[IGSREPORT-21138] Wk 1702 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Sep 6 08:17:48 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1702 (Aug 19, 2012 - Aug 25, 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:
igs1702[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1702[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1702[0-6].cls IGS GPS clock combination summary report.
igs17027.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17027.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 27 9 27 KOUC KOUC
0 | EMR | 9 9
0 | ESA | 9 27 9 27 TLSE NNOR TLSE
0 | GFZ | 9 23 27 LHAZ TLSE
0 | GRG | CAGZ CAGZ NRMD
0 | JPL | 9
0 | MIT | 18 26 28 18 26 28 MAC1
1 | COD | 9 27 9 27 KOUC FLRS KOUC XMIS
1 | EMR | 9 9 YELL
1 | ESA | 9 27 9 27 HOLM YAKT
1 | GFZ | 9 23 27 ARTU HOB2 LHAZ NRMD NYAL SCOR THTI YELL
1 | GRG | USNO WROC YEBE HOLM SOFI USNO WROC
1 | JPL | 27
1 | MIT | 26 28 26 28 TLSE SOFI TLSE
2 | COD | 27 27 FLRS TLSE
2 | EMR | 9 9 THTI
2 | ESA | 27 27 NNOR THTI
2 | GFZ | 9 23 27 SANT
2 | GRG | 9 9 THTI WROC WROC
2 | JPL | 9
2 | MIT | 9 26 9 26 IRKJ GMAS
3 | COD | 9 27 9 27 KOUC FLRS KOUC
3 | ESA | 9 27 9 27 MATE ARTU OHI2
3 | GFZ | 9 27 BOR1 HOB2 MATE SANT TWTF UNSA
3 | GRG | HOB2 SPT0 BRUX HOB2 IRKJ SPT0 WIND
3 | JPL | 9 27
3 | MIT | IRKJ
4 | COD | 9 27 9 27 KOUC KARR KOUC
4 | EMR | 9 9
4 | ESA | 9 27 9 27 NNOR
4 | GFZ | 9 23 27 NYAL
4 | GRG | WROC KIT3 LHAZ WROC
4 | JPL | REUN
4 | MIT | 1 1 KARR
5 | COD | 9 27 9 27 KOUC KOUC
5 | EMR | CHUR CHUR MATE
5 | ESA | 9 27 9 27 IRKJ MATE NNOR
5 | GFZ | 9 23 27 HOB2 THTI WUHN
5 | GRG | 13 13 HOB2 MATE WROC BUCU HOB2 WROC
5 | MIT | 28 28 SPT0 BAKO SPT0
6 | COD | 9 27 8 9 27 CHUR CHUR FLRS
6 | EMR | MCM4 MCM4 THTI
6 | ESA | 8 9 27 8 9 27 TIXI
6 | GFZ | 8 9 23 27 30 ALRT INVK IRKJ
6 | GRG | USNO YEBE BRMU GOLD KIT3 LHAZ USNO
6 | JPL | 8
6 | MIT | 28 28 DAV1 IRKJ
5. 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.
6. 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 | 1.0 -3.4 -9.6 -13 16 -16 -.27
ESA | 0 | 6.0 -2.0 24.2 -22 -4 134 -.65
GFZ | 0 | -.5 1.2 .5 -48 -18 -18 -.53
GRG | 0 | 7.3 -5.1 24.6 -43 24 -32 -.44
JPL | 0 | 1.6 .9 -2.5 -22 -3 -17 -.18
MIT | 0 | 2.3 -2.5 13.9 -16 17 -40 -.44
NGS | 0 | 6.8 -2.4 21.6 -17 -42 -4 -.25
EMR | 1 | 2.2 -.8 -2.8 -6 -1 -10 -.29
ESA | 1 | 4.6 2.3 22.3 58 -33 110 -.60
GFZ | 1 | -.4 .7 .4 -67 -22 -23 -.41
GRG | 1 | 7.1 -15.5 21.5 -30 18 -25 -.48
JPL | 1 | -2.2 3.8 .4 -73 -21 -22 -.20
MIT | 1 | 3.9 3.2 10.6 -17 20 -50 -.43
NGS | 1 | -.2 5.2 14.4 25 2 -4 -.21
EMR | 2 | -.4 -7.6 -1.5 -4 5 -12 -.27
ESA | 2 | 3.0 5.4 21.3 101 3 71 -.52
GFZ | 2 | -.7 2.0 -.4 -30 -21 -20 -.34
GRG | 2 | .0 -10.2 20.1 -36 -6 -32 -.30
JPL | 2 | -6.4 2.4 -2.4 5 -69 10 -.27
MIT | 2 | 2.2 .4 10.7 -14 14 -48 -.43
NGS | 2 | 4.0 -.8 13.0 -19 -35 -2 -.15
EMR | 3 | 2.8 -4.3 -1.1 -4 6 -14 -.24
ESA | 3 | -1.5 3.5 18.6 82 24 101 -.71
GFZ | 3 | -.2 .7 -.1 -40 -18 -19 -.51
GRG | 3 | 3.7 -1.1 18.7 -37 23 -16 -.15
JPL | 3 | -2.3 11.0 -.5 24 1 -14 -.22
MIT | 3 | 3.5 .7 11.7 -17 9 -48 -.50
NGS | 3 | .8 4.9 16.3 13 -20 -2 -.37
EMR | 4 | 3.1 3.2 -3.7 -8 5 -3 -.12
ESA | 4 | -2.1 4.4 26.4 95 88 74 -.90
GFZ | 4 | -1.3 .8 -.3 -61 0 -17 -.39
GRG | 4 | 4.6 -5.9 14.5 -29 22 -8 -.33
JPL | 4 | -3.9 6.7 .3 39 12 14 -.14
MIT | 4 | 4.2 3.3 13.2 -18 15 -42 -.46
NGS | 4 | -3.0 -.2 5.4 -35 6 -3 -.17
EMR | 5 | .4 -5.2 -1.3 -7 14 -16 -.16
ESA | 5 | -2.0 6.3 23.6 135 70 74 -.66
GFZ | 5 | -.8 .9 .9 -37 -6 -17 -.50
GRG | 5 | 4.3 -2.6 22.4 -49 37 -35 -.46
JPL | 5 | .6 4.5 2.2 17 0 14 -.09
MIT | 5 | 3.3 3.0 12.7 -19 16 -51 -.31
NGS | 5 | 3.4 1.5 18.9 -14 -38 6 -.20
EMR | 6 | 3.1 -.3 4.2 -7 9 -10 -.24
ESA | 6 | 2.6 .6 20.7 43 -19 105 -.52
GFZ | 6 | -.6 .6 .5 -45 -12 -8 -.39
GRG | 6 | 2.8 3.3 14.0 -35 19 5 -.50
JPL | 6 | -.2 6.0 3.2 -28 -6 -18 -.19
MIT | 6 | 3.6 1.3 12.9 -21 18 -70 -.24
NGS | 6 | 1.8 -6.4 7.5 -67 -22 -2 -.27
7. 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.
8. 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
combinatino; 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.
9. 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 1.1702.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1702.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 2.1702.[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 3.1702.[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 5.1702.0-6).
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 1702 summary. (Aug 19, 2012 - Aug 25, 2012)
Table 1.1702.a GPS week: 1702 MJD: 56158.000-56164.000
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 257| 0 0 2 -21 -6 25 -.54 12 11 | -485 86 19 72
| 0 1 2 33 36 20 .02 | 534 916
emr 93| -1 -2 -7 12 -45 -21 .15 16 16 | 2832 -308 15 106
| 0 1 2 34 39 7 .01 | 1223 895
esa 177| 0 0 1 -128 17 5 .03 8 7 | -1100 387 17 133
| 1 0 1 81 68 20 .02 | 346 419
gfz 196| 0 1 -2 89 -10 -10 -.46 10 10 | 60 214 23 150
| 0 0 0 66 41 15 .01 | 374 587
grg 124| 2 0 11 53 -25 11 .35 14 14 | 91 -7 18 148
| 1 0 1 35 31 10 .06 | 225 516
igr n/a| 0 0 0 0 -7 -6 -.24 5 5 | 8278 -526 22 93
| 0 0 0 32 34 11 .05 | 1680 755
jpl 152| 0 0 -4 11 7 10 .34 14 13 | 3337 -435 20 121
| 1 1 2 59 46 18 .03 | 1581 853
mit 253| 0 0 0 7 -25 2 -.27 11 11 | -3 -50 23 183
| 0 0 0 44 37 19 .04 | 256 551
ngs 246| 0 0 1 37 58 -6 .22 12 10 | -520 113 2048 3612
| 0 1 5 40 36 14 .03 | 476 840
sio 245| 1 1 -2 -8 17 16 -.30 20 19 | --- --- --- ---
| 1 1 1 38 34 17 .03 | --- ---
Table 1.1702.b GPS week : 1702 MJD: 56158.000-56164.000
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 6 5 5 |
2 | 6 4 5 5 5 5 5 |
3 | 5 4 4 4 5 4 5 |
4 | 5 5 4 4 5 4 4 |
5 | 4 4 5 5 5 5 5 |
6 | 5 4 4 4 4 4 4 |
7 | 5 6 5 6 6 6 5 |
8 | 4 4 4 4 5 5 5 |
9 | 6 5 5 5 5 5 6 |
10 | 4 4 4 4 4 4 4 |
11 | 5 4 5 4 5 4 4 |
12 | 6 5 5 5 5 5 5 |
13 | 5 5 5 5 5 5 4 |
14 | 6 5 5 5 5 5 5 |
15 | 5 5 6 6 6 6 6 |
16 | 6 5 5 6 6 6 5 |
17 | 6 5 5 5 5 5 5 |
18 | 5 4 4 4 5 5 4 |
19 | 5 5 5 5 5 5 4 |
20 | 5 5 5 4 5 5 5 |
21 | 5 5 5 6 5 5 5 |
22 | 5 4 4 4 5 5 4 |
23 | 5 5 5 6 5 5 5 |
25 | 6 5 5 5 5 5 5 |
26 | 4 4 4 4 4 5 4 |
27 | 6 5 6 5 6 6 6 |
28 | 5 4 5 5 5 5 5 |
29 | 6 5 6 5 5 5 5 |
30 | 4 4 4 4 4 5 3 |
31 | 6 6 5 6 6 5 5 |
32 | 4 4 4 4 4 5 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 2.1702.0 GPS week: 1702 Day: 0 MJD: 56158.000
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 257| 0 0 -1 -64 -49 27 -.54 11 11 | -335 4 21 86
| 94 24 |
emr 93| -3 -3 -11 -8 -62 -18 .15 17 17 | 4089 -992 16 97
| -44 23 |
esa 177| 2 0 1 31 40 27 .01 7 7 | -640 -87 17 151
| -59 -24 |
gfz 196| 0 2 -1 -36 28 -19 -.44 10 9 | 504 -118 22 160
| 15 -37 |
grg 124| 2 0 12 15 -75 -1 .33 15 14 | 327 -199 18 128
| -8 -4 |
igr n/a| 0 0 0 -37 -45 -24 -.32 5 5 | 10836 -1369 26 100
| -25 17 |
jpl 152| -1 1 -8 -5 -42 14 .32 14 13 | 5630 -1278 20 118
| 27 8 |
mit 253| 0 0 0 -83 -15 -12 -.33 16 16 | 228 -290 28 164
| 19 16 |
ngs 246| 0 -2 4 59 47 -15 .26 13 12 | -516 488 2073 3784
| -138 85 |
sio 245| 1 2 -3 -76 -8 -9 -.26 22 20 | --- --- --- ---
| -8 -29 |
Table 2.1702.1 GPS week: 1702 Day: 1 MJD: 56159.000
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 257| 0 0 1 -50 0 60 -.54 14 13 | -1114 1011 26 87
| 102 -15 |
emr 93| 0 -1 -8 -24 -49 -10 .16 16 16 | 2523 843 12 111
| -33 19 |
esa 177| 0 0 2 -108 100 23 .04 7 7 | -1504 291 17 164
| 38 -63 |
gfz 196| -1 1 -2 118 -39 -33 -.47 10 9 | -47 208 24 159
| -4 -32 |
grg 124| 3 0 12 29 -33 13 .32 15 14 | 33 -186 18 151
| 5 -37 |
igr n/a| 0 0 0 -3 -20 -11 -.28 5 5 | 8992 246 25 120
| -41 5 |
jpl 152| 0 0 -4 110 27 7 .36 14 13 | 3850 342 20 131
| 18 -30 |
mit 253| 0 0 -1 0 -83 -24 -.29 10 10 | -183 93 21 179
| -1 23 |
ngs 246| -1 0 0 -22 -5 11 .23 11 10 | -1047 812 2113 3629
| -151 9 |
sio 245| 1 3 -3 -39 -13 -3 -.29 21 19 | --- --- --- ---
| -5 -31 |
Table 2.1702.2 GPS week: 1702 Day: 2 MJD: 56160.000
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 257| 0 -1 1 -2 -46 2 -.54 12 11 | 117 -1019 23 70
| 115 9 |
emr 93| -1 -5 -10 20 -81 -20 .14 16 16 | 4482 470 14 105
| -12 9 |
esa 177| 0 1 0 -176 26 5 .02 7 7 | -793 351 17 124
| 93 0 |
gfz 196| -1 2 -1 76 -62 -6 -.44 9 9 | -45 556 24 144
| 29 -4 |
grg 124| 2 0 10 74 -16 -4 .28 15 14 | -45 513 19 157
| 10 -56 |
igr n/a| 0 0 0 34 -36 3 -.23 5 5 | 9439 204 23 88
| -9 15 |
jpl 152| 3 -1 -3 5 92 23 .31 14 13 | 4494 482 21 109
| 47 24 |
mit 253| 0 0 0 57 -42 -2 -.25 12 12 | 64 120 23 177
| 5 11 |
ngs 246| -1 0 2 67 53 -7 .21 10 9 | 50 -981 2217 3643
| -58 -33 |
sio 245| 2 1 -3 24 -20 21 -.30 20 20 | --- --- --- ---
| -16 -16 |
Table 2.1702.3 GPS week: 1702 Day: 3 MJD: 56161.000
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 257| 0 0 4 17 -7 28 -.56 12 10 | -993 458 18 74
| 53 15 |
emr 93| -1 -3 -7 50 -37 -15 .16 16 16 | 3230 -440 17 116
| -43 22 |
esa 177| -1 -1 0 -123 4 18 .04 8 8 | -1587 988 17 120
| 34 -10 |
gfz 196| 0 2 -3 110 -11 -18 -.48 10 9 | -530 1024 22 157
| -7 -12 |
grg 124| 4 -1 12 73 -50 21 .31 14 13 | -207 782 20 152
| -13 -13 |
igr n/a| 0 0 0 29 -10 -5 -.29 5 5 | 8511 -557 20 82
| -24 21 |
jpl 152| 0 0 -4 -10 -26 3 .33 13 13 | 3799 -559 19 110
| -23 72 |
mit 253| 0 0 0 9 20 -7 -.30 11 11 | -407 815 26 223
| 17 11 |
ngs 246| 0 2 2 -12 64 -11 .20 10 9 | -981 344 1917 3613
| -60 -12 |
sio 245| 1 3 0 18 24 32 -.32 19 20 | --- --- --- ---
| -20 -16 |
Table 2.1702.4 GPS week: 1702 Day: 4 MJD: 56162.000
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 257| 0 -1 3 -10 58 -1 -.54 12 11 | -975 1300 14 65
| 86 -32 |
emr 93| -1 -1 -6 23 36 -18 .13 16 16 | 2628 -842 15 121
| -43 5 |
esa 177| 0 0 3 -167 -65 -31 -.01 9 9 | -1078 691 18 126
| 62 36 |
gfz 196| -1 2 -2 182 -21 8 -.47 11 10 | -63 174 25 142
| -36 -18 |
grg 124| 1 0 9 49 15 19 .38 13 12 | -88 156 17 159
| -7 -34 |
igr n/a| 0 0 1 -8 52 -10 -.18 5 5 | 7454 -768 21 85
| 7 1 |
jpl 152| 1 0 -4 -86 31 19 .30 14 13 | 2664 -837 21 130
| 25 44 |
mit 253| 0 0 0 29 -8 6 -.23 12 12 | -180 259 23 194
| 10 25 |
ngs 246| -1 0 -2 36 68 13 .15 11 10 | -931 1193 1813 3490
| -34 -18 |
sio 245| 0 0 -2 2 67 20 -.33 19 19 | --- --- --- ---
| -16 -29 |
Table 2.1702.5 GPS week: 1702 Day: 5 MJD: 56163.000
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 257| 0 0 3 11 7 29 -.48 12 10 | 115 -1059 16 56
| 57 27 |
emr 93| -2 -3 -6 56 -50 -33 .15 15 15 | 1934 -1586 17 93
| -47 32 |
esa 177| 0 0 -2 -226 -72 0 .05 8 8 | -1117 -164 20 129
| 114 34 |
gfz 196| -1 1 -1 97 57 -14 -.47 10 9 | 567 -838 23 144
| -12 -17 |
grg 124| 1 0 13 113 -21 10 .44 15 14 | 234 -511 19 143
| -46 -16 |
igr n/a| 0 0 0 33 22 12 -.20 4 4 | 6833 -1572 20 78
| -3 -20 |
jpl 152| 0 0 -5 28 -12 34 .38 14 14 | 1941 -1594 19 112
| -38 43 |
mit 253| 0 1 0 27 7 29 -.26 10 10 | 273 -885 22 179
| 3 27 |
ngs 246| 0 0 9 47 118 -24 .23 13 11 | 31 -958 2093 3628
| -36 51 |
sio 245| 0 0 -4 -13 58 36 -.29 21 19 | --- --- --- ---
| -23 -8 |
Table 2.1702.6 GPS week: 1702 Day: 6 MJD: 56164.000
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 257| 0 0 4 -54 -8 31 -.54 12 11 | -211 -91 16 67
| 82 0 |
emr 93| 0 -1 -3 -28 -73 -28 .12 15 15 | 942 386 18 102
| -25 25 |
esa 177| 0 0 1 -125 89 -5 .02 8 7 | -986 642 16 119
| 25 -23 |
gfz 196| 0 0 -3 78 -26 7 -.47 14 13 | 37 498 25 144
| -18 -8 |
grg 124| 2 0 12 18 3 19 .40 15 14 | 386 -606 19 147
| -21 -71 |
igr n/a| 0 0 1 -42 -13 -10 -.19 4 4 | 5884 130 22 104
| -8 1 |
jpl 152| 0 1 -1 37 -18 -25 .35 14 14 | 983 398 21 139
| -33 23 |
mit 253| 1 0 1 13 -57 26 -.25 6 6 | 182 -468 22 166
| -12 24 |
ngs 246| 0 0 -6 86 59 -15 .23 11 10 | -252 -102 2115 3503
| -41 5 |
sio 245| 0 1 0 25 10 16 -.34 20 17 | --- --- --- ---
| -56 -34 |
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 3.1702.0 GPS week: 1702 Day: 0 MJD: 56158.000
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 25 6 10 15 5 14 15 10 12 5 | 44 43 48 38 46 41 47 40 46 46 43
2 | 13 16 8 9 17 4 15 20 17 23 5 | 27 34 27 24 37 24 33 28 28 24 27
3 | 9 14 6 7 14 5 12 16 14 19 4 | 15 23 15 11 17 11 26 14 18 21 17
4 | 17 12 5 9 10 5 12 18 12 30 4 | 68 80 72 71 75 71 81 71 76 78 73
5 | 8 14 5 8 11 4 12 16 12 33 4 | 28 36 32 32 39 30 37 28 35 44 34
6 | 7 14 6 9 14 5 11 17 16 21 4 | 15 27 17 14 22 13 26 16 23 21 18
7E | 12 19 7 9 13 7 17 15 11 17 5 | 21 28 24 21 32 20 27 24 26 24 22
8 | 13 12 5 6 13 3 10 18 9 27 4 | 42 53 42 44 42 43 55 41 45 39 46
9E | 16 19 7 9 16 7 14 18 17 25 5 | 37 35 35 40 32 36 35 35 36 35 35
10 | 14 9 4 7 15 4 8 16 10 16 4 | 29 30 30 29 41 29 33 23 28 22 31
11E | 6 16 5 9 12 4 12 15 13 10 4 | 23 28 25 21 26 21 26 19 30 25 24
12 | 16 16 8 12 18 6 14 17 22 32 6 | 22 31 23 27 24 20 29 26 24 20 23
13 | 8 12 7 8 18 6 14 13 12 15 4 | 16 21 13 13 30 12 24 13 18 13 15
14 | 6 19 8 13 14 4 17 16 18 22 6 | 19 26 19 18 25 15 25 15 22 19 18
15 | 17 18 8 9 15 5 17 14 11 26 5 | 18 27 16 17 24 13 24 17 19 20 17
16 | 10 19 8 11 16 4 16 19 13 31 5 | 15 26 17 20 24 13 25 13 19 20 18
17 | 10 18 11 10 17 5 17 18 13 19 5 | 14 25 18 13 24 14 29 13 24 16 17
18 | 10 14 6 9 13 5 11 16 14 28 4 | 19 22 19 22 23 18 24 20 19 22 18
19 | 10 19 7 7 15 6 12 17 11 24 4 | 23 28 20 15 30 18 27 18 26 19 21
20 | 10 12 5 11 12 3 14 13 11 30 4 | 26 27 26 27 32 25 31 24 30 29 27
21 | 10 15 7 12 16 4 15 15 13 20 5 | 25 32 22 21 28 21 31 24 22 27 23
22 | 9 14 5 10 11 4 13 16 13 22 4 | 25 25 25 23 34 24 29 25 25 24 25
23 | 8 16 8 9 14 5 18 15 10 21 5 | 15 23 15 13 22 12 24 17 21 12 15
25 | 13 22 8 10 18 5 13 16 15 17 5 | 26 28 24 25 28 22 32 27 21 22 23
26 | 8 17 7 9 12 4 8 12 9 14 4 | 16 25 19 20 27 17 22 19 19 20 20
27E | 17 21 7 10 13 8 15 17 15 21 5 | 36 36 35 40 33 36 36 34 34 33 35
28 | 10 18 7 13 14 4 13 15 11 26 5 | 17 29 23 29 23 21 29 19 20 22 23
29 | 11 19 7 13 16 5 18 14 18 21 5 | 29 29 24 25 27 22 32 24 30 25 27
30 | 10 13 5 6 11 4 8 18 11 21 4 | 22 23 22 22 22 19 25 23 22 30 22
31E | 11 19 8 11 20 4 16 14 12 14 5 | 26 36 31 23 40 26 32 23 33 26 30
32 | 9 14 6 10 11 3 8 15 11 16 4 | 16 22 19 15 27 16 24 17 21 21 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 7 10 14 5 14 16 13 22 |T 24 30 25 24 30 23 31 24 27 26 26
WRMS | 11 17 7 9 14 5 13 16 12 20 |NE 23 29 24 23 30 21 30 22 26 25 24
MEDI | 10 16 7 9 14 5 14 16 12 21 |MD 23 28 23 22 28 21 29 23 24 22 23
Table 3.1702.1 GPS week: 1702 Day: 1 MJD: 56159.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 26 7 8 15 5 12 11 9 12 5 | 31 32 34 30 37 30 38 30 40 32 32
2 | 13 14 7 9 16 3 13 9 10 23 4 | 22 27 23 19 33 19 28 21 26 19 23
3 | 8 10 5 8 9 4 13 11 10 16 3 | 12 20 15 13 18 11 24 14 20 20 14
4 | 27 13 6 10 23 4 13 12 15 35 5 | 98 111 106 104 103 102 112 104 103 114 106
5 | 11 12 7 9 12 4 12 12 8 29 4 | 21 31 25 24 31 22 34 24 31 32 26
6 | 9 10 5 6 11 4 12 11 9 16 3 | 11 23 16 13 20 13 27 15 22 20 17
7E | 12 21 6 13 15 6 17 12 17 22 5 | 24 28 24 28 28 21 28 25 30 32 24
8 | 14 13 5 7 12 5 12 12 11 23 4 | 27 42 30 29 33 31 39 34 33 37 31
9E | 19 17 8 10 12 9 16 10 11 25 4 | 36 37 36 39 30 35 32 39 35 35 33
10 | 15 7 5 8 12 3 8 11 12 15 3 | 18 18 20 20 20 16 21 17 20 13 18
11E | 9 14 6 8 16 3 11 10 13 10 4 | 19 26 25 20 26 20 24 19 33 20 23
12 | 18 17 8 10 17 5 15 9 11 27 5 | 17 29 17 23 22 13 27 19 24 17 18
13 | 9 13 7 9 17 5 13 10 10 14 4 | 12 22 15 17 29 11 25 12 18 13 15
14 | 11 16 7 14 14 3 17 9 10 23 5 | 12 23 14 18 21 12 22 15 22 18 14
15 | 18 20 9 10 14 4 18 10 10 23 5 | 15 26 20 19 21 16 24 20 24 18 18
16 | 10 14 10 12 18 4 16 10 10 28 5 | 12 23 19 18 22 12 25 13 18 13 15
17 | 10 16 6 10 17 3 15 11 13 15 5 | 11 23 12 12 22 8 23 10 24 13 13
18 | 10 11 6 10 10 5 13 9 11 30 4 | 11 20 16 17 15 13 19 18 17 18 15
19 | 14 16 7 11 16 5 15 12 12 20 5 | 14 26 21 15 31 15 25 16 27 16 19
20 | 11 12 7 11 14 4 14 10 14 23 4 | 17 22 23 22 22 18 25 18 26 25 20
21 | 8 18 5 11 17 3 12 8 8 19 4 | 19 23 15 19 21 15 23 18 17 21 16
22 | 10 13 5 8 10 5 12 9 12 20 4 | 15 21 17 17 23 14 24 18 18 18 17
23 | 8 17 8 11 14 4 19 12 11 20 5 | 14 25 18 19 24 12 27 14 20 14 17
25 | 15 22 3 8 18 4 13 11 7 20 4 | 14 25 18 21 25 15 29 21 24 19 18
26 | 10 14 10 8 11 3 10 8 11 17 4 | 12 22 21 18 23 15 24 20 24 19 18
27E | 20 17 9 12 12 9 16 9 10 19 5 | 36 39 36 41 31 36 34 39 42 37 35
28 | 11 13 6 11 12 2 12 10 9 22 4 | 12 25 16 20 20 16 23 17 21 16 17
29 | 28 20 6 9 15 5 16 9 10 19 4 | 16 23 14 18 21 13 23 19 20 18 15
30 | 10 9 5 6 13 4 7 11 10 17 3 | 18 23 22 19 23 17 26 22 22 22 20
31E | 10 20 9 11 17 4 16 8 13 15 5 | 22 31 25 22 29 22 30 23 35 30 24
32 | 10 14 7 7 12 4 8 11 14 15 4 | 15 23 24 17 23 18 25 17 23 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 16 7 10 15 5 14 10 11 21 |T 20 28 23 23 27 20 29 22 27 24 22
WRMS | 13 16 7 9 14 5 13 10 10 19 |NE 18 27 22 22 26 18 28 21 26 22 21
MEDI | 11 14 7 10 14 4 13 10 11 20 |MD 16 25 20 19 23 16 25 19 24 19 18
Table 3.1702.2 GPS week: 1702 Day: 2 MJD: 56160.000
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 23 8 11 16 5 13 13 11 10 5 | 33 33 38 31 41 33 39 36 38 35 34
2 | 12 14 7 9 13 4 15 12 9 25 4 | 22 32 27 20 30 22 30 27 28 26 25
3 | 9 13 6 10 15 5 13 12 8 16 4 | 11 24 16 11 19 14 27 17 21 23 16
4 | 14 11 6 9 8 5 11 13 10 19 4 | 43 52 46 47 49 47 52 51 46 51 47
5 | 10 14 7 9 12 4 13 13 13 27 4 | 21 32 30 26 30 25 35 29 30 28 28
6 | 8 12 6 9 16 4 12 11 7 15 4 | 12 26 17 14 20 14 28 21 20 23 17
7E | 12 20 9 11 11 6 17 13 12 11 5 | 17 27 19 17 23 14 23 16 24 18 17
8 | 15 12 8 6 14 5 12 14 7 21 4 | 59 68 58 60 60 60 68 65 64 65 63
9E | 21 17 8 11 16 9 16 10 10 21 5 | 38 37 36 41 30 35 31 37 35 30 34
10 | 10 8 5 5 15 5 8 10 10 16 3 | 20 21 21 22 29 22 25 23 23 17 21
11E | 8 20 7 9 18 4 12 13 11 8 5 | 19 29 23 18 24 17 20 21 21 20 19
12 | 15 15 7 9 17 6 13 9 9 25 4 | 15 27 19 21 22 16 25 21 23 16 18
13 | 8 14 8 7 17 7 14 11 9 17 4 | 11 23 14 14 29 11 23 14 15 13 13
14 | 11 18 7 11 13 4 17 10 8 25 4 | 12 24 18 17 21 15 23 21 21 17 17
15 | 11 19 12 10 14 5 17 11 13 23 5 | 19 26 18 21 24 15 24 20 18 18 16
16 | 12 17 9 9 17 4 17 11 9 30 5 | 12 24 18 17 22 14 27 18 17 16 15
17 | 10 13 7 10 19 3 14 13 11 15 5 | 14 21 13 13 22 12 23 19 23 15 13
18 | 11 12 7 8 11 3 12 12 9 34 4 | 14 21 21 19 16 17 24 22 21 20 19
19 | 7 14 8 8 20 4 15 12 9 19 4 | 15 26 20 14 33 15 30 20 25 17 20
20 | 9 12 7 12 11 6 16 10 10 22 4 | 19 26 23 24 27 23 27 23 30 26 24
21 | 11 15 7 10 16 6 13 13 13 25 5 | 21 30 26 22 26 22 28 28 24 25 23
22 | 11 14 5 6 9 3 12 10 8 23 3 | 15 21 21 21 21 19 26 25 21 18 21
23 | 9 19 8 9 15 5 18 14 7 21 5 | 11 26 16 15 24 11 24 17 17 11 14
25 | 17 24 7 8 19 6 14 12 9 19 5 | 18 27 23 20 26 17 29 25 20 21 19
26 | 8 11 8 10 14 4 9 10 12 13 4 | 13 22 21 16 23 16 23 22 23 16 19
27E | 21 20 8 12 13 9 17 9 18 16 5 | 49 49 46 52 40 45 43 48 55 42 47
28 | 10 13 9 11 16 4 15 14 8 21 5 | 12 22 22 23 21 16 23 18 17 19 17
29 | 13 19 7 11 15 4 18 13 12 19 5 | 17 23 14 13 22 13 23 21 21 19 13
30 | 11 12 6 5 14 4 9 13 10 19 4 | 15 21 21 15 22 16 26 21 20 18 18
31E | 12 18 8 11 18 5 16 12 11 16 5 | 17 29 25 21 29 21 27 28 27 24 23
32 | 9 12 7 11 13 5 11 11 9 17 4 | 15 23 22 20 25 20 26 21 23 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 7 9 15 5 14 12 10 20 |T 20 28 24 22 27 21 29 25 26 23 22
WRMS | 11 16 7 9 14 5 13 12 9 20 |NE 17 26 21 19 25 18 27 23 23 21 20
MEDI | 11 14 7 9 15 5 14 12 10 19 |MD 17 26 21 20 24 17 26 21 23 20 19
Table 3.1702.3 GPS week: 1702 Day: 3 MJD: 56161.000
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 23 7 10 15 5 12 10 10 13 5 | 36 35 41 35 43 35 40 34 36 37 36
2 | 10 15 6 10 16 3 14 11 10 22 4 | 23 32 26 23 33 24 31 27 29 24 25
3 | 6 12 6 8 12 3 9 10 10 16 3 | 13 19 17 15 16 11 22 14 18 20 14
4 | 12 10 9 10 9 6 9 12 11 18 4 | 54 62 60 59 61 56 61 57 60 59 58
5 | 10 13 6 11 13 4 11 14 7 25 4 | 24 33 29 27 34 24 33 25 31 22 28
6 | 7 12 6 7 10 3 9 9 10 12 3 | 13 24 18 15 19 14 25 16 21 21 17
7E | 11 21 7 11 14 6 17 12 13 12 5 | 36 37 31 30 34 30 35 30 39 30 31
8 | 19 12 7 8 12 9 11 12 9 17 4 | 92 99 94 97 93 92 99 90 90 89 94
9E | 22 18 11 6 11 7 13 8 12 24 4 | 35 34 30 35 25 33 32 31 32 25 29
10 | 10 9 7 8 12 5 10 12 9 15 4 | 19 24 22 21 29 20 25 19 22 16 21
11E | 8 16 8 6 14 3 10 10 7 11 4 | 20 30 28 23 27 22 27 21 26 19 24
12 | 13 16 9 10 16 4 14 9 11 23 4 | 16 28 21 22 25 18 28 20 25 14 20
13 | 9 15 8 9 17 4 14 10 11 17 4 | 16 26 17 18 31 14 26 12 18 14 17
14 | 10 14 8 12 14 5 15 11 11 22 5 | 17 24 19 22 24 16 22 18 23 19 17
15 | 11 17 12 14 11 4 16 10 15 23 5 | 20 26 21 22 24 15 24 18 21 18 18
16 | 11 18 10 14 15 4 16 10 11 27 5 | 15 26 22 23 23 15 26 16 19 14 18
17 | 9 18 7 10 15 5 14 11 13 12 5 | 9 25 14 12 21 11 23 9 23 12 14
18 | 10 12 8 9 11 5 13 12 9 27 4 | 18 21 19 20 21 17 21 21 20 20 17
19 | 8 15 6 9 15 5 12 11 10 18 4 | 19 25 20 14 30 17 25 18 24 16 19
20 | 8 12 7 9 12 3 14 9 8 20 4 | 21 29 28 27 31 25 29 22 30 28 27
21 | 11 23 10 13 16 5 15 10 13 22 5 | 15 32 21 16 22 15 26 19 19 21 17
22 | 10 13 6 6 11 4 12 10 6 23 3 | 24 24 23 23 27 21 26 24 24 22 21
23 | 8 18 10 12 16 3 16 13 11 20 5 | 15 27 21 18 26 14 27 15 19 16 18
25 | 10 20 6 8 15 5 13 10 8 18 4 | 15 26 22 18 27 17 30 21 24 18 21
26 | 10 10 9 10 12 5 9 9 9 13 4 | 17 22 22 19 27 17 25 20 21 17 20
27E | 22 18 10 10 12 6 14 9 14 19 5 | 32 30 30 33 26 30 31 28 31 26 28
28 | 9 14 8 13 13 5 15 11 9 20 4 | 14 27 23 28 22 20 29 18 23 21 21
29 | 15 17 10 11 12 4 18 12 12 16 5 | 13 23 14 15 21 12 24 18 25 20 16
30 | 10 12 7 9 15 4 6 10 11 16 4 | 24 27 26 23 25 21 29 25 26 24 24
31E | 11 20 7 9 18 6 18 10 11 15 5 | 36 41 36 38 42 35 39 35 41 33 37
32 | 8 17 5 9 11 4 8 10 7 15 4 | 17 26 25 20 28 20 24 18 23 21 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 8 10 14 5 13 11 10 19 |T 23 31 27 26 30 23 31 24 28 24 25
WRMS | 10 16 8 9 13 5 13 11 9 20 |NE 19 27 23 22 27 19 28 20 24 21 21
MEDI | 10 15 7 10 13 5 13 10 10 18 |MD 19 27 22 22 27 20 27 20 24 21 21
Table 3.1702.4 GPS week: 1702 Day: 4 MJD: 56162.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 26 7 7 13 4 16 12 10 10 5 | 30 29 35 30 38 32 36 35 39 29 32
2 | 9 16 10 11 13 2 13 10 13 20 5 | 20 27 24 21 32 22 27 26 31 22 24
3 | 11 12 9 9 13 5 10 13 10 17 4 | 12 21 16 14 15 14 23 18 21 21 15
4 | 14 11 7 11 11 5 11 13 12 21 4 | 30 43 33 34 39 33 41 32 38 43 35
5 | 8 13 8 11 11 5 11 13 11 28 4 | 22 33 29 28 32 26 34 29 30 17 28
6 | 10 12 9 8 14 5 11 11 9 13 4 | 13 27 19 14 20 16 26 18 24 22 18
7E | 10 21 8 12 15 5 16 12 11 14 5 | 24 32 23 24 31 23 28 28 32 30 25
8E | 19 11 8 12 13 6 14 15 10 30 5 | 77 81 76 80 79 76 81 81 82 84 79
9E | 22 17 12 10 12 8 15 10 14 23 5 | 38 38 39 38 29 34 36 34 37 31 34
10 | 11 9 5 7 10 5 7 12 11 15 3 | 18 21 25 25 24 22 22 20 23 13 22
11E | 8 19 8 8 13 4 12 13 12 9 5 | 14 29 23 20 25 19 23 19 28 17 20
12 | 13 16 7 9 12 5 15 13 9 23 4 | 20 30 20 23 25 20 28 25 27 20 22
13 | 8 16 10 11 16 5 13 12 11 19 5 | 15 26 19 19 31 16 25 17 20 15 18
14 | 10 16 8 11 11 4 18 12 10 18 5 | 15 24 18 21 26 17 24 20 21 19 18
15 | 14 17 11 15 12 5 18 11 11 27 5 | 21 28 21 25 27 20 28 23 26 26 21
16 | 11 17 12 12 13 5 16 12 12 28 5 | 15 26 18 23 22 17 28 17 20 14 18
17 | 7 17 10 9 12 4 18 12 12 12 5 | 13 25 20 14 23 14 26 16 21 15 17
18 | 10 13 9 13 11 4 16 12 10 23 5 | 17 24 19 23 18 18 25 21 18 20 17
19 | 8 15 9 10 13 3 15 14 6 17 4 | 19 25 19 15 29 19 28 22 25 16 20
20 | 10 13 7 10 12 3 13 11 10 19 4 | 22 25 25 23 29 23 28 26 24 29 24
21 | 10 17 8 14 15 5 15 12 10 20 5 | 21 27 18 22 25 19 26 23 22 26 19
22 | 9 14 8 9 8 4 16 11 11 22 4 | 17 23 23 24 25 20 23 23 18 18 20
23 | 7 17 10 11 13 4 16 11 12 20 5 | 13 24 18 17 26 15 24 19 20 15 17
25 | 10 22 8 9 12 5 14 13 9 18 5 | 22 27 25 24 27 20 32 26 27 21 24
26 | 8 11 9 11 10 5 9 12 9 17 4 | 14 22 23 21 26 17 22 20 21 12 20
27E | 24 19 11 15 14 7 14 11 12 16 5 | 42 42 40 43 38 38 40 39 42 38 39
28 | 11 14 10 14 11 4 14 10 13 19 5 | 13 26 24 27 24 20 26 18 25 21 22
29 | 18 19 8 11 12 4 12 14 11 17 5 | 12 24 16 20 19 16 23 24 23 25 18
30 | 15 11 8 7 13 4 6 11 12 16 4 | 17 24 21 26 24 21 26 28 25 23 24
31E | 12 18 9 12 15 5 17 12 11 14 5 | 19 29 24 23 27 24 27 22 30 24 23
32 | 12 15 7 8 10 3 12 11 10 14 4 | 17 23 22 19 27 20 28 22 23 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 9 11 13 5 14 12 11 19 |T 21 29 25 25 28 22 29 25 27 24 24
WRMS | 11 16 9 10 12 5 13 12 10 19 |NE 17 26 22 22 26 19 27 22 24 20 21
MEDI | 10 16 8 11 12 5 14 12 11 18 |MD 18 26 23 23 26 20 27 23 25 21 21
Table 3.1702.5 GPS week: 1702 Day: 5 MJD: 56163.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 22 10 8 18 5 12 12 10 13 5 | 30 26 33 29 40 29 37 32 33 27 30
2 | 8 14 7 9 14 4 13 9 9 20 4 | 20 29 24 21 34 22 29 25 30 18 25
3 | 9 11 9 6 17 5 11 10 10 20 4 | 13 23 19 13 19 15 25 20 23 22 17
4 | 14 12 7 10 9 4 11 9 12 21 4 | 40 49 45 41 47 45 49 45 43 52 44
5 | 9 15 8 11 13 4 14 10 12 31 4 | 21 34 29 26 33 24 33 26 32 13 28
6 | 9 11 7 5 16 4 10 7 10 18 3 | 14 25 20 15 21 17 24 19 25 22 18
7E | 12 23 10 11 20 5 19 11 18 22 6 | 33 37 29 32 37 30 35 33 39 34 31
8E | 21 12 9 10 12 6 15 11 15 24 5 | 63 68 60 63 64 62 68 67 63 64 64
9E | 21 16 11 9 14 5 14 10 15 28 5 | 40 34 35 38 29 33 33 37 32 23 33
10 | 9 8 6 7 13 3 9 10 9 16 3 | 15 18 17 18 24 18 19 21 20 16 18
11E | 6 11 10 6 16 4 10 9 13 11 4 | 14 21 20 15 28 15 18 18 21 17 16
12 | 12 14 7 9 13 6 13 9 13 24 4 | 22 31 23 23 26 23 30 25 25 19 24
13 | 8 15 6 9 17 3 14 9 11 17 4 | 14 25 15 16 32 16 26 17 19 13 17
14 | 8 14 7 10 15 3 15 10 13 18 4 | 14 22 17 19 24 15 23 20 24 16 17
15 | 15 19 10 11 11 5 18 11 14 29 5 | 21 31 23 22 27 19 26 23 25 23 21
16 | 10 16 10 12 18 5 16 9 17 30 5 | 15 25 20 18 24 15 27 17 21 10 17
17 | 9 15 11 11 13 4 16 10 12 12 5 | 13 20 13 10 24 13 22 15 26 12 14
18 | 8 12 8 12 11 5 15 9 8 24 4 | 16 23 18 21 18 18 21 21 20 19 17
19 | 10 15 9 8 16 4 14 10 8 19 4 | 20 29 22 15 33 20 29 21 27 14 22
20 | 9 14 7 10 14 4 13 11 14 17 4 | 19 26 23 23 29 22 26 26 29 27 24
21 | 9 15 7 12 18 5 16 9 12 22 5 | 23 28 24 22 28 21 25 27 25 22 22
22 | 9 14 8 7 12 5 17 7 12 20 4 | 15 22 20 20 22 16 21 21 20 14 17
23 | 8 17 6 12 16 4 16 9 12 19 5 | 16 26 19 17 27 17 26 18 23 17 18
25 | 9 20 6 8 15 3 15 9 17 20 5 | 22 29 23 24 26 22 34 26 24 19 24
26 | 8 14 9 11 11 3 8 10 14 18 4 | 15 24 21 21 26 19 24 22 22 14 20
27E | 23 18 11 12 14 6 16 10 15 23 5 | 36 32 33 36 27 32 31 36 32 23 32
28 | 12 15 11 12 13 4 14 10 13 21 5 | 11 22 20 20 22 14 22 14 16 18 16
29 | 18 18 8 10 11 4 15 11 16 20 5 | 16 25 17 18 23 17 24 23 29 21 19
30 | 12 12 5 9 18 6 12 9 16 19 4 | 34 43 40 36 36 37 45 35 44 40 37
31E | 9 14 6 9 13 5 15 10 13 13 4 | 20 25 22 21 30 20 26 25 29 21 23
32 | 9 13 9 7 16 5 11 9 13 14 4 | 17 24 22 18 27 20 26 21 22 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 8 10 15 4 14 10 13 21 |T 22 28 24 23 29 22 29 25 27 22 24
WRMS | 10 15 8 9 14 4 13 10 11 19 |NE 19 27 22 21 27 20 27 23 25 20 21
MEDI | 9 14 8 10 14 4 14 10 13 20 |MD 19 26 22 21 27 20 26 23 25 19 21
Table 3.1702.6 GPS week: 1702 Day: 6 MJD: 56164.000
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 21 5 13 16 4 14 6 12 13 4 | 40 37 46 40 48 40 47 38 49 41 41
2 | 8 13 8 14 16 3 16 5 11 19 4 | 23 31 30 25 40 26 33 25 31 21 28
3 | 10 11 6 13 17 5 12 6 14 18 4 | 13 25 20 13 20 16 27 16 26 28 19
4 | 15 11 6 15 12 4 10 4 7 25 3 | 31 40 36 36 39 34 40 35 36 41 36
5 | 8 14 8 16 13 3 13 7 11 34 4 | 26 36 36 34 40 32 37 29 35 22 33
6 | 9 11 6 13 15 4 11 6 13 20 4 | 11 25 15 11 18 14 24 14 23 26 16
7E | 9 19 7 14 14 5 18 6 12 15 5 | 37 42 39 37 41 35 41 35 44 42 38
8E | 17 16 11 17 16 7 15 8 12 22 5 | 97 94 97 101 95 92 95 94 93 101 95
9E | 25 16 13 13 14 6 15 6 19 31 5 | 39 39 38 41 27 36 39 35 36 31 34
10 | 8 8 6 13 16 3 8 5 10 16 3 | 21 24 26 29 35 25 27 24 25 22 25
11E | 7 19 7 8 16 4 12 7 8 7 4 | 14 30 23 18 26 17 23 15 26 19 19
12 | 14 16 9 14 11 8 18 6 10 25 4 | 25 33 25 24 30 26 32 25 26 21 25
13 | 9 16 7 11 17 4 13 5 7 17 4 | 20 31 25 23 35 20 31 19 22 20 22
14 | 8 14 7 16 15 3 18 5 12 22 4 | 15 23 17 19 25 15 25 15 23 22 16
15 | 14 20 11 20 13 5 17 7 13 28 5 | 24 31 24 33 33 23 30 22 28 26 24
16 | 12 14 8 16 14 4 16 6 9 29 4 | 16 26 23 25 25 18 28 16 26 17 20
17 | 9 16 8 13 13 4 18 6 8 13 4 | 16 26 21 13 25 16 30 15 24 20 19
18 | 7 12 7 16 9 4 13 5 10 23 4 | 19 26 23 22 25 20 25 18 24 25 19
19 | 9 16 4 13 14 4 12 5 9 16 4 | 24 32 24 18 36 24 33 24 28 22 25
20 | 11 12 7 13 16 4 14 7 14 15 4 | 29 38 38 40 44 35 39 33 42 40 36
21 | 7 17 8 17 19 4 13 4 11 16 4 | 18 29 25 15 31 21 28 21 21 21 21
22 | 7 13 7 11 12 3 15 5 13 22 4 | 19 24 22 22 29 19 25 19 22 21 20
23 | 12 16 7 13 16 4 17 6 12 21 4 | 17 30 22 23 32 19 31 18 25 24 21
25 | 8 22 6 10 11 4 13 7 10 19 4 | 21 28 25 21 33 23 34 25 26 21 24
26 | 9 12 9 17 14 3 10 6 8 13 4 | 17 21 24 20 31 20 23 20 21 18 20
27E | 25 20 12 13 18 5 18 7 17 25 5 | 35 38 33 37 31 32 39 32 30 33 31
28 | 10 14 9 15 11 4 17 7 12 24 4 | 16 28 28 31 27 23 31 21 28 29 25
29 | 20 18 7 12 12 4 16 6 12 19 4 | 15 27 19 18 27 18 27 19 30 27 21
30 | 12 10 5 10 14 5 8 4 9 13 3 | 20 30 28 29 30 24 31 25 27 24 27
31E | 10 16 6 8 21 5 18 6 13 12 5 | 17 27 21 20 27 18 25 19 28 19 20
32 | 10 13 7 14 16 3 8 6 7 15 4 | 21 33 30 32 36 28 32 27 33 31 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 8 14 15 4 14 6 11 20 |T 24 32 29 28 33 26 33 25 30 28 27
WRMS | 11 15 7 13 14 4 14 6 10 17 |NE 20 29 26 24 31 23 30 22 28 25 24
MEDI | 10 16 7 13 14 4 14 6 11 19 |MD 20 30 25 24 31 23 31 22 27 24 24
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 4.1702 GPS week: 1702 MJD: 56158.0-56164.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3010 |U 6 7 19 |U 35 23 233 |U 21 18 45 |
emr | emr 2967 | 8 8 21 |U 55 34 317 | 21 20 50 |
esa | esa 2976 | 6 6 19 |U 35 23 240 | 20 15 40 |
gfz | gfz 2965 |U 6 6 19 |U 47 31 290 |U 22 17 44 |
grg | grg 2976 |U 8 8 26 |U 51 36 296 | 21 17 47 |
igr | igr 2976 | 6 6 18 | 37 23 273 | 20 17 44 |
igs | igs 2959 | 6 6 19 | 42 26 251 | 21 17 44 |
jpl | jpl 2966 | 7 7 20 |U 47 28 281 | 20 18 48 |
mit | mit 2976 | 7 7 19 |U 52 33 306 |U 23 21 45 |
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 5.1702.0 GPS week: 1702 Day: 0 MJD: 56158.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 5 6 19 | 9 12 35 | ---- ---- ---- |
emr | emr 2968 | 6 6 20 | 22 12 59 | ---- ---- ---- |
esa | esa 2976 | 4 6 18 | 9 12 38 | ---- ---- ---- |
gfz | gfz 2968 | 5 6 20 | 9 11 37 | ---- ---- ---- |
grg | grg 2976 | 6 8 28 | 19 17 46 | ---- ---- ---- |
igr | igr 2976 | 5 6 19 | 9 12 39 | ---- ---- ---- |
igs | igs 2944 | 4 6 19 | 18 10 51 | ---- ---- ---- |
jpl | jpl 2968 | 6 8 20 | 26 12 60 | ---- ---- ---- |
mit | mit 2976 | 5 5 18 | 20 12 50 | ---- ---- ---- |
Table 5.1702.1 GPS week: 1702 Day: 1 MJD: 56159.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 7 6 16 | 7 6 22 | ---- ---- ---- |
emr | emr 2968 | 8 8 19 | 14 13 31 | ---- ---- ---- |
esa | esa 2976 | 6 7 18 | 7 8 20 | ---- ---- ---- |
gfz | gfz 2967 | 6 7 19 | 10 12 24 | ---- ---- ---- |
grg | grg 2976 | 10 10 28 | 15 14 36 | ---- ---- ---- |
igr | igr 2976 | 6 8 19 | 7 7 21 | ---- ---- ---- |
igs | igs 2943 | 6 7 18 | 10 9 25 | ---- ---- ---- |
jpl | jpl 2968 | 7 7 20 | 15 10 33 | ---- ---- ---- |
mit | mit 2976 | 7 7 19 | 15 11 41 | ---- ---- ---- |
Table 5.1702.2 GPS week: 1702 Day: 2 MJD: 56160.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 5 7 21 | 203 118 1501 | ---- ---- ---- |
emr | emr 2968 | 8 10 23 | 283 169 1989 | ---- ---- ---- |
esa | esa 2976 | 6 8 21 | 208 113 1544 | ---- ---- ---- |
gfz | gfz 2966 | 6 7 21 | 259 133 1860 | ---- ---- ---- |
grg | grg 2976 | 7 8 26 | 266 164 1848 | ---- ---- ---- |
igr | igr 2976 | 6 7 21 | 222 115 1772 | ---- ---- ---- |
igs | igs 2952 | 6 7 21 | 210 118 1561 | ---- ---- ---- |
jpl | jpl 2968 | 8 8 23 | 223 130 1753 | ---- ---- ---- |
mit | mit 2976 | 7 8 22 | 268 161 1923 | ---- ---- ---- |
Table 5.1702.3 GPS week: 1702 Day: 3 MJD: 56161.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 7 6 17 | 6 7 21 | ---- ---- ---- |
emr | emr 2968 | 8 7 21 | 12 10 32 | ---- ---- ---- |
esa | esa 2976 | 6 5 16 | 6 7 24 | ---- ---- ---- |
gfz | gfz 2967 | 6 5 16 | 13 14 29 | ---- ---- ---- |
grg | grg 2976 | 7 8 24 | 14 14 30 | ---- ---- ---- |
igr | igr 2976 | 6 5 15 | 6 6 24 | ---- ---- ---- |
igs | igs 2970 | 6 5 17 | 13 9 31 | ---- ---- ---- |
jpl | jpl 2966 | 8 6 18 | 19 13 34 | ---- ---- ---- |
mit | mit 2976 | 6 5 16 | 15 11 33 | ---- ---- ---- |
Table 5.1702.4 GPS week: 1702 Day: 4 MJD: 56162.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 16 | 5 6 13 | 46 28 96 |
emr | emr 2968 | 8 8 22 | 17 9 35 | 44 31 100 |
esa | esa 2976 | 7 6 18 | 5 7 13 | 41 20 81 |
gfz | gfz 2964 | 7 6 18 | 15 16 30 | 43 24 91 |
grg | grg 2976 | 8 9 24 | 14 15 26 | 40 19 83 |
igr | igr 2976 | 7 6 17 | 5 7 14 | 41 24 91 |
igs | igs 2974 | 7 7 18 | 12 9 22 | 43 26 90 |
jpl | jpl 2965 | 8 8 21 | 12 7 26 | 41 27 96 |
mit | mit 2976 | 8 6 16 | 13 11 23 | 49 34 89 |
Table 5.1702.5 GPS week: 1702 Day: 5 MJD: 56163.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 8 22 | 8 7 19 | 9 17 22 |
emr | emr 2966 | 9 8 23 | 19 11 33 | 10 17 28 |
esa | esa 2976 | 7 7 21 | 7 6 20 | 10 15 21 |
gfz | gfz 2963 | 7 6 20 | 10 15 27 | 13 17 25 |
grg | grg 2976 | 9 8 33 | 16 14 47 | 12 20 37 |
igr | igr 2976 | 7 6 21 | 7 7 18 | 10 17 24 |
igs | igs 2974 | 7 6 21 | 17 13 33 | 9 15 23 |
jpl | jpl 2964 | 8 6 21 | 15 9 27 | 11 16 26 |
mit | mit 2976 | 7 8 20 | 18 13 38 | 11 19 28 |
Table 5.1702.6 GPS week: 1702 Day: 6 MJD: 56164.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 19 | 5 7 20 | 8 9 19 |
emr | emr 2964 | 9 7 19 | 19 11 38 | 10 12 23 |
esa | esa 2976 | 6 6 18 | 5 9 18 | 9 10 17 |
gfz | gfz 2963 | 6 6 18 | 12 15 24 | 9 9 16 |
grg | grg 2976 | 9 8 21 | 16 16 40 | 12 11 22 |
igr | igr 2976 | 7 6 17 | 5 7 20 | 9 9 17 |
igs | igs 2959 | 7 6 19 | 16 12 34 | 10 11 19 |
jpl | jpl 2963 | 8 8 19 | 21 18 35 | 10 10 21 |
mit | mit 2976 | 7 7 20 | 15 13 37 | 10 11 19 |
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 6.1702 GPS week: 1702 MJD: 56158.500-56164.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -3 -89 29 -10 6 | 7 15
| 20 26 73 50 9 | 4
emr uuuuu | -18 30 -145 -33 7 | 17 24
| 13 15 78 54 5 | 6
esa uuuuu | 8 -49 74 119 4 | 14 19
| 25 42 51 36 4 | 5
gfz uuuuu | 19 0 -12 -62 2 | 6 13
| 15 25 106 59 4 | 5
grg uuuux | 34 7 -89 -14 -11 | 45 57
| 23 24 39 74 44 | 4
igr xxxxx | -5 10 -1 -10 9 | 4 16
| 24 16 43 55 5 | 7
irf xxxxx | 1 -5 46 -8 -8 | 5 12
| 13 17 72 22 5 | 3
jpl uuuuu | -25 -8 -47 0 7 | 47 48
| 24 35 58 49 13 | 5
mit uuuuu | -19 -11 158 -5 -12 | 18 21
| 13 22 140 48 10 | 2
ngs uuuuu | -11 69 -57 -77 -2 | 12 17
| 40 42 184 140 4 | 4
sio xxxxx | 24 16 65 -121 12 | 40 42
| 11 24 71 69 5 | 8
Table 7.1702.0 GPS week: 1702 Day: 0 MJD: 56158.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -24 -124 1 -26 0 | 1 11
emr uuuuu | -23 14 -239 57 13 | 8 17
esa uuuuu | 24 29 48 133 -4 | 8 12
gfz uuuuu | 37 -45 139 -46 -1 | 0 11
grg uuuux | 4 -22 -99 -80 -47 | 47 56
igr xxxxx | -17 -5 -7 -51 0 | -5 13
irf xxxxx | 0 -30 190 3 -6 | 1 11
jpl uuuuu | -8 -57 -14 -26 -10 | 41 42
mit uuuuu | -16 -49 443 31 -9 | 15 18
ngs uuuuu | -85 108 -363 -212 4 | 5 14
sio xxxxx | 29 -22 -27 -109 12 | 29 31
Table 7.1702.1 GPS week: 1702 Day: 1 MJD: 56159.500
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 | -7 -114 43 -11 3 | 2 12
emr uuuuu | -41 21 -89 -15 4 | 11 20
esa uuuuu | 41 -50 -20 53 6 | 8 13
gfz uuuuu | 10 -8 71 -81 -1 | 1 11
grg uuuux | 15 -17 -44 -7 -55 | 46 56
igr xxxxx | -27 29 -29 16 11 | -4 13
irf xxxxx | -22 -12 63 14 -3 | 2 11
jpl uuuuu | 8 -30 22 -17 5 | 42 43
mit uuuuu | -45 -11 170 60 -3 | 15 19
ngs uuuuu | -31 139 -158 -47 -8 | 8 15
sio xxxxx | 9 -7 10 -69 9 | 32 34
Table 7.1702.2 GPS week: 1702 Day: 2 MJD: 56160.500
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 | -15 -92 139 -51 -1 | 5 15
emr uuuuu | -15 35 -88 -54 13 | 14 23
esa uuuuu | -6 -70 80 124 8 | 12 18
gfz uuuuu | -2 -6 42 46 1 | 4 13
grg uuuux | 50 13 -54 -90 -58 | 44 55
igr xxxxx | -21 32 -38 88 13 | 0 16
irf xxxxx | -6 23 36 -1 -10 | 5 13
jpl uuuuu | -30 -24 19 -8 -7 | 45 47
mit uuuuu | -17 18 97 10 -15 | 18 22
ngs uuuuu | 27 81 -171 -148 -6 | 11 17
sio xxxxx | 10 39 127 -152 12 | 37 40
Table 7.1702.3 GPS week: 1702 Day: 3 MJD: 56161.500
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 | -10 -62 -1 23 0 | 8 15
emr uuuuu | -17 34 -207 -40 5 | 19 25
esa uuuuu | 15 -43 64 175 7 | 16 20
gfz uuuuu | 17 -2 -48 -118 -3 | 7 13
grg uuuux | 18 4 -75 -97 -19 | 41 54
igr xxxxx | -16 15 -12 -71 11 | 5 16
irf xxxxx | 5 -9 44 -31 -5 | 7 13
jpl uuuuu | -67 14 -50 -2 8 | 47 48
mit uuuuu | -6 -26 149 -6 -6 | 19 22
ngs uuuuu | 17 51 38 -24 0 | 14 17
sio xxxxx | 21 11 37 -158 13 | 41 44
Table 7.1702.4 GPS week: 1702 Day: 4 MJD: 56162.500
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 | 39 -85 49 -91 11 | 6 14
emr uuuuu | 2 44 -236 -18 6 | 21 26
esa uuuuu | -29 -61 111 118 2 | 16 20
gfz uuuuu | 25 37 -60 -35 2 | 7 13
grg uuuux | 41 8 -160 80 33 | 41 55
igr xxxxx | 6 -6 21 -44 12 | 6 16
irf xxxxx | 7 1 39 13 -8 | 6 12
jpl uuuuu | -37 -24 -85 109 7 | 47 49
mit uuuuu | -18 -9 181 5 -13 | 18 22
ngs uuuuu | 25 35 100 -266 -1 | 14 17
sio xxxxx | 36 17 120 5 16 | 42 45
Table 7.1702.5 GPS week: 1702 Day: 5 MJD: 56163.500
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 | -5 -53 72 52 23 | 9 16
emr uuuuu | -10 51 -96 -36 7 | 22 27
esa uuuuu | -12 -110 99 106 6 | 18 22
gfz uuuuu | 39 16 -44 -68 10 | 9 14
grg uuuux | 38 50 -113 51 34 | 47 60
igr xxxxx | 42 7 86 -28 11 | 9 18
irf xxxxx | 22 4 -24 -13 -19 | 7 13
jpl uuuuu | -21 42 -131 -32 24 | 50 52
mit uuuuu | -5 1 22 -59 -34 | 19 22
ngs uuuuu | -29 40 167 27 -2 | 14 18
sio xxxxx | 30 27 161 -194 19 | 46 49
Table 7.1702.6 GPS week: 1702 Day: 6 MJD: 56164.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 0 -95 -98 31 9 | 15 21
emr uuuuu | -25 12 -64 -123 0 | 26 31
esa uuuuu | 23 -38 135 125 1 | 22 25
gfz uuuuu | 8 5 -185 -129 3 | 13 18
grg uuuux | 71 8 -78 43 36 | 51 65
igr xxxxx | -1 -5 -28 20 5 | 15 20
irf xxxxx | 0 -13 -24 -44 -5 | 9 12
jpl uuuuu | -23 20 -90 -24 23 | 56 58
mit uuuuu | -24 -1 44 -74 -7 | 19 22
ngs uuuuu | -5 28 -11 132 -2 | 18 19
sio xxxxx | 34 43 23 -169 3 | 52 55
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