[IGSREPORT-30039] Wk 2326 IGS Final Orbits
acc
acc at igs.org
Fri Aug 23 13:24:17 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2326 (Aug 04, 2024 - Aug 10, 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_20242170000_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 | ESA | FAIR FLIN WHIT CZTG FAIR FLIN WHIT
0 | GFZ | 5 13 SEYG SEYG
0 | GRG | 13 21 FAIR COCO FAIR IRKJ KIRU WIND
0 | JGX | HERS URUM
0 | MIT | CHTI HOB2 MAC1 MAR6 PDEL POHN SAMO SFER STJ3 TLSE
0 | MIT | VNDP YEL2 CHTI HOB2 MAC1 MAR6 PDEL POHN PTAG SAMO
0 | MIT | SFER STJ3 TLSE TUVA VNDP YEL2
1 | COD | DAV1 FALK JFNG DAV1 JFNG WIND
1 | GFZ | POHN FALK POHN
1 | GRG | 21 13 21 JFNG PIE1 BJFS COCO IRKJ JFNG
1 | MIT | BUCU CHTI FLRS HERS MARS MIZU PDEL PTGG SFER VNDP
1 | MIT | BUCU CHTI FLRS HERS MARS MIZU PDEL PTGG SFER VNDP
2 | COD | 13 13 IRKJ
2 | ESA | FAA1 JFNG SGOC
2 | GFZ | 21
2 | GRG | 21 CZTG JFNG TONG COCO CZTG JFNG TONG
2 | MIT | FLIN KAT1 METG MOBS NYA1 SFER FLIN KAT1 METG MOBS
2 | MIT | NYA1 SFER
3 | COD | DAV1 DJIG DAV1
3 | ESA | JFNG JFNG
3 | GRG | CZTG COCO CZTG DJIG IRKJ SEYG TONG
3 | JGX | URUM
3 | MIT | BRST FLIN GLPS MAR6 PDEL SFER YAR3 BRST FLIN GLPS
3 | MIT | MAR6 PDEL SFER YAR3
4 | COD | DAV1 KARR MATE SEYG KARR MATE
4 | ESA | JFNG
4 | GRG | IRKJ JFNG TONG CZTG DAEJ IRKJ JFNG SEYG SGOC TONG
4 | JGX | JFNG PIMO
4 | MIT | GAMG JOZ2 KITG METG MIZU SFER VNDP GAMG JOZ2 KITG
4 | MIT | METG MIZU SFER VNDP
5 | COD | DAV1 SGOC DAV1 SGOC
5 | ESA | JFNG
5 | GFZ | 21
5 | GRG | 29 29 BRST CZTG DAV1 HOLB TONG WIND BRST COCO CZTG
5 | GRG | DAV1 HOLB TONG WIND
5 | MIT | BRST GAMG PTGG TLSE TONG YAR3 YEBE BRST GAMG PTGG
5 | MIT | TLSE TONG YAR3 YEBE
6 | ESA | JFNG JFNG
6 | GFZ | 5 AREQ SEYG
6 | GRG | 29 29 AREQ CHPI TONG CHPI DJIG TONG
6 | MIT | BRST FLRS GAMG JOZ2 KITG MELI NYA1 PTGG REYK SFER
6 | MIT | YEBE BRST FLRS GAMG JOZ2 KITG MELI NYA1 PTGG REYK
6 | MIT | SFER 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
----+--------+---------------
5 | GRG | 29
6 | GRG | 29
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 G29 | 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 | 1.9 -.3 1.1 8 -3 -21 -.05
EMR | 0 | 5.6 -7.4 -13.4 19 -9 19 -.32
ESA | 0 | .2 .9 .3 -16 -8 4 -.70
GFZ | 0 | .2 -.7 -1.2 -21 -14 1 -.07
GRG | 0 | .7 .3 -1.3 38 20 20 -.25
JGX | 0 | .5 -3.4 -3.8 3 -28 39 -.36
JPL | 0 | -.4 -13.8 -3.2 -12 78 -43 .34
MIT | 0 | -1.7 -5.4 11.5 0 6 16 -.06
NGS | 0 | 4.9 1.4 -12.9 40 -5 12 -.27
SIO | 0 | -.4 -5.8 -6.3 -39 66 -37 -.18
COD | 1 | 1.7 -.2 .8 1 3 -24 -.07
EMR | 1 | 9.6 -6.2 -16.4 18 -4 22 .00
ESA | 1 | -.6 .9 .5 3 -3 1 -.57
GFZ | 1 | -.3 -.2 -.8 -24 -6 -12 -.08
GRG | 1 | -.1 -.4 -1.3 38 12 4 -.12
JGX | 1 | -1.4 -4.3 -3.6 22 -10 12 -.20
JPL | 1 | -1.9 -7.0 -2.8 -12 57 -45 .25
MIT | 1 | .3 -3.6 9.4 -27 16 4 -.14
NGS | 1 | -1.7 -2.6 -11.6 20 22 -4 -.45
SIO | 1 | 1.6 -3.7 -10.8 7 23 -7 -.04
COD | 2 | 1.4 -.1 .4 7 -17 -17 -.13
EMR | 2 | 2.8 -1.1 -22.9 7 4 6 -.19
ESA | 2 | -.5 .6 .3 -12 -8 5 -.78
GFZ | 2 | -.4 .1 -.7 -4 -16 -19 -.18
GRG | 2 | -.2 -.2 -1.1 39 -13 11 -.24
JGX | 2 | -4.3 -6.4 -4.2 10 -1 -11 -.37
JPL | 2 | -5.5 -4.6 -1.5 -15 51 -26 -.01
MIT | 2 | -4.2 -4.9 13.9 6 9 7 -.21
NGS | 2 | -2.8 -.1 -8.9 17 30 -23 -.49
SIO | 2 | -4.5 -2.0 -5.3 -6 52 14 -.25
COD | 3 | 1.1 -.1 .2 10 -12 -16 -.21
EMR | 3 | .7 -.4 -20.7 7 3 7 -.23
ESA | 3 | .1 .9 .1 -7 -21 -6 -.62
GFZ | 3 | -.4 .8 -.1 -23 -12 -20 .14
GRG | 3 | -.5 -.7 -1.4 26 -10 2 -.05
JGX | 3 | -1.4 -3.6 -3.6 2 -12 19 -.41
JPL | 3 | -5.4 2.0 -1.2 -12 43 -32 .10
MIT | 3 | -2.6 -1.6 15.6 12 7 18 .05
NGS | 3 | -.7 8.0 -9.2 60 10 -38 -.37
SIO | 3 | -6.3 3.2 -8.2 -6 26 -18 -.06
COD | 4 | 1.0 -.3 .1 5 -3 -20 -.24
EMR | 4 | 6.1 -8.9 -14.3 4 12 1 -.07
ESA | 4 | .1 .6 -.3 -2 -16 20 -.65
GFZ | 4 | .0 -.1 -1.4 -12 -23 -5 -.06
GRG | 4 | 1.0 -.9 -2.0 13 5 37 -.11
JGX | 4 | 2.4 -2.0 -7.2 20 -21 23 -.23
JPL | 4 | -1.0 -5.6 .7 -13 40 -14 .35
MIT | 4 | -.7 -2.2 18.0 -10 -3 24 -.18
NGS | 4 | -2.7 .2 -.7 -3 34 -5 -.39
SIO | 4 | -.1 1.4 -3.8 12 -52 25 -.23
COD | 5 | .7 .3 -.2 18 -1 -21 -.35
EMR | 5 | 9.4 -2.7 -18.1 23 -8 23 -.29
ESA | 5 | -.2 .7 -.0 13 -32 11 -.86
GFZ | 5 | -.1 -.5 -1.0 -2 -28 10 -.22
GRG | 5 | 1.0 -1.0 -1.3 -1 -1 31 -.08
JGX | 5 | 5.2 .4 -9.9 36 -33 37 -.38
JPL | 5 | 4.0 -5.0 -1.4 -11 41 -16 .43
MIT | 5 | 1.7 .6 17.5 0 -8 30 -.13
NGS | 5 | -3.4 3.4 -4.6 22 35 -32 -.57
SIO | 5 | .0 6.5 -2.1 66 -31 36 -.16
COD | 6 | .9 -.2 -.0 -1 0 -16 -.27
EMR | 6 | 8.1 -.3 -18.5 15 -9 24 -.16
ESA | 6 | .2 1.2 .0 13 -20 4 -.54
GFZ | 6 | .7 -.6 -.9 7 -23 9 .05
GRG | 6 | .9 -.4 -1.3 16 -7 27 -.12
JGX | 6 | 2.7 .7 -6.1 33 -28 41 -.25
JPL | 6 | -.6 -1.5 -1.2 -8 40 -27 .20
MIT | 6 | -2.9 .2 17.8 -6 5 36 .05
NGS | 6 | .4 1.7 1.2 -13 17 14 -.30
SIO | 6 | 2.1 2.4 -2.5 -21 35 42 .12
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 1.2326.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2326.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 2.2326.[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 3.2326.[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 5.2326.0-6). 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 2326 summary. (Aug 04, 2024 - Aug 10, 2024)
Table 1.2326.a GPS week: 2326 MJD: 60526.000-60532.000
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 788| 0 0 4 8 0 -8 -.02 7 6 | -805 188 5 86
| 0 0 0 7 5 17 .02 | 113 236
emr 108| 0 0 -3 -4 13 11 -.00 9 9 | -2200 479 81 130
| 1 0 1 13 9 13 .01 | 699 805
esa 150| 0 0 0 -8 0 -14 -.03 10 10 | -1526 773 7 87
| 0 0 1 7 6 6 .02 | 270 352
gfz 122| 0 0 2 32 2 -33 .09 9 9 | -107 45 9 108
| 0 0 1 17 9 13 .03 | 122 164
grg 121| 2 0 4 11 0 -10 .03 14 9 | 7 -11 9 131
| 0 0 1 15 19 19 .01 | 47 84
jgx n/a| 0 0 -3 6 -14 5 -.04 10 10 | -34 85 29 100
| 0 0 1 18 7 25 .02 | 86 163
jpl n/a| 0 -2 5 4 -10 2 .13 25 26 | -2761 -210 84 159
| 0 1 0 11 10 15 .01 | 1103 672
mit 368| 0 0 -2 -27 -3 41 .03 7 6 | 4556 -606 70 563
| 0 0 0 23 24 45 .01 | 6265 611
ngs 288| 0 0 -3 10 4 -21 -.09 10 8 | 12817 134 494 742
| 0 0 4 23 13 29 .02 | 6047 159
sio 346| 0 0 0 -17 -7 5 .01 7 7 | --- --- --- ---
| 0 0 0 6 17 22 .01 | --- ---
Table 1.2326.b GPS week : 2326 MJD: 60526.000-60532.000
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 | 6 7 6 7 6 6 9 |
2 | 3 4 3 3 3 3 4 |
3 | 3 3 3 3 3 3 3 |
4 | 5 4 4 4 4 4 4 |
5 | 3 2 3 3 3 3 3 |
6 | 3 3 3 3 4 3 3 |
7 | 3 4 3 3 3 3 3 |
8 | 3 3 3 3 3 3 3 |
9 | 4 4 3 3 4 3 4 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 3 4 4 4 3 |
12 | 3 3 3 3 3 3 3 |
13 | 3 4 4 3 0 4 3 |
14 | 3 3 3 3 4 3 3 |
15 | 3 4 4 4 4 4 4 |
16 | 3 3 3 3 3 4 4 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 3 4 3 4 4 |
19 | 3 3 3 3 3 3 3 |
20 | 3 3 3 3 3 3 3 |
21 | 4 3 3 4 4 4 4 |
22 | 3 3 3 3 3 2 3 |
23 | 3 3 3 3 3 3 3 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 3 3 3 |
27 | 3 3 3 3 3 3 3 |
28 | 3 3 3 3 3 3 3 |
29 | 4 4 4 4 4 5 5 |
30 | 3 3 3 3 3 2 3 |
31 | 3 3 3 3 3 3 3 |
32 | 4 3 4 3 3 3 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2326.0 GPS week: 2326 Day: 0 MJD: 60526.000
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 786| 0 0 3 13 9 -1 -.02 6 6 | -956 124 5 87
emr 106| 1 -1 -1 2 12 -1 .01 10 10 | -2667 1457 68 131
esa 150| 0 0 0 -13 9 -15 -.04 10 10 | -2000 1240 7 82
gfz 120| 0 1 1 20 0 -15 .06 9 10 | -2 -120 11 104
grg 119| 3 0 6 17 41 -1 .05 10 9 | 25 -84 11 154
jgx n/a| -1 1 0 17 -20 29 -.00 11 11 | -81 14 37 104
jpl n/a| -1 -4 5 9 3 -24 .14 25 25 | -2374 887 82 157
mit 368| -1 0 -2 -39 -30 37 .03 8 6 | 11518 -481 34 1036
ngs 289| 0 0 -10 8 21 -8 -.08 10 8 | 14779 106 465 800
sio 350| 0 0 0 -25 -23 -26 .02 7 7 | --- --- --- ---
Table 2.2326.1 GPS week: 2326 Day: 1 MJD: 60527.000
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 786| 0 0 4 16 -5 0 -.00 7 6 | -783 134 6 82
emr 111| 2 0 -2 4 0 25 .02 9 9 | -1856 471 85 136
esa 150| 0 0 1 0 3 -6 -.02 10 10 | -1542 888 7 92
gfz 123| -1 0 0 37 1 -21 .08 9 9 | -11 0 9 106
grg 116| 3 0 5 24 0 -19 .03 12 10 | 69 -1 10 124
jgx n/a| -1 0 -2 25 -16 33 -.03 11 10 | 52 22 27 103
jpl n/a| 0 -2 6 11 -13 -1 .14 25 25 | -1414 -529 83 157
mit 368| 0 0 0 -61 17 -32 .02 7 7 | 11119 0 36 140
ngs 290| -1 0 -7 -13 5 20 -.09 9 8 | 14935 97 503 704
sio 351| 0 0 0 -13 -34 9 -.00 8 7 | --- --- --- ---
Table 2.2326.2 GPS week: 2326 Day: 2 MJD: 60528.000
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 786| 0 0 3 0 -2 7 .01 6 6 | -736 83 6 93
emr 109| 0 0 -5 1 13 17 -.00 10 10 | -2119 613 93 134
esa 150| 1 0 0 -7 7 -8 -.05 10 9 | -1310 482 7 88
gfz 122| 0 0 3 33 -13 -24 .14 9 9 | -228 185 9 115
grg 123| 2 0 4 35 0 -2 .04 10 8 | -50 163 8 129
jgx n/a| 0 0 -2 -20 0 16 -.07 9 9 | -45 138 30 103
jpl n/a| -1 0 4 10 -17 18 .11 26 26 | -1915 -152 86 172
mit 368| 0 -1 -2 -13 -6 0 .01 7 6 | 609 -1227 64 285
ngs 287| 0 1 -3 -4 -3 -18 -.12 10 9 | 14938 170 515 681
sio 351| -1 0 0 -19 0 3 .01 8 7 | --- --- --- ---
Table 2.2326.3 GPS week: 2326 Day: 3 MJD: 60529.000
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 785| 0 0 4 9 -1 14 -.01 7 7 | -744 129 5 80
emr 109| 0 0 -3 -16 26 30 -.02 10 10 | -1490 -582 85 137
esa 150| 1 1 -1 -13 -4 -9 -.01 10 10 | -1129 287 8 91
gfz 124| 0 0 3 11 12 -38 .06 8 8 | -39 -157 8 104
grg 124| 1 0 2 2 -8 23 .04 10 9 | 31 -37 9 139
jgx n/a| 0 0 -1 -17 -14 20 -.05 9 9 | 42 -56 26 108
jpl n/a| 0 -1 4 -6 -25 16 .14 25 25 | -2067 -1111 81 157
mit 368| 0 0 -2 -6 -22 34 .02 7 6 | 11010 -60 34 61
ngs 291| 0 0 -3 38 -13 -74 -.09 10 9 | 15031 -25 506 691
sio 348| -1 0 0 -11 9 -22 .01 7 6 | --- --- --- ---
Table 2.2326.4 GPS week: 2326 Day: 4 MJD: 60530.000
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 786| 0 0 4 8 5 -26 -.02 7 7 | -725 177 6 83
emr 106| 0 0 -3 -5 13 4 -.02 9 9 | -1680 -600 78 129
esa 150| 0 0 0 -19 0 -24 -.07 11 10 | -1611 520 8 83
gfz 125| -1 0 4 14 6 -54 .09 9 10 | -292 292 9 117
grg 122| 2 0 3 3 -14 -18 .03 10 10 | -5 11 9 124
jgx n/a| 0 0 -3 8 -12 -15 -.02 9 8 | -27 81 27 91
jpl n/a| -1 -2 6 0 -16 -1 .12 25 26 | -3250 -632 85 159
mit 368| 0 0 -3 -34 8 86 .05 8 7 | -51 -1220 38 60
ngs 289| 0 0 -2 46 -1 -17 -.09 9 8 | 15399 333 507 885
sio 352| 0 0 0 -15 -16 16 .02 8 7 | --- --- --- ---
Table 2.2326.5 GPS week: 2326 Day: 5 MJD: 60531.000
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 792| 0 -1 4 -3 -1 -27 -.03 7 7 | -714 -30 6 89
emr 111| 2 0 -3 8 25 5 .00 9 9 | -3541 782 83 126
esa 150| 0 0 0 2 -1 -20 -.01 10 10 | -1525 1118 8 92
gfz 124| 0 0 3 48 11 -37 .10 9 9 | 0 -18 9 107
grg 118| 2 0 4 0 3 -11 .03 16 9 | 42 -72 10 136
jgx n/a| 0 0 -5 24 -14 -22 -.05 10 9 | 17 -26 31 103
jpl n/a| 0 -1 4 20 2 -5 .12 26 27 | -4054 -359 87 164
mit 368| -1 0 -1 -43 -27 91 .04 7 6 | -752 -1259 43 1060
ngs 289| -2 0 0 -3 24 -44 -.10 10 9 | 15523 -75 417 742
sio 338| -1 0 1 -8 12 17 .00 7 6 | --- --- --- ---
Table 2.2326.6 GPS week: 2326 Day: 6 MJD: 60532.000
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 797| 0 0 4 11 -3 -25 -.06 7 7 | -981 704 7 92
emr 108| 1 -1 -5 -28 4 -3 .01 9 9 | -2051 1213 80 123
esa 150| 0 0 0 -5 -8 -15 -.02 10 10 | -1567 877 7 83
gfz 121| 0 0 0 58 -3 -41 .12 9 9 | -177 134 10 105
grg 126| 1 0 3 -7 -13 -39 .02 26 9 | -57 -63 9 117
jgx n/a| 0 1 -4 10 -22 -23 -.04 10 10 | -198 426 28 88
jpl n/a| 0 -1 5 -14 -6 17 .13 25 25 | -4256 420 86 150
mit 368| -1 0 -2 6 33 69 .05 7 6 | -1557 5 241 1303
ngs 284| 0 0 3 -2 0 -9 -.07 9 8 | -884 335 551 693
sio 335| 0 0 1 -26 2 37 -.01 8 7 | --- --- --- ---
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 3.2326.0 GPS week: 2326 Day: 0 MJD: 60526.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 13 --- --- --- 9 --- --- 15 9 8 6 | 27 --- --- --- 24 --- --- 27 26 22 24
2 | 6 8 7 11 14 10 9 9 13 7 3 | 39 38 37 42 35 40 42 40 39 39 38
3 | 6 10 11 8 10 8 8 5 7 8 3 | 35 34 36 37 34 36 38 35 29 33 33
4E | 11 9 22 10 11 13 51 8 20 8 4 | 29 30 39 34 32 31 35 32 35 31 30
5 | 5 10 6 11 9 8 9 7 7 4 2 | 39 35 36 40 40 36 39 37 37 37 37
6 | 6 11 9 9 12 7 9 6 9 5 3 | 37 40 40 36 41 38 40 36 41 38 37
7 | 6 9 7 8 12 11 7 9 8 8 3 | 39 40 38 38 41 44 42 38 41 38 39
8 | 5 11 7 9 13 9 9 9 11 7 3 | 36 36 38 39 31 37 40 40 37 37 36
9E | 6 12 11 7 12 10 9 8 14 8 3 | 33 32 35 35 33 35 34 33 35 32 32
10 | 5 7 9 9 7 8 9 6 6 8 2 | 33 31 33 35 32 32 39 32 32 35 32
11 | 7 8 16 9 11 9 59 7 11 7 3 | 47 50 53 47 48 47 60 47 51 49 48
12 | 5 9 7 6 7 14 11 4 8 7 2 | 27 29 28 30 27 32 29 27 29 29 28
13E | 4 7 8 11 13 14 9 6 11 4 3 | 41 25 25 28 30 24 27 25 31 27 41
14 | 5 18 6 7 6 8 53 6 7 8 3 | 26 29 23 26 25 26 28 24 27 24 24
15E | 6 11 14 9 8 12 14 9 9 8 3 | 63 59 57 60 63 57 59 67 66 66 62
16 | 5 8 5 7 8 22 7 5 7 11 3 | 22 25 22 22 22 26 24 23 21 25 22
17 | 5 7 8 15 13 9 9 6 11 9 3 | 32 34 33 34 31 34 33 33 36 35 32
18 | 6 8 16 8 9 12 55 8 12 5 3 | 57 62 59 56 59 58 65 59 60 58 58
19 | 5 7 9 11 13 12 10 8 10 6 3 | 33 33 32 30 31 33 30 33 40 34 32
20 | 6 11 6 10 7 8 9 5 6 7 2 | 26 22 23 27 24 24 26 23 23 23 23
21 | 5 10 9 11 14 15 8 9 12 8 3 | 40 42 41 41 37 46 43 40 41 41 40
22 | 4 7 6 10 7 7 8 6 6 8 2 | 26 26 25 24 25 26 25 25 28 26 25
23 | 5 7 12 10 6 12 51 6 9 8 3 | 26 28 28 30 30 29 37 30 26 31 27
24 | 7 8 10 13 8 12 14 5 7 5 3 | 27 30 30 27 27 28 29 26 28 26 27
25 | 7 13 8 8 5 7 13 5 7 7 2 | 25 32 27 26 28 25 31 23 25 26 25
26 | 8 10 6 7 6 9 10 5 7 6 2 | 22 30 24 22 23 24 30 21 25 22 22
27 | 3 14 7 12 10 8 10 8 9 8 3 | 28 29 29 32 27 28 31 32 27 31 28
28M | 6 8 8 7 9 10 54 6 9 10 2 | 50 51 53 51 52 50 73 52 55 52 51
29 | 8 8 8 9 14 15 7 18 13 7 4 | 218 219 220 220 217 219 219 221 224 220 220
30 | 4 8 9 5 9 8 9 5 7 7 2 | 22 22 22 20 21 24 25 20 22 21 20
31M | 7 9 5 8 8 15 10 5 7 10 3 | 31 35 28 30 26 29 36 27 30 24 28
32E | 8 9 8 9 16 13 12 13 13 9 4 | 31 26 27 28 27 27 29 30 28 29 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 10 10 9 10 11 25 8 10 7 |T 39 40 40 40 38 40 43 39 40 39 39
WRMS | 6 10 10 10 9 11 25 6 8 7 |NE 39 41 40 40 39 41 43 39 40 40 39
MEDI | 6 9 8 9 9 10 9 6 9 8 |MD 32 32 33 34 31 32 35 32 31 31 32
Table 3.2326.1 GPS week: 2326 Day: 1 MJD: 60527.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 13 --- --- --- 9 --- --- 17 13 10 6 | 18 --- --- --- 16 --- --- 25 22 18 18
2 | 9 9 7 11 13 9 10 10 10 10 3 | 25 24 24 25 23 25 26 29 24 26 24
3 | 6 8 10 6 9 8 8 5 9 9 2 | 21 22 23 19 21 20 24 21 18 20 19
4E | 10 9 24 10 12 10 51 7 12 7 4 | 18 20 28 23 20 20 23 21 16 20 18
5 | 5 9 6 5 9 8 9 5 7 5 2 | 23 21 19 23 21 20 24 23 19 20 20
6 | 8 13 9 7 12 7 8 5 10 4 3 | 23 23 26 22 28 22 25 22 24 22 22
7 | 6 10 10 11 34 11 8 5 7 9 4 | 25 26 22 25 35 25 24 25 26 24 23
8 | 5 9 8 8 12 7 10 6 6 9 2 | 24 25 26 25 22 25 26 25 25 23 23
9E | 7 11 10 9 14 9 8 6 11 9 3 | 19 18 21 21 18 17 19 20 20 20 18
10 | 6 6 10 10 9 12 10 4 8 7 2 | 20 19 23 20 20 18 24 20 21 21 19
11 | 7 8 17 7 11 11 62 5 12 5 3 | 18 21 23 23 23 20 29 22 18 23 20
12 | 4 6 7 6 9 18 8 8 10 7 3 | 19 16 16 21 16 19 21 19 22 20 18
13E | 9 9 7 9 20 11 11 6 14 9 3 | 40 26 25 24 30 24 27 23 28 23 38
14 | 5 18 5 10 6 8 53 7 8 7 3 | 9 15 10 17 13 13 15 15 11 13 10
15E | 8 12 14 9 11 13 12 7 9 13 3 | 59 54 53 54 59 54 55 56 56 54 55
16 | 5 7 5 8 6 21 8 6 7 11 3 | 15 16 16 20 12 18 18 16 18 19 16
17 | 4 8 6 9 12 8 9 7 9 7 2 | 20 19 16 21 20 19 20 21 22 19 19
18 | 9 10 17 10 10 9 55 6 11 7 3 | 25 31 30 29 31 28 35 33 30 32 29
19 | 7 7 9 10 11 12 12 7 11 5 3 | 15 13 15 18 17 16 15 18 19 15 15
20 | 6 10 6 5 10 8 11 4 7 4 2 | 17 16 16 18 15 16 19 17 15 15 15
21 | 7 8 7 7 14 12 8 8 10 6 3 | 27 30 30 27 25 31 30 29 33 30 28
22 | 4 7 5 8 8 7 6 7 5 8 2 | 16 19 17 20 16 18 18 18 16 16 16
23 | 7 8 12 8 8 9 53 5 9 7 3 | 18 22 20 24 23 23 27 23 18 23 20
24 | 6 7 8 8 10 9 11 5 7 4 2 | 24 21 24 24 20 21 25 21 21 20 21
25 | 7 11 8 5 7 9 12 4 10 8 2 | 15 27 20 20 18 13 27 17 16 17 17
26 | 6 10 6 9 6 9 12 6 6 6 2 | 15 25 18 18 14 16 26 17 18 15 16
27 | 4 12 7 11 11 8 10 6 8 7 3 | 19 21 22 23 20 19 23 21 20 20 19
28 | 7 9 8 6 10 10 51 7 10 8 3 | 52 50 51 50 49 48 61 51 51 50 50
29 | 8 6 8 11 14 14 8 17 13 9 4 | 127 129 128 126 124 128 126 129 130 128 128
30 | 4 8 8 9 10 7 7 5 8 6 2 | 18 19 18 14 18 17 21 16 20 17 16
31 | 7 10 8 9 9 12 11 5 9 8 3 | 29 30 25 27 22 28 31 26 29 25 26
32E | 9 9 7 9 13 11 10 9 11 9 3 | 21 17 18 17 16 17 20 21 19 19 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 10 9 12 11 25 7 9 8 |T 26 26 26 27 25 25 29 26 26 25 25
WRMS | 6 9 10 9 10 10 25 7 8 7 |NE 23 25 25 25 24 24 27 25 25 24 23
MEDI | 7 9 8 9 10 9 10 6 9 7 |MD 20 21 22 23 20 20 24 21 20 20 19
Table 3.2326.2 GPS week: 2326 Day: 2 MJD: 60528.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 14 --- --- --- 8 --- --- 15 11 9 6 | 26 --- --- --- 18 --- --- 28 20 20 22
2 | 7 7 8 9 10 10 10 8 11 10 3 | 25 22 24 26 23 25 24 26 19 26 23
3 | 5 10 11 8 9 6 7 5 8 10 3 | 28 28 29 29 28 25 30 26 26 27 26
4E | 8 9 26 9 14 9 54 5 15 6 4 | 18 22 30 22 22 21 25 19 20 19 19
5 | 5 8 6 9 6 8 10 4 8 6 2 | 31 29 30 33 32 28 33 30 30 29 30
6 | 8 12 9 9 14 6 8 6 11 5 3 | 35 35 37 37 37 34 35 33 36 34 34
7 | 6 8 8 11 11 11 7 5 7 6 2 | 29 29 26 30 27 30 30 25 25 25 26
8 | 4 9 7 7 11 5 10 5 7 9 2 | 26 26 27 27 27 26 29 24 24 25 25
9E | 6 12 9 8 12 9 9 7 9 6 3 | 22 23 24 25 25 24 23 23 23 24 22
10 | 4 8 10 10 6 8 11 5 11 7 2 | 28 27 29 32 27 26 32 27 31 30 28
11 | 7 7 18 8 10 9 62 5 10 8 3 | 27 28 34 30 31 28 39 28 29 31 28
12 | 6 7 6 7 7 14 11 6 9 7 2 | 27 28 27 30 25 29 28 26 27 26 26
13E | 7 14 7 10 6 8 15 9 16 10 3 | 26 23 24 24 22 23 26 20 24 19 23
14 | 4 19 5 9 4 8 52 7 9 7 3 | 13 15 13 20 15 15 18 16 17 15 13
15E | 7 10 13 10 9 11 12 8 9 11 3 | 58 53 52 56 56 52 55 54 56 53 54
16 | 5 7 5 6 5 18 7 7 8 11 3 | 20 18 20 22 18 20 19 19 20 23 19
17 | 5 9 6 13 11 8 7 7 11 6 3 | 27 24 22 25 27 26 25 24 27 24 24
18 | 6 9 16 9 10 7 56 7 11 6 3 | 29 32 35 28 32 29 41 31 29 30 30
19 | 8 9 7 10 12 10 9 7 11 6 3 | 28 24 27 27 27 27 24 24 27 26 25
20 | 6 9 6 8 7 9 12 6 15 5 2 | 23 20 22 23 22 22 25 20 26 20 21
21 | 7 8 9 11 12 13 8 6 6 7 3 | 35 35 37 36 30 38 35 36 34 36 35
22 | 5 9 7 7 5 7 6 6 8 8 2 | 17 18 16 20 16 16 19 17 20 16 16
23 | 5 7 11 9 6 9 53 5 11 7 2 | 19 20 20 25 22 23 24 22 20 24 20
24 | 5 7 9 8 11 7 13 5 7 5 2 | 25 24 26 26 25 23 27 23 25 22 23
25 | 7 12 8 8 5 6 13 6 9 10 3 | 19 29 23 25 21 20 31 20 20 19 21
26 | 5 10 6 6 6 8 11 7 7 8 2 | 20 27 22 21 19 18 27 20 21 20 20
27 | 5 11 7 6 9 6 11 6 10 8 2 | 23 25 25 26 23 23 26 23 21 23 22
28 | 6 7 8 6 7 8 51 5 9 6 2 | 55 56 58 57 60 56 68 57 59 58 56
29 | 6 6 8 12 14 12 9 16 11 9 4 | 203 203 203 204 194 202 202 202 202 202 202
30 | 6 8 10 10 10 7 8 5 7 6 2 | 26 26 25 25 27 25 27 22 23 23 23
31 | 6 8 5 7 9 11 11 6 9 6 2 | 30 34 26 28 28 29 33 27 29 27 28
32E | 7 11 7 17 15 9 13 5 11 8 3 | 23 22 24 33 25 23 27 25 25 25 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 10 10 9 10 9 26 7 10 8 |T 32 33 33 34 32 32 35 31 32 31 31
WRMS | 6 10 9 9 8 9 26 6 9 7 |NE 32 33 33 34 31 32 35 31 31 31 31
MEDI | 6 9 8 9 9 8 11 6 9 7 |MD 26 26 26 27 25 25 27 24 25 25 23
Table 3.2326.3 GPS week: 2326 Day: 3 MJD: 60529.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 16 --- --- --- 11 --- --- 16 14 8 6 | 34 --- --- --- 21 --- --- 29 23 17 23
2 | 8 8 7 10 12 9 10 8 10 5 3 | 23 21 24 26 24 21 24 25 24 23 22
3 | 5 8 11 9 11 5 8 4 6 6 2 | 26 26 28 27 26 24 29 25 22 25 24
4E | 9 9 25 7 12 6 52 5 11 4 3 | 19 23 33 23 25 23 27 22 18 21 21
5 | 8 11 8 8 6 7 10 5 11 12 3 | 29 26 26 30 29 26 31 27 30 31 27
6 | 10 12 9 7 13 8 8 5 11 6 3 | 25 27 25 23 25 28 25 23 25 22 23
7 | 7 7 9 9 9 9 7 8 7 3 2 | 38 38 38 36 34 38 37 35 39 34 36
8 | 4 9 9 7 8 6 9 5 7 6 2 | 32 31 35 33 34 31 34 31 30 30 31
9E | 9 12 10 10 12 9 10 7 10 6 3 | 20 22 22 24 23 20 23 19 20 18 19
10 | 6 8 10 9 6 8 12 4 8 6 2 | 27 26 27 28 27 24 32 27 25 27 26
11 | 8 9 16 8 11 10 58 7 11 6 3 | 24 28 33 25 32 25 39 27 28 28 26
12 | 8 5 5 5 6 14 10 5 10 6 2 | 22 21 21 22 22 22 23 22 22 22 21
13E | 8 11 7 10 8 9 11 7 15 9 3 | 39 35 35 36 34 33 37 34 43 35 38
14 | 6 19 6 9 4 7 54 7 8 7 3 | 16 20 17 22 20 16 21 18 16 18 16
15E | 7 10 13 9 13 11 13 8 13 8 3 | 73 70 67 71 74 70 70 74 71 72 71
16 | 5 7 5 9 5 19 8 8 9 9 3 | 17 16 17 18 17 18 17 18 16 17 16
17 | 4 7 7 10 13 6 8 6 9 7 2 | 25 26 24 25 27 25 26 23 26 24 23
18 | 8 10 16 10 9 9 51 8 12 5 3 | 27 31 36 33 33 28 41 31 29 32 30
19 | 7 8 8 9 12 9 10 8 13 6 3 | 27 26 25 23 26 26 23 20 29 23 23
20 | 6 11 5 6 8 8 12 5 11 6 2 | 18 17 16 18 18 16 20 16 19 16 16
21 | 8 9 9 11 16 11 7 7 10 7 3 | 30 30 33 34 32 31 32 30 33 31 30
22 | 5 6 7 7 9 6 7 7 7 7 2 | 18 20 20 21 19 18 20 17 19 17 17
23 | 7 5 12 6 6 9 49 4 12 5 2 | 15 17 16 21 21 18 25 17 15 17 16
24 | 6 7 9 7 9 7 14 6 10 5 2 | 22 22 23 22 24 20 27 19 20 19 20
25 | 8 13 10 8 5 6 14 5 12 8 3 | 20 28 23 19 22 19 30 20 21 20 20
26 | 5 11 6 7 6 8 12 8 7 5 2 | 18 25 22 19 18 17 27 21 19 18 18
27 | 5 10 7 7 8 6 11 6 9 5 2 | 23 23 25 23 23 22 27 22 22 21 21
28 | 7 8 7 7 6 7 50 7 13 4 2 | 33 31 34 32 37 33 50 34 40 36 33
29 | 9 7 10 10 14 13 8 17 14 9 4 | 175 175 177 176 178 176 176 178 181 176 177
30 | 5 7 11 7 10 7 7 6 5 6 2 | 21 22 21 19 22 21 23 17 17 19 19
31 | 6 9 7 7 8 11 11 6 8 3 2 | 32 33 31 28 30 28 35 28 26 27 28
32E | 8 11 7 8 11 10 12 5 11 8 3 | 23 24 23 22 24 20 23 21 21 24 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 10 10 8 10 9 25 7 10 7 |T 30 31 32 31 31 30 34 30 30 30 29
WRMS | 7 10 10 8 9 9 25 6 9 6 |NE 30 30 31 30 30 29 33 29 30 29 28
MEDI | 7 9 9 8 9 8 11 6 10 6 |MD 24 26 25 24 25 24 27 23 23 23 23
Table 3.2326.4 GPS week: 2326 Day: 4 MJD: 60530.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 12 --- --- --- 9 --- --- 14 12 8 5 | 17 --- --- --- 13 --- --- 23 19 17 16
2 | 8 9 8 9 17 6 12 8 7 7 3 | 29 28 29 30 26 28 29 32 31 28 28
3 | 6 8 11 8 10 7 10 6 7 7 2 | 20 21 22 21 18 19 25 19 20 19 19
4E | 10 9 26 12 14 7 54 6 13 6 4 | 18 22 33 20 24 21 27 25 22 23 21
5 | 6 10 6 9 6 7 8 6 8 11 2 | 21 23 21 25 22 20 23 23 22 28 22
6 | 12 12 9 9 12 6 10 5 12 7 3 | 35 32 34 31 33 32 35 31 29 31 31
7 | 7 7 10 11 11 6 7 10 7 8 3 | 39 39 40 39 36 39 37 41 39 41 39
8 | 6 10 9 7 9 6 10 6 8 8 2 | 20 21 21 21 20 20 24 23 22 23 20
9E | 10 13 11 11 14 8 10 14 12 4 4 | 20 23 22 23 21 21 23 26 25 21 21
10 | 4 8 11 10 6 6 11 7 8 7 2 | 20 21 22 23 20 18 24 20 25 18 20
11 | 8 6 18 10 10 9 61 6 12 6 3 | 22 25 28 25 27 24 30 27 20 28 24
12 | 4 6 5 5 7 15 9 7 8 5 2 | 20 19 19 21 18 21 21 19 20 20 19
X13E | 3 --- --- --- --- --- --- --- --- --- 0 | 53 --- --- --- --- --- --- --- --- --- 52
14 | 5 18 7 12 5 7 52 8 8 10 3 | 13 17 14 22 16 16 18 18 13 19 14
15E | 7 9 13 13 10 12 12 8 12 14 4 | 60 57 53 56 57 53 59 61 59 63 57
16 | 5 8 6 6 5 20 10 7 7 8 3 | 14 15 12 16 12 14 12 18 17 18 14
17 | 7 8 6 15 13 8 8 6 8 9 3 | 22 23 20 25 23 22 24 24 22 24 21
18 | 7 10 15 8 9 9 50 7 12 5 3 | 24 27 26 26 30 25 31 27 28 25 25
19 | 9 8 8 11 12 10 10 6 8 8 3 | 23 22 22 21 23 23 23 22 22 24 21
20 | 6 11 5 9 7 7 11 4 8 6 2 | 17 17 16 18 16 16 18 17 17 16 15
21 | 7 8 10 10 17 9 8 7 9 10 3 | 39 42 41 42 37 42 41 41 45 37 40
22 | 5 7 7 10 8 6 5 6 5 8 2 | 15 19 16 22 16 16 18 19 15 20 16
23 | 6 7 13 12 6 8 50 4 11 4 3 | 18 20 22 26 22 20 26 22 19 22 20
24 | 7 7 9 9 12 7 12 8 16 8 3 | 24 23 24 25 22 21 26 22 29 22 22
25 | 6 12 9 9 7 9 13 6 10 6 3 | 16 25 18 20 17 13 26 19 18 17 17
26 | 5 11 8 5 6 6 12 6 7 7 2 | 17 25 18 18 15 16 26 21 20 20 18
27 | 5 10 8 11 8 5 11 6 7 7 2 | 20 20 21 23 22 19 22 22 21 22 20
28 | 6 8 8 7 10 8 51 5 11 7 2 | 18 16 19 18 25 17 36 20 19 20 18
29 | 6 7 9 8 13 12 9 17 9 8 3 | 180 178 177 180 188 180 179 181 181 178 179
30 | 5 7 10 8 10 4 9 8 5 9 2 | 21 23 22 21 21 22 23 22 23 24 21
31 | 6 8 7 5 10 10 11 6 7 8 2 | 32 33 30 31 29 31 34 31 31 30 30
32E | 11 13 8 8 11 7 11 9 10 6 3 | 23 23 23 24 24 21 24 25 26 24 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 10 9 10 9 25 8 9 8 |T 29 29 29 30 28 28 32 30 29 29 28
WRMS | 7 9 10 10 10 8 26 7 8 7 |NE 28 30 29 30 28 28 31 30 29 29 28
MEDI | 6 8 9 9 10 7 11 6 8 7 |MD 20 23 22 23 22 21 25 23 22 23 21
Table 3.2326.5 GPS week: 2326 Day: 5 MJD: 60531.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 15 --- --- --- 9 --- --- 13 9 7 6 | 24 --- --- --- 14 --- --- 23 24 21 18
2 | 10 8 7 8 16 7 11 7 8 8 3 | 32 29 32 33 30 30 29 32 29 29 30
3 | 6 7 11 6 9 5 8 5 8 7 2 | 22 22 23 20 21 19 25 20 17 22 20
4E | 9 8 25 10 12 5 55 5 16 7 4 | 17 19 27 19 22 19 24 19 19 19 18
5 | 6 7 6 10 6 6 9 6 9 5 2 | 20 20 19 22 19 19 21 19 21 21 19
6 | 11 12 8 9 8 6 11 5 12 6 3 | 41 44 46 44 47 40 43 45 42 46 43
7 | 7 7 7 10 11 7 8 7 8 5 2 | 43 43 39 40 41 42 41 38 39 41 40
8 | 7 8 8 9 10 6 9 5 10 9 2 | 19 21 22 22 24 20 20 20 22 20 19
9E | 10 10 9 9 13 5 10 8 9 5 3 | 21 20 22 22 23 20 23 22 23 20 20
10 | 5 7 10 11 5 5 12 5 7 7 2 | 21 20 22 24 20 20 24 19 18 22 20
11 | 7 9 16 9 10 7 62 6 13 9 3 | 23 26 26 23 29 24 28 27 23 30 24
12 | 4 7 6 8 10 14 10 6 13 4 3 | 19 16 17 20 18 20 21 20 18 20 18
X13E | 14 10 9 17 12 10 12 9 --- 8 4 | 15 15 13 17 16 13 16 15 --- 15 13
14 | 5 18 4 9 7 5 54 8 5 5 3 | 8 14 9 16 13 12 14 13 7 14 8
15 | 8 12 13 10 23 11 12 7 11 11 4 | 84 79 80 80 83 80 83 83 80 84 81
16 | 5 7 5 8 5 22 9 6 10 11 3 | 16 15 17 22 16 17 16 18 17 21 17
17 | 7 7 7 9 14 7 9 6 9 7 2 | 22 21 18 23 23 21 23 21 22 21 20
18 | 7 9 18 15 10 11 53 7 11 6 3 | 28 31 27 30 31 28 29 32 27 31 29
19 | 8 7 8 9 13 10 9 7 10 7 3 | 21 19 19 20 22 20 20 20 20 21 19
20 | 5 10 5 10 7 7 12 6 7 7 2 | 18 18 17 19 17 17 22 16 18 22 17
21 | 10 7 7 10 18 10 10 8 8 9 3 | 46 47 49 48 45 50 44 48 47 47 47
22 | 5 6 6 8 8 6 4 6 4 6 2 | 12 15 14 17 13 13 16 13 12 14 12
23 | 6 6 12 11 7 10 49 4 12 7 3 | 17 20 19 23 20 21 22 23 21 22 19
24 | 6 7 9 9 12 8 12 7 10 5 2 | 25 23 25 25 24 22 27 24 24 21 23
25 | 6 12 8 7 7 10 15 7 11 5 3 | 15 27 20 19 17 14 28 18 19 16 17
26 | 6 10 6 10 5 9 12 7 10 6 2 | 16 25 20 22 17 17 27 20 18 20 19
27 | 6 9 7 10 8 6 9 5 10 9 2 | 23 24 23 25 24 23 23 22 22 19 21
28 | 7 9 8 8 10 9 50 7 13 8 3 | 25 27 28 27 28 27 38 24 27 28 25
29 | 7 9 9 13 69 24 12 18 12 7 5 | 512 511 511 507 499 505 513 513 515 510 511
30 | 5 7 8 7 10 4 6 6 7 6 2 | 22 24 22 22 23 21 23 19 20 23 20
31 | 6 8 8 8 11 10 11 7 13 8 3 | 26 27 22 27 22 26 30 23 25 23 23
32E | 10 12 8 9 12 7 12 6 14 8 3 | 22 21 23 22 24 21 24 21 21 23 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 10 9 16 10 26 7 10 7 |T 39 41 41 41 40 40 43 40 40 40 39
WRMS | 7 9 10 9 9 9 27 6 9 6 |NE 42 44 44 45 42 43 45 43 42 43 42
MEDI | 7 8 8 9 10 7 11 6 10 7 |MD 22 22 22 22 22 21 24 21 22 21 20
Table 3.2326.6 GPS week: 2326 Day: 6 MJD: 60532.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 14 --- --- --- 10 --- --- 11 --- --- 8 | 34 --- --- --- 26 --- --- 35 --- --- 30
2 | 10 8 8 13 16 7 9 7 8 10 3 | 32 32 32 36 31 31 31 33 32 31 31
3 | 6 7 11 7 10 4 8 7 10 7 2 | 26 28 28 25 28 26 27 25 25 25 25
4E | 8 8 23 10 12 5 55 6 13 7 4 | 21 26 38 29 29 27 32 24 22 25 25
5 | 6 9 6 9 7 8 10 6 7 9 2 | 30 30 30 33 30 28 34 31 33 31 30
6 | 12 9 8 9 14 6 10 5 10 5 3 | 40 38 40 41 46 38 42 41 38 39 39
7 | 7 7 10 13 7 9 8 8 6 7 3 | 52 53 53 53 50 52 52 46 50 48 50
8 | 7 9 8 11 10 6 9 6 7 8 3 | 24 23 23 24 28 21 23 20 23 21 21
9E | 10 10 9 12 13 10 10 5 11 7 3 | 24 23 24 28 29 26 23 23 26 23 23
10 | 6 8 10 9 7 9 12 5 6 6 2 | 26 26 26 29 26 26 30 27 27 25 26
11 | 8 8 16 8 11 10 57 5 10 8 3 | 27 30 35 34 34 28 42 32 28 34 30
12 | 5 7 5 7 7 15 11 5 10 6 2 | 27 28 27 29 27 28 29 28 31 27 27
13E | 6 9 8 8 6 10 10 7 10 9 3 | 16 15 14 17 15 13 17 18 9 16 14
14 | 6 19 6 11 5 6 52 7 7 9 3 | 20 21 21 26 23 22 28 22 22 22 20
15 | 9 10 11 8 11 12 12 8 12 11 3 | 66 63 61 64 64 63 66 66 64 65 63
16 | 5 7 6 8 6 24 11 6 9 9 3 | 24 22 23 24 22 23 22 25 24 24 23
17 | 6 6 6 11 12 8 9 7 9 8 3 | 26 26 21 25 27 24 26 26 26 23 23
18 | 8 10 18 10 9 11 55 5 10 6 3 | 30 34 34 34 34 30 42 36 34 34 32
19 | 6 7 7 11 12 11 8 8 9 6 3 | 22 21 23 27 27 24 25 24 25 22 22
20 | 7 9 4 9 10 7 12 8 7 10 3 | 22 23 22 26 23 22 25 21 25 24 22
21 | 12 7 9 10 12 10 8 7 7 13 3 | 48 51 52 52 48 52 49 51 50 50 50
22 | 4 6 7 11 8 7 5 6 6 7 2 | 23 24 24 29 24 24 24 22 23 20 22
23 | 6 8 11 6 6 10 51 4 10 5 2 | 28 32 30 31 32 30 41 32 29 31 30
24 | 7 8 9 6 10 8 12 6 10 7 2 | 31 32 33 33 31 33 35 30 31 27 30
25 | 7 12 9 6 6 11 12 6 9 7 3 | 22 33 29 28 24 21 32 26 28 24 25
26 | 6 10 6 8 6 10 13 7 7 8 2 | 23 30 25 23 22 22 30 26 23 26 24
27 | 6 10 8 6 10 7 11 5 7 6 2 | 26 26 25 25 29 25 25 23 27 23 24
28 | 7 9 8 9 11 11 50 7 11 6 3 | 94 94 95 93 95 95 102 95 98 94 94
29 | 6 9 8 7 137 20 10 16 12 12 4 | 762 764 763 758 739 761 759 762 763 758 761
30 | 5 6 9 12 10 5 8 6 6 8 2 | 30 31 29 29 32 30 31 26 29 28 28
31 | 7 8 7 8 10 12 12 7 10 6 3 | 47 47 44 43 45 48 49 44 46 44 44
32E | 11 11 8 7 12 9 13 5 12 7 3 | 28 28 28 28 28 30 31 27 28 24 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 10 9 26 10 25 7 9 8 |T 54 56 56 57 55 55 58 55 56 55 54
WRMS | 7 9 10 9 9 10 25 6 8 7 |NE 58 60 60 61 58 59 62 58 60 59 57
MEDI | 7 8 8 9 10 9 11 6 9 7 |MD 27 30 29 29 29 28 31 27 28 26 26
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 4.2326 GPS week: 2326 MJD: 60526.0-60532.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 9 10 26 |U 8 10 35 |U 12 13 29 |
emr | emr 2961 |U 12 14 31 |U 7 13 43 | 13 14 29 |
esa | esa 2962 | 12 15 37 |U 8 15 44 |U 12 13 34 |
gfz | gfz 2962 |U 10 11 26 |U 8 13 34 | 11 13 26 |
grg | grg 3055 |U 9 11 26 |U 9 15 42 | 11 12 30 |
igs | igs 2957 | 8 10 24 | 7 11 34 | 11 12 26 |
jgx | jgx 2962 |U 9 10 24 |U 8 10 32 | 11 13 28 |
jpl | jpl 2962 | 15 16 37 | 11 21 48 | 13 12 37 |
mit | mit 3058 |U 9 11 26 |U 9 12 37 |U 12 10 31 |
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 5.2326.0 GPS week: 2326 Day: 0 MJD: 60526.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 10 30 | 7 12 32 | 15 17 40 |
emr | emr 2976 | 9 9 30 | 8 16 40 | 14 15 26 |
esa | esa 2976 | 11 12 35 | 8 17 39 | 11 15 35 |
gfz | gfz 2976 | 10 10 28 | 9 15 41 | 12 15 31 |
grg | grg 3072 | 10 11 31 | 8 17 36 | 13 13 36 |
igs | igs 2976 | 9 9 30 | 7 14 30 | 12 13 30 |
jgx | jgx 2976 | 10 8 30 | 8 12 28 | 14 14 34 |
jpl | jpl 2976 | 15 13 33 | 11 25 47 | 12 12 33 |
mit | mit 3072 | 9 10 33 | 9 14 34 | 13 11 34 |
Table 5.2326.1 GPS week: 2326 Day: 1 MJD: 60527.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 8 28 | 9 10 35 | 11 8 38 |
emr | emr 2975 | 24 16 31 | 9 13 39 | 12 13 33 |
esa | esa 2976 | 12 13 38 | 10 15 38 | 11 14 37 |
gfz | gfz 2975 | 8 8 25 | 8 12 27 | 10 8 32 |
grg | grg 3070 | 8 9 24 | 10 14 36 | 10 7 37 |
igs | igs 2976 | 7 8 22 | 8 11 30 | 10 8 33 |
jgx | jgx 2976 | 8 9 21 | 8 9 29 | 10 9 34 |
jpl | jpl 2976 | 14 14 36 | 13 24 43 | 12 14 40 |
mit | mit 3072 | 7 6 21 | 10 10 34 | 10 10 38 |
Table 5.2326.2 GPS week: 2326 Day: 2 MJD: 60528.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 9 20 | 7 11 28 | 11 12 24 |
emr | emr 2976 | 9 13 28 | 8 14 39 | 13 13 26 |
esa | esa 2976 | 10 13 33 | 8 15 42 | 11 11 32 |
gfz | gfz 2976 | 12 11 28 | 7 14 23 | 11 13 23 |
grg | grg 3071 | 8 9 22 | 7 16 32 | 11 10 24 |
igs | igs 2943 | 7 9 19 | 7 12 28 | 10 10 21 |
jgx | jgx 2976 | 7 10 21 | 7 10 25 | 11 10 24 |
jpl | jpl 2976 | 14 16 36 | 13 21 46 | 14 10 37 |
mit | mit 3072 | 7 8 19 | 9 12 30 | 11 7 26 |
Table 5.2326.3 GPS week: 2326 Day: 3 MJD: 60529.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 14 17 37 | 6 9 31 | 11 17 22 |
emr | emr 2974 | 14 18 43 | 5 12 37 | 13 15 23 |
esa | esa 2976 | 14 20 52 | 7 14 43 | 11 15 30 |
gfz | gfz 2975 | 14 18 35 | 7 12 32 | 11 15 19 |
grg | grg 3067 | 13 17 37 | 8 13 40 | 11 15 26 |
igs | igs 2976 | 13 17 36 | 6 10 33 | 9 14 20 |
jgx | jgx 2976 | 13 16 35 | 7 8 32 | 9 15 21 |
jpl | jpl 2976 | 17 26 52 | 10 19 44 | 12 12 34 |
mit | mit 3072 | 13 19 39 | 9 9 36 | 10 12 28 |
Table 5.2326.4 GPS week: 2326 Day: 4 MJD: 60530.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 8 23 | 7 7 35 | 14 16 20 |
emr | emr 2880 | 10 11 31 | 7 11 43 | 15 18 27 |
esa | esa 2880 | 11 13 36 | 8 12 48 | 14 15 29 |
gfz | gfz 2880 | 7 8 24 | 7 10 34 | 13 16 20 |
grg | grg 2971 | 8 9 23 | 9 13 46 | 12 15 22 |
igs | igs 2880 | 7 8 22 | 7 9 37 | 13 15 18 |
jgx | jgx 2880 | 8 7 19 | 8 10 37 | 12 16 19 |
jpl | jpl 2880 | 15 15 39 | 11 19 57 | 14 13 33 |
mit | mit 2976 | 7 8 21 | 8 14 39 | 13 13 23 |
Table 5.2326.5 GPS week: 2326 Day: 5 MJD: 60531.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 10 24 | 8 11 35 | 13 16 31 |
emr | emr 2976 | 10 13 28 | 7 13 43 | 13 17 35 |
esa | esa 2976 | 11 14 31 | 9 16 44 | 14 14 40 |
gfz | gfz 2976 | 6 12 23 | 9 14 35 | 12 15 29 |
grg | grg 3067 | 7 14 23 | 10 15 45 | 13 16 35 |
igs | igs 2976 | 6 10 22 | 7 12 35 | 13 14 32 |
jgx | jgx 2976 | 6 11 24 | 8 10 29 | 13 18 32 |
jpl | jpl 2976 | 16 14 35 | 11 21 41 | 15 14 41 |
mit | mit 3072 | 8 12 24 | 9 12 34 | 15 12 38 |
Table 5.2326.6 GPS week: 2326 Day: 6 MJD: 60532.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 8 21 | 8 9 49 | 10 8 30 |
emr | emr 2976 | 12 16 26 | 8 14 57 | 11 11 32 |
esa | esa 2976 | 12 17 35 | 9 16 53 | 13 10 34 |
gfz | gfz 2976 | 8 12 19 | 10 12 43 | 11 8 30 |
grg | grg 3067 | 10 11 19 | 11 15 60 | 11 9 30 |
igs | igs 2976 | 8 10 18 | 8 12 47 | 10 7 28 |
jgx | jgx 2976 | 9 10 18 | 9 12 46 | 11 11 30 |
jpl | jpl 2976 | 13 15 28 | 11 18 61 | 14 9 42 |
mit | mit 3072 | 13 13 22 | 10 15 49 | 10 6 31 |
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 6.2326 GPS week: 2326 MJD: 60526.500-60532.500
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 -17 42 -27 0 | -5 25
| 10 10 37 43 2 | 2
emr uuuuu | -10 -10 88 -5 -6 | -10 31
| 13 16 65 51 10 | 2
esa uuuuu | 18 2 52 179 6 | 0 25
| 6 4 37 19 3 | 3
gfz uuuuu | -5 -41 59 98 1 | 1 22
| 16 15 94 97 5 | 2
grg uuuuu | -9 2 -25 -15 -1 | 1 24
| 10 6 66 45 2 | 3
irf xxxxx | -9 5 -12 11 2 | -1 26
| 6 7 15 9 3 | 2
jgx uuuuu | 13 -6 9 76 -2 | 9 26
| 10 18 39 16 4 | 3
mit uuuuu | 5 39 -96 -151 2 | 17 29
| 19 19 43 27 3 | 2
ngs uuuuu | -10 21 -128 -63 -2 | 4 26
| 29 50 146 147 7 | 3
sio xxxxx | 10 48 -59 3 2 | 22 33
| 47 36 79 66 8 | 2
Table 7.2326.0 GPS week: 2326 Day: 0 MJD: 60526.500
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 -24 78 -67 1 | -3 24
emr uuuuu | -10 -22 172 -31 8 | -8 31
esa uuuuu | 12 9 62 171 3 | 1 25
gfz uuuuu | 5 -38 143 158 0 | 4 21
grg uuuuu | -28 5 -152 -1 1 | 4 24
irf xxxxx | -12 3 -23 -2 0 | 1 26
jgx uuuuu | 23 -16 -48 96 -6 | 13 27
mit uuuuu | 19 36 -159 -154 4 | 18 30
ngs uuuuu | -17 49 -128 -27 -9 | 10 26
sio xxxxx | -25 71 -119 -4 17 | 22 34
Table 7.2326.1 GPS week: 2326 Day: 1 MJD: 60527.500
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 | 10 -20 76 -16 1 | -4 25
emr uuuuu | 9 -34 148 -18 -5 | -8 31
esa uuuuu | 17 -5 -1 160 8 | 0 26
gfz uuuuu | 12 -52 143 245 1 | 3 22
grg uuuuu | -7 -2 -33 45 -4 | 3 24
irf xxxxx | -7 -5 -11 -1 2 | 0 26
jgx uuuuu | 12 -28 37 73 -6 | 12 28
mit uuuuu | -11 43 -66 -139 5 | 18 30
ngs uuuuu | -46 88 -340 -269 -2 | 8 28
sio xxxxx | -2 -4 -44 -46 6 | 23 35
Table 7.2326.2 GPS week: 2326 Day: 2 MJD: 60528.500
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 -7 65 28 2 | -6 26
emr uuuuu | 5 -19 114 100 -6 | -10 32
esa uuuuu | 12 0 56 160 7 | -1 26
gfz uuuuu | 16 -61 114 143 11 | 0 23
grg uuuuu | -8 -6 -54 -28 -5 | 1 25
irf xxxxx | -2 -1 6 18 1 | -2 27
jgx uuuuu | -4 21 31 88 -7 | 10 28
mit uuuuu | -3 6 -91 -180 1 | 17 29
ngs uuuuu | -27 78 -266 -250 -11 | 5 28
sio xxxxx | -13 38 -16 53 2 | 22 34
Table 7.2326.3 GPS week: 2326 Day: 3 MJD: 60529.500
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 -27 16 -72 3 | -8 25
emr uuuuu | -26 -1 72 -42 -6 | -13 33
esa uuuuu | 16 5 118 163 10 | -4 24
gfz uuuuu | -18 -29 48 66 0 | -1 21
grg uuuuu | -9 7 16 38 -3 | -3 23
irf xxxxx | -3 7 -11 15 5 | -5 26
jgx uuuuu | 13 17 12 67 -3 | 5 25
mit uuuuu | 10 38 -90 -112 1 | 15 27
ngs uuuuu | 18 -11 -179 -17 -5 | 1 26
sio xxxxx | 21 73 -198 49 -6 | 19 30
Table 7.2326.4 GPS week: 2326 Day: 4 MJD: 60530.500
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 -18 19 27 0 | -8 25
emr uuuuu | -12 0 44 22 -21 | -13 33
esa uuuuu | 23 3 48 196 3 | -2 25
gfz uuuuu | -25 -15 104 -57 -2 | -1 21
grg uuuuu | -4 -1 -26 -24 1 | -3 23
irf xxxxx | -9 5 -23 20 7 | -4 26
jgx uuuuu | 13 -8 -38 60 2 | 5 25
mit uuuuu | 30 70 -149 -155 6 | 16 28
ngs uuuuu | -10 -43 48 -26 4 | 0 26
sio xxxxx | 80 52 -8 -65 -4 | 19 30
Table 7.2326.5 GPS week: 2326 Day: 5 MJD: 60531.500
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 61 -66 -1 | -6 24
emr uuuuu | -20 -3 -20 -32 -17 | -11 30
esa uuuuu | 28 3 23 202 9 | 1 23
gfz uuuuu | -11 -39 -78 93 -1 | 1 20
grg uuuuu | -14 10 40 -64 1 | 0 23
irf xxxxx | -13 12 10 19 -1 | -1 25
jgx uuuuu | 11 -17 56 90 1 | 7 25
mit uuuuu | 11 33 -41 -130 -5 | 18 29
ngs uuuuu | -29 -7 -62 1 7 | 3 26
sio xxxxx | 58 8 -71 101 -3 | 22 31
Table 7.2326.6 GPS week: 2326 Day: 6 MJD: 60532.500
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 | -9 -24 -19 -20 -4 | -4 24
emr uuuuu | -19 11 84 -34 1 | -10 29
esa uuuuu | 21 2 57 198 4 | 4 26
gfz uuuuu | -15 -50 -63 36 -4 | 3 22
grg uuuuu | 6 3 31 -71 -1 | 1 24
irf xxxxx | -19 14 -31 7 0 | 1 26
jgx uuuuu | 26 -9 11 56 4 | 8 26
mit uuuuu | -24 50 -78 -187 2 | 20 30
ngs uuuuu | 40 -6 33 146 1 | 3 27
sio xxxxx | -52 96 39 -67 6 | 24 33
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