[IGSREPORT-30186] Wk 2339 IGS Final Orbits
acc
acc at igs.org
Fri Nov 22 05:58:27 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2339 (Nov 03, 2024 - Nov 09, 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_20243080000_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 | ADIS CRO1 DARW FALK GUAM HOFN MATE SCUB SEYG SGPO
0 | COD | MATE
0 | ESA | SYOG
0 | GFZ | 21 26 PTVL PTVL SYOG
0 | GRG | IRKJ NRMD SVTL KIRI NRMD SCUB SVTL
0 | JPL | BADG SGOC BADG CHTI FTNA GUAM IISC NRMD PTGG SGOC
0 | MIT | FLIN PDEL SFER WILL FLIN PDEL SFER WILL
1 | COD | AREQ
1 | ESA | BAKE FAIR QAQ1 BAKE QAQ1
1 | GFZ | 4 24 AREQ KIT3 LAUT AREQ KIT3 LAUT
1 | GRG | CZTG GMSD SCUB SEYG CZTG GMSD KIRI NRMD SEYG
1 | JPL | BADG CPVG NRMD THU2 BADG CPVG IISC MAC1 MONP NRMD
1 | JPL | THU2 ZAMB
1 | MIT | BADG DRAO MCM4 NRC1 PDEL SFER TLSG ZECK BADG DRAO
1 | MIT | MCM4 NRC1 PDEL SFER TLSG ZECK
2 | COD | 25 25 AREQ CCJ2 GAMB KOUR MCIL THU2 AREQ CZTG
2 | ESA | THU2 THU2
2 | GFZ | 25 POHN POHN
2 | GRG | AREQ CZTG KIRI NRMD SCUB AREQ CZTG KIRI NRMD
2 | JGX | BOAV
2 | JPL | AREQ AREQ CHTI FTNA NRMD PGEN PTGG THU2
2 | MIT | DRAO MGUE SFER DRAO MGUE SFER
3 | COD | ASCG BOGT CCJ2 CRO1 DARW DGAR FALK GAMB HRAO LPGS
3 | COD | MCIL MOBS NKLG NRMD PDEL STHL SUTM UFPR YKRO
3 | GFZ | NRMD PTVL
3 | GRG | NRMD
3 | JGX | BELE
3 | JPL | BOGT RIO2 BOGT CRO1 FALK HRAO LPGS MBAR NRMD RIO2
3 | JPL | STHL UFPR YKRO ZAMB
3 | MIT | DRAO IRKJ SFER TRO1 YEL2 DRAO IRKJ SFER TRO1 YEL2
4 | COD | BOAV CZTG PIE1 SEYG WHIT BOAV CZTG PIE1 WHIT
4 | ESA | FALK HRAO SEYG
4 | GFZ | LAUT HRAO KOUR LAUT
4 | GRG | BRFT CZTG MAJU NRMD PIE1 CZTG KIRI NRMD PIE1 SEYG
4 | JPL | BADG OHI3 SEYG BADG GLPS HRAO OHI3
4 | MIT | AMC4 BRST FLIN MDVJ SFER TLSE TLSG AMC4 BRST FLIN
4 | MIT | MDVJ SFER TLSG
5 | COD | GUAT CZTG GUAT POVE SCRZ
5 | EMR | BADG BADG
5 | ESA | AREQ CHPI SAVO VILL CHPI SAVO THU2 URUM VILL
5 | GFZ | AREQ POVE PTVL POVE PTVL
5 | GRG | CZTG GMSD CZTG GMSD
5 | JPL | BADG BADG GLPS HOLB
5 | MIT | BRUX DRAO KERG TLSE TRO1 YEL2 DRAO KERG TLSE TRO1
5 | MIT | YEL2
6 | COD | 12 CZTG SCUB URUM
6 | ESA | FAIR WHIT FAIR WHIT
6 | GFZ | 5 5 POHN HRAO POHN
6 | GRG | CZTG TRO1 CZTG FLIN
6 | JGX | POVE POVE
6 | JPL | MAC1 RIO2 THU2 FAIR GLPS KOUR MAC1 RIO2 THU2 TRO1
6 | MIT | AMC4 IRKJ SFER STJ3 AMC4 IRKJ SFER STJ3
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
----+--------+--------+-------------
1 | COD | ~10:20 | ~ -0.15 ns
4 | COD | ~14:00 | ~ -0.13 ns
5 | COD | ~13:25 | ~ 0.13 ns
6 | COD | ~09:55 | ~ -0.14 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
----+--------+---------------
0 | EMR | ALL (high Transformation - See Table 2)
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
Starting 28-Nov-2022, all IGS products, are based on the IGS realization of
the ITRF2020 reference frame (IGS20). Starting from the same date, the IGS
products are based on the repro3 standards, including long filename formats.
For more information see IGSMAIL #8238, #8256, #8274 and #8282.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .3 -1.7 -.4 -9 13 -31 .03
EMR | 0 | 4.1 3.0 -6.2 23 -26 16 .56
ESA | 0 | .2 -.4 .8 0 -10 -11 -.52
GFZ | 0 | .1 -1.8 .2 -31 12 2 .31
GRG | 0 | .2 -.6 -1.1 34 18 -2 -.12
JGX | 0 | 3.3 7.1 7.5 -2 -7 20 -.32
JPL | 0 | 2.0 2.4 -3.9 8 -9 -10 -.07
MIT | 0 | 5.0 5.6 27.3 16 -2 -10 .05
NGS | 0 | 5.8 13.3 17.3 27 39 -38 .00
SIO | 0 | 1.5 8.0 11.4 155 -7 10 -.15
COD | 1 | .5 -1.3 -.4 -11 3 -30 -.05
EMR | 1 | 1.8 1.9 -3.9 24 -11 18 .08
ESA | 1 | .3 -.3 .8 -2 -7 -3 -.48
GFZ | 1 | .6 -1.1 .2 -31 -7 0 .24
GRG | 1 | .0 -1.0 -.9 23 -6 4 -.06
JGX | 1 | .0 5.4 3.0 10 -3 14 -.08
JPL | 1 | 1.9 2.9 -4.5 13 -17 -9 .02
MIT | 1 | 3.2 6.0 27.0 43 -10 21 -.28
NGS | 1 | 6.7 4.2 17.1 24 -1 -3 -.25
SIO | 1 | 1.8 6.0 11.7 71 10 24 -.04
COD | 2 | .2 -1.3 -.4 -14 4 -27 -.12
EMR | 2 | -7.3 2.7 -3.0 31 -24 31 -.19
ESA | 2 | -.3 -.1 1.3 -12 -11 -13 -.58
GFZ | 2 | .2 -.4 .7 -16 -18 -20 .41
GRG | 2 | .8 -.9 -.6 13 0 16 -.23
JGX | 2 | -1.3 6.0 8.4 -15 6 13 -.38
JPL | 2 | .0 6.0 -3.4 8 -11 -7 -.06
MIT | 2 | 1.4 7.2 23.9 42 -11 27 -.30
NGS | 2 | .7 .0 21.4 20 8 -22 -.14
SIO | 2 | -.5 7.5 16.7 138 -13 22 -.33
COD | 3 | .5 -1.5 -1.1 -24 -1 -12 -.24
EMR | 3 | 6.3 12.4 -4.9 35 -27 24 -.33
ESA | 3 | .3 .5 .9 -7 -6 -3 -.91
GFZ | 3 | .6 .4 .7 -25 14 1 .15
GRG | 3 | -.0 .8 -1.4 12 5 6 -.30
JGX | 3 | -1.7 12.9 6.3 12 14 -3 -.52
JPL | 3 | .4 11.1 -3.6 19 -13 1 -.02
MIT | 3 | 3.2 6.8 27.0 27 -8 -10 -.31
NGS | 3 | -.8 13.1 8.1 47 23 -10 -.62
SIO | 3 | 1.5 7.8 11.5 127 -7 27 -.16
COD | 4 | .0 -1.4 -1.0 -26 -5 -29 -.09
EMR | 4 | 2.6 8.5 -8.8 42 -24 25 -.42
ESA | 4 | .1 .2 .9 -13 -22 -9 -.80
GFZ | 4 | .3 -1.0 .6 -34 0 -2 .11
GRG | 4 | .1 1.0 -1.5 28 8 -3 -.31
JGX | 4 | -.2 11.0 6.4 13 6 4 -.69
JPL | 4 | 4.3 5.1 -8.8 31 -24 9 -.19
MIT | 4 | .5 8.5 24.8 26 3 -11 -.30
NGS | 4 | 2.9 8.6 11.4 43 20 -16 -.33
SIO | 4 | 2.5 11.7 12.0 139 -62 35 -.29
COD | 5 | .1 -2.0 -1.2 -18 -3 -28 -.08
EMR | 5 | 2.4 1.2 -8.0 24 -38 55 -.25
ESA | 5 | .1 1.4 .3 2 -23 -10 -.88
GFZ | 5 | 1.0 -1.1 -.5 -18 -24 -1 .08
GRG | 5 | .8 -.7 -1.6 15 13 2 -.20
JGX | 5 | .3 7.7 4.6 4 -8 23 -.70
JPL | 5 | 2.0 3.3 -5.5 17 -32 -10 -.24
MIT | 5 | 1.0 5.8 25.6 20 -10 -7 -.11
NGS | 5 | 5.1 8.2 6.2 47 4 -34 -.25
SIO | 5 | 1.9 6.7 12.3 84 -72 25 -.16
COD | 6 | -.0 -1.5 -1.3 -12 2 -41 -.05
EMR | 6 | -1.8 1.9 -7.9 33 -20 36 .04
ESA | 6 | -.1 -.7 .9 -4 -7 -3 -.51
GFZ | 6 | .7 -1.6 .4 -25 4 -5 .46
GRG | 6 | -.3 -.9 -1.5 17 6 -6 .09
JGX | 6 | .9 7.1 4.3 9 -14 9 -.26
JPL | 6 | .2 -1.0 -6.7 21 2 10 -.05
MIT | 6 | 1.9 4.7 23.7 51 -5 4 -.03
NGS | 6 | .9 8.9 5.9 55 3 1 -.11
SIO | 6 | 4.8 2.6 7.8 28 -14 7 .12
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.atx
The JPL final solution has not yet adopted IGS20/igs20.atx after GPS Week 2238,
which causes their orbit and clock residuals to be higher than for the other
centres; from GPS Week 2238 and until they switch to IGS20/igs20.atx, the JPL
solution is excluded from the weekly SINEX combination, as well as from orbit
and clock combinations.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.2339.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2339.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 2.2339.[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 3.2339.[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 5.2339.0-6). 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 2339 summary. (Nov 03, 2024 - Nov 09, 2024)
Table 1.2339.a GPS week: 2339 MJD: 60617.000-60623.000
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 781| 0 0 3 -7 8 13 .01 9 8 | -815 144 6 109
| 0 0 1 14 9 31 .03 | 192 302
emr 109| -1 -2 -3 3 3 313 .14 76 76 | -893 -1008 164 236
| 3 1 1 23 11 900 .24 | 1358 2589
esa 150| 0 -1 5 -37 8 -8 -.01 9 9 | -650 -64 6 69
| 0 0 0 7 10 12 .02 | 300 387
gfz 125| 1 1 4 4 16 -26 .10 11 11 | -1 -77 11 119
| 0 0 1 11 8 14 .04 | 115 184
grg 127| 0 0 -2 -1 -5 -20 -.02 9 8 | 0 -12 7 126
| 0 0 0 15 11 13 .01 | 50 78
igr n/a| 0 0 0 -7 3 0 .02 3 3 | -5493 38 9 77
| 0 0 0 10 5 15 .01 | 469 479
jgx n/a| -1 0 4 2 -27 -15 -.05 10 10 | -101 141 36 97
| 0 0 0 10 5 10 .01 | 229 300
jpl 120| -1 0 0 14 -13 -11 .06 10 10 | -1876 68 7 70
| 0 1 1 13 10 8 .01 | 417 530
mit 368| 1 0 -7 14 -2 63 .01 9 9 | -5516 85 59 84
| 0 0 1 30 36 52 .01 | 371 307
ngs 271| 0 0 -1 -2 0 -7 -.07 12 11 | -788 112 534 728
| 1 1 4 16 31 13 .02 | 172 232
sio 339| 0 0 -4 7 3 17 -.02 10 9 | --- --- --- ---
| 0 0 1 13 8 24 .01 | --- ---
Table 1.2339.b GPS week : 2339 MJD: 60617.000-60623.000
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 | 4 4 3 3 3 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 3 4 3 3 4 4 3 |
6 | 3 3 3 3 3 3 3 |
7 | 3 3 3 3 3 3 3 |
8 | 3 3 3 3 3 2 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 3 3 3 3 4 |
12 | 4 4 4 4 3 4 5 |
13 | 3 4 3 3 3 3 3 |
14 | 5 5 6 6 6 5 5 |
15 | 3 3 3 3 3 3 3 |
16 | 4 4 5 4 4 4 5 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 4 4 3 3 3 |
19 | 4 4 4 3 3 3 3 |
20 | 4 3 3 3 3 3 3 |
21 | 4 3 4 3 3 3 3 |
22 | 3 3 3 3 3 3 4 |
23 | 4 4 4 4 4 4 4 |
24 | 3 3 3 3 3 2 3 |
25 | 6 6 6 5 4 4 4 |
26 | 5 5 5 4 4 4 4 |
27 | 3 3 3 3 3 3 3 |
28 | 3 3 3 3 3 3 3 |
29 | 4 3 4 3 3 3 3 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2339.0 GPS week: 2339 Day: 0 MJD: 60617.000
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 784| 0 0 4 -13 14 72 -.01 8 8 | -939 516 6 105
emr 114| 2 -5 0 -35 -11 2354 .68 472 472 | 2105 -6789 930 975
esa 150| 0 -2 5 -35 11 -16 .01 9 9 | -578 -88 6 71
gfz 129| 1 2 7 6 21 -12 .12 12 11 | 41 -163 10 124
grg 127| 0 0 -2 11 9 -4 -.02 9 8 | 43 -122 7 120
igr n/a| 0 0 0 -3 2 -2 .03 3 3 | -4934 -320 9 69
jgx n/a| -2 0 4 -16 -31 -5 -.04 11 11 | -156 301 38 96
jpl 120| -2 -1 -2 9 -17 -10 .06 10 10 | -1711 -1 8 68
mit 368| 0 0 -8 10 -64 -16 .01 9 8 | -5163 139 61 81
ngs 274| 0 2 0 10 54 -6 -.07 11 10 | -762 253 499 721
sio 346| 0 0 -5 2 9 -5 -.01 9 10 | --- --- --- ---
Table 2.2339.1 GPS week: 2339 Day: 1 MJD: 60618.000
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 784| 0 -1 1 22 2 -6 -.03 9 8 | -663 -27 6 116
emr 110| -3 -2 -3 -15 -2 -9 .09 10 10 | -1327 -321 43 89
esa 150| 0 -1 6 -32 26 2 .02 10 10 | -719 115 6 78
gfz 128| 1 1 4 -1 12 -2 .08 13 12 | -163 123 12 130
grg 129| 0 1 -2 3 0 -33 -.02 9 9 | -16 95 7 116
igr n/a| 0 0 0 -26 6 0 .02 4 4 | -5487 -576 10 89
jgx n/a| -1 0 3 11 -25 -30 -.04 11 11 | 71 -7 33 96
jpl 120| 0 0 0 -7 0 -6 .09 9 9 | -1909 -459 7 57
mit 368| 2 0 -8 55 -24 58 .01 11 10 | -5596 -357 64 87
ngs 274| 0 0 1 -25 4 -6 -.07 11 11 | -665 -24 535 680
sio 342| 0 1 -3 -7 0 32 -.01 10 9 | --- --- --- ---
Table 2.2339.2 GPS week: 2339 Day: 2 MJD: 60619.000
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 -21 20 15 -.01 9 8 | -593 -326 6 101
emr 106| -6 -2 -4 9 8 7 .08 11 11 | -1681 -106 32 95
esa 150| 1 0 4 -34 12 -3 .01 10 10 | -215 -760 6 75
gfz 127| 0 1 3 21 32 -45 .07 11 11 | 94 14 11 117
grg 128| 0 0 -3 -4 -8 -20 -.03 10 9 | 19 -67 7 130
igr n/a| 0 0 0 -9 4 18 .02 3 3 | -6148 17 9 72
jgx n/a| 0 0 4 10 -20 -6 -.06 10 10 | 81 -275 35 107
jpl 120| -2 0 0 7 -15 -4 .08 10 10 | -2487 -63 7 66
mit 368| 2 0 -7 3 -1 31 .02 10 9 | -6022 -234 58 83
ngs 273| 1 0 4 4 -44 -3 -.07 12 12 | -623 -246 501 709
sio 343| 1 0 -3 16 7 32 -.02 9 8 | --- --- --- ---
Table 2.2339.3 GPS week: 2339 Day: 3 MJD: 60620.000
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 4 -8 15 22 .01 8 8 | -1028 392 7 109
emr 109| 0 -1 -3 34 11 -53 .06 9 9 | -1832 686 31 115
esa 150| 0 -1 6 -33 9 11 .00 10 9 | -811 -137 6 64
gfz 124| 0 0 2 5 8 -25 .13 10 10 | 38 -289 11 109
grg 128| 0 0 -1 11 -2 -6 -.05 10 8 | -46 79 8 131
igr n/a| 0 0 0 -6 8 19 .02 3 3 | -6023 781 10 84
jgx n/a| -1 0 4 0 -34 -6 -.05 10 10 | -132 210 38 95
jpl 120| -2 0 0 24 -17 0 .05 9 9 | -2389 1025 7 65
mit 368| 1 0 -6 -5 -18 37 .02 10 9 | -5896 527 60 82
ngs 274| 0 0 -5 -7 21 6 -.08 12 11 | -1000 351 578 763
sio 341| 0 0 -3 -12 1 13 -.03 8 8 | --- --- --- ---
Table 2.2339.4 GPS week: 2339 Day: 4 MJD: 60621.000
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 4 -19 9 -19 .02 8 8 | -671 -5 6 104
emr 110| -1 0 -5 16 21 -55 .03 10 10 | -869 -791 36 114
esa 150| 0 0 6 -44 0 -14 -.02 9 9 | -318 -256 7 69
gfz 126| 0 2 4 -12 8 -32 .17 12 11 | 1 -148 11 116
grg 126| 0 0 0 6 -15 -30 -.02 8 8 | 86 -44 7 129
igr n/a| 0 0 0 9 2 -7 .02 3 3 | -5137 -326 9 68
jgx n/a| 0 0 3 0 -28 -13 -.08 10 10 | 65 20 39 110
jpl 120| -1 0 2 36 -18 -23 .07 10 10 | -1353 -359 7 74
mit 368| 0 0 -5 -16 29 116 .00 9 8 | -5296 -4 60 89
ngs 269| 1 0 -3 16 -14 -18 -.03 11 11 | -668 -5 544 743
sio 341| 1 0 -5 18 5 49 -.03 10 9 | --- --- --- ---
Table 2.2339.5 GPS week: 2339 Day: 5 MJD: 60622.000
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 5 -5 -8 26 .06 8 7 | -1068 407 7 110
emr 111| 0 -1 -5 18 8 -28 .03 10 10 | -1437 72 38 149
esa 150| 0 0 5 -30 4 -25 -.03 9 9 | -860 437 7 65
gfz 122| 1 1 2 13 12 -29 .05 10 10 | -155 178 11 120
grg 125| 0 0 -1 -9 3 -10 -.02 8 7 | -33 -43 8 138
igr n/a| 0 0 0 -3 7 -19 .00 3 3 | -5629 326 9 86
jgx n/a| 0 0 4 11 -21 -28 -.04 10 10 | -570 685 37 92
jpl 120| -3 -1 0 19 -26 -20 .05 10 10 | -1669 -200 7 78
mit 368| 0 0 -5 -6 25 82 .01 8 8 | -5614 295 55 81
ngs 268| 0 0 -5 -23 -11 -32 -.10 13 13 | -1059 401 520 762
sio 328| 0 0 -2 10 14 22 -.02 9 9 | --- --- --- ---
Table 2.2339.6 GPS week: 2339 Day: 6 MJD: 60623.000
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| -1 0 4 -6 6 -15 -.00 9 8 | -743 51 8 118
emr 106| 0 -1 -2 -5 -8 -22 .04 10 10 | -1210 192 44 117
esa 150| 1 0 7 -49 -5 -16 -.03 9 9 | -1054 239 6 63
gfz 124| 1 0 4 -2 21 -37 .09 11 11 | 133 -260 12 121
grg 126| 0 0 -2 -32 -23 -35 -.02 9 8 | -48 12 7 122
igr n/a| 0 0 0 -7 -6 -16 .02 4 3 | -5099 368 10 71
jgx n/a| -1 0 5 0 -31 -15 -.05 10 10 | -69 58 35 86
jpl 120| -1 0 0 11 3 -16 .05 10 10 | -1618 539 7 82
mit 368| 0 0 -6 59 39 134 .01 9 8 | -5029 229 59 85
ngs 271| -1 0 -6 4 -11 8 -.05 12 12 | -743 54 566 719
sio 332| 0 0 -6 22 -12 -22 -.02 11 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 3.2339.0 GPS week: 2339 Day: 0 MJD: 60617.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
2 | 9 479 5 12 8 2 8 7 8 10 9 3 | 19 189 21 28 19 21 19 19 21 17 24 19
3 | 8 481 13 8 8 3 11 9 9 9 9 3 | 26 215 29 31 25 26 26 28 26 27 28 26
4 | 8 467 8 9 8 3 7 22 10 8 11 3 | 27 194 27 35 32 29 28 29 32 32 36 29
5 | 8 475 5 10 12 2 12 12 4 8 6 3 | 43 202 41 42 43 42 43 40 42 40 41 41
6 | 8 481 9 13 7 3 7 8 10 7 13 3 | 27 205 26 29 24 24 21 26 21 25 25 23
7 | 6 471 10 10 8 3 9 7 6 12 5 2 | 61 207 61 62 54 58 59 60 58 58 56 58
8 | 7 473 8 8 5 3 8 7 6 9 7 2 | 24 189 26 23 21 23 21 23 21 24 25 22
9 | 6 462 10 7 8 4 7 9 8 11 7 3 | 20 200 20 23 17 19 17 27 21 22 23 19
10 | 10 484 9 10 7 3 8 11 6 12 7 3 | 21 215 24 20 22 21 20 22 20 23 25 20
11 | 10 469 10 12 9 3 12 9 13 11 10 3 | 33 215 37 41 35 35 33 36 37 35 39 35
12E | 8 473 12 10 17 4 16 11 7 11 12 4 | 105 143 109 107 102 106 108 106 104 105 106 105
13 | 6 482 8 10 6 3 6 8 9 10 12 3 | 14 187 15 11 13 13 12 20 18 14 16 13
14E | 10 469 19 13 13 4 12 11 16 14 14 5 | 71 278 79 75 66 73 72 73 82 75 81 74
15 | 6 466 7 8 8 2 9 7 7 12 8 2 | 39 195 40 41 37 38 42 37 36 39 39 38
16E | 11 475 10 8 11 3 14 10 7 14 9 3 | 63 169 65 61 62 63 65 61 62 66 64 62
17 | 9 477 6 14 8 3 9 8 7 8 12 3 | 25 183 23 32 23 24 23 25 25 25 27 24
18 | 8 478 9 9 9 3 10 12 11 13 6 3 | 37 214 42 39 41 39 42 41 39 40 40 39
19 | 7 474 6 14 8 2 15 9 10 7 14 3 | 25 186 26 32 23 24 21 25 27 23 28 24
20E | 9 468 6 10 9 3 11 9 10 13 9 3 | 25 229 23 22 24 23 23 23 26 24 26 22
21 | 12 476 5 9 11 3 14 7 9 10 8 3 | 20 184 20 24 19 19 17 19 20 20 24 18
22E | 6 473 7 11 8 3 8 8 10 9 10 3 | 42 175 38 38 39 38 37 39 42 41 40 38
23 | 8 482 14 13 10 3 14 12 6 10 6 3 | 32 229 39 30 37 35 32 40 38 33 38 35
24 | 6 456 10 8 4 2 9 7 6 9 8 2 | 24 202 25 25 24 23 22 28 20 25 20 22
25E | 10 463 17 34 13 4 12 8 10 11 14 5 | 40 196 45 47 46 42 41 37 46 43 46 42
26E | 9 458 10 27 12 4 12 12 8 15 6 4 | 23 207 28 30 24 26 27 27 27 26 23 25
27 | 7 476 8 8 6 3 7 8 7 11 8 2 | 24 193 25 22 23 23 20 23 20 21 25 21
28 | 7 477 6 8 6 3 9 9 7 11 5 2 | 38 200 36 39 41 37 38 38 34 39 38 37
29 | 7 473 6 8 8 3 15 9 10 12 11 3 | 26 189 25 25 24 25 27 24 28 24 26 24
30 | 8 462 9 9 7 3 7 7 7 8 6 2 | 31 201 27 30 23 26 26 28 22 28 22 25
31 | 7 468 8 8 6 3 13 9 5 12 8 3 | 48 212 49 48 43 45 46 47 45 41 44 45
32 | 7 473 8 11 6 3 6 12 7 11 9 3 | 23 188 26 24 24 24 23 32 21 22 24 23
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 472 9 12 9 3 11 10 9 11 9 |T 34 199 36 36 33 34 33 35 34 34 36 33
WRMS | 8 472 9 11 8 3 11 10 8 10 10 |NE 28 199 29 31 28 28 27 30 28 28 30 27
MEDI | 8 473 8 10 8 3 9 9 8 11 9 |MD 27 200 27 31 24 26 27 28 27 27 28 25
Table 3.2339.1 GPS week: 2339 Day: 1 MJD: 60618.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
2 | 10 9 7 14 11 4 9 7 10 12 8 3 | 19 181 19 24 17 19 19 17 20 21 20 17
3 | 8 10 12 9 7 3 10 9 11 17 7 3 | 22 166 27 26 22 23 21 25 25 26 23 22
4 | 7 19 6 15 8 3 10 18 14 8 11 4 | 19 161 23 36 25 23 24 26 28 22 27 23
5 | 9 11 7 16 11 3 12 12 9 10 7 3 | 30 165 28 34 30 29 28 27 33 26 28 28
6 | 9 9 10 14 9 4 8 6 9 9 9 3 | 25 187 26 26 22 23 21 26 21 24 23 22
7 | 7 8 11 9 8 3 10 7 10 7 9 3 | 38 197 41 40 35 38 39 41 40 40 37 38
8 | 6 10 9 9 6 3 7 7 11 12 7 2 | 23 191 27 23 22 24 22 25 25 27 24 23
9 | 7 10 8 7 7 4 9 8 9 11 9 3 | 18 177 21 21 19 18 15 26 21 19 24 19
10 | 10 13 9 10 5 2 9 8 7 8 8 3 | 22 175 24 20 23 21 20 23 21 20 24 21
11 | 9 13 11 10 9 3 10 10 12 11 9 3 | 23 178 24 23 27 22 22 26 24 24 25 23
12E | 9 9 11 12 7 3 16 10 11 11 11 3 | 70 162 75 71 72 72 73 73 71 70 71 72
13 | 6 8 10 23 10 4 6 10 10 7 15 3 | 14 185 16 17 15 13 12 21 15 16 15 12
14E | 13 10 22 14 17 5 11 12 22 13 19 5 | 53 119 56 51 50 51 52 53 58 52 58 52
15 | 7 10 7 7 8 2 12 7 9 7 10 3 | 28 171 27 26 28 26 29 27 25 26 23 25
16E | 13 10 13 10 10 5 15 9 13 15 14 4 | 41 159 50 46 43 48 50 48 47 50 48 46
17 | 10 6 11 11 11 4 11 8 9 10 11 3 | 22 175 21 25 18 20 17 23 21 23 24 20
18 | 8 14 10 8 7 3 10 11 11 16 8 3 | 24 172 27 27 29 25 29 29 28 26 25 26
19 | 11 8 8 12 10 4 15 8 11 14 14 3 | 21 181 21 24 18 19 16 20 22 24 22 18
20E | 10 10 7 10 8 3 11 7 9 13 8 3 | 31 150 27 25 29 28 28 28 26 33 29 27
21 | 11 8 6 7 9 4 12 9 11 11 8 3 | 21 175 19 21 19 21 20 20 19 26 20 18
22E | 8 7 8 12 7 4 7 5 10 10 10 2 | 31 148 30 29 29 29 27 30 35 28 36 30
23 | 8 11 16 13 8 3 13 12 7 14 6 3 | 21 165 29 23 28 24 23 29 29 20 27 24
24 | 7 7 9 14 7 3 7 8 11 7 6 2 | 23 178 23 23 19 21 19 25 19 21 19 20
X25E | 13 11 19 30 17 5 11 --- 12 17 14 6 | 36 118 39 36 44 36 34 --- 41 41 40 36
26E | 8 9 9 30 12 3 12 11 12 15 7 4 | 27 165 28 29 27 27 29 27 27 30 27 26
27 | 8 10 9 8 5 4 6 8 11 11 8 2 | 22 190 27 24 23 24 24 25 25 23 25 23
28 | 8 8 6 8 8 2 9 7 9 10 6 2 | 25 196 28 29 27 28 28 29 28 30 32 27
29 | 6 9 6 8 6 4 16 11 10 15 8 3 | 23 188 22 24 22 23 23 22 24 24 22 21
30 | 7 7 9 10 9 3 8 8 11 6 9 2 | 21 177 24 22 20 21 18 26 21 21 20 20
31 | 8 11 10 13 8 4 11 9 9 10 7 3 | 36 187 35 32 32 33 35 38 32 31 31 33
32 | 6 13 8 11 6 2 8 9 10 8 7 3 | 19 173 25 22 22 23 21 31 20 22 23 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 9 10 10 13 9 4 11 9 11 11 10 |T 27 171 29 29 27 27 27 29 28 28 28 26
WRMS | 8 10 10 12 9 4 11 9 10 11 9 |NE 23 179 25 25 23 23 22 26 24 24 24 22
MEDI | 8 10 9 11 8 3 10 8 10 11 8 |MD 23 175 27 25 25 24 23 26 25 26 25 23
Table 3.2339.2 GPS week: 2339 Day: 2 MJD: 60619.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
2 | 9 9 9 14 7 3 10 8 10 11 9 3 | 20 73 22 28 21 22 20 20 22 25 25 20
3 | 7 10 13 10 6 2 8 9 9 9 9 3 | 26 62 30 26 25 25 26 27 27 23 27 25
4 | 9 19 8 9 8 2 8 20 12 7 10 4 | 25 62 28 25 29 27 28 29 30 25 32 25
5 | 8 13 6 8 11 3 11 14 7 10 6 3 | 44 55 41 44 41 43 43 39 43 43 45 42
6 | 9 10 9 10 5 3 8 7 8 12 8 3 | 28 74 27 30 24 25 24 28 24 27 28 25
7 | 6 8 9 8 8 3 8 6 8 8 8 2 | 48 88 47 50 43 47 45 49 48 48 46 46
8 | 7 10 9 8 6 3 6 5 11 11 10 2 | 20 78 25 20 20 20 20 21 21 19 24 20
9 | 7 11 9 8 8 3 7 8 7 9 5 2 | 19 71 22 24 19 22 19 26 23 23 25 21
10 | 8 13 9 14 6 2 8 9 9 8 9 3 | 26 68 29 29 26 26 25 27 25 26 29 25
11 | 8 14 12 7 8 3 8 10 10 12 7 3 | 18 57 25 26 23 22 20 25 21 24 23 21
12E | 15 12 9 15 10 3 15 10 9 14 7 4 | 66 79 69 69 65 68 70 68 66 71 70 68
13 | 6 9 7 11 6 3 6 9 10 9 10 2 | 17 73 19 15 17 16 15 23 16 19 16 16
14E | 16 11 23 13 23 4 11 13 19 20 21 6 | 53 66 59 52 49 53 52 53 61 52 60 53
15 | 8 9 5 6 7 3 10 7 9 9 8 2 | 32 66 32 32 32 32 33 33 29 34 32 31
16E | 16 10 11 11 20 4 13 9 10 15 11 4 | 48 60 54 49 46 51 52 50 50 56 52 49
17 | 9 11 7 10 10 3 9 8 9 11 9 3 | 28 67 26 29 24 27 26 28 26 28 27 26
18 | 9 14 9 8 8 3 10 12 11 17 9 3 | 21 61 24 26 24 23 24 28 23 29 28 24
19 | 10 13 5 12 7 2 15 8 11 8 14 3 | 25 66 25 30 21 24 21 25 25 24 28 23
20E | 7 14 6 10 9 3 8 9 6 11 8 3 | 25 46 25 28 24 23 21 21 25 25 24 23
21 | 12 8 7 9 24 4 14 8 10 10 12 4 | 20 75 21 23 26 20 18 21 21 23 24 19
22E | 7 11 8 12 10 3 8 8 11 10 8 3 | 38 60 34 34 33 35 32 37 36 39 34 35
23 | 9 11 17 10 9 3 10 12 8 18 9 3 | 28 64 34 28 30 30 27 34 31 24 34 29
24 | 7 7 10 8 6 2 6 8 10 11 6 2 | 27 66 27 23 23 25 25 30 22 32 27 25
X25E | 12 30 16 19 12 5 8 --- 13 23 12 5 | 39 74 39 40 41 38 37 --- 41 43 38 37
26E | 10 10 10 28 12 6 13 10 12 20 8 4 | 21 53 22 31 19 21 20 20 21 22 24 19
27 | 9 10 9 7 5 3 5 7 10 13 8 2 | 20 75 25 21 19 21 20 21 20 21 21 20
28 | 9 8 5 6 7 3 9 8 10 13 7 2 | 22 81 24 25 24 23 24 24 29 24 29 23
29 | 9 12 6 7 8 4 16 10 10 13 11 3 | 22 73 20 23 21 21 22 21 24 21 21 20
30 | 6 9 8 10 7 3 8 7 8 7 8 2 | 27 65 26 30 22 25 24 28 22 28 26 24
31 | 7 11 9 6 7 3 11 10 7 14 8 3 | 41 83 42 41 37 41 40 46 40 39 42 40
32 | 6 13 8 7 5 2 5 10 9 8 7 2 | 25 69 27 28 25 26 24 33 22 24 29 26
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 9 11 10 11 10 3 10 10 10 12 9 |T 29 68 31 31 28 29 28 31 30 31 31 29
WRMS | 8 11 10 11 9 3 10 10 9 12 8 |NE 25 70 27 27 25 25 24 28 25 26 27 24
MEDI | 9 11 9 10 8 3 8 9 10 11 8 |MD 26 67 27 28 24 25 24 28 25 25 28 25
Table 3.2339.3 GPS week: 2339 Day: 3 MJD: 60620.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
2 | 6 6 8 12 7 2 9 7 11 13 5 3 | 22 70 24 29 23 24 25 24 24 29 24 23
3 | 7 10 13 8 7 2 6 8 11 12 6 3 | 26 65 30 25 25 24 24 25 23 27 25 24
4 | 7 17 6 9 9 2 7 20 13 11 8 3 | 23 65 24 28 25 25 25 29 26 28 28 23
5 | 7 13 5 10 12 4 10 12 6 12 9 3 | 40 74 39 40 38 40 39 37 39 43 38 38
6 | 9 8 9 9 6 3 7 7 7 12 10 3 | 27 62 27 27 24 26 24 26 24 24 25 24
7 | 6 8 11 7 7 3 10 6 8 9 8 2 | 48 72 46 48 41 46 45 47 44 43 42 44
8 | 6 9 8 8 5 2 9 7 7 11 6 2 | 25 65 26 24 24 24 28 26 24 27 28 24
9 | 7 9 9 9 7 4 7 8 8 12 9 3 | 26 65 26 30 24 27 25 32 26 24 26 26
10 | 10 10 10 10 5 3 8 7 6 8 6 2 | 28 67 29 27 26 26 26 27 24 26 26 25
11 | 8 12 11 8 8 4 10 9 8 11 10 3 | 28 63 32 27 31 28 27 30 29 28 33 28
12E | 12 9 9 10 10 5 15 9 9 13 9 3 | 44 72 44 42 44 44 45 44 45 45 44 43
13 | 5 8 8 12 6 4 6 8 9 11 7 2 | 23 65 25 17 23 22 21 26 22 22 20 21
14E | 13 10 22 13 30 4 12 13 18 14 17 5 | 75 90 75 74 71 73 75 75 80 77 79 75
15 | 7 8 6 7 6 3 10 6 10 11 6 2 | 43 76 44 40 42 43 45 42 41 41 41 41
16E | 10 9 12 11 14 2 14 9 10 19 8 4 | 44 73 47 44 45 45 48 45 46 45 42 44
17 | 8 8 8 10 9 2 11 8 8 10 7 3 | 28 63 27 32 24 28 27 27 26 31 27 26
18 | 9 13 9 9 7 3 10 13 11 16 8 3 | 27 64 34 29 31 29 29 34 28 31 33 29
19 | 10 6 7 10 8 2 14 7 9 11 9 3 | 25 58 26 29 22 25 24 24 24 28 27 23
20E | 8 11 7 10 8 3 8 9 7 7 9 2 | 29 66 27 25 28 29 28 26 26 29 30 26
21 | 8 7 6 7 6 3 12 7 10 13 5 2 | 21 70 21 24 23 22 23 24 24 25 23 21
22E | 7 7 7 14 9 4 8 5 9 6 10 3 | 36 51 33 37 30 33 32 35 37 35 38 34
23 | 8 10 18 13 9 3 11 12 6 14 7 3 | 26 63 31 24 29 28 27 30 28 24 30 26
24 | 7 7 9 10 7 3 7 7 9 11 5 2 | 27 64 30 26 27 28 24 30 26 29 29 26
X25E | 14 15 15 12 15 5 9 --- 13 14 12 4 | 33 71 36 36 41 33 32 --- 36 35 37 33
26E | 10 10 9 12 13 3 11 11 12 17 9 3 | 29 74 32 30 28 29 31 31 31 29 32 29
27 | 7 6 8 9 5 3 5 6 10 10 5 2 | 23 66 26 26 24 25 28 27 23 26 27 24
28 | 7 8 6 7 7 2 8 8 7 8 7 2 | 19 64 25 24 24 23 21 23 23 25 28 22
29 | 7 8 4 7 8 3 16 11 10 12 12 3 | 28 58 24 26 24 25 29 26 27 23 24 24
30 | 8 9 8 8 8 3 9 6 10 9 9 2 | 29 63 28 26 24 27 27 29 24 26 23 25
31 | 8 10 8 7 6 3 11 8 8 11 9 3 | 42 77 45 40 41 41 40 45 41 34 40 40
32 | 6 9 9 7 5 3 5 10 10 7 8 2 | 23 64 26 24 23 25 25 31 21 22 24 24
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 9 10 10 10 3 10 9 10 12 8 |T 31 67 32 31 30 31 31 32 31 31 32 30
WRMS | 8 9 9 10 8 3 10 9 9 11 8 |NE 27 65 29 28 27 27 27 29 27 27 28 26
MEDI | 8 9 8 9 7 3 9 8 9 11 8 |MD 28 65 29 28 26 28 27 29 26 28 28 26
Table 3.2339.4 GPS week: 2339 Day: 4 MJD: 60621.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
2 | 6 5 6 12 9 3 11 10 6 13 8 3 | 22 59 21 24 20 19 20 19 20 21 22 19
3 | 8 9 13 9 6 2 7 7 7 7 8 2 | 28 59 32 27 25 26 25 26 24 28 24 25
4 | 6 17 6 10 8 1 9 19 12 12 10 3 | 24 44 25 29 25 25 25 27 25 31 24 23
5 | 9 10 5 16 15 3 10 14 6 11 9 3 | 38 45 36 42 36 36 37 33 35 40 39 36
6 | 6 8 8 16 6 3 8 8 8 9 9 3 | 25 69 25 26 22 22 22 25 22 25 23 22
7 | 5 9 7 9 7 3 10 7 7 8 9 2 | 42 85 41 43 38 40 42 43 43 37 40 40
8 | 6 10 8 9 5 1 7 5 8 9 7 2 | 28 70 28 27 25 27 27 26 26 28 28 26
9 | 6 10 8 7 5 2 8 8 7 10 11 2 | 23 62 21 26 19 21 19 26 22 21 21 21
10 | 11 12 11 9 7 3 9 8 7 10 10 3 | 29 57 32 27 26 27 25 29 28 27 30 26
11 | 8 12 11 10 8 2 8 10 6 13 9 3 | 27 62 32 29 31 28 27 31 30 29 32 29
12E | 10 9 9 6 13 4 12 7 10 9 8 3 | 57 29 55 56 53 55 56 57 54 57 55 55
13 | 6 9 9 8 5 3 7 8 11 9 9 2 | 15 61 16 20 14 16 12 22 16 15 14 14
14E | 11 14 18 21 15 8 20 12 27 17 27 6 | 63 90 68 61 63 63 63 64 72 68 75 64
15 | 7 9 7 8 7 2 9 7 9 8 8 2 | 43 57 42 42 40 41 40 42 40 37 40 40
16E | 11 8 9 14 11 3 15 8 9 16 10 3 | 55 36 55 56 50 54 54 52 52 53 53 53
17 | 8 8 10 10 10 3 11 8 8 10 11 3 | 25 48 23 26 22 23 22 25 24 24 27 22
18 | 10 12 9 10 8 3 9 11 8 12 9 3 | 34 59 35 38 35 35 33 40 34 37 37 35
19 | 8 7 7 10 7 3 15 9 7 11 10 3 | 22 53 22 25 18 20 20 22 20 21 23 19
20E | 8 9 6 8 6 3 8 8 7 6 10 2 | 23 50 22 23 22 21 21 23 23 22 27 21
21 | 9 6 6 9 8 2 14 8 6 12 8 3 | 23 56 22 24 21 21 22 21 21 22 23 20
22E | 6 7 7 13 7 4 7 6 11 9 11 3 | 31 27 30 28 31 30 30 31 33 36 36 30
23 | 10 9 18 17 8 3 11 13 6 13 8 4 | 20 54 26 22 27 22 22 26 24 22 26 22
24 | 9 8 9 9 7 3 5 9 6 14 7 2 | 23 57 23 23 21 22 17 27 19 24 24 21
25E | 13 10 13 20 9 3 9 11 11 9 10 4 | 35 54 38 33 40 35 35 36 37 34 38 35
26E | 12 11 8 23 11 3 11 11 10 17 11 4 | 28 55 28 24 24 26 27 26 28 28 27 25
27 | 8 8 8 10 6 2 8 6 8 7 6 2 | 28 61 26 24 24 25 26 25 25 26 26 24
28 | 7 7 4 9 6 3 8 8 8 7 11 2 | 25 75 27 26 27 25 25 25 29 26 33 26
29 | 9 10 6 10 9 4 15 11 6 10 13 3 | 31 68 28 30 28 29 31 28 30 29 27 28
30 | 6 9 9 9 8 5 8 7 10 6 10 2 | 22 61 22 23 19 20 20 24 19 19 21 19
31 | 7 10 7 9 5 4 11 10 7 12 8 2 | 32 67 33 31 32 31 31 38 32 30 31 32
32 | 7 10 7 6 6 1 6 10 9 8 8 2 | 28 48 27 29 25 28 26 35 25 27 30 27
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 10 9 12 8 3 10 10 9 11 10 |T 30 57 31 31 29 29 29 31 30 30 31 29
WRMS | 8 10 9 11 8 3 10 10 8 11 9 |NE 26 60 27 27 25 25 25 28 26 26 27 25
MEDI | 8 9 8 10 7 3 9 8 8 10 9 |MD 28 57 28 27 25 26 26 27 26 28 27 26
Table 3.2339.5 GPS week: 2339 Day: 5 MJD: 60622.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
2 | 5 8 7 8 8 3 9 7 8 19 11 3 | 29 43 30 34 29 31 31 30 32 38 31 30
3 | 10 9 12 7 7 3 7 9 9 29 8 3 | 39 27 41 38 38 38 38 39 37 41 38 37
4 | 5 17 7 9 8 2 8 19 10 13 9 3 | 39 28 40 44 43 42 42 43 44 39 44 41
5 | 8 10 6 14 10 5 12 12 9 12 8 3 | 73 48 76 75 73 75 76 73 76 78 74 74
6 | 6 8 9 13 7 3 4 7 7 10 10 2 | 32 42 34 35 29 31 30 31 30 29 29 30
7 | 5 9 9 6 4 3 10 6 5 10 9 2 | 44 49 44 46 42 44 43 45 45 39 43 43
8 | 5 7 8 7 6 2 6 6 7 10 8 2 | 30 41 32 32 30 31 31 32 31 33 29 30
9 | 8 10 10 8 4 3 8 9 7 16 9 3 | 32 36 31 35 31 32 30 36 32 34 32 32
10 | 10 10 10 9 8 4 9 9 7 9 5 2 | 40 29 41 37 38 39 40 40 39 41 40 39
11 | 7 12 11 9 9 3 8 9 8 15 10 3 | 30 38 33 35 33 31 33 32 34 31 33 32
12E | 11 11 8 10 11 4 14 13 15 9 12 4 | 107 84 114 110 107 111 112 109 112 110 111 110
13 | 6 9 9 7 6 3 8 9 8 13 12 3 | 22 40 25 22 21 23 22 26 23 25 20 22
14E | 15 13 16 14 13 5 15 11 14 13 13 4 | 61 93 60 59 60 57 57 61 63 59 60 59
15 | 8 10 8 7 6 2 9 6 7 12 9 2 | 43 31 45 42 42 42 43 42 44 41 42 42
16E | 11 9 9 12 12 3 13 12 8 9 7 3 | 71 52 75 73 66 73 75 71 74 71 74 71
17 | 7 8 8 9 9 2 8 9 7 8 10 2 | 36 40 35 37 34 36 37 36 37 38 37 35
18 | 9 13 8 8 7 3 9 11 7 10 9 3 | 36 39 37 35 37 36 37 39 37 36 37 36
19 | 8 10 5 12 8 2 12 9 10 16 9 3 | 33 41 34 35 30 33 32 32 34 39 33 32
20E | 9 9 7 9 8 4 7 7 9 16 10 3 | 32 50 32 32 30 32 33 31 32 40 33 31
21 | 7 7 6 8 7 3 13 9 7 11 9 2 | 28 47 28 29 26 28 27 28 30 31 29 27
22E | 9 7 7 9 5 5 8 7 9 9 11 2 | 42 50 42 41 40 42 38 44 45 48 47 42
23 | 9 9 17 9 9 3 11 12 4 14 9 3 | 30 29 36 32 34 33 36 37 34 31 34 33
24 | 5 5 9 8 4 2 6 7 6 9 6 2 | 30 28 36 30 31 34 34 36 32 37 32 32
25E | 11 11 14 19 9 3 12 11 12 11 7 4 | 29 49 33 26 29 27 28 29 32 28 31 28
26E | 10 13 8 15 12 3 13 12 7 16 12 4 | 32 47 33 33 30 31 32 30 35 28 36 31
27 | 6 7 8 7 7 3 7 7 7 13 6 2 | 30 45 31 30 28 30 31 30 31 31 30 29
28 | 7 7 6 7 7 2 7 7 7 9 10 2 | 34 43 35 38 35 36 36 34 36 37 38 35
29 | 8 8 7 10 7 4 15 10 5 11 11 3 | 30 46 29 31 28 29 28 26 29 29 27 27
30 | 6 10 7 8 6 3 8 6 7 10 8 2 | 35 28 36 36 34 36 35 36 35 36 36 34
31 | 7 9 8 7 5 2 12 8 7 9 10 2 | 41 40 43 43 39 42 41 45 42 40 43 41
32 | 7 10 8 8 4 3 6 10 7 8 6 2 | 35 32 36 33 36 36 36 42 35 33 36 36
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 10 9 10 8 3 10 10 8 13 9 |T 39 43 41 40 38 40 40 40 41 41 40 39
WRMS | 7 10 9 10 7 3 10 10 8 13 9 |NE 33 37 35 35 33 34 34 35 34 35 34 33
MEDI | 8 9 8 9 7 3 9 9 7 11 9 |MD 34 41 36 35 34 36 36 36 35 37 36 34
Table 3.2339.6 GPS week: 2339 Day: 6 MJD: 60623.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
2 | 8 6 7 9 9 2 9 6 8 11 7 2 | 21 49 20 22 21 20 21 20 23 23 20 20
3 | 7 11 12 16 9 3 10 9 10 13 7 3 | 32 47 37 36 33 32 31 32 32 33 30 32
4 | 5 16 7 10 8 2 9 18 9 14 8 3 | 34 38 34 37 37 35 37 37 37 36 37 35
5E | 8 9 8 7 10 5 9 12 8 10 10 3 | 97 71 97 99 95 97 97 95 101 98 95 97
6 | 7 8 8 17 7 4 7 8 9 10 10 3 | 24 59 25 25 22 22 21 24 22 22 23 22
7 | 5 9 9 8 3 4 9 7 7 10 9 2 | 55 76 54 53 49 52 50 54 53 51 48 51
8 | 6 8 8 7 6 3 8 6 6 10 6 2 | 29 56 32 31 28 30 29 31 31 31 30 30
9 | 10 11 9 10 5 4 6 8 6 12 7 2 | 29 53 29 32 27 29 30 32 28 27 28 28
10 | 11 11 10 10 10 3 9 10 7 14 9 3 | 36 42 38 36 34 35 34 35 33 39 35 34
11 | 8 12 11 6 11 3 7 10 10 12 15 3 | 42 62 46 44 46 43 43 45 46 44 47 44
12E | 11 14 7 11 16 5 15 16 17 13 25 5 | 135 98 139 140 136 139 138 135 139 136 140 137
13 | 6 8 9 6 6 3 7 7 7 10 12 2 | 14 62 16 16 14 14 12 21 15 16 16 14
14E | 13 11 19 14 13 5 12 14 13 20 16 4 | 83 122 87 81 81 82 82 83 89 88 90 84
15 | 6 8 8 8 8 4 9 7 7 10 10 2 | 60 60 58 57 57 57 60 57 60 55 59 57
16E | 11 10 11 18 19 4 14 16 11 14 12 4 | 75 41 78 78 71 76 79 75 78 77 78 76
17 | 8 6 6 12 9 3 8 7 8 8 11 2 | 29 46 26 31 27 28 29 30 29 29 28 28
18 | 10 13 9 9 8 3 8 10 7 11 8 3 | 50 63 51 51 51 49 50 52 51 51 50 50
19 | 8 9 5 13 9 3 13 8 9 13 11 3 | 26 50 26 28 22 25 26 26 27 31 23 25
20E | 7 9 8 11 6 3 8 9 9 17 8 3 | 23 55 23 27 23 23 23 24 25 29 24 23
21 | 9 8 5 8 8 3 12 7 7 9 8 2 | 25 51 21 22 20 22 22 21 21 23 20 21
22E | 13 9 9 11 8 5 9 8 10 12 13 3 | 49 37 45 45 46 47 46 48 49 52 46 46
23 | 11 10 16 19 12 4 9 13 6 15 9 4 | 24 49 32 27 32 29 28 33 31 33 30 28
24 | 8 6 9 8 6 3 6 7 6 12 11 2 | 26 50 29 24 25 25 24 30 24 28 26 25
25E | 12 12 12 13 8 4 11 12 12 14 9 4 | 43 66 43 40 46 42 40 41 47 47 46 43
26E | 11 10 9 19 9 4 11 12 8 15 6 3 | 31 47 33 28 28 30 31 30 32 32 30 29
27 | 7 13 8 9 8 4 7 7 6 8 5 2 | 31 54 33 34 28 32 31 33 34 32 30 31
28 | 8 8 5 8 8 3 7 9 7 10 9 2 | 36 71 39 38 39 38 39 40 37 40 41 38
29 | 9 7 5 10 7 4 16 11 7 14 9 3 | 39 69 35 36 35 36 38 35 38 34 32 35
30 | 8 9 8 8 6 3 8 8 9 8 13 2 | 28 48 28 28 25 27 24 30 23 27 23 25
31 | 8 8 8 7 5 2 9 8 7 14 8 2 | 43 61 44 41 39 40 41 45 39 35 37 40
32 | 7 10 8 7 5 3 8 11 8 9 8 2 | 33 45 34 34 35 35 35 41 32 36 38 35
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 9 10 9 11 9 4 10 10 9 12 11 |T 42 58 42 42 41 41 41 43 42 43 41 41
WRMS | 8 10 9 11 8 3 10 10 8 12 9 |NE 33 54 34 34 32 32 32 34 33 33 32 32
MEDI | 8 9 8 10 8 3 9 9 8 12 9 |MD 33 54 34 36 34 35 34 35 33 34 32 34
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 4.2339 GPS week: 2339 MJD: 60617.0-60623.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 |U 9 12 22 |U 13 12 46 |U 13 17 36 |
emr | emr 2969 |U 18 17 42 |U 22 22 90 | 19 20 48 |
esa | esa 2976 | 18 14 44 |U 12 17 55 |U 14 20 39 |
gfz | gfz 2975 |U 8 10 22 |U 11 12 39 | 11 12 31 |
grg | grg 2975 |U 9 12 19 |U 13 13 38 | 11 13 30 |
igr | igr 2976 | 9 10 21 | 12 11 41 | 11 14 30 |
igs | igs 2975 | 10 10 21 | 11 11 41 | 11 14 30 |
jgx | jgx 2976 |U 8 9 21 |U 12 13 39 | 10 13 29 |
jpl | jpl 2934 | 18 14 34 | 10 15 52 | 15 20 36 |
mit | mit 2976 |U 8 10 17 |U 13 11 41 |U 10 11 30 |
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 5.2339.0 GPS week: 2339 Day: 0 MJD: 60617.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 15 17 | 10 13 50 | 12 17 31 |
emr | emr 2962 | 44 46 92 | 81 71 316 | 44 39 98 |
esa | esa 2976 | 17 16 38 | 11 16 56 | 15 21 35 |
gfz | gfz 2975 | 8 11 14 | 12 12 42 | 12 12 23 |
grg | grg 2976 | 10 13 15 | 11 14 40 | 11 15 28 |
igr | igr 2976 | 9 11 16 | 10 13 46 | 12 15 28 |
igs | igs 2976 | 10 11 15 | 10 12 46 | 11 14 26 |
jgx | jgx 2976 | 7 9 15 | 10 13 44 | 10 13 27 |
jpl | jpl 2976 | 17 17 30 | 9 18 54 | 13 19 34 |
mit | mit 2976 | 9 10 15 | 10 13 48 | 10 11 27 |
Table 5.2339.1 GPS week: 2339 Day: 1 MJD: 60618.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 10 28 | 12 15 52 | 11 16 29 |
emr | emr 2967 | 13 14 35 | 13 15 61 | 13 16 38 |
esa | esa 2976 | 17 15 49 | 12 17 61 | 13 18 37 |
gfz | gfz 2976 | 8 7 25 | 9 11 38 | 10 12 26 |
grg | grg 2976 | 9 10 20 | 12 16 40 | 10 11 28 |
igr | igr 2976 | 9 9 25 | 11 13 44 | 10 12 26 |
igs | igs 2976 | 9 9 26 | 11 13 44 | 10 12 27 |
jgx | jgx 2976 | 9 7 25 | 12 15 40 | 9 13 26 |
jpl | jpl 2880 | 14 13 39 | 11 14 54 | 14 19 32 |
mit | mit 2976 | 8 8 21 | 12 14 44 | 8 10 27 |
Table 5.2339.2 GPS week: 2339 Day: 2 MJD: 60619.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 11 27 | 13 12 45 | 17 18 34 |
emr | emr 2968 | 15 12 38 | 14 13 42 | 14 19 37 |
esa | esa 2976 | 18 12 47 | 12 16 48 | 12 21 37 |
gfz | gfz 2976 | 8 12 28 | 12 18 54 | 11 13 27 |
grg | grg 2976 | 9 12 20 | 13 14 34 | 9 14 23 |
igr | igr 2976 | 10 10 26 | 11 10 34 | 10 14 28 |
igs | igs 2973 | 10 10 27 | 11 11 35 | 10 14 26 |
jgx | jgx 2976 | 8 10 24 | 15 17 52 | 8 15 27 |
jpl | jpl 2880 | 19 12 38 | 11 12 49 | 15 19 31 |
mit | mit 2976 | 9 11 22 | 12 10 33 | 9 14 29 |
Table 5.2339.3 GPS week: 2339 Day: 3 MJD: 60620.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 11 24 | 13 12 37 | 10 16 33 |
emr | emr 2964 | 13 9 36 | 14 12 60 | 13 13 40 |
esa | esa 2976 | 17 13 42 | 13 15 51 | 11 19 38 |
gfz | gfz 2976 | 8 11 20 | 10 10 28 | 8 7 28 |
grg | grg 2975 | 10 12 18 | 14 12 30 | 9 10 30 |
igr | igr 2976 | 10 10 20 | 12 11 33 | 9 13 30 |
igs | igs 2976 | 10 10 21 | 12 11 35 | 9 12 30 |
jgx | jgx 2976 | 9 10 21 | 12 14 26 | 8 10 27 |
jpl | jpl 2880 | 17 9 31 | 9 9 45 | 16 18 33 |
mit | mit 2976 | 10 12 21 | 12 10 36 | 8 10 30 |
Table 5.2339.4 GPS week: 2339 Day: 4 MJD: 60621.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 10 21 | 14 14 44 | 14 16 36 |
emr | emr 2975 | 13 11 29 | 13 16 58 | 16 18 36 |
esa | esa 2976 | 17 12 38 | 14 18 60 | 15 20 34 |
gfz | gfz 2976 | 6 10 22 | 11 12 41 | 12 12 29 |
grg | grg 2976 | 7 11 19 | 15 13 45 | 11 12 28 |
igr | igr 2976 | 8 9 18 | 13 12 45 | 12 15 29 |
igs | igs 2976 | 8 9 19 | 13 12 44 | 12 14 29 |
jgx | jgx 2976 | 7 9 20 | 14 13 39 | 11 14 29 |
jpl | jpl 2976 | 17 13 27 | 12 18 55 | 14 22 31 |
mit | mit 2976 | 7 9 16 | 15 12 44 | 11 11 29 |
Table 5.2339.5 GPS week: 2339 Day: 5 MJD: 60622.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 14 19 | 14 13 46 | 14 16 35 |
emr | emr 2976 | 13 14 30 | 11 18 44 | 15 14 36 |
esa | esa 2976 | 19 17 43 | 13 20 51 | 15 20 41 |
gfz | gfz 2976 | 8 8 20 | 11 12 35 | 10 11 29 |
grg | grg 2975 | 8 13 16 | 14 12 39 | 11 11 31 |
igr | igr 2976 | 10 12 17 | 13 13 39 | 12 14 30 |
igs | igs 2976 | 10 12 17 | 12 13 39 | 12 14 31 |
jgx | jgx 2976 | 9 11 18 | 13 12 34 | 11 13 26 |
jpl | jpl 2976 | 19 18 35 | 11 20 51 | 14 18 38 |
mit | mit 2976 | 7 10 12 | 14 10 39 | 10 11 29 |
Table 5.2339.6 GPS week: 2339 Day: 6 MJD: 60623.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 12 20 | 14 7 46 | 14 22 52 |
emr | emr 2976 | 16 15 36 | 12 12 53 | 17 20 53 |
esa | esa 2976 | 19 17 48 | 12 14 58 | 16 23 49 |
gfz | gfz 2976 | 9 8 27 | 11 8 38 | 16 20 52 |
grg | grg 2976 | 8 12 27 | 14 9 38 | 13 17 45 |
igr | igr 2976 | 10 12 24 | 12 8 43 | 13 16 41 |
igs | igs 2976 | 11 12 25 | 12 8 43 | 13 17 44 |
jgx | jgx 2976 | 8 10 23 | 12 9 35 | 12 16 43 |
jpl | jpl 2976 | 21 20 36 | 10 16 55 | 18 24 56 |
mit | mit 2976 | 6 10 15 | 14 8 46 | 13 13 39 |
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 6.2339 GPS week: 2339 MJD: 60617.500-60623.500
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 | -5 -6 79 9 -2 | -1 23
| 16 12 76 68 6 | 3
emr uuuux | 8 -31 117 122 6 | 2 31
| 16 22 77 48 30 | 6
esa uuuuu | -17 32 -53 -57 -6 | 19 30
| 10 7 67 52 5 | 3
gfz uuuuu | -25 6 -144 -65 0 | 6 24
| 17 12 51 85 5 | 3
grg uuuuu | -8 14 17 -36 5 | 0 22
| 11 8 69 42 4 | 4
igr xxxxx | 3 -5 45 14 1 | 5 23
| 8 9 40 42 3 | 4
irf xxxxx | -3 -7 -42 -8 -4 | 5 24
| 6 8 28 19 4 | 3
jgx uuuuu | 18 -13 31 -61 -3 | 8 24
| 11 9 38 25 4 | 3
jpl uuuuu | 17 -21 79 15 -2 | 7 24
| 17 14 31 63 19 | 6
mit uuuuu | 13 3 -194 31 4 | 22 32
| 8 11 31 97 3 | 4
ngs uuuuu | 8 1 141 77 4 | 12 24
| 40 20 143 75 7 | 3
sio xxxxx | 20 -76 -85 -79 2 | 29 32
| 50 41 74 50 12 | 8
Table 7.2339.0 GPS week: 2339 Day: 0 MJD: 60617.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 12 -7 137 66 -9 | -1 23
emr xxxxx | 25 -69 273 69 70 | -9 24
esa uuuuu | -20 33 -72 -93 -3 | 18 31
gfz uuuuu | -54 -8 -85 -229 2 | 2 26
grg uuuuu | -11 -3 65 -65 5 | -5 24
igr xxxxx | 11 -12 83 -50 6 | 1 24
irf xxxxx | 3 -7 -15 14 -2 | 2 25
jgx uuuuu | 31 0 81 -78 1 | 5 25
jpl uuuuu | 34 -19 139 52 9 | -1 26
mit uuuuu | 25 -8 -172 182 3 | 17 30
ngs uuuuu | -33 10 -114 76 -6 | 9 24
sio xxxxx | 11 -105 -116 -90 14 | 12 21
Table 7.2339.1 GPS week: 2339 Day: 1 MJD: 60618.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -6 -34 30 -85 -12 | 1 23
emr uuuux | 9 -14 148 194 -1 | 1 33
esa uuuuu | -31 23 -41 -2 -8 | 22 32
gfz uuuuu | -28 -4 -118 -78 -1 | 6 25
grg uuuuu | -4 14 -62 -14 3 | -1 23
igr xxxxx | -7 11 72 16 -1 | 5 24
irf xxxxx | -10 -3 -83 -6 -5 | 6 25
jgx uuuuu | 16 -21 3 -78 -2 | 9 25
jpl uuuuu | 9 -1 94 -70 10 | 4 26
mit uuuuu | 14 21 -243 42 6 | 20 31
ngs uuuuu | 24 17 170 132 4 | 11 24
sio xxxxx | -55 -33 51 -103 6 | 26 31
Table 7.2339.2 GPS week: 2339 Day: 2 MJD: 60619.500
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 | -33 4 148 -50 -3 | -2 24
emr uuuux | 17 -28 100 172 13 | 1 33
esa uuuuu | -15 37 -135 6 -10 | 21 32
gfz uuuuu | -41 -2 -161 -107 -6 | 6 25
grg uuuuu | -1 17 -4 -88 1 | -1 23
igr xxxxx | 9 -1 54 57 -2 | 5 24
irf xxxxx | -8 -17 -73 16 -9 | 5 25
jgx uuuuu | 9 -26 -4 -56 -7 | 8 25
jpl uuuuu | -3 -9 61 -79 17 | 5 26
mit uuuuu | 13 -6 -217 120 5 | 20 32
ngs uuuuu | 86 5 297 175 3 | 11 24
sio xxxxx | 1 -110 -120 -169 8 | 31 32
Table 7.2339.3 GPS week: 2339 Day: 3 MJD: 60620.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -9 -1 108 -54 1 | -5 23
emr uuuux | -19 -50 104 85 -4 | 0 33
esa uuuuu | -17 41 -118 -82 -6 | 16 29
gfz uuuuu | -11 8 -212 -35 -2 | 3 24
grg uuuuu | 0 16 -35 42 2 | -3 22
igr xxxxx | 6 0 -10 58 2 | 2 23
irf xxxxx | -1 -11 -49 -10 -1 | 2 24
jgx uuuuu | 34 -12 77 -13 -7 | 5 24
jpl uuuuu | 13 -23 57 20 4 | 3 24
mit uuuuu | 5 7 -216 44 8 | 18 30
ngs uuuuu | 14 12 296 4 1 | 9 22
sio xxxxx | 3 -118 -95 -69 -4 | 31 32
Table 7.2339.4 GPS week: 2339 Day: 4 MJD: 60621.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -8 -3 116 68 2 | -2 24
emr uuuux | -10 -28 53 116 -12 | 5 33
esa uuuuu | -16 34 -60 -105 -11 | 19 30
gfz uuuuu | -9 27 -98 -40 8 | 6 25
grg uuuuu | -12 13 -35 -31 6 | 1 23
igr xxxxx | -3 -15 -15 -31 3 | 7 25
irf xxxxx | 4 -14 -28 -14 -7 | 5 25
jgx uuuuu | 13 -7 25 -51 -7 | 9 25
jpl uuuuu | 20 -43 63 68 -8 | 10 24
mit uuuuu | 21 6 -169 -27 0 | 23 34
ngs uuuuu | 8 -6 137 14 6 | 12 25
sio xxxxx | 76 -98 -180 -47 -17 | 36 38
Table 7.2339.5 GPS week: 2339 Day: 5 MJD: 60622.500
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 -2 83 62 6 | 4 22
emr uuuux | 20 -25 93 135 -15 | 10 30
esa uuuuu | -21 21 -12 -109 -7 | 23 31
gfz uuuuu | -17 12 -207 0 -6 | 13 25
grg uuuuu | -31 19 60 -46 4 | 7 21
igr xxxxx | -6 -10 70 6 1 | 13 23
irf xxxxx | 0 -4 -12 -18 -10 | 10 23
jgx uuuuu | 7 -20 47 -63 -3 | 13 24
jpl uuuuu | 43 -33 87 61 -4 | 16 21
mit uuuuu | 8 11 -164 -95 2 | 29 35
ngs uuuuu | -22 9 50 146 4 | 18 26
sio xxxxx | 92 -54 -100 -10 -8 | 36 37
Table 7.2339.6 GPS week: 2339 Day: 6 MJD: 60623.500
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 -2 -70 56 -1 | -2 19
emr uuuux | 13 -1 46 82 -8 | 5 31
esa uuuuu | 2 32 65 -12 3 | 15 23
gfz uuuuu | -18 8 -127 32 5 | 6 20
grg uuuuu | 1 24 127 -49 14 | 2 18
igr xxxxx | 11 -8 61 42 -1 | 7 19
irf xxxxx | -11 9 -34 -40 2 | 3 20
jgx uuuuu | 13 -8 -13 -88 1 | 7 18
jpl uuuuu | 0 -19 52 54 -40 | 11 20
mit uuuuu | 2 -9 -178 -45 3 | 24 31
ngs uuuuu | -22 -42 150 -8 17 | 13 22
sio xxxxx | 9 -17 -35 -62 17 | 30 34
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