[IGSREPORT-22701] Wk 1788 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat May 3 07:30:28 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1788 (Apr 13, 2014 - Apr 19, 2014)
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:
igs1788[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1788[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1788[0-6].cls IGS GPS clock combination summary report.
igs17887.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17887.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 | MAC1 MAL2
0 | EMR | 32 32
0 | ESA | UNSA
0 | GFZ | 1 2 1
0 | GRG | 32 KELY MAL2 MAW1 KELY MAL2 MAW1
0 | JPL | 10 32
0 | MIT | 10 10 32 HLFX MDVJ WUHN BRFT MDVJ XMIS
1 | COD | BRAZ
1 | EMR | 32 32 MCM4 USNO YAKT
1 | ESA | UNSA
1 | GFZ | 1 2 1 32
1 | GRG | 32 BRAZ NTUS TRO1 BRAZ HYDE KELY NTUS NYAL TRO1
1 | JPL | 22 28 32
1 | MIT | 23 23 32 HYDE YELL GOPE HYDE MDVJ YELL
2 | COD | REUN
2 | EMR | 32 32
2 | ESA | INVK PIMO INVK PIMO SEY1 UNSA
2 | GFZ | 1 2 1 32 NTUS BAKO NTUS
2 | GRG | 32 32 ARTU DARW GUUG MAL2 NTUS WUHN ARTU DARW GUUG
2 | GRG | LPGS MAL2 NTUS PIMO WUHN
2 | JPL | 32
2 | MIT | 28 32 MDVJ
3 | COD | 32
3 | ESA | 32 CHUM
3 | GFZ | 1 1 13 32 CHUM
3 | GRG | FAA1 GRAZ KELY MAL2 FAA1 GRAZ MAL2 NTUS
3 | JPL | 10 32
3 | MIT | 13 24 13 24 32 BAKO BAKO
4 | COD | 32
4 | EMR | TSKB TSKB
4 | ESA | 32 NTUS SEY1 NTUS UNSA
4 | GFZ | 1 2 1
4 | GRG | ALRT NTUS WUHN ALRT HYDE NTUS WUHN
4 | JPL | 8 32
4 | MIT | ALRT HYDE ALRT HYDE MDVJ
5 | COD | 32
5 | ESA | 32
5 | GFZ | 1 2 1 WUHN WUHN
5 | GRG | PIMO
5 | MIT | 31 31 CAS1 CAS1 MDVJ
6 | COD | 32
6 | EMR | WUHN YAKT
6 | ESA | 32
6 | GFZ | 1 1
6 | GRG | WUHN DARW MONP SPT0 WUHN
6 | JPL | 10
6 | MIT | MDVJ
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
----+------------+----------
G31 | 2014_04_15 | 2014037
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
----+--------+---------------
0 | GRG | 6
2 | GRG | 6
3 | GRG | 6
4 | GRG | 6
5 | GRG | 6
8. 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.
9. 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 | -.6 1.3 -.3 -25 6 -20 .69
EMR | 0 | -6.9 .1 18.7 -3 16 -53 .54
ESA | 0 | 2.7 -2.7 24.2 -34 -62 32 .15
GFZ | 0 | -1.0 .6 -1.2 -17 -21 -1 .29
GRG | 0 | .4 -5.5 9.3 -16 -1 -20 1.03
JPL | 0 | -.4 -4.7 21.9 -43 -10 -2 .13
MIT | 0 | 1.1 -4.5 21.2 45 -20 39 .69
NGS | 0 | -4.8 -4.9 19.9 -80 11 -27 .81
SIO | 0 | -.2 3.1 19.6 -4 -62 21 .65
COD | 1 | -1.1 .4 -.7 -30 5 -11 .70
EMR | 1 | .6 3.2 25.4 -10 10 -44 .56
ESA | 1 | 4.0 2.1 24.0 17 -40 21 .35
GFZ | 1 | .4 .1 -.6 -23 -27 5 .01
GRG | 1 | -2.3 .2 13.8 -3 -10 -18 1.03
JPL | 1 | .6 -1.3 24.6 -20 -10 -60 -.03
MIT | 1 | -.7 -2.3 21.3 -2 -27 -7 .63
NGS | 1 | 2.3 -6.0 24.9 -100 -43 -7 .65
SIO | 1 | -.6 4.6 23.0 5 -64 -13 .80
COD | 2 | -.6 .3 -1.6 -28 16 -60 .62
EMR | 2 | .9 1.4 14.5 -2 22 -48 .74
ESA | 2 | 5.2 3.6 29.0 52 -78 20 .55
GFZ | 2 | 1.3 .5 -1.6 -16 -37 3 .10
GRG | 2 | 5.5 -8.0 23.0 -10 19 -44 1.06
JPL | 2 | 7.1 -4.0 24.0 13 75 12 -.16
MIT | 2 | 4.5 -4.1 19.0 0 -31 -27 .72
NGS | 2 | 7.0 -11.2 27.2 -127 -66 -8 .72
SIO | 2 | .1 6.2 33.9 58 -8 102 .46
COD | 3 | -2.0 .4 -2.0 -28 23 -37 .70
EMR | 3 | .9 -5.6 24.4 -1 18 -45 .70
ESA | 3 | 4.3 4.2 20.9 87 -95 38 .54
GFZ | 3 | .4 .2 -1.2 -21 -37 3 .19
GRG | 3 | 2.5 -.8 20.2 -4 31 -16 1.10
JPL | 3 | 3.3 -2.4 25.8 -99 -11 31 .68
MIT | 3 | 3.6 -6.2 24.2 4 27 -75 .70
NGS | 3 | 6.1 -2.9 19.5 -57 -59 10 1.06
SIO | 3 | -1.6 -2.3 30.6 -40 -13 -68 .51
COD | 4 | -1.9 .7 -2.8 -10 13 -33 .67
EMR | 4 | -2.2 -4.3 16.5 0 23 -48 .71
ESA | 4 | 5.6 1.1 22.3 72 -53 15 .56
GFZ | 4 | .1 -.1 -1.6 -12 -29 -20 .10
GRG | 4 | .7 -10.9 5.7 7 25 1 .93
JPL | 4 | 1.4 3.2 19.4 -31 -35 14 .62
MIT | 4 | 1.6 -8.0 20.8 -16 19 -138 .69
NGS | 4 | 8.2 -16.6 20.2 -122 -64 -21 1.00
SIO | 4 | -4.5 .4 28.7 -38 38 -233 .38
COD | 5 | .1 1.0 -2.3 -9 -9 -31 .73
EMR | 5 | -.5 1.4 23.0 0 26 -52 .63
ESA | 5 | 9.5 7.9 27.9 102 -171 78 .50
GFZ | 5 | -.1 .0 -1.7 -5 -29 -7 .18
GRG | 5 | 6.1 -6.9 3.9 13 7 13 .97
JPL | 5 | 5.9 2.0 17.8 -20 29 -21 .48
MIT | 5 | 1.3 -2.8 20.1 4 -5 -30 .77
NGS | 5 | 2.8 -9.5 27.4 -106 -48 -15 .89
SIO | 5 | -.2 5.6 19.1 64 35 -89 .47
COD | 6 | .0 .7 -1.1 -14 3 -9 .81
EMR | 6 | 3.7 -6.8 24.3 4 17 -36 .56
ESA | 6 | 2.9 3.4 28.1 33 -66 34 .30
GFZ | 6 | .5 .1 -1.2 -1 -33 -1 -.01
GRG | 6 | -.8 -10.4 12.8 -26 17 -21 .74
JPL | 6 | 11.0 -6.2 21.0 -6 -9 4 .21
MIT | 6 | .3 -5.3 23.3 93 27 3 .63
NGS | 6 | 4.8 -12.4 24.0 -134 -80 -31 .41
SIO | 6 | 3.5 4.9 45.9 -11 72 4103 .34
10. 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.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; 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 1.1788.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1788.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 2.1788.[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 3.1788.[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 5.1788.0-6). 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 1788 summary. (Apr 13, 2014 - Apr 19, 2014)
Table 1.1788.a GPS week: 1788 MJD: 56760.000-56766.000
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 244| 0 0 -1 0 15 0 .11 10 9 | -970 34 19 109
| 0 0 2 19 21 16 .03 | 163 340
emr 79| -1 1 2 -25 -9 -1 .24 15 15 | 2483 -565 17 141
| 1 1 0 11 20 15 .03 | 1391 969
esa 150| 1 0 -1 34 -48 -2 -.23 6 6 | -1504 744 10 147
| 0 0 0 30 33 14 .02 | 1647 1299
gfz 200| 0 0 -3 9 32 19 .12 11 11 | 234 -141 12 125
| 0 1 1 24 31 17 .03 | 494 866
grg 175| -1 -2 6 -18 25 -11 .39 18 17 | -33 -144 17 158
| 2 2 4 27 17 36 .15 | 330 804
igr n/a| 0 0 -3 -30 20 -1 -.20 6 6 | 5385 -456 17 78
| 0 0 0 32 31 17 .01 | 924 1048
jpl 80| 0 3 -6 -16 -1 22 .01 16 16 | 2267 -441 19 155
| 1 2 1 16 32 27 .04 | 1039 1043
mit 300| 0 -1 7 30 4 -2 -.27 15 14 | -41 -261 23 215
| 0 0 1 58 38 52 .04 | 236 658
ngs 230| -1 0 4 -65 39 -23 .07 13 11 | -20799 -2387 1885 3352
| 0 1 2 56 44 19 .03 | 33992 4232
sio 436| -1 2 -9 -29 -15 540 -.46 22 20 | --- --- --- ---
| 1 1 0 24 25 1548 .07 | --- ---
Table 1.1788.b GPS week : 1788 MJD: 56760.000-56766.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 3 4 4 4 4 |
2 | 5 5 5 5 5 5 5 |
3 | 4 4 3 4 4 4 4 |
4 | 4 4 4 4 4 4 5 |
5 | 5 5 5 6 5 6 6 |
6 | 0 0 0 0 0 0 0 |
7 | 5 4 4 4 4 5 5 |
8 | 4 4 3 3 4 4 5 |
9 | 4 4 3 3 4 4 5 |
10 | 8 7 7 6 7 6 7 |
11 | 4 4 4 4 4 4 4 |
12 | 6 6 7 6 6 6 6 |
13 | 5 5 5 5 5 5 4 |
14 | 4 4 4 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 6 5 5 4 6 6 |
17 | 5 5 5 5 5 5 5 |
18 | 4 4 4 4 4 5 5 |
19 | 4 4 4 4 4 4 5 |
20 | 5 5 5 5 5 5 5 |
21 | 4 5 5 5 5 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 6 6 5 6 6 6 6 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 5 4 4 |
26 | 4 4 4 4 4 5 5 |
27 | 5 4 4 5 5 4 5 |
28 | 3 4 3 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 0 0 0 0 14 12 0 |
31 | 5 5 0 6 5 6 6 |
32 | 5 6 6 6 5 5 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1788.0 GPS week: 1788 Day: 0 MJD: 56760.000
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 248| 0 0 2 19 40 11 .08 9 9 | -753 -56 25 120
emr 80| -3 1 1 -37 9 -22 .29 14 14 | 4018 398 14 132
esa 150| 1 0 -1 -13 -44 0 -.24 6 6 | -2975 1402 9 153
gfz 203| 0 -2 -4 10 29 -10 .10 11 10 | -254 1057 11 120
grg 186| -2 -2 8 8 10 -30 .44 19 17 | -136 65 16 140
igr n/a| 0 0 -3 -1 36 -1 -.21 5 5 | 6596 387 17 70
jpl 80| 0 2 -5 -6 4 25 .09 14 14 | 3586 513 19 172
mit 300| 0 -1 6 115 1 62 -.29 18 15 | -144 -7 24 236
ngs 232| -1 1 0 -42 -8 -37 .07 13 11 | -743 -46 1935 3392
sio 507| 0 3 -9 2 2 97 -.39 22 21 | --- --- --- ---
Table 2.1788.1 GPS week: 1788 Day: 1 MJD: 56761.000
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 249| 1 0 0 -3 -8 2 .09 11 10 | -1088 482 20 117
emr 80| -1 2 0 -14 7 -5 .26 15 15 | 4733 -986 17 135
esa 150| 1 0 -1 25 -14 -1 -.26 6 6 | -1814 1869 10 177
gfz 201| 0 0 -4 10 33 11 .11 11 10 | 151 418 12 127
grg 188| -2 -2 6 0 1 -47 .36 15 14 | -164 365 16 144
igr n/a| 0 0 -4 -18 10 0 -.21 5 5 | 6827 -973 17 90
jpl 80| 0 6 -7 -1 16 -20 -.01 16 17 | 3848 -936 20 172
mit 300| -1 0 6 12 -16 25 -.30 16 15 | 55 -112 25 223
ngs 235| -2 0 3 -40 13 5 .08 12 9 | -945 380 1623 3498
sio 512| -2 2 -9 -41 -37 -29 -.42 22 20 | --- --- --- ---
Table 2.1788.2 GPS week: 1788 Day: 2 MJD: 56762.000
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 248| 0 0 -3 3 42 -25 .10 10 10 | -1052 -83 19 105
emr 80| -1 1 2 -20 -16 -10 .22 16 15 | 2719 -572 14 128
esa 150| 1 0 -1 68 -36 11 -.21 6 6 | -1367 315 11 170
gfz 201| 0 0 -3 48 9 30 .14 11 10 | 408 -969 13 129
grg 186| 1 0 9 -29 29 -15 .24 15 15 | -308 282 18 162
igr n/a| 0 0 -4 -14 16 7 -.21 5 5 | 5210 -115 16 64
jpl 80| -1 4 -5 -5 16 8 .01 15 15 | 2273 -178 17 147
mit 300| 0 -1 5 1 -46 4 -.24 15 13 | -300 113 20 211
ngs 232| -2 -2 4 -163 25 -14 .13 12 10 | -865 -124 1788 3141
sio 490| -2 3 -9 -4 -15 50 -.41 23 21 | --- --- --- ---
Table 2.1788.3 GPS week: 1788 Day: 3 MJD: 56763.000
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 239| 0 0 0 -20 -7 9 .12 9 8 | -896 -212 21 104
emr 80| 0 0 3 -43 -39 17 .24 15 15 | 1752 -979 17 150
esa 150| 0 0 -1 53 -69 -2 -.21 6 6 | -4157 2585 10 129
gfz 201| 0 0 -1 -7 8 40 .15 11 11 | -560 552 12 120
grg 138| 2 2 -1 -41 38 -47 .20 16 15 | 36 -292 16 144
igr n/a| 0 0 -2 -8 36 8 -.21 6 6 | 4823 -827 17 74
jpl 80| 1 1 -7 -47 -16 34 -.03 17 17 | 1755 -641 18 177
mit 300| 0 -2 8 -11 73 -24 -.21 14 13 | 110 -450 22 193
ngs 233| 0 -1 3 17 132 -21 .05 13 11 | -843 -218 2000 3409
sio 389| 0 0 -10 -73 22 -67 -.57 22 20 | --- --- --- ---
Table 2.1788.4 GPS week: 1788 Day: 4 MJD: 56764.000
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 237| 0 0 -1 -28 7 25 .08 10 10 | -788 -438 20 109
emr 80| 0 0 1 -30 -28 20 .24 15 15 | 1422 -1839 19 157
esa 150| 1 1 -2 51 -20 -32 -.23 7 6 | 500 -451 11 137
gfz 199| 0 0 -1 -4 12 32 .13 11 12 | 708 -1120 14 142
grg 180| 0 -2 3 12 47 49 .35 15 14 | 388 -1208 15 150
igr n/a| 0 1 -3 -77 -27 23 -.20 7 6 | 4780 -1828 18 93
jpl 80| -1 3 -6 -29 -44 69 -.02 17 17 | 1608 -1879 21 151
mit 300| 0 -2 6 44 -18 -99 -.31 14 15 | 14 -1063 26 219
ngs 232| -2 -2 3 -58 29 -17 .05 13 11 | -68039 -8418 1856 3134
sio 387| -2 1 -9 -24 -54 -192 -.47 22 19 | --- --- --- ---
Table 2.1788.5 GPS week: 1788 Day: 5 MJD: 56765.000
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 239| 1 1 -2 3 29 -6 .11 10 9 | -1015 81 16 99
emr 79| -1 3 2 -19 15 -9 .25 16 16 | 1418 -1008 20 140
esa 150| 1 0 -2 54 -112 7 -.21 7 7 | 50 -1102 11 129
gfz 199| 0 0 -4 32 100 24 .08 12 11 | 793 -924 13 124
grg 178| -2 -3 9 -23 11 22 .52 20 18 | 405 -1172 19 174
igr n/a| 0 0 -5 -78 71 -11 -.19 8 8 | 4813 -1126 20 80
jpl 80| -1 0 -6 -11 47 8 .02 16 15 | 1539 -1162 19 138
mit 300| 0 0 8 -47 11 -15 -.28 15 15 | 320 -1068 24 202
ngs 223| -1 0 8 -103 47 -23 .09 14 13 | -72991 -8726 2104 3456
sio 384| 0 2 -9 -35 -25 -118 -.53 23 18 | --- --- --- ---
Table 2.1788.6 GPS week: 1788 Day: 6 MJD: 56766.000
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 251| 0 0 -4 25 4 -13 .17 9 9 | -1198 465 18 109
emr 80| 0 0 2 -16 -12 2 .21 16 16 | 1325 1030 23 146
esa 150| 2 0 -1 1 -41 3 -.22 7 7 | -770 591 10 140
gfz 198| 0 0 -3 -22 30 6 .15 11 11 | 393 -1 12 114
grg 173| -2 -6 13 -60 38 -15 .63 29 25 | -454 948 23 193
igr n/a| 0 0 -4 -16 3 -31 -.18 8 8 | 4651 1285 20 81
jpl 80| 0 3 -4 -16 -32 27 .01 17 16 | 1261 1195 19 134
mit 300| -1 -1 7 94 27 33 -.24 15 15 | -345 760 21 221
ngs 228| 0 0 6 -69 35 -56 .04 13 11 | -1172 437 1892 3437
sio 385| 0 2 -8 -30 -2 4046 -.41 23 20 | --- --- --- ---
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 3.1788.0 GPS week: 1788 Day: 0 MJD: 56760.000
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 9 5 10 14 5 13 10 10 15 3 | 25 30 20 25 30 22 33 17 26 32 23
2 | 8 16 8 12 16 4 17 14 13 24 4 | 27 32 30 34 42 29 28 28 35 22 30
3 | 8 7 5 11 19 5 7 12 18 29 4 | 22 24 18 23 30 18 21 23 19 33 21
4 | 9 10 5 7 24 4 8 9 7 27 3 | 23 24 24 25 43 21 21 28 24 32 25
5E | 8 17 7 11 15 4 18 22 10 15 4 | 36 37 34 33 38 34 35 24 32 25 34
X6E | 3 --- --- --- 618 64 --- --- --- --- 0 | 57 --- --- --- 170 47 --- --- --- --- 57
7 | 10 14 6 12 20 4 10 13 17 17 4 | 25 30 20 29 36 22 26 18 25 27 23
8 | 7 10 5 10 27 3 9 14 12 22 4 | 16 24 13 18 31 15 23 21 18 28 17
9 | 7 10 4 8 23 4 10 13 11 27 3 | 20 27 18 22 34 19 25 24 17 35 20
10E | 19 18 7 17 19 6 16 52 14 13 7 | 60 60 59 61 59 58 57 55 59 59 58
11 | 8 8 5 12 17 4 9 13 13 11 3 | 44 53 45 50 61 44 48 51 44 43 47
12E | 11 20 7 12 29 7 27 14 12 18 6 | 23 27 18 26 30 17 25 21 25 18 20
13 | 14 16 6 14 20 3 13 23 7 17 5 | 33 38 33 44 48 34 39 38 30 39 35
14 | 9 17 4 10 13 7 13 14 15 20 4 | 36 36 39 48 44 39 36 36 35 35 38
15 | 8 19 7 11 14 5 16 13 17 22 4 | 23 33 19 25 31 18 23 22 23 19 21
16E | 7 14 6 13 21 5 18 15 13 20 4 | 25 27 21 22 34 19 26 18 26 18 22
17 | 8 17 9 10 17 4 20 12 12 26 4 | 36 40 38 36 45 33 32 41 34 28 36
18E | 7 14 5 9 19 5 13 14 13 18 4 | 23 23 21 23 22 18 20 23 22 20 20
19 | 8 12 5 13 15 5 13 9 14 21 4 | 28 34 27 34 35 25 28 33 26 25 29
20E | 8 14 7 11 21 5 15 16 12 16 4 | 23 27 21 21 29 20 26 24 25 32 22
21 | 7 16 7 9 17 7 18 17 8 20 4 | 29 30 29 32 42 28 25 29 26 27 28
22E | 8 11 5 10 17 7 14 11 13 24 4 | 19 18 19 19 21 16 18 17 17 29 17
23 | 11 15 6 15 17 6 14 32 10 29 5 | 27 36 30 41 39 30 33 36 30 37 30
24 | 8 14 7 9 15 7 11 9 13 17 4 | 27 32 24 30 32 23 31 23 22 31 26
25E | 8 15 7 7 21 5 11 17 12 14 4 | 25 32 20 24 33 20 28 23 27 19 24
26 | 9 12 6 8 24 4 11 9 10 31 4 | 31 25 32 33 41 28 27 27 25 40 29
X27 | 7 6 3 15 --- 5 11 14 18 10 4 | 39 41 37 42 --- 36 41 46 33 35 39
28E | 6 8 5 7 13 4 13 8 12 12 3 | 16 19 16 20 26 14 16 19 19 15 16
29 | 8 19 7 9 18 5 18 19 12 30 5 | 34 36 32 38 43 31 31 38 33 40 33
X30 | 3 --- --- --- --- 15 --- --- --- --- 0 | 34 --- --- --- --- 34 --- --- --- --- 34
31 | 8 16 6 10 15 5 11 21 15 17 4 | 26 26 14 19 23 19 17 14 28 14 23
32E | 15 13 7 11 14 5 15 24 14 30 5 | 70 71 67 76 72 68 73 75 71 81 70
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 6 11 19 5 14 18 13 22 |T 30 33 27 32 42 28 30 29 29 31 30
WRMS | 9 14 6 10 17 5 14 15 11 21 |NE 28 32 27 32 38 27 29 29 27 31 28
MEDI | 8 14 6 10 17 5 13 14 12 20 |MD 27 30 24 29 35 23 27 24 26 29 26
Table 3.1788.1 GPS week: 1788 Day: 1 MJD: 56761.000
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 11 5 9 11 4 15 9 13 17 3 | 22 30 20 28 28 19 29 17 25 28 22
2 | 9 19 9 14 13 5 21 12 9 31 5 | 21 28 22 25 26 18 24 21 26 21 21
3 | 8 8 4 9 14 3 11 11 13 30 3 | 20 19 15 20 24 16 19 19 18 32 17
4 | 13 13 6 9 16 7 9 10 14 23 4 | 22 21 23 24 29 18 21 21 23 22 21
5E | 17 17 6 11 18 5 18 12 9 18 5 | 18 20 14 23 16 15 20 18 21 22 15
X6E | 1 --- --- --- --- 68 --- --- --- --- 0 | 54 --- --- --- --- 32 --- --- --- --- 53
7 | 7 14 6 14 15 4 12 11 9 18 4 | 24 28 19 27 32 18 26 16 24 22 21
8 | 9 10 5 9 18 4 10 16 9 26 3 | 16 22 16 20 27 14 23 20 17 28 17
9 | 7 10 5 8 16 3 12 17 7 33 3 | 18 23 20 23 28 18 23 22 20 35 19
10E | 13 24 11 17 16 6 15 35 25 18 7 | 48 47 45 42 45 46 44 54 52 50 44
11 | 14 10 4 9 13 5 13 13 12 14 4 | 30 41 29 37 44 31 36 32 33 31 33
12E | 10 22 7 12 22 5 30 12 6 12 5 | 23 27 19 27 26 18 26 19 25 17 19
13 | 11 14 7 10 17 4 14 20 9 15 4 | 26 31 23 26 36 21 30 24 23 24 24
14 | 8 17 5 10 11 5 17 11 10 17 4 | 23 29 24 33 31 23 24 22 25 23 24
15 | 11 16 7 9 16 4 20 12 8 23 4 | 23 27 22 29 32 19 24 26 26 20 23
16E | 17 19 9 12 21 6 21 12 15 13 5 | 34 32 29 28 35 25 34 26 34 26 29
17 | 13 20 8 10 11 5 21 13 12 28 5 | 25 32 25 27 31 21 27 29 25 20 24
18E | 9 13 5 9 17 4 12 15 8 17 4 | 20 18 19 23 18 15 17 19 19 21 17
19 | 10 12 6 7 12 4 16 10 11 22 3 | 23 28 20 24 27 19 23 21 20 20 21
20E | 11 15 6 11 15 3 18 13 11 22 4 | 27 23 21 21 25 21 24 24 24 33 21
21 | 11 14 7 11 14 3 18 16 9 21 4 | 24 25 24 28 31 21 22 22 25 22 22
22E | 9 13 5 9 14 5 15 10 16 22 4 | 17 18 16 18 17 13 16 16 19 26 14
23 | 13 14 6 12 16 6 13 30 12 26 5 | 25 29 23 26 29 20 27 30 20 30 21
24 | 8 13 5 8 15 3 14 10 11 15 3 | 25 26 22 31 34 21 27 20 26 26 24
25E | 10 13 5 8 14 5 13 14 7 9 3 | 26 27 19 24 31 19 26 19 26 18 22
26 | 9 13 6 8 18 4 13 8 11 27 4 | 23 22 22 25 31 23 20 22 25 30 22
X27 | 11 6 4 10 --- 4 15 14 12 11 4 | 31 31 27 30 --- 27 32 32 29 25 28
28E | 10 12 6 8 16 4 13 7 9 12 3 | 21 21 17 20 24 16 18 19 22 17 18
29 | 11 17 7 12 11 4 20 20 7 32 4 | 26 29 21 29 26 22 26 28 25 33 22
X30 | 1 --- --- --- --- 26 --- --- --- --- 0 | 38 --- --- --- --- 23 --- --- --- --- 36
31 | 9 17 8 13 16 4 14 19 12 15 5 | 17 26 11 20 19 13 17 15 23 13 14
32E | 14 14 7 13 13 4 15 28 16 36 5 | 35 46 36 43 40 37 44 48 34 55 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 11 15 5 16 16 12 22 |T 25 27 22 26 29 21 25 24 25 26 23
WRMS | 10 15 6 10 14 5 17 15 9 20 |NE 23 27 21 26 29 20 25 22 23 25 22
MEDI | 10 14 6 10 15 4 15 12 11 18 |MD 23 27 21 26 29 19 24 21 25 24 22
Table 3.1788.2 GPS week: 1788 Day: 2 MJD: 56762.000
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 9 3 7 11 5 13 9 10 17 3 | 23 28 22 28 28 22 32 21 27 31 23
2 | 10 18 8 12 12 4 19 14 8 34 4 | 24 30 29 30 32 23 27 25 31 28 26
3 | 8 7 3 8 12 4 10 11 12 40 3 | 20 22 17 20 25 17 21 21 18 41 18
4 | 8 12 5 12 18 6 9 10 9 17 3 | 21 24 21 26 24 19 20 24 26 21 21
5E | 13 18 6 13 16 4 23 14 12 16 5 | 22 26 25 30 25 24 26 29 33 27 24
X6E | 3 --- --- --- 417 58 --- --- --- --- 0 | 62 --- --- --- 110 25 --- --- --- --- 62
7 | 7 15 6 11 15 5 11 11 11 15 4 | 28 28 22 29 32 20 23 19 26 20 22
8 | 7 11 4 9 8 3 10 13 7 25 3 | 19 23 17 22 21 15 22 21 21 29 18
9 | 6 12 4 9 7 2 11 12 8 30 3 | 22 23 20 24 22 18 21 23 19 33 20
10E | 13 31 8 15 16 6 17 27 31 22 7 | 34 45 35 32 32 31 33 38 37 37 32
11 | 11 10 5 10 14 6 11 11 12 12 3 | 36 46 37 42 54 37 45 40 45 36 40
12E | 9 24 7 12 33 6 29 11 10 14 6 | 25 28 22 30 29 19 27 20 26 18 21
13 | 11 15 7 15 17 6 13 15 10 18 4 | 31 32 27 39 38 26 30 29 29 28 28
14 | 7 17 4 12 14 6 16 9 9 20 4 | 30 31 29 38 35 29 30 29 33 29 30
15 | 11 17 7 10 15 4 17 14 13 18 4 | 23 29 24 28 31 18 21 23 32 13 22
16E | 14 15 6 11 14 4 17 11 13 21 4 | 27 26 24 27 32 23 26 25 32 24 24
17 | 13 18 7 10 9 4 22 13 9 28 4 | 26 33 29 32 36 26 30 35 33 24 28
18E | 8 11 7 11 13 4 11 16 15 15 4 | 27 22 26 29 29 21 22 23 20 23 22
19 | 8 14 6 9 14 4 14 12 11 22 4 | 23 29 21 29 31 20 25 27 22 20 23
20E | 11 16 7 10 21 4 15 9 9 17 4 | 24 28 19 23 22 19 25 24 22 30 19
21 | 10 14 7 11 16 5 18 13 13 22 4 | 24 26 24 30 32 21 23 22 26 21 23
22E | 8 13 4 10 15 6 9 7 9 16 3 | 25 22 24 25 24 21 23 20 21 27 21
23 | 12 15 5 13 13 7 13 28 10 32 5 | 26 31 25 33 30 22 26 31 25 34 24
24 | 8 14 4 9 10 3 13 10 12 14 3 | 27 28 23 31 29 21 31 23 25 23 24
25E | 7 10 4 11 13 4 13 12 11 8 3 | 25 28 22 28 27 21 29 22 27 18 23
26 | 7 13 7 9 11 3 10 9 13 27 3 | 27 22 26 25 26 22 20 23 23 29 23
X27 | 11 11 3 11 --- 5 14 14 14 13 4 | 33 34 31 33 --- 29 38 38 27 28 31
28E | 6 11 5 7 10 3 13 5 8 10 3 | 23 26 20 25 29 19 22 20 24 18 21
29 | 10 17 5 12 12 5 20 20 14 28 5 | 29 29 25 34 32 23 27 29 27 31 25
X30 | 3 --- --- --- --- 22 --- --- --- --- 0 | 34 --- --- --- --- 29 --- --- --- --- 34
X31 | 3 --- --- --- --- 29 --- --- --- --- 0 | 46 --- --- --- --- 37 --- --- --- --- 47
32E | 17 18 8 11 17 6 16 33 16 45 6 | 30 38 31 35 37 31 39 50 30 61 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 6 11 15 5 15 15 12 23 |T 28 28 24 29 32 23 27 26 27 27 26
WRMS | 10 15 6 10 15 5 15 13 10 21 |NE 27 28 24 30 31 23 26 26 27 27 26
MEDI | 8 14 6 11 14 5 13 12 11 18 |MD 26 28 24 29 30 22 26 24 26 28 23
Table 3.1788.3 GPS week: 1788 Day: 3 MJD: 56763.000
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 6 8 13 6 12 10 14 16 3 | 21 28 21 24 25 18 30 19 25 25 22
2 | 10 20 10 10 16 5 18 14 11 36 5 | 26 31 29 32 25 28 27 29 33 35 26
3 | 8 8 5 11 17 3 11 10 12 36 3 | 21 19 16 18 21 13 14 21 19 35 16
4 | 10 10 7 9 13 7 10 13 11 18 3 | 30 27 29 29 29 25 21 30 29 23 27
5E | 11 20 5 16 21 5 27 13 12 17 5 | 26 25 21 24 20 18 26 20 23 18 20
X6E | 2 --- --- --- 301 91 --- --- --- --- 0 | 75 --- --- --- 87 26 --- --- --- --- 74
7 | 8 16 6 13 16 2 15 12 12 18 4 | 28 32 21 27 34 21 25 16 22 25 23
8 | 6 10 5 9 10 3 11 12 6 21 3 | 20 24 13 16 17 14 20 20 17 23 16
9 | 4 10 4 9 10 5 11 11 7 27 3 | 23 26 20 21 21 20 21 24 18 31 20
10E | 10 18 11 11 17 6 15 20 27 19 6 | 43 47 44 43 42 43 43 44 46 49 42
11 | 7 11 4 12 15 7 13 13 11 13 3 | 41 52 43 45 51 40 45 47 41 42 44
12E | 8 22 7 11 23 6 33 12 10 13 5 | 23 30 17 25 27 18 31 21 26 21 20
13 | 8 16 6 12 18 4 15 14 10 21 4 | 29 33 29 33 43 24 32 23 25 29 28
14 | 8 19 7 11 13 7 18 9 16 22 4 | 26 29 29 35 35 29 28 24 31 28 27
15 | 10 18 6 13 15 6 20 10 14 20 4 | 24 34 19 25 30 17 23 24 29 20 22
16E | 10 13 5 12 17 5 19 12 15 22 4 | 26 21 18 20 27 16 21 16 23 17 18
17 | 10 19 6 13 14 6 19 13 12 24 4 | 31 34 28 34 31 26 26 38 25 24 28
18E | 7 12 4 12 16 5 14 9 15 15 4 | 18 19 15 19 18 14 16 17 27 16 15
19 | 7 13 7 12 15 7 18 13 9 28 4 | 24 29 20 26 24 16 24 27 19 15 22
20E | 8 16 6 12 18 9 18 11 14 16 4 | 24 29 17 22 22 15 28 19 19 25 20
21 | 10 18 6 12 15 7 19 11 9 16 4 | 27 30 27 30 30 24 25 28 24 20 25
22E | 6 9 4 9 20 5 11 8 13 19 3 | 14 15 12 16 16 10 16 12 20 23 12
23 | 7 17 8 15 18 7 14 30 12 35 5 | 25 32 25 32 33 20 26 26 23 33 23
24 | 7 13 6 8 15 8 16 6 9 19 3 | 24 30 23 28 30 21 28 19 22 27 23
25E | 9 12 5 9 16 4 15 10 8 10 3 | 20 26 17 22 23 15 23 16 20 14 18
26 | 7 13 5 11 14 4 13 11 10 25 3 | 26 24 25 27 31 23 23 20 24 30 24
X27 | 7 9 5 14 --- 4 14 16 14 13 4 | 33 33 31 32 --- 28 35 38 29 25 32
28E | 6 13 4 11 16 4 17 11 8 10 3 | 18 21 13 20 20 14 17 17 22 15 15
29 | 9 20 6 11 12 5 24 19 14 33 5 | 27 32 27 31 32 24 29 34 28 34 27
X30 | 2 --- --- --- --- 24 --- --- --- --- 0 | 36 --- --- --- --- 34 --- --- --- --- 34
X31 | 18 19 7 14 21 7 13 18 --- 23 6 | 33 36 23 31 36 24 25 16 --- 22 25
32E | 14 18 7 11 15 8 20 24 24 23 6 | 45 51 40 45 48 42 46 47 46 41 43
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 6 11 16 6 17 14 13 22 |T 28 29 23 27 30 22 26 25 26 26 25
WRMS | 8 15 6 11 15 6 17 13 11 20 |NE 27 30 24 28 30 23 26 26 25 27 25
MEDI | 8 13 6 11 16 6 15 12 12 19 |MD 26 29 21 27 29 21 25 21 24 25 23
Table 3.1788.4 GPS week: 1788 Day: 4 MJD: 56764.000
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 7 5 8 11 8 15 10 14 16 3 | 22 28 21 25 30 23 32 20 28 24 23
2 | 12 17 8 9 11 5 18 13 12 37 4 | 29 33 31 33 34 28 33 28 33 37 29
3 | 6 8 5 10 11 10 10 13 14 46 3 | 24 22 21 22 22 21 20 23 30 51 22
4 | 15 12 7 8 14 8 12 11 11 19 4 | 33 29 29 30 36 26 24 32 33 26 29
5E | 10 19 7 11 12 5 19 15 14 16 5 | 24 27 20 25 23 20 27 23 30 23 22
X6E | 2 --- --- --- 307 110 --- --- --- --- 0 | 71 --- --- --- 98 50 --- --- --- --- 71
7 | 10 15 6 10 14 6 15 12 14 15 4 | 26 29 21 28 35 24 25 18 25 23 23
8 | 9 11 5 8 12 4 11 13 10 24 3 | 18 24 20 23 26 19 22 24 20 29 20
9 | 11 11 5 9 11 4 14 15 11 28 4 | 24 28 25 27 31 23 26 28 25 36 25
10E | 13 24 15 11 18 7 15 24 23 22 6 | 36 42 30 36 38 35 36 30 43 37 32
11 | 9 10 6 9 11 9 17 12 9 10 3 | 43 49 42 46 52 41 43 43 42 38 44
12E | 10 21 6 10 32 6 29 13 15 14 6 | 23 26 18 24 31 18 26 18 27 13 19
13 | 13 14 7 12 18 7 16 14 15 17 5 | 25 31 26 31 37 24 29 23 25 28 26
14 | 7 19 7 15 10 7 18 8 13 19 4 | 23 26 25 31 27 21 25 20 32 22 24
15 | 13 18 6 12 12 5 21 17 9 16 4 | 29 33 25 28 33 24 30 31 28 20 27
16E | 8 13 8 10 12 5 17 11 11 21 4 | 30 29 26 27 34 27 29 23 34 24 27
17 | 9 17 7 11 10 8 23 17 14 24 5 | 29 32 27 32 34 24 29 35 30 21 28
18E | 7 13 7 12 19 4 13 13 11 17 4 | 32 31 28 34 31 28 28 31 34 28 31
19 | 7 12 5 9 13 7 15 13 13 22 4 | 27 29 25 29 28 24 28 27 31 21 26
20E | 13 15 8 10 19 7 15 12 12 16 4 | 26 25 25 22 24 22 23 20 27 26 22
21 | 10 16 8 11 14 8 16 12 15 22 4 | 26 32 27 33 34 30 31 29 27 26 27
22E | 6 9 5 10 17 5 11 9 12 14 3 | 19 18 16 20 22 16 19 16 19 18 17
23 | 13 16 6 15 13 6 16 28 12 24 5 | 22 29 24 30 27 19 24 27 26 23 21
24 | 8 11 6 11 12 8 12 9 13 17 3 | 26 28 21 26 34 24 27 23 27 28 25
25E | 6 9 6 19 14 7 18 15 6 13 4 | 23 25 18 35 28 21 25 22 25 16 22
26 | 8 11 3 8 16 5 12 11 12 18 3 | 25 22 22 22 29 23 23 20 25 24 22
X27 | 11 11 7 10 --- 11 12 13 19 12 4 | 38 31 30 32 --- 29 33 36 39 27 33
28E | 10 12 6 9 13 6 18 11 9 8 4 | 23 20 16 21 23 19 21 18 22 19 18
29 | 11 19 7 13 11 6 21 20 9 31 5 | 30 33 28 34 31 29 29 32 32 35 29
X30 | 12 --- --- --- --- 17 --- --- 15 --- 13 | 25 --- --- --- --- 22 --- --- 10 --- 23
31 | 11 13 6 15 14 7 14 16 8 24 4 | 22 27 17 26 29 18 22 16 25 18 19
32E | 15 19 6 11 19 7 19 12 15 30 5 | 48 57 46 51 48 48 56 48 51 49 48
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 7 11 15 7 17 14 13 22 |T 28 29 25 29 33 25 28 26 29 27 27
WRMS | 10 15 6 12 14 6 17 15 11 19 |NE 26 29 25 29 32 24 27 26 28 27 25
MEDI | 10 13 6 10 13 7 15 13 12 18 |MD 26 29 25 28 31 24 27 23 28 24 25
Table 3.1788.5 GPS week: 1788 Day: 5 MJD: 56765.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 5 8 15 11 15 9 15 14 3 | 23 30 21 29 33 22 31 22 29 25 24
2 | 12 17 8 15 18 7 16 13 10 43 5 | 20 28 21 29 30 19 24 23 27 38 21
3 | 7 8 4 9 21 6 12 15 13 50 4 | 24 23 23 24 29 20 21 24 27 48 22
4 | 9 10 4 9 28 12 12 11 10 23 4 | 24 20 20 22 38 19 18 25 23 25 21
5E | 10 22 6 16 17 8 22 17 12 15 5 | 17 22 14 27 20 16 25 22 22 21 16
X6E | 3 --- --- --- 172 100 --- --- --- --- 0 | 79 --- --- --- 91 50 --- --- --- --- 77
7 | 5 13 7 15 18 5 16 15 15 15 4 | 27 30 22 29 34 20 27 20 25 20 23
8 | 6 10 6 13 26 7 11 13 11 26 4 | 21 24 18 22 31 17 23 24 21 29 20
9 | 6 11 5 11 26 6 13 13 14 24 4 | 23 24 21 25 33 19 25 25 25 29 22
10E | 14 21 10 11 25 8 18 22 17 23 6 | 40 45 36 38 45 37 41 37 45 39 38
11 | 6 11 7 11 12 12 12 12 21 21 4 | 37 46 37 37 50 36 41 40 42 41 38
12E | 11 21 7 11 20 8 28 14 15 11 5 | 26 28 21 32 29 22 34 23 31 19 23
13 | 8 16 5 11 18 8 17 14 13 14 4 | 27 30 23 30 37 21 27 22 22 23 24
14 | 7 19 8 11 15 7 13 11 16 16 4 | 28 29 28 34 33 27 31 22 30 24 26
15 | 11 17 7 13 20 5 16 12 13 20 4 | 26 32 25 29 35 21 27 29 33 18 25
16E | 15 18 8 14 20 7 22 11 15 32 5 | 26 25 23 28 34 21 26 21 29 24 22
17 | 11 17 6 13 17 10 20 17 11 26 5 | 27 32 22 24 35 21 30 33 28 25 25
18E | 10 13 6 10 24 9 15 14 12 13 4 | 33 32 34 39 37 31 35 30 36 34 33
19 | 5 12 6 13 12 4 15 13 15 23 4 | 26 29 26 28 30 23 26 27 27 21 25
20E | 6 17 5 12 28 9 14 12 12 12 4 | 25 31 24 25 35 21 26 26 27 27 24
21 | 10 13 6 11 18 8 19 17 10 18 4 | 25 28 23 30 35 24 28 25 27 23 25
22E | 8 8 7 10 16 9 9 11 14 13 3 | 23 21 19 25 25 20 23 18 24 25 20
23 | 9 18 7 16 16 8 13 27 17 26 5 | 27 32 23 31 33 21 27 28 27 26 23
24 | 11 12 5 11 19 7 13 11 12 22 4 | 24 24 20 30 34 19 27 21 24 23 22
25E | 9 13 6 11 16 7 13 17 10 12 4 | 26 26 21 28 30 23 27 23 29 16 23
26 | 9 12 9 9 28 7 13 10 18 19 5 | 21 21 20 22 35 18 19 19 27 18 19
X27 | 8 9 5 12 --- 8 15 12 13 15 4 | 34 30 30 30 --- 26 36 33 30 23 30
28E | 8 18 6 9 22 7 12 9 11 11 4 | 24 29 19 24 29 17 21 20 24 19 21
29 | 10 18 8 12 12 9 19 24 11 27 5 | 30 31 28 33 31 23 32 33 28 26 27
X30 | 10 --- --- --- --- 16 --- --- 13 --- 11 | 28 --- --- --- --- 24 --- --- 13 --- 25
31 | 18 20 9 17 17 13 13 19 16 17 6 | 22 33 18 29 31 24 24 19 22 15 20
32E | 11 22 6 11 16 8 13 14 19 27 5 | 46 54 42 50 51 46 53 45 51 42 47
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 7 12 20 8 16 15 14 23 |T 28 29 24 29 35 24 28 25 28 26 26
WRMS | 9 16 7 11 18 8 15 15 13 18 |NE 25 28 23 28 34 22 27 25 26 26 24
MEDI | 9 13 6 11 18 8 14 13 13 19 |MD 26 29 22 29 33 21 27 24 27 24 23
Table 3.1788.6 GPS week: 1788 Day: 6 MJD: 56766.000
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 10 21 5 15 10 14 15 4 | 24 32 23 26 39 23 35 25 32 30 26
2 | 12 18 10 10 26 7 18 15 12 47 5 | 34 37 39 39 53 36 37 40 45 50 37
3 | 8 13 5 10 32 9 10 12 14 44 4 | 23 23 20 20 39 16 18 23 29 48 20
4 | 10 12 4 6 44 7 10 11 10 18 4 | 33 30 32 33 67 29 28 41 35 31 33
5E | 8 22 6 14 28 8 25 14 10 14 5 | 24 28 21 28 29 22 32 25 26 26 23
X6E | 4 --- --- --- --- 54 --- --- --- --- 0 | 52 --- --- --- --- 30 --- --- --- --- 51
7 | 5 16 5 15 28 8 12 16 15 17 4 | 31 30 25 35 45 25 26 24 23 25 26
8 | 8 13 6 9 40 8 12 13 10 25 4 | 24 25 26 26 49 22 26 28 22 34 24
9 | 8 12 5 9 41 6 12 13 11 28 4 | 27 26 28 30 52 26 29 30 27 38 27
10E | 12 26 14 9 30 10 19 23 19 24 6 | 45 52 46 42 39 45 47 38 49 47 43
11 | 7 13 5 12 18 7 14 11 13 18 4 | 54 60 53 56 74 51 53 58 58 55 55
12E | 9 20 6 10 34 8 28 15 10 14 5 | 23 24 16 24 32 16 28 17 25 18 17
13 | 9 16 5 12 25 10 14 15 9 18 4 | 27 29 26 34 42 23 28 27 25 28 26
14 | 10 22 7 12 23 8 20 11 11 21 5 | 33 28 27 35 41 26 28 25 29 27 28
15 | 10 19 8 11 27 5 19 17 14 21 5 | 26 35 22 27 38 21 30 28 29 27 25
16E | 14 17 6 13 24 8 24 14 14 21 5 | 27 28 25 25 34 24 31 26 33 23 25
17 | 10 20 5 14 26 9 18 17 12 25 5 | 33 34 30 36 49 32 31 43 37 31 33
18E | 7 13 6 11 33 9 19 14 10 13 4 | 40 43 42 41 36 37 39 47 44 46 41
19 | 6 18 7 11 16 8 17 13 14 31 4 | 27 31 26 27 38 22 26 31 30 26 26
20E | 15 15 6 12 28 10 16 11 14 16 5 | 28 26 19 19 28 17 23 22 27 26 20
21 | 9 17 7 10 23 7 19 13 13 22 4 | 34 35 37 41 50 36 31 37 39 32 36
22E | 6 11 3 9 27 6 11 10 11 16 3 | 24 21 19 22 31 19 19 20 26 25 20
23 | 13 20 6 17 25 9 15 27 13 24 6 | 22 31 22 33 34 19 25 27 28 26 21
24 | 5 12 7 9 28 10 13 10 14 18 4 | 27 25 23 24 39 23 28 25 24 27 23
25E | 5 12 8 11 28 8 15 14 12 14 4 | 23 23 22 23 33 16 22 20 25 19 20
26 | 8 13 6 7 39 6 12 12 12 16 4 | 23 20 23 23 47 19 22 18 21 22 21
X27 | 10 14 7 14 --- 9 14 11 18 16 5 | 39 35 38 39 --- 31 36 42 36 26 37
28E | 8 12 3 11 26 6 12 10 7 8 3 | 28 27 24 25 36 27 26 28 27 27 26
29 | 11 18 7 12 23 6 23 19 8 31 5 | 35 35 34 39 48 31 33 38 34 38 34
X30 | 4 --- --- --- --- 27 --- --- --- --- 0 | 31 --- --- --- --- 20 --- --- --- --- 30
31 | 12 18 8 14 25 10 17 16 16 23 5 | 29 27 15 26 36 16 22 19 20 19 20
32E | 10 16 6 12 25 12 13 15 14 22 4 | 52 61 49 56 63 52 59 54 53 51 52
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 7 11 29 8 17 15 13 23 |T 31 32 28 31 42 26 30 30 31 31 29
WRMS | 9 16 7 11 25 8 16 15 11 20 |NE 30 31 28 32 46 26 29 31 31 32 28
MEDI | 8 16 6 11 27 8 15 13 12 18 |MD 28 29 25 28 39 23 28 27 29 27 26
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 4.1788 GPS week: 1788 MJD: 56760.0-56766.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3003 |U 5 4 11 |U 9 11 32 |U 8 8 18 |
emr | emr 2858 | 7 6 16 |U 10 10 31 | 9 9 19 |
esa | esa 2866 | 5 4 14 |U 9 11 31 |U 9 9 18 |
gfz | gfz 2858 |U 5 5 15 |U 10 12 35 |U 9 8 19 |
grg | grg 2838 |U 25 21 45 |U 12 12 40 |U 11 11 22 |
igr | igr 2854 | 5 4 14 | 9 10 31 | 8 9 17 |
igs | igs 2847 | 5 4 13 | 9 11 31 | 8 8 16 |
jpl | jpl 2858 | 7 6 19 |U 10 12 32 | 12 14 23 |
mit | mit 2866 | 6 5 14 |U 11 11 42 |U 13 11 88 |
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 5.1788.0 GPS week: 1788 Day: 0 MJD: 56760.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3013 | 4 3 10 | 11 18 22 | 5 6 18 |
emr | emr 2872 | 7 5 11 | 11 11 31 | 7 8 18 |
esa | esa 2880 | 4 2 13 | 10 17 24 | 7 9 22 |
gfz | gfz 2872 | 5 4 12 | 9 16 25 | 6 8 20 |
grg | grg 2880 | 8 5 18 | 13 18 41 | 8 9 20 |
igr | igr 2880 | 5 3 11 | 9 14 24 | 6 7 19 |
igs | igs 2875 | 4 2 10 | 10 15 24 | 6 9 20 |
jpl | jpl 2872 | 6 5 20 | 10 11 30 | 8 9 25 |
mit | mit 2880 | 7 3 14 | 11 14 38 | 7 10 19 |
Table 5.1788.1 GPS week: 1788 Day: 1 MJD: 56761.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 6 5 13 | 7 7 35 | 7 9 18 |
emr | emr 2872 | 6 6 19 | 7 7 24 | 8 9 19 |
esa | esa 2880 | 6 5 19 | 7 8 29 | 7 9 17 |
gfz | gfz 2873 | 6 5 18 | 7 9 31 | 6 7 17 |
grg | grg 2784 | 6 5 17 | 8 7 28 | 9 8 19 |
igr | igr 2880 | 6 5 18 | 6 7 28 | 7 8 14 |
igs | igs 2850 | 5 5 17 | 8 7 28 | 7 9 16 |
jpl | jpl 2872 | 14 8 26 | 7 10 24 | 24 45 41 |
mit | mit 2880 | 6 5 18 | 9 10 40 | 7 10 16 |
Table 5.1788.2 GPS week: 1788 Day: 2 MJD: 56762.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2921 | 5 4 13 | 8 11 44 | 15 11 23 |
emr | emr 2776 | 6 9 19 | 10 11 39 | 13 9 20 |
esa | esa 2784 | 6 5 17 | 9 11 42 | 16 12 26 |
gfz | gfz 2776 | 6 5 16 | 11 17 48 | 11 8 21 |
grg | grg 2784 | 58 50 49 | 12 13 55 | 18 14 30 |
igr | igr 2768 | 5 4 14 | 9 10 41 | 11 8 19 |
igs | igs 2710 | 6 5 15 | 12 14 42 | 11 9 17 |
jpl | jpl 2776 | 7 7 18 | 10 11 34 | 13 9 18 |
mit | mit 2784 | 7 7 13 | 11 13 59 | 13 11 23 |
Table 5.1788.3 GPS week: 1788 Day: 3 MJD: 56763.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 3 3 9 | 15 14 40 | 8 6 17 |
emr | emr 2872 | 6 5 13 | 14 13 43 | 10 7 19 |
esa | esa 2880 | 4 4 10 | 15 11 41 | 8 6 17 |
gfz | gfz 2872 | 7 7 13 | 18 16 53 | 11 8 21 |
grg | grg 2880 | 30 26 90 | 17 16 47 | 10 9 16 |
igr | igr 2878 | 4 4 12 | 15 13 42 | 9 9 18 |
igs | igs 2865 | 5 4 10 | 16 13 41 | 8 7 15 |
jpl | jpl 2872 | 5 5 17 | 12 12 41 | 10 7 20 |
mit | mit 2880 | 6 4 12 | 19 14 43 | 8 9 18 |
Table 5.1788.4 GPS week: 1788 Day: 4 MJD: 56764.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3016 | 6 7 13 | 8 8 33 | 8 9 14 |
emr | emr 2872 | 7 6 12 | 8 7 29 | 9 10 16 |
esa | esa 2880 | 5 4 12 | 7 11 32 | 8 9 14 |
gfz | gfz 2872 | 5 4 12 | 8 9 34 | 8 9 15 |
grg | grg 2880 | 48 42 93 | 9 11 38 | 11 11 16 |
igr | igr 2865 | 6 4 13 | 8 8 32 | 8 11 10 |
igs | igs 2879 | 5 4 11 | 7 8 32 | 8 9 13 |
jpl | jpl 2872 | 5 6 15 | 9 9 31 | 10 11 16 |
mit | mit 2880 | 5 4 12 | 9 9 38 | 34 17 502 |
Table 5.1788.5 GPS week: 1788 Day: 5 MJD: 56765.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 5 4 11 | 8 8 22 | 8 7 14 |
emr | emr 2872 | 8 6 23 | 11 10 29 | 12 11 18 |
esa | esa 2880 | 6 4 17 | 8 8 25 | 9 8 12 |
gfz | gfz 2873 | 6 5 17 | 9 10 28 | 9 8 16 |
grg | grg 2880 | 11 8 34 | 14 10 41 | 12 10 20 |
igr | igr 2852 | 5 5 18 | 8 9 26 | 10 9 15 |
igs | igs 2877 | 6 4 17 | 9 8 25 | 10 9 15 |
jpl | jpl 2872 | 7 6 26 | 10 14 28 | 11 10 17 |
mit | mit 2880 | 7 5 20 | 10 9 28 | 11 11 16 |
Table 5.1788.6 GPS week: 1788 Day: 6 MJD: 56766.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3014 | 5 4 12 | 7 10 27 | 7 7 20 |
emr | emr 2871 | 8 7 15 | 6 10 22 | 8 9 21 |
esa | esa 2880 | 5 4 12 | 7 8 22 | 7 7 19 |
gfz | gfz 2872 | 5 6 13 | 7 9 27 | 8 8 22 |
grg | grg 2784 | 12 14 17 | 7 9 28 | 13 13 34 |
igr | igr 2858 | 5 4 12 | 7 8 25 | 8 8 20 |
igs | igs 2878 | 5 5 12 | 6 8 24 | 8 7 20 |
jpl | jpl 2872 | 7 5 15 | 9 16 37 | 8 7 20 |
mit | mit 2880 | 5 5 13 | 9 10 49 | 8 10 19 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1788 GPS week: 1788 MJD: 56760.500-56766.500
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 | 11 -12 68 163 -2 | 19 23
| 16 25 83 75 5 | 2
emr uuuuu | 52 -21 123 -1 5 | 37 41
| 33 21 101 49 15 | 3
esa uuuuu | 11 -1 -26 130 -1 | 15 20
| 9 10 25 59 5 | 3
gfz uuuuu | -15 -23 69 50 -3 | 29 31
| 13 29 50 98 5 | 2
grg uuuuu | -32 12 -102 -280 0 | 34 37
| 14 14 55 68 13 | 4
igr xxxxx | -2 50 89 -104 -3 | 1 11
| 32 29 56 88 5 | 3
irf xxxxx | -11 12 -100 -91 4 | 1 11
| 5 16 25 41 7 | 2
jpl uuuuu | 9 -8 1 -154 -13 | 31 34
| 31 21 106 107 14 | 6
mit uuuuu | -25 12 -213 -268 7 | 28 30
| 24 49 85 80 9 | 1
ngs uuuuu | -34 53 17 -94 1 | 9 12
| 59 74 76 105 4 | 1
sio xxxxx | 23 44 55 -282 -14 | 85 86
| 10 24 44 41 8 | 5
Table 7.1788.0 GPS week: 1788 Day: 0 MJD: 56760.500
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 | -12 -7 -36 286 -9 | 20 25
emr uuuuu | 7 -21 280 0 26 | 33 39
esa uuuuu | 19 6 -41 104 -6 | 18 22
gfz uuuuu | -25 -20 69 -24 -5 | 29 32
grg uuuuu | -21 20 -87 -271 -10 | 39 41
igr xxxxx | -29 27 72 -8 0 | 3 12
irf xxxxx | -9 30 -101 -88 -7 | 4 13
jpl uuuuu | -2 -4 114 -251 5 | 37 39
mit uuuuu | -11 27 -226 -259 -6 | 29 32
ngs uuuuu | 14 17 -89 -92 4 | 9 13
sio xxxxx | 14 47 92 -291 -4 | 88 89
Table 7.1788.1 GPS week: 1788 Day: 1 MJD: 56761.500
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 | 19 -1 -30 107 -3 | 19 24
emr uuuuu | 13 -45 102 -19 25 | 32 38
esa uuuuu | 9 11 -13 116 0 | 16 21
gfz uuuuu | -31 -23 162 -108 2 | 29 32
grg uuuuu | -27 -3 -68 -174 -3 | 37 39
igr xxxxx | -8 47 60 -49 -3 | 2 12
irf xxxxx | -10 6 -105 -43 1 | 1 12
jpl uuuuu | -21 -7 72 -80 -4 | 35 37
mit uuuuu | 12 16 -282 -182 -2 | 27 30
ngs uuuuu | 9 35 -1 65 -1 | 9 12
sio xxxxx | 26 47 -10 -232 -19 | 87 89
Table 7.1788.2 GPS week: 1788 Day: 2 MJD: 56762.500
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 | -7 -16 66 123 -4 | 21 25
emr uuuuu | 55 -41 19 -36 -5 | 40 43
esa uuuuu | 2 -10 9 153 -6 | 18 22
gfz uuuuu | 3 -75 111 86 -9 | 33 34
grg uuuuu | -44 10 -111 -286 -18 | 38 41
igr xxxxx | 8 33 13 -87 -8 | 5 10
irf xxxxx | -18 -18 -65 -91 1 | 4 12
jpl uuuuu | -11 -35 -43 -185 -21 | 37 38
mit uuuuu | -2 -3 -124 -261 5 | 29 32
ngs uuuuu | 1 176 -13 -22 9 | 10 13
sio xxxxx | 33 6 29 -287 -8 | 90 91
Table 7.1788.3 GPS week: 1788 Day: 3 MJD: 56763.500
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 | 36 13 68 207 3 | 20 24
emr uuuuu | 97 -7 229 -55 3 | 39 43
esa uuuuu | 21 -10 -7 130 7 | 16 21
gfz uuuuu | -4 -2 39 66 5 | 30 33
grg uuuuu | -41 30 -197 -345 6 | 33 37
igr xxxxx | -30 22 114 -83 -5 | 2 11
irf xxxxx | -14 8 -82 -85 14 | 1 12
jpl uuuuu | 27 33 -56 -330 -38 | 33 36
mit uuuuu | -41 4 -142 -198 17 | 27 30
ngs uuuuu | -154 -33 -41 -59 -4 | 10 13
sio xxxxx | 22 56 72 -227 -28 | 88 89
Table 7.1788.4 GPS week: 1788 Day: 4 MJD: 56764.500
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 | 8 13 186 171 -2 | 19 23
emr uuuuu | 79 -35 133 36 1 | 40 44
esa uuuuu | -2 -12 -62 156 2 | 15 20
gfz uuuuu | -7 -16 31 189 -6 | 30 32
grg uuuuu | -52 5 -150 -364 -4 | 32 35
igr xxxxx | 63 56 188 -82 3 | 1 10
irf xxxxx | -15 18 -145 -77 2 | 1 12
jpl uuuuu | 55 -15 137 -74 -9 | 28 33
mit uuuuu | -50 97 -364 -389 5 | 27 30
ngs uuuuu | -25 -15 58 -168 1 | 8 11
sio xxxxx | 38 85 12 -292 -19 | 84 85
Table 7.1788.5 GPS week: 1788 Day: 5 MJD: 56765.500
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 | 17 -36 72 191 -5 | 16 20
emr uuuuu | 66 -10 84 90 4 | 37 41
esa uuuuu | 6 8 -46 29 0 | 12 16
gfz uuuuu | -26 -41 42 124 -10 | 27 28
grg uuuuu | -12 -3 -46 -214 8 | 29 31
igr xxxxx | -14 106 60 -135 -9 | -1 8
irf xxxxx | -7 18 -107 -79 10 | -1 10
jpl uuuuu | -25 -6 -78 -32 -12 | 25 29
mit uuuuu | -33 15 -185 -222 15 | 26 28
ngs uuuuu | -20 88 140 -262 1 | 7 9
sio xxxxx | 12 36 92 -302 -9 | 79 80
Table 7.1788.6 GPS week: 1788 Day: 6 MJD: 56766.500
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 | 13 -52 149 59 5 | 15 19
emr uuuuu | 46 15 11 -22 -17 | 39 42
esa uuuuu | 19 4 -24 223 -1 | 11 16
gfz uuuuu | -18 18 28 16 0 | 25 28
grg uuuuu | -25 29 -54 -305 21 | 29 31
igr xxxxx | -5 61 116 -282 3 | -2 10
irf xxxxx | -6 26 -96 -176 10 | 0 9
jpl uuuuu | 39 -19 -140 -126 -11 | 23 29
mit uuuuu | -48 -68 -168 -362 15 | 27 29
ngs uuuuu | -62 103 64 -120 -2 | 7 9
sio xxxxx | 18 35 99 -346 -10 | 78 79
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