 -51 |
igr n/a| 0 0 0 -17 13 -17 -.19 5 4 | 4903 2053 21 102
| 27 -19 |
jpl 80| 0 1 -1 -48 8 -1 .36 14 13 | 636 1984 20 125
| 28 11 |
mit 240| 0 0 0 21 2 11 -.24 6 6 | -246 590 24 180
| 6 6 |
ngs 238| 0 0 -1 70 59 -41 .23 11 9 | 57 -571 2259 3961
| -70 31 |
sio 275| 0 0 2 -8 46 -23 -.20 22 21 | --- --- --- ---
| 36 -69 |
Table 2.1703.2 GPS week: 1703 Day: 2 MJD: 56167.000
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 259| 0 0 1 -16 4 -23 -.52 12 10 | -770 231 29 68
| 80 -27 |
emr 78| -2 -2 0 -8 -34 -19 .15 17 17 | -273 1853 20 108
| 34 -9 |
esa 177| 0 0 0 -98 48 32 .05 7 7 | -895 2129 25 127
| 46 -56 |
gfz 189| 0 1 -6 99 10 -26 -.44 11 10 | -40 717 23 127
| -15 -31 |
grg 118| 1 0 10 15 -29 -34 .33 16 16 | -289 540 26 140
| 32 -59 |
igr n/a| 0 0 0 -5 -5 -31 -.17 5 5 | 5341 1708 22 75
| 37 -13 |
jpl 80| 0 0 -1 -15 26 24 .38 15 14 | 969 1777 23 110
| 46 -35 |
mit 240| 1 0 0 -29 -62 -12 -.19 9 8 | -307 343 29 168
| 2 31 |
ngs 236| -1 0 1 168 26 -1 .23 13 11 | -874 438 1872 3605
| -118 17 |
sio 267| 1 0 2 -52 -1 -32 -.20 20 19 | --- --- --- ---
| 32 -62 |
Table 2.1703.3 GPS week: 1703 Day: 3 MJD: 56168.000
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 259| -1 0 1 -72 -7 78 -.53 13 12 | -671 108 28 75
| 122 -7 |
emr 80| -3 -5 0 -17 -44 8 .16 17 17 | 999 344 16 98
| 23 0 |
esa 177| 0 1 0 -189 16 11 .03 8 8 | -287 479 28 171
| 71 -51 |
gfz 186| 0 4 -4 129 52 0 -.43 11 10 | 78 -158 27 138
| -15 -33 |
grg 118| 3 -1 10 -14 -33 19 .26 17 18 | -143 93 27 144
| 53 -44 |
igr n/a| 1 0 0 -25 -9 -19 -.19 5 5 | 6507 526 24 83
| 8 -1 |
jpl 80| 0 -1 -3 113 -41 3 .36 15 14 | 2200 736 25 140
| -14 -20 |
mit 240| 2 0 -2 23 -21 -16 -.24 11 10 | -156 48 30 165
| -20 27 |
ngs 234| 0 0 3 91 32 -45 .18 12 10 | -773 231 1610 3485
| -74 16 |
sio 267| 1 -1 1 -38 -4 -39 -.18 20 20 | --- --- --- ---
| 17 -39 |
Table 2.1703.4 GPS week: 1703 Day: 4 MJD: 56169.000
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 259| -1 0 3 -33 -23 13 -.54 12 11 | -371 -174 30 86
| 89 16 |
emr 79| -2 -3 0 8 -89 -17 .07 17 17 | 613 2232 20 118
| -43 -6 |
esa 177| 0 0 0 -162 5 15 -.02 9 8 | -777 196 26 190
| 71 -24 |
gfz 185| -2 2 -1 141 -25 0 -.49 10 9 | -130 413 25 138
| -43 -10 |
grg 115| 3 0 11 17 -46 -5 .30 15 15 | -66 -91 23 172
| 26 -46 |
igr n/a| 0 0 0 -20 -35 -15 -.19 4 4 | 6333 2085 25 78
| 18 12 |
jpl 80| 0 -1 0 104 78 11 .32 15 14 | 2201 2413 22 135
| -28 -51 |
mit 240| 0 0 0 -17 -7 -29 -.18 9 9 | -203 -33 35 200
| 8 10 |
ngs 235| -2 0 -5 7 46 29 .29 12 9 | -409 -240 2103 3933
| -66 6 |
sio 263| 1 1 0 -56 -7 -42 -.19 21 20 | --- --- --- ---
| 14 -42 |
Table 2.1703.5 GPS week: 1703 Day: 5 MJD: 56170.000
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 259| 0 0 3 -39 66 22 -.54 11 10 | -198 -124 30 71
| 108 -5 |
emr 78| 0 -4 -1 -10 11 -19 .07 17 17 | 2845 1187 17 97
| 7 -5 |
esa 177| -1 0 0 -157 -117 11 -.02 9 9 | 301 -1588 26 132
| 28 45 |
gfz 183| 0 2 -3 105 -69 -7 -.46 10 8 | 303 -580 25 131
| -2 -7 |
grg 115| 2 0 12 36 3 3 .35 16 15 | 12 197 25 155
| 3 -68 |
igr n/a| 0 0 -1 -12 38 -2 -.20 5 5 | 8476 924 25 85
| 12 -12 |
jpl 80| 1 -2 -1 74 52 3 .29 15 14 | 4644 1182 23 116
| 11 -23 |
mit 239| 0 0 -2 15 0 -14 -.22 12 12 | 70 -263 32 156
| -2 27 |
ngs 232| -1 1 0 -1 192 1 .31 11 9 | -221 -73 2060 3951
| -5 30 |
sio 268| 3 1 0 -15 34 -34 -.18 22 21 | --- --- --- ---
| 5 -64 |
Table 2.1703.6 GPS week: 1703 Day: 6 MJD: 56171.000
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 259| 0 -1 1 -13 53 26 -.59 11 10 | -648 575 27 63
| 108 12 |
emr 79| 1 0 -2 13 7 2 .14 17 17 | 3356 1207 19 87
| -19 -14 |
esa 177| -1 -2 -2 -164 -45 -1 -.06 10 9 | -1988 2646 27 140
| 40 31 |
gfz 186| -1 1 -1 38 -31 -6 -.46 11 10 | -31 446 25 130
| 8 -3 |
grg 115| 2 0 8 69 -23 20 .35 15 15 | 160 218 35 161
| -26 -50 |
igr n/a| 0 0 -1 -21 25 -9 -.16 6 5 | 8545 952 24 81
| 18 15 |
jpl 80| 0 1 -3 96 -20 10 .29 15 14 | 4901 1614 25 126
| 2 10 |
mit 240| 0 0 -2 -28 12 -13 -.17 8 8 | -103 525 32 166
| 17 4 |
ngs 234| -1 0 5 59 83 9 .31 11 9 | -383 141 2141 3605
| -22 14 |
sio 268| 1 3 0 -53 45 0 -.19 23 20 | --- --- --- ---
| 22 -73 |
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 3.1703.0 GPS week: 1703 Day: 0 MJD: 56165.000
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 24 8 10 13 5 13 8 11 12 5 | 36 34 37 33 36 33 36 33 36 32 33
2 | 12 16 9 12 14 4 18 5 9 21 4 | 14 20 14 15 19 12 20 12 19 13 12
3 | 6 8 6 9 13 6 10 6 7 21 3 | 19 21 20 21 21 18 21 18 22 18 18
4 | 13 11 6 13 11 4 11 7 17 21 4 | 21 28 23 21 23 22 28 22 29 32 22
5 | 8 14 9 13 13 4 13 5 15 38 4 | 20 31 24 25 30 22 30 23 22 29 24
6 | 8 9 7 9 12 4 10 6 7 18 3 | 21 27 22 19 24 19 25 20 24 21 21
7E | 11 19 6 13 16 5 17 7 13 28 5 | 16 31 23 18 25 20 28 18 33 39 22
8E | 17 14 8 14 14 6 14 9 10 18 4 | 45 47 47 48 47 47 48 45 53 49 47
9E | 22 18 12 10 16 7 15 10 19 26 5 | 57 65 63 59 69 58 65 62 63 76 62
10 | 12 9 7 13 13 2 10 5 9 21 3 | 23 26 28 28 33 28 28 27 32 22 28
11E | 12 15 6 10 14 4 11 5 9 12 4 | 28 29 26 21 29 23 28 23 32 27 25
12 | 12 17 10 13 15 6 16 11 13 27 5 | 18 26 24 27 23 20 25 21 22 22 21
13 | 8 18 7 10 16 5 16 6 10 23 4 | 21 32 23 19 37 21 35 20 27 19 24
14 | 10 17 7 13 12 4 18 6 12 24 4 | 18 25 22 27 30 20 24 22 26 17 21
15 | 15 23 10 14 15 5 18 9 12 25 5 | 26 28 25 24 29 23 26 25 19 21 21
16 | 12 16 10 14 15 4 16 7 10 28 5 | 20 26 23 27 23 20 28 17 22 21 20
17 | 14 15 6 12 16 6 18 8 9 15 4 | 18 26 17 12 26 17 29 17 25 18 18
18 | 8 12 7 12 13 4 14 5 10 23 4 | 19 32 27 20 28 22 30 24 27 16 24
19 | 9 17 7 11 20 3 15 6 12 20 4 | 19 27 15 12 24 15 24 14 19 16 15
20 | 11 12 6 11 15 3 17 6 11 25 4 | 23 28 24 23 28 23 30 23 29 21 24
21 | 8 15 7 12 17 4 12 6 13 18 4 | 12 19 16 10 16 13 17 13 16 9 15
22 | 7 15 7 8 9 3 13 6 8 24 3 | 23 31 28 24 33 26 31 26 32 28 27
23 | 9 18 8 13 16 4 21 7 10 23 5 | 18 27 23 18 27 18 30 16 23 17 19
25 | 9 24 7 9 14 5 13 8 9 19 4 | 21 28 26 26 33 25 34 27 26 21 26
26 | 9 11 12 11 11 3 12 6 16 16 4 | 21 24 29 25 29 24 24 25 19 23 23
27E | 22 20 11 11 16 7 16 11 17 20 5 | 48 60 55 50 62 51 62 53 55 63 54
28 | 14 16 8 12 16 4 18 5 10 26 4 | 19 30 32 33 30 26 30 24 28 27 27
29 | 15 21 9 12 16 5 18 7 13 22 5 | 14 26 16 13 22 13 25 15 26 17 15
30 | 7 9 6 9 13 4 9 4 11 15 3 | 24 23 23 25 25 21 25 21 25 23 22
31E | 11 18 6 10 18 4 21 8 11 14 5 | 18 25 25 15 30 20 26 17 31 24 21
32 | 10 14 7 9 15 4 10 6 8 19 4 | 25 24 20 22 27 22 24 19 20 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 8 11 15 5 15 7 12 22 |T 23 29 26 24 30 23 30 23 28 25 24
WRMS | 11 16 8 11 14 4 14 6 9 20 |NE 20 27 23 22 27 21 27 21 24 20 21
MEDI | 11 16 7 12 15 4 15 6 11 21 |MD 21 27 24 23 28 22 28 22 26 21 22
Table 3.1703.1 GPS week: 1703 Day: 1 MJD: 56166.000
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 25 10 10 15 5 10 6 9 12 4 | 21 28 25 23 29 22 26 23 24 25 22
2 | 12 12 13 12 15 3 17 4 11 17 4 | 15 21 20 19 16 15 20 15 17 19 15
3 | 10 11 8 10 12 6 12 5 7 23 3 | 15 17 16 17 14 14 19 15 20 20 14
4 | 12 13 8 12 11 4 13 7 14 22 4 | 25 36 26 30 29 26 32 26 32 35 28
5 | 10 15 10 12 11 4 13 6 9 35 4 | 17 29 24 23 26 20 29 20 26 27 22
6 | 10 11 7 10 11 6 10 5 6 19 3 | 14 24 17 15 18 15 22 14 22 23 16
7E | 10 24 7 10 15 4 14 8 12 33 5 | 13 27 22 14 22 16 23 18 27 33 19
8E | 16 15 9 12 13 5 13 10 9 18 4 | 43 40 39 39 40 41 42 40 40 41 39
9E | 23 18 17 11 17 7 17 9 21 27 6 | 76 80 80 79 90 82 87 81 84 90 81
10 | 9 8 5 9 13 3 9 5 11 17 3 | 22 29 26 27 29 25 29 23 29 28 26
11E | 11 16 11 10 18 4 10 5 9 15 4 | 14 23 17 17 20 14 17 15 20 20 14
12 | 16 15 9 12 13 8 17 6 11 25 4 | 16 25 18 22 20 16 23 16 20 20 17
13 | 7 16 12 9 18 4 14 5 12 23 4 | 21 33 21 17 37 19 34 19 23 18 22
14 | 11 16 7 14 14 4 17 5 8 18 4 | 16 23 17 21 26 15 23 16 19 15 16
15 | 9 19 10 14 13 6 18 7 11 23 5 | 18 27 22 23 24 19 23 18 22 21 19
16 | 12 17 10 15 12 7 17 7 7 27 4 | 14 23 17 20 19 15 23 14 19 14 15
17 | 12 14 8 12 15 5 13 5 11 16 4 | 13 24 19 13 26 14 24 17 24 19 18
18 | 8 13 6 12 10 4 14 4 9 22 3 | 15 29 23 13 25 17 29 18 24 17 20
19 | 8 16 9 12 17 3 13 5 7 20 4 | 14 22 13 14 22 12 21 12 18 15 13
20 | 10 13 7 11 15 4 14 6 11 22 4 | 16 24 21 20 22 17 26 18 25 16 19
21 | 9 19 7 13 16 4 15 5 10 15 4 | 9 18 11 8 8 8 15 9 13 7 10
22 | 8 12 7 8 9 4 14 6 11 24 3 | 20 30 23 17 30 21 31 22 25 28 23
23 | 8 18 10 12 13 4 16 6 12 23 4 | 13 23 15 13 23 12 23 13 16 15 13
25 | 13 25 8 10 17 5 13 6 7 16 5 | 22 29 23 19 27 18 33 19 20 23 20
26 | 11 11 11 11 12 5 9 5 11 15 4 | 17 22 24 25 23 20 21 20 23 24 21
27E | 23 17 21 14 18 8 16 10 19 23 6 | 65 68 67 66 77 69 74 68 68 75 67
28 | 14 14 10 11 12 4 15 6 10 27 4 | 17 28 24 26 27 21 29 23 26 25 24
29 | 11 19 14 11 12 4 15 6 12 23 5 | 16 24 14 13 21 15 21 16 21 16 15
30 | 10 9 9 9 12 5 9 6 8 16 3 | 18 18 17 17 17 17 19 19 24 19 17
31E | 10 15 7 10 22 5 15 5 10 16 4 | 16 25 20 20 21 16 23 15 24 21 18
32 | 8 15 9 9 17 4 8 5 11 19 4 | 22 26 24 23 26 21 23 19 22 27 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 10 11 14 5 14 6 11 22 |T 21 28 24 23 27 21 28 21 26 25 22
WRMS | 10 16 9 10 13 4 13 6 9 21 |NE 16 25 19 18 23 17 25 17 22 20 18
MEDI | 10 15 9 11 13 4 14 6 11 22 |MD 16 25 21 20 24 17 23 18 23 21 19
Table 3.1703.2 GPS week: 1703 Day: 2 MJD: 56167.000
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 24 4 7 15 5 12 7 13 10 4 | 35 37 38 35 38 37 38 36 38 38 36
2 | 11 13 7 9 22 4 15 7 12 18 4 | 16 20 19 18 27 18 23 19 22 22 18
3 | 9 11 6 13 13 7 12 6 10 17 4 | 11 17 14 20 19 15 16 13 23 17 14
4 | 12 13 5 8 15 4 11 9 12 22 4 | 30 36 32 29 34 31 37 31 32 42 31
5 | 12 15 8 10 15 4 14 9 13 35 4 | 20 30 26 21 31 23 31 24 29 24 24
6 | 9 10 5 9 13 6 10 5 10 16 3 | 13 23 17 18 23 17 23 16 26 21 18
7E | 13 25 5 13 15 4 18 11 14 15 5 | 11 31 22 18 28 18 22 22 25 22 19
8E | 16 11 8 12 18 6 12 12 13 18 5 | 22 30 25 26 28 27 31 31 28 31 26
9E | 32 16 11 14 21 8 19 12 21 18 6 | 76 89 85 82 86 80 90 89 93 90 86
10 | 8 8 3 9 16 3 9 7 10 20 3 | 20 26 25 22 30 22 26 22 24 22 23
11E | 6 19 4 8 16 5 12 6 12 9 4 | 17 28 21 17 27 20 23 18 25 22 19
12 | 13 19 8 14 17 6 19 10 11 24 5 | 16 27 19 27 21 16 25 19 23 19 18
13 | 6 14 7 12 18 4 16 7 13 23 4 | 23 36 28 28 42 27 38 28 31 28 29
14 | 10 20 7 14 16 4 16 8 11 16 5 | 14 26 18 23 28 17 24 20 24 16 19
15 | 10 20 10 12 15 5 19 9 12 22 5 | 18 26 22 21 25 18 25 20 23 21 19
16 | 12 16 9 15 13 4 19 8 12 26 5 | 16 24 21 24 24 18 26 17 20 17 18
17 | 7 14 7 10 16 3 17 10 9 17 4 | 13 24 25 13 28 18 29 18 23 16 20
18 | 9 16 6 14 11 4 14 9 14 24 4 | 16 33 23 18 27 22 31 26 35 20 24
19 | 9 16 8 12 19 5 17 7 12 19 5 | 13 25 18 13 24 15 24 13 25 15 15
20 | 7 13 5 13 17 3 16 8 12 19 4 | 17 26 22 21 25 20 26 21 29 18 21
X21 | 8 --- 6 --- --- 6 --- 7 --- --- 7 | 7 --- 11 --- --- 9 --- 13 --- --- 11
22 | 10 20 5 9 12 5 15 7 11 25 4 | 21 33 26 21 34 26 34 28 36 32 28
23 | 6 14 7 12 16 4 19 8 10 23 4 | 11 22 18 16 23 15 24 15 18 14 15
25 | 13 28 5 8 19 5 13 7 8 18 5 | 17 30 24 25 28 21 32 23 25 22 23
26 | 7 10 10 8 13 2 9 7 11 16 4 | 17 19 24 20 23 18 22 20 22 25 19
27E | 22 15 10 15 18 10 18 14 24 19 6 | 61 75 68 66 69 65 74 73 79 77 69
28 | 12 13 7 9 14 5 17 8 9 28 4 | 17 28 28 28 29 25 29 23 27 25 25
29 | 15 22 10 13 14 4 18 8 14 23 5 | 15 28 18 17 22 15 24 18 26 18 17
30 | 13 11 6 10 14 4 9 8 10 15 3 | 14 18 18 18 20 16 22 15 23 18 17
31E | 12 21 5 13 24 5 17 8 11 11 5 | 16 27 22 15 26 18 24 22 25 24 19
32 | 8 15 7 8 18 3 10 9 11 15 4 | 15 23 20 18 25 18 23 18 24 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 7 11 16 5 15 9 13 20 |T 20 30 25 24 30 23 30 24 30 26 24
WRMS | 10 17 7 10 16 5 14 8 11 19 |NE 16 25 21 20 26 19 26 19 25 20 20
MEDI | 10 15 7 12 16 4 15 8 12 18 |MD 16 27 22 21 27 18 25 20 25 22 19
Table 3.1703.3 GPS week: 1703 Day: 3 MJD: 56168.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 24 7 8 19 4 14 8 10 13 5 | 25 24 26 23 31 24 28 26 26 23 24
2 | 12 13 6 8 14 6 16 9 13 16 4 | 23 28 28 26 29 26 30 29 29 32 27
3 | 9 10 7 13 19 6 12 14 9 16 4 | 17 19 18 20 20 16 17 23 16 20 16
4 | 10 16 5 9 14 6 14 12 11 23 4 | 23 34 23 22 26 21 30 27 26 36 25
5 | 10 15 6 9 12 5 13 10 10 34 4 | 19 30 25 22 29 23 29 26 30 25 24
6 | 8 10 6 10 14 4 10 10 9 15 4 | 14 20 18 16 21 15 20 21 17 20 16
7E | 14 23 6 10 15 6 17 13 13 15 5 | 18 31 24 16 24 18 26 25 26 20 21
8E | 21 12 7 13 14 5 14 13 14 19 5 | 54 51 49 47 53 49 51 53 55 51 50
9E | 17 19 16 15 21 9 18 8 22 19 6 | 87 95 94 87 94 90 96 91 93 93 91
10 | 12 9 6 8 15 4 9 11 9 19 4 | 20 30 30 27 32 25 27 28 27 22 27
11E | 7 18 7 8 14 6 12 9 11 13 4 | 13 27 21 15 25 15 21 17 20 23 17
12 | 14 17 8 13 19 10 18 7 10 21 5 | 23 31 23 30 23 21 30 22 24 21 22
13 | 6 13 5 10 17 5 13 9 12 21 4 | 26 33 30 28 39 28 36 32 31 25 30
14 | 11 19 6 11 17 3 18 8 9 18 5 | 22 28 25 23 28 20 27 22 20 19 21
15 | 15 19 10 11 17 4 20 11 13 24 5 | 18 34 29 23 28 22 29 28 26 22 24
16 | 12 21 12 16 16 5 20 14 14 26 6 | 19 24 25 27 25 21 25 25 21 18 21
17 | 11 16 5 8 18 4 13 12 9 19 4 | 12 27 18 13 26 15 25 19 25 18 18
18 | 17 19 8 13 14 3 16 10 10 23 5 | 18 35 28 21 25 22 31 26 27 19 24
19 | 10 16 8 12 22 4 12 15 11 18 5 | 16 25 19 13 22 14 21 22 20 17 15
20 | 8 13 8 15 18 3 15 10 9 16 5 | 15 24 24 23 25 19 27 22 24 12 21
22 | 19 18 6 10 14 5 16 10 13 25 4 | 23 31 27 21 30 24 31 26 27 31 25
23 | 7 15 6 12 16 5 17 10 10 21 4 | 14 24 18 18 24 15 27 18 15 13 16
25 | 12 24 6 9 19 5 15 9 9 19 5 | 24 31 29 32 32 26 37 30 31 24 28
26 | 10 9 7 11 15 5 11 10 14 17 4 | 17 25 26 21 29 23 25 26 23 25 23
27E | 18 18 13 15 21 10 17 11 20 18 6 | 80 86 85 78 87 80 87 82 80 85 82
28 | 17 15 10 11 15 4 15 11 7 31 4 | 21 31 28 28 31 24 31 26 23 28 26
29 | 17 18 8 15 15 6 17 9 13 21 5 | 24 30 18 18 23 19 28 23 26 21 20
30 | 14 13 6 11 16 3 12 9 13 17 4 | 19 18 22 23 22 18 19 25 21 23 20
31E | 17 16 7 13 22 5 18 10 11 19 5 | 17 21 18 11 19 12 21 18 25 24 15
32 | 6 15 9 8 19 3 10 10 9 14 4 | 13 18 15 14 23 15 19 16 21 16 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 17 8 11 17 5 15 11 12 20 |T 24 32 28 26 31 25 31 29 29 27 26
WRMS | 12 17 8 10 18 5 14 10 10 20 |NE 18 27 23 21 26 20 26 24 23 20 21
MEDI | 12 16 7 11 16 5 15 10 11 19 |MD 19 28 25 22 26 21 27 25 25 22 22
Table 3.1703.4 GPS week: 1703 Day: 4 MJD: 56169.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 18 22 9 7 14 5 10 9 12 16 4 | 47 56 56 50 56 50 57 53 49 55 52
2E | 13 14 10 9 13 5 13 11 13 27 4 | 14 18 17 16 20 15 18 15 18 26 14
3 | 5 12 5 10 15 4 11 8 8 18 4 | 13 15 14 20 15 14 15 15 18 15 13
4 | 16 18 7 8 10 5 15 12 13 27 4 | 53 65 55 59 60 58 65 57 60 67 59
5 | 12 14 8 9 14 3 12 8 7 34 4 | 16 27 21 22 28 20 29 21 24 21 22
6 | 8 12 5 10 11 5 9 7 8 14 3 | 8 19 15 17 17 13 18 14 20 18 14
7E | 11 21 8 9 16 4 17 11 12 15 5 | 13 26 19 16 20 15 23 18 25 17 17
8E | 19 13 9 8 14 5 15 12 9 18 4 | 32 34 29 34 35 31 38 30 31 31 31
9E | 14 17 12 13 19 7 16 11 18 24 6 | 47 58 54 51 66 50 60 48 54 55 54
10 | 10 10 7 7 13 3 8 8 7 20 3 | 18 27 21 24 29 22 25 22 25 20 23
11E | 8 16 6 8 21 4 12 9 12 17 4 | 13 24 22 20 31 17 21 16 26 25 19
12 | 13 18 10 12 17 5 18 6 14 22 5 | 21 27 24 26 25 21 25 23 35 18 22
13 | 14 16 6 11 17 4 14 8 11 24 4 | 58 66 59 58 63 57 64 58 61 60 59
14 | 12 20 7 13 14 4 17 9 15 17 5 | 16 26 19 21 29 16 25 18 27 19 19
15 | 12 20 11 9 13 4 17 6 16 25 5 | 19 28 22 21 24 17 25 18 22 20 18
16 | 10 21 13 15 15 5 19 11 11 30 6 | 13 23 21 26 20 17 23 17 23 21 18
17 | 10 17 8 6 18 5 14 10 9 18 4 | 9 24 18 11 27 14 24 16 23 16 17
18 | 10 20 6 12 11 2 15 9 10 21 4 | 16 30 26 14 25 19 28 23 27 20 21
19 | 8 19 8 13 21 4 15 10 10 19 5 | 16 26 13 16 25 14 23 17 18 15 14
20 | 9 15 6 13 14 4 15 10 10 18 4 | 15 27 25 21 27 21 26 21 29 14 22
21 | 8 13 6 10 14 5 15 6 10 14 4 | 18 13 10 11 12 19 14 11 12 11 9
22 | 13 19 6 10 11 3 14 9 10 25 4 | 18 29 22 19 31 20 30 23 25 30 22
23 | 10 19 8 12 16 3 18 9 10 22 5 | 16 23 19 18 26 14 25 14 22 15 17
25 | 15 21 7 7 17 4 15 7 8 19 4 | 21 29 24 27 34 24 33 27 33 22 25
26 | 9 11 11 8 9 3 8 5 14 19 4 | 16 22 20 20 24 17 22 18 20 23 18
27E | 16 17 12 12 14 7 18 11 16 21 5 | 43 55 50 44 56 46 57 45 48 48 49
28 | 11 18 12 9 12 3 15 10 7 31 5 | 16 30 32 26 31 24 29 24 30 29 26
29 | 14 19 13 13 14 3 18 8 12 21 5 | 14 23 15 13 21 12 22 13 20 18 13
30 | 9 13 8 10 14 4 11 9 12 19 4 | 11 18 14 22 16 13 15 19 24 23 15
31E | 10 18 7 13 25 6 20 11 13 14 6 | 10 26 18 16 20 14 22 20 26 22 17
32 | 7 16 4 8 15 5 9 10 11 16 4 | 15 18 16 16 25 14 18 13 17 17 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 9 10 15 4 15 9 12 21 |T 21 30 25 25 30 23 29 24 28 26 24
WRMS | 11 17 8 9 15 4 14 9 9 20 |NE 17 26 21 21 26 19 25 20 25 21 20
MEDI | 11 17 8 10 14 4 15 9 11 19 |MD 16 26 21 21 26 17 25 19 25 21 19
Table 3.1703.5 GPS week: 1703 Day: 5 MJD: 56170.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 9 21 8 8 10 7 12 10 9 19 4 | 16 22 24 19 23 19 21 21 22 17 18
2E | 11 12 8 8 12 4 14 13 8 30 4 | 17 23 22 23 22 21 23 23 23 29 20
3 | 8 11 6 8 13 5 11 12 12 16 4 | 15 21 16 19 15 15 20 22 26 23 17
4E | 13 14 9 7 21 7 13 14 11 27 5 | 25 39 33 26 34 27 37 27 33 41 30
5 | 15 13 8 8 13 5 13 13 9 34 4 | 21 27 24 17 27 18 29 24 26 19 22
6 | 8 11 6 5 15 4 11 11 14 12 4 | 13 21 18 18 20 15 21 21 27 24 18
7E | 10 21 5 9 18 4 15 16 7 13 5 | 21 30 23 21 27 20 27 24 28 23 22
8E | 14 13 9 11 17 5 14 14 11 20 5 | 49 46 48 50 52 47 48 47 48 48 47
9E | 15 18 14 11 20 7 16 10 13 29 6 | 61 69 67 63 72 64 72 66 70 69 67
10 | 8 10 9 8 16 4 10 13 8 19 4 | 13 21 19 17 24 14 20 19 19 16 17
11E | 11 23 5 7 13 4 12 10 9 23 4 | 16 27 15 15 24 13 19 19 22 28 15
12 | 15 16 8 14 18 6 17 10 16 21 5 | 23 28 18 25 23 20 27 25 24 19 21
13 | 10 15 8 9 17 4 15 12 9 23 4 | 42 50 45 49 55 44 52 45 47 46 47
14 | 8 19 9 11 14 3 18 10 10 18 5 | 16 26 21 22 28 17 26 22 26 18 20
15 | 10 16 9 10 13 4 18 13 12 26 5 | 18 26 21 17 23 16 26 23 24 19 19
16 | 10 20 16 12 15 6 19 11 15 29 6 | 16 24 26 23 18 18 23 18 24 24 18
17 | 10 14 6 7 15 5 12 13 9 19 4 | 13 24 21 14 27 15 23 21 27 15 19
18 | 7 18 8 11 12 3 15 12 11 22 5 | 14 26 22 17 26 17 27 25 27 17 20
19 | 10 21 9 13 17 4 18 13 10 19 5 | 15 25 13 14 23 12 23 16 20 12 13
20 | 10 16 7 11 14 3 14 11 10 20 4 | 12 23 20 17 24 17 25 20 28 16 19
21E | 7 13 9 10 11 4 12 10 11 12 4 | 23 17 16 17 19 20 19 18 21 15 15
22 | 8 18 5 9 12 4 14 11 12 27 4 | 18 29 24 19 32 22 30 27 28 32 24
23 | 7 19 8 13 13 5 18 11 12 22 5 | 14 24 14 16 21 12 24 19 21 11 14
25 | 10 26 6 8 22 6 15 11 9 22 5 | 21 29 27 24 30 24 34 29 26 21 24
26 | 5 10 10 7 15 3 8 10 11 15 4 | 17 21 20 15 23 16 20 21 19 21 17
27E | 15 20 13 13 19 7 18 12 14 20 6 | 58 67 63 58 70 60 67 62 61 64 62
28 | 13 14 12 8 12 4 14 16 8 33 5 | 13 27 25 25 27 21 28 26 25 28 24
29 | 12 16 12 9 13 4 16 15 12 20 5 | 14 26 15 16 22 15 26 24 26 16 18
30 | 7 10 9 8 13 5 9 11 13 17 4 | 17 18 17 22 21 16 19 24 24 27 19
31E | 11 19 9 11 27 6 20 13 12 19 6 | 11 21 18 13 21 15 22 20 25 21 16
32 | 10 16 7 7 13 5 10 12 8 15 4 | 15 16 14 15 20 12 19 15 16 17 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 9 10 16 5 15 12 11 22 |T 21 28 24 23 28 22 28 26 28 25 23
WRMS | 10 17 9 8 15 5 14 12 9 21 |NE 17 25 20 20 25 17 25 23 25 21 20
MEDI | 10 16 8 9 14 4 14 12 11 20 |MD 16 26 21 19 24 17 25 23 26 21 19
Table 3.1703.6 GPS week: 1703 Day: 6 MJD: 56171.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 15 23 9 11 16 5 13 7 13 20 5 | 27 33 31 28 34 28 33 27 27 29 27
2E | 15 13 8 10 11 4 15 8 13 24 4 | 18 16 17 16 19 14 22 15 19 26 15
3 | 7 12 7 6 15 6 10 8 8 15 3 | 21 20 26 22 25 23 21 18 30 24 21
4E | 13 15 11 12 17 11 14 12 17 23 5 | 56 61 52 52 60 54 60 53 62 62 56
5 | 10 15 9 9 11 6 13 7 8 38 4 | 25 33 28 30 37 25 33 25 31 26 28
6 | 7 13 7 12 14 4 12 7 10 13 4 | 19 23 25 14 24 20 25 17 28 23 19
7E | 9 20 9 12 15 5 16 9 11 12 5 | 14 27 19 19 22 17 22 19 26 19 19
8E | 18 15 7 6 17 8 13 8 9 18 4 | 53 56 55 54 55 56 56 56 51 54 53
9E | 12 17 16 12 21 9 15 10 14 35 6 | 54 63 63 60 69 61 62 65 65 63 62
10 | 10 10 6 8 14 4 9 8 6 20 3 | 26 32 29 33 40 29 32 28 35 25 31
11E | 7 17 8 9 14 5 12 7 13 31 4 | 29 39 38 34 38 32 36 29 35 43 33
12 | 9 18 13 15 14 7 16 7 13 27 5 | 24 28 26 33 25 22 27 24 29 25 24
13 | 10 15 9 10 15 5 12 9 10 21 4 | 38 41 36 35 43 39 41 40 41 40 37
14 | 8 17 7 12 16 5 18 5 8 19 4 | 20 27 23 24 33 19 28 19 23 20 22
15 | 12 16 11 8 13 5 19 7 10 28 5 | 25 27 26 25 29 21 26 24 23 22 22
16 | 11 20 12 12 16 6 19 7 12 30 5 | 24 23 29 28 26 22 27 20 26 21 22
17 | 11 15 14 12 15 5 12 9 12 19 5 | 15 28 21 17 28 18 29 21 31 18 21
18 | 8 19 10 14 9 4 16 7 11 22 5 | 18 30 24 19 30 21 30 23 28 16 22
19 | 8 18 10 9 16 4 15 6 10 20 4 | 19 28 18 16 27 17 27 16 20 15 17
20 | 11 15 6 11 14 5 16 6 7 32 4 | 17 26 26 23 32 22 27 21 30 23 24
21E | 6 17 7 11 13 4 13 6 14 14 4 | 18 19 14 15 18 16 17 11 17 12 13
22 | 9 17 9 10 14 3 17 8 13 30 5 | 25 35 30 26 39 28 35 28 30 37 29
23 | 8 20 9 10 14 2 18 7 10 24 5 | 21 26 23 19 29 18 27 17 24 15 20
25 | 13 23 7 11 16 5 15 8 8 22 5 | 22 30 29 29 34 26 33 29 30 23 27
26 | 6 12 9 7 14 4 9 6 10 19 3 | 20 24 23 26 31 21 22 22 24 21 23
27E | 15 16 15 15 16 7 17 11 12 26 6 | 50 59 59 55 62 57 59 61 61 58 58
28 | 14 14 10 11 15 5 13 9 8 29 4 | 22 33 34 37 36 29 34 28 35 33 32
29 | 15 20 15 12 12 4 21 7 9 20 5 | 22 27 17 17 22 18 28 17 25 24 18
30 | 9 13 7 6 14 4 10 8 8 18 3 | 21 17 21 17 22 18 20 17 22 20 17
31E | 9 21 9 13 23 6 16 8 11 17 5 | 13 24 19 14 22 12 22 13 20 22 15
32 | 11 17 6 8 14 4 10 7 6 17 4 | 24 28 30 28 35 26 27 24 26 28 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 10 11 15 6 15 8 11 23 |T 25 31 29 27 33 26 31 26 31 28 27
WRMS | 10 17 9 10 15 5 14 8 9 20 |NE 22 27 25 24 30 22 28 22 28 23 23
MEDI | 10 17 9 11 14 5 15 7 10 21 |MD 22 28 26 26 31 22 28 23 28 24 23
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 4.1703 GPS week: 1703 MJD: 56165.0-56171.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2948 |U 7 8 19 |U 6 7 21 |U 16 12 42 |
emr | emr 2936 | 8 10 21 |U 24 16 51 | 18 13 48 |
esa | esa 2948 | 7 9 20 |U 6 8 21 | 17 11 42 |
gfz | gfz 2935 |U 7 9 19 |U 13 14 33 |U 18 12 43 |
grg | grg 2948 |U 10 13 27 |U 18 19 53 | 31 16 77 |
igr | igr 2948 | 7 9 21 | 6 7 21 | 17 12 44 |
igs | igs 2928 | 7 9 20 | 11 11 32 | 17 13 45 |
jpl | jpl 2935 | 8 10 22 |U 24 18 55 | 17 15 45 |
mit | mit 2948 | 8 9 19 |U 20 18 44 |U 29 18 65 |
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 5.1703.0 GPS week: 1703 Day: 0 MJD: 56165.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 5 19 | 7 10 24 | 7 7 12 |
emr | emr 2964 | 9 7 21 | 8 9 27 | 9 8 18 |
esa | esa 2976 | 8 7 20 | 7 9 22 | 6 9 13 |
gfz | gfz 2963 | 8 7 19 | 13 14 26 | 6 8 13 |
grg | grg 2976 | 12 14 33 | 13 20 42 | 10 12 23 |
igr | igr 2976 | 8 7 21 | 7 8 22 | 7 7 13 |
igs | igs 2958 | 8 6 20 | 8 10 34 | 6 8 15 |
jpl | jpl 2962 | 8 9 23 | 20 15 48 | 8 9 19 |
mit | mit 2976 | 8 6 17 | 14 17 41 | 7 9 16 |
Table 5.1703.1 GPS week: 1703 Day: 1 MJD: 56166.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 7 12 | 6 7 24 | 30 13 63 |
emr | emr 2964 | 7 9 15 | 14 8 34 | 38 17 73 |
esa | esa 2976 | 6 8 14 | 5 9 24 | 37 13 74 |
gfz | gfz 2964 | 5 9 14 | 13 15 33 | 35 15 61 |
grg | grg 2976 | 10 15 25 | 18 18 40 | 19 18 36 |
igr | igr 2974 | 6 8 15 | 6 7 23 | 36 15 74 |
igs | igs 2967 | 6 9 14 | 14 11 34 | 36 15 74 |
jpl | jpl 2963 | 6 10 16 | 14 11 35 | 36 20 66 |
mit | mit 2976 | 6 9 15 | 14 14 35 | 31 18 73 |
Table 5.1703.2 GPS week: 1703 Day: 2 MJD: 56167.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 8 9 22 | 6 6 16 | 26 22 103 |
emr | emr 2868 | 9 10 22 | 30 17 58 | 24 25 105 |
esa | esa 2880 | 8 9 23 | 6 7 18 | 25 17 92 |
gfz | gfz 2867 | 8 9 22 | 15 16 38 | 29 19 107 |
grg | grg 2880 | 11 12 27 | 17 15 42 | 25 25 111 |
igr | igr 2880 | 9 9 23 | 6 5 19 | 25 19 100 |
igs | igs 2862 | 8 9 22 | 9 11 24 | 24 22 99 |
jpl | jpl 2868 | 10 10 23 | 26 19 53 | 25 26 99 |
mit | mit 2880 | 9 15 22 | 16 15 34 | 25 28 95 |
Table 5.1703.3 GPS week: 1703 Day: 3 MJD: 56168.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 6 7 18 | 5 7 20 | 10 9 15 |
emr | emr 2868 | 8 12 24 | 26 19 60 | 10 11 23 |
esa | esa 2880 | 7 9 20 | 5 8 22 | 9 9 17 |
gfz | gfz 2868 | 7 11 20 | 15 15 33 | 10 11 17 |
grg | grg 2880 | 9 10 22 | 13 18 38 | 14 14 27 |
igr | igr 2880 | 7 9 21 | 5 6 21 | 10 10 16 |
igs | igs 2877 | 7 9 22 | 9 11 33 | 9 10 18 |
jpl | jpl 2867 | 8 11 25 | 27 23 66 | 10 11 19 |
mit | mit 2880 | 8 8 21 | 14 13 46 | 10 13 21 |
Table 5.1703.4 GPS week: 1703 Day: 4 MJD: 56169.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 9 24 | 4 7 15 | 7 8 16 |
emr | emr 2964 | 8 10 26 | 25 17 50 | 9 6 19 |
esa | esa 2976 | 8 10 24 | 5 7 15 | 8 6 16 |
gfz | gfz 2965 | 7 9 19 | 13 17 34 | 8 8 17 |
grg | grg 2976 | 9 14 28 | 18 17 44 | 90 9 189 |
igr | igr 2976 | 8 9 24 | 4 6 16 | 7 6 15 |
igs | igs 2972 | 7 9 25 | 10 11 28 | 8 12 19 |
jpl | jpl 2964 | 8 10 25 | 27 19 59 | 9 7 21 |
mit | mit 2976 | 7 9 23 | 20 21 41 | 70 21 122 |
Table 5.1703.5 GPS week: 1703 Day: 5 MJD: 56170.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 9 21 | 7 8 24 | ---- ---- ---- |
emr | emr 2964 | 8 9 21 | 31 20 61 | ---- ---- ---- |
esa | esa 2976 | 7 9 21 | 7 8 24 | ---- ---- ---- |
gfz | gfz 2961 | 7 10 19 | 11 9 32 | ---- ---- ---- |
grg | grg 2976 | 9 14 27 | 27 21 57 | ---- ---- ---- |
igr | igr 2976 | 8 9 22 | 7 7 22 | ---- ---- ---- |
igs | igs 2931 | 8 9 22 | 12 12 33 | ---- ---- ---- |
jpl | jpl 2962 | 9 10 25 | 31 21 63 | ---- ---- ---- |
mit | mit 2976 | 8 9 19 | 30 22 53 | ---- ---- ---- |
Table 5.1703.6 GPS week: 1703 Day: 6 MJD: 56171.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 9 19 | 6 8 23 | ---- ---- ---- |
emr | emr 2960 | 6 11 19 | 31 22 70 | ---- ---- ---- |
esa | esa 2976 | 6 10 18 | 6 8 24 | ---- ---- ---- |
gfz | gfz 2963 | 7 12 19 | 14 9 37 | ---- ---- ---- |
grg | grg 2976 | 9 12 28 | 20 28 109 | ---- ---- ---- |
igr | igr 2975 | 7 12 18 | 6 8 23 | ---- ---- ---- |
igs | igs 2935 | 7 10 19 | 14 12 35 | ---- ---- ---- |
jpl | jpl 2959 | 8 11 19 | 26 19 62 | ---- ---- ---- |
mit | mit 2976 | 7 9 18 | 30 25 60 | ---- ---- ---- |
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 6.1703 GPS week: 1703 MJD: 56165.500-56171.500
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 -95 13 2 -4 | 16 23
| 18 25 59 37 12 | 2
emr uuuuu | -2 -8 -178 -15 -8 | 25 30
| 13 30 114 67 13 | 2
esa uuuuu | 7 -46 40 109 -2 | 23 26
| 32 18 50 77 13 | 2
gfz uuuuu | 5 23 -10 9 2 | 13 19
| 11 17 89 94 9 | 2
grg uuuux | 44 -9 -34 -19 -22 | 33 50
| 19 26 76 65 23 | 8
igr xxxxx | -6 -16 2 0 -10 | 14 21
| 20 10 30 33 11 | 2
irf xxxxx | -7 3 16 -10 0 | 2 11
| 12 5 33 23 6 | 2
jpl uuuuu | 9 -7 -66 -41 0 | 60 61
| 19 24 45 39 12 | 3
mit uuuuu | -25 0 100 -22 -3 | 8 16
| 20 14 50 72 13 | 4
ngs uuuuu | -18 68 4 -79 1 | 14 18
| 20 39 86 110 5 | 1
sio xxxxx | 48 -20 180 188 8 | 58 60
| 26 13 56 42 10 | 4
Table 7.1703.0 GPS week: 1703 Day: 0 MJD: 56165.500
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 -54 59 48 18 | 13 21
emr uuuuu | -10 -34 -188 -100 3 | 24 30
esa uuuuu | 38 -46 70 136 6 | 20 24
gfz uuuuu | -12 47 -97 -59 12 | 11 16
grg uuuux | 23 -2 -95 49 -54 | 48 61
igr xxxxx | -24 -17 22 20 5 | 14 20
irf xxxxx | -15 -3 -28 -37 -10 | 5 12
jpl uuuuu | -13 -24 -89 -3 10 | 55 57
mit uuuuu | -37 -12 75 -79 -22 | 14 20
ngs uuuuu | 22 96 109 31 -2 | 15 18
sio xxxxx | 18 -38 225 174 25 | 51 54
Table 7.1703.1 GPS week: 1703 Day: 1 MJD: 56166.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 19 -126 -39 4 -9 | 16 23
emr uuuuu | 4 -40 35 -88 -10 | 26 31
esa uuuuu | -8 -40 37 204 -4 | 22 26
gfz uuuuu | 0 27 -61 -119 -1 | 12 18
grg uuuux | 56 4 33 76 -12 | 38 52
igr xxxxx | 24 -24 18 51 -9 | 16 21
irf xxxxx | 5 3 -10 -26 3 | 3 12
jpl uuuuu | -6 -25 33 -21 4 | 57 59
mit uuuuu | -1 -3 10 -77 5 | 11 18
ngs uuuuu | -26 73 -85 46 2 | 14 18
sio xxxxx | 74 -33 172 250 2 | 55 58
Table 7.1703.2 GPS week: 1703 Day: 2 MJD: 56167.500
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 -73 43 -65 -6 | 16 23
emr uuuuu | -10 -27 -151 66 -1 | 27 31
esa uuuuu | 37 -39 5 123 1 | 22 26
gfz uuuuu | 12 22 -126 -50 1 | 13 18
grg uuuux | 40 -25 13 -33 -29 | 32 47
igr xxxxx | -6 -30 -41 -15 -12 | 16 21
irf xxxxx | -19 7 -5 -28 0 | 3 12
jpl uuuuu | 16 -39 -76 -100 7 | 58 60
mit uuuuu | -50 5 97 -67 -3 | 10 18
ngs uuuuu | -36 125 135 -21 1 | 14 18
sio xxxxx | 43 -25 176 176 9 | 57 59
Table 7.1703.3 GPS week: 1703 Day: 3 MJD: 56168.500
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 -116 -56 17 1 | 17 23
emr uuuuu | -16 -17 -203 47 6 | 27 30
esa uuuuu | 35 -65 25 34 15 | 22 26
gfz uuuuu | 17 21 24 144 14 | 13 18
grg uuuux | 28 -47 31 -51 -48 | 29 46
igr xxxxx | -15 -2 43 21 0 | 15 21
irf xxxxx | -16 6 16 12 -4 | 2 12
jpl uuuuu | 4 20 -92 -18 13 | 60 61
mit uuuuu | -43 26 101 -57 -18 | 8 16
ngs uuuuu | -32 80 0 -130 -3 | 14 18
sio xxxxx | 23 -11 211 237 13 | 59 61
Table 7.1703.4 GPS week: 1703 Day: 4 MJD: 56169.500
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 | -31 -94 44 33 -14 | 18 24
emr uuuuu | -9 38 -344 -55 -29 | 27 31
esa uuuuu | 9 -76 -18 145 -9 | 25 29
gfz uuuuu | -5 38 102 110 -4 | 16 21
grg uuuux | 31 -31 18 -120 -8 | 27 46
igr xxxxx | -27 -23 -9 -1 -24 | 17 22
irf xxxxx | -15 -5 62 18 8 | 1 12
jpl uuuuu | 36 23 -79 -92 -13 | 64 65
mit uuuuu | -25 -13 166 100 13 | 6 15
ngs uuuuu | -21 61 -49 -270 0 | 14 18
sio xxxxx | 27 -19 256 180 1 | 62 64
Table 7.1703.5 GPS week: 1703 Day: 5 MJD: 56170.500
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 | 12 -101 -49 -1 3 | 15 22
emr uuuuu | 12 0 -239 -8 -21 | 23 29
esa uuuuu | -38 -21 136 144 2 | 23 27
gfz uuuuu | 14 9 1 1 6 | 14 19
grg uuuux | 75 4 -76 -19 11 | 27 46
igr xxxxx | 19 -5 -28 -30 -6 | 12 20
irf xxxxx | 7 7 25 -18 1 | 0 9
jpl uuuuu | 30 -4 -66 -40 -4 | 61 63
mit uuuuu | -20 9 140 -29 -5 | 4 11
ngs uuuuu | -23 12 -68 -122 12 | 13 16
sio xxxxx | 71 2 127 170 9 | 61 63
Table 7.1703.6 GPS week: 1703 Day: 6 MJD: 56171.500
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 -103 88 -18 -17 | 17 24
emr uuuuu | 17 24 -160 36 -6 | 21 27
esa uuuuu | -28 -35 21 -23 -24 | 24 28
gfz uuuuu | 6 -3 87 36 -11 | 16 22
grg uuuux | 53 31 -160 -36 -12 | 33 49
igr xxxxx | -12 -13 11 -45 -23 | 12 20
irf xxxxx | 3 5 51 11 0 | 1 10
jpl uuuuu | -7 3 -95 -13 -19 | 64 65
mit uuuuu | -1 -12 111 59 8 | 4 11
ngs uuuuu | -11 27 -13 -84 0 | 15 20
sio xxxxx | 76 -17 94 127 -5 | 64 66
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