[IGSREPORT-24250] Wk 1882 IGS Final Orbits
IGS ACC
acc at igs.org
Fri Feb 19 04:58:17 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1882 (Jan 31, 2016 - Feb 06, 2016)
Contacts: acc at igs.org
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:
igs1882[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1882[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1882[0-6].cls IGS GPS clock combination summary report.
igs18827.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18827.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 | 6 6 KARR
0 | EMR | 1
0 | ESA | 1 2 3 6 10 1 3 10
0 | GFZ | 1 KARR
0 | GRG | 3 8 10 1 6 10 ALRT ARTU BJFS BRUX CHTI DRAG DUBO
0 | GRG | FAIR GODE HOFN HOLB KARR KELY NRIL SCOR SFER SHAO
0 | GRG | SUTH TRO1 WIND XMIS YELL KARR XMIS
0 | JPL | 1 10
0 | MIT | MAS1 MAS1
1 | COD | MAG0
1 | ESA | 1 3 6 10 1 3 6 10 ARTU MAG0 ARTU THTI
1 | GFZ | NRMD NRMD
1 | GRG | 10 10 ARTU MCIL WIND WIND
1 | JPL | 10
1 | MIT | PIMO PIMO
2 | ESA | 1 2 3 6 10 1 3 10 CHUR KIT3 MAL2
2 | GFZ | KARR POHN
2 | GRG | 3 10 21 10 21 COCO DGAR KARR LPGS MAL2 XMIS LPGS
2 | GRG | NKLG XMIS
2 | JPL | SANT
2 | MIT | BOR1 SANT BOR1 SANT
3 | COD | CHUR KARR CHUR DAV1
3 | ESA | 1 3 6 10 10
3 | GFZ | ALGO ARTU KARR POHN ALGO ARTU POHN TWTF
3 | GRG | 10 10 21 DAV1 ARTU DAV1 SCOR
4 | COD | MAL2 SYOG ARTU MAL2 SYOG
4 | ESA | 1 3 6 10 1 3 ARTU TWTF ARTU
4 | GFZ | ALGO INVK POHN ALGO INVK POHN
4 | GRG | 6 10 10 ARTU CAS1 MAL2 MCIL SYOG TONG ARTU MAL2
5 | ESA | 1 2 3 6 10 1 3 6 10 MAL2 SYOG TONG SYOG THTI
5 | GFZ | MAL2 MAW1 SYOG MAL2 MAW1 POHN SYOG
5 | GRG | 10 10 DRAG MAW1 DRAG MAW1
5 | MIT | SOFI SOFI
6 | COD | ARTU NRMD ARTU NRMD
6 | ESA | 1 3 6 10 1 3 6 10 ARTU NKLG REUN SYOG TONG ARTU DGAV
6 | ESA | THTI
6 | GFZ | REUN POHN REUN TONG
6 | GRG | 10 10 REUN
6 | JPL | 10 ARTU POHN TUVA
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | GRG | ~23:55 | ~ -0.15 ns
3 | COD | ~18:25 | ~ 0.32 ns
6. 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.
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
----+--------+---------------
4 | GRG | 10
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 G04 | | | | 4 | 4 | 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 | -1.9 -1.4 -2.3 -62 23 -27 .62
EMR | 0 | -2.2 15.4 15.6 -31 -22 25 .35
ESA | 0 | -.6 -2.1 -.6 -21 -37 7 .43
GFZ | 0 | -.0 -1.2 -1.3 -72 -99 -11 .64
GRG | 0 | 11.1 3.8 2.7 30 19 96 .66
JPL | 0 | 7.1 4.4 13.8 -55 13 -7 .45
MIT | 0 | 9.2 .4 10.5 -3 -5 -24 .83
NGS | 0 | 8.8 -5.0 8.6 -25 -53 54 .50
SIO | 0 | 8.1 -1.1 3.8 -26 -31 -9 .49
COD | 1 | -1.4 -2.1 -1.6 -77 -14 11 .44
EMR | 1 | -.4 8.8 23.2 4 -16 3 .35
ESA | 1 | -.1 -1.1 .7 -33 -43 38 .13
GFZ | 1 | .4 -.6 -.2 -52 -91 -15 .51
GRG | 1 | 11.9 2.0 -.9 43 17 114 .58
JPL | 1 | .7 2.2 14.1 -34 -22 20 .45
MIT | 1 | 4.5 .1 11.9 20 -9 -27 .74
NGS | 1 | 5.1 -.7 18.3 -91 -52 43 .60
SIO | 1 | 4.9 .6 13.4 -34 -32 -12 .52
COD | 2 | -1.6 -1.0 -.3 -10 -7 -4 .78
EMR | 2 | 2.8 3.0 18.9 29 -8 -9 .59
ESA | 2 | -.3 -2.1 -.7 -22 -28 18 .57
GFZ | 2 | -.5 -1.6 -1.3 -46 -82 4 .88
GRG | 2 | 8.7 .3 -5.9 -2 41 121 .49
JPL | 2 | .5 6.0 10.6 11 42 23 .22
MIT | 2 | 3.0 -1.3 11.3 28 -7 -18 .87
NGS | 2 | 1.5 -.7 15.9 -54 -27 23 .72
SIO | 2 | 6.0 .6 11.4 -7 -26 -2 .58
COD | 3 | -1.0 -2.4 .8 -38 0 -5 .91
EMR | 3 | 2.8 4.2 20.2 14 -20 21 .77
ESA | 3 | -.2 -4.3 -.2 -34 -21 -29 .63
GFZ | 3 | .4 -2.5 -2.1 -57 -111 -23 .74
GRG | 3 | 2.3 .5 -7.1 22 16 116 .90
JPL | 3 | 1.9 -.6 12.7 -20 25 14 .46
MIT | 3 | 1.7 .3 9.8 1 6 -36 .89
NGS | 3 | 1.4 -.0 19.3 -69 -35 -14 .83
SIO | 3 | 1.9 -.7 10.0 -26 -20 0 .72
COD | 4 | -2.2 -1.5 -2.3 -34 4 -12 .83
EMR | 4 | 3.2 .4 13.6 -2 -15 45 .71
ESA | 4 | -1.1 -3.5 -.9 -25 -12 22 .83
GFZ | 4 | -.8 -2.2 -1.9 -79 -92 -10 .82
GRG | 4 | 1.7 3.2 -22.5 15 1 147 1.34
JPL | 4 | -1.6 -.8 9.2 24 50 -6 .96
MIT | 4 | 1.6 .7 6.9 3 -1 -4 .97
NGS | 4 | .2 -5.4 5.5 -3 -16 9 1.11
SIO | 4 | 2.6 5.2 12.1 -6 -13 -14 .85
COD | 5 | -2.5 -1.5 -2.9 -23 -6 -7 .81
EMR | 5 | 9.1 4.6 20.6 19 15 9 .54
ESA | 5 | -.3 -1.7 .0 -4 -42 57 .52
GFZ | 5 | -.1 -1.7 -1.1 -67 -98 -24 .55
GRG | 5 | .3 .7 -15.2 13 23 122 .88
JPL | 5 | -.4 2.3 13.4 14 7 -16 .51
MIT | 5 | .6 .3 11.2 22 1 -32 .98
NGS | 5 | -.2 .1 14.9 -52 -34 25 .82
SIO | 5 | 2.2 3.4 17.3 3 -49 -26 .47
COD | 6 | -1.3 -1.3 -2.6 -17 8 -24 .70
EMR | 6 | 2.8 6.0 15.9 6 -7 3 .44
ESA | 6 | -.0 -1.3 -.5 -2 -39 44 .32
GFZ | 6 | .0 -1.6 -.9 -39 -94 -28 .65
GRG | 6 | 4.2 -.0 -14.3 20 8 131 .42
JPL | 6 | -3.3 1.8 3.5 -23 38 35 .27
MIT | 6 | .3 1.7 6.4 7 -1 -2 .87
NGS | 6 | .2 1.9 6.4 -2 -14 9 .74
SIO | 6 | -.9 1.7 10.0 -2 -27 -2 .54
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 1.1882.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1882.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 2.1882.[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 3.1882.[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 5.1882.0-6). 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 1882 summary. (Jan 31, 2016 - Feb 06, 2016)
Table 1.1882.a GPS week: 1882 MJD: 57418.000-57424.000
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 243| 0 1 0 -10 -1 -3 -.01 14 13 | -815 -427 14 134
| 0 0 1 17 15 13 .04 | 110 224
emr 80| 0 2 5 -6 -8 16 .23 12 12 | 4034 525 15 138
| 2 3 2 22 15 17 .01 | 1740 1142
esa 150| 0 0 3 -15 -10 12 -.29 12 12 | 606 -1283 12 214
| 0 0 1 11 20 12 .02 | 490 1125
gfz 204| 0 -1 -3 10 -11 15 .08 11 11 | -246 52 10 107
| 0 0 1 16 16 14 .04 | 260 345
grg 118| 0 3 -8 -10 70 20 .00 19 18 | -176 90 16 224
| 0 1 4 20 20 16 .04 | 108 127
igr n/a| 0 0 -2 -19 17 -1 .01 5 4 | 1061 332 14 99
| 0 0 0 15 10 9 .01 | 1388 1019
jpl 80| 0 0 6 36 23 -14 .25 11 11 | 1148 491 15 111
| 0 1 0 25 19 30 .06 | 1594 999
mit 348| 1 -2 -5 -15 -6 -12 -.22 12 12 | -16 -38 46 389
| 0 0 0 37 16 10 .03 | 105 183
ngs 224| 0 0 1 -17 -14 -2 -.04 9 8 | -792 -483 915 1948
| 0 1 2 8 17 18 .04 | 107 232
sio 300| 0 -3 -4 8 -9 -14 -.06 14 14 | --- --- --- ---
| 0 1 2 37 36 28 .07 | --- ---
Table 1.1882.b GPS week : 1882 MJD: 57418.000-57424.000
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 | 9 4 4 4 5 4 4 |
2 | 5 4 4 4 4 5 5 |
3 | 4 4 3 4 4 4 4 |
4 | --- --- --- 0 0 0 0 |
5 | 6 5 5 5 5 5 5 |
6 | 7 5 4 5 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 4 3 4 4 4 4 4 |
9 | 4 4 3 3 3 4 4 |
10 | 12 12 12 12 12 11 13 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 4 5 5 5 |
13 | 5 5 4 5 4 4 5 |
14 | 4 4 4 4 4 4 4 |
15 | 5 4 4 4 4 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 4 4 4 4 4 4 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 5 5 5 |
20 | 5 5 5 5 4 5 5 |
21 | 4 4 5 5 4 4 4 |
22 | 5 5 5 5 5 5 5 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 4 4 4 4 |
25 | 5 4 5 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 6 5 5 5 5 6 6 |
30 | 4 4 4 4 4 4 4 |
31 | 5 4 4 4 4 4 4 |
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 2.1882.0 GPS week: 1882 Day: 0 MJD: 57418.000
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 245| 0 1 2 -16 13 -28 .00 20 14 | -755 -609 16 120
emr 80| -5 10 5 -48 -2 26 .24 14 14 | 3933 -1581 15 146
esa 150| 0 0 1 -17 -23 -6 -.30 13 12 | -10 325 13 206
gfz 204| 0 -2 -4 10 -18 18 .09 11 10 | -174 204 11 94
grg 119| 1 1 -3 22 85 19 -.00 20 18 | -175 131 17 249
igr n/a| 0 -1 -2 0 0 2 .01 5 5 | 1755 -1628 15 60
jpl 80| -1 3 7 5 2 -49 .37 12 12 | 1209 -1390 16 101
mit 348| 2 -2 -6 36 10 -14 -.18 12 11 | -124 268 48 414
ngs 228| 0 -2 1 -17 -27 31 -.08 10 8 | -641 -850 821 2125
sio 299| 0 -6 -5 63 14 10 -.01 16 15 | --- --- --- ---
Table 2.1882.1 GPS week: 1882 Day: 1 MJD: 57419.000
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 245| -1 1 0 17 11 -16 .06 13 12 | -900 -229 16 137
emr 80| -2 2 2 13 -2 -7 .22 11 11 | 2373 99 14 112
esa 150| 0 1 5 -19 -6 23 -.28 12 12 | 412 -683 11 163
gfz 205| 0 -1 -5 31 15 -15 .09 11 10 | -333 34 10 146
grg 118| 0 2 -3 -2 68 29 -.03 18 18 | -325 198 14 207
igr n/a| 0 0 -3 -8 29 -12 .02 4 4 | -72 111 14 88
jpl 80| -1 0 6 23 16 10 .25 10 10 | -408 310 15 119
mit 348| 2 -2 -6 -43 -20 1 -.20 12 11 | -133 -56 40 385
ngs 228| 0 0 3 -7 -25 -5 -.09 9 8 | -896 -257 980 2265
sio 302| 1 -3 -7 -58 -27 16 .01 15 15 | --- --- --- ---
Table 2.1882.2 GPS week: 1882 Day: 2 MJD: 57420.000
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 247| -1 0 -2 -5 -6 1 -.00 12 12 | -750 -613 13 118
emr 80| 1 1 5 19 -33 -1 .22 12 12 | 2252 999 14 143
esa 150| 0 0 3 -34 6 5 -.31 13 13 | 146 -172 10 202
gfz 206| 1 0 -2 5 -12 16 .03 11 10 | -660 274 11 93
grg 117| 0 3 -6 -19 81 34 -.06 18 17 | -216 -42 15 213
igr n/a| 0 0 -3 -45 25 -12 -.01 5 5 | -462 516 15 75
jpl 80| -1 1 6 18 54 19 .24 10 10 | -573 1013 14 102
mit 348| 1 -1 -6 0 -7 -25 -.23 12 12 | -7 -304 45 338
ngs 224| 0 0 1 -18 -20 -5 -.05 9 7 | -761 -594 1094 2134
sio 303| 0 -3 -5 10 -5 -41 -.01 15 16 | --- --- --- ---
Table 2.1882.3 GPS week: 1882 Day: 3 MJD: 57421.000
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 243| 0 0 -2 -32 3 8 -.01 12 12 | -854 -169 13 212
emr 80| -1 2 6 2 -8 28 .22 11 11 | 2978 1451 14 165
esa 150| 0 0 2 -17 1 1 -.33 12 13 | 628 -1767 10 287
gfz 205| 0 -1 -6 -13 -6 30 .02 11 11 | 133 -380 12 121
grg 119| 0 3 -9 -7 47 36 .02 19 18 | -200 259 15 250
igr n/a| 0 0 -3 -19 19 13 .01 5 5 | 75 731 15 145
jpl 80| 0 0 6 29 35 -17 .19 10 10 | 409 941 16 151
mit 348| 1 -2 -5 16 -29 -26 -.20 12 11 | -35 89 72 391
ngs 225| 0 0 4 -15 7 -16 -.01 9 8 | -853 -191 962 1844
sio 304| 0 -2 -3 23 -61 -3 -.01 14 14 | --- --- --- ---
Table 2.1882.4 GPS week: 1882 Day: 4 MJD: 57422.000
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 241| 0 0 0 -11 3 0 -.04 12 12 | -651 -666 14 115
emr 80| 0 0 5 -8 -5 41 .24 11 11 | 3927 1907 15 122
esa 150| 0 -1 4 -8 10 17 -.29 12 12 | 591 -1965 17 240
gfz 205| 0 -1 -2 12 -4 18 .11 11 11 | -421 621 10 110
grg 120| 0 3 -14 -38 36 5 .00 18 19 | -249 118 19 232
igr n/a| 0 0 -1 -23 15 -1 -.00 4 4 | 541 1668 16 96
jpl 80| 0 0 8 65 11 -46 .22 10 10 | 866 1722 17 123
mit 348| 0 -2 -5 -62 -2 -3 -.23 13 12 | -62 -41 40 397
ngs 222| 0 0 -1 -6 -31 7 -.03 9 8 | -662 -630 872 1577
sio 301| 0 -2 -2 -5 2 -42 -.12 14 13 | --- --- --- ---
Table 2.1882.5 GPS week: 1882 Day: 5 MJD: 57423.000
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 241| -1 0 -2 -27 -1 1 -.06 14 13 | -811 -528 13 112
emr 80| 1 1 8 -6 15 11 .25 11 11 | 6281 713 16 125
esa 150| 1 0 3 1 -17 26 -.26 12 12 | 1327 -2806 15 223
gfz 203| 0 0 -3 -2 -12 17 .14 12 11 | -26 -276 12 92
grg 118| 0 4 -15 -30 84 -8 .02 20 19 | -52 70 19 210
igr n/a| 0 0 -1 -6 22 0 .02 5 5 | 2456 870 14 78
jpl 80| 0 0 7 75 5 -36 .23 10 10 | 2904 880 17 95
mit 348| 1 -2 -4 -6 -12 -13 -.24 12 11 | 118 -37 41 415
ngs 222| -1 0 2 -31 10 0 -.02 9 8 | -825 -512 910 1865
sio 294| 1 -2 -6 0 -38 8 -.16 13 12 | --- --- --- ---
Table 2.1882.6 GPS week: 1882 Day: 6 MJD: 57424.000
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 243| 0 2 0 1 -32 8 .01 14 14 | -989 -177 13 129
emr 80| 0 0 6 -19 -20 15 .21 11 11 | 6495 91 20 156
esa 150| 1 1 4 -13 -48 19 -.29 13 13 | 1149 -1918 9 183
gfz 205| 0 0 -2 29 -38 20 .08 11 10 | -247 -112 10 99
grg 120| 0 4 -7 0 85 24 .07 19 18 | -17 -101 16 211
igr n/a| 0 0 -1 -30 8 1 .02 4 4 | 3135 60 14 153
jpl 80| -1 0 5 39 39 17 .25 11 11 | 3629 -39 14 88
mit 348| 1 -2 -4 -51 15 -7 -.27 12 12 | 128 -187 40 383
ngs 220| -1 0 -1 -24 -9 -27 .02 9 8 | -909 -350 768 1827
sio 303| 0 0 0 29 48 -48 -.11 12 11 | --- --- --- ---
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 3.1882.0 GPS week: 1882 Day: 0 MJD: 57418.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 59 18 20 12 55 15 16 11 11 12 8 | 55 24 25 17 40 20 21 14 19 17 13
2E | 11 12 8 15 19 4 15 12 8 16 4 | 23 29 22 26 19 22 28 25 22 31 23
3 | 12 10 13 6 9 4 7 12 8 15 3 | 22 31 29 23 22 25 31 18 27 33 25
5 | 16 13 15 14 21 7 14 16 13 20 5 | 47 49 46 34 32 40 49 34 44 39 40
6E | 54 19 19 10 17 8 14 12 15 14 7 | 50 26 24 19 19 21 22 17 20 20 18
7 | 10 13 6 7 19 3 14 12 10 13 4 | 32 30 24 29 30 28 31 24 29 19 26
8 | 10 11 11 8 14 5 12 9 12 12 3 | 22 27 25 20 22 21 27 20 18 27 21
9 | 13 10 13 7 11 4 11 13 8 14 4 | 57 56 49 53 57 51 53 53 50 50 51
X10 | 19 20 14 --- 42 8 16 29 45 --- 12 | 74 77 79 --- 107 82 78 63 113 --- 84
11E | 18 12 11 6 13 4 10 9 11 18 4 | 51 52 41 45 47 44 51 43 49 46 46
12 | 23 17 11 13 20 4 12 12 11 14 5 | 36 30 24 28 29 26 30 22 24 24 25
13 | 10 15 14 11 20 5 12 12 10 11 4 | 38 37 36 40 46 37 38 38 33 36 36
14 | 11 10 12 9 17 4 10 15 8 17 4 | 29 33 30 36 39 32 31 35 30 34 31
15 | 12 16 12 11 16 3 12 13 9 17 4 | 30 33 27 36 36 32 32 32 29 35 30
16 | 15 12 8 10 17 5 12 14 9 18 4 | 28 27 22 20 24 21 26 20 22 15 21
17 | 15 19 11 14 15 4 10 13 9 11 4 | 31 32 26 37 26 28 32 28 26 28 28
18 | 16 13 13 14 20 4 15 13 11 18 5 | 26 30 22 33 33 24 28 30 21 28 24
19 | 13 23 10 18 18 4 13 14 9 14 5 | 27 32 22 36 22 24 29 28 21 24 24
20 | 17 14 17 14 21 6 12 13 10 20 5 | 33 30 26 37 38 29 31 32 26 34 29
21E | 9 11 9 10 22 4 13 8 11 12 4 | 28 28 28 27 30 28 30 26 32 25 28
22 | 11 11 13 12 24 5 11 14 10 23 5 | 33 33 31 36 38 30 30 38 25 34 31
23 | 10 11 11 8 14 4 10 10 7 16 3 | 33 36 30 30 33 29 30 29 25 20 28
24 | 14 12 14 7 15 5 10 10 7 16 4 | 28 27 30 27 23 28 25 23 27 28 25
25 | 14 23 12 7 15 6 11 8 9 14 4 | 27 31 30 26 25 27 30 23 24 28 25
26 | 11 11 14 10 16 5 10 10 7 16 4 | 29 30 34 25 28 31 31 29 30 32 29
27 | 10 10 12 8 14 4 11 9 7 15 3 | 22 30 26 20 28 22 28 21 21 24 23
28 | 12 13 11 11 19 6 9 11 7 10 4 | 25 28 18 26 27 20 26 21 19 18 21
29 | 21 19 12 13 21 5 14 12 11 21 5 | 30 29 20 24 26 24 29 20 25 21 22
30 | 9 12 14 7 20 4 9 8 7 10 3 | 27 22 29 20 22 24 25 20 23 16 21
31 | 16 15 8 10 23 6 12 13 9 18 4 | 30 30 21 28 37 26 28 26 28 23 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 20 14 13 11 20 5 12 12 10 16 |T 34 33 29 29 33 29 32 28 30 27 29
WRMS | 14 14 12 10 18 5 12 11 8 15 |NE 32 34 30 30 34 30 33 29 30 27 29
MEDI | 13 13 12 10 18 4 12 12 9 15 |MD 30 30 26 28 29 27 30 26 25 28 25
Table 3.1882.1 GPS week: 1882 Day: 1 MJD: 57419.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 17 8 16 10 11 6 10 12 13 11 4 | 26 23 25 21 23 22 23 17 30 20 21
2E | 13 8 9 8 16 6 10 11 6 12 3 | 27 27 24 27 27 24 26 26 29 31 26
3 | 12 8 15 7 11 4 7 8 7 15 3 | 23 24 22 19 19 19 25 19 24 28 20
5 | 15 13 14 13 19 5 11 17 13 19 5 | 38 37 34 28 26 28 36 26 33 28 30
6E | 23 8 15 13 20 5 10 10 11 10 4 | 27 22 23 24 27 20 22 22 20 22 20
7 | 11 13 7 7 16 4 12 12 7 13 3 | 37 29 25 31 24 28 32 24 31 24 27
8 | 8 7 10 8 9 3 10 10 6 10 3 | 29 30 26 22 23 24 29 22 25 26 24
9 | 9 8 13 8 10 3 8 12 5 15 3 | 41 40 32 37 37 35 40 36 36 40 36
X10 | 19 18 15 --- 42 7 19 29 47 --- 12 | 63 65 65 --- 82 65 64 60 93 --- 69
11E | 20 7 12 8 18 7 8 14 11 14 4 | 81 77 74 71 78 71 78 74 75 74 75
12 | 18 11 10 13 23 4 10 13 11 14 4 | 34 30 23 30 26 25 28 20 28 21 24
13 | 9 11 14 12 20 4 11 13 11 13 4 | 33 34 28 32 36 29 32 28 27 29 28
14 | 10 8 12 11 18 4 9 13 7 15 4 | 24 25 24 29 27 23 24 26 23 26 23
15 | 8 12 12 9 15 3 11 14 8 18 4 | 27 30 23 26 26 24 27 22 22 27 23
16 | 20 12 6 13 17 5 11 14 11 18 4 | 36 26 22 24 25 21 25 19 22 17 21
17 | 11 11 13 13 18 3 9 12 9 10 4 | 28 32 27 34 27 27 32 26 29 26 27
18 | 18 13 11 14 22 5 14 15 12 19 5 | 31 28 25 28 27 23 26 28 24 26 24
19 | 11 13 13 15 18 3 11 14 9 15 4 | 27 30 25 32 24 25 32 26 27 22 24
20 | 13 11 13 13 20 6 13 13 9 16 4 | 33 27 25 29 27 25 27 29 24 30 25
21E | 12 8 6 9 26 4 12 8 9 11 4 | 24 23 18 24 19 19 22 21 22 23 20
22 | 12 11 14 11 21 5 11 15 9 21 4 | 31 27 27 27 27 24 26 28 23 28 24
23 | 11 7 11 7 14 3 7 10 7 17 3 | 32 27 23 26 20 24 27 23 25 19 23
24 | 9 11 12 9 19 4 8 12 8 18 4 | 28 27 28 27 24 24 25 23 25 28 24
25 | 10 16 12 10 18 5 10 9 8 13 4 | 27 29 29 28 27 25 29 24 26 27 25
26 | 10 10 13 9 15 3 9 8 7 13 3 | 29 30 30 25 26 27 28 26 27 29 26
27 | 9 10 12 10 11 3 9 9 7 12 3 | 29 29 26 25 26 24 31 22 25 24 25
28 | 13 11 12 12 21 4 9 12 7 12 4 | 30 30 24 31 30 23 30 22 25 22 24
29 | 16 12 11 15 21 4 13 12 10 22 5 | 31 27 22 32 25 23 27 20 25 21 23
30 | 11 12 12 8 18 3 8 10 5 8 3 | 33 27 32 31 20 27 31 25 30 25 26
31 | 11 13 10 9 23 3 10 11 9 13 4 | 25 27 17 25 30 21 26 21 24 23 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 11 12 11 18 4 10 12 9 15 |T 32 31 28 29 29 27 31 26 29 27 27
WRMS | 12 11 12 10 18 4 10 11 8 15 |NE 31 30 27 28 28 26 30 25 28 25 26
MEDI | 11 11 12 10 18 4 10 12 9 14 |MD 29 28 25 28 26 24 27 24 25 26 24
Table 3.1882.2 GPS week: 1882 Day: 2 MJD: 57420.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 17 8 15 12 13 7 10 10 8 14 4 | 19 18 23 16 20 16 20 16 17 21 16
2E | 16 10 8 10 18 5 9 15 11 14 4 | 21 23 19 19 19 17 21 26 20 19 18
3 | 9 9 15 9 10 4 7 9 6 12 3 | 19 26 25 18 19 19 25 17 23 24 21
5 | 10 12 17 12 20 5 12 16 10 20 5 | 36 41 38 30 27 32 39 29 37 35 33
6E | 18 10 15 11 17 4 10 13 6 12 4 | 19 21 19 19 16 16 17 15 14 20 15
7 | 10 14 8 9 19 5 12 12 8 13 4 | 30 28 22 27 24 24 28 24 29 21 24
8 | 8 9 10 8 14 4 10 9 7 11 3 | 22 25 22 16 23 18 24 18 17 24 19
9 | 11 8 13 7 11 4 9 9 6 14 3 | 42 40 34 37 39 36 38 39 36 39 37
X10 | 21 18 15 --- 43 9 18 29 43 --- 12 | 57 61 63 --- 83 63 58 53 92 --- 67
11 | 18 9 13 8 19 6 10 12 7 15 4 | 54 52 49 50 52 49 55 48 51 48 50
12 | 19 11 10 13 21 4 11 14 9 16 4 | 31 25 18 25 22 19 25 13 20 19 19
13 | 9 12 15 10 19 4 12 13 8 12 4 | 27 29 27 28 34 27 30 28 24 30 26
14 | 9 9 12 11 16 5 10 10 8 14 3 | 30 27 28 32 34 29 28 34 28 33 29
15 | 7 11 13 8 17 4 10 13 8 16 4 | 27 28 24 31 31 28 29 29 26 34 26
16 | 16 11 7 12 20 6 10 13 11 16 4 | 27 22 19 21 25 20 22 19 23 19 20
17 | 10 15 13 14 15 4 8 13 8 11 4 | 22 29 19 30 23 22 28 23 23 25 23
18 | 15 12 14 14 18 4 13 15 11 20 5 | 29 26 24 30 30 24 27 31 25 33 26
19 | 10 17 12 16 17 4 10 13 8 14 4 | 19 27 16 27 20 18 25 22 17 19 18
20 | 11 14 12 12 17 5 13 14 9 18 4 | 23 25 23 27 27 23 26 27 23 28 23
21E | 14 10 8 9 25 5 16 14 9 11 4 | 21 21 15 19 25 17 22 17 17 17 17
22 | 14 11 14 13 24 6 13 13 8 21 5 | 32 27 27 29 35 27 28 32 26 33 27
23 | 8 7 10 9 12 5 6 11 8 17 3 | 28 26 24 24 23 23 24 26 21 20 23
24 | 8 12 16 9 13 6 8 10 7 16 3 | 24 21 24 23 20 21 21 20 21 28 20
25 | 11 18 14 11 13 5 12 9 11 12 4 | 20 25 24 22 20 19 23 17 18 23 19
26 | 9 11 13 11 15 5 8 9 10 14 4 | 32 32 34 27 32 30 31 30 34 36 31
27 | 9 11 12 8 18 5 10 8 8 12 3 | 18 25 18 16 26 16 23 16 16 20 18
28 | 13 11 12 11 19 4 7 12 7 10 4 | 22 26 17 17 26 17 23 16 19 18 18
29 | 17 13 11 14 20 4 11 15 10 22 5 | 30 26 19 26 22 20 27 22 20 27 22
30 | 10 11 14 7 20 5 8 14 5 7 3 | 26 25 29 21 24 24 27 23 25 20 23
31 | 12 11 10 9 21 3 10 12 8 18 4 | 24 25 19 26 33 23 26 24 25 27 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 13 11 18 5 10 12 9 15 |T 27 28 25 25 28 24 28 25 26 26 25
WRMS | 12 12 13 10 17 5 10 12 7 16 |NE 27 28 25 25 28 24 28 25 26 26 25
MEDI | 11 11 13 11 18 5 10 13 8 14 |MD 26 26 23 26 25 22 26 23 23 24 23
Table 3.1882.3 GPS week: 1882 Day: 3 MJD: 57421.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 13 11 16 8 13 6 10 10 7 9 3 | 19 22 24 21 24 20 19 17 20 19 18
2E | 13 11 10 13 22 4 9 13 8 12 4 | 38 37 34 36 40 36 35 39 37 39 36
3 | 11 9 13 9 11 5 8 9 9 16 3 | 20 27 27 22 21 22 27 20 23 28 22
X4 | 2 --- --- --- --- >>>> --- --- --- --- 0 | 9999 --- --- --- --- 74 --- --- --- --- 9999
5 | 10 12 17 12 19 6 13 15 9 18 5 | 34 42 40 27 28 34 40 26 38 32 33
6E | 15 9 16 14 28 5 10 12 9 12 4 | 20 23 22 20 22 21 19 18 23 24 19
7 | 8 14 7 10 17 5 12 12 9 14 4 | 29 28 23 28 31 27 28 25 27 22 24
8 | 11 9 10 8 17 4 9 10 8 10 3 | 28 32 30 28 30 28 29 25 31 31 28
9 | 10 8 13 7 8 4 8 8 6 15 3 | 45 46 41 47 52 45 47 45 45 47 45
X10 | 22 20 13 --- 44 6 16 30 46 --- 12 | 80 83 84 --- 99 84 79 72 112 --- 86
11 | 17 10 11 6 20 7 8 12 9 13 4 | 48 44 38 43 43 41 43 39 43 40 41
12 | 14 12 10 12 17 6 9 12 9 15 4 | 35 29 27 31 29 26 27 22 27 24 26
13 | 9 12 12 13 17 5 14 14 11 10 4 | 35 33 30 38 40 32 31 34 25 33 30
14 | 8 11 10 12 15 4 11 12 9 15 4 | 30 28 31 39 35 31 25 36 26 35 30
15 | 8 11 11 12 15 5 12 11 10 15 4 | 30 28 27 34 34 29 26 31 22 34 27
16 | 20 9 7 12 20 5 10 12 11 15 4 | 37 30 26 30 33 27 30 22 30 22 27
17 | 10 12 13 15 15 4 10 12 10 9 4 | 27 36 28 35 28 29 31 26 34 27 29
18 | 13 12 13 14 23 5 12 14 12 16 4 | 28 24 25 31 33 23 23 30 22 26 24
19 | 12 13 13 17 17 4 12 13 11 14 4 | 24 33 26 33 26 27 29 26 32 25 26
20 | 12 12 13 14 19 5 12 13 12 17 4 | 29 25 25 31 33 23 22 26 20 23 23
21E | 18 9 6 15 28 5 9 13 9 14 4 | 28 31 27 33 29 29 27 30 32 26 27
22 | 10 12 13 12 29 5 12 13 11 22 5 | 29 30 33 36 38 29 27 36 24 34 29
23 | 8 9 11 9 14 6 8 8 8 14 3 | 27 27 27 28 29 28 28 26 23 20 25
24 | 12 9 13 6 15 5 10 12 9 19 4 | 27 25 27 25 21 23 21 23 20 29 22
25 | 10 22 12 7 13 5 11 9 8 11 4 | 31 33 34 28 27 29 29 25 29 31 28
26 | 11 9 13 8 15 3 8 8 10 10 3 | 32 29 35 29 30 30 30 27 28 29 28
27 | 13 8 12 7 18 4 9 10 8 10 3 | 31 31 30 29 32 28 29 25 32 27 28
28 | 7 10 10 12 18 6 8 10 8 11 3 | 24 27 24 25 29 24 26 22 24 24 22
29 | 18 10 12 16 20 4 12 13 10 20 5 | 34 31 28 34 29 26 28 24 26 25 26
30 | 9 8 14 7 21 5 8 12 8 9 3 | 22 22 28 23 24 23 23 22 22 21 21
31 | 9 10 8 9 22 3 11 10 7 12 3 | 27 28 22 28 35 24 24 24 23 23 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 12 11 19 5 10 12 9 14 |T 31 32 30 30 33 31 30 28 30 28 29
WRMS | 12 11 13 11 18 5 10 11 8 14 |NE 31 32 31 30 33 31 30 28 30 28 29
MEDI | 11 10 12 12 17 5 10 12 9 14 |MD 29 29 27 30 30 28 28 26 26 27 27
Table 3.1882.4 GPS week: 1882 Day: 4 MJD: 57422.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 13 11 14 10 14 7 10 17 10 16 4 | 23 25 26 25 24 23 26 28 28 28 24
2E | 11 10 6 12 20 3 10 18 8 12 4 | 33 33 34 39 33 31 34 31 32 36 32
3 | 10 8 14 10 13 3 7 9 12 12 3 | 30 29 31 27 25 27 29 27 30 30 27
X4 | 1 --- --- --- --- 39 --- --- --- --- 0 | 9999 --- --- --- --- 46 --- --- --- --- 9999
5 | 8 11 18 11 19 4 10 18 10 17 4 | 35 38 36 34 29 32 39 30 32 35 32
6E | 12 10 12 11 23 5 9 14 8 11 4 | 24 27 27 25 29 23 23 26 25 25 24
7 | 8 11 6 8 16 4 11 14 9 14 3 | 33 32 27 33 34 29 31 28 31 26 29
8 | 10 7 12 8 15 4 10 13 8 10 3 | 33 37 32 30 31 29 33 31 29 33 31
9 | 6 7 12 8 11 4 8 8 6 14 3 | 43 47 42 45 51 43 47 44 44 47 44
X10 | 17 18 11 --- 65 9 15 27 45 --- 12 | 75 79 79 --- 112 78 76 65 99 --- 79
11 | 16 10 12 7 21 5 7 14 8 14 4 | 42 41 35 39 41 36 40 38 38 38 37
12 | 19 9 9 11 21 2 8 14 10 13 4 | 38 32 27 33 31 29 31 25 30 25 28
13 | 7 12 13 15 16 3 11 14 9 10 4 | 35 38 35 39 42 34 35 35 33 33 34
14 | 8 9 13 11 17 6 9 11 8 13 3 | 32 31 34 39 35 34 30 34 37 35 32
15 | 8 10 11 11 14 3 12 13 10 14 4 | 35 34 33 38 38 33 34 34 32 36 33
16 | 22 9 6 12 17 4 9 10 10 15 4 | 36 30 25 31 27 27 28 27 27 24 26
17 | 9 10 10 14 19 3 9 12 9 13 4 | 33 35 33 39 29 31 34 31 33 35 32
18 | 15 11 14 13 21 4 11 15 10 15 4 | 30 29 28 33 36 28 28 32 28 27 27
19 | 11 14 11 16 22 4 12 13 10 16 4 | 32 34 32 39 28 29 31 31 31 31 30
20 | 11 8 12 11 22 5 11 14 9 15 4 | 31 32 31 35 40 30 30 34 30 32 30
21E | 9 7 7 10 26 3 10 10 9 9 3 | 32 32 32 31 37 30 31 32 31 31 31
22 | 15 11 13 10 22 5 9 15 12 21 5 | 32 30 33 32 34 29 28 34 30 34 29
23 | 9 8 12 10 16 3 8 9 10 16 3 | 29 32 31 34 34 29 32 30 29 27 29
24 | 9 10 14 7 14 5 9 15 7 13 3 | 29 30 32 32 30 28 28 26 27 29 27
25 | 11 18 13 6 16 4 11 9 5 10 4 | 28 31 32 30 28 29 31 26 29 28 28
26 | 14 10 13 9 17 3 8 10 7 11 3 | 32 31 33 30 29 30 31 28 31 33 30
27 | 10 9 11 7 12 4 9 10 8 12 3 | 27 34 30 31 29 29 33 28 30 32 29
28 | 8 14 10 11 21 4 11 12 8 10 4 | 27 32 28 32 32 26 30 27 28 29 27
29 | 18 13 9 13 20 5 9 14 10 20 5 | 37 32 29 33 26 28 31 26 28 27 28
30 | 10 10 14 10 21 4 11 14 7 7 4 | 30 30 33 30 30 27 27 29 30 27 28
31 | 9 10 9 8 21 3 10 11 6 15 3 | 28 30 27 33 36 29 30 27 28 26 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 10 12 11 18 4 10 13 9 14 |T 33 34 32 33 35 31 33 31 33 31 31
WRMS | 12 10 12 11 19 4 10 12 8 13 |NE 34 34 33 33 35 32 33 31 33 30 31
MEDI | 10 10 12 10 19 4 10 13 9 13 |MD 32 32 32 33 31 29 31 30 30 31 29
Table 3.1882.5 GPS week: 1882 Day: 5 MJD: 57423.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 12 12 13 9 15 6 9 12 9 8 4 | 18 21 23 18 19 18 23 18 22 18 18
2E | 16 11 8 11 23 5 10 15 7 13 4 | 29 27 23 23 31 23 27 29 26 25 24
3 | 10 7 12 9 18 4 8 9 8 11 3 | 22 27 26 23 22 22 27 20 28 26 23
X4 | 2 --- --- --- --- 47 --- --- --- --- 0 | 9999 --- --- --- --- 31 --- --- --- --- 9999
5 | 10 10 15 13 19 7 12 17 12 17 4 | 30 33 29 27 24 26 33 25 32 29 27
6E | 16 10 14 9 20 5 11 11 8 8 4 | 24 24 24 20 28 20 22 21 22 21 21
7 | 10 12 8 11 17 4 10 13 8 13 4 | 27 28 21 29 28 25 30 22 24 23 23
8 | 11 11 10 11 15 4 10 12 8 10 3 | 24 29 25 27 23 25 31 28 26 32 26
9 | 9 8 12 9 15 5 7 8 5 15 3 | 37 42 36 38 46 36 44 37 37 43 38
X10 | 19 19 13 --- 43 8 15 28 49 25 11 | 59 63 64 --- 81 63 61 53 85 5 64
11 | 10 10 13 8 21 9 8 12 10 13 4 | 35 38 33 38 41 34 41 34 39 33 36
12 | 21 12 10 11 23 4 10 13 10 12 4 | 33 29 20 25 26 22 28 21 24 24 23
13 | 9 12 12 14 16 4 12 14 10 10 4 | 31 32 29 32 30 28 32 30 25 27 27
14 | 8 10 13 10 19 5 11 13 8 15 4 | 27 25 26 32 30 26 25 30 29 31 26
15 | 11 13 11 15 16 3 11 13 9 15 4 | 30 27 27 35 28 27 27 27 25 29 26
16 | 27 11 8 15 20 6 9 13 11 16 5 | 34 26 19 22 22 22 22 22 24 21 20
17 | 10 10 10 16 18 3 10 11 8 11 4 | 30 34 27 35 26 28 34 28 29 28 28
18 | 17 13 12 15 24 5 14 15 12 18 5 | 25 22 20 29 30 20 24 23 19 20 19
19 | 11 13 10 19 18 4 14 12 9 16 4 | 26 31 24 33 24 25 33 29 25 25 25
20 | 10 11 13 14 22 6 13 12 10 14 4 | 25 22 21 29 32 20 24 24 20 26 21
21E | 15 9 9 10 25 5 12 10 10 8 4 | 26 25 21 27 34 22 25 25 24 23 23
22 | 15 12 13 10 29 6 11 14 11 22 5 | 25 24 21 23 32 20 23 24 21 27 20
23 | 10 9 12 9 18 5 9 10 8 14 3 | 28 29 28 30 31 27 29 26 26 23 26
24 | 8 8 12 11 17 6 8 13 6 10 3 | 25 27 26 27 24 23 25 22 22 24 23
25 | 15 17 13 6 17 4 10 7 7 11 4 | 28 30 30 26 23 24 29 23 24 26 25
26 | 18 11 13 8 17 5 10 10 6 9 4 | 33 31 33 27 27 29 27 29 30 30 28
27 | 12 13 12 11 17 7 10 9 8 9 4 | 21 29 23 24 23 23 30 26 25 27 24
28 | 8 10 11 12 20 4 9 11 8 11 3 | 23 31 21 30 31 24 29 26 27 25 25
29 | 20 16 11 12 20 5 11 18 13 20 5 | 32 30 22 26 24 24 29 21 24 24 23
30 | 9 12 14 8 17 5 10 12 7 9 3 | 24 25 30 26 24 25 28 24 25 23 24
31 | 10 10 11 8 23 4 11 10 8 13 4 | 24 30 23 31 34 25 28 26 28 27 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 11 12 12 20 5 10 12 9 13 |T 28 29 26 28 29 26 29 26 27 25 26
WRMS | 13 11 12 11 19 5 10 11 8 12 |NE 28 30 26 28 29 26 30 26 28 25 26
MEDI | 11 11 12 11 18 5 10 12 8 13 |MD 27 29 24 27 28 25 28 25 25 25 24
Table 3.1882.6 GPS week: 1882 Day: 6 MJD: 57424.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 10 15 10 17 3 11 7 9 7 3 | 34 42 41 37 40 38 43 37 39 39 38
2E | 17 13 8 15 31 5 11 16 8 10 5 | 44 44 40 42 45 40 43 44 44 43 42
3 | 9 13 14 8 14 4 10 7 8 10 3 | 40 48 44 39 39 41 48 40 42 47 42
X4 | 2 --- --- --- --- 79 --- --- --- --- 0 | 9999 --- --- --- --- 42 --- --- --- --- 9999
5 | 8 14 16 10 19 5 13 15 10 14 4 | 48 54 47 45 43 46 54 44 49 48 47
6E | 11 10 13 12 24 5 10 12 6 11 4 | 39 42 44 40 38 40 41 41 39 42 40
7 | 9 10 10 9 16 4 13 10 7 12 3 | 45 40 36 43 45 41 42 38 41 38 39
8 | 9 9 14 9 16 3 10 9 7 8 3 | 42 46 41 42 42 43 47 41 43 46 43
9 | 11 10 12 12 11 5 10 5 6 14 3 | 67 69 61 66 72 65 69 66 65 68 66
X10 | 19 22 13 --- 42 8 18 32 46 --- 12 | 97 102 104 --- 127 105 100 89 135 --- 107
11 | 14 10 14 8 19 4 10 10 9 8 4 | 55 58 50 55 58 53 60 52 55 55 54
12 | 20 12 11 10 20 4 12 16 9 11 4 | 50 47 42 41 44 41 46 40 42 41 42
13 | 10 15 12 14 15 3 13 16 11 10 4 | 53 50 49 52 53 49 51 51 47 51 49
14 | 11 9 13 8 20 4 9 12 9 13 4 | 42 40 43 46 46 43 40 47 45 46 43
15 | 10 14 14 11 17 3 12 13 9 13 4 | 46 44 41 47 47 44 42 45 42 49 43
16 | 23 10 11 14 18 6 10 12 8 15 4 | 49 44 39 41 41 42 42 41 45 39 41
17 | 13 13 10 13 15 5 11 12 8 11 4 | 50 52 48 53 47 47 53 48 49 46 49
18 | 19 13 14 15 25 6 12 14 10 16 5 | 44 40 39 48 50 42 40 42 40 40 40
19 | 15 15 9 16 15 4 14 12 8 14 4 | 46 49 46 50 43 45 50 47 46 45 46
20 | 12 11 15 11 22 4 12 14 10 11 4 | 45 39 37 44 52 41 42 45 38 42 41
21E | 15 8 9 8 25 4 8 11 9 9 4 | 45 42 41 45 46 44 42 40 44 41 42
22 | 17 11 13 10 26 4 11 15 9 19 5 | 43 43 41 44 49 41 41 45 40 40 40
23 | 12 9 12 10 15 4 10 9 9 14 3 | 44 43 42 43 45 42 44 41 42 36 41
24 | 12 8 14 8 12 4 8 10 9 10 3 | 43 39 41 37 36 39 39 37 38 37 37
25 | 13 13 13 9 18 4 9 10 7 9 3 | 47 45 48 42 43 43 46 41 43 44 43
26 | 15 9 15 7 18 4 9 11 7 9 3 | 48 46 47 42 42 45 44 44 47 46 44
27 | 10 11 15 8 16 3 11 10 9 8 3 | 41 47 42 43 44 44 48 44 46 45 44
28 | 10 12 11 10 17 5 10 11 8 11 3 | 43 47 40 45 46 42 45 44 43 42 42
29 | 23 12 11 10 19 6 12 20 13 18 5 | 51 46 42 45 42 42 43 41 42 41 42
30 | 12 14 15 11 16 5 10 12 7 7 4 | 43 40 44 40 41 39 40 40 40 40 39
31 | 14 10 11 7 25 5 8 10 7 15 4 | 39 42 39 41 47 40 43 40 42 40 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 11 13 11 19 4 11 12 9 12 |T 47 47 45 44 48 45 47 45 47 44 45
WRMS | 14 11 13 10 18 4 11 12 8 11 |NE 48 48 45 44 49 45 47 45 47 44 46
MEDI | 12 11 13 10 18 4 10 12 9 11 |MD 45 44 42 43 45 42 43 42 43 42 42
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 4.1882 GPS week: 1882 MJD: 57418.0-57424.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2911 |U 5 4 12 |U 9 13 31 |U 5 5 14 |
emr | emr 437 | 6 6 17 |U 12 12 31 | 9 5 15 |
esa | esa 2880 | 5 5 14 |U 10 13 37 | 8 6 18 |
gfz | gfz 2784 |U 5 5 13 |U 9 13 39 |U 7 6 18 |
grg | grg 2879 |U 6 7 15 |U 10 13 39 | 12 9 24 |
igr | igr 2874 | 5 4 13 | 9 16 36 | 7 5 15 |
igs | igs 2870 | 5 5 13 | 9 12 35 | 8 5 16 |
jpl | jpl 2880 | 6 5 15 |U 11 16 35 | 9 5 18 |
mit | mit 2880 | 7 6 16 |U 12 19 42 |U 9 7 24 |
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 5.1882.0 GPS week: 1882 Day: 0 MJD: 57418.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 7 5 13 | 14 31 40 | 6 5 13 |
emr | emr 30 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
esa | esa 2880 | 7 6 15 | 15 26 53 | 17 12 23 |
gfz | gfz 2784 | 7 6 14 | 15 28 55 | 13 10 21 |
grg | grg 2880 | 8 9 15 | 15 28 49 | 15 11 20 |
igr | igr 2842 | 7 6 14 | 14 54 57 | 15 10 20 |
igs | igs 2816 | 7 7 15 | 15 24 52 | 16 9 18 |
jpl | jpl 2880 | 7 7 16 | 18 52 53 | 14 11 25 |
mit | mit 2880 | 14 11 19 | 18 46 57 | 14 9 23 |
Table 5.1882.1 GPS week: 1882 Day: 1 MJD: 57419.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 5 4 15 | 10 11 25 | 5 5 13 |
emr | emr 2880 | 6 6 17 | 12 12 31 | 9 5 15 |
esa | esa 2880 | 5 5 17 | 10 10 35 | 7 4 15 |
gfz | gfz 2784 | 5 5 15 | 11 11 25 | 8 4 17 |
grg | grg 2880 | 7 7 19 | 11 13 31 | 10 7 20 |
igr | igr 2880 | 5 4 15 | 10 12 27 | 5 3 14 |
igs | igs 2880 | 5 5 16 | 11 11 28 | 8 4 15 |
jpl | jpl 2880 | 5 5 18 | 10 11 25 | 10 4 15 |
mit | mit 2880 | 5 6 16 | 13 9 40 | 9 5 17 |
Table 5.1882.2 GPS week: 1882 Day: 2 MJD: 57420.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 6 4 13 | 6 13 42 | 4 5 17 |
emr | emr 30 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
esa | esa 2880 | 6 5 14 | 7 14 46 | 5 5 16 |
gfz | gfz 2784 | 6 4 12 | 7 14 45 | 6 5 19 |
grg | grg 2880 | 6 7 14 | 7 14 49 | 11 12 32 |
igr | igr 2880 | 5 5 13 | 6 13 47 | 5 4 16 |
igs | igs 2880 | 5 5 13 | 6 14 46 | 6 5 17 |
jpl | jpl 2880 | 5 5 15 | 6 12 48 | 8 5 17 |
mit | mit 2880 | 6 5 15 | 7 13 51 | 7 7 21 |
Table 5.1882.3 GPS week: 1882 Day: 3 MJD: 57421.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 5 4 12 | 11 9 28 | 5 5 12 |
emr | emr 30 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
esa | esa 2880 | 5 4 13 | 12 9 31 | 7 5 17 |
gfz | gfz 2784 | 5 5 11 | 11 8 34 | 6 5 17 |
grg | grg 2880 | 6 6 16 | 11 7 33 | 13 11 27 |
igr | igr 2880 | 6 4 13 | 11 9 29 | 6 4 15 |
igs | igs 2880 | 5 5 12 | 11 9 30 | 7 5 15 |
jpl | jpl 2880 | 5 5 13 | 13 9 30 | 8 4 17 |
mit | mit 2880 | 9 9 28 | 19 30 46 | 13 16 56 |
Table 5.1882.4 GPS week: 1882 Day: 4 MJD: 57422.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2944 | 6 5 11 | 7 7 23 | 4 3 10 |
emr | emr 30 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
esa | esa 2880 | 6 7 13 | 9 11 28 | 6 5 17 |
gfz | gfz 2784 | 6 6 11 | 8 8 31 | 5 4 18 |
grg | grg 2880 | 7 7 14 | 9 10 32 | 11 8 25 |
igr | igr 2880 | 6 6 11 | 9 8 26 | 5 3 13 |
igs | igs 2880 | 6 6 11 | 8 8 29 | 5 4 14 |
jpl | jpl 2880 | 6 6 14 | 10 9 30 | 7 3 14 |
mit | mit 2880 | 5 6 11 | 9 14 33 | 5 5 15 |
Table 5.1882.5 GPS week: 1882 Day: 5 MJD: 57423.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2959 | 3 3 9 | 7 8 27 | 6 5 15 |
emr | emr 30 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
esa | esa 2880 | 5 4 12 | 7 9 31 | 8 6 17 |
gfz | gfz 2784 | 4 3 11 | 7 11 44 | 6 6 19 |
grg | grg 2879 | 5 5 14 | 8 11 39 | 10 8 22 |
igr | igr 2880 | 3 3 11 | 7 9 31 | 7 5 16 |
igs | igs 2880 | 4 3 11 | 8 8 30 | 6 6 16 |
jpl | jpl 2880 | 5 4 13 | 9 9 29 | 8 5 21 |
mit | mit 2880 | 4 4 11 | 8 10 37 | 6 6 16 |
Table 5.1882.6 GPS week: 1882 Day: 6 MJD: 57424.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2956 | 4 3 12 | 7 9 31 | 6 5 18 |
emr | emr 30 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
esa | esa 2880 | 5 5 16 | 9 11 39 | 8 7 19 |
gfz | gfz 2784 | 5 5 16 | 8 10 37 | 6 6 16 |
grg | grg 2880 | 5 5 17 | 7 8 38 | 11 8 23 |
igr | igr 2880 | 4 4 14 | 8 10 33 | 6 5 15 |
igs | igs 2880 | 4 4 15 | 8 10 34 | 6 5 16 |
jpl | jpl 2880 | 5 5 16 | 8 11 34 | 7 6 19 |
mit | mit 2880 | 4 4 15 | 9 10 34 | 6 5 18 |
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 6.1882 GPS week: 1882 MJD: 57418.500-57424.500
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 12 7 -6 -1 | 4 19
| 19 15 105 190 5 | 2
emr uuuuu | 7 -10 60 -16 6 | 44 50
| 26 15 129 70 10 | 4
esa uuuuu | 6 6 56 61 4 | 17 26
| 15 17 59 79 3 | 2
gfz uuuuu | 8 -32 70 58 2 | 9 22
| 11 18 125 30 4 | 2
grg uuuuu | -48 14 -185 -78 -2 | 51 55
| 15 25 22 66 8 | 3
igr xxxxx | -12 21 73 57 3 | -3 20
| 14 19 51 58 3 | 2
irf xxxxx | 19 -1 -65 -53 2 | -6 21
| 11 10 58 26 3 | 2
jpl uuuuu | -11 -56 58 65 9 | 31 42
| 24 22 32 81 16 | 3
mit uuuuu | 22 18 -149 -143 -7 | 14 24
| 24 17 120 42 4 | 3
ngs uuuuu | -7 29 -20 55 -2 | 8 22
| 39 28 183 116 7 | 3
sio uuxux | 16 34 -344 -76 6 | 56 59
| 10 11 97 68 6 | 2
Table 7.1882.0 GPS week: 1882 Day: 0 MJD: 57418.500
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 8 -138 274 0 | 4 18
emr uuuuu | 53 11 -1 109 21 | 37 43
esa uuuuu | 9 22 -22 71 -1 | 14 23
gfz uuuuu | -2 -35 48 45 -1 | 7 19
grg uuuuu | -74 -23 -142 -161 2 | 46 52
igr xxxxx | -10 -10 92 61 3 | -4 19
irf xxxxx | 6 -18 -2 -73 1 | -8 21
jpl uuuuu | 25 -54 92 157 36 | 26 35
mit uuuuu | -1 15 6 -167 -9 | 17 25
ngs uuuuu | -31 24 9 -140 -11 | 10 22
sio uuxux | 19 38 -294 -116 5 | 55 57
Table 7.1882.1 GPS week: 1882 Day: 1 MJD: 57419.500
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 6 -42 -62 -1 | 5 19
emr uuuuu | 10 10 -90 -39 7 | 41 49
esa uuuuu | 14 32 14 94 8 | 16 25
gfz uuuuu | 0 -26 33 40 2 | 9 21
grg uuuuu | -41 -12 -201 -80 3 | 48 53
igr xxxxx | -13 21 124 60 5 | -2 20
irf xxxxx | 15 -9 -25 -46 1 | -6 21
jpl uuuuu | -1 -38 17 58 19 | 31 42
mit uuuuu | 31 -10 -48 -94 -11 | 16 25
ngs uuuuu | -11 24 147 68 -6 | 10 22
sio uuxux | 18 21 -336 -92 4 | 56 59
Table 7.1882.2 GPS week: 1882 Day: 2 MJD: 57420.500
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 4 84 -96 5 | 6 19
emr uuuuu | 20 -12 -109 -71 4 | 45 51
esa uuuuu | -6 13 36 111 4 | 18 26
gfz uuuuu | 20 -18 -33 77 0 | 12 22
grg uuuuu | -59 18 -209 -160 -8 | 52 56
igr xxxxx | -20 48 116 77 0 | -1 19
irf xxxxx | 22 -2 -91 -56 1 | -4 19
jpl uuuuu | -46 -43 50 -40 5 | 34 45
mit uuuuu | 42 9 -192 -134 -6 | 17 25
ngs uuuuu | 2 11 179 207 -5 | 11 22
sio uuxux | 26 52 -422 -117 13 | 57 60
Table 7.1882.3 GPS week: 1882 Day: 3 MJD: 57421.500
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 13 148 -339 -4 | 4 20
emr uuuuu | -5 -23 135 43 -3 | 44 51
esa uuuuu | 4 2 44 159 1 | 16 26
gfz uuuuu | 4 -8 -91 42 1 | 9 22
grg uuuuu | -30 24 -186 -48 1 | 50 55
igr xxxxx | 9 26 49 158 0 | -4 22
irf xxxxx | 16 1 -157 -25 5 | -6 22
jpl uuuuu | -14 -41 72 137 -13 | 32 44
mit uuuuu | -1 31 -331 -147 -4 | 13 24
ngs uuuuu | 29 -4 93 115 10 | 6 22
sio uuxux | 9 39 -438 -67 10 | 55 59
Table 7.1882.4 GPS week: 1882 Day: 4 MJD: 57422.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 26 -97 103 -6 | 5 19
emr uuuuu | -31 -15 190 -86 13 | 45 51
esa uuuuu | -20 -3 155 -55 3 | 17 26
gfz uuuuu | -4 -31 71 30 7 | 9 22
grg uuuuu | -38 46 -198 26 -2 | 52 56
igr xxxxx | -4 27 -2 58 5 | -4 21
irf xxxxx | 17 9 -103 -91 5 | -5 21
jpl uuuuu | -15 -54 20 140 -4 | 31 44
mit uuuuu | 9 22 -236 -222 -1 | 12 24
ngs uuuuu | 54 21 -39 110 -1 | 7 22
sio uuxux | 2 23 -441 -164 10 | 56 59
Table 7.1882.5 GPS week: 1882 Day: 5 MJD: 57423.500
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 35 12 49 -6 | 1 17
emr uuuuu | -7 -28 206 -56 5 | 44 50
esa uuuuu | 16 -15 55 -39 8 | 15 23
gfz uuuuu | 21 -40 269 58 8 | 7 20
grg uuuuu | -45 37 -181 -45 -17 | 52 56
igr xxxxx | -9 2 19 -34 7 | -7 20
irf xxxxx | 14 8 -73 -60 3 | -8 20
jpl uuuuu | 7 -104 97 -18 7 | 28 41
mit uuuuu | 9 18 -185 -120 -8 | 9 21
ngs uuuuu | -29 80 -265 84 0 | 3 19
sio uuxux | 9 26 -175 33 -5 | 54 57
Table 7.1882.6 GPS week: 1882 Day: 6 MJD: 57424.500
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 | 18 -10 84 33 6 | 6 20
emr uuuuu | 9 -12 89 -9 -7 | 50 57
esa uuuuu | 27 -7 107 87 5 | 20 30
gfz uuuuu | 14 -64 194 118 -2 | 12 26
grg uuuuu | -49 12 -180 -80 6 | 55 59
igr xxxxx | -37 32 110 19 1 | -1 23
irf xxxxx | 42 2 -4 -17 -2 | -3 22
jpl uuuuu | -37 -56 55 23 10 | 33 47
mit uuuuu | 61 42 -56 -117 -10 | 12 24
ngs uuuuu | -62 50 -264 -57 -2 | 8 23
sio uuxux | 30 40 -304 -9 2 | 59 62
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