[IGSREPORT-22034] Wk 1750 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Aug 9 05:24:43 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1750 (Jul 21, 2013 - Jul 27, 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:
igs1750[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1750[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1750[0-6].cls IGS GPS clock combination summary report.
igs17507.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17507.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 6 KOUC MOBS TSKB USNO JOZ2 KOUC MOBS REYK TLSE TSKB
0 | COD | USNO
0 | EMR | 3 HERS HERS
0 | ESA | 6 IRKJ KOUC KOUR NTUS IRKJ KOUC KOUR NTUS UNSA
0 | GFZ | 6 6 THTI
0 | GRG | 3 PDEL TLSE IRKT PDEL TLSE
0 | JPL | 3
0 | MIT | 8 9 19 26 3 8 9 19 26 NICO NTUS NYAL USNO CRO1 NICO
0 | MIT | NTUS NYAL USNO
1 | COD | 6 KOUC XMIS KOUC XMIS
1 | EMR | 3 HERS
1 | ESA | 6 KOUC KOUC
1 | GFZ | 6 6 IRKT DRAG IRKT
1 | GRG | 3
1 | JPL | 3
1 | MIT | 7 26 3 7 26 NICO NTUS NICO NTUS
2 | COD | KOUC HERT JOZ2 KOUC MOBS TSKB
2 | EMR | 3 6 TLSE YAKT
2 | ESA | KOUC WES2 KOUC WES2
2 | GFZ | 6 KERG
2 | GRG | 3 6 IRKT NICO POL2 POLV USNO IRKT NICO POL2 POLV
2 | GRG | REYK USNO
2 | MIT | 18 22 26 3 6 9 15 18 22 24 26 CONZ NICO NTUS REYK
2 | MIT | CONZ NICO NTUS REYK USNO
3 | COD | KOUC MAR6 MOBS FLRS JOZ2 KOUC MOBS
3 | EMR | 6 HARB HARB
3 | ESA | 6 KOUC KOUC LPGS
3 | GFZ | TSKB
3 | GRG | 6 DGAR HARB IRKJ NTUS USNO DGAR HARB IRKJ NTUS USNO
3 | JPL | AUCK
3 | MIT | 6 NTUS GOPE MDVJ NTUS
4 | COD | KOUC FLRS KOUC
4 | EMR | 6
4 | ESA | CAGZ CHTI KOUC CAGZ CHTI KOUC
4 | GFZ | NRMD CHTI HARB NRMD
4 | GRG | 6 DGAR HARB LPGS WES2 DGAR HARB LPGS WES2
4 | JPL | BOGT GUAO
4 | MIT | 6 8 15 6 8 15 NICO MDVJ NICO TSKB
5 | COD | KOUC WES2 JOZ2 KOUC WES2
5 | EMR | 9 6 9
5 | ESA | KOUC MATE KOUC MATE
5 | GFZ | CHTI IISC MATE SUWN AUCK CHTI MATE SUWN
5 | GRG | 6 IRKT NKLG ADIS IRKT NKLG
5 | JPL | 6 9
5 | MIT | 9 11 18 28 6 7 9 11 18 28 MIZU MIZU NICO
6 | COD | KOUC KOUC
6 | EMR | 9 HARB WHIT
6 | ESA | IRKJ
6 | GRG | 9 CAGZ IRKJ WHIT ADIS CAGZ WHIT
6 | JPL | 9 18
6 | MIT | 7 7 9 28 MDVJ GOPE MDVJ NICO SPT0 TLSE WSRT
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
----+--------+--------+-------------
3 | COD | ~03:30 | ~ 0.14 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G12 | 2013_07_24 | 2013042
G12 | 2013_07_25 | 2013042
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G03 | 4 | 4 | | | | | |
PRN G06 | 4 | | | | | | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.1 -.1 .2 -50 33 -26 .25
EMR | 0 | -2.3 6.4 -.9 -17 -17 -11 .09
ESA | 0 | 1.4 -6.4 8.0 22 -30 -29 -.02
GFZ | 0 | -.1 .1 .3 -26 -18 -9 -.43
GRG | 0 | 7.4 -7.1 5.4 -34 24 -23 .12
JPL | 0 | -2.8 -.7 .7 -28 42 27 -.10
MIT | 0 | 1.4 -4.8 8.1 -11 6 -44 .11
NGS | 0 | 3.2 -2.8 3.4 -27 -6 21 .48
SIO | 0 | 1.4 1.4 -19.4 0 -125 19 -.15
COD | 1 | -.2 -1.1 .0 -49 40 -45 .28
EMR | 1 | -5.6 1.6 -8.6 -25 -5 -26 .10
ESA | 1 | -4.6 -10.2 12.3 11 -5 -71 -.02
GFZ | 1 | .1 .1 .7 -27 -29 -7 -.58
GRG | 1 | 4.0 -12.3 6.5 -58 18 -21 .23
JPL | 1 | -10.3 2.0 2.4 -49 28 -41 -.05
MIT | 1 | -3.0 -10.5 13.7 -5 13 -45 .15
NGS | 1 | -4.5 -5.2 11.0 -74 25 -31 .33
SIO | 1 | -4.0 -2.0 -15.3 -1 -78 164 -.01
COD | 2 | .0 -.2 .3 -42 43 -42 .13
EMR | 2 | -10.3 -3.7 -4.0 -7 2 -19 .14
ESA | 2 | -5.9 -6.4 18.1 63 -38 -52 .07
GFZ | 2 | -.2 .0 .4 -18 -25 -25 -.60
GRG | 2 | -.7 -5.6 3.6 -21 30 -21 .10
JPL | 2 | -6.5 -.3 1.4 -45 29 9 -.06
MIT | 2 | -5.8 -2.5 11.0 -3 13 -43 .16
NGS | 2 | -5.1 -2.0 10.9 -58 17 -29 .36
SIO | 2 | -4.8 -4.0 -32.7 -30 -135 -14 -.08
COD | 3 | -.4 .3 .0 -49 49 -37 .18
EMR | 3 | -5.2 -2.4 -4.7 -1 -12 -3 .21
ESA | 3 | -.2 -5.2 11.3 50 -32 -52 .13
GFZ | 3 | .1 .5 .3 -21 -33 -11 -.70
GRG | 3 | .1 -2.8 5.0 -37 2 -5 .30
JPL | 3 | .1 4.0 2.2 -73 44 22 .07
MIT | 3 | 3.3 -3.0 11.0 -4 0 -40 .14
NGS | 3 | -3.9 -5.7 9.6 -77 23 -37 .47
SIO | 3 | -.2 3.4 -24.4 7 -115 -31 -.16
COD | 4 | .2 -.5 -.8 -41 57 -27 .41
EMR | 4 | .9 -6.4 -6.6 -4 7 -28 .31
ESA | 4 | .9 -8.3 16.7 46 -38 -37 .30
GFZ | 4 | .4 -.1 .5 -30 -18 -23 -.48
GRG | 4 | 3.3 -12.4 11.6 -50 21 -36 .20
JPL | 4 | 5.0 3.1 8.9 -43 -11 8 -.14
MIT | 4 | 4.2 -2.3 11.9 -4 -2 -36 .27
NGS | 4 | .9 -1.8 3.9 -25 0 6 .34
SIO | 4 | 2.5 -.2 -23.6 33 -151 -20 -.0
COD | 5 | .4 -.5 -.4 -35 28 -21 .35
EMR | 5 | 3.6 -5.3 -6.4 -21 11 -38 .08
ESA | 5 | 4.4 -11.0 17.4 30 -22 -36 -.04
GFZ | 5 | .4 .0 -.1 -11 -30 -23 -.21
GRG | 5 | 9.7 -15.0 16.8 -15 23 -45 .22
JPL | 5 | 4.2 -2.3 6.3 -73 -12 -45 -.01
MIT | 5 | 7.2 -4.3 13.8 -8 9 -48 .20
NGS | 5 | .8 -3.1 12.4 -66 -2 3 .40
SIO | 5 | 2.9 -4.5 -40.7 -100 -180 -77 .08
COD | 6 | .6 .2 -.1 -39 -2 -22 .07
EMR | 6 | -7.7 -1.5 -4.8 -21 1 -32 -.14
ESA | 6 | -6.1 -3.8 18.9 21 -56 -13 -.19
GFZ | 6 | .0 .1 .3 -30 -37 -20 -.65
GRG | 6 | -2.7 -4.5 24.2 -35 44 -35 -.04
JPL | 6 | -6.3 .6 4.7 -46 6 -36 -.05
MIT | 6 | 2.8 -1.4 13.0 -6 12 -56 .03
NGS | 6 | -1.2 -7.1 13.0 -102 10 -18 .19
SIO | 6 | -6.2 2.0 -31.5 -29 -73 -39 -.12
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1750.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1750.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 2.1750.[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 3.1750.[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 5.1750.0-6). 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 1750 summary. (Jul 21, 2013 - Jul 27, 2013)
Table 1.1750.a GPS week: 1750 MJD: 56494.000-56500.000
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 263| 0 0 0 17 4 8 .16 10 9 | -1374 291 19 92
| 0 0 0 26 28 14 .03 | 255 345
emr 80| -2 -2 -9 -1 -20 18 .20 15 15 | 2736 765 16 116
| 1 1 2 19 19 10 .03 | 652 556
esa 150| 1 0 2 -2 -16 -22 -.04 6 5 | -1079 1247 13 112
| 0 0 0 13 11 13 .02 | 516 1292
gfz 193| 0 1 0 -1 -13 -11 -.62 9 9 | -164 509 12 76
| 0 0 0 62 64 23 .02 | 495 647
grg 134| 1 0 8 -24 12 3 .40 15 14 | -187 328 23 152
| 1 0 3 13 12 21 .03 | 237 410
igr n/a| 0 0 1 0 -4 14 -.31 4 4 | 1793 892 16 70
| 0 0 0 10 16 4 .02 | 733 572
jpl 80| 0 1 -9 -8 10 17 .18 14 13 | 2067 813 15 94
| 1 1 2 27 32 15 .02 | 681 567
mit 236| 1 -1 2 -11 -8 19 .01 13 11 | -204 319 25 222
| 1 0 1 21 15 5 .04 | 261 434
ngs 232| 0 0 0 15 45 7 .20 10 9 | -1334 316 1677 3242
| 1 0 3 38 12 15 .03 | 287 383
sio 415| 0 1 -4 -26 -147 -4 -.64 22 21 | --- --- --- ---
| 1 1 1 38 41 86 .04 | --- ---
Table 1.1750.b GPS week : 1750 MJD: 56494.000-56500.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 3 4 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 4 5 5 5 4 4 3 |
4 | 3 4 4 3 4 3 4 |
5 | 3 4 4 4 3 4 4 |
6 | 5 4 4 5 4 5 7 |
7 | 4 6 4 5 5 5 5 |
8 | 4 4 3 4 3 3 3 |
9 | 4 4 4 4 4 4 4 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 4 4 5 4 |
12 | 4 5 4 0 0 4 4 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 5 4 4 |
15 | 4 5 5 4 4 4 4 |
16 | 4 5 5 5 4 5 5 |
17 | 4 4 4 4 4 5 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 5 4 4 5 4 |
20 | 4 4 4 3 3 4 4 |
21 | 5 4 4 4 5 4 4 |
22 | 3 3 3 3 3 3 3 |
23 | 4 4 4 4 4 5 4 |
24 | 4 6 5 4 5 4 4 |
25 | 4 4 4 4 3 4 4 |
26 | 3 3 4 4 4 4 4 |
27 | 4 5 4 4 4 5 4 |
28 | 4 4 3 4 4 3 3 |
29 | 5 5 5 5 5 5 4 |
30 | 0 0 0 0 0 0 0 |
31 | 4 5 4 4 4 5 4 |
32 | 3 3 3 3 3 3 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1750.0 GPS week: 1750 Day: 0 MJD: 56494.000
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 263| -1 -1 0 21 8 17 .16 9 9 | -1300 370 17 94
emr 81| -2 0 -5 24 -16 14 .17 14 14 | 2490 209 19 101
esa 150| 0 -1 1 16 -4 -28 -.06 5 5 | -340 -510 13 104
gfz 190| -2 0 0 -123 -55 -3 -.61 9 9 | 300 -53 12 72
grg 134| 3 0 5 -18 16 16 .34 16 14 | -14 -204 22 158
igr n/a| 0 0 1 14 6 9 -.31 4 4 | 1015 342 16 80
jpl 80| 0 1 -6 23 21 15 .16 14 13 | 1429 276 15 93
mit 236| -1 0 4 -19 -2 19 -.03 12 11 | 187 -423 26 197
ngs 236| 2 1 -3 60 31 0 .23 9 8 | -1329 477 1269 2971
sio 421| -1 3 -3 -10 -157 12 -.65 22 23 | --- --- --- ---
Table 2.1750.1 GPS week: 1750 Day: 1 MJD: 56495.000
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 263| 0 0 0 36 -15 36 .14 11 10 | -1046 -164 23 89
emr 80| -3 0 -8 -7 -51 8 .23 15 15 | 1932 1527 19 87
esa 150| 1 0 1 -21 -22 -44 -.04 6 6 | -1761 1966 13 102
gfz 193| 0 1 0 -29 22 11 -.62 9 9 | -353 692 13 71
grg 135| 1 0 2 -18 21 6 .42 16 14 | -240 601 27 142
igr n/a| 0 0 1 -1 -33 12 -.31 5 5 | 870 1528 16 56
jpl 80| 2 0 -10 -10 -35 3 .19 14 13 | 1300 1446 17 88
mit 236| 0 -2 1 5 16 18 .00 10 9 | -314 485 23 212
ngs 233| 1 0 4 61 59 -14 .22 11 10 | -962 -214 2027 3048
sio 417| 0 2 -6 12 -113 178 -.63 22 22 | --- --- --- ---
Table 2.1750.2 GPS week: 1750 Day: 2 MJD: 56496.000
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 0 -12 30 0 .13 9 9 | -1224 271 17 80
emr 80| -3 -2 -6 -20 -3 10 .18 16 16 | 2656 900 18 135
esa 150| 1 0 1 9 -11 -19 -.04 6 5 | -782 29 16 121
gfz 195| 0 1 -2 33 -50 -17 -.65 9 9 | 20 705 12 76
grg 135| 0 0 6 -10 25 18 .39 15 13 | 46 -31 17 138
igr n/a| 0 0 1 -4 6 9 -.31 4 4 | 1801 899 16 67
jpl 80| 0 2 -6 -7 7 30 .15 15 14 | 2138 804 15 104
mit 236| 0 -2 2 2 -35 14 -.00 11 9 | -224 500 25 243
ngs 237| -1 1 0 -16 51 11 .25 9 9 | -1022 69 1567 3061
sio 416| -1 1 -4 -35 -186 -16 -.71 21 19 | --- --- --- ---
Table 2.1750.3 GPS week: 1750 Day: 3 MJD: 56497.000
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 265| 0 0 0 23 7 6 .20 9 9 | -1457 206 20 79
emr 80| -2 -2 -9 -11 4 27 .21 15 15 | 3358 667 15 130
esa 150| 1 0 1 -14 -1 -34 -.02 6 6 | -1257 1181 15 128
gfz 194| 0 2 -1 10 -91 5 -.62 7 7 | 99 -27 14 85
grg 134| 1 0 6 -26 16 25 .41 14 15 | -217 462 17 155
igr n/a| 0 0 1 -17 11 19 -.32 4 4 | 2219 817 16 80
jpl 80| 0 -1 -7 -42 68 5 .18 14 13 | 2477 872 15 88
mit 236| 2 -1 2 -1 -4 9 .04 12 11 | -411 673 23 229
ngs 234| -1 0 2 27 60 -2 .19 9 8 | -1380 155 1404 2883
sio 415| 2 1 -3 -5 -134 -59 -.58 22 21 | --- --- --- ---
Table 2.1750.4 GPS week: 1750 Day: 4 MJD: 56498.000
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 0 57 -47 -5 .15 10 10 | -1227 -36 20 85
emr 80| 0 -3 -11 -2 -30 33 .25 16 16 | 3121 713 16 119
esa 150| 0 0 3 4 -34 -9 -.04 5 5 | -1375 689 14 117
gfz 190| 0 3 0 -7 94 -58 -.65 8 8 | -375 1209 12 69
grg 132| 2 0 12 -50 -3 -16 .40 14 13 | 41 -20 26 156
igr n/a| 0 1 1 3 6 16 -.30 4 4 | 2227 930 16 72
jpl 80| -2 1 -10 6 -11 47 .21 14 13 | 2439 894 16 87
mit 236| 2 0 1 -49 -8 20 .08 12 11 | 144 -163 28 214
ngs 225| 0 0 -4 1 43 23 .17 10 8 | -1353 280 1921 3901
sio 403| 0 0 -3 -9 -160 -17 -.60 22 22 | --- --- --- ---
Table 2.1750.5 GPS week: 1750 Day: 5 MJD: 56499.000
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 262| 0 0 0 -16 11 -4 .18 10 9 | -1554 519 22 115
emr 80| 0 -3 -10 -18 -35 7 .17 14 14 | 3605 -5 14 134
esa 150| 0 0 2 -10 -25 -8 -.03 5 5 | -586 2206 10 101
gfz 194| -1 2 0 67 29 -9 -.64 9 9 | 263 -301 13 80
grg 134| 1 0 10 -16 -6 -34 .40 14 13 | -318 616 34 160
igr n/a| 0 0 0 9 -18 15 -.34 5 5 | 2935 75 18 65
jpl 80| -1 2 -10 -44 4 11 .17 14 13 | 3157 -74 16 113
mit 238| 2 -2 1 8 -16 23 -.00 14 13 | -386 697 24 218
ngs 233| 0 1 -1 16 46 29 .18 11 10 | -1473 441 1729 3462
sio 420| 1 1 -3 -105 -201 -86 -.67 23 19 | --- --- --- ---
Table 2.1750.6 GPS week: 1750 Day: 6 MJD: 56500.000
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| 0 0 0 12 36 9 .14 9 9 | -1816 871 20 104
emr 80| -1 -4 -13 27 -8 26 .16 14 14 | 1994 1350 13 109
esa 150| 0 0 2 -3 -16 -14 -.06 5 5 | -1455 3170 15 113
gfz 195| -1 1 0 38 -40 -8 -.58 9 9 | -1108 1341 13 80
grg 134| 2 0 11 -30 18 7 .42 14 13 | -612 878 18 155
igr n/a| 0 0 0 -6 -6 18 -.28 5 5 | 1486 1657 17 76
jpl 80| 0 0 -12 18 21 8 .21 14 14 | 1529 1479 15 89
mit 236| 3 -1 0 -28 -9 28 .01 16 13 | -424 464 28 243
ngs 232| 0 0 3 -41 27 6 .19 10 9 | -1824 1004 1825 3374
sio 419| 1 2 -5 -34 -80 -40 -.67 24 22 | --- --- --- ---
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 3.1750.0 GPS week: 1750 Day: 0 MJD: 56494.000
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 11 4 8 11 4 11 8 13 11 3 | 20 21 15 10 26 13 27 16 24 15 16
2 | 11 12 6 9 15 5 13 14 10 23 4 | 22 26 24 20 28 22 26 30 31 24 23
3E | 6 17 7 11 12 5 16 13 11 27 4 | 153 154 151 150 153 152 158 147 157 148 152
4 | 9 9 5 7 15 4 10 6 6 14 3 | 19 23 22 18 26 19 22 22 21 18 19
5 | 7 12 4 8 12 2 11 11 8 25 3 | 34 31 30 29 34 29 30 34 34 30 30
6E | 8 16 7 15 13 4 19 25 6 27 5 | 153 156 152 151 157 150 154 145 150 158 152
7 | 9 16 6 7 22 2 18 12 8 17 4 | 59 59 53 53 72 53 57 61 61 53 56
8 | 10 10 4 9 12 4 10 11 11 16 3 | 37 35 36 37 37 34 36 39 37 41 35
9 | 9 11 5 12 13 5 11 8 9 22 3 | 63 69 58 53 62 59 69 61 66 58 61
10 | 9 8 4 7 11 4 8 9 6 28 2 | 32 36 34 32 37 32 35 33 38 30 34
11 | 8 14 4 9 19 3 9 12 8 10 3 | 26 30 24 22 38 23 28 21 27 17 24
12 | 9 14 6 13 20 4 14 13 10 24 4 | 17 20 10 17 22 10 19 17 18 18 12
13 | 9 14 4 7 21 4 14 7 8 19 3 | 25 28 17 13 37 16 25 20 25 17 19
14 | 15 15 6 9 12 4 15 11 10 19 4 | 25 21 17 14 27 14 19 19 19 21 16
15 | 7 15 5 11 14 4 15 16 8 20 4 | 24 27 18 20 31 17 28 23 22 22 20
16 | 15 16 5 11 15 5 16 9 10 30 4 | 27 24 18 21 26 18 24 19 24 28 19
17E | 13 12 5 9 18 4 18 9 8 11 4 | 25 25 19 13 26 16 23 23 28 16 20
18 | 7 12 6 12 8 4 10 13 7 30 3 | 20 24 21 24 25 22 22 30 25 24 21
19E | 5 20 4 7 15 3 13 17 11 9 4 | 28 30 23 24 26 22 22 29 27 24 24
20 | 8 11 6 12 17 3 13 8 8 39 3 | 31 26 31 30 30 28 25 26 30 42 28
21 | 8 19 9 9 21 5 17 17 6 19 5 | 33 33 30 28 39 29 33 36 33 24 30
22 | 6 11 6 7 6 3 9 12 7 27 3 | 32 29 28 29 33 29 29 36 31 30 29
23 | 10 14 4 5 16 3 16 10 7 28 3 | 28 27 21 14 30 19 27 24 27 24 21
24 | 13 14 5 9 13 5 13 15 8 17 4 | 47 49 47 52 47 46 45 44 46 45 46
25 | 9 12 5 8 16 6 11 9 10 12 3 | 22 27 22 18 32 18 28 23 28 20 22
26 | 9 10 6 9 8 5 9 8 10 11 3 | 21 26 17 19 19 14 22 17 20 18 17
X27E | 11 15 5 8 --- 5 14 13 9 12 4 | 28 26 24 14 --- 20 26 24 26 19 22
28 | 6 11 4 10 18 4 12 8 9 36 3 | 28 29 22 23 37 21 30 26 26 34 24
29E | 8 18 7 8 23 4 19 13 9 9 4 | 26 23 18 20 22 17 23 27 27 18 20
X30 | 3 --- --- --- --- 56 --- --- --- --- 0 | 52 --- --- --- --- 14 --- --- --- --- 50
31 | 7 17 5 7 21 5 21 9 9 11 4 | 47 52 46 48 56 46 50 47 51 44 47
32 | 6 7 4 7 15 2 10 8 11 17 3 | 30 30 30 26 34 27 30 29 30 25 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 5 9 16 4 14 12 9 22 |T 38 39 34 33 42 32 38 37 39 35 35
WRMS | 9 14 5 9 14 4 13 11 8 23 |NE 27 27 23 22 30 21 26 25 27 24 24
MEDI | 8 14 5 9 15 4 13 11 9 19 |MD 28 28 24 23 32 22 28 27 28 24 24
Table 3.1750.1 GPS week: 1750 Day: 1 MJD: 56495.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 17 7 11 9 7 15 8 12 13 4 | 21 20 16 10 25 11 25 15 21 12 14
2 | 7 16 7 7 16 6 16 9 10 20 4 | 21 24 22 17 26 19 23 22 25 20 19
3E | 5 17 6 13 24 5 18 10 13 26 4 | 164 166 166 165 166 165 164 173 169 165 167
4 | 13 12 5 7 14 5 11 6 6 15 3 | 20 22 20 19 25 19 22 19 22 18 18
5 | 17 14 5 9 13 4 11 8 10 26 4 | 32 27 26 24 30 25 26 24 28 23 24
6E | 7 17 5 9 19 5 15 7 9 27 4 | 132 135 127 128 137 128 136 132 128 137 130
7 | 11 22 9 10 25 6 21 26 9 31 6 | 60 64 61 61 68 58 63 63 60 61 60
8 | 9 10 5 7 15 4 9 10 9 17 3 | 48 46 44 42 48 44 47 44 49 44 44
9 | 9 10 5 10 15 5 9 10 11 22 3 | 44 49 44 42 46 42 48 45 41 40 43
10 | 8 8 5 8 15 3 7 8 10 26 3 | 23 26 25 22 27 24 27 21 26 26 22
11 | 8 17 5 8 18 5 12 9 13 9 4 | 21 24 17 18 33 17 23 19 24 14 18
12 | 11 16 7 11 20 5 14 14 12 24 4 | 23 26 16 16 16 17 24 18 22 16 16
13 | 5 13 5 9 21 4 14 7 9 19 3 | 20 23 16 12 36 14 22 17 23 15 16
14 | 8 17 6 10 14 4 16 9 12 21 4 | 18 24 17 13 26 14 20 17 19 20 15
15 | 12 19 6 10 14 4 19 14 12 20 4 | 22 29 17 15 27 16 28 19 23 18 18
16 | 15 17 5 9 16 5 16 10 15 29 4 | 24 24 19 15 23 15 22 17 23 24 17
17E | 15 13 5 7 17 4 16 9 8 12 4 | 23 24 18 14 29 17 23 22 27 17 19
18 | 5 11 6 13 8 5 12 11 11 29 3 | 20 21 19 21 18 18 18 22 22 19 17
19E | 7 17 7 8 10 2 12 11 11 10 3 | 25 23 19 16 21 17 22 22 25 20 18
20 | 9 10 6 8 15 3 11 7 11 39 3 | 23 21 24 21 24 20 20 19 32 37 21
21 | 10 20 6 7 12 6 17 12 9 16 4 | 26 29 23 20 31 23 29 26 27 18 23
22 | 8 11 5 5 8 4 10 11 8 25 3 | 26 23 21 17 23 20 23 25 23 23 21
23 | 8 15 5 7 15 3 15 9 8 27 3 | 21 22 15 12 28 12 21 17 21 23 15
24 | 24 20 8 13 14 5 16 7 14 10 5 | 112 109 102 96 106 99 104 100 103 105 101
25 | 7 13 4 6 16 4 12 7 11 14 3 | 29 32 28 25 32 26 34 29 31 24 27
26 | 9 11 7 8 10 4 8 9 8 13 3 | 21 24 18 12 22 18 25 22 21 22 18
X27E | 7 17 5 6 --- 7 14 14 14 11 4 | 23 23 21 14 --- 15 22 24 25 17 19
28 | 6 12 4 8 18 4 12 6 14 36 3 | 23 28 21 17 34 18 25 21 26 31 21
29E | 13 21 8 12 16 4 20 11 13 12 5 | 35 32 31 26 29 28 31 31 38 27 28
X30 | 4 --- --- --- --- 51 --- --- --- --- 0 | 46 --- --- --- --- 14 --- --- --- --- 44
31 | 10 20 6 10 22 5 20 7 12 11 4 | 39 44 35 35 48 35 40 37 38 33 36
32 | 6 7 6 6 10 2 7 7 12 15 2 | 28 30 30 26 31 28 30 32 32 27 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 9 16 5 14 10 11 22 |T 37 39 34 31 41 32 38 35 38 35 34
WRMS | 10 15 6 9 14 5 13 9 10 22 |NE 25 25 21 18 27 19 25 22 25 22 21
MEDI | 8 16 6 8 15 4 14 9 11 20 |MD 23 26 21 19 29 19 25 22 26 23 21
Table 3.1750.2 GPS week: 1750 Day: 2 MJD: 56496.000
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 15 6 10 13 5 14 9 10 11 3 | 19 20 15 12 22 11 23 15 18 12 13
2 | 10 15 5 8 14 5 16 10 8 20 4 | 18 22 20 16 27 18 24 23 22 21 19
3E | 7 19 8 16 15 6 25 16 9 33 5 | 150 150 150 141 151 146 150 141 153 156 148
4 | 7 13 6 5 10 4 14 11 9 17 3 | 14 20 18 16 21 14 23 18 20 16 16
5 | 12 13 8 8 9 5 12 8 10 26 3 | 27 23 28 22 30 20 26 27 28 23 25
6E | 7 15 5 9 19 5 14 16 11 33 4 | 80 79 76 79 80 76 81 73 77 77 76
7 | 7 19 6 7 19 5 19 10 7 14 4 | 50 51 45 43 61 43 48 48 49 40 47
8 | 9 12 5 8 10 3 11 8 9 12 3 | 31 40 32 30 34 30 39 32 35 27 32
9 | 9 17 6 10 11 4 18 9 11 21 4 | 56 63 55 51 53 54 62 55 55 54 55
10 | 7 9 6 7 12 6 9 9 7 25 3 | 23 25 26 25 30 25 27 27 27 31 25
11 | 8 15 5 7 21 4 11 12 10 12 4 | 23 28 20 17 36 21 26 17 23 14 20
12 | 9 14 6 12 17 5 15 14 9 23 4 | 13 17 10 13 21 11 18 19 17 19 11
13 | 8 13 4 8 22 4 13 9 9 16 3 | 19 24 16 13 36 13 24 19 20 16 17
14 | 13 15 6 10 14 3 18 8 9 21 4 | 22 21 19 14 28 16 20 20 23 20 17
15 | 11 18 5 10 13 3 16 13 13 16 4 | 25 23 17 16 29 16 23 22 23 18 18
16 | 11 19 6 10 16 3 20 11 9 26 4 | 20 25 17 16 26 14 26 17 21 19 16
17E | 13 15 4 7 15 4 17 8 12 12 4 | 24 27 20 16 30 17 23 23 31 17 21
18 | 7 15 6 11 9 3 12 10 5 26 3 | 22 21 24 18 25 19 19 27 25 21 21
19E | 8 27 5 11 18 3 13 13 9 12 4 | 32 40 27 30 34 28 30 27 30 25 28
20 | 7 11 5 9 15 3 12 7 9 40 3 | 22 22 24 23 26 21 24 21 28 38 22
21 | 7 20 6 7 13 4 16 11 8 15 4 | 28 31 27 22 36 24 31 29 30 20 27
22 | 5 14 5 9 8 5 15 8 5 23 3 | 27 28 28 25 31 27 26 31 30 26 27
23 | 7 16 4 7 15 4 18 12 7 27 3 | 21 24 17 12 30 13 23 18 19 22 17
24E | 13 15 9 9 17 6 16 8 10 9 4 | 58 57 56 58 58 54 57 55 54 56 55
25 | 8 11 4 7 18 4 13 14 10 12 4 | 25 28 25 24 27 24 31 28 29 26 24
26 | 8 13 5 8 9 3 9 11 13 17 3 | 19 22 14 10 19 12 21 19 22 20 15
X27E | 8 18 5 9 --- 7 13 12 13 12 4 | 23 25 20 13 --- 15 23 20 24 15 19
28 | 9 12 3 7 13 3 12 6 12 35 3 | 24 27 20 20 32 18 27 21 26 30 22
29E | 6 20 6 12 10 3 23 10 11 9 4 | 18 24 17 20 24 15 23 23 26 19 17
X30 | 2 --- --- --- --- 35 --- --- --- --- 0 | 32 --- --- --- --- 30 --- --- --- --- 31
31 | 7 20 5 9 16 5 17 9 9 14 4 | 36 39 32 34 46 31 38 34 38 29 34
32 | 5 9 4 7 12 3 8 7 6 19 2 | 28 29 26 23 31 25 28 27 30 19 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 6 9 15 4 15 11 9 21 |T 32 34 30 28 37 28 34 31 33 30 30
WRMS | 9 16 5 9 13 4 14 9 9 19 |NE 22 24 21 18 28 19 25 22 24 21 20
MEDI | 8 15 5 9 14 4 14 10 9 17 |MD 24 25 24 20 30 20 26 23 27 21 22
Table 3.1750.3 GPS week: 1750 Day: 3 MJD: 56497.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 14 5 7 12 4 13 9 8 8 3 | 18 22 18 13 25 11 24 20 22 14 16
2 | 11 16 5 7 15 5 14 14 8 20 4 | 25 28 25 23 30 24 25 34 31 29 25
3E | 11 17 8 8 12 6 16 27 8 30 5 | 146 150 145 153 149 148 149 158 151 148 149
4 | 6 14 6 6 14 4 12 10 6 15 3 | 23 24 24 22 29 21 22 26 26 22 22
5 | 14 12 5 7 10 5 12 10 8 27 3 | 37 31 32 30 35 30 29 36 35 32 32
6E | 7 15 6 8 15 5 15 21 11 32 4 | 118 119 118 113 121 114 120 116 113 120 116
7 | 14 18 7 7 19 3 19 11 10 13 4 | 64 66 60 59 71 59 63 65 63 54 61
8 | 11 11 6 6 13 3 11 11 10 12 3 | 63 58 59 59 58 57 60 62 57 62 59
9 | 9 16 6 8 13 4 17 10 7 19 4 | 109 117 109 105 109 107 116 108 111 108 109
10 | 9 9 4 5 17 4 10 9 6 29 3 | 35 35 38 37 38 35 39 38 39 36 36
11 | 9 19 6 5 20 5 10 12 11 12 4 | 25 29 22 20 38 22 27 21 25 19 22
X12 | 3 --- --- --- --- 91 --- --- --- --- 0 | 106 --- --- --- --- 130 --- --- --- --- 104
13 | 9 12 6 6 22 3 12 9 6 19 3 | 24 27 19 17 39 17 24 22 26 17 20
14 | 14 15 6 7 14 4 19 9 10 22 4 | 26 25 24 18 32 20 23 24 24 23 21
15 | 7 16 5 7 13 3 17 13 9 17 4 | 24 27 20 17 31 19 27 25 28 18 22
16 | 8 18 9 9 19 4 17 11 10 28 4 | 24 28 23 22 26 20 26 24 25 28 22
17E | 13 15 6 7 18 3 16 12 9 13 4 | 32 30 29 24 32 25 27 29 36 21 28
18 | 7 13 7 9 9 3 13 15 7 28 3 | 23 23 22 21 24 21 22 29 23 20 20
19E | 10 17 7 9 12 3 11 12 9 13 4 | 30 29 26 23 30 22 25 27 30 22 25
20 | 9 10 7 6 15 3 11 7 7 39 3 | 27 22 26 23 29 23 22 25 27 40 24
21 | 11 19 4 7 11 3 15 14 10 16 4 | 31 31 27 26 36 25 30 32 28 24 27
22 | 6 11 5 4 10 3 14 9 9 25 3 | 32 29 28 25 32 26 27 32 26 25 27
23 | 10 17 7 4 16 4 15 13 8 27 4 | 26 28 21 17 30 17 24 21 27 21 20
24E | 12 15 6 7 13 7 15 11 8 11 4 | 31 33 32 28 31 28 29 31 31 27 29
25 | 6 11 5 6 16 4 12 11 12 12 3 | 20 24 21 17 29 17 28 23 19 16 19
26 | 9 13 5 6 9 4 8 17 10 16 3 | 25 28 21 19 25 19 25 28 25 24 22
X27E | 13 15 5 7 --- 6 13 11 12 10 4 | 25 23 22 16 --- 16 24 21 23 16 19
28 | 10 11 5 8 12 3 11 7 9 37 3 | 24 29 23 24 32 18 26 22 26 33 23
29E | 8 17 10 10 13 4 18 14 11 10 4 | 29 30 27 29 30 23 31 31 31 26 26
X30 | 3 --- --- --- --- 45 --- --- --- --- 0 | 44 --- --- --- --- 23 --- --- --- --- 42
31 | 6 19 8 7 16 4 22 9 7 13 4 | 55 58 52 51 62 51 55 53 57 48 53
32 | 7 6 6 5 13 2 9 5 8 17 2 | 37 36 36 33 37 33 37 35 39 32 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 6 7 14 4 14 12 9 22 |T 42 41 38 36 44 38 40 40 40 37 39
WRMS | 9 15 6 7 15 4 13 11 8 21 |NE 32 29 26 24 32 28 28 28 28 26 30
MEDI | 9 15 6 7 13 4 13 11 9 17 |MD 29 29 26 23 32 23 27 29 28 25 25
Table 3.1750.4 GPS week: 1750 Day: 4 MJD: 56498.000
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 13 4 8 11 5 15 13 12 12 3 | 21 21 16 12 24 14 24 21 20 18 16
2 | 10 20 3 7 16 3 13 14 9 22 4 | 26 30 23 22 28 21 26 32 24 31 23
3 | 8 20 6 6 12 5 15 11 8 28 4 | 110 114 110 112 110 110 116 111 119 115 112
4 | 7 14 7 6 12 4 12 12 7 14 3 | 18 24 17 18 25 15 20 23 15 20 17
5 | 9 12 3 7 11 4 11 12 10 29 3 | 29 27 27 27 30 26 28 34 28 30 27
6E | 7 18 5 10 11 6 15 19 6 31 4 | 81 85 81 78 85 78 82 87 82 92 81
7 | 11 18 7 10 12 4 18 17 9 12 4 | 100 100 96 101 101 98 99 103 101 99 99
8 | 7 11 4 8 12 3 10 11 9 15 3 | 32 31 26 24 28 24 30 31 28 27 27
9E | 12 18 6 9 12 9 18 11 9 22 4 | 113 116 113 113 112 114 114 112 114 113 112
10 | 8 9 3 6 12 5 8 9 7 27 2 | 25 29 28 25 32 27 27 29 23 29 26
11 | 8 13 4 9 21 2 8 14 10 16 4 | 24 25 21 18 38 19 23 23 20 24 21
X12 | 5 --- --- --- --- 17 --- --- --- --- 0 | 23 --- --- --- --- 20 --- --- --- --- 22
13 | 8 15 4 7 21 3 14 11 9 19 4 | 23 29 21 15 40 17 27 22 23 17 21
14 | 15 18 4 8 14 4 18 9 10 22 4 | 24 26 18 18 31 16 23 23 20 22 18
15 | 11 16 5 9 15 6 16 12 11 16 4 | 28 32 22 21 34 21 31 28 30 21 24
16 | 16 16 6 9 14 6 15 12 7 26 4 | 27 24 19 18 24 19 25 22 21 25 19
17E | 16 16 6 5 16 4 15 8 9 13 4 | 33 34 25 23 34 24 30 32 31 32 27
18 | 11 13 8 12 8 4 11 20 4 28 4 | 21 23 23 25 28 20 25 32 19 24 20
19E | 10 22 6 8 15 4 11 13 8 17 4 | 30 29 20 19 27 20 24 27 27 27 22
20 | 8 10 4 10 15 4 12 8 8 40 3 | 25 22 25 20 28 21 19 23 23 40 22
21 | 12 18 5 10 15 3 16 17 9 16 4 | 28 31 25 26 39 24 32 33 28 22 27
22 | 7 11 4 5 8 4 11 12 7 24 3 | 27 28 26 25 31 24 28 31 21 25 25
23 | 8 18 5 7 16 4 17 12 9 28 4 | 26 29 21 15 32 17 27 23 25 23 21
24E | 11 17 8 8 12 4 17 11 19 11 4 | 33 34 31 31 34 29 33 32 33 30 30
25 | 8 12 4 8 14 3 13 11 7 13 3 | 20 28 20 18 28 18 30 25 24 19 21
26 | 9 11 5 8 12 4 7 13 11 14 3 | 25 29 19 15 26 18 24 28 22 25 20
X27E | 10 16 5 8 --- 6 11 16 6 14 4 | 25 25 17 14 --- 15 24 25 22 20 19
28 | 7 12 4 10 12 4 10 9 16 35 3 | 28 30 20 21 32 20 29 26 26 33 23
29E | 13 23 7 12 14 4 19 11 12 10 5 | 25 30 23 24 29 21 25 28 32 21 23
X30 | 5 --- --- --- --- 30 --- --- --- --- 0 | 30 --- --- --- --- 31 --- --- --- --- 28
31 | 10 17 5 6 17 4 18 7 9 14 4 | 72 77 72 71 72 73 77 76 76 72 73
32 | 7 7 5 5 14 3 8 8 9 18 3 | 30 32 32 28 35 28 31 33 31 31 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 5 8 14 4 14 12 10 22 |T 36 39 34 33 41 32 38 39 36 37 34
WRMS | 10 16 5 8 13 4 13 11 8 22 |NE 25 27 22 20 30 20 26 27 23 25 22
MEDI | 9 16 5 8 14 4 13 12 9 17 |MD 27 29 23 22 32 21 27 28 25 25 23
Table 3.1750.5 GPS week: 1750 Day: 5 MJD: 56499.000
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 13 6 10 10 4 16 14 16 15 4 | 21 25 18 18 29 15 26 21 23 16 19
2 | 7 17 6 8 16 4 17 16 9 21 4 | 22 27 21 19 31 19 24 28 23 25 21
3 | 9 18 6 6 14 5 15 14 8 28 4 | 108 110 104 102 109 102 107 104 103 112 105
4 | 7 12 5 7 11 3 10 12 8 13 3 | 24 23 21 22 25 20 23 21 24 18 21
5 | 10 13 4 6 10 3 10 15 13 29 3 | 34 29 28 24 34 24 27 32 24 29 27
6E | 7 18 7 10 17 5 18 14 11 28 4 | 135 136 134 132 142 134 134 127 135 131 134
7E | 12 19 7 10 13 7 19 27 10 19 5 | 72 76 72 70 72 70 72 73 71 71 71
8 | 8 10 3 7 10 5 11 13 9 16 3 | 35 36 32 33 36 30 34 34 34 31 33
9E | 9 15 6 8 14 5 18 12 10 25 4 | 83 89 83 80 83 85 87 83 78 82 83
10 | 6 8 4 7 13 3 8 12 9 31 3 | 24 23 25 23 26 22 21 24 21 29 23
11 | 8 13 5 11 21 4 13 15 14 15 4 | 27 28 21 24 40 20 26 24 23 24 23
12 | 12 15 4 9 13 4 12 10 9 22 3 | 20 18 11 10 10 15 15 14 12 11 16
13 | 8 15 4 8 20 3 15 16 7 19 4 | 23 28 20 18 40 17 24 22 23 16 21
14 | 13 15 5 8 14 4 17 12 11 21 4 | 24 30 24 19 33 22 25 24 26 24 23
15 | 6 17 5 13 15 6 16 13 10 18 4 | 25 29 21 20 35 18 25 22 25 19 22
16 | 15 16 7 11 12 6 15 20 12 27 4 | 27 27 21 20 25 19 26 24 21 25 20
17E | 12 16 5 6 16 5 15 16 12 15 4 | 37 36 31 29 35 27 33 34 38 22 32
18 | 8 10 5 10 9 4 11 19 6 29 3 | 21 21 22 15 23 17 17 26 20 21 17
19E | 10 17 6 9 18 5 11 15 13 14 4 | 32 31 26 22 30 22 26 27 26 23 25
20 | 7 10 5 12 14 3 13 11 10 41 3 | 26 23 29 27 28 23 21 24 22 39 25
21 | 11 15 5 10 12 6 14 18 12 16 4 | 24 30 22 22 37 20 28 26 25 16 23
22 | 6 10 5 8 8 3 11 11 7 25 3 | 25 28 28 18 31 24 27 26 24 22 24
23 | 9 18 5 8 15 3 21 16 9 27 4 | 24 26 21 19 32 17 25 21 23 22 20
24E | 11 14 5 7 14 5 17 10 12 10 4 | 22 22 17 13 28 15 25 19 21 15 17
25 | 10 11 4 7 14 4 14 8 11 14 3 | 24 27 23 18 28 20 31 23 24 20 22
26 | 6 10 6 6 11 3 8 14 12 12 3 | 22 27 21 16 28 19 24 24 22 19 20
X27E | 11 17 6 6 --- 6 11 20 16 13 4 | 28 29 24 16 --- 18 25 27 21 23 22
28 | 8 11 4 9 11 5 14 9 8 37 3 | 28 31 25 25 33 21 29 25 27 33 25
29E | 12 17 7 14 13 5 15 12 11 12 4 | 30 31 28 27 33 24 27 30 31 25 27
X30 | 3 --- --- --- --- 45 --- --- --- --- 0 | 47 --- --- --- --- 39 --- --- --- --- 46
31E | 20 18 6 11 15 9 16 14 11 19 5 | 98 96 91 95 94 86 93 84 96 79 93
32 | 7 8 4 6 11 3 9 11 10 24 3 | 39 39 41 37 45 35 38 41 42 38 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 9 14 5 14 14 11 23 |T 38 39 35 33 42 33 37 36 36 34 35
WRMS | 9 14 5 9 13 5 13 13 10 19 |NE 26 27 23 21 30 21 25 25 24 23 24
MEDI | 8 15 5 8 13 4 14 14 10 19 |MD 26 29 24 22 33 21 26 26 24 24 23
Table 3.1750.6 GPS week: 1750 Day: 6 MJD: 56500.000
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 12 5 9 13 4 13 15 10 18 3 | 21 24 18 15 26 16 26 20 19 19 17
2 | 9 17 6 7 14 6 15 16 15 22 4 | 23 21 22 20 30 20 23 31 23 26 21
3 | 6 13 4 7 11 5 11 11 7 29 3 | 102 105 99 95 103 97 103 104 101 100 100
4 | 8 13 4 7 11 4 13 10 11 15 3 | 23 21 21 20 27 19 24 22 24 17 21
5 | 12 13 5 4 8 2 10 11 11 27 3 | 36 29 35 30 40 30 29 36 30 31 32
6E | 11 18 7 15 16 7 19 45 13 48 6 | 171 172 171 171 172 169 175 181 170 182 171
7E | 15 16 5 12 15 5 16 19 9 14 4 | 66 70 62 64 70 65 68 70 69 62 65
8 | 8 8 5 9 10 5 11 12 9 19 3 | 32 32 29 27 30 26 33 30 32 34 28
9E | 9 17 5 8 11 6 18 12 8 25 4 | 110 113 111 110 111 111 116 109 116 115 111
10 | 6 9 4 6 11 6 8 9 7 31 2 | 33 30 35 34 41 33 34 34 34 41 33
11 | 6 12 4 8 21 3 11 17 11 17 4 | 29 28 28 22 44 25 29 24 27 24 26
12 | 8 14 5 7 14 5 12 12 11 22 3 | 12 15 8 9 10 13 13 11 12 12 13
13 | 7 14 4 5 19 5 15 12 7 20 3 | 23 27 21 17 39 18 24 21 22 24 21
14 | 6 18 5 8 13 5 17 14 8 22 4 | 21 25 22 21 31 17 22 24 22 25 20
15 | 8 15 7 12 13 5 18 14 10 17 4 | 28 32 23 23 33 21 31 24 27 22 24
16 | 13 14 6 11 15 5 15 17 11 27 4 | 28 29 26 27 28 21 28 25 24 26 24
17E | 12 15 6 6 16 4 19 12 11 14 4 | 31 28 23 21 30 21 27 24 28 17 24
18 | 8 13 5 8 9 3 11 21 8 29 3 | 24 21 25 27 28 23 23 33 24 25 23
19E | 9 12 4 10 16 5 10 13 11 18 3 | 25 24 19 15 24 16 23 19 22 20 18
20 | 7 11 5 13 14 3 15 13 8 39 3 | 33 26 34 33 37 29 24 28 32 39 31
21 | 10 19 4 7 13 4 15 16 9 16 4 | 29 29 25 25 37 25 29 31 28 24 26
22 | 6 11 4 5 7 3 12 11 11 25 3 | 32 27 31 30 36 29 28 34 28 32 30
23 | 10 18 4 5 15 4 20 13 9 27 4 | 25 26 22 19 33 19 24 23 23 28 21
24E | 14 17 3 7 10 6 17 11 14 9 4 | 32 35 31 33 33 30 31 35 32 33 30
25 | 8 10 3 12 12 5 12 11 8 16 3 | 19 23 19 19 29 17 28 22 20 18 20
26 | 9 16 7 9 11 7 10 13 7 12 3 | 20 29 17 14 24 16 24 19 19 16 18
X27E | 8 18 4 10 --- 6 13 14 11 13 4 | 26 27 23 21 --- 19 27 24 24 20 22
28 | 7 11 4 10 10 4 12 11 10 35 3 | 26 30 23 25 31 22 30 27 31 38 25
29E | 10 16 6 9 14 5 16 10 11 13 4 | 29 32 26 31 29 28 31 30 30 34 27
X30 | 3 --- --- --- --- 34 --- --- --- --- 0 | 40 --- --- --- --- 30 --- --- --- --- 39
31E | 10 18 5 8 12 8 16 9 7 14 3 | 68 71 65 67 68 65 69 66 68 62 66
32 | 8 9 3 8 30 6 12 21 9 24 4 | 90 90 87 87 76 84 88 92 84 88 87
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 5 9 14 5 14 16 10 24 |T 40 41 38 37 45 36 41 41 40 40 38
WRMS | 9 14 5 9 13 5 14 13 9 22 |NE 29 29 27 25 33 25 29 29 27 29 27
MEDI | 8 14 5 8 13 5 13 13 10 20 |MD 29 29 25 25 33 23 28 28 28 26 25
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 4.1750 GPS week: 1750 MJD: 56494.0-56500.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 |U 8 10 22 |U 6 7 24 |U 9 9 20 |
emr | emr 2943 | 12 13 29 |U 9 10 35 | 10 9 23 |
esa | esa 2948 | 10 12 28 |U 6 8 26 | 10 9 21 |
gfz | gfz 2940 |U 10 12 27 |U 6 8 27 |U 10 10 23 |
grg | grg 2852 |U 12 14 36 |U 8 12 36 | 13 13 30 |
igr | igr 2947 | 10 12 27 | 6 8 26 | 10 9 21 |
igs | igs 2915 | 10 12 27 | 6 8 27 | 10 9 21 |
jpl | jpl 2942 | 11 12 27 |U 7 9 30 |U 10 10 22 |
mit | mit 2948 | 10 12 28 |U 9 12 42 |U 12 10 24 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1750.0 GPS week: 1750 Day: 0 MJD: 56494.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 5 8 17 | 5 5 23 | 10 8 18 |
emr | emr 2968 | 9 7 16 | 12 8 72 | 9 10 22 |
esa | esa 2976 | 6 10 18 | 5 7 26 | 10 9 21 |
gfz | gfz 2968 | 5 9 15 | 5 7 24 | 10 9 20 |
grg | grg 2880 | 6 9 17 | 6 9 31 | 11 13 25 |
igr | igr 2971 | 6 8 17 | 5 7 28 | 10 9 20 |
igs | igs 2965 | 5 9 16 | 5 6 26 | 10 10 21 |
jpl | jpl 2967 | 6 7 14 | 7 9 47 | 8 7 20 |
mit | mit 2976 | 7 13 27 | 14 15 93 | 13 9 19 |
Table 5.1750.1 GPS week: 1750 Day: 1 MJD: 56495.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 8 14 20 | 6 5 22 | 9 10 23 |
emr | emr 2968 | 13 16 36 | 8 10 27 | 10 12 24 |
esa | esa 2976 | 11 17 35 | 5 7 24 | 10 8 22 |
gfz | gfz 2968 | 11 17 33 | 6 7 25 | 10 8 22 |
grg | grg 2880 | 11 17 37 | 8 8 33 | 13 12 22 |
igr | igr 2976 | 10 16 33 | 4 7 24 | 10 7 20 |
igs | igs 2962 | 11 17 33 | 6 7 26 | 10 8 21 |
jpl | jpl 2968 | 12 15 35 | 5 8 26 | 10 9 19 |
mit | mit 2976 | 10 18 33 | 6 7 31 | 11 8 23 |
Table 5.1750.2 GPS week: 1750 Day: 2 MJD: 56496.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 | 11 12 20 | 11 11 29 | 10 9 22 |
emr | emr 2970 | 15 15 24 | 9 14 31 | 12 11 23 |
esa | esa 2976 | 12 16 23 | 11 12 31 | 11 12 24 |
gfz | gfz 2968 | 13 16 21 | 11 13 34 | 11 13 24 |
grg | grg 2880 | 14 16 24 | 10 13 34 | 15 16 32 |
igr | igr 2976 | 12 15 21 | 11 12 30 | 12 12 23 |
igs | igs 2894 | 13 16 21 | 11 13 32 | 11 11 23 |
jpl | jpl 2970 | 12 14 23 | 10 12 30 | 10 11 24 |
mit | mit 2976 | 12 16 19 | 12 15 37 | 14 13 27 |
Table 5.1750.3 GPS week: 1750 Day: 3 MJD: 56497.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2931 | 7 8 20 | 6 8 24 | 9 9 21 |
emr | emr 2876 | 10 9 32 | 9 11 28 | 10 9 23 |
esa | esa 2880 | 9 9 31 | 6 10 26 | 10 11 19 |
gfz | gfz 2872 | 8 8 29 | 6 9 26 | 11 11 21 |
grg | grg 2784 | 18 15 63 | 10 21 45 | 16 18 38 |
igr | igr 2880 | 8 8 29 | 6 8 27 | 10 11 20 |
igs | igs 2839 | 8 8 30 | 6 10 26 | 10 10 21 |
jpl | jpl 2875 | 8 8 28 | 6 9 23 | 11 11 23 |
mit | mit 2880 | 7 9 28 | 6 11 26 | 9 11 23 |
Table 5.1750.4 GPS week: 1750 Day: 4 MJD: 56498.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 8 8 20 | 4 8 18 | 7 7 16 |
emr | emr 2876 | 13 9 29 | 6 8 18 | 8 11 25 |
esa | esa 2880 | 9 10 24 | 5 6 20 | 8 7 25 |
gfz | gfz 2869 | 9 10 25 | 5 6 20 | 9 7 25 |
grg | grg 2784 | 10 10 28 | 7 8 20 | 10 9 33 |
igr | igr 2880 | 10 10 26 | 5 6 19 | 9 7 25 |
igs | igs 2848 | 10 9 26 | 5 7 22 | 9 7 24 |
jpl | jpl 2876 | 13 11 30 | 5 7 20 | 10 8 25 |
mit | mit 2880 | 11 9 25 | 9 19 39 | 15 11 32 |
Table 5.1750.5 GPS week: 1750 Day: 5 MJD: 56499.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3038 | 7 11 29 | 6 5 28 | 11 10 20 |
emr | emr 2972 | 10 16 32 | 8 8 36 | 10 6 22 |
esa | esa 2976 | 8 11 32 | 6 6 30 | 9 8 19 |
gfz | gfz 2969 | 9 13 37 | 6 6 30 | 12 14 30 |
grg | grg 2880 | 11 16 43 | 8 10 36 | 12 11 30 |
igr | igr 2975 | 8 12 31 | 6 5 28 | 9 9 20 |
igs | igs 2966 | 8 12 32 | 6 6 31 | 10 8 20 |
jpl | jpl 2972 | 10 15 32 | 7 10 34 | 10 9 20 |
mit | mit 2976 | 8 10 32 | 6 9 35 | 10 8 21 |
Table 5.1750.6 GPS week: 1750 Day: 6 MJD: 56500.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 13 12 29 | 5 10 27 | 10 10 23 |
emr | emr 2972 | 15 15 31 | 8 12 36 | 9 9 19 |
esa | esa 2976 | 13 12 31 | 5 10 27 | 9 7 18 |
gfz | gfz 2968 | 13 12 31 | 5 9 27 | 9 7 19 |
grg | grg 2880 | 16 17 40 | 8 16 50 | 11 14 32 |
igr | igr 2975 | 14 12 32 | 5 8 25 | 9 7 18 |
igs | igs 2936 | 13 11 31 | 5 9 27 | 9 7 19 |
jpl | jpl 2972 | 14 15 30 | 6 9 32 | 10 14 24 |
mit | mit 2976 | 13 11 30 | 6 10 31 | 10 8 24 |
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 6.1750 GPS week: 1750 MJD: 56494.500-56500.500
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 -18 -25 -57 -1 | 13 23
| 17 13 56 106 6 | 4
emr uuuuu | 44 4 -35 -4 6 | 53 56
| 24 25 88 98 11 | 6
esa uuuuu | 12 -19 55 114 -2 | 16 22
| 9 11 27 49 3 | 4
gfz uuuuu | 34 16 85 -2 -4 | 7 18
| 14 27 91 55 5 | 3
grg uuuux | 6 29 -71 -63 4 | 9 18
| 8 16 37 95 28 | 4
igr xxxxx | 4 3 73 18 -4 | 8 18
| 17 15 37 30 4 | 4
irf xxxxx | 5 7 -21 -30 -1 | 7 17
| 7 7 46 33 3 | 3
jpl uuuuu | -18 6 90 -70 7 | 26 32
| 37 29 105 51 10 | 5
mit uuuuu | 5 11 -114 -92 3 | 16 22
| 14 24 102 97 5 | 3
ngs uuuuu | -66 9 -103 -25 1 | 9 16
| 37 35 110 56 4 | 4
sio xxxxx | 136 29 71 32 -1 | 32 36
| 34 63 92 105 4 | 2
Table 7.1750.0 GPS week: 1750 Day: 0 MJD: 56494.500
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 | -33 0 -9 -132 5 | 8 17
emr uuuuu | 75 -24 -16 155 -2 | 45 47
esa uuuuu | 2 -18 58 11 1 | 10 16
gfz uuuuu | 15 44 -49 1 4 | 2 14
grg uuuux | 14 37 -101 -28 -40 | 8 15
igr xxxxx | -20 23 14 -40 -1 | 3 14
irf xxxxx | 1 6 18 5 2 | 3 13
jpl uuuuu | -14 -27 22 -2 1 | 18 24
mit uuuuu | -10 8 -9 21 -3 | 12 18
ngs uuuuu | -22 -1 -1 10 -4 | 3 10
sio xxxxx | 128 -22 171 113 -7 | 31 33
Table 7.1750.1 GPS week: 1750 Day: 1 MJD: 56495.500
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 | -37 -22 -54 -248 -3 | 11 21
emr uuuuu | 57 -1 -21 49 6 | 47 49
esa uuuuu | 11 -3 15 120 -1 | 13 19
gfz uuuuu | 40 19 156 36 2 | 5 17
grg uuuux | 14 28 -32 -97 -26 | 6 15
igr xxxxx | 21 14 62 35 0 | 5 16
irf xxxxx | 9 12 56 16 0 | 5 15
jpl uuuuu | 26 6 119 -107 9 | 21 27
mit uuuuu | 11 -5 14 0 2 | 14 20
ngs uuuuu | -113 -9 -248 65 -3 | 5 12
sio xxxxx | 125 4 152 139 -2 | 31 34
Table 7.1750.2 GPS week: 1750 Day: 2 MJD: 56496.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -31 -6 -39 -10 -3 | 11 21
emr uuuuu | 43 12 57 35 1 | 50 52
esa uuuuu | 2 -14 34 100 -3 | 13 20
gfz uuuuu | 48 -21 127 64 -6 | 5 17
grg uuuux | 1 8 -73 -167 -2 | 4 14
igr xxxxx | 15 0 38 28 -4 | 7 17
irf xxxxx | -6 11 -45 -25 -4 | 5 16
jpl uuuuu | 20 -24 178 -68 -2 | 24 30
mit uuuuu | -17 26 -135 -91 -2 | 14 20
ngs uuuuu | -44 35 -130 -55 7 | 6 13
sio xxxxx | 132 57 -3 54 -4 | 31 34
Table 7.1750.3 GPS week: 1750 Day: 3 MJD: 56497.500
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 | 5 -32 -122 -14 7 | 12 21
emr uuuuu | 28 9 21 -18 5 | 52 54
esa uuuuu | 26 -11 84 159 -1 | 15 20
gfz uuuuu | 27 38 41 46 -8 | 6 17
grg uuuux | 6 26 -17 -197 11 | 6 14
igr xxxxx | 5 8 82 19 -6 | 8 16
irf xxxxx | 11 -1 -15 -32 1 | 6 16
jpl uuuuu | -86 41 97 -117 -4 | 25 30
mit uuuuu | 5 -12 -76 -51 6 | 14 20
ngs uuuuu | -52 -40 -82 -80 0 | 8 14
sio xxxxx | 117 8 153 83 2 | 31 34
Table 7.1750.4 GPS week: 1750 Day: 4 MJD: 56498.500
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 | 0 -35 61 -7 -5 | 16 25
emr uuuuu | 51 16 -159 -8 19 | 55 58
esa uuuuu | 20 -26 83 133 -3 | 18 24
gfz uuuuu | 19 40 -5 -93 -3 | 8 18
grg uuuux | 3 48 -77 17 16 | 10 19
igr xxxxx | -20 -12 104 3 -3 | 10 18
irf xxxxx | 13 -6 -25 -34 0 | 9 18
jpl uuuuu | -18 17 -114 -33 7 | 28 33
mit uuuuu | 13 -20 -108 -82 8 | 16 24
ngs uuuuu | -97 6 69 -85 -1 | 11 17
sio xxxxx | 156 -44 84 65 3 | 33 36
Table 7.1750.5 GPS week: 1750 Day: 5 MJD: 56499.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -15 -9 6 80 2 | 18 28
emr uuuuu | 50 44 -156 -100 23 | 61 65
esa uuuuu | 10 -26 36 136 -1 | 21 27
gfz uuuuu | 40 -14 195 -32 -10 | 12 21
grg uuuux | 13 10 -75 -31 30 | 15 26
igr xxxxx | 12 -20 120 50 -6 | 14 22
irf xxxxx | 9 11 -63 -59 -6 | 13 22
jpl uuuuu | -28 43 165 -133 19 | 33 39
mit uuuuu | 22 38 -245 -203 1 | 21 29
ngs uuuuu | -101 -2 -132 -48 1 | 15 21
sio xxxxx | 201 144 -57 -130 -2 | 37 41
Table 7.1750.6 GPS week: 1750 Day: 6 MJD: 56500.500
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 | -33 -20 -15 -71 -10 | 15 26
emr uuuuu | 1 -29 26 -141 -7 | 60 64
esa uuuuu | 11 -33 72 142 -9 | 18 25
gfz uuuuu | 48 3 133 -38 -5 | 9 21
grg uuuux | -8 45 -124 59 36 | 14 25
igr xxxxx | 14 7 89 32 -11 | 11 20
irf xxxxx | 1 14 -74 -80 -1 | 10 21
jpl uuuuu | -23 -13 161 -28 22 | 31 37
mit uuuuu | 11 39 -241 -236 11 | 19 28
ngs uuuuu | -31 71 -200 15 5 | 14 21
sio xxxxx | 94 57 -1 -100 5 | 34 39
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