[IGSREPORT-22160] Wk 1758 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Oct 3 05:43:31 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1758 (Sep 15, 2013 - Sep 21, 2013)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1758[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1758[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1758[0-6].cls IGS GPS clock combination summary report.
igs17587.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17587.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 | CONZ HOB2 JOZ2 KOUC NRIL NYA1 OPMT REYK TSKB XMIS
0 | COD | ARTU CONZ KOUC NYA1 USNO XMIS
0 | EMR | 4 4
0 | ESA | ARTU
0 | GRG | NYAL BARH NYAL
0 | JPL | 4 8
0 | MIT | 31 31 MDVJ NICO NYAL MDVJ NICO NYAL
1 | COD | AUCK MOBS NRMD TIDB TSKB XMIS MOBS NRMD XMIS
1 | GFZ | KOUC TLSE KOUC
1 | GRG | IRKJ TLSE IRKJ TLSE
1 | MIT | TLSE MIZU NICO TLSE TSKB
2 | COD | CHTI KARR KOUC REYK KARR KOUC REYK
2 | EMR | OPMT
2 | ESA | UNSA
2 | GRG | BOGT IRKJ NOVM NRMD USN3 ADIS BOGT IRKJ NOVM NRMD
2 | GRG | USN3
2 | JPL | 21
2 | MIT | 9 15 17 9 15 17 21 DAEJ IRKJ NICO DAEJ IRKJ MDVJ
2 | MIT | NICO TIDB
3 | COD | 16 ANKR ASPA BAKO BRAZ BRFT BRST BRUX CHTI CHUR DARW
3 | COD | FLRS GLSV GOLD HARB HERT HOB2 HRAO JOZ2 KARR KOUC
3 | COD | KOUR LAMA MAC1 MAG0 MCM4 MDVJ NRIL NTUS ONSA PRDS
3 | COD | REYK SCH2 SYDN SYOG TLSE TOW2 TRO1 TSKB TWTF WAB2
3 | COD | WSRT WTZR XMIS ZAMB HERT JOZ2 KOUC REYK XMIS
3 | EMR | HERS HERS
3 | ESA | THTI
3 | GFZ | THTI MATE
3 | GRG | IRKJ LPGS NOVM THTI ADIS IRKJ LPGS NOVM THTI
3 | JPL | 9
3 | MIT | 12 16 21 12 16 21 MDVJ NICO MDVJ NICO USNO
4 | COD | ALIC AREQ BRFT HERT JOZ2 KOUC REUN REYK SYOG XMIS
4 | COD | ZAMB ZECK HERT KOUC NKLG REYK XMIS
4 | EMR | YELL YELL
4 | ESA | NKLG
4 | GFZ | NOVM STJO NOVM STJO
4 | GRG | 21 21 IRKJ NRMD IRKJ NRMD
4 | MIT | 9 10 24 26 32 9 10 24 26 32 MDVJ NICO TNML MDVJ NICO
4 | MIT | TNML
5 | COD | ALIC KOUC MAW1 REYK USNO XMIS KOUC XMIS
5 | EMR | YELL HERS YELL
5 | ESA | UNSA
5 | GRG | GUUG IRKJ GUUG IRKJ
5 | MIT | 4 21 32 9 GOPE MAW1 NICO MDVJ NICO TSKB
6 | COD | GRAZ KOUC NNOR XMIS GRAZ KOUC NNOR XMIS
6 | ESA | UNSA
6 | GFZ | MATE MATE
6 | GRG | HYDE IRKJ HYDE IRKJ ISPA NYAL TNML
6 | MIT | SPT0 SPT0
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | GRG | ~11:31 | ~ 0.18 ns
5 | GRG | ~05:34 | ~ 0.14 ns
5 | MIT | ~23:32 | ~ 0.03 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. 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 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | 1.0 .1 .5 -47 21 -15 .10
EMR | 0 | .8 9.8 11.7 5 20 -29 -.02
ESA | 0 | 1.2 6.2 7.4 21 -39 58 -.09
GFZ | 0 | -.1 .0 -1.1 -11 -1 19 -.06
GRG | 0 | 5.2 5.2 22.9 -11 59 -17 .05
JPL | 0 | .6 14.3 8.7 -66 20 29 .10
MIT | 0 | .0 2.1 9.8 5 19 -49 .08
NGS | 0 | 4.4 4.6 18.7 -56 -21 28 .28
SIO | 0 | 1.1 .9 32.0 35 121 17 -.15
COD | 1 | 1.0 -.3 .8 -31 17 26 -.11
EMR | 1 | 2.6 8.3 10.9 7 8 -50 -.26
ESA | 1 | -2.8 9.9 4.0 17 -52 81 -.06
GFZ | 1 | .5 .3 -.3 -20 -13 12 -.37
GRG | 1 | 6.6 2.5 19.2 -34 39 -13 .01
JPL | 1 | -.4 5.2 12.9 -89 -12 25 .02
MIT | 1 | 1.0 2.9 8.4 -7 -1 -34 .07
NGS | 1 | 1.7 -2.5 18.2 -77 -35 5 .17
SIO | 1 | .7 3.4 34.2 36 113 -18 -.27
COD | 2 | .7 .3 .6 -65 27 11 -.20
EMR | 2 | 4.9 10.2 8.1 11 11 -20 -.15
ESA | 2 | -4.0 5.9 1.7 7 -15 57 -.39
GFZ | 2 | .3 .3 -.4 -17 -18 14 -.37
GRG | 2 | 2.2 8.7 17.4 -46 23 -38 -.22
JPL | 2 | -5.8 9.4 6.1 -72 -13 -13 -.01
MIT | 2 | -2.3 1.9 3.3 -12 -2 -41 -.02
NGS | 2 | .5 -5.6 1.8 -34 0 2 -.22
SIO | 2 | -.5 3.8 31.3 65 100 1 -.30
COD | 3 | .8 .3 .8 -47 32 26 -.17
EMR | 3 | 7.3 7.2 8.3 5 12 -35 -.01
ESA | 3 | .0 7.8 -1.3 4 -16 41 -.30
GFZ | 3 | .2 .5 -.3 -18 -20 1 -.33
GRG | 3 | -.6 2.1 11.2 -18 12 -19 -.15
JPL | 3 | -.4 -1.1 14.1 -75 -34 -20 -.18
MIT | 3 | 1.0 1.1 8.3 -6 -4 -42 .06
NGS | 3 | 6.6 .7 11.9 -60 -25 38 .0
SIO | 3 | .4 2.5 32.7 21 82 26 -.33
COD | 4 | .7 -.2 .3 -47 29 40 -.22
EMR | 4 | -1.7 5.3 11.8 -7 16 -23 -.05
ESA | 4 | .9 1.3 3.4 -7 -49 30 -.34
GFZ | 4 | .5 .1 -.8 -14 -22 27 -.14
GRG | 4 | -3.1 1.5 10.7 -44 21 -17 -.20
JPL | 4 | .4 -1.1 17.0 -77 -8 -36 .17
MIT | 4 | 1.2 2.4 8.3 -10 -4 -37 .05
NGS | 4 | 4.9 -7.3 6.8 -49 -6 23 -.06
SIO | 4 | 3.1 -1.5 26.5 12 51 120 -.27
COD | 5 | .1 -.4 -.4 -46 22 -1 .05
EMR | 5 | 4.3 12.5 11.2 11 3 -43 -.02
ESA | 5 | -2.5 4.6 .9 11 -34 58 -.39
GFZ | 5 | .5 .2 -.5 -23 -21 20 -.26
GRG | 5 | -3.0 2.6 11.0 -33 26 1 -.06
JPL | 5 | 1.6 5.1 11.5 -109 39 -9 -.13
MIT | 5 | 1.8 7.4 7.7 -7 4 -35 -.03
NGS | 5 | 4.6 .3 19.9 -74 -26 26 .01
SIO | 5 | 2.8 4.0 29.1 54 68 -68 -.23
COD | 6 | .4 .0 -.3 -63 32 35 -.23
EMR | 6 | 6.2 6.7 7.1 -4 3 -25 -.21
ESA | 6 | -3.4 5.6 1.4 2 -39 78 -.44
GFZ | 6 | .2 .1 -.5 -19 -10 26 -.39
GRG | 6 | 2.3 4.4 6.1 -10 13 -8 -.01
JPL | 6 | .2 3.7 11.1 -80 41 -20 -.34
MIT | 6 | .8 5.5 5.2 -6 -1 -40 -.09
NGS | 6 | 5.1 .0 12.6 -63 -29 31 -.15
SIO | 6 | .7 4.7 13.2 26 29 -94 -.34
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1758.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1758.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 2.1758.[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 3.1758.[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 5.1758.0-6). 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 1758 summary. (Sep 15, 2013 - Sep 21, 2013)
Table 1.1758.a GPS week: 1758 MJD: 56550.000-56556.000
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 259| 1 0 1 -6 33 8 .10 10 10 | -784 -201 18 141
| 0 0 1 20 21 23 .02 | 468 699
emr 80| 0 1 3 0 7 -5 .08 16 16 | 3989 187 13 115
| 1 0 0 12 7 12 .05 | 673 967
esa 150| 0 0 0 16 5 19 -.21 6 6 | -1591 1181 9 116
| 0 0 0 16 18 10 .03 | 840 1715
gfz 197| -2 0 -1 3 -4 8 .06 10 10 | 9 164 11 87
| 1 0 0 19 12 12 .03 | 690 821
grg 138| 1 0 2 22 6 -9 .37 15 13 | -10 -76 17 154
| 1 1 3 31 37 18 .04 | 224 498
igr n/a| 0 0 0 3 12 -14 -.43 5 5 | -10270 702 15 80
| 0 0 0 15 15 14 .03 | 1284 900
jpl 80| 0 -1 -3 -16 14 -10 .10 15 15 | 3382 79 15 105
| 1 1 2 16 19 16 .01 | 912 928
mit 235| 0 -2 -3 -14 3 -19 -.19 14 13 | 55 -119 26 232
| 0 0 1 36 21 6 .05 | 341 592
ngs 239| 0 0 2 -39 -65 -36 .06 11 9 | 665637 -285631 1846 3495
| 1 0 2 47 55 19 .02 | 1217003 488006
sio 456| 0 0 -4 26 83 -52 -.66 20 21 | --- --- --- ---
| 1 0 2 28 40 81 .03 | --- ---
Table 1.1758.b GPS week : 1758 MJD: 56550.000-56556.000
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 5 5 4 4 4 4 |
2 | 5 4 5 4 4 4 4 |
3 | 3 4 4 4 4 4 4 |
4 | 5 5 5 4 4 4 4 |
5 | 4 4 5 5 4 5 5 |
6 | 4 4 4 4 4 4 4 |
7 | 5 5 5 5 5 4 5 |
8 | 6 7 6 5 4 4 4 |
9 | 4 4 4 4 3 3 3 |
10 | 4 3 4 4 4 4 3 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 5 4 4 4 4 |
15 | 4 5 5 5 5 4 5 |
16 | 5 5 6 5 5 4 5 |
17 | 5 5 5 5 5 5 5 |
18 | 4 5 5 5 5 4 4 |
19 | 5 4 5 5 5 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 5 4 8 5 5 |
22 | 4 5 5 5 5 4 4 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 5 4 5 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 4 4 5 5 5 5 |
28 | 5 4 4 4 4 4 4 |
29 | 4 4 5 4 4 5 4 |
30 | 0 0 --- --- --- 0 0 |
31 | 5 5 6 5 5 5 5 |
32 | 4 3 3 3 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1758.0 GPS week: 1758 Day: 0 MJD: 56550.000
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 258| 0 0 0 -39 15 -27 .11 10 9 | -1210 143 18 115
emr 80| -1 0 3 -13 8 5 .14 16 16 | 3301 1865 15 118
esa 150| 1 0 0 14 -8 12 -.16 5 5 | -1986 1516 8 103
gfz 198| -3 1 -1 -31 -17 13 .05 12 13 | 62 -391 13 81
grg 139| 1 0 5 56 44 11 .39 14 14 | -109 160 19 143
igr n/a| 0 0 0 -9 3 -23 -.44 5 5 | -12767 2343 16 74
jpl 80| 0 -1 -1 -44 38 3 .12 16 15 | 2531 1680 16 96
mit 237| -1 -1 -5 16 -20 -14 -.26 15 12 | -172 49 24 188
ngs 243| 0 0 3 28 -9 -20 .01 11 10 | -1283 282 1769 3214
sio 467| 1 0 -8 46 105 -38 -.68 23 20 | --- --- --- ---
Table 2.1758.1 GPS week: 1758 Day: 1 MJD: 56551.000
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 264| 0 0 1 -4 4 -7 .10 10 9 | -1312 674 22 121
emr 81| 2 1 3 -1 3 -28 .11 17 17 | 3952 -340 15 104
esa 150| 0 1 -1 32 -1 33 -.17 6 6 | -1626 1234 10 119
gfz 195| -1 0 -1 9 0 19 .07 10 10 | -1405 1688 11 83
grg 141| 2 -2 2 56 17 -15 .34 14 13 | 246 -401 19 140
igr n/a| -1 0 -1 -19 10 -36 -.38 5 4 | -10634 258 17 79
jpl 80| 0 -3 -4 -12 28 3 .10 15 15 | 4040 -356 15 95
mit 237| 0 -3 -3 -12 23 -29 -.25 13 12 | 267 -374 23 233
ngs 242| -1 0 4 -78 -66 -33 .06 10 8 | -1304 683 1816 3411
sio 454| 0 -1 -3 29 129 -97 -.69 21 22 | --- --- --- ---
Table 2.1758.2 GPS week: 1758 Day: 2 MJD: 56552.000
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 258| 1 0 3 0 53 30 .11 10 10 | -977 295 20 110
emr 80| 2 2 4 -6 12 -10 .09 17 17 | 5119 -1359 13 117
esa 150| 0 1 -1 23 32 22 -.23 6 6 | -1476 -1108 9 118
gfz 197| 0 0 -2 -3 10 4 .06 10 10 | -107 346 12 86
grg 139| 2 0 6 8 -6 -24 .32 15 14 | -47 308 23 129
igr n/a| 0 0 0 10 0 -22 -.41 5 5 | -10022 -475 15 76
jpl 80| 0 0 0 -20 4 -23 .11 16 15 | 5151 -1348 17 111
mit 235| 0 -3 -3 -38 -13 -15 -.22 15 14 | 21 165 27 219
ngs 241| -2 0 -2 -49 -155 -54 .07 12 11 | -968 299 1818 3160
sio 467| 2 -1 -2 39 87 -66 -.65 19 21 | --- --- --- ---
Table 2.1758.3 GPS week: 1758 Day: 3 MJD: 56553.000
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 261| 2 -1 0 -22 30 24 .11 11 11 | -714 -13 16 127
emr 80| 1 2 3 6 -6 -1 .09 16 16 | 3587 494 13 114
esa 150| 0 0 0 28 0 5 -.21 5 5 | -1392 1430 8 104
gfz 200| -2 1 -1 19 -24 -15 .01 10 9 | 494 442 11 80
grg 137| 2 2 2 -25 13 -34 .33 14 13 | -162 378 13 124
igr n/a| 0 0 -1 6 -3 -9 -.44 4 4 | -10481 1322 15 90
jpl 80| -2 0 -5 -5 -3 0 .10 15 15 | 3054 609 16 109
mit 237| 0 -3 -2 -54 11 -20 -.17 14 13 | -187 304 25 243
ngs 246| 0 0 3 -42 -9 -9 .08 11 9 | -554 -190 1824 3673
sio 447| 1 -1 -2 -22 100 -19 -.66 19 23 | --- --- --- ---
Table 2.1758.4 GPS week: 1758 Day: 4 MJD: 56554.000
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 261| 1 0 3 26 68 -3 .07 10 10 | -464 -591 20 123
emr 80| 0 1 4 22 11 -2 .01 15 15 | 3430 251 12 109
esa 150| 0 0 -1 -16 -18 8 -.22 7 7 | -2488 3946 13 122
gfz 200| -2 0 0 28 2 22 .05 10 9 | 333 -227 12 85
grg 137| 1 2 1 34 49 -8 .38 16 13 | 72 -103 14 114
igr n/a| 0 0 0 23 14 -1 -.43 5 5 | -9843 337 15 78
jpl 80| -1 -1 -5 2 -12 -1 .08 14 14 | 2930 -97 17 99
mit 229| 0 -3 -2 49 34 -25 -.15 14 14 | -10 160 25 226
ngs 240| 0 -1 0 -111 -100 -27 .07 11 9 | -515 -496 1585 3499
sio 448| 0 0 -3 60 98 105 -.67 20 22 | --- --- --- ---
Table 2.1758.5 GPS week: 1758 Day: 5 MJD: 56555.000
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 257| 1 0 1 -2 37 4 .08 9 9 | 56 -1443 17 121
emr 80| 0 1 2 4 13 8 .03 15 15 | 3854 72 14 100
esa 150| 0 0 0 18 28 26 -.23 6 6 | 80 -785 9 105
gfz 198| -2 0 -1 2 -4 13 .09 10 9 | 717 -908 11 86
grg 136| 2 1 -1 -5 -20 -11 .38 15 14 | 274 -1036 16 133
igr n/a| 0 0 0 16 40 3 -.45 5 5 | -9508 431 15 71
jpl 80| 0 -2 -3 -32 16 -23 .10 15 14 | 2790 -148 15 106
mit 236| 1 -2 -4 -37 6 -9 -.15 14 14 | 721 -1367 31 221
ngs 232| -1 0 4 2 -94 -50 .09 10 9 | 3077440 -999999 2199 3903
sio 459| -1 0 -4 32 63 -110 -.65 20 19 | --- --- --- ---
Table 2.1758.6 GPS week: 1758 Day: 6 MJD: 56556.000
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 259| 0 0 3 -4 28 37 .13 10 10 | -867 -476 19 273
emr 80| 0 1 2 -7 9 -10 .12 16 16 | 4681 327 12 147
esa 150| 1 0 0 10 4 24 -.24 5 5 | -2249 2036 9 144
gfz 194| -4 1 0 -2 0 1 .08 11 10 | -28 199 12 108
grg 138| 0 0 -1 34 -55 17 .43 15 13 | -348 158 17 300
igr n/a| 0 0 0 -3 23 -9 -.46 5 5 | -8637 699 15 96
jpl 80| 0 -2 -1 -1 30 -36 .12 14 14 | 3178 213 15 123
mit 234| 0 -1 -4 -24 -20 -24 -.13 14 13 | -252 228 27 299
ngs 232| 0 0 2 -27 -23 -61 .06 10 9 | 1586648 -999999 1911 3606
sio 450| -3 0 -4 1 2 -141 -.61 21 19 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1758.0 GPS week: 1758 Day: 0 MJD: 56550.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 15 5 8 8 6 14 12 13 14 4 | 59 57 55 58 61 54 62 59 56 57 57
2E | 16 14 6 12 17 5 17 12 12 28 4 | 42 34 38 42 44 35 33 38 35 26 37
3 | 7 12 3 12 13 4 10 9 8 17 3 | 21 23 21 27 28 18 25 20 19 18 21
4E | 10 15 7 16 16 7 16 23 7 42 5 | 90 90 88 89 91 86 90 85 86 96 88
5 | 10 13 6 9 14 5 19 11 13 10 4 | 21 21 15 23 31 12 21 19 19 12 18
6 | 6 14 3 13 12 3 12 9 11 21 3 | 22 23 22 27 28 18 24 22 17 24 21
7 | 8 26 5 11 12 5 19 10 14 13 4 | 25 30 19 25 30 14 27 19 20 10 20
8E | 14 16 7 12 17 8 17 32 20 27 6 | 119 121 117 120 120 115 121 120 121 121 118
9 | 7 11 5 11 11 6 14 18 9 23 3 | 20 25 17 19 20 13 25 24 18 25 18
10 | 9 9 5 8 19 4 9 10 11 26 3 | 20 23 17 24 27 15 19 17 18 22 18
11 | 8 11 6 10 20 5 12 12 10 18 4 | 26 26 21 26 36 17 26 23 22 23 23
12 | 11 18 6 10 19 7 19 25 11 22 5 | 23 22 18 24 32 18 21 30 19 20 19
13 | 5 15 4 10 14 3 14 10 11 28 3 | 32 37 31 37 41 30 34 23 28 23 31
14 | 10 16 6 14 12 5 17 9 10 21 4 | 33 35 33 40 41 32 32 36 33 27 34
15 | 9 16 4 12 12 5 20 14 12 16 4 | 30 31 28 32 37 26 29 33 26 31 29
16 | 12 19 5 17 13 3 19 16 10 20 5 | 22 21 17 29 25 16 22 19 19 18 17
17 | 10 15 4 12 15 4 16 21 10 40 4 | 31 29 28 38 36 26 28 33 23 36 28
18 | 10 16 5 14 13 4 19 11 10 16 4 | 20 25 21 30 31 21 23 26 23 17 22
19 | 12 16 6 15 10 4 17 12 12 25 4 | 27 29 23 31 30 23 28 22 21 22 23
20 | 8 16 4 10 11 5 17 9 7 18 3 | 29 26 24 29 33 20 24 23 24 13 25
21E | 9 16 5 12 14 4 15 18 8 21 4 | 45 38 42 47 46 38 41 36 42 34 41
22 | 7 17 5 11 13 4 18 13 8 16 4 | 28 32 27 34 37 26 29 33 28 21 29
23 | 6 17 5 13 11 3 16 9 10 24 3 | 26 30 24 32 29 23 28 20 24 21 24
24 | 9 16 7 10 12 6 15 12 13 14 4 | 21 24 22 20 25 18 23 18 22 15 20
25 | 8 19 6 9 14 6 14 14 11 16 4 | 20 32 19 18 28 16 27 21 17 16 20
26 | 12 11 5 11 12 7 13 16 11 20 4 | 25 26 26 32 34 25 24 31 25 29 26
X27 | 9 12 4 11 --- 5 14 10 9 20 3 | 30 31 27 28 --- 25 36 28 29 27 28
28 | 9 17 4 11 16 5 17 19 8 24 4 | 27 27 29 37 40 25 28 36 26 27 29
29 | 7 19 6 12 13 7 17 9 8 24 4 | 33 41 32 32 35 31 39 33 34 37 33
X30 | 3 --- --- --- --- 56 --- --- --- --- 0 | 1 --- --- --- --- 1 --- --- --- --- 1
31 | 9 23 5 14 19 5 19 10 13 16 5 | 22 25 20 28 36 19 26 21 28 20 22
32 | 9 11 4 10 13 5 11 15 7 24 3 | 15 20 15 14 18 11 22 17 18 24 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 5 12 14 5 16 15 11 23 |T 31 34 30 35 38 27 33 31 30 29 29
WRMS | 9 16 5 13 14 5 15 12 10 20 |NE 24 27 22 28 31 19 26 24 23 22 22
MEDI | 9 16 5 11 13 5 16 12 10 21 |MD 26 29 24 30 33 21 27 24 24 23 23
Table 3.1758.1 GPS week: 1758 Day: 1 MJD: 56551.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 17 19 8 9 15 9 15 11 12 12 4 | 76 83 76 78 80 76 79 75 78 77 78
2 | 7 16 5 9 17 3 13 8 9 18 3 | 27 27 26 30 29 22 28 28 27 21 26
3 | 7 14 4 10 14 3 9 12 9 14 3 | 22 25 21 25 22 21 24 22 23 21 21
4E | 10 17 11 12 19 8 18 9 11 26 5 | 79 89 79 84 82 81 88 81 86 80 82
5 | 10 14 6 10 14 8 17 12 8 12 4 | 22 23 16 22 31 13 24 19 19 12 19
6 | 6 14 5 9 17 3 8 12 10 16 3 | 19 22 19 21 24 18 23 21 20 20 19
7 | 9 21 6 9 15 4 18 12 8 14 4 | 26 25 16 21 31 14 24 21 22 13 19
8E | 20 18 9 8 16 7 18 29 19 32 6 | 128 131 127 130 130 124 129 128 132 129 128
9 | 12 10 5 9 10 5 10 16 7 25 3 | 25 25 20 22 22 16 24 23 22 28 21
10 | 8 11 4 7 15 4 11 9 8 24 3 | 21 24 17 22 22 15 21 19 22 26 19
11 | 11 13 5 7 20 4 9 8 10 12 3 | 26 24 17 22 35 15 23 19 22 17 21
12 | 7 19 8 11 14 5 18 19 7 21 4 | 22 25 21 25 28 18 24 25 22 17 21
13 | 6 14 4 8 16 4 12 11 9 24 3 | 26 32 26 30 37 22 32 21 28 19 27
14 | 10 16 6 12 14 4 17 10 10 22 4 | 27 30 26 27 30 25 28 27 27 22 26
15 | 12 17 6 9 11 5 20 13 9 17 4 | 27 26 22 26 28 18 25 24 23 22 23
16 | 11 22 4 12 13 4 15 16 8 19 4 | 18 23 15 22 23 18 22 20 21 18 17
17 | 14 17 6 12 12 4 15 14 10 40 4 | 31 27 24 35 31 22 30 27 26 31 26
18 | 7 21 6 10 17 5 18 13 9 18 4 | 16 25 19 21 25 16 23 21 18 17 18
19 | 9 18 6 10 14 4 15 11 11 21 4 | 23 29 20 24 29 19 29 20 24 20 22
20 | 7 19 6 7 14 2 12 10 11 20 4 | 29 28 26 28 34 22 28 26 29 17 26
21E | 8 15 7 8 11 3 11 13 8 11 3 | 41 38 42 40 42 36 38 40 39 32 40
22 | 9 20 6 12 15 3 18 16 9 16 4 | 20 28 22 29 32 21 26 27 25 21 23
23 | 7 16 5 10 13 4 13 10 10 24 3 | 23 26 22 26 27 19 27 20 25 18 22
24 | 10 13 7 12 7 5 14 12 11 16 4 | 21 23 21 20 26 16 25 19 19 17 20
25 | 5 19 7 9 10 6 12 13 8 14 3 | 19 29 20 18 25 18 27 21 20 16 20
26 | 11 11 6 9 12 4 10 13 6 19 3 | 20 21 17 23 22 16 20 20 19 22 18
X27 | 8 13 4 8 --- 5 14 11 11 16 3 | 23 26 23 21 --- 20 33 22 26 22 23
28 | 8 18 4 11 16 5 12 10 9 21 4 | 25 26 26 32 34 21 29 25 24 21 26
29 | 10 18 8 14 12 3 15 10 9 21 4 | 24 28 22 26 24 21 28 23 22 22 22
X30 | 1 --- --- --- --- 951 --- --- --- --- 0 | 1 --- --- --- --- 1 --- --- --- --- 1
31 | 11 18 6 12 19 5 21 10 9 15 4 | 20 25 19 23 38 18 27 22 25 18 21
32 | 9 11 5 9 14 4 9 11 5 26 3 | 20 20 19 20 20 16 20 17 23 26 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 6 10 14 5 15 13 10 21 |T 29 33 28 32 35 25 33 29 30 27 28
WRMS | 9 17 6 10 13 4 15 12 8 22 |NE 22 25 20 24 28 17 25 21 22 20 20
MEDI | 9 17 6 9 14 4 14 12 9 19 |MD 23 26 21 25 29 18 27 22 23 21 21
Table 3.1758.2 GPS week: 1758 Day: 2 MJD: 56552.000
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 16 7 7 16 7 13 15 15 15 4 | 56 51 50 52 55 50 56 53 55 49 52
2 | 13 15 7 10 16 4 17 15 12 20 4 | 26 21 21 25 27 17 20 24 25 18 21
3 | 8 15 5 12 13 5 13 17 11 13 4 | 22 21 21 29 21 19 23 26 27 20 22
4 | 20 17 8 8 22 6 16 12 8 24 5 | 43 47 38 41 47 38 49 42 45 45 41
5 | 11 14 6 10 15 6 17 15 11 14 4 | 20 19 14 20 28 12 18 24 20 12 16
6 | 8 15 4 9 10 4 10 14 10 14 3 | 23 20 23 27 23 19 24 24 23 20 22
7 | 10 20 6 11 13 5 18 14 12 13 4 | 26 25 16 22 28 13 23 19 22 12 18
8E | 13 21 8 10 16 8 19 25 19 24 5 | 96 112 100 103 103 100 107 107 101 104 102
9 | 5 15 5 8 9 5 11 16 12 22 3 | 21 26 17 20 20 15 24 22 25 26 19
10 | 9 14 5 7 15 3 12 11 9 22 3 | 22 22 16 20 23 16 19 17 19 22 17
11 | 9 16 6 7 20 4 12 12 14 12 4 | 24 24 21 25 34 16 26 19 29 17 21
12 | 8 20 8 13 17 5 20 18 12 17 5 | 24 22 16 24 29 13 21 25 25 15 18
13 | 6 15 5 9 14 4 14 10 11 20 3 | 29 34 24 29 36 24 31 21 26 20 26
14 | 14 17 8 10 11 5 14 13 12 20 4 | 32 30 28 27 33 25 29 29 29 23 27
15 | 8 18 4 11 11 4 22 14 15 17 4 | 30 28 25 30 31 22 28 27 31 23 26
16 | 11 20 5 14 15 3 19 22 16 19 5 | 21 23 18 27 26 17 24 21 25 18 19
17 | 10 17 6 8 13 5 16 18 15 38 4 | 29 27 26 32 30 21 28 28 26 29 25
18 | 9 18 6 12 16 3 17 18 14 17 4 | 23 26 20 23 28 18 24 24 25 15 20
19 | 11 20 6 11 12 5 15 16 11 21 4 | 22 28 22 29 27 20 28 21 28 18 23
20 | 6 19 6 8 14 4 20 10 10 18 4 | 26 25 26 25 30 19 25 21 24 15 23
21 | 9 19 6 7 17 4 11 20 17 13 4 | 40 36 37 40 40 32 37 31 43 27 37
22 | 9 19 5 11 13 4 15 16 10 16 4 | 24 30 24 30 33 24 29 29 25 21 25
23 | 7 18 5 11 13 5 17 11 9 23 4 | 26 27 20 25 26 17 27 19 20 17 21
24 | 11 15 5 9 9 7 14 12 10 16 3 | 21 22 18 18 25 14 26 19 26 20 19
25 | 11 15 5 11 14 5 13 16 14 15 4 | 22 24 17 17 27 13 26 22 25 16 18
26 | 10 12 4 6 12 4 13 10 11 20 3 | 26 22 22 25 28 21 21 23 27 26 22
X27 | 9 13 5 8 --- 6 13 17 13 17 4 | 28 25 26 29 --- 23 32 27 29 24 26
28 | 6 17 6 8 17 5 18 15 10 20 4 | 26 25 27 32 35 20 25 28 26 21 26
29 | 12 18 5 12 14 5 19 12 13 21 4 | 30 34 28 29 30 25 35 29 30 28 27
31 | 12 25 5 13 18 5 21 13 14 16 5 | 22 27 20 22 34 17 25 22 29 17 21
32 | 8 11 5 7 13 4 11 10 6 25 3 | 16 19 16 17 17 13 21 15 15 24 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 6 10 15 5 16 15 12 19 |T 28 29 25 29 32 23 30 27 29 24 26
WRMS | 10 17 6 10 14 5 15 14 11 21 |NE 24 25 21 25 28 18 25 23 25 19 21
MEDI | 9 17 5 10 14 5 15 15 12 18 |MD 26 25 22 27 28 19 26 24 26 20 22
Table 3.1758.3 GPS week: 1758 Day: 3 MJD: 56553.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 15 5 9 9 6 14 17 12 13 4 | 38 39 33 35 39 34 42 39 36 36 35
2 | 12 15 6 10 11 3 15 13 11 22 4 | 27 27 24 26 27 20 24 28 27 24 24
3 | 10 12 3 10 11 5 11 17 10 12 3 | 24 22 21 27 24 20 24 27 22 21 22
4 | 16 12 8 9 14 4 13 13 9 25 4 | 56 53 54 56 54 51 53 52 52 58 53
5 | 12 14 6 9 19 4 18 15 9 14 4 | 23 20 17 22 31 14 22 22 21 14 19
6 | 10 12 4 9 11 4 10 16 11 14 3 | 26 24 27 31 27 24 28 28 23 24 25
7 | 10 22 5 11 15 4 20 12 10 11 4 | 25 27 19 23 33 17 25 19 23 12 20
8E | 10 18 6 12 12 7 16 20 13 25 4 | 153 158 154 156 156 150 155 151 154 154 154
9 | 8 10 5 10 7 5 10 17 11 22 3 | 23 26 20 21 26 17 26 23 24 25 21
10 | 7 13 5 7 14 4 12 12 8 24 3 | 22 21 19 21 22 16 20 21 21 24 19
11 | 9 11 4 10 17 4 14 11 8 9 3 | 28 27 22 26 32 21 28 22 25 19 24
12 | 8 16 6 11 19 5 18 10 10 16 4 | 29 25 22 27 31 20 25 27 25 20 23
13 | 6 13 5 7 15 3 15 9 13 18 3 | 29 35 27 34 37 25 33 23 31 20 29
14 | 11 16 5 11 12 4 16 12 10 19 4 | 29 32 31 35 34 29 32 36 37 27 32
15 | 10 16 6 10 11 4 18 15 14 17 4 | 30 28 30 35 35 25 27 32 26 27 29
16 | 15 22 5 12 17 4 18 19 9 19 5 | 23 26 22 30 28 19 25 26 21 19 21
17 | 17 19 7 11 13 6 20 18 14 40 5 | 32 32 28 35 35 27 34 36 30 36 29
18 | 13 17 6 14 15 4 17 16 8 17 4 | 21 26 23 29 31 21 27 31 25 17 23
19 | 12 19 5 12 10 4 19 17 9 20 4 | 27 30 24 31 29 23 30 27 23 23 25
20 | 7 17 5 6 14 3 19 10 7 17 4 | 26 25 22 25 32 19 26 22 25 16 22
21 | 8 20 5 9 16 3 8 14 13 14 4 | 37 36 33 38 41 31 37 34 36 26 35
22 | 12 17 5 12 16 3 17 14 8 16 4 | 24 30 27 37 37 26 31 34 28 22 28
23 | 7 14 4 7 14 3 15 10 11 22 3 | 25 27 22 26 27 19 27 21 26 19 23
24 | 11 14 4 9 9 5 12 10 10 14 3 | 27 25 18 20 26 17 26 20 22 18 21
25 | 7 19 5 8 12 5 12 9 9 14 3 | 25 33 20 22 29 18 29 23 23 20 23
26 | 9 11 5 9 12 5 11 8 19 17 4 | 27 28 26 31 30 25 26 25 26 25 26
X27 | 12 13 5 9 --- 3 15 20 10 15 4 | 32 31 29 32 --- 28 38 33 30 28 30
28 | 8 17 4 11 15 3 18 13 9 18 4 | 28 26 27 34 38 24 26 33 29 26 28
29 | 11 18 5 14 13 7 15 10 10 20 4 | 34 37 30 33 31 32 37 33 35 31 31
31 | 10 23 4 12 18 4 19 14 8 16 4 | 22 26 16 23 34 15 23 22 23 16 19
32 | 9 9 4 8 11 5 13 12 6 25 3 | 20 20 17 22 22 16 21 18 20 24 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 5 10 14 4 15 14 11 19 |T 32 32 29 33 35 27 33 31 31 28 30
WRMS | 11 16 5 9 13 4 15 13 9 23 |NE 26 27 23 28 30 21 27 26 25 22 24
MEDI | 10 16 5 10 13 4 15 13 10 17 |MD 27 27 24 30 31 21 27 27 25 24 24
Table 3.1758.4 GPS week: 1758 Day: 4 MJD: 56554.000
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 14 6 9 11 6 13 16 11 10 4 | 37 37 34 37 41 32 38 34 40 32 36
2 | 13 13 6 8 14 4 13 10 9 19 4 | 27 21 21 26 27 16 22 23 28 12 23
3 | 12 10 5 10 9 5 11 23 10 13 4 | 18 18 18 23 21 17 21 25 29 17 20
4 | 9 12 7 13 10 5 12 14 10 26 4 | 52 48 42 49 44 43 47 40 49 52 45
5 | 9 12 6 9 16 5 16 13 11 14 4 | 25 23 19 23 30 15 25 19 28 15 22
6 | 12 10 5 8 11 4 8 18 12 15 4 | 20 22 22 26 25 20 24 24 31 20 23
7 | 12 21 7 10 13 6 17 16 8 14 4 | 33 32 23 29 37 22 27 26 29 20 26
8E | 10 19 5 7 12 6 15 16 8 24 4 | 122 122 117 116 121 115 121 117 117 122 118
9 | 8 11 4 8 8 4 10 15 6 20 3 | 22 25 16 19 21 15 24 19 23 25 19
10 | 7 11 6 8 12 4 11 15 11 24 3 | 21 22 18 20 18 17 19 19 27 24 19
11 | 8 11 6 7 16 4 11 14 9 7 3 | 26 26 26 27 36 22 29 23 34 21 27
12 | 11 15 7 10 18 5 17 12 14 21 4 | 27 25 23 27 34 22 24 29 31 23 25
13 | 8 12 5 8 11 4 13 10 8 18 3 | 32 34 27 30 38 25 33 25 29 19 29
14 | 11 14 7 12 14 4 16 10 10 22 4 | 31 31 29 32 32 26 30 30 30 21 29
15 | 10 17 7 10 13 5 17 13 13 18 4 | 27 30 29 34 33 25 27 28 33 23 28
16 | 12 17 5 12 14 3 16 19 15 21 5 | 25 24 19 25 26 20 24 24 33 17 22
17 | 10 17 7 11 12 5 18 15 11 39 4 | 35 31 31 36 34 27 33 34 31 31 31
18 | 12 18 8 13 19 4 17 14 10 15 5 | 18 23 18 24 31 17 24 23 22 12 19
19 | 12 18 8 12 10 3 16 18 9 22 4 | 25 29 27 29 30 23 30 26 34 22 27
20 | 8 14 8 7 13 4 16 10 16 16 4 | 26 24 18 25 31 19 24 20 29 12 22
21 | 13 24 13 12 49 4 14 13 14 15 7 | 31 32 31 34 53 28 34 31 32 22 30
22 | 11 16 7 12 16 5 16 15 9 15 4 | 21 28 19 29 35 20 26 24 27 14 23
23 | 6 14 6 9 12 3 14 10 9 23 3 | 24 26 20 23 26 18 25 20 26 18 22
24 | 11 14 5 10 11 4 13 10 16 14 4 | 24 23 19 21 28 16 24 20 29 17 21
25 | 11 16 7 8 15 5 12 12 15 15 4 | 24 30 23 22 32 19 30 24 31 20 25
26 | 6 12 5 8 11 3 10 10 11 20 3 | 25 23 23 29 26 22 21 19 30 21 24
X27 | 9 10 5 7 --- 3 12 27 10 17 4 | 29 28 27 28 --- 25 34 30 39 23 29
28 | 7 14 4 7 15 2 15 13 7 18 3 | 25 24 23 30 37 21 26 30 27 23 26
29 | 10 15 8 11 14 9 16 11 10 23 4 | 29 29 27 30 30 27 32 30 31 28 28
31 | 10 20 8 11 19 4 20 15 8 18 5 | 24 30 20 25 37 18 27 24 31 19 23
32 | 11 9 6 8 14 5 11 16 13 24 4 | 16 17 14 18 20 14 20 16 26 24 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 7 10 16 5 14 14 11 20 |T 29 30 26 30 34 24 30 28 33 24 28
WRMS | 10 15 7 9 13 5 14 14 9 22 |NE 25 26 22 26 29 20 26 24 29 20 24
MEDI | 10 14 6 9 13 4 14 14 10 18 |MD 25 26 23 27 31 21 26 24 30 21 25
Table 3.1758.5 GPS week: 1758 Day: 5 MJD: 56555.000
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 14 6 10 12 6 13 19 9 12 4 | 34 33 31 35 38 29 33 32 35 32 32
2 | 11 15 5 9 14 4 16 10 9 19 4 | 25 18 18 23 25 15 20 20 24 14 20
3 | 8 13 5 9 9 4 12 24 8 13 4 | 21 20 20 20 18 18 19 26 22 18 19
4 | 7 15 9 9 10 5 10 14 12 28 4 | 39 40 37 37 37 34 37 33 34 43 36
5 | 17 15 8 10 16 5 21 14 15 15 5 | 28 19 12 18 27 11 21 19 19 14 16
6 | 8 13 6 7 11 4 9 16 9 14 3 | 22 22 21 21 22 18 22 20 22 17 19
7 | 8 19 4 9 13 5 18 10 7 11 4 | 27 29 23 27 34 22 26 25 27 21 24
8 | 6 19 6 9 16 5 15 12 10 24 4 | 178 180 174 175 179 173 177 174 177 175 176
9 | 7 12 5 8 10 4 10 11 9 20 3 | 20 26 18 20 21 15 22 18 21 24 18
10 | 6 14 6 8 12 5 12 13 9 22 3 | 16 17 13 16 15 11 14 19 18 20 13
11 | 8 12 5 8 19 4 13 12 13 9 4 | 22 22 15 22 33 14 23 17 22 15 18
12 | 10 15 6 10 19 5 17 16 10 21 4 | 25 21 17 23 31 17 21 26 24 20 20
13 | 7 15 5 10 13 3 15 8 11 19 3 | 28 30 24 28 32 22 30 22 21 19 24
14 | 7 14 4 11 16 6 14 14 7 23 4 | 23 29 23 27 28 20 28 29 28 18 24
15 | 6 17 7 10 15 5 17 16 10 19 4 | 24 25 21 26 28 18 24 24 21 18 21
16 | 8 17 6 12 13 3 17 15 9 24 4 | 21 21 16 23 24 15 22 19 21 14 18
17 | 9 18 9 9 10 3 17 15 10 40 4 | 30 28 27 31 29 22 28 27 25 31 26
18 | 9 15 6 12 18 4 15 16 7 14 4 | 18 22 17 22 26 15 22 22 21 11 18
19 | 9 18 6 9 11 3 16 19 11 22 4 | 24 27 22 25 25 21 28 24 25 19 22
20 | 11 16 5 11 12 4 21 10 8 18 4 | 25 21 19 23 27 17 21 20 20 15 19
21 | 9 12 5 8 33 3 12 11 9 11 4 | 36 33 33 35 44 28 33 32 34 22 33
22 | 9 14 4 11 16 3 12 14 7 14 4 | 20 25 20 27 30 19 25 23 23 16 20
23 | 7 17 5 12 11 4 16 9 9 24 4 | 25 26 20 25 23 17 26 18 23 18 21
24 | 10 14 6 8 11 5 12 10 10 12 3 | 21 21 16 18 24 12 21 18 20 16 17
25 | 13 16 6 10 11 6 11 14 13 16 4 | 22 27 20 16 27 14 25 20 20 17 19
26 | 10 11 6 7 14 4 11 10 12 18 3 | 21 19 19 22 21 17 17 17 19 21 17
X27 | 11 14 8 8 --- 4 15 20 13 16 5 | 29 25 24 24 --- 19 31 23 25 19 24
28 | 7 17 6 10 16 3 18 13 11 18 4 | 21 21 21 28 32 17 22 25 22 19 21
29 | 12 17 7 12 11 4 19 13 11 27 4 | 24 29 24 26 26 21 31 24 28 24 24
X30 | 2 --- --- --- --- 46 --- --- --- --- 0 | 1 --- --- --- --- 1 --- --- --- --- 1
31 | 7 20 6 15 20 6 22 18 10 15 5 | 18 24 17 24 36 15 25 24 25 15 19
32 | 8 12 5 9 9 7 13 16 10 25 3 | 16 14 12 17 15 12 16 18 16 21 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 6 10 15 5 15 14 10 20 |T 28 29 25 29 32 22 29 27 28 24 25
WRMS | 9 15 6 9 14 5 14 14 9 19 |NE 21 23 19 23 26 16 23 21 22 18 19
MEDI | 8 15 6 9 13 4 15 14 10 18 |MD 23 25 20 24 27 17 24 23 22 19 20
Table 3.1758.6 GPS week: 1758 Day: 6 MJD: 56556.000
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 14 6 7 9 7 12 14 7 13 3 | 36 35 33 36 39 32 38 36 33 34 34
2 | 10 14 6 8 15 4 12 11 11 21 4 | 24 18 20 23 25 16 19 23 24 20 20
3 | 9 12 4 13 11 4 10 19 8 15 3 | 21 19 24 30 25 21 24 25 23 18 22
4 | 15 15 5 8 13 4 9 13 9 30 4 | 62 59 55 58 53 55 55 53 56 65 56
5 | 9 15 7 11 18 3 17 12 11 13 4 | 21 22 14 22 30 14 20 20 22 15 17
6 | 11 13 4 11 14 3 9 12 9 16 3 | 27 22 30 33 32 26 28 25 26 23 27
7 | 9 24 5 8 14 4 17 12 9 12 4 | 25 27 20 24 31 17 23 20 23 18 20
8 | 7 15 4 9 19 7 14 13 8 24 4 | 156 162 156 155 151 154 155 155 153 157 156
9 | 5 10 4 9 12 4 10 11 9 21 3 | 19 23 17 20 20 14 21 17 20 25 17
10 | 7 12 4 8 14 4 8 13 7 22 3 | 17 20 14 17 18 12 16 19 15 21 14
11 | 9 12 4 8 15 4 12 13 9 12 3 | 31 30 28 32 38 25 34 26 30 23 29
12 | 10 20 5 12 16 6 18 13 10 24 4 | 30 22 21 29 34 20 22 25 25 17 22
13 | 6 15 5 8 13 3 12 9 8 22 3 | 33 35 31 35 39 30 34 27 32 24 32
14 | 12 15 5 12 11 5 14 15 8 23 4 | 30 33 34 38 35 30 32 38 35 26 33
15 | 10 16 5 16 12 3 16 14 12 19 4 | 32 29 27 41 37 27 30 34 29 30 30
16 | 11 22 5 15 13 5 17 16 12 24 5 | 19 24 19 25 25 17 21 18 25 15 18
17 | 16 18 5 9 12 5 16 15 12 39 4 | 31 30 30 36 36 26 32 36 31 37 30
18 | 11 19 5 13 13 4 13 14 8 15 4 | 19 24 18 23 27 15 21 23 22 15 19
19 | 10 18 6 14 10 3 15 18 8 24 4 | 29 30 31 36 32 27 32 30 28 24 29
20 | 9 14 5 9 12 4 15 11 13 16 4 | 22 22 20 24 26 15 20 21 20 13 19
21 | 9 14 6 6 36 6 11 10 8 12 4 | 36 32 31 36 50 29 35 31 35 26 33
22 | 10 19 4 10 14 3 12 15 9 15 4 | 18 26 21 28 32 19 24 24 27 15 22
23 | 8 18 6 12 12 4 16 10 11 27 4 | 27 28 25 29 27 21 27 22 25 23 24
24 | 9 15 4 10 10 5 15 10 10 15 3 | 21 21 17 17 24 13 24 19 19 14 18
25 | 14 17 5 8 12 5 11 15 10 15 4 | 26 28 21 19 29 16 25 18 21 15 20
26 | 11 12 4 13 12 4 10 13 11 18 3 | 25 26 25 33 31 26 24 27 32 27 27
X27 | 8 13 5 12 --- 4 15 18 10 21 4 | 37 31 36 37 --- 31 41 29 34 27 34
28 | 6 18 4 11 16 3 15 13 7 20 4 | 23 23 25 35 37 22 25 31 24 26 25
29 | 12 18 5 9 10 6 16 15 8 27 4 | 36 37 33 34 34 31 37 31 32 35 32
X30 | 4 --- --- --- --- 39 --- --- --- --- 0 | 1 --- --- --- --- 1 --- --- --- --- 1
31 | 11 18 5 13 18 6 18 20 11 16 5 | 23 24 18 23 36 17 25 29 30 18 21
32 | 9 11 6 11 12 5 10 17 11 25 4 | 17 20 15 16 14 11 18 20 15 25 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 5 11 15 5 14 14 10 21 |T 30 31 29 33 35 25 31 30 31 28 28
WRMS | 10 16 5 10 13 5 14 13 9 19 |NE 24 26 23 28 29 20 26 25 25 21 22
MEDI | 9 15 5 10 13 4 14 13 9 20 |MD 25 26 25 30 32 21 25 25 26 23 22
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 4.1758 GPS week: 1758 MJD: 56550.0-56556.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3005 |U 6 7 17 |U 7 9 22 |U 8 10 22 |
emr | emr 2974 | 8 8 19 |U 7 8 27 | 9 10 25 |
esa | esa 2976 | 6 8 17 |U 6 9 24 | 8 9 22 |
gfz | gfz 2971 |U 6 8 17 |U 7 9 23 |U 9 9 24 |
grg | grg 2880 |U 35 30 69 |U 16 15 49 | 27 22 68 |
igr | igr 2975 | 6 8 16 | 6 9 23 | 8 9 22 |
igs | igs 2976 | 6 7 17 | 6 9 23 | 8 9 23 |
jpl | jpl 2973 | 7 8 18 |U 7 8 24 |U 9 10 23 |
mit | mit 2976 | 9 9 26 |U 7 10 25 |U 12 14 38 |
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 5.1758.0 GPS week: 1758 Day: 0 MJD: 56550.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 6 9 23 | ---- ---- ---- | 9 14 26 |
emr | emr 2970 | 8 8 22 | ---- ---- ---- | 10 14 28 |
esa | esa 2976 | 6 9 24 | ---- ---- ---- | 8 12 27 |
gfz | gfz 2968 | 6 9 22 | ---- ---- ---- | 12 11 41 |
grg | grg 2880 | 88 53 97 | ---- ---- ---- | 61 47 139 |
igr | igr 2975 | 6 9 22 | ---- ---- ---- | 9 12 26 |
igs | igs 2976 | 6 8 23 | ---- ---- ---- | 8 12 27 |
jpl | jpl 2969 | 7 11 28 | ---- ---- ---- | 9 13 29 |
mit | mit 2976 | 6 9 24 | ---- ---- ---- | 9 11 30 |
Table 5.1758.1 GPS week: 1758 Day: 1 MJD: 56551.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3014 | ---- ---- ---- | 6 9 18 | 10 12 20 |
emr | emr 2972 | ---- ---- ---- | 6 8 26 | 12 11 22 |
esa | esa 2976 | ---- ---- ---- | 5 8 22 | 11 10 20 |
gfz | gfz 2968 | ---- ---- ---- | 5 9 19 | 11 11 20 |
grg | grg 2880 | ---- ---- ---- | 8 12 23 | 14 14 29 |
igr | igr 2976 | ---- ---- ---- | 5 9 21 | 11 10 20 |
igs | igs 2976 | ---- ---- ---- | 5 8 20 | 11 10 20 |
jpl | jpl 2972 | ---- ---- ---- | 6 9 24 | 11 10 20 |
mit | mit 2976 | ---- ---- ---- | 6 10 24 | 11 13 24 |
Table 5.1758.2 GPS week: 1758 Day: 2 MJD: 56552.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 4 11 | 6 9 20 | 9 8 18 |
emr | emr 2972 | 10 5 12 | 8 7 24 | 10 8 22 |
esa | esa 2976 | 7 4 11 | 6 8 22 | 10 9 19 |
gfz | gfz 2972 | 6 4 9 | 6 8 22 | 10 8 18 |
grg | grg 2880 | 7 7 27 | 7 11 24 | 12 10 21 |
igr | igr 2976 | 5 3 7 | 6 8 19 | 10 8 19 |
igs | igs 2976 | 7 3 9 | 6 8 20 | 10 8 19 |
jpl | jpl 2972 | 10 5 8 | 7 8 19 | 11 10 18 |
mit | mit 2976 | 7 3 8 | 6 8 22 | 10 9 22 |
Table 5.1758.3 GPS week: 1758 Day: 3 MJD: 56553.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 12 17 | 8 11 30 | 6 9 18 |
emr | emr 2976 | 8 12 20 | 8 10 37 | 8 11 22 |
esa | esa 2976 | 6 15 15 | 8 11 33 | 7 10 19 |
gfz | gfz 2972 | 7 17 16 | 8 10 30 | 7 10 19 |
grg | grg 2880 | 8 16 18 | 10 11 36 | 8 11 24 |
igr | igr 2976 | 7 14 15 | 8 10 30 | 6 9 18 |
igs | igs 2976 | 7 12 16 | 8 10 32 | 6 9 19 |
jpl | jpl 2976 | 7 8 17 | 11 8 34 | 8 10 19 |
mit | mit 2976 | 7 6 18 | 9 12 28 | 9 11 20 |
Table 5.1758.4 GPS week: 1758 Day: 4 MJD: 56554.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 21 | 7 8 16 | 8 8 19 |
emr | emr 2976 | 7 8 24 | 7 8 24 | 9 7 25 |
esa | esa 2976 | 6 6 23 | 6 8 17 | 8 8 19 |
gfz | gfz 2972 | 6 5 22 | 6 9 18 | 8 8 19 |
grg | grg 2880 | 6 8 23 | 8 8 23 | 11 8 22 |
igr | igr 2976 | 6 6 22 | 6 8 17 | 8 8 19 |
igs | igs 2976 | 6 6 22 | 6 8 17 | 8 7 20 |
jpl | jpl 2975 | 6 6 21 | 6 9 18 | 9 8 21 |
mit | mit 2976 | 23 21 78 | 9 11 20 | 20 21 44 |
Table 5.1758.5 GPS week: 1758 Day: 5 MJD: 56555.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 7 4 16 | 5 11 22 | 8 7 27 |
emr | emr 2976 | 6 6 21 | 6 8 26 | 9 6 30 |
esa | esa 2976 | 6 4 19 | 6 10 23 | 7 7 27 |
gfz | gfz 2972 | 6 5 19 | 6 10 23 | 8 6 28 |
grg | grg 2880 | 45 48 122 | 30 21 96 | 43 34 138 |
igr | igr 2976 | 6 4 18 | 6 10 23 | 7 6 27 |
igs | igs 2976 | 6 4 19 | 5 10 23 | 7 6 28 |
jpl | jpl 2976 | 5 7 20 | 5 9 25 | 8 6 28 |
mit | mit 2976 | 6 5 18 | 6 13 26 | 15 22 90 |
Table 5.1758.6 GPS week: 1758 Day: 6 MJD: 56556.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3038 | 6 8 13 | 7 8 27 | 8 13 26 |
emr | emr 2976 | 8 11 14 | 9 10 27 | 9 10 28 |
esa | esa 2976 | 7 10 13 | 7 9 29 | 8 11 24 |
gfz | gfz 2976 | 7 10 12 | 8 9 30 | 8 11 25 |
grg | grg 2880 | 58 45 130 | 36 27 93 | 42 30 101 |
igr | igr 2976 | 7 10 13 | 7 8 26 | 8 11 24 |
igs | igs 2976 | 6 10 12 | 7 9 27 | 8 11 25 |
jpl | jpl 2976 | 8 10 14 | 7 8 25 | 9 11 27 |
mit | mit 2976 | 7 10 13 | 8 9 31 | 9 13 34 |
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 6.1758 GPS week: 1758 MJD: 56550.500-56556.500
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 | -45 -4 66 40 -3 | 22 26
| 21 21 83 102 3 | 2
emr uuxuu | 19 -41 378 154 -16 | 54 57
| 13 16 165 45 12 | 6
esa uuuuu | -30 8 -38 -108 -3 | 17 22
| 15 13 30 51 6 | 1
gfz uuuuu | -3 -16 56 -65 6 | -2 16
| 19 15 67 131 4 | 4
grg uuuux | 37 -15 52 171 19 | -7 17
| 25 21 32 57 25 | 4
igr xxxxx | 0 9 -76 55 -2 | -4 15
| 14 16 29 50 3 | 2
irf xxxxx | -3 -7 -30 -52 0 | -1 15
| 7 12 28 45 4 | 2
jpl uuuuu | 5 0 105 262 -11 | 40 43
| 30 29 80 112 8 | 4
mit uuuuu | -38 2 -83 -203 -2 | 12 19
| 20 23 68 110 10 | 2
ngs uuuuu | 107 37 -78 12 -1 | 9 16
| 62 56 134 185 6 | 2
sio xxxxx | -84 -25 -126 46 -4 | 34 37
| 45 24 50 94 4 | 2
Table 7.1758.0 GPS week: 1758 Day: 0 MJD: 56550.500
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 | -28 30 170 13 1 | 22 25
emr uuxuu | 29 -61 667 69 -8 | 62 66
esa uuuuu | -20 15 0 -90 4 | 17 21
gfz uuuuu | 25 9 150 -103 10 | -5 14
grg uuuux | 8 -44 18 160 26 | -11 16
igr xxxxx | 18 8 -110 123 -3 | -2 15
irf xxxxx | -1 14 -39 -67 -5 | -1 13
jpl uuuuu | -11 45 173 65 -17 | 47 50
mit uuuuu | -21 45 -167 -231 -13 | 15 20
ngs uuuuu | 57 -66 -316 261 -4 | 9 14
sio xxxxx | -125 17 -203 37 -3 | 37 40
Table 7.1758.1 GPS week: 1758 Day: 1 MJD: 56551.500
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 | -21 11 -6 -66 0 | 20 24
emr uuxuu | 36 -63 512 211 -15 | 58 61
esa uuuuu | -29 2 -34 -24 3 | 15 20
gfz uuuuu | 10 -23 103 135 12 | -7 14
grg uuuux | 7 -40 93 97 -1 | -12 15
igr xxxxx | -13 35 -68 67 -3 | -5 16
irf xxxxx | -9 -2 -56 -10 -1 | -3 14
jpl uuuuu | -35 15 149 302 -17 | 43 46
mit uuuuu | -38 11 -146 -122 -9 | 12 19
ngs uuuuu | 87 40 -66 -269 -5 | 6 13
sio xxxxx | -133 -17 -135 131 -5 | 34 38
Table 7.1758.2 GPS week: 1758 Day: 2 MJD: 56552.500
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 | -78 -9 25 -84 -3 | 20 23
emr uuxuu | 18 -34 354 183 -17 | 55 58
esa uuuuu | -49 -1 -36 -162 -5 | 16 20
gfz uuuuu | -2 -19 70 111 5 | -5 15
grg uuuux | 55 7 71 229 -9 | -11 15
igr xxxxx | 17 1 -113 5 -7 | -6 16
irf xxxxx | -9 -5 7 -5 -3 | -4 14
jpl uuuuu | 26 4 48 429 -9 | 39 42
mit uuuuu | -58 -8 28 -160 -11 | 10 18
ngs uuuuu | 209 62 -144 -119 6 | 6 12
sio xxxxx | -111 -54 -43 81 -11 | 32 35
Table 7.1758.3 GPS week: 1758 Day: 3 MJD: 56553.500
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 | -43 -2 97 67 -1 | 22 26
emr uuxuu | 25 -40 275 149 -17 | 56 59
esa uuuuu | -24 -5 -69 -105 -4 | 17 22
gfz uuuuu | -1 -23 -7 -143 2 | -3 17
grg uuuux | 54 5 19 114 2 | -9 14
igr xxxxx | 5 5 -55 -23 -4 | -5 16
irf xxxxx | 8 -17 -40 -69 2 | -2 15
jpl uuuuu | 20 -16 62 249 -21 | 40 43
mit uuuuu | -8 -22 -81 -175 0 | 11 18
ngs uuuuu | 38 82 77 107 4 | 8 16
sio xxxxx | -70 -27 -105 78 -5 | 32 35
Table 7.1758.4 GPS week: 1758 Day: 4 MJD: 56554.500
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 | -69 -40 -39 11 -3 | 24 29
emr uuxuu | 7 -39 180 173 -29 | 54 57
esa uuuuu | -15 33 -1 -120 -1 | 19 24
gfz uuuuu | -33 -38 -23 -181 2 | 1 18
grg uuuux | 21 -21 36 237 56 | -7 16
igr xxxxx | -5 -11 -55 53 2 | -3 17
irf xxxxx | 3 -18 -60 -8 0 | 1 17
jpl uuuuu | 54 -41 96 325 -6 | 40 42
mit uuuuu | -26 -21 -126 -60 1 | 13 21
ngs uuuuu | 102 104 66 -50 4 | 10 20
sio xxxxx | -33 -24 -162 154 -6 | 34 37
Table 7.1758.5 GPS week: 1758 Day: 5 MJD: 56555.500
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 | -45 -7 43 153 -8 | 24 29
emr uuxuu | -1 -16 271 133 -30 | 51 55
esa uuuuu | -53 4 -73 -174 -10 | 19 24
gfz uuuuu | -1 -6 -2 -158 8 | 2 17
grg uuuux | 46 -2 91 142 13 | -2 20
igr xxxxx | -20 -2 -40 63 0 | -2 15
irf xxxxx | -1 -20 -34 -101 5 | 1 17
jpl uuuuu | -8 20 218 215 -7 | 38 41
mit uuuuu | -61 1 -59 -284 8 | 13 21
ngs uuuuu | 172 2 -59 193 -2 | 11 19
sio xxxxx | -95 -52 -101 -72 0 | 34 37
Table 7.1758.6 GPS week: 1758 Day: 6 MJD: 56556.500
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 -11 170 186 -3 | 22 25
emr uuxuu | 16 -34 389 162 6 | 44 47
esa uuuuu | -19 8 -57 -78 -9 | 16 21
gfz uuuuu | -18 -13 101 -115 4 | 2 16
grg uuuux | 70 -11 36 216 46 | -1 20
igr xxxxx | -3 26 -89 96 0 | -4 13
irf xxxxx | -9 -2 10 -107 6 | 0 15
jpl uuuuu | -14 -25 -12 247 2 | 35 36
mit uuuuu | -52 10 -33 -392 13 | 11 19
ngs uuuuu | 82 37 -107 -39 -9 | 10 18
sio xxxxx | -18 -16 -132 -87 0 | 32 34
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