[IGSREPORT-30107] Wk 2332 IGS Final Orbits
acc
acc at igs.org
Fri Oct 4 01:08:36 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2332 (Sep 15, 2024 - Sep 21, 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_20242590000_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 | INVK POL2 SCUB
0 | ESA | FAIR NRMD POL2 SYOG WHIT FAIR FLIN NRMD POL2 SYOG
0 | ESA | WHIT
0 | GFZ | 13 LAUT POL2 SYOG IRKJ LAUT POL2 SCUB SYOG
0 | GRG | 13 13 21 CZTG CZTG POL2
0 | JGX | NRMD NRMD
0 | JPL | BADG CHTI CZTG BADG CAS1 CHTI CZTG DAV1 INVK OHI3
0 | JPL | PIMO
0 | MIT | ABPO GAMG GMSD KITG MAR6 PDEL ROTH SFER SOFI TRO1
0 | MIT | WTZZ ABPO GAMG GMSD KITG MAR6 PDEL ROTH SFER SOFI
0 | MIT | TRO1 WTZZ
1 | COD | 6 6 BADG FLRS GOLD HOLB LMMF POHN SGOC THU2 YEL2
1 | COD | GOLD SGOC
1 | ESA | FAIR POL2 FAIR POL2
1 | GFZ | 6 6 13 PIE1 POHN IRKJ PIE1 POHN
1 | GRG | 21 CZTG LPGS SGOC
1 | JPL | BADG CHTI HOLB MAW1 MBAR SYOG THU2 YEL2
1 | MIT | DAV1 FLIN GAMG HOB2 REYK SFER TONG VNDP DAV1 FLIN
1 | MIT | GAMG HOB2 REYK SFER TONG VNDP
2 | COD | 28 18 28 DAV1 SCUB CZTG DAV1
2 | EMR | BADG BADG
2 | ESA | FAIR FLIN WHIT FAIR FLIN NRMD WHIT
2 | GFZ | 13 28 PTVL PTVL SCUB
2 | GRG | 13 13 GMSD GMSD
2 | JGX | NRMD
2 | JPL | BADG CHTI SYOG BADG CHTI FAIR SCH2 SYOG
2 | MIT | ABPO BRST FLIN HOB2 IRKJ MDVJ MOBS REYK ROTH SFER
2 | MIT | YEL2 ABPO BRST FLIN HOB2 IRKJ MDVJ MOBS REYK ROTH
2 | MIT | SFER YEL2
3 | COD | 7 30 7 30 DJIG FALK MELI SCUB SEYG TWTF MELI
3 | ESA | CZTG DGAR CZTG DGAR HKSL
3 | GFZ | LAUT FALK LAUT
3 | GRG | 13 13 21 CZTG PIMO CZTG PIMO
3 | JPL | BADG BADG DGAR DJIG FALK IISC MAJU PIMO SGOC SYOG
3 | MIT | BREW GAMG IRKJ KERG MAW1 REYK SFER TLSE TONG YEL2
3 | MIT | BREW GAMG HERS IRKJ KERG MAW1 REYK SFER TLSE TONG
3 | MIT | YEL2
4 | COD | 11 11 BRAZ CUSV SCUB SEYG BRAZ SEYG
4 | ESA | IISC SEYG SYOG YEL2 IISC SEYG SYOG YEL2
4 | GFZ | 13 21 POHN POHN
4 | GRG | 13 13 21 CZTG CZTG
4 | JGX | CHUR CHUR
4 | JPL | CHTI IISC CAS1 CUSV DJIG IISC
4 | MIT | ABPO GAMG JOZ2 MDVJ METG SFER STJO TLSE VNDP YEL2
4 | MIT | ABPO GAMG JOZ2 MDVJ METG SFER STJO TLSE VNDP YEL2
5 | COD | BOGT PIMO POHN SEYG SGOC
5 | ESA | PIMO SEYG SEYG
5 | GFZ | 13 AREQ POHN SCUB AREQ BRUX POHN SCUB
5 | GRG | BOGT CZTG DAV1 CZTG DAV1 PIMO
5 | JGX | NTUS
5 | JPL | GUAM IISC BADG CHTI CUSV DJIG GUAM IISC OHI3 PIMO
5 | JPL | POHN SGOC
5 | MIT | BRST GANP GRAC HOB2 QUIN SFER TONG BRST GANP GRAC
5 | MIT | HOB2 QUIN SFER TONG
6 | COD | AREQ CUSV DGAR FALK GUAM LAUT PIMO POHN SGOC AREQ
6 | COD | DGAR
6 | EMR | BADG BADG
6 | ESA | SEYG TUVA SEYG TUVA
6 | GFZ | 13 13 POHN FALK POHN
6 | GRG | 13 13 CZTG GUAM SCUB CZTG GUAM THTG
6 | JPL | BADG BADG CUSV DGAR FALK IISC KIRI PIMO POHN SGOC
6 | MIT | FLIN GAMG GUAT KIR0 MAR6 PDEL TONG VNDP YAR3 FLIN
6 | MIT | GAMG GUAT KIR0 MAR6 PDEL TONG VNDP YAR3
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. 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 G18 | 4 | | | | | | |
PRN G19 | | | | 4 | | | |
7. 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.
8. 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 | 1.6 -1.8 .9 5 -1 -14 -.14
EMR | 0 | 2.9 -2.8 -4.6 13 -6 13 -.14
ESA | 0 | .5 -.3 .5 18 -19 7 -.60
GFZ | 0 | .7 -.8 -.0 -9 -12 13 .12
GRG | 0 | 1.3 -1.1 -1.5 8 22 15 -.24
JGX | 0 | 5.9 3.5 -10.5 52 -18 29 -.11
JPL | 0 | .9 .8 -6.1 25 -19 -6 -.22
MIT | 0 | 3.9 1.0 21.0 21 -31 -12 -.34
NGS | 0 | 2.4 2.1 12.1 -15 38 8 -.35
SIO | 0 | 3.4 .1 .6 22 20 -6 -.42
COD | 1 | 1.3 -1.6 1.2 8 3 -11 -.13
EMR | 1 | 2.9 3.9 .2 5 -6 13 -.34
ESA | 1 | .2 -.4 .6 1 -3 -8 -.90
GFZ | 1 | .5 -.6 -.4 5 -15 4 .07
GRG | 1 | .8 -1.1 -1.7 13 -1 17 -.19
JGX | 1 | 4.4 4.2 -5.5 34 -1 14 -.20
JPL | 1 | 4.0 2.8 -2.4 27 -10 0 -.17
MIT | 1 | 6.2 -1.8 23.1 22 -15 -9 -.36
NGS | 1 | -.9 6.2 13.1 1 56 -17 -.57
SIO | 1 | 3.8 -.2 6.8 66 -74 58 -.31
COD | 2 | 1.0 -1.2 1.1 4 -2 -10 -.15
EMR | 2 | -2.7 .1 -1.5 10 -12 9 -.23
ESA | 2 | .3 -.2 1.2 12 -12 7 -.72
GFZ | 2 | .7 -.8 .1 -13 -16 -1 .09
GRG | 2 | .1 -1.2 -1.1 -7 8 10 -.11
JGX | 2 | 3.6 2.1 -4.9 40 0 16 -.12
JPL | 2 | -.4 -1.1 -1.2 20 -2 -8 -.23
MIT | 2 | 4.0 -2.0 25.5 14 -25 6 -.36
NGS | 2 | .7 2.1 7.8 -10 26 -9 -.41
SIO | 2 | 4.1 .5 8.0 20 1 43 -.41
COD | 3 | .5 -.9 1.1 -2 4 -14 -.13
EMR | 3 | 2.2 -4.7 4.4 8 -12 13 -.17
ESA | 3 | .3 -.3 .7 19 -14 5 -.56
GFZ | 3 | .7 -.7 -.1 -8 -14 3 .24
GRG | 3 | .1 -1.0 -1.8 12 14 36 -.10
JGX | 3 | 2.7 2.3 -5.4 32 -4 15 -.17
JPL | 3 | -1.6 -.4 -.9 28 -4 -2 -.05
MIT | 3 | 1.6 -.2 21.8 15 -24 12 -.01
NGS | 3 | -.5 1.6 15.1 -24 52 -3 -.18
SIO | 3 | 4.2 .6 5.3 27 -87 124 -.18
COD | 4 | .7 -.8 .8 9 -5 -16 -.06
EMR | 4 | 4.3 3.8 .5 13 -7 16 -.23
ESA | 4 | .4 -.1 .7 -2 -12 0 -.61
GFZ | 4 | .8 -1.3 -.8 -17 -1 16 .17
GRG | 4 | 1.4 -.6 -1.6 1 13 36 -.10
JGX | 4 | 5.9 4.1 -5.9 44 -19 30 -.16
JPL | 4 | 2.6 5.3 -1.2 30 -19 4 -.11
MIT | 4 | 6.2 -.8 19.9 14 -21 -3 -.18
NGS | 4 | 6.8 4.5 9.8 -2 18 17 -.21
SIO | 4 | 3.6 2.8 -2.2 17 -132 63 -.26
COD | 5 | 1.1 -.4 .8 6 -7 -13 -.08
EMR | 5 | 5.1 1.8 .6 8 -9 9 .03
ESA | 5 | .7 .3 .1 15 -19 12 -.51
GFZ | 5 | 1.0 -.9 -.7 -6 -7 30 .18
GRG | 5 | .5 -.7 -2.1 11 11 27 .09
JGX | 5 | 5.3 1.8 -6.2 38 -11 35 -.07
JPL | 5 | 4.1 1.7 -3.2 22 -16 -6 -.02
MIT | 5 | 6.4 -.5 15.2 27 -18 0 -.12
NGS | 5 | 8.2 2.9 6.1 7 -4 11 -.10
SIO | 5 | 3.9 4.1 -1.6 -13 -129 62 -.26
COD | 6 | 1.2 -1.2 .6 6 1 -11 .03
EMR | 6 | 6.5 1.0 -1.3 -5 -16 14 -.28
ESA | 6 | 1.0 .4 .8 25 -13 13 -.47
GFZ | 6 | 1.5 -1.3 -.3 -9 -26 6 .13
GRG | 6 | .5 -.4 -1.5 25 13 54 -.08
JGX | 6 | 3.9 -.1 -4.5 27 3 48 -.11
JPL | 6 | 1.1 -1.6 -4.4 10 -12 -7 -.02
MIT | 6 | 3.9 2.6 13.9 23 -25 -11 .08
NGS | 6 | 6.2 5.2 8.2 17 15 27 -.18
SIO | 6 | 3.2 6.2 -3.4 42 19 62 -.08
9. 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.
10. 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 1.2332.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2332.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 2.2332.[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 3.2332.[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 5.2332.0-6). 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 2332 summary. (Sep 15, 2024 - Sep 21, 2024)
Table 1.2332.a GPS week: 2332 MJD: 60568.000-60574.000
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 772| 0 0 1 13 5 -14 -.03 8 7 | -701 51 5 85
| 1 0 0 11 16 18 .02 | 67 131
emr 112| -1 0 1 0 4 -24 .04 8 8 | -2107 1356 33 104
| 1 1 0 11 7 17 .01 | 571 1062
esa 150| 0 0 4 -25 -5 -25 -.02 10 10 | -1031 -254 6 77
| 0 0 0 8 8 14 .01 | 337 646
gfz 124| -1 0 1 23 9 -41 .05 13 12 | -69 21 11 121
| 1 0 1 10 13 19 .03 | 63 120
grg 122| 1 0 0 -2 20 -19 -.02 10 9 | -23 33 8 127
| 0 0 1 11 17 8 .01 | 126 242
jgx n/a| 0 0 -2 -5 -22 -15 -.05 10 10 | -12 26 35 91
| 0 1 1 10 12 17 .01 | 136 252
jpl 120| -1 0 0 8 -8 -7 .09 9 9 | -1411 -227 8 66
| 0 0 0 12 8 15 .02 | 1280 721
mit 365| 1 0 -4 2 -6 112 -.02 11 8 | 6446 865 57 82
| 1 0 1 24 24 45 .01 | 490 306
ngs 278| 0 0 0 -1 11 -3 -.12 12 10 | 10677 45 517 753
| 0 0 1 25 11 23 .02 | 7729 94
sio 337| 1 -1 -2 -23 -5 33 -.01 12 9 | --- --- --- ---
| 0 1 1 8 8 30 .02 | --- ---
Table 1.2332.b GPS week : 2332 MJD: 60568.000-60574.000
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 | 10 10 11 7 9 12 12 |
2 | 4 4 4 3 3 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 3 3 3 3 3 3 3 |
5 | 3 3 3 3 3 3 3 |
6 | 5 7 6 4 4 5 4 |
7 | 3 3 4 4 4 3 3 |
8 | 2 3 3 2 3 2 2 |
9 | 3 3 3 2 3 2 3 |
10 | 3 3 3 3 3 3 3 |
11 | 5 6 6 7 5 5 5 |
12 | 3 3 3 3 3 3 3 |
13 | 3 3 3 4 3 3 4 |
14 | 2 3 3 3 3 3 3 |
15 | 3 3 3 3 3 3 3 |
16 | 3 3 4 3 3 3 3 |
17 | 3 3 3 4 6 3 3 |
18 | 7 8 5 5 5 5 5 |
19 | 3 3 3 4 3 3 3 |
20 | 3 3 4 3 3 3 3 |
21 | 4 4 3 4 4 3 3 |
22 | 2 3 3 3 3 3 3 |
23 | 3 3 3 3 3 3 3 |
24 | 4 4 4 4 4 4 4 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 2 3 3 3 |
27 | 3 3 3 3 3 3 3 |
28 | 6 7 7 6 6 5 5 |
29 | 3 3 3 3 3 3 3 |
30 | 4 4 4 5 4 4 4 |
31 | 3 3 3 3 4 4 4 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2332.0 GPS week: 2332 Day: 0 MJD: 60568.000
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 778| -1 0 1 25 8 14 -.03 8 6 | -695 144 6 91
emr 115| 1 0 0 5 -7 -38 .04 8 8 | -3093 2520 32 101
esa 150| 0 0 3 -17 0 -16 -.02 10 10 | -853 -246 7 75
gfz 122| 0 0 0 17 8 -37 .06 11 9 | -146 105 11 114
grg 123| 0 1 0 -20 16 -14 -.02 10 8 | 29 15 9 134
jgx n/a| 0 0 -3 16 -1 0 -.05 10 10 | 6 86 38 88
jpl 120| -2 0 0 18 -11 8 .07 9 9 | -277 147 10 66
mit 365| 0 0 -3 -32 -3 59 -.02 11 8 | 5552 1072 61 78
ngs 282| 0 0 -1 -11 -3 22 -.12 13 11 | 15029 94 416 700
sio 338| 1 -1 0 -19 -1 -4 -.01 13 11 | --- --- --- ---
Table 2.2332.1 GPS week: 2332 Day: 1 MJD: 60569.000
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 777| 0 0 0 22 17 -6 -.01 9 7 | -762 161 6 92
emr 113| 0 3 1 8 2 -11 .03 8 8 | -1783 69 27 99
esa 150| 0 0 5 -38 -2 -39 -.04 11 9 | -1207 343 6 72
gfz 124| -1 0 1 14 -5 -48 .06 12 11 | 0 -76 13 112
grg 125| 1 0 0 4 -14 -15 -.02 10 8 | -27 58 9 140
jgx n/a| 0 0 -3 -12 -20 -22 -.06 10 10 | -18 31 43 106
jpl 120| 0 1 0 17 -8 0 .12 10 10 | -374 166 9 65
mit 365| 0 -1 -3 -12 19 116 -.01 12 8 | 6322 1122 51 74
ngs 283| -1 1 0 -5 17 -4 -.15 13 10 | 14930 166 467 802
sio 338| 0 -3 -2 -16 -6 22 .03 15 11 | --- --- --- ---
Table 2.2332.2 GPS week: 2332 Day: 2 MJD: 60570.000
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 775| 0 0 0 17 11 -21 -.06 8 7 | -756 78 6 90
emr 108| -3 0 2 12 1 -16 .05 9 9 | -2243 1725 31 100
esa 150| 0 0 4 -23 0 -12 -.01 11 10 | -1430 450 7 75
gfz 125| 0 0 0 8 10 -33 .06 13 11 | -31 -5 11 119
grg 124| 1 1 0 -15 31 -32 .01 9 8 | -93 121 9 126
jgx n/a| 0 1 -3 -4 -26 -18 -.04 10 10 | -33 78 31 89
jpl 120| -2 0 0 -6 5 7 .08 10 10 | -191 -607 9 63
mit 365| 2 -1 -3 0 -46 113 -.04 11 9 | 7069 737 62 81
ngs 276| 0 0 -2 20 17 0 -.10 13 12 | 14942 105 583 839
sio 337| 2 -2 -2 -22 -10 32 -.01 12 9 | --- --- --- ---
Table 2.2332.3 GPS week: 2332 Day: 3 MJD: 60571.000
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 770| -1 0 0 17 27 -14 -.02 7 6 | -650 -170 6 84
emr 115| -1 -1 1 -11 18 -49 .01 8 8 | -2017 1080 40 117
esa 150| 0 0 4 -19 -18 -48 -.02 10 11 | -387 -1421 6 82
gfz 126| 0 0 0 28 0 -67 .05 15 12 | -75 48 12 128
grg 123| 1 0 1 6 12 -19 -.03 10 8 | 186 -343 8 124
jgx n/a| 0 1 -2 -13 -32 -19 -.05 10 10 | 215 -387 35 84
jpl 120| -1 1 -1 17 -3 -28 .08 9 9 | -982 -1237 7 61
mit 365| 2 0 -4 3 -13 172 -.01 11 9 | 6770 304 62 83
ngs 276| 0 0 0 7 -2 -26 -.10 12 10 | 15581 -87 633 822
sio 339| 2 -1 -3 -38 -20 91 .02 13 10 | --- --- --- ---
Table 2.2332.4 GPS week: 2332 Day: 4 MJD: 60572.000
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 770| 0 0 0 16 -2 -44 -.03 7 6 | -788 182 5 79
emr 111| -1 1 0 8 6 0 .02 9 9 | -1949 1344 50 120
esa 150| 0 0 4 -34 -2 -12 .00 10 9 | -1080 -115 8 82
gfz 125| -2 0 2 29 7 -18 .02 13 15 | -158 169 10 124
grg 123| 1 0 1 -5 26 -32 -.01 9 8 | 2 27 9 111
jgx n/a| 0 0 -2 -2 -28 -45 -.03 10 10 | 18 2 35 87
jpl 120| -1 1 0 20 -21 0 .07 9 9 | -1900 -1030 9 68
mit 365| 2 0 -5 0 -3 82 -.03 11 8 | 6361 713 60 91
ngs 278| 0 0 0 -7 28 31 -.12 13 11 | 15521 78 494 699
sio 342| 1 -1 -2 -30 -3 50 -.04 12 8 | --- --- --- ---
Table 2.2332.5 GPS week: 2332 Day: 5 MJD: 60573.000
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 769| 0 0 0 -5 4 -7 -.01 8 7 | -620 40 6 82
emr 112| -1 1 1 -18 2 -15 .05 8 8 | -2416 2711 26 97
esa 150| 0 0 4 -25 -16 -17 -.02 9 9 | -1243 -52 6 75
gfz 127| -2 0 3 25 8 -21 .10 12 12 | -6 -186 10 122
grg 119| 1 0 0 12 34 -9 -.02 10 9 | -233 462 9 112
jgx n/a| -1 0 -1 -8 -35 8 -.06 9 9 | -255 462 33 93
jpl 120| -1 0 1 1 -11 -15 .11 9 9 | -3117 525 8 67
mit 365| 2 0 -5 16 23 72 -.02 9 8 | 6280 1172 52 86
ngs 279| 2 0 -1 31 8 -28 -.11 11 10 | -621 35 552 799
sio 335| 1 0 -2 -18 3 13 -.03 10 8 | --- --- --- ---
Table 2.2332.6 GPS week: 2332 Day: 6 MJD: 60574.000
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 767| 1 -1 2 1 -26 -23 -.01 8 7 | -637 -75 5 80
emr 112| -2 0 1 -5 9 -38 .05 8 8 | -1249 46 26 98
esa 150| 0 0 5 -16 0 -34 -.02 10 10 | -1021 -739 7 79
gfz 124| -2 0 2 37 37 -65 .01 12 12 | -73 92 12 132
grg 121| 2 0 -1 -3 35 -15 -.01 11 10 | -29 -103 8 147
jgx n/a| 0 -1 0 -12 -9 -13 -.06 9 9 | -18 -90 31 94
jpl 120| -2 1 1 -8 -10 -26 .11 9 9 | -3041 445 8 78
mit 365| 2 0 -7 45 -22 173 -.02 9 7 | 6768 935 53 82
ngs 277| 0 0 1 -47 14 -18 -.12 10 9 | -641 -76 477 613
sio 335| 1 0 -3 -18 2 28 -.02 10 9 | --- --- --- ---
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 3.2332.0 GPS week: 2332 Day: 0 MJD: 60568.000
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 | 22 --- --- --- 11 --- --- 25 16 16 9 | 49 --- --- --- 38 --- --- 42 24 25 38
2E | 6 7 7 8 15 9 7 11 13 18 3 | 18 18 19 17 23 21 17 19 18 22 17
3 | 6 7 8 6 8 5 8 9 8 9 2 | 22 25 24 22 23 22 26 25 21 21 22
4 | 7 7 9 7 11 6 9 7 9 7 2 | 51 50 52 52 48 50 52 49 51 53 50
5 | 6 7 8 10 7 9 9 7 11 11 2 | 41 39 39 43 41 37 39 43 37 43 40
6E | 19 10 15 14 16 7 12 11 20 13 4 | 101 94 94 96 94 93 93 97 90 101 95
7E | 8 6 8 12 8 13 7 8 10 10 3 | 148 145 145 147 149 146 145 145 146 149 146
8 | 7 5 8 6 6 7 5 7 9 11 2 | 25 25 27 25 24 25 27 25 26 25 25
9 | 6 8 8 8 9 5 7 7 10 8 2 | 33 33 33 33 31 30 33 30 29 32 31
10 | 5 6 7 9 5 8 8 10 9 12 2 | 28 27 27 23 26 26 29 25 26 25 26
11E | 10 9 18 10 11 11 13 17 15 19 4 | 129 126 124 127 127 125 126 128 132 128 126
12 | 5 7 5 7 6 17 5 5 14 9 2 | 44 42 47 49 44 49 48 47 43 47 45
13 | 7 7 7 10 8 11 8 5 12 10 3 | 26 29 27 27 27 23 30 24 24 27 25
14 | 7 7 7 7 7 6 5 5 11 7 2 | 67 64 64 63 64 64 67 64 66 65 65
15 | 6 7 5 8 8 11 6 6 13 9 2 | 44 42 42 43 40 41 42 42 43 42 42
16 | 3 8 5 8 9 17 7 10 13 13 3 | 24 23 23 24 26 18 23 26 25 31 23
17 | 7 7 8 7 7 6 6 6 13 9 2 | 20 21 17 22 18 17 21 20 22 19 18
18E | 11 13 28 32 13 9 23 26 18 28 7 | 162 161 158 167 163 162 161 163 164 169 162
19 | 6 5 7 11 8 13 4 6 20 8 3 | 47 49 46 50 48 44 47 49 53 48 48
20 | 6 8 9 11 8 10 9 5 15 9 3 | 25 25 24 28 26 24 26 24 27 25 24
21E | 8 6 8 8 21 14 9 11 8 17 3 | 36 37 37 38 46 38 36 38 36 39 37
22 | 7 5 6 8 7 7 5 4 12 8 2 | 30 32 29 29 31 31 33 33 38 35 31
23 | 5 9 8 7 8 8 6 9 9 12 2 | 24 25 25 27 29 27 27 28 26 30 26
24E | 11 12 11 12 23 10 8 12 15 12 4 | 29 26 28 26 26 28 26 30 28 26 26
25 | 6 7 8 7 5 8 8 7 16 11 2 | 29 32 32 30 28 27 33 27 29 31 29
26 | 7 7 7 8 4 8 7 9 11 13 2 | 23 24 26 23 22 23 25 25 23 27 23
27 | 8 6 6 7 6 7 5 7 6 11 2 | 29 27 29 29 27 29 31 27 26 29 28
28E | 15 9 23 17 11 10 16 30 15 25 6 | 67 69 73 68 68 68 71 81 67 77 70
29 | 6 6 6 6 7 13 6 5 13 11 2 | 40 41 39 41 40 43 41 41 35 39 40
30E | 8 7 13 17 10 13 7 10 12 11 3 | 69 70 70 67 71 68 67 71 67 72 69
31E | 7 6 5 9 6 10 5 9 10 13 2 | 119 119 120 119 121 121 120 122 120 124 120
32 | 5 7 8 6 5 7 7 7 7 14 2 | 26 26 28 27 23 23 29 22 24 25 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 8 10 11 10 10 9 11 13 13 |T 50 50 50 51 50 49 51 51 49 51 49
WRMS | 6 8 10 9 8 10 9 8 11 11 |NE 33 33 33 33 32 32 34 33 32 33 32
MEDI | 7 7 8 8 8 9 7 7 12 11 |MD 33 33 33 33 31 31 33 33 29 32 31
Table 3.2332.1 GPS week: 2332 Day: 1 MJD: 60569.000
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 | 21 --- --- --- 9 --- --- 23 20 17 9 | 35 --- --- --- 24 --- --- 30 21 24 24
2E | 7 9 9 8 10 10 8 12 9 19 3 | 21 21 24 20 23 25 21 22 23 24 21
3 | 7 8 9 8 9 7 8 7 12 9 2 | 21 25 26 22 21 22 27 23 23 24 22
4 | 7 6 9 6 9 7 9 6 10 8 2 | 46 46 48 48 46 47 46 45 46 47 46
5 | 8 7 8 8 8 9 9 6 12 14 3 | 28 29 27 31 28 29 27 29 29 35 28
6E | 27 21 12 30 15 8 17 12 24 20 6 | 73 71 73 69 72 72 75 75 78 74 71
7E | 9 8 8 8 8 11 12 9 11 9 3 | 83 82 79 79 83 80 78 83 81 81 80
8 | 8 7 7 6 5 7 7 7 7 10 2 | 24 24 25 23 20 22 25 25 26 28 23
9 | 7 7 6 8 9 6 8 8 11 8 2 | 33 34 33 32 30 32 34 33 30 33 32
10 | 4 7 8 11 7 6 8 10 8 11 2 | 23 24 25 20 22 23 27 23 22 24 22
11E | 10 11 19 17 13 9 12 23 22 23 5 | 72 74 70 66 74 72 72 73 81 71 71
12 | 4 5 5 7 8 15 6 4 13 8 2 | 40 40 41 44 38 42 42 40 37 41 40
13 | 6 8 7 10 9 11 9 7 11 12 3 | 22 27 20 23 21 24 28 21 22 25 22
14 | 7 7 6 9 7 7 6 7 11 9 2 | 52 51 50 50 52 50 52 52 49 54 51
15 | 7 6 5 8 8 9 7 8 12 9 2 | 32 30 28 29 28 27 30 30 32 30 29
16 | 5 7 6 7 7 17 9 10 12 13 3 | 21 21 22 24 21 19 23 21 24 27 21
17 | 4 7 7 8 8 6 6 8 9 9 2 | 26 27 24 26 22 23 28 26 25 28 25
18E | 12 12 26 24 11 8 20 35 19 43 7 | 140 143 139 140 143 140 141 147 139 150 141
19 | 5 7 7 10 11 12 7 11 10 8 3 | 52 53 54 54 53 52 55 54 55 53 53
20 | 7 7 10 9 9 11 9 6 13 11 3 | 21 22 21 23 22 21 23 20 19 25 21
21E | 7 11 9 12 18 14 7 11 9 18 4 | 44 41 45 43 52 48 42 43 46 43 43
22 | 6 7 6 10 8 7 6 7 8 10 2 | 23 27 23 23 26 23 28 27 22 28 24
23 | 6 8 9 9 8 8 7 9 13 9 2 | 19 22 21 26 23 24 21 23 23 25 21
24E | 7 9 10 18 17 9 11 10 11 11 4 | 37 36 40 41 35 39 38 38 34 38 37
25 | 8 7 9 8 5 7 9 7 11 10 2 | 32 35 34 33 31 31 37 33 31 34 33
26 | 9 5 8 6 5 8 8 7 8 12 2 | 23 23 25 22 23 23 26 22 24 26 23
27 | 8 7 9 9 4 6 8 8 7 8 2 | 26 26 26 25 23 22 25 25 25 27 24
28E | 14 7 27 14 15 10 18 29 23 29 6 | 65 68 74 67 70 68 71 73 64 75 68
29 | 5 7 5 9 6 12 6 6 14 10 2 | 28 27 28 31 28 28 30 29 27 26 28
30E | 9 8 13 18 10 13 7 9 13 10 3 | 59 56 59 63 59 56 60 57 62 57 58
31E | 7 5 6 7 8 9 6 9 9 10 2 | 82 84 84 83 88 83 83 87 80 86 84
32 | 6 7 8 8 6 7 8 9 9 13 2 | 26 29 30 27 26 25 30 27 26 29 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 8 11 12 10 10 10 12 13 15 |T 41 42 42 42 41 41 43 42 41 43 41
WRMS | 7 8 9 11 8 10 10 8 10 11 |NE 29 30 30 30 28 29 31 29 29 31 29
MEDI | 7 7 8 9 8 9 8 8 11 10 |MD 32 30 30 31 28 29 30 30 29 30 28
Table 3.2332.2 GPS week: 2332 Day: 2 MJD: 60570.000
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 | 21 --- --- --- 11 --- --- 32 20 13 10 | 47 --- --- --- 45 --- --- 48 40 35 42
2E | 9 10 8 10 12 9 9 12 10 14 3 | 26 30 29 27 30 30 31 30 30 32 28
3 | 6 12 10 12 9 9 9 9 12 9 3 | 29 35 32 28 30 31 36 30 29 30 30
4 | 6 9 9 6 9 7 9 5 12 7 2 | 32 34 36 38 36 36 35 34 39 36 34
5 | 6 7 8 8 7 8 9 8 13 11 2 | 45 47 48 52 48 48 48 49 46 51 47
X6E | 10 15 16 22 17 10 --- 9 16 22 5 | 58 55 58 63 60 57 --- 57 62 59 57
7E | 11 6 10 10 10 12 9 13 10 14 3 | 100 100 98 97 97 96 100 99 97 99 98
8 | 7 8 9 7 8 7 10 10 9 13 3 | 29 32 30 31 29 31 35 28 31 31 30
9 | 5 9 8 9 8 6 6 8 9 6 2 | 29 32 32 33 30 29 32 27 31 30 29
10 | 6 7 10 8 5 7 9 8 9 10 2 | 32 33 33 30 32 29 35 32 35 30 31
11E | 12 12 23 14 13 9 17 25 17 29 6 | 98 96 91 100 96 94 93 96 97 99 95
12 | 5 5 6 5 8 14 7 6 14 7 2 | 37 37 38 38 36 39 39 38 34 40 37
13 | 7 10 7 9 8 9 10 7 14 8 3 | 33 37 35 37 33 36 40 33 37 37 34
14 | 6 9 6 12 8 7 6 6 12 6 2 | 41 44 43 40 42 40 43 43 42 41 41
15 | 8 8 6 6 6 8 8 8 17 10 2 | 40 38 38 36 36 38 38 35 32 36 36
16 | 6 8 6 8 10 17 9 12 11 13 3 | 37 39 38 38 37 34 37 36 38 36 36
17 | 5 7 6 11 6 9 6 9 10 8 2 | 33 25 33 24 19 20 26 21 23 20 33
18E | 10 11 21 29 13 6 17 17 17 13 5 | 79 78 81 80 79 81 79 78 73 76 78
19 | 9 10 6 11 7 11 8 12 15 9 3 | 49 54 51 50 48 46 54 46 51 45 48
20 | 12 7 7 6 10 11 10 8 16 13 3 | 33 34 35 38 32 35 35 36 31 38 33
21E | 7 8 9 8 13 11 9 12 9 10 3 | 31 33 30 30 33 32 30 32 29 32 30
22 | 4 7 7 11 6 5 5 7 13 7 2 | 38 41 39 39 39 38 42 41 39 40 39
23 | 6 8 8 9 8 7 8 9 11 11 2 | 32 33 33 33 35 33 33 35 34 32 32
24E | 6 9 11 21 17 10 11 8 17 11 4 | 23 24 28 28 26 25 24 24 23 26 23
25 | 6 8 9 8 6 8 11 7 12 8 2 | 26 28 29 25 25 22 32 23 24 23 25
26 | 8 6 8 7 7 7 10 11 12 10 3 | 33 32 34 30 31 32 34 28 34 30 31
27 | 9 8 8 7 6 6 9 12 7 13 3 | 31 32 31 31 32 31 35 29 30 30 30
28E | 10 13 26 41 9 11 17 24 21 23 6 | 48 47 50 48 47 46 47 47 45 47 44
29 | 5 8 6 10 10 14 7 7 16 10 3 | 36 37 36 38 38 39 38 38 37 37 36
30E | 10 10 12 13 11 10 8 6 16 9 3 | 38 41 41 35 38 38 53 38 43 38 38
31E | 7 7 6 9 6 12 8 8 17 10 3 | 84 83 83 87 86 83 83 84 84 82 83
32 | 7 9 8 7 5 7 10 5 11 8 2 | 27 34 31 27 27 25 32 28 28 31 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 9 11 13 9 10 10 11 13 12 |T 42 43 43 42 42 41 43 41 42 42 41
WRMS | 7 9 10 11 8 10 10 9 12 9 |NE 34 36 35 35 34 33 37 34 34 34 34
MEDI | 7 8 8 9 8 9 9 8 12 10 |MD 33 37 36 37 36 36 36 35 35 36 34
Table 3.2332.3 GPS week: 2332 Day: 3 MJD: 60571.000
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 --- --- --- 10 --- --- 22 15 11 7 | 54 --- --- --- 44 --- --- 48 42 48 47
2E | 5 8 9 11 9 11 8 10 12 15 3 | 41 43 45 43 44 44 43 40 45 48 42
3 | 5 11 8 7 7 5 8 10 11 7 2 | 42 45 44 42 44 44 46 42 47 44 43
4 | 6 7 9 8 7 7 8 5 10 7 2 | 41 44 44 44 45 41 43 41 40 45 42
5 | 6 8 7 9 6 9 10 9 7 10 2 | 47 50 50 53 52 50 50 47 51 49 49
6E | 8 7 11 36 11 8 8 9 13 10 4 | 48 46 48 48 45 46 49 43 48 46 45
7E | 8 8 12 10 10 15 9 15 15 19 4 | 67 65 64 65 69 63 63 72 73 75 67
8 | 5 6 8 7 6 6 6 8 9 9 2 | 36 41 41 40 40 39 42 34 38 41 38
9 | 8 7 7 8 6 5 6 8 6 7 2 | 39 44 41 44 41 40 42 37 44 40 40
10 | 6 9 9 9 7 8 9 7 10 12 2 | 42 42 43 41 39 37 44 38 41 41 40
11E | 9 13 26 37 13 11 17 31 24 32 7 | 79 77 74 93 77 78 76 84 86 84 78
12 | 5 5 5 8 6 14 7 5 12 8 2 | 42 46 46 45 44 47 49 45 45 46 45
13 | 5 9 6 9 22 12 8 9 13 16 3 | 34 40 36 37 33 39 39 34 40 40 35
14 | 7 8 6 11 7 8 6 6 13 6 2 | 41 44 45 47 44 44 44 41 47 44 43
15 | 7 6 6 8 6 9 6 7 9 7 2 | 46 49 47 48 46 46 47 45 44 48 46
16 | 5 7 5 9 10 17 7 10 10 10 3 | 36 40 39 40 40 36 38 35 37 41 37
X17 | 3 --- 5 --- --- --- --- --- --- --- 4 | 27 --- 26 --- --- --- --- --- --- --- 26
18E | 10 9 22 18 10 8 17 20 16 18 5 | 109 111 112 112 111 109 112 111 112 115 110
19 | 12 9 7 10 11 14 11 17 16 10 4 | 153 156 157 158 158 156 155 156 160 157 156
20 | 6 8 7 8 7 10 10 5 9 7 2 | 36 40 40 42 40 39 40 38 41 41 38
21E | 8 7 11 13 21 14 9 8 14 16 4 | 34 34 35 34 40 35 32 35 38 38 34
22 | 6 6 7 10 8 7 5 7 13 8 2 | 45 46 44 48 43 43 46 43 51 44 44
23 | 6 9 8 8 8 8 9 8 10 9 2 | 38 38 39 40 39 36 40 37 38 41 38
24E | 7 8 10 22 17 14 11 9 15 10 4 | 28 34 34 32 31 33 32 30 34 36 30
25 | 5 7 9 8 4 7 11 6 9 12 2 | 40 44 43 39 41 37 45 37 41 41 40
26 | 5 6 8 9 7 5 8 7 7 8 2 | 40 41 42 38 39 39 43 36 36 40 39
27 | 7 8 7 10 7 7 6 8 8 9 2 | 36 39 39 39 38 38 40 35 34 39 37
28E | 11 11 20 31 8 13 13 20 13 27 5 | 38 35 39 40 39 35 38 43 41 49 37
29 | 5 6 6 6 5 12 8 8 10 7 2 | 37 41 40 41 42 41 42 36 42 42 39
X30E | 9 11 13 19 15 10 --- 9 19 4 4 | 54 57 59 59 58 55 --- 54 64 58 56
31E | 8 9 6 10 8 8 12 13 12 13 3 | 101 102 101 102 101 103 101 105 104 104 102
32 | 6 8 8 9 5 9 7 7 10 12 2 | 37 40 39 34 36 36 39 33 35 39 36
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 8 10 15 10 10 9 11 12 13 |T 49 52 51 52 51 50 52 50 52 53 49
WRMS | 6 8 11 12 8 10 9 9 10 10 |NE 44 48 46 48 47 46 48 44 47 48 45
MEDI | 6 8 8 9 8 9 8 8 12 10 |MD 41 44 43 42 43 41 43 41 42 44 40
Table 3.2332.4 GPS week: 2332 Day: 4 MJD: 60572.000
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 --- --- --- 12 --- --- 26 20 12 8 | 43 --- --- --- 35 --- --- 43 23 28 37
2E | 5 11 10 9 8 10 7 11 14 12 3 | 52 57 58 54 55 57 55 52 57 57 55
3 | 6 8 8 7 6 9 7 12 7 9 2 | 35 38 40 41 36 36 39 40 39 43 37
4 | 5 9 8 6 8 8 9 7 12 8 2 | 59 62 64 65 63 61 62 60 58 66 62
5 | 6 7 6 7 7 8 9 6 11 8 2 | 34 34 33 36 33 33 34 35 38 36 34
6E | 6 8 10 29 11 9 8 9 11 7 3 | 49 47 50 50 49 48 50 49 51 49 48
7E | 6 6 10 10 8 12 15 13 12 11 3 | 66 64 61 64 63 62 68 68 60 69 64
8 | 7 9 7 7 6 9 8 9 10 8 2 | 37 39 42 40 37 38 40 37 39 41 38
9 | 5 11 6 8 6 7 8 7 8 7 2 | 55 57 56 56 54 53 54 52 58 57 54
10 | 6 8 9 10 7 7 9 9 10 7 2 | 41 42 45 41 39 39 44 40 40 40 41
11E | 10 11 19 29 18 8 12 15 11 15 5 | 84 84 79 90 76 85 83 87 84 88 82
12 | 8 7 5 10 8 13 6 4 9 7 2 | 47 50 50 50 48 50 51 49 51 52 49
13 | 7 9 6 12 10 11 8 8 11 7 3 | 31 38 30 31 25 33 34 31 35 34 31
14 | 6 7 8 11 9 5 7 6 16 8 2 | 64 66 67 66 66 65 67 65 70 68 66
15 | 6 7 6 5 8 9 6 8 15 8 2 | 44 46 42 43 44 40 43 40 43 43 42
16 | 4 8 4 6 10 17 11 8 14 9 3 | 35 34 37 36 35 32 35 33 35 39 34
X17 | 9 --- --- 14 --- --- --- 8 --- 10 6 | 29 --- --- 33 --- --- --- 28 --- 28 28
18E | 9 11 20 16 13 9 17 20 19 21 5 | 34 37 42 39 37 38 41 38 41 39 37
19 | 7 6 6 10 9 11 7 9 13 7 2 | 84 87 88 90 89 86 86 88 92 87 87
20 | 7 9 6 7 9 10 8 9 11 6 2 | 35 37 37 36 34 32 36 36 39 37 35
21E | 10 10 8 9 16 13 8 10 14 11 3 | 56 60 61 58 60 60 57 57 57 63 58
22 | 5 6 6 11 8 9 5 7 14 10 2 | 34 38 36 37 32 35 38 35 43 39 36
23 | 6 8 8 8 7 7 7 6 13 6 2 | 33 35 37 36 33 35 36 32 34 37 34
24E | 5 10 11 15 12 10 10 11 16 10 3 | 43 46 46 49 42 43 43 43 46 44 43
25 | 6 9 8 9 6 7 11 7 14 13 3 | 46 52 51 51 48 46 52 46 47 52 48
26 | 5 9 7 7 6 6 8 7 10 7 2 | 35 38 40 36 36 34 39 34 36 36 36
27 | 7 7 7 6 6 8 9 9 15 6 2 | 36 37 40 36 36 37 39 35 36 39 37
28E | 11 12 19 35 11 11 12 24 14 30 6 | 44 46 51 51 45 45 47 58 47 62 47
29 | 4 6 5 8 9 12 8 6 12 10 2 | 39 43 43 42 39 39 43 42 41 46 41
30E | 9 9 13 17 12 7 12 9 21 11 4 | 70 71 70 71 67 67 56 68 78 73 69
31E | 9 11 5 8 7 11 14 14 9 20 4 | 96 96 96 98 97 96 97 101 96 102 97
32 | 6 9 9 9 6 6 9 11 13 11 3 | 42 45 47 45 41 40 46 42 40 44 43
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 10 13 9 10 9 11 13 12 |T 47 50 51 50 48 48 50 48 50 51 48
WRMS | 6 9 9 15 8 10 9 8 11 8 |NE 42 45 46 45 43 43 45 42 44 45 43
MEDI | 6 9 8 9 8 9 8 9 13 9 |MD 43 46 46 45 42 40 44 42 43 44 42
Table 3.2332.5 GPS week: 2332 Day: 5 MJD: 60573.000
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 --- --- --- 14 --- --- 20 --- --- 11 | 31 --- --- --- 34 --- --- 42 --- --- 32
2E | 9 9 10 9 10 9 8 10 9 13 3 | 29 26 30 26 27 27 30 30 30 31 27
3 | 6 7 9 11 8 6 7 12 12 7 3 | 20 23 21 21 18 18 24 24 24 21 20
4 | 8 9 7 7 9 6 9 6 12 7 2 | 37 35 36 35 34 35 36 35 37 38 35
5 | 6 8 5 9 8 8 9 7 9 12 2 | 28 24 25 30 25 22 26 31 28 35 26
6E | 7 7 10 36 16 10 7 11 14 9 4 | 65 63 64 67 62 62 64 71 68 69 65
7E | 7 6 8 7 12 13 7 10 12 9 3 | 109 108 108 109 106 108 109 113 111 111 109
8 | 7 8 7 8 6 4 6 7 10 7 2 | 20 22 21 22 19 19 22 20 19 21 19
9 | 7 6 6 7 8 5 5 6 7 5 2 | 26 29 28 27 25 26 30 24 26 27 26
10 | 5 8 8 8 7 5 7 7 9 8 2 | 23 26 26 21 22 22 26 24 24 22 23
11E | 11 11 18 19 12 11 13 17 16 21 5 | 130 129 126 125 125 129 128 132 134 131 128
12 | 6 7 6 8 8 13 6 5 11 8 2 | 29 29 30 29 28 31 30 32 33 33 29
13 | 7 9 6 8 9 10 9 6 10 12 3 | 26 32 28 30 36 28 34 30 31 33 29
14 | 7 7 7 7 11 5 6 6 11 7 2 | 43 44 43 47 42 45 44 42 46 46 43
15 | 7 6 6 5 8 9 7 8 9 7 2 | 30 30 29 28 25 25 29 27 29 28 27
16 | 9 8 6 7 9 14 9 9 11 9 3 | 27 25 28 27 26 23 26 27 28 27 25
17 | 6 7 6 7 10 6 7 6 11 7 2 | 22 21 15 24 15 15 22 24 20 25 22
18E | 11 10 17 16 11 7 13 19 15 17 4 | 54 52 53 56 53 53 52 57 57 57 53
19 | 6 8 6 10 11 12 8 12 15 7 3 | 85 85 83 85 81 83 82 81 83 84 82
20 | 6 9 7 7 8 11 9 7 9 8 2 | 20 20 19 22 18 18 21 24 22 25 19
21E | 7 8 9 8 7 12 7 10 7 12 3 | 43 41 42 41 41 40 42 45 44 44 42
22 | 7 6 5 8 11 8 7 8 7 8 2 | 22 26 26 26 20 23 28 29 29 30 25
23 | 6 8 8 6 9 8 8 7 13 9 2 | 13 18 18 20 19 19 17 21 18 19 17
24E | 9 10 10 17 19 10 12 9 17 7 4 | 21 24 27 34 25 22 26 27 30 28 24
25 | 6 8 9 8 7 6 9 6 10 7 2 | 22 26 25 22 20 18 27 20 19 22 21
26 | 7 7 8 8 8 6 7 5 11 8 2 | 25 25 27 24 23 22 26 24 24 26 23
27 | 8 8 7 9 7 6 7 8 12 8 2 | 22 21 20 20 19 19 23 20 18 20 19
28E | 15 11 19 28 9 12 12 9 14 14 5 | 35 35 39 37 39 34 37 41 35 42 36
29 | 6 6 4 7 9 13 6 8 8 13 2 | 23 24 23 25 22 24 24 28 28 28 24
30E | 9 8 13 12 15 10 12 6 15 10 3 | 43 43 44 42 45 40 36 42 47 47 42
31E | 9 10 6 8 10 10 9 15 9 14 3 | 144 142 143 144 145 142 143 150 142 145 144
32 | 7 8 8 10 6 8 8 7 12 8 2 | 20 24 24 20 17 19 25 20 18 20 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 8 9 12 10 9 9 9 11 10 |T 40 41 41 41 39 39 41 42 42 43 39
WRMS | 7 8 9 12 9 9 9 8 10 8 |NE 27 29 28 28 26 26 29 29 28 30 27
MEDI | 7 8 7 8 9 9 8 8 11 8 |MD 27 26 28 28 25 25 29 29 29 30 26
Table 3.2332.6 GPS week: 2332 Day: 6 MJD: 60574.000
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 | 18 --- --- --- 14 --- --- 18 --- --- 12 | 45 --- --- --- 42 --- --- 47 --- --- 42
2E | 7 8 10 12 10 8 8 9 12 11 3 | 22 21 21 23 23 20 19 22 29 23 21
3 | 7 7 11 8 8 6 7 8 8 5 2 | 24 25 27 23 25 22 27 23 24 23 23
4 | 6 7 8 7 10 9 7 8 12 8 2 | 48 47 50 49 48 46 49 49 49 54 48
5 | 6 7 7 8 9 8 9 7 7 8 2 | 45 42 43 49 44 40 43 46 43 45 44
6E | 7 8 11 34 10 8 7 8 13 9 4 | 80 80 80 78 81 77 75 80 85 80 79
7E | 8 8 8 7 11 10 9 9 10 10 3 | 146 145 143 143 145 144 143 142 145 144 143
8 | 5 8 8 6 7 5 7 5 8 8 2 | 18 22 23 22 22 21 22 20 21 20 20
9 | 8 8 7 8 8 6 8 9 12 8 2 | 37 38 37 39 35 35 39 39 37 40 37
10 | 6 6 8 5 9 8 9 5 9 12 2 | 31 31 30 28 29 29 32 27 29 30 29
11E | 11 13 19 17 13 9 13 20 15 22 5 | 139 138 132 135 136 136 135 135 144 136 136
12 | 6 8 6 9 11 11 6 6 10 6 2 | 41 40 42 41 40 45 45 42 44 42 42
13 | 10 10 6 8 32 10 9 7 7 11 4 | 28 34 27 30 30 28 33 28 28 29 28
14 | 7 6 9 8 9 5 7 7 9 7 2 | 59 59 57 58 57 57 58 56 56 57 57
15 | 8 6 5 7 9 9 5 8 7 8 2 | 36 38 36 38 33 35 37 34 32 35 35
16 | 8 8 7 9 10 14 8 6 10 10 3 | 25 23 23 21 26 19 22 20 22 25 21
17 | 7 8 6 7 8 6 7 6 9 8 2 | 21 20 15 25 15 15 21 21 20 21 22
18E | 10 10 19 13 11 7 16 17 16 16 4 | 74 74 73 71 76 76 76 76 71 78 74
19 | 6 6 6 9 10 13 7 11 10 10 3 | 84 86 85 86 84 85 86 83 89 83 85
20 | 7 8 7 8 7 9 9 6 7 9 2 | 25 25 25 27 26 22 27 28 24 26 25
21E | 5 6 10 8 8 11 10 8 9 11 3 | 32 29 28 29 32 27 26 30 34 31 29
22 | 8 7 6 6 9 9 5 7 7 9 2 | 24 26 22 24 20 23 26 26 25 26 24
23 | 7 7 7 6 11 8 8 7 14 9 2 | 22 21 22 24 23 23 23 24 24 25 22
24E | 8 10 10 10 18 10 11 7 13 11 3 | 25 26 28 32 24 28 27 26 25 25 25
25 | 6 10 9 8 10 5 9 8 8 6 2 | 27 30 28 26 27 23 30 25 24 24 25
26 | 10 7 10 10 10 5 7 6 13 6 3 | 27 26 30 24 24 25 29 23 29 26 25
27 | 6 8 7 7 8 6 8 6 9 8 2 | 21 24 25 23 24 24 26 21 20 23 22
28E | 15 10 19 33 11 10 13 10 14 12 5 | 45 45 48 50 47 44 48 47 46 45 45
29 | 7 6 4 8 10 13 7 5 8 6 2 | 34 33 33 34 34 36 34 34 33 34 33
30E | 12 9 12 13 14 9 15 16 11 14 4 | 73 72 73 72 73 73 65 79 77 74 73
31E | 11 9 7 10 10 9 10 17 8 14 3 | 145 143 146 145 146 144 144 144 147 150 145
32 | 7 8 8 6 6 8 9 9 8 9 2 | 22 27 26 24 20 21 27 21 22 24 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 8 10 12 11 9 9 9 10 10 |T 47 48 47 48 47 46 48 47 48 48 46
WRMS | 7 8 10 12 10 9 9 7 9 9 |NE 33 34 33 34 33 32 35 33 33 33 33
MEDI | 7 8 8 8 10 9 8 8 9 9 |MD 32 33 30 32 32 29 33 30 32 31 29
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 4.2332 GPS week: 2332 MJD: 60568.0-60574.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 9 9 28 |U 9 18 45 |U 18 22 66 |
emr | emr 2933 |U 12 14 31 |U 11 18 50 | 24 23 62 |
esa | esa 2948 | 13 19 29 |U 10 20 44 |U 19 22 64 |
gfz | gfz 2959 |U 10 13 26 |U 8 18 43 | 18 20 62 |
grg | grg 3039 |U 12 13 35 |U 9 18 43 | 27 22 74 |
igs | igs 2959 | 10 10 26 | 9 18 42 | 18 20 64 |
jgx | jgx 2948 |U 9 10 27 | 9 18 44 | 17 21 65 |
jpl | jpl 2921 | 11 11 31 | 10 22 48 | 19 22 59 |
mit | mit 3058 |U 27 18 59 |U 12 24 48 |U 20 16 58 |
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 5.2332.0 GPS week: 2332 Day: 0 MJD: 60568.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 9 31 | 9 13 40 | 11 12 46 |
emr | emr 2958 | 18 25 30 | 11 14 43 | 24 18 48 |
esa | esa 2976 | 13 18 23 | 11 17 41 | 14 14 43 |
gfz | gfz 2975 | 11 16 23 | 9 16 37 | 14 13 40 |
grg | grg 3072 | 15 21 53 | 10 15 39 | 21 18 58 |
igs | igs 2976 | 9 10 21 | 10 14 38 | 11 11 41 |
jgx | jgx 2976 | 9 10 22 | 10 14 39 | 10 9 39 |
jpl | jpl 2976 | 10 9 25 | 10 19 42 | 14 14 41 |
mit | mit 3072 | 13 10 44 | 12 17 46 | 13 9 32 |
Table 5.2332.1 GPS week: 2332 Day: 1 MJD: 60569.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 11 31 | 8 19 45 | 12 17 43 |
emr | emr 2960 | 13 13 33 | 12 18 51 | 12 17 43 |
esa | esa 2976 | 16 19 37 | 9 21 38 | 15 14 44 |
gfz | gfz 2975 | 14 13 36 | 8 21 42 | 11 14 42 |
grg | grg 3070 | 13 13 35 | 9 21 39 | 12 15 50 |
igs | igs 2976 | 13 12 34 | 9 21 42 | 12 16 44 |
jgx | jgx 2976 | 13 14 35 | 11 20 47 | 11 14 44 |
jpl | jpl 2976 | 14 11 38 | 10 22 43 | 13 17 41 |
mit | mit 3072 | 127 67 243 | 10 23 44 | 15 11 36 |
Table 5.2332.2 GPS week: 2332 Day: 2 MJD: 60570.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 9 23 | 10 17 53 | 57 53 201 |
emr | emr 2956 | 11 14 30 | 8 20 53 | 61 52 162 |
esa | esa 2976 | 13 23 25 | 8 17 39 | 53 74 191 |
gfz | gfz 2976 | 7 14 18 | 9 18 43 | 54 57 188 |
grg | grg 3064 | 8 10 25 | 9 17 40 | 64 45 167 |
igs | igs 2976 | 8 11 24 | 7 17 41 | 57 53 199 |
jgx | jgx 2976 | 7 9 27 | 8 18 43 | 58 64 210 |
jpl | jpl 2880 | 11 12 27 | 9 28 53 | 52 67 169 |
mit | mit 3072 | 14 20 28 | 7 24 47 | 51 36 199 |
Table 5.2332.3 GPS week: 2332 Day: 3 MJD: 60571.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 11 25 | 10 23 37 | 11 21 46 |
emr | emr 2862 | 10 13 27 | 12 17 46 | 13 17 38 |
esa | esa 2880 | 12 22 24 | 11 25 47 | 13 14 47 |
gfz | gfz 2880 | 9 12 25 | 9 21 45 | 11 15 46 |
grg | grg 2970 | 13 17 41 | 10 18 42 | 21 20 59 |
igs | igs 2879 | 9 12 22 | 9 22 40 | 11 16 43 |
jgx | jgx 2880 | 9 11 21 | 9 22 43 | 9 15 41 |
jpl | jpl 2784 | 11 11 25 | 11 22 43 | 15 15 45 |
mit | mit 2976 | 15 9 26 | 20 38 58 | 12 11 27 |
Table 5.2332.4 GPS week: 2332 Day: 4 MJD: 60572.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 7 27 | 9 18 44 | 11 15 43 |
emr | emr 2862 | 13 12 30 | 10 20 55 | 29 21 70 |
esa | esa 2880 | 12 19 28 | 10 19 41 | 13 13 48 |
gfz | gfz 2959 | 8 10 26 | 7 15 39 | 12 12 45 |
grg | grg 2969 | 9 10 30 | 8 15 41 | 27 19 71 |
igs | igs 2954 | 7 8 24 | 8 16 43 | 10 12 44 |
jgx | jgx 2880 | 8 10 26 | 6 17 40 | 9 12 45 |
jpl | jpl 2880 | 9 14 33 | 9 23 51 | 11 12 42 |
mit | mit 3072 | 10 7 20 | 15 27 46 | 14 13 31 |
Table 5.2332.5 GPS week: 2332 Day: 5 MJD: 60573.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 9 28 | 11 17 51 | 13 20 46 |
emr | emr 2964 | 9 11 29 | 12 18 56 | 12 17 40 |
esa | esa 2976 | 15 19 33 | 11 19 55 | 14 15 41 |
gfz | gfz 2975 | 12 19 24 | 9 16 50 | 13 16 43 |
grg | grg 3068 | 12 11 32 | 12 18 57 | 22 20 69 |
igs | igs 2976 | 11 11 27 | 10 17 50 | 12 17 42 |
jgx | jgx 2976 | 8 10 27 | 8 19 50 | 10 17 43 |
jpl | jpl 2976 | 13 12 32 | 12 22 55 | 14 17 41 |
mit | mit 3072 | 7 7 26 | 9 18 51 | 23 19 45 |
Table 5.2332.6 GPS week: 2332 Day: 6 MJD: 60574.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 8 31 | ---- ---- ---- | 12 17 35 |
emr | emr 2975 | 8 8 37 | ---- ---- ---- | 14 18 36 |
esa | esa 2976 | 13 16 36 | ---- ---- ---- | 14 11 34 |
gfz | gfz 2973 | 9 8 30 | ---- ---- ---- | 14 13 34 |
grg | grg 3061 | 12 10 30 | ---- ---- ---- | 19 17 43 |
igs | igs 2976 | 10 9 30 | ---- ---- ---- | 12 12 33 |
jgx | jgx 2976 | 8 9 31 | ---- ---- ---- | 11 14 34 |
jpl | jpl 2976 | 12 11 39 | ---- ---- ---- | 15 16 37 |
mit | mit 3072 | 4 4 21 | ---- ---- ---- | 14 14 34 |
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 6.2332 GPS week: 2332 MJD: 60568.500-60574.500
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 | 1 -9 -17 35 2 | 0 35
| 26 10 36 66 5 | 4
emr uuuuu | 0 -4 15 73 -6 | 2 36
| 13 17 71 67 11 | 5
esa uuuuu | 9 11 69 -6 8 | 18 39
| 10 9 47 50 6 | 4
gfz uuuuu | -16 -22 -9 7 -2 | 8 35
| 30 12 58 178 5 | 4
grg uuuuu | -23 10 -41 -69 0 | 6 34
| 33 15 83 121 4 | 4
irf xxxxx | -9 3 -19 6 -4 | -1 34
| 6 6 15 24 2 | 5
jgx uuuuu | 16 8 -14 5 3 | 14 36
| 8 12 48 25 4 | 4
jpl uuuuu | 5 -13 42 36 8 | 17 38
| 19 15 66 51 11 | 4
mit uuuuu | 3 11 -57 -115 -9 | 29 46
| 26 12 51 96 6 | 5
ngs uuuxu | 2 8 27 2 -4 | 17 38
| 44 31 79 238 6 | 4
sio xxxxx | 52 23 -149 26 13 | 67 76
| 80 34 65 87 12 | 4
Table 7.2332.0 GPS week: 2332 Day: 0 MJD: 60568.500
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 -24 -36 -45 1 | 0 29
emr uuuuu | -17 7 -49 -19 -9 | 6 30
esa uuuuu | 6 1 99 10 8 | 18 35
gfz uuuuu | 14 -18 -16 232 3 | 9 32
grg uuuuu | -3 28 -23 38 -3 | 8 30
irf xxxxx | -15 3 -1 -12 -3 | 2 29
jgx uuuuu | 7 -1 -31 22 -3 | 15 33
jpl uuuuu | -5 -20 39 -45 5 | 13 33
mit uuuuu | -6 18 9 -125 1 | 32 43
ngs uuuxu | 28 20 45 103 1 | 20 36
sio xxxxx | -45 36 -230 144 22 | 62 69
Table 7.2332.1 GPS week: 2332 Day: 1 MJD: 60569.500
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 | -25 -5 -36 -1 -7 | 5 29
emr uuuuu | 4 -11 11 42 4 | 9 30
esa uuuuu | 18 20 113 36 4 | 22 38
gfz uuuuu | 17 -24 40 84 -4 | 14 34
grg uuuuu | 26 12 -119 86 -3 | 12 31
irf xxxxx | -6 -7 2 -11 -8 | 6 29
jgx uuuuu | 17 18 -11 27 -1 | 20 34
jpl uuuuu | -3 -28 67 20 25 | 18 34
mit uuuuu | -24 12 -30 -285 -5 | 37 46
ngs uuuxu | -24 15 -20 -193 -15 | 24 38
sio xxxxx | 76 -25 -153 -56 33 | 69 75
Table 7.2332.2 GPS week: 2332 Day: 2 MJD: 60570.500
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 -69 -24 4 | -4 31
emr uuuuu | -17 -19 72 91 -16 | 2 30
esa uuuuu | 15 5 83 32 16 | 13 32
gfz uuuuu | 4 -7 65 40 -6 | 4 31
grg uuuuu | -4 25 -79 5 0 | 2 28
irf xxxxx | -19 3 -18 -8 -2 | -4 30
jgx uuuuu | 25 10 -31 -2 2 | 10 30
jpl uuuuu | -26 -19 81 27 11 | 13 31
mit uuuuu | -20 7 -16 -161 -10 | 28 41
ngs uuuxu | 43 29 -104 -15 -4 | 13 33
sio xxxxx | -16 6 -101 15 12 | 64 70
Table 7.2332.3 GPS week: 2332 Day: 3 MJD: 60571.500
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 | -25 -6 23 50 3 | 3 34
emr uuuuu | -1 -14 125 63 -23 | 6 32
esa uuuuu | 18 5 36 49 11 | 20 40
gfz uuuuu | -23 -46 0 -93 7 | 10 34
grg uuuuu | -19 9 -132 -38 5 | 8 32
irf xxxxx | -7 2 -42 19 -6 | 1 32
jgx uuuuu | 26 28 -73 -33 9 | 15 35
jpl uuuuu | 1 -20 29 66 -3 | 20 38
mit uuuuu | -9 26 -88 -133 -15 | 32 45
ngs uuuxu | 60 11 55 269 4 | 19 38
sio xxxxx | 71 32 -238 -7 6 | 70 78
Table 7.2332.4 GPS week: 2332 Day: 4 MJD: 60572.500
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 | 13 -11 17 85 7 | -5 40
emr uuuuu | -1 -13 48 204 -8 | -5 42
esa uuuuu | 3 26 82 -70 13 | 13 41
gfz uuuuu | -65 -18 -109 -327 -5 | 3 38
grg uuuuu | -53 13 -37 -181 1 | 0 37
irf xxxxx | -4 11 -23 51 -3 | -8 40
jgx uuuuu | 11 6 -48 1 5 | 8 37
jpl uuuuu | 30 -17 146 123 -5 | 14 42
mit uuuuu | 40 9 -128 22 -9 | 23 47
ngs uuuxu | 1 11 -12 268 -2 | 11 40
sio xxxxx | 152 37 -150 88 15 | 63 74
Table 7.2332.5 GPS week: 2332 Day: 5 MJD: 60573.500
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 6 -35 146 4 | 2 40
emr uuuuu | 16 29 -70 64 4 | 0 42
esa uuuuu | 11 8 91 -31 3 | 21 45
gfz uuuuu | -26 -26 7 5 -4 | 9 38
grg uuuuu | -71 -15 -12 -220 -4 | 6 38
irf xxxxx | -5 -2 -24 16 -6 | -2 39
jgx uuuuu | 14 -3 72 -14 2 | 14 40
jpl uuuuu | 16 7 -14 44 15 | 21 43
mit uuuuu | 37 16 -106 -72 -17 | 28 49
ngs uuuxu | -33 -61 135 -36 -4 | 16 42
sio xxxxx | 143 77 -93 -97 -5 | 72 82
Table 7.2332.6 GPS week: 2332 Day: 6 MJD: 60574.500
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 | 50 -5 17 35 -1 | 1 40
emr uuuuu | 15 -5 -30 65 3 | -2 42
esa uuuuu | -9 15 -24 -66 0 | 21 45
gfz uuuuu | -32 -16 -52 106 -7 | 9 38
grg uuuuu | -37 -1 116 -171 3 | 5 38
irf xxxxx | -7 11 -26 -13 -3 | -4 40
jgx uuuuu | 10 -5 24 36 5 | 14 40
jpl uuuuu | 20 9 -57 15 11 | 22 44
mit uuuuu | 7 -13 -40 -53 -11 | 25 48
ngs uuuxu | -62 30 89 -381 -5 | 15 42
sio xxxxx | -19 -4 -78 93 6 | 70 81
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