[IGSREPORT-21767] Wk 1735 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Apr 26 09:09:33 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1735 (Apr 07, 2013 - Apr 13, 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:
igs1735[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1735[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1735[0-6].cls IGS GPS clock combination summary report.
igs17357.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17357.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 | COD | FLRS
0 | EMR | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
0 | EMR | 21 22 23 24 25 26 28 29 30 31 32 ALGO AREQ DRAO KOKB
0 | EMR | MCM4 MDO1 MIZU NNOR SCH2 STR1 SYOG THU3 WHIT WSRT
0 | EMR | YELL ALBH ALGO AREQ CRO1 DRAO FAIR IRKT JPLM KERG
0 | EMR | KOKB MCM4 MDO1 MIZU NNOR NRC1 PIE1 QAQ1 SCH2 STJO
0 | EMR | STR1 SYOG THU3 USN3 WHIT WSRT YELL
0 | ESA | UNSA
0 | GFZ | KOUR
0 | GRG | HYDE HYDE NOT1
0 | MIT | 30 30
1 | COD | KOUC WROC KOUC WROC
1 | EMR | WUHN
1 | ESA | MAR6 KOUR MAR6
1 | GRG | 5 5 NTUS YELL KOUR LHAZ NOVM NRMD
1 | MIT | 30 30 WROC HYDE KOSG NTUS WROC
2 | COD | KOUC KOUC
2 | ESA | HERS KOUR KOUR MAL2
2 | GFZ | SUTH
2 | GRG | NYAL KOUC NYAL TIXI TRO1
2 | MIT | 28 30 28 30 HYDE WROC HYDE NTUS WROC
3 | COD | KOUC KOUC TLSE
3 | EMR | YELL MCM4 WUHN YELL
3 | ESA | SCUB SCUB UNSA
3 | GFZ | LHAZ WSRT
3 | GRG | MDVJ NICO NTUS MAL2 MDVJ NICO NTUS SCUB TLSE WIND
3 | MIT | 30 30 WROC WROC
4 | COD | 9 9 KOUC
4 | EMR | MATE
4 | ESA | MAL2 MATE SCUB UNSA
4 | GFZ | LHAZ SCUB
4 | GRG | CAS1 HYDE MCM4 CAS1 HYDE
4 | JPL | 10 CAS1 MATE NAMA
4 | MIT | 9 30 9 10 30 NYAL DARW
5 | COD | 10 10 TSKB
5 | EMR | WUHN
5 | ESA | 10 10 NTUS NTUS UNSA
5 | GFZ | 10 21 WSRT
5 | GRG | ARTU NICO NTUS POLV REUN
5 | JPL | NAMA
5 | MIT | 30 30 HYDE NICO HYDE
6 | COD | 10 10 KOUC KOUC
6 | EMR | WUHN
6 | ESA | 10 21 10 21 NTUS UNSA
6 | GFZ | 10 OPMT
6 | GRG | NICO LHAZ NICO
6 | MIT | 30 30 CAS1 CAS1 HYDE
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. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G08 | 2013_04_12 | 2013026
7. 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 | COD | 9
3 | GRG | 9
8. 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 G09 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G27 | | | | | | | 4 |
9. 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.
10. 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 | -.8 .8 -2.1 -50 18 -10 .24
EMR | 0 | 1.7 -3.7 6.0 11 -5 9 .20
ESA | 0 | .9 5.0 16.3 46 -87 57 .22
GFZ | 0 | -.3 .5 -.7 -25 -21 2 .09
GRG | 0 | -3.1 -2.5 12.0 -15 9 13 .49
JPL | 0 | 3.3 -2.8 16.7 -79 -22 2 .39
MIT | 0 | .6 -.5 16.9 -6 -4 -26 .23
NGS | 0 | 1.3 -3.9 16.6 -113 -30 5 .71
SIO | 0 | -3.3 1.6 -65.4 -70 -312 -172 .26
COD | 1 | -.9 1.3 -1.9 -53 -2 3 .29
EMR | 1 | 6.0 -.9 8.0 7 2 13 .33
ESA | 1 | 2.1 4.1 14.1 45 -68 52 .51
GFZ | 1 | .1 .7 -.6 -36 -22 13 .14
GRG | 1 | -1.0 2.5 5.5 -20 9 17 .52
JPL | 1 | 2.9 2.7 6.3 -66 -18 13 .56
MIT | 1 | 3.0 1.1 16.4 -8 -1 -21 .27
NGS | 1 | -2.6 -5.3 4.3 -76 12 -30 .87
SIO | 1 | -3.3 3.1 -71.5 -55 -327 -241 .35
COD | 2 | -.3 .9 -.7 -48 -8 -6 .18
EMR | 2 | 4.0 -2.2 8.8 10 0 12 .43
ESA | 2 | 2.4 6.2 20.8 54 -85 72 .36
GFZ | 2 | -.5 .4 -.6 -31 -26 3 .14
GRG | 2 | -.8 -1.3 19.4 -15 16 -54 .32
JPL | 2 | 7.8 2.7 13.8 -86 23 -22 .48
MIT | 2 | 3.5 -2.8 18.5 -9 -4 -21 .16
NGS | 2 | 2.7 -.1 19.3 -107 -52 31 .71
SIO | 2 | 2.9 1.5 -79.5 -52 -491 -236 .45
COD | 3 | -1.6 .9 -1.6 -57 13 46 .19
EMR | 3 | 4.6 -.4 10.4 12 -1 8 .32
ESA | 3 | 1.5 -1.7 10.6 21 -26 -14 .21
GFZ | 3 | -.7 .8 -.5 -37 -14 -3 -.02
GRG | 3 | 6.8 -7.2 23.7 -25 9 -52 .64
JPL | 3 | 5.3 -3.0 9.9 -24 46 -53 .43
MIT | 3 | 5.6 -2.6 16.5 -11 -1 -21 .21
NGS | 3 | 3.9 -3.3 4.7 -62 -29 34 .71
SIO | 3 | 2.3 1.4 -63.9 -95 -510 37 .32
COD | 4 | -1.5 .7 -1.1 -54 11 -14 -.04
EMR | 4 | -.4 -6.9 12.5 11 -4 10 .36
ESA | 4 | 2.2 -2.1 21.8 37 -31 -5 .20
GFZ | 4 | -.6 .8 -.8 -41 -13 -6 -.11
GRG | 4 | .6 -1.5 25.1 -22 2 -20 .39
JPL | 4 | 8.4 -3.1 15.0 -53 10 -12 .71
MIT | 4 | 4.5 -5.1 16.4 -15 1 -20 .03
NGS | 4 | 1.0 -4.8 9.6 -101 -22 12 .79
SIO | 4 | -.6 -.2 -81.2 -135 -496 -124 .16
COD | 5 | -.7 1.3 -1.3 -45 -12 2 .15
EMR | 5 | 3.5 -8.4 9.4 1 1 10 .32
ESA | 5 | 3.4 3.4 18.4 63 -39 9 .33
GFZ | 5 | -.5 .7 -.4 -37 -22 -5 -.26
GRG | 5 | 5.0 -2.7 22.5 -13 -17 6 .47
JPL | 5 | 3.5 -3.2 21.5 -28 -55 3 .11
MIT | 5 | 5.1 1.2 14.5 -2 2 -11 .15
NGS | 5 | 5.1 3.7 11.2 -47 -66 69 .52
SIO | 5 | .8 1.9 -55.2 -95 -394 -18 .10
COD | 6 | -.9 1.1 -1.4 -49 12 -7 .12
EMR | 6 | 3.0 -11.7 13.2 -3 -2 19 .37
ESA | 6 | 4.2 1.1 23.8 56 -38 6 .25
GFZ | 6 | -.3 .5 -.1 -28 -16 -6 -.32
GRG | 6 | 6.1 1.5 21.7 -35 14 -16 .35
JPL | 6 | 10.1 -.2 15.8 -26 36 37 .47
MIT | 6 | 2.4 -1.7 16.6 2 -5 -10 .16
NGS | 6 | 1.9 -2.8 15.2 -117 -22 4 .74
SIO | 6 | .7 -.9 -51.4 -89 -388 50 .30
11. 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.
12. 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 1.1735.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1735.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 2.1735.[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 3.1735.[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 5.1735.0-6). 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 1735 summary. (Apr 07, 2013 - Apr 13, 2013)
Table 1.1735.a GPS week: 1735 MJD: 56389.000-56395.000
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 265| 0 0 1 27 -20 14 -.41 10 10 | -412 -740 24 88
| 0 0 1 15 21 13 .04 | 496 1044
emr 80| 0 0 -1 -34 -8 -15 .27 14 14 | 4467 -319 11 76
| 0 2 2 15 19 9 .03 | 854 783
esa 150| 0 0 3 21 11 9 .13 7 6 | -1473 964 35 148
| 0 0 2 17 10 14 .06 | 542 1067
gfz 201| 0 0 -3 -48 -58 15 -.35 10 9 | 185 -327 20 97
| 1 0 1 47 50 10 .03 | 210 453
grg 134| 2 1 8 -9 7 -9 .58 16 15 | 114 -167 17 134
| 1 0 2 16 18 22 .05 | 250 369
igr n/a| 0 0 -2 13 45 -20 -.12 4 4 | 2723 -308 19 88
| 0 0 0 16 17 7 .02 | 933 775
jpl 80| -1 1 -9 -13 -8 0 .34 15 15 | 4401 -211 18 116
| 2 2 3 26 16 11 .03 | 991 823
mit 239| 0 -1 1 21 15 -3 -.54 11 10 | 551 -2567 24 193
| 1 0 1 21 14 12 .05 | 955 3741
ngs 243| -1 0 -2 7 60 -20 .37 11 9 | -893 238 1764 3530
| 0 0 4 25 45 31 .05 | 801 1756
sio 290| 1 3 0 -98 -324 -72 -.30 19 18 | --- --- --- ---
| 0 0 1 37 211 105 .04 | --- ---
Table 1.1735.b GPS week : 1735 MJD: 56389.000-56395.000
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 4 4 4 |
2 | 5 5 5 6 5 5 5 |
3 | 4 4 3 4 4 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 4 4 5 5 4 5 5 |
6 | 4 3 4 3 3 3 3 |
7 | 5 5 5 5 4 4 4 |
8 | 4 4 4 4 5 0 4 |
9 | 4 4 4 0 3 4 4 |
10 | 4 4 5 6 6 6 5 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 6 5 5 5 |
13 | 4 4 4 4 5 5 4 |
14 | 4 4 5 4 4 4 5 |
15 | 6 5 6 6 5 5 5 |
16 | 4 4 4 4 4 4 4 |
17 | 5 4 5 6 5 5 5 |
18 | 4 5 4 4 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 4 5 5 4 4 4 4 |
21 | 4 4 4 5 4 5 5 |
22 | 4 4 4 4 3 4 3 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 4 4 5 4 |
25 | 4 4 4 4 5 4 4 |
26 | 3 3 3 5 3 4 3 |
27 | 0 0 0 0 0 0 0 |
28 | 4 4 4 5 4 5 4 |
29 | 4 4 4 5 5 4 5 |
30 | 5 5 4 5 5 7 8 |
31 | 5 4 4 5 4 4 4 |
32 | 4 4 4 4 4 4 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
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 2.1735.0 GPS week: 1735 Day: 0 MJD: 56389.000
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| 0 0 0 11 -25 2 -.47 8 9 | -899 -1680 24 88
emr 80| 0 0 -4 -42 -38 -11 .27 14 14 | 3134 1038 0 0
esa 150| 0 0 1 15 16 1 .08 6 6 | -1403 142 33 152
gfz 200| 0 0 -1 23 -32 0 -.35 11 10 | 138 -481 21 101
grg 135| 0 0 5 -10 3 9 .62 14 14 | -120 -120 18 124
igr n/a| 0 0 -2 -2 20 -26 -.15 4 4 | 1077 955 19 83
jpl 80| 0 0 -10 -51 -16 -19 .32 14 15 | 2387 952 19 113
mit 240| 0 -1 2 42 15 15 -.58 12 12 | -434 -965 18 184
ngs 245| -1 0 4 -20 64 7 .37 11 10 | -536 -905 1722 3200
sio 278| 0 4 1 -98 -323 -155 -.31 20 18 | --- --- --- ---
Table 2.1735.1 GPS week: 1735 Day: 1 MJD: 56390.000
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 -1 3 47 19 6 -.42 10 11 | 164 -2279 24 90
emr 80| 1 1 -2 -45 -10 -31 .28 14 14 | 5605 238 12 79
esa 150| 0 1 1 10 -5 5 .08 6 5 | -1332 -466 30 142
gfz 202| 0 0 -3 6 -10 16 -.38 10 10 | 172 -108 19 90
grg 135| 0 1 2 0 23 5 .61 16 15 | 367 -364 14 110
igr n/a| 0 0 -2 4 45 -29 -.12 4 4 | 3594 166 18 79
jpl 80| 3 0 -3 -25 -27 11 .37 14 14 | 4853 300 15 100
mit 239| -1 -1 3 -4 9 9 -.58 10 10 | 45 -876 25 193
ngs 243| -2 0 -4 -18 23 -35 .39 12 10 | 320 -1690 2016 3894
sio 273| 0 3 3 -113 -330 -244 -.32 20 18 | --- --- --- ---
Table 2.1735.2 GPS week: 1735 Day: 2 MJD: 56391.000
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 0 0 8 -26 17 -.42 10 10 | 207 -747 21 87
emr 80| 0 0 -3 -24 -10 -9 .27 15 15 | 5023 -172 12 84
esa 150| 0 1 4 25 18 10 .12 7 7 | -2572 2509 40 148
gfz 200| -1 0 -5 -41 -43 29 -.38 10 9 | -169 190 21 98
grg 134| 4 1 11 -15 33 -49 .63 15 14 | -254 61 16 136
igr n/a| 0 0 -4 1 42 -9 -.10 5 5 | 3264 52 20 97
jpl 80| -3 0 -10 -31 2 2 .34 16 16 | 4549 294 17 112
mit 240| 1 -2 1 16 27 0 -.53 10 10 | 874 -1343 24 198
ngs 243| 0 0 0 27 4 -11 .39 11 10 | -1040 833 1849 3512
sio 269| 2 3 0 -26 126 -22 -.25 19 18 | --- --- --- ---
Table 2.1735.3 GPS week: 1735 Day: 3 MJD: 56392.000
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| 1 0 2 37 -13 43 -.34 14 14 | -1021 453 28 80
emr 80| 1 1 0 -33 24 -5 .21 13 13 | 4923 -1289 11 83
esa 150| 0 0 0 32 27 36 .25 8 8 | -1716 1226 22 134
gfz 200| -2 0 -1 -102 -152 20 -.39 11 10 | 393 -174 20 84
grg 136| 1 2 10 -41 -20 -17 .54 16 15 | 245 -234 20 148
igr n/a| 0 0 -1 7 70 -18 -.14 5 5 | 3399 -1030 22 81
jpl 80| 0 0 -6 13 17 9 .28 14 14 | 4983 -709 17 135
mit 240| 0 -1 3 19 -7 -8 -.59 10 9 | 1157 -3734 26 201
ngs 244| 0 0 -5 43 102 -72 .27 11 9 | -1724 3013 1873 3994
sio 304| 0 3 2 -116 -512 34 -.38 19 16 | --- --- --- ---
Table 2.1735.4 GPS week: 1735 Day: 4 MJD: 56393.000
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 267| 0 0 0 23 -20 11 -.43 10 10 | -144 615 24 91
emr 80| 1 -1 1 -20 -1 -28 .29 15 15 | 3987 -629 13 103
esa 150| 0 1 6 24 6 2 .13 6 6 | -1193 803 40 172
gfz 203| 0 0 -4 -66 -99 27 -.29 9 8 | 412 -940 22 102
grg 135| 2 1 9 12 -10 -18 .63 16 15 | 360 -679 14 139
igr n/a| 0 0 -3 24 57 -12 -.09 5 4 | 2749 -312 18 119
jpl 80| -3 4 -12 -12 -20 -10 .35 17 17 | 4516 -99 19 117
mit 240| 1 -2 0 14 35 -11 -.46 11 9 | 1832 -1514 27 191
ngs 245| 0 -1 -4 16 124 -4 .40 11 10 | -2062 2033 1755 2964
sio 301| 1 2 0 -149 -479 -129 -.28 19 19 | --- --- --- ---
Table 2.1735.5 GPS week: 1735 Day: 5 MJD: 56394.000
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| 0 1 4 41 -25 13 -.39 10 10 | -506 -904 28 85
emr 80| 0 -3 0 -58 -1 -16 .27 14 14 | 4803 -423 17 89
esa 150| 0 0 4 -5 14 20 .15 7 7 | -1185 2120 36 142
gfz 202| -1 0 -4 -71 -55 10 -.34 10 9 | 29 103 20 97
grg 135| 1 2 9 -3 13 15 .53 17 18 | -48 491 20 133
igr n/a| 0 0 -2 17 26 -22 -.12 4 4 | 3160 -684 20 83
jpl 80| -1 2 -9 -8 4 4 .39 16 15 | 5467 -704 22 127
mit 240| 2 -2 1 56 24 -7 -.51 10 9 | 1160 -10468 31 217
ngs 241| 0 0 -7 19 20 -44 .41 11 9 | -527 -926 1610 3543
sio 303| 1 2 1 -84 -386 -15 -.31 18 18 | --- --- --- ---
Table 2.1735.6 GPS week: 1735 Day: 6 MJD: 56395.000
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 0 1 20 -51 4 -.39 10 9 | -686 -640 24 97
emr 80| 1 -4 -3 -14 -19 -9 .31 15 15 | 3800 -998 13 99
esa 150| 0 1 4 50 3 -8 .12 6 6 | -916 417 44 148
gfz 204| 0 0 -5 -87 -19 5 -.33 9 8 | 322 -885 19 112
grg 134| 3 2 8 -11 12 -11 .53 17 16 | 251 -329 17 148
igr n/a| 0 0 -3 43 55 -26 -.12 4 4 | 1819 -1304 19 75
jpl 80| -2 0 -10 25 -17 5 .34 16 15 | 4052 -1513 19 109
mit 240| 1 -1 0 5 6 -21 -.53 12 10 | -777 925 21 172
ngs 243| 0 0 0 -17 82 16 .36 10 8 | -688 -686 1524 3605
sio 302| 1 3 -1 -97 -366 27 -.27 19 18 | --- --- --- ---
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 3.1735.0 GPS week: 1735 Day: 0 MJD: 56389.000
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 10 6 10 12 3 15 8 12 14 3 | 30 33 27 27 32 27 36 29 32 27 28
2 | 10 19 8 14 15 5 20 12 9 22 5 | 16 24 16 18 23 12 24 11 16 18 13
3 | 8 7 6 11 14 3 10 12 13 17 3 | 27 32 29 27 33 27 29 27 29 27 28
4 | 7 14 5 8 8 5 11 12 10 12 3 | 14 24 17 13 20 14 21 13 18 18 15
5 | 8 19 6 8 17 5 17 10 9 18 4 | 29 30 25 26 34 26 29 30 30 22 25
6 | 7 7 6 11 11 4 9 12 13 24 3 | 20 26 28 21 29 22 25 25 25 28 23
7 | 7 13 6 10 16 5 12 18 13 15 4 | 15 21 15 15 30 12 21 22 22 20 15
8 | 8 12 6 8 13 4 14 17 9 13 4 | 15 21 11 12 12 8 20 18 13 13 10
9 | 8 12 7 11 14 3 11 12 10 18 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
10 | 7 11 7 11 8 3 13 9 8 19 3 | 52 51 52 47 49 52 54 53 52 48 50
11 | 7 13 4 8 18 5 12 9 12 14 3 | 38 44 39 39 52 36 40 36 38 38 38
12 | 10 17 7 8 19 4 22 12 11 16 4 | 18 22 15 13 28 11 23 18 21 14 14
13 | 8 16 7 15 13 4 14 13 8 20 4 | 20 33 26 28 33 25 31 27 25 34 24
14 | 8 13 6 15 13 5 13 14 12 25 4 | 30 35 34 41 36 33 35 37 34 33 34
15 | 21 18 8 8 14 6 16 16 12 31 5 | 22 28 23 20 30 20 26 21 25 25 21
16 | 4 14 7 11 14 3 19 10 7 20 4 | 13 23 20 20 29 16 25 13 21 17 18
17 | 10 19 8 14 11 3 16 13 14 26 4 | 23 28 23 23 29 18 25 27 19 22 21
18 | 5 21 6 12 16 5 13 11 10 21 4 | 25 29 25 32 26 24 23 26 26 20 24
19 | 7 11 8 10 14 5 13 10 13 31 4 | 16 23 21 16 23 15 18 15 19 20 16
20E | 5 13 7 12 16 5 14 13 11 13 4 | 15 24 20 18 25 18 17 19 25 18 18
21 | 6 12 5 10 17 3 16 10 8 20 3 | 10 19 11 13 28 9 19 15 15 20 10
22 | 5 13 5 10 14 3 13 10 11 20 3 | 27 29 28 32 34 27 27 30 30 22 27
23 | 6 14 5 17 11 3 12 16 8 30 4 | 18 29 23 29 27 22 27 24 23 36 22
24 | 11 13 6 11 15 5 12 12 9 10 4 | 25 28 23 24 30 22 29 26 23 24 23
25 | 9 14 5 12 12 4 11 12 7 10 3 | 11 26 18 17 28 13 24 15 19 15 15
26 | 6 8 6 7 13 4 9 7 8 10 3 | 24 26 25 24 28 25 28 25 24 27 24
X27 | 7 --- --- --- --- 65 --- --- --- --- 0 | 40 --- --- --- --- 47 --- --- --- --- 41
28 | 8 12 5 13 19 4 16 8 10 12 4 | 12 21 12 17 30 11 21 17 17 12 13
29 | 8 16 6 11 15 5 19 12 7 39 4 | 30 35 31 29 34 27 33 30 31 36 29
X30 | 9 13 8 15 14 14 --- 9 17 --- 5 | 15 26 18 20 23 20 --- 16 21 --- 17
31 | 9 15 7 13 18 2 13 9 14 14 4 | 14 24 15 19 33 14 21 16 20 15 16
32 | 10 12 6 14 12 6 14 12 11 20 4 | 13 22 19 16 20 13 21 11 24 24 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 6 11 14 4 14 12 11 20 |T 21 27 22 23 29 21 26 23 24 23 22
WRMS | 9 14 6 10 14 4 15 12 10 18 |NE 16 26 19 19 28 16 24 18 20 22 17
MEDI | 8 13 6 11 14 4 13 12 10 18 |MD 20 26 23 20 29 20 25 22 23 22 21
Table 3.1735.1 GPS week: 1735 Day: 1 MJD: 56390.000
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 11 6 10 13 4 12 7 12 15 3 | 23 27 24 21 30 22 32 21 34 21 23
2 | 9 21 7 12 14 5 18 10 9 21 4 | 12 24 15 13 22 8 21 10 17 16 12
3 | 10 8 5 10 16 4 9 10 12 19 3 | 33 33 34 31 33 32 35 31 34 33 31
4 | 9 15 5 8 10 4 11 7 13 13 3 | 13 22 15 10 20 11 17 10 22 17 14
5 | 7 17 5 6 20 4 20 10 9 17 4 | 29 34 28 32 39 29 31 29 35 29 29
6 | 8 7 4 11 12 4 9 7 12 24 3 | 26 30 26 25 31 24 29 25 29 26 26
7 | 11 13 7 11 18 5 13 17 9 12 4 | 17 20 15 15 29 12 22 20 21 19 15
8 | 8 11 6 6 12 3 12 14 9 14 3 | 15 18 10 12 12 9 20 15 16 15 11
9 | 9 11 6 9 15 3 12 8 12 19 3 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
10 | 9 10 7 12 11 3 11 8 7 18 3 | 48 53 50 50 49 50 50 52 51 48 50
11 | 15 12 5 11 19 4 9 8 16 17 4 | 29 32 27 26 39 24 31 26 23 31 26
12 | 12 18 6 7 21 4 23 11 12 15 5 | 16 22 14 10 26 10 23 16 23 13 13
13 | 11 15 5 10 16 5 12 11 12 17 4 | 18 27 18 18 32 18 28 19 24 25 19
14 | 7 15 7 15 14 4 15 9 11 23 4 | 23 33 30 34 33 27 32 28 30 27 29
15 | 17 19 6 9 15 4 17 11 15 27 5 | 15 27 16 17 29 16 25 16 24 19 16
16 | 9 13 6 10 14 3 17 10 10 24 4 | 10 19 12 10 25 9 18 10 20 13 11
17 | 11 18 6 11 9 3 16 9 11 24 4 | 13 25 16 17 22 13 25 18 21 14 15
18 | 8 18 4 13 19 4 16 10 12 22 4 | 19 25 19 24 24 19 23 17 22 18 19
19 | 15 13 7 11 15 2 13 9 11 30 4 | 18 21 16 17 23 14 19 16 22 18 16
20E | 10 12 6 11 19 3 10 15 14 14 4 | 16 22 19 16 24 16 19 19 27 16 17
21 | 7 15 5 10 16 5 14 10 11 20 4 | 7 18 8 12 26 6 20 12 15 16 9
22 | 8 11 6 11 18 2 13 11 14 21 4 | 19 26 19 22 28 20 25 19 23 22 20
23 | 12 14 5 10 15 4 12 12 11 28 4 | 19 23 18 18 27 17 24 18 23 31 18
24 | 9 13 5 10 16 5 11 11 15 12 4 | 22 26 21 22 29 20 28 23 30 21 21
25 | 8 16 5 10 12 5 10 9 9 8 3 | 11 25 15 12 25 11 23 13 19 14 14
26 | 9 8 4 7 10 3 8 7 7 12 2 | 18 20 19 19 24 18 22 18 22 17 18
X27 | 7 --- --- --- --- 56 --- --- --- --- 0 | 60 --- --- --- --- 26 --- --- --- --- 61
28 | 8 14 5 10 18 4 12 9 10 14 3 | 15 21 14 16 29 14 23 15 19 13 14
29 | 13 15 6 7 15 6 19 10 11 35 4 | 24 24 20 18 23 17 25 17 27 29 19
X30 | 12 11 5 14 14 6 --- 10 18 --- 4 | 18 23 13 17 22 16 --- 16 24 --- 17
31 | 11 12 7 12 19 4 11 10 15 15 4 | 15 22 15 19 36 14 21 16 24 14 16
32 | 11 15 6 10 16 4 9 10 15 20 4 | 12 25 17 13 22 11 21 11 22 23 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 6 10 16 4 14 10 12 20 |T 20 25 19 19 27 17 25 19 24 21 20
WRMS | 11 14 5 10 15 4 14 10 10 18 |NE 15 23 15 14 26 12 22 14 21 19 14
MEDI | 9 13 6 10 15 4 12 10 12 18 |MD 18 24 17 17 26 16 23 17 23 19 17
Table 3.1735.2 GPS week: 1735 Day: 2 MJD: 56391.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 6 8 11 4 16 8 12 14 3 | 22 26 21 18 25 20 30 22 22 20 20
2 | 9 17 7 12 15 3 24 10 11 20 4 | 14 21 13 17 22 10 25 13 21 14 12
3 | 7 9 4 10 14 3 12 9 7 16 3 | 18 21 21 16 25 17 21 14 24 16 18
4 | 9 14 5 7 14 3 13 7 9 9 3 | 17 22 17 15 20 15 23 10 23 11 15
5E | 8 20 5 10 15 8 17 14 11 14 4 | 33 35 32 37 35 31 36 43 37 34 33
6 | 7 10 6 12 13 4 10 7 9 20 3 | 21 29 24 24 29 21 26 15 27 12 23
7 | 7 12 6 9 19 3 14 14 13 12 4 | 13 18 12 15 30 11 22 15 23 15 12
8 | 7 11 8 7 14 5 14 14 10 16 4 | 13 16 12 10 14 11 22 12 22 11 10
9 | 6 13 5 9 14 4 14 7 8 19 3 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
10 | 10 14 8 10 12 9 18 11 15 20 4 | 57 60 60 63 55 56 60 57 52 53 57
11 | 10 14 6 11 17 5 12 8 9 16 4 | 31 34 33 30 42 29 32 28 33 32 30
12 | 10 20 6 6 23 3 28 12 9 16 5 | 15 23 16 11 30 11 26 16 22 11 13
13 | 9 16 7 8 14 6 15 9 10 15 4 | 18 29 20 21 31 20 31 21 21 23 19
14 | 14 17 7 11 10 5 17 13 14 24 4 | 26 27 23 29 28 24 28 24 23 25 23
15 | 20 22 8 8 15 3 18 14 13 28 5 | 27 26 18 19 29 16 26 20 24 21 18
16 | 5 16 7 10 15 5 19 9 10 21 4 | 12 22 16 15 27 12 22 11 17 13 13
17 | 15 17 8 12 10 5 19 12 12 25 5 | 20 24 19 19 25 12 22 21 21 18 15
18E | 8 18 5 13 12 6 17 9 11 17 4 | 27 27 25 30 23 25 28 28 29 24 24
19 | 8 14 7 10 13 3 14 9 10 29 3 | 17 22 19 20 21 15 24 15 22 16 17
20E | 8 9 8 9 23 4 14 12 13 10 4 | 17 19 18 14 23 16 21 18 26 17 16
21 | 6 15 7 12 13 7 18 6 10 20 4 | 13 19 14 13 27 10 23 14 21 15 12
22E | 11 14 6 10 9 5 13 12 11 19 4 | 29 27 27 30 28 28 28 28 33 24 26
23 | 8 13 7 10 14 4 13 11 9 29 4 | 18 25 20 23 24 19 26 20 24 29 19
24 | 10 12 4 8 16 3 14 10 9 9 3 | 19 26 23 20 30 18 27 17 28 18 20
25 | 10 14 7 9 16 6 11 11 8 9 4 | 12 22 17 13 28 11 23 13 19 12 13
26 | 6 10 6 7 11 4 10 8 8 11 3 | 26 28 26 23 32 25 29 25 28 29 25
X27 | 6 --- --- --- --- 69 --- --- --- --- 0 | 48 --- --- --- --- 40 --- --- --- --- 47
28 | 8 13 7 9 19 5 17 7 8 12 4 | 13 18 14 14 28 10 23 15 20 11 12
29 | 11 17 7 8 11 5 20 10 11 32 4 | 24 27 24 23 27 20 28 21 27 29 22
X30 | 11 15 5 8 11 8 --- 10 14 --- 4 | 18 28 14 18 18 13 --- 17 20 --- 17
31 | 8 12 7 8 19 4 15 8 13 14 4 | 15 24 15 16 36 14 24 14 25 10 16
32 | 12 13 8 11 15 5 11 11 11 17 4 | 16 24 19 13 21 14 23 11 26 21 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 7 10 15 5 16 10 11 19 |T 21 25 21 20 27 19 26 19 25 20 20
WRMS | 10 15 7 9 14 5 16 10 10 18 |NE 16 23 17 16 27 14 25 15 22 17 15
MEDI | 8 14 7 9 14 5 14 10 10 16 |MD 18 24 19 18 27 16 26 17 23 18 18
Table 3.1735.3 GPS week: 1735 Day: 3 MJD: 56392.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1M | 11 9 6 9 13 3 16 7 9 12 3 | 37 35 32 34 37 33 40 33 42 33 33
2 | 12 18 12 16 15 6 19 14 12 19 5 | 15 21 22 18 21 12 22 18 19 15 13
3M | 10 8 4 10 14 3 9 6 11 14 3 | 24 25 24 26 25 23 25 22 29 21 23
4 | 15 12 8 10 14 5 10 10 7 11 4 | 19 20 18 14 19 13 18 14 21 11 13
5E | 13 18 8 12 17 7 20 9 11 11 5 | 26 28 24 27 25 23 29 24 26 21 22
6M | 7 8 6 8 11 4 8 6 8 17 3 | 29 30 33 30 33 29 32 25 31 22 28
7M | 13 13 10 11 19 4 11 10 13 10 4 | 18 20 18 18 28 13 22 15 23 15 13
8M | 14 12 9 7 11 5 12 9 7 16 3 | 20 18 18 11 13 13 20 15 20 12 12
X9M | 474 --- 5 --- 551 178 --- --- --- --- 0 | 9999 --- 9999 --- 9999 9999 --- --- --- --- 9999
10E | 15 15 12 19 20 5 14 23 7 31 6 | 78 74 71 69 72 72 76 79 76 83 72
11M | 9 10 6 9 21 6 10 7 8 16 3 | 30 36 30 33 43 31 37 31 31 32 30
12 | 16 16 9 9 20 5 25 12 14 15 5 | 25 22 17 14 26 18 24 19 29 14 15
13 | 14 14 8 9 16 4 12 6 10 16 4 | 23 30 30 24 32 24 33 24 30 27 24
14M | 8 14 8 11 13 6 14 9 15 21 4 | 28 30 36 34 35 30 33 31 37 28 31
15M | 29 20 7 11 17 8 19 7 14 30 5 | 32 27 27 21 30 25 26 20 34 26 22
16M | 9 13 7 9 16 5 17 9 10 17 4 | 16 22 18 16 24 17 23 14 27 15 15
17M | 20 17 15 13 15 3 15 13 14 25 5 | 26 25 28 25 28 20 25 26 26 21 21
18E | 8 16 6 14 12 7 12 10 12 14 4 | 18 20 20 20 19 17 20 19 24 15 16
19M | 12 12 6 10 12 5 11 7 12 30 3 | 22 22 24 16 24 18 21 14 30 20 18
20E | 6 8 7 9 14 5 11 9 12 8 3 | 22 28 31 23 29 25 26 27 31 26 25
21 | 11 11 8 8 17 5 14 9 16 18 4 | 18 19 20 14 25 12 23 13 24 13 13
22E | 7 9 6 11 10 6 10 11 13 14 3 | 24 21 24 22 25 23 24 23 28 19 20
23 | 9 11 9 10 16 4 11 8 10 29 4 | 20 24 29 25 27 22 27 20 29 28 22
24M | 13 12 7 8 15 6 11 14 10 12 4 | 44 45 46 40 47 40 46 39 47 41 42
25 | 12 15 7 8 10 4 12 10 13 10 4 | 16 25 20 14 23 17 25 16 30 14 16
26M | 26 8 9 10 17 5 13 8 6 23 4 | 31 22 31 27 26 23 27 23 27 22 23
X27M | 6 --- --- --- --- 42 --- --- --- --- 0 | 35 --- --- --- --- 27 --- --- --- --- 37
28M | 19 13 12 13 20 4 15 9 6 12 5 | 23 24 23 20 34 16 26 21 23 14 17
29 | 14 17 8 8 12 4 19 10 12 32 4 | 30 30 30 24 27 26 31 25 36 31 26
X30M | 14 12 8 13 13 6 --- 9 13 --- 4 | 21 25 17 23 20 16 --- 16 25 --- 17
31 | 16 12 10 7 21 5 12 6 14 13 4 | 18 21 21 13 36 17 24 13 29 10 16
32 | 12 12 8 10 16 6 12 7 12 16 4 | 15 21 22 16 22 15 24 12 25 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 13 8 11 16 5 14 10 11 19 |T 25 27 26 23 29 22 28 23 30 23 22
WRMS | 14 13 8 10 15 5 14 9 9 16 |NE 20 23 23 17 26 17 25 18 27 18 17
MEDI | 12 12 8 10 15 5 12 9 12 16 |MD 23 24 24 22 26 22 25 20 29 21 21
Table 3.1735.4 GPS week: 1735 Day: 4 MJD: 56393.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 5 7 13 5 19 10 14 15 4 | 23 20 16 19 23 17 31 18 23 22 16
2 | 9 20 8 10 16 4 24 15 8 18 5 | 16 23 15 18 23 13 25 20 20 14 13
3 | 9 10 5 9 14 3 12 5 13 14 3 | 14 20 17 15 22 13 19 12 25 11 15
4 | 12 11 6 6 13 6 11 16 7 11 3 | 19 20 16 15 20 12 22 17 19 12 14
5E | 11 19 5 10 13 5 18 8 10 14 4 | 21 24 13 21 18 14 22 14 20 15 15
6 | 8 8 4 8 11 3 12 5 12 15 3 | 32 36 35 31 39 33 35 31 39 30 33
7 | 14 12 8 8 19 5 11 10 13 10 4 | 24 23 17 16 30 17 22 13 30 15 16
X8 | 7 --- 5 --- --- 6 16 9 --- --- 5 | 14 --- 14 --- --- 13 21 14 --- --- 11
X9 | 6 9 4 7 12 3 --- 8 8 21 3 | 9999 9999 9999 9999 9999 9999 --- 9999 9999 9999 9999
10E | 12 19 10 15 17 8 25 21 13 34 6 | 90 92 88 91 90 89 95 96 92 92 90
11 | 11 12 6 8 19 7 13 7 12 16 4 | 25 36 33 30 45 30 32 26 30 31 29
12 | 13 19 5 7 24 3 25 11 12 17 5 | 17 21 15 12 28 13 23 17 22 12 12
13 | 12 19 7 10 17 5 16 10 9 16 4 | 19 28 21 24 33 21 31 20 24 24 20
14 | 6 15 7 9 13 4 14 11 12 21 4 | 26 24 27 28 29 24 30 29 29 21 25
15 | 16 19 4 8 14 7 21 7 11 22 4 | 19 23 16 16 26 17 24 17 28 16 15
16 | 6 15 6 7 16 5 22 6 13 18 4 | 10 22 16 16 27 14 26 11 23 13 14
17 | 12 18 7 10 12 5 25 12 8 24 4 | 24 25 25 22 25 19 24 26 24 21 20
18E | 7 14 4 9 14 4 15 8 12 16 3 | 22 19 18 21 21 17 23 20 30 17 18
19 | 7 12 6 9 16 4 15 7 11 29 3 | 17 21 21 16 25 15 23 13 25 19 17
20E | 7 10 6 8 14 4 14 16 11 15 4 | 23 27 27 23 28 24 29 25 30 26 24
21 | 8 12 6 7 17 3 19 7 11 17 3 | 14 17 12 15 25 9 27 11 21 11 10
22E | 6 12 3 8 11 4 13 10 9 13 3 | 19 21 18 23 20 17 22 20 20 18 18
23 | 9 14 7 11 17 5 16 9 10 29 4 | 21 25 20 27 25 20 26 19 26 29 20
24 | 11 13 4 9 16 3 15 10 8 10 3 | 28 30 25 22 31 23 30 26 27 24 23
25 | 11 22 7 9 15 4 14 13 10 8 4 | 15 29 18 15 26 12 25 13 21 10 13
26 | 7 7 4 8 11 4 14 7 9 10 3 | 23 25 23 22 26 22 23 19 28 19 21
X27 | 6 --- --- --- --- 56 --- --- --- --- 0 | 101 --- --- --- --- 84 --- --- --- --- 102
28 | 8 11 7 11 18 7 20 6 13 12 4 | 17 21 20 17 32 18 22 20 29 15 16
29 | 9 16 6 8 15 5 20 13 13 33 4 | 23 28 24 23 26 22 30 20 25 29 21
X30 | 11 11 6 13 11 9 --- 16 21 --- 5 | 16 26 18 23 24 17 --- 18 29 --- 18
31 | 13 13 6 6 19 4 14 7 11 12 4 | 19 21 16 16 35 14 23 14 28 10 16
32 | 12 15 6 8 17 4 15 7 9 18 4 | 14 26 18 17 24 12 25 14 21 21 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 6 9 16 5 17 11 11 19 |T 24 26 22 22 29 22 27 21 27 21 22
WRMS | 10 15 6 8 15 4 17 9 10 19 |NE 18 23 17 18 26 15 25 16 22 16 15
MEDI | 9 13 6 8 15 4 15 9 11 16 |MD 19 24 18 21 26 17 25 18 25 18 17
Table 3.1735.5 GPS week: 1735 Day: 5 MJD: 56394.000
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 12 8 8 15 5 14 13 14 14 4 | 23 24 22 24 24 23 29 28 30 23 22
2 | 9 19 8 13 18 4 23 13 8 20 5 | 15 22 16 17 20 11 23 19 21 16 13
3 | 11 10 5 9 15 3 12 7 8 13 3 | 19 21 20 18 23 17 21 18 20 15 18
4 | 7 9 5 8 13 4 11 14 8 10 3 | 16 19 18 13 18 13 20 17 23 11 15
5E | 10 21 6 9 15 6 16 11 11 16 4 | 22 26 19 22 22 18 22 20 26 18 19
6 | 9 9 5 8 14 5 10 7 9 15 3 | 54 53 53 48 51 53 53 52 56 51 51
7 | 9 11 8 7 23 3 11 7 11 10 4 | 15 22 13 13 32 11 20 10 23 13 13
X8 | 7 --- --- --- --- 20 --- --- --- --- 0 | 17 --- --- --- --- 14 --- --- --- --- 14
9 | 7 10 6 8 19 4 13 9 11 22 3 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
10E | 15 18 11 15 17 5 22 20 12 20 6 | 71 75 72 76 70 70 72 68 72 76 71
11 | 10 12 8 10 19 4 13 9 12 15 4 | 24 33 28 26 38 23 30 24 24 29 25
12 | 11 16 6 7 22 3 25 11 12 16 5 | 15 20 14 12 25 10 24 16 21 11 12
13 | 12 16 7 9 19 3 15 8 13 15 4 | 17 29 20 21 33 18 28 19 23 21 19
14 | 8 15 7 12 13 3 16 10 10 22 4 | 18 24 25 28 28 22 26 26 27 22 23
15 | 12 21 7 9 18 4 19 7 11 24 4 | 19 24 21 19 28 18 25 17 28 16 18
16 | 8 14 6 8 18 3 20 5 11 17 4 | 10 22 16 15 26 11 24 10 22 11 13
17 | 11 19 7 10 11 5 19 12 10 24 4 | 21 24 19 17 22 14 22 20 21 20 16
18E | 7 14 4 10 18 4 13 9 8 19 3 | 19 23 20 24 27 18 21 18 23 23 19
19 | 8 12 7 8 13 3 15 7 12 30 3 | 15 21 19 16 21 13 21 13 21 19 15
20E | 7 11 7 10 12 5 13 12 10 9 3 | 16 22 19 19 22 16 20 19 22 19 17
21 | 8 17 8 10 26 3 19 8 13 19 4 | 12 23 10 14 30 9 25 10 20 13 11
22E | 10 13 5 9 14 3 13 10 12 17 3 | 19 23 21 25 24 20 24 19 27 21 20
23 | 10 12 7 12 17 4 14 9 13 29 4 | 17 24 17 24 26 17 23 16 27 27 18
24 | 11 13 7 10 17 4 14 15 10 10 4 | 31 34 32 30 38 29 37 30 37 29 30
25 | 9 16 6 10 13 4 11 12 6 9 3 | 11 23 19 14 23 11 21 13 18 10 13
26 | 10 10 7 8 12 2 13 8 9 11 3 | 12 19 21 17 22 17 23 15 27 12 16
X27 | 7 --- --- --- --- 49 --- --- --- --- 0 | 125 --- --- --- --- 129 --- --- --- --- 125
28 | 8 13 7 11 21 5 19 9 11 12 4 | 13 19 13 16 31 11 23 16 18 14 12
29 | 10 15 6 6 14 3 18 14 10 34 4 | 19 28 22 19 23 18 25 19 27 27 19
X30 | 15 15 --- 12 15 12 --- 11 --- --- 6 | 16 30 --- 21 20 18 --- 16 --- --- 17
31 | 13 14 8 10 20 5 14 7 10 13 4 | 18 25 17 19 35 15 24 15 25 11 17
32 | 13 12 6 8 22 5 13 9 13 19 4 | 17 29 20 19 31 17 27 16 25 24 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 7 10 17 4 16 10 11 18 |T 23 26 22 22 28 22 26 20 26 21 23
WRMS | 10 14 7 9 18 4 15 9 9 18 |NE 15 23 17 17 25 13 23 16 22 16 15
MEDI | 9 13 7 9 17 4 14 9 11 16 |MD 17 24 19 19 26 17 24 18 23 19 18
Table 3.1735.6 GPS week: 1735 Day: 6 MJD: 56395.000
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 15 8 8 14 3 16 12 12 14 4 | 26 28 19 27 22 23 32 28 26 23 22
2 | 8 18 7 13 17 3 22 19 9 19 5 | 16 22 14 20 24 10 24 21 15 17 13
3 | 9 10 5 7 16 2 11 8 10 14 3 | 19 21 19 16 24 18 21 18 25 17 18
4 | 5 13 5 8 13 3 12 14 10 9 3 | 17 18 15 15 19 11 21 16 19 12 14
5E | 7 21 7 12 18 5 19 8 8 18 4 | 19 26 17 23 24 17 25 18 24 18 17
6 | 8 11 6 6 13 3 10 8 9 15 3 | 53 57 55 49 59 51 57 51 51 47 53
7 | 11 11 6 8 22 4 11 6 8 7 3 | 18 25 18 17 33 17 25 17 24 16 17
8 | 8 10 6 7 11 9 14 10 9 22 3 | 16 9 4 7 9 7 11 6 7 6 10
9 | 8 11 6 8 16 3 13 10 8 20 3 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
10E | 11 18 8 13 17 6 18 18 5 17 5 | 101 100 96 98 97 95 100 101 100 97 98
11 | 9 14 6 7 18 3 13 10 17 16 4 | 37 43 41 36 53 38 40 38 35 41 38
12 | 10 20 7 7 22 3 25 11 11 18 5 | 20 22 15 13 28 14 24 18 25 13 14
13 | 8 15 5 8 19 4 14 10 10 16 4 | 23 33 25 28 37 26 34 28 25 30 25
14 | 7 20 7 10 14 6 17 12 10 25 4 | 32 31 32 38 35 33 35 37 31 31 32
15 | 12 20 5 9 16 5 19 8 11 28 4 | 22 28 21 22 31 20 25 19 27 19 20
16 | 8 14 7 7 19 2 19 5 13 18 4 | 14 22 16 9 24 12 25 9 22 10 12
17 | 11 20 6 9 11 4 21 12 10 24 4 | 32 27 28 28 29 25 25 32 29 26 25
18E | 8 14 5 10 20 4 11 9 12 17 4 | 32 29 28 29 30 27 34 24 34 27 28
19 | 12 13 8 6 12 2 14 8 11 32 4 | 19 22 21 13 25 15 22 14 22 22 16
20E | 7 12 7 10 14 4 13 13 10 11 4 | 18 24 21 19 22 18 21 20 26 20 19
21 | 12 14 9 10 17 5 18 9 10 18 4 | 14 21 16 17 29 11 26 12 17 14 13
22E | 6 11 5 7 16 4 13 10 8 15 3 | 25 27 24 24 30 24 32 22 28 25 23
23 | 9 12 6 10 17 4 14 12 10 30 4 | 22 28 23 28 31 24 29 24 27 33 23
24 | 10 15 6 9 16 3 15 13 12 11 4 | 26 33 27 27 36 24 33 23 33 25 26
25 | 10 16 6 10 15 5 13 14 9 10 4 | 14 24 16 13 24 11 24 16 20 11 13
26 | 8 11 7 9 11 2 12 9 7 12 3 | 27 23 26 27 27 25 25 22 27 21 24
X27 | 7 --- --- --- --- 57 --- --- --- --- 0 | 207 --- --- --- --- 203 --- --- --- --- 207
28 | 9 13 5 9 18 4 15 10 8 10 4 | 19 19 16 16 30 15 22 19 20 14 15
29 | 12 16 7 7 14 4 18 16 10 34 4 | 30 31 28 25 32 26 31 30 29 33 26
X30 | 19 15 --- 13 16 23 --- 11 --- --- 7 | 19 26 --- 21 18 18 --- 16 --- --- 16
31 | 10 14 7 9 23 5 13 7 10 11 4 | 17 27 15 18 37 17 26 14 22 13 17
32E | 16 14 7 11 19 6 13 21 7 30 5 | 29 35 30 30 36 24 33 20 31 27 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 6 9 17 4 16 12 10 19 |T 31 29 25 25 31 29 30 24 28 24 29
WRMS | 9 15 6 8 16 4 15 10 8 18 |NE 19 25 18 19 29 16 26 19 22 19 17
MEDI | 9 14 6 9 16 4 14 10 10 17 |MD 22 26 21 22 29 20 25 20 26 21 20
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 4.1735 GPS week: 1735 MJD: 56389.0-56395.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 |U 6 5 14 |U 8 10 26 |U 7 6 17 |
emr | emr 2933 | 8 7 16 |U 10 13 33 | 7 6 17 |
esa | esa 2934 | 6 4 13 |U 8 10 27 | 6 6 18 |
gfz | gfz 2926 |U 8 6 21 |U 8 10 26 |U 6 6 16 |
grg | grg 2948 |U 9 9 26 |U 11 16 43 | 8 9 23 |
igr | igr 2941 | 6 5 13 | 7 10 25 | 6 5 16 |
igs | igs 2948 | 6 5 13 | 8 12 28 | 6 5 15 |
jpl | jpl 2836 | 7 6 16 |U 9 13 32 | 7 6 20 |
mit | mit 2948 | 8 10 22 |U 10 15 35 |U 8 7 18 |
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 5.1735.0 GPS week: 1735 Day: 0 MJD: 56389.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 5 4 12 | 5 9 22 | 5 4 15 |
emr | emr 2976 | 6 6 16 | 7 6 22 | 5 4 16 |
esa | esa 2976 | 5 4 10 | 4 6 20 | 5 4 16 |
gfz | gfz 2975 | 22 16 60 | 4 7 22 | 5 4 15 |
grg | grg 2976 | 8 7 24 | 8 9 37 | 9 5 17 |
igr | igr 2976 | 7 5 12 | 4 6 20 | 5 4 14 |
igs | igs 2976 | 7 5 12 | 4 6 20 | 5 4 14 |
jpl | jpl 2880 | 6 6 13 | 5 6 19 | 7 5 18 |
mit | mit 2976 | 5 6 10 | 5 6 22 | 5 5 13 |
Table 5.1735.1 GPS week: 1735 Day: 1 MJD: 56390.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 | 6 3 15 | 6 10 23 | 5 6 16 |
emr | emr 2976 | 7 6 14 | 7 8 25 | 5 5 14 |
esa | esa 2976 | 7 3 13 | 6 8 24 | 5 5 17 |
gfz | gfz 2976 | 6 3 13 | 6 9 25 | 5 5 16 |
grg | grg 2976 | 7 6 15 | 8 12 31 | 7 8 26 |
igr | igr 2976 | 7 4 14 | 5 8 24 | 5 6 16 |
igs | igs 2976 | 6 4 12 | 6 8 23 | 5 5 16 |
jpl | jpl 2877 | 6 5 15 | 6 8 23 | 5 6 18 |
mit | mit 2976 | 6 3 13 | 6 7 26 | 5 7 18 |
Table 5.1735.2 GPS week: 1735 Day: 2 MJD: 56391.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 6 5 13 | 10 11 22 | 5 4 14 |
emr | emr 2976 | 9 9 17 | 12 9 28 | 6 6 14 |
esa | esa 2976 | 6 5 12 | 11 9 25 | 5 4 16 |
gfz | gfz 2975 | 6 5 13 | 11 9 25 | 6 5 14 |
grg | grg 2976 | 8 7 16 | 12 17 36 | 6 7 16 |
igr | igr 2976 | 7 6 13 | 10 9 22 | 5 4 15 |
igs | igs 2976 | 7 6 13 | 11 9 23 | 5 4 14 |
jpl | jpl 2879 | 8 7 19 | 11 8 29 | 6 6 18 |
mit | mit 2976 | 6 5 11 | 10 9 23 | 7 5 15 |
Table 5.1735.3 GPS week: 1735 Day: 3 MJD: 56392.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 8 11 16 | 7 7 33 | 11 12 28 |
emr | emr 2880 | 7 8 13 | 6 6 22 | 8 8 23 |
esa | esa 2976 | 5 4 13 | 9 9 28 | 10 11 26 |
gfz | gfz 2879 | 5 5 11 | 6 7 23 | 7 9 26 |
grg | grg 2975 | 8 10 24 | 8 22 34 | 10 11 24 |
igr | igr 2876 | 5 5 10 | 6 6 20 | 8 8 22 |
igs | igs 2880 | 5 5 10 | 6 6 21 | 8 7 21 |
jpl | jpl 2783 | 6 6 13 | 7 8 25 | 10 10 27 |
mit | mit 2880 | 5 5 11 | 6 7 22 | 13 10 22 |
Table 5.1735.4 GPS week: 1735 Day: 4 MJD: 56393.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3027 | 7 3 13 | 10 16 36 | 7 7 18 |
emr | emr 2876 | 9 7 18 | 16 24 55 | 8 9 18 |
esa | esa 2976 | 7 4 13 | 10 14 37 | 7 7 18 |
gfz | gfz 2875 | 7 4 16 | 11 13 37 | 7 9 15 |
grg | grg 2880 | 10 8 28 | 12 16 41 | 7 11 19 |
igr | igr 2976 | 7 4 13 | 9 14 36 | 7 7 16 |
igs | igs 2976 | 7 4 13 | 10 14 36 | 7 8 16 |
jpl | jpl 2780 | 7 7 15 | 12 22 57 | 8 7 24 |
mit | mit 2976 | 6 3 11 | 15 24 51 | 9 9 22 |
Table 5.1735.5 GPS week: 1735 Day: 5 MJD: 56394.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2945 | 6 7 18 | 9 11 21 | 6 5 18 |
emr | emr 2876 | 9 8 22 | 12 18 48 | 6 6 18 |
esa | esa 2784 | 7 8 20 | 9 14 26 | 6 4 20 |
gfz | gfz 2872 | 6 7 19 | 9 14 25 | 5 3 13 |
grg | grg 2880 | 11 11 38 | 12 19 60 | 9 10 29 |
igr | igr 2859 | 7 8 20 | 9 13 25 | 5 4 17 |
igs | igs 2879 | 8 8 21 | 10 17 36 | 5 4 15 |
jpl | jpl 2779 | 8 9 22 | 10 17 33 | 5 4 20 |
mit | mit 2880 | 23 29 71 | 10 19 34 | 9 8 17 |
Table 5.1735.6 GPS week: 1735 Day: 6 MJD: 56395.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 5 4 10 | 7 10 22 | 7 5 11 |
emr | emr 2972 | 8 7 14 | 11 18 32 | 8 6 15 |
esa | esa 2880 | 4 3 11 | 9 11 31 | 7 5 12 |
gfz | gfz 2936 | 5 4 12 | 8 11 24 | 8 6 12 |
grg | grg 2976 | 14 13 36 | 13 20 60 | 11 10 27 |
igr | igr 2951 | 5 4 11 | 8 11 26 | 7 4 13 |
igs | igs 2975 | 5 4 12 | 10 21 33 | 6 4 11 |
jpl | jpl 2876 | 7 6 14 | 12 20 36 | 7 4 15 |
mit | mit 2976 | 7 15 25 | 18 34 66 | 7 6 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 6.1735 GPS week: 1735 MJD: 56389.500-56395.500
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 | 50 -23 79 257 -2 | 9 17
| 30 15 70 110 14 | 2
emr uuuuu | -11 65 41 34 -17 | 34 38
| 18 18 100 79 11 | 5
esa uuuuu | -12 -8 -73 6 -1 | 20 25
| 13 13 77 73 15 | 3
gfz uuuuu | 32 28 76 -105 -5 | 13 16
| 8 15 62 50 4 | 1
grg uuuux | 6 2 100 -108 -26 | -2 25
| 16 15 46 49 27 | 9
igr xxxxx | -57 6 24 -63 -6 | 2 9
| 14 11 30 33 2 | 2
irf xxxxx | -1 -11 2 -62 -4 | 4 10
| 6 9 29 21 3 | 1
jpl uuuuu | -16 -2 -20 -27 -4 | 28 31
| 19 34 94 74 12 | 2
mit uuuuu | 12 -30 -118 -65 -3 | 15 18
| 11 17 65 53 6 | 1
ngs uuuuu | -63 -11 -1 -42 3 | 5 10
| 41 26 110 158 8 | 3
sio xxxxx | 412 126 -178 -123 -2 | 51 52
| 61 35 79 62 7 | 2
Table 7.1735.0 GPS week: 1735 Day: 0 MJD: 56389.500
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 | 33 -10 -2 160 -10 | 11 12
emr uuuuu | 13 64 143 60 -24 | 43 45
esa uuuuu | -21 -28 -11 -36 -3 | 22 23
gfz uuuuu | 42 2 159 -183 -1 | 15 16
grg uuuux | 11 -4 76 -120 12 | 10 34
igr xxxxx | -38 10 51 -52 -4 | 5 8
irf xxxxx | 7 -14 6 -75 -2 | 7 10
jpl uuuuu | -28 42 46 -11 -16 | 31 32
mit uuuuu | 29 -21 -153 -81 0 | 18 19
ngs uuuuu | -64 8 -174 128 9 | 5 9
sio xxxxx | 358 164 -217 -153 6 | 50 51
Table 7.1735.1 GPS week: 1735 Day: 1 MJD: 56390.500
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 | -6 -33 77 120 -5 | 7 13
emr uuuuu | -7 64 135 161 -22 | 37 41
esa uuuuu | -9 -4 -46 -41 -11 | 18 20
gfz uuuuu | 24 39 7 -149 -11 | 11 14
grg uuuux | -15 -11 118 -112 -11 | 7 32
igr xxxxx | -62 -3 16 -64 -8 | 1 9
irf xxxxx | -5 -19 17 -94 -7 | 3 10
jpl uuuuu | 17 36 9 49 -14 | 27 30
mit uuuuu | 23 -51 -76 -99 -6 | 15 17
ngs uuuuu | -24 -12 -87 157 7 | 2 7
sio xxxxx | 352 110 -78 -155 0 | 48 49
Table 7.1735.2 GPS week: 1735 Day: 2 MJD: 56391.500
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 | 51 -17 178 248 -7 | 7 12
emr uuuuu | -7 80 19 10 -12 | 35 39
esa uuuuu | -31 -9 -100 -87 -4 | 17 20
gfz uuuuu | 27 42 47 -58 -2 | 11 14
grg uuuux | 0 0 75 -24 -3 | 2 26
igr xxxxx | -54 19 67 1 -5 | 0 8
irf xxxxx | -7 -21 -33 -72 -2 | 2 9
jpl uuuuu | -28 17 -10 49 -11 | 26 29
mit uuuuu | 10 -45 -186 -116 -3 | 14 17
ngs uuuuu | -17 -35 79 49 6 | 3 8
sio xxxxx | 475 93 -176 -207 -1 | 50 51
Table 7.1735.3 GPS week: 1735 Day: 3 MJD: 56392.500
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 | 80 -20 -14 462 27 | 6 12
emr uuuuu | -25 74 52 73 -18 | 35 39
esa uuuuu | -10 -8 -216 57 32 | 17 20
gfz uuuuu | 39 41 135 -41 -7 | 12 15
grg uuuux | 31 32 172 -68 -26 | -4 17
igr xxxxx | -64 17 38 -97 -6 | 0 8
irf xxxxx | -5 -8 42 -57 -8 | 3 9
jpl uuuuu | -21 -34 134 -20 -1 | 26 29
mit uuuuu | 0 -31 -40 -111 -14 | 14 17
ngs uuuuu | -64 -36 -5 -255 -14 | 4 9
sio xxxxx | 482 125 -88 -133 -16 | 51 52
Table 7.1735.4 GPS week: 1735 Day: 4 MJD: 56393.500
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 | 60 -9 64 285 -12 | 11 22
emr uuuuu | -29 26 54 -90 -28 | 33 37
esa uuuuu | 8 3 -109 127 -11 | 23 30
gfz uuuuu | 32 30 75 -111 -3 | 13 17
grg uuuux | 24 -7 148 -126 -41 | -5 17
igr xxxxx | -57 10 -22 -86 -8 | 2 10
irf xxxxx | -2 -8 27 -61 0 | 4 11
jpl uuuuu | -6 -11 -124 -168 -8 | 28 31
mit uuuuu | -2 -30 -49 -62 5 | 15 18
ngs uuuuu | -116 -15 45 -140 6 | 6 10
sio xxxxx | 472 153 -150 -126 0 | 52 53
Table 7.1735.5 GPS week: 1735 Day: 5 MJD: 56394.500
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 | 58 -52 113 285 -7 | 12 22
emr uuuuu | -33 66 43 -22 -20 | 30 35
esa uuuuu | -20 9 14 -23 -3 | 23 30
gfz uuuuu | 40 20 109 -106 -8 | 14 17
grg uuuux | -4 -5 53 -175 -54 | -9 21
igr xxxxx | -43 -2 7 -60 -8 | 2 10
irf xxxxx | -2 5 -21 -37 -5 | 5 11
jpl uuuuu | -40 -15 -127 -31 19 | 28 31
mit uuuuu | 14 2 -200 17 -4 | 16 19
ngs uuuuu | -38 -26 -31 -58 7 | 8 12
sio xxxxx | 384 160 -260 -27 -2 | 53 54
Table 7.1735.6 GPS week: 1735 Day: 6 MJD: 56395.500
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 | 79 -19 137 237 3 | 10 21
emr uuuuu | 10 77 -159 48 5 | 25 29
esa uuuuu | -1 -21 -44 48 -3 | 23 30
gfz uuuuu | 22 22 -3 -84 -1 | 13 17
grg uuuux | -1 9 60 -133 -58 | -16 28
igr xxxxx | -81 -8 12 -84 -4 | 1 10
irf xxxxx | 6 -10 -25 -34 -1 | 4 11
jpl uuuuu | -6 -47 -66 -57 1 | 29 33
mit uuuuu | 9 -32 -123 -4 1 | 16 18
ngs uuuuu | -118 36 162 -174 -2 | 10 13
sio xxxxx | 362 76 -280 -56 -3 | 52 53
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