[IGSREPORT-21931] Wk 1744 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jun 28 10:19:34 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1744 (Jun 09, 2013 - Jun 15, 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:
igs1744[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1744[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1744[0-6].cls IGS GPS clock combination summary report.
igs17447.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17447.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 | 26 26 KOUC MOBS FLRS KOUC MOBS XMIS
0 | ESA | 26 26 IRKJ KOUC NANO IRKJ KOUC NANO RAMO
0 | GFZ | 26 26
0 | GRG | 13 13 ALIC DARW IRKJ MATE NTUS POL2 YIBL IRKJ NTUS
0 | MIT | KOSG MDVJ DAV1 KOSG MDVJ YIBL
1 | COD | 26 26 REYK XMIS REYK XMIS
1 | EMR | HERS TLSE YELL HERS TLSE YELL
1 | ESA | 26 26 IRKJ IRKJ UNSA
1 | GFZ | 26 26 ALRT ALRT MDVJ NRIL
1 | GRG | IRKJ NTUS REUN IRKJ RAMO REUN
1 | JPL | YELL
1 | MIT | MDVJ MDVJ
2 | COD | 26 26 FLRS FLRS GOPE XMIS
2 | EMR | WUHN WUHN
2 | ESA | 26 26 IRKJ KOUC IRKJ KOUC UNSA
2 | GFZ | 26 26 REUN
2 | GRG | GOPE GUUG IRKJ LPGS PIMO SPT0 XMIS GOPE IRKJ LPGS
2 | GRG | PIMO
2 | JPL | RAMO
2 | MIT | 7 16 7 16 MDVJ MDVJ
3 | COD | 26 26 REUN REUN REYK
3 | EMR | MATE
3 | ESA | 26 26 NRMD NRMD UNSA
3 | GFZ | 26 26 IRKJ KOSG MATE AUCK KOSG MATE
3 | GRG | ARTU ASPA AUCK BOGT BRMU BRUX CHUR DARW DGAR FAA1
3 | GRG | GLSV GOPE GUAT GUUG IRKJ ISPA KOUR MAC1 MAW1 MCIL
3 | GRG | MDVJ NKLG NOVM NRIL NTUS PDEL PIMO POL2 REYK SCUB
3 | GRG | SPT0 TOW2 XMIS FAA1 IRKJ NKLG NTUS
3 | MIT | MDVJ
4 | COD | CHUR CONZ FLRS KOUC REYK XMIS CONZ FLRS KOUC REYK
4 | COD | XMIS
4 | EMR | 26 WUHN WUHN
4 | ESA | CHUR KOUC ABMF CHUR KOUC
4 | GFZ | 26 26 MATE MATE
4 | GRG | 26 26 ABMF BRAZ FAA1 IRKJ MCIL NOVM NTUS DUBO GUAM
4 | GRG | IRKJ MCIL NOVM NTUS
4 | JPL | RAMO
4 | MIT | 10 13 16 23 26 10 23 CONZ MDVJ CONZ GOPE MDVJ
5 | COD | KOUC KOUC
5 | EMR | 26 26 WUHN WUHN
5 | ESA | IRKJ KOUC IRKJ KOUC UNSA
5 | GFZ | 26 26 MDVJ MDVJ
5 | GRG | 26 26 CONZ GLSV IRKJ GLSV IRKJ
5 | MIT | 26 26 MDVJ
6 | COD | KOUC MOBS KOUC MOBS XMIS
6 | EMR | 26 26 THTI
6 | ESA | IRKJ KOUC ARTU IRKJ KOUC UNSA
6 | GFZ | 26 26 NTUS NTUS
6 | GRG | 26 26 IRKJ PDEL THTI WTZR XMIS ARTU IRKJ PDEL THTI
6 | MIT | 5 6 16 23 26 5 6 16 23 26 MDVJ NTUS TWTF MDVJ NTUS
6 | MIT | TWTF
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
----+------------+----------
G04 | 2013_06_12 | 2013033
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
----+--------+---------------
6 | MIT | 26
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 G27 | 4 | | | 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 | .3 1.1 -.6 -39 5 -13 .08
EMR | 0 | -2.2 -4.8 10.7 -51 -24 -24 .23
ESA | 0 | .4 -1.2 3.2 65 -34 21 .19
GFZ | 0 | -.8 .4 -.4 -7 -29 -12 -.18
GRG | 0 | 5.1 -6.4 34.4 -28 31 -48 .41
JPL | 0 | 1.5 -6.6 13.0 -64 1 -121 .19
MIT | 0 | 2.7 -2.8 18.7 -6 4 -47 .24
NGS | 0 | -1.8 -5.6 18.6 -78 -11 -23 .32
SIO | 0 | -1.0 -3.0 -38.6 -116 -204 -113 .24
COD | 1 | .2 .0 -.8 -31 3 -21 .24
EMR | 1 | 1.2 -4.3 11.2 -17 4 -34 .32
ESA | 1 | -1.0 -3.2 1.9 51 -35 -4 .10
GFZ | 1 | -.7 .1 -.5 -19 -22 -10 -.01
GRG | 1 | 8.6 -7.0 31.8 -25 27 -76 .68
JPL | 1 | -2.2 -4.7 11.4 -86 -28 -13 .60
MIT | 1 | -2.1 -4.0 17.0 -18 17 -58 .33
NGS | 1 | -5.7 -6.1 18.4 -94 -9 -46 .53
SIO | 1 | 1.2 -2.2 -26.6 -76 -153 22 .47
COD | 2 | -.2 .8 -.4 -29 8 -9 .12
EMR | 2 | 2.9 5.1 6.6 -15 14 -17 .05
ESA | 2 | -1.0 -1.3 -.4 39 11 -44 .26
GFZ | 2 | -.3 -.1 -.8 -19 -22 -8 -.17
GRG | 2 | 1.8 -.6 23.5 -30 15 -3 .39
JPL | 2 | -1.7 -1.5 11.1 -43 14 -42 .35
MIT | 2 | -1.3 1.4 19.2 -8 -3 -39 .27
NGS | 2 | 4.0 -8.7 24.3 -130 -45 -3 .57
SIO | 2 | .8 .4 -38.5 -51 -192 -53 .05
COD | 3 | .4 -.3 -.5 -27 17 -16 .13
EMR | 3 | .2 -.5 5.1 -7 17 -29 -.03
ESA | 3 | .6 -1.6 1.1 37 -14 -39 .18
GFZ | 3 | .0 -.4 -.5 -14 -28 -5 -.15
GRG | 3 | 5.2 -9.9 30.3 -27 50 -28 .27
JPL | 3 | 3.4 -1.7 9.7 -38 44 -20 .33
MIT | 3 | .7 -1.9 21.1 -7 3 -45 .05
NGS | 3 | 4.5 -7.3 18.9 -91 -48 -5 .34
SIO | 3 | 2.9 -3.3 -34.2 -87 -164 -122 .08
COD | 4 | -.5 .1 -2.1 -12 48 -33 .20
EMR | 4 | 5.0 -.1 11.2 -45 -18 -34 .18
ESA | 4 | -2.9 -3.3 2.1 44 14 -37 .25
GFZ | 4 | -.5 -.4 -1.2 -1 -22 -19 .11
GRG | 4 | 3.4 -6.3 30.9 3 41 -9 .33
JPL | 4 | 4.9 -3.0 12.3 -39 53 -54 .38
MIT | 4 | 3.4 .9 16.7 -8 7 -49 .06
NGS | 4 | .1 -11.7 12.2 -107 2 -15 .28
SIO | 4 | 2.5 -3.6 -10.7 -26 -84 16 .05
COD | 5 | -.5 .5 -1.8 -29 33 -38 .24
EMR | 5 | 2.1 .8 7.4 -48 -17 -31 .20
ESA | 5 | .6 -4.3 6.1 44 1 -32 .20
GFZ | 5 | -1.0 .3 -.8 -15 -11 -25 -.08
GRG | 5 | 7.6 -2.4 29.9 -7 33 -47 .23
JPL | 5 | 2.7 .5 13.0 -50 42 -30 .05
MIT | 5 | 3.4 1.3 18.2 -8 15 -55 .04
NGS | 5 | 1.4 -9.0 13.1 -90 -9 -3 .29
SIO | 5 | 2.6 -2.0 -16.9 -35 -112 -44 .03
COD | 6 | -.9 .5 -1.8 -33 25 2 .11
EMR | 6 | 5.3 -3.6 9.5 -48 -19 -29 .10
ESA | 6 | 6.0 -5.6 .1 36 -3 -37 .07
GFZ | 6 | -.1 .3 -.4 -17 -19 -18 -.40
GRG | 6 | 10.4 -3.7 19.9 -38 33 -47 .30
JPL | 6 | 10.6 -2.9 14.5 -37 41 -47 .18
MIT | 6 | 6.0 -.9 17.7 1 -4 -43 -.02
NGS | 6 | 8.0 -3.6 7.7 -43 -30 38 .19
SIO | 6 | 6.2 -2.2 -13.1 -63 -135 -80 -.08
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 1.1744.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1744.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 2.1744.[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 3.1744.[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 5.1744.0-6). 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 1744 summary. (Jun 09, 2013 - Jun 15, 2013)
Table 1.1744.a GPS week: 1744 MJD: 56452.000-56458.000
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 271| -1 1 -6 16 8 5 -.45 10 10 | -1027 -308 18 86
| 0 0 1 19 15 5 .02 | 292 498
emr 79| 1 -1 -1 -10 -42 21 .33 14 14 | 1679 672 15 91
| 0 1 0 14 16 7 .01 | 1322 730
esa 150| 0 0 1 7 16 -15 .07 5 5 | -1 -1464 14 116
| 0 0 1 10 23 9 .03 | 653 1172
gfz 201| 0 0 0 9 -6 -3 -.46 10 10 | -262 604 12 72
| 0 0 1 41 46 9 .04 | 507 763
grg 138| 1 0 13 4 16 0 .61 15 14 | -142 233 21 153
| 0 0 3 17 24 20 .09 | 125 422
igr n/a| 0 0 -3 11 4 -23 -.18 5 4 | 1940 336 14 73
| 0 0 1 15 24 19 .04 | 1262 780
jpl 80| 0 0 -5 -6 -31 -29 .37 13 13 | 1257 670 14 98
| 0 1 1 23 8 9 .01 | 1319 741
mit 236| 1 0 2 0 1 6 -.51 14 11 | -76 74 23 217
| 0 0 1 23 23 17 .02 | 139 382
ngs 243| 0 0 0 -48 0 18 .36 10 9 | -1014 -384 1817 3464
| 1 1 3 29 50 21 .02 | 317 540
sio 431| 0 0 -8 -105 -158 -62 -.18 19 18 | --- --- --- ---
| 0 0 1 30 51 71 .07 | --- ---
Table 1.1744.b GPS week : 1744 MJD: 56452.000-56458.000
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 | 4 4 4 4 5 4 4 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 3 0 4 3 3 |
5 | 4 5 4 5 5 4 5 |
6 | 3 3 3 3 3 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 4 3 3 3 3 |
9 | 3 4 4 4 3 3 4 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 3 3 4 3 3 |
12 | 6 6 6 6 5 6 5 |
13 | 4 3 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 5 5 4 4 5 4 5 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 5 4 4 4 4 4 4 |
19 | 5 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 3 |
21 | 3 4 3 4 3 4 3 |
22 | 4 4 4 4 4 4 3 |
23 | 5 4 4 5 4 4 4 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 5 5 5 5 6 7 7 |
27 | 0 0 0 0 0 0 0 |
28 | 3 4 5 3 4 4 4 |
29 | 5 5 4 5 5 4 4 |
30 | 0 0 0 0 0 0 0 |
31 | 4 4 3 4 4 4 4 |
32 | 3 3 3 3 3 3 3 |
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 2.1744.0 GPS week: 1744 Day: 0 MJD: 56452.000
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 269| -1 2 -6 -24 -1 12 -.44 10 10 | -900 -157 18 70
emr 80| 0 -2 0 -3 -41 25 .33 13 13 | 1668 776 17 92
esa 150| 0 0 0 8 0 -13 .09 6 5 | -617 -381 16 108
gfz 199| 0 -1 0 50 -17 1 -.47 10 9 | -646 1124 13 76
grg 139| 0 1 16 5 22 -19 .53 15 14 | -45 395 22 146
igr n/a| 0 0 -2 -14 15 -25 -.15 4 4 | 3216 227 14 72
jpl 80| 1 3 -3 -26 -41 -47 .37 13 12 | 1416 642 15 99
mit 235| 0 0 3 -16 8 -9 -.53 12 11 | -69 441 19 193
ngs 245| 1 -1 0 -38 54 36 .36 10 9 | -921 -192 1949 3455
sio 432| 0 0 -6 -173 -221 -147 -.07 19 18 | --- --- --- ---
Table 2.1744.1 GPS week: 1744 Day: 1 MJD: 56453.000
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 271| -1 2 -8 24 19 -4 -.44 10 10 | -938 -260 21 89
emr 79| 1 -3 -2 4 -18 34 .33 14 14 | 1853 147 18 70
esa 150| 0 0 0 -9 50 -21 .07 5 5 | 1118 -3312 12 100
gfz 199| 1 0 0 42 -84 9 -.50 10 10 | -272 323 14 69
grg 139| 3 1 15 37 2 0 .57 16 14 | -225 516 23 139
igr n/a| 0 0 -1 13 44 -42 -.12 4 4 | 2738 86 14 70
jpl 80| 1 -1 -6 -15 -37 -25 .38 13 12 | 1422 291 15 95
mit 236| 0 -1 4 6 -42 15 -.51 13 12 | -325 587 26 223
ngs 241| -2 0 3 -70 20 8 .38 10 9 | -959 -296 2119 3445
sio 427| 1 0 -8 -99 -190 15 -.14 21 19 | --- --- --- ---
Table 2.1744.2 GPS week: 1744 Day: 2 MJD: 56454.000
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 269| -2 2 -6 18 -14 4 -.50 9 9 | -750 -762 19 108
emr 80| 2 0 -2 3 -70 12 .33 14 14 | 1091 -331 15 94
esa 150| 0 0 0 19 6 -30 .01 4 4 | -568 -831 18 122
gfz 198| 0 0 -1 -71 22 -10 -.53 11 11 | 66 -244 12 73
grg 138| 2 0 10 -1 -15 36 .69 14 13 | -65 174 16 140
igr n/a| 0 0 -1 29 24 -54 -.15 4 4 | 1930 -962 15 71
jpl 80| 0 0 -5 38 -41 -36 .36 13 13 | 930 -581 15 97
mit 236| 1 -1 3 -27 -3 24 -.51 14 12 | 106 -208 20 215
ngs 239| 0 -1 6 -23 70 28 .36 9 8 | -772 -797 1801 3068
sio 430| 0 0 -8 -104 -205 -41 -.13 19 17 | --- --- --- ---
Table 2.1744.3 GPS week: 1744 Day: 3 MJD: 56455.000
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 274| -1 1 -6 31 0 6 -.45 9 9 | -954 -688 20 93
emr 80| 2 0 -1 -8 -53 17 .32 15 15 | -357 1747 15 109
esa 150| 0 0 1 -5 4 -16 .08 5 5 | -94 -1337 13 113
gfz 200| 1 -1 -1 26 42 -15 -.42 9 9 | -1087 1950 11 73
grg 141| 1 0 15 -12 38 -3 .76 15 15 | -376 664 24 184
igr n/a| 0 0 -4 24 -9 -22 -.17 5 4 | -133 1392 15 73
jpl 80| 0 1 -6 -15 -23 -22 .37 14 13 | -709 1679 15 104
mit 237| 1 -1 2 31 -4 -21 -.49 12 11 | -142 -47 20 202
ngs 244| -1 -1 0 -58 -5 48 .36 10 9 | -1044 -559 1622 3593
sio 435| 0 -1 -8 -94 -170 -163 -.19 18 16 | --- --- --- ---
Table 2.1744.4 GPS week: 1744 Day: 4 MJD: 56456.000
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 270| 0 1 -7 32 3 6 -.44 9 9 | -1241 -383 19 90
emr 79| 1 -3 -1 -12 -42 23 .35 14 14 | 954 851 14 91
esa 150| 0 0 1 14 47 -19 .06 5 5 | -406 -657 15 120
gfz 204| 0 -1 0 -5 -41 -13 -.41 9 9 | -390 686 12 72
grg 140| 1 1 13 10 20 4 .64 15 14 | -66 -610 21 174
igr n/a| 0 1 -3 4 -11 -9 -.19 6 5 | 547 795 15 73
jpl 80| 0 -1 -6 10 -24 -19 .37 13 13 | 126 1211 15 113
mit 237| 0 0 0 -9 -3 6 -.49 13 11 | 22 -534 29 260
ngs 246| 0 2 1 -89 -60 11 .36 12 10 | -1195 -506 1893 3484
sio 425| 0 0 -8 -78 -89 15 -.22 20 19 | --- --- --- ---
Table 2.1744.5 GPS week: 1744 Day: 5 MJD: 56457.000
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 276| -1 1 -4 12 31 5 -.44 10 10 | -1590 701 16 75
emr 79| 1 -2 -1 -25 -35 16 .32 14 14 | 2850 164 12 90
esa 150| 0 0 3 10 18 -2 .10 5 5 | 655 -2931 17 134
gfz 206| 0 0 0 -1 -10 4 -.44 9 9 | 440 -174 12 78
grg 136| 2 0 10 4 -5 13 .55 16 14 | -181 70 18 139
igr n/a| 0 0 -4 21 -15 -1 -.24 5 4 | 2450 -123 14 78
jpl 80| 0 -1 -6 -20 -22 -28 .40 13 12 | 2400 356 13 89
mit 234| 1 0 0 -9 32 5 -.52 13 10 | -121 91 24 211
ngs 248| -1 0 0 -1 -45 -17 .35 11 9 | -1597 666 2025 3576
sio 435| 0 0 -10 -93 -108 -38 -.20 20 20 | --- --- --- ---
Table 2.1744.6 GPS week: 1744 Day: 6 MJD: 56458.000
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 274| -2 1 -4 18 21 2 -.45 10 10 | -819 -612 18 78
emr 80| 1 -2 -2 -34 -33 20 .35 14 14 | 3696 1355 17 95
esa 150| 0 0 2 11 -8 -3 .07 5 4 | -99 -801 13 115
gfz 206| 0 0 1 25 43 -2 -.46 10 9 | 51 569 14 67
grg 139| 1 0 8 -12 54 -25 .56 16 12 | -40 426 25 149
igr n/a| 0 0 -3 0 -19 -6 -.22 5 4 | 2837 937 15 75
jpl 80| 0 2 -5 -15 -29 -24 .38 13 13 | 3217 1093 15 94
mit 237| 1 0 1 33 21 27 -.55 18 11 | -4 191 26 215
ngs 244| 0 0 -5 -59 -36 14 .33 11 9 | -611 -1010 1316 3633
sio 435| -1 0 -9 -97 -121 -74 -.28 21 19 | --- --- --- ---
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 3.1744.0 GPS week: 1744 Day: 0 MJD: 56452.000
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 7 4 8 10 6 16 9 10 23 3 | 42 52 49 47 61 46 59 49 48 50 49
2 | 9 8 5 14 13 4 10 11 8 20 3 | 21 22 22 28 26 20 24 26 22 23 21
3 | 11 12 7 6 11 4 12 11 9 15 3 | 74 78 76 72 77 74 76 70 75 81 74
4 | 23 8 5 7 12 4 8 12 8 16 4 | 16 14 14 9 17 16 17 15 12 16 14
5 | 13 14 5 9 13 4 16 12 9 19 4 | 35 43 32 31 40 33 47 28 36 36 34
6 | 9 11 6 8 11 4 10 12 7 16 3 | 16 22 18 18 22 15 23 16 17 21 16
7 | 10 10 5 7 19 4 13 13 9 24 3 | 37 36 35 31 47 32 37 27 38 28 34
8 | 7 7 5 8 13 3 8 10 7 18 3 | 24 28 26 27 24 26 27 28 25 32 25
9 | 9 8 6 6 11 3 9 10 8 24 3 | 26 30 30 26 26 28 31 28 31 39 28
10 | 8 6 3 10 12 3 7 11 8 12 3 | 16 23 19 16 27 18 24 23 19 25 18
11 | 7 11 5 7 12 4 12 13 13 12 3 | 44 51 44 44 59 44 52 48 47 40 46
12 | 14 29 8 15 18 6 21 11 13 16 6 | 56 56 58 57 59 55 58 52 60 51 56
13E | 8 11 5 8 19 3 11 14 9 9 4 | 21 21 21 18 31 18 25 20 22 19 19
14E | 8 11 6 9 15 4 10 13 10 14 3 | 23 26 23 22 27 22 24 22 26 26 22
15E | 8 17 6 8 15 3 18 14 9 19 4 | 29 31 29 28 28 30 31 37 34 33 29
16E | 9 17 6 16 26 5 15 14 9 15 5 | 26 30 31 37 44 30 31 32 30 32 29
17 | 7 12 6 11 18 3 16 7 11 14 4 | 17 21 16 17 32 17 24 18 26 18 17
18 | 10 18 5 9 19 4 18 10 10 24 4 | 22 32 23 26 36 24 30 24 30 22 23
19 | 8 15 6 11 17 4 14 22 10 22 4 | 18 27 21 22 32 20 27 26 25 23 21
20 | 8 12 5 12 11 5 12 12 11 18 4 | 22 27 23 27 32 25 28 25 24 20 23
21 | 5 10 4 7 12 5 10 10 12 21 3 | 20 30 28 24 33 26 31 25 33 27 26
22 | 9 14 6 9 16 3 14 8 12 23 4 | 26 30 26 31 40 27 29 26 31 25 26
23E | 10 13 6 10 21 5 13 16 9 11 4 | 32 36 37 35 37 35 37 38 34 37 34
24 | 14 12 5 11 16 4 12 8 8 14 4 | 20 25 23 18 32 20 31 19 28 21 21
25 | 9 14 6 7 17 5 11 10 11 17 4 | 16 23 18 14 31 16 25 17 24 21 17
26E | 14 16 8 12 14 4 14 17 10 31 4 | 58 50 52 58 42 53 52 59 50 44 52
X27 | 8 --- --- --- --- 48 --- --- --- --- 0 | 151 --- --- --- --- 150 --- --- --- --- 153
28E | 7 11 6 10 14 4 9 8 9 19 3 | 32 35 35 34 38 34 38 29 34 31 33
29 | 8 18 6 10 12 4 18 14 11 28 4 | 16 25 16 17 23 17 27 17 20 29 16
X30 | 8 --- --- --- --- 42 --- --- --- --- 0 | 41 --- --- --- --- 28 --- --- --- --- 41
31 | 10 15 6 7 19 4 15 8 9 15 4 | 22 25 22 21 35 22 27 19 26 20 21
32 | 8 9 4 7 11 3 8 9 13 12 3 | 22 28 22 22 28 22 30 19 25 27 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 6 10 15 4 13 12 10 19 |T 32 32 29 29 36 32 34 29 31 30 33
WRMS | 10 13 5 9 14 4 12 11 9 18 |NE 32 32 28 28 36 32 34 28 31 30 33
MEDI | 9 12 6 9 14 4 12 11 9 17 |MD 23 28 23 26 32 26 30 26 28 27 25
Table 3.1744.1 GPS week: 1744 Day: 1 MJD: 56453.000
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 8 4 11 11 5 15 11 12 17 3 | 22 31 28 26 38 26 37 30 27 33 26
2 | 8 10 6 12 13 3 10 13 6 20 3 | 23 21 20 30 19 20 19 27 21 21 20
3 | 8 15 6 9 24 6 16 9 12 51 4 | 117 121 116 118 115 116 120 118 120 134 117
4 | 12 7 5 10 14 3 10 12 7 17 3 | 21 15 14 14 12 18 14 18 12 21 16
5 | 14 17 6 10 15 7 16 13 7 18 4 | 23 31 24 25 29 22 31 27 27 29 24
6 | 7 10 4 9 11 5 11 11 10 19 3 | 13 16 16 17 18 14 19 18 15 22 12
7 | 10 12 5 9 19 5 12 10 8 21 3 | 26 33 28 33 35 27 34 32 31 33 28
8 | 9 7 3 10 12 3 8 14 7 18 3 | 19 24 24 23 24 21 26 26 23 30 21
9 | 10 8 4 8 10 5 9 19 7 27 3 | 19 23 24 22 23 20 23 28 25 36 21
10 | 9 8 3 12 12 4 8 14 6 12 3 | 16 22 18 17 22 16 21 26 21 25 18
11 | 7 12 4 8 12 3 10 12 12 13 3 | 24 34 27 26 40 26 35 32 27 27 27
12 | 14 28 6 16 25 5 25 13 11 15 6 | 34 35 28 31 32 27 37 28 30 25 27
13E | 8 12 4 10 11 3 12 9 8 8 3 | 17 24 20 23 27 19 23 23 23 20 20
14E | 8 11 4 8 23 4 10 16 11 17 4 | 25 25 25 24 21 23 23 24 27 23 23
15E | 10 17 7 8 14 3 17 23 9 17 4 | 33 33 37 33 30 33 31 38 37 36 33
16 | 10 20 6 15 23 5 12 13 15 14 5 | 26 32 30 26 37 26 28 28 33 27 26
17 | 7 13 5 10 17 3 15 11 10 15 4 | 19 23 17 18 27 16 22 22 23 24 17
18 | 10 15 7 9 17 3 18 9 9 23 4 | 23 25 22 22 25 20 27 22 23 15 19
19 | 7 16 4 9 15 2 14 19 10 22 4 | 17 26 20 15 28 17 25 21 20 19 17
20 | 10 14 5 11 10 4 12 12 10 17 3 | 24 23 23 24 23 21 23 20 23 19 20
21 | 7 11 6 7 13 4 12 10 11 21 3 | 18 19 26 19 21 20 19 20 24 17 19
22 | 8 13 5 9 15 3 14 11 11 22 3 | 22 23 23 22 24 20 24 21 20 20 19
23E | 9 14 4 9 15 3 13 12 11 10 3 | 29 38 34 30 34 32 34 37 36 34 32
24 | 15 12 5 7 18 5 12 11 11 11 4 | 24 20 21 15 26 18 24 15 27 18 18
25 | 9 16 5 6 21 4 13 11 10 24 4 | 18 19 21 13 28 15 22 18 20 16 16
26E | 13 19 6 15 15 5 12 14 11 30 4 | 54 46 51 55 37 49 46 56 47 38 49
X27 | 8 --- --- --- --- 24 --- --- --- --- 0 | 139 --- --- --- --- 134 --- --- --- --- 141
28E | 9 11 4 11 17 3 11 16 9 18 3 | 42 44 44 44 42 42 45 48 46 46 43
29 | 11 18 4 11 14 4 17 14 12 28 4 | 15 20 18 19 22 16 21 23 18 30 16
X30 | 8 --- --- --- --- 48 --- --- --- --- 0 | 34 --- --- --- --- 32 --- --- --- --- 36
31 | 8 14 6 6 21 4 15 9 13 15 4 | 17 23 20 17 33 19 22 16 24 19 17
32 | 9 8 4 8 11 5 8 12 13 14 3 | 17 25 20 19 21 20 25 21 24 25 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 10 16 4 13 13 10 21 |T 30 29 27 27 30 29 30 29 29 29 29
WRMS | 10 14 5 10 14 4 12 12 9 19 |NE 29 28 26 25 29 28 29 27 27 28 29
MEDI | 9 12 5 9 15 4 12 12 10 17 |MD 23 24 23 23 27 20 24 24 24 25 20
Table 3.1744.2 GPS week: 1744 Day: 2 MJD: 56454.000
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 5 10 11 5 18 8 9 12 3 | 38 42 36 36 48 36 45 40 38 35 37
2 | 7 10 3 17 11 5 10 17 7 21 3 | 26 24 20 34 23 24 26 27 24 21 21
3 | 9 13 4 10 17 6 12 11 8 14 3 | 97 98 95 94 89 97 97 97 106 96 95
4 | 8 8 3 9 12 4 8 15 9 19 3 | 18 17 13 8 17 15 18 14 15 17 14
5 | 11 15 4 9 15 5 16 16 10 20 4 | 27 36 27 25 34 27 38 28 29 31 27
6 | 8 10 3 11 11 5 10 12 6 14 3 | 21 25 18 19 22 19 24 20 22 20 17
7 | 9 12 3 12 17 5 14 9 10 20 3 | 34 40 35 36 40 33 38 35 35 37 34
8 | 10 8 3 11 13 3 9 17 8 19 3 | 19 27 20 23 23 19 25 24 24 28 20
9 | 9 8 5 9 12 4 11 20 8 25 3 | 17 27 22 20 24 20 28 26 24 36 20
10 | 8 7 3 12 11 4 8 16 5 16 3 | 18 24 17 18 25 19 24 24 20 23 18
11 | 8 12 4 10 13 3 10 11 9 11 3 | 35 41 34 32 48 36 41 40 39 34 35
12 | 8 26 6 17 18 5 24 13 10 13 5 | 28 36 25 27 33 24 36 25 30 24 25
13E | 7 12 3 10 11 3 14 13 7 9 3 | 20 23 18 17 29 18 24 21 23 17 18
14E | 7 14 5 9 15 3 11 15 8 17 3 | 25 28 22 23 24 21 24 19 23 20 21
15E | 9 16 4 10 15 4 18 14 9 9 4 | 30 30 28 31 32 28 30 34 32 27 28
16 | 8 22 4 15 17 5 16 14 9 16 4 | 21 34 24 27 34 25 29 25 31 23 24
17 | 7 11 5 10 17 5 13 12 11 18 3 | 21 24 17 17 34 20 26 21 26 21 18
18 | 7 15 5 13 13 3 17 10 8 24 3 | 23 29 21 27 28 22 27 22 28 21 21
19 | 7 14 4 12 14 4 14 15 10 20 3 | 18 27 18 17 31 19 27 19 26 19 18
20 | 8 14 4 13 11 6 13 9 10 17 3 | 24 29 22 25 29 26 28 25 26 21 23
21 | 6 9 3 8 10 4 10 10 7 23 2 | 18 26 19 21 25 19 24 20 27 20 20
22 | 8 13 4 12 13 3 13 10 8 22 3 | 26 29 23 28 32 27 28 23 32 25 24
23E | 9 14 6 10 11 4 15 13 11 13 4 | 19 22 19 22 25 18 22 22 22 22 18
24 | 12 13 5 10 16 4 11 9 10 10 3 | 24 26 22 21 29 19 30 21 25 23 21
25 | 11 16 4 10 14 4 12 13 10 17 4 | 22 28 19 16 24 18 26 21 21 18 18
26E | 15 19 6 12 16 5 14 14 10 29 4 | 56 50 50 55 45 52 49 58 47 41 50
X27 | 9 --- --- --- --- 39 --- --- --- --- 0 | 110 --- --- --- --- 101 --- --- --- --- 112
28 | 15 14 4 10 23 6 10 23 8 29 4 | 67 73 70 72 77 69 73 70 69 68 70
29 | 8 16 5 11 14 4 18 17 9 27 4 | 25 28 17 17 28 19 29 21 20 30 19
X30 | 8 --- --- --- --- 52 --- --- --- --- 0 | 58 --- --- --- --- 34 --- --- --- --- 58
31 | 6 14 4 8 15 4 14 8 7 16 3 | 21 27 21 21 33 20 26 19 25 18 20
32 | 9 9 3 8 12 3 7 9 10 12 3 | 21 27 17 17 24 19 25 19 24 23 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 4 11 14 4 13 14 9 19 |T 32 33 26 28 33 30 32 29 31 28 30
WRMS | 9 14 4 11 13 4 13 12 8 17 |NE 31 32 25 26 32 29 32 27 29 27 30
MEDI | 8 13 4 10 13 4 13 13 9 17 |MD 24 28 21 23 29 21 27 23 26 23 21
Table 3.1744.3 GPS week: 1744 Day: 3 MJD: 56455.000
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 5 8 9 2 16 9 13 13 3 | 33 41 38 35 47 34 44 38 38 29 37
2 | 5 11 7 15 11 3 10 15 7 22 3 | 17 19 16 25 19 16 17 23 15 15 15
3 | 10 13 5 6 14 5 15 8 14 14 3 | 73 74 76 71 79 73 76 71 72 82 73
X4 | 8 --- --- --- --- 55 --- --- --- --- 0 | 136 --- --- --- --- 80 --- --- --- --- 135
5 | 15 17 5 11 13 5 15 16 10 19 4 | 35 37 27 23 32 28 38 27 29 33 28
6 | 9 12 5 7 13 7 11 9 8 15 3 | 16 18 14 11 22 12 17 16 15 17 12
7 | 8 12 5 7 14 5 13 9 7 20 3 | 25 26 23 19 34 19 24 18 24 20 21
8 | 7 9 4 7 12 4 9 11 7 19 3 | 18 24 19 16 21 20 25 22 22 27 18
9 | 8 11 7 7 11 3 10 13 9 27 3 | 17 26 21 13 24 21 27 22 26 35 19
10 | 7 9 5 7 13 3 9 12 7 16 3 | 12 19 14 12 25 11 15 16 18 20 13
11 | 7 11 4 8 12 3 11 11 10 13 3 | 34 39 36 30 49 31 39 38 34 30 34
12 | 14 30 7 15 19 5 23 12 11 12 6 | 27 33 17 21 30 18 25 19 26 16 18
13E | 9 11 4 7 15 3 13 13 8 11 3 | 21 24 21 16 30 17 23 17 22 18 18
14E | 7 13 5 8 20 5 11 12 10 15 4 | 17 19 17 15 25 16 18 16 23 20 16
15E | 7 15 4 12 17 5 18 9 14 10 4 | 28 32 28 25 30 28 29 32 36 31 28
16 | 8 21 5 13 14 5 16 11 10 15 4 | 18 24 20 22 28 19 22 17 24 17 18
17 | 7 13 5 9 19 5 15 13 11 18 4 | 15 20 13 14 33 14 20 16 21 16 12
18 | 8 17 7 9 15 5 17 9 10 22 4 | 18 24 21 20 33 19 25 19 21 19 19
19 | 8 14 6 7 16 5 14 12 10 18 4 | 13 21 15 12 29 12 21 14 17 14 13
20 | 6 14 5 9 11 4 14 10 7 19 3 | 21 24 19 20 28 20 23 20 17 14 18
21 | 9 11 5 8 16 5 12 10 12 20 3 | 17 20 20 16 25 16 19 16 17 17 16
22 | 8 15 5 9 16 5 14 10 10 21 4 | 25 27 27 25 38 24 27 21 26 22 24
23E | 10 16 5 8 18 4 16 18 10 12 4 | 34 36 33 35 35 32 36 34 36 36 32
24 | 12 14 5 12 16 6 12 10 9 9 4 | 18 25 19 12 28 16 27 16 22 17 17
25 | 10 15 4 8 15 5 14 10 6 19 3 | 13 22 13 9 25 10 21 13 17 16 11
26E | 14 21 7 10 13 8 17 19 11 31 5 | 57 53 50 55 46 53 51 59 49 41 51
X27 | 8 --- --- --- --- 24 --- --- --- --- 0 | 150 --- --- --- --- 154 --- --- --- --- 152
28 | 9 11 4 6 12 5 10 12 7 21 3 | 36 42 37 35 44 38 42 39 38 37 37
29 | 9 18 5 12 16 5 18 13 9 26 4 | 15 20 9 14 21 10 23 16 13 26 10
X30 | 8 --- --- --- --- 27 --- --- --- --- 0 | 25 --- --- --- --- 19 --- --- --- --- 26
31 | 8 16 6 9 13 4 13 9 16 15 4 | 15 22 18 18 31 16 22 15 28 17 17
32 | 7 9 4 7 12 4 10 11 9 16 3 | 16 20 15 11 23 12 21 10 18 18 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 5 9 15 5 14 12 10 18 |T 31 28 24 22 32 28 28 24 26 24 30
WRMS | 9 15 5 9 15 4 13 11 9 16 |NE 32 27 22 20 31 28 27 22 24 23 30
MEDI | 8 13 5 8 14 5 14 11 10 18 |MD 18 24 20 19 30 19 24 19 23 20 18
Table 3.1744.4 GPS week: 1744 Day: 4 MJD: 56456.000
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 4 8 11 6 17 10 15 17 4 | 30 41 36 34 47 34 43 36 36 29 35
2 | 7 13 7 15 13 4 12 20 9 23 4 | 24 19 16 33 16 20 19 30 20 24 19
3 | 10 10 4 6 12 7 13 8 17 16 3 | 39 40 38 36 38 39 40 35 43 41 37
4 | 8 10 5 11 12 5 10 17 9 24 3 | 21 13 9 10 10 14 13 15 13 21 21
5 | 11 16 5 11 13 7 15 19 7 21 4 | 29 37 29 27 30 26 37 30 30 32 28
6 | 9 12 3 8 10 7 11 10 11 16 3 | 17 21 15 13 16 14 17 19 19 18 14
7 | 9 12 4 8 16 4 13 10 12 24 3 | 26 28 24 23 32 23 27 26 28 30 23
8 | 8 8 3 4 12 4 9 12 9 20 2 | 17 20 16 18 18 15 21 20 22 26 16
9 | 7 10 4 6 12 4 9 12 9 28 3 | 19 22 20 16 21 17 24 20 24 35 18
10 | 7 7 4 6 11 5 8 13 7 16 3 | 13 20 15 17 23 16 19 21 17 24 15
11 | 8 13 4 8 14 6 11 11 12 15 3 | 27 39 32 30 45 33 37 32 36 31 32
12 | 9 25 5 13 20 7 20 12 13 15 5 | 24 31 20 23 30 18 28 17 26 17 19
13E | 7 12 3 6 13 4 14 13 9 10 3 | 15 18 14 14 21 12 17 17 18 16 13
14E | 8 11 4 8 14 5 9 10 14 16 3 | 17 19 17 17 19 17 19 19 24 21 17
15E | 6 19 4 10 21 7 18 9 13 12 4 | 23 25 20 25 27 20 24 26 26 27 21
16 | 9 19 5 13 17 9 16 11 17 18 4 | 20 26 19 21 24 21 22 20 30 23 19
17 | 9 14 4 9 17 3 17 13 13 18 4 | 18 22 16 21 29 17 25 25 24 26 17
18 | 7 14 6 9 15 4 16 10 8 22 3 | 21 26 21 24 27 20 26 22 24 19 20
19 | 8 13 4 8 16 8 12 10 14 20 3 | 13 21 16 14 27 15 20 16 25 17 15
20 | 9 13 4 12 8 6 13 11 9 18 3 | 18 24 23 25 28 23 25 25 24 21 22
21 | 5 9 4 6 14 4 13 11 11 22 3 | 18 21 18 17 23 15 20 20 21 17 17
22 | 9 13 4 7 15 5 13 11 13 22 3 | 27 27 25 27 31 25 26 25 29 24 25
23E | 9 14 5 7 18 4 13 18 9 13 4 | 29 37 34 31 37 31 35 36 34 31 32
24 | 10 11 4 11 13 6 13 10 8 13 3 | 18 21 16 19 26 13 26 16 20 16 16
25 | 10 14 6 8 12 4 14 12 9 17 3 | 23 25 20 20 27 18 25 22 21 21 19
26E | 11 20 9 14 13 10 15 31 18 37 6 | 57 51 51 57 44 52 50 62 49 40 50
X27 | 8 --- --- --- --- 40 --- --- --- --- 0 | 122 --- --- --- --- 118 --- --- --- --- 124
28 | 6 10 3 7 20 4 9 13 10 23 3 | 26 30 27 25 39 26 31 28 31 28 26
29 | 15 16 5 12 16 4 18 11 12 26 4 | 19 20 14 18 20 13 23 21 16 29 14
X30 | 8 --- --- --- --- 88 --- --- --- --- 0 | 77 --- --- --- --- 25 --- --- --- --- 75
31 | 11 15 5 9 20 4 10 7 13 16 4 | 21 22 17 16 31 16 22 16 21 17 16
32 | 9 8 4 6 11 4 6 12 11 14 3 | 15 22 18 15 21 16 21 17 21 22 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 5 9 15 6 13 13 12 20 |T 27 26 21 22 27 24 26 24 25 24 26
WRMS | 9 14 5 9 14 5 13 11 10 19 |NE 27 25 20 21 26 24 25 22 24 24 26
MEDI | 9 13 4 8 13 5 13 11 11 18 |MD 21 22 19 21 27 18 24 21 24 24 19
Table 3.1744.5 GPS week: 1744 Day: 5 MJD: 56457.000
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 8 5 9 9 5 16 10 11 23 3 | 26 36 33 27 39 25 42 26 31 21 30
2 | 5 11 7 14 12 5 11 16 7 22 4 | 19 16 19 29 15 18 15 24 21 20 17
3 | 12 12 5 9 14 5 13 8 13 13 3 | 47 48 48 48 47 45 48 47 46 48 46
4 | 8 8 5 8 11 6 8 12 9 24 3 | 19 10 10 13 10 16 11 16 15 22 18
5 | 11 14 5 7 12 5 16 20 9 26 4 | 22 29 22 21 29 21 31 26 25 31 22
6 | 10 11 4 10 10 4 9 7 11 12 3 | 14 17 12 12 13 11 17 15 17 13 11
7 | 7 11 4 10 20 6 12 9 6 24 3 | 14 20 13 15 26 13 18 14 19 24 12
8 | 10 7 4 8 14 3 7 12 6 20 3 | 11 15 13 13 18 12 18 14 19 23 11
9 | 8 7 6 7 13 3 9 13 7 26 3 | 10 17 14 12 20 13 19 15 20 32 12
10 | 9 7 4 4 13 4 8 11 9 14 3 | 11 19 16 13 21 13 21 18 19 20 15
11 | 7 11 4 7 12 4 10 11 12 15 3 | 24 31 26 24 36 22 30 21 24 19 24
12 | 10 26 7 13 23 5 21 12 13 15 5 | 17 27 17 18 29 14 24 16 21 16 14
13E | 8 11 4 9 17 3 11 14 9 12 3 | 10 16 13 12 21 11 16 17 19 14 11
14E | 8 12 5 7 16 5 9 13 11 18 3 | 13 15 11 11 12 10 12 15 15 18 9
15E | 10 14 5 8 18 5 18 10 15 14 4 | 19 21 20 21 23 19 23 25 21 27 18
16 | 11 22 5 13 18 6 15 12 10 17 4 | 16 25 17 17 28 17 19 17 23 18 15
17 | 7 13 6 6 19 3 18 9 10 17 4 | 14 21 18 15 28 16 21 18 23 23 15
18 | 9 15 6 9 16 4 16 9 12 22 4 | 17 22 16 17 20 13 22 16 19 12 14
19 | 6 13 4 11 16 3 13 11 9 20 3 | 10 21 13 13 24 10 20 13 18 12 12
20 | 10 13 5 10 9 4 12 11 11 19 3 | 15 23 18 19 22 17 23 20 18 16 17
21 | 6 10 4 8 11 5 13 9 13 22 3 | 17 19 18 17 16 13 18 18 22 16 16
22 | 10 15 5 9 18 5 14 7 14 20 4 | 20 22 19 21 25 17 23 19 20 18 17
23E | 8 11 3 10 17 6 11 11 7 11 3 | 35 38 36 34 37 34 36 38 37 34 35
24 | 13 12 5 8 18 5 12 7 12 11 4 | 18 18 17 13 29 12 23 11 20 14 14
25 | 7 16 5 7 18 4 13 14 12 16 4 | 16 23 17 17 26 15 24 22 22 17 16
26E | 15 27 11 12 14 7 16 38 19 37 7 | 55 48 46 53 40 50 44 62 48 40 47
X27 | 7 --- --- --- --- 31 --- --- --- --- 0 | 113 --- --- --- --- 107 --- --- --- --- 116
28 | 9 11 4 7 24 5 10 8 6 17 3 | 21 28 27 23 42 26 29 23 31 24 25
29 | 10 18 5 8 14 4 17 11 11 27 4 | 17 21 13 15 19 12 23 19 14 25 13
X30 | 7 --- --- --- --- 88 --- --- --- --- 0 | 71 --- --- --- --- 13 --- --- --- --- 71
31 | 11 14 5 7 23 4 10 8 14 18 4 | 16 21 14 12 34 13 21 13 21 14 14
32 | 10 9 4 6 11 4 7 11 9 15 3 | 13 21 16 10 19 13 21 16 23 21 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 9 16 5 13 13 11 20 |T 23 23 19 19 25 20 23 21 23 21 23
WRMS | 10 14 5 9 14 4 12 10 9 20 |NE 23 22 18 18 24 19 23 19 21 20 23
MEDI | 9 12 5 8 14 5 12 11 11 18 |MD 17 21 17 17 24 14 21 18 21 20 15
Table 3.1744.6 GPS week: 1744 Day: 6 MJD: 56458.000
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 | 13 9 3 8 7 4 16 10 10 22 3 | 39 50 44 44 54 42 51 45 46 35 44
2 | 9 12 6 18 11 4 12 17 9 22 4 | 16 18 17 32 16 15 16 25 17 18 15
3 | 10 11 5 7 13 7 12 9 13 14 3 | 38 39 37 41 35 35 41 41 37 41 37
4 | 7 9 4 11 8 4 11 13 10 24 3 | 18 11 8 12 8 11 11 11 10 21 17
5 | 17 17 5 9 13 6 19 24 9 26 5 | 38 42 33 30 35 32 45 33 35 40 33
6 | 9 12 4 8 22 5 11 9 10 13 3 | 12 16 10 11 26 10 18 12 15 14 9
7 | 10 12 4 10 21 6 14 10 8 25 3 | 20 21 17 19 32 13 19 14 19 21 15
8 | 11 9 4 12 13 4 10 10 8 20 3 | 11 17 15 15 20 14 17 14 17 23 13
9 | 7 10 4 13 13 4 10 13 11 28 3 | 13 19 18 17 20 16 19 19 20 32 16
10 | 9 7 3 10 12 5 10 15 9 17 3 | 13 19 18 19 22 13 19 22 18 23 16
11 | 9 11 3 9 11 4 11 10 8 13 3 | 37 46 40 40 52 40 43 40 39 33 40
12 | 11 23 4 13 23 4 21 13 11 16 5 | 26 27 18 22 30 19 25 19 26 17 18
13E | 11 14 4 8 17 3 12 19 9 14 4 | 14 15 12 11 19 8 16 18 16 13 10
14E | 11 11 3 7 14 4 10 14 10 23 3 | 17 16 13 18 14 14 17 17 18 23 12
15E | 9 16 5 10 24 4 18 18 12 15 4 | 24 23 21 24 29 23 24 32 31 29 22
16 | 11 23 5 11 21 5 14 15 11 17 4 | 12 25 17 18 30 16 20 15 24 19 15
17 | 8 11 4 9 17 4 15 12 9 18 3 | 10 19 13 12 29 10 21 12 18 17 12
18 | 7 17 5 7 15 4 16 8 9 21 3 | 15 26 22 22 30 19 27 19 23 16 19
19 | 9 12 4 10 15 5 12 11 12 18 3 | 11 19 14 15 25 12 19 9 22 11 12
20 | 8 12 4 11 10 4 12 11 8 19 3 | 22 27 26 30 29 26 25 27 22 21 25
21 | 5 11 4 6 12 2 11 10 14 23 3 | 14 23 21 17 25 17 23 21 23 20 18
22 | 10 14 4 7 14 4 13 8 8 21 3 | 25 29 28 27 36 26 29 27 26 25 26
23E | 10 16 4 10 10 4 13 11 7 13 3 | 32 39 36 37 37 36 38 38 39 40 36
24 | 14 13 5 9 20 4 12 10 12 12 4 | 14 19 15 14 29 11 22 11 20 14 13
25 | 8 15 6 6 17 3 12 14 12 15 4 | 14 24 19 14 31 12 23 10 23 15 16
26E | 17 19 11 15 15 11 17 68 27 41 6 | 60 52 55 60 46 56 51 81 55 47 54
X27 | 7 --- --- --- --- 38 --- --- --- --- 0 | 132 --- --- --- --- 124 --- --- --- --- 134
28 | 7 11 3 13 24 4 10 8 8 20 3 | 24 31 27 30 42 28 30 27 33 30 27
29 | 16 15 4 7 14 2 18 11 10 27 4 | 16 21 12 15 21 14 26 15 19 28 13
X30 | 7 --- --- --- --- 35 --- --- --- --- 0 | 38 --- --- --- --- 24 --- --- --- --- 38
31 | 10 13 4 8 23 4 12 15 10 16 4 | 11 21 14 13 35 12 20 17 19 16 13
32 | 8 8 4 6 11 3 7 12 10 16 3 | 13 19 16 14 20 13 19 14 19 20 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 10 16 5 13 18 11 21 |T 24 25 21 23 29 23 25 23 24 24 25
WRMS | 10 14 4 9 12 4 13 11 9 19 |NE 24 24 20 21 28 23 25 20 23 22 25
MEDI | 9 12 4 9 14 4 12 11 10 18 |MD 16 21 18 18 29 16 22 19 22 21 16
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 4.1744 GPS week: 1744 MJD: 56452.0-56458.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 |U 7 8 17 |U 6 10 26 |U 8 7 16 |
emr | emr 2862 | 10 8 22 |U 9 16 33 | 9 8 20 |
esa | esa 2866 | 7 8 21 |U 5 8 21 | 8 7 16 |
gfz | gfz 2862 |U 7 8 21 |U 7 20 39 |U 8 7 16 |
grg | grg 2866 |U 11 13 33 |U 11 23 47 | 13 11 26 |
igr | igr 2866 | 7 8 21 | 5 8 22 | 7 7 16 |
igs | igs 2855 | 7 7 20 | 6 16 29 | 8 7 16 |
jpl | jpl 2862 | 8 8 23 | 7 19 37 | 9 8 19 |
mit | mit 2866 | 8 8 21 |U 6 17 31 |U 9 9 20 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1744.0 GPS week: 1744 Day: 0 MJD: 56452.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 | 11 8 19 | 4 8 29 | 9 7 12 |
emr | emr 2876 | 14 11 30 | 9 17 30 | 11 9 16 |
esa | esa 2880 | 11 8 27 | 4 6 23 | 10 7 13 |
gfz | gfz 2876 | 11 8 27 | 5 10 32 | 10 6 13 |
grg | grg 2880 | 13 13 36 | 13 19 48 | 16 12 27 |
igr | igr 2880 | 12 9 27 | 5 6 25 | 9 7 13 |
igs | igs 2878 | 11 9 27 | 5 18 31 | 10 7 13 |
jpl | jpl 2876 | 12 9 31 | 6 21 33 | 11 8 14 |
mit | mit 2880 | 11 9 27 | 5 17 28 | 11 9 21 |
Table 5.1744.1 GPS week: 1744 Day: 1 MJD: 56453.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 6 6 11 | 7 8 28 | 8 7 21 |
emr | emr 2876 | 7 6 15 | 9 17 24 | 9 7 25 |
esa | esa 2880 | 4 3 13 | 4 5 18 | 7 6 19 |
gfz | gfz 2876 | 3 4 13 | 5 16 44 | 7 5 18 |
grg | grg 2880 | 11 10 35 | 10 22 39 | 13 10 26 |
igr | igr 2880 | 3 3 13 | 4 5 20 | 7 6 19 |
igs | igs 2878 | 3 3 12 | 6 22 30 | 7 6 20 |
jpl | jpl 2876 | 5 4 15 | 6 26 33 | 8 8 24 |
mit | mit 2880 | 4 5 12 | 4 18 27 | 8 8 20 |
Table 5.1744.2 GPS week: 1744 Day: 2 MJD: 56454.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 6 10 17 | 6 10 29 | 5 5 15 |
emr | emr 2876 | 10 8 25 | 10 13 35 | 8 7 22 |
esa | esa 2880 | 7 9 24 | 6 7 29 | 6 5 18 |
gfz | gfz 2877 | 7 9 23 | 6 23 45 | 7 5 17 |
grg | grg 2880 | 10 17 29 | 9 16 35 | 13 11 30 |
igr | igr 2880 | 7 10 24 | 6 6 29 | 6 5 16 |
igs | igs 2878 | 7 8 23 | 6 15 35 | 6 6 18 |
jpl | jpl 2876 | 8 10 29 | 6 18 34 | 7 6 21 |
mit | mit 2880 | 15 13 33 | 6 16 36 | 9 7 20 |
Table 5.1744.3 GPS week: 1744 Day: 3 MJD: 56455.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2950 | 5 8 15 | 6 11 20 | 9 8 18 |
emr | emr 2780 | 8 7 16 | 12 18 37 | 11 8 19 |
esa | esa 2784 | 6 8 19 | 6 10 17 | 10 7 17 |
gfz | gfz 2780 | 6 8 17 | 8 25 41 | 10 7 17 |
grg | grg 2783 | 7 9 21 | 14 21 42 | 13 9 22 |
igr | igr 2784 | 5 9 18 | 6 10 15 | 9 7 19 |
igs | igs 2782 | 6 7 16 | 8 18 36 | 10 7 16 |
jpl | jpl 2780 | 7 8 19 | 9 19 47 | 10 8 19 |
mit | mit 2784 | 5 8 16 | 8 20 39 | 10 8 18 |
Table 5.1744.4 GPS week: 1744 Day: 4 MJD: 56456.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 8 10 25 | 5 8 22 | 6 8 17 |
emr | emr 2876 | 12 14 30 | 8 15 29 | 9 11 22 |
esa | esa 2880 | 11 12 31 | 4 7 17 | 6 9 17 |
gfz | gfz 2876 | 11 12 33 | 7 19 42 | 8 11 17 |
grg | grg 2880 | 15 20 49 | 10 34 70 | 10 11 30 |
igr | igr 2880 | 11 12 30 | 5 8 18 | 6 10 18 |
igs | igs 2880 | 11 12 30 | 6 18 28 | 6 9 17 |
jpl | jpl 2876 | 11 13 27 | 6 18 33 | 7 11 21 |
mit | mit 2880 | 9 10 30 | 6 17 30 | 8 11 25 |
Table 5.1744.5 GPS week: 1744 Day: 5 MJD: 56457.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 6 6 16 | 6 12 26 | 7 6 10 |
emr | emr 2876 | 8 6 17 | 10 14 37 | 7 7 14 |
esa | esa 2880 | 5 5 15 | 7 11 23 | 7 7 12 |
gfz | gfz 2876 | 6 5 16 | 7 25 37 | 8 6 11 |
grg | grg 2880 | 8 13 30 | 11 27 60 | 13 16 26 |
igr | igr 2880 | 5 5 16 | 6 10 24 | 7 6 11 |
igs | igs 2840 | 5 5 14 | 7 10 22 | 7 7 12 |
jpl | jpl 2876 | 7 6 18 | 7 16 36 | 7 5 14 |
mit | mit 2880 | 5 7 14 | 7 16 25 | 10 11 14 |
Table 5.1744.6 GPS week: 1744 Day: 6 MJD: 56458.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 7 8 15 | 7 11 27 | 8 6 18 |
emr | emr 2876 | 10 9 20 | 9 17 36 | 9 8 23 |
esa | esa 2880 | 9 8 20 | 6 10 21 | 8 6 18 |
gfz | gfz 2876 | 9 8 18 | 8 23 35 | 8 7 17 |
grg | grg 2879 | 10 12 34 | 10 21 36 | 11 8 22 |
igr | igr 2879 | 9 8 20 | 6 10 21 | 9 7 18 |
igs | igs 2849 | 9 7 18 | 7 9 22 | 9 7 18 |
jpl | jpl 2874 | 9 7 21 | 9 19 44 | 9 7 24 |
mit | mit 2880 | 8 6 16 | 8 16 30 | 9 7 20 |
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 6.1744 GPS week: 1744 MJD: 56452.500-56458.500
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 -24 -52 -74 -3 | 6 21
| 10 13 57 88 3 | 4
emr uuuuu | 40 30 -47 39 -3 | 26 34
| 14 19 59 88 7 | 4
esa uuuuu | -9 -11 28 -13 -6 | 16 25
| 14 10 32 69 4 | 3
gfz uuuuu | 9 7 55 -29 2 | 9 21
| 19 10 37 57 2 | 3
grg uuuux | 7 -27 99 -163 -9 | -1 31
| 29 19 40 79 40 | 8
igr xxxxx | -3 -5 53 22 2 | 3 20
| 28 12 45 61 5 | 4
irf xxxxx | 6 5 -43 -12 4 | 4 20
| 15 7 21 36 3 | 3
jpl uuuuu | 47 -15 64 124 -8 | 31 38
| 22 25 84 61 7 | 5
mit uuuuu | 8 4 -191 65 10 | 18 27
| 31 18 57 74 4 | 4
ngs uuuuu | -26 47 11 44 2 | 12 20
| 52 27 108 102 5 | 3
sio xxxxx | 155 123 -122 145 8 | 33 38
| 62 38 100 48 4 | 3
Table 7.1744.0 GPS week: 1744 Day: 0 MJD: 56452.500
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 -2 -58 -199 3 | 3 20
emr uuuuu | 40 13 35 150 -5 | 28 35
esa uuuuu | -14 -16 0 -85 -3 | 15 24
gfz uuuuu | 33 -1 26 -13 2 | 6 20
grg uuuux | 9 -20 116 -84 -20 | -11 42
igr xxxxx | -21 5 61 71 8 | -2 19
irf xxxxx | 18 8 -57 58 9 | 0 17
jpl uuuuu | 65 18 150 68 -3 | 32 39
mit uuuuu | 35 18 -194 216 12 | 12 21
ngs uuuuu | -82 7 -12 83 -7 | 8 17
sio xxxxx | 228 194 -179 219 9 | 28 33
Table 7.1744.1 GPS week: 1744 Day: 1 MJD: 56453.500
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 | -26 -43 45 -108 -2 | 4 21
emr uuuuu | 28 18 -108 120 1 | 25 31
esa uuuuu | -32 -5 51 -75 -7 | 15 23
gfz uuuuu | 26 1 77 18 4 | 6 20
grg uuuux | 37 -67 157 -131 -18 | -13 42
igr xxxxx | -30 -8 -15 124 2 | -1 20
irf xxxxx | 2 5 -70 2 3 | 1 19
jpl uuuuu | 82 -4 -11 230 -6 | 31 37
mit uuuuu | -3 34 -242 34 4 | 13 23
ngs uuuuu | -25 56 -46 41 1 | 9 17
sio xxxxx | 170 153 -276 115 0 | 29 34
Table 7.1744.2 GPS week: 1744 Day: 2 MJD: 56454.500
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 | -35 -17 -65 -130 -1 | 13 22
emr uuuuu | 67 5 26 92 -10 | 32 38
esa uuuuu | -6 -8 25 -72 -10 | 23 28
gfz uuuuu | 23 16 48 -67 2 | 14 24
grg uuuux | 51 -10 53 -121 38 | -2 31
igr xxxxx | -46 -11 54 -1 -7 | 8 20
irf xxxxx | 30 -9 -27 -27 5 | 9 21
jpl uuuuu | 57 -47 -48 176 -22 | 39 43
mit uuuuu | 38 -4 -179 64 14 | 22 30
ngs uuuuu | -99 57 64 196 7 | 16 23
sio xxxxx | 222 88 -105 114 11 | 37 42
Table 7.1744.3 GPS week: 1744 Day: 3 MJD: 56455.500
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 | -23 -27 -92 -73 -3 | 10 20
emr uuuuu | 48 29 -61 26 -12 | 29 36
esa uuuuu | -11 5 7 9 -8 | 19 25
gfz uuuuu | -6 -5 10 -100 6 | 12 22
grg uuuux | -5 -17 54 -101 53 | 6 26
igr xxxxx | 11 -28 101 17 2 | 5 20
irf xxxxx | 10 5 -53 -19 5 | 7 20
jpl uuuuu | 43 -45 144 83 -11 | 34 40
mit uuuuu | 44 -16 -192 70 12 | 21 29
ngs uuuuu | -39 59 157 87 4 | 15 22
sio xxxxx | 182 122 -136 183 9 | 35 39
Table 7.1744.4 GPS week: 1744 Day: 4 MJD: 56456.500
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 | -15 -32 -11 8 -5 | 5 21
emr uuuuu | 38 42 -100 27 2 | 24 35
esa uuuuu | -18 -12 -8 8 -9 | 15 25
gfz uuuuu | 4 3 44 -59 1 | 9 22
grg uuuux | -26 -27 127 -171 -17 | 7 26
igr xxxxx | 18 0 114 14 4 | 2 21
irf xxxxx | 0 9 -52 -12 5 | 4 21
jpl uuuuu | 28 -25 130 119 -8 | 28 37
mit uuuuu | 0 5 -267 69 14 | 18 27
ngs uuuuu | 33 76 122 -34 4 | 12 21
sio xxxxx | 72 99 -160 177 13 | 32 37
Table 7.1744.5 GPS week: 1744 Day: 5 MJD: 56457.500
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 | -38 -25 -50 -85 -3 | 4 20
emr uuuuu | 27 55 -29 -64 -1 | 22 32
esa uuuuu | 4 -14 80 105 0 | 13 24
gfz uuuuu | -17 14 55 -50 3 | 8 21
grg uuuux | 9 -26 69 -300 -49 | 2 24
igr xxxxx | 20 7 23 -68 5 | 3 21
irf xxxxx | -11 14 -9 -55 1 | 4 21
jpl uuuuu | 32 4 -6 67 -4 | 26 35
mit uuuuu | -36 5 -89 -17 7 | 19 28
ngs uuuuu | 32 11 -147 65 -1 | 12 21
sio xxxxx | 93 93 27 107 5 | 33 39
Table 7.1744.6 GPS week: 1744 Day: 6 MJD: 56458.500
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 | -40 -18 -131 68 -6 | 5 21
emr uuuuu | 30 48 -92 -78 7 | 22 32
esa uuuuu | 11 -26 44 21 -3 | 14 25
gfz uuuuu | 0 20 125 69 0 | 10 22
grg uuuux | -26 -22 114 -237 -50 | 1 26
igr xxxxx | 25 -1 30 -3 -3 | 4 22
irf xxxxx | -7 6 -30 -32 2 | 5 21
jpl uuuuu | 25 -5 90 123 -3 | 25 34
mit uuuuu | -20 -14 -172 18 7 | 21 30
ngs uuuuu | -3 65 -58 -128 4 | 13 22
sio xxxxx | 121 112 -25 96 7 | 35 41
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