[IGSREPORT-30139] Wk 2335 IGS Final Orbits
acc
acc at igs.org
Fri Oct 25 05:55:52 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2335 (Oct 06, 2024 - Oct 12, 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_20242800000_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 | ALGO AREQ ASCG BAKE BHR4 BJFS BRAZ BRFT BRST BRUX
0 | COD | CAS1 CEDU CHUR CKIS COCO CPVG CRO1 CZTG DAEJ DARW
0 | COD | DAV1 DJIG DRAO FAIR FALK FLIN FLRS GAMB GODE GOLD
0 | COD | GRAC GUAM GUAT HOB2 HOFN HOLB HRAO INVK JOG2 KARR
0 | COD | KIRU KITG KOUG KOUR KRGG LPGS MAC1 MADR MAL2 MANA
0 | COD | MAS1 MATE MAW1 MAYG MCIL MDO1 MELI MGUE MKEA MOBS
0 | COD | MONP NANO NICO NIUM NKLG NLIB NNOR NYA2 OUS2 PIE1
0 | COD | POL2 POVE PTAG PTVL QAQ1 REUN REYK RIO2 SANT SAVO
0 | COD | SCH2 SCOR SEYG STHL STJ3 STK2 SUTH SUTM SVTL SYOG
0 | COD | TASH THTG TOW2 TRO1 TWTF ULAB UNSA URUM WARK WHIT
0 | COD | WIND WTZR XMIS YAR2 YEL2 YELL YKRO DGAR IRKJ
0 | EMR | BADG
0 | GFZ | LAUT LAUT
0 | GRG | IRKJ KIRI
0 | JGX | PIMO
0 | JPL | BADG IISC BADG CHTI CUSV FTNA IISC PGEN THU2
0 | MIT | MDVJ PDEL SFER TLSE TRO1 YAR3 YEL2 MDVJ PDEL SFER
0 | MIT | TLSE TRO1 YAR3 YEL2
1 | COD | BADG BAKE BRAZ MONP SGOC TWTF BRAZ TWTF
1 | ESA | FAIR JOG2 KIRU FAIR JOG2 KIRU
1 | GFZ | 5 5 LAUT LAUT MONP
1 | GRG | 13 CPVG CZTG CPVG CZTG KIRI
1 | JGX | SIN1
1 | JPL | CZTG SYOG BADG BAKE CHTI CPVG CZTG FTNA MAC1 SYOG
1 | MIT | BRST MDVJ NIUM SFER YEL2 BRST HERS MDVJ NIUM SFER
1 | MIT | YEL2
2 | COD | BAKE FLRS GUAT MAC1 MAL2 MGUE AREQ GUAT
2 | EMR | BADG
2 | ESA | MAL2 WHIT FLIN MAL2 WHIT
2 | GFZ | MAL2 POHN MAL2 MAS1 POHN
2 | GRG | 26 26 FAIR GMSD KIRI KIRU FAIR GMSD KIRI KIRU MGUE
2 | JPL | BADG CHTI FTNA BADG BAKE CHTI FAIR FTNA MAC1 SCH2
2 | JPL | SYOG
2 | MIT | MOBS MOBS
3 | COD | BJFS BOGT BRAZ CCJ2 CRO1 CUSV CZTG DARW DGAR DJIG
3 | COD | FAIR FALK FLIN FLRS GUAM GUAT HOLB JOG2 KOUR MADR
3 | COD | NANO POVE RIO2 SANT SGOC SVTL THTG THU2 TOW2 UNSA
3 | COD | VILL CZTG MATE NANO
3 | EMR | BADG BADG
3 | ESA | FAIR WHIT FAIR NRMD WHIT
3 | GFZ | LAUT LAUT
3 | GRG | CZTG CZTG FAIR KIRI
3 | JGX | NRMD SIN1
3 | JPL | BADG BADG CHTI GUAM NRMD
3 | MIT | GMSD MDVJ PDEL SFER TLSE YEL2 GMSD MDVJ PDEL SFER
3 | MIT | TLSE YEL2
4 | COD | BADG CPVG CRO1 DJIG FLRS KOUR MAW1 MAYG PDEL POL2
4 | COD | YELL MAYG
4 | ESA | AREQ CZTG AREQ CZTG NRMD SEYG
4 | GFZ | 13 LAUT BADG LAUT
4 | GRG | 13 13 ASCG CZTG MAYG POL2 SEYG ADIS CZTG FAIR FLIN
4 | GRG | KIRI MAYG NRMD POL2 SEYG
4 | JGX | ALBH BREW CEDU CZTG DAV1 GLSV HLFX NRC1 PALM STJ3
4 | JGX | SYOG ALBH BADG BREW CEDU CZTG DAV1 GODN HLFX KOUG
4 | JGX | NANO NRC1 PALM STJ3 SYOG UCAL
4 | JPL | CHTI FTNA MAW1 NRMD
4 | MIT | BRST IRKJ SFER STJO YAR3 BRST IRKJ SFER STJO YAR3
5 | COD | CZTG MATE
5 | ESA | FAIR FLIN FAIR FLIN NRMD
5 | GFZ | LAUT LAUT
5 | GRG | FAIR WARK FAIR KIRI NRMD
5 | JGX | BADG BREW DYNG FAA1 GLSV KIRI KIRU MAC1 NANO QAQ1
5 | JGX | SCH2 ALBH BREW GLSV HERS NANO OUS2 QAQ1 SCH2 UCAL
5 | JPL | CHTI MAC1 NRMD REYK
5 | MIT | ABPO ALBH BADG FALK FLRS KOUG MADR MGUE NYAL STJ3
5 | MIT | SVTL TLSE YELL ABPO ALBH BADG FALK FLRS HERS KOUG
5 | MIT | MADR MGUE NYAL STJ3 SVTL TLSE
6 | COD | DARW DAV1 FLRS GUAM GUAT MCIL DAV1 GUAT
6 | ESA | AREQ FAIR AREQ CUSV FAIR NRMD
6 | GFZ | LAUT AREQ LAUT
6 | GRG | AREQ SYOG AREQ BHR4 NRMD SYOG
6 | JGX | NRMD
6 | JPL | BADG CHTI FTNA
6 | MIT | ABPO NYAL ABPO GANP NYAL
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 | ~20:00 | ~ -0.13 ns
5 | COD | ~05:20 | ~ -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
----+--------+---------------
2 | GRG | 26
2 | JGX | 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 | 4 | 4 | 4 | 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 | .9 -.9 1.4 -17 22 -35 -.13
EMR | 0 | 2.8 2.3 -1.1 7 -10 15 -.24
ESA | 0 | .5 .0 .6 1 -11 -3 -.59
GFZ | 0 | .3 -1.4 -.1 -17 -16 -7 .15
GRG | 0 | -.1 -.1 -1.0 3 21 9 -.02
JGX | 0 | -2.1 3.9 1.5 10 16 3 -.26
JPL | 0 | .1 5.1 -3.3 18 -6 -8 -.11
MIT | 0 | -4.6 .4 24.2 2 8 -25 -.28
NGS | 0 | 1.1 7.7 12.2 23 19 -26 -.03
COD | 1 | .8 -1.5 1.1 -15 19 -25 -.24
EMR | 1 | 1.9 6.2 -3.7 6 -13 27 -.48
ESA | 1 | -.1 .0 .3 13 -17 -3 -.60
GFZ | 1 | .0 -1.0 -.4 12 -8 -17 .09
GRG | 1 | .2 .5 -1.1 26 9 5 -.16
JGX | 1 | -1.1 6.5 1.6 21 9 7 -.19
JPL | 1 | .5 6.5 -6.2 23 -11 -7 -.28
MIT | 1 | -2.4 1.3 22.9 17 8 0 -.45
NGS | 1 | -1.2 4.5 21.7 -18 46 -26 -.44
COD | 2 | 1.0 -2.0 1.0 -2 31 -28 -.02
EMR | 2 | 4.7 1.9 -2.5 9 -16 27 -.51
ESA | 2 | .4 -.4 .4 5 -15 -11 -.53
GFZ | 2 | -.2 -1.4 -.7 -14 -14 -2 .12
GRG | 2 | .1 -.5 -1.1 28 6 10 -.02
JGX | 2 | .9 2.7 2.7 10 6 12 -.14
JPL | 2 | 1.6 3.2 -9.5 30 2 -20 -.02
MIT | 2 | -4.3 4.0 16.6 25 4 -12 -.09
NGS | 2 | -4.1 5.4 9.7 -5 75 -66 -.39
COD | 3 | 1.6 -1.4 1.2 -1 29 -31 -.01
EMR | 3 | 2.8 .7 -3.0 10 -10 13 -.15
ESA | 3 | -.1 .3 .8 2 -24 4 -.67
GFZ | 3 | .6 -.5 -.1 -26 -7 2 -.01
GRG | 3 | .9 -1.1 -1.0 10 10 25 -.07
JGX | 3 | .9 -.8 3.1 -8 -2 20 -.15
JPL | 3 | 2.2 -.6 -6.2 18 -17 -12 .18
MIT | 3 | .4 2.3 21.8 36 -4 -14 -.23
NGS | 3 | .7 5.0 21.4 -13 29 -25 -.20
COD | 4 | 1.5 -1.4 1.0 2 -6 -32 .01
EMR | 4 | 2.0 3.1 -5.9 11 -7 10 -.10
ESA | 4 | -.1 -.5 -.2 1 -12 -20 -.43
GFZ | 4 | .6 -1.4 -.6 3 -16 -12 .38
GRG | 4 | .6 -1.3 -1.1 12 38 13 .09
JGX | 4 | -.7 2.5 3.1 2 19 -5 -.25
JPL | 4 | -3.8 1.7 -5.6 9 -12 -15 -.01
MIT | 4 | -5.5 -2.2 25.4 13 20 -26 -.12
NGS | 4 | -2.2 5.8 21.7 -21 55 -32 .19
COD | 5 | .6 -.8 1.1 -11 -13 -33 -.17
EMR | 5 | 2.8 3.0 -1.9 2 -11 17 -.21
ESA | 5 | -.1 .3 .9 -4 -21 -13 -.72
GFZ | 5 | .4 -1.2 -.0 -25 -14 4 .28
GRG | 5 | .3 -.9 -.8 12 29 3 -.06
JGX | 5 | 2.7 .5 2.3 -19 15 4 -.11
JPL | 5 | -4.2 4.9 -4.6 -11 -4 -5 -.11
MIT | 5 | -4.0 2.8 12.8 -28 2 -4 -.03
NGS | 5 | -1.7 5.6 6.6 11 19 -7 -.25
COD | 6 | .3 -1.5 .6 -6 7 -35 -.07
EMR | 6 | -.6 -.3 -3.9 8 -9 8 -.04
ESA | 6 | -.5 .5 .8 2 -13 -7 -.56
GFZ | 6 | -.0 -1.0 -.2 -14 -5 0 .29
GRG | 6 | .1 -1.1 -1.5 5 20 8 -.10
JGX | 6 | .1 2.1 3.3 5 15 16 -.08
JPL | 6 | -.3 .3 -4.4 17 -8 -4 .21
MIT | 6 | -1.0 1.3 18.6 31 1 -6 -.14
NGS | 6 | 2.2 5.2 16.8 -12 17 -23 -.22
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 1.2335.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2335.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 2.2335.[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 3.2335.[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 5.2335.0-6). 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 2335 summary. (Oct 06, 2024 - Oct 12, 2024)
Table 1.2335.a GPS week: 2335 MJD: 60589.000-60595.000
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 786| 0 0 4 -16 14 14 -.00 8 8 | -645 112 6 99
| 0 0 0 7 11 12 .02 | 198 284
emr 110| 0 0 -2 0 5 -3 .04 9 9 | -1456 921 31 99
| 0 1 1 14 9 17 .03 | 797 1467
esa 150| 0 0 3 -19 -7 3 -.03 8 8 | -719 -214 7 74
| 0 0 1 11 9 9 .02 | 266 337
gfz 127| 1 0 2 37 14 -30 .04 10 11 | -15 -87 11 127
| 1 0 1 18 15 20 .03 | 115 194
grg 122| 0 0 -1 -3 7 2 -.02 12 8 | -3 -3 7 125
| 0 1 2 6 13 11 .01 | 54 128
igr n/a| 0 0 0 -2 -4 7 .00 3 3 | -767 591 9 71
| 0 0 0 15 8 12 .01 | 1929 705
jgx n/a| 0 0 2 -9 -14 -7 -.07 10 10 | -142835 -142897 41 1348
| 0 0 1 11 10 16 .01 | 377973 377946
jpl 120| -1 0 0 16 -11 8 .05 9 9 | -1070 -40 6 64
| 0 0 0 12 7 10 .02 | 655 735
mit 359| 0 0 -9 -2 -6 10 -.00 9 9 | 7888 -16780 53 75
| 0 0 2 33 28 44 .02 | 24129 47025
ngs 274| 0 0 1 16 -15 -3 -.07 12 12 | 4478 -2088 515 722
| 1 0 5 19 26 25 .04 | 8840 5769
Table 1.2335.b GPS week : 2335 MJD: 60589.000-60595.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 7 13 --- --- --- --- --- |
2 | 3 4 4 3 4 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 3 3 4 4 4 4 4 |
5 | 3 3 3 3 3 3 3 |
6 | 3 3 3 4 4 3 3 |
7 | 4 4 3 3 3 3 3 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 4 3 3 |
10 | 4 3 3 3 3 3 3 |
11 | 4 4 4 5 5 4 4 |
12 | 3 3 3 4 4 3 3 |
13 | 3 4 3 3 3 3 3 |
14 | 3 4 4 4 4 4 4 |
15 | 3 3 3 3 3 3 3 |
16 | 3 4 3 3 4 4 4 |
17 | 2 3 3 3 3 3 3 |
18 | 4 5 4 4 5 4 4 |
19 | 3 3 3 3 3 3 3 |
20 | 3 3 3 3 4 3 4 |
21 | 4 4 4 3 4 4 4 |
22 | 3 3 3 3 3 3 3 |
23 | 3 3 3 3 4 3 3 |
24 | 4 3 3 3 4 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 7 3 4 3 3 |
27 | 3 3 3 3 3 3 3 |
28 | 4 4 4 4 4 4 4 |
29 | 3 3 3 4 4 3 3 |
30 | 4 3 3 3 3 4 3 |
31 | 3 4 4 3 4 4 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 2.2335.0 GPS week: 2335 Day: 0 MJD: 60589.000
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 789| 0 0 6 -9 12 8 -.03 8 8 | -384 -35 7 92
emr 108| 0 0 0 -22 17 -8 .05 8 8 | -2271 2983 27 109
esa 150| 0 -1 0 -21 -4 10 -.00 8 8 | -1216 -115 9 79
gfz 128| 0 0 5 32 22 0 .01 10 11 | -192 227 12 127
grg 125| 1 0 0 -16 21 -5 -.03 8 8 | -26 -63 8 116
igr n/a| 0 0 0 -8 -17 11 .01 3 3 | -4050 1369 10 73
jgx n/a| -1 0 1 -21 -20 9 -.09 10 10 | -37 -38 32 98
jpl 120| -1 0 0 13 -5 14 .04 8 8 | -2221 801 7 75
mit 359| 1 0 -13 38 -49 -36 .02 9 9 | -4025 1319 63 80
ngs 274| -2 0 1 38 -19 17 -.08 11 11 | 15297 53 578 784
Table 2.2335.1 GPS week: 2335 Day: 1 MJD: 60590.000
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 791| 0 0 4 -21 6 6 -.02 8 8 | -843 301 7 95
emr 111| 0 0 -4 7 6 -8 .07 9 9 | -1278 596 30 96
esa 150| 0 -1 3 -11 -8 17 -.05 8 8 | -771 -217 7 83
gfz 129| 1 0 1 67 8 -29 .03 9 10 | 61 -173 12 122
grg 126| 0 0 2 -3 13 -12 -.03 8 8 | -16 44 8 116
igr n/a| 0 0 -1 2 -14 19 .02 3 3 | -2509 1197 11 63
jgx n/a| -1 0 1 -4 -15 -9 -.06 10 10 | 5 3 34 104
jpl 120| -2 0 0 33 -9 16 .05 9 9 | -1425 657 7 72
mit 359| 0 0 -11 -54 -8 7 -.01 9 9 | -3385 2955 58 81
ngs 269| 0 0 2 -9 0 10 -.05 12 12 | 19316 -15159 444 619
Table 2.2335.2 GPS week: 2335 Day: 2 MJD: 60591.000
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 789| -1 0 4 -19 15 28 .01 7 7 | -635 24 6 93
emr 112| 0 -2 -2 -2 3 22 .08 10 10 | -2738 2679 32 106
esa 150| 0 0 4 -27 0 -7 -.03 8 8 | -402 -802 7 72
gfz 128| 1 0 4 25 -10 -55 .07 10 10 | -100 91 12 126
grg 122| 1 0 -2 0 3 0 -.04 36 8 | -16 96 7 105
igr n/a| 0 0 0 -10 0 0 .02 3 3 | -1308 1246 10 74
jgx n/a| 0 0 1 2 -24 -34 -.07 14 14 | -999999 -999999 32 96
jpl 120| -2 0 0 21 -5 0 .09 10 10 | -761 509 7 60
mit 359| 0 0 -9 17 -10 27 -.01 10 9 | -1036 698 48 75
ngs 277| -1 1 -1 3 2 2 -.09 10 10 | -634 21 470 701
Table 2.2335.3 GPS week: 2335 Day: 3 MJD: 60592.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 785| 0 0 3 -15 36 6 .03 7 7 | -944 649 7 94
emr 113| 0 -1 -3 16 -11 -28 .04 9 9 | -1273 -11 34 100
esa 150| 0 0 1 -26 -10 1 -.04 9 8 | -799 -171 8 73
gfz 125| 1 1 0 28 3 -51 .00 10 10 | 146 -342 11 133
grg 123| 1 0 0 2 -7 17 -.03 7 7 | 40 -114 8 141
igr n/a| 0 0 0 -7 -1 -13 .01 3 3 | 70 560 9 61
jgx n/a| 0 0 1 -24 -28 -9 -.06 9 9 | 41 -85 27 90
jpl 120| -1 1 0 22 -18 -9 .06 8 8 | -111 -51 7 61
mit 359| 0 0 -10 4 24 92 .01 10 10 | -58 819 55 68
ngs 273| -1 0 5 9 0 -27 -.09 12 12 | -912 625 510 736
Table 2.2335.4 GPS week: 2335 Day: 4 MJD: 60593.000
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 1 4 -4 0 8 .01 8 8 | -640 28 7 106
emr 106| 0 0 -3 -11 15 16 .01 11 10 | -701 -303 32 86
esa 150| 0 0 4 -30 8 -8 -.04 9 9 | -462 -421 7 75
gfz 126| 4 0 0 55 35 -26 .07 12 12 | 22 -184 12 121
grg 121| 0 -2 -1 -3 25 -5 -.00 8 8 | 99 -212 8 139
igr n/a| 0 0 0 0 1 7 -.01 4 4 | 683 308 10 74
jgx n/a| 0 0 0 -18 -10 5 -.05 11 11 | 149 -283 97 6711
jpl 120| -1 0 -1 15 -23 9 .02 9 9 | -820 -305 6 61
mit 359| 0 0 -9 1 -29 24 -.03 10 10 | 756 161 55 76
ngs 273| 0 1 8 3 -47 -43 -.00 14 13 | -640 26 575 737
Table 2.2335.5 GPS week: 2335 Day: 5 MJD: 60594.000
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 782| 0 0 4 -12 19 35 .00 7 7 | -447 -237 6 115
emr 108| 0 0 0 18 7 -6 .02 9 9 | -525 -801 32 98
esa 150| 0 -1 3 2 -17 9 -.05 8 8 | -674 300 7 74
gfz 126| 1 0 2 39 17 -12 .05 10 10 | -88 -31 10 134
grg 121| 0 0 -3 3 -5 7 -.01 8 7 | -48 133 7 132
igr n/a| 0 0 0 27 1 22 -.01 3 3 | 1040 -166 9 88
jgx n/a| 0 0 3 -1 1 -22 -.06 9 9 | 19 45 41 2257
jpl 120| -1 0 -1 -7 -14 19 .05 9 9 | -927 -814 7 64
mit 359| 0 1 -5 -41 0 -39 -.01 9 9 | 62444 -123402 41 81
ngs 276| 0 0 -7 39 10 28 -.09 15 15 | -452 -234 530 711
Table 2.2335.6 GPS week: 2335 Day: 6 MJD: 60595.000
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 787| 0 0 5 -28 11 5 -.00 8 8 | -627 56 7 98
emr 116| 0 -1 -2 -1 -1 -13 .04 9 9 | -1406 1305 30 98
esa 150| 0 0 3 -23 -20 2 .00 8 8 | -715 -76 7 64
gfz 127| 1 0 3 12 24 -40 .05 11 12 | 41 -200 11 129
grg 119| 0 1 -3 -6 -1 15 -.02 9 8 | -56 91 8 128
igr n/a| 0 0 0 -20 0 7 -.01 4 4 | 701 -374 10 66
jgx n/a| 0 0 3 0 -6 5 -.08 9 9 | -29 76 28 84
jpl 120| -1 1 -1 17 -2 7 .02 8 8 | -1230 -1078 6 59
mit 359| 0 0 -9 16 29 -3 -.00 8 8 | 521 -14 53 70
ngs 278| 2 0 0 30 -55 -9 -.11 11 11 | -625 47 501 770
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 3.2335.0 GPS week: 2335 Day: 0 MJD: 60589.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 11 --- --- --- 12 15 --- --- 10 13 6 | 29 --- --- --- 20 22 --- --- 22 22 22
2 | 7 7 8 12 7 3 9 8 13 14 3 | 29 28 31 32 28 29 31 27 33 30 29
3 | 8 6 9 12 6 3 6 7 10 11 3 | 40 40 39 40 38 38 36 40 39 38 39
4 | 6 10 6 10 8 2 7 11 8 9 3 | 21 21 24 21 22 22 21 24 25 22 21
5 | 8 6 6 8 8 2 11 8 9 8 3 | 38 34 37 38 38 38 36 36 39 39 37
6E | 7 10 7 8 7 2 9 7 9 11 3 | 26 26 26 24 25 25 25 25 24 26 24
7 | 12 8 7 7 9 2 11 8 8 14 3 | 31 24 26 25 28 26 26 26 28 29 26
8 | 6 7 8 8 4 2 8 6 10 13 2 | 34 35 35 37 35 35 33 37 37 37 35
9 | 8 10 6 10 5 4 5 7 7 12 2 | 47 46 44 44 44 44 44 47 45 42 44
10 | 14 11 9 12 9 4 8 8 9 10 3 | 40 41 41 39 41 39 39 40 39 40 39
X11E | 9 14 10 12 9 4 --- 10 12 13 4 | 30 31 36 35 33 32 --- 36 34 28 32
12 | 7 7 6 7 9 3 12 7 8 10 3 | 24 26 24 26 24 25 23 25 25 26 24
13 | 6 8 6 10 7 4 9 8 10 11 3 | 30 32 30 28 34 30 31 33 32 29 30
14 | 7 8 13 12 7 2 6 8 8 10 3 | 55 56 58 53 55 56 56 58 54 61 56
15 | 6 6 5 7 6 2 8 5 11 6 2 | 54 52 53 52 53 53 54 53 52 54 53
16 | 8 7 5 11 12 3 12 9 6 11 3 | 33 32 33 35 35 33 32 32 32 35 32
17 | 5 6 4 7 5 3 7 6 8 7 2 | 35 37 33 34 33 35 34 35 34 38 34
18E | 9 11 13 8 8 3 11 14 13 13 4 | 29 36 36 32 34 32 33 37 33 27 32
19 | 5 7 5 9 7 2 11 6 8 15 3 | 38 38 36 34 37 36 34 37 36 42 36
20 | 7 7 8 10 10 2 13 7 8 9 3 | 30 26 27 27 30 28 29 27 30 29 27
21 | 7 7 7 10 7 3 17 9 12 11 3 | 23 22 25 27 23 24 24 22 29 25 23
22 | 5 6 6 8 7 2 8 5 7 8 2 | 33 34 33 32 32 33 33 34 31 37 33
23 | 7 10 8 9 9 3 11 7 7 10 3 | 49 50 51 51 53 51 50 52 55 51 51
24 | 11 7 10 21 9 3 8 7 12 10 4 | 30 26 31 29 29 27 26 28 27 28 27
25 | 6 10 9 11 8 4 7 7 7 10 3 | 28 33 32 29 30 29 29 31 27 29 29
26 | 7 7 8 10 8 2 7 7 9 13 3 | 292 292 295 292 296 292 290 293 294 294 293
27 | 7 9 8 10 6 4 5 7 9 12 3 | 35 36 37 38 35 36 35 38 36 38 36
28 | 11 9 17 11 8 3 10 13 9 11 4 | 34 40 46 39 40 40 39 43 37 36 39
29 | 6 7 6 8 8 5 11 6 8 10 2 | 26 22 24 23 24 25 23 23 25 28 24
30 | 11 9 9 14 13 3 8 9 6 9 3 | 35 29 33 30 30 30 30 31 30 30 30
31 | 8 7 7 12 8 2 12 8 10 11 3 | 35 33 32 37 33 34 34 32 33 35 33
32 | 6 8 8 10 5 2 8 7 9 13 3 | 38 41 40 38 36 38 37 41 37 37 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 8 8 10 8 3 10 8 9 11 |T 42 42 43 42 42 41 42 43 42 42 41
WRMS | 8 8 8 11 8 3 10 8 9 11 |NE 43 43 44 43 43 43 43 44 43 44 42
MEDI | 7 7 8 10 8 3 8 7 9 11 |MD 33 34 33 34 33 33 33 35 33 35 32
Table 3.2335.1 GPS week: 2335 Day: 1 MJD: 60590.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 26 --- --- --- 8 23 --- --- 13 36 12 | 29 --- --- --- 21 21 --- --- 21 20 22
2 | 7 10 8 7 8 3 10 12 13 12 3 | 41 40 39 45 42 42 39 40 44 43 41
3 | 8 8 9 9 8 3 6 9 8 14 3 | 52 53 54 53 51 53 52 52 52 57 52
4 | 9 13 5 10 7 3 8 12 10 11 3 | 29 29 31 33 30 31 30 31 32 31 30
5 | 8 9 5 6 7 4 9 8 9 8 2 | 55 53 55 56 55 56 53 54 55 53 54
6E | 9 10 8 9 7 4 8 7 11 12 3 | 46 46 48 46 46 47 46 47 48 47 46
7 | 10 10 7 15 11 4 12 11 11 13 4 | 47 44 44 46 46 45 45 43 44 48 44
8 | 6 7 8 9 4 3 10 9 8 13 3 | 41 41 41 43 41 43 39 43 40 42 41
9 | 9 14 7 6 6 4 6 10 10 13 3 | 48 49 48 49 47 47 47 50 48 47 48
10 | 7 7 8 10 8 3 7 6 8 8 2 | 52 56 57 55 54 55 54 56 54 52 54
X11E | 9 14 12 8 9 4 --- 11 11 14 4 | 24 26 33 30 30 28 --- 32 28 23 27
12 | 6 9 6 7 10 3 14 9 8 11 3 | 39 41 39 41 41 40 41 39 41 37 39
13 | 8 11 7 8 15 3 11 9 11 11 3 | 42 45 46 43 55 45 46 47 47 44 46
14 | 8 11 14 13 8 2 7 10 6 15 3 | 55 60 58 58 59 58 57 57 57 61 57
15 | 6 9 4 6 7 3 8 4 11 9 2 | 46 47 46 45 46 48 47 46 47 45 46
16 | 9 9 5 8 11 3 11 10 7 16 3 | 50 49 51 55 51 52 50 50 50 57 51
17 | 5 11 5 8 6 3 9 7 7 10 2 | 40 43 40 42 38 42 41 42 40 43 40
18E | 9 11 13 11 10 4 12 16 16 16 4 | 22 27 28 26 27 25 24 30 28 25 25
19 | 5 10 5 11 7 3 11 6 8 14 3 | 42 43 43 42 41 44 43 43 42 46 42
20 | 7 7 8 11 10 3 12 8 8 9 3 | 47 44 46 48 47 46 44 45 44 42 45
21 | 8 8 7 11 8 3 14 12 12 15 3 | 35 36 34 38 36 36 32 36 40 39 35
22 | 7 9 7 12 8 3 8 8 7 11 3 | 46 49 50 45 47 48 48 47 46 48 47
23 | 7 10 7 9 9 3 10 8 7 12 3 | 53 58 60 58 57 57 57 61 60 55 57
24 | 10 10 9 10 8 4 7 8 10 11 3 | 44 44 49 45 48 45 44 45 43 41 44
25 | 6 9 8 7 9 3 7 9 8 11 3 | 42 46 45 43 45 44 43 46 40 41 43
26 | 9 8 9 12 7 4 7 9 9 12 3 | 353 353 352 355 357 352 349 352 352 353 353
27 | 7 9 8 10 4 2 9 7 8 10 2 | 43 43 45 49 43 45 44 46 41 45 44
28 | 11 9 16 8 7 3 11 12 9 13 4 | 55 54 59 58 57 57 58 58 56 58 56
29 | 7 6 5 7 9 4 11 8 9 10 2 | 36 33 33 34 33 35 36 34 36 35 34
30 | 10 10 8 8 12 4 6 8 7 10 3 | 46 46 45 43 48 45 43 45 42 39 44
31 | 9 8 6 12 10 3 16 10 10 12 3 | 54 51 53 57 54 53 55 52 51 57 53
32 | 10 8 7 8 7 3 9 9 9 11 3 | 43 48 49 48 44 46 44 49 44 45 46
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 9 8 9 8 3 10 9 9 12 |T 53 54 55 55 54 54 55 55 53 53 53
WRMS | 8 9 8 10 8 3 10 9 9 12 |NE 55 57 57 58 56 56 56 57 55 56 55
MEDI | 8 9 7 9 8 3 9 9 9 12 |MD 44 46 46 45 46 45 44 46 44 45 44
Table 3.2335.2 GPS week: 2335 Day: 2 MJD: 60591.000
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 10 7 12 7 3 10 12 17 11 3 | 34 36 34 35 35 34 35 35 39 42 35
3 | 7 6 10 9 5 4 8 10 11 10 3 | 53 55 53 52 51 50 50 53 50 53 52
4 | 7 11 6 11 6 3 7 13 10 13 3 | 23 24 22 28 26 22 21 20 28 26 23
5 | 7 7 7 7 8 3 10 9 8 8 2 | 55 52 50 51 51 50 50 51 51 54 51
6E | 8 9 8 6 8 3 7 8 11 8 3 | 37 36 35 36 37 35 34 36 37 37 35
7 | 8 9 6 12 8 3 8 11 9 12 3 | 41 39 39 41 42 40 38 40 41 45 40
8 | 5 10 9 8 4 1 8 9 11 8 2 | 38 43 40 39 38 39 38 42 40 42 39
9 | 7 11 7 9 6 3 6 9 8 13 3 | 51 53 51 49 50 50 46 54 51 54 50
10 | 9 9 9 9 4 2 5 7 8 8 2 | 53 52 51 48 52 51 50 51 52 56 51
X11E | 9 15 12 10 9 6 --- 11 9 12 4 | 27 29 33 34 30 27 --- 33 30 28 29
12 | 6 9 6 7 10 4 11 10 7 12 3 | 41 40 38 40 42 39 37 39 40 41 39
13 | 7 10 5 10 6 3 8 10 10 8 3 | 39 42 38 37 35 39 36 43 39 40 38
14 | 7 11 14 13 7 2 8 9 7 11 3 | 48 49 52 44 48 47 47 50 47 47 47
15 | 7 6 4 6 7 2 7 6 9 11 2 | 47 48 46 45 47 46 45 47 45 47 46
16 | 9 11 4 7 10 4 14 11 8 7 3 | 42 41 41 42 39 40 41 41 39 41 40
17 | 5 9 5 8 6 3 6 7 8 9 2 | 39 40 37 38 37 39 37 40 38 44 38
18E | 8 12 14 8 8 3 13 15 11 13 4 | 27 26 31 27 30 28 29 33 27 28 27
19 | 6 8 5 9 6 2 12 7 8 10 2 | 44 43 42 44 41 42 39 43 44 48 42
20 | 6 8 7 12 8 3 10 9 8 9 3 | 43 41 40 42 41 41 39 41 42 41 41
21 | 7 9 6 9 7 3 12 12 13 11 3 | 35 37 33 33 37 35 32 36 40 42 35
22 | 6 8 7 6 9 2 7 8 7 8 2 | 46 49 47 45 46 46 44 48 46 51 46
23 | 7 8 8 7 9 3 8 9 9 11 3 | 53 49 51 47 54 51 51 50 53 53 51
24 | 11 8 9 8 8 4 8 9 9 11 3 | 44 41 43 39 41 40 37 40 38 40 40
25 | 7 9 8 10 7 4 6 10 8 10 3 | 38 41 38 36 40 36 36 39 37 40 37
26 | 11 22 14 14 193 6 59 20 14 12 6 | 837 837 839 839 810 837 820 836 837 836 838
27 | 5 9 8 9 4 3 8 7 8 6 2 | 41 43 40 41 39 41 41 43 40 44 41
28 | 8 8 16 13 8 2 8 11 9 15 4 | 42 47 47 43 46 43 42 47 45 47 44
29 | 7 6 6 8 9 4 10 8 11 8 3 | 34 32 30 31 33 31 30 30 32 35 31
30 | 8 9 9 12 9 4 6 7 9 9 3 | 56 56 58 53 56 55 52 56 55 48 55
31 | 8 8 6 17 10 4 13 10 10 15 4 | 47 48 45 52 45 46 45 47 48 48 46
32 | 6 9 7 10 5 2 7 8 7 11 2 | 42 45 43 44 42 41 38 45 40 42 42
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 10 8 10 36 3 14 10 10 10 |T 67 68 67 66 66 66 66 68 67 69 66
WRMS | 7 10 8 10 8 3 14 10 9 10 |NE 71 72 71 70 70 70 68 71 71 73 70
MEDI | 7 9 7 9 8 3 8 9 9 11 |MD 42 43 41 42 41 41 39 43 40 44 41
Table 3.2335.3 GPS week: 2335 Day: 3 MJD: 60592.000
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 | 4 9 8 11 6 4 9 9 12 13 3 | 40 42 40 42 39 39 42 39 40 44 40
3 | 6 7 10 10 7 3 7 7 12 9 3 | 37 37 38 36 34 37 36 37 31 38 35
4 | 9 13 6 14 6 3 7 13 9 11 3 | 40 43 44 50 44 44 44 43 40 45 42
5 | 6 8 9 10 7 4 11 9 12 10 3 | 41 41 40 42 40 41 39 39 38 42 39
6E | 7 12 9 9 11 2 9 7 10 13 3 | 39 40 41 39 40 39 38 39 35 38 38
7 | 7 8 7 11 8 3 11 8 9 9 3 | 41 38 38 39 39 40 42 38 37 43 38
8 | 5 8 9 11 5 2 6 7 8 12 2 | 38 40 37 37 34 37 37 38 34 41 36
9 | 9 14 8 9 6 5 7 7 10 15 3 | 36 40 37 37 34 37 35 39 31 35 35
10 | 11 7 9 10 6 2 7 7 8 7 3 | 39 39 40 40 39 39 39 39 33 41 38
X11E | 10 16 10 15 9 5 --- 10 10 17 4 | 38 40 43 45 40 40 --- 43 34 37 39
12 | 6 9 8 9 8 4 14 7 11 13 3 | 40 41 39 41 39 40 41 40 38 39 39
13 | 6 10 7 10 5 2 9 7 13 10 3 | 39 41 39 37 39 38 39 42 34 42 38
14 | 9 9 13 17 7 3 8 9 8 16 3 | 41 44 48 38 42 44 43 47 40 49 43
15 | 7 8 6 7 7 2 7 4 9 11 2 | 49 51 48 48 46 48 47 48 42 51 47
16 | 8 10 6 10 11 3 11 9 7 8 3 | 41 41 39 42 41 40 39 39 37 43 39
17 | 5 7 6 10 6 3 7 5 7 9 2 | 38 40 39 41 36 40 38 40 35 38 38
18E | 8 11 13 11 10 4 11 14 13 18 4 | 39 40 41 40 42 38 38 42 35 42 39
19 | 4 6 6 10 6 3 11 5 8 11 2 | 38 38 40 40 36 39 37 40 35 37 37
20 | 7 10 7 9 8 2 11 9 9 15 3 | 38 39 38 37 37 37 36 37 34 34 36
21 | 6 10 8 10 7 4 11 9 12 10 3 | 37 41 37 38 37 36 39 37 37 40 37
22 | 6 6 7 9 7 3 7 6 9 15 2 | 39 40 40 39 37 39 37 41 33 40 38
23 | 7 10 8 9 9 3 8 8 8 9 3 | 39 39 41 40 41 39 40 39 38 40 39
24 | 8 10 10 8 6 2 6 7 10 12 3 | 39 39 39 33 37 37 35 37 32 35 36
25 | 6 10 11 8 5 3 6 9 7 12 3 | 39 41 40 40 39 39 37 40 35 41 38
26 | 8 8 8 11 8 3 9 7 9 11 3 | 597 598 597 598 593 596 596 597 595 597 596
27 | 6 9 8 10 5 3 6 6 8 8 2 | 39 40 39 39 37 39 39 40 33 42 38
28 | 9 10 13 9 8 3 10 12 10 11 3 | 38 42 44 48 42 41 41 45 40 41 41
29 | 5 9 8 9 9 5 13 8 12 14 3 | 39 39 36 39 38 38 38 37 39 40 37
30 | 9 9 9 9 10 2 7 8 7 10 3 | 42 39 42 38 39 41 39 40 34 55 39
31 | 8 9 7 8 7 2 13 8 10 11 3 | 37 36 34 39 36 37 37 35 33 37 35
32 | 5 9 8 9 5 3 7 9 10 9 2 | 33 38 37 39 34 35 35 39 30 38 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 9 10 7 3 9 8 10 12 |T 57 58 57 58 56 57 57 57 53 58 56
WRMS | 7 9 8 10 7 3 9 8 10 12 |NE 59 60 59 59 58 59 58 59 55 61 58
MEDI | 7 9 8 10 7 3 8 8 9 11 |MD 39 40 40 39 39 39 39 39 35 41 38
Table 3.2335.4 GPS week: 2335 Day: 4 MJD: 60593.000
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 | 6 10 10 11 7 4 13 12 12 20 4 | 30 30 29 34 32 31 29 30 34 42 31
3 | 7 9 10 9 8 4 8 8 10 9 3 | 45 49 46 45 45 43 42 46 43 48 45
4 | 8 14 8 13 7 4 10 14 11 9 3 | 32 35 34 38 36 34 32 35 36 39 33
5 | 8 7 7 9 7 3 13 8 11 15 3 | 50 44 49 49 50 48 46 47 48 51 48
6E | 8 14 9 10 9 4 8 9 9 12 3 | 42 43 42 42 44 42 39 39 42 44 41
7 | 7 8 9 9 8 3 11 8 9 14 3 | 36 37 34 38 37 37 35 35 36 44 36
8 | 6 9 11 12 5 5 10 7 9 12 3 | 35 36 36 39 35 37 33 38 33 37 35
9 | 7 16 7 9 6 4 12 8 10 11 3 | 45 48 44 41 44 44 42 45 42 48 44
10 | 7 11 10 13 7 4 9 8 7 12 3 | 51 47 52 48 51 50 48 51 49 57 50
X11E | 11 17 10 22 9 5 --- 9 11 18 5 | 30 30 34 43 33 32 --- 32 29 32 31
12 | 8 9 7 12 10 4 15 9 9 16 3 | 39 35 38 40 39 37 35 36 39 42 37
13 | 7 10 7 11 8 4 11 9 9 15 3 | 37 40 37 38 42 38 37 41 39 39 38
14 | 9 11 13 20 7 2 7 9 9 20 4 | 44 45 48 44 44 45 43 46 43 52 44
15 | 6 7 5 10 5 2 9 5 9 13 2 | 47 43 47 48 48 47 43 46 45 49 46
16 | 9 11 6 13 11 5 13 11 10 11 3 | 36 34 36 40 35 36 34 37 36 40 35
17 | 6 10 7 12 7 4 7 7 9 12 3 | 36 39 35 36 32 37 33 36 34 39 35
18E | 9 12 13 15 11 4 9 14 14 20 4 | 27 27 31 26 34 28 27 34 27 34 28
19 | 5 11 8 11 8 3 10 7 11 13 3 | 41 41 39 40 37 39 36 37 40 40 39
20 | 8 7 9 11 8 2 15 8 9 20 3 | 40 37 38 38 40 38 36 37 39 44 38
21 | 6 10 8 11 7 6 16 10 12 18 3 | 32 32 30 31 34 32 29 31 35 41 31
22 | 7 6 8 10 7 3 8 7 9 14 3 | 40 39 41 40 38 39 37 39 39 45 39
23 | 7 12 9 12 10 4 12 9 9 13 3 | 50 45 52 47 53 50 52 52 52 50 50
24 | 11 12 9 10 10 3 7 8 9 15 3 | 38 36 42 36 40 38 36 39 37 45 38
25 | 6 12 10 11 6 3 10 9 10 14 3 | 38 34 39 38 39 37 35 39 35 44 37
26 | 9 13 10 14 9 4 11 8 10 13 3 | 555 558 555 554 555 555 554 555 558 551 555
27 | 7 10 9 11 6 4 8 8 8 9 3 | 40 44 41 46 41 43 42 46 42 46 42
28 | 9 10 14 16 9 3 13 13 9 14 4 | 42 42 48 41 47 43 43 46 41 43 43
29 | 10 8 7 11 9 4 10 7 10 15 3 | 36 28 32 31 33 31 30 31 30 37 31
X30 | 8 9 10 9 10 3 7 8 8 --- 3 | 44 43 46 42 44 43 41 42 43 --- 43
31 | 8 10 7 15 12 3 16 9 9 14 4 | 43 43 42 46 44 43 43 42 42 49 43
32 | 7 10 8 12 7 3 11 7 10 9 3 | 43 41 43 42 43 40 38 44 42 46 42
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 11 9 12 8 4 11 9 10 14 |T 56 55 56 56 57 56 55 56 55 60 55
WRMS | 8 10 9 12 8 4 11 9 10 13 |NE 58 58 59 58 59 58 56 58 58 63 58
MEDI | 7 10 9 11 8 4 10 8 9 14 |MD 40 40 41 40 40 39 37 39 39 44 39
Table 3.2335.5 GPS week: 2335 Day: 5 MJD: 60594.000
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 8 9 8 8 3 11 10 12 12 3 | 19 17 19 19 17 18 21 18 20 25 17
3 | 8 9 11 6 8 3 7 8 12 15 3 | 28 32 31 30 28 29 31 30 32 31 29
4 | 9 14 5 10 9 2 7 15 10 7 3 | 21 22 21 26 25 22 22 24 22 24 21
5 | 8 7 6 11 9 2 9 9 7 10 3 | 25 22 21 26 23 22 22 20 26 21 22
6E | 7 9 8 11 8 4 10 9 11 11 3 | 63 67 64 66 62 65 67 65 69 65 65
7 | 8 9 8 12 8 4 10 10 8 11 3 | 23 19 18 26 21 20 22 18 19 20 19
8 | 5 8 8 9 5 2 8 7 11 8 2 | 29 31 29 30 29 28 29 32 32 28 29
9 | 10 12 7 9 5 4 6 8 11 16 3 | 33 37 31 34 30 31 32 36 34 28 32
10 | 6 8 9 11 8 3 9 7 6 13 3 | 26 26 24 20 24 23 22 25 27 25 23
X11E | 9 16 10 13 11 5 --- 9 8 15 4 | 26 26 32 32 32 27 --- 30 25 23 27
12 | 5 7 5 7 10 2 12 11 8 10 3 | 23 24 21 24 22 23 21 23 22 26 22
13 | 4 9 6 9 6 3 9 9 10 15 3 | 19 23 20 17 20 19 18 24 21 21 19
14 | 8 10 13 15 7 3 8 9 6 14 3 | 40 43 45 42 42 43 41 41 42 39 41
15 | 5 6 4 7 6 2 8 6 9 11 2 | 28 27 26 28 26 28 25 27 31 25 27
16 | 10 8 6 11 8 2 14 10 6 17 3 | 19 19 18 25 18 18 20 17 20 20 18
17 | 6 8 6 7 6 3 8 8 8 12 2 | 26 28 24 28 22 26 24 28 25 29 25
18E | 8 12 13 14 8 3 11 15 10 16 4 | 27 30 31 28 33 28 29 34 25 30 29
19 | 6 9 6 9 8 3 10 7 10 14 3 | 27 27 25 26 23 25 24 27 26 32 25
20 | 6 9 8 12 9 3 7 11 8 13 3 | 20 18 17 22 19 17 17 17 21 17 17
21 | 7 8 7 8 8 4 11 10 13 15 3 | 20 19 19 20 18 18 19 19 23 26 18
22 | 7 7 7 9 10 3 7 6 9 14 3 | 24 23 22 26 19 22 20 21 23 26 21
23 | 6 10 8 11 10 2 8 8 10 13 3 | 20 24 25 24 28 23 23 25 29 23 23
24 | 8 9 9 9 7 3 6 9 8 15 3 | 25 22 25 23 24 22 19 24 19 25 22
25 | 6 9 10 9 8 3 9 8 7 11 3 | 19 21 22 20 21 19 16 23 17 20 19
26 | 6 10 9 10 8 3 8 9 10 14 3 | 547 547 546 549 544 547 542 547 538 545 545
27 | 6 8 8 9 4 3 6 8 8 24 3 | 26 26 26 25 25 25 25 29 26 34 25
28 | 8 8 13 8 7 2 7 13 9 18 3 | 29 31 35 31 34 32 30 36 32 37 32
29 | 6 6 5 10 8 3 10 8 9 12 2 | 23 21 21 24 19 21 18 21 20 21 20
X30 | 8 10 9 9 11 4 9 7 6 --- 3 | 25 21 25 23 24 22 19 23 21 --- 21
31 | 9 11 5 9 8 2 11 8 10 38 4 | 26 28 26 29 27 26 29 28 31 40 27
32 | 5 9 6 8 4 3 7 9 7 12 2 | 25 30 27 27 21 24 23 31 27 19 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 8 10 8 3 9 9 9 15 |T 42 43 43 44 42 42 42 43 43 44 42
WRMS | 7 9 8 10 7 3 9 9 9 15 |NE 43 43 43 44 42 42 41 44 43 45 42
MEDI | 7 9 8 9 8 3 8 9 9 13 |MD 25 26 25 26 24 23 22 25 25 25 23
Table 3.2335.6 GPS week: 2335 Day: 6 MJD: 60595.000
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 | 8 8 6 10 11 3 9 7 9 10 3 | 19 20 22 20 21 20 22 19 23 21 19
3 | 7 12 9 9 8 4 6 8 10 10 3 | 43 46 45 45 44 42 42 45 43 41 43
4 | 8 14 5 12 9 2 10 15 7 12 3 | 29 30 30 32 32 29 29 32 30 34 29
5 | 8 8 8 11 10 3 10 8 9 11 3 | 33 29 31 35 31 31 29 30 35 36 31
6 | 7 10 10 9 12 3 7 7 8 8 3 | 74 74 76 75 75 75 75 75 73 72 74
7 | 7 9 7 8 10 3 9 7 8 10 3 | 24 19 21 22 23 21 20 20 23 22 20
8 | 6 9 8 8 5 3 6 6 8 6 2 | 36 37 35 35 35 34 33 36 35 35 35
9 | 9 11 7 9 5 4 9 7 7 12 3 | 40 42 38 42 39 39 37 42 40 35 39
10 | 12 8 9 11 10 3 8 8 8 8 3 | 34 34 34 31 33 32 32 34 33 29 32
X11E | 11 15 8 15 11 4 --- 8 8 16 4 | 32 31 35 37 35 32 --- 34 31 28 32
12 | 5 8 6 11 9 2 12 9 5 11 3 | 23 20 22 25 22 22 21 23 25 20 22
13 | 8 8 6 10 6 5 9 8 9 10 2 | 25 30 25 25 26 26 25 30 29 26 26
14 | 10 10 12 16 8 4 8 9 8 12 3 | 55 56 57 54 53 54 53 57 55 55 54
15 | 7 6 5 7 6 2 9 5 8 9 2 | 46 43 43 43 43 43 44 43 43 44 43
16 | 8 11 5 9 10 3 14 9 7 16 3 | 24 27 27 27 25 25 26 25 27 27 25
17 | 8 8 5 13 7 3 6 6 10 10 3 | 31 33 28 31 32 29 31 31 34 32 31
18 | 10 12 14 15 7 5 10 14 10 13 4 | 36 38 37 35 40 34 34 38 36 37 36
19 | 7 6 5 12 8 3 11 5 12 12 3 | 34 35 32 33 33 32 32 33 37 34 33
20 | 8 8 7 11 11 3 12 9 8 10 3 | 23 19 21 22 23 20 20 20 24 24 21
21 | 8 7 6 15 10 2 12 9 10 10 3 | 19 21 20 20 21 19 19 19 23 19 19
22 | 8 6 6 10 8 2 7 5 9 13 2 | 30 30 30 29 31 29 31 31 33 32 30
23 | 8 10 7 10 11 2 9 8 8 9 3 | 35 35 38 38 42 37 36 39 41 34 37
24 | 10 8 9 14 6 3 7 7 9 11 3 | 27 25 28 26 25 24 22 27 24 24 24
25 | 5 9 10 12 9 4 7 7 6 11 3 | 23 26 27 26 25 23 22 25 26 25 24
26 | 8 8 9 12 8 4 7 8 8 12 3 | 568 569 568 569 569 568 565 570 567 569 569
27 | 7 11 8 10 7 4 6 7 7 9 2 | 32 34 33 35 31 32 31 34 32 34 32
28 | 9 8 14 13 7 4 8 14 6 13 3 | 38 42 46 42 42 42 39 47 43 38 42
29 | 6 7 6 11 9 5 12 7 11 10 3 | 22 19 19 23 20 20 20 20 22 17 19
30 | 9 9 8 13 13 4 9 7 4 10 3 | 30 27 29 28 31 27 24 28 27 26 27
31 | 8 8 6 9 8 3 11 8 9 11 3 | 32 34 31 33 32 31 31 32 33 34 31
32 | 6 10 7 11 5 4 7 9 9 6 2 | 23 27 27 25 25 24 24 30 25 25 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 9 8 11 9 4 9 8 8 11 |T 49 50 50 50 50 48 48 50 50 49 49
WRMS | 8 9 8 12 8 4 9 8 8 11 |NE 49 50 50 50 50 49 48 50 51 49 49
MEDI | 8 8 7 11 8 3 9 8 8 10 |MD 32 31 31 32 32 31 31 32 33 32 31
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2335 GPS week: 2335 MJD: 60589.0-60595.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3000 |U 13 10 20 |U 9 12 26 |U 19 26 46 |
emr | emr 2975 |U 19 14 35 |U 11 14 38 | 21 29 51 |
esa | esa 2976 | 16 12 29 |U 11 18 45 |U 21 31 48 |
gfz | gfz 2975 |U 11 6 20 |U 7 10 28 | 23 28 58 |
grg | grg 2999 |U 12 7 20 |U 10 13 33 | 19 26 46 |
igr | igr 2976 | 12 8 21 | 9 12 27 | 21 28 49 |
igs | igs 2976 | 13 9 22 | 8 12 28 | 19 25 44 |
jgx | jgx 2880 |U 11 10 21 |U 9 13 25 | 22 25 52 |
jpl | jpl 2976 | 20 15 37 | 10 19 37 | 23 30 58 |
mit | mit 3003 |U 12 9 20 |U 9 14 27 |U 22 27 44 |
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 5.2335.0 GPS week: 2335 Day: 0 MJD: 60589.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 9 21 | 8 11 29 | 11 9 22 |
emr | emr 2976 | 14 12 37 | 10 14 34 | 14 13 25 |
esa | esa 2976 | 13 9 34 | 8 20 45 | 13 13 25 |
gfz | gfz 2976 | 10 8 21 | 7 10 29 | 9 8 23 |
grg | grg 3071 | 10 6 22 | 8 12 35 | 10 6 22 |
igr | igr 2976 | 9 7 22 | 7 12 28 | 11 8 20 |
igs | igs 2976 | 10 8 24 | 7 12 29 | 11 7 21 |
jgx | jgx 2880 | 10 8 21 | 9 13 25 | 11 5 20 |
jpl | jpl 2976 | 16 14 41 | 9 20 40 | 17 14 30 |
mit | mit 3072 | 11 11 17 | 8 14 31 | 36 14 20 |
Table 5.2335.1 GPS week: 2335 Day: 1 MJD: 60590.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 | 14 8 20 | 6 12 23 | 13 12 30 |
emr | emr 2976 | 20 12 35 | 10 15 33 | 12 11 29 |
esa | esa 2976 | 17 11 28 | 9 19 36 | 13 10 30 |
gfz | gfz 2975 | 13 7 21 | 6 9 27 | 10 17 37 |
grg | grg 3051 | 13 7 18 | 8 12 28 | 12 13 34 |
igr | igr 2976 | 13 7 20 | 7 12 23 | 11 10 28 |
igs | igs 2976 | 14 7 21 | 6 12 22 | 11 9 27 |
jgx | jgx 2880 | 13 7 20 | 8 13 22 | 11 9 29 |
jpl | jpl 2976 | 21 15 36 | 8 20 30 | 14 12 35 |
mit | mit 3072 | 11 8 21 | 7 14 24 | 12 12 30 |
Table 5.2335.2 GPS week: 2335 Day: 2 MJD: 60591.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 13 10 21 | 10 13 27 | 15 10 31 |
emr | emr 2976 | 30 20 47 | 14 15 37 | 17 14 40 |
esa | esa 2976 | 16 11 29 | 12 17 43 | 17 13 41 |
gfz | gfz 2976 | 10 7 23 | 8 10 31 | 15 9 35 |
grg | grg 2976 | 9 7 21 | 11 14 33 | 15 9 36 |
igr | igr 2976 | 13 9 29 | 10 13 30 | 16 9 36 |
igs | igs 2976 | 17 11 28 | 10 12 29 | 16 9 35 |
jgx | jgx 2880 | 11 14 35 | 12 17 29 | 19 14 51 |
jpl | jpl 2976 | 30 19 46 | 12 18 35 | 20 17 42 |
mit | mit 2976 | 13 11 21 | 11 12 32 | 15 10 31 |
Table 5.2335.3 GPS week: 2335 Day: 3 MJD: 60592.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 13 9 18 | 8 14 32 | 9 6 23 |
emr | emr 2976 | 18 17 32 | 12 13 49 | 13 15 30 |
esa | esa 2976 | 15 10 26 | 11 18 54 | 14 13 30 |
gfz | gfz 2976 | 11 4 17 | 7 10 31 | 10 8 23 |
grg | grg 2975 | 13 5 17 | 9 13 36 | 10 7 26 |
igr | igr 2976 | 12 6 17 | 8 13 32 | 10 6 24 |
igs | igs 2976 | 12 7 18 | 8 13 34 | 10 6 24 |
jgx | jgx 2880 | 11 7 17 | 9 14 29 | 10 8 27 |
jpl | jpl 2976 | 18 14 32 | 11 20 45 | 14 12 35 |
mit | mit 2976 | 12 6 16 | 8 14 28 | 8 6 25 |
Table 5.2335.4 GPS week: 2335 Day: 4 MJD: 60593.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 13 10 20 | 9 12 22 | 25 30 32 |
emr | emr 2976 | 17 11 28 | 12 13 40 | 25 23 38 |
esa | esa 2976 | 17 12 25 | 12 17 45 | 30 33 31 |
gfz | gfz 2975 | 12 6 21 | 8 11 25 | 38 43 67 |
grg | grg 2975 | 14 9 22 | 10 14 27 | 30 30 34 |
igr | igr 2976 | 13 8 19 | 10 12 27 | 38 44 65 |
igs | igs 2976 | 13 8 20 | 9 11 27 | 27 30 26 |
jgx | jgx 2880 | 13 8 21 | 9 13 23 | 43 24 39 |
jpl | jpl 2976 | 19 17 35 | 11 17 36 | 32 34 63 |
mit | mit 2976 | 13 9 24 | 9 16 29 | 22 30 28 |
Table 5.2335.5 GPS week: 2335 Day: 5 MJD: 60594.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 12 12 18 | 9 11 24 | 49 109 164 |
emr | emr 2976 | 14 13 32 | 12 14 37 | 52 120 163 |
esa | esa 2976 | 15 15 25 | 12 18 44 | 45 125 154 |
gfz | gfz 2974 | 9 7 16 | 8 11 26 | 66 104 200 |
grg | grg 2976 | 10 9 17 | 10 11 26 | 42 113 143 |
igr | igr 2976 | 10 9 16 | 10 11 22 | 48 112 152 |
igs | igs 2976 | 11 9 18 | 10 11 26 | 49 110 153 |
jgx | jgx 2880 | 9 12 15 | 10 11 27 | 48 112 177 |
jpl | jpl 2976 | 17 13 32 | 11 21 35 | 47 109 170 |
mit | mit 2976 | 11 10 19 | 10 13 27 | 52 109 152 |
Table 5.2335.6 GPS week: 2335 Day: 6 MJD: 60595.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 14 12 25 | 9 12 28 | 9 7 24 |
emr | emr 2973 | 17 14 32 | 10 15 40 | 12 11 31 |
esa | esa 2976 | 19 16 34 | 10 18 45 | 14 14 28 |
gfz | gfz 2975 | 11 6 20 | 7 13 24 | 10 7 20 |
grg | grg 2975 | 13 7 23 | 12 13 47 | 10 5 24 |
igr | igr 2976 | 11 9 23 | 8 13 25 | 10 7 21 |
igs | igs 2976 | 13 10 24 | 8 13 27 | 10 6 22 |
jgx | jgx 2880 | 12 11 22 | 9 13 23 | 9 5 20 |
jpl | jpl 2976 | 19 16 35 | 11 20 39 | 14 13 31 |
mit | mit 2976 | 12 11 21 | 8 15 21 | 8 7 21 |
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 6.2335 GPS week: 2335 MJD: 60589.500-60595.500
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 13 67 70 2 | -3 36
| 11 16 39 28 5 | 4
emr uuuuu | 5 -5 7 100 1 | -4 30
| 18 11 67 42 3 | 3
esa uuuuu | -4 10 -28 -144 -4 | 20 39
| 9 12 35 20 6 | 3
gfz uuuuu | -19 -36 -87 -27 -2 | 0 34
| 15 21 60 149 6 | 3
grg uuuuu | -7 7 36 1 1 | 4 32
| 10 6 26 70 6 | 3
igr xxxxx | 2 -3 -8 -28 -1 | 1 33
| 9 14 55 21 4 | 3
irf xxxxx | -9 3 -30 -2 -1 | 2 35
| 5 6 12 13 3 | 3
jgx uuuuu | -6 6 38 -117 -5 | 9 35
| 10 11 31 45 3 | 3
jpl uuuuu | 7 -14 80 13 -3 | 6 34
| 15 8 25 47 8 | 3
mit uuuuu | 25 21 -191 177 4 | 10 34
| 15 21 48 57 3 | 4
ngs uuuuu | 10 -20 52 -101 4 | 6 34
| 21 32 79 169 10 | 4
Table 7.2335.0 GPS week: 2335 Day: 0 MJD: 60589.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -4 -5 27 23 -6 | -2 27
emr uuuuu | -2 14 65 133 5 | -1 22
esa uuuuu | -8 8 -55 -141 -2 | 23 35
gfz uuuuu | -38 -39 -52 -87 -10 | 5 26
grg uuuuu | -15 10 51 -33 -2 | 8 27
igr xxxxx | 16 -5 32 -59 0 | 3 25
irf xxxxx | -8 11 -29 10 -4 | 5 27
jgx uuuuu | -2 11 43 -136 -2 | 12 29
jpl uuuuu | 10 -14 75 -34 3 | 8 27
mit uuuuu | 24 31 -185 237 6 | 10 28
ngs uuuuu | 47 -34 -15 58 6 | 7 29
Table 7.2335.1 GPS week: 2335 Day: 1 MJD: 60590.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -1 25 119 100 2 | -8 33
emr uuuuu | 4 -12 -33 96 1 | -7 26
esa uuuuu | -3 7 -57 -124 -10 | 18 35
gfz uuuuu | -30 -69 -53 -248 -6 | -2 31
grg uuuuu | -16 16 46 -96 -3 | 2 30
igr xxxxx | 12 -7 -38 -13 1 | -2 29
irf xxxxx | -3 5 -7 13 3 | -1 31
jgx uuuuu | -1 0 66 -52 -2 | 7 31
jpl uuuuu | 24 -20 55 51 3 | 3 29
mit uuuuu | 18 19 -102 260 7 | 5 29
ngs uuuuu | 13 39 -77 56 3 | 2 31
Table 7.2335.2 GPS week: 2335 Day: 2 MJD: 60591.500
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 17 89 81 10 | -9 33
emr uuuuu | 20 -7 65 127 1 | -8 26
esa uuuuu | -13 17 -30 -139 -5 | 16 34
gfz uuuuu | -11 -32 -68 -176 -2 | -4 31
grg uuuuu | -17 6 18 -57 -6 | -1 28
igr xxxxx | 0 4 8 -6 -1 | -3 29
irf xxxxx | -3 4 -36 13 1 | -3 30
jgx uuuuu | 5 -10 -23 -106 -1 | 4 30
jpl uuuuu | 12 -25 80 98 3 | 1 28
mit uuuuu | 34 13 -216 199 0 | 5 29
ngs uuuuu | -9 2 38 -1 2 | 0 30
Table 7.2335.3 GPS week: 2335 Day: 3 MJD: 60592.500
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 | -28 14 49 95 5 | 0 41
emr uuuuu | 32 -21 -69 139 -1 | -1 33
esa uuuuu | -10 23 -68 -187 -9 | 23 43
gfz uuuuu | -13 -13 -46 -19 -3 | 3 38
grg uuuuu | -7 -2 73 -7 2 | 5 35
igr xxxxx | 1 3 78 -20 -6 | 5 36
irf xxxxx | -10 4 -25 -19 -5 | 5 38
jgx uuuuu | 4 23 70 -159 -3 | 12 39
jpl uuuuu | 11 -8 53 0 4 | 9 38
mit uuuuu | 35 -11 -174 152 3 | 13 39
ngs uuuuu | -16 -20 64 -39 1 | 8 39
Table 7.2335.4 GPS week: 2335 Day: 4 MJD: 60593.500
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 -9 64 42 0 | -1 41
emr uuuuu | 1 1 -44 113 -2 | -3 34
esa uuuuu | -10 17 -1 -140 -6 | 20 42
gfz uuuuu | -32 -57 -127 132 -4 | 0 37
grg uuuuu | -1 5 36 40 3 | 3 35
igr xxxxx | 4 -6 -15 -13 -5 | 2 36
irf xxxxx | -16 6 -48 -8 -3 | 3 38
jgx uuuuu | -8 16 50 -60 -9 | 10 38
jpl uuuuu | 20 -18 121 -14 -9 | 8 37
mit uuuuu | -1 51 -259 141 1 | 12 38
ngs uuuuu | 20 -27 121 -406 26 | 7 38
Table 7.2335.5 GPS week: 2335 Day: 5 MJD: 60594.500
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 | -11 14 106 70 2 | -1 41
emr uuuuu | -24 2 -34 26 4 | -4 34
esa uuuuu | 11 -14 28 -135 -4 | 19 43
gfz uuuuu | 3 -29 -207 101 6 | -1 39
grg uuuuu | 6 0 36 49 4 | 3 35
igr xxxxx | -6 -29 -24 -45 -3 | 1 37
irf xxxxx | -7 -7 -38 -9 0 | 2 39
jgx uuuuu | -18 4 31 -148 -8 | 9 40
jpl uuuuu | -10 1 72 10 -7 | 7 38
mit uuuuu | 47 40 -189 104 6 | 12 38
ngs uuuuu | -3 -51 152 -171 -5 | 9 36
Table 7.2335.6 GPS week: 2335 Day: 6 MJD: 60595.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 36 16 75 0 | 1 40
emr uuuuu | 6 -9 97 62 -1 | -2 34
esa uuuuu | 5 10 -16 -143 7 | 20 43
gfz uuuuu | -12 -15 -54 106 5 | 1 39
grg uuuuu | 3 11 -11 108 11 | 5 35
igr xxxxx | -9 16 -95 -44 5 | 2 37
irf xxxxx | -14 0 -31 -12 -1 | 3 39
jgx uuuuu | -21 -1 31 -157 -6 | 10 39
jpl uuuuu | -17 -15 100 -20 -17 | 7 38
mit uuuuu | 20 5 -216 144 4 | 14 38
ngs uuuuu | 19 -50 82 -205 -3 | 12 36
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