[IGSREPORT-23362] Wk 1829 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Feb 13 09:37:09 PST 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1829 (Jan 25, 2015 - Jan 31, 2015)
Contacts: igs.acc 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:
igs1829[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1829[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1829[0-6].cls IGS GPS clock combination summary report.
igs18297.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18297.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 | KOUC MAR6 KOUC MAR6 XMIS
0 | EMR | 8
0 | ESA | NTUS NTUS
0 | GFZ | 1 2 3 6 30 1 3 6 8 30
0 | GRG | 32 MCM4 SANT SANT
0 | JPL | 8
0 | MIT | 11 22 6 8 11 19 22
1 | COD | TLSE
1 | EMR | 8
1 | ESA | 32 32 HYDE
1 | GFZ | 1 2 3 6 30 32 1 3 6 8 30 32 KELY TLSE
1 | GRG | DRAG MCM4 TLSE WES2 DRAG KELY TLSE WES2
1 | JPL | 8 NRIL
1 | MIT | 11 21 32 19 21 28 32 SPT0 SPT0
2 | COD | KOUC MAR6 CONZ HARB KELY KOUC MAR6 MOBS REUN REYK
2 | COD | SOFI
2 | EMR | 8
2 | ESA | KELY
2 | GFZ | 1 2 3 6 9 30 1 3 6 8 30 CONZ HARB REUN REYK SOFI
2 | GRG | DRAG MCM4 NKLG DRAG HARB NKLG REUN TLSE
2 | MIT | 19 28 32 1 8 19 23 25 27 28 32 MDVJ NTUS
3 | COD | KOUC MAR6 KOUC MAR6
3 | EMR | 8 8
3 | ESA | 22 29 32 BRST DRAG HOFN KOUR WTZR
3 | GFZ | 1 2 3 6 30 1 3 6 30 DAV1 TLSE
3 | GRG | 4 NOVM BOGT BRST DAV1 DRAG KELY NOVM WES2
3 | JPL | 8 CHUR
3 | MIT | 8 TLSE BAKO TLSE WUHN
4 | COD | HOB2 HYDE HOB2
4 | EMR | 4
4 | ESA | BARH HOB2
4 | GFZ | 1 2 3 6 9 30 1 3 6 30 BARH DAV1 HOB2 HYDE KOUC KOUR
4 | GFZ | RABT REUN SCOR SOFI STHL TOW2 BARH HOB2 RABT TOW2
4 | GRG | 4 NYA1 SANT DAV1 NYA1 SANT TIXI
4 | JPL | 4
4 | MIT | 8 28 4 8 28 29 HOB2 KOUR BAKO CRO1 HOB2 KOUR
5 | COD | 4 NTUS NTUS QAQ1 SYOG
5 | EMR | 4
5 | ESA | 4 WTZR WTZR
5 | GFZ | 1 2 3 4 6 9 30 1 3 6 30 ARTU ASPA AUCK BAKE BARH
5 | GFZ | BJFS BOGT BRFT CEDU CHTI CHUR DARW DRAG GLPS GUAM
5 | GFZ | GUUG HOB2 HOFN ISPA KELY KERG KOUC KOUR MAL2 MAS1
5 | GFZ | MATE MDVJ NANO NICO NKLG NRIL NYA1 PERT PIE1 PIMO
5 | GFZ | QAQ1 REUN SCOR SFER SOFI SSIA STHL SYOG THTI TOW2
5 | GFZ | WHIT WSRT XMIS ZECK INVK
5 | GRG | 4 ALBH ALGO ALRT BRFT CRO1 DARW GODE HNPT HOLB HYDE
5 | GRG | JPLM KOUR LAMA MDVJ MONP NLIB NOVM NRC1 NYAL SOFI
5 | GRG | STJO SYOG TIDB TOW2 TWTF WES2 WILL WTZR WUHN SYOG
5 | GRG | WES2 WTZR
5 | MIT | 22 4 28 SPT0 SPT0
6 | EMR | 4 4 8
6 | GFZ | 1 2 3 6 30 1 3 6 30
6 | GRG | 4 4 HYDE HYDE
6 | JPL | 4 8 SCOR
6 | MIT | 4 8 10 11 18 22 28 32 5 8 18 22 CONZ HOB2
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 | GFZ | ~09:05 | ~ 0.13 ns
3 | GRG | ~13:40 | ~ -0.21 ns
6 | MIT | ~01:00 | ~ -0.05 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
2 | COD | 8
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 G08 | | | | | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -2.0 -1.0 -3.0 -18 -4 16 .70
EMR | 0 | 2.5 6.0 14.0 56 14 -11 .40
ESA | 0 | .6 -2.4 -.5 -25 -19 42 .68
GFZ | 0 | -.1 .5 -2.3 -30 -60 19 .67
GRG | 0 | 5.7 -.1 -18.4 3 -29 74 .64
JPL | 0 | 3.3 3.9 10.4 -15 25 18 .28
MIT | 0 | 6.1 2.1 .5 17 20 -30 .62
NGS | 0 | 1.7 1.7 9.8 -7 -3 6 .69
SIO | 0 | 5.2 1.7 11.9 4 16 -3 .51
COD | 1 | -2.6 .4 -3.2 -13 -3 1 .54
EMR | 1 | 7.3 5.7 17.0 49 18 -10 .57
ESA | 1 | .7 -2.2 -.6 -21 -13 44 .72
GFZ | 1 | .0 .5 -2.3 -21 -55 18 .71
GRG | 1 | 8.8 -.5 -7.1 -5 -26 47 .89
JPL | 1 | 5.6 2.3 12.7 -62 41 -35 .23
MIT | 1 | 7.8 2.8 3.7 26 19 -30 .67
NGS | 1 | 4.0 1.1 6.7 4 -5 18 .79
SIO | 1 | 8.8 -1.6 16.1 -1 27 -13 .76
COD | 2 | -1.8 .0 -2.4 -35 30 -25 .46
EMR | 2 | 2.5 4.6 11.7 48 34 1 .42
ESA | 2 | .2 -.4 -.1 -33 -19 42 .36
GFZ | 2 | -.3 1.0 -1.1 -39 -61 8 .45
GRG | 2 | 5.2 -1.4 -13.5 7 -21 64 .84
JPL | 2 | 6.5 3.3 9.1 -26 4 -12 .28
MIT | 2 | 12.3 .7 4.0 34 22 -33 .43
NGS | 2 | 5.8 4.0 1.3 8 -15 15 .26
SIO | 2 | 4.2 .8 5.2 5 33 21 .52
COD | 3 | -1.7 .8 -1.6 -6 6 -29 .51
EMR | 3 | -4.2 .5 13.1 42 37 -16 .46
ESA | 3 | -.2 -.7 -.8 -18 -25 48 .19
GFZ | 3 | -.5 -.9 -2.1 -16 -66 23 .61
GRG | 3 | -.5 -1.3 -20.2 6 -34 59 1.14
JPL | 3 | -4.8 -3.1 3.7 -53 3 -22 .76
MIT | 3 | 8.1 -.8 2.1 34 24 -27 .73
NGS | 3 | 1.2 -2.9 .0 1 5 -10 .56
SIO | 3 | -.1 -2.4 8.0 8 2 10 .50
COD | 4 | -1.0 .5 -.4 -55 5 -49 .54
EMR | 4 | 4.2 5.2 10.0 47 48 1 .14
ESA | 4 | -.4 -.5 -.4 -29 -10 45 .33
GFZ | 4 | .0 .4 -2.0 -18 -56 12 .55
GRG | 4 | -.3 -3.0 -12.2 10 -22 61 .79
JPL | 4 | .4 -2.0 -1.0 -35 43 -20 .23
MIT | 4 | 6.5 -1.0 -4.6 22 25 -34 .47
NGS | 4 | 6.7 -1.0 -3.5 34 -14 27 .60
SIO | 4 | -.2 -5.0 1.8 -3 14 -4 .38
COD | 5 | .0 1.0 .1 -45 -32 -1 .37
EMR | 5 | 5.0 2.4 8.5 43 43 -9 .08
ESA | 5 | -.5 -.9 -.2 -54 -8 28 .15
GFZ | 5 | 1.2 .3 -1.0 -53 -71 12 .49
GRG | 5 | 7.2 -2.5 -15.7 -2 -15 35 1.24
JPL | 5 | .6 -.5 -.1 -14 41 0 .10
MIT | 5 | 3.8 1.2 -2.6 -2 21 -38 .30
NGS | 5 | 3.6 1.5 1.2 -5 -7 5 .17
SIO | 5 | 2.6 2.3 5.1 -21 12 0 .39
COD | 6 | -.3 1.8 -.5 -3 -16 -17 .72
EMR | 6 | 4.0 3.8 9.0 36 32 -6 .43
ESA | 6 | .1 -2.7 -1.6 -16 -14 34 .71
GFZ | 6 | .9 .1 -2.2 -31 -89 -1 .59
GRG | 6 | 8.2 -.7 2.6 -8 -10 19 .91
JPL | 6 | 2.2 4.0 4.7 -33 27 -38 .58
MIT | 6 | 3.9 2.4 -2.5 12 16 -41 .53
NGS | 6 | 7.0 -1.2 -3.2 25 -23 25 .36
SIO | 6 | 1.0 -3.4 -1.6 3 0 7 .56
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 1.1829.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1829.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 2.1829.[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 3.1829.[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 5.1829.0-6). 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 1829 summary. (Jan 25, 2015 - Jan 31, 2015)
Table 1.1829.a GPS week: 1829 MJD: 57047.000-57053.000
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 248| 0 1 5 17 10 -12 .01 14 13 | -505 -730 15 118
| 0 0 2 26 24 26 .03 | 303 740
emr 79| 0 0 3 0 -11 32 .22 13 13 | 4976 -368 13 153
| 0 1 1 12 19 27 .02 | 477 966
esa 150| 0 0 5 -2 4 -7 -.32 12 12 | -261 119 10 162
| 0 0 1 12 13 7 .01 | 1031 1104
gfz 199| 0 -2 -5 28 -3 9 .09 11 10 | 158 -47 11 168
| 0 1 1 17 15 14 .03 | 499 789
grg 175| 3 0 -6 -14 3 -26 .20 16 15 | 176 -197 15 167
| 0 0 3 24 31 15 .04 | 448 712
igr n/a| 0 0 0 -4 0 -6 -.13 5 5 | 4917 -625 15 91
| 0 0 0 11 9 17 .05 | 1018 825
jpl 80| 0 1 3 -29 13 -17 .17 11 11 | 5036 -389 16 115
| 1 1 0 31 29 16 .02 | 474 970
mit 348| 1 -1 -4 3 0 21 -.16 15 14 | 16 -375 25 203
| 1 0 0 36 24 22 .03 | 344 626
ngs 227| -1 1 -1 -14 -10 -9 -.09 9 8 | -393 -827 1215 2643
| 0 0 1 11 16 19 .02 | 314 752
sio 322| -1 -2 -1 19 -8 28 -.13 16 15 | --- --- --- ---
| 1 0 2 32 50 11 .02 | --- ---
Table 1.1829.b GPS week : 1829 MJD: 57047.000-57053.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 3 4 5 4 4 4 |
2 | 6 4 5 5 5 5 5 |
3 | 4 4 4 4 5 4 4 |
4 | 4 4 4 6 7 7 6 |
5 | 5 5 4 5 5 5 5 |
6 | 4 4 4 4 4 5 4 |
7 | 4 4 4 4 4 4 4 |
8 | 8 11 9 12 14 0 10 |
9 | 4 4 4 4 4 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 5 4 4 |
12 | 5 5 5 5 6 5 5 |
13 | 5 5 5 5 5 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 6 5 5 5 5 5 5 |
16 | 4 5 5 5 5 5 5 |
17 | 5 5 5 5 5 6 5 |
18 | 5 5 5 5 5 5 5 |
19 | 4 5 4 5 5 5 4 |
20 | 5 5 5 5 5 5 4 |
21 | 4 4 5 4 4 4 4 |
22 | 4 4 4 4 4 5 5 |
23 | 5 5 5 5 5 5 4 |
24 | 5 5 5 5 5 5 5 |
25 | 4 4 5 4 5 4 4 |
27 | 4 5 4 4 4 4 4 |
28 | 5 4 4 4 5 5 5 |
29 | 5 5 5 5 5 6 5 |
30 | 6 5 4 4 4 4 4 |
31 | 4 4 5 4 5 4 4 |
32 | 4 4 3 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1829.0 GPS week: 1829 Day: 0 MJD: 57047.000
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 252| -1 0 3 24 36 -13 -.03 13 13 | -161 -1573 16 107
emr 79| 0 1 2 0 3 -13 .22 13 13 | 5800 -1756 16 160
esa 150| 0 0 5 11 30 -9 -.32 12 13 | 58 -234 13 160
gfz 200| 0 -2 -2 34 -3 32 .09 11 11 | 658 -715 17 177
grg 175| 3 0 -11 -38 14 -39 .20 16 16 | 530 -851 16 148
igr n/a| 0 0 -1 -9 17 -32 -.16 5 5 | 6820 -1696 16 86
jpl 80| 2 1 4 19 -17 17 .14 13 13 | 5846 -1750 18 117
mit 348| 0 0 -4 -71 0 0 -.12 14 12 | 444 -903 32 184
ngs 229| 0 0 0 0 14 -12 -.05 9 8 | 24 -1863 1661 2912
sio 327| -2 -1 -3 -13 -96 32 -.13 14 13 | --- --- --- ---
Table 2.1829.1 GPS week: 1829 Day: 1 MJD: 57048.000
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 252| -1 1 1 8 21 -62 .01 13 13 | -226 -1634 19 127
emr 80| 0 1 2 17 -13 40 .21 13 13 | 4535 370 14 169
esa 150| 0 0 5 -8 -15 -7 -.34 12 12 | 595 -395 9 152
gfz 203| 0 -3 -4 6 -31 14 .13 10 10 | 340 -260 9 158
grg 174| 5 -1 -6 -30 29 -4 .22 16 16 | 73 131 14 158
igr n/a| -1 0 -1 -17 0 -9 -.15 5 5 | 5638 -515 14 94
jpl 80| 2 3 3 -41 -14 -22 .16 11 11 | 4606 368 17 127
mit 349| 1 -1 -4 24 24 -2 -.12 15 13 | -39 -217 24 230
ngs 229| -2 0 0 -13 -6 18 -.10 9 8 | -194 -1456 1066 2617
sio 323| -2 -2 -3 43 34 26 -.16 16 15 | --- --- --- ---
Table 2.1829.2 GPS week: 1829 Day: 2 MJD: 57049.000
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 249| 0 1 2 38 35 -14 -.02 13 12 | -679 -838 14 118
emr 80| 0 0 4 11 3 30 .21 12 12 | 4728 211 12 153
esa 150| 0 0 6 -26 5 9 -.33 13 13 | -2103 1947 10 153
gfz 200| 0 -1 -5 14 1 9 .09 10 10 | -77 323 9 174
grg 174| 2 -2 -4 -7 20 -36 .26 17 15 | -148 80 15 188
igr n/a| -1 0 0 -13 1 -24 -.16 5 5 | 5000 -656 15 92
jpl 80| 1 1 4 0 7 -31 .15 11 11 | 4789 194 16 135
mit 349| 3 -2 -3 7 -42 0 -.14 17 15 | -521 421 26 202
ngs 227| -1 0 -1 -28 0 -21 -.12 9 7 | -441 -1183 1026 2220
sio 326| -2 -2 -5 -2 -41 41 -.13 16 15 | --- --- --- ---
Table 2.1829.3 GPS week: 1829 Day: 3 MJD: 57050.000
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 249| 0 0 5 31 6 16 .08 13 12 | -374 -877 16 120
emr 80| -1 0 4 0 -29 11 .22 13 13 | 4922 1073 12 153
esa 150| 0 0 5 2 1 -6 -.30 12 12 | -432 1454 9 175
gfz 203| 0 -2 -6 12 8 17 .11 11 10 | -748 1327 10 164
grg 174| 3 0 -8 15 0 -45 .20 16 15 | -303 763 15 189
igr n/a| 0 0 0 0 -9 2 -.16 5 4 | 4110 978 17 92
jpl 80| 2 2 3 -49 -11 -29 .18 11 11 | 4949 1060 15 130
mit 349| 2 -2 -3 17 26 33 -.17 16 14 | -330 183 22 171
ngs 228| -1 1 -2 -18 -1 2 -.09 9 8 | -390 -757 1281 2562
sio 324| -1 -2 -1 31 16 24 -.10 16 15 | --- --- --- ---
Table 2.1829.4 GPS week: 1829 Day: 4 MJD: 57051.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 2 8 -28 -6 -26 .02 15 13 | -999 446 16 119
emr 80| 0 1 1 -15 -43 74 .22 13 13 | 5426 -1062 12 133
esa 150| 0 0 7 2 5 -12 -.30 13 13 | 965 -800 12 189
gfz 200| 0 -4 -4 39 16 -13 .08 11 10 | 114 -391 12 166
grg 177| 3 0 -7 20 26 -8 .16 15 15 | 92 -271 16 168
igr n/a| 0 0 1 11 0 12 -.01 6 5 | 4655 -1113 16 84
jpl 80| -1 0 2 -47 41 -17 .17 11 11 | 5516 -1114 16 96
mit 350| 1 -1 -4 43 -3 30 -.21 16 14 | 197 -1338 23 191
ngs 230| 0 1 -2 -17 -26 -13 -.11 9 8 | -973 420 1302 2487
sio 328| 0 -4 -1 38 -14 26 -.12 17 15 | --- --- --- ---
Table 2.1829.5 GPS week: 1829 Day: 5 MJD: 57052.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 1 6 0 -31 10 .00 15 13 | -726 -261 15 116
emr 80| 0 0 3 6 10 41 .22 12 12 | 4920 -644 14 144
esa 150| 0 0 3 -3 1 -12 -.30 12 12 | 71 -458 10 158
gfz 198| 1 -2 -7 44 -1 8 .09 12 11 | 89 389 11 172
grg 176| 2 0 -5 -21 -3 -20 .18 15 15 | -17 142 17 180
igr n/a| 0 0 0 11 -7 12 -.15 4 4 | 4199 -454 13 98
jpl 80| 0 0 3 -17 53 -12 .18 11 11 | 4963 -678 15 96
mit 350| 0 -1 -4 -9 11 46 -.18 15 13 | 59 -88 20 187
ngs 228| -2 2 -2 2 -28 -43 -.10 10 9 | -537 -460 871 2318
sio 315| -1 -3 1 -25 -15 40 -.17 17 17 | --- --- --- ---
Table 2.1829.6 GPS week: 1829 Day: 6 MJD: 57053.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 240| -1 3 7 49 13 1 -.00 15 13 | -373 -378 14 120
emr 80| -1 0 1 -15 -9 44 .26 12 12 | 4504 -770 13 165
esa 150| 1 0 2 3 5 -10 -.32 13 13 | -981 -678 10 151
gfz 193| 1 -1 -5 49 -11 0 .03 11 10 | 734 -1006 12 167
grg 177| 2 -1 1 -40 -62 -29 .16 14 14 | 1009 -1377 17 144
igr n/a| 0 0 0 -13 -7 -5 -.13 5 4 | 4001 -920 14 93
jpl 80| 0 0 3 -69 38 -28 .20 11 11 | 4584 -807 16 110
mit 345| 0 -2 -4 10 -16 45 -.17 14 13 | 306 -683 32 259
ngs 221| -1 0 -4 -25 -23 1 -.06 10 8 | -246 -494 1301 3391
sio 311| 0 -2 2 61 53 7 -.13 15 13 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1829.0 GPS week: 1829 Day: 0 MJD: 57047.000
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 14 9 12 4 13 12 8 7 4 | 61 64 64 62 64 60 69 59 60 63 62
2 | 14 16 9 10 19 5 28 13 9 13 5 | 36 32 31 36 35 29 33 32 30 37 31
X3 | 8 8 15 9 --- 3 12 11 7 8 3 | 41 41 47 37 --- 38 42 33 38 40 38
4 | 13 10 8 6 14 5 11 11 9 9 3 | 48 47 46 47 45 47 47 45 45 45 45
5 | 18 15 13 15 17 6 13 17 9 17 5 | 48 45 40 36 34 36 44 37 37 40 38
6 | 15 11 13 9 15 3 9 9 5 12 3 | 70 73 77 80 79 74 74 74 76 78 75
7E | 9 17 9 9 18 4 13 11 10 10 4 | 28 27 22 30 25 22 29 25 27 24 25
X8E | 32 20 16 14 16 8 19 18 21 --- 7 | 54 33 40 42 10 41 37 43 44 --- 41
9 | 8 8 18 7 13 4 9 11 5 10 3 | 37 40 31 35 41 34 40 34 35 37 35
10 | 13 10 13 10 12 3 9 12 12 13 4 | 36 35 33 43 44 34 35 41 30 40 36
11E | 10 12 8 6 15 4 10 10 8 7 3 | 59 65 64 63 62 63 67 62 62 62 62
12 | 18 14 11 16 20 4 15 15 10 13 5 | 33 33 28 39 37 27 33 30 31 30 30
13 | 10 16 16 13 21 3 13 14 10 13 5 | 34 41 34 46 55 37 42 38 42 34 39
14 | 12 14 14 13 18 4 16 16 10 15 5 | 34 32 31 44 43 32 32 38 33 35 33
15 | 16 14 15 14 18 4 16 16 14 18 5 | 48 50 48 50 49 45 49 41 48 50 46
16 | 14 13 11 11 14 6 11 11 9 18 4 | 32 28 26 33 28 26 29 26 27 26 26
17 | 10 16 10 12 18 5 12 15 8 13 4 | 25 32 23 28 32 22 30 21 25 27 24
18 | 15 13 14 13 15 5 12 11 10 17 4 | 31 28 33 39 34 28 32 32 30 34 30
19 | 9 14 10 11 15 4 12 13 10 13 4 | 26 27 22 26 28 21 29 20 24 24 22
20 | 12 11 16 12 13 5 10 20 10 18 5 | 31 34 30 40 38 32 35 39 30 36 33
21 | 13 14 8 8 16 4 11 9 8 14 4 | 45 42 43 46 46 41 45 43 45 48 43
22 | 11 11 14 9 13 6 10 11 8 16 4 | 39 39 40 47 45 40 41 43 43 43 41
23 | 13 12 15 10 14 4 12 19 8 19 4 | 31 32 24 33 33 26 34 27 25 24 27
24E | 20 11 15 10 21 5 11 21 8 12 5 | 29 29 32 29 36 25 26 27 27 27 26
25 | 10 12 12 11 15 4 11 10 7 12 4 | 24 34 32 30 33 26 32 25 27 29 28
27 | 10 10 14 9 12 6 11 10 8 18 4 | 32 32 35 29 28 29 33 27 31 35 30
28 | 12 13 11 12 16 7 13 19 9 13 4 | 28 34 26 32 34 26 32 34 27 31 28
29 | 16 17 7 13 13 4 14 14 11 17 5 | 35 34 27 33 29 27 32 27 28 33 29
X30E | 22 27 14 11 17 5 15 11 12 --- 6 | 37 35 30 27 28 24 28 26 27 --- 26
31E | 15 12 9 8 16 3 11 14 14 10 4 | 29 29 27 31 34 27 31 28 33 32 29
32 | 10 13 9 7 11 5 8 11 7 13 3 | 17 19 16 22 23 15 21 18 16 18 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 13 12 11 16 5 13 14 9 14 |T 37 37 35 39 38 34 38 35 35 37 35
WRMS | 13 13 13 11 16 5 13 12 8 13 |NE 33 34 31 36 36 30 34 31 31 33 31
MEDI | 13 13 13 10 15 4 12 12 9 13 |MD 34 34 32 36 34 29 33 33 31 35 31
Table 3.1829.1 GPS week: 1829 Day: 1 MJD: 57048.000
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 10 12 8 12 3 8 6 7 13 3 | 42 45 48 41 48 44 47 43 45 43 44
2 | 8 15 8 10 19 6 12 14 8 16 4 | 33 35 29 29 34 29 34 30 33 27 30
X3 | 7 8 11 9 --- 3 11 8 5 11 3 | 36 38 35 34 --- 32 39 31 36 34 34
4 | 10 12 8 8 18 4 10 13 10 14 4 | 69 71 70 71 67 71 70 68 71 68 69
5 | 9 13 14 12 14 6 13 16 8 21 4 | 34 40 35 34 32 32 40 31 33 34 33
6 | 12 13 13 9 19 3 8 11 9 15 4 | 52 56 53 55 54 55 59 54 55 55 54
7E | 12 19 7 10 15 3 11 14 10 11 4 | 26 30 24 31 34 25 30 28 30 28 27
X8E | 43 21 18 16 --- 10 18 29 30 --- 10 | 52 30 31 28 --- 30 33 41 38 --- 29
9 | 10 9 16 8 12 4 11 13 8 12 3 | 29 36 24 28 35 29 35 30 32 28 29
10 | 7 10 11 7 15 5 8 15 9 15 3 | 27 28 25 27 28 26 28 29 23 28 25
11E | 14 11 9 7 13 5 9 7 9 11 3 | 51 53 51 48 52 51 53 51 53 51 50
12 | 17 13 11 12 22 5 11 17 11 19 5 | 31 30 23 31 37 25 31 25 30 21 27
13 | 7 14 16 12 21 5 14 15 7 13 4 | 29 36 28 33 44 27 37 31 29 27 30
14 | 13 13 13 14 19 5 13 15 10 18 5 | 28 33 28 39 37 30 30 31 30 30 29
15 | 13 13 15 12 18 4 15 16 11 20 5 | 34 38 32 34 35 32 37 30 34 35 32
16 | 17 11 11 11 18 4 13 12 10 18 4 | 31 30 24 25 27 22 29 25 23 20 23
17 | 11 13 11 14 18 4 10 22 8 14 4 | 31 39 29 37 36 31 36 29 31 28 31
18 | 16 13 13 14 14 9 12 11 9 17 4 | 28 27 25 30 27 22 27 26 24 24 24
19 | 13 13 11 10 14 4 14 16 11 17 4 | 29 31 22 23 27 22 29 24 22 23 22
20 | 11 12 13 10 14 5 9 21 9 22 4 | 25 31 25 25 23 24 28 30 22 25 23
21 | 14 15 8 8 14 5 15 12 7 10 4 | 30 31 26 29 36 29 33 31 32 30 29
22 | 16 10 12 11 14 7 10 12 9 14 4 | 33 36 31 37 35 34 36 33 33 29 32
23 | 10 12 15 15 15 4 11 20 9 20 5 | 28 33 25 30 32 26 32 29 24 21 26
24E | 14 12 14 8 20 5 8 25 9 13 5 | 34 34 37 32 41 31 33 31 33 34 32
25 | 10 11 13 7 19 4 10 17 9 13 4 | 24 32 29 25 32 24 30 24 27 24 25
27 | 16 12 14 10 15 4 10 14 9 19 4 | 28 29 29 22 27 25 29 26 27 28 25
28 | 10 12 13 10 13 5 12 14 7 13 4 | 28 35 25 29 32 25 32 28 26 26 27
29 | 19 17 9 14 16 5 14 16 11 20 5 | 32 32 22 30 31 24 32 29 27 26 26
30E | 15 21 13 9 15 6 10 10 9 11 4 | 34 36 32 27 35 25 30 29 28 23 28
31E | 15 11 7 8 21 4 9 12 8 13 4 | 37 38 36 38 44 37 39 40 41 40 38
32 | 10 14 9 7 12 3 8 10 5 13 3 | 22 20 19 18 19 18 20 22 20 23 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 13 12 10 16 5 11 15 9 16 |T 33 35 31 32 35 30 35 32 32 31 31
WRMS | 13 13 12 10 16 5 11 13 8 15 |NE 29 32 26 29 31 26 31 28 27 26 27
MEDI | 12 13 12 10 15 5 11 14 9 14 |MD 31 34 29 30 35 29 33 30 30 28 29
Table 3.1829.2 GPS week: 1829 Day: 2 MJD: 57049.000
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 13 10 13 5 9 8 9 12 3 | 62 64 66 68 64 65 65 63 62 67 64
2E | 11 15 9 9 29 6 11 20 8 19 5 | 36 35 31 34 31 30 34 36 33 37 32
X3 | 9 9 12 10 --- 4 11 9 9 13 4 | 34 33 34 26 --- 30 34 31 33 34 31
4 | 9 13 11 8 18 5 15 12 9 12 4 | 70 74 69 70 72 70 77 72 69 70 70
5 | 8 12 15 9 12 5 11 17 8 19 4 | 34 38 34 33 33 31 37 29 32 34 32
6 | 16 12 12 10 16 4 8 12 7 15 4 | 74 74 71 75 73 73 73 74 76 76 74
7E | 12 13 9 10 17 4 13 18 7 13 4 | 25 25 20 29 25 22 25 25 26 24 23
X8E | 75 21 18 13 --- 11 --- 28 15 --- 9 | 77 26 37 33 --- 32 --- 47 36 --- 33
9 | 13 9 16 7 12 4 9 17 5 10 3 | 34 35 26 30 37 29 36 31 30 30 31
10 | 10 8 11 8 17 4 7 13 8 14 3 | 28 26 25 32 34 25 28 31 28 29 27
11E | 11 11 11 6 14 4 8 11 7 10 3 | 49 55 51 52 52 52 50 50 51 56 51
12 | 15 14 13 12 22 4 12 21 10 17 5 | 26 31 21 30 36 23 29 24 27 21 25
13 | 9 15 16 13 19 3 14 17 8 12 4 | 31 39 26 35 44 29 36 32 29 27 31
14 | 9 13 15 13 16 5 12 13 13 16 4 | 30 31 28 39 34 28 28 33 34 33 30
15 | 11 13 15 12 18 3 14 19 11 15 5 | 38 42 37 39 42 34 39 33 31 38 35
16 | 22 10 11 10 15 5 9 13 12 20 5 | 33 27 21 22 23 21 24 22 22 17 21
17 | 7 14 12 14 18 4 10 27 9 10 4 | 27 32 23 34 33 23 28 18 27 24 25
18 | 16 10 12 12 14 6 12 13 10 19 4 | 24 22 22 30 25 20 24 26 20 26 22
19 | 12 11 10 9 14 4 9 18 9 16 4 | 26 29 20 23 25 20 25 23 20 23 21
20 | 12 11 14 11 15 5 8 23 8 20 4 | 28 32 28 34 33 27 30 31 27 28 28
21 | 11 14 8 8 18 5 16 13 11 15 4 | 32 35 29 34 37 30 36 35 28 34 31
22 | 12 10 13 9 12 5 11 12 8 15 4 | 33 35 30 39 40 33 38 36 35 37 35
23 | 8 11 15 12 13 5 10 19 8 19 4 | 26 30 24 32 29 25 31 27 24 22 25
24E | 15 11 15 11 17 5 9 26 9 16 5 | 27 26 29 24 30 22 24 27 23 25 23
25 | 12 12 14 8 18 4 12 19 8 13 4 | 22 31 26 25 31 23 26 25 25 21 24
27 | 14 11 15 7 11 5 8 15 7 20 4 | 26 28 30 25 24 23 25 25 23 31 24
28 | 8 12 12 10 17 6 9 18 7 10 4 | 27 35 25 30 32 22 28 28 25 28 27
29 | 15 14 11 12 18 4 17 18 11 21 5 | 29 29 21 27 29 21 28 27 24 25 24
30E | 10 16 14 9 17 5 9 14 4 12 4 | 28 28 30 27 31 22 24 25 24 24 25
31E | 22 10 9 9 14 5 9 9 11 16 4 | 37 35 32 36 38 35 34 33 35 43 34
32 | 8 10 8 9 13 5 9 11 6 12 3 | 13 18 14 18 15 13 16 19 15 17 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 13 10 17 5 11 17 9 16 |T 35 35 31 35 36 30 34 33 32 33 31
WRMS | 12 12 13 10 15 5 11 15 7 15 |NE 28 31 25 30 31 25 29 27 26 27 26
MEDI | 11 12 12 10 16 5 10 17 8 15 |MD 30 32 28 32 33 27 29 31 28 28 28
Table 3.1829.3 GPS week: 1829 Day: 3 MJD: 57050.000
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 | 20 14 13 13 14 8 10 17 9 9 4 | 127 128 124 119 124 119 126 125 121 124 123
2E | 9 17 8 9 19 3 11 19 8 17 4 | 23 26 16 18 18 16 19 20 19 20 17
X3 | 13 11 12 14 --- 4 13 8 7 12 4 | 46 50 47 47 --- 43 52 43 47 48 46
4E | 24 16 14 12 22 9 18 14 11 20 5 | 141 139 134 135 132 136 139 139 133 142 136
5 | 8 14 14 12 12 4 12 15 9 20 4 | 39 46 38 34 35 36 44 33 36 40 36
6E | 13 13 12 10 20 7 8 11 6 13 4 | 87 87 89 91 90 84 87 91 84 94 88
7E | 15 13 8 10 15 2 13 15 9 12 4 | 25 30 24 30 28 26 29 28 32 25 26
X8E | 59 19 19 19 --- 18 15 33 24 --- 12 | 74 31 33 33 --- 39 30 48 40 --- 36
9 | 10 8 15 9 16 3 9 10 6 11 3 | 32 40 27 31 39 31 38 34 31 29 32
10 | 8 9 12 8 16 4 8 11 5 15 3 | 33 34 29 37 41 32 31 36 33 34 32
11E | 12 12 8 7 14 4 10 10 9 12 3 | 69 77 74 73 74 73 76 73 76 72 74
12 | 17 12 12 14 22 4 11 20 10 19 5 | 31 30 21 31 33 23 28 26 27 19 25
13 | 11 14 16 12 19 4 14 15 11 16 5 | 34 45 34 43 51 36 41 39 38 34 38
14 | 11 14 14 10 16 4 11 17 9 17 4 | 34 37 33 44 44 35 34 42 38 41 37
15 | 11 14 14 12 15 4 14 20 12 17 5 | 36 44 35 41 37 35 39 38 38 41 36
16 | 19 13 11 13 17 4 11 11 10 22 5 | 32 32 19 25 25 22 25 23 25 19 22
17 | 7 15 12 15 18 4 11 27 7 15 5 | 28 36 23 35 33 25 30 25 29 26 26
18 | 16 13 13 13 13 5 11 15 12 19 4 | 26 27 23 29 27 21 25 28 23 27 23
19 | 12 14 9 9 17 5 11 15 12 18 4 | 27 31 17 23 27 19 25 25 20 23 21
20 | 12 12 14 12 15 4 11 23 8 20 5 | 27 34 24 30 33 25 30 32 25 24 26
21E | 12 14 9 8 16 4 9 12 8 13 4 | 41 41 39 42 40 39 39 41 42 42 40
22 | 12 13 13 10 12 5 9 16 8 17 4 | 38 39 33 43 42 36 40 42 38 38 37
23 | 11 10 12 16 16 4 11 12 8 21 4 | 28 35 25 32 34 27 34 28 24 19 27
24E | 16 11 14 11 15 5 11 20 7 12 4 | 29 34 34 29 37 28 30 30 32 30 30
25 | 11 12 13 8 15 3 9 16 9 13 4 | 25 31 27 25 29 24 28 23 27 23 25
27 | 10 12 12 9 13 5 10 14 7 19 4 | 26 30 25 22 25 21 27 25 26 30 24
28 | 8 11 11 12 13 3 11 18 7 13 4 | 28 34 26 29 31 26 30 31 26 30 27
29 | 18 16 10 12 17 4 14 18 10 21 5 | 28 30 17 26 27 20 26 27 23 23 22
30E | 13 12 13 9 18 3 11 11 8 12 4 | 32 31 30 23 28 26 26 27 28 26 26
31E | 14 13 9 10 17 4 10 10 8 12 4 | 42 43 39 44 45 41 44 42 50 44 43
32 | 12 11 9 9 13 4 6 15 7 10 3 | 16 20 13 16 18 14 16 21 19 15 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 13 12 11 16 5 11 16 9 16 |T 42 44 37 41 43 38 41 41 40 40 39
WRMS | 12 13 12 10 15 4 11 14 8 15 |NE 30 35 26 32 33 27 32 31 29 29 28
MEDI | 12 13 12 11 16 4 11 15 8 15 |MD 32 34 29 32 34 28 30 32 32 30 30
Table 3.1829.4 GPS week: 1829 Day: 4 MJD: 57051.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 13 11 13 8 16 5 8 9 7 15 3 | 69 69 75 68 67 68 70 70 69 67 69
2E | 12 14 7 10 22 5 10 18 8 17 4 | 38 40 32 32 33 32 37 32 36 29 33
X3 | 9 9 12 14 --- 4 12 16 10 16 4 | 47 47 46 35 --- 43 47 41 43 46 42
4E | 32 29 15 15 19 6 15 15 16 22 7 | 113 116 112 115 112 111 115 112 117 109 113
5 | 11 12 16 11 12 8 13 18 11 21 5 | 41 44 39 36 35 37 43 33 37 39 37
6E | 7 9 13 7 15 6 8 11 8 11 3 | 37 40 38 36 35 35 39 38 39 40 37
7E | 11 14 8 11 10 3 14 15 11 13 4 | 30 34 28 31 33 29 32 32 36 28 30
X8E | 39 --- 15 28 --- 12 --- 28 24 --- 13 | 63 --- 9999 9999 --- 9999 --- 9999 9999 --- 9999
9 | 14 7 16 10 10 3 8 9 7 13 3 | 36 40 30 35 42 34 40 35 36 31 35
10 | 4 8 13 8 14 5 8 12 7 14 3 | 26 31 24 27 29 27 29 33 33 29 28
11E | 28 8 10 9 15 5 8 11 9 18 4 | 56 44 43 43 45 43 43 45 41 47 43
12 | 20 12 15 15 20 7 11 17 9 20 5 | 30 32 22 32 34 25 31 27 28 24 27
13 | 8 14 17 13 20 6 14 15 8 14 4 | 35 43 32 41 49 36 43 38 36 36 37
14 | 12 13 15 12 16 7 9 15 9 18 4 | 29 35 27 38 38 30 32 37 33 35 32
15 | 16 11 15 13 15 7 14 17 9 20 5 | 38 41 35 36 37 35 39 35 34 37 34
16 | 17 12 8 13 13 3 10 12 12 22 4 | 33 28 21 24 24 23 25 22 23 20 22
17 | 8 10 12 17 18 4 13 28 8 12 5 | 26 34 25 33 33 25 31 25 28 24 26
18 | 20 13 13 11 14 8 11 15 12 21 5 | 28 24 18 22 24 19 23 23 19 26 19
19 | 10 12 10 11 14 5 12 18 9 18 4 | 27 32 19 25 26 24 28 27 21 23 23
20 | 7 11 14 12 14 6 11 23 9 22 4 | 25 33 25 28 31 25 29 30 29 23 25
21E | 15 12 9 7 18 7 10 14 11 14 4 | 35 31 30 30 30 30 31 30 35 32 30
22 | 13 10 13 10 11 6 11 16 9 16 4 | 35 39 31 35 40 33 37 41 33 39 35
23 | 8 10 12 14 12 4 10 12 11 22 4 | 32 36 29 38 38 31 37 31 31 24 31
24E | 10 15 16 8 15 6 11 20 8 14 4 | 28 34 33 28 33 29 31 31 29 33 29
25 | 16 18 16 9 14 6 11 13 9 14 4 | 26 34 29 26 31 27 30 25 29 26 27
27 | 18 11 13 8 10 4 10 15 6 21 4 | 27 32 26 21 27 25 29 26 25 30 25
28 | 9 15 12 12 14 5 12 20 9 12 4 | 28 36 26 30 32 26 29 29 30 29 28
29 | 19 17 11 12 16 6 14 16 11 21 5 | 33 34 23 28 31 26 28 30 33 26 27
30E | 9 10 14 10 14 4 10 14 6 14 4 | 31 33 33 28 33 28 29 30 33 28 29
31E | 27 12 8 11 14 4 8 11 10 16 4 | 30 33 25 29 33 28 31 32 34 36 29
32 | 9 10 9 9 13 4 7 15 7 12 3 | 16 18 15 16 14 14 17 22 15 17 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 13 13 11 15 6 11 16 9 17 |T 37 38 33 34 36 33 36 35 35 34 33
WRMS | 13 13 13 10 15 5 11 14 8 15 |NE 30 34 27 30 32 28 32 30 29 29 28
MEDI | 12 12 13 11 14 5 11 15 9 16 |MD 32 34 29 31 33 29 31 31 33 29 29
Table 3.1829.5 GPS week: 1829 Day: 5 MJD: 57052.000
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 | 14 13 13 10 14 4 9 9 6 18 4 | 37 38 40 36 37 38 38 35 40 38 37
2E | 16 12 8 10 20 4 10 20 8 17 4 | 31 31 24 25 28 22 28 24 25 22 24
X3 | 7 10 12 12 --- 4 10 10 7 19 4 | 32 33 33 24 --- 29 35 29 32 34 30
4E | 38 11 11 12 19 7 13 23 15 19 6 | 141 138 135 133 135 134 137 139 137 135 136
5 | 8 14 15 11 15 5 14 19 11 20 5 | 35 40 34 36 32 31 39 30 31 36 33
6E | 17 12 12 9 15 4 8 13 9 18 4 | 39 44 41 43 42 41 45 42 42 43 41
7E | 12 13 7 11 12 2 14 14 11 14 4 | 24 27 21 28 29 22 27 27 29 22 24
X8E | 4 --- --- --- --- --- --- --- --- --- 0 | 43 --- --- --- --- --- --- --- --- --- 9999
9 | 11 9 15 10 9 3 8 9 8 13 3 | 31 36 28 33 34 28 35 30 29 29 30
10 | 6 10 13 8 14 4 9 13 10 19 4 | 39 38 35 40 41 35 37 41 36 41 37
11E | 19 10 8 10 14 4 8 12 7 21 4 | 70 71 69 68 69 69 69 70 68 72 68
12 | 18 12 15 14 20 5 9 14 11 18 5 | 26 28 17 30 31 21 28 23 25 22 23
13 | 11 14 16 12 20 4 13 13 10 14 5 | 26 35 27 33 40 27 34 26 29 25 28
14 | 12 11 15 10 16 5 12 14 14 14 4 | 25 30 28 34 34 29 29 30 33 29 28
15 | 16 13 15 13 18 5 13 16 11 19 5 | 30 34 29 31 30 26 32 28 26 32 27
16 | 14 14 9 13 14 5 10 11 13 18 4 | 27 24 20 22 24 19 24 16 20 14 18
17 | 9 16 11 19 17 4 11 30 10 13 5 | 27 37 25 33 36 26 33 26 30 24 27
18 | 22 13 14 12 15 5 11 14 15 19 5 | 26 23 21 25 20 16 24 20 21 19 18
19 | 9 13 9 14 15 4 11 14 8 18 4 | 24 27 17 21 28 18 25 21 19 23 20
20 | 9 12 14 12 11 5 9 20 12 21 4 | 25 29 25 29 26 22 27 25 23 22 23
21E | 19 11 7 9 17 5 11 13 8 14 4 | 39 37 35 36 38 36 38 39 36 37 36
22 | 17 11 12 11 13 5 11 16 14 17 4 | 35 37 32 37 40 32 40 33 39 29 34
23 | 8 11 13 15 12 3 12 11 12 23 4 | 27 31 26 31 27 25 31 24 25 21 24
24E | 16 11 14 10 17 6 10 14 9 11 4 | 23 23 29 26 30 20 24 21 22 21 22
25 | 10 14 14 10 15 5 10 10 9 13 4 | 23 30 27 27 29 23 28 22 26 24 24
27 | 13 12 12 11 9 5 10 11 8 18 4 | 25 29 24 18 23 19 23 21 21 26 21
28 | 8 17 14 12 14 4 11 18 10 12 4 | 25 33 22 26 32 22 27 25 23 22 23
29 | 15 17 12 15 18 5 15 15 11 21 5 | 31 30 19 31 29 21 26 24 25 28 24
30E | 10 12 14 10 13 3 10 12 7 13 4 | 24 27 29 23 31 21 24 26 23 20 23
31E | 17 10 8 9 11 5 9 10 9 14 3 | 32 36 31 36 40 33 38 32 37 36 34
32 | 10 10 8 10 12 3 6 13 7 12 3 | 16 16 14 18 14 12 15 18 12 18 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 12 12 12 15 4 11 15 10 17 |T 34 36 31 34 36 30 35 32 32 32 31
WRMS | 13 12 12 11 15 4 11 13 9 17 |NE 27 31 25 28 30 24 29 25 26 25 25
MEDI | 12 12 12 11 15 4 10 13 10 18 |MD 27 31 27 31 31 25 29 26 26 25 24
Table 3.1829.6 GPS week: 1829 Day: 6 MJD: 57053.000
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 13 13 10 15 3 9 8 8 13 4 | 44 45 47 43 43 43 44 44 43 46 43
2E | 17 14 9 9 15 3 11 18 8 14 4 | 36 37 31 33 32 30 33 30 33 32 31
X3 | 10 10 13 12 --- 5 11 12 7 14 4 | 60 58 61 48 --- 53 57 51 54 59 54
4E | 25 12 10 12 19 6 14 20 15 18 5 | 128 123 120 120 121 120 124 128 117 126 122
5 | 12 13 15 12 13 5 14 17 10 17 4 | 48 48 44 42 41 43 51 38 42 47 43
6E | 15 9 13 10 17 3 7 12 5 11 4 | 32 36 34 36 36 33 35 35 36 32 34
7E | 8 14 8 10 11 2 14 11 11 12 4 | 30 33 29 35 35 30 35 33 37 31 32
X8E | 50 17 15 19 --- 13 16 24 25 --- 10 | 47 15 9999 9999 --- 9999 15 9999 9999 --- 9999
9 | 12 8 17 8 9 3 6 10 6 9 3 | 37 42 31 40 45 37 43 39 38 37 38
10 | 12 10 15 10 12 4 10 12 8 11 4 | 32 32 35 43 38 32 34 37 35 34 34
11E | 19 9 9 10 11 3 8 8 9 18 4 | 58 61 64 61 60 60 59 61 65 58 60
12 | 16 11 13 14 16 6 11 16 11 16 4 | 27 30 21 32 33 23 29 26 25 23 24
13 | 13 13 14 13 18 4 12 13 9 13 4 | 36 44 37 48 55 40 47 43 43 40 42
14 | 12 9 13 12 14 5 12 14 13 15 4 | 40 38 35 49 45 38 36 46 38 42 39
15 | 16 13 14 12 12 6 13 18 13 17 5 | 38 43 38 39 39 36 41 38 38 41 37
16 | 16 13 8 15 15 4 12 11 10 22 4 | 29 26 20 26 29 22 26 21 22 18 21
17 | 12 15 12 13 18 4 11 27 10 10 5 | 32 35 27 36 38 28 33 27 29 28 28
18 | 14 13 13 11 13 7 11 17 12 20 4 | 22 26 21 27 25 18 24 26 18 26 19
19 | 9 13 10 12 14 4 13 13 11 15 4 | 27 28 18 26 28 20 27 24 20 24 21
20 | 10 12 14 11 12 4 10 15 9 18 4 | 27 31 26 34 32 27 32 26 26 28 27
21E | 17 12 8 7 18 5 11 15 9 11 4 | 30 26 23 26 26 24 28 27 25 29 24
22 | 13 12 15 10 12 7 11 14 9 18 4 | 34 37 30 38 40 32 36 40 37 35 34
23 | 7 11 14 14 12 5 10 11 8 17 4 | 30 36 30 41 38 32 39 35 32 29 33
24E | 17 13 15 8 15 5 11 14 12 10 4 | 28 32 34 31 38 29 33 29 32 31 30
25 | 10 10 15 8 13 4 10 13 7 9 3 | 24 29 27 26 29 23 27 22 22 24 23
27 | 18 11 14 9 11 4 10 9 7 14 4 | 27 29 23 20 26 19 25 20 19 26 21
28 | 10 17 13 11 15 3 11 15 7 10 4 | 25 36 24 28 36 24 30 30 25 27 26
29 | 17 12 13 13 18 5 13 16 10 20 5 | 26 28 19 30 31 21 25 25 24 24 23
30E | 12 14 14 11 17 3 10 9 7 12 4 | 31 35 33 30 36 26 31 29 29 25 29
31E | 27 9 9 10 13 4 7 11 8 9 4 | 35 33 30 36 40 32 34 35 35 36 33
32 | 14 11 8 10 14 4 7 10 8 10 3 | 15 15 12 16 16 11 16 16 15 14 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 12 13 11 14 5 11 14 10 15 |T 36 37 34 38 39 33 37 36 35 35 34
WRMS | 13 12 13 10 14 4 11 13 8 13 |NE 31 34 28 34 34 28 33 31 30 31 29
MEDI | 14 12 13 11 14 4 11 13 9 14 |MD 32 35 30 35 36 30 33 30 32 31 31
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 4.1829 GPS week: 1829 MJD: 57047.0-57053.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2961 |U 7 7 20 |U 13 12 42 |U 8 9 21 |
emr | emr 2944 | 16 10 23 |U 12 12 39 | 7 8 18 |
esa | esa 2962 | 9 9 22 |U 13 12 42 | 7 7 17 |
gfz | gfz 2956 |U 9 8 18 |U 13 13 42 |U 7 7 18 |
grg | grg 2797 | 7 8 22 |U 15 13 45 |U 8 11 26 |
igr | igr 2954 | 8 7 22 | 12 12 39 | 6 7 16 |
igs | igs 2942 | 9 8 17 | 13 12 40 | 6 8 16 |
jpl | jpl 2930 | 16 10 23 |U 13 13 40 |U 8 8 18 |
mit | mit 2962 | 14 11 29 |U 17 19 59 |U 7 9 19 |
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 5.1829.0 GPS week: 1829 Day: 0 MJD: 57047.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 8 6 14 | 11 9 36 | 9 13 30 |
emr | emr 2972 | 10 7 22 | 8 8 32 | 7 7 20 |
esa | esa 2976 | 7 6 22 | 9 9 31 | 7 6 14 |
gfz | gfz 2972 | 11 6 19 | 10 9 34 | 5 6 20 |
grg | grg 2880 | 6 5 20 | 10 9 35 | 6 5 16 |
igr | igr 2973 | 6 4 14 | 10 8 31 | 5 7 17 |
igs | igs 2972 | 7 4 17 | 10 8 32 | 6 7 16 |
jpl | jpl 2971 | 12 9 21 | 11 11 35 | 7 9 19 |
mit | mit 2976 | 9 6 19 | 12 13 33 | 6 8 18 |
Table 5.1829.1 GPS week: 1829 Day: 1 MJD: 57048.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 19 | 8 9 29 | 9 10 21 |
emr | emr 2972 | 11 6 22 | 7 12 24 | 8 7 15 |
esa | esa 2976 | 6 8 21 | 7 11 25 | 8 8 17 |
gfz | gfz 2972 | 6 7 18 | 9 13 26 | 13 10 16 |
grg | grg 2784 | 6 6 24 | 9 11 34 | 18 34 44 |
igr | igr 2947 | 6 6 15 | 7 10 23 | 7 8 14 |
igs | igs 2943 | 6 7 16 | 8 10 26 | 7 7 13 |
jpl | jpl 2972 | 8 7 21 | 9 17 26 | 9 8 15 |
mit | mit 2976 | 15 10 21 | 9 10 30 | 7 7 17 |
Table 5.1829.2 GPS week: 1829 Day: 2 MJD: 57049.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 20 | 12 11 49 | 10 12 24 |
emr | emr 2972 | 6 4 13 | 10 10 42 | 9 10 20 |
esa | esa 2976 | 7 7 16 | 11 10 44 | 8 8 19 |
gfz | gfz 2972 | 6 5 11 | 11 10 41 | 6 6 17 |
grg | grg 2784 | 5 6 18 | 13 12 37 | 9 9 16 |
igr | igr 2969 | 5 5 11 | 11 11 44 | 7 7 18 |
igs | igs 2964 | 5 6 10 | 12 11 39 | 7 8 17 |
jpl | jpl 2878 | 7 6 15 | 12 10 42 | 10 10 23 |
mit | mit 2976 | 11 8 26 | 12 10 44 | 8 10 22 |
Table 5.1829.3 GPS week: 1829 Day: 3 MJD: 57050.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 8 8 25 | 11 13 35 | 8 8 16 |
emr | emr 2972 | 9 9 23 | 11 13 34 | 8 9 14 |
esa | esa 2976 | 19 12 28 | 10 13 37 | 7 6 15 |
gfz | gfz 2972 | 16 9 26 | 12 15 38 | 6 6 16 |
grg | grg 2784 | 7 8 29 | 13 15 40 | 7 7 24 |
igr | igr 2974 | 16 9 64 | 10 14 35 | 6 6 16 |
igs | igs 2972 | 19 11 27 | 10 13 36 | 6 7 15 |
jpl | jpl 2972 | 11 11 25 | 10 13 32 | 7 7 14 |
mit | mit 2976 | 9 10 25 | 12 14 43 | 7 9 18 |
Table 5.1829.4 GPS week: 1829 Day: 4 MJD: 57051.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 8 12 26 | 22 19 61 | 9 7 17 |
emr | emr 2876 | 9 12 27 | 21 20 57 | 8 6 19 |
esa | esa 2976 | 7 11 22 | 22 21 68 | 7 5 18 |
gfz | gfz 2964 | 12 13 21 | 22 25 68 | 6 5 16 |
grg | grg 2784 | 8 13 18 | 21 19 78 | 6 6 26 |
igr | igr 2966 | 8 10 19 | 22 19 57 | 6 4 17 |
igs | igs 2956 | 8 11 18 | 23 19 66 | 6 5 16 |
jpl | jpl 2876 | 10 11 26 | 20 19 58 | 8 6 19 |
mit | mit 2976 | 25 21 53 | 23 32 62 | 8 8 18 |
Table 5.1829.5 GPS week: 1829 Day: 5 MJD: 57052.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 6 11 19 | 21 14 56 | 7 7 17 |
emr | emr 2876 | 9 13 30 | 22 14 61 | 6 8 17 |
esa | esa 2880 | 9 12 28 | 20 14 61 | 5 6 16 |
gfz | gfz 2877 | 8 10 23 | 21 14 58 | 5 8 20 |
grg | grg 2784 | 7 10 20 | 24 15 62 | 6 7 26 |
igr | igr 2880 | 7 11 19 | 20 14 58 | 5 6 15 |
igs | igs 2840 | 8 11 21 | 21 14 57 | 5 7 16 |
jpl | jpl 2875 | 9 12 28 | 20 12 61 | 6 7 14 |
mit | mit 2880 | 14 12 42 | 20 13 54 | 6 9 19 |
Table 5.1829.6 GPS week: 1829 Day: 6 MJD: 57053.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 14 | 7 9 27 | 7 7 24 |
emr | emr 2968 | 59 18 27 | 8 10 23 | 6 11 22 |
esa | esa 2976 | 6 7 18 | 8 8 26 | 7 10 18 |
gfz | gfz 2968 | 5 5 11 | 9 8 28 | 7 10 22 |
grg | grg 2784 | 6 7 23 | 11 10 29 | 6 11 29 |
igr | igr 2970 | 7 6 12 | 8 10 25 | 6 9 18 |
igs | igs 2950 | 7 7 11 | 8 10 25 | 7 11 22 |
jpl | jpl 2968 | 58 15 25 | 7 13 27 | 7 10 21 |
mit | mit 2976 | 18 9 18 | 31 38 150 | 8 14 25 |
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 6.1829 GPS week: 1829 MJD: 57047.500-57053.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 3 -19 105 74 2 | 11 21
| 24 25 43 106 4 | 2
emr uuuuu | -29 11 4 -3 14 | 37 43
| 11 18 55 94 8 | 6
esa uuuuu | -12 9 -56 -76 -4 | 16 26
| 9 11 74 67 2 | 1
gfz uuuuu | -8 -43 15 -181 -4 | 16 25
| 26 16 86 124 5 | 1
grg uuuuu | 31 23 -180 98 15 | 33 37
| 30 24 136 144 8 | 5
igr xxxxx | -18 -11 41 25 -3 | 0 19
| 9 22 68 39 3 | 1
irf xxxxx | 10 -3 -34 6 -2 | 9 19
| 5 8 41 45 7 | 1
jpl uuuuu | -7 21 171 24 -4 | 27 35
| 32 22 119 52 18 | 4
mit uuuuu | 25 -3 -133 82 0 | 28 32
| 24 25 103 41 12 | 3
ngs uuuuu | 5 5 -24 38 -6 | 14 24
| 43 3 118 120 4 | 1
sio uuxxx | 11 11 -322 -81 13 | 55 58
| 17 24 115 92 10 | 6
Table 7.1829.0 GPS week: 1829 Day: 0 MJD: 57047.500
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 | -14 -25 142 159 4 | 10 20
emr uuuuu | -30 24 -23 -47 8 | 33 40
esa uuuuu | -21 21 -191 35 -3 | 17 26
gfz uuuuu | 23 -34 96 -11 -4 | 17 24
grg uuuuu | 9 53 -327 -11 11 | 27 32
igr xxxxx | -19 21 14 45 -6 | 1 17
irf xxxxx | 8 -12 38 54 8 | 8 19
jpl uuuuu | 39 5 -80 -10 -35 | 35 37
mit uuuuu | 19 -17 73 108 17 | 24 30
ngs uuuuu | -38 4 125 -142 -5 | 16 24
sio uuxxx | 36 -6 -319 73 22 | 48 51
Table 7.1829.1 GPS week: 1829 Day: 1 MJD: 57048.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 3 -22 119 -30 6 | 8 21
emr uuuuu | -11 -9 67 0 14 | 30 38
esa uuuuu | -9 18 -114 -49 -6 | 15 26
gfz uuuuu | 20 -25 21 -130 -6 | 15 24
grg uuuuu | 13 43 -366 15 3 | 27 32
igr xxxxx | -32 -9 85 53 0 | -2 20
irf xxxxx | 9 -2 -35 14 4 | 7 19
jpl uuuuu | 4 3 242 -52 -12 | 29 36
mit uuuuu | 31 -3 -120 77 11 | 24 30
ngs uuuuu | -33 1 -18 140 -7 | 14 25
sio uuxxx | 13 17 -298 -22 13 | 49 51
Table 7.1829.2 GPS week: 1829 Day: 2 MJD: 57049.500
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 | -27 -44 14 12 5 | 10 21
emr uuuuu | -32 25 50 149 8 | 33 40
esa uuuuu | -7 19 -53 -92 -3 | 16 26
gfz uuuuu | 13 -42 91 -111 -13 | 16 24
grg uuuuu | -5 16 -273 -55 24 | 29 33
igr xxxxx | -17 -9 83 53 -4 | 0 19
irf xxxxx | 12 7 -68 58 1 | 9 19
jpl uuuuu | 14 2 290 36 -14 | 27 36
mit uuuuu | 41 40 -190 91 6 | 28 32
ngs uuuuu | -6 11 -113 0 -5 | 14 25
sio uuxxx | 17 -2 -282 -124 22 | 52 54
Table 7.1829.3 GPS week: 1829 Day: 3 MJD: 57050.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 -25 123 -76 3 | 11 21
emr uuuuu | -17 34 50 85 4 | 36 42
esa uuuuu | 2 -1 -20 -68 -1 | 16 26
gfz uuuuu | -20 -35 67 -108 1 | 15 24
grg uuuuu | 50 -1 -75 69 24 | 31 35
igr xxxxx | -4 -11 83 39 -2 | -1 19
irf xxxxx | 13 -10 1 30 -3 | 10 19
jpl uuuuu | 3 46 193 90 -7 | 26 35
mit uuuuu | 45 -10 -110 119 -1 | 29 33
ngs uuuuu | -17 2 -183 -29 -13 | 14 25
sio uuxxx | -6 -18 -212 -147 21 | 54 57
Table 7.1829.4 GPS week: 1829 Day: 4 MJD: 57051.500
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 26 128 114 -3 | 12 22
emr uuuuu | -32 5 -18 -126 25 | 39 44
esa uuuuu | -7 -4 25 -82 -3 | 17 27
gfz uuuuu | -27 -75 34 -241 -1 | 16 25
grg uuuuu | 21 -13 -57 151 16 | 35 40
igr xxxxx | -16 -52 107 35 -4 | 0 19
irf xxxxx | 16 -6 -59 -26 -9 | 11 19
jpl uuuuu | -15 39 187 89 11 | 25 34
mit uuuuu | 36 11 -231 25 -11 | 31 34
ngs uuuuu | 9 6 -101 91 -6 | 13 24
sio uuxxx | 0 20 -203 -153 13 | 58 61
Table 7.1829.5 GPS week: 1829 Day: 5 MJD: 57052.500
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 | 40 2 118 132 -3 | 12 22
emr uuuuu | -43 -15 -11 -72 18 | 41 47
esa uuuuu | -21 6 -3 -191 -5 | 17 27
gfz uuuuu | -28 -47 -73 -355 2 | 16 25
grg uuuuu | 50 20 -94 140 13 | 37 42
igr xxxxx | -17 -19 -1 -56 -6 | -1 19
irf xxxxx | 9 6 -75 -30 -9 | 10 18
jpl uuuuu | -51 2 207 22 10 | 25 34
mit uuuuu | 26 -3 -222 125 -11 | 29 33
ngs uuuuu | 38 5 -1 217 -2 | 12 23
sio uuxxx | 27 55 -531 -21 -3 | 61 64
Table 7.1829.6 GPS week: 1829 Day: 6 MJD: 57053.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -8 -42 89 207 3 | 13 22
emr uuuuu | -35 11 -88 -9 21 | 46 50
esa uuuuu | -20 1 -35 -88 -8 | 18 27
gfz uuuuu | -38 -41 -131 -313 -7 | 18 26
grg uuuuu | 82 40 -67 374 13 | 41 45
igr xxxxx | -22 1 -82 3 0 | 0 19
irf xxxxx | 0 -6 -43 -61 -8 | 10 18
jpl uuuuu | -44 47 158 -5 17 | 26 35
mit uuuuu | -26 -42 -134 31 -9 | 30 33
ngs uuuuu | 83 6 124 -14 -2 | 13 23
sio uuxxx | -9 14 -406 -172 2 | 63 65
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