[IGSREPORT-29893] Wk 2313 IGS Final Orbits
acc
acc at igs.org
Sat May 25 23:54:08 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2313 (May 05, 2024 - May 11, 2024)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
IGS0OPSFIN_${yyyy}${doy}0000_01D_15M_ORB.SP3 IGS GPS ephemeris files in SP3
format.
IGS0OPSFIN_${yyyy}${doy}0000_01D_05M_CLK.CLK IGS GPS satellite and station
clocks in clock RINEX format.
IGS0OPSFIN_${yyyy}${doy}0000_01D_01D_CLS.SUM IGS GPS clock combination summary
report.
IGS0OPSFIN_${yyyy}${doy}0000_07D_01D_ERP.ERP Earth Rotation Parameters (ERP)
and their rates as well as
Universal Time (UT1-UTC) and
Length Of Day (LOD) associated
with IGS ephemerides.
IGS0OPSFIN_20241260000_07D_01D_SUM.SUM Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, ESA, GFZ, and GRG.
The other centres are excluded because of either poorer consistency, or 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.
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 | SCRZ SCRZ
0 | GFZ | POHN POHN SCUB
0 | MIT | DARW YAR3 DARW DRAO GLPS GMSD MAR6 MKEA NOT1 SFER
0 | MIT | TLSE TONG VNDP YAR3 YEBE
1 | COD | MAW1 SVTL CZTG
1 | ESA | JFNG JFNG
1 | GFZ | LAUT LAUT
1 | GRG | MAYG SVTL
1 | MIT | DARW GMSD JFNG METG SFER STJO VNDP YAR3 YEBE DARW
1 | MIT | GMSD HERS JFNG METG SFER STJO VNDP YAR3 YEBE
2 | COD | CPVG JFNG MATE SCUB CPVG DAV1 JFNG MATE SCUB
2 | ESA | JFNG JFNG
2 | GFZ | DAV1 LAUT DAV1 LAUT
2 | GRG | 10 10 SVTL AREQ BJFS SVTL
2 | MIT | CHTI DARW FLIN GMSD HERS NLIB NOT1 NYA1 SFER CHTI
2 | MIT | DARW FLIN GMSD HERS NLIB NOT1 NYA1 SFER
3 | COD | POHN SCUB POHN SCUB
3 | ESA | 3 25 3 25 JFNG KIT3 WIND JFNG KIT3
3 | GFZ | 5 21 LAUT LAUT
3 | GRG | DAV1 SVTL DAV1 MAC1 SVTL WIND
3 | MIT | PTAG PTAG
4 | COD | 25 25 AREQ HRAO SVTL AREQ HRAO SCUB
4 | ESA | NRMD NRMD
4 | GFZ | 21 POHN POHN
4 | GRG | CZTG DAV1 POL2 COCO CZTG DAV1 POL2 SVTL
4 | MIT | BRUX NOT1 SFER YEBE BRUX SFER YEBE
5 | ESA | JFNG JFNG
5 | GFZ | 5 AREQ LAUT AREQ LAUT
5 | GRG | AREQ CZTG DAV1 SCUB AREQ COCO CZTG DAV1 SVTL
5 | JGX | HERS HLFX NLIB SUTM
5 | MIT | BRST GMSD KAT1 KIT3 MAR6 MOBS NOT1 REYK SCH2 SFER
5 | MIT | STJ3 STR1 YAR3 YEL2 BRST GMSD HERS KAT1 KIT3 MAR6
5 | MIT | MOBS NOT1 REYK SCH2 SFER STJ3 STR1 YAR3 YEL2
6 | COD | KARR
6 | ESA | FAIR FLIN KIRU MAW1 PTVL FAIR FLIN KIRU MAW1 PTVL
6 | GFZ | DGAR POHN DGAR POHN WHIT
6 | GRG | 24 AREQ CZTG KIRU SVTL SYOG CZTG FAIR KIRU SVTL SYOG
6 | JGX | THTI
6 | MIT | DGAR FALK KOUG NOT1 NYA1 PDEL SFER THTG TRO1 VNDP
6 | MIT | WTZZ YEBE DGAR FALK KOUG NOT1 NYA1 PDEL SFER THTG
6 | MIT | TRO1 VNDP WTZZ YEBE
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. 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 | GRG | 10
3 | GRG | 3
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G03 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G04 | | | | | | | 4 |
PRN G09 | | | | | 4 | 4 | 4 |
PRN G10 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
Starting 28-Nov-2022, all IGS products, are based on the IGS realization of
the ITRF2020 reference frame (IGS20). Starting from the same date, the IGS
products are based on the repro3 standards, including long filename formats.
For more information see IGSMAIL #8238, #8256, #8274 and #8282.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .2 -.7 -.2 8 4 -6 .01
EMR | 0 | 1.6 2.0 -9.2 19 -16 23 -.07
ESA | 0 | -.0 .1 .6 -1 -15 26 -.48
GFZ | 0 | .5 .3 -.5 -1 -13 -9 .27
GRG | 0 | .4 .0 .0 41 -1 -3 -.06
JGX | 0 | .1 -1.6 -10.5 42 -34 35 .14
JPL | 0 | -2.8 1.7 1.4 7 51 -26 .79
MIT | 0 | -.4 -4.3 20.0 2 -3 17 .11
COD | 1 | -.0 -.5 .5 -2 0 -10 .08
EMR | 1 | .1 5.3 -8.8 3 -6 2 -.02
ESA | 1 | -.1 .4 .3 5 -20 13 -.33
GFZ | 1 | .3 -.3 -.8 7 -17 7 .32
GRG | 1 | -.1 1.2 -.2 27 -10 4 -.09
JGX | 1 | -2.5 -1.0 -11.8 43 -32 12 .13
JPL | 1 | -3.9 -.8 -5.7 -5 56 -45 .85
MIT | 1 | -2.8 3.0 20.5 15 3 5 .17
COD | 2 | .0 -1.0 .3 -3 -5 -6 .06
EMR | 2 | 6.3 -1.4 -10.4 -1 -21 16 .20
ESA | 2 | .2 .1 .6 -6 -14 7 -.43
GFZ | 2 | .1 -.8 -.7 -16 -21 23 .43
GRG | 2 | -.2 1.1 .5 25 -5 14 -.09
JGX | 2 | .6 -3.6 -10.9 36 -31 22 .13
JPL | 2 | -.0 1.4 2.7 -10 68 -53 .68
MIT | 2 | -1.9 -2.2 24.2 -24 -2 7 .35
COD | 3 | .2 -.6 -.2 2 4 -5 -.01
EMR | 3 | 8.3 -3.6 -7.7 2 4 -20 -.12
ESA | 3 | .0 -.1 .2 -9 -18 7 -.60
GFZ | 3 | .1 -.7 -.8 -15 -17 21 .19
GRG | 3 | .1 .2 .4 -7 -8 18 -.18
JGX | 3 | .4 -1.4 -3.7 21 -28 23 .04
JPL | 3 | 5.3 -4.3 -.6 21 59 -34 .72
MIT | 3 | 3.9 -2.6 26.4 -11 -3 14 .09
COD | 4 | .1 -.2 -.5 5 7 -4 -.03
EMR | 4 | 2.4 -5.1 -7.7 9 2 -4 -.15
ESA | 4 | .7 .3 .1 -7 -9 11 -.54
GFZ | 4 | .4 .3 -1.2 17 -14 19 .29
GRG | 4 | .1 .2 .2 1 -13 23 -.13
JGX | 4 | .3 -1.9 -2.9 15 -27 45 -.15
JPL | 4 | 2.9 -4.4 -1.5 -5 52 -13 .52
MIT | 4 | .5 -2.5 25.8 -35 -7 22 .04
COD | 5 | .1 -.2 -.4 -3 11 2 .03
EMR | 5 | 4.5 -3.5 -12.2 -14 2 -12 -.18
ESA | 5 | -.1 .3 .6 -6 -16 13 -.61
GFZ | 5 | -.2 .1 -1.1 4 -21 7 .27
GRG | 5 | .1 .5 -.6 16 1 4 -.04
JGX | 5 | 2.0 -2.8 -1.8 16 -17 28 -.01
JPL | 5 | -2.8 -9.0 .3 28 45 -14 .38
MIT | 5 | .3 -2.8 25.2 2 10 9 -.15
COD | 6 | .1 -.5 -.1 -8 6 -2 -.03
EMR | 6 | 5.7 5.7 -10.8 -6 -7 12 .11
ESA | 6 | -.1 .4 .9 -15 -25 25 -.31
GFZ | 6 | -.1 .3 -1.2 -2 -23 3 .39
GRG | 6 | .8 1.1 -.1 17 -16 16 .08
JGX | 6 | 2.0 -2.1 -9.0 24 -18 23 -.14
JPL | 6 | -4.4 -2.5 -7.8 34 30 3 .54
MIT | 6 | 3.7 1.0 9.9 -6 -2 7 .26
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.atx
The JPL final solution has not yet adopted IGS20/igs20.atx after GPS Week 2238,
which causes their orbit and clock residuals to be higher than for the other
centres; from GPS Week 2238 and until they switch to IGS20/igs20.atx, the JPL
solution is excluded from the weekly SINEX combination, as well as from orbit
and clock combinations.
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 1.2313.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2313.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 2.2313.[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 3.2313.[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 5.2313.0-6). 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 2313 summary. (May 05, 2024 - May 11, 2024)
Table 1.2313.a GPS week: 2313 MJD: 60435.000-60441.000
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 820| -1 0 0 0 20 15 -.03 7 6 | -752 260 5 88
| 0 0 0 11 10 13 .02 | 36 91
emr 100| 0 1 -1 -2 10 -11 .07 12 12 | 1712 -5966 66 120
| 2 1 1 6 18 16 .04 | 7475 15066
esa 150| 0 0 2 -8 -10 -3 -.02 11 10 | -1575 1415 6 80
| 0 0 1 7 8 12 .02 | 315 524
gfz 122| 0 0 0 20 0 -20 .11 12 10 | -145 23 9 108
| 0 1 2 11 9 17 .03 | 140 181
grg 122| 2 0 3 -5 0 15 .02 14 9 | -48 45 8 136
| 1 0 1 14 12 6 .02 | 84 107
igr n/a| 0 0 0 -7 18 -8 .01 4 4 | 2119 -778 11 77
| 0 0 1 5 10 11 .01 | 1608 808
jgx n/a| 0 0 -7 31 11 -51 -.03 12 12 | -145 590 35 398
| 0 1 2 11 10 39 .02 | 800 2094
jpl n/a| 0 0 0 19 -3 7 .16 27 27 | -1288 122 87 181
| 1 1 1 17 17 16 .03 | 1265 739
mit 357| 0 0 -1 -24 -11 7 -.02 9 8 | 5168 -6898 47 77
| 0 0 0 17 21 29 .01 | 2397 3135
ngs 292| 0 0 2 5 -25 15 -.08 11 9 | -759 269 556 743
| 1 0 4 34 28 22 .03 | 38 90
Table 1.2313.b GPS week : 2313 MJD: 60435.000-60441.000
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 | 7 11 11 7 12 11 13 |
2 | 3 4 4 4 4 4 4 |
3 | 4 4 4 20 4 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 3 3 3 3 3 3 4 |
6 | 3 3 3 4 4 4 4 |
7 | 3 3 3 3 3 3 3 |
8 | 3 3 4 3 3 3 4 |
9 | 3 3 3 3 3 3 3 |
10 | 3 4 12 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 4 4 4 4 4 4 4 |
13 | 3 3 3 3 3 3 3 |
14 | 5 5 6 6 7 7 6 |
15 | 3 3 4 3 3 4 3 |
16 | 4 4 5 4 4 5 4 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 4 4 4 4 4 |
19 | 3 3 4 4 3 4 4 |
20 | 3 4 4 4 4 4 3 |
21 | 3 3 4 4 4 4 3 |
22 | 3 3 4 4 4 4 4 |
23 | 4 4 4 4 4 5 4 |
24 | 3 3 3 3 4 4 4 |
25 | 5 6 6 7 6 5 6 |
26 | 6 6 7 7 6 5 4 |
27 | 3 3 4 4 3 3 4 |
28 | 3 3 3 3 3 3 3 |
29 | 4 4 4 4 4 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 4 |
32 | 3 3 3 3 3 3 3 |
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 2.2313.0 GPS week: 2313 Day: 0 MJD: 60435.000
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 824| -1 0 0 6 19 0 -.01 6 6 | -704 108 5 88
emr 109| -1 5 0 -8 10 -19 .04 11 11 | -1648 116 51 113
esa 150| 0 0 1 -9 -19 6 .01 10 10 | -1553 963 6 79
gfz 122| 0 0 1 5 7 -18 .12 9 9 | -352 226 8 112
grg 126| 3 0 4 7 -3 11 -.00 9 8 | -109 -148 8 122
igr n/a| 0 0 0 -4 19 -18 .02 3 3 | 2739 176 10 70
jgx n/a| 1 -1 -8 34 7 0 -.01 9 9 | -90 -164 24 96
jpl n/a| -2 4 2 16 -16 18 .11 26 26 | -2551 672 89 185
mit 357| 0 0 -2 -56 -22 31 -.03 9 7 | 9284 -12959 38 66
ngs 295| 0 0 5 8 -1 -4 -.06 10 8 | -711 133 598 827
Table 2.2313.1 GPS week: 2313 Day: 1 MJD: 60436.000
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 824| -1 0 0 -11 5 6 -.01 6 6 | -780 287 5 89
emr 102| 0 3 -2 10 31 -39 .09 10 10 | -1180 503 60 118
esa 150| 0 0 1 5 1 -5 .00 10 10 | -1034 1050 7 84
gfz 122| -1 -2 3 21 0 3 .07 10 9 | -127 53 9 116
grg 122| 3 0 3 4 26 8 .02 8 7 | -37 90 8 136
igr n/a| 0 0 0 -7 19 -2 .01 3 3 | 3302 243 10 70
jgx n/a| 0 -1 -9 28 22 -71 -.02 11 11 | -42 78 28 115
jpl n/a| 0 0 0 20 -7 -20 .16 26 26 | -1519 1135 86 175
mit 357| 0 0 0 -19 -13 19 -.01 8 7 | 6354 -5882 43 67
ngs 296| -1 0 -1 -21 -52 51 -.07 10 9 | -782 290 565 746
Table 2.2313.2 GPS week: 2313 Day: 2 MJD: 60437.000
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 825| 0 0 0 -2 29 19 -.03 8 7 | -711 225 5 89
emr 103| 0 0 -2 -8 -5 -2 .05 13 13 | -845 98 70 133
esa 150| -1 0 0 -3 -8 12 -.01 11 11 | -1745 1908 7 79
gfz 123| -1 0 0 22 -5 0 .15 13 11 | -258 138 9 109
grg 123| 1 0 3 0 -2 19 .03 36 9 | -4 -17 9 128
igr n/a| 0 0 0 1 26 6 .01 5 4 | 3386 -225 11 81
jgx n/a| 1 -1 -12 37 -4 -93 -.04 17 17 | 3 -34 34 110
jpl n/a| 1 1 0 17 2 8 .16 27 27 | -758 828 86 187
mit 357| 0 0 0 -15 15 -24 -.03 9 8 | 6449 -6372 44 77
ngs 293| 0 0 4 -13 -27 15 -.08 10 8 | -715 224 549 706
Table 2.2313.3 GPS week: 2313 Day: 3 MJD: 60438.000
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 821| -1 0 -1 -19 31 40 -.02 9 7 | -767 284 5 97
emr 87| 3 1 -3 -7 28 -9 .07 14 14 | -679 -815 61 108
esa 150| 0 0 2 -13 -13 -4 -.03 15 10 | -1267 776 5 84
gfz 124| -1 -1 -2 15 -13 -29 .11 16 10 | 52 -258 11 111
grg 121| 0 0 4 -15 5 26 -.01 17 10 | 69 23 10 148
igr n/a| 0 0 -2 -9 32 -4 -.01 7 4 | 3505 -1431 11 74
jgx n/a| 0 0 -9 51 25 -99 -.05 15 15 | 43 49 34 111
jpl n/a| 1 0 -2 15 19 10 .19 28 28 | 363 -101 92 199
mit 357| 0 0 -1 -23 -24 -12 -.00 12 8 | 3949 -2322 72 89
ngs 290| 0 0 10 64 -50 35 -.16 14 10 | -767 281 582 792
Table 2.2313.4 GPS week: 2313 Day: 4 MJD: 60439.000
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 819| 0 0 0 8 28 13 -.03 6 6 | -736 416 6 95
emr 100| -2 0 0 -2 -7 8 .06 11 11 | 18651 -40110 67 121
esa 150| 0 0 1 -16 0 -24 -.05 11 10 | -1822 2036 6 82
gfz 122| 0 -1 -1 33 5 -21 .15 13 11 | 3 -59 11 108
grg 120| 3 0 1 -33 -10 14 .03 9 9 | 11 60 9 132
igr n/a| 0 0 -1 -14 24 -10 .02 4 4 | 2020 -1563 12 66
jgx n/a| 0 0 -6 30 3 -61 -.04 13 12 | -14 134 30 110
jpl n/a| -1 0 0 -10 -33 9 .19 26 26 | 235 -654 88 192
mit 357| 0 0 0 -31 -5 12 -.02 9 8 | 4705 -6952 50 83
ngs 289| 1 0 2 33 -41 12 -.06 11 10 | -747 433 561 740
Table 2.2313.5 GPS week: 2313 Day: 5 MJD: 60440.000
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 815| 0 0 0 0 15 20 -.05 7 7 | -770 235 5 87
emr 102| -1 0 0 0 -13 2 .14 12 12 | -1166 -1049 88 129
esa 150| 0 0 3 -11 -17 2 -.02 10 9 | -1722 1259 6 79
gfz 123| 0 1 1 36 14 -29 .07 12 11 | -156 -138 10 112
grg 122| 2 0 1 -3 -3 11 .04 10 10 | -187 122 8 154
igr n/a| 0 0 0 -10 2 0 .03 4 3 | 546 -1210 11 88
jgx n/a| 0 -2 -3 28 13 -18 -.00 12 12 | -1792 5231 65 2136
jpl n/a| -1 -1 2 35 10 30 .18 26 26 | -2091 -540 86 166
mit 357| 0 0 -1 -20 13 -27 -.04 9 7 | 3360 -6856 46 87
ngs 293| 1 0 0 -2 -34 14 -.07 12 10 | -777 241 536 774
Table 2.2313.6 GPS week: 2313 Day: 6 MJD: 60441.000
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 813| -1 -1 0 13 10 9 -.07 7 7 | -801 267 5 77
emr 103| 0 1 0 -4 26 -18 .07 11 11 | -1147 -505 65 122
esa 150| 0 0 4 -9 -16 -14 -.03 10 9 | -1886 1918 6 79
gfz 122| 0 -1 0 11 -3 -47 .10 11 13 | -181 201 9 94
grg 122| 3 1 4 -1 -6 19 .03 10 9 | -79 186 9 137
igr n/a| 0 0 0 -8 6 -27 .02 3 3 | -661 -1439 13 90
jgx n/a| 0 0 -5 11 12 -16 -.04 10 10 | 876 -1161 34 111
jpl n/a| 0 0 0 43 0 -5 .15 26 26 | -2700 -484 87 164
mit 357| 0 0 0 -1 -44 51 .00 9 8 | 2081 -6944 36 73
ngs 293| 0 0 -2 -33 26 -13 -.08 12 10 | -818 285 503 622
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 3.2313.0 GPS week: 2313 Day: 0 MJD: 60435.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 9 --- --- --- 10 6 --- --- 12 --- 7 | 55 --- --- --- 53 55 --- --- 58 --- 55
2 | 7 9 8 8 9 4 10 11 7 11 3 | 32 33 33 33 33 32 31 32 35 33 32
3 | 6 12 9 7 8 2 5 10 16 8 3 | 462 457 461 460 464 461 461 458 460 461 460
4 | 4 22 3 6 5 2 6 50 10 8 3 | 27 36 28 29 29 28 28 43 31 30 28
5 | 8 9 5 10 8 2 9 9 9 10 3 | 29 29 29 32 33 30 33 31 28 35 30
6 | 5 10 9 6 6 4 7 9 4 11 2 | 38 32 37 34 38 34 31 38 34 34 35
7 | 4 8 8 7 5 4 7 9 8 7 2 | 59 59 59 56 58 57 57 61 59 57 58
8 | 5 10 9 8 6 2 6 9 7 10 3 | 25 28 27 25 24 25 28 27 28 26 25
9 | 3 10 6 6 4 2 6 11 6 9 2 | 27 35 29 28 28 28 27 34 28 29 28
10 | 6 9 10 7 10 3 7 8 9 7 3 | 343 345 341 347 340 343 341 342 347 343 343
11 | 7 9 16 8 8 3 8 63 7 10 3 | 30 30 35 32 35 32 30 41 32 35 32
12E | 5 12 13 8 8 3 13 14 6 8 3 | 58 62 65 61 56 60 60 61 58 57 59
13 | 8 7 7 6 6 3 5 8 10 8 2 | 19 23 21 24 20 20 21 22 20 22 20
14E | 5 8 24 10 12 4 7 50 9 16 4 | 34 39 47 32 37 36 37 45 35 32 35
15 | 4 9 5 10 5 3 10 6 9 9 3 | 30 28 29 32 26 29 32 29 27 27 28
16E | 6 13 13 11 10 3 16 13 7 11 4 | 27 34 34 29 23 29 29 31 26 30 27
17 | 6 8 7 8 6 3 6 10 5 7 2 | 31 33 32 33 31 32 32 34 31 32 31
18 | 7 9 15 8 7 4 9 61 8 12 3 | 36 37 36 40 37 36 36 42 37 37 36
19 | 4 10 6 9 7 3 12 8 4 9 3 | 30 31 32 34 31 31 30 30 32 33 31
20 | 8 10 6 13 9 3 8 10 4 11 3 | 99 96 97 98 96 96 96 96 95 97 97
21 | 7 7 6 10 8 4 11 10 7 10 3 | 35 35 33 36 34 32 29 36 33 32 33
22E | 6 7 7 9 8 2 9 11 7 10 3 | 31 35 36 33 32 33 32 35 32 35 32
23 | 6 8 15 7 10 4 8 62 6 11 3 | 60 58 64 62 59 60 58 79 62 60 60
24 | 6 10 9 6 7 2 10 9 6 7 2 | 36 38 34 34 32 35 39 38 34 31 34
25E | 10 11 16 21 19 3 12 16 12 9 5 | 86 85 88 86 87 85 91 77 89 85 86
26E | 7 20 10 17 20 3 8 19 24 16 6 | 69 71 69 68 65 66 63 68 68 69 66
27 | 5 7 8 8 6 2 6 7 5 9 2 | 28 29 32 27 27 30 30 29 27 28 28
28 | 4 10 6 7 8 3 7 48 7 10 2 | 52 50 51 52 55 51 53 60 51 49 51
29 | 4 9 6 8 6 2 16 9 7 13 3 | 26 25 25 31 26 27 27 26 27 27 26
30 | 4 7 9 6 6 3 5 8 6 7 2 | 38 39 37 36 38 37 38 41 37 35 37
31 | 3 9 7 8 9 3 7 12 7 10 2 | 48 49 48 48 45 48 51 52 46 49 47
32 | 3 10 8 9 5 2 8 12 8 9 3 | 28 32 28 26 27 27 23 32 29 27 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 11 10 9 9 3 9 26 9 10 |T 63 64 65 64 63 63 63 66 63 63 63
WRMS | 6 11 10 9 8 3 9 26 7 8 |NE 35 35 35 36 35 34 34 38 35 35 34
MEDI | 6 9 8 8 8 3 8 10 7 10 |MD 34 35 35 34 34 33 32 38 34 34 33
Table 3.2313.1 GPS week: 2313 Day: 1 MJD: 60436.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 16 --- --- --- 10 13 --- --- 16 --- 10 | 53 --- --- --- 55 53 --- --- 58 --- 54
2 | 9 9 9 7 8 4 12 8 7 14 3 | 21 22 23 22 22 20 21 21 19 22 20
3 | 6 10 9 8 7 3 8 11 13 9 3 | 397 394 394 397 400 397 396 398 395 397 396
4 | 4 21 4 7 7 3 10 49 9 10 3 | 15 22 16 19 19 14 19 23 17 14 14
5 | 5 8 7 11 6 2 11 10 9 9 3 | 30 28 29 32 31 29 31 30 27 27 29
6 | 8 13 9 7 7 3 10 10 5 8 3 | 27 23 27 29 26 25 25 28 25 23 25
7 | 5 7 7 5 5 3 11 8 8 8 2 | 34 35 32 35 33 34 34 38 34 37 34
8 | 4 8 8 8 6 2 10 8 6 9 2 | 24 23 25 23 22 23 25 24 25 26 23
9 | 5 9 6 5 5 2 9 11 5 11 2 | 24 32 25 23 25 24 25 31 22 23 24
10 | 8 9 11 11 10 4 9 12 11 8 3 | 357 359 360 361 359 359 356 360 361 358 359
11 | 7 10 14 8 7 3 10 62 5 11 3 | 28 30 32 33 33 29 31 36 32 29 30
12E | 5 12 12 11 7 5 15 12 7 11 3 | 50 52 55 49 50 51 55 52 48 45 50
13 | 5 6 7 6 4 3 8 7 8 8 2 | 16 21 19 16 18 16 19 22 17 15 17
14E | 7 9 25 13 11 5 10 53 9 11 4 | 20 25 28 23 22 22 23 29 23 18 21
15 | 5 8 6 7 4 3 10 9 7 8 2 | 20 22 19 23 20 20 23 26 22 21 20
16E | 5 11 13 8 9 5 16 11 9 9 3 | 29 34 35 31 29 30 31 30 29 28 30
17 | 7 10 6 7 6 3 10 9 4 8 2 | 24 27 24 27 24 24 25 29 25 27 24
18 | 7 10 15 12 7 5 10 60 6 10 3 | 35 37 36 41 37 35 38 41 37 36 36
19 | 7 11 7 8 7 3 14 8 5 8 3 | 20 23 25 27 24 22 25 25 25 25 23
20 | 6 9 8 10 12 4 11 9 6 8 3 | 95 97 96 94 91 95 96 97 93 95 94
21 | 8 7 7 7 7 4 13 9 8 12 3 | 28 29 26 28 28 24 25 27 26 23 26
22E | 6 7 7 8 6 3 12 7 7 7 3 | 23 24 23 18 22 22 23 25 22 22 21
23 | 6 9 14 10 11 3 10 58 7 11 3 | 45 45 47 45 45 43 44 53 45 44 45
24 | 5 7 10 7 6 3 12 11 6 7 2 | 29 31 29 29 30 29 31 36 29 26 28
25E | 10 12 16 21 18 3 11 17 12 12 5 | 52 53 53 54 53 51 53 46 54 49 51
26E | 12 11 14 29 11 4 10 --- 15 14 5 | 51 50 52 59 49 49 49 --- 50 47 49
27 | 5 8 9 7 6 2 11 8 7 9 2 | 25 26 28 25 25 26 26 27 25 30 25
28 | 5 10 6 8 9 3 9 49 6 9 3 | 37 38 38 39 41 38 40 45 39 39 38
29 | 5 11 6 8 5 3 17 12 5 14 3 | 23 21 19 25 22 21 22 25 23 22 21
30 | 5 7 9 7 5 3 9 9 7 6 2 | 25 29 26 24 26 25 25 30 24 27 25
31 | 5 9 7 5 9 4 12 10 8 10 3 | 34 35 30 31 32 32 34 37 29 33 31
32 | 4 12 7 7 5 3 10 14 8 7 2 | 21 27 21 19 19 20 19 27 20 18 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 10 10 10 8 3 11 26 8 10 |T 53 55 54 54 54 53 54 57 53 53 53
WRMS | 6 10 10 9 7 3 11 26 7 9 |NE 26 28 27 28 27 26 27 31 27 26 26
MEDI | 5 9 8 8 7 3 10 10 7 9 |MD 28 29 28 29 28 26 26 30 26 27 26
Table 3.2313.2 GPS week: 2313 Day: 2 MJD: 60437.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 12 --- --- --- 13 13 --- --- 18 --- 10 | 34 --- --- --- 34 30 --- --- 29 --- 30
2 | 9 8 9 7 10 5 14 10 10 10 3 | 34 32 34 35 36 34 33 35 35 33 33
3 | 7 14 12 7 11 4 11 11 12 6 4 | 618 617 625 615 620 616 616 616 621 618 619
4M | 4 20 7 7 5 3 12 46 10 6 3 | 22 27 22 24 22 21 22 30 23 22 21
5 | 5 8 4 10 7 3 12 10 8 11 3 | 29 30 30 34 31 31 31 32 29 38 31
6 | 6 13 10 8 6 3 13 9 5 8 3 | 41 37 42 41 41 40 36 42 38 39 39
7 | 6 8 6 9 9 4 13 8 6 8 3 | 52 51 51 48 52 49 49 53 49 49 50
8M | 8 10 9 12 9 3 9 10 8 9 3 | 27 27 28 27 26 25 22 31 25 27 25
9M | 7 12 6 8 4 3 12 12 6 8 3 | 26 35 30 28 27 27 27 35 28 29 28
10 | 19 40 26 25 195 17 57 42 25 18 12 | 969 972 978 981 905 975 962 973 975 969 973
11 | 6 9 14 14 8 2 14 64 5 10 3 | 26 29 29 30 31 27 30 32 27 26 27
12E | 4 11 13 9 12 5 19 13 6 10 4 | 28 31 32 31 26 30 31 30 29 31 29
13 | 7 7 7 9 5 3 12 9 8 9 3 | 21 26 25 28 23 25 24 29 23 28 24
14E | 8 9 26 20 14 4 14 53 13 15 5 | 34 39 46 31 39 36 35 42 34 34 35
15 | 6 10 7 10 5 3 17 10 7 11 3 | 25 25 26 29 24 26 29 29 23 24 24
16E | 7 13 13 12 10 4 19 13 11 12 4 | 24 25 27 27 23 24 25 24 26 25 24
17 | 7 11 8 11 7 3 14 9 6 9 3 | 29 34 31 30 31 30 28 34 28 31 29
18 | 10 11 14 8 9 5 14 62 5 10 4 | 26 31 29 30 30 28 29 34 28 27 28
19 | 5 13 8 10 8 3 15 8 7 8 3 | 34 35 37 35 33 35 35 36 33 36 34
20 | 6 9 6 14 9 5 14 9 6 11 3 | 101 101 100 99 99 100 97 99 102 102 100
21 | 9 7 6 6 10 4 15 9 9 10 3 | 34 33 33 34 37 32 32 34 33 31 32
22E | 9 7 8 10 7 4 16 8 7 11 3 | 27 29 29 26 29 27 29 29 27 30 27
23 | 6 11 13 7 11 4 15 59 7 12 4 | 49 47 51 50 50 48 43 64 50 49 48
24 | 7 8 9 5 9 3 17 10 7 7 3 | 31 30 32 32 26 31 35 35 28 29 29
25E | 11 16 16 13 26 6 10 21 14 12 6 | 58 58 60 58 58 57 59 72 57 51 56
26E | 13 12 16 44 5 4 13 14 12 10 7 | 38 39 42 56 41 40 42 43 43 43 40
27M | 10 8 8 15 11 3 12 7 6 10 3 | 29 28 31 34 31 29 25 31 29 34 29
28 | 5 12 7 11 9 3 12 46 7 7 3 | 44 44 43 44 45 44 44 45 42 41 42
29 | 6 8 6 8 9 4 21 11 6 11 3 | 25 21 22 27 25 24 23 26 24 23 23
30 | 6 9 9 10 10 3 12 9 6 10 3 | 40 42 40 36 40 38 41 42 38 38 38
31 | 5 9 8 8 9 3 15 11 7 6 3 | 50 51 50 52 45 49 52 54 45 45 48
32 | 5 12 9 7 6 3 12 14 9 8 3 | 25 31 23 22 24 24 23 31 25 21 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 11 13 36 5 17 27 9 10 |T 82 85 86 86 81 82 84 88 82 84 82
WRMS | 7 13 11 11 9 4 17 27 8 8 |NE 32 33 33 34 33 32 32 36 32 32 32
MEDI | 7 10 9 10 9 3 14 11 7 10 |MD 31 33 32 34 31 31 32 35 29 33 30
Table 3.2313.3 GPS week: 2313 Day: 3 MJD: 60438.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 9 --- --- --- 12 10 --- --- 10 --- 7 | 47 --- --- --- 46 42 --- --- 39 --- 43
2 | 6 9 8 7 12 5 14 9 8 11 3 | 34 34 33 33 31 33 34 31 34 37 33
3M | 35 56 63 52 78 37 38 53 45 46 19 | 925 931 925 933 924 930 921 929 902 929 922
4M | 5 19 7 6 10 3 13 47 14 10 4 | 52 55 53 53 54 53 55 54 53 57 53
5 | 6 10 6 11 8 2 13 11 9 9 3 | 36 34 34 35 38 34 33 35 35 39 35
6 | 8 11 8 11 9 4 12 10 6 11 3 | 39 37 38 35 38 35 32 38 37 35 36
7 | 3 6 7 7 7 4 13 7 7 9 2 | 56 56 53 55 52 53 53 58 51 46 52
8 | 7 10 10 8 7 3 9 9 9 11 3 | 30 33 32 31 28 30 29 33 31 27 29
9M | 5 10 7 5 7 3 12 11 9 10 3 | 105 106 107 109 105 105 103 110 108 102 105
10M | 9 8 11 8 13 5 11 9 12 7 4 | 595 595 592 596 594 593 596 592 599 595 594
11 | 7 11 12 13 8 3 14 60 5 10 3 | 26 30 30 34 31 27 27 35 28 28 28
12E | 6 12 11 10 10 3 18 10 6 12 4 | 31 34 33 36 30 31 34 35 31 34 31
13 | 6 6 7 9 5 3 10 10 8 12 3 | 24 28 24 26 24 23 24 27 23 24 24
14E | 8 8 22 11 16 5 14 50 16 15 5 | 36 38 42 36 38 36 36 41 32 30 35
15 | 5 11 7 8 6 3 15 7 7 10 3 | 31 30 30 32 28 29 30 32 27 27 28
16E | 7 10 12 7 11 4 16 11 11 12 4 | 31 29 32 30 29 29 28 29 31 32 29
17M | 7 9 5 8 7 3 14 9 6 10 3 | 31 35 32 34 30 33 32 36 33 32 31
18 | 7 10 13 6 8 5 14 63 9 9 3 | 29 32 31 31 33 29 32 39 27 28 29
19 | 7 9 6 13 7 3 16 7 7 10 3 | 30 35 33 36 32 32 29 34 34 32 32
20E | 5 10 7 16 7 3 14 10 9 13 3 | 97 99 96 97 96 95 94 94 96 97 96
21 | 7 8 7 9 12 4 15 9 8 9 3 | 39 39 37 40 37 37 38 37 37 38 37
22E | 14 8 6 13 12 4 15 8 7 13 4 | 31 35 34 36 31 33 33 32 33 32 31
23 | 6 10 12 8 11 4 15 60 6 11 3 | 44 41 47 45 48 43 39 60 44 49 44
24 | 9 7 8 6 9 3 14 12 8 9 3 | 34 35 31 32 29 31 36 37 30 29 31
25E | 11 17 18 24 19 7 13 --- 15 19 6 | 60 59 61 65 67 58 58 --- 63 60 60
26E | 11 9 15 47 13 4 11 11 11 9 7 | 38 38 39 50 40 36 37 34 37 35 37
27 | 10 7 8 9 8 3 9 8 8 13 3 | 29 32 30 27 27 28 29 31 31 31 28
28M | 6 9 7 5 10 3 12 53 6 12 3 | 29 25 27 23 24 24 26 37 24 23 24
29 | 6 10 5 10 6 3 20 11 7 8 3 | 25 22 23 28 24 24 22 25 25 29 24
30 | 5 8 9 7 8 4 12 8 6 9 3 | 36 37 31 34 33 33 35 36 32 28 32
31M | 5 8 8 6 9 3 14 9 9 10 3 | 42 43 40 40 40 41 43 46 37 38 40
32 | 5 13 7 8 8 3 9 12 7 10 3 | 27 32 27 25 28 25 24 36 27 29 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 15 16 17 7 15 28 12 14 |T 84 87 86 87 84 83 85 89 83 85 83
WRMS | 7 14 10 10 10 4 14 28 8 10 |NE 34 34 33 34 33 32 32 37 32 33 32
MEDI | 7 10 8 8 9 3 14 10 8 10 |MD 34 35 33 35 33 33 34 36 33 32 32
Table 3.2313.4 GPS week: 2313 Day: 4 MJD: 60439.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 13 --- --- --- 10 10 --- --- 23 --- 11 | 32 --- --- --- 33 34 --- --- 47 --- 35
2 | 6 9 7 9 12 4 11 8 8 13 3 | 19 18 19 21 20 20 22 20 20 21 18
3 | 8 15 9 8 9 4 10 12 11 12 4 | 579 571 572 577 578 575 573 575 576 577 576
4 | 6 20 5 8 8 2 11 45 12 8 3 | 97 99 101 101 101 100 101 100 99 99 99
5 | 7 10 6 8 7 2 12 12 8 12 3 | 23 19 22 23 24 22 23 21 24 27 22
6 | 6 14 8 14 10 4 11 8 6 8 3 | 26 27 28 26 27 24 25 29 24 26 25
7 | 5 7 5 8 10 3 11 10 6 10 3 | 42 40 39 43 42 40 40 43 38 34 39
8 | 6 10 10 7 6 3 9 7 6 9 3 | 22 24 26 26 22 24 24 25 24 23 23
9 | 4 10 5 7 7 2 10 12 8 7 2 | 348 347 347 347 346 347 346 347 348 347 348
10 | 8 9 11 10 14 5 10 9 12 8 4 | 759 761 760 762 744 759 755 760 762 755 759
11 | 6 12 12 11 8 3 14 59 4 13 3 | 21 25 27 29 28 24 25 37 24 21 23
12E | 4 14 12 10 11 4 16 9 8 14 4 | 34 38 34 36 30 32 34 35 33 33 33
13 | 5 7 8 8 7 3 8 10 9 11 3 | 17 20 20 20 19 20 19 25 19 24 18
14E | 9 9 29 18 14 6 10 53 23 17 6 | 28 26 34 25 28 26 28 31 31 29 26
15 | 5 8 6 7 7 3 15 8 9 9 3 | 30 28 28 32 27 29 31 32 28 28 28
16E | 7 11 13 9 9 5 18 10 10 16 4 | 25 25 26 25 23 23 25 24 26 24 23
17 | 4 10 6 8 6 4 11 8 5 8 2 | 27 28 25 29 26 27 25 30 25 28 26
18 | 8 12 16 9 9 5 15 61 6 12 4 | 23 28 29 29 27 25 27 38 26 25 25
19 | 5 13 6 10 7 4 15 7 7 8 3 | 29 29 29 33 29 29 28 31 30 29 28
20E | 7 9 6 13 6 4 13 10 6 12 3 | 79 78 78 78 78 78 78 79 78 75 78
21 | 7 9 5 11 14 5 13 8 8 12 3 | 18 23 18 22 17 18 20 23 22 21 18
22E | 7 7 7 11 9 3 13 7 8 11 3 | 23 25 26 29 25 24 24 27 28 27 24
23 | 6 12 14 9 14 3 14 58 9 13 4 | 35 35 37 38 37 35 36 45 37 34 35
24 | 6 10 9 14 9 3 14 8 8 11 3 | 21 23 22 23 19 21 26 26 20 21 20
25E | 7 17 20 31 11 6 16 --- 13 16 6 | 66 65 73 75 70 66 68 --- 66 66 66
26E | 8 10 13 38 9 3 11 12 15 13 6 | 36 37 37 47 37 35 37 36 37 36 36
27 | 5 11 8 6 8 3 9 9 6 11 3 | 24 26 26 28 24 24 24 27 24 25 24
28 | 4 9 7 7 9 3 11 52 7 10 3 | 71 69 74 71 71 71 71 77 70 67 70
29 | 5 12 8 7 7 3 21 12 7 12 3 | 31 29 29 34 33 30 34 32 32 33 31
30 | 5 7 9 7 8 3 9 10 7 12 3 | 32 33 30 31 32 31 30 35 31 31 30
31 | 4 9 8 8 10 3 13 10 8 11 3 | 43 46 45 45 41 44 45 48 40 43 42
32 | 5 14 7 12 7 4 9 12 9 9 3 | 17 28 17 17 17 17 19 30 16 20 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 11 11 13 9 4 13 26 9 11 |T 83 86 86 87 83 83 85 89 84 85 83
WRMS | 6 11 10 11 9 4 12 26 8 10 |NE 25 27 26 28 26 25 27 31 26 26 25
MEDI | 6 10 8 9 9 3 11 10 8 11 |MD 29 28 29 31 28 29 28 32 30 29 28
Table 3.2313.5 GPS week: 2313 Day: 5 MJD: 60440.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 16 --- --- --- 8 11 --- --- 17 --- 10 | 41 --- --- --- 46 46 --- --- 45 --- 43
2 | 7 9 7 9 11 4 9 11 7 14 3 | 21 23 21 20 24 20 22 21 22 25 21
3 | 9 16 9 8 9 4 8 12 10 15 4 | 199 195 195 197 201 197 197 196 194 201 197
4 | 5 23 5 6 9 3 8 48 10 9 3 | 145 147 145 145 145 146 146 146 147 143 145
5 | 7 13 6 9 8 2 13 10 6 9 3 | 26 23 23 27 25 25 24 26 25 25 24
6 | 7 16 9 7 11 3 9 10 7 8 3 | 32 30 33 32 33 30 30 31 29 31 30
7 | 5 10 6 7 10 3 10 7 8 10 3 | 46 46 46 49 48 46 45 49 44 47 46
8 | 7 13 8 9 8 3 7 7 6 12 3 | 26 30 29 28 25 27 26 29 26 28 26
9 | 4 12 5 8 6 3 9 12 6 5 2 | 636 640 639 638 639 637 637 638 636 636 637
10 | 8 11 12 13 14 4 9 10 9 11 4 | 769 768 768 776 765 770 763 770 776 768 770
11 | 7 14 13 10 9 2 11 61 5 10 3 | 25 27 28 30 29 25 24 31 28 27 26
12E | 6 12 10 13 14 4 13 8 7 12 4 | 46 46 48 53 41 48 51 47 42 47 46
13 | 6 8 8 10 8 3 9 9 9 10 3 | 17 19 19 18 15 17 17 23 18 17 16
14E | 9 10 28 19 15 7 10 54 27 17 7 | 29 29 36 27 32 29 28 33 31 28 27
15 | 8 11 6 8 9 4 14 9 9 11 3 | 23 23 19 23 17 20 21 25 19 20 20
16E | 7 12 11 13 13 6 16 11 10 15 4 | 25 29 28 29 23 28 30 29 25 28 25
17 | 7 13 5 9 7 3 10 11 5 11 3 | 24 27 22 28 25 24 23 28 21 24 23
18 | 9 15 14 8 10 4 15 60 7 14 4 | 26 27 27 28 28 24 26 32 24 26 25
19 | 5 14 6 11 11 3 14 9 6 14 3 | 31 32 32 39 31 33 32 31 34 37 32
20E | 7 10 8 12 7 3 16 9 5 10 3 | 68 65 67 66 68 66 65 65 65 65 66
21 | 6 7 6 9 10 5 11 9 8 15 3 | 24 25 21 21 24 21 22 23 25 27 22
22E | 9 7 6 8 6 3 11 9 6 16 3 | 29 29 30 33 29 30 29 29 28 30 29
23 | 6 12 16 11 14 4 14 60 6 14 4 | 40 43 46 44 41 41 42 51 44 44 42
24 | 8 12 10 7 9 3 16 9 5 11 3 | 29 31 29 30 22 29 33 34 25 30 27
25E | 8 15 17 23 10 5 14 9 7 13 5 | 83 83 87 84 87 85 84 83 89 83 85
26E | 9 11 12 29 7 3 12 10 12 14 5 | 52 51 50 54 49 49 52 44 47 49 49
27 | 7 10 8 8 8 3 8 9 6 13 3 | 33 37 34 36 31 34 33 36 34 33 33
28 | 5 11 7 6 9 3 12 47 7 9 3 | 86 87 86 87 87 87 88 91 89 87 87
29 | 7 16 7 11 9 2 19 15 4 10 4 | 25 31 23 29 29 27 34 28 25 27 26
30 | 5 9 8 7 11 3 9 9 6 8 3 | 32 32 33 33 33 32 32 36 30 32 31
31 | 5 10 8 7 8 3 13 11 7 11 3 | 40 40 38 38 36 37 39 43 37 36 37
32 | 5 12 6 11 7 3 10 11 9 10 3 | 27 36 29 27 27 28 30 33 26 27 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 10 12 10 4 12 26 9 12 |T 86 88 88 89 86 86 87 89 85 88 85
WRMS | 7 12 9 11 10 3 12 26 7 10 |NE 28 29 28 30 28 27 28 31 27 29 27
MEDI | 7 12 8 9 9 3 11 10 7 11 |MD 31 32 33 33 31 30 32 33 30 31 30
Table 3.2313.6 GPS week: 2313 Day: 6 MJD: 60441.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 16 --- --- --- 13 15 --- --- 23 --- 12 | 45 --- --- --- 50 42 --- --- 58 --- 49
2 | 8 10 6 7 10 3 9 11 9 14 3 | 32 34 35 34 35 35 36 34 32 35 33
3 | 7 12 10 7 9 3 8 13 8 16 3 | 283 283 284 281 281 282 281 281 283 281 282
4 | 5 19 4 8 7 2 10 48 10 11 3 | 245 248 248 244 248 247 247 249 245 249 246
5 | 7 11 7 10 10 3 9 12 9 11 3 | 46 40 42 47 43 42 42 43 45 46 43
6 | 9 12 10 13 10 3 9 10 8 10 3 | 46 43 50 49 46 46 41 46 45 48 45
7 | 5 8 5 8 8 3 8 8 11 8 3 | 60 56 58 63 60 59 59 61 58 59 59
8 | 5 11 9 9 10 3 9 8 14 16 4 | 42 47 44 43 40 44 46 43 47 41 43
9 | 5 11 6 7 7 2 10 12 11 12 3 | 901 903 905 906 906 903 904 904 904 904 904
10 | 9 10 11 10 11 4 5 11 7 11 3 | 486 485 487 486 486 487 482 487 484 488 486
11 | 8 12 14 9 9 4 10 61 8 14 4 | 57 58 59 59 59 57 57 66 59 59 58
12E | 7 11 11 13 14 4 14 9 9 12 4 | 46 50 48 52 42 46 52 46 44 45 46
13 | 5 8 8 7 6 2 6 9 9 7 2 | 25 29 25 26 25 26 24 32 25 28 25
14E | 9 12 26 25 11 6 8 51 18 13 6 | 71 71 72 72 65 69 70 71 68 66 69
15 | 6 9 7 6 5 3 12 9 9 10 3 | 45 45 42 45 43 43 46 47 41 41 43
16E | 6 10 11 12 9 4 14 11 10 12 4 | 30 32 26 27 29 26 29 27 29 29 28
17 | 6 9 7 9 5 3 11 10 6 7 2 | 28 30 29 32 27 29 26 33 28 29 28
18 | 10 12 14 8 9 4 8 61 8 11 4 | 50 55 49 52 51 49 49 56 46 50 49
19 | 6 9 7 8 6 3 17 8 6 15 3 | 49 46 51 54 45 49 48 49 48 53 48
20E | 6 8 8 9 9 3 11 10 7 11 3 | 82 81 82 86 82 82 80 81 79 83 81
21 | 8 9 5 6 10 3 9 10 8 14 3 | 29 35 33 32 36 32 36 31 29 32 31
22E | 7 9 7 17 10 3 7 9 10 8 3 | 27 30 26 35 26 28 28 32 30 30 28
23 | 7 11 15 7 13 3 8 61 7 12 3 | 64 66 68 66 65 65 62 76 64 66 64
24 | 9 9 10 9 19 4 7 12 6 10 4 | 32 34 31 32 33 31 30 38 29 32 30
25E | 9 12 16 32 10 5 15 9 9 11 5 | 126 123 125 129 128 128 130 121 124 130 126
26E | 8 8 10 13 8 3 8 9 14 12 4 | 51 49 49 51 50 47 49 43 54 46 49
27 | 8 12 8 7 11 2 7 13 9 15 3 | 50 64 54 54 51 53 55 56 57 55 54
28 | 6 10 7 4 10 4 9 51 7 7 3 | 67 68 67 68 73 66 68 79 66 67 68
29 | 8 14 7 8 10 3 15 12 7 10 3 | 34 34 31 36 38 34 40 36 34 37 35
30 | 5 7 9 7 7 3 6 10 9 6 2 | 38 38 39 40 38 37 36 43 37 38 38
31 | 6 13 7 7 9 3 11 9 8 12 3 | 51 53 50 51 50 51 52 55 46 54 50
32 | 4 14 6 11 6 4 8 11 8 11 3 | 28 36 29 24 28 28 28 35 26 28 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 11 10 11 10 3 10 26 9 12 |T 102 105 104 105 102 101 104 106 102 104 102
WRMS | 7 11 9 13 9 3 10 26 8 10 |NE 42 43 42 43 43 42 42 46 41 43 41
MEDI | 7 11 8 8 9 3 9 11 9 11 |MD 46 49 49 51 46 46 49 47 46 48 48
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 4.2313 GPS week: 2313 MJD: 60435.0-60441.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 10 10 29 | 0 0 0 |U 30 36 92 |
emr | emr 2938 |U 15 12 32 | 0 0 0 | 34 32 70 |
esa | esa 2976 | 11 16 30 | 0 0 0 |U 29 35 60 |
gfz | gfz 2975 |U 10 8 26 | 0 0 0 | 44 30 72 |
grg | grg 3072 |U 11 9 30 | 0 0 0 | 31 38 67 |
igr | igr 2962 | 9 8 24 | 0 0 0 | 28 45 61 |
igs | igs 2962 | 10 8 24 | 0 0 0 | 27 34 60 |
jgx | jgx 2976 |U 11 9 28 | 0 0 0 | 32 31 66 |
jpl | jpl 2934 | 13 14 30 | 0 0 0 | 32 38 75 |
mit | mit 3072 |U 10 10 28 | 0 0 0 |U 28 29 69 |
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 5.2313.0 GPS week: 2313 Day: 0 MJD: 60435.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 13 11 27 | ---- ---- ---- | 9 11 33 |
emr | emr 2964 | 12 7 33 | ---- ---- ---- | 15 18 30 |
esa | esa 2976 | 13 16 33 | ---- ---- ---- | 12 11 28 |
gfz | gfz 2976 | 12 7 26 | ---- ---- ---- | 9 11 27 |
grg | grg 3072 | 12 7 29 | ---- ---- ---- | 10 11 27 |
igr | igr 2880 | 10 7 23 | ---- ---- ---- | 10 11 25 |
igs | igs 2880 | 11 6 23 | ---- ---- ---- | 10 11 25 |
jgx | jgx 2976 | 11 6 24 | ---- ---- ---- | 8 11 25 |
jpl | jpl 2976 | 14 10 32 | ---- ---- ---- | 14 12 38 |
mit | mit 3072 | 11 8 26 | ---- ---- ---- | 10 10 28 |
Table 5.2313.1 GPS week: 2313 Day: 1 MJD: 60436.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 9 27 | ---- ---- ---- | 10 15 35 |
emr | emr 2967 | 12 10 34 | ---- ---- ---- | 15 20 36 |
esa | esa 2976 | 11 20 34 | ---- ---- ---- | 14 18 32 |
gfz | gfz 2975 | 9 8 24 | ---- ---- ---- | 10 16 34 |
grg | grg 3072 | 9 9 27 | ---- ---- ---- | 11 14 32 |
igr | igr 2976 | 8 10 24 | ---- ---- ---- | 11 16 31 |
igs | igs 2976 | 8 9 24 | ---- ---- ---- | 10 15 31 |
jgx | jgx 2976 | 9 7 25 | ---- ---- ---- | 9 16 31 |
jpl | jpl 2880 | 10 16 32 | ---- ---- ---- | 19 14 33 |
mit | mit 3072 | 8 10 26 | ---- ---- ---- | 9 12 33 |
Table 5.2313.2 GPS week: 2313 Day: 2 MJD: 60437.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 14 28 | ---- ---- ---- | 10 22 35 |
emr | emr 2959 | 19 19 42 | ---- ---- ---- | 15 17 34 |
esa | esa 2976 | 12 20 32 | ---- ---- ---- | 12 9 25 |
gfz | gfz 2976 | 11 11 26 | ---- ---- ---- | 9 9 21 |
grg | grg 3072 | 12 12 30 | ---- ---- ---- | 10 10 23 |
igr | igr 2976 | 11 12 25 | ---- ---- ---- | 9 9 23 |
igs | igs 2976 | 11 13 26 | ---- ---- ---- | 9 12 24 |
jgx | jgx 2976 | 15 19 36 | ---- ---- ---- | 12 36 48 |
jpl | jpl 2976 | 15 24 37 | ---- ---- ---- | 14 17 34 |
mit | mit 3072 | 10 12 27 | ---- ---- ---- | 9 9 21 |
Table 5.2313.3 GPS week: 2313 Day: 3 MJD: 60438.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 13 31 | ---- ---- ---- | 16 11 33 |
emr | emr 2872 | 13 10 27 | ---- ---- ---- | 16 14 27 |
esa | esa 2976 | 11 14 31 | ---- ---- ---- | 16 11 23 |
gfz | gfz 2976 | 10 9 29 | ---- ---- ---- | 11 11 25 |
grg | grg 3072 | 11 9 34 | ---- ---- ---- | 15 12 30 |
igr | igr 2976 | 9 6 21 | ---- ---- ---- | 10 11 23 |
igs | igs 2975 | 9 7 24 | ---- ---- ---- | 11 10 25 |
jgx | jgx 2976 | 11 8 33 | ---- ---- ---- | 12 13 28 |
jpl | jpl 2880 | 16 11 30 | ---- ---- ---- | 18 16 41 |
mit | mit 3072 | 8 11 32 | ---- ---- ---- | 11 22 34 |
Table 5.2313.4 GPS week: 2313 Day: 4 MJD: 60439.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 9 32 | ---- ---- ---- | 10 10 27 |
emr | emr 2868 | 14 8 32 | ---- ---- ---- | 14 12 24 |
esa | esa 2976 | 11 17 29 | ---- ---- ---- | 14 11 23 |
gfz | gfz 2976 | 10 7 25 | ---- ---- ---- | 12 11 21 |
grg | grg 3072 | 11 8 29 | ---- ---- ---- | 10 11 23 |
igr | igr 2976 | 9 7 23 | ---- ---- ---- | 10 10 22 |
igs | igs 2976 | 9 7 23 | ---- ---- ---- | 10 10 21 |
jgx | jgx 2976 | 10 6 25 | ---- ---- ---- | 9 12 20 |
jpl | jpl 2880 | 14 12 28 | ---- ---- ---- | 18 13 36 |
mit | mit 3072 | 9 8 28 | ---- ---- ---- | 10 9 24 |
Table 5.2313.5 GPS week: 2313 Day: 5 MJD: 60440.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 8 33 | ---- ---- ---- | 108 89 369 |
emr | emr 2968 | 22 19 36 | ---- ---- ---- | 97 28 171 |
esa | esa 2976 | 12 12 26 | ---- ---- ---- | 87 75 173 |
gfz | gfz 2976 | 12 7 28 | ---- ---- ---- | 205 54 264 |
grg | grg 3072 | 13 7 33 | ---- ---- ---- | 105 37 215 |
igr | igr 2976 | 11 6 25 | ---- ---- ---- | 87 74 175 |
igs | igs 2976 | 11 6 26 | ---- ---- ---- | 86 75 174 |
jgx | jgx 2976 | 13 9 29 | ---- ---- ---- | 123 24 200 |
jpl | jpl 2976 | 14 8 29 | ---- ---- ---- | 93 85 213 |
mit | mit 3072 | 12 11 29 | ---- ---- ---- | 97 36 230 |
Table 5.2313.6 GPS week: 2313 Day: 6 MJD: 60441.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 7 25 | ---- ---- ---- | 48 97 113 |
emr | emr 2974 | 11 8 23 | ---- ---- ---- | 63 113 164 |
esa | esa 2976 | 10 14 23 | ---- ---- ---- | 51 110 118 |
gfz | gfz 2976 | 9 6 23 | ---- ---- ---- | 54 98 114 |
grg | grg 3072 | 11 8 28 | ---- ---- ---- | 60 175 118 |
igr | igr 2976 | 8 8 24 | ---- ---- ---- | 58 184 126 |
igs | igs 2976 | 8 6 22 | ---- ---- ---- | 52 104 117 |
jgx | jgx 2976 | 10 8 22 | ---- ---- ---- | 53 103 112 |
jpl | jpl 2976 | 11 15 23 | ---- ---- ---- | 50 112 133 |
mit | mit 3072 | 9 8 25 | ---- ---- ---- | 49 107 113 |
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 6.2313 GPS week: 2313 MJD: 60435.500-60441.500
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 | -18 5 -13 -4 -6 | 1 30
| 12 15 39 57 6 | 4
emr uuuuu | -10 9 38 33 1 | 5 28
| 24 20 83 38 10 | 4
esa uuuuu | 28 -1 64 101 -5 | 19 32
| 11 10 35 45 4 | 5
gfz uuuuu | 6 -13 -117 59 6 | 7 28
| 18 9 154 115 4 | 3
grg uuuuu | 1 8 0 61 3 | 2 26
| 7 14 46 103 3 | 4
igr xxxxx | -22 7 -25 -23 -7 | 4 27
| 10 5 38 55 4 | 4
irf xxxxx | 4 -11 14 -6 -1 | 1 27
| 12 11 27 22 6 | 5
jgx uuuuu | -23 -31 1 -46 -2 | 8 29
| 12 15 26 49 5 | 4
mit uuuuu | 7 15 -31 -174 1 | 18 33
| 25 25 58 62 6 | 4
ngs uuuxu | 13 -10 68 -135 0 | 10 26
| 67 62 147 404 6 | 3
Table 7.2313.0 GPS week: 2313 Day: 0 MJD: 60435.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -30 -10 18 57 4 | 7 32
emr uuuuu | 1 15 70 71 -16 | 11 29
esa uuuuu | 34 -1 112 71 0 | 27 39
gfz uuuuu | -25 -22 174 -76 8 | 10 31
grg uuuuu | 5 -1 -40 95 1 | 9 30
igr xxxxx | -20 15 -52 84 1 | 10 29
irf xxxxx | -6 -9 -2 20 -10 | 9 30
jgx uuuuu | -18 -21 -16 22 1 | 14 34
mit uuuuu | -19 4 -114 -233 -7 | 25 38
ngs uuuxu | 94 49 -202 438 10 | 14 29
Table 7.2313.1 GPS week: 2313 Day: 1 MJD: 60436.500
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 | -6 16 18 -17 -5 | 4 32
emr uuuuu | -32 -24 17 75 -2 | 7 29
esa uuuuu | 15 -12 26 121 -7 | 24 37
gfz uuuuu | 9 -12 -117 63 2 | 9 31
grg uuuuu | -15 5 -33 81 5 | 6 29
igr xxxxx | -25 11 -94 -6 -7 | 8 29
irf xxxxx | -12 -34 -8 4 -5 | 6 29
jgx uuuuu | -23 -25 23 -6 6 | 11 33
mit uuuuu | -30 -16 -28 -237 -5 | 22 36
ngs uuuxu | 94 51 109 172 2 | 12 28
Table 7.2313.2 GPS week: 2313 Day: 2 MJD: 60437.500
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 12 -41 63 -7 | -1 33
emr uuuuu | 3 -6 73 -37 0 | 3 30
esa uuuuu | 21 -15 96 37 -5 | 18 34
gfz uuuuu | 1 -18 -52 -34 12 | 4 30
grg uuuuu | 6 9 39 261 1 | 1 28
igr xxxxx | -30 0 -39 -23 -7 | 3 30
irf xxxxx | -3 -16 -19 -44 -2 | -1 29
jgx uuuuu | -13 -23 -48 -112 -2 | 7 31
mit uuuuu | 1 1 -80 -224 -3 | 17 34
ngs uuuxu | 22 19 35 172 0 | 8 28
Table 7.2313.3 GPS week: 2313 Day: 3 MJD: 60438.500
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 22 -29 10 1 | -6 31
emr uuuuu | -37 31 -38 49 -3 | -1 28
esa uuuuu | 32 3 79 155 -2 | 13 29
gfz uuuuu | 17 -6 -144 -49 8 | 0 27
grg uuuuu | -1 20 -43 58 -1 | -4 24
igr xxxxx | -37 7 7 -46 -6 | -2 28
irf xxxxx | 3 -7 0 -9 7 | -5 27
jgx uuuuu | -43 -53 -7 -73 1 | 2 28
mit uuuuu | 16 22 -50 -167 7 | 12 30
ngs uuuxu | 29 -96 287 -159 -8 | 5 26
Table 7.2313.4 GPS week: 2313 Day: 4 MJD: 60439.500
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 -8 44 -7 -10 | 2 26
emr uuuuu | 11 17 96 20 9 | 6 26
esa uuuuu | 14 13 16 106 -11 | 20 30
gfz uuuuu | -5 -22 -332 176 7 | 9 25
grg uuuuu | 6 30 12 -3 1 | 2 23
igr xxxxx | -27 5 -1 -13 -8 | 5 25
irf xxxxx | 19 -2 44 -17 -3 | 2 26
jgx uuuuu | -6 -47 20 -95 -4 | 10 27
mit uuuuu | 26 63 -20 -166 3 | 19 33
ngs uuuxu | -17 -86 119 -467 2 | 11 25
Table 7.2313.5 GPS week: 2313 Day: 5 MJD: 60440.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -20 17 -55 -30 -10 | 0 27
emr uuuuu | 18 29 -98 22 17 | 5 26
esa uuuuu | 40 7 57 65 -4 | 17 30
gfz uuuuu | 14 -12 -184 123 1 | 8 25
grg uuuuu | 2 -10 79 -30 3 | 0 23
igr xxxxx | -7 1 7 -78 -13 | 2 26
irf xxxxx | 7 0 45 -11 1 | -1 26
jgx uuuuu | -28 -37 18 -19 -11 | 8 28
mit uuuuu | 13 15 62 -77 7 | 17 32
ngs uuuxu | -44 -34 105 -598 -4 | 10 25
Table 7.2313.6 GPS week: 2313 Day: 6 MJD: 60441.500
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 | 2 -14 -44 -107 -12 | -1 26
emr uuuuu | -37 -2 142 29 0 | 6 28
esa uuuuu | 39 -1 61 150 -3 | 16 28
gfz uuuuu | 29 1 -168 211 6 | 8 25
grg uuuuu | 3 2 -17 -35 10 | 0 24
igr xxxxx | -11 6 -6 -77 -10 | 0 23
irf xxxxx | 16 -13 38 17 4 | -2 24
jgx uuuuu | -28 -14 18 -38 -3 | 6 25
mit uuuuu | 43 12 13 -117 4 | 17 31
ngs uuuxu | -85 23 25 -503 -3 | 9 24
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