[IGSREPORT-30176] Wk 2338 IGS Final Orbits
acc
acc at igs.org
Fri Nov 15 04:52:35 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2338 (Oct 27, 2024 - Nov 02, 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_20243010000_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 | DJIG
0 | EMR | BADG BADG
0 | ESA | CPVG LAUT LAUT SCUB
0 | GFZ | 21 POHN POHN
0 | GRG | 17 SEYG KIRI NRMD SCUB SEYG
0 | JPL | IISC THU2 CHTI FTNA GUAM IISC NRMD SUTM THU2
0 | MIT | ABPO CRO1 DAEJ SFER TLSE TRO1 YAR3 ABPO CRO1 DAEJ
0 | MIT | SFER TLSE TRO1 YAR3
1 | COD | BAKE DARW DGAR IISC KIT3 MONP NRMD SCUB SCUB
1 | GFZ | 21 POHN DGAR POHN SCUB
1 | GRG | DAV1 FLIN KIRI NRMD DAV1 FLIN KIRI NRMD
1 | JPL | BADG BAKE BADG BAKE CHTI FTNA IISC MONP NRMD SGOC
1 | JPL | THU2
1 | MIT | ABPO GMSD MDVJ SFER STJ3 TLSE YEL2 ABPO GMSD MDVJ
1 | MIT | SFER STJ3 TLSE YEL2
2 | COD | BAKE DARW DGAR HOLB MATE NICO MATE
2 | EMR | BRAZ NYAL
2 | ESA | MADR NICO MADR NICO
2 | GFZ | 24 PTVL PTVL
2 | GRG | CZTG NRMD SYOG CZTG KIRI NRMD SYOG
2 | JPL | BADG IISC NRMD SYOG BADG BAKE CHTI DGAR FTNA HOLB
2 | JPL | IISC NRMD PGEN PTGG SYOG THU2
2 | MIT | AMC4 BRST MDVJ TRO1 YAR3 YEL2 AMC4 BRST MDVJ YAR3
2 | MIT | YEL2
3 | COD | CRO1 GUAM JOG2 KIT3 LPGS NRMD OUS2 POHN RIO2 SEYG
3 | COD | SGOC SUTM TASH UNSA URUM JOG2 NRMD RIO2 SEYG
3 | EMR | AREQ
3 | ESA | THU2 AREQ
3 | GFZ | 5 5 IRKJ POHN IRKJ MONP NYA2 OUS2 POHN RIO2 TASH
3 | GFZ | UNSA
3 | GRG | CZTG GMSD KIRI LPGS NRMD OUS2 SCUB CZTG GMSD KIRI
3 | GRG | LPGS NRMD OUS2 SCUB
3 | JPL | HOLB THU2 BADG CHTI GLPS HOLB SGOC SUTM THU2 URUM
3 | MIT | AMC4 GANP GOLD MADR NRC1 PDEL TLSE YAR3 AMC4 GANP
3 | MIT | GOLD MADR NRC1 PDEL TLSE YAR3
4 | COD | DAV1 FLRS GODE HKSL LAUT MATE POHN POVE SGOC TWTF
4 | COD | DAV1 GODE MATE TWTF
4 | EMR | AREQ AREQ
4 | ESA | UNSA UNSA
4 | GFZ | GODE POHN TASH GODE GOLD POHN TASH
4 | GRG | 16 AREQ CZTG HOLB KIRI NRMD SCUB AREQ CZTG HOLB KIRI
4 | GRG | NRMD
4 | JPL | BADG NRMD BADG GUAM HKSL IISC NRMD SGOC UNSA
4 | MIT | AMC4 FLIN NANO TLSE AMC4 FLIN NANO TLSE
5 | ALL | 26
5 | COD | BADG BOGT GUAM LPGS NICO NNOR SAVO SCUB ULAB GODE
5 | COD | ULAB
5 | ESA | GODE DYNG NICO SYOG
5 | GFZ | POHN GODE IRKJ POHN SCUB
5 | GRG | 21 CZTG GODE PTGG CZTG KIRI NRMD PTGG SYOG
5 | JPL | PGEN SGOC BADG CHTI CPVG FTNA GUAM NRMD PGEN SGOC
5 | MIT | DRAO STJ3 TRO1 YAR3 YEL2 DRAO HERS STJ3 TRO1 YAR3
5 | MIT | YEL2
6 | ALL | 26
6 | COD | ADIS DARW DYNG FAIR FLIN HOB2 MOBS NNOR NRMD SCUB
6 | COD | SEYG ADIS
6 | ESA | BOGT CCJ2 FAIR SYOG BOGT CCJ2 FAIR SYOG
6 | GFZ | LAUT LAUT
6 | GRG | 21 CZTG NRMD SYOG CZTG KIRI NRMD SYOG
6 | JGX | GUAM GUAM
6 | JPL | GUAM SGOC CHTI FAIR FTNA GUAM NRMD PGEN POHN PTGG
6 | JPL | SGOC THU2
6 | MIT | GUAM IRKJ MDVJ SFER GUAM HERS IRKJ MDVJ SFER
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | COD | ~02:00 | ~ -0.12 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
6 | GFZ | 26
6 | GRG | 26
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G26 | | | | | | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
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.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .2 -2.2 -.6 -5 2 -18 -.11
EMR | 0 | .8 -.5 -5.3 17 -13 16 -.13
ESA | 0 | .4 .9 .3 0 -16 -9 -.67
GFZ | 0 | .0 -.8 .2 -32 2 -20 .29
GRG | 0 | -.1 -.9 -2.1 25 16 1 -.16
JGX | 0 | -2.6 2.8 6.2 -17 13 -6 -.32
JPL | 0 | -1.4 1.1 -2.8 -1 10 -13 -.07
MIT | 0 | -.8 -1.3 27.2 11 13 -35 -.32
NGS | 0 | -2.7 3.7 1.3 13 37 -42 .06
COD | 1 | .1 -1.7 -.2 5 12 -24 -.09
EMR | 1 | 2.5 -.9 -7.9 33 -15 17 .18
ESA | 1 | .1 .4 .8 -13 3 -15 -.55
GFZ | 1 | .6 .1 -.1 -19 -7 11 .46
GRG | 1 | .4 -.8 -1.8 18 7 30 .07
JGX | 1 | .5 .6 2.9 2 7 16 .09
JPL | 1 | 4.2 5.4 -6.3 12 -3 -13 -.01
MIT | 1 | 2.6 -.6 26.0 14 4 -21 -.04
NGS | 1 | 3.1 -2.7 4.8 9 22 -29 -.07
COD | 2 | .6 -1.9 -.3 0 1 -20 .05
EMR | 2 | 7.7 3.8 -7.8 16 -23 3 .10
ESA | 2 | .5 .6 .4 1 -9 -4 -.55
GFZ | 2 | .6 -1.1 -.5 -20 -9 3 .10
GRG | 2 | .7 -.6 -1.6 16 18 13 -.17
JGX | 2 | 3.3 6.6 5.0 11 5 12 -.18
JPL | 2 | 2.4 6.9 -4.2 28 -9 5 -.25
MIT | 2 | 5.6 4.2 24.0 30 6 4 -.16
NGS | 2 | 8.7 5.4 5.9 24 -2 -18 -.12
COD | 3 | .8 -1.1 -.1 -6 9 -22 -.09
EMR | 3 | 2.8 5.0 -3.7 33 -28 31 -.02
ESA | 3 | .4 .1 .7 -15 -17 -3 -.69
GFZ | 3 | .8 -.7 -.3 -26 -10 -3 .18
GRG | 3 | 1.4 -.9 -1.3 12 2 28 -.01
JGX | 3 | .4 9.4 4.3 0 2 3 -.12
JPL | 3 | 2.9 6.4 -1.3 8 -13 5 -.30
MIT | 3 | 9.0 .7 26.3 44 -10 -19 -.05
NGS | 3 | 4.0 8.3 6.8 33 3 -10 -.11
COD | 4 | .9 -1.8 .1 -12 8 -29 .04
EMR | 4 | 3.4 4.6 -2.2 33 -30 31 -.18
ESA | 4 | .2 -1.7 -.3 18 -22 -5 -.47
GFZ | 4 | .1 -1.7 -.2 -15 -7 2 .21
GRG | 4 | .5 -.4 -1.4 20 0 10 -.09
JGX | 4 | 3.7 6.3 11.8 -21 6 25 -.29
JPL | 4 | 1.5 5.9 .3 3 -8 1 -.06
MIT | 4 | 4.0 2.8 23.2 48 -7 -3 -.09
NGS | 4 | 8.9 4.2 12.4 22 5 -21 -.28
COD | 5 | .6 -1.9 .3 -15 27 -33 -.04
EMR | 5 | 3.5 5.1 -4.4 35 -15 15 -.14
ESA | 5 | -.2 -1.0 .7 -9 -2 -21 -.64
GFZ | 5 | .2 -1.1 .2 -34 5 -5 .04
GRG | 5 | .1 -.4 -.3 -9 0 26 -.07
JGX | 5 | 1.2 6.7 8.5 -1 -6 11 -.45
JPL | 5 | 1.4 2.0 -9.9 -13 27 -24 -.08
MIT | 5 | 4.6 2.2 24.5 41 7 -6 -.12
NGS | 5 | 4.3 5.2 12.0 25 22 -18 -.40
COD | 6 | .5 -1.5 -.2 -26 21 -24 -.14
EMR | 6 | 7.8 6.5 -4.7 27 -22 21 -.13
ESA | 6 | .1 -.1 .3 5 -8 -1 -.61
GFZ | 6 | .5 -.7 -.0 -25 10 -6 .36
GRG | 6 | -.1 .0 -.5 0 13 19 -.27
JGX | 6 | 1.2 7.0 10.8 -7 -10 19 -.31
JPL | 6 | 2.8 8.5 -3.4 16 13 -15 -.05
MIT | 6 | 4.2 3.7 26.7 17 -15 9 -.13
NGS | 6 | 3.8 12.6 33.4 25 39 -19 -.26
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
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 1.2338.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2338.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 2.2338.[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 3.2338.[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 5.2338.0-6). 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 2338 summary. (Oct 27, 2024 - Nov 02, 2024)
Table 1.2338.a GPS week: 2338 MJD: 60610.000-60616.000
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 780| 0 0 1 0 16 18 .00 9 8 | -717 97 6 99
| 0 0 0 19 12 11 .02 | 86 157
emr 108| 0 0 -3 5 -7 -16 .05 9 9 | -1679 363 31 95
| 0 0 1 5 12 7 .01 | 458 1049
esa 150| 0 -1 5 -31 4 -2 .00 9 9 | -700 -212 6 83
| 0 0 0 15 9 10 .02 | 485 763
gfz 128| 0 0 4 -2 14 -25 .10 11 10 | -33 -74 10 125
| 0 0 2 17 10 11 .03 | 93 134
grg 126| 0 0 -2 5 0 5 -.06 10 8 | -37 36 7 120
| 0 0 1 12 6 15 .02 | 58 131
igr n/a| 0 0 0 -16 0 3 .00 4 3 | -4088 -369 10 79
| 0 0 1 6 8 7 .01 | 1070 331
jgx n/a| 0 0 5 6 -19 -19 -.06 10 10 | -12 -51 36 107
| 0 0 0 12 4 11 .01 | 71 183
jpl 120| -2 0 0 -1 -4 1 .04 9 9 | -2512 59 7 69
| 1 1 0 17 10 10 .03 | 387 296
mit 356| 1 0 -10 9 -3 31 -.00 10 9 | -4215 -114 62 90
| 0 0 0 42 23 38 .01 | 1019 167
ngs 269| 0 0 -2 7 -11 -1 -.08 11 11 | -717 96 491 692
| 0 0 6 18 21 22 .01 | 85 155
Table 1.2338.b GPS week : 2338 MJD: 60610.000-60616.000
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
------+------------------------------------+------------------------------------------
2 | 3 3 3 3 3 3 3 |
3 | 3 3 3 4 3 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 3 4 3 3 3 3 4 |
6 | 3 3 3 3 3 3 4 |
7 | 3 3 3 3 3 3 3 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 4 |
10 | 3 3 4 3 4 3 3 |
11 | 4 4 4 4 4 4 5 |
12 | 4 4 4 4 4 4 4 |
13 | 3 3 3 3 3 3 3 |
14 | 4 4 5 5 5 5 5 |
15 | 3 3 3 3 3 3 3 |
16 | 4 4 4 4 5 4 4 |
17 | 3 3 3 3 3 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 3 3 3 3 3 4 4 |
20 | 3 5 3 4 4 3 3 |
21 | 3 3 4 4 4 4 4 |
22 | 3 3 3 4 3 3 3 |
23 | 3 4 4 4 4 4 4 |
24 | 3 3 3 3 3 3 3 |
25 | 4 4 4 4 4 5 5 |
26 | 4 4 6 5 5 6 14 |
27 | 3 3 3 3 3 3 3 |
28 | 3 3 3 3 3 3 3 |
29 | 3 3 3 3 3 3 4 |
30 | 3 3 3 3 3 4 3 |
31 | 3 4 3 3 3 3 3 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2338.0 GPS week: 2338 Day: 0 MJD: 60610.000
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 780| 0 0 1 19 34 18 .02 7 7 | -740 164 7 101
emr 107| 0 0 0 12 -22 -24 .04 9 9 | -2513 2605 32 83
esa 150| 0 -2 5 -40 -12 7 .02 9 9 | -1154 383 6 84
gfz 129| 1 1 2 -26 28 -18 .09 8 9 | -45 -100 10 120
grg 123| 0 0 -2 4 -4 32 -.05 9 9 | -122 217 7 121
igr n/a| 0 0 0 -13 -1 11 .01 3 3 | -2259 -380 9 92
jgx n/a| 0 0 6 -6 -11 -27 -.04 9 9 | -131 235 30 105
jpl 120| -2 1 0 -17 -4 2 -.00 9 9 | -2058 138 6 59
mit 356| 0 0 -9 0 -22 -18 .00 9 9 | -2389 -120 62 91
ngs 271| 0 0 -6 36 -11 12 -.06 10 10 | -735 154 442 672
Table 2.2338.1 GPS week: 2338 Day: 1 MJD: 60611.000
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 781| 0 0 1 13 8 4 .03 7 7 | -787 196 6 96
emr 106| 0 0 -4 -1 6 -26 .02 9 9 | -1323 -624 30 77
esa 150| 0 -1 5 -39 8 -19 .00 8 8 | -648 50 6 66
gfz 128| 0 0 6 13 18 -35 .07 9 9 | -91 105 9 125
grg 125| 0 0 -2 11 5 22 -.05 10 8 | -50 141 8 129
igr n/a| 0 0 2 -14 -9 0 -.01 4 4 | -2952 -1010 10 70
jgx n/a| 0 0 5 13 -20 -11 -.06 9 9 | -44 112 31 99
jpl 120| -2 1 0 -1 -4 -18 .02 9 9 | -2150 -489 6 65
mit 356| 1 0 -10 -17 -20 103 -.01 9 9 | -3228 -455 58 87
ngs 270| 0 0 -2 5 1 -45 -.07 10 9 | -783 192 463 692
Table 2.2338.2 GPS week: 2338 Day: 2 MJD: 60612.000
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| 0 0 2 4 12 37 .00 7 7 | -786 137 6 101
emr 107| -1 -2 -3 9 -24 -7 .06 9 9 | -1515 -96 31 89
esa 150| 0 0 6 -28 5 -8 .01 9 9 | 322 -1891 5 76
gfz 129| 0 1 1 -11 7 -38 .14 12 11 | 55 -156 12 126
grg 128| 0 1 -1 13 5 0 -.07 8 8 | -80 71 7 107
igr n/a| 0 0 1 -20 -12 -8 .03 3 3 | -4205 -363 10 77
jgx n/a| 0 0 6 4 -23 -35 -.07 10 10 | -56 -18 37 106
jpl 120| -3 -1 0 10 -14 7 .03 9 9 | -2831 -18 8 76
mit 356| 1 0 -9 8 20 23 -.00 9 8 | -4337 -98 62 80
ngs 274| 0 0 -4 -17 0 -9 -.09 10 10 | -786 136 523 724
Table 2.2338.3 GPS week: 2338 Day: 3 MJD: 60613.000
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 779| 0 0 1 14 19 12 -.03 9 8 | -782 317 7 100
emr 109| 0 0 -2 -3 -3 -22 .07 9 9 | -1455 -171 31 105
esa 150| 1 -1 6 -42 1 5 .02 9 9 | -959 133 6 125
gfz 128| 0 0 4 5 11 -29 .07 10 9 | 8 -3 10 127
grg 128| 0 0 -3 -2 4 0 -.06 9 8 | 44 -116 6 118
igr n/a| 0 0 0 -26 8 0 -.00 3 3 | -4430 -466 12 87
jgx n/a| 0 0 5 -10 -14 -2 -.04 10 10 | 79 -195 40 103
jpl 120| -2 0 0 -22 3 16 .04 9 9 | -2818 -75 8 71
mit 356| 1 0 -10 55 -23 9 .02 10 9 | -4669 13 67 101
ngs 275| 0 1 -4 1 1 17 -.08 11 11 | -782 315 517 706
Table 2.2338.4 GPS week: 2338 Day: 4 MJD: 60614.000
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 780| 1 0 1 -16 33 28 -.00 9 8 | -561 -145 6 96
emr 110| -1 0 -2 4 -6 -15 .05 9 9 | -2053 339 33 105
esa 150| 0 -1 5 -5 1 -11 -.02 9 8 | -986 152 6 76
gfz 128| 0 0 6 4 0 -29 .10 10 9 | 92 -302 10 126
grg 128| 1 1 -1 23 -8 -3 -.09 9 8 | -7 -69 7 121
igr n/a| 0 0 0 -18 7 0 -.01 3 3 | -4943 39 11 86
jgx n/a| -1 0 5 12 -19 -20 -.05 10 10 | -10 -37 42 114
jpl 120| -2 0 0 0 -19 0 .08 9 9 | -2988 366 8 72
mit 356| 1 0 -10 -33 24 56 .00 9 9 | -4850 -145 61 89
ngs 271| 0 0 -5 25 1 -11 -.06 12 11 | -560 -148 498 672
Table 2.2338.5 GPS week: 2338 Day: 5 MJD: 60615.000
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 780| 0 0 1 0 4 12 .01 9 8 | -727 72 6 95
emr 114| -2 0 -2 8 -1 -6 .06 10 10 | -1687 453 30 110
esa 150| 0 -1 5 -48 20 0 -.02 9 9 | -807 -196 7 74
gfz 128| 1 0 5 -22 27 -6 .09 11 11 | -183 32 10 126
grg 126| 0 1 0 -15 -9 -8 -.02 9 8 | -65 111 7 123
igr n/a| 0 0 0 -12 8 13 -.00 3 3 | -4860 -111 10 75
jgx n/a| 0 0 6 5 -22 -25 -.08 10 10 | 45 -295 34 111
jpl 120| 0 0 0 -9 10 2 .06 9 9 | -2596 375 8 73
mit 356| 1 0 -9 78 -20 22 -.01 10 9 | -4947 62 60 90
ngs 266| 0 0 -5 -1 -14 17 -.09 11 11 | -732 86 468 657
Table 2.2338.6 GPS week: 2338 Day: 6 MJD: 60616.000
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 783| 0 0 1 -35 4 15 -.00 11 8 | -639 -60 6 106
emr 109| 0 0 -4 4 3 -15 .05 11 11 | -1210 35 35 99
esa 150| 0 0 5 -16 9 4 .01 10 9 | -668 -121 6 82
gfz 127| 0 0 1 18 10 -18 .13 17 10 | -73 -98 11 131
grg 128| 2 0 -4 3 4 -4 -.05 19 9 | 16 -100 7 121
igr n/a| 0 0 -2 -7 2 6 .01 6 3 | -4972 -296 11 71
jgx n/a| -1 -1 4 23 -22 -10 -.06 11 11 | 29 -160 41 113
jpl 120| 0 3 -1 28 -3 2 .05 11 11 | -2148 116 8 68
mit 356| 1 0 -12 -28 20 22 -.01 11 9 | -5089 -61 70 94
ngs 260| -1 1 12 0 -57 6 -.09 15 15 | -641 -58 531 726
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 3.2338.0 GPS week: 2338 Day: 0 MJD: 60610.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 7 7 7 7 9 3 9 7 11 12 3 | 20 21 23 23 22 21 23 19 25 23 21
3 | 7 10 12 11 7 2 7 9 11 8 3 | 28 27 33 29 26 27 27 28 27 24 26
4 | 4 18 6 9 8 2 9 19 11 8 4 | 12 20 14 18 17 14 14 21 19 16 13
5 | 7 7 5 7 10 2 11 10 6 10 3 | 21 17 18 24 18 20 21 17 22 22 19
6 | 6 8 8 11 9 3 7 9 7 9 3 | 24 24 26 21 19 23 21 24 21 24 22
7 | 5 9 10 7 7 2 8 7 8 7 2 | 41 40 42 44 37 39 40 40 38 38 39
8 | 5 7 8 6 6 3 7 7 7 7 2 | 24 25 26 25 23 24 22 24 22 23 23
9 | 6 9 8 6 8 3 9 9 11 10 3 | 17 26 20 23 18 21 19 26 23 19 20
10 | 6 7 9 6 8 2 6 7 11 9 2 | 21 20 25 19 20 21 21 20 20 21 20
X11 | 9 14 10 9 12 4 --- 9 8 9 3 | 52 53 56 57 53 54 --- 53 52 51 53
12E | 8 8 12 11 12 4 13 9 7 12 3 | 40 39 42 41 43 40 40 40 39 40 39
13 | 5 8 7 9 5 2 7 7 11 9 2 | 14 19 17 15 12 14 13 19 17 17 15
14E | 11 10 17 8 14 3 8 15 12 12 4 | 42 46 47 45 48 44 45 46 44 42 44
15 | 5 9 7 5 8 2 7 8 7 9 2 | 30 27 29 30 26 28 28 29 30 29 28
16E | 9 11 8 9 16 4 12 12 7 15 4 | 36 35 35 39 31 34 34 32 32 34 34
17 | 8 11 7 8 8 3 8 7 7 8 3 | 24 26 21 23 20 22 22 23 23 23 22
18 | 8 13 11 7 9 4 7 13 14 13 3 | 53 53 55 53 52 54 54 56 51 53 53
19 | 6 10 5 10 8 3 10 8 7 9 3 | 22 23 21 21 18 20 18 20 21 21 20
20 | 8 8 7 9 10 3 9 9 6 11 3 | 66 66 65 64 71 63 63 64 66 59 65
21 | 11 6 6 9 8 3 11 6 10 10 3 | 18 17 19 22 17 17 19 17 22 20 17
22E | 8 7 6 10 10 3 6 6 8 9 2 | 30 29 25 28 30 28 27 28 31 29 28
23 | 7 10 11 6 10 2 12 10 9 8 3 | 36 37 41 38 41 38 36 41 42 38 38
24 | 5 8 8 8 5 2 6 6 8 7 2 | 27 26 27 24 23 24 24 26 23 23 24
25E | 6 13 12 10 10 4 13 11 5 8 3 | 21 26 26 20 24 21 22 25 22 21 21
26E | 8 9 9 11 8 3 12 10 10 11 3 | 108 107 108 108 100 106 106 80 108 106 107
27 | 6 8 8 7 6 2 6 7 7 5 2 | 23 23 26 26 22 23 21 22 20 21 22
28 | 7 7 8 6 7 3 7 9 9 9 2 | 31 32 33 35 35 33 32 34 29 34 32
29 | 6 7 6 8 7 3 12 9 7 10 3 | 32 31 32 34 30 31 31 31 35 31 31
30 | 6 8 9 6 8 2 9 5 7 11 2 | 27 26 27 24 22 24 24 26 23 22 24
31 | 6 9 7 10 7 3 9 8 9 12 3 | 93 94 94 89 92 93 92 94 98 92 93
32 | 6 9 7 7 6 2 8 10 11 11 3 | 18 27 23 21 18 21 18 27 18 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 9 8 9 3 9 9 9 10 |T 33 34 35 34 33 33 32 33 34 33 33
WRMS | 7 9 9 9 9 3 9 9 9 10 |NE 33 34 35 34 32 33 31 34 33 33 33
MEDI | 6 9 8 8 8 3 8 9 8 9 |MD 27 27 27 26 24 24 24 27 25 24 24
Table 3.2338.1 GPS week: 2338 Day: 1 MJD: 60611.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 9 5 5 8 7 5 10 7 10 9 2 | 17 18 19 21 18 19 21 17 23 19 18
3 | 4 7 11 11 6 3 6 8 8 9 2 | 20 22 24 21 20 19 18 19 19 21 19
4 | 5 17 6 9 8 4 11 17 10 7 3 | 8 16 9 13 11 8 10 16 16 11 7
5 | 9 7 5 15 10 4 8 11 5 11 3 | 20 17 17 23 18 18 18 16 18 21 17
6 | 7 9 7 8 6 3 7 8 7 7 2 | 21 23 23 18 19 18 18 22 18 20 19
7 | 5 8 8 6 7 3 9 6 5 9 2 | 27 27 26 29 24 26 25 27 26 26 25
8 | 6 6 8 6 6 3 6 6 7 12 2 | 22 23 25 24 22 23 23 22 20 27 22
9 | 4 11 6 7 8 4 7 10 5 11 2 | 15 25 16 16 12 14 14 24 19 16 16
10 | 12 9 9 10 7 4 7 6 7 9 3 | 20 20 23 20 18 19 17 18 18 21 18
X11 | 10 16 8 8 10 3 --- 9 7 12 4 | 33 37 36 37 36 34 --- 36 31 36 34
12E | 8 9 11 8 11 7 14 8 7 9 3 | 29 30 34 31 31 33 32 29 35 34 31
13 | 7 8 7 9 5 4 7 7 12 12 3 | 12 18 14 12 10 12 11 17 17 16 13
14E | 9 10 18 8 13 3 9 11 12 14 4 | 28 34 34 34 33 30 30 32 34 26 30
15 | 6 8 6 6 7 3 8 5 7 9 2 | 19 20 18 22 17 20 19 20 20 21 19
16E | 8 9 6 13 12 4 13 9 8 13 3 | 35 38 38 43 37 37 38 35 34 39 36
17 | 7 11 5 6 8 3 6 6 8 6 2 | 19 23 17 20 16 18 17 21 20 20 18
18 | 9 13 10 8 9 4 9 13 14 16 4 | 32 35 32 35 33 32 32 36 31 34 32
19 | 7 10 4 10 7 3 9 6 6 11 2 | 18 19 17 18 15 15 14 17 17 20 16
20 | 9 8 6 16 30 4 7 11 6 9 4 | 60 60 59 59 73 59 58 58 58 56 59
21 | 10 7 5 9 6 5 13 6 9 7 3 | 16 18 16 20 16 16 18 16 20 16 16
22E | 7 9 5 6 7 4 7 5 8 8 2 | 21 23 19 22 23 21 19 20 24 24 21
23 | 9 10 12 12 9 3 11 10 7 12 3 | 23 26 26 25 27 24 25 26 28 23 24
24 | 7 8 9 11 5 3 6 5 9 7 2 | 24 22 23 19 18 19 18 22 18 20 19
25E | 7 11 12 10 8 4 13 12 8 9 3 | 24 27 29 23 25 25 24 30 27 26 25
26E | 10 8 9 8 10 4 15 10 11 12 3 | 92 91 92 92 85 91 89 67 94 91 91
27 | 6 5 7 6 8 3 6 6 7 7 2 | 21 23 24 26 21 21 20 21 19 22 21
28 | 7 7 7 8 9 2 8 8 9 9 2 | 28 30 30 33 34 30 30 30 29 31 30
29 | 5 6 5 9 8 5 13 9 9 10 3 | 24 22 22 24 21 22 23 21 23 25 22
30 | 7 7 9 7 7 4 7 6 7 6 2 | 25 25 25 26 20 22 23 26 18 23 23
31 | 7 8 7 8 13 5 11 8 16 8 3 | 91 92 92 88 88 91 91 92 94 93 91
32 | 7 11 7 9 7 3 8 10 10 10 3 | 16 26 20 17 14 17 13 26 15 17 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 8 9 10 4 9 9 9 10 |T 27 30 29 29 27 27 26 28 28 28 27
WRMS | 7 9 8 9 8 4 9 9 9 9 |NE 27 29 29 28 27 26 26 28 27 28 26
MEDI | 7 8 7 8 8 4 8 8 8 9 |MD 22 23 24 23 21 21 20 22 20 23 21
Table 3.2338.2 GPS week: 2338 Day: 2 MJD: 60612.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 5 7 7 14 8 2 9 6 9 16 3 | 37 37 38 39 35 37 35 35 37 38 36
3 | 7 9 12 11 6 3 8 8 9 10 3 | 36 37 38 35 34 36 35 36 35 38 35
4 | 5 18 6 6 10 2 9 18 10 9 4 | 31 35 32 33 33 31 32 33 34 33 31
5 | 7 9 5 6 10 2 10 10 6 11 3 | 31 30 26 30 30 27 26 27 29 33 28
6 | 6 11 7 15 6 4 8 7 8 8 3 | 35 36 36 33 33 33 31 35 32 33 33
7 | 5 9 8 9 8 3 9 6 7 9 2 | 39 41 40 42 37 39 38 40 38 37 38
8 | 5 8 8 7 6 3 7 6 7 8 2 | 34 35 34 34 32 32 32 35 30 31 33
9 | 6 9 7 5 8 2 7 9 6 9 2 | 32 39 33 33 32 33 31 37 34 35 33
10 | 14 11 10 13 6 3 8 6 6 12 3 | 37 35 36 32 34 33 34 34 31 36 34
X11 | 10 15 10 8 9 4 --- 10 8 11 4 | 35 36 39 36 37 36 --- 38 35 37 36
12E | 9 10 13 10 9 4 15 9 10 10 3 | 44 46 45 44 44 44 44 44 43 44 44
13 | 7 7 6 6 5 3 7 6 10 8 2 | 31 35 30 32 30 29 25 32 28 30 30
14E | 10 12 19 8 12 3 8 13 12 16 4 | 43 47 47 44 43 43 43 45 41 44 43
15 | 5 7 6 6 6 3 10 5 8 7 2 | 33 34 32 32 32 31 31 33 31 32 32
16E | 11 9 9 13 9 5 12 9 7 14 3 | 38 41 41 37 38 40 39 39 36 38 38
17 | 6 11 7 7 8 3 7 5 7 6 2 | 38 39 36 38 35 36 35 38 34 37 36
18 | 8 11 12 8 8 3 8 14 10 10 3 | 35 36 38 34 37 34 34 40 32 34 35
19 | 4 10 4 8 7 2 10 6 9 12 2 | 34 35 33 35 32 32 30 34 31 36 33
20 | 8 9 6 7 14 4 10 9 5 11 3 | 60 61 60 59 54 59 59 60 58 60 58
21 | 8 6 6 10 8 3 14 7 9 18 3 | 36 36 35 34 32 34 32 34 35 40 34
22E | 7 10 7 10 7 4 7 4 7 11 2 | 40 41 39 42 41 39 37 39 38 44 40
23 | 8 10 13 10 8 2 11 11 8 10 3 | 39 41 42 38 42 39 39 43 41 39 40
24 | 6 6 9 14 5 2 6 7 8 5 2 | 37 37 34 35 31 34 33 35 30 33 33
25E | 11 12 13 10 12 5 12 12 5 9 4 | 36 38 40 37 39 37 36 39 36 38 37
26E | 10 9 9 42 8 5 16 11 15 12 6 | 58 58 56 59 53 56 59 49 55 56 56
27 | 8 7 7 7 4 1 7 6 8 7 2 | 31 36 34 34 30 31 31 33 28 28 31
28 | 6 7 7 6 7 3 9 7 8 9 2 | 24 24 26 25 28 26 23 27 26 28 25
29 | 7 8 5 7 7 3 14 9 9 10 3 | 33 31 30 32 30 31 33 31 31 29 31
30 | 6 8 8 6 7 2 6 7 7 6 2 | 31 33 33 32 31 31 29 33 29 32 31
31 | 6 8 7 9 8 3 11 8 8 11 3 | 73 75 74 72 72 74 74 74 72 73 73
32 | 7 9 8 8 5 3 7 10 10 9 3 | 39 44 40 39 39 40 39 44 37 39 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 9 12 8 3 10 9 9 10 |T 38 39 38 38 37 37 36 38 36 38 37
WRMS | 7 9 9 11 8 3 10 9 8 10 |NE 37 38 38 36 36 36 36 38 35 37 36
MEDI | 7 9 7 8 8 3 9 8 8 10 |MD 36 37 36 35 34 34 34 36 34 37 35
Table 3.2338.3 GPS week: 2338 Day: 3 MJD: 60613.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 9 7 6 8 10 4 8 8 12 13 3 | 19 22 22 24 18 21 19 17 22 24 19
3 | 8 8 11 9 8 2 8 8 12 12 3 | 26 26 31 27 26 26 25 26 26 29 25
4 | 7 17 6 7 10 3 9 17 15 12 4 | 16 23 16 20 19 16 15 21 23 20 16
5 | 9 9 6 11 9 3 8 11 8 11 3 | 30 28 27 29 30 27 27 27 29 31 28
6 | 7 9 7 8 8 3 9 6 9 8 2 | 26 25 28 25 24 24 23 26 24 26 24
7 | 7 8 9 9 8 3 12 6 10 11 3 | 35 34 33 37 32 31 32 33 33 30 32
8 | 7 8 8 6 7 2 9 6 7 10 2 | 25 25 25 25 23 24 23 25 22 28 23
9 | 5 9 6 7 7 4 8 8 11 10 3 | 22 29 23 24 22 22 18 29 26 23 23
10 | 13 9 9 6 5 2 9 8 7 11 3 | 28 26 28 25 24 25 23 26 23 28 24
X11 | 9 14 9 7 9 3 --- 9 9 9 3 | 30 33 35 34 34 32 --- 34 29 30 32
12E | 10 9 11 7 10 5 14 9 8 12 3 | 33 31 33 30 31 32 33 31 31 32 30
13 | 6 6 6 11 8 3 7 7 11 8 2 | 17 21 19 18 19 17 16 21 19 20 18
14E | 15 9 20 7 15 3 10 14 15 16 5 | 28 28 35 28 30 26 25 30 27 23 26
15 | 6 7 7 6 7 3 12 5 7 12 2 | 33 32 32 34 30 31 33 31 30 29 31
16E | 11 9 9 8 11 5 15 9 10 13 3 | 20 20 24 19 21 21 23 20 21 26 20
17 | 8 11 8 9 9 2 9 6 8 9 3 | 29 30 26 30 25 26 26 29 27 28 27
18 | 8 13 11 10 8 4 10 12 11 11 3 | 32 34 36 37 33 33 31 38 30 33 33
19 | 8 10 5 11 7 2 11 6 9 7 3 | 24 25 23 28 21 22 21 24 24 24 22
20 | 11 9 7 12 14 3 8 9 10 10 3 | 47 47 43 44 48 44 43 44 40 42 43
21 | 13 6 6 12 10 5 13 8 11 12 3 | 21 23 23 27 19 23 21 20 22 26 21
22E | 17 7 7 11 9 3 7 5 10 8 3 | 32 25 24 29 26 24 20 26 28 26 25
23 | 9 10 14 9 9 2 12 11 7 13 3 | 23 25 29 23 26 26 23 29 28 29 25
24 | 6 7 9 8 6 2 7 6 7 11 2 | 24 26 25 24 22 22 20 24 21 20 22
25E | 8 10 14 12 12 4 12 13 7 13 4 | 45 48 49 42 46 46 44 50 45 44 45
26E | 13 8 9 30 11 4 14 8 13 14 5 | 110 109 110 109 103 109 108 85 112 110 109
27 | 9 6 8 7 6 2 8 5 9 6 2 | 23 23 23 21 20 22 21 24 22 23 21
28 | 6 7 7 7 8 2 8 8 8 8 2 | 20 25 24 23 27 24 20 25 24 25 23
29 | 5 8 6 10 6 4 14 10 9 13 3 | 33 31 32 31 32 32 35 31 35 38 32
30 | 8 6 9 7 10 2 8 6 7 10 3 | 25 24 23 22 23 21 20 23 20 21 21
31 | 5 8 7 10 9 3 11 8 8 8 3 | 49 50 50 50 47 49 49 50 52 48 49
32 | 8 9 7 9 5 2 9 9 11 12 3 | 18 26 21 19 18 20 19 26 18 20 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 9 9 10 9 3 10 9 10 11 |T 30 31 31 30 29 29 28 30 30 30 29
WRMS | 8 9 9 9 8 3 10 9 9 11 |NE 26 28 28 27 26 26 25 28 26 28 26
MEDI | 8 9 8 9 9 3 9 8 9 11 |MD 26 26 27 27 26 25 23 26 26 28 25
Table 3.2338.4 GPS week: 2338 Day: 4 MJD: 60614.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 9 6 7 7 9 2 6 7 11 11 3 | 29 29 32 31 29 30 32 30 34 33 30
3 | 7 10 11 7 6 3 7 8 9 8 3 | 32 30 36 33 30 32 31 33 31 31 31
4 | 6 19 6 6 11 2 8 19 11 8 4 | 22 26 24 26 25 24 25 27 26 26 22
5 | 7 8 5 8 11 3 10 10 6 10 3 | 28 25 26 27 29 26 27 24 26 30 26
6 | 8 10 7 7 7 3 8 6 8 8 2 | 28 29 29 26 26 27 26 29 27 25 26
7 | 6 8 9 8 9 2 9 8 7 8 2 | 36 35 35 38 32 35 36 34 33 35 34
8 | 7 6 7 8 6 2 9 6 8 11 2 | 28 31 30 30 28 29 30 31 27 29 28
9 | 6 10 8 6 7 3 9 8 9 9 3 | 26 32 29 28 26 29 29 33 30 31 28
10 | 13 8 9 12 6 2 8 8 10 10 3 | 31 30 32 33 29 30 30 31 29 31 29
X11 | 9 16 8 6 10 3 --- 9 7 11 3 | 29 32 34 32 34 31 --- 34 31 25 31
12E | 11 10 10 11 11 4 13 9 8 13 3 | 40 41 42 44 38 41 41 39 41 42 40
13 | 5 8 6 9 7 2 7 6 12 12 3 | 21 27 22 24 21 22 20 26 20 20 21
14E | 11 10 19 9 13 4 10 14 11 18 4 | 39 42 44 41 38 40 39 41 37 38 38
15 | 6 7 7 6 7 2 10 6 7 11 2 | 34 36 33 36 33 33 34 34 32 33 33
16E | 11 8 9 11 23 3 12 8 9 16 4 | 30 32 33 34 33 31 33 31 32 37 31
17 | 8 9 6 9 10 3 9 6 10 8 3 | 30 30 28 33 26 29 29 30 28 29 28
18 | 10 13 10 7 8 3 10 13 11 16 4 | 29 33 36 33 32 32 29 38 31 35 32
19 | 6 10 4 9 8 2 11 6 11 8 3 | 25 25 25 26 22 24 23 25 24 24 23
20E | 8 9 7 7 11 4 11 8 8 17 3 | 79 81 80 79 81 79 82 80 81 77 80
21 | 15 6 5 9 9 2 14 9 9 13 3 | 28 28 27 30 22 27 28 28 31 32 27
22E | 8 8 6 9 7 3 7 6 8 15 3 | 46 45 42 44 41 43 41 42 42 51 43
23 | 8 9 14 11 9 2 10 12 8 14 3 | 31 35 37 35 35 34 35 38 37 32 34
24 | 7 9 9 6 8 1 7 5 7 14 3 | 23 31 28 27 26 27 25 29 23 28 25
25E | 9 8 13 8 8 4 10 12 6 11 3 | 31 32 35 33 32 30 30 34 31 27 31
26E | 15 8 9 25 9 4 13 9 13 12 4 | 140 141 140 139 132 139 142 92 139 143 140
27 | 8 7 7 8 6 2 8 5 9 13 3 | 25 30 30 27 28 28 30 30 26 29 27
28 | 7 7 7 7 9 2 8 8 9 13 3 | 22 25 25 24 26 24 24 27 28 25 24
29 | 8 6 5 8 8 3 12 8 9 14 3 | 31 29 31 30 30 31 33 30 30 32 29
30 | 8 9 8 9 10 2 8 6 7 7 3 | 24 27 26 24 23 24 24 26 23 25 23
31 | 6 10 7 11 8 3 11 7 8 12 3 | 72 74 73 74 71 71 72 74 72 76 72
32 | 7 9 7 10 5 2 6 9 11 9 3 | 33 38 35 35 32 35 33 41 32 38 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 9 9 10 9 3 10 9 9 12 |T 36 38 38 37 35 36 37 36 36 37 36
WRMS | 8 9 8 9 8 3 10 9 9 11 |NE 31 33 34 33 31 32 32 34 32 33 31
MEDI | 8 9 7 8 8 3 9 8 9 11 |MD 30 31 32 33 30 30 30 31 31 31 30
Table 3.2338.5 GPS week: 2338 Day: 5 MJD: 60615.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 9 7 7 8 9 3 8 7 10 10 3 | 19 21 23 27 19 21 21 18 25 22 20
3 | 7 10 12 8 7 3 8 9 13 9 3 | 24 24 29 25 23 23 20 24 26 25 23
4M | 6 18 6 8 10 3 10 19 12 8 4 | 12 21 16 17 16 12 13 21 18 17 13
5M | 9 10 5 13 9 2 10 12 8 7 3 | 45 44 45 45 45 44 46 43 45 44 44
6 | 7 9 8 12 7 3 6 7 9 8 3 | 27 27 27 26 25 25 23 27 24 24 24
7M | 5 8 9 9 8 3 10 7 6 14 3 | 27 28 26 31 26 27 28 29 26 30 27
8 | 6 8 6 9 5 2 7 6 6 9 2 | 20 23 24 24 20 22 21 22 21 24 21
9M | 6 11 8 9 7 4 8 9 7 8 3 | 21 28 24 27 21 22 20 29 22 23 23
10 | 11 9 8 9 6 3 8 7 9 12 3 | 25 24 28 26 22 25 23 25 22 28 23
X11 | 10 14 8 9 9 3 --- 10 9 9 3 | 36 40 38 39 40 38 --- 38 36 39 37
12E | 8 10 10 10 17 5 15 8 11 14 4 | 37 38 42 40 42 38 41 40 43 44 40
13M | 5 7 8 8 5 2 6 7 12 7 2 | 17 20 16 16 15 16 13 20 17 15 15
14E | 13 11 20 14 12 3 10 10 13 15 4 | 24 27 34 33 29 26 26 27 26 23 26
15M | 5 8 8 7 5 2 9 6 15 10 3 | 44 45 45 45 43 45 44 44 47 46 44
16E | 12 9 10 12 8 2 15 8 8 13 3 | 24 27 30 28 22 26 28 24 26 29 25
17M | 12 10 11 12 8 4 10 8 10 7 3 | 32 32 30 35 30 30 29 31 29 32 30
18 | 8 13 10 7 6 3 7 13 11 13 3 | 37 39 37 39 38 37 39 41 37 35 37
19M | 10 9 8 11 9 2 12 6 10 10 3 | 26 26 26 28 24 25 23 25 23 28 24
20E | 7 9 8 10 11 3 9 9 9 9 3 | 49 52 49 50 54 50 49 51 52 49 50
21 | 12 7 5 10 19 4 14 8 9 11 4 | 21 23 22 29 19 23 21 20 23 25 20
22E | 9 8 7 16 7 2 6 6 9 10 3 | 31 30 31 38 30 31 30 30 35 33 31
23 | 10 9 13 12 8 3 13 12 7 12 3 | 23 27 28 26 28 26 25 29 27 28 25
24 | 7 6 10 7 7 3 6 7 7 14 3 | 23 28 25 24 23 23 21 27 21 23 23
25E | 10 9 15 26 7 5 11 10 15 14 5 | 29 30 31 33 29 29 28 30 35 36 29
X26E | 16 13 9 20 14 3 11 --- 14 15 5 | 194 201 198 199 193 197 197 --- 194 196 196
27 | 7 7 7 6 6 3 7 6 7 11 2 | 20 21 23 21 20 20 20 22 20 23 20
28 | 9 9 8 8 8 2 10 8 8 11 3 | 33 36 36 36 36 35 35 38 34 39 35
29 | 6 8 6 9 7 4 15 8 7 15 3 | 33 31 32 29 31 31 30 30 31 32 30
30M | 9 10 9 8 10 3 6 9 16 11 3 | 26 27 26 24 23 24 21 29 29 25 24
31 | 8 10 8 11 8 3 12 8 8 8 3 | 37 40 37 34 35 36 36 40 35 32 36
32 | 7 10 6 9 4 2 7 9 9 12 3 | 18 27 20 15 15 18 16 27 15 22 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 10 9 11 9 3 10 9 10 11 |T 33 35 35 35 33 33 32 30 34 35 33
WRMS | 8 10 9 11 8 3 10 9 9 11 |NE 26 28 28 28 26 26 25 28 26 28 26
MEDI | 8 9 8 9 8 3 9 8 9 11 |MD 26 28 29 29 26 26 25 29 26 28 25
Table 3.2338.6 GPS week: 2338 Day: 6 MJD: 60616.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs IGS | cod emr esa gfz grg igr jgx jpl mit ngs IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 10 7 4 10 8 3 9 8 11 12 3 | 19 18 21 25 20 20 21 19 26 26 20
3 | 8 9 11 11 7 3 11 9 11 13 3 | 28 27 33 31 26 28 27 27 28 25 27
4 | 8 18 7 9 11 3 10 17 12 14 4 | 16 22 18 20 21 16 19 22 26 24 17
5 | 10 9 7 11 13 4 13 10 8 15 3 | 33 30 30 32 30 30 30 29 30 37 30
6 | 7 10 8 13 8 3 8 8 10 13 3 | 26 25 26 23 21 22 21 24 21 24 22
7 | 5 7 9 12 8 2 9 6 8 9 3 | 76 76 76 77 73 75 75 75 75 76 75
8 | 7 9 7 9 6 3 7 6 10 16 3 | 26 27 27 24 24 25 26 26 24 29 25
9 | 6 11 9 15 8 5 9 10 8 13 3 | 19 29 21 25 21 23 19 28 23 22 21
10 | 7 9 8 12 8 2 7 9 10 11 3 | 24 22 28 27 23 23 23 22 22 23 22
X11 | 10 15 9 14 9 3 --- 9 8 19 4 | 48 48 51 52 51 48 --- 51 46 53 49
12E | 10 9 10 9 9 5 15 9 8 19 4 | 50 50 53 48 49 50 49 47 49 52 49
13 | 5 8 8 8 7 3 9 7 12 12 3 | 17 21 19 22 17 18 15 21 16 21 17
14E | 14 11 18 7 13 4 12 12 14 20 5 | 38 40 43 40 38 38 39 39 41 41 38
15 | 8 6 7 8 7 3 11 6 11 10 3 | 36 36 36 40 36 36 35 38 35 37 36
16E | 11 11 8 9 16 4 15 12 9 18 4 | 31 38 38 33 27 34 36 37 33 37 33
17 | 11 9 7 8 9 3 9 8 12 13 3 | 27 25 20 25 21 21 19 23 24 27 22
18 | 9 13 9 8 9 3 9 14 14 13 4 | 50 53 54 54 52 52 50 56 48 55 51
19 | 9 11 6 11 8 2 12 8 14 15 3 | 21 18 18 25 17 17 14 16 20 24 17
20E | 7 10 7 11 11 3 8 7 10 11 3 | 53 54 53 50 57 52 51 53 53 52 53
21 | 12 9 5 8 19 4 13 9 10 12 4 | 19 19 19 23 21 20 20 18 24 25 19
22E | 10 9 6 11 6 3 7 7 12 15 3 | 31 27 25 30 23 25 25 27 27 31 26
23 | 8 9 15 17 10 3 11 13 7 10 4 | 27 31 36 33 34 32 29 34 34 32 31
24 | 7 6 10 7 7 2 6 7 8 12 2 | 20 23 24 21 18 20 18 24 18 24 19
25E | 9 9 15 28 8 4 11 11 10 17 5 | 77 78 79 79 78 77 77 78 77 78 77
26E | 42 30 26 68 90 28 29 34 29 40 13 | 475 473 472 477 431 467 476 485 477 478 474
27 | 6 7 7 9 6 3 6 7 8 15 2 | 23 24 25 21 21 22 22 23 22 25 22
28 | 7 7 8 6 6 3 10 8 8 14 3 | 31 31 33 33 33 32 30 34 33 37 32
29 | 9 9 5 9 7 3 15 9 10 17 3 | 38 37 38 35 36 37 39 37 39 38 36
30 | 8 7 8 10 8 3 8 7 7 8 2 | 32 33 31 31 31 30 30 33 30 33 31
31 | 6 12 8 10 7 3 10 9 12 10 3 | 59 63 60 58 57 58 59 63 58 61 59
32 | 6 11 6 9 7 2 8 10 10 10 3 | 22 30 25 21 22 23 20 30 21 23 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 10 17 19 6 11 11 11 15 |T 48 49 49 49 46 47 47 49 48 50 47
WRMS | 8 11 9 10 9 3 11 11 9 15 |NE 30 31 33 32 30 30 28 32 30 33 30
MEDI | 8 9 8 10 8 3 9 9 10 13 |MD 31 30 31 31 27 30 27 30 30 32 30
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 4.2338 GPS week: 2338 MJD: 60610.0-60616.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 |U 10 14 23 |U 11 17 49 |U 12 13 32 |
emr | emr 2970 |U 14 14 30 |U 13 17 54 | 13 12 30 |
esa | esa 2976 | 16 19 43 |U 12 19 51 |U 16 19 32 |
gfz | gfz 2975 |U 10 10 24 |U 11 15 38 | 11 9 25 |
grg | grg 2975 |U 11 12 21 |U 12 18 43 | 11 11 25 |
igr | igr 2975 | 11 12 23 | 11 16 42 | 11 11 26 |
igs | igs 2975 | 11 13 24 | 11 15 43 | 12 12 25 |
jgx | jgx 2880 |U 11 12 24 |U 12 17 46 | 9 10 27 |
jpl | jpl 2962 | 18 18 33 | 10 17 51 | 15 17 31 |
mit | mit 2976 |U 10 11 21 |U 11 16 43 |U 10 9 26 |
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 5.2338.0 GPS week: 2338 Day: 0 MJD: 60610.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 15 30 | 13 18 45 | 13 11 34 |
emr | emr 2974 | 16 17 36 | 15 16 48 | 14 13 29 |
esa | esa 2976 | 15 22 42 | 14 19 43 | 18 19 33 |
gfz | gfz 2976 | 10 11 30 | 13 17 40 | 13 8 28 |
grg | grg 2976 | 12 15 27 | 13 18 45 | 13 10 31 |
igr | igr 2976 | 11 13 27 | 12 17 38 | 13 9 28 |
igs | igs 2976 | 12 15 29 | 12 16 38 | 13 11 28 |
jgx | jgx 2880 | 10 13 28 | 14 19 45 | 11 10 30 |
jpl | jpl 2976 | 19 17 36 | 11 16 41 | 17 20 29 |
mit | mit 2976 | 8 12 24 | 13 16 36 | 11 8 27 |
Table 5.2338.1 GPS week: 2338 Day: 1 MJD: 60611.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 15 12 23 | 11 18 45 | 12 13 30 |
emr | emr 2976 | 17 10 29 | 11 17 50 | 12 13 29 |
esa | esa 2976 | 20 16 41 | 11 21 39 | 16 22 34 |
gfz | gfz 2976 | 14 9 22 | 12 16 37 | 11 9 25 |
grg | grg 2976 | 15 11 23 | 11 17 33 | 12 12 27 |
igr | igr 2976 | 15 9 23 | 10 16 36 | 11 12 26 |
igs | igs 2976 | 15 10 24 | 10 15 36 | 11 13 25 |
jgx | jgx 2880 | 14 10 23 | 11 19 43 | 9 12 26 |
jpl | jpl 2976 | 20 14 31 | 9 18 42 | 15 18 28 |
mit | mit 2976 | 16 12 22 | 9 13 37 | 10 8 26 |
Table 5.2338.2 GPS week: 2338 Day: 2 MJD: 60612.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 16 23 | 10 16 47 | 11 15 33 |
emr | emr 2976 | 12 14 30 | 12 15 56 | 10 11 27 |
esa | esa 2976 | 14 20 41 | 11 18 51 | 16 20 29 |
gfz | gfz 2976 | 7 10 20 | 11 16 35 | 10 11 22 |
grg | grg 2975 | 8 13 20 | 10 17 37 | 10 12 23 |
igr | igr 2976 | 8 12 21 | 10 15 42 | 10 11 22 |
igs | igs 2976 | 8 13 22 | 10 14 43 | 10 13 22 |
jgx | jgx 2880 | 7 12 18 | 10 17 52 | 8 11 25 |
jpl | jpl 2976 | 15 16 30 | 10 15 51 | 14 16 27 |
mit | mit 2976 | 7 13 18 | 10 17 43 | 9 11 25 |
Table 5.2338.3 GPS week: 2338 Day: 3 MJD: 60613.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 14 21 | 9 15 51 | 12 14 30 |
emr | emr 2971 | 12 12 26 | 11 14 68 | 13 11 30 |
esa | esa 2976 | 15 19 42 | 10 18 60 | 16 18 35 |
gfz | gfz 2976 | 9 11 18 | 10 13 39 | 13 9 30 |
grg | grg 2976 | 10 14 17 | 9 15 45 | 11 11 28 |
igr | igr 2976 | 10 12 20 | 9 13 47 | 11 12 27 |
igs | igs 2976 | 10 12 21 | 8 13 49 | 12 11 26 |
jgx | jgx 2880 | 8 11 15 | 9 14 48 | 9 10 26 |
jpl | jpl 2976 | 15 15 30 | 9 15 58 | 15 13 30 |
mit | mit 2976 | 9 11 17 | 9 13 47 | 11 8 26 |
Table 5.2338.4 GPS week: 2338 Day: 4 MJD: 60614.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 14 19 | 11 18 50 | 13 17 31 |
emr | emr 2967 | 14 15 29 | 13 23 45 | 14 15 27 |
esa | esa 2976 | 15 20 41 | 13 25 41 | 18 20 31 |
gfz | gfz 2976 | 8 7 19 | 13 17 30 | 12 11 22 |
grg | grg 2976 | 10 10 19 | 12 18 36 | 12 12 22 |
igr | igr 2976 | 9 12 22 | 12 19 37 | 13 15 25 |
igs | igs 2976 | 9 12 22 | 12 18 36 | 13 13 22 |
jgx | jgx 2880 | 8 9 16 | 12 17 36 | 11 11 29 |
jpl | jpl 2976 | 15 19 32 | 11 23 46 | 17 18 28 |
mit | mit 2976 | 9 12 17 | 11 14 37 | 13 12 25 |
Table 5.2338.5 GPS week: 2338 Day: 5 MJD: 60615.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 15 29 | 13 19 46 | 11 7 33 |
emr | emr 2966 | 12 11 28 | 14 19 50 | 12 8 32 |
esa | esa 2976 | 17 20 49 | 13 20 57 | 15 15 33 |
gfz | gfz 2975 | 13 12 40 | 12 15 36 | 10 8 21 |
grg | grg 2975 | 11 13 22 | 14 20 42 | 11 8 26 |
igr | igr 2975 | 10 12 25 | 11 17 41 | 10 8 24 |
igs | igs 2974 | 10 12 25 | 12 17 42 | 11 7 24 |
jgx | jgx 2880 | 13 10 39 | 12 17 41 | 7 6 24 |
jpl | jpl 2880 | 17 17 29 | 13 20 49 | 13 15 26 |
mit | mit 2976 | 12 11 36 | 11 17 41 | 9 7 22 |
Table 5.2338.6 GPS week: 2338 Day: 6 MJD: 60616.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 13 19 | 11 15 60 | 13 16 36 |
emr | emr 2966 | 16 22 29 | 12 14 63 | 14 14 36 |
esa | esa 2976 | 15 17 43 | 12 16 66 | 16 18 33 |
gfz | gfz 2976 | 7 11 21 | 11 13 48 | 11 10 27 |
grg | grg 2976 | 9 12 20 | 12 20 60 | 10 11 21 |
igr | igr 2975 | 13 17 24 | 11 13 52 | 11 13 28 |
igs | igs 2974 | 14 19 27 | 11 14 55 | 12 13 28 |
jgx | jgx 2880 | 15 23 32 | 13 18 55 | 11 12 31 |
jpl | jpl 2976 | 21 29 44 | 9 13 73 | 16 17 46 |
mit | mit 2976 | 9 11 17 | 12 21 62 | 10 12 28 |
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 6.2338 GPS week: 2338 MJD: 60610.500-60616.500
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 | -16 -4 41 -48 -3 | -3 20
| 12 30 72 78 3 | 2
emr uuuuu | 24 -15 81 138 -3 | -10 21
| 13 21 74 49 6 | 3
esa uuuuu | -11 20 -1 -14 -1 | 16 27
| 12 12 30 52 6 | 2
gfz uuuuu | -19 -2 -85 -12 5 | -5 22
| 17 20 96 120 6 | 2
grg uuuuu | -8 6 -15 -50 0 | -7 21
| 9 14 40 58 3 | 2
igr xxxxx | 6 10 11 49 5 | -7 22
| 11 9 37 46 3 | 2
irf xxxxx | -8 2 -22 -3 3 | -3 21
| 5 8 8 14 3 | 2
jgx uuuuu | 15 -15 42 -94 2 | 1 20
| 9 13 34 38 3 | 2
jpl uuuuu | -1 0 77 14 -1 | -3 24
| 14 23 57 58 13 | 2
mit uuuuu | 4 15 -142 13 0 | 13 24
| 12 18 29 36 4 | 2
ngs uuuuu | 28 -8 -7 86 -2 | 7 21
| 54 46 148 180 3 | 2
Table 7.2338.0 GPS week: 2338 Day: 0 MJD: 60610.500
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 | -22 -27 -39 68 1 | -1 15
emr uuuuu | 42 -22 64 125 -5 | -7 17
esa uuuuu | 3 24 60 -76 5 | 17 24
gfz uuuuu | -11 31 -182 47 13 | -7 18
grg uuuuu | -7 -3 65 -131 -2 | -7 16
igr xxxxx | 14 3 61 62 4 | -8 19
irf xxxxx | -1 12 -14 -8 8 | -6 18
jgx uuuuu | 4 -3 73 -109 0 | 1 15
jpl uuuuu | 3 26 54 110 -20 | -1 22
mit uuuuu | 21 45 -125 48 4 | 12 20
ngs uuuuu | -19 -75 87 -115 2 | 7 19
Table 7.2338.1 GPS week: 2338 Day: 1 MJD: 60611.500
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 | -7 -12 48 -27 -2 | 0 14
emr uuuuu | 14 12 -15 86 -2 | -6 16
esa uuuuu | -20 33 -7 -46 2 | 18 24
gfz uuuuu | 4 -13 -152 203 3 | -5 16
grg uuuuu | -8 -5 -6 -19 4 | -6 16
igr xxxxx | 17 7 7 50 5 | -6 17
irf xxxxx | -17 -2 -20 -20 3 | -3 14
jgx uuuuu | 18 -22 50 -108 4 | 2 14
jpl uuuuu | 0 20 16 -26 -8 | 0 21
mit uuuuu | 6 27 -119 -23 -2 | 14 19
ngs uuuuu | 5 -55 217 -31 -1 | 9 17
Table 7.2338.2 GPS week: 2338 Day: 2 MJD: 60612.500
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 | -7 -15 33 22 -4 | -5 18
emr uuuuu | 43 -2 64 92 -13 | -11 21
esa uuuuu | -10 15 -16 -75 7 | 13 22
gfz uuuuu | -12 20 -197 -11 13 | -9 19
grg uuuuu | -16 -2 -37 17 3 | -11 19
igr xxxxx | 20 15 27 100 9 | -11 20
irf xxxxx | -7 4 -15 -15 7 | -6 18
jgx uuuuu | 28 -11 61 -21 8 | -3 16
jpl uuuuu | 13 -4 119 9 -12 | -6 24
mit uuuuu | -13 17 -115 38 0 | 10 20
ngs uuuuu | -22 -16 85 -107 -8 | 5 19
Table 7.2338.3 GPS week: 2338 Day: 3 MJD: 60613.500
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 | -22 -36 -24 -101 -5 | -1 21
emr uuuuu | 15 -13 185 97 -1 | -8 22
esa uuuuu | 0 33 -4 11 -1 | 18 30
gfz uuuuu | -9 -5 -100 6 4 | -4 25
grg uuuuu | -11 7 -28 -75 -2 | -6 23
igr xxxxx | 1 20 -18 63 3 | -5 25
irf xxxxx | -3 12 -33 1 3 | -1 23
jgx uuuuu | 20 2 -1 -64 4 | 3 23
jpl uuuuu | -1 0 143 9 -1 | -2 26
mit uuuuu | 11 10 -154 58 6 | 15 26
ngs uuuuu | 1 -1 -54 79 -2 | 10 24
Table 7.2338.4 GPS week: 2338 Day: 4 MJD: 60614.500
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 | -39 29 133 -35 -7 | -1 21
emr uuuuu | 25 2 9 201 -3 | -10 22
esa uuuuu | -5 -2 -14 -3 -4 | 17 29
gfz uuuuu | -23 -6 15 -155 3 | -3 25
grg uuuuu | -10 -5 1 -40 0 | -6 23
igr xxxxx | -9 18 27 -18 9 | -5 25
irf xxxxx | -8 -6 -18 0 0 | -1 23
jgx uuuuu | 7 -14 86 -117 2 | 2 23
jpl uuuuu | 12 9 14 -12 18 | -3 25
mit uuuuu | 7 -13 -136 -27 -4 | 15 27
ngs uuuuu | 41 -1 -153 270 -3 | 8 23
Table 7.2338.5 GPS week: 2338 Day: 5 MJD: 60615.500
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 -10 -4 -119 -4 | -5 24
emr uuuuu | 17 -28 161 175 0 | -13 25
esa uuuuu | -15 23 12 45 -7 | 15 30
gfz uuuuu | -35 -15 36 -49 2 | -4 26
grg uuuuu | 12 18 -41 11 1 | -8 25
igr xxxxx | 5 -5 23 93 6 | -6 25
irf xxxxx | -11 5 -23 -5 3 | -3 25
jgx uuuuu | 20 -34 16 -112 -2 | 1 24
jpl uuuuu | -30 -8 144 -63 6 | -5 25
mit uuuuu | -10 16 -144 -17 2 | 13 27
ngs uuuuu | 65 40 -207 171 1 | 6 24
Table 7.2338.6 GPS week: 2338 Day: 6 MJD: 60616.500
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 45 141 -146 -1 | -6 24
emr uuuuu | 14 -51 102 186 5 | -14 25
esa uuuuu | -32 13 -36 45 -7 | 14 29
gfz uuuuu | -45 -24 -17 -129 -2 | -3 26
grg uuuuu | -16 31 -56 -111 -4 | -9 25
igr xxxxx | -4 10 -52 -8 1 | -5 26
irf xxxxx | -8 -7 -32 23 -1 | -2 25
jgx uuuuu | 9 -23 11 -128 0 | 1 24
jpl uuuuu | -1 -43 49 67 11 | -6 24
mit uuuuu | 10 1 -200 12 -2 | 13 27
ngs uuuuu | 128 52 -27 335 -4 | 5 22
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