[IGSREPORT-29901] Wk 2314 IGS Final Orbits
acc
acc at igs.org
Fri May 31 07:20:30 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2314 (May 12, 2024 - May 18, 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_20241330000_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 | MATE MATE
0 | ESA | JFNG JFNG
0 | GFZ | POHN POHN
0 | GRG | GODE JFNG MAYG SYOG TONG WIND COCO JFNG WIND
0 | MIT | DARW MAR6 NLIB NOT1 NYA1 SFER STJO TLSE TONG YEBE
0 | MIT | YEL2 DARW MAR6 NLIB NOT1 NYA1 SFER STJO TLSE TONG
0 | MIT | YEBE YEL2
1 | COD | 12 12
1 | ESA | JFNG FLIN JFNG
1 | GRG | 13 13 CCJ2 DAV1 GAMB JFNG MAL2 SYOG WIND COCO DAV1
1 | GRG | JFNG WIND
1 | MIT | CHPI FLRS HOLB MAR6 NOT1 NYA1 REYK SFER STJ3 TLSE
1 | MIT | TONG YEBE YEL2 CHPI FLRS HOLB MAR6 NOT1 NYA1 REYK
1 | MIT | SFER STJ3 TLSE TONG YEBE YEL2
2 | COD | 16 22 16 22 DAV1 NICO SVTL NICO
2 | ESA | JFNG
2 | GFZ | POHN
2 | GRG | JFNG JFNG PIE1 SVTL TONG WIND
2 | MIT | CHPI DARW DRAO FLIN NLIB NOT1 NYA1 REYK SFER TONG
2 | MIT | TOW2 YAR3 YEBE YEL2 CHPI DARW DRAO FLIN NLIB NOT1
2 | MIT | NYA1 REYK SFER TONG TOW2 YAR3 YEBE YEL2
3 | COD | ASCG KOKB NICO ASCG NICO
3 | ESA | JFNG JFNG
3 | GRG | AREQ ASCG SVTL ASCG COCO FAA1 SVTL
3 | MIT | CHPI COCO NOT1 NYA1 SFER STR1 TLSE TONG TRO1 VNDP
3 | MIT | YAR3 YEBE YEL2 CHPI COCO NOT1 NYA1 SFER STR1 TLSE
3 | MIT | TONG TRO1 VNDP YAR3 YEBE YEL2
4 | COD | CZTG CZTG
4 | ESA | SEYG
4 | GFZ | 25 LAUT LAUT
4 | GRG | SCUB SVTL DAV1 MAW1 SVTL TONG WIND
4 | MIT | CHPI CHTI GAMG GMSD NOT1 NYA1 SCH2 SFER STR1 TOW2
4 | MIT | VNDP WILL WTZZ YEBE CHPI CHTI GAMG GMSD KOKV NOT1
4 | MIT | NYA1 SCH2 SFER STR1 TOW2 VNDP WILL WTZZ YEBE
5 | COD | CPVG HYDE LMMF MATE SCUB WTZR CPVG MATE WTZR
5 | ESA | SEYG SEYG
5 | GFZ | POHN YELL POHN SCUB YELL
5 | GRG | 22 SVTL COCO SVTL
5 | MIT | CHPI NLIB NOT1 NYA1 SFER STR1 TONG TOW2 TRO1 YEBE
5 | MIT | CHPI NLIB NOT1 NYA1 SFER STR1 TLSE TONG TOW2 TRO1
5 | MIT | YEBE
6 | COD | AREQ ASCG CPVG
6 | ESA | FAIR FAIR JFNG YEL2
6 | GFZ | LAUT LAUT SCUB
6 | GRG | 12 12 CZTG FAIR JFNG MAYG SCUB CZTG FAIR HYDE JFNG
6 | GRG | SVTL
6 | JGX | JFNG
6 | MIT | IQAL IRKJ KITG MAR6 NYA1 SFER TIDB TLSE TONG YEBE
6 | MIT | YEL2 HERS IQAL IRKJ KITG MAR6 NYA1 SFER TIDB TLSE
6 | MIT | TONG YEBE YEL2
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. 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.
7. 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]
-------+-----+---------------------------------------------------
EMR | 0 | 8.4 -4.8 -7.5 -12 7 -11 .15
ESA | 0 | .2 .4 1.0 -8 -11 10 -.36
GFZ | 0 | .2 -.7 -.6 -7 -12 -8 .50
GRG | 0 | -.3 .3 -.2 23 -6 20 -.14
JGX | 0 | 5.4 -3.5 -6.8 24 -20 30 .0
JPL | 0 | .3 -2.0 -5.0 4 39 -48 .44
MIT | 0 | 5.5 -4.9 16.7 4 3 -2 .18
NGS | 0 | 3.6 -4.6 .4 -36 19 17 .18
EMR | 1 | -.1 -2.8 -9.1 -9 14 -26 .12
ESA | 1 | -.3 .2 1.1 -16 -13 21 -.67
GFZ | 1 | -.3 -.4 -.3 5 -13 -7 .32
GRG | 1 | .0 .3 -.0 13 -5 -1 -.14
JGX | 1 | -1.5 -.4 -4.5 16 -18 10 -.04
JPL | 1 | -3.4 -5.4 -1.2 7 44 -44 .68
MIT | 1 | -4.2 -5.3 13.5 15 0 -9 .16
NGS | 1 | 1.2 1.2 -3.8 19 2 3 .00
EMR | 2 | -2.3 -3.2 -10.2 4 -10 5 .12
ESA | 2 | -.1 .8 .9 -12 -7 -5 -.65
GFZ | 2 | -.2 -.0 .1 -7 -9 -20 .23
GRG | 2 | -.0 .0 .5 8 -5 -6 -.20
JGX | 2 | -2.3 -5.5 -1.7 11 -22 22 .09
JPL | 2 | -5.7 -4.0 -3.9 5 29 -41 .36
MIT | 2 | -5.1 -3.7 16.4 14 1 8 .02
NGS | 2 | 1.8 -4.9 -9.9 -3 -15 -10 -.07
EMR | 3 | .3 -3.0 -11.4 -6 0 -3 -.05
ESA | 3 | -.9 .3 .6 -9 -8 8 -.62
GFZ | 3 | -.8 .4 -.3 -7 -17 -22 .27
GRG | 3 | -.2 .3 .7 7 -3 1 -.18
JGX | 3 | -.9 -6.0 -1.1 18 -5 17 -.20
JPL | 3 | -7.5 -2.7 -9.0 5 33 -20 .47
MIT | 3 | -6.3 -7.0 16.9 9 10 23 .25
NGS | 3 | -5.7 -2.1 1.7 -18 46 -10 -.09
EMR | 4 | .4 -1.9 -2.6 -4 4 -9 .08
ESA | 4 | .4 .1 .1 -1 -7 11 -.41
GFZ | 4 | -.1 -.3 -.4 -10 -15 -7 .37
GRG | 4 | .4 .2 -.4 5 -3 -7 .06
JGX | 4 | 1.6 -.8 -1.9 19 -11 46 -.06
JPL | 4 | -6.2 -3.7 -2.6 8 18 -23 .43
MIT | 4 | -3.2 -2.7 16.5 16 -1 2 .14
NGS | 4 | 1.0 -2.3 1.0 -27 17 -11 .06
EMR | 5 | 1.2 -4.9 -5.2 -4 -11 -2 .02
ESA | 5 | .5 .5 .4 -3 1 6 -.58
GFZ | 5 | .1 .2 -.7 -1 -13 0 .33
GRG | 5 | -.5 .1 .1 9 9 -2 -.09
JGX | 5 | 2.2 -2.8 -5.7 28 -17 31 .03
JPL | 5 | -4.5 -8.5 -4.4 -5 20 -32 .55
MIT | 5 | -.9 -2.0 11.3 6 2 4 .12
NGS | 5 | 1.5 -2.7 9.0 -48 23 -13 -.11
EMR | 6 | 8.2 -5.9 -3.3 -1 10 5 -.00
ESA | 6 | .4 1.0 1.0 -22 -2 10 -.46
GFZ | 6 | .6 .1 -.6 -5 -18 -13 .36
GRG | 6 | .1 .2 .5 17 7 2 .03
JGX | 6 | .1 -5.3 -.8 9 -17 16 -.03
JPL | 6 | -4.7 -2.7 -9.3 1 20 -53 .48
MIT | 6 | 1.0 -5.1 13.2 27 -5 15 .28
NGS | 6 | 2.0 -5.3 4.9 -34 8 -5 .04
8. 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.
9. 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 1.2314.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2314.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 2.2314.[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 3.2314.[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 5.2314.0-6). 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 2314 summary. (May 12, 2024 - May 18, 2024)
Table 1.2314.a GPS week: 2314 MJD: 60442.000-60448.000
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 814| -1 0 -1 4 6 15 -.01 7 6 | -709 82 5 88
| 0 0 1 12 6 9 .02 | 262 334
emr 100| 0 0 1 -2 10 -4 .05 10 10 | -1146 -554 55 118
| 0 1 1 17 8 19 .02 | 437 733
esa 150| 0 0 2 -12 -7 -11 -.04 9 9 | -1472 1094 5 84
| 0 0 1 16 6 7 .01 | 242 394
gfz 123| 0 -1 3 10 0 -52 .10 9 9 | -42 -108 8 94
| 0 0 1 13 11 9 .02 | 149 254
grg 122| 1 0 1 -12 -6 -1 .02 9 8 | 50 -90 8 141
| 0 0 1 12 12 12 .02 | 55 80
igr n/a| 0 0 0 -3 4 -14 .01 3 3 | -4521 -580 9 79
| 0 0 0 10 6 6 .01 | 1553 703
jgx n/a| 0 0 -2 22 20 19 -.02 10 10 | 46 -77 29 106
| 0 0 0 12 10 17 .02 | 79 101
jpl n/a| -2 0 0 22 -21 1 .17 26 26 | -2637 -126 84 172
| 0 0 0 16 15 14 .02 | 533 640
mit 362| 0 1 -5 -7 -6 34 -.01 8 7 | -1408 -6826 48 86
| 0 0 1 35 18 32 .01 | 1369 315
ngs 291| 0 0 1 9 -13 -8 -.07 11 9 | -756 142 525 789
| 0 0 3 20 32 24 .02 | 149 193
Table 1.2314.b GPS week : 2314 MJD: 60442.000-60448.000
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 | 16 11 9 10 10 7 8 |
2 | 3 4 4 4 4 4 3 |
3 | 4 4 4 4 4 3 4 |
4 | 3 3 3 3 3 3 3 |
5 | 3 3 4 3 3 6 4 |
6 | 3 3 3 3 3 3 3 |
7 | 2 2 3 3 3 2 3 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 4 4 4 4 4 5 4 |
11 | 4 4 4 4 4 3 4 |
12 | 5 5 5 4 4 4 4 |
13 | 3 3 3 3 3 3 3 |
14 | 5 5 5 5 5 4 5 |
15 | 3 4 3 3 3 3 3 |
16 | 4 5 4 4 4 4 4 |
17 | 3 3 3 3 3 5 3 |
18 | 4 4 4 3 4 4 3 |
19 | 4 4 3 4 3 4 4 |
20 | 3 3 3 3 4 3 3 |
21 | 3 4 4 3 4 3 3 |
22 | 3 3 3 3 4 4 3 |
23 | 4 4 4 4 4 4 4 |
24 | 3 3 3 3 3 3 3 |
25 | 5 5 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 3 3 3 3 3 3 3 |
28 | 3 3 3 3 3 3 3 |
29 | 4 4 3 3 4 4 3 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
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 2.2314.0 GPS week: 2314 Day: 0 MJD: 60442.000
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 811| -1 0 0 2 8 -1 -.03 6 6 | -747 151 5 91
emr 104| 0 -2 1 2 0 0 .09 10 10 | -766 -1209 72 120
esa 150| -1 0 3 0 -11 -3 -.05 10 9 | -1391 1505 5 81
gfz 122| 0 0 0 13 2 -34 .08 9 9 | 76 -82 9 98
grg 120| 2 0 2 -6 -2 13 .05 8 8 | 45 48 8 142
igr n/a| 0 0 0 0 6 -10 .03 3 3 | -1946 -1406 9 72
jgx n/a| -1 -1 -3 18 6 11 -.03 9 9 | 15 99 29 123
jpl n/a| -2 -1 0 30 -23 0 .15 25 25 | -1802 -711 83 184
mit 362| 1 1 -4 -22 -17 8 -.01 8 7 | 961 -7243 44 81
ngs 295| 0 2 3 -5 28 5 -.04 11 9 | -751 150 506 676
Table 2.2314.1 GPS week: 2314 Day: 1 MJD: 60443.000
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 811| -1 0 0 10 4 27 -.03 7 6 | -1007 467 5 87
emr 104| 1 0 1 -26 13 -19 .07 10 10 | -1368 -540 52 116
esa 150| 0 0 3 -32 -15 -7 -.05 9 9 | -1200 865 6 92
gfz 124| 0 0 3 9 15 -54 .09 10 11 | 97 -227 8 111
grg 123| 1 0 1 -30 16 4 -.00 9 8 | 35 -106 9 168
igr n/a| 0 0 0 -17 0 -26 .01 3 3 | -3528 -557 9 69
jgx n/a| -1 0 -2 2 17 21 -.04 10 10 | -36 -8 26 109
jpl n/a| -1 -2 0 17 1 -19 .18 26 26 | -2690 -178 84 175
mit 362| 0 2 -4 37 -4 2 -.02 8 7 | -453 -6727 50 122
ngs 292| 0 1 -3 23 -61 18 -.04 12 11 | -996 445 553 803
Table 2.2314.2 GPS week: 2314 Day: 2 MJD: 60444.000
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 811| 0 0 0 -14 2 10 -.02 6 6 | -712 159 6 98
emr 102| 0 1 2 28 8 -20 .07 10 10 | -1443 -8 60 138
esa 150| 0 0 3 3 -5 -9 -.06 9 9 | -1571 1387 6 88
gfz 124| 1 -1 2 27 5 -55 .13 10 9 | -81 -23 9 96
grg 123| 2 0 1 6 -14 -5 .04 9 8 | 39 -34 7 149
igr n/a| 0 0 0 8 0 -12 .00 3 3 | -3979 -595 10 77
jgx n/a| -1 -1 -1 36 20 36 -.05 10 10 | 65 -94 28 97
jpl n/a| -2 0 0 53 -26 0 .17 26 26 | -2598 128 86 181
mit 362| 0 1 -6 -47 -12 24 -.03 8 7 | -1035 -6502 51 88
ngs 293| 0 1 -2 4 25 10 -.08 11 10 | -728 186 459 668
Table 2.2314.3 GPS week: 2314 Day: 3 MJD: 60445.000
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 814| 0 0 -1 -2 -1 24 .00 7 7 | -786 148 5 83
emr 95| 0 0 0 -5 15 7 .03 9 9 | -812 -1160 62 110
esa 150| 0 0 2 -25 0 -15 -.04 9 9 | -1614 1561 6 83
gfz 123| 0 -1 2 1 -4 -52 .09 8 8 | 24 -286 10 94
grg 125| 2 0 2 -22 -15 -11 .02 9 8 | 124 -58 8 126
igr n/a| 0 0 0 -9 7 -7 .02 3 3 | -4435 -986 10 81
jgx n/a| -1 -1 -2 18 14 17 -.03 10 10 | 136 -84 30 103
jpl n/a| -3 -1 -1 4 -9 20 .16 26 26 | -2428 -460 85 160
mit 362| 0 0 -5 26 9 22 -.02 7 6 | -1470 -6938 45 76
ngs 287| 0 1 3 19 -12 7 -.09 10 9 | -781 140 538 762
Table 2.2314.4 GPS week: 2314 Day: 4 MJD: 60446.000
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 816| -1 -1 -1 18 10 16 .00 7 7 | -809 30 5 86
emr 95| 0 0 3 -20 26 29 .02 10 10 | -509 -1443 36 109
esa 150| 0 0 4 -10 -3 -5 -.02 9 10 | -1120 505 6 72
gfz 123| 0 -2 5 -12 7 -57 .09 9 10 | -250 226 8 89
grg 122| 2 0 -2 -19 -3 -9 .03 9 9 | 103 -173 9 138
igr n/a| 0 0 0 -15 13 -12 .00 3 3 | -5418 -1180 9 76
jgx n/a| 0 0 -2 28 31 42 -.02 11 11 | 97 -197 33 108
jpl n/a| -4 0 1 4 -17 18 .16 26 26 | -2853 -915 84 173
mit 362| 0 1 -5 25 -15 20 -.01 8 7 | -2407 -7222 55 79
ngs 289| 0 0 0 -17 -36 -31 -.09 10 9 | -805 37 568 891
Table 2.2314.5 GPS week: 2314 Day: 5 MJD: 60447.000
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 817| -1 0 -3 1 5 19 -.00 6 6 | -155 -612 5 84
emr 106| 0 0 1 4 4 -24 .04 9 9 | -1592 35 49 118
esa 150| -1 0 1 5 1 -22 -.04 9 10 | -1774 926 6 88
gfz 124| 0 0 4 21 -2 -50 .11 9 9 | 73 -509 9 87
grg 123| 1 0 2 -2 0 -16 .01 11 8 | -49 -171 8 147
igr n/a| 0 0 0 6 7 -13 .01 3 3 | -6564 557 9 95
jgx n/a| -1 0 -3 35 36 21 .00 10 10 | -72 -73 30 104
jpl n/a| -3 0 0 24 -33 -1 .20 26 26 | -3586 933 85 166
mit 362| 0 0 -7 -40 -29 73 .01 8 8 | -2958 -6663 49 89
ngs 291| 0 0 6 -2 -10 -20 -.10 10 9 | -486 -193 524 900
Table 2.2314.6 GPS week: 2314 Day: 6 MJD: 60448.000
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 820| -1 0 -2 19 18 13 -.02 6 6 | -747 232 5 92
emr 99| 1 1 2 -4 5 -3 .05 10 10 | -1532 442 59 116
esa 150| 0 0 1 -31 -14 -18 -.05 9 9 | -1638 912 6 85
gfz 123| 0 -1 1 14 -19 -65 .12 9 9 | -239 144 8 87
grg 124| 0 -1 0 -11 -22 12 .01 8 8 | 55 -138 7 122
igr n/a| 0 0 0 2 -3 -20 -.01 3 3 | -5782 103 9 84
jgx n/a| 0 0 -2 17 16 -12 -.01 9 9 | 120 -185 28 101
jpl n/a| -3 0 0 21 -43 -10 .14 26 26 | -2505 320 83 169
mit 362| 0 1 -4 -28 27 85 -.00 8 7 | -2497 -6489 42 73
ngs 292| 0 0 4 44 -29 -47 -.09 11 10 | -748 232 529 823
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 3.2314.0 GPS week: 2314 Day: 0 MJD: 60442.000
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 | 25 --- --- --- 15 20 --- --- 24 --- 16 | 56 --- --- --- 42 44 --- --- 47 --- 47
2 | 9 9 5 7 9 5 7 7 6 12 3 | 20 20 20 21 18 20 21 19 20 20 18
3 | 5 15 9 7 12 2 8 12 9 9 3 | 22 24 24 19 24 21 22 22 21 23 21
4 | 5 18 3 8 6 3 8 48 6 6 3 | 42 46 42 44 43 42 43 55 41 42 42
5 | 4 10 6 7 7 3 9 11 8 9 3 | 71 69 70 68 72 70 72 69 68 71 70
6 | 6 11 9 5 5 3 7 9 6 13 3 | 26 29 29 25 27 26 26 31 23 28 26
7 | 3 8 5 6 7 3 7 8 6 6 2 | 45 42 42 47 48 43 46 48 45 42 44
8 | 5 7 8 7 5 2 7 7 5 13 2 | 30 29 32 31 30 29 30 31 29 24 29
9 | 4 10 5 6 5 2 6 11 7 8 2 | 30 35 31 29 31 31 31 36 28 33 30
10 | 8 10 11 9 12 3 6 11 6 9 3 | 28 27 28 28 25 26 25 28 24 26 25
11 | 7 11 15 10 9 4 8 62 16 12 4 | 43 46 48 43 47 45 45 61 38 46 43
12E | 9 10 15 14 19 4 13 8 6 16 5 | 134 134 134 131 137 132 132 134 131 133 133
13 | 5 6 7 7 4 3 7 9 8 7 2 | 16 19 18 17 17 18 15 24 16 18 16
14E | 8 8 23 10 11 4 7 53 14 14 5 | 34 39 46 38 39 37 37 43 40 31 37
15 | 7 8 6 8 7 3 14 7 8 12 3 | 70 69 69 72 68 70 75 72 68 68 70
16E | 6 9 12 12 11 3 13 10 8 13 4 | 118 114 116 118 115 117 116 117 116 110 116
17 | 5 8 6 8 4 3 8 8 7 9 2 | 26 25 22 27 27 25 23 27 23 23 24
18 | 7 10 13 9 7 4 8 58 4 15 3 | 50 53 51 49 49 51 47 62 48 52 49
19 | 4 11 8 8 7 4 15 9 9 11 3 | 28 25 25 31 28 27 29 26 27 26 27
20E | 7 9 8 9 6 2 8 7 5 9 3 | 59 55 56 57 58 56 55 59 56 56 57
21 | 9 9 4 9 7 5 9 7 5 12 3 | 18 20 16 19 16 17 18 19 16 17 16
22E | 8 8 6 11 10 3 9 6 6 8 3 | 88 91 88 88 89 89 91 89 90 89 89
23 | 6 10 15 9 13 4 8 60 7 15 4 | 54 56 60 58 52 55 54 68 54 58 55
24 | 6 8 9 7 5 3 9 11 5 13 3 | 30 32 30 28 28 29 29 34 26 27 28
25E | 7 11 15 22 7 4 13 10 5 10 4 | 31 29 32 30 31 30 28 29 28 30 29
26E | 8 8 8 11 7 3 12 8 10 11 3 | 37 32 34 35 33 33 32 34 36 30 33
27 | 5 8 7 9 6 3 6 8 6 10 2 | 28 29 30 33 27 28 28 31 26 24 27
28 | 5 9 6 8 7 3 9 48 10 9 3 | 39 37 39 41 42 39 40 55 40 40 39
29 | 7 8 7 8 7 3 17 10 5 11 3 | 36 35 32 39 36 35 39 37 34 38 35
30 | 5 7 9 6 5 3 7 9 7 7 2 | 25 27 25 27 25 26 26 28 25 25 25
31 | 3 9 6 5 6 2 8 9 5 10 2 | 40 45 40 40 40 40 40 47 42 42 40
32 | 5 10 7 5 6 4 7 12 7 9 2 | 37 40 35 37 33 36 37 40 34 33 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 10 10 9 8 3 9 25 8 11 |T 44 44 44 44 43 43 43 47 42 42 42
WRMS | 6 10 9 9 8 3 9 25 7 9 |NE 33 34 33 33 33 32 33 37 31 32 32
MEDI | 6 9 8 8 7 3 8 9 6 10 |MD 36 35 34 37 33 35 37 37 34 33 35
Table 3.2314.1 GPS week: 2314 Day: 1 MJD: 60443.000
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 | 15 --- --- --- 18 14 --- --- 13 --- 11 | 43 --- --- --- 34 33 --- --- 35 --- 34
2 | 10 8 6 8 9 4 10 10 10 13 3 | 22 23 24 23 22 24 23 25 22 25 22
3 | 6 15 8 7 11 2 7 10 8 12 3 | 26 29 27 25 26 25 25 26 25 28 25
4 | 5 17 4 7 7 2 10 48 6 13 3 | 39 42 39 42 41 40 40 45 38 41 39
5 | 4 9 8 11 8 4 11 10 8 10 3 | 65 62 63 65 64 64 64 63 63 61 63
6 | 5 10 9 8 4 4 7 9 6 12 3 | 26 28 27 24 25 26 24 28 24 24 25
7 | 4 6 6 7 6 3 8 7 4 7 2 | 37 39 37 40 38 38 37 42 38 41 38
8 | 5 9 8 8 6 1 8 8 5 14 3 | 26 26 29 28 26 26 26 29 25 27 26
9 | 6 9 6 6 4 3 7 10 5 9 2 | 27 36 31 32 30 31 31 35 28 33 30
10 | 11 9 9 9 12 3 9 10 7 12 3 | 28 25 27 29 26 26 24 29 25 30 25
11 | 7 9 14 12 8 3 6 66 6 14 3 | 32 34 33 31 35 33 33 40 32 30 32
12E | 7 12 11 14 16 3 13 8 9 12 4 | 115 113 114 113 116 114 112 115 117 116 115
13 | 4 6 6 9 4 2 7 9 7 9 2 | 18 22 17 18 17 18 18 25 19 18 18
14E | 8 9 21 11 15 4 9 53 15 14 5 | 31 35 40 37 38 35 34 39 38 36 35
15 | 4 11 6 9 7 2 14 8 9 15 3 | 40 41 39 42 40 41 41 43 41 34 40
16E | 11 9 11 15 10 5 14 11 12 15 4 | 99 98 99 99 99 99 97 98 97 96 98
17 | 7 11 5 6 6 4 10 9 7 9 3 | 23 26 21 24 23 24 22 28 23 26 23
18 | 6 10 12 9 7 5 10 58 6 14 3 | 35 37 36 38 36 35 35 40 35 34 35
19 | 5 13 6 9 7 5 15 9 8 11 3 | 21 25 20 23 21 22 24 25 23 23 22
20E | 7 7 8 9 6 3 9 7 7 11 3 | 41 39 39 40 43 39 39 40 41 40 40
21 | 7 8 5 9 16 4 11 10 8 13 3 | 20 23 21 23 22 22 21 24 20 23 20
22E | 9 7 6 8 7 3 8 7 8 13 3 | 71 76 74 74 74 75 76 76 75 77 74
23 | 5 9 16 7 11 4 9 60 8 21 4 | 40 40 44 43 40 40 40 52 40 42 40
24 | 9 10 9 7 4 3 7 9 5 11 3 | 31 33 32 31 30 31 28 34 28 27 30
25E | 7 11 13 27 8 4 13 9 7 14 5 | 28 26 30 31 26 26 25 27 29 29 26
26E | 7 8 9 14 10 3 13 8 14 11 4 | 33 29 33 35 33 31 30 32 32 28 31
27 | 5 8 8 7 8 1 7 7 6 13 2 | 25 25 27 28 25 25 24 29 26 23 25
28 | 6 9 6 5 9 3 9 47 8 9 3 | 23 22 24 25 27 22 24 33 25 21 23
29 | 7 10 6 7 7 3 19 10 5 12 3 | 24 21 20 25 22 23 24 26 24 24 22
30 | 6 7 8 6 5 2 9 7 6 8 2 | 27 30 27 29 27 28 27 31 26 27 27
31 | 4 10 6 8 9 3 10 9 6 11 3 | 30 33 29 27 30 29 32 36 30 31 30
32 | 5 10 6 9 6 3 9 11 6 7 2 | 36 38 36 37 34 36 36 40 34 34 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 10 9 10 9 3 10 26 8 12 |T 36 37 37 38 37 36 36 40 36 37 36
WRMS | 6 10 9 11 8 3 10 26 7 11 |NE 28 29 28 29 28 28 28 32 27 28 27
MEDI | 6 9 8 8 7 3 9 9 7 12 |MD 30 33 31 31 30 31 30 34 29 30 30
Table 3.2314.2 GPS week: 2314 Day: 2 MJD: 60444.000
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 --- --- --- 9 12 --- --- 15 --- 8 | 30 --- --- --- 30 30 --- --- 33 --- 30
2 | 10 8 6 10 10 4 8 9 12 16 3 | 24 25 25 28 26 25 26 26 27 31 25
3 | 5 14 9 8 13 3 6 13 8 15 3 | 24 26 26 24 27 23 26 26 22 23 23
4 | 3 17 3 9 7 3 8 50 8 10 3 | 29 28 29 29 29 27 30 35 29 28 28
5 | 4 9 8 10 14 2 10 11 6 10 3 | 67 66 64 65 64 65 67 65 64 70 65
6 | 5 10 9 7 4 2 7 9 6 11 3 | 26 27 29 27 28 27 27 29 24 27 26
7 | 4 7 5 7 7 2 9 7 5 8 2 | 34 33 32 36 34 33 34 37 34 35 33
8 | 5 7 8 7 5 2 8 7 5 12 2 | 26 26 29 27 27 26 28 29 26 24 26
9 | 4 12 5 6 7 2 6 11 5 7 2 | 25 31 25 23 24 24 26 31 23 24 24
10 | 13 11 10 11 11 3 8 10 6 9 4 | 33 30 31 31 31 29 30 33 29 29 29
11 | 6 11 13 10 8 2 9 68 5 11 3 | 27 30 34 34 34 31 32 41 30 34 31
12E | 5 12 4 20 16 5 15 15 9 7 4 | 59 57 59 62 68 58 58 58 55 61 59
13 | 5 8 6 14 4 2 8 8 7 9 3 | 20 22 21 25 19 21 21 25 20 23 20
14E | 8 8 21 11 13 4 8 55 16 18 5 | 16 21 28 26 22 20 22 26 22 20 19
15 | 5 7 6 5 5 3 13 6 8 11 3 | 47 45 44 48 45 46 48 48 48 51 46
16E | 7 9 9 9 9 4 15 10 8 15 3 | 50 50 52 53 50 51 55 51 54 50 51
17 | 6 8 5 7 6 3 9 8 8 12 3 | 24 28 23 27 26 25 26 29 24 25 24
18 | 6 12 12 9 7 2 10 58 5 11 3 | 31 34 34 32 34 32 33 43 32 34 32
19 | 6 10 6 9 7 4 16 8 6 11 3 | 25 25 26 29 26 26 29 26 25 25 25
20E | 8 7 8 9 6 2 9 8 7 8 3 | 46 47 48 46 48 46 47 46 46 48 46
21 | 9 6 4 12 9 4 9 8 10 12 3 | 21 23 23 25 22 22 24 25 24 26 22
22E | 5 12 4 12 9 3 9 10 6 10 3 | 46 46 45 48 48 46 48 47 46 48 46
23 | 7 8 16 10 12 4 9 61 6 14 4 | 42 41 50 47 44 45 44 55 43 46 44
24 | 8 9 9 8 6 3 8 9 4 9 3 | 26 28 26 27 24 26 26 31 24 28 25
25E | 8 12 12 11 10 4 13 10 8 11 4 | 22 24 24 29 23 23 22 23 22 24 22
26E | 6 8 8 11 11 3 12 9 12 12 3 | 27 25 28 30 27 26 30 29 27 27 26
27 | 7 8 7 7 5 3 10 7 6 10 2 | 26 26 28 27 26 26 28 30 25 24 25
28 | 3 9 5 6 8 3 10 50 7 9 2 | 45 45 46 47 45 46 48 56 47 45 46
29 | 7 8 5 7 6 3 16 9 6 13 3 | 29 26 27 31 29 30 32 31 30 34 29
30 | 4 6 9 5 8 3 6 8 5 9 2 | 24 25 23 25 23 24 24 28 23 26 23
31 | 4 8 6 6 7 2 10 8 6 10 2 | 42 47 44 44 43 43 45 49 44 44 43
32 | 5 9 8 10 6 3 9 12 7 11 3 | 24 29 23 29 23 25 25 31 24 23 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 10 9 10 9 3 10 26 8 11 |T 32 33 33 34 33 32 34 36 32 34 32
WRMS | 6 10 9 9 8 3 10 26 7 10 |NE 28 29 29 30 29 28 30 33 28 30 28
MEDI | 6 9 8 9 7 3 9 9 6 11 |MD 27 28 29 29 28 27 30 31 27 28 26
Table 3.2314.3 GPS week: 2314 Day: 3 MJD: 60445.000
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 | 15 --- --- --- 10 9 --- --- 16 --- 10 | 30 --- --- --- 28 28 --- --- 31 --- 28
2 | 9 7 5 8 9 4 7 8 12 11 3 | 20 19 20 23 22 21 22 21 22 20 20
3 | 6 13 9 7 13 3 6 11 8 11 3 | 22 23 24 20 26 21 22 24 18 22 20
4 | 5 16 5 4 7 4 9 50 8 9 3 | 19 20 20 21 22 20 21 35 21 22 19
5 | 6 8 7 8 12 2 12 9 5 7 3 | 77 74 74 75 75 74 76 74 73 77 75
6 | 5 9 7 7 5 2 8 9 6 11 2 | 25 26 26 24 25 24 25 30 22 23 24
7 | 6 5 6 5 8 3 7 8 5 11 2 | 42 43 41 43 40 41 42 44 41 38 41
8 | 4 8 8 8 5 2 7 8 8 11 2 | 19 19 21 21 18 19 21 19 18 19 18
9 | 5 9 6 5 6 4 7 9 5 8 2 | 18 25 19 19 17 18 19 27 16 21 18
10 | 12 9 10 10 12 3 8 9 7 6 3 | 26 25 25 26 26 24 23 25 21 26 23
11 | 9 10 11 10 7 3 10 63 5 13 3 | 15 22 20 20 21 18 20 30 16 20 18
12E | 5 9 5 12 6 3 14 11 7 13 3 | 50 49 50 50 44 49 49 50 48 51 48
13 | 7 7 7 6 5 3 8 8 7 6 2 | 16 21 15 15 15 15 17 21 16 18 16
14E | 7 8 21 9 11 4 8 55 16 13 5 | 18 21 28 20 20 19 20 27 21 20 19
15 | 6 8 6 8 7 3 11 7 8 7 3 | 49 47 46 47 46 46 49 51 44 42 46
16E | 9 8 6 10 7 5 14 10 8 13 3 | 35 33 35 35 36 36 37 31 34 33 34
17 | 9 8 5 11 7 4 8 9 6 8 3 | 20 24 18 23 20 21 20 27 18 21 20
18 | 7 10 11 7 6 3 10 58 7 10 3 | 16 23 21 21 22 19 19 34 21 17 19
19 | 6 10 6 10 7 4 15 9 6 14 3 | 20 20 20 24 20 22 23 23 20 27 20
20E | 7 7 8 6 6 3 10 8 6 10 3 | 26 26 27 25 28 26 27 26 26 28 26
21 | 8 7 4 6 9 5 11 8 9 13 3 | 17 20 17 19 19 19 20 19 18 22 17
22E | 8 7 5 9 12 4 8 10 5 10 3 | 48 50 48 51 49 50 49 50 47 49 48
23 | 8 8 16 9 14 3 9 59 6 10 4 | 39 41 48 48 44 43 41 56 41 43 42
24 | 9 7 9 7 7 3 10 8 7 11 3 | 26 26 23 28 20 24 21 31 23 22 23
25E | 5 10 12 5 10 3 14 10 5 9 3 | 18 22 20 20 18 20 20 19 18 19 18
26E | 6 6 9 12 10 3 13 7 9 8 3 | 24 19 22 26 21 22 23 22 21 22 21
27 | 5 5 7 8 4 2 8 8 7 11 2 | 20 19 22 24 20 20 22 23 18 20 19
28 | 6 8 5 6 8 3 10 50 6 10 2 | 19 20 21 22 19 20 23 35 20 21 19
29 | 5 8 7 7 6 4 16 10 5 9 3 | 22 23 20 26 23 24 27 23 20 24 22
30 | 5 7 8 5 10 3 7 8 6 8 2 | 22 24 20 22 18 21 21 25 22 21 20
31 | 4 8 7 4 7 3 10 8 5 8 2 | 43 45 41 41 40 42 41 48 42 40 42
32 | 4 9 7 8 16 4 9 10 5 5 3 | 20 26 20 22 21 20 18 28 18 18 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 9 8 9 3 10 26 7 10 |T 27 28 28 29 27 27 28 32 26 27 26
WRMS | 7 9 9 8 8 3 10 26 6 9 |NE 23 25 23 25 23 23 24 29 22 23 22
MEDI | 6 8 7 8 7 3 9 9 6 10 |MD 22 24 22 24 22 21 22 27 21 22 20
Table 3.2314.4 GPS week: 2314 Day: 4 MJD: 60446.000
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 | 14 --- --- --- 13 11 --- --- 14 --- 10 | 27 --- --- --- 24 25 --- --- 24 --- 23
2 | 10 8 5 8 10 3 8 9 11 13 3 | 18 18 18 20 19 18 20 18 21 23 18
3 | 8 20 9 10 14 3 6 11 10 9 4 | 21 29 23 23 24 20 20 22 16 20 19
4 | 6 17 5 8 9 4 8 50 7 8 3 | 29 32 29 29 30 26 29 39 28 29 28
5E | 6 8 10 8 10 2 14 9 6 10 3 | 79 80 79 80 73 79 82 79 79 80 79
6 | 6 11 8 6 6 3 8 10 7 11 3 | 23 24 26 23 23 22 21 25 19 21 22
7 | 5 8 5 7 7 3 6 8 6 7 2 | 36 38 37 38 41 37 39 40 41 38 38
8 | 6 9 9 9 6 2 8 7 6 10 3 | 19 21 22 20 19 19 21 22 17 20 19
9 | 4 12 6 7 7 3 8 9 6 10 2 | 19 28 21 20 19 19 22 28 17 19 20
10 | 14 9 11 14 13 2 7 11 8 6 4 | 26 23 25 28 25 22 20 22 21 22 22
11 | 7 12 10 12 8 2 13 62 7 10 3 | 20 24 23 27 25 21 25 32 19 19 21
12E | 5 8 8 10 12 3 15 11 7 9 3 | 29 29 29 32 32 30 26 31 28 28 28
13 | 6 10 8 9 7 3 9 8 9 6 3 | 12 20 11 13 12 12 13 20 12 14 12
14E | 8 10 21 7 18 4 7 57 12 9 4 | 15 23 27 19 22 18 19 27 19 15 17
15 | 6 8 6 6 8 5 13 9 10 9 3 | 42 45 42 46 44 42 48 44 41 49 44
16E | 5 9 6 12 7 3 17 10 9 13 3 | 59 58 61 59 59 59 64 59 59 54 59
X17 | 8 --- 4 7 6 3 10 --- 5 9 3 | 20 --- 17 18 20 19 22 --- 18 21 18
18 | 10 12 12 8 7 3 10 58 10 12 4 | 17 24 20 21 20 19 20 30 21 17 18
19 | 6 11 5 8 7 4 17 10 7 8 3 | 19 21 20 21 18 20 22 20 21 22 19
20E | 8 10 9 7 8 2 10 10 6 12 3 | 32 29 30 30 34 30 30 30 30 33 30
21 | 8 7 5 9 9 4 10 8 12 12 3 | 17 18 14 17 18 15 17 18 20 20 15
22E | 5 9 6 17 17 4 7 15 8 9 4 | 22 28 24 24 30 24 25 27 25 26 23
23 | 7 9 17 13 10 3 8 56 9 11 4 | 51 50 58 60 49 52 51 61 53 51 52
24 | 8 10 9 8 9 3 9 10 7 7 3 | 22 26 21 20 22 20 19 27 21 19 20
25E | 5 10 12 15 8 3 17 10 5 12 4 | 16 17 19 23 17 16 15 18 16 18 15
26E | 7 9 8 9 12 3 10 8 10 11 3 | 22 19 21 21 21 20 21 22 20 20 19
27 | 7 7 7 9 7 2 9 7 7 11 3 | 19 19 20 17 17 17 18 21 17 18 17
28 | 7 13 5 7 9 3 7 45 7 9 3 | 36 38 35 38 34 36 35 45 35 37 35
29 | 7 9 7 9 7 4 17 11 5 11 3 | 23 20 20 26 20 22 26 22 21 23 21
30 | 4 9 9 6 8 3 6 11 6 5 2 | 19 24 19 19 22 19 21 27 20 16 19
31 | 5 10 6 6 8 3 8 10 6 8 2 | 40 42 38 36 39 39 38 43 38 37 38
32 | 6 9 8 7 6 2 7 12 10 7 3 | 29 30 28 27 28 27 27 33 24 26 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 10 9 9 9 3 11 26 8 10 |T 27 29 28 28 28 27 28 31 26 27 26
WRMS | 7 10 10 10 9 3 11 26 7 9 |NE 23 26 24 24 24 23 24 28 23 24 23
MEDI | 6 9 8 8 8 3 9 10 7 9 |MD 22 24 23 23 23 21 22 27 21 22 21
Table 3.2314.5 GPS week: 2314 Day: 5 MJD: 60447.000
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 --- --- --- 7 10 --- --- 11 --- 7 | 24 --- --- --- 22 25 --- --- 24 --- 22
2 | 8 8 6 13 9 4 8 9 14 8 3 | 20 20 18 21 19 18 20 19 25 20 18
3 | 5 11 11 6 12 4 6 11 9 8 3 | 19 20 20 18 19 17 18 20 15 20 17
4 | 6 15 4 5 5 3 7 49 9 9 3 | 29 32 31 31 31 31 30 37 29 36 30
5E | 5 10 11 9 37 3 14 11 8 9 5 | 85 84 84 82 83 84 87 85 84 83 83
6 | 5 8 10 11 5 3 7 9 6 10 3 | 22 24 24 24 22 21 20 27 18 21 21
7 | 5 4 4 5 6 3 6 7 6 8 2 | 36 35 34 35 33 33 35 39 35 31 34
8 | 4 6 9 11 5 1 6 9 7 9 2 | 19 21 22 22 19 19 20 21 18 19 19
9 | 5 10 5 9 4 3 5 8 8 11 2 | 21 26 21 20 20 21 20 27 19 23 20
10 | 12 9 11 10 21 3 7 9 9 9 4 | 29 26 26 27 28 25 23 26 24 27 24
11 | 6 9 13 10 8 3 8 63 6 9 3 | 26 29 28 30 29 28 28 30 26 29 27
12E | 6 10 8 11 6 3 14 12 6 10 3 | 45 43 43 41 43 42 41 43 43 42 42
13 | 5 9 7 10 5 4 8 6 9 6 3 | 13 18 10 12 12 12 14 19 14 13 12
14E | 8 8 20 8 12 3 7 55 13 12 4 | 14 18 24 18 18 15 15 24 20 15 16
15 | 6 7 7 8 5 3 12 7 9 7 3 | 37 34 32 36 34 34 38 37 33 35 34
16E | 5 8 7 11 7 3 15 10 9 9 3 | 72 70 69 71 69 70 69 72 71 71 70
X17 | 7 --- 7 18 8 5 --- --- 8 13 4 | 18 --- 16 28 20 20 --- --- 21 20 18
18 | 8 10 12 8 8 3 12 54 9 12 3 | 28 32 28 28 30 27 31 32 28 27 28
19 | 6 11 6 12 8 3 14 9 8 12 3 | 21 23 22 28 22 23 23 25 25 24 22
20E | 9 6 8 7 6 2 9 9 6 9 3 | 52 51 50 50 50 49 50 52 48 50 50
21 | 6 7 5 11 8 4 11 10 10 9 3 | 17 18 14 18 17 15 17 18 18 20 15
22E | 7 8 6 8 18 3 7 9 8 15 3 | 26 29 27 26 31 27 26 30 30 28 26
23E | 7 7 19 10 7 3 8 59 7 10 3 | 66 67 70 69 66 67 67 75 67 69 67
24 | 8 8 9 6 6 4 7 9 7 9 3 | 17 22 21 20 17 19 17 25 17 20 18
X25E | 4 10 12 --- 8 5 13 10 8 --- 4 | 17 19 19 --- 17 17 17 19 18 --- 16
26E | 9 9 8 13 10 3 10 9 8 10 3 | 20 19 19 22 20 17 18 20 19 20 18
27 | 4 5 8 8 6 2 8 8 8 10 2 | 19 21 23 21 19 19 20 22 18 21 19
28 | 5 11 5 6 7 3 9 46 6 7 2 | 38 38 38 40 43 38 42 44 40 38 39
29 | 7 11 8 10 6 3 18 10 7 11 4 | 25 26 23 32 26 27 30 28 25 28 26
30 | 6 7 9 6 7 3 7 8 7 8 2 | 17 21 17 16 17 17 18 21 17 17 16
31 | 5 8 7 5 5 3 7 8 5 10 2 | 38 41 39 36 36 38 39 44 39 34 38
32 | 5 8 11 9 5 2 7 10 11 9 3 | 27 30 26 30 26 26 26 32 27 25 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 9 9 9 11 3 10 26 8 10 |T 29 31 30 31 29 29 30 33 29 30 29
WRMS | 6 9 10 9 8 3 10 26 8 9 |NE 24 26 24 26 24 24 25 28 24 24 23
MEDI | 6 8 8 9 7 3 8 9 8 9 |MD 24 26 24 28 22 25 23 27 25 25 22
Table 3.2314.6 GPS week: 2314 Day: 6 MJD: 60448.000
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 | 10 --- --- --- 7 11 --- --- 15 --- 8 | 33 --- --- --- 33 30 --- --- 31 --- 31
2 | 8 9 5 9 8 4 9 10 9 12 3 | 28 29 28 28 28 27 29 29 28 29 27
3 | 6 15 9 7 13 3 6 11 10 12 3 | 24 31 26 24 23 23 25 29 19 27 23
4 | 7 19 5 6 7 3 6 50 6 11 3 | 46 50 46 46 45 46 46 58 45 46 45
5E | 5 9 7 10 13 3 12 11 6 11 3 | 101 100 102 101 96 101 103 101 101 103 101
6 | 4 11 8 7 7 2 7 11 6 10 2 | 31 34 32 31 31 30 29 35 29 30 30
7 | 4 6 6 6 9 2 9 8 5 14 2 | 50 48 50 49 53 49 51 53 51 42 49
8 | 6 8 10 9 4 2 7 8 6 13 3 | 23 22 24 23 23 22 24 22 21 21 22
9 | 4 11 7 4 7 3 5 10 6 12 2 | 31 36 34 32 30 32 34 35 31 33 32
10 | 9 12 10 7 11 4 9 12 7 9 3 | 46 43 42 43 38 41 42 42 41 43 41
11 | 6 13 9 11 8 3 12 65 7 11 3 | 40 45 44 45 42 42 45 51 42 43 42
12E | 6 11 7 14 8 3 15 14 6 11 3 | 55 55 57 58 56 56 56 56 57 57 56
13 | 5 9 7 8 6 3 7 8 8 7 2 | 18 24 16 18 17 19 19 23 20 21 18
14E | 7 10 19 12 12 2 8 55 11 14 4 | 14 21 31 29 22 20 19 29 20 16 19
15 | 6 7 5 6 8 3 10 9 8 10 2 | 66 65 65 68 63 65 70 66 63 68 66
16E | 5 9 7 8 9 3 15 10 10 12 3 | 95 96 95 93 97 95 92 97 99 94 95
X17 | 8 9 6 7 5 5 --- 11 7 12 3 | 24 22 20 23 23 23 --- 25 24 24 22
18 | 7 10 11 9 6 3 9 58 7 10 3 | 45 45 45 49 44 46 47 50 44 47 45
19 | 5 13 7 9 6 4 15 10 9 11 3 | 22 25 23 27 25 24 25 26 27 27 24
20E | 9 8 8 7 7 3 9 12 8 9 3 | 77 76 74 73 75 74 74 75 74 76 74
21 | 7 8 5 12 8 4 10 10 8 12 3 | 21 24 21 22 21 19 22 23 20 23 20
22E | 5 9 4 9 10 4 8 11 8 9 3 | 33 32 34 35 39 34 35 34 36 33 34
23E | 7 8 17 11 12 3 7 57 8 12 4 | 69 68 74 70 67 70 70 79 69 77 69
24 | 7 11 8 7 7 3 7 10 8 7 3 | 28 29 27 28 25 27 26 33 27 26 26
25E | 6 13 12 14 8 3 9 12 8 9 3 | 18 22 21 28 19 19 18 20 21 19 19
26E | 6 12 9 11 10 4 10 10 10 11 3 | 23 20 22 23 24 21 23 22 23 21 21
27 | 6 8 8 10 4 3 7 8 8 11 3 | 23 25 26 26 25 23 25 25 25 24 24
28 | 5 11 4 5 8 3 6 47 7 9 2 | 46 47 46 48 52 47 50 59 48 49 48
29 | 4 8 6 8 6 3 12 11 8 12 3 | 29 30 26 32 30 29 32 29 29 31 29
30 | 4 8 9 7 8 3 9 8 7 11 3 | 24 26 22 24 24 24 27 27 24 22 23
31 | 5 9 7 6 7 3 7 10 5 9 2 | 56 57 58 55 55 55 54 62 55 56 55
32 | 4 10 8 9 6 2 7 13 9 7 2 | 34 35 33 36 34 33 33 39 34 33 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 10 9 9 8 3 9 26 8 11 |T 39 41 40 41 39 39 41 43 39 40 39
WRMS | 6 10 9 9 8 3 9 26 7 10 |NE 34 36 34 35 34 33 35 38 33 34 33
MEDI | 6 9 7 8 8 3 9 11 8 11 |MD 31 34 33 32 31 30 33 35 31 33 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 4.2314 GPS week: 2314 MJD: 60442.0-60448.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 10 12 32 |U 8 16 27 |U 10 10 26 |
emr | emr 2934 |U 11 11 27 | 11 20 40 | 17 15 28 |
esa | esa 2976 | 10 15 27 |U 8 19 39 |U 13 9 23 |
gfz | gfz 2961 |U 10 10 31 |U 8 14 29 | 11 10 26 |
grg | grg 3070 |U 11 10 32 |U 10 14 31 | 11 9 27 |
igr | igr 2975 | 9 9 25 | 8 15 29 | 11 9 24 |
igs | igs 2975 | 9 9 26 | 8 15 29 | 10 9 23 |
jgx | jgx 2948 |U 11 10 27 |U 9 16 28 | 10 9 25 |
jpl | jpl 2948 | 12 12 31 | 11 20 54 | 18 12 33 |
mit | mit 3072 |U 10 11 29 |U 10 15 31 |U 10 9 25 |
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 5.2314.0 GPS week: 2314 Day: 0 MJD: 60442.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 14 20 36 | ---- ---- ---- | 12 10 27 |
emr | emr 2976 | 14 15 36 | ---- ---- ---- | 14 15 30 |
esa | esa 2976 | 13 14 27 | ---- ---- ---- | 13 11 26 |
gfz | gfz 2976 | 14 16 33 | ---- ---- ---- | 12 9 27 |
grg | grg 3072 | 15 17 37 | ---- ---- ---- | 12 8 26 |
igr | igr 2976 | 13 16 30 | ---- ---- ---- | 12 9 27 |
igs | igs 2976 | 13 16 31 | ---- ---- ---- | 12 9 25 |
jgx | jgx 2976 | 15 18 33 | ---- ---- ---- | 11 10 26 |
jpl | jpl 2976 | 14 15 31 | ---- ---- ---- | 18 13 39 |
mit | mit 3072 | 12 16 37 | ---- ---- ---- | 11 10 24 |
Table 5.2314.1 GPS week: 2314 Day: 1 MJD: 60443.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 9 32 | 8 20 27 | 12 11 23 |
emr | emr 2976 | 10 10 24 | 12 27 41 | 17 15 26 |
esa | esa 2976 | 9 15 26 | 9 25 39 | 14 11 21 |
gfz | gfz 2976 | 9 8 28 | 7 17 37 | 13 11 25 |
grg | grg 3071 | 11 8 31 | 11 18 35 | 12 9 25 |
igr | igr 2976 | 8 6 24 | 8 20 33 | 12 10 22 |
igs | igs 2976 | 9 7 25 | 8 19 34 | 12 10 21 |
jgx | jgx 2976 | 10 9 28 | 8 22 37 | 11 10 22 |
jpl | jpl 2976 | 12 11 32 | 12 24 55 | 19 16 32 |
mit | mit 3072 | 9 9 30 | 10 19 38 | 11 9 26 |
Table 5.2314.2 GPS week: 2314 Day: 2 MJD: 60444.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 11 32 | 11 15 25 | 8 9 26 |
emr | emr 2974 | 13 11 36 | 12 17 35 | 14 11 29 |
esa | esa 2976 | 11 22 36 | 9 15 33 | 12 8 21 |
gfz | gfz 2976 | 11 12 30 | 10 11 23 | 9 8 26 |
grg | grg 3072 | 11 13 35 | 13 12 28 | 10 8 27 |
igr | igr 2976 | 10 13 30 | 10 12 25 | 10 8 24 |
igs | igs 2976 | 11 12 30 | 10 12 23 | 9 7 23 |
jgx | jgx 2976 | 12 11 30 | 10 14 25 | 9 8 24 |
jpl | jpl 2976 | 13 15 40 | 11 18 51 | 18 11 37 |
mit | mit 3072 | 11 15 32 | 11 13 27 | 9 8 25 |
Table 5.2314.3 GPS week: 2314 Day: 3 MJD: 60445.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 9 31 | 10 15 26 | 9 13 29 |
emr | emr 2976 | 9 10 23 | 14 16 30 | 13 14 29 |
esa | esa 2976 | 9 12 23 | 11 15 40 | 11 9 22 |
gfz | gfz 2976 | 10 5 25 | 10 14 27 | 8 11 25 |
grg | grg 3071 | 12 7 30 | 12 14 28 | 8 9 26 |
igr | igr 2976 | 9 5 22 | 11 14 29 | 8 11 25 |
igs | igs 2976 | 9 5 22 | 11 14 28 | 8 10 24 |
jgx | jgx 2976 | 11 6 24 | 11 15 30 | 7 10 23 |
jpl | jpl 2976 | 11 7 27 | 14 18 48 | 16 13 33 |
mit | mit 3072 | 10 10 27 | 12 17 32 | 8 8 25 |
Table 5.2314.4 GPS week: 2314 Day: 4 MJD: 60446.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 9 31 | 6 16 25 | 10 10 24 |
emr | emr 2784 | 10 7 25 | 10 21 49 | 23 18 28 |
esa | esa 2976 | 8 17 26 | 7 18 39 | 12 8 23 |
gfz | gfz 2975 | 11 9 39 | 8 13 24 | 10 10 24 |
grg | grg 3072 | 10 9 30 | 9 14 26 | 11 8 27 |
igr | igr 2976 | 8 7 23 | 7 13 27 | 10 9 23 |
igs | igs 2976 | 8 7 23 | 7 14 26 | 10 8 22 |
jgx | jgx 2976 | 9 7 25 | 7 13 25 | 10 9 23 |
jpl | jpl 2880 | 12 9 32 | 10 21 52 | 19 11 34 |
mit | mit 3072 | 8 11 24 | 10 15 32 | 10 11 23 |
Table 5.2314.5 GPS week: 2314 Day: 5 MJD: 60447.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 9 10 32 | 7 19 29 | 10 10 31 |
emr | emr 2880 | 10 14 20 | 8 23 49 | 28 19 38 |
esa | esa 2976 | 9 18 27 | 7 23 43 | 13 9 28 |
gfz | gfz 2873 | 9 11 32 | 6 15 34 | 11 12 37 |
grg | grg 3062 | 10 11 35 | 7 14 37 | 13 11 33 |
igr | igr 2970 | 8 9 24 | 6 17 33 | 11 10 29 |
igs | igs 2970 | 8 9 25 | 6 17 33 | 11 9 29 |
jgx | jgx 2880 | 9 9 26 | 7 18 28 | 11 10 28 |
jpl | jpl 2880 | 12 12 27 | 10 25 62 | 21 11 38 |
mit | mit 3072 | 9 8 27 | 8 17 33 | 9 8 28 |
Table 5.2314.6 GPS week: 2314 Day: 6 MJD: 60448.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 14 29 | 7 12 32 | 11 9 23 |
emr | emr 2976 | 10 13 27 | 10 16 38 | 14 11 17 |
esa | esa 2976 | 10 10 26 | 8 18 38 | 14 8 19 |
gfz | gfz 2976 | 9 11 29 | 6 13 28 | 13 10 19 |
grg | grg 3072 | 9 8 28 | 8 11 34 | 13 10 25 |
igr | igr 2976 | 8 8 23 | 7 13 28 | 12 9 18 |
igs | igs 2976 | 8 9 23 | 7 12 28 | 12 9 18 |
jgx | jgx 2880 | 9 10 25 | 8 15 26 | 13 9 25 |
jpl | jpl 2976 | 14 14 31 | 9 15 57 | 18 10 21 |
mit | mit 3072 | 10 10 26 | 8 12 26 | 11 8 22 |
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 6.2314 GPS week: 2314 MJD: 60442.500-60448.500
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 -3 32 19 2 | -2 21
| 10 17 51 40 7 | 4
emr uuuuu | -3 5 46 46 -2 | 11 24
| 14 13 36 52 9 | 2
esa uuuuu | 25 5 35 93 -5 | 15 26
| 7 13 47 25 3 | 4
gfz uuuuu | -6 -21 69 -98 -3 | 13 24
| 12 4 69 124 2 | 2
grg uuuuu | -14 14 -24 -148 4 | 8 20
| 16 5 34 105 3 | 2
igr xxxxx | -11 -3 9 -71 2 | 1 17
| 5 4 29 39 5 | 3
irf xxxxx | 6 8 3 41 -4 | 0 22
| 13 9 16 21 2 | 3
jgx uuuuu | -30 -24 68 -21 2 | 10 20
| 7 10 27 26 2 | 3
mit uuuuu | 28 6 -70 107 -7 | 19 29
| 16 18 53 91 3 | 3
ngs uuuuu | 0 19 -200 -53 3 | 12 21
| 37 16 56 200 3 | 3
Table 7.2314.0 GPS week: 2314 Day: 0 MJD: 60442.500
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 -2 33 63 -9 | 4 22
emr uuuuu | 4 2 4 59 9 | 12 27
esa uuuuu | 33 -1 21 79 -7 | 21 29
gfz uuuuu | 11 -21 -42 68 -2 | 16 25
grg uuuuu | 1 8 -42 -16 6 | 8 20
igr xxxxx | -12 -2 -20 -109 2 | 5 20
irf xxxxx | 5 9 6 20 -6 | 4 21
jgx uuuuu | -17 -19 58 -2 3 | 13 23
mit uuuuu | 12 10 23 -21 -5 | 24 32
ngs uuuuu | -56 24 -96 -338 2 | 15 23
Table 7.2314.1 GPS week: 2314 Day: 1 MJD: 60443.500
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 | -12 -16 -18 -10 -4 | 3 22
emr uuuuu | -33 11 73 -16 8 | 13 27
esa uuuuu | 34 15 89 126 -8 | 20 28
gfz uuuuu | -14 -14 33 80 -4 | 16 25
grg uuuuu | -14 19 -41 -79 3 | 9 20
igr xxxxx | -5 4 1 -35 10 | 4 20
irf xxxxx | 0 15 32 37 -6 | 3 21
jgx uuuuu | -31 -20 122 -57 3 | 13 23
mit uuuuu | 20 3 -44 88 -4 | 23 31
ngs uuuuu | 56 3 -256 -272 3 | 15 23
Table 7.2314.2 GPS week: 2314 Day: 2 MJD: 60444.500
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 29 71 36 -1 | -3 24
emr uuuuu | 3 -14 -6 22 2 | 10 27
esa uuuuu | 28 1 -4 56 -8 | 15 28
gfz uuuuu | -19 -23 33 -92 -2 | 12 25
grg uuuuu | 9 9 27 -56 5 | 6 21
igr xxxxx | -6 -2 1 -120 3 | 0 20
irf xxxxx | -1 -1 -8 9 -2 | -1 24
jgx uuuuu | -31 -19 66 -13 2 | 9 23
mit uuuuu | 21 -28 -62 20 -6 | 18 30
ngs uuuuu | -36 40 -195 -24 2 | 12 23
Table 7.2314.3 GPS week: 2314 Day: 3 MJD: 60445.500
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 | 4 1 -16 78 7 | -7 21
emr uuuuu | -5 4 65 124 -7 | 7 23
esa uuuuu | 18 4 72 92 -2 | 11 24
gfz uuuuu | -12 -21 114 -181 -5 | 10 24
grg uuuuu | -9 11 -5 -146 -2 | 5 20
igr xxxxx | -20 -2 -6 -64 2 | -3 17
irf xxxxx | -15 7 5 38 -1 | -3 23
jgx uuuuu | -36 -19 34 -41 5 | 6 19
mit uuuuu | 19 13 -62 85 -11 | 16 28
ngs uuuuu | 3 2 -245 -87 5 | 9 19
Table 7.2314.4 GPS week: 2314 Day: 4 MJD: 60446.500
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 -22 -11 7 7 | -6 21
emr uuuuu | -3 29 87 -12 -8 | 9 23
esa uuuuu | 25 -8 77 81 -3 | 11 24
gfz uuuuu | -17 -18 173 -209 1 | 10 24
grg uuuuu | -32 20 -48 -248 5 | 6 20
igr xxxxx | -10 -2 32 -39 4 | -2 17
irf xxxxx | 9 22 10 60 -1 | -2 23
jgx uuuuu | -26 -42 55 20 0 | 8 19
mit uuuuu | 23 29 -81 215 -7 | 16 28
ngs uuuuu | 21 16 -233 83 0 | 10 20
Table 7.2314.5 GPS week: 2314 Day: 5 MJD: 60447.500
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 1 118 -23 10 | -3 18
emr uuuuu | 9 -3 35 53 -17 | 12 21
esa uuuuu | 16 -6 -38 126 -3 | 13 23
gfz uuuuu | -4 -25 99 -147 -4 | 14 23
grg uuuuu | -25 12 -66 -185 4 | 9 19
igr xxxxx | -15 -8 -7 -103 -2 | 1 14
irf xxxxx | 19 -3 -20 65 -5 | 1 20
jgx uuuuu | -38 -36 79 -17 1 | 10 19
mit uuuuu | 37 17 -140 148 -9 | 19 28
ngs uuuuu | 6 38 -162 33 7 | 12 19
Table 7.2314.6 GPS week: 2314 Day: 6 MJD: 60448.500
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 | -29 -15 45 -16 4 | -1 18
emr uuuuu | 4 8 66 91 -1 | 12 21
esa uuuuu | 22 31 25 91 -5 | 13 23
gfz uuuuu | 9 -23 75 -202 -2 | 14 23
grg uuuuu | -32 21 9 -305 7 | 10 19
igr xxxxx | -8 -7 64 -27 -6 | 2 13
irf xxxxx | 24 10 -1 58 -6 | 1 20
jgx uuuuu | -34 -15 63 -39 -1 | 11 19
mit uuuuu | 60 -3 -123 216 -10 | 19 28
ngs uuuuu | 4 8 -212 234 0 | 14 20
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