[IGSREPORT-24525] Wk 1899 IGS Final Orbits
IGS ACC
acc at igs.org
Thu Jun 16 16:57:01 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1899 (May 29, 2016 - Jun 04, 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:
igs1899[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1899[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1899[0-6].cls IGS GPS clock combination summary report.
igs18997.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18997.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 | 21 ZECK FAA1 MAC1 SYOG ZECK
0 | ESA | MAL2 MAL2 MAW1
0 | GFZ | 32 32 BJNM FAA1 IRKJ MAC1 MAL2 BJNM FAA1 IRKJ MAL2
0 | GFZ | NRMD
0 | GRG | HARB POHN ALRT ARTU POHN
0 | JPL | TUVA
1 | GFZ | 32 32 BJNM DRAG HYDE IRKJ MAL2 POHN SYOG IRKJ MAL2
1 | GFZ | POHN SYOG
1 | GRG | 18 18 FAA1 HARB POTS DRAG FAA1 HARB HYDE NNOR POTS
1 | GRG | SYOG
1 | JPL | 18
2 | COD | BOGT MAW1 NKLG
2 | ESA | BOGT MAL2 TWTF DRAG MAW1
2 | GFZ | 32 32 ALGO BJNM FAA1 IRKJ MAL2 ONSA POHN SYOG TWTF
2 | GFZ | BJNM FAA1 IRKJ ONSA POHN SYOG
2 | GRG | BOGT DRAG NNOR BOGT DRAG FAA1 HARB NNOR SYOG TWTF
2 | JPL | TUVA
3 | COD | GODE
3 | EMR | SYOG YAKT
3 | ESA | QAQ1 THTI QAQ1 THTI
3 | GFZ | 32 32 ALGO BRFT FAA1 GMSD GODE IRKJ MAL2 MAS1 NLIB
3 | GFZ | PRDS STHL SYOG ALGO IRKJ MAL2
3 | GRG | 18 DRAG GODE MAL2 DRAG FAA1 GODE SYOG
3 | JPL | THTI TUVA
4 | COD | HOB2 MAL2 HOB2 MAL2
4 | EMR | YAKT
4 | ESA | HOB2 DRAG HOB2
4 | GFZ | 32 32 ALGO BJNM DRAG FAA1 IRKJ MAL2 SYOG TWTF HOB2
4 | GFZ | MAL2 TWTF
4 | GRG | COCO HARB COCO DRAG HARB TWTF
4 | MIT | TWTF TWTF
5 | COD | 8 27 FAA1 FAA1 HOB2
5 | EMR | 8 27 8 27 THU3 YAKT
5 | ESA | HOB2 MAL2 DRAG HOB2 MAL2 REUN TONG
5 | GFZ | 32 32 ALGO DRAG FAA1 HOB2 MAL2 MATE POHN ALGO FAA1
5 | GFZ | HOB2 MAL2 MATE POHN
5 | GRG | BRFT HARB BRFT DRAG HARB SYOG
5 | JPL | 27 TUVA
5 | MIT | HOB2 HOB2
6 | COD | MAL2
6 | EMR | 8 HOB2
6 | ESA | DRAG
6 | GFZ | 32 32 ALGO FAA1 HOB2 MAL2 THU3 FAA1 IRKJ THU3
6 | GRG | 18 HARB DRAG HARB MAL2
6 | JPL | 8
6 | MIT | HOB2 IRKJ
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G08 | | | | | | 4 | 4 |
PRN G27 | | | | | | 4 | |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .0 -1.5 -.9 -31 -23 -20 .74
EMR | 0 | 4.6 -9.3 12.1 43 -4 8 .82
ESA | 0 | -.8 -2.3 -.2 -8 -23 51 .78
GFZ | 0 | -.5 -1.4 -2.0 -38 -71 -17 .95
GRG | 0 | 5.6 -9.5 -3.0 -31 -47 85 .78
JPL | 0 | 7.0 -7.3 12.7 1 1 19 1.04
MIT | 0 | -.3 -4.8 18.9 1 1 -53 .98
NGS | 0 | 3.3 -7.6 25.2 -170 -51 -39 .88
SIO | 0 | 3.2 -3.5 16.2 -9 -22 8 1.01
COD | 1 | .4 -1.9 -1.0 -40 -24 -27 .71
EMR | 1 | .8 -8.7 11.6 50 2 -24 .75
ESA | 1 | -.3 -2.8 -.5 -12 -23 25 .68
GFZ | 1 | .4 -1.2 -1.1 -49 -89 -4 .73
GRG | 1 | 8.6 -11.8 6.1 -16 -80 93 .79
JPL | 1 | -.0 -5.9 9.4 -4 3 18 .94
MIT | 1 | -3.9 -5.6 16.6 16 -7 -40 1.05
NGS | 1 | -3.1 -5.4 13.1 -85 -24 -32 .88
SIO | 1 | .7 -2.0 22.0 -31 -17 -1 .77
COD | 2 | -.9 -.5 -1.2 -25 -11 -3 .81
EMR | 2 | .3 -.7 13.4 36 -13 20 .86
ESA | 2 | -.4 -2.3 -.5 -5 -31 52 .81
GFZ | 2 | .2 -1.2 -1.3 -53 -79 -11 .86
GRG | 2 | 8.7 -2.7 11.4 -28 -72 117 .51
JPL | 2 | -.5 2.4 10.3 -17 10 1 .37
MIT | 2 | -3.1 -2.7 18.2 19 3 -30 .97
NGS | 2 | -2.6 -1.0 31.1 -187 -33 -54 .68
SIO | 2 | 5.0 1.1 20.9 2 -21 19 .75
COD | 3 | .1 -1.5 -.4 -71 -18 -27 .66
EMR | 3 | -2.0 2.5 11.3 32 -17 21 .85
ESA | 3 | -.2 -2.8 -1.0 -29 -25 10 .61
GFZ | 3 | .7 -.8 -1.2 -61 -84 -48 .73
GRG | 3 | 4.5 -3.7 -5.5 -2 -95 94 .37
JPL | 3 | 5.8 -.1 7.5 -17 28 34 .40
MIT | 3 | .3 -4.4 21.1 17 1 -22 .98
NGS | 3 | 1.1 -7.3 18.8 -121 -40 -14 .78
SIO | 3 | 4.5 -.3 24.4 -16 -15 12 .76
COD | 4 | -.2 -1.4 -1.2 -46 15 -16 .76
EMR | 4 | -2.7 3.5 9.4 17 -5 -20 .60
ESA | 4 | -.7 -1.5 -1.4 -6 -14 30 .35
GFZ | 4 | .1 -1.5 -2.2 -56 -70 -23 .62
GRG | 4 | 5.4 -3.4 5.3 -4 -64 85 .47
JPL | 4 | -3.6 2.6 9.2 -14 29 8 .36
MIT | 4 | -1.8 -7.9 15.6 -3 2 -32 1.07
NGS | 4 | -.1 -7.7 19.3 -134 -22 -18 .94
SIO | 4 | 2.7 -3.8 21.2 -19 -22 8 .88
COD | 5 | -.9 -2.2 -1.0 -64 -4 -22 .86
EMR | 5 | -14.4 19.6 13.7 58 18 -5 .61
ESA | 5 | -1.5 -2.1 -.5 -5 -13 44 .46
GFZ | 5 | .3 -1.1 -.8 -39 -89 -8 .67
GRG | 5 | 6.4 -2.1 17.0 -30 -73 85 .26
JPL | 5 | -13.1 -2.5 9.3 3 -9 -39 .71
MIT | 5 | -6.5 -6.3 16.2 7 -13 -14 .90
NGS | 5 | -6.3 -15.6 26.6 -210 4 -92 .77
SIO | 5 | 1.8 -3.5 27.3 -31 1 -36 .55
COD | 6 | -.1 -1.2 -.2 -45 -14 -6 .72
EMR | 6 | -4.1 2.9 18.9 43 1 -31 .63
ESA | 6 | -.1 -2.5 -.9 -18 -35 6 .54
GFZ | 6 | .8 -.9 -1.1 -51 -88 -42 .51
GRG | 6 | 2.3 -5.4 19.0 -32 -85 102 .61
JPL | 6 | 3.5 -7.8 5.3 21 -10 -27 .38
MIT | 6 | -3.5 -12.0 15.9 -12 -5 -38 .89
NGS | 6 | 3.9 -10.5 19.5 -154 -26 -19 .81
SIO | 6 | -.5 -7.0 11.6 -38 -4 -6 .46
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1899.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1899.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 2.1899.[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 3.1899.[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 5.1899.0-6). 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 1899 summary. (May 29, 2016 - Jun 04, 2016)
Table 1.1899.a GPS week: 1899 MJD: 57537.000-57543.000
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 239| 0 0 -3 13 0 -7 .13 11 11 | -1331 160 13 165
| 1 0 2 20 15 15 .06 | 103 175
emr 80| 0 3 2 23 5 9 .29 10 10 | 4036 -257 15 124
| 2 5 2 13 20 16 .04 | 602 403
esa 150| 0 0 -4 -3 0 8 -.47 7 7 | -709 -50 7 162
| 0 0 1 10 11 17 .02 | 521 1084
gfz 207| 0 0 1 0 -14 -20 .11 11 11 | -357 150 11 145
| 1 1 1 15 4 11 .02 | 311 452
grg 115| 2 -2 -4 -20 28 44 -.13 15 14 | -73 101 13 198
| 1 1 6 17 19 15 .11 | 123 173
igr n/a| 0 0 -1 12 14 -4 -.03 4 4 | 11370 -154 15 88
| 0 0 1 11 11 12 .01 | 480 353
jpl 80| -1 1 0 11 20 1 .29 9 9 | 2421 -184 15 124
| 3 1 0 16 17 14 .04 | 658 374
mit 350| 0 -2 5 -22 -31 -3 -.12 13 12 | -135 -104 47 366
| 0 1 1 22 23 17 .05 | 165 145
ngs 227| 0 0 7 -11 -4 -2 .12 11 9 | -1293 126 811 1970
| 1 0 3 14 15 25 .08 | 110 160
sio 298| 0 0 -3 -3 -26 -18 -.06 15 14 | --- --- --- ---
| 1 0 0 22 22 46 .06 | --- ---
Table 1.1899.b GPS week : 1899 MJD: 57537.000-57543.000
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 | 3 3 3 3 3 4 4 |
2 | 4 5 4 4 4 4 4 |
3 | 3 3 3 3 3 4 3 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 4 4 4 4 4 |
6 | 3 3 3 3 3 3 3 |
7 | 4 4 4 4 4 4 4 |
8 | 3 4 4 4 5 7 10 |
9 | 4 3 3 3 3 3 4 |
10 | 3 3 3 3 3 4 4 |
11 | 4 4 4 4 4 5 5 |
12 | 5 4 5 5 4 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 5 5 |
15 | 4 4 4 4 4 4 4 |
16 | 5 5 5 5 5 6 6 |
17 | 4 4 3 3 3 4 3 |
18 | 4 4 5 5 4 5 5 |
19 | 5 4 4 4 4 5 4 |
20 | 3 4 4 3 3 4 4 |
21 | 5 5 5 5 5 6 5 |
22 | 3 3 3 3 3 4 3 |
23 | 4 4 5 4 5 5 4 |
24 | 4 4 4 3 3 4 4 |
25 | 3 3 3 3 3 4 4 |
26 | 3 3 3 3 3 4 3 |
27 | 3 3 4 3 4 7 4 |
28 | 4 3 3 4 4 5 4 |
29 | 4 4 5 4 4 4 4 |
30 | 3 3 3 3 3 4 3 |
31 | 4 4 3 3 4 4 4 |
32 | 3 3 3 3 3 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 2.1899.0 GPS week: 1899 Day: 0 MJD: 57537.000
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 242| 0 0 -4 -3 8 -21 .12 10 10 | -1413 343 13 161
emr 80| 1 -2 0 3 3 -6 .32 9 9 | 4625 -484 13 141
esa 150| -1 0 -2 4 -8 13 -.46 6 6 | -1511 929 7 164
gfz 208| -1 1 2 11 -11 -14 .15 11 11 | -597 250 12 178
grg 118| 0 0 -9 -32 38 28 -.30 14 14 | -116 127 13 248
igr n/a| 0 0 -2 17 -5 5 -.02 4 4 | 11674 -92 15 112
jpl 80| 0 2 0 30 2 -5 .33 8 8 | 2865 -71 17 127
mit 350| 1 0 6 -26 -36 14 -.11 14 13 | -60 -104 51 308
ngs 227| 0 1 8 -24 16 -4 .04 10 8 | -1417 345 699 2195
sio 300| 0 0 -2 18 -35 -3 -.03 15 14 | --- --- --- ---
Table 2.1899.1 GPS week: 1899 Day: 1 MJD: 57538.000
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 -2 -12 13 -23 .06 11 10 | -1227 104 13 165
emr 80| 0 -1 1 32 25 10 .27 8 8 | 4031 175 13 117
esa 150| 0 -1 -4 -5 12 13 -.51 8 8 | -1136 314 8 159
gfz 208| 0 0 2 -7 -16 -35 .11 11 11 | -626 589 11 136
grg 116| 3 -2 -8 7 4 31 .06 18 17 | -127 82 12 153
igr n/a| 0 0 0 3 22 -5 -.05 4 4 | 11390 167 14 95
jpl 80| 0 0 0 1 13 16 .27 7 7 | 2619 210 15 124
mit 350| 0 0 5 -14 -67 15 -.18 13 12 | -145 -59 43 345
ngs 225| 0 0 4 -18 -13 -30 .01 10 8 | -1211 89 760 2062
sio 299| 0 1 -2 0 -31 31 -.12 15 13 | --- --- --- ---
Table 2.1899.2 GPS week: 1899 Day: 2 MJD: 57539.000
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 240| 0 0 -5 9 -9 -7 .10 11 11 | -1298 166 12 161
emr 80| 0 0 0 21 -15 5 .32 8 8 | 4360 -10 12 119
esa 150| 0 -1 -5 10 -21 23 -.48 8 8 | -18 -1727 8 166
gfz 209| 0 0 0 8 -21 -23 .11 11 11 | 1 -374 10 126
grg 115| 0 -2 -3 -10 60 37 -.14 12 12 | 50 -80 12 197
igr n/a| 0 0 -1 -6 10 -20 -.05 4 4 | 11702 -22 16 96
jpl 80| 0 1 0 1 26 -19 .28 8 8 | 2987 -106 16 144
mit 350| 0 -1 4 -42 4 6 -.17 12 11 | 159 -241 46 400
ngs 226| 0 1 13 -16 -7 -33 .08 11 9 | -1286 163 944 1900
sio 292| 0 0 -3 -1 -7 18 -.14 14 13 | --- --- --- ---
Table 2.1899.3 GPS week: 1899 Day: 3 MJD: 57540.000
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 -1 -1 4 -21 -5 .17 12 11 | -1524 409 14 161
emr 80| -1 2 2 25 2 30 .33 8 8 | 4298 67 12 102
esa 150| 0 0 -3 -21 5 -20 -.46 6 6 | -389 -1009 7 154
gfz 207| 0 0 3 -21 -7 -35 .11 11 11 | -415 203 11 152
grg 113| 2 -2 -12 -4 36 44 -.14 14 13 | -264 368 14 191
igr n/a| 0 0 0 23 26 -16 -.04 4 4 | 11597 90 15 70
jpl 80| 0 1 0 3 47 -7 .32 8 8 | 2822 -219 14 124
mit 350| 0 -2 5 9 -35 -1 -.12 12 11 | -368 176 42 387
ngs 227| 0 0 6 3 -14 15 .13 10 8 | -1400 245 727 1871
sio 297| 1 1 -3 18 -42 15 -.07 14 14 | --- --- --- ---
Table 2.1899.4 GPS week: 1899 Day: 4 MJD: 57541.000
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 0 -3 42 -16 -13 .09 12 11 | -1326 192 13 166
emr 80| 0 4 2 17 -25 8 .31 10 10 | 4542 -965 15 131
esa 150| 0 -1 -5 1 5 10 -.46 7 7 | -265 -487 8 163
gfz 208| 0 -1 2 10 -12 -11 .12 11 10 | 129 -566 10 141
grg 116| 2 -3 -2 -36 26 45 -.13 13 12 | 38 -136 13 210
igr n/a| 0 -1 -2 21 16 -4 -.03 4 4 | 11837 -879 15 92
jpl 80| -2 2 0 -7 32 8 .25 9 9 | 2710 -958 14 109
mit 350| 1 -2 6 -37 -13 -28 -.12 12 11 | -94 -269 44 390
ngs 229| 0 0 4 14 17 16 .18 10 9 | -1115 -97 791 1973
sio 302| 1 1 -2 -15 -47 -37 -.07 15 14 | --- --- --- ---
Table 2.1899.5 GPS week: 1899 Day: 5 MJD: 57542.000
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| 2 -2 0 39 16 -6 .22 13 12 | -1258 -73 18 171
emr 80| -3 13 5 18 23 31 .22 14 14 | 3236 -105 17 128
esa 150| 1 -1 -6 -3 9 27 -.45 8 7 | -811 283 8 161
gfz 206| -1 -2 0 -20 -14 -5 .09 11 10 | -646 370 11 138
grg 113| 4 -4 -1 -37 4 51 -.05 17 17 | -149 114 15 183
igr n/a| 0 -1 -3 6 24 -1 -.02 5 5 | 10754 -34 17 64
jpl 80| -7 2 0 14 26 -3 .23 11 11 | 1512 73 15 126
mit 350| 1 -4 2 2 -25 -11 -.05 13 12 | -245 -98 56 374
ngs 227| 1 0 9 -23 -22 -16 .20 12 10 | -1248 -59 1104 2019
sio 301| 3 0 -4 0 -37 -58 .02 16 17 | --- --- --- ---
Table 2.1899.6 GPS week: 1899 Day: 6 MJD: 57543.000
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 -6 15 12 24 .18 11 10 | -1274 -18 13 175
emr 80| 3 4 4 46 25 -11 .23 14 14 | 3164 -479 23 131
esa 150| 0 0 -3 -6 1 -7 -.48 8 7 | -839 1341 9 171
gfz 206| -3 0 0 15 -15 -14 .09 11 11 | -346 582 13 146
grg 116| 0 -2 7 -27 27 74 -.19 18 16 | 56 236 13 209
igr n/a| -1 0 -3 20 7 14 -.04 5 4 | 10638 -314 17 90
jpl 80| 2 -1 -1 38 -3 19 .31 11 11 | 1433 -222 16 115
mit 350| 0 -3 5 -50 -47 -21 -.07 13 11 | -194 -138 51 359
ngs 232| -1 0 4 -14 -6 34 .19 11 8 | -1374 198 654 1775
sio 299| 0 1 -4 -45 14 -93 .01 14 13 | --- --- --- ---
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 3.1899.0 GPS week: 1899 Day: 0 MJD: 57537.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 5 4 10 7 3 8 11 7 12 2 | 20 24 15 24 18 18 26 18 23 22 19
2 | 9 10 8 14 17 4 9 18 14 17 4 | 25 29 24 22 22 21 27 26 26 19 22
3 | 8 9 5 9 9 3 8 11 4 9 2 | 42 43 37 45 34 39 45 39 43 41 40
X4 | 3 --- --- --- --- 67 --- --- --- --- 0 | 45 --- --- --- --- 31 --- --- --- --- 44
5 | 7 7 6 9 14 4 8 18 11 18 3 | 41 41 38 36 40 37 40 37 38 37 37
6 | 10 7 6 9 10 3 8 11 5 14 3 | 20 24 14 19 23 17 24 16 18 26 18
7 | 7 10 6 13 14 5 11 19 11 16 4 | 21 24 14 24 22 18 24 17 23 15 17
8E | 8 6 7 9 16 3 8 12 8 15 3 | 141 141 137 141 143 140 112 139 136 143 139
9 | 13 19 5 7 11 3 9 9 6 7 3 | 21 28 14 20 20 17 25 19 23 20 18
10 | 6 8 4 5 8 3 8 10 9 15 2 | 43 44 39 41 36 40 44 43 44 38 40
11 | 5 9 12 11 11 3 8 14 8 17 3 | 22 30 23 29 22 23 29 24 31 24 24
12 | 10 9 7 15 17 5 8 17 13 21 4 | 24 23 17 23 21 17 22 15 23 18 17
13 | 11 7 4 8 17 4 8 12 10 13 3 | 22 25 19 25 24 21 24 22 25 18 20
14 | 10 12 6 11 14 4 7 15 11 16 3 | 22 19 12 21 18 14 18 18 21 15 15
15 | 9 7 4 11 16 4 8 16 11 16 3 | 26 24 18 27 26 21 26 20 25 15 20
16 | 15 10 7 17 15 5 9 24 11 19 4 | 29 24 17 21 27 17 24 17 19 13 17
17E | 12 10 6 11 15 4 12 12 10 11 3 | 29 26 21 28 23 23 27 23 28 25 23
18 | 9 5 8 19 8 3 5 15 14 18 4 | 23 23 23 23 22 20 24 27 29 22 22
19E | 24 10 7 12 17 3 9 19 9 14 4 | 35 27 21 25 26 22 27 23 25 21 22
20 | 7 7 8 8 8 4 7 14 8 15 3 | 26 27 26 27 24 23 25 30 29 20 24
21 | 9 9 9 13 14 4 9 24 16 18 4 | 30 28 23 27 26 24 28 29 31 21 24
22 | 7 5 7 12 8 3 6 13 9 13 3 | 28 24 24 30 21 23 25 23 29 22 23
23 | 17 10 4 14 18 4 7 14 12 16 4 | 27 20 14 21 25 15 22 19 19 13 16
24 | 7 15 5 9 13 4 8 10 8 19 3 | 21 23 15 20 23 19 23 22 23 22 18
25 | 5 12 5 6 14 4 6 9 9 13 3 | 15 22 12 19 19 13 18 15 18 21 15
26 | 10 9 5 8 12 4 8 12 6 9 3 | 26 26 16 22 26 20 27 17 23 19 20
27E | 7 9 6 7 14 4 7 10 6 12 3 | 91 93 89 91 89 91 28 89 91 92 90
28 | 6 7 4 12 14 4 9 10 8 20 3 | 20 23 17 24 20 16 21 18 19 18 17
29E | 11 10 7 12 16 4 13 15 14 11 4 | 31 26 26 30 26 26 27 28 34 26 25
30 | 7 7 5 7 13 3 8 15 9 10 3 | 25 24 17 23 23 19 25 21 24 21 20
31 | 10 8 6 9 13 4 8 13 10 15 3 | 26 27 15 22 20 17 25 12 20 15 18
32 | 11 7 6 8 13 3 8 11 8 10 3 | 34 34 31 29 37 30 34 30 30 33 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 9 6 11 14 4 8 14 10 15 |T 32 32 26 31 30 27 29 28 31 28 28
WRMS | 10 9 6 11 14 4 8 13 8 14 |NE 26 27 20 25 24 21 26 22 26 21 22
MEDI | 9 9 6 10 14 4 8 13 9 15 |MD 26 26 19 24 23 21 25 22 25 21 20
Table 3.1899.1 GPS week: 1899 Day: 1 MJD: 57538.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 7 6 9 19 5 6 8 5 12 3 | 21 26 15 20 22 17 24 17 19 24 19
2 | 8 7 10 12 24 4 8 17 15 21 4 | 25 26 22 19 33 19 25 20 20 21 21
3 | 9 7 7 8 17 4 8 9 7 9 3 | 30 36 25 32 29 30 36 28 31 32 30
X4 | 2 --- --- --- --- 26 --- --- --- --- 0 | 36 --- --- --- --- 24 --- --- --- --- 35
5 | 8 6 8 10 15 4 7 15 10 21 3 | 22 25 21 25 28 20 25 19 22 27 21
6 | 9 7 5 6 16 4 6 11 6 12 3 | 20 24 13 18 25 16 23 15 16 20 17
7 | 9 8 7 12 15 4 10 16 11 17 4 | 20 23 15 25 22 19 24 18 21 18 18
8E | 11 6 7 10 16 5 6 12 11 15 3 | 112 114 110 112 115 111 90 113 113 115 111
9 | 9 12 8 6 19 3 7 7 7 8 3 | 21 26 14 22 27 17 24 16 19 17 18
10 | 7 7 6 9 17 6 7 9 9 13 3 | 27 31 24 29 29 25 30 27 26 24 26
11 | 9 11 16 11 19 5 6 12 8 14 4 | 21 26 19 25 24 21 25 22 24 23 21
12 | 15 7 8 12 14 6 8 16 13 22 4 | 27 23 16 22 28 17 22 16 21 22 18
13 | 11 7 7 9 19 3 7 13 10 13 3 | 23 23 16 23 28 19 23 19 23 17 19
14 | 10 8 9 12 28 4 8 12 9 15 4 | 24 21 18 27 27 19 20 18 18 18 18
15 | 8 7 6 11 19 3 7 13 11 14 3 | 24 23 18 28 29 20 23 17 22 17 20
16 | 14 10 7 17 20 4 8 21 12 21 4 | 26 24 16 21 33 17 23 18 18 15 17
17E | 13 8 7 9 15 3 9 9 11 11 3 | 30 27 23 30 31 25 27 24 29 27 25
18 | 10 5 10 18 15 4 5 16 11 21 4 | 19 19 19 22 23 15 17 18 16 18 15
19E | 20 8 7 8 17 3 6 14 10 15 4 | 33 27 21 26 35 24 27 23 27 26 24
20 | 7 6 10 9 14 3 6 14 9 16 3 | 18 19 18 22 21 16 17 20 15 19 16
21 | 10 6 10 15 20 6 7 24 15 18 4 | 28 27 22 24 32 22 26 22 20 19 22
22 | 9 5 8 10 16 4 5 10 9 13 3 | 26 22 20 25 27 22 23 16 19 21 20
23 | 15 12 7 13 24 5 7 13 12 16 4 | 26 22 17 21 31 18 23 17 17 13 17
24 | 10 9 7 9 20 4 8 11 10 9 3 | 24 21 18 21 30 20 22 19 24 18 19
25 | 11 8 7 6 10 5 6 7 10 18 3 | 15 21 10 19 24 14 17 14 17 23 15
26 | 11 8 7 11 17 3 7 7 6 13 3 | 23 24 16 20 29 19 24 18 20 19 19
27E | 10 6 5 10 22 3 7 8 12 11 3 | 82 84 79 80 86 81 28 81 83 83 81
28 | 7 7 7 11 16 5 6 10 9 16 3 | 21 23 18 25 29 18 23 17 20 16 18
29E | 10 9 8 15 22 5 10 15 12 12 4 | 30 26 24 33 33 26 25 26 30 27 26
30 | 14 7 5 9 13 4 7 13 5 9 3 | 26 22 14 22 25 18 23 19 22 20 19
31 | 12 7 9 10 16 5 5 12 9 15 3 | 27 27 18 25 28 21 23 14 20 16 20
32 | 11 8 6 9 24 3 6 10 5 9 3 | 25 27 21 28 33 23 27 23 23 25 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 8 8 11 18 4 7 13 10 15 |T 29 29 23 28 32 24 26 24 26 25 25
WRMS | 10 8 8 11 17 4 7 12 8 13 |NE 23 24 17 23 27 19 23 18 20 20 20
MEDI | 10 7 7 10 17 4 7 12 10 14 |MD 25 24 18 25 29 19 24 19 21 20 19
Table 3.1899.2 GPS week: 1899 Day: 2 MJD: 57539.000
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 5 7 8 6 4 5 7 7 10 2 | 23 25 14 23 17 18 26 21 22 25 20
2 | 8 8 9 12 11 4 9 16 12 18 4 | 22 27 21 19 23 20 28 26 23 23 22
3 | 8 7 10 8 7 3 8 11 7 9 3 | 34 40 26 38 33 33 42 33 44 36 35
X4 | 3 --- --- --- --- 64 --- --- --- --- 0 | 37 --- --- --- --- 49 --- --- --- --- 37
5 | 9 6 9 10 9 4 6 14 11 18 3 | 32 32 27 26 24 25 31 25 27 32 27
6 | 8 8 5 5 8 5 8 10 8 9 2 | 19 27 15 20 19 17 26 18 19 24 20
7 | 9 9 7 12 10 4 11 14 9 14 3 | 21 25 15 23 22 20 26 21 26 23 20
8E | 16 10 8 10 15 4 10 11 12 12 4 | 75 76 75 75 78 73 60 75 76 74 74
9 | 12 11 7 7 10 4 9 8 8 9 3 | 20 22 8 20 20 14 24 18 23 19 17
10 | 7 7 5 12 5 4 7 9 8 15 3 | 33 33 28 31 28 29 35 31 40 32 31
11 | 8 10 16 12 11 5 7 11 6 11 3 | 21 26 18 23 22 19 26 24 27 20 21
12 | 15 14 8 15 17 7 9 16 13 19 5 | 30 31 22 23 24 20 22 21 27 27 22
13 | 11 8 7 10 13 4 8 13 11 14 3 | 23 22 16 21 25 18 24 23 22 17 19
14 | 11 8 7 14 17 4 8 11 10 16 4 | 20 16 12 21 20 15 16 17 23 17 14
15 | 11 9 7 11 16 3 7 13 13 14 4 | 27 23 17 22 27 18 24 20 22 19 19
16 | 16 10 7 17 13 5 8 22 15 19 5 | 29 25 18 24 29 19 24 21 25 19 19
17E | 13 7 6 8 10 5 10 8 10 10 3 | 34 31 27 32 25 29 32 28 29 33 29
18 | 11 7 10 18 8 6 5 15 14 23 4 | 20 18 18 19 17 15 17 21 22 26 17
19E | 19 9 8 8 12 5 7 12 10 14 4 | 34 31 25 29 26 25 31 26 27 28 27
20 | 9 6 12 13 9 5 7 13 12 17 3 | 22 19 20 24 21 18 19 25 24 23 20
21 | 10 9 10 14 13 5 9 26 14 22 5 | 28 27 22 23 28 22 29 25 26 24 23
22 | 7 6 11 11 7 3 5 11 10 12 3 | 24 23 20 28 24 23 24 19 32 21 22
23 | 19 10 8 14 14 3 7 12 12 18 4 | 27 20 12 19 24 15 23 16 22 15 16
24 | 14 11 7 9 12 5 10 8 8 7 3 | 26 27 17 19 23 18 24 22 26 21 21
25 | 6 8 7 8 12 4 7 8 12 8 3 | 18 22 17 22 21 17 19 17 22 21 18
26 | 8 7 5 9 7 4 7 6 8 11 2 | 20 22 16 20 24 18 23 20 24 24 19
27E | 10 7 7 9 16 4 8 8 12 10 3 | 58 60 57 60 55 57 23 57 63 55 57
28 | 7 6 7 10 10 4 7 9 9 19 3 | 22 25 19 26 23 19 23 20 24 23 20
29E | 12 12 8 18 18 5 13 14 13 12 4 | 27 24 22 30 25 23 25 26 31 26 24
30 | 10 8 5 7 9 4 7 8 6 8 2 | 27 25 18 25 25 21 25 22 28 26 23
31 | 11 6 6 10 10 5 5 10 11 10 3 | 23 24 16 23 26 18 21 16 25 18 19
32 | 11 7 7 9 17 4 8 8 8 10 3 | 32 33 25 30 33 27 31 27 27 30 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 8 8 11 12 4 8 12 11 14 |T 28 28 22 27 26 24 26 25 28 26 25
WRMS | 11 8 8 11 12 4 8 11 9 13 |NE 25 25 18 23 23 20 25 21 25 23 21
MEDI | 10 8 7 10 11 4 8 11 10 12 |MD 26 25 18 23 24 19 24 22 26 24 21
Table 3.1899.3 GPS week: 1899 Day: 3 MJD: 57540.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 8 5 8 11 3 6 7 7 8 2 | 22 27 18 23 24 19 25 20 24 24 21
2 | 11 7 8 11 17 4 9 15 13 18 4 | 26 28 23 22 25 22 25 24 24 17 22
3 | 7 8 5 7 11 4 8 6 5 9 2 | 37 43 33 40 32 37 43 37 39 37 37
X4 | 3 --- --- --- --- 63 --- --- --- --- 0 | 65 --- --- --- --- 28 --- --- --- --- 64
5 | 9 6 7 9 13 4 8 13 11 19 3 | 38 34 32 32 37 33 36 30 33 35 32
6 | 9 6 4 6 7 4 6 9 7 9 2 | 20 26 18 22 25 19 24 18 22 23 20
7 | 11 10 6 12 12 5 10 12 9 15 3 | 24 24 15 23 20 19 24 17 23 18 18
8E | 17 12 6 9 14 5 10 10 12 12 4 | 132 134 130 132 135 131 112 134 133 133 132
9 | 12 8 5 6 11 4 10 8 8 9 3 | 22 24 13 21 24 17 24 20 22 18 18
10 | 7 7 5 10 10 4 6 9 7 13 2 | 38 39 35 40 32 36 38 37 36 32 35
11 | 8 13 14 11 12 4 8 10 8 11 4 | 21 29 21 26 26 21 28 25 27 20 23
12 | 14 9 5 16 16 5 10 15 12 21 4 | 29 27 18 26 25 20 24 17 25 21 20
13 | 9 10 5 10 15 3 9 13 12 13 3 | 24 23 18 24 24 20 25 22 23 16 20
14 | 13 8 5 12 17 3 8 12 10 17 3 | 24 23 20 23 24 19 21 21 22 17 19
15 | 8 8 4 13 18 4 8 13 10 15 3 | 27 26 20 26 30 22 26 21 24 14 21
16 | 15 11 7 18 15 5 8 21 13 19 4 | 29 25 19 24 29 19 23 20 21 16 19
17E | 16 7 5 8 16 3 7 8 8 11 3 | 34 30 29 31 36 29 30 27 34 30 29
18 | 9 7 10 22 11 4 5 14 9 22 4 | 21 23 20 25 22 20 21 23 21 22 19
19E | 21 7 6 7 12 4 7 11 9 12 3 | 30 25 22 25 28 23 24 26 28 22 22
20 | 8 6 8 9 12 3 8 9 7 14 3 | 25 23 21 25 20 22 21 25 25 19 21
21 | 11 8 8 14 17 4 8 26 14 20 5 | 28 30 22 29 30 23 28 27 27 20 24
22 | 7 5 7 9 11 4 5 10 8 14 3 | 25 27 22 27 23 22 25 21 25 21 22
23 | 17 11 5 13 17 4 8 12 13 18 4 | 27 22 15 21 28 17 22 20 23 12 17
24 | 10 9 4 9 14 4 9 10 9 8 3 | 26 26 18 23 25 20 24 25 24 22 21
25 | 11 9 4 7 14 2 10 7 9 14 3 | 20 23 13 22 25 16 22 17 20 20 17
26 | 9 7 5 8 12 4 7 8 8 9 2 | 27 27 18 24 27 20 26 21 24 22 22
27E | 14 7 5 9 15 3 8 9 10 10 3 | 84 88 83 88 87 86 32 85 91 86 85
28 | 12 9 6 11 14 4 7 11 11 20 3 | 25 26 18 21 24 17 23 20 19 19 18
29E | 8 9 5 12 20 5 13 14 12 11 4 | 27 26 22 30 28 24 24 26 30 23 24
30 | 11 9 4 8 13 4 8 9 7 8 3 | 28 24 16 22 22 21 24 20 27 21 21
31 | 7 7 7 9 17 3 6 10 11 14 3 | 24 28 17 25 26 20 25 17 22 17 20
32 | 11 9 6 9 17 4 8 8 7 10 3 | 31 35 28 27 38 28 33 28 26 31 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 8 6 11 14 4 8 12 10 14 |T 33 32 26 31 32 27 29 28 31 27 29
WRMS | 11 8 6 11 13 4 8 11 8 14 |NE 27 27 20 25 26 22 26 22 24 21 23
MEDI | 11 8 5 9 14 4 8 10 9 13 |MD 27 26 20 25 26 21 25 22 24 21 21
Table 3.1899.4 GPS week: 1899 Day: 4 MJD: 57541.000
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 | 5 7 6 9 9 4 7 10 8 10 2 | 23 24 14 25 20 19 24 20 25 25 19
2 | 10 10 8 12 15 5 10 13 13 18 4 | 27 25 21 24 25 21 26 25 25 18 21
3 | 9 9 7 9 9 4 8 7 7 13 3 | 26 37 20 28 27 26 36 28 28 32 27
X4 | 3 --- --- --- --- 39 --- --- --- --- 0 | 40 --- --- --- --- 32 --- --- --- --- 39
5 | 10 9 8 8 12 4 8 12 12 18 3 | 28 31 27 27 29 25 31 26 31 32 27
6 | 8 9 6 6 8 3 6 8 8 13 2 | 20 24 15 19 19 16 24 17 20 23 17
7 | 11 10 5 14 13 4 9 13 9 16 4 | 25 27 13 25 21 19 24 17 26 21 19
8E | 29 11 6 11 14 5 11 13 13 16 5 | 137 137 136 140 140 137 98 141 135 144 137
9 | 13 10 6 6 11 5 9 8 7 9 3 | 20 24 12 18 21 15 24 18 19 17 17
10 | 9 8 4 11 9 5 9 12 9 13 3 | 32 33 27 35 25 29 33 32 33 30 29
11 | 7 13 17 10 12 4 9 11 8 12 4 | 19 28 18 25 25 19 27 23 24 18 20
12 | 11 10 6 15 13 4 9 14 12 22 4 | 25 24 15 21 20 16 22 11 21 15 15
13 | 10 9 5 11 14 4 12 13 11 17 4 | 25 23 16 24 26 18 24 22 23 15 18
14 | 9 11 9 11 14 4 8 13 10 18 4 | 22 21 15 19 18 14 18 18 19 15 15
15 | 9 9 7 11 15 3 10 13 10 16 3 | 25 24 16 23 25 19 25 20 23 12 18
16 | 19 10 7 19 15 5 9 23 15 18 5 | 33 26 18 22 26 18 24 17 23 12 17
17E | 9 8 6 8 17 4 9 10 9 11 3 | 21 21 17 24 21 19 22 19 28 21 18
18 | 9 7 9 20 10 4 9 13 11 19 4 | 20 18 17 19 18 13 20 18 19 18 14
19E | 14 12 7 7 12 5 7 12 11 12 3 | 31 29 26 29 25 27 30 31 33 27 26
20 | 5 8 10 9 10 3 9 10 9 14 3 | 20 17 16 20 17 16 15 22 21 18 16
21 | 9 10 9 14 13 3 10 26 13 19 5 | 28 27 21 26 24 21 28 24 25 14 21
22 | 8 6 11 10 7 4 5 11 9 12 3 | 21 22 17 20 19 16 21 16 23 20 17
23 | 20 11 7 14 15 4 7 14 11 19 4 | 28 20 14 18 24 14 21 17 19 9 14
24 | 6 11 6 11 11 4 11 13 7 9 3 | 21 25 16 20 22 16 23 21 21 20 18
25 | 7 10 5 7 12 4 11 8 10 13 3 | 16 21 9 21 17 13 22 13 19 12 13
26 | 10 8 5 7 13 4 8 9 9 8 3 | 25 28 17 23 25 19 25 20 25 19 20
27E | 15 10 6 11 14 3 11 7 12 11 3 | 98 96 93 99 104 95 32 96 95 98 96
28 | 13 9 7 11 11 5 7 12 10 22 4 | 23 25 17 22 21 16 22 18 22 16 17
29E | 10 11 6 12 17 4 12 10 11 10 4 | 26 22 17 27 24 21 22 19 27 19 19
30 | 10 8 6 9 13 4 11 10 7 9 3 | 24 24 14 20 23 18 23 19 25 22 19
31 | 10 9 6 9 17 6 7 12 10 13 3 | 24 27 14 23 23 17 22 15 22 17 18
32 | 8 10 7 6 15 4 9 9 9 12 3 | 31 35 28 27 33 29 33 26 25 32 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 10 7 11 13 4 9 12 10 15 |T 30 31 23 29 29 25 27 26 29 26 25
WRMS | 11 10 7 10 12 4 9 11 9 14 |NE 24 25 17 22 22 19 24 20 23 19 19
MEDI | 9 10 6 11 13 4 9 12 10 13 |MD 25 25 17 23 24 19 24 20 24 19 18
Table 3.1899.5 GPS week: 1899 Day: 5 MJD: 57542.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 14 7 8 11 4 7 8 8 13 3 | 25 30 14 26 19 20 28 22 24 23 20
2 | 7 11 10 10 19 4 9 13 15 19 4 | 22 30 20 22 25 18 24 21 24 17 20
3 | 9 13 7 9 11 4 12 6 7 12 3 | 29 38 17 23 25 22 37 25 27 27 25
X4 | 4 --- --- --- --- 48 --- --- --- --- 0 | 38 --- --- --- --- 30 --- --- --- --- 35
5 | 8 10 8 8 13 4 10 13 14 19 4 | 29 27 26 25 25 23 26 22 29 33 24
6 | 13 11 6 4 10 5 8 10 10 9 3 | 17 28 11 18 20 15 24 16 20 20 16
7 | 15 16 5 13 12 6 10 13 11 17 4 | 25 30 14 22 20 18 27 15 26 18 18
X8E | 22 26 8 12 19 8 --- 12 24 18 6 | 155 157 156 162 159 161 --- 156 165 159 158
9 | 8 15 6 8 17 4 9 7 6 9 3 | 20 27 13 21 23 16 24 17 20 16 16
10 | 13 13 7 10 12 5 12 12 10 14 4 | 29 29 20 23 21 21 29 23 30 21 22
11 | 6 20 16 10 17 5 9 10 9 18 4 | 22 36 19 23 26 19 30 23 23 23 21
12 | 14 14 8 17 18 6 12 15 14 21 5 | 23 29 15 23 24 16 23 10 23 19 15
13 | 13 13 7 9 15 4 9 13 12 15 4 | 22 23 12 18 22 14 21 17 17 13 14
14 | 10 18 8 14 24 4 10 12 8 20 4 | 22 26 17 26 24 16 21 17 18 18 15
15 | 11 11 6 13 20 5 9 13 12 14 4 | 25 23 14 23 27 18 23 19 20 13 17
16 | 14 19 7 17 23 6 15 23 14 20 5 | 29 34 18 22 34 18 27 17 24 13 17
17E | 12 11 5 7 19 4 11 13 10 13 4 | 34 33 27 35 28 29 32 27 37 32 29
18 | 12 12 9 20 14 5 9 14 13 17 4 | 21 21 16 18 18 14 19 17 17 17 13
19E | 12 13 8 9 17 5 10 21 14 10 4 | 23 29 18 23 19 20 26 23 24 22 19
20 | 14 13 9 9 12 5 9 9 13 12 4 | 26 16 14 16 18 15 14 17 23 15 14
21 | 15 15 10 14 17 6 11 26 13 19 5 | 26 28 19 23 27 19 26 26 23 17 20
22 | 10 10 8 9 14 4 7 11 8 16 3 | 22 25 15 15 23 14 21 15 20 20 15
23 | 15 14 8 10 22 6 10 12 12 20 4 | 24 24 15 19 29 15 23 17 18 12 15
24 | 9 21 5 8 25 6 10 10 9 10 4 | 23 32 14 21 31 18 21 23 22 24 19
25 | 12 10 5 9 16 4 9 6 9 15 3 | 14 22 10 20 24 12 19 11 17 16 12
26 | 10 13 6 7 18 5 9 8 7 14 3 | 24 32 15 21 30 17 26 17 26 19 19
27E | 21 21 11 16 20 11 23 8 30 20 6 | 161 156 153 158 156 156 88 157 161 161 156
28 | 14 13 7 10 18 5 10 16 11 21 4 | 20 26 15 18 25 14 24 19 22 14 15
29E | 13 12 7 12 13 4 15 8 10 7 4 | 29 27 19 29 20 21 21 21 27 21 21
30 | 13 11 5 10 16 5 10 13 10 9 3 | 26 27 12 20 24 16 24 17 27 22 18
31 | 19 16 7 10 18 6 8 11 9 15 4 | 32 31 14 24 26 17 24 13 21 15 18
32 | 9 16 5 11 20 4 9 8 7 12 3 | 26 34 21 30 34 24 30 22 20 29 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 14 8 11 17 5 11 13 12 16 |T 33 36 25 31 33 27 26 27 32 28 27
WRMS | 12 14 7 10 17 5 11 12 10 17 |NE 24 28 15 21 24 17 24 18 22 19 18
MEDI | 12 13 7 10 17 5 10 12 10 15 |MD 25 29 15 23 25 18 24 19 23 19 18
Table 3.1899.6 GPS week: 1899 Day: 6 MJD: 57543.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 15 8 7 11 4 7 10 7 11 3 | 27 30 18 25 21 21 28 24 28 31 22
2 | 8 14 7 10 15 3 8 12 9 17 3 | 26 28 23 25 22 23 28 27 26 18 22
3 | 10 10 5 10 9 3 9 8 7 10 3 | 44 50 35 41 39 39 47 40 44 44 41
X4 | 5 --- --- --- --- 57 --- --- --- --- 0 | 45 --- --- --- --- 29 --- --- --- --- 44
5 | 7 19 8 8 9 3 10 12 12 17 4 | 38 44 34 37 36 35 39 35 42 40 36
6 | 11 10 4 3 8 3 7 11 6 11 2 | 23 26 17 22 22 20 26 19 23 27 20
7 | 8 12 6 11 15 4 10 12 9 13 3 | 23 26 16 25 26 19 24 16 25 20 19
8E | 31 25 15 12 58 14 29 18 38 19 10 | 266 263 261 264 264 259 295 267 263 266 263
9 | 9 14 8 6 16 3 10 10 8 9 3 | 22 28 16 23 28 21 28 23 27 23 21
10 | 9 10 5 14 10 4 8 9 9 13 3 | 45 44 38 45 37 40 44 42 48 39 41
11 | 8 24 16 11 14 5 9 9 8 10 4 | 24 39 23 27 28 23 30 24 27 22 23
12 | 10 16 7 17 19 5 12 15 10 19 4 | 26 28 17 24 24 17 24 14 23 19 18
13 | 10 11 6 9 14 5 10 12 8 16 3 | 23 26 15 22 28 19 26 21 23 13 19
X14 | 10 12 8 --- 18 4 9 14 11 18 4 | 26 19 21 --- 24 18 20 20 22 19 18
15 | 10 10 7 10 13 3 11 15 10 16 4 | 27 25 17 26 27 22 26 23 23 16 21
16 | 11 19 7 16 22 5 13 24 13 18 5 | 27 32 17 22 28 18 24 18 22 14 17
17E | 7 11 5 7 11 5 10 9 6 10 3 | 31 32 27 33 30 30 33 28 33 35 29
18 | 11 8 8 21 11 4 8 15 10 18 4 | 27 22 21 23 23 18 22 26 25 27 21
19E | 12 11 7 7 17 4 7 19 8 8 3 | 24 25 21 24 25 21 27 30 30 22 22
20 | 8 10 9 10 11 3 10 12 7 15 3 | 27 23 22 26 22 21 20 27 24 20 21
21 | 12 14 8 15 17 4 11 25 13 17 5 | 26 33 23 31 27 24 30 30 29 19 25
22 | 7 9 7 10 11 4 7 13 10 12 3 | 29 28 21 27 26 22 24 22 29 23 22
23 | 16 13 7 11 18 4 9 12 9 18 4 | 28 26 18 23 30 20 26 21 24 12 19
24 | 7 14 5 10 23 3 8 14 7 11 3 | 23 21 14 19 31 18 22 25 23 25 19
25 | 10 12 6 9 15 3 9 6 5 19 3 | 17 21 13 22 21 15 19 15 19 25 15
26 | 10 9 6 7 19 3 8 10 7 8 3 | 26 26 17 22 29 19 25 19 24 19 20
X27E | 10 17 6 8 25 6 --- 5 12 10 4 | 110 109 108 111 105 110 --- 105 113 107 108
28 | 6 11 8 9 18 5 8 15 10 22 4 | 21 27 18 24 24 18 24 22 24 20 18
29E | 9 15 7 12 11 3 16 9 8 11 3 | 29 24 21 29 24 22 22 22 28 24 22
30 | 6 9 5 6 18 3 8 11 8 8 3 | 27 26 18 24 30 19 25 19 28 25 22
31 | 14 10 5 9 20 5 7 10 10 12 3 | 28 28 15 25 28 18 23 14 23 18 19
32 | 9 13 6 12 19 4 8 10 9 11 3 | 35 39 34 35 44 35 39 31 32 40 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 8 11 18 5 11 13 11 14 |T 38 39 31 37 37 32 36 34 37 34 33
WRMS | 10 14 7 11 16 4 11 11 8 13 |NE 28 29 20 26 27 22 27 23 27 23 23
MEDI | 10 12 7 10 15 4 9 12 9 13 |MD 27 28 21 25 28 21 26 23 26 23 21
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 4.1899 GPS week: 1899 MJD: 57537.0-57543.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2984 |U 6 8 18 |U 6 8 22 |U 9 11 20 |
emr | emr 2976 | 8 10 20 |U 8 8 22 | 12 13 23 |
esa | esa 2976 | 7 8 17 |U 7 8 26 | 10 12 22 |
gfz | gfz 2962 |U 6 8 19 |U 7 7 23 |U 10 12 22 |
grg | grg 2976 |U 7 9 20 |U 7 8 26 | 11 13 24 |
igr | igr 2970 | 6 8 18 | 7 7 21 | 10 11 22 |
igs | igs 2976 | 6 8 18 | 6 7 22 | 10 12 22 |
jpl | jpl 2948 | 7 9 19 |U 7 8 23 | 11 12 24 |
mit | mit 2976 | 6 9 21 |U 8 8 26 |U 10 12 20 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1899.0 GPS week: 1899 Day: 0 MJD: 57537.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 8 11 | 9 7 20 | 10 9 24 |
emr | emr 2976 | 7 14 16 | 10 7 22 | 12 10 25 |
esa | esa 2976 | 6 9 12 | 10 8 22 | 10 11 26 |
gfz | gfz 2976 | 5 10 14 | 10 8 22 | 11 15 27 |
grg | grg 2976 | 5 8 12 | 10 8 18 | 13 12 31 |
igr | igr 2976 | 5 10 12 | 10 7 21 | 10 10 24 |
igs | igs 2976 | 5 10 11 | 10 7 20 | 11 11 26 |
jpl | jpl 2976 | 6 11 14 | 9 8 24 | 13 11 27 |
mit | mit 2976 | 5 10 13 | 10 8 20 | 11 12 25 |
Table 5.1899.1 GPS week: 1899 Day: 1 MJD: 57538.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 10 16 | 5 9 20 | 8 12 15 |
emr | emr 2976 | 8 13 17 | 6 9 20 | 11 12 19 |
esa | esa 2976 | 6 10 14 | 5 10 21 | 8 13 18 |
gfz | gfz 2976 | 6 9 14 | 5 10 24 | 9 12 19 |
grg | grg 2976 | 7 12 15 | 5 11 27 | 11 19 21 |
igr | igr 2976 | 6 10 14 | 5 9 21 | 8 12 17 |
igs | igs 2976 | 6 10 14 | 5 9 21 | 9 13 17 |
jpl | jpl 2976 | 7 11 16 | 5 8 23 | 11 13 18 |
mit | mit 2976 | 7 10 18 | 6 11 21 | 10 15 19 |
Table 5.1899.2 GPS week: 1899 Day: 2 MJD: 57539.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 11 | 5 7 22 | 7 9 15 |
emr | emr 2976 | 6 4 16 | 6 8 22 | 10 11 17 |
esa | esa 2976 | 6 4 12 | 5 8 24 | 8 10 16 |
gfz | gfz 2976 | 5 4 12 | 5 7 24 | 8 10 15 |
grg | grg 2976 | 6 4 16 | 5 10 29 | 9 11 20 |
igr | igr 2976 | 5 3 12 | 5 7 21 | 7 10 15 |
igs | igs 2976 | 5 3 12 | 5 7 22 | 8 10 15 |
jpl | jpl 2976 | 5 6 16 | 6 8 23 | 10 13 18 |
mit | mit 2976 | 5 4 13 | 7 7 27 | 7 11 15 |
Table 5.1899.3 GPS week: 1899 Day: 3 MJD: 57540.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 | 7 5 17 | 7 10 21 | 7 13 17 |
emr | emr 2976 | 8 8 19 | 7 9 23 | 11 15 24 |
esa | esa 2976 | 7 6 16 | 8 9 26 | 9 14 24 |
gfz | gfz 2976 | 6 6 18 | 8 9 23 | 9 13 20 |
grg | grg 2976 | 7 6 21 | 7 9 24 | 9 13 20 |
igr | igr 2976 | 6 6 17 | 7 9 21 | 8 14 21 |
igs | igs 2976 | 6 6 17 | 7 9 23 | 9 14 22 |
jpl | jpl 2976 | 7 8 17 | 7 9 26 | 10 12 24 |
mit | mit 2976 | 6 5 19 | 10 9 28 | 8 12 19 |
Table 5.1899.4 GPS week: 1899 Day: 4 MJD: 57541.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 8 17 | 5 6 18 | 12 11 23 |
emr | emr 2976 | 6 9 19 | 7 6 20 | 15 16 28 |
esa | esa 2976 | 7 8 16 | 5 5 19 | 13 13 26 |
gfz | gfz 2976 | 6 8 19 | 5 5 20 | 13 11 26 |
grg | grg 2976 | 6 9 22 | 6 6 23 | 14 13 28 |
igr | igr 2976 | 6 7 17 | 5 5 18 | 13 12 26 |
igs | igs 2976 | 6 8 18 | 5 5 19 | 13 13 26 |
jpl | jpl 2976 | 6 6 16 | 5 6 21 | 14 16 31 |
mit | mit 2976 | 7 9 24 | 7 6 25 | 12 9 22 |
Table 5.1899.5 GPS week: 1899 Day: 5 MJD: 57542.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 9 18 | 8 8 31 | 11 10 24 |
emr | emr 2976 | 10 12 22 | 9 7 28 | 13 15 24 |
esa | esa 2976 | 5 9 18 | 8 13 43 | 11 10 25 |
gfz | gfz 2976 | 6 10 20 | 9 7 25 | 11 9 26 |
grg | grg 2976 | 6 10 20 | 8 8 32 | 11 12 27 |
igr | igr 2939 | 6 10 20 | 9 7 25 | 11 10 25 |
igs | igs 2976 | 6 9 19 | 8 6 25 | 11 10 26 |
jpl | jpl 2880 | 7 9 18 | 8 7 26 | 11 11 28 |
mit | mit 2976 | 5 11 24 | 10 8 33 | 10 14 20 |
Table 5.1899.6 GPS week: 1899 Day: 6 MJD: 57543.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 11 32 | 6 7 24 | 9 11 21 |
emr | emr 2976 | 11 13 34 | 11 10 22 | 12 11 25 |
esa | esa 2976 | 10 13 34 | 5 6 23 | 10 12 22 |
gfz | gfz 2880 | 10 13 35 | 6 7 22 | 10 12 21 |
grg | grg 2976 | 11 11 35 | 8 7 29 | 10 14 24 |
igr | igr 2976 | 10 13 34 | 6 6 22 | 10 12 22 |
igs | igs 2976 | 10 12 33 | 5 6 23 | 10 12 22 |
jpl | jpl 2880 | 11 12 35 | 6 8 21 | 10 11 24 |
mit | mit 2976 | 10 12 35 | 7 9 25 | 10 13 23 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1899 GPS week: 1899 MJD: 57537.500-57543.500
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 3 9 41 3 | 12 21
| 23 20 110 161 4 | 2
emr uuxux | 27 -39 101 188 -14 | 28 36
| 29 50 235 96 14 | 5
esa uuuuu | 1 -5 64 22 1 | 1 18
| 11 17 73 54 4 | 3
gfz uuuuu | 1 12 -51 -65 1 | -2 19
| 13 31 137 75 3 | 3
grg uuuuu | -60 39 0 -161 2 | -2 17
| 15 15 48 73 7 | 3
igr xxxxx | -23 -7 26 -25 3 | -8 19
| 13 16 59 26 4 | 2
irf xxxxx | 11 -6 -50 -83 7 | -7 18
| 11 11 64 41 4 | 2
jpl uuuuu | -29 -15 91 -18 -14 | 7 22
| 15 30 79 60 15 | 7
mit uuuuu | 10 9 -131 -182 0 | 12 21
| 15 14 135 73 7 | 4
ngs uuxuu | 19 9 19 13 3 | 2 18
| 32 53 318 61 5 | 3
sio uuuux | 41 10 -121 72 -2 | 52 54
| 16 23 58 64 5 | 4
Table 7.1899.0 GPS week: 1899 Day: 0 MJD: 57537.500
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 | -34 12 0 -46 0 | 14 22
emr uuxux | 24 10 -199 121 0 | 32 38
esa uuuuu | 17 -7 -37 59 -3 | 4 18
gfz uuuuu | 20 -39 97 51 5 | 1 18
grg uuuuu | -58 22 12 -155 5 | 0 17
igr xxxxx | -1 -15 41 24 3 | -7 18
irf xxxxx | 28 -20 -104 -49 1 | -6 18
jpl uuuuu | -1 -53 168 -24 2 | 15 21
mit uuuuu | 30 -10 -235 -126 -9 | 17 24
ngs uuxuu | -50 85 -309 -93 -4 | 6 18
sio uuuux | 54 -19 -160 94 -10 | 58 60
Table 7.1899.1 GPS week: 1899 Day: 1 MJD: 57538.500
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 | -34 13 71 -42 -1 | 16 23
emr uuxux | -6 -54 47 72 -9 | 34 40
esa uuuuu | -2 -5 58 -25 -1 | 5 18
gfz uuuuu | 10 4 0 -20 2 | 3 18
grg uuuuu | -73 32 -80 -157 8 | 2 18
igr xxxxx | -22 9 -76 -15 3 | -5 17
irf xxxxx | 12 -1 -119 -50 2 | -4 17
jpl uuuuu | -25 -4 80 7 -10 | 15 21
mit uuuuu | 29 6 -274 -107 -5 | 18 24
ngs uuxuu | 37 54 -324 34 2 | 7 19
sio uuuux | 67 -2 -70 149 2 | 57 59
Table 7.1899.2 GPS week: 1899 Day: 2 MJD: 57539.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -15 -2 23 -98 4 | 12 20
emr uuxux | 50 -26 16 138 -9 | 30 37
esa uuuuu | 12 -35 134 -49 1 | 2 17
gfz uuuuu | -1 -9 97 -78 -1 | 0 18
grg uuuuu | -84 37 21 -81 8 | -1 16
igr xxxxx | -20 15 -16 -33 2 | -8 18
irf xxxxx | 12 12 -103 -54 9 | -7 18
jpl uuuuu | -40 9 -25 38 -17 | 11 19
mit uuuuu | -2 17 -284 -128 2 | 13 21
ngs uuxuu | 28 34 -202 81 1 | 3 17
sio uuuux | 33 12 -57 106 1 | 53 55
Table 7.1899.3 GPS week: 1899 Day: 3 MJD: 57540.500
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 17 -52 -33 10 | 10 21
emr uuxux | 20 -41 120 186 -6 | 27 37
esa uuuuu | -4 7 55 -31 2 | -1 20
gfz uuuuu | -8 23 -17 -105 -2 | -3 21
grg uuuuu | -54 30 -33 -117 -4 | -3 18
igr xxxxx | -34 -28 5 -26 2 | -10 22
irf xxxxx | 6 -13 -37 -80 6 | -8 20
jpl uuuuu | -27 3 46 62 -10 | 6 24
mit uuuuu | 1 -11 -69 -171 -5 | 10 22
ngs uuxuu | 38 -7 -73 4 7 | 0 20
sio uuuux | 19 0 -50 135 -6 | 50 54
Table 7.1899.4 GPS week: 1899 Day: 4 MJD: 57541.500
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 -38 207 49 1 | 11 22
emr uuxux | 67 13 -97 216 -10 | 26 36
esa uuuuu | -11 -1 49 57 10 | -1 18
gfz uuuuu | -21 19 -162 -95 1 | -5 19
grg uuuuu | -59 42 16 -197 3 | -5 16
igr xxxxx | -36 -22 92 -58 5 | -11 21
irf xxxxx | 16 -16 -20 -111 9 | -9 20
jpl uuuuu | -33 16 46 -30 -29 | 4 22
mit uuuuu | 14 19 -84 -252 -1 | 8 19
ngs uuxuu | 14 -68 313 78 6 | -1 18
sio uuuux | 43 13 -177 20 -2 | 48 51
Table 7.1899.5 GPS week: 1899 Day: 5 MJD: 57542.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 31 -5 -43 381 4 | 13 23
emr uuxux | 42 -35 419 211 -43 | 27 36
esa uuuuu | -12 -13 180 62 -1 | 2 19
gfz uuuuu | 2 56 -276 -25 4 | -3 19
grg uuuuu | -58 68 -8 -303 2 | -2 16
igr xxxxx | -36 -3 79 -27 9 | -8 19
irf xxxxx | -9 4 -23 -160 10 | -5 18
jpl uuuuu | -47 -21 119 -113 -38 | 2 22
mit uuuuu | -10 19 -46 -305 9 | 10 20
ngs uuxuu | 36 -39 396 14 10 | 2 18
sio uuuux | 30 16 -166 -12 -2 | 50 53
Table 7.1899.6 GPS week: 1899 Day: 6 MJD: 57543.500
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 | -20 23 -140 77 2 | 10 19
emr uuxux | -11 -136 403 371 -19 | 18 31
esa uuuuu | 7 17 10 79 0 | -2 17
gfz uuuuu | 1 31 -93 -183 0 | -6 17
grg uuuuu | -37 43 73 -117 -10 | -5 15
igr xxxxx | -14 -5 59 -42 -2 | -10 19
irf xxxxx | 14 -8 60 -75 11 | -8 17
jpl uuuuu | -34 -57 207 -68 5 | -6 24
mit uuuuu | 8 22 74 -187 7 | 7 16
ngs uuxuu | 32 8 331 -27 0 | -1 16
sio uuuux | 39 54 -165 13 4 | 46 48
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