[IGSREPORT-21826] Wk 1738 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri May 17 11:16:12 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1738 (Apr 28, 2013 - May 04, 2013)
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 at each SP3 epoch. 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 with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations 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 over each daily arc. 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 10 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:
igs1738[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1738[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1738[0-6].cls IGS GPS clock combination summary report.
igs17387.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17387.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the 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 week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
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 | EMR | 30 32 HERS MCM4 ALBH HERS MCM4
0 | ESA | 30 DARW UNSA
0 | GFZ | 30 32 RAMO
0 | GRG | DARW KIT3 NTUS RAMO REUN
0 | JPL | 30 32
0 | MIT | 30 30 32 MDVJ
1 | COD | FLRS
1 | EMR | 30 MCM4 MCM4
1 | ESA | UNSA
1 | GFZ | 30 ASPA IRKJ LHAZ
1 | GRG | FAA1 FAA1 KOUR
1 | JPL | 30 32
1 | MIT | 31 32 30 31 32 IRKJ PTBB IRKJ PTBB
2 | COD | 3 BRFT HERT FLRS
2 | EMR | 3 MCM4 MCM4 THTI WUHN
2 | ESA | UNSA VILL
2 | GRG | 3 LHAZ NOVM PIMO POLV THTI
2 | JPL | 8
2 | MIT | 30 31 32 30 31 32 MDVJ
3 | COD | 30 30
3 | EMR | 30 32 MCM4 MATE MCM4 WHIT WUHN
3 | ESA | MATE TIXI TRO1 UNSA
3 | GFZ | 30 32 IRKJ MATE UNSA
3 | GRG | NICO CEDU MAC1 NICO NTUS
3 | MIT | 30 2 30 32 CAS1 DAV1 IRKJ NTUS CAS1 DAV1 IRKJ MDVJ
4 | COD | FLRS JOZ2
4 | ESA | 30 UNSA
4 | GFZ | GRAS
4 | GRG | USNO HERT MAC1 USNO
4 | JPL | 9 10
4 | MIT | 30 32 30 32 MAC1 CRO1 MAC1 MDVJ
5 | COD | 30 NICO
5 | ESA | ALIC UNSA VILL
5 | GFZ | BOGT LHAZ
5 | GRG | 32 32 BOGT DUBO NICO NTUS SPT0 BOGT DUBO NKLG NTUS
5 | GRG | SPT0
5 | MIT | 30 32 30 32 IRKJ MDVJ NICO MDVJ
6 | COD | 30 JOZ2
6 | EMR | 32 THTI TLSE
6 | ESA | MAL2 UNSA
6 | GFZ | 32 IRKJ POTS TLSE
6 | GRG | FAA1 FAA1 FAIR KIT3
6 | JPL | 32
6 | MIT | 20 23 30 20 23 32 REYK MDVJ REYK
5. 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 AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
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 G27 | | | | | | 4 | |
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 RX, RY and RZ 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 | -.7 1.7 -.8 -36 -11 -17 .20
EMR | 0 | .9 -9.1 22.6 7 -4 11 .13
ESA | 0 | 1.4 .8 28.4 13 -43 -6 .05
GFZ | 0 | -.6 .7 -.4 -17 -57 -1 .08
GRG | 0 | 2.6 .7 29.5 2 -22 -21 .42
JPL | 0 | 5.3 -.6 19.6 -28 21 -2 .21
MIT | 0 | -3.9 -7.7 27.9 0 5 -32 .30
NGS | 0 | -2.8 -1.3 24.1 -157 -11 -22 .96
SIO | 0 | -1.2 -1.5 43.0 -48 129 138 .32
COD | 1 | -.4 .3 -.6 -58 -13 -10 .09
EMR | 1 | 6.1 -7.5 26.0 10 6 5 .26
ESA | 1 | 7.4 .9 28.5 35 -55 14 .04
GFZ | 1 | -.5 .9 -.5 -10 -56 0 -.36
GRG | 1 | 2.5 -2.3 22.9 -19 8 -17 .40
JPL | 1 | 8.4 -2.7 23.5 -38 27 -5 .55
MIT | 1 | 1.4 -6.1 29.5 8 -1 -28 .27
NGS | 1 | 6.4 -4.1 32.3 -217 -49 33 .60
SIO | 1 | -3.5 -1.7 26.1 -101 86 -54 .27
COD | 2 | -.8 1.0 -2.3 -49 2 -17 .18
EMR | 2 | 4.3 3.2 14.9 2 -2 13 .19
ESA | 2 | 3.3 4.6 35.6 57 -75 11 .13
GFZ | 2 | -.5 .8 -.7 -16 -38 -3 -.37
GRG | 2 | 2.3 3.1 22.1 -3 28 -1 .34
JPL | 2 | 4.5 -.4 21.5 -31 55 6 .37
MIT | 2 | 3.8 .1 29.1 4 1 -24 .17
NGS | 2 | 5.3 -3.4 34.2 -221 -47 36 .58
SIO | 2 | 3.6 1.6 24.4 -46 -22 13 .18
COD | 3 | .1 .8 -2.1 -26 -13 -3 .33
EMR | 3 | .2 -5.3 22.7 1 -5 -4 .43
ESA | 3 | 6.8 1.4 34.5 39 -101 1 .27
GFZ | 3 | -.1 .7 -.6 -12 -33 -3 -.21
GRG | 3 | 3.8 4.3 26.9 -11 16 -5 .38
JPL | 3 | 7.4 -7.0 22.8 -12 6 -7 .76
MIT | 3 | 3.8 .2 26.0 -4 -1 -17 .39
NGS | 3 | 2.4 -3.2 31.1 -230 -33 15 .62
SIO | 3 | 4.2 .2 18.6 15 -9 67 .40
COD | 4 | .3 1.1 -1.4 -33 -21 11 .32
EMR | 4 | -2.2 -1.9 17.5 -4 -5 -14 .28
ESA | 4 | 2.7 -.5 35.4 41 -73 -6 .35
GFZ | 4 | -.6 .4 .2 -27 -32 -7 -.18
GRG | 4 | -4.4 6.7 20.0 -14 49 -4 .72
JPL | 4 | 3.2 -6.5 12.4 -10 29 23 .52
MIT | 4 | 3.6 2.8 25.7 -5 4 -24 .23
NGS | 4 | 3.8 1.9 25.9 -132 -73 45 .59
SIO | 4 | 2.9 -3.4 38.0 -111 36 43 .38
COD | 5 | -.2 1.2 -1.4 -36 -14 -8 .42
EMR | 5 | -4.6 -9.8 13.6 6 5 -8 .29
ESA | 5 | 1.8 .2 25.8 43 -64 -6 .25
GFZ | 5 | -1.0 .5 .1 -29 -19 -14 -.09
GRG | 5 | 5.6 3.1 26.2 -14 32 -19 .45
JPL | 5 | 3.3 -4.2 17.6 -43 22 -42 .35
MIT | 5 | .1 .5 24.9 -7 -1 -14 .15
NGS | 5 | 11.0 -3.2 33.0 -180 -75 68 .59
SIO | 5 | 4.0 -1.0 33.6 -30748 949 -1537 .59
COD | 6 | -.7 .6 -1.1 -49 8 -15 .20
EMR | 6 | 5.8 -3.2 13.8 -7 11 -24 .26
ESA | 6 | 2.1 3.3 26.9 113 -87 7 .28
GFZ | 6 | -.4 .3 .0 -21 -22 -5 -.13
GRG | 6 | 6.9 6.4 27.1 -15 6 -6 .30
JPL | 6 | 6.6 .8 23.2 -70 40 -67 .21
MIT | 6 | .6 4.2 24.8 -3 -4 -24 .11
NGS | 6 | 7.2 -2.0 37.9 -228 -60 52 .58
SIO | 6 | 7.0 -1.6 33.5 -41 29 114 .17
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 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 seven 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 1.1738.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1738.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 2.1738.[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 3.1738.[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 part,
Table 5, is similar to Table 4 and contains daily precise navigation
statistics (Tables 5.1738.0-6). The sixth part, Table 6, is a weekly
summary of daily ERP combination statistics. The seventh part, Table 7,
contains the daily ERP statistics. But this is not the IGS official ERP
combination products (which come from the accompanying SINEX combination)
but provided to check combination consistency, etc.
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 1738 summary. (Apr 28, 2013 - May 04, 2013)
Table 1.1738.a GPS week: 1738 MJD: 56410.000-56416.000
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 263| 0 0 -4 12 -3 19 -.36 12 11 | -1051 -277 21 92
| 0 1 2 22 27 5 .03 | 699 864
emr 79| 0 -1 -2 -26 -8 20 .31 16 16 | -570673 -12837 16 96
| 2 1 1 18 12 29 .05 | 535462 11945
esa 150| 1 0 0 3 -29 4 .06 6 6 | -982 43 14 112
| 0 0 0 28 17 10 .02 | 1411 1393
gfz 193| -1 0 -2 -37 2 14 -.42 11 10 | 85 126 20 100
| 0 1 0 47 44 9 .02 | 366 623
grg 135| 1 2 5 -5 35 -14 .62 13 12 | -195 346 17 141
| 0 1 1 12 11 14 .04 | 214 484
igr n/a| 0 0 -3 -9 33 -22 -.17 4 4 | 4104 608 18 88
| 0 0 1 17 18 11 .02 | 631 927
jpl 80| 0 1 -7 -13 10 -25 .27 15 15 | 1616 544 19 117
| 1 1 1 30 14 18 .04 | 661 961
mit 235| -1 -1 3 8 17 0 -.56 12 11 | -652 438 23 198
| 0 1 1 21 16 18 .05 | 1028 1283
ngs 243| 0 0 8 27 25 -29 .28 12 10 | -710 -432 1845 3943
| 0 0 2 44 31 18 .04 | 650 1004
sio 326| -3 0 -9 -79 30 4 -.49 18 18 | --- --- --- ---
| 0 0 0 56 43 63 .03 | --- ---
Table 1.1738.b GPS week : 1738 MJD: 56410.000-56416.000
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 3 4 4 4 3 |
2 | 5 4 4 4 4 5 4 |
3 | 4 3 3 3 4 4 3 |
4 | 4 4 4 4 4 5 4 |
5 | 5 4 5 4 5 5 5 |
6 | 4 3 3 3 4 4 3 |
7 | 5 5 5 4 4 4 5 |
8 | 4 3 4 3 3 4 3 |
9 | 3 3 4 4 4 4 4 |
10 | 7 6 6 6 6 6 6 |
11 | 4 4 4 4 4 4 4 |
12 | 6 6 6 6 6 6 5 |
13 | 5 5 5 5 4 5 5 |
14 | 5 5 4 4 5 4 4 |
15 | 5 7 6 4 5 6 5 |
16 | 5 4 4 4 4 5 4 |
17 | 5 5 5 5 5 5 5 |
18 | 5 4 5 5 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 5 5 5 5 4 5 4 |
21 | 5 4 5 4 4 4 4 |
22 | 4 4 4 4 4 4 3 |
23 | 5 5 4 4 6 5 5 |
24 | 4 5 4 5 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 3 4 3 3 4 4 |
27 | 0 0 0 0 0 0 0 |
28 | 4 4 4 4 4 4 3 |
29 | 5 5 5 5 5 5 4 |
30 | 8 7 8 8 7 10 12 |
31 | 5 5 5 5 5 5 4 |
32 | 6 6 6 5 5 5 5 |
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
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1738.0 GPS week: 1738 Day: 0 MJD: 56410.000
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 -3 -8 -45 16 -.36 12 12 | -356 -815 21 87
emr 79| 1 -2 -1 -26 -27 -1 .30 17 17 | 2558 -1120 18 88
esa 150| 1 0 -1 -34 -41 0 .05 7 7 | -112 -1226 13 91
gfz 190| 0 0 -2 -30 37 27 -.42 11 10 | 95 109 22 99
grg 134| 1 0 5 9 21 -22 .57 13 12 | -236 233 17 145
igr n/a| 0 0 -3 -14 8 0 -.15 5 5 | 4633 -942 18 93
jpl 80| 0 0 -7 -45 -4 -11 .27 16 15 | 2371 -1055 21 121
mit 238| -1 -2 5 29 21 -4 -.50 11 10 | 442 -831 25 182
ngs 244| -2 0 5 97 74 -17 .35 12 9 | -885 590 2013 4142
sio 310| -3 0 -9 -74 100 110 -.46 18 19 | --- --- --- ---
Table 2.1738.1 GPS week: 1738 Day: 1 MJD: 56411.000
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 268| 1 2 -5 35 -29 20 -.34 12 13 | -1008 -16 22 112
emr 80| 0 -1 0 0 -5 -1 .37 17 16 | 910 528 21 111
esa 150| 0 0 0 0 -5 16 .07 6 6 | -486 -1095 14 111
gfz 196| 0 0 -3 -55 -19 25 -.42 11 11 | -118 89 22 100
grg 139| 1 0 1 0 31 -14 .57 13 12 | -489 465 16 147
igr n/a| 0 0 -1 16 17 -28 -.20 5 5 | 3302 558 19 80
jpl 80| 0 3 -7 -19 25 -8 .27 15 14 | 984 557 18 113
mit 238| -1 -3 6 13 -13 -25 -.51 12 9 | -641 807 23 193
ngs 247| 0 0 11 -6 40 -54 .27 13 10 | -1043 -209 1758 3369
sio 309| -3 0 -8 -136 36 -91 -.47 17 19 | --- --- --- ---
Table 2.1738.2 GPS week: 1738 Day: 2 MJD: 56412.000
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 266| 1 -1 -3 15 1 24 -.38 12 11 | -787 -1411 22 90
emr 80| 0 1 -2 -19 -11 48 .36 16 16 | -999999 -21668 17 89
esa 150| 1 0 -1 0 -50 12 .05 6 6 | -80 -783 17 126
gfz 197| -1 0 -1 -16 44 6 -.40 11 10 | -11 716 20 98
grg 138| 1 3 4 -13 50 -16 .62 14 13 | -221 457 17 150
igr n/a| 0 0 -4 10 20 -31 -.16 4 4 | 3716 1492 20 96
jpl 80| -3 2 -8 12 13 -12 .34 15 14 | 1388 1572 20 133
mit 236| 0 -3 5 -2 28 -23 -.52 12 10 | -883 -75 24 209
ngs 245| 0 0 8 18 -11 -37 .29 12 10 | -396 -702 1523 3497
sio 311| -1 0 -8 -94 -34 -30 -.47 17 18 | --- --- --- ---
Table 2.1738.3 GPS week: 1738 Day: 3 MJD: 56413.000
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 266| 0 0 -4 -14 5 29 -.33 10 10 | -2318 882 22 88
emr 80| -1 0 0 -61 6 40 .32 16 16 | -999999 -23072 16 111
esa 150| 1 0 0 -15 -46 -11 .07 5 5 | -959 127 11 106
gfz 195| -2 -1 -2 50 51 13 -.38 11 11 | 834 -1045 20 105
grg 136| 3 3 5 0 46 4 .61 14 13 | 28 -143 18 138
igr n/a| 0 0 -3 -32 37 -32 -.16 4 4 | 4575 -168 17 74
jpl 80| -1 0 -10 -21 0 -48 .26 15 15 | 2257 -283 22 129
mit 236| 0 -1 2 37 24 7 -.56 12 11 | -2782 3144 23 202
ngs 246| -1 0 7 13 -5 -30 .25 12 10 | 422 -2279 2000 3921
sio 303| -1 1 -11 -3 0 32 -.47 17 16 | --- --- --- ---
Table 2.1738.4 GPS week: 1738 Day: 4 MJD: 56414.000
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 -2 48 -12 14 -.40 11 11 | -1595 577 25 101
emr 81| -1 -1 -2 -21 -21 -24 .31 14 14 | 1811 320 12 90
esa 150| 1 0 0 23 -29 4 .04 6 6 | -786 1628 17 132
gfz 190| -1 -1 -3 -102 -7 1 -.45 12 10 | 197 686 20 90
grg 134| 1 3 6 -3 41 6 .64 13 13 | -318 1299 18 121
igr n/a| 0 0 -4 -8 49 -23 -.18 5 4 | 4274 746 19 94
jpl 80| 0 0 -8 35 21 -11 .22 15 14 | 1759 514 17 106
mit 236| 0 0 2 -23 29 12 -.60 14 12 | -317 -13 22 185
ngs 240| 0 1 5 -13 30 0 .27 12 10 | -1650 602 2182 4959
sio 353| -3 1 -10 -160 58 33 -.51 19 17 | --- --- --- ---
Table 2.1738.5 GPS week: 1738 Day: 5 MJD: 56415.000
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 255| 0 0 -8 8 32 17 -.40 12 12 | -923 -41 18 75
emr 80| -4 -3 -2 -22 -5 49 .24 16 16 | -999999 -21946 19 100
esa 150| 1 0 0 -5 -22 12 .04 6 6 | -4097 2294 16 108
gfz 191| -1 -1 -2 -62 -18 13 -.42 13 12 | -306 548 21 109
grg 133| 0 3 6 -28 37 -32 .67 13 13 | 146 -108 18 135
igr n/a| 0 0 -4 -15 40 -23 -.17 4 4 | 3384 1749 19 80
jpl 80| 0 0 -5 -5 -8 -32 .23 15 15 | 590 1602 19 115
mit 229| -1 0 2 16 27 5 -.61 13 12 | -295 55 23 198
ngs 240| 0 1 11 83 4 -45 .25 12 11 | -968 -68 1883 4556
sio 345| -3 0 -10 -22 45 6 -.54 19 18 | --- --- --- ---
Table 2.1738.6 GPS week: 1738 Day: 6 MJD: 56416.000
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 258| 0 0 -5 2 23 14 -.34 10 10 | -371 -1120 20 93
emr 79| 1 -2 -4 -35 4 32 .24 16 16 | -999999 -22906 10 84
esa 150| 0 0 0 54 -11 -4 .10 6 6 | -356 -643 14 114
gfz 193| 0 -1 -1 -49 -71 11 -.43 9 9 | -90 -221 18 104
grg 134| 1 2 6 0 23 -24 .66 11 11 | -279 219 19 152
igr n/a| -1 0 -4 -21 57 -18 -.18 4 4 | 4847 824 16 102
jpl 80| 0 0 -6 -51 26 -50 .32 15 15 | 1964 904 16 107
mit 236| -2 0 2 -10 4 25 -.62 12 11 | -91 -18 25 218
ngs 242| 0 0 10 -1 45 -17 .29 12 10 | -453 -961 1559 3163
sio 355| -3 0 -9 -62 9 -30 -.50 19 17 | --- --- --- ---
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 3.1738.0 GPS week: 1738 Day: 0 MJD: 56410.000
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 10 5 9 11 4 13 6 8 14 3 | 22 27 22 20 30 19 32 18 29 21 21
2 | 11 21 9 10 10 6 17 13 7 29 4 | 28 30 31 30 29 29 27 28 31 25 27
3 | 12 9 5 13 7 3 9 9 10 14 3 | 17 22 19 22 23 19 21 22 28 21 19
4 | 10 12 9 8 9 5 9 15 8 20 4 | 30 33 38 32 36 32 32 34 36 30 33
5E | 10 18 5 10 15 4 21 10 10 15 4 | 29 33 29 25 28 28 34 24 28 26 26
6 | 11 8 4 13 8 3 10 9 8 15 3 | 18 23 20 26 25 21 21 25 30 20 21
7 | 10 16 8 12 18 4 12 12 12 20 4 | 21 29 20 21 33 18 25 19 26 27 19
8 | 6 15 7 10 7 4 14 8 9 12 3 | 14 25 18 15 18 13 23 14 23 18 15
9 | 8 10 5 9 8 5 13 9 9 11 3 | 25 27 23 21 23 22 26 20 27 23 21
10E | 19 24 9 11 16 5 16 18 26 18 6 | 41 50 42 37 41 39 43 35 54 44 41
11 | 11 13 8 11 11 4 14 8 11 17 4 | 39 46 44 47 54 44 45 46 51 39 44
12E | 16 22 8 9 21 5 28 6 13 10 5 | 18 26 15 16 23 14 26 17 27 18 15
13 | 11 18 7 12 17 5 14 13 12 16 4 | 20 28 26 28 37 23 29 26 23 30 24
14 | 10 20 7 14 12 5 15 13 9 23 4 | 25 26 27 31 32 26 27 25 25 31 24
15 | 22 14 5 10 16 4 20 7 12 15 5 | 28 25 21 20 30 19 23 17 26 21 18
16 | 11 19 6 12 13 2 20 9 7 14 4 | 49 53 51 48 55 49 54 50 58 50 50
17 | 17 23 8 9 11 6 17 11 11 20 5 | 29 36 34 31 34 29 30 36 38 29 30
18E | 9 13 6 14 18 4 15 10 9 11 4 | 31 33 31 26 34 28 31 29 30 26 29
19 | 9 12 5 12 11 4 15 13 8 22 4 | 17 25 21 26 26 21 22 26 29 24 21
20E | 9 19 8 12 18 5 15 8 10 9 4 | 24 32 26 22 26 19 26 19 23 27 21
21 | 11 17 7 12 11 4 16 11 11 21 4 | 28 29 29 31 32 28 26 33 30 31 27
22E | 9 11 5 11 11 4 13 9 9 13 3 | 17 19 16 13 19 13 17 16 26 15 14
23 | 13 17 8 13 14 6 15 11 10 24 4 | 26 36 32 27 35 26 30 31 30 29 28
24 | 14 13 8 8 16 3 12 8 11 26 4 | 26 25 21 19 29 19 26 16 27 21 19
25E | 10 22 7 9 12 4 13 9 10 12 4 | 12 30 19 13 22 15 22 15 23 14 15
26 | 9 11 5 8 10 5 11 10 9 14 3 | 25 24 24 23 26 21 23 18 23 23 21
X27E | 6 --- --- --- --- 49 --- --- --- --- 0 | 85 --- --- --- --- 82 --- --- --- --- 85
28 | 10 13 6 6 12 4 12 7 10 10 3 | 59 60 60 60 60 58 60 59 63 61 59
29 | 12 18 7 11 13 2 19 14 8 26 4 | 25 28 25 23 28 23 26 24 30 31 23
30E | 18 32 16 14 15 16 17 17 29 --- 7 | 26 38 34 20 23 30 28 18 45 --- 25
31 | 10 22 6 11 17 5 15 13 9 24 4 | 19 31 20 19 35 19 26 20 29 19 20
32E | 17 21 6 9 14 8 19 17 14 14 5 | 29 35 26 27 25 24 30 21 27 25 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 7 11 13 5 16 11 12 18 |T 28 31 27 26 31 27 29 25 32 27 27
WRMS | 12 17 7 10 12 5 15 10 9 19 |NE 24 28 25 25 30 23 27 24 29 25 23
MEDI | 11 17 7 11 12 4 15 10 10 15 |MD 25 29 26 25 29 23 26 24 29 25 23
Table 3.1738.1 GPS week: 1738 Day: 1 MJD: 56411.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 7 5 12 10 4 12 5 14 12 3 | 22 23 19 15 28 16 30 14 25 14 18
2 | 10 18 6 9 11 4 17 13 8 28 4 | 17 23 18 19 21 16 22 20 20 17 16
3 | 8 8 4 12 8 3 11 6 8 16 3 | 17 19 15 19 20 17 17 18 31 18 16
4 | 10 12 4 9 12 5 9 10 9 14 3 | 19 23 24 22 28 21 25 22 28 20 23
5E | 11 17 5 10 12 5 18 12 9 17 4 | 27 30 23 23 29 22 28 28 32 24 24
6 | 7 9 4 11 6 4 11 5 7 17 3 | 18 18 16 18 18 17 15 17 30 17 16
7 | 10 14 8 11 17 5 14 14 8 18 4 | 19 24 15 17 31 14 20 19 26 21 15
8 | 6 14 5 10 7 4 13 10 8 13 3 | 16 24 14 16 19 13 22 17 26 18 14
9 | 7 9 3 8 8 3 11 10 6 11 2 | 18 24 17 18 22 15 24 18 22 19 17
10E | 15 29 7 11 12 6 18 14 23 21 6 | 29 49 30 28 37 27 36 31 47 36 31
11 | 12 12 6 11 11 5 12 6 17 16 4 | 28 37 27 29 41 29 35 29 30 24 28
12E | 14 21 6 9 25 7 28 9 11 13 5 | 15 25 11 13 23 10 26 14 23 16 12
13 | 13 17 6 11 17 4 12 12 13 17 4 | 20 26 19 19 34 16 24 18 29 19 18
14 | 8 21 5 14 12 4 14 11 14 21 4 | 19 27 20 23 27 18 23 17 25 24 18
15 | 37 17 6 11 16 6 21 11 18 16 6 | 38 23 18 16 30 19 23 18 29 20 18
16E | 8 17 5 14 14 5 19 7 10 21 4 | 28 29 27 25 36 24 31 25 35 20 26
17 | 14 19 6 13 10 5 17 10 13 17 4 | 20 31 19 21 25 19 25 24 26 20 18
18E | 8 15 6 12 9 3 16 8 10 14 4 | 24 29 25 23 30 22 27 22 35 26 24
19 | 9 13 4 11 11 4 14 11 11 23 3 | 17 22 16 16 20 18 19 17 27 17 15
20E | 12 19 6 14 15 8 16 10 12 9 4 | 21 27 21 15 26 17 25 20 25 17 18
21 | 9 18 5 12 11 5 15 12 11 20 4 | 25 25 23 25 25 24 24 24 33 20 22
22E | 9 16 5 10 11 3 13 12 11 11 3 | 17 18 13 13 16 10 15 14 24 12 11
23 | 13 17 6 14 14 5 13 13 12 24 4 | 25 31 27 27 37 24 29 21 36 20 25
24 | 9 13 6 8 22 5 14 11 13 13 4 | 16 23 15 11 28 14 22 15 26 14 14
25E | 8 18 5 10 17 4 10 12 10 14 4 | 14 22 14 10 18 12 19 14 24 13 11
26 | 8 11 3 7 10 3 10 7 10 13 3 | 23 20 18 20 25 16 20 17 22 17 17
X27E | 6 --- --- --- --- 41 --- --- --- --- 0 | 105 --- --- --- --- 103 --- --- --- --- 103
28E | 12 13 5 11 11 8 11 10 14 9 4 | 46 45 42 42 48 38 45 37 45 38 42
29 | 12 16 6 10 13 4 19 17 11 25 4 | 19 24 18 16 21 16 24 16 26 19 16
30E | 15 33 18 12 9 9 15 18 27 --- 7 | 24 38 32 21 25 22 26 15 44 --- 22
31 | 11 20 6 12 20 5 12 16 15 24 5 | 19 28 16 15 36 13 26 15 25 15 16
32E | 16 24 7 11 14 9 17 20 18 15 5 | 30 35 27 27 29 29 33 31 34 29 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 6 11 13 5 15 12 13 17 |T 24 27 20 20 27 21 25 20 29 20 22
WRMS | 13 16 6 11 12 5 14 9 10 19 |NE 20 24 18 19 26 17 23 18 27 18 18
MEDI | 10 17 6 11 12 5 14 11 11 16 |MD 20 25 19 19 27 17 24 18 27 19 18
Table 3.1738.2 GPS week: 1738 Day: 2 MJD: 56412.000
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 | 7 11 3 11 10 3 10 7 11 10 3 | 20 28 19 18 27 18 29 17 31 16 20
2 | 12 17 6 8 11 4 16 8 7 29 4 | 21 24 23 21 24 19 24 25 27 23 21
3 | 9 10 4 10 8 4 9 8 10 16 3 | 17 15 17 21 19 16 15 18 29 16 16
4 | 12 12 4 9 12 3 8 14 10 15 3 | 22 29 28 25 34 24 28 31 34 26 27
5E | 10 18 6 11 13 4 18 9 11 13 4 | 21 25 21 20 24 19 23 19 34 19 19
6 | 7 10 3 9 8 4 9 8 9 18 3 | 18 17 18 23 20 17 18 22 29 19 18
7 | 13 15 7 13 19 3 15 12 14 15 5 | 26 26 21 18 30 21 25 25 32 25 20
8 | 7 15 4 10 12 3 12 11 8 13 3 | 23 25 18 16 17 19 25 25 32 26 19
9 | 9 12 3 7 11 3 13 14 6 14 3 | 20 26 16 15 21 16 25 18 23 20 16
10E | 18 19 10 11 18 5 16 13 23 24 6 | 25 37 30 26 33 28 38 30 48 36 30
11 | 10 13 5 12 9 4 11 6 11 15 3 | 25 37 33 37 41 32 34 32 40 26 32
12E | 17 27 8 10 25 5 24 11 10 12 6 | 23 29 16 17 24 15 26 19 24 20 16
13 | 10 16 7 12 17 3 14 12 11 16 4 | 18 26 20 22 34 19 27 19 25 24 19
14 | 8 17 5 10 16 5 15 10 13 19 4 | 20 24 21 23 29 22 25 20 26 25 20
15 | 28 18 6 13 16 4 20 10 12 15 6 | 36 24 18 20 31 16 22 14 25 16 17
16E | 9 20 5 13 12 4 17 7 11 20 4 | 23 27 22 20 28 22 27 19 31 25 21
17 | 17 18 7 13 9 4 19 15 14 18 5 | 27 32 26 27 31 24 31 32 32 25 25
18E | 11 12 8 12 14 5 16 16 10 15 4 | 42 46 47 44 47 44 49 45 51 44 45
19 | 9 15 6 11 11 4 14 14 11 23 4 | 15 20 16 20 20 17 19 20 30 18 16
20E | 10 16 6 12 12 6 19 8 14 10 4 | 19 28 21 16 27 19 27 21 24 21 19
21 | 12 16 7 12 12 4 17 11 11 19 4 | 28 23 23 30 26 24 22 28 29 23 23
22E | 9 13 5 9 16 4 14 11 9 12 4 | 17 20 16 15 21 14 21 16 28 17 16
23 | 9 14 7 12 14 4 13 12 11 23 4 | 26 36 28 30 39 27 33 26 38 23 28
24 | 9 12 6 7 18 4 14 13 11 13 4 | 17 25 16 14 25 15 29 18 26 21 16
25E | 11 14 8 9 14 4 11 13 14 13 4 | 14 21 16 12 26 13 25 18 21 17 14
26 | 12 12 4 8 13 4 10 9 12 11 3 | 21 24 21 20 21 20 24 20 23 22 19
X27E | 6 --- --- --- --- 80 --- --- --- --- 0 | 88 --- --- --- --- 55 --- --- --- --- 91
28E | 10 11 5 10 12 4 12 19 11 16 4 | 36 34 32 34 36 32 33 38 40 38 32
29 | 14 20 9 10 13 4 18 13 10 23 5 | 23 25 20 18 24 16 26 19 31 21 19
X30E | 15 --- 13 13 15 13 --- 14 29 --- 7 | 21 --- 28 20 25 26 --- 18 45 --- 21
31 | 11 20 8 10 18 3 14 14 16 21 5 | 17 28 18 20 36 18 29 20 29 21 19
32E | 13 19 7 14 14 5 15 18 18 15 5 | 22 32 21 22 23 21 27 21 33 23 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 11 14 4 15 12 12 17 |T 24 27 22 22 27 22 26 23 31 23 23
WRMS | 11 16 6 10 13 4 14 10 10 18 |NE 22 25 21 21 27 20 25 22 29 21 20
MEDI | 10 15 6 11 13 4 14 12 11 15 |MD 21 26 21 20 26 19 26 20 30 22 19
Table 3.1738.3 GPS week: 1738 Day: 3 MJD: 56413.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 10 3 11 10 4 14 10 11 12 3 | 21 26 24 21 29 21 30 21 28 20 21
2 | 11 19 6 7 8 3 17 10 10 29 4 | 20 28 25 24 27 23 24 27 27 25 23
3 | 6 11 3 12 9 3 10 8 12 14 3 | 25 25 28 26 27 25 29 28 29 29 26
4 | 11 11 5 8 13 3 10 18 11 14 4 | 24 31 31 30 34 29 28 36 33 31 30
5E | 8 18 4 11 11 3 20 11 9 11 4 | 28 34 30 29 35 29 34 31 35 30 30
6 | 5 11 4 11 7 3 10 7 10 14 3 | 23 25 28 30 28 25 25 29 29 27 26
7 | 11 15 6 11 15 3 14 9 11 16 4 | 24 29 20 24 32 21 25 20 26 28 21
8 | 7 16 4 7 10 3 10 9 9 11 3 | 20 27 23 22 22 21 28 24 30 25 23
9 | 7 12 5 6 14 3 13 13 12 13 3 | 24 29 23 22 24 22 29 25 25 25 23
10E | 18 27 7 10 15 5 18 15 20 20 5 | 37 49 37 34 39 34 43 37 51 43 37
11 | 13 13 6 14 9 5 14 10 12 14 4 | 34 45 42 46 51 42 41 42 40 35 41
12E | 15 23 6 8 20 6 26 15 11 17 5 | 21 32 19 21 26 17 32 26 31 28 20
13 | 10 17 5 12 17 3 13 14 12 17 4 | 15 29 21 26 36 19 27 21 26 25 21
14 | 7 15 5 15 12 7 17 7 11 21 4 | 24 26 25 33 28 26 25 22 21 30 23
15 | 10 17 4 9 14 4 13 10 9 17 3 | 25 33 26 25 34 26 27 26 30 26 25
16E | 10 14 4 13 11 5 17 7 11 17 4 | 25 21 23 19 26 19 27 22 31 26 21
17 | 14 20 6 14 12 3 18 13 10 19 4 | 27 32 26 30 31 23 28 32 32 25 25
18E | 11 17 5 13 19 4 14 12 8 15 4 | 38 41 41 30 43 37 38 39 35 43 37
19 | 9 18 6 12 10 3 16 12 11 22 4 | 18 25 22 25 26 21 21 22 22 19 20
20E | 10 15 5 12 21 4 16 13 13 14 4 | 19 24 20 16 25 16 24 17 33 24 18
21 | 7 15 5 12 11 3 17 10 9 20 3 | 32 28 33 31 34 32 32 33 31 31 30
22E | 6 13 6 11 13 3 9 12 11 14 3 | 14 20 19 19 19 14 17 15 25 17 14
23 | 8 19 6 13 14 4 14 14 10 25 4 | 33 41 36 36 42 35 37 35 39 32 35
24 | 13 12 4 9 20 6 16 16 12 12 4 | 28 28 22 19 30 21 26 22 26 22 21
25E | 10 16 6 12 16 5 12 13 12 13 4 | 18 26 21 18 24 17 24 20 22 19 18
26 | 6 13 5 8 10 3 10 9 13 11 3 | 22 26 25 25 24 24 27 26 24 25 24
X27E | 6 --- --- --- --- 53 --- --- --- --- 0 | 100 --- --- --- --- 115 --- --- --- --- 101
28E | 10 12 5 8 14 4 14 12 12 8 4 | 34 31 34 34 35 33 35 35 32 38 31
29 | 13 17 6 12 11 5 21 16 7 21 4 | 26 27 25 25 28 23 29 24 30 29 24
X30E | 16 21 10 16 30 12 --- 14 30 --- 7 | 24 36 27 20 37 23 --- 22 46 --- 25
31 | 11 18 7 12 18 4 14 10 15 20 4 | 22 27 22 23 36 20 29 20 27 24 21
32E | 14 18 6 14 12 5 16 20 16 14 5 | 25 26 21 23 19 20 24 19 30 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 5 11 14 4 15 12 12 17 |T 27 29 26 26 30 27 28 26 30 27 27
WRMS | 10 16 5 11 13 4 15 11 10 16 |NE 24 29 26 27 31 24 28 26 28 26 25
MEDI | 10 16 5 12 13 4 14 12 11 14 |MD 24 28 25 25 29 23 28 25 30 26 23
Table 3.1738.4 GPS week: 1738 Day: 4 MJD: 56414.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 9 4 12 9 4 15 10 12 14 3 | 22 29 21 20 30 20 32 18 28 18 22
2 | 14 14 6 10 11 4 18 11 8 31 4 | 23 24 22 26 28 19 26 27 25 25 21
3 | 6 9 3 13 10 3 8 11 13 21 3 | 16 17 16 19 23 15 18 18 17 15 15
4 | 12 9 6 9 12 4 10 19 7 20 4 | 25 28 29 30 33 27 30 35 30 29 28
5E | 11 18 6 14 15 4 20 12 12 10 4 | 24 27 22 25 29 21 29 27 26 27 22
6 | 7 7 5 12 8 4 9 12 14 20 3 | 19 20 19 19 24 18 20 21 19 17 17
7 | 10 14 6 15 14 3 13 12 13 16 4 | 28 27 22 25 35 22 26 20 30 24 22
8 | 8 10 4 10 8 3 12 8 12 12 3 | 24 28 19 19 24 21 29 19 32 21 21
9 | 10 9 3 8 13 3 12 15 6 14 3 | 23 26 20 18 23 21 28 27 26 25 21
10E | 18 18 10 13 18 6 15 18 22 21 6 | 28 38 27 31 38 28 36 33 42 36 30
11 | 12 13 5 13 9 4 11 10 7 17 3 | 35 47 42 39 51 38 43 38 44 33 40
12E | 15 23 5 9 21 5 27 14 11 13 5 | 28 33 23 24 31 23 35 28 31 30 25
13 | 10 16 5 13 17 4 12 13 8 16 4 | 21 26 20 20 34 18 26 20 21 21 19
14 | 9 16 6 11 10 6 15 11 17 21 4 | 26 28 26 28 31 22 27 22 26 27 24
15 | 22 18 4 10 14 4 17 12 11 17 5 | 30 29 21 22 32 20 29 21 30 23 22
16E | 7 14 6 14 11 5 16 9 9 19 4 | 22 25 20 21 27 20 27 19 27 23 20
17 | 12 18 6 15 10 5 16 13 10 22 4 | 29 30 24 26 29 23 30 27 30 22 23
18E | 7 12 6 10 18 5 16 11 13 15 4 | 56 64 58 59 61 56 63 56 58 57 58
19 | 7 13 6 15 12 5 14 12 12 22 4 | 19 24 21 24 26 21 22 20 25 16 19
20E | 12 13 6 12 12 5 16 11 14 17 4 | 18 21 16 19 20 15 20 17 27 21 15
21 | 14 14 5 12 11 5 16 12 11 22 4 | 31 29 32 32 33 30 30 36 27 32 29
22E | 6 11 5 9 15 5 13 12 13 14 3 | 20 27 22 21 24 17 23 19 24 20 20
23 | 10 16 5 15 20 7 14 37 12 31 6 | 62 66 57 56 59 55 62 57 57 57 57
24 | 10 12 5 9 13 4 13 17 8 12 4 | 20 26 18 18 27 16 26 22 21 18 18
25E | 11 14 6 9 13 4 14 13 11 12 4 | 20 24 18 16 22 15 27 19 20 18 16
26 | 12 8 3 7 10 3 8 10 9 11 3 | 26 22 22 18 24 21 21 20 23 19 20
X27E | 7 --- --- --- --- 61 --- --- --- --- 0 | 122 --- --- --- --- 93 --- --- --- --- 119
28E | 10 11 5 9 11 4 12 17 11 19 4 | 32 29 26 29 30 27 31 30 34 32 28
29 | 15 17 5 11 12 6 20 11 8 21 4 | 29 30 26 25 28 24 31 26 27 29 25
X30E | 23 22 7 18 --- 16 16 15 27 --- 7 | 32 34 28 19 --- 30 31 19 47 --- 27
31 | 7 19 9 9 14 5 12 10 13 20 4 | 29 34 25 28 39 27 32 21 31 26 26
32E | 14 15 6 12 12 5 13 17 17 18 4 | 24 27 20 25 20 23 26 20 32 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 6 12 13 5 15 14 12 19 |T 30 30 25 25 31 26 30 25 30 26 27
WRMS | 11 14 6 10 13 4 14 12 10 17 |NE 26 29 25 25 31 23 29 25 28 24 24
MEDI | 10 14 5 12 12 4 14 12 12 17 |MD 25 28 22 24 29 21 29 21 27 23 22
Table 3.1738.5 GPS week: 1738 Day: 5 MJD: 56415.000
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 13 3 13 12 3 15 9 15 17 4 | 19 25 19 24 30 18 30 19 24 22 19
2 | 15 17 7 13 11 3 18 17 11 32 5 | 21 21 21 19 22 16 25 22 33 19 18
3 | 11 12 4 12 9 2 10 12 9 20 3 | 24 22 20 23 21 20 21 24 31 21 20
4 | 13 15 6 12 13 3 10 20 10 21 4 | 20 27 26 21 32 22 27 24 38 20 24
5E | 12 24 7 13 13 4 20 15 14 13 5 | 20 28 24 21 29 22 30 22 39 20 22
6 | 9 12 4 12 10 3 8 12 10 18 3 | 23 19 19 21 23 19 20 23 28 18 18
7 | 6 14 7 15 13 3 14 13 11 20 4 | 19 23 18 19 27 16 23 18 29 26 17
8 | 7 16 4 12 12 3 16 8 8 14 3 | 15 23 15 16 19 15 26 15 24 18 15
9 | 10 17 4 9 14 5 14 14 5 14 4 | 16 21 17 17 21 13 20 16 26 13 15
10E | 21 22 10 15 13 5 15 18 19 20 6 | 32 44 33 31 40 31 39 37 47 35 34
11 | 11 13 4 12 13 4 12 8 11 18 3 | 33 41 36 36 48 32 41 32 37 29 35
12E | 16 25 7 10 24 4 26 13 16 16 6 | 23 31 21 19 26 17 29 18 25 17 19
13 | 10 14 6 14 14 4 17 14 13 17 4 | 17 25 20 23 32 17 23 19 30 22 19
14 | 9 16 4 14 12 4 16 13 11 21 4 | 23 24 24 28 26 22 23 24 34 25 22
15 | 16 20 5 14 16 4 18 22 12 17 5 | 28 25 23 18 30 19 23 28 33 20 21
16E | 10 18 6 18 11 4 15 11 12 21 4 | 26 29 22 21 27 20 26 19 29 21 21
17 | 14 20 7 16 12 6 20 11 9 24 5 | 25 28 23 24 34 18 28 23 33 17 22
18E | 8 12 6 15 16 3 14 10 10 15 4 | 37 41 40 43 42 36 41 38 47 40 39
19 | 9 16 5 12 9 3 14 9 10 23 3 | 19 24 19 20 25 17 22 16 27 16 18
20E | 13 12 5 15 17 4 14 11 12 19 4 | 14 23 17 19 28 15 22 18 28 25 16
21 | 12 16 6 14 11 4 14 10 13 22 4 | 30 26 25 32 23 26 24 32 30 31 24
22E | 12 12 6 11 15 3 9 12 11 14 4 | 16 19 18 18 18 12 17 17 28 17 15
23 | 10 14 7 16 13 5 17 16 11 24 4 | 34 40 36 39 45 35 36 33 42 33 35
24 | 10 13 8 9 13 2 13 13 8 14 4 | 15 24 19 16 24 14 23 15 24 14 15
25E | 12 12 7 10 13 3 16 14 11 15 4 | 18 18 19 14 20 13 24 17 23 16 15
26 | 13 16 3 8 12 5 11 15 9 13 4 | 17 21 16 14 18 14 19 22 24 16 15
X27E | 8 --- --- --- --- 75 --- --- --- --- 0 | 156 --- --- --- --- 133 --- --- --- --- 156
28E | 9 14 6 10 14 5 13 9 11 12 4 | 22 19 18 23 25 18 18 24 30 20 18
29 | 14 18 7 12 10 4 18 16 10 24 4 | 25 28 22 22 20 18 25 22 23 24 19
X30E | 26 20 11 --- --- 14 13 24 36 --- 9 | 34 33 26 --- --- 22 29 22 45 --- 23
31 | 17 16 6 9 15 6 13 8 12 21 4 | 34 30 27 27 37 27 30 24 30 27 26
32E | 15 18 6 17 12 4 11 18 19 23 5 | 22 29 22 25 21 19 24 21 32 25 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 13 13 4 15 13 12 19 |T 27 26 22 23 27 23 26 22 31 22 25
WRMS | 12 16 6 12 13 4 15 12 11 18 |NE 22 25 22 22 27 19 25 22 30 21 20
MEDI | 11 16 6 12 13 4 14 13 11 18 |MD 22 25 21 21 26 18 24 22 30 20 19
Table 3.1738.6 GPS week: 1738 Day: 6 MJD: 56416.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 11 5 8 8 3 13 8 13 16 3 | 22 24 22 22 27 22 28 20 31 17 20
2 | 11 17 7 8 8 4 17 10 11 29 4 | 29 29 32 32 33 28 28 33 32 30 29
3 | 8 11 5 10 10 3 10 13 6 24 3 | 18 20 19 21 22 19 19 27 27 23 18
4 | 8 12 4 7 11 4 11 16 13 19 3 | 33 34 37 35 41 33 35 41 39 34 35
5E | 8 21 6 9 11 4 23 10 13 11 4 | 22 25 20 21 27 19 28 23 30 21 20
6 | 7 10 5 12 7 3 10 11 8 19 3 | 21 22 20 27 26 23 19 29 34 21 22
7 | 14 19 9 12 13 4 17 15 13 19 5 | 29 26 20 23 31 20 25 22 26 27 20
8 | 6 16 4 6 9 3 13 11 9 14 3 | 26 25 19 23 20 21 26 23 31 23 21
9 | 10 13 3 4 13 3 11 13 7 13 3 | 27 24 22 22 24 22 24 24 28 20 21
10E | 17 20 10 10 12 6 17 19 16 21 5 | 33 45 35 35 44 33 45 39 52 37 37
11 | 10 12 5 10 8 3 11 7 14 17 3 | 44 51 48 51 57 47 48 48 50 43 48
12E | 12 27 5 8 13 4 25 9 12 13 5 | 19 33 22 21 29 21 33 25 31 26 22
13 | 8 18 6 11 17 3 16 15 13 19 4 | 17 23 18 19 33 18 23 21 28 25 16
14 | 8 18 6 9 11 5 17 15 10 22 4 | 26 25 25 27 29 23 24 24 25 31 23
15 | 12 23 7 9 15 3 18 12 8 18 4 | 23 25 23 21 33 20 24 21 31 21 20
16E | 7 20 6 14 10 4 16 9 12 18 4 | 26 26 26 23 28 24 30 26 31 29 23
17 | 15 22 8 13 11 4 20 9 11 24 5 | 30 30 30 31 32 26 30 32 35 22 27
18E | 7 13 5 8 16 4 14 9 14 15 4 | 45 46 47 49 49 47 45 47 44 48 45
19 | 8 15 4 10 11 4 14 7 12 24 3 | 19 22 21 23 27 20 21 23 29 17 20
20E | 8 13 6 11 12 4 15 10 13 19 4 | 20 20 19 19 19 16 21 18 21 28 16
21 | 9 16 6 9 8 4 14 10 15 23 4 | 41 36 40 42 37 40 35 46 43 41 39
22E | 7 13 4 7 12 4 9 10 10 13 3 | 15 18 15 15 21 12 16 16 21 15 12
23 | 9 16 6 14 12 4 17 13 14 25 4 | 33 39 32 34 37 31 36 37 33 39 32
24 | 10 12 4 7 12 2 14 13 13 15 3 | 19 21 16 14 27 15 26 21 25 17 16
25E | 7 12 8 7 11 4 12 11 7 14 3 | 16 21 21 16 23 17 23 19 25 18 16
26 | 13 14 6 5 7 4 9 13 7 11 3 | 25 18 21 23 21 22 21 27 25 21 20
X27E | 6 --- --- --- --- 91 --- --- --- --- 0 | 97 --- --- --- --- 113 --- --- --- --- 99
28E | 7 13 4 6 8 4 11 8 9 9 3 | 38 39 34 37 35 35 37 35 36 38 34
29 | 10 18 6 7 8 5 18 10 11 32 4 | 30 32 32 29 32 29 31 34 36 35 29
X30E | 26 29 8 --- --- 22 --- 29 32 --- 11 | 34 37 28 --- --- 30 --- 27 57 --- 27
31 | 9 14 5 9 15 5 12 6 15 19 4 | 26 28 25 27 37 26 32 25 35 31 26
32E | 13 16 8 8 12 6 13 15 20 18 4 | 25 27 25 28 22 25 24 24 35 27 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 6 9 11 4 15 12 12 19 |T 29 28 26 27 30 28 28 28 33 27 27
WRMS | 10 16 6 9 11 4 15 11 10 17 |NE 26 27 26 27 31 25 27 28 32 26 25
MEDI | 8 16 6 9 11 4 14 11 12 18 |MD 26 26 23 23 29 23 26 25 31 26 22
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1738 GPS week: 1738 MJD: 56410.0-56416.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 |U 7 6 15 |U 7 10 25 |U 8 7 17 |
emr | emr 2950 | 8 7 19 |U 8 10 31 | 9 8 20 |
esa | esa 2976 | 7 5 16 |U 7 9 25 | 8 8 19 |
gfz | gfz 2937 |U 6 5 16 |U 7 9 27 |U 8 7 20 |
grg | grg 2934 |U 9 9 30 |U 11 16 39 | 12 11 28 |
igr | igr 2933 | 7 6 16 | 7 10 25 | 8 8 19 |
igs | igs 2954 | 7 5 16 | 7 10 25 | 8 8 19 |
jpl | jpl 2923 | 8 7 18 |U 9 11 33 |U 11 11 24 |
mit | mit 2976 | 7 6 16 |U 8 11 36 |U 9 7 21 |
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 5.1738.0 GPS week: 1738 Day: 0 MJD: 56410.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 5 3 10 | 6 10 26 | 5 4 14 |
emr | emr 2964 | 7 7 17 | 7 12 30 | 7 7 18 |
esa | esa 2976 | 7 4 14 | 5 8 27 | 6 5 14 |
gfz | gfz 2964 | 6 4 16 | 6 10 28 | 5 4 14 |
grg | grg 2976 | 7 6 32 | 9 22 42 | 9 8 27 |
igr | igr 2976 | 7 3 15 | 6 9 29 | 6 6 14 |
igs | igs 2961 | 6 4 15 | 5 8 27 | 6 5 14 |
jpl | jpl 2964 | 8 5 15 | 9 13 37 | 8 6 19 |
mit | mit 2976 | 7 4 16 | 9 14 53 | 6 5 15 |
Table 5.1738.1 GPS week: 1738 Day: 1 MJD: 56411.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 5 5 16 | 5 13 17 | 9 8 16 |
emr | emr 2964 | 7 8 21 | 8 11 19 | 11 10 20 |
esa | esa 2976 | 7 5 19 | 7 10 21 | 9 8 19 |
gfz | gfz 2964 | 6 5 18 | 7 10 20 | 9 7 19 |
grg | grg 2975 | 10 7 28 | 12 14 26 | 13 9 27 |
igr | igr 2973 | 7 5 18 | 6 12 21 | 9 9 20 |
igs | igs 2973 | 7 5 20 | 7 13 23 | 9 8 19 |
jpl | jpl 2963 | 6 8 19 | 9 13 24 | 16 14 29 |
mit | mit 2976 | 7 6 19 | 8 14 22 | 10 8 19 |
Table 5.1738.2 GPS week: 1738 Day: 2 MJD: 56412.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 8 7 18 | 9 12 32 | 9 10 21 |
emr | emr 2871 | 11 8 21 | 9 11 34 | 11 9 23 |
esa | esa 2976 | 10 8 19 | 9 12 33 | 9 9 24 |
gfz | gfz 2963 | 9 7 21 | 8 9 33 | 8 8 22 |
grg | grg 2974 | 11 11 30 | 10 15 41 | 11 11 29 |
igr | igr 2858 | 9 8 21 | 9 11 34 | 8 8 22 |
igs | igs 2971 | 9 7 19 | 8 10 32 | 9 9 23 |
jpl | jpl 2871 | 10 8 17 | 11 11 34 | 10 10 23 |
mit | mit 2976 | 8 8 18 | 9 11 35 | 9 7 26 |
Table 5.1738.3 GPS week: 1738 Day: 3 MJD: 56413.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 11 11 19 | 7 8 28 | 8 6 18 |
emr | emr 2964 | 9 7 20 | 8 8 50 | 9 8 21 |
esa | esa 2976 | 7 6 17 | 6 8 25 | 8 8 21 |
gfz | gfz 2963 | 8 7 16 | 6 9 24 | 7 7 21 |
grg | grg 2976 | 8 8 26 | 11 17 48 | 11 7 25 |
igr | igr 2880 | 8 6 17 | 6 9 22 | 8 9 21 |
igs | igs 2965 | 6 5 17 | 6 7 22 | 8 7 20 |
jpl | jpl 2872 | 9 7 21 | 7 11 38 | 13 9 25 |
mit | mit 2976 | 8 4 20 | 8 10 64 | 7 5 20 |
Table 5.1738.4 GPS week: 1738 Day: 4 MJD: 56414.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3027 | 7 6 13 | 8 13 25 | 9 7 16 |
emr | emr 2963 | 8 6 15 | 10 8 30 | 10 6 19 |
esa | esa 2976 | 6 5 11 | 8 11 26 | 8 7 18 |
gfz | gfz 2962 | 5 5 11 | 9 10 33 | 9 7 19 |
grg | grg 2879 | 10 7 30 | 10 15 38 | 12 13 30 |
igr | igr 2954 | 6 6 11 | 8 12 26 | 8 8 19 |
igs | igs 2969 | 6 5 11 | 8 12 27 | 8 7 18 |
jpl | jpl 2958 | 7 8 18 | 9 14 34 | 11 10 25 |
mit | mit 2976 | 5 6 11 | 8 12 25 | 8 5 17 |
Table 5.1738.5 GPS week: 1738 Day: 5 MJD: 56415.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | ---- ---- ---- | 7 9 24 | 8 6 19 |
emr | emr 2964 | ---- ---- ---- | 7 12 27 | 9 9 19 |
esa | esa 2976 | ---- ---- ---- | 6 10 22 | 8 8 20 |
gfz | gfz 2874 | ---- ---- ---- | 6 10 24 | 7 7 22 |
grg | grg 2879 | ---- ---- ---- | 13 17 35 | 13 11 29 |
igr | igr 2970 | ---- ---- ---- | 7 10 20 | 9 9 21 |
igs | igs 2969 | ---- ---- ---- | 7 11 24 | 8 8 20 |
jpl | jpl 2964 | ---- ---- ---- | 7 9 30 | 13 11 24 |
mit | mit 2976 | ---- ---- ---- | 6 12 19 | 11 11 28 |
Table 5.1738.6 GPS week: 1738 Day: 6 MJD: 56416.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 5 7 16 | 6 6 21 | 7 9 15 |
emr | emr 2964 | 6 8 19 | 10 7 31 | 8 10 18 |
esa | esa 2976 | 5 6 14 | 7 8 21 | 8 12 20 |
gfz | gfz 2872 | 5 5 16 | 8 9 26 | 8 11 21 |
grg | grg 2880 | 11 13 33 | 12 11 44 | 14 15 31 |
igr | igr 2922 | 5 7 16 | 7 8 21 | 8 9 18 |
igs | igs 2870 | 5 5 18 | 8 8 24 | 7 10 19 |
jpl | jpl 2872 | 7 7 21 | 11 10 32 | 10 15 27 |
mit | mit 2976 | 10 7 15 | 7 8 34 | 8 8 23 |
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 6.1738 GPS week: 1738 MJD: 56410.500-56416.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 31 -21 90 214 2 | 3 9
| 16 16 68 62 5 | 2
emr uuuux | 51 19 117 -28 9 | 29 33
| 18 18 89 92 25 | 6
esa uuuuu | 10 0 -65 191 -3 | 9 13
| 10 14 45 32 3 | 3
gfz uuuuu | 36 38 17 -82 -4 | 10 14
| 23 20 50 75 4 | 4
grg uuuxx | -45 -12 52 -490 12 | 9 16
| 13 8 29 48 26 | 4
igr xxxxx | -40 24 52 -102 3 | -2 7
| 11 11 35 20 3 | 1
irf xxxxx | -8 -7 -25 -131 0 | 0 9
| 6 10 25 32 6 | 2
jpl uuuuu | -11 8 37 -147 0 | 13 18
| 12 21 89 43 13 | 5
mit uuuuu | -29 -1 -88 -266 1 | 17 20
| 17 18 49 55 9 | 2
ngs uuuuu | -52 -22 -30 -203 0 | 5 10
| 42 58 99 92 5 | 2
sio xxxxx | -11 112 -434 -46 3 | 39 41
| 52 34 58 103 3 | 2
Table 7.1738.0 GPS week: 1738 Day: 0 MJD: 56410.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 45 -16 148 240 -2 | 4 8
emr uuuux | 65 26 149 -28 17 | 19 22
esa uuuuu | 22 5 -63 168 -4 | 13 15
gfz uuuuu | 77 74 -83 1 0 | 12 14
grg uuuxx | -35 -20 63 -445 -7 | 3 17
igr xxxxx | -43 25 81 -90 6 | -2 6
irf xxxxx | -4 14 -67 -82 8 | -1 7
jpl uuuuu | -9 40 -118 -175 -21 | 21 27
mit uuuuu | -25 25 -118 -216 11 | 15 17
ngs uuuuu | -136 -118 130 -163 3 | 6 9
sio xxxxx | -81 142 -493 80 1 | 43 46
Table 7.1738.1 GPS week: 1738 Day: 1 MJD: 56411.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 42 -50 191 97 4 | 4 8
emr uuuux | 61 -4 263 27 45 | 22 26
esa uuuuu | 0 7 -133 178 -6 | 13 15
gfz uuuuu | 58 29 -15 25 -10 | 14 15
grg uuuxx | -35 -16 84 -544 2 | 6 14
igr xxxxx | -29 15 28 -122 -2 | -1 6
irf xxxxx | -11 -12 -23 -132 4 | 1 8
jpl uuuuu | -10 26 -47 -176 4 | 18 24
mit uuuuu | -40 -5 -53 -261 9 | 17 20
ngs uuuuu | -61 8 -11 -136 -2 | 7 10
sio xxxxx | -42 143 -454 -31 6 | 42 45
Table 7.1738.2 GPS week: 1738 Day: 2 MJD: 56412.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 28 -14 88 188 -1 | 3 8
emr uuuux | 81 12 163 96 26 | 26 31
esa uuuuu | 6 16 -84 193 -3 | 10 12
gfz uuuuu | 27 15 41 -143 -3 | 11 14
grg uuuxx | -56 -8 -3 -529 -9 | 7 14
igr xxxxx | -28 9 43 -99 3 | -3 7
irf xxxxx | -11 -8 4 -107 7 | 0 8
jpl uuuuu | 3 -5 97 -135 11 | 14 19
mit uuuuu | -60 -19 -2 -181 11 | 17 19
ngs uuuuu | -24 -18 -124 -248 -1 | 5 9
sio xxxxx | 42 80 -356 15 7 | 39 41
Table 7.1738.3 GPS week: 1738 Day: 3 MJD: 56413.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 31 -3 77 249 11 | 3 8
emr uuuux | 38 35 75 16 10 | 30 35
esa uuuuu | -2 -3 -67 180 -4 | 9 11
gfz uuuuu | 29 31 59 -158 -4 | 11 13
grg uuuxx | -49 -20 72 -549 -2 | 8 14
igr xxxxx | -31 31 66 -112 3 | -2 7
irf xxxxx | -17 -4 -41 -151 -3 | 1 8
jpl uuuuu | 1 9 51 -173 -11 | 12 16
mit uuuuu | -34 21 -130 -312 -3 | 17 20
ngs uuuuu | -16 -50 12 -174 -6 | 6 9
sio xxxxx | 34 72 -474 -111 2 | 36 37
Table 7.1738.4 GPS week: 1738 Day: 4 MJD: 56414.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 49 -26 21 239 1 | 5 9
emr uuuux | 43 40 -8 -106 10 | 35 37
esa uuuuu | 10 -22 18 152 2 | 9 11
gfz uuuuu | 30 38 29 -132 -8 | 11 13
grg uuuxx | -61 -6 29 -447 38 | 9 14
igr xxxxx | -52 41 84 -116 4 | -1 6
irf xxxxx | 1 -15 -16 -175 -3 | 2 7
jpl uuuuu | -31 -19 98 -66 -4 | 11 15
mit uuuuu | -8 -24 -111 -342 -3 | 19 21
ngs uuuuu | -61 53 -105 -118 4 | 6 9
sio xxxxx | -7 122 -392 -182 -1 | 38 39
Table 7.1738.5 GPS week: 1738 Day: 5 MJD: 56415.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -29 -4 291 -4 | 5 10
emr uuuux | 34 27 41 -17 -20 | 37 38
esa uuuuu | 24 13 -76 250 -6 | 8 11
gfz uuuuu | 16 56 38 -123 0 | 8 13
grg uuuxx | -55 2 63 -466 60 | 12 17
igr xxxxx | -43 19 75 -112 5 | -1 7
irf xxxxx | -8 -12 2 -113 -5 | 1 8
jpl uuuuu | -13 -12 128 -181 8 | 9 14
mit uuuuu | -24 -1 -67 -264 -7 | 19 21
ngs uuuuu | -15 -55 33 -389 6 | 6 9
Table 7.1738.6 GPS week: 1738 Day: 6 MJD: 56416.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 24 -8 109 193 4 | 0 15
emr uuuux | 38 -3 136 -184 -25 | 32 38
esa uuuuu | 13 -15 -48 213 -1 | 3 15
gfz uuuuu | 15 24 49 -43 -4 | 3 15
grg uuuxx | -26 -13 56 -450 3 | 15 20
igr xxxxx | -53 29 -11 -65 -1 | -5 13
irf xxxxx | -7 -8 -37 -154 -4 | -3 16
jpl uuuuu | -18 17 50 -122 13 | 4 14
mit uuuuu | -13 -6 -133 -283 -8 | 14 22
ngs uuuuu | -53 24 -144 -194 -6 | 2 12
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