[IGSREPORT-21336] Wk 1712 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Nov 15 12:22:56 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1712 (Oct 28, 2012 - Nov 03, 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:
igs1712[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1712[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1712[0-6].cls IGS GPS clock combination summary report.
igs17127.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17127.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL.
The other centres are excluded because of poorer consistency (GRG), they provide
broadcast clocks (NGS), or clock corrections are not provided (SIO). The clock
information not used is still compared to combination for completeness. The
value of 999999.999999 microseconds, according to the sp3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks contributed
from that AC should not be included with weight in this combination. This is
done to ensure a high level of consistency between the TRF and the orbital
frame. However, there is an exception for the clocks if the AC is the reference
center. In that case, only the clocks from that AC are included with weight.
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. Starting 16-Sep-2012 (GPS Week 1706,
day 0, MJD 56186) the CODE Analysis Center began submitting two solutions: COD
(1d SNX with 3d orbital arcs) and COF (1d SNX with 1d orbital arcs). The COD
clocks and orbits are included for comparison only; the COF solution is
included with weight, and is the reference clock center.
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 | COF | KOUC KOUC
0 | EMR | 32 32
0 | ESA | AREQ
0 | GFZ | 32 ARTU BOGT LHAZ POLV RESO SOFI YELL
0 | GRG | MCM4 SOFI YEBE BARH MCM4 NTUS SOFI YEBE
0 | JPL | 21 32
0 | MIT | 16 21 22 32 16 21 22 24 32 AREQ NTUS SOFI GMAS NICO
0 | MIT | NTUS SOFI
1 | COF | HERT MATE HERT MATE
1 | EMR | 32 32 WUHN
1 | ESA | AREQ
1 | GFZ | BOGT BOR1 CHPI MCM4 PALM POLV SFER WSRT
1 | GRG | 13 13 NOVM
1 | JPL | 21 REUN
1 | MIT | 24 32 24 32 GMAS
2 | COF | 32 32 KOUC KOUC
2 | EMR | HERS HERS
2 | ESA | 32 32
2 | GFZ | ARTU BOGT LHAZ LPGS
2 | GRG | HYDE LPGS HYDE LPGS
2 | JPL | PIMO
2 | MIT | GMAS JPLM
3 | ALL | 13
3 | COD | KOSG
3 | COF | 32 32 KOUC KOSG KOUC SUTM
3 | EMR | THTI
3 | ESA | 32 32 AREQ
3 | GFZ | BOGT METS POLV SFER
3 | GRG | 13 HYDE HYDE LHAZ RAMO
3 | JPL | 30
4 | COF | 18 22 30 32 18 22 32 KOUC MATE MOBS ALRT FLRS KOUC
4 | COF | MATE MOBS
4 | EMR | 30
4 | ESA | 30 32 32 FLIN TIXI
4 | GFZ | BOGT
4 | GRG | 30 ALRT MAC1 USNO XMIS MAL2 MATE USNO XMIS
4 | JPL | 30
4 | MIT | 5 24 5 24 30 MAC1 NTUS
5 | COF | 30 32 30 32 ALIC KOUC ALIC FLRS KOUC
5 | EMR | CHUR
5 | ESA | 30 32 30 32 CHUR AREQ
5 | GFZ | ASPA HOFN LHAZ POLV
5 | GRG | WSRT ADIS THTI WSRT
5 | JPL | 10
5 | MIT | 2 10 21 2 10 21 24 GMAS
6 | COD | KOUC KOUC
6 | COF | 30 32 10 30 32 KOUC AREQ KOUC
6 | ESA | 10 30 32 10 30 32 MATE MATE
6 | GFZ | 10 30 ABPO KERG LHAZ MAC1 SUTM
6 | GRG | SOFI WSRT ADIS AREQ KOUC SOFI WSRT
6 | JPL | MAC1
6 | MIT | 19 22 19 22 MAC1 GMAS MAC1
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | ESA | ALL (high Transformation - See Table 2)
4 | ESA | ALL (high Transformation - See Table 2)
4 | SIO | ALL (high Transformation - See Table 2)
5 | SIO | ALL (high Transformation - See Table 2)
6 | ESA | ALL (high Transformation - See Table 2)
6 | SIO | ALL (high Transformation - See Table 2)
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G30 | | | | 1 | | | |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products,
are based on the updated IGS08 frame (IGb08).
For more information see IGSMAIL #6663.
8. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the current IGS reference frame. These rotations were
estimated in the IGS SINEX combination process, performed by the IGS Reference
Frame Coordinator at the Institut Geographique National (IGN). 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]
-------+-----+---------------------------------------------------
COD | 0 | .2 1.3 .0 -45 -2 -20 -.24
COF | 0 | .3 1.2 -.7 -44 -5 -9 -.08
EMR | 0 | 2.1 6.1 5.3 1 10 8 .22
ESA | 0 | 5.8 3.9 -9.2 108 -237 126 -.12
GFZ | 0 | -.4 .7 -.3 -40 -44 -18 .0
GRG | 0 | 1.8 1.3 -4.4 -23 47 -72 .14
JPL | 0 | .0 -.6 10.4 -38 1 24 .03
MIT | 0 | 6.1 7.2 4.5 -7 5 -34 .09
NGS | 0 | 5.8 -2.4 6.0 -41 -21 40 .26
SIO | 0 | 3.1 1.9 -15.8 38 -137 -109 .11
COD | 1 | .2 1.2 .0 -38 5 -10 -.23
COF | 1 | .2 1.1 .5 -25 17 -22 -.40
EMR | 1 | 8.9 11.0 8.5 -3 7 -3 -.04
ESA | 1 | 9.1 8.4 -17.4 200 -352 106 -.22
GFZ | 1 | .2 .8 .0 -31 -52 -30 -.09
GRG | 1 | 5.5 7.0 4.7 -36 24 -49 -.02
JPL | 1 | 6.5 7.9 12.8 -42 22 -16 -.31
MIT | 1 | 12.5 6.3 5.6 -9 0 -22 -.02
NGS | 1 | 9.0 -.2 6.5 -38 -43 69 .05
SIO | 1 | 2.6 4.9 -13.4 34 -74 -243 -.08
COD | 2 | 1.0 1.4 .2 -36 -3 -32 -.31
COF | 2 | 1.1 1.8 .2 -42 -5 -24 -.24
EMR | 2 | 3.4 9.4 6.8 3 0 1 .09
ESA | 2 | 8.4 6.6 -14.2 171 -305 126 -.25
GFZ | 2 | .6 .8 -.5 -28 -50 -22 -.20
GRG | 2 | -1.4 -1.1 1.2 -32 27 -50 .34
JPL | 2 | 2.0 10.3 11.9 -38 6 -39 -.08
MIT | 2 | 6.2 8.3 2.4 -5 3 -28 .0
NGS | 2 | 11.4 1.0 6.3 -29 -41 82 .18
SIO | 2 | 4.7 2.3 -20.1 62 -177 -96 -.01
COD | 3 | .9 1.0 -.4 -42 -11 -5 -.25
COF | 3 | 1.0 .9 -.4 -40 -16 -1 -.25
EMR | 3 | 5.7 10.7 4.3 -5 -2 0 .04
ESA | 3 | 11.7 6.8 -16.6 191 -388 128 -.24
GFZ | 3 | .4 1.0 -.8 4 -69 -19 -.18
GRG | 3 | .5 -1.6 -2.5 -16 52 -56 .24
JPL | 3 | 6.1 5.7 8.6 -77 42 -1 .02
MIT | 3 | 6.8 9.6 1.3 -7 2 -30 .01
NGS | 3 | 2.8 5.1 .4 5 -11 30 .23
SIO | 3 | 2.7 3.8 -23.0 41 -175 -192 -.15
COD | 4 | .9 1.1 -.3 -40 -4 -18 -.21
COF | 4 | .7 1.3 -.8 -35 6 -14 -.18
EMR | 4 | 5.5 11.9 .4 10 15 5 .0
ESA | 4 | 10.5 7.9 -19.0 242 -369 121 .03
GFZ | 4 | 1.1 .8 .9 -21 -79 -29 -.12
GRG | 4 | 1.9 .2 -.4 -5 50 -31 .17
JPL | 4 | -1.5 8.0 7.4 -65 26 -13 .34
MIT | 4 | 7.0 11.1 -2.9 -6 2 -26 .06
NGS | 4 | 3.8 2.2 -.2 5 -17 29 .30
SIO | 4 | 4.7 4.5 -31.4 29 -261 -262 -.03
COD | 5 | .6 .7 .0 -49 3 -19 -.18
COF | 5 | .7 .5 .3 -51 12 -23 -.12
EMR | 5 | 3.9 12.9 -1.6 -1 14 4 .21
ESA | 5 | 7.6 4.1 -18.8 172 -314 128 .24
GFZ | 5 | 1.1 .0 .0 -28 -56 -12 .03
GRG | 5 | 3.5 1.5 6.5 -16 35 -34 .20
JPL | 5 | -1.6 4.9 4.5 -24 19 -41 .09
MIT | 5 | 7.8 7.5 .7 0 -2 -28 .18
NGS | 5 | 1.6 2.1 -.4 -2 -8 24 .32
SIO | 5 | 1.5 4.2 -45.9 92 -252 -183 .21
COD | 6 | .5 .9 .5 -55 3 -20 -.17
COF | 6 | .9 .8 .2 -41 1 -25 -.19
EMR | 6 | 7.3 5.6 -5.7 13 12 -11 .22
ESA | 6 | 7.8 5.4 -15.3 176 -343 103 .25
GFZ | 6 | 1.4 -.4 -.4 -22 -46 -26 .05
GRG | 6 | 2.1 1.8 -6.9 -15 46 -44 .35
JPL | 6 | 2.8 -2.2 2.7 0 -2 10 .32
MIT | 6 | 7.7 7.9 -2.9 -3 7 -31 .16
NGS | 6 | 3.2 3.2 7.3 -37 -11 27 .47
SIO | 6 | 3.2 2.5 -53.6 114 -361 -120 .12
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and ERPs
as generated by IGN). For more information see IGSMAIL #2750. Because of this
change in alignment, Table 2 has been enhanced with one additional line per AC.
This additional line shows 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.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) the igs08.atx absolute
antenna model file gives updated (IGSMAIL #6662) values for the JPSREGANT_DD
and JPSREGANT_SD antennas, plus updates for GPS IIF transmit antennas. This
updated file should be used in conjunction with IGb08. Though, igs08.atx is
also still consistent with IGS08.
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 1.1712.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1712.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 2.1712.[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 3.1712.[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 5.1712.0-6).
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 1712 summary. (Oct 28, 2012 - Nov 03, 2012)
Table 1.1712.a GPS week: 1712 MJD: 56228.000-56234.000
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 261| 0 0 0 100 -53 4 -.45 11 11 | -678 -314 42 100
| 0 0 2 34 59 16 .03 | 826 1400
cof 254| 1 0 0 85 -79 13 -.44 12 12 | -641 -309 20 95
| 1 0 1 39 63 19 .02 | 827 1403
emr 80| -2 1 1 -5 -53 7 .27 16 16 | 2424 333 15 100
| 1 1 2 44 47 22 .03 | 854 582
esa 175| 0 0 1 -236 325 12 .04 7 7 | -1326 1092 12 115
| 0 0 1 113 126 19 .03 | 743 814
gfz 184| -1 0 -1 -9 16 10 -.43 13 12 | -139 217 21 142
| 1 0 1 61 65 19 .05 | 284 337
grg 126| 0 0 -1 36 -129 -25 .43 15 14 | -168 110 14 155
| 1 1 1 57 34 17 .07 | 326 467
igr n/a| 0 0 0 10 -42 -23 -.15 4 4 | 4350 496 17 100
| 0 0 0 30 58 12 .01 | 851 548
jpl 80| -1 0 0 66 -54 5 .42 14 13 | 3234 86 17 160
| 1 0 1 62 55 11 .02 | 978 523
mit 239| 0 0 -1 18 -60 0 -.17 6 6 | -122 -107 21 200
| 0 0 0 45 56 12 .02 | 393 567
ngs 239| 0 0 2 70 5 5 .39 12 10 | -682 -243 1708 3441
| 0 0 3 74 62 28 .02 | 594 1031
sio 272| 0 -1 0 -119 339 -171 -.21 18 16 | --- --- --- ---
| 0 1 1 69 235 66 .03 | --- ---
Table 1.1712.b GPS week : 1712 MJD: 56228.000-56234.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 5 4 4 |
2 | 4 4 4 5 5 5 5 |
3 | 4 3 3 4 4 4 4 |
4 | 4 4 4 4 4 3 4 |
5 | 4 3 4 4 4 4 5 |
6 | 3 3 3 4 5 4 4 |
7 | 4 4 4 4 5 5 5 |
8 | 4 3 3 4 4 4 4 |
9 | 4 4 3 4 4 4 4 |
10 | 6 6 7 6 7 6 5 |
11 | 4 3 4 4 5 4 4 |
12 | 4 5 5 6 6 5 6 |
13 | 4 4 4 5 5 4 5 |
14 | 4 4 4 4 5 5 5 |
15 | 4 4 4 5 5 4 4 |
16 | 4 4 4 5 5 4 4 |
17 | 4 4 4 5 5 4 5 |
18 | 3 4 4 4 4 4 4 |
19 | 4 5 5 5 5 5 5 |
20 | 3 3 4 4 5 3 4 |
21 | 4 4 4 4 5 4 4 |
22 | 3 3 3 4 5 4 4 |
23 | 4 4 4 5 6 5 5 |
24 | 8 9 8 9 12 10 15 |
25 | 5 4 5 5 5 5 5 |
26 | 3 3 3 4 4 3 4 |
27 | 0 0 0 0 0 0 0 |
28 | 4 3 4 4 4 4 4 |
29 | 4 4 4 5 5 5 5 |
30 | 4 4 5 6 6 5 6 |
31 | 4 4 5 5 5 5 6 |
32 | 4 4 5 5 6 5 6 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1712.0 GPS week: 1712 Day: 0 MJD: 56228.000
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 265| -1 0 -1 90 -44 -1 -.41 10 10 | -1403 413 34 112
| 1 1 |
cof 259| 1 0 0 95 -46 17 -.42 11 11 | -1365 401 18 106
| 58 36 |
emr 80| -1 1 1 -15 -26 25 .23 16 16 | 1772 628 12 106
| 48 -31 |
esa 175| 0 0 2 -71 163 30 .06 6 6 | -1318 788 11 161
| -36 134 |
gfz 187| -2 0 -3 -30 -86 -4 -.35 11 10 | 196 69 22 190
| -39 -55 |
grg 128| 0 2 -3 42 -129 -47 .49 17 16 | -464 398 16 152
| 31 -16 |
igr n/a| 0 -1 0 15 -35 -21 -.14 4 4 | 3370 473 16 108
| -53 93 |
jpl 80| 0 0 -1 76 -12 6 .44 13 13 | 2877 613 16 155
| 60 22 |
mit 240| 0 0 -2 1 -126 -15 -.14 7 6 | -372 291 20 241
| -8 1 |
ngs 242| 0 -1 5 130 27 13 .42 13 10 | -1300 274 1737 3592
| -158 39 |
sio 285| 0 -2 -1 -140 177 -99 -.20 18 15 | --- --- --- ---
| 75 -93 |
Table 2.1712.1 GPS week: 1712 Day: 1 MJD: 56229.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 264| 0 0 -1 117 -140 22 -.46 12 12 | -1860 1596 38 100
| 57 33 |
cof 259| 2 0 -1 68 -184 18 -.43 13 12 | -1821 1601 22 96
| 69 34 |
emr 80| 0 3 3 37 -116 33 .24 17 17 | 1850 880 13 103
| 18 -46 |
esa 175| 0 0 0 -254 288 30 .06 6 6 | -1681 1906 12 111
| 62 31 |
gfz 189| 0 0 0 22 79 1 -.41 12 11 | -72 55 22 141
| -13 -58 |
grg 128| -1 1 -2 116 -146 -9 .42 14 14 | -577 627 14 168
| 12 17 |
igr n/a| 1 0 0 39 -131 -16 -.16 4 4 | 3380 1006 17 107
| -2 44 |
jpl 80| -2 0 0 95 -150 13 .43 14 14 | 3214 718 16 163
| 64 15 |
mit 240| 1 0 -1 60 -60 14 -.18 5 5 | -620 715 21 205
| -19 -15 |
ngs 241| 0 0 2 146 -100 -23 .39 12 9 | -1458 1044 1543 3273
| -56 132 |
sio 214| 0 -3 0 -43 41 -230 -.24 17 15 | --- --- --- ---
| 51 -36 |
Table 2.1712.2 GPS week: 1712 Day: 2 MJD: 56230.000
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 262| 0 0 -1 111 -108 15 -.46 14 13 | -383 -462 48 90
| 48 0 |
cof 258| 2 0 -3 104 -122 21 -.44 14 14 | -354 -443 19 79
| 40 34 |
emr 80| 0 2 3 3 -89 16 .27 16 16 | 2764 534 15 103
| 27 -33 |
esa 175| 0 0 1 -209 213 13 -.01 6 6 | -1590 1398 11 102
| 28 72 |
gfz 188| -2 0 -2 101 -10 12 -.45 13 12 | -89 -222 19 124
| -45 -81 |
grg 127| -1 0 1 74 -178 -22 .50 15 14 | 177 -628 15 161
| 31 15 |
igr n/a| 0 0 0 20 -101 -32 -.15 4 4 | 4432 530 17 86
| -47 45 |
jpl 80| 0 -1 1 75 -85 7 .39 15 14 | 3961 162 17 152
| 36 1 |
mit 240| 0 0 -1 79 -110 -4 -.17 7 6 | -21 -196 19 173
| 5 -3 |
ngs 240| 1 1 0 84 -31 -19 .40 12 9 | -370 -483 1433 3190
| -105 39 |
sio 282| 0 -1 0 -64 205 -85 -.20 17 16 | --- --- --- ---
| 48 -143 |
Table 2.1712.3 GPS week: 1712 Day: 3 MJD: 56231.000
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 261| -1 0 1 103 34 19 -.46 11 10 | 751 -3007 34 90
| -12 -6 |
cof 254| 2 -1 2 87 6 37 -.43 14 13 | 792 -3012 21 91
| 30 43 |
emr 80| 0 0 2 18 15 21 .25 15 15 | 4042 -558 15 107
| 22 -1 |
esa 175| 1 0 3 -243 506 29 .07 9 9 | -206 308 12 126
| 10 -8 |
gfz 186| -2 -2 -3 -94 -17 51 -.43 15 15 | 175 406 24 159
| -22 -63 |
grg 126| 0 0 0 15 -74 -25 .48 16 15 | 339 -284 14 147
| 29 -9 |
igr n/a| 1 0 1 12 22 1 -.16 5 5 | 5697 -391 16 119
| -40 68 |
jpl 80| -3 0 2 155 -49 18 .42 13 13 | 4725 -495 16 158
| -4 23 |
mit 240| 0 0 0 -50 -69 6 -.18 5 5 | 634 -1002 22 203
| 9 -4 |
ngs 239| 2 0 -1 29 75 32 .40 11 10 | 332 -2301 1783 3632
| -67 -18 |
sio 280| -1 0 1 -101 293 -184 -.20 15 15 | --- --- --- ---
| 21 -138 |
Table 2.1712.4 GPS week: 1712 Day: 4 MJD: 56232.000
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 260| -1 1 3 34 -7 0 -.46 12 11 | -458 -656 70 106
| 48 4 |
cof 251| 0 1 0 23 -48 25 -.46 12 12 | -408 -660 23 98
| 31 17 |
emr 80| -3 0 2 -83 -32 -4 .28 16 16 | 2745 -339 18 79
| 15 -16 |
esa 175| 1 2 0 -447 463 -9 .00 9 8 | -520 -123 15 119
| 90 3 |
gfz 178| 0 0 0 -3 91 13 -.50 13 13 | -204 197 22 127
| -42 -85 |
grg 128| 2 -1 0 -59 -112 -6 .39 14 14 | -253 338 17 162
| 57 27 |
igr n/a| 1 0 0 -45 3 -30 -.15 5 5 | 4816 -56 19 100
| -42 56 |
jpl 80| -1 -1 0 47 -31 10 .39 13 13 | 3697 -693 22 155
| 14 -21 |
mit 240| 1 0 -1 46 18 -9 -.17 7 7 | -228 189 25 200
| -19 -40 |
ngs 235| 0 -1 0 -75 66 -29 .38 11 10 | -579 -256 1795 3458
| -46 12 |
sio 284| 0 0 1 -70 526 -262 -.21 18 17 | --- --- --- ---
| 33 -265 |
Table 2.1712.5 GPS week: 1712 Day: 5 MJD: 56233.000
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 260| 0 0 1 149 -76 -24 -.48 10 10 | -732 -202 35 108
| 42 -10 |
cof 250| 2 0 0 152 -111 -5 -.48 12 12 | -697 -191 21 106
| 41 24 |
emr 80| -5 0 1 40 -94 -14 .28 16 16 | 1555 934 16 105
| 26 -4 |
esa 175| 1 0 0 -175 273 11 .01 7 7 | -2401 2093 11 100
| 33 76 |
gfz 183| -1 0 -2 -8 -10 -2 -.46 14 14 | -400 167 20 118
| -21 -47 |
grg 124| 0 0 -1 63 -154 -49 .30 16 15 | -181 -158 14 153
| 27 36 |
igr n/a| 0 0 0 39 -62 -30 -.16 4 4 | 3927 1076 19 88
| -3 71 |
jpl 80| -3 -1 2 63 -71 -7 .41 14 13 | 2108 225 18 173
| 76 -25 |
mit 239| 0 0 0 5 -87 -5 -.18 7 6 | -238 -547 21 190
| 17 -21 |
ngs 240| 0 0 0 82 -24 36 .35 11 10 | -730 -132 1983 3512
| -185 38 |
sio 281| -1 0 1 -178 392 -202 -.25 18 18 | --- --- --- ---
| 112 -230 |
Table 2.1712.6 GPS week: 1712 Day: 6 MJD: 56234.000
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 95 -31 -1 -.41 11 10 | -665 116 39 96
| 51 21 |
cof 253| 0 0 0 65 -46 -20 -.44 11 11 | -637 138 18 89
| 48 40 |
emr 80| -1 0 -2 -37 -31 -24 .33 15 15 | 2242 258 17 102
| 2 1 |
esa 175| 0 1 1 -253 370 -16 .06 9 9 | -1571 1278 12 90
| 31 48 |
gfz 181| 0 -1 0 -56 68 0 -.43 11 10 | -583 852 19 140
| -50 -18 |
grg 127| 0 1 -1 1 -109 -15 .43 16 15 | -218 480 13 147
| 23 46 |
igr n/a| 0 0 0 -12 4 -32 -.15 4 4 | 4829 840 15 96
| -26 33 |
jpl 80| 0 0 0 -51 21 -12 .45 13 13 | 2056 74 16 169
| 74 -35 |
mit 239| 1 0 -1 -12 13 17 -.15 6 6 | -11 -199 21 189
| -3 -28 |
ngs 240| 0 0 8 95 29 25 .39 11 10 | -671 151 1683 3431
| -83 46 |
sio 278| -1 0 3 -236 738 -132 -.16 20 19 | --- --- --- ---
| 125 -352 |
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 3.1712.0 GPS week: 1712 Day: 0 MJD: 56228.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 9 14 15 8 11 16 4 11 5 11 13 3 | 32 33 36 38 36 48 35 51 37 41 41 37
2 | 7 7 18 6 14 16 5 16 8 12 22 4 | 18 22 28 22 20 28 18 30 18 26 17 19
3 | 6 10 11 5 10 17 4 9 8 11 16 3 | 17 19 24 24 22 33 20 30 19 27 25 21
4 | 7 7 11 5 10 15 4 11 5 14 35 4 | 34 33 30 30 38 35 31 28 34 25 32 30
5E | 8 8 15 5 12 15 6 17 7 12 10 3 | 34 35 43 40 39 47 38 42 39 42 36 38
6 | 5 8 10 5 12 14 2 9 5 8 11 3 | 24 26 29 29 24 34 26 33 24 28 28 25
7 | 13 9 13 7 10 14 5 15 5 11 18 3 | 17 21 22 18 18 25 15 21 15 22 17 14
8 | 11 12 12 6 10 12 4 11 6 11 23 3 | 17 21 20 15 16 19 14 22 15 18 18 13
9 | 12 8 13 6 11 12 3 10 9 15 15 3 | 15 17 20 15 18 21 15 24 17 23 20 15
10E | 15 18 26 8 14 19 6 18 8 32 25 6 | 22 24 36 23 28 27 20 30 25 40 23 22
11 | 8 14 17 6 8 15 5 12 5 10 10 3 | 30 29 40 30 33 44 31 40 33 30 31 31
12 | 10 11 21 6 10 18 6 20 8 11 14 4 | 19 24 24 21 22 30 19 27 21 27 20 19
13 | 9 9 13 6 13 20 4 14 7 12 13 3 | 18 23 29 22 24 35 20 29 20 21 20 20
X14 | 8 11 17 5 11 --- 4 12 7 11 12 3 | 17 22 21 18 23 --- 18 27 19 21 19 17
15 | 9 10 16 7 7 15 4 14 8 12 17 3 | 18 17 24 21 20 33 18 27 21 26 19 19
16 | 6 8 16 6 10 19 3 15 5 9 14 3 | 20 24 27 23 19 31 20 27 20 24 17 20
17 | 14 10 17 5 15 13 4 15 6 13 27 4 | 31 30 30 29 35 36 30 32 30 27 30 28
18E | 6 7 9 7 10 14 3 10 5 11 11 3 | 36 35 37 35 28 41 34 42 32 35 36 33
19 | 7 11 13 6 8 10 3 10 6 11 24 3 | 23 25 27 27 25 30 25 31 25 26 29 24
20E | 9 11 12 6 9 20 5 11 5 7 12 3 | 41 41 46 41 47 43 43 43 44 48 47 42
21 | 12 9 16 5 12 16 4 14 5 10 15 3 | 21 23 32 19 18 27 18 30 17 22 15 18
22E | 9 9 11 6 8 19 2 11 5 8 11 3 | 22 25 27 25 23 34 21 28 22 27 25 22
23 | 13 13 14 7 12 18 6 14 7 13 17 4 | 18 26 27 21 19 26 17 28 18 20 18 18
X24 | 35 22 --- 11 --- 23 15 --- 9 --- --- 8 | 111 108 --- 110 --- 118 109 --- 111 --- --- 110
25 | 7 13 25 6 12 39 6 15 7 10 20 5 | 24 25 25 24 30 39 23 32 24 31 31 23
26 | 9 9 13 4 8 13 4 10 5 11 18 3 | 22 24 29 26 31 33 22 28 29 24 21 25
X27 | 53 9 --- --- --- --- 70 --- --- --- --- 0 | 29 46 --- --- --- --- 22 --- --- --- --- 48
28 | 8 10 17 5 10 17 4 13 6 7 10 3 | 16 19 22 18 17 31 15 25 16 21 19 17
29 | 11 14 18 6 11 16 5 15 5 13 26 4 | 24 28 28 27 29 29 26 29 27 25 23 25
30 | 9 8 16 5 15 16 4 12 8 12 23 4 | 40 44 47 44 42 42 43 47 40 44 41 41
31 | 9 13 19 5 14 15 3 15 6 11 13 4 | 20 24 29 22 23 32 19 31 20 29 22 20
32E | 15 15 18 6 10 15 5 15 8 20 10 4 | 39 42 48 43 38 49 42 50 42 51 42 42
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 11 16 6 11 17 4 13 7 13 18 |T 27 29 30 29 26 36 27 32 28 29 26 28
WRMS | 10 11 16 6 10 16 4 13 6 10 15 |NE 25 28 27 27 24 35 25 29 26 25 23 26
MEDI | 9 10 15 6 10 16 4 13 6 11 15 |MD 22 25 28 24 24 33 21 30 24 26 23 22
Table 3.1712.1 GPS week: 1712 Day: 1 MJD: 56229.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 10 13 18 9 10 12 3 12 6 8 10 3 | 27 29 33 37 29 44 34 49 34 38 36 33
2 | 10 7 20 9 16 11 4 17 5 11 23 4 | 19 24 34 26 23 28 21 31 21 23 16 20
3 | 8 9 12 3 12 12 4 9 4 14 16 3 | 20 22 27 20 22 25 19 26 19 23 18 17
4 | 10 5 14 4 11 11 4 10 4 13 30 3 | 40 41 35 33 39 34 38 35 38 33 39 33
5E | 8 7 17 5 9 13 3 16 4 10 15 3 | 33 34 42 33 30 40 33 38 33 37 32 31
6 | 8 11 12 4 12 10 3 7 5 15 11 3 | 22 24 30 22 25 27 22 29 20 27 20 19
7 | 8 14 15 8 14 14 4 15 5 12 15 4 | 22 26 29 22 23 27 24 28 21 24 25 19
8 | 12 8 14 6 8 10 4 12 5 9 13 3 | 18 21 24 14 15 16 16 22 15 16 22 12
9 | 12 13 12 6 11 13 5 9 6 8 17 3 | 18 20 28 20 18 25 18 25 18 18 23 16
10E | 17 17 22 10 13 22 5 18 5 27 19 5 | 29 30 42 31 26 36 29 39 30 40 29 27
11 | 9 9 17 6 8 14 6 13 3 9 11 3 | 24 26 36 28 23 36 25 36 25 25 27 24
12 | 16 18 22 8 10 14 4 21 6 7 16 4 | 25 30 32 24 21 31 23 30 21 28 22 21
13 | 7 10 16 7 12 19 4 15 5 11 12 3 | 24 27 31 21 21 36 22 32 21 24 25 21
14 | 12 12 17 8 12 13 4 13 5 11 15 3 | 20 26 30 19 23 26 20 28 19 23 23 19
15 | 16 13 16 5 9 21 4 15 6 9 20 4 | 20 19 25 19 16 36 18 27 18 23 19 17
16 | 8 10 14 5 11 16 4 13 4 9 17 3 | 22 23 28 21 22 31 20 25 21 23 15 18
17 | 10 10 18 5 15 8 5 15 5 10 24 4 | 25 24 30 23 24 26 25 27 24 21 24 21
18E | 15 20 13 7 12 12 3 9 5 11 12 3 | 28 32 29 23 26 31 24 29 27 26 28 25
19 | 26 29 14 5 10 11 5 14 7 16 22 4 | 34 36 28 21 18 24 20 28 18 20 19 17
20E | 6 10 14 5 8 10 4 14 5 10 16 3 | 44 45 46 43 41 47 43 47 42 40 45 40
21 | 11 10 16 7 12 14 5 13 5 13 16 3 | 16 18 30 15 14 27 16 28 15 23 15 14
22E | 7 9 13 7 12 16 2 10 5 6 10 3 | 21 21 26 23 18 27 21 31 20 24 23 19
23 | 9 10 19 5 12 16 4 17 5 8 16 3 | 24 28 29 21 18 31 22 30 22 25 21 19
X24 | 31 19 --- 15 --- 21 12 --- 9 --- --- 8 | 73 73 --- 72 --- 82 76 --- 76 --- --- 73
25 | 13 11 25 8 13 15 4 18 5 9 18 4 | 22 26 31 23 24 34 24 32 22 24 30 21
26 | 11 9 11 4 10 13 3 9 3 7 15 2 | 26 27 33 27 25 33 27 30 29 30 26 25
X27 | 63 14 --- --- --- --- 133 --- --- --- --- 0 | 29 81 --- --- --- --- 62 --- --- --- --- 80
28 | 11 9 17 6 9 15 4 13 5 8 7 3 | 18 21 28 18 17 29 17 25 18 22 19 15
29 | 14 12 19 4 14 14 4 17 5 11 23 4 | 22 29 30 21 23 25 21 28 20 24 19 18
30 | 14 10 16 4 16 15 3 14 8 10 24 4 | 63 63 66 65 67 64 62 68 63 63 63 64
31 | 12 13 21 6 15 16 5 17 6 10 15 4 | 18 21 28 16 17 27 18 29 16 24 17 14
32E | 14 16 17 7 8 15 6 15 6 18 12 4 | 33 36 45 37 30 45 36 46 36 45 39 36
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 13 17 6 12 14 4 14 5 12 17 |T 27 31 32 27 24 33 28 32 26 27 25 26
WRMS | 12 12 17 6 11 14 4 14 5 9 15 |NE 25 29 29 24 21 31 25 29 23 24 22 24
MEDI | 11 10 16 6 12 14 4 14 5 10 16 |MD 24 26 30 23 23 31 22 29 21 24 23 20
Table 3.1712.2 GPS week: 1712 Day: 2 MJD: 56230.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 12 13 16 10 10 11 5 12 8 10 11 3 | 26 27 32 33 33 46 33 45 33 38 37 33
2 | 11 12 16 6 16 13 3 14 7 12 23 4 | 16 18 30 23 23 25 21 27 21 26 14 20
3 | 10 9 9 3 12 13 4 9 5 8 20 3 | 15 14 23 18 25 26 16 21 17 23 15 17
4 | 11 11 13 5 13 11 2 12 5 10 29 4 | 24 30 22 23 27 23 24 22 22 27 28 22
5E | 8 10 14 6 12 11 4 14 7 12 16 3 | 38 38 45 43 45 42 41 42 41 40 49 41
6 | 9 8 9 3 15 10 2 8 4 11 15 3 | 19 19 24 21 30 26 18 24 21 24 18 19
7 | 12 13 14 5 14 13 4 20 5 6 14 3 | 19 17 23 15 20 25 16 23 15 22 16 14
8 | 14 10 11 5 13 12 3 13 7 7 10 3 | 14 15 20 13 18 17 16 19 16 19 20 13
9 | 12 13 11 4 14 11 3 10 4 9 15 3 | 10 15 20 15 14 21 15 22 14 24 17 14
10E | 23 29 22 11 14 21 7 17 9 31 17 6 | 28 36 33 25 22 26 19 28 22 35 21 20
11 | 10 10 18 5 7 12 3 13 7 15 10 3 | 21 24 34 24 26 36 23 32 25 25 26 24
12 | 14 11 22 6 17 19 3 24 7 12 16 4 | 22 24 27 23 29 30 23 28 21 30 20 21
13 | 7 10 16 7 13 15 3 15 5 10 14 3 | 18 19 29 20 23 36 21 28 20 24 19 20
14 | 9 10 19 5 13 13 4 13 5 9 12 3 | 12 16 24 17 19 22 17 22 14 21 15 16
15 | 19 16 13 3 11 15 4 15 5 9 17 3 | 16 17 25 19 17 30 19 25 19 26 18 18
16 | 9 12 17 6 10 15 4 15 9 10 18 4 | 14 17 24 17 17 30 17 22 17 24 12 16
17 | 15 13 18 5 17 11 5 17 6 11 23 4 | 19 28 26 20 29 26 24 26 22 31 23 23
18E | 15 21 11 7 13 16 4 11 6 10 11 4 | 33 34 29 31 30 38 31 33 27 32 30 30
19 | 31 33 12 5 11 10 4 12 5 8 22 4 | 32 33 25 20 25 24 17 24 20 22 20 19
20E | 7 10 12 5 10 18 4 17 5 9 12 3 | 35 36 40 36 37 43 37 38 38 38 41 36
21 | 14 12 14 4 13 13 3 15 6 12 19 3 | 13 13 26 19 16 27 16 27 14 26 12 17
22E | 9 8 12 5 13 18 3 11 6 8 7 3 | 15 14 19 18 16 20 16 20 16 20 16 16
23 | 11 13 18 6 13 15 4 18 6 14 17 4 | 20 21 27 18 20 28 19 26 19 22 18 17
X24 | 25 25 --- 10 --- 20 11 --- 10 --- --- 8 | 89 93 --- 88 --- 92 91 --- 91 --- --- 89
25 | 12 17 25 10 14 17 3 17 6 7 16 4 | 21 26 24 23 21 32 22 31 21 28 29 21
26 | 9 9 10 5 13 13 3 9 6 11 13 3 | 15 16 21 19 16 25 18 20 18 21 19 17
X27 | 36 12 --- --- --- --- 42 --- --- --- --- 0 | 20 36 --- --- --- --- 38 --- --- --- --- 35
28 | 12 10 15 3 14 17 6 11 8 9 9 3 | 15 15 23 17 17 30 16 20 18 21 16 15
29 | 14 14 15 5 13 14 4 17 8 9 25 4 | 22 23 27 24 28 26 26 26 28 31 21 24
30E | 32 16 19 8 16 22 5 15 10 11 26 5 | 55 68 73 64 64 68 64 73 61 65 67 65
31 | 12 16 17 10 14 17 4 17 8 9 14 4 | 17 21 25 18 17 27 17 25 13 23 13 15
32E | 15 15 19 7 11 16 4 16 8 19 10 4 | 31 31 43 35 29 41 33 43 33 42 34 35
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 14 14 16 6 13 15 4 15 7 12 17 |T 23 26 28 25 25 32 25 28 25 28 23 25
WRMS | 13 14 16 6 12 14 4 14 6 9 16 |NE 21 23 25 22 22 30 23 25 22 25 19 22
MEDI | 12 12 15 5 13 14 4 14 6 10 15 |MD 19 21 25 20 23 27 19 26 21 25 19 20
Table 3.1712.3 GPS week: 1712 Day: 3 MJD: 56231.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 9 13 18 7 14 12 4 10 4 7 11 4 | 27 26 30 32 34 45 31 45 32 39 36 34
2 | 7 9 17 11 17 14 6 14 6 11 20 4 | 17 19 29 21 22 25 17 28 19 25 16 19
3 | 6 11 9 10 13 12 4 8 5 9 18 3 | 14 15 21 18 24 22 18 22 16 24 17 18
4 | 8 7 10 7 12 11 5 12 3 9 25 4 | 27 29 24 25 34 27 27 24 29 30 29 26
5E | 8 12 13 8 13 17 3 14 6 10 10 4 | 45 50 49 50 50 45 47 46 46 51 46 46
6 | 8 10 10 8 14 11 3 8 5 11 16 3 | 19 20 24 22 29 26 22 25 21 23 24 22
7 | 11 14 15 9 12 16 5 14 5 10 14 4 | 19 23 24 16 22 26 15 23 17 23 16 16
8 | 8 11 10 7 15 17 4 11 5 9 12 3 | 12 16 17 12 18 16 10 18 13 16 16 11
9 | 11 15 11 7 16 10 4 12 5 8 16 4 | 15 16 21 17 18 20 16 23 16 21 18 15
10E | 19 18 20 14 14 27 6 17 7 22 16 6 | 26 32 35 29 30 33 26 34 28 38 27 28
11 | 7 9 14 7 12 14 5 12 5 10 10 3 | 25 22 34 25 27 38 24 33 24 28 25 26
12 | 13 15 20 11 15 17 5 22 7 13 14 5 | 16 20 27 21 22 29 18 26 20 28 16 17
13 | 7 12 14 8 17 20 4 11 6 9 11 4 | 17 23 28 22 28 36 21 28 21 20 20 21
14 | 8 12 15 8 15 11 3 13 5 9 12 4 | 17 20 25 23 20 24 19 25 17 20 17 17
15 | 9 11 14 9 12 16 4 14 4 14 16 4 | 19 18 23 19 22 30 14 25 16 21 17 15
16 | 6 14 15 9 13 18 7 13 6 8 15 4 | 14 20 23 22 19 27 17 22 14 23 15 14
17 | 11 10 15 10 21 11 5 16 6 10 22 5 | 23 21 26 26 34 27 23 26 24 23 23 22
18E | 8 9 10 9 12 18 4 11 3 10 7 3 | 31 29 35 35 29 37 32 37 30 34 33 31
19 | 26 28 12 10 13 11 5 11 5 10 22 5 | 27 28 25 25 29 27 24 26 22 27 23 23
20E | 6 10 10 9 13 22 3 14 3 12 12 4 | 35 38 36 38 40 47 35 39 36 32 35 36
21 | 9 11 15 6 13 16 4 13 5 8 19 4 | 15 17 29 17 17 25 15 26 14 19 13 15
22E | 6 10 11 9 14 18 4 10 5 9 8 3 | 21 23 24 23 21 18 21 25 18 22 18 18
23 | 11 15 16 7 18 15 4 14 5 12 15 4 | 14 22 26 19 25 27 17 24 18 21 17 17
X24 | 26 20 --- 15 --- 18 9 --- 7 --- --- 9 | 97 102 --- 96 --- 107 98 --- 99 --- --- 100
25 | 10 17 24 8 13 15 3 18 5 14 11 5 | 18 21 23 25 30 32 22 29 22 27 25 20
26 | 9 14 13 10 13 13 5 8 8 10 9 4 | 19 19 25 20 23 27 19 26 24 21 20 21
X27 | 64 9 --- --- --- --- 56 --- --- --- --- 0 | 32 54 --- --- --- --- 44 --- --- --- --- 56
28 | 9 11 14 10 17 18 5 12 5 9 9 4 | 13 16 21 16 23 28 12 21 14 19 16 13
29 | 11 12 15 10 11 13 7 15 6 14 24 5 | 16 22 26 23 30 23 25 26 26 28 21 23
30E | 16 19 16 8 20 22 8 17 9 12 19 5 | 132 135 130 130 121 127 129 133 126 133 125 128
31 | 9 14 18 10 18 15 4 14 6 14 13 5 | 15 18 26 20 21 26 17 26 14 27 13 16
32E | 14 16 18 8 13 18 5 15 6 18 13 5 | 31 32 44 37 31 39 34 44 33 41 37 35
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 11 14 15 9 15 16 5 13 5 11 15 |T 27 30 31 29 29 35 28 31 28 30 25 28
WRMS | 10 13 15 9 15 15 5 13 5 10 15 |NE 21 25 25 24 24 30 23 25 23 24 19 23
MEDI | 9 12 14 9 13 16 4 13 5 10 14 |MD 19 22 26 23 25 27 21 26 21 24 20 21
Table 3.1712.4 GPS week: 1712 Day: 4 MJD: 56232.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 14 13 16 9 10 13 4 12 6 9 11 4 | 28 30 36 37 32 44 35 49 37 38 37 37
2 | 10 8 17 9 15 13 6 14 8 8 24 4 | 18 23 33 22 23 26 20 30 24 28 17 23
3 | 11 10 9 6 16 11 3 8 6 9 19 4 | 16 17 23 18 25 22 17 22 19 24 15 19
4 | 7 5 12 7 14 12 4 10 7 12 25 4 | 28 28 24 25 30 28 26 25 30 25 25 25
5E | 9 8 13 7 10 13 4 14 6 8 13 4 | 54 51 55 50 51 59 50 52 57 53 48 54
6 | 13 20 10 7 13 13 2 8 7 9 17 4 | 20 24 25 20 28 24 20 25 22 25 20 21
7 | 12 14 16 8 12 19 4 14 6 13 15 5 | 17 20 24 16 17 25 14 22 17 24 10 15
8 | 13 10 12 8 11 10 6 11 5 11 10 4 | 11 16 18 14 16 13 13 17 16 17 16 12
9 | 10 7 10 10 12 15 4 11 5 13 19 4 | 12 15 23 18 16 23 15 23 15 28 15 16
10E | 16 14 24 11 12 16 6 19 9 19 27 6 | 23 25 35 24 25 30 20 28 21 39 33 23
11 | 9 11 17 9 9 15 4 11 5 15 13 4 | 22 25 38 29 28 36 24 35 28 33 25 29
12 | 12 11 23 9 11 14 6 23 7 13 17 6 | 15 18 28 22 21 28 19 27 20 32 14 19
13 | 9 13 15 9 15 19 4 13 7 13 13 5 | 16 20 27 16 20 32 16 26 20 19 16 18
14 | 7 11 17 8 12 13 5 12 8 11 15 4 | 15 18 27 17 20 25 16 23 18 20 16 17
15 | 9 10 16 10 10 15 5 15 6 9 19 4 | 19 22 26 24 23 31 20 27 20 22 22 21
16 | 8 10 16 8 12 15 4 11 7 10 18 4 | 14 12 25 15 22 24 14 22 15 20 11 15
17 | 11 10 15 8 15 11 5 15 7 12 25 4 | 22 25 27 26 31 26 24 26 26 27 26 23
18E | 10 8 11 9 10 13 5 11 5 8 23 3 | 38 37 37 39 36 42 35 40 36 38 37 37
19 | 20 19 11 5 13 9 6 11 7 11 23 4 | 27 28 26 25 27 23 23 27 25 27 20 23
20E | 7 11 11 7 13 17 5 12 6 11 26 4 | 35 38 39 36 36 45 34 35 37 35 38 36
21 | 11 7 15 8 11 13 6 12 8 11 23 4 | 17 14 30 16 17 28 15 27 21 23 17 19
22E | 8 8 15 12 12 18 5 10 6 11 10 4 | 29 27 33 26 30 27 25 30 30 23 27 27
23 | 12 17 15 9 16 18 4 15 8 12 19 5 | 16 20 27 16 20 26 15 26 19 20 14 17
X24 | 26 15 --- 18 --- 28 20 --- 11 --- --- 12 | 88 87 --- 93 --- 99 88 --- 91 --- --- 90
25 | 11 10 26 10 10 14 7 16 8 6 10 5 | 20 23 27 25 23 33 22 30 21 31 22 22
26 | 9 10 10 8 10 12 5 9 5 8 6 3 | 14 16 26 18 20 22 17 26 16 22 19 17
X27 | 55 8 --- --- --- --- 115 --- --- --- --- 0 | 34 59 --- --- --- --- 70 --- --- --- --- 58
28 | 12 8 12 6 13 16 5 12 6 8 8 4 | 12 12 20 17 15 29 12 20 16 21 14 14
29 | 9 10 17 8 13 12 7 14 8 13 26 5 | 18 19 27 23 22 22 22 24 24 27 19 20
30E | 19 17 19 11 17 15 7 17 11 12 21 6 | 94 97 106 100 109 104 100 105 96 96 104 99
31 | 10 12 15 9 15 16 4 13 8 9 16 5 | 15 17 26 19 22 30 17 25 18 25 16 18
32E | 16 16 17 9 16 15 5 16 8 16 10 6 | 28 30 43 34 32 38 31 43 31 38 31 33
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 12 16 9 13 14 5 13 7 11 18 |T 26 28 32 28 27 34 27 31 28 30 24 28
WRMS | 11 12 16 8 13 14 5 13 7 10 17 |NE 21 24 26 23 22 29 23 26 24 25 18 24
MEDI | 11 10 15 9 12 14 5 12 7 11 17 |MD 19 23 27 23 23 28 20 26 21 25 19 21
Table 3.1712.5 GPS week: 1712 Day: 5 MJD: 56233.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 11 16 12 4 16 14 4 12 6 12 13 4 | 30 28 36 35 31 45 34 49 35 41 37 35
2 | 7 7 18 9 20 13 5 17 7 11 24 4 | 20 21 32 21 26 26 19 31 23 25 18 22
3 | 9 12 11 4 15 13 2 10 4 7 20 3 | 18 20 20 20 17 22 16 22 17 22 16 17
4 | 4 6 10 4 12 13 4 9 5 8 27 3 | 22 22 19 17 22 22 19 19 21 19 21 17
5E | 8 7 13 6 13 11 4 16 7 11 22 3 | 36 38 40 38 39 40 37 40 37 42 42 38
6 | 12 11 11 6 17 11 3 8 3 11 15 3 | 20 24 22 24 21 22 21 24 20 27 21 20
7 | 8 13 17 8 15 23 4 13 7 12 19 4 | 19 21 26 18 21 30 16 23 20 22 16 16
8 | 10 10 11 6 14 15 5 10 6 9 12 3 | 15 17 19 11 18 20 11 21 16 15 19 11
9 | 10 11 12 9 11 12 6 11 6 10 16 3 | 17 16 20 14 12 20 12 24 14 22 14 13
10E | 13 12 24 7 15 13 5 21 8 19 22 5 | 31 33 43 31 33 31 30 40 33 40 41 31
11 | 7 8 16 4 13 15 4 11 5 10 15 3 | 22 21 36 23 23 34 22 35 24 31 24 24
12 | 10 10 21 9 15 17 6 24 6 12 15 5 | 20 18 25 18 21 28 13 26 16 25 13 15
13 | 8 11 15 6 15 23 4 13 8 7 15 4 | 19 23 30 23 24 36 20 29 23 22 18 21
14 | 9 9 15 11 12 16 2 12 9 12 13 4 | 15 16 22 22 17 24 14 23 14 22 14 16
15 | 13 9 15 5 11 17 5 16 7 9 18 4 | 16 18 23 17 16 30 14 25 15 22 16 15
16 | 7 13 19 6 11 16 5 14 8 10 18 4 | 14 18 25 17 15 26 15 24 15 20 13 14
17 | 8 9 15 7 15 12 3 16 7 9 27 4 | 21 16 23 17 24 21 15 24 18 21 16 15
18E | 11 15 13 6 13 15 3 11 6 10 7 4 | 24 27 31 31 29 31 28 31 26 31 28 27
19 | 21 25 13 7 13 12 5 12 5 12 23 4 | 21 22 24 23 20 23 18 26 19 23 16 18
20E | 6 9 11 5 11 12 5 12 4 11 12 3 | 23 23 28 22 18 28 21 26 24 26 24 21
21 | 10 10 15 6 13 16 3 13 5 11 25 4 | 13 16 29 17 17 27 15 26 16 20 17 17
22E | 7 8 20 7 14 14 2 12 5 11 9 4 | 26 25 37 28 30 32 25 28 25 25 24 25
23 | 10 13 17 8 16 21 5 16 7 11 17 4 | 18 23 26 20 21 29 18 27 20 20 16 18
X24 | 31 28 --- 13 --- 22 11 --- 10 --- --- 9 | 73 73 --- 74 --- 81 69 --- 71 --- --- 72
25 | 10 15 22 7 13 17 6 16 6 9 8 4 | 18 20 19 16 21 28 16 25 16 22 17 15
26 | 9 9 11 4 12 11 5 8 5 8 9 3 | 22 23 29 22 25 26 21 27 26 28 25 23
X27 | 46 13 --- --- --- --- 103 --- --- --- --- 0 | 32 43 --- --- --- --- 55 --- --- --- --- 42
28 | 7 8 14 5 15 17 5 12 6 7 14 3 | 15 16 20 14 17 26 11 23 17 18 19 12
29 | 7 14 15 9 12 14 4 15 9 14 25 4 | 20 23 24 23 24 21 18 26 23 25 18 19
30E | 16 19 17 9 14 18 6 15 11 12 23 5 | 95 96 103 97 104 103 97 100 98 96 93 98
31 | 10 12 16 9 16 21 4 12 9 11 14 4 | 17 19 24 20 15 27 15 26 14 23 16 16
32E | 14 19 19 7 16 16 4 17 8 13 11 5 | 32 35 42 34 30 37 33 45 32 40 33 34
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 12 16 7 14 16 4 14 7 11 18 |T 25 26 29 26 25 32 24 30 25 27 23 24
WRMS | 10 12 16 7 14 15 4 13 6 10 18 |NE 21 23 24 21 20 28 20 26 21 23 18 20
MEDI | 10 11 15 7 14 15 4 12 6 11 15 |MD 20 22 25 22 21 28 18 26 20 23 18 18
Table 3.1712.6 GPS week: 1712 Day: 6 MJD: 56234.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 11 10 16 8 9 16 5 13 4 10 13 4 | 34 36 41 40 37 53 40 56 41 46 46 42
2 | 11 7 17 10 18 12 5 17 6 11 26 5 | 22 24 33 23 26 26 22 35 24 29 24 25
3 | 9 10 11 7 12 19 3 6 7 9 22 4 | 19 17 26 20 20 28 15 23 17 22 18 18
4 | 7 5 10 7 10 12 4 9 4 13 25 3 | 32 32 30 30 32 32 30 29 31 26 28 29
5E | 10 7 15 8 11 11 5 18 7 12 13 4 | 45 45 51 49 44 51 45 50 47 54 44 47
6 | 8 9 8 8 12 16 3 8 5 10 16 3 | 24 21 30 26 31 33 23 28 24 23 27 24
7 | 9 9 16 8 11 21 4 15 5 11 18 4 | 21 22 27 16 20 28 16 26 16 21 18 18
8 | 11 9 9 8 10 13 5 11 4 11 11 3 | 13 15 16 13 16 15 11 17 13 18 15 12
9 | 8 8 12 10 10 16 4 10 4 12 19 4 | 13 14 21 15 12 22 12 21 14 23 16 14
10E | 12 10 19 12 12 12 5 17 6 14 31 5 | 24 26 40 29 26 35 28 37 30 38 32 29
11 | 7 8 15 8 11 18 4 11 4 9 17 4 | 27 28 38 28 27 44 28 38 29 28 31 29
12 | 16 11 21 15 10 13 7 20 7 14 18 5 | 22 23 31 19 18 30 15 30 18 25 14 20
13 | 9 9 15 10 11 21 4 13 6 13 18 4 | 24 25 34 24 27 41 22 33 22 21 26 24
14 | 7 10 16 10 11 18 3 13 7 12 16 5 | 18 19 23 21 22 27 16 24 17 22 18 17
15 | 10 9 13 8 8 20 4 16 4 9 19 4 | 20 21 27 22 20 36 19 29 19 24 25 21
16 | 7 11 12 10 12 15 4 12 5 11 20 4 | 16 17 24 17 13 25 14 25 16 25 13 17
17 | 9 12 16 9 12 12 5 16 6 9 28 4 | 32 32 32 29 32 32 28 28 28 26 29 27
18E | 10 9 12 9 10 15 3 10 4 10 16 3 | 34 36 36 36 32 40 33 40 34 37 34 35
19 | 19 21 12 8 11 13 5 10 5 14 26 5 | 29 29 29 27 29 29 24 28 26 24 25 25
20E | 9 12 10 9 9 14 4 10 5 11 12 4 | 26 30 36 29 28 33 27 34 28 29 32 29
21 | 8 7 14 7 10 13 5 14 5 9 28 4 | 19 19 32 18 12 28 15 31 16 24 20 19
22E | 9 8 13 7 11 16 3 9 5 11 12 4 | 36 37 35 32 32 34 32 36 34 33 34 34
23 | 12 13 15 13 12 18 5 15 5 13 20 5 | 22 26 32 24 22 31 20 33 20 22 23 21
X24 | 21 16 --- 10 --- 46 10 --- 9 --- --- 14 | 109 112 --- 105 --- 116 106 --- 107 --- --- 108
25 | 9 10 23 9 8 12 4 17 6 13 11 5 | 25 24 24 23 23 33 20 33 21 28 22 22
26 | 5 7 10 6 10 14 4 8 6 10 11 3 | 20 19 20 18 18 25 17 20 19 19 18 18
X27 | 49 8 --- --- --- --- 49 --- --- --- --- 0 | 19 52 --- --- --- --- 25 --- --- --- --- 51
28 | 8 6 10 7 9 13 4 11 5 9 10 3 | 17 17 21 14 19 27 14 20 17 21 18 17
29 | 9 13 15 15 8 15 7 13 6 12 24 4 | 24 30 29 30 30 29 26 27 28 25 23 26
30E | 16 18 19 11 13 16 5 16 9 12 35 5 | 109 110 111 106 106 110 105 112 102 110 115 107
31 | 12 16 16 7 12 22 4 13 7 12 24 5 | 19 20 26 17 18 29 14 25 14 23 21 15
32E | 18 18 20 12 10 18 5 17 8 14 13 5 | 35 37 50 37 32 47 35 48 34 41 35 38
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 11 11 15 9 11 16 4 13 6 11 20 |T 29 31 33 30 27 37 28 33 29 30 28 30
WRMS | 10 11 15 9 10 15 4 13 6 10 19 |NE 25 27 28 25 22 34 23 28 24 24 22 26
MEDI | 9 9 15 9 11 15 4 13 5 11 18 |MD 24 25 30 24 26 32 22 29 24 25 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 4.1712 GPS week: 1712 MJD: 56228.0-56234.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 |U 4 4 12 |U 7 9 23 |U 7 8 16 |
cof | cof 3031 |U 4 4 12 |U 7 9 23 |U 7 7 16 |
emr | emr 2870 | 8 7 18 |U 9 8 26 | 10 11 21 |
esa | esa 2976 | 5 4 14 |U 7 10 24 | 8 9 18 |
gfz | gfz 2868 |U 6 5 13 |U 7 8 23 |U 9 11 20 |
grg | grg 2933 |U 9 9 22 |U 8 11 30 | 10 11 23 |
igr | igr 2966 | 6 5 14 | 6 9 23 | 9 9 18 |
igs | igs 2968 | 6 5 15 | 7 9 24 | 8 8 17 |
jpl | jpl 2868 | 7 7 18 |U 7 10 26 | 10 11 24 |
mit | mit 2976 | 7 5 15 |U 8 9 27 |U 9 9 20 |
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 5.1712.0 GPS week: 1712 Day: 0 MJD: 56228.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3038 | 4 4 9 | 7 8 26 | 5 4 11 |
cof | cof 3038 | 4 4 9 | 7 9 27 | 5 4 11 |
emr | emr 2872 | 8 8 12 | 9 7 30 | 7 7 16 |
esa | esa 2976 | 6 6 12 | 7 7 27 | 6 6 14 |
gfz | gfz 2873 | 7 7 10 | 7 7 25 | 6 6 15 |
grg | grg 2880 | 7 9 16 | 8 9 33 | 8 8 21 |
igr | igr 2976 | 7 6 12 | 7 7 26 | 6 6 14 |
igs | igs 2974 | 6 6 11 | 7 7 27 | 7 6 13 |
jpl | jpl 2869 | 12 8 15 | 7 7 29 | 10 9 38 |
mit | mit 2976 | 7 6 12 | 8 7 27 | 8 9 20 |
Table 5.1712.1 GPS week: 1712 Day: 1 MJD: 56229.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 3 3 12 | ---- ---- ---- | 6 7 13 |
cof | cof 3030 | 3 3 11 | ---- ---- ---- | 5 6 12 |
emr | emr 2872 | 7 5 18 | ---- ---- ---- | 8 8 21 |
esa | esa 2976 | 4 3 15 | ---- ---- ---- | 6 7 14 |
gfz | gfz 2870 | 6 3 13 | ---- ---- ---- | 7 7 15 |
grg | grg 2975 | 7 8 20 | ---- ---- ---- | 9 11 21 |
igr | igr 2948 | 5 3 12 | ---- ---- ---- | 8 8 16 |
igs | igs 2965 | 5 3 15 | ---- ---- ---- | 6 7 14 |
jpl | jpl 2871 | 7 6 18 | ---- ---- ---- | 7 9 17 |
mit | mit 2976 | 5 3 13 | ---- ---- ---- | 8 9 16 |
Table 5.1712.2 GPS week: 1712 Day: 2 MJD: 56230.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 5 4 11 | 6 11 21 | 7 6 16 |
cof | cof 3037 | 4 4 11 | 6 11 20 | 6 6 16 |
emr | emr 2871 | 8 8 18 | 9 12 29 | 10 10 22 |
esa | esa 2976 | 6 5 14 | 7 12 25 | 7 7 18 |
gfz | gfz 2870 | 5 6 13 | 7 10 25 | 8 8 19 |
grg | grg 2975 | 7 9 23 | 8 12 25 | 10 9 26 |
igr | igr 2967 | 6 6 14 | 7 11 25 | 7 7 17 |
igs | igs 2973 | 6 5 16 | 7 12 24 | 7 6 17 |
jpl | jpl 2870 | 6 7 19 | 7 13 28 | 11 11 22 |
mit | mit 2976 | 5 6 14 | 8 12 25 | 9 7 18 |
Table 5.1712.3 GPS week: 1712 Day: 3 MJD: 56231.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 4 5 12 | 6 9 24 | 8 8 16 |
cof | cof 3039 | 4 5 12 | 6 9 23 | 8 8 17 |
emr | emr 2872 | 7 6 14 | 8 7 27 | 11 10 17 |
esa | esa 2976 | 4 4 12 | 6 10 24 | 10 9 20 |
gfz | gfz 2868 | 5 5 11 | 6 7 26 | 10 25 29 |
grg | grg 2970 | 6 6 16 | 7 9 25 | 11 9 20 |
igr | igr 2953 | 5 4 13 | 6 10 24 | 9 8 19 |
igs | igs 2974 | 4 4 12 | 6 8 24 | 8 8 16 |
jpl | jpl 2868 | 6 6 16 | 7 9 28 | 11 11 21 |
mit | mit 2976 | 5 5 12 | 7 8 24 | 10 9 21 |
Table 5.1712.4 GPS week: 1712 Day: 4 MJD: 56232.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 | 4 5 14 | 5 8 19 | 8 9 19 |
cof | cof 3035 | 4 5 14 | 5 8 18 | 8 9 20 |
emr | emr 2867 | 8 7 21 | 7 8 19 | 10 11 20 |
esa | esa 2976 | 5 5 19 | 5 11 19 | 9 10 19 |
gfz | gfz 2867 | 5 7 19 | 5 9 21 | 9 9 19 |
grg | grg 2879 | 7 9 21 | 6 12 27 | 10 8 21 |
igr | igr 2966 | 6 6 19 | 5 11 18 | 10 10 22 |
igs | igs 2952 | 5 6 19 | 5 9 20 | 10 10 21 |
jpl | jpl 2865 | 6 7 20 | 6 11 19 | 9 11 20 |
mit | mit 2976 | 6 6 19 | 7 11 22 | 10 9 21 |
Table 5.1712.5 GPS week: 1712 Day: 5 MJD: 56233.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3019 | 5 5 14 | 10 9 28 | 10 12 21 |
cof | cof 3019 | 5 5 13 | 9 9 28 | 9 12 21 |
emr | emr 2868 | 8 7 20 | 12 8 28 | 14 19 28 |
esa | esa 2976 | 6 5 13 | 8 9 24 | 10 13 24 |
gfz | gfz 2866 | 6 6 13 | 9 7 21 | 12 16 25 |
grg | grg 2976 | 13 10 39 | 10 14 40 | 10 20 32 |
igr | igr 2976 | 6 5 14 | 8 8 23 | 10 14 23 |
igs | igs 2971 | 6 5 14 | 9 8 23 | 9 13 21 |
jpl | jpl 2867 | 7 9 18 | 10 10 28 | 12 17 27 |
mit | mit 2976 | 11 8 18 | 9 8 35 | 10 13 25 |
Table 5.1712.6 GPS week: 1712 Day: 6 MJD: 56234.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 7 4 16 | 6 9 20 | 9 8 18 |
cof | cof 3022 | 7 4 16 | 6 9 20 | 9 8 17 |
emr | emr 2868 | 9 6 22 | 8 9 23 | 11 12 25 |
esa | esa 2976 | 7 4 15 | 7 10 25 | 10 9 18 |
gfz | gfz 2866 | 7 5 15 | 6 8 22 | 8 8 19 |
grg | grg 2880 | 15 10 20 | 7 10 31 | 10 11 22 |
igr | igr 2976 | 7 4 15 | 6 9 24 | 10 9 18 |
igs | igs 2972 | 8 5 18 | 6 10 25 | 8 8 18 |
jpl | jpl 2867 | 8 7 21 | 7 10 27 | 11 11 23 |
mit | mit 2976 | 10 6 15 | 7 11 27 | 9 8 17 |
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 6.1712 GPS week: 1712 MJD: 56228.500-56234.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 2 -31 3 109 -2 | 0 13
| 23 24 125 134 6 | 3
cof uuuuu | -24 -43 1 9 -5 | -3 14
| 17 13 63 76 4 | 2
emr uuuuu | 27 -20 84 146 7 | 15 21
| 31 18 86 129 11 | 3
esa uuuuu | -43 -29 -22 -147 -4 | -1 13
| 35 37 80 68 4 | 2
gfz uuuuu | 66 35 -10 -78 -5 | 8 14
| 26 11 39 32 4 | 2
grg uuuux | -8 -28 24 -61 -19 | -2 36
| 33 20 68 37 37 | 10
igr xxxxx | -50 33 -17 -5 -2 | 1 12
| 20 16 44 91 4 | 2
irf xxxxx | 8 2 15 -6 -1 | -2 8
| 17 8 13 23 3 | 1
jpl uuuuu | 11 -44 -13 148 -1 | 38 41
| 23 31 48 59 5 | 2
mit uuuuu | 24 5 -6 40 2 | -6 13
| 12 17 54 49 7 | 2
ngs uuuxu | -33 102 -26 72 2 | 5 10
| 42 51 99 269 4 | 2
sio xuuuu | 188 -64 -27 -55 17 | 16 23
| 100 41 63 94 3 | 4
Table 7.1712.0 GPS week: 1712 Day: 0 MJD: 56228.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 33 -9 215 -80 -3 | 3 19
cof uuuuu | -2 -66 30 26 -5 | 0 19
emr uuuuu | 65 -56 188 263 -3 | 15 24
esa uuuuu | -100 28 58 -165 -7 | 2 19
gfz uuuuu | 89 31 -77 -41 -4 | 10 19
grg uuuux | 50 -39 130 -52 22 | -19 55
igr xxxxx | -59 45 -1 -137 1 | 2 16
irf xxxxx | 34 -8 -3 31 1 | 0 13
jpl uuuuu | 12 -68 -91 158 -4 | 40 43
mit uuuuu | 33 0 -66 79 6 | -4 17
ngs uuuxu | -5 150 -81 -311 -3 | 7 16
sio xuuuu | 127 -83 33 -83 18 | 13 22
Table 7.1712.1 GPS week: 1712 Day: 1 MJD: 56229.500
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 -40 11 263 3 | 0 16
cof uuuuu | -20 -52 70 64 -5 | -4 16
emr uuuuu | 60 -1 14 294 -5 | 12 21
esa uuuuu | -17 -45 67 -160 1 | -2 16
gfz uuuuu | 72 30 -13 -86 -5 | 7 16
grg uuuux | -3 5 34 -50 6 | -14 53
igr xxxxx | -30 19 32 -55 -3 | -1 14
irf xxxxx | 14 17 24 1 2 | -4 8
jpl uuuuu | -1 -47 -6 162 2 | 37 40
mit uuuuu | 29 36 -53 26 4 | -7 14
ngs uuuxu | -118 73 -89 -19 -3 | 3 9
sio xuuuu | 50 -34 8 56 20 | 11 18
Table 7.1712.2 GPS week: 1712 Day: 2 MJD: 56230.500
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 | 17 -42 -216 153 -9 | 2 16
cof uuuuu | -17 -34 -39 88 -9 | -2 13
emr uuuuu | 50 -21 84 264 2 | 14 22
esa uuuuu | -55 -22 9 -170 -10 | 1 14
gfz uuuuu | 98 51 9 -94 2 | 9 16
grg uuuux | 2 -25 -6 -19 16 | -4 42
igr xxxxx | -28 53 -34 -19 0 | 1 13
irf xxxxx | 17 6 32 10 -1 | -3 8
jpl uuuuu | 16 -30 2 248 -10 | 40 42
mit uuuuu | 20 1 56 49 6 | -8 14
ngs uuuxu | -22 111 -83 -138 1 | 3 10
sio xuuuu | 160 -42 -146 -90 20 | 15 22
Table 7.1712.3 GPS week: 1712 Day: 3 MJD: 56231.500
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 13 -7 32 -11 | 2 16
cof uuuuu | -46 -29 -60 -90 -12 | -2 14
emr uuuuu | -2 -21 25 107 -3 | 15 22
esa xxxxx | 5 -9 -49 -262 -2 | 0 15
gfz uuuuu | 60 23 -4 -115 -7 | 10 15
grg uuuux | 6 -28 62 -115 -8 | 8 23
igr xxxxx | -71 41 -50 -77 -9 | 2 12
irf xxxxx | -3 1 15 -35 0 | -3 9
jpl uuuuu | -26 5 1 151 -2 | 39 42
mit uuuuu | 1 -8 36 52 7 | -8 14
ngs uuuxu | 15 68 -79 -46 3 | 4 9
sio xuuuu | 135 -20 -27 -179 16 | 16 23
Table 7.1712.4 GPS week: 1712 Day: 4 MJD: 56232.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -23 -52 18 189 -1 | -4 9
cof uuuuu | -36 -35 -87 -6 3 | -6 12
emr uuuuu | -3 -19 175 84 20 | 11 17
esa xxxxx | -22 -94 -11 -139 -1 | -3 11
gfz uuuuu | 66 38 -7 -104 -8 | 6 10
grg uuuux | -46 -61 58 -91 -47 | 7 23
igr xxxxx | -75 38 -37 77 4 | -1 10
irf xxxxx | -19 -4 22 -29 -7 | -4 9
jpl uuuuu | 2 -18 52 132 -1 | 36 37
mit uuuuu | 21 15 -45 -7 -13 | -5 11
ngs uuuxu | -31 42 -34 298 5 | 3 8
sio xxxxx | 246 -37 -37 -20 18 | 16 22
Table 7.1712.5 GPS week: 1712 Day: 5 MJD: 56233.500
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 | 25 -39 20 -27 1 | -2 9
cof uuuuu | -9 -38 21 -94 -4 | -4 11
emr uuuuu | 19 -23 138 -41 22 | 17 21
esa uuuuu | -61 -30 -162 -74 -2 | 0 9
gfz uuuuu | 62 24 -30 -28 -8 | 8 11
grg uuuux | -21 -24 -45 -83 -73 | 5 24
igr xxxxx | -56 6 -72 78 -3 | 3 9
irf xxxxx | 15 3 13 -7 3 | -2 6
jpl uuuuu | 40 -73 -64 138 6 | 39 39
mit uuuuu | 36 -14 59 113 7 | -4 10
ngs uuuxu | -23 188 188 305 0 | 6 9
sio xxxxx | 245 -109 35 -137 16 | 21 26
Table 7.1712.6 GPS week: 1712 Day: 6 MJD: 56234.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -21 -51 -19 235 5 | -2 9
cof uuuuu | -40 -48 72 75 -4 | -5 12
emr uuuuu | -1 -2 -34 47 14 | 20 24
esa xxxxx | -48 -31 -67 -58 -10 | -1 9
gfz uuuuu | 18 50 52 -76 -6 | 6 9
grg uuuux | -46 -23 -65 -18 -50 | -1 33
igr xxxxx | -33 26 46 99 -2 | 2 9
irf xxxxx | 0 0 1 -13 -2 | -1 6
jpl uuuuu | 35 -74 12 47 5 | 39 39
mit uuuuu | 28 3 -31 -30 -2 | -2 8
ngs uuuxu | -46 83 -3 412 8 | 6 9
sio xxxxx | 352 -125 -57 70 11 | 23 28
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