[IGSREPORT-24412] Wk 1892 IGS Final Orbits
IGS ACC
acc at igs.org
Thu Apr 28 16:00:10 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1892 (Apr 10, 2016 - Apr 16, 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:
igs1892[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1892[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1892[0-6].cls IGS GPS clock combination summary report.
igs18927.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18927.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 | SYOG
0 | ESA | SYOG SYOG
0 | GFZ | 18 32 32 ALGO BJNM SYOG XMIS ALGO BJNM POHN
0 | GRG | 18 INVK RABT SYOG INVK RABT SYOG
0 | JPL | INVK
1 | COD | BJNM BJNM SYOG
1 | ESA | DUBO MAL2 WHIT BAKE DUBO MAL2 WHIT
1 | GFZ | 18 32 32 ALGO BJNM USUD ALGO BJNM MAS1 USUD
1 | GRG | DUBO PDEL PDEL
2 | COD | ZECK
2 | ESA | TWTF TIXI TWTF
2 | GFZ | 18 32 32 ALGO BJNM DRAG INVK KARR POHN SYOG WUHN
2 | GFZ | XMIS YAR2 ALGO INVK KARR POHN WUHN YAR2
2 | GRG | KARR RABT KARR RABT XMIS
2 | JPL | INVK
3 | COD | INVK BJNM MAW1 NTUS TWTF
3 | EMR | FAIR FAIR
3 | ESA | BJNM DAV1 FLIN WTZR BJNM DAV1 FLIN KELY WTZR
3 | GFZ | 18 32 32 ALGO BAKE BJNM DARW DGAR DRAG GMSD IENG
3 | GFZ | IRKJ KARR MCIL NANO PDEL PIMO REUN SCOR TRO1 TWTF
3 | GFZ | VILL ALGO KARR NANO POHN TWTF
3 | GRG | KARR XMIS DRAG KARR POTS SYOG XMIS
3 | MIT | INVK SYOG
4 | COD | BJNM MAC1 MAW1 BJNM GLSV KARR MAC1 MAW1 TWTF
4 | EMR | SYOG
4 | ESA | 21 MAW1 NTUS SYOG MAW1 NOVM TIXI
4 | GFZ | 18 32 32 ALGO TRO1 YAR2 NTUS
4 | GRG | DRAG GLSV NRIL TRO1 XMIS DRAG NRIL XMIS
4 | MIT | NTUS NTUS
5 | COD | CHUR
5 | EMR | YAKT
5 | ESA | BJNM BJNM POTS
5 | GFZ | 18 32 18 32 ALGO BJNM KARR MAL2 POHN BJNM DGAR MAL2
5 | GFZ | NOVM PIMO POHN REUN
5 | GRG | KARR MAL2 SYOG
5 | MIT | SYOG SYOG
6 | COD | KOUC KOUC MAW1 REUN
6 | ESA | SYOG SYOG
6 | GFZ | 18 32 18 25 32 BJNM BJNM DGAV HYDE KARR
6 | GRG | DAV1 KARR NKLG POHN SYOG WIND DAV1 KARR POHN POTS
6 | GRG | REDU SYOG WIND
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
----+--------+--------+-------------
1 | GFZ | ~20:00 | ~ -0.11 ns
4 | GFZ | ~19:30 | ~ -0.10 ns
5 | GFZ | ~21:20 | ~ -0.12 ns
6 | GFZ | ~02:00 | ~ -0.11 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. 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 | -.8 -1.0 -.7 -23 -9 -6 .59
EMR | 0 | 6.0 -7.7 9.1 68 0 -14 .67
ESA | 0 | .5 -4.0 .2 8 -40 38 .56
GFZ | 0 | .6 -.5 -.7 -34 -83 -46 .47
GRG | 0 | 12.3 1.4 17.4 22 -40 161 .32
JPL | 0 | 3.6 -7.7 5.3 -26 42 51 .75
MIT | 0 | 4.4 -4.3 18.0 17 2 -22 .67
NGS | 0 | 7.2 -8.9 26.2 -165 -91 -25 .65
SIO | 0 | 8.4 -3.1 -11.3 -10 -4 -7 .42
COD | 1 | -1.1 -1.6 -.8 -20 2 -4 1.07
EMR | 1 | 2.2 -3.7 11.7 34 -9 -4 .70
ESA | 1 | 1.0 -5.2 .2 -22 -9 23 .80
GFZ | 1 | .8 -1.4 -2.3 -27 -84 -32 1.08
GRG | 1 | 3.7 .4 16.6 1 -47 172 .58
JPL | 1 | 1.1 -6.3 -3.6 -20 39 71 1.08
MIT | 1 | 4.9 -6.1 12.9 8 -9 -16 1.20
NGS | 1 | 3.3 -7.9 23.3 -130 -72 6 .87
SIO | 1 | 3.6 -2.7 -13.3 -9 -8 3 1.18
COD | 2 | -.9 -1.8 .0 -49 -20 -38 .77
EMR | 2 | 2.3 -9.0 6.7 46 -14 -2 .70
ESA | 2 | -.5 -3.5 -.3 -19 -36 12 .64
GFZ | 2 | 1.0 -1.4 -2.4 -48 -85 -33 .91
GRG | 2 | .3 .7 16.2 29 -36 191 .08
JPL | 2 | 3.6 -13.4 -.7 -35 11 55 1.11
MIT | 2 | 5.3 -8.2 14.9 8 12 -27 .99
NGS | 2 | 4.3 -10.4 16.1 -99 -58 -13 .90
SIO | 2 | 1.8 -2.2 -11.1 -36 7 2 .97
COD | 3 | -.8 -1.0 .3 -21 -23 -10 .94
EMR | 3 | -.2 -6.5 4.5 14 -13 -9 .88
ESA | 3 | -.8 -2.0 .5 -11 -39 27 .65
GFZ | 3 | .4 -1.3 -1.4 -39 -86 -23 .88
GRG | 3 | 2.8 -3.5 16.2 18 -47 172 .70
JPL | 3 | 3.1 -14.3 .7 -7 45 7 1.15
MIT | 3 | 3.4 -9.7 14.8 18 -12 3 .97
NGS | 3 | 1.3 -10.9 14.7 -110 -39 -18 .83
SIO | 3 | 3.0 -2.3 -5.4 -28 -12 29 .81
COD | 4 | -1.2 -.7 -.3 -25 -6 -39 .75
EMR | 4 | 4.4 -4.1 2.9 53 -11 18 .91
ESA | 4 | -.6 -2.0 -.6 -20 -21 29 .54
GFZ | 4 | .9 -1.1 -.8 -49 -89 -21 .68
GRG | 4 | 4.4 -2.0 5.1 -9 -37 176 .57
JPL | 4 | 3.7 -14.0 .6 -1 25 -4 1.05
MIT | 4 | 2.7 -8.5 11.4 7 -13 -25 .94
NGS | 4 | .4 -9.3 17.7 -123 -32 -47 .72
SIO | 4 | 2.8 -2.2 -7.1 -35 -29 11 .72
COD | 5 | -.5 -1.1 -1.0 -34 -20 -13 .69
EMR | 5 | 3.0 -10.1 -8.5 33 -1 -28 .65
ESA | 5 | -.2 -3.7 .3 -10 -18 38 .39
GFZ | 5 | .3 -.7 -1.6 -49 -95 -27 .69
GRG | 5 | 7.3 .7 6.2 36 -42 195 .39
JPL | 5 | .7 -10.0 .4 9 -3 56 .91
MIT | 5 | 3.6 -8.9 10.8 16 -11 -23 .78
NGS | 5 | 5.5 -4.5 17.2 -84 -69 46 .76
SIO | 5 | 4.0 -3.4 -12.5 -8 -39 8 .85
COD | 6 | -1.3 -.9 -.4 -26 -9 -28 .75
EMR | 6 | 3.8 -7.9 -3.2 58 -3 -17 .83
ESA | 6 | -1.2 -2.9 2.3 -3 -37 22 .81
GFZ | 6 | .3 -.9 -1.5 -5 -39 -27 .91
GRG | 6 | 7.4 -6.9 -1.8 5 -61 142 .63
JPL | 6 | .4 -14.4 -3.4 -23 -11 27 .94
MIT | 6 | 4.5 -9.2 10.4 -7 -12 -34 .91
NGS | 6 | 2.2 -4.4 12.6 -59 -53 5 .83
SIO | 6 | 4.1 -3.7 -20.4 -16 -41 20 .97
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 1.1892.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1892.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 2.1892.[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 3.1892.[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 5.1892.0-6). 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 1892 summary. (Apr 10, 2016 - Apr 16, 2016)
Table 1.1892.a GPS week: 1892 MJD: 57488.000-57494.000
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 246| 0 0 -2 3 16 -15 .04 12 12 | -1182 121 12 155
| 0 0 1 11 15 18 .05 | 116 255
emr 80| 1 0 -3 -1 -27 0 .41 11 11 | 5495 627 14 146
| 0 2 0 8 4 24 .04 | 1256 346
esa 150| 0 0 -4 -1 0 9 -.50 9 9 | -469 -542 8 164
| 0 0 1 9 15 16 .04 | 494 839
gfz 206| 0 1 -1 -12 -2 5 .11 12 12 | -278 23 13 213
| 0 0 1 34 21 17 .04 | 253 187
grg 126| 1 0 9 -7 43 28 .08 16 15 | -89 60 13 199
| 0 0 4 25 19 22 .06 | 89 151
igr n/a| 0 0 -4 -14 12 -8 -.01 5 4 | 9152 261 16 90
| 0 0 1 15 14 14 .05 | 796 363
jpl 80| 0 -1 -1 0 24 11 .39 10 10 | 3626 475 15 134
| 1 1 0 11 31 33 .04 | 1107 418
mit 349| 0 -1 2 -2 -24 -31 -.46 19 16 | -39 -101 43 365
| 0 0 1 21 12 22 .07 | 125 197
ngs 226| -1 0 6 10 -7 -4 -.02 10 9 | -1189 189 787 1876
| 0 0 2 17 22 18 .02 | 92 164
sio 299| 0 2 -1 -3 -29 -19 -.07 14 13 | --- --- --- ---
| 0 0 2 7 13 25 .07 | --- ---
Table 1.1892.b GPS week : 1892 MJD: 57488.000-57494.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 3 3 3 3 3 3 |
2 | 5 4 4 5 5 4 5 |
3 | 4 4 3 4 4 3 3 |
4 | 0 0 0 0 0 0 0 |
5 | 5 5 5 4 4 4 4 |
6 | 3 4 3 4 3 3 3 |
7 | 5 5 5 6 6 6 6 |
8 | 4 3 3 3 4 3 4 |
9 | 4 3 3 4 3 3 4 |
10 | 4 3 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 6 5 5 5 |
13 | 5 4 4 5 5 4 4 |
14 | 5 4 5 5 5 4 5 |
15 | 4 4 5 5 5 4 5 |
16 | 5 5 4 5 4 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 6 5 5 |
20 | 5 5 5 5 5 5 5 |
21 | 4 4 4 4 4 4 4 |
22 | 5 4 4 4 4 5 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 3 3 4 3 3 3 |
25 | 4 4 5 5 4 4 4 |
26 | 4 4 4 4 4 4 5 |
27 | 4 3 3 3 3 3 4 |
28 | 4 4 3 3 4 3 3 |
29 | 5 5 5 5 5 5 5 |
30 | 4 3 3 4 3 3 4 |
31 | 5 5 5 5 4 4 5 |
32 | 7 7 6 6 6 6 6 |
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 2.1892.0 GPS week: 1892 Day: 0 MJD: 57488.000
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 244| 0 0 -2 5 3 -19 -.05 13 13 | -1143 219 14 149
emr 80| 1 0 -2 7 -30 1 .32 10 10 | 3333 1043 16 179
esa 150| 0 0 -8 7 4 29 -.43 12 12 | 283 -1147 10 152
gfz 201| 0 2 -4 -24 -20 14 .03 12 11 | -76 -160 10 136
grg 123| 0 0 13 -8 48 8 -.01 17 16 | -36 -59 15 187
igr n/a| -1 0 -6 -24 2 -2 -.01 5 5 | 7774 833 18 64
jpl 80| 1 -1 -1 -14 25 29 .30 9 9 | 1726 1043 14 128
mit 350| 1 -1 1 26 -12 -35 -.41 17 15 | -171 -37 45 340
ngs 223| -1 0 8 6 1 -29 -.05 11 9 | -1149 229 949 1742
sio 301| 0 1 -1 -8 -14 -24 -.07 14 13 | --- --- --- ---
Table 2.1892.1 GPS week: 1892 Day: 1 MJD: 57489.000
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 244| 0 0 -4 -10 -5 6 -.02 11 11 | -1307 301 12 154
emr 80| 1 2 -2 -12 -35 -34 .45 11 11 | 4401 976 17 156
esa 150| 0 -1 -3 -21 -11 0 -.55 8 8 | 1 -1631 8 147
gfz 206| 0 1 -2 57 35 -14 .11 12 12 | -81 -184 15 202
grg 122| 2 0 16 -57 48 16 .11 16 16 | -135 130 15 210
igr n/a| 0 0 -5 -22 -11 -14 .05 4 4 | 8507 486 18 80
jpl 80| 0 0 -1 19 60 52 .39 9 9 | 2672 669 16 130
mit 350| 1 -1 1 -25 -17 -39 -.37 18 17 | 3 -179 42 356
ngs 225| -1 0 4 22 -41 1 -.00 10 9 | -1197 144 664 1754
sio 303| -1 1 -3 -6 -21 -29 .03 15 16 | --- --- --- ---
Table 2.1892.2 GPS week: 1892 Day: 2 MJD: 57490.000
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| 0 0 -1 0 12 -52 .05 12 11 | -1313 348 13 160
emr 80| 2 -2 -3 3 -25 -21 .42 12 12 | 5319 567 15 154
esa 150| 0 0 -4 -1 -24 29 -.55 8 8 | -764 955 8 146
gfz 209| 0 0 0 -15 -24 -18 .06 12 12 | -611 208 17 180
grg 125| 0 1 11 -14 25 49 .08 16 15 | -210 266 14 184
igr n/a| 0 0 -5 7 22 -11 .04 4 5 | 9038 450 18 78
jpl 80| 0 0 -1 -10 40 46 .40 9 9 | 3370 775 16 118
mit 350| 0 -1 0 -3 -51 -34 -.39 19 17 | -260 252 43 378
ngs 226| 0 1 4 21 27 -13 -.01 10 8 | -1313 366 810 2000
sio 300| 0 2 -2 -5 -18 -14 -.03 14 13 | --- --- --- ---
Table 2.1892.3 GPS week: 1892 Day: 3 MJD: 57491.000
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 0 -1 -10 11 -12 .04 12 12 | -1239 230 12 141
emr 80| 1 1 -2 -11 -27 -10 .41 11 11 | 5749 532 16 140
esa 150| 0 -1 -3 -1 -5 12 -.49 8 8 | -954 -642 9 157
gfz 207| -1 1 0 -1 -11 17 .13 12 12 | -437 84 13 159
grg 128| 2 0 11 15 8 10 .04 18 16 | -168 132 13 192
igr n/a| 0 0 -5 -28 5 -24 .04 5 5 | 9417 312 16 87
jpl 80| 0 0 -1 0 54 -25 .40 10 10 | 3990 659 16 131
mit 350| 0 -1 3 6 -27 2 -.46 19 17 | 46 -237 39 366
ngs 227| 0 0 4 21 -15 4 -.05 11 10 | -1279 296 651 2024
sio 289| -1 1 -3 -9 -19 7 -.06 14 14 | --- --- --- ---
Table 2.1892.4 GPS week: 1892 Day: 4 MJD: 57492.000
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 246| 0 0 -2 13 34 -13 .09 11 11 | -1105 134 12 165
emr 80| 2 0 -4 -1 -22 35 .44 11 11 | 6494 -6 15 126
esa 150| 0 0 -4 4 0 0 -.46 8 8 | -800 -812 7 160
gfz 208| 0 1 0 -44 0 16 .15 13 13 | 33 -114 13 267
grg 128| 2 0 7 3 61 69 .05 17 16 | -14 168 12 190
igr n/a| 0 0 -4 6 24 -9 -.05 4 4 | 10120 -186 16 102
jpl 80| -1 -3 -2 7 24 -33 .42 11 11 | 4758 -25 17 155
mit 349| 0 -2 2 12 -26 -29 -.49 19 17 | 20 35 44 387
ngs 225| -1 2 8 -19 -15 -23 -.02 10 9 | -1097 141 873 1819
sio 303| 0 2 0 13 -41 0 -.09 14 14 | --- --- --- ---
Table 2.1892.5 GPS week: 1892 Day: 5 MJD: 57493.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 0 -1 19 25 -2 .09 12 12 | -986 -404 11 161
emr 80| 2 -1 -4 -1 -28 14 .41 11 11 | 6346 556 12 143
esa 150| 0 0 -4 4 17 -16 -.50 9 9 | -875 51 8 205
gfz 207| -1 1 0 -39 -11 -1 .13 11 10 | -232 25 12 338
grg 128| 0 0 5 18 65 30 .13 15 14 | 40 -142 12 232
igr n/a| 0 1 -2 -23 31 -18 -.06 4 4 | 9787 -74 16 125
jpl 80| -2 -1 0 1 -20 10 .39 10 10 | 4596 -38 15 130
mit 350| 0 -2 3 -1 -17 -70 -.55 20 16 | 80 -226 44 354
ngs 227| 0 0 4 -5 11 4 -.03 9 8 | -1063 -135 769 1868
sio 300| 0 2 -1 -1 -45 -7 -.18 13 12 | --- --- --- ---
Table 2.1892.6 GPS week: 1892 Day: 6 MJD: 57494.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| -1 0 -1 6 33 -14 .06 12 12 | -1186 24 13 161
emr 80| 1 -3 -3 7 -22 16 .40 11 11 | 6829 721 12 126
esa 150| 0 0 -5 -1 19 9 -.51 9 8 | -178 -572 11 183
gfz 208| 0 0 -1 -20 18 24 .14 12 12 | -542 304 13 209
grg 128| 1 0 2 -10 44 15 .16 14 13 | -105 -73 11 198
igr n/a| 0 1 -2 -16 10 20 -.05 4 4 | 9421 10 16 100
jpl 80| 0 0 -3 -4 -13 1 .40 10 10 | 4271 244 15 148
mit 350| 0 -2 4 -34 -17 -13 -.55 20 15 | 3 -315 49 376
ngs 229| 0 1 8 26 -21 24 -.01 10 9 | -1230 283 798 1925
sio 302| 0 2 3 -4 -40 -70 -.11 13 12 | --- --- --- ---
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 3.1892.0 GPS week: 1892 Day: 0 MJD: 57488.000
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 6 13 5 12 5 6 12 8 16 3 | 33 41 33 38 45 34 43 40 41 40 38
2 | 15 8 13 11 11 5 8 21 10 18 4 | 26 29 23 27 29 21 27 37 29 23 25
3 | 9 10 12 8 14 4 10 13 8 13 3 | 34 41 42 34 28 36 38 39 38 40 36
X4E | 2 --- --- --- --- 24 --- --- --- --- 0 | 45 --- --- --- --- 36 --- --- --- --- 45
5 | 6 13 11 13 21 5 10 17 11 12 4 | 22 29 20 24 25 23 27 15 22 20 20
6 | 10 6 14 6 12 6 5 12 7 10 3 | 36 42 34 40 46 37 43 43 44 38 39
7 | 14 7 12 12 13 4 9 35 13 15 5 | 31 37 28 35 28 32 34 39 33 30 29
8 | 8 7 13 11 11 4 7 14 7 11 3 | 38 38 43 42 43 38 41 42 42 36 38
9 | 8 9 13 8 12 4 8 13 11 8 3 | 25 31 28 25 26 26 31 30 27 29 27
X10 | 9 9 11 --- 10 5 7 13 10 --- 4 | 53 56 57 --- 49 55 56 54 48 --- 53
11 | 10 6 18 9 18 7 6 9 10 12 4 | 29 39 29 35 50 31 39 38 39 43 36
12E | 13 13 8 17 20 4 17 14 9 12 5 | 32 32 26 30 29 27 33 27 31 31 28
13 | 13 13 9 13 22 4 7 13 9 19 4 | 29 35 27 32 34 29 32 29 27 25 28
14 | 17 9 11 14 19 6 8 13 12 15 4 | 29 24 24 31 29 26 25 22 23 21 22
15 | 11 13 7 11 16 4 11 14 9 12 4 | 26 31 20 31 24 27 29 25 25 25 24
16E | 15 18 8 12 19 4 9 13 9 9 4 | 33 34 28 27 34 28 31 28 34 30 29
17 | 13 7 13 9 16 4 9 21 10 12 4 | 30 31 24 31 36 26 32 33 33 28 28
18 | 21 11 11 12 19 4 10 17 12 16 5 | 33 31 24 26 31 26 33 17 28 26 25
19 | 15 11 14 11 17 5 9 26 11 15 5 | 26 31 22 27 35 23 31 37 30 25 25
20 | 11 11 12 15 20 6 9 17 10 16 4 | 18 23 17 20 18 15 20 18 15 14 14
21 | 13 9 12 10 14 5 8 14 12 16 4 | 30 34 25 29 36 27 34 32 34 35 30
22 | 13 9 13 10 23 5 8 18 9 14 4 | 22 23 24 18 23 20 24 21 23 19 17
23 | 17 9 10 13 17 4 8 16 12 19 4 | 26 31 23 31 27 25 29 26 29 24 24
24 | 9 8 13 10 15 4 7 21 8 9 3 | 24 30 25 33 29 30 30 30 30 26 27
25E | 13 13 12 11 17 6 10 12 9 9 4 | 45 50 49 47 54 45 48 45 43 48 46
26E | 16 13 13 10 18 5 10 10 9 9 4 | 44 43 46 44 44 44 40 44 41 47 42
27 | 8 8 15 10 14 3 10 9 9 7 3 | 22 24 23 19 28 20 26 21 23 19 21
28E | 12 7 7 7 18 4 9 10 10 8 3 | 28 27 23 23 26 24 30 28 30 26 25
29 | 13 10 11 13 19 7 15 13 15 13 4 | 22 24 17 20 25 16 24 19 23 18 18
30 | 7 7 14 6 12 4 9 12 10 10 3 | 31 38 28 31 31 32 35 30 32 31 31
31 | 13 12 10 14 16 6 9 15 12 17 4 | 30 37 26 35 32 32 36 26 29 25 28
32 | 23 19 7 21 14 11 12 31 17 26 6 | 59 78 64 67 67 66 75 85 59 82 68
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 10 12 12 17 5 9 17 11 14 |T 31 35 29 31 34 30 34 32 32 30 30
WRMS | 13 10 12 11 16 5 9 15 9 13 |NE 30 34 28 31 33 29 34 32 31 29 29
MEDI | 13 9 12 11 16 5 9 14 10 12 |MD 30 32 26 31 31 27 32 30 30 26 28
Table 3.1892.1 GPS week: 1892 Day: 1 MJD: 57489.000
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 5 4 6 13 5 5 13 7 9 2 | 27 32 22 28 32 26 35 29 31 31 27
2 | 7 9 12 13 13 4 9 22 10 20 4 | 21 26 24 22 20 20 27 30 23 21 21
3 | 9 10 6 8 15 5 9 16 8 14 3 | 30 33 24 28 23 27 32 33 31 36 28
X4E | 2 --- --- --- --- 32 --- --- --- --- 0 | 49 --- --- --- --- 39 --- --- --- --- 49
5 | 7 22 7 14 19 5 11 20 10 13 4 | 23 32 19 27 24 23 30 18 26 21 21
6 | 10 7 7 9 13 5 8 15 8 14 3 | 27 36 25 30 33 28 37 32 32 32 29
7 | 11 8 8 10 14 5 9 37 13 19 5 | 33 33 30 32 24 30 32 38 32 23 27
8 | 7 7 5 7 11 4 8 15 7 12 3 | 36 40 32 33 34 36 36 39 38 41 35
9 | 7 9 4 7 12 2 9 16 9 12 3 | 24 29 20 23 21 24 28 27 28 28 23
X10 | 5 7 6 --- 8 4 9 14 6 --- 3 | 36 40 31 --- 30 36 40 38 35 --- 35
11 | 6 6 14 10 16 5 7 11 8 13 3 | 24 33 27 28 36 26 35 28 31 35 28
12E | 14 14 7 18 20 3 17 16 13 16 5 | 29 28 21 28 24 23 31 21 32 26 23
13 | 9 11 8 13 22 4 7 15 8 15 4 | 28 36 28 31 36 28 34 28 31 26 28
14 | 15 10 7 12 17 6 8 14 9 17 4 | 29 25 19 23 22 22 24 17 24 18 20
15 | 7 12 5 11 21 3 10 14 8 15 4 | 25 30 19 26 24 22 26 20 25 22 21
16E | 16 15 6 15 18 3 11 13 8 13 4 | 27 26 21 25 28 23 24 24 28 28 23
17 | 12 9 9 12 16 4 9 24 9 13 4 | 26 28 22 27 27 21 29 23 26 21 22
18 | 17 9 7 12 19 2 10 17 11 18 4 | 30 29 21 25 27 24 29 13 25 21 22
19 | 15 12 10 15 17 4 9 29 11 19 5 | 26 32 21 22 26 21 30 28 24 15 20
20 | 9 13 9 14 20 4 11 19 10 17 4 | 20 24 18 21 20 18 24 23 20 19 17
21 | 7 8 9 11 13 4 8 12 9 15 3 | 25 29 26 25 28 24 28 25 27 29 25
22 | 12 14 9 10 22 5 7 18 9 13 4 | 20 23 17 19 23 18 23 20 24 18 17
23 | 13 10 8 13 16 4 10 18 11 19 4 | 22 25 19 23 21 20 25 22 25 19 19
24 | 8 8 5 7 14 4 6 20 8 12 3 | 24 28 19 24 21 24 27 22 28 19 21
25E | 14 13 6 9 19 5 11 14 7 8 4 | 45 48 44 44 41 44 49 47 49 44 44
26E | 14 14 6 12 19 4 8 12 9 12 4 | 47 48 42 48 48 45 46 46 48 45 44
27 | 6 7 4 8 13 3 8 10 7 11 2 | 24 26 19 25 25 22 27 22 26 19 21
28E | 11 7 7 8 17 4 10 12 7 10 3 | 31 26 27 25 24 25 27 27 30 26 25
29 | 11 12 8 15 20 4 13 15 12 17 4 | 25 26 20 24 20 18 25 18 25 17 19
30 | 8 8 4 6 11 5 7 13 9 17 3 | 31 33 25 29 24 29 33 25 32 26 27
31 | 11 12 8 17 14 5 12 16 11 17 4 | 30 36 24 29 27 28 36 18 28 26 26
32 | 20 17 12 18 13 7 12 35 13 26 6 | 46 62 39 48 46 48 56 71 41 66 48
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 8 12 16 4 9 18 10 15 |T 29 32 24 28 27 26 31 28 29 27 26
WRMS | 11 11 8 12 16 4 9 17 9 16 |NE 27 31 23 26 26 25 31 27 28 25 24
MEDI | 9 10 7 11 16 4 9 15 9 14 |MD 27 30 22 26 25 24 30 25 28 26 23
Table 3.1892.2 GPS week: 1892 Day: 2 MJD: 57490.000
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 | 4 8 5 6 11 5 4 15 7 8 2 | 29 34 25 30 36 27 35 32 33 33 30
2 | 8 11 13 12 12 4 7 22 9 15 4 | 21 25 22 26 22 20 25 32 27 22 21
3 | 9 10 6 7 14 4 7 17 6 12 3 | 32 35 28 30 29 31 34 34 34 34 30
X4E | 3 --- --- --- --- 50 --- --- --- --- 0 | 67 --- --- --- --- 36 --- --- --- --- 65
5 | 8 20 7 13 17 4 9 21 9 11 4 | 22 30 20 27 25 23 27 13 28 22 21
6 | 7 6 7 6 12 5 6 17 7 11 3 | 33 36 24 35 36 29 37 35 35 32 31
7 | 12 9 8 11 15 4 9 41 12 17 5 | 29 33 24 29 26 27 30 40 27 22 24
8 | 9 6 5 10 11 4 7 15 9 10 3 | 27 30 22 26 27 26 32 30 29 30 25
9 | 8 8 6 6 11 4 8 16 11 8 3 | 22 26 14 19 22 22 25 27 24 25 20
X10 | 10 7 4 --- 10 4 7 13 6 11 3 | 44 46 38 --- 40 41 42 43 39 34 40
11 | 9 7 14 10 14 5 7 11 9 11 3 | 25 35 27 27 38 25 36 30 30 35 29
12E | 15 15 8 16 23 3 16 17 13 13 5 | 31 28 22 26 24 22 30 24 25 27 23
13 | 11 13 7 12 23 3 8 15 9 15 4 | 31 37 29 35 40 30 35 25 34 26 29
14 | 16 11 9 14 15 7 9 15 9 17 4 | 31 23 22 28 28 23 24 17 23 18 20
15 | 10 16 6 14 21 3 11 16 7 14 4 | 24 32 20 31 28 25 29 23 28 24 23
16E | 14 14 7 17 17 3 9 13 8 10 4 | 26 23 20 24 32 21 25 21 26 24 22
17 | 12 10 9 9 15 4 7 25 10 15 4 | 30 29 21 27 29 23 30 26 29 24 24
18 | 18 12 7 15 23 4 10 19 12 16 5 | 34 29 21 24 30 22 28 13 29 22 22
19 | 12 12 11 11 18 4 9 31 11 18 5 | 25 29 22 26 29 22 30 32 27 19 22
20 | 10 14 9 15 19 4 11 18 8 13 4 | 18 24 17 22 21 16 21 19 22 21 16
21 | 7 9 11 12 15 4 8 12 10 14 3 | 28 28 27 27 31 25 30 26 30 29 26
22 | 10 12 10 10 21 4 9 20 9 15 4 | 20 23 21 17 26 19 25 21 24 19 17
23 | 16 11 8 12 19 4 9 18 12 19 4 | 26 26 21 27 26 22 26 24 27 22 21
24 | 9 9 5 6 15 5 7 21 8 8 3 | 22 29 17 26 26 24 27 23 25 20 21
25 | 18 14 7 13 21 6 10 14 9 8 4 | 76 80 76 78 78 75 76 77 73 80 77
26 | 20 12 7 13 14 7 9 13 7 11 4 | 85 87 82 84 81 82 82 84 79 84 83
27 | 7 7 5 9 14 4 7 9 7 9 2 | 18 21 10 17 24 18 23 18 19 15 16
28E | 9 9 6 8 15 3 6 11 9 9 3 | 22 25 17 19 26 19 22 19 24 23 19
29 | 12 13 8 15 19 4 12 15 14 15 4 | 25 24 17 22 26 17 23 17 20 17 17
30 | 8 8 4 6 10 5 6 15 11 16 3 | 27 33 21 26 26 28 32 25 29 23 25
31 | 13 11 9 15 15 4 12 18 10 15 4 | 30 36 26 31 32 29 37 22 27 23 27
32 | 18 19 13 16 13 6 12 35 14 21 6 | 54 69 49 57 58 57 66 78 53 69 57
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 8 12 16 4 9 19 10 14 |T 32 34 26 30 32 28 33 30 31 29 29
WRMS | 11 12 8 12 15 5 9 17 8 13 |NE 27 31 23 27 30 25 31 27 28 26 25
MEDI | 10 11 7 12 15 4 9 16 9 13 |MD 27 29 22 27 28 24 30 25 28 24 23
Table 3.1892.3 GPS week: 1892 Day: 3 MJD: 57491.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 6 5 10 7 6 6 16 10 8 2 | 31 38 29 32 41 29 37 38 35 35 33
2 | 6 10 13 12 13 4 10 21 12 19 4 | 27 30 24 32 27 22 29 36 27 25 25
3 | 7 13 8 9 11 4 8 17 10 13 3 | 30 34 25 27 27 28 30 29 27 32 26
X4E | 1 --- --- --- --- 55 --- --- --- --- 0 | 56 --- --- --- --- 42 --- --- --- --- 55
5 | 8 11 7 14 17 4 11 18 13 11 4 | 28 32 22 32 26 24 31 19 30 25 25
6 | 9 5 8 6 9 6 9 16 13 11 3 | 32 40 30 38 42 31 42 40 38 33 35
7 | 11 10 10 10 15 4 10 43 12 17 5 | 28 34 26 31 25 27 32 43 29 25 25
8 | 9 8 6 9 12 4 8 16 10 9 3 | 23 29 23 26 29 27 30 32 28 29 25
9 | 12 10 6 8 13 4 10 15 6 9 3 | 25 24 14 21 19 21 25 25 23 23 19
X10 | 9 7 6 --- 12 3 8 14 6 10 3 | 37 43 35 --- 36 41 43 40 40 28 39
11 | 8 7 15 11 13 6 8 13 10 11 4 | 27 38 30 29 44 27 37 35 36 37 32
12E | 18 13 7 16 27 4 16 14 15 13 5 | 30 29 20 28 21 23 30 23 27 26 23
13 | 10 13 7 15 25 5 9 14 10 19 4 | 27 37 27 33 36 27 34 28 30 23 28
14 | 19 11 8 13 20 6 8 13 11 17 4 | 29 24 19 23 28 20 24 16 20 17 18
15 | 11 14 7 15 18 4 11 15 12 12 4 | 23 30 21 33 26 25 29 23 30 25 24
16E | 17 13 8 18 27 4 9 12 9 11 4 | 28 25 22 28 23 22 26 23 24 26 23
17 | 12 6 9 8 17 5 9 24 9 15 4 | 31 31 26 31 33 25 33 31 31 21 27
18 | 15 11 6 13 22 4 10 19 12 17 4 | 29 28 20 23 25 22 27 12 26 17 20
19 | 16 9 11 11 19 5 9 32 12 19 5 | 31 34 27 34 31 27 35 37 34 23 28
20 | 10 11 9 15 20 5 10 18 13 12 4 | 21 25 20 27 21 19 24 23 23 18 19
21 | 10 11 10 15 18 5 8 12 11 16 4 | 30 33 25 32 32 25 30 30 26 29 27
22 | 11 8 10 10 19 4 8 19 12 15 4 | 21 24 20 20 25 17 23 21 23 18 17
23 | 14 7 7 10 19 4 10 16 12 22 4 | 25 24 17 24 26 20 25 21 23 19 18
24 | 8 8 5 7 15 4 9 18 11 10 3 | 21 27 20 27 28 25 28 23 29 18 22
25 | 16 13 6 11 28 5 10 11 9 10 4 | 57 63 58 63 66 60 63 61 63 61 60
26 | 14 15 6 12 18 5 7 11 9 10 4 | 64 64 63 66 66 65 64 64 67 65 63
27 | 7 10 6 8 15 4 9 11 11 9 3 | 19 22 16 20 25 20 23 21 22 19 18
28E | 8 9 6 7 13 5 10 12 8 10 3 | 26 26 23 25 29 22 28 26 29 22 24
29 | 13 16 9 16 23 5 11 15 13 17 5 | 26 27 19 26 21 17 25 18 20 18 18
30 | 8 9 6 8 12 4 7 19 10 13 3 | 25 32 18 26 25 26 30 25 29 21 23
31 | 13 12 8 16 17 4 9 16 10 16 4 | 28 37 26 33 31 29 36 24 29 25 27
32 | 22 16 14 18 15 6 12 32 12 21 6 | 49 66 48 59 57 56 64 72 48 66 56
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 8 12 18 5 10 19 11 14 |T 30 33 26 31 31 28 33 30 31 28 28
WRMS | 12 11 8 12 16 5 10 17 10 14 |NE 27 32 24 29 30 26 31 29 29 25 25
MEDI | 10 10 7 11 17 4 9 16 11 13 |MD 28 31 23 28 28 25 30 26 29 25 25
Table 3.1892.4 GPS week: 1892 Day: 4 MJD: 57492.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 7 6 10 10 4 7 16 9 9 3 | 28 34 24 29 34 26 35 35 29 34 29
2 | 8 10 11 14 12 4 10 21 12 18 4 | 24 27 23 29 20 21 27 33 25 22 23
3 | 12 12 6 9 14 3 8 14 9 9 3 | 22 30 20 22 24 22 27 23 24 26 22
X4 | 3 --- --- --- --- 64 --- --- --- --- 0 | 100 --- --- --- --- 70 --- --- --- --- 99
5 | 9 11 7 14 19 4 9 18 11 14 4 | 23 32 19 26 24 21 29 16 21 15 21
6 | 7 6 6 11 12 4 9 13 10 11 3 | 31 37 25 35 39 31 40 37 37 32 33
7 | 11 9 8 13 15 5 8 47 11 16 5 | 29 35 26 32 28 27 32 47 26 22 25
8 | 7 8 6 9 15 5 8 18 7 13 3 | 20 26 18 21 23 20 27 28 18 27 21
9 | 10 8 7 8 12 3 10 15 9 7 3 | 23 28 17 24 23 21 28 26 21 21 22
X10 | 9 9 6 --- 9 3 7 14 7 10 3 | 39 41 32 --- 34 36 40 37 33 23 36
11 | 8 7 15 13 14 5 8 12 11 12 4 | 28 36 25 27 40 26 35 33 31 35 30
12E | 14 14 6 18 23 5 19 16 13 12 5 | 29 32 22 28 22 25 31 24 30 27 25
13 | 9 11 9 16 25 4 7 12 8 18 4 | 26 34 25 30 36 24 31 24 27 22 26
14 | 12 17 8 16 19 5 10 14 10 17 4 | 27 26 21 25 27 21 23 15 21 13 19
15 | 8 12 7 14 20 3 16 14 10 13 4 | 24 33 20 26 23 22 28 23 27 24 23
16E | 9 10 6 16 22 4 11 13 9 11 4 | 23 26 20 25 24 23 27 19 22 22 22
17 | 9 8 10 13 16 4 11 25 10 13 4 | 28 30 22 30 29 23 30 27 26 23 24
18 | 20 9 8 15 20 5 11 23 12 18 5 | 36 30 23 26 29 25 31 16 23 20 23
19 | 15 12 10 13 19 5 12 32 12 18 5 | 28 30 22 26 27 22 30 35 25 20 22
20 | 14 14 9 20 20 5 12 18 12 16 5 | 23 28 19 25 19 19 24 21 20 17 18
21 | 6 8 10 13 14 4 9 13 10 15 4 | 24 29 25 28 25 23 30 26 23 28 24
22 | 13 11 9 12 20 4 9 19 10 14 4 | 18 21 13 15 23 14 21 18 16 14 13
23 | 18 10 7 13 19 4 12 16 12 17 4 | 25 27 17 23 24 19 26 18 20 15 19
24 | 8 8 5 10 11 3 8 18 10 10 3 | 23 31 19 23 25 24 27 26 26 21 23
25 | 9 12 6 9 19 4 11 11 11 9 3 | 40 42 37 41 43 37 39 37 36 35 37
26 | 11 14 6 11 17 4 9 12 8 12 3 | 39 38 33 39 42 36 37 36 36 41 36
27 | 7 8 5 7 13 5 8 12 6 12 3 | 20 25 16 21 20 20 24 20 19 22 19
28E | 8 9 8 10 18 3 8 11 9 9 3 | 24 28 22 25 27 21 26 24 22 24 23
29 | 17 14 8 17 20 4 14 15 15 18 5 | 28 27 20 22 18 19 25 18 20 21 19
30 | 7 9 5 9 11 4 7 20 9 10 3 | 28 34 22 29 27 26 32 27 26 24 26
31 | 12 10 7 17 17 3 11 18 9 15 4 | 30 37 27 35 34 30 36 30 26 26 29
32 | 18 16 13 19 15 8 15 27 11 21 6 | 46 62 43 49 50 47 58 64 41 56 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 8 13 17 4 11 19 10 14 |T 29 32 23 27 28 26 30 27 25 24 27
WRMS | 11 11 8 13 16 4 11 17 9 14 |NE 26 31 22 27 27 24 30 27 25 23 24
MEDI | 9 10 7 13 17 4 9 16 10 13 |MD 27 30 22 26 27 23 30 26 25 23 23
Table 3.1892.5 GPS week: 1892 Day: 5 MJD: 57493.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 6 4 7 10 4 7 14 10 12 3 | 26 31 23 26 32 25 33 30 23 30 26
2 | 8 9 12 11 11 5 9 22 8 14 4 | 24 26 22 22 18 19 25 29 19 21 20
3 | 8 8 6 9 10 4 8 13 5 11 3 | 21 28 19 21 25 22 27 22 24 26 22
X4 | 2 --- --- --- --- 67 --- --- --- --- 0 | 67 --- --- --- --- 33 --- --- --- --- 66
5 | 10 10 9 12 14 4 12 17 11 13 4 | 27 33 20 27 28 24 31 15 26 20 23
6 | 6 6 6 8 8 4 7 13 5 8 2 | 29 36 24 33 33 27 39 31 29 29 30
7 | 13 8 9 12 13 5 9 51 10 14 5 | 27 34 25 30 27 25 32 50 27 21 24
8 | 8 6 5 10 11 3 9 17 5 9 3 | 26 29 23 26 29 23 30 31 27 26 25
9 | 11 7 4 7 13 2 9 13 6 12 3 | 20 25 12 22 21 18 25 21 20 25 19
X10 | 7 8 7 --- 8 3 8 13 6 9 3 | 30 36 28 --- 31 31 38 35 29 22 31
11 | 10 6 15 9 14 5 7 11 10 14 4 | 24 34 25 25 37 25 35 29 27 35 27
12E | 12 14 7 16 16 4 16 15 9 11 4 | 30 31 21 32 26 26 29 22 26 31 26
13 | 13 11 9 12 21 6 7 12 7 14 4 | 27 31 22 28 38 25 32 22 25 23 24
14 | 16 11 10 11 15 5 9 14 9 15 4 | 26 21 18 22 23 19 23 14 21 15 17
15 | 9 13 9 12 16 3 14 13 8 12 4 | 24 32 20 30 28 25 31 22 28 26 25
16E | 13 16 7 15 17 5 10 13 8 12 4 | 25 28 23 27 28 25 31 23 27 26 25
17 | 8 8 9 8 14 3 9 24 8 10 3 | 26 30 21 26 30 23 30 25 25 22 24
18 | 17 11 9 13 18 4 14 24 11 17 5 | 29 28 19 25 27 21 31 20 22 19 21
19 | 14 11 10 11 14 5 10 34 10 15 4 | 25 28 22 23 27 20 31 34 24 18 21
20 | 10 14 10 17 17 4 12 18 10 16 4 | 19 23 17 23 21 15 23 20 17 18 16
21 | 8 12 11 10 12 3 9 15 9 17 4 | 25 26 23 22 21 21 28 25 21 31 23
22 | 12 10 10 9 20 4 9 19 9 17 4 | 19 21 18 19 27 18 24 21 20 19 16
23 | 20 10 7 13 21 4 12 16 9 15 4 | 25 27 17 24 27 20 27 19 21 18 20
24 | 7 8 6 7 11 4 9 19 7 8 3 | 21 28 15 21 23 20 26 23 22 21 20
25 | 9 12 6 6 20 4 10 12 5 9 3 | 35 38 31 37 42 31 35 31 31 33 33
26 | 15 17 6 13 14 4 8 13 10 11 4 | 36 35 29 35 35 32 34 31 34 32 32
27 | 10 8 5 7 11 2 12 12 9 9 3 | 17 20 14 21 23 15 22 21 19 15 16
28E | 8 9 7 8 13 4 8 13 7 6 3 | 20 26 18 21 23 19 24 18 20 21 20
29 | 15 14 8 14 18 4 16 16 11 15 4 | 26 24 18 20 20 17 24 18 17 17 17
30 | 9 8 6 6 10 4 7 22 7 11 3 | 25 34 22 25 30 24 32 23 26 24 25
31 | 11 10 9 12 14 4 9 16 9 13 4 | 28 33 24 26 29 24 33 22 25 20 24
32 | 20 14 12 18 11 7 13 27 10 19 5 | 43 61 40 44 49 46 57 63 44 59 48
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 9 11 15 4 10 20 9 13 |T 27 30 21 26 28 23 30 26 24 24 25
WRMS | 12 11 9 10 14 4 10 16 8 12 |NE 25 29 21 25 27 22 30 26 24 23 23
MEDI | 10 10 8 11 14 4 9 15 9 12 |MD 26 29 22 25 27 23 31 23 25 22 24
Table 3.1892.6 GPS week: 1892 Day: 6 MJD: 57494.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 6 6 9 10 5 6 12 6 7 2 | 33 39 31 38 44 34 38 40 34 36 35
2 | 8 9 11 12 11 4 10 23 9 18 4 | 26 28 24 27 26 23 29 40 26 30 25
3 | 10 8 7 9 8 4 9 10 9 6 3 | 26 27 20 23 22 20 27 20 22 22 21
X4 | 2 --- --- --- --- 39 --- --- --- --- 0 | 69 --- --- --- --- 51 --- --- --- --- 68
5 | 7 12 8 13 16 4 9 18 9 11 4 | 24 32 20 25 30 22 30 13 25 18 22
6 | 8 6 6 6 6 3 8 13 8 10 2 | 36 42 32 38 43 35 44 44 41 35 38
7 | 12 8 9 11 15 5 10 50 10 14 5 | 29 36 27 33 31 29 34 53 28 26 27
8 | 10 8 7 10 11 4 9 17 10 19 4 | 30 34 28 31 30 30 34 37 34 43 32
9 | 8 7 5 13 9 3 11 13 11 11 3 | 22 24 13 21 19 18 26 21 22 24 19
X10 | 6 6 6 --- 7 3 10 14 8 8 3 | 39 42 35 --- 34 37 41 36 33 23 36
11 | 11 4 15 11 14 7 8 11 7 10 3 | 31 40 31 36 46 33 38 37 35 39 35
12 | 12 16 6 16 16 5 17 15 12 12 4 | 46 49 43 42 42 44 50 45 44 43 44
13 | 11 13 8 13 20 4 7 12 7 9 4 | 22 30 19 26 36 22 29 18 25 19 23
14 | 16 11 9 11 17 4 10 15 13 15 4 | 26 20 19 25 24 18 21 16 25 15 18
15 | 10 15 6 15 14 3 13 15 8 16 4 | 25 30 16 29 26 22 29 19 25 27 22
16E | 19 15 9 13 14 4 8 14 12 10 4 | 31 27 23 25 25 23 27 24 25 27 24
17 | 10 8 10 9 13 4 10 24 10 12 4 | 24 26 19 26 28 21 28 28 24 18 21
18 | 17 11 11 12 17 5 12 24 10 17 5 | 27 27 19 24 26 20 26 21 22 13 18
19 | 14 10 10 10 16 5 11 35 13 16 5 | 24 27 18 22 27 19 29 37 24 15 19
20 | 9 11 10 16 16 5 12 21 9 15 4 | 15 21 14 23 23 14 21 24 20 17 15
21 | 11 9 10 13 12 4 8 17 10 14 4 | 27 32 25 32 32 25 33 33 30 31 28
22 | 13 9 13 10 17 5 8 19 11 12 4 | 20 23 18 22 26 18 23 22 21 18 17
23 | 20 10 7 11 16 4 11 15 16 16 4 | 28 28 17 22 22 19 25 17 23 17 19
24 | 8 8 6 7 10 3 8 16 9 11 3 | 23 32 22 28 31 27 30 26 28 23 25
25 | 6 12 8 14 16 3 12 12 11 7 4 | 51 54 50 49 55 50 51 51 54 48 50
26 | 18 20 8 12 11 4 9 12 8 8 4 | 48 50 45 52 50 47 48 50 45 50 47
27 | 10 9 5 9 11 3 10 12 10 12 3 | 20 23 15 25 21 21 25 21 24 23 20
28E | 6 9 6 8 16 4 10 10 8 9 3 | 22 26 18 21 26 20 25 19 22 20 21
29 | 13 11 10 15 15 2 15 17 16 15 5 | 26 25 20 21 19 18 26 19 21 20 18
30 | 8 9 6 9 11 4 8 24 8 11 3 | 25 35 21 29 28 27 32 32 28 26 26
31 | 16 10 10 15 13 3 12 17 10 12 4 | 28 36 25 34 34 29 36 28 28 25 28
32 | 21 15 12 15 11 6 14 25 14 18 5 | 50 67 46 60 58 53 66 69 48 65 56
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 9 12 14 4 10 20 10 13 |T 30 33 24 30 31 27 32 30 29 27 28
WRMS | 12 11 8 12 13 4 10 15 9 12 |NE 27 31 22 28 30 25 31 29 27 25 25
MEDI | 10 9 8 11 14 4 10 15 10 12 |MD 26 30 21 26 28 23 29 28 25 24 24
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 4.1892 GPS week: 1892 MJD: 57488.0-57494.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 |U 5 4 12 |U 8 11 29 |U 6 6 15 |
emr | emr 2976 | 6 6 16 |U 9 13 32 | 8 7 17 |
esa | esa 2976 | 5 5 13 |U 8 13 32 | 6 6 16 |
gfz | gfz 2880 |U 5 5 14 |U 8 12 31 |U 7 6 16 |
grg | grg 2976 |U 6 6 15 |U 9 11 32 | 9 9 19 |
igr | igr 2976 | 5 5 12 | 8 12 29 | 6 6 15 |
igs | igs 2976 | 5 5 12 | 8 12 29 | 7 6 15 |
jpl | jpl 2976 | 6 5 16 |U 8 12 32 | 7 7 17 |
mit | mit 2976 |U 5 5 14 |U 9 14 32 |U 9 9 18 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1892.0 GPS week: 1892 Day: 0 MJD: 57488.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 6 11 | 7 11 26 | 5 6 16 |
emr | emr 2976 | 4 6 13 | 10 14 34 | 7 8 19 |
esa | esa 2976 | 4 5 11 | 9 15 35 | 6 7 17 |
gfz | gfz 2880 | 5 6 11 | 8 13 26 | 5 5 15 |
grg | grg 2976 | 5 6 13 | 9 9 28 | 8 8 20 |
igr | igr 2976 | 4 5 10 | 8 13 31 | 5 6 17 |
igs | igs 2976 | 4 5 10 | 8 12 29 | 5 6 16 |
jpl | jpl 2976 | 6 8 14 | 9 13 32 | 5 6 16 |
mit | mit 2976 | 4 6 10 | 10 16 33 | 10 17 27 |
Table 5.1892.1 GPS week: 1892 Day: 1 MJD: 57489.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 4 4 13 | 9 10 23 | 9 7 16 |
emr | emr 2976 | 5 5 15 | 10 14 28 | 10 8 18 |
esa | esa 2976 | 4 4 14 | 9 12 27 | 8 6 17 |
gfz | gfz 2880 | 4 5 12 | 9 11 24 | 9 8 14 |
grg | grg 2976 | 4 3 18 | 8 10 23 | 11 11 19 |
igr | igr 2976 | 5 4 13 | 8 11 23 | 9 7 17 |
igs | igs 2976 | 4 4 14 | 9 11 24 | 9 8 17 |
jpl | jpl 2976 | 6 5 16 | 9 11 24 | 9 7 18 |
mit | mit 2976 | 5 6 16 | 10 13 24 | 10 9 16 |
Table 5.1892.2 GPS week: 1892 Day: 2 MJD: 57490.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 17 | 5 8 25 | 7 9 17 |
emr | emr 2976 | 6 6 23 | 7 10 27 | 8 8 16 |
esa | esa 2976 | 5 5 18 | 5 9 25 | 6 9 14 |
gfz | gfz 2880 | 5 5 16 | 4 8 21 | 8 8 20 |
grg | grg 2976 | 7 8 18 | 6 10 25 | 10 11 20 |
igr | igr 2976 | 5 5 16 | 5 8 21 | 7 8 17 |
igs | igs 2976 | 5 5 17 | 5 8 21 | 7 9 16 |
jpl | jpl 2976 | 5 4 20 | 5 9 24 | 7 9 16 |
mit | mit 2976 | 6 6 19 | 6 10 22 | 9 9 21 |
Table 5.1892.3 GPS week: 1892 Day: 3 MJD: 57491.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 9 | 9 16 34 | 5 5 16 |
emr | emr 2976 | 7 6 14 | 11 18 35 | 7 6 20 |
esa | esa 2976 | 6 4 9 | 10 16 39 | 6 5 17 |
gfz | gfz 2880 | 5 4 11 | 10 17 37 | 5 4 16 |
grg | grg 2976 | 6 5 14 | 11 15 37 | 6 6 17 |
igr | igr 2976 | 6 4 9 | 9 16 36 | 5 4 15 |
igs | igs 2976 | 5 4 9 | 10 16 36 | 5 4 15 |
jpl | jpl 2976 | 7 5 12 | 9 16 36 | 5 6 17 |
mit | mit 2976 | 5 3 11 | 9 17 35 | 6 6 15 |
Table 5.1892.4 GPS week: 1892 Day: 4 MJD: 57492.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 3 4 11 | 13 13 45 | 5 5 14 |
emr | emr 2976 | 5 5 15 | 14 15 44 | 6 5 16 |
esa | esa 2976 | 4 4 11 | 12 14 43 | 6 6 18 |
gfz | gfz 2880 | 4 4 13 | 13 16 46 | 6 6 15 |
grg | grg 2976 | 6 7 16 | 15 15 56 | 9 10 20 |
igr | igr 2976 | 4 5 13 | 12 14 42 | 6 6 16 |
igs | igs 2976 | 4 4 12 | 12 14 43 | 6 6 16 |
jpl | jpl 2976 | 5 5 17 | 13 13 48 | 6 6 19 |
mit | mit 2976 | 5 4 11 | 13 14 47 | 9 9 15 |
Table 5.1892.5 GPS week: 1892 Day: 5 MJD: 57493.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 4 13 | 8 14 35 | 7 7 13 |
emr | emr 2976 | 8 6 19 | 8 13 36 | 9 6 15 |
esa | esa 2976 | 7 5 15 | 8 14 36 | 7 7 14 |
gfz | gfz 2880 | 7 5 17 | 9 13 35 | 8 7 16 |
grg | grg 2976 | 7 5 17 | 7 11 33 | 9 9 20 |
igr | igr 2976 | 6 4 14 | 8 13 34 | 7 7 14 |
igs | igs 2976 | 7 5 14 | 7 12 34 | 8 7 13 |
jpl | jpl 2976 | 7 6 16 | 8 12 34 | 9 6 14 |
mit | mit 2976 | 7 4 16 | 9 18 40 | 9 8 14 |
Table 5.1892.6 GPS week: 1892 Day: 6 MJD: 57494.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 11 | 5 8 17 | 6 6 13 |
emr | emr 2976 | 8 7 17 | 6 7 17 | 7 5 12 |
esa | esa 2976 | 5 5 12 | 6 9 21 | 7 5 13 |
gfz | gfz 2880 | 5 4 14 | 6 7 28 | 7 5 14 |
grg | grg 2976 | 6 6 13 | 6 10 24 | 9 8 18 |
igr | igr 2976 | 5 5 12 | 5 7 19 | 6 5 13 |
igs | igs 2976 | 5 5 12 | 5 7 18 | 7 5 13 |
jpl | jpl 2976 | 6 6 16 | 6 8 24 | 8 7 16 |
mit | mit 2976 | 5 4 15 | 7 11 26 | 8 8 15 |
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 6.1892 GPS week: 1892 MJD: 57488.500-57494.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -17 -19 114 20 -2 | 24 33
| 21 13 51 101 4 | 4
emr uuuuu | 46 10 -108 202 -9 | 68 74
| 14 18 121 57 13 | 3
esa uuuuu | -12 -8 56 -93 -7 | 34 42
| 15 17 64 55 6 | 2
gfz uuuuu | -18 11 60 -242 0 | 25 35
| 34 20 90 139 4 | 4
grg uuuux | -35 1 -53 26 -24 | 54 63
| 12 19 42 69 20 | 1
igr xxxxx | -20 21 30 -23 -2 | 6 26
| 6 15 30 35 4 | 4
irf xxxxx | 14 -4 -57 -42 -4 | 12 31
| 10 9 21 36 10 | 6
jpl uuuuu | -8 6 83 94 0 | 45 50
| 31 18 59 55 8 | 3
mit uuuuu | 28 15 -183 -130 20 | 34 46
| 15 25 34 68 11 | 12
ngs uuuuu | -19 -15 -34 -16 -4 | 18 32
| 25 9 67 146 3 | 4
sio uuuux | 49 10 -70 89 2 | 72 76
| 20 16 34 58 5 | 5
Table 7.1892.0 GPS week: 1892 Day: 0 MJD: 57488.500
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 | -3 -37 67 119 -5 | 22 32
emr uuuuu | 58 -24 58 101 -24 | 69 75
esa uuuuu | -32 -13 68 -179 -7 | 35 43
gfz uuuuu | -8 42 -46 -279 -2 | 23 34
grg uuuux | -41 18 -127 -27 -19 | 54 63
igr xxxxx | -15 28 22 -54 1 | 3 26
irf xxxxx | -3 7 -79 -38 10 | 6 31
jpl uuuuu | -14 11 25 8 -15 | 45 50
mit uuuuu | 15 13 -231 -66 33 | 19 36
ngs uuuuu | -38 -20 59 148 -5 | 15 31
sio uuuux | 60 25 -43 115 1 | 69 74
Table 7.1892.1 GPS week: 1892 Day: 1 MJD: 57489.500
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 | 3 -7 173 36 -7 | 20 32
emr uuuuu | 59 15 -7 192 6 | 64 71
esa uuuuu | -8 22 -27 -86 -16 | 33 41
gfz uuuuu | 0 1 84 -248 1 | 21 33
grg uuuux | -27 34 -70 120 -30 | 54 63
igr xxxxx | -16 30 53 -41 2 | 2 26
irf xxxxx | 30 -7 -41 2 8 | 5 31
jpl uuuuu | -52 -20 58 157 -1 | 42 48
mit uuuuu | 39 -33 -138 -59 30 | 22 38
ngs uuuuu | -11 -10 -63 -163 -5 | 14 31
sio uuuux | 38 -11 -117 179 7 | 67 72
Table 7.1892.2 GPS week: 1892 Day: 2 MJD: 57490.500
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 -10 127 -39 4 | 21 32
emr uuuuu | 54 -2 -122 198 8 | 65 72
esa uuuuu | 18 -3 23 -44 -13 | 33 41
gfz uuuuu | 33 16 98 -14 -6 | 23 35
grg uuuux | -33 -3 -67 117 -16 | 55 63
igr xxxxx | -25 15 83 -40 3 | 4 27
irf xxxxx | 10 -21 -73 -20 -3 | 9 31
jpl uuuuu | -25 1 173 62 5 | 43 49
mit uuuuu | 2 16 -213 -176 22 | 27 43
ngs uuuuu | -57 0 -115 -205 -7 | 17 31
sio uuuux | 27 -12 -100 121 -3 | 70 75
Table 7.1892.3 GPS week: 1892 Day: 3 MJD: 57491.500
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 -5 180 -20 -1 | 21 32
emr uuuuu | 25 30 -249 226 -10 | 65 72
esa uuuuu | -12 6 51 -42 -6 | 32 40
gfz uuuuu | -1 -15 129 -136 -3 | 22 34
grg uuuux | -25 -13 -45 -1 -39 | 55 63
igr xxxxx | -17 39 -6 -65 -7 | 4 27
irf xxxxx | 18 -7 -52 -21 1 | 10 32
jpl uuuuu | -30 -2 161 58 3 | 43 48
mit uuuuu | 38 7 -201 -116 24 | 31 47
ngs uuuuu | 10 -21 -117 -112 -3 | 16 31
sio uuuux | 23 8 -35 84 7 | 68 73
Table 7.1892.4 GPS week: 1892 Day: 4 MJD: 57492.500
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 | -30 -18 49 -15 1 | 24 35
emr uuuuu | 30 19 -15 277 -7 | 68 75
esa uuuuu | -16 -21 13 -154 0 | 34 42
gfz uuuuu | -40 24 -18 -456 3 | 25 36
grg uuuux | -46 -6 -15 26 -58 | 55 63
igr xxxxx | -23 -9 9 30 -2 | 7 27
irf xxxxx | 14 2 -77 -59 -10 | 15 33
jpl uuuuu | 3 -3 68 129 3 | 46 51
mit uuuuu | 31 31 -155 -120 13 | 40 52
ngs uuuuu | 6 -14 26 116 -9 | 20 33
sio uuuux | 60 24 -73 84 1 | 73 78
Table 7.1892.5 GPS week: 1892 Day: 5 MJD: 57493.500
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 | -10 -35 78 178 -1 | 27 35
emr uuuuu | 53 23 -192 171 -23 | 71 76
esa uuuuu | -11 -26 168 -49 -4 | 36 43
gfz uuuuu | -39 18 -21 -250 3 | 28 37
grg uuuux | -53 -23 0 -62 -11 | 52 63
igr xxxxx | -30 21 22 2 -7 | 10 26
irf xxxxx | 12 5 -54 -107 -16 | 18 32
jpl uuuuu | 28 36 44 94 12 | 47 53
mit uuuuu | 25 26 -185 -258 7 | 45 55
ngs uuuuu | -34 -14 -7 -12 -2 | 21 33
sio uuuux | 58 12 -30 31 -5 | 76 80
Table 7.1892.6 GPS week: 1892 Day: 6 MJD: 57494.500
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 | -57 -21 126 -120 -1 | 30 35
emr uuuuu | 43 12 -231 249 -14 | 72 76
esa uuuuu | -22 -18 99 -101 -3 | 38 42
gfz uuuuu | -70 -8 194 -310 4 | 31 36
grg uuuux | -21 2 -50 11 3 | 52 63
igr xxxxx | -12 22 27 6 -4 | 12 24
irf xxxxx | 16 -4 -22 -54 -16 | 20 29
jpl uuuuu | 33 22 50 150 -5 | 51 54
mit uuuuu | 45 44 -156 -114 7 | 52 54
ngs uuuuu | -8 -26 -22 114 1 | 24 31
sio uuuux | 76 25 -90 6 4 | 80 81
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