[IGSREPORT-28618] Wk 2204 IGS Final Orbits
acc
acc at igs.org
Fri Apr 22 04:36:55 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2204 (Apr 03, 2022 - Apr 09, 2022)
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:
igs2204[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2204[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2204[0-6].cls IGS GPS clock combination summary report.
igs22047.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs22047.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, 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.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
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 | AREQ FAA1 KOUR SGOC
0 | EMR | AREQ
0 | GFZ | WSRT POHN SCUB WSRT
0 | GRG | 13 19 13 SEYG SGOC
1 | COD | BADG DAV1 GRAC SAMO SYDN YAKT DAV1 SYDN
1 | EMR | CHUR YELL
1 | ESA | DAV1 DAV1 PTBB TONG
1 | GFZ | DAV1 DAV1
1 | GRG | MCM4 SGOC SVTL XMIS MCM4 SGOC SVTL
1 | JPL | SVTL BADG SVTL
2 | COD | AREQ MAYG OUS2 AREQ
2 | ESA | OUS2 CPVG OUS2 PTBB
2 | GFZ | AREQ ZAMB AREQ NIST NYA1 ZAMB
2 | GRG | 1 1 CPVG HYDE BRFT CPVG HYDE
2 | MIT | PIE1
2 | NGS | 11
3 | COD | BADG CRO1 SUTH CRO1 SUTH
3 | EMR | MCM4
3 | ESA | DJIG PTBB
3 | GFZ | 13 28 CRO1 CRO1
3 | GRG | CRO1 DAEJ CRO1 DAEJ
3 | JPL | BADG
3 | NGS | 11
4 | COD | DAV1 KIRI SGOC ZAMB
4 | EMR | MCM4 HARB IRKJ MCM4 NIST
4 | ESA | CHUR DAV1 CHUR ZAMB
4 | GFZ | GRAC IRKJ ZAMB DAV1 GRAC IRKJ ZAMB
4 | GRG | DAV1 IRKJ OUS2
4 | JPL | DAEJ MCM4 DAEJ DAV1 KIRI MCM4
4 | MIT | YEL2
5 | COD | FAA1 UNSA GRAC
5 | EMR | MCM4 MDVJ
5 | GFZ | KIT3 KIT3 UNSA
5 | GRG | 13 13 HYDE KIT3 SGOC HYDE KIT3 NKLG SGOC
5 | NGS | 11
6 | COD | ASCG DARW DAV1 FAA1 MAYG THTI YKRO
6 | EMR | MCM4 NIST
6 | ESA | DAV1 DAV1
6 | GFZ | FAIR GODE HRAO FAIR GODE HRAO
6 | GRG | DAEJ GRAC GRAC
6 | JPL | CHUR
6 | NGS | 11
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G21 | 2022_04_08 | 2022019
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 | 1
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 G01 | 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.
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 | .4 -.0 .4 7 3 0 -.39
EMR | 0 | -7.1 4.3 -16.9 -6 -24 10 -.09
ESA | 0 | -.5 -1.0 -.3 -19 -3 23 -.40
GFZ | 0 | .3 -.3 -.2 7 -12 11 -.22
GRG | 0 | -.4 -2.6 -27.2 24 -17 -25 -.08
JPL | 0 | -2.2 -4.3 -6.4 1 0 0 -.28
MIT | 0 | -1.5 2.3 -5.6 6 14 -16 -.17
NGS | 0 | -3.5 -.3 -.8 -20 45 10 -.10
SIO | 0 | -1.8 3.1 -3.0 1 37 37 -.22
COD | 1 | .3 -.1 .8 1 -3 -3 -.34
EMR | 1 | -1.2 1.2 -22.9 8 -38 6 -.09
ESA | 1 | -.7 -1.0 .1 4 1 34 -.36
GFZ | 1 | .4 -.4 -.0 5 -9 7 -.15
GRG | 1 | .8 1.4 -32.0 31 -20 -37 -.24
JPL | 1 | 3.2 -5.6 -13.7 -6 6 -9 .01
MIT | 1 | 1.8 4.3 -9.4 10 8 -29 -.15
NGS | 1 | 1.4 2.7 -11.0 18 38 23 .01
SIO | 1 | .1 4.6 -8.0 -1 66 58 -.20
COD | 2 | .1 .2 .5 6 2 0 -.34
EMR | 2 | .8 2.5 -19.1 -21 -21 -5 -.02
ESA | 2 | -1.0 -.8 -.3 -8 -2 31 -.38
GFZ | 2 | .7 -.4 .2 7 -13 5 -.30
GRG | 2 | -.3 5.4 -30.7 34 -14 -23 -.15
JPL | 2 | 3.5 .3 -9.9 -2 6 5 -.06
MIT | 2 | 2.1 7.3 -12.5 12 34 -16 -.15
NGS | 2 | -.1 -1.0 .5 -1 14 12 -.10
SIO | 2 | 2.3 3.7 2.3 32 -52 91 -.41
COD | 3 | .2 -.1 .3 5 -5 3 -.31
EMR | 3 | -3.3 2.6 -15.5 6 -28 3 -.01
ESA | 3 | -1.0 -1.1 -.3 -4 -7 27 -.44
GFZ | 3 | .4 -.3 .4 17 -5 -1 -.25
GRG | 3 | .0 4.0 -30.1 20 -17 -22 -.09
JPL | 3 | .8 5.3 -8.8 -10 3 -13 -.07
MIT | 3 | .4 5.5 -6.9 3 38 -23 -.07
NGS | 3 | .6 .1 -7.1 10 36 11 .0
SIO | 3 | -.4 1.9 4.2 53 -42 62 -.41
COD | 4 | .2 -.1 .6 0 1 -2 -.23
EMR | 4 | -3.3 3.7 -12.5 -16 -18 9 .01
ESA | 4 | -.9 -1.4 .0 -17 6 27 -.48
GFZ | 4 | .6 -.1 .6 12 -9 3 -.31
GRG | 4 | -1.6 -3.6 -25.8 19 -22 -18 -.05
JPL | 4 | -2.9 -6.5 -10.2 -12 17 -12 -.07
MIT | 4 | -1.1 4.7 -5.9 -13 17 -11 -.0
NGS | 4 | -1.4 -5.1 -1.7 -49 34 -2 -.23
SIO | 4 | .7 1.4 4.3 7 -67 107 -.38
COD | 5 | .3 -.0 .6 3 -3 -1 -.27
EMR | 5 | -.7 -6.4 -17.8 19 -43 14 -.06
ESA | 5 | -1.1 -1.2 -.3 0 -6 40 -.51
GFZ | 5 | .5 -.3 .4 10 -11 7 -.30
GRG | 5 | -.6 -2.9 -27.3 11 -8 -54 -.17
JPL | 5 | .4 -3.1 -4.3 -4 9 -8 -.15
MIT | 5 | -2.2 1.8 -1.5 4 10 3 -.17
NGS | 5 | .4 -6.7 -6.5 -51 22 8 -.15
SIO | 5 | -3.2 2.8 6.1 50 -61 156 -.27
COD | 6 | .3 -.1 .5 2 3 -7 -.30
EMR | 6 | -10.8 -1.7 -11.4 -2 -23 -13 .10
ESA | 6 | -.4 -1.3 -.3 0 8 32 -.34
GFZ | 6 | .4 -.5 .3 1 -7 11 -.13
GRG | 6 | -1.6 -1.5 -21.5 14 -18 -34 -.13
JPL | 6 | .7 -4.0 -6.3 12 8 -6 -.21
MIT | 6 | -.3 4.2 -.7 -6 25 -16 -.08
NGS | 6 | -3.0 -1.3 -6.2 -25 59 13 -.10
SIO | 6 | -.9 3.6 7.9 41 -69 143 -.11
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
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 1.2204.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2204.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 2.2204.[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 3.2204.[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 5.2204.0-6). 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 2204 summary. (Apr 03, 2022 - Apr 09, 2022)
Table 1.2204.a GPS week: 2204 MJD: 59672.000-59678.000
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 644| 0 0 7 -7 13 5 -.02 8 8 | -577 188 6 88
| 0 0 0 13 16 20 .02 | 293 291
emr 80| -5 2 -3 14 28 -7 .01 13 13 | 204554 48 13 117
| 1 1 1 6 7 11 .03 | 339 610
esa 150| 0 0 1 0 4 9 -.04 8 8 | -480 -396 8 89
| 0 0 1 7 11 16 .02 | 125 558
gfz 236| 0 1 6 3 11 -3 .12 11 11 | -47 26 13 77
| 1 0 1 27 13 17 .02 | 228 298
grg 114| 2 -1 -13 0 30 -14 -.10 12 10 | -6 -59 8 148
| 0 0 3 11 6 26 .02 | 146 340
igr n/a| 0 0 2 -3 12 -18 .01 5 4 | -1739 -412 12 97
| 0 0 1 8 9 12 .01 | 1075 648
jpl 80| 0 -1 0 6 4 -15 .15 9 9 | -2200 -61 8 87
| 0 1 2 10 12 12 .02 | 448 683
mit 363| 1 0 -2 -3 27 -28 -.03 7 7 | -2890 -368 25 1590
| 0 0 1 8 16 32 .01 | 1152 659
ngs 205| 0 0 1 0 30 -17 -.04 9 9 | -63003 -2637 849 1952
| 0 0 2 17 11 23 .02 | 58526 2902
sio 500| 1 0 0 -5 -155 73 -.03 9 8 | --- --- --- ---
| 0 0 1 25 30 40 .02 | --- ---
Table 1.2204.b GPS week : 2204 MJD: 59672.000-59678.000
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 | 3 3 7 3 3 4 3 |
2 | 3 4 4 4 4 4 4 |
3 | 3 3 3 3 3 3 3 |
4 | 4 3 4 3 3 3 4 |
5 | 3 3 3 3 3 3 3 |
6 | 3 3 3 3 3 3 4 |
7 | 4 4 3 4 4 4 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 7 6 5 6 7 8 8 |
12 | 3 3 3 3 3 3 3 |
13 | 3 3 3 3 4 3 3 |
14 | 3 3 3 3 3 3 3 |
15 | 4 3 3 3 3 3 3 |
16 | 3 4 3 3 3 4 3 |
17 | 3 3 3 3 3 3 3 |
18 | 5 5 5 5 5 5 5 |
19 | 3 3 3 3 3 3 3 |
20 | 3 3 3 3 3 3 3 |
21 | 3 4 4 3 3 --- 4 |
22 | 3 3 3 3 3 3 3 |
23 | 3 3 3 4 3 4 3 |
24 | 4 4 4 5 4 4 4 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 3 3 3 |
27 | 3 3 3 3 4 3 3 |
28 | 4 4 3 4 4 3 4 |
29 | 4 4 4 3 4 3 4 |
30 | 4 4 4 4 4 4 4 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 3 3 3 3 2 |
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 2.2204.0 GPS week: 2204 Day: 0 MJD: 59672.000
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 636| 0 -1 7 -14 22 14 -.06 8 8 | -519 513 6 92
emr 80| -5 4 -2 10 39 2 .02 12 12 | 204213 253 12 113
esa 150| 0 0 0 -2 -5 38 -.02 8 8 | -562 11 9 85
gfz 215| -1 0 6 10 26 35 .12 11 10 | -465 347 13 79
grg 106| 2 -2 -12 10 34 27 -.13 11 10 | -174 163 9 172
igr n/a| 0 0 1 8 27 0 .03 5 5 | -471 -411 12 102
jpl 80| 0 -1 -1 26 14 4 .15 9 9 | -2101 -272 9 91
mit 363| 1 0 -2 -8 18 -78 -.03 7 6 | -1769 -469 27 1547
ngs 200| 1 0 1 2 23 -4 -.01 9 9 | -589 636 864 1880
sio 471| 1 0 1 -12 -162 13 -.02 9 8 | --- --- --- ---
Table 2.2204.1 GPS week: 2204 Day: 1 MJD: 59673.000
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 643| 0 0 7 -14 5 18 -.02 8 8 | -647 339 6 81
emr 80| -5 3 -4 18 26 7 .03 13 13 | 204660 436 15 97
esa 150| 0 0 2 8 0 16 -.02 7 7 | -586 -276 8 99
gfz 241| -1 1 7 13 0 -8 .12 11 10 | -21 180 12 68
grg 119| 2 -1 -18 9 34 -4 -.09 11 10 | -104 227 10 159
igr n/a| 0 0 4 0 7 -23 .01 5 4 | -648 -195 12 84
jpl 80| -1 0 0 10 3 -9 .12 8 8 | -2034 632 10 76
mit 363| 1 0 -3 0 7 -48 -.03 7 7 | -1872 -76 25 1715
ngs 199| 1 0 0 30 34 -18 -.04 11 11 | -541 193 817 1644
sio 498| 1 1 2 -46 -93 61 -.05 9 9 | --- --- --- ---
Table 2.2204.2 GPS week: 2204 Day: 2 MJD: 59674.000
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 653| 0 0 7 -6 7 0 -.01 9 7 | -438 97 6 83
emr 80| -2 4 -3 12 27 -12 .02 13 13 | 205098 -452 15 123
esa 150| -1 0 0 -7 1 10 -.01 8 7 | -435 -261 8 92
gfz 240| 0 1 8 21 12 0 .10 11 12 | 168 125 13 77
grg 119| 3 -1 -17 4 37 -29 -.11 22 11 | 93 23 9 135
igr n/a| 0 0 3 -16 8 -12 .01 4 4 | -823 -1055 12 90
jpl 80| 0 -1 -4 1 0 -10 .16 10 10 | -1378 -957 7 78
mit 363| 0 0 -3 8 36 -27 -.01 6 7 | -2063 -857 28 1462
ngs 210| 0 0 5 -12 38 12 -.04 9 9 | -99462 -4866 733 1819
sio 524| 1 0 1 -11 -188 55 -.05 10 8 | --- --- --- ---
Table 2.2204.3 GPS week: 2204 Day: 3 MJD: 59675.000
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 647| 0 0 6 17 19 8 -.02 8 8 | -228 -403 6 87
emr 80| -4 2 -3 18 19 0 -.03 12 12 | 204608 -768 15 144
esa 150| 0 0 4 -10 -10 16 -.04 8 8 | -221 -1563 8 97
gfz 241| 0 1 7 31 9 -6 .13 11 12 | 212 -455 13 69
grg 116| 2 -1 -14 -18 31 -12 -.08 11 11 | 201 -640 9 136
igr n/a| 0 0 2 -4 22 -12 -.01 5 5 | -1932 -1227 12 107
jpl 80| -1 -1 -2 -3 -8 -17 .14 9 9 | -2463 -692 8 108
mit 363| 1 0 -2 -8 27 -41 -.04 7 7 | -2978 -1240 24 1871
ngs 205| 0 1 -1 -18 45 5 -.03 8 8 | -103942 -4876 1101 2352
sio 472| 0 0 -1 3 -150 48 -.04 9 8 | --- --- --- ---
Table 2.2204.4 GPS week: 2204 Day: 4 MJD: 59676.000
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 641| 0 0 6 0 30 35 -.03 8 8 | -1172 183 6 85
emr 80| -5 3 -3 22 18 -7 -.03 13 13 | 204065 1059 13 132
esa 150| 0 0 1 2 9 0 -.03 8 8 | -551 -84 8 86
gfz 241| 1 1 5 17 -9 -14 .15 11 11 | 11 159 14 87
grg 116| 1 0 -11 6 30 -2 -.10 11 10 | -173 320 8 142
igr n/a| 0 0 1 2 0 -12 .00 5 4 | -2771 679 12 85
jpl 80| -1 -3 0 0 8 -19 .14 9 9 | -2837 966 11 101
mit 363| 1 0 -1 -16 29 -26 -.03 7 7 | -3619 735 26 1529
ngs 209| 0 0 1 8 37 -50 -.03 8 9 | -1382 550 885 2063
sio 530| 1 0 0 -21 -157 86 -.02 9 9 | --- --- --- ---
Table 2.2204.5 GPS week: 2204 Day: 5 MJD: 59677.000
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 642| 0 0 8 -15 26 -4 -.02 9 8 | -577 321 7 101
emr 80| -5 0 -6 19 32 -27 .03 13 13 | 204708 -272 14 132
esa 150| -1 0 0 7 16 -13 -.06 8 8 | -525 -613 9 84
gfz 239| 2 1 6 -44 16 -14 .11 12 11 | -43 -333 16 82
grg 108| 2 -2 -12 -14 18 -17 -.08 11 10 | 98 -223 9 178
igr n/a| 0 1 2 -4 9 -36 .01 4 4 | -2547 -652 12 110
jpl 80| 0 0 0 -2 21 -33 .17 8 8 | -2282 -162 8 78
mit 363| 0 0 0 -4 13 7 -.04 7 7 | -2936 -721 24 1215
ngs 209| 1 0 2 5 11 -42 -.06 8 8 | -117022 -4912 763 2053
sio 482| 0 0 0 32 -160 135 -.02 10 8 | --- --- --- ---
Table 2.2204.6 GPS week: 2204 Day: 6 MJD: 59678.000
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 648| 0 0 5 -20 -16 -30 .00 9 8 | -463 269 7 89
emr 80| -7 1 -2 2 35 -13 .02 13 13 | 204532 81 13 80
esa 150| 0 0 0 7 18 0 -.06 8 8 | -485 9 8 85
gfz 240| 2 1 2 -23 25 -14 .09 11 10 | -194 164 15 81
grg 116| 0 -2 -8 -2 27 -59 -.08 10 10 | 11 -286 8 115
igr n/a| 0 0 1 -13 12 -30 .01 5 5 | -2984 -24 12 102
jpl 80| 0 0 2 12 -12 -24 .18 9 9 | -2308 55 9 77
mit 363| 0 0 0 6 58 14 -.04 7 6 | -4999 52 25 1796
ngs 208| 0 0 -2 -17 24 -22 -.05 9 9 | -118088 -5187 786 1854
sio 525| 1 0 1 14 -178 110 -.01 9 8 | --- --- --- ---
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 3.2204.0 GPS week: 2204 Day: 0 MJD: 59672.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 16 8 11 9 4 8 6 7 11 3 | 159 157 158 156 163 158 156 158 156 166 158
2 | 7 13 8 12 8 3 8 8 12 8 3 | 61 65 58 57 60 59 63 62 58 63 60
3 | 5 9 9 9 8 4 8 7 9 9 3 | 22 28 26 20 22 23 28 21 23 23 22
4 | 10 15 7 11 11 6 9 10 9 8 3 | 74 70 71 80 70 72 71 72 75 74 72
5 | 5 9 9 11 5 4 8 5 10 8 2 | 28 30 26 31 29 28 30 28 30 31 28
6 | 7 10 9 10 10 5 8 6 12 7 3 | 32 34 33 32 39 30 32 31 29 32 31
7E | 14 12 7 11 10 3 10 5 8 8 3 | 25 29 25 31 28 27 29 29 30 32 27
8 | 9 10 7 6 10 4 8 7 9 9 3 | 22 28 26 25 26 23 27 20 23 27 23
9 | 8 9 10 8 10 4 7 6 7 6 2 | 21 22 22 19 22 20 24 19 20 21 19
10 | 6 8 9 5 5 4 9 7 8 10 2 | 22 28 25 26 25 23 27 22 22 25 23
X11 | 13 18 --- --- 20 15 11 9 --- --- 7 | 85 79 --- --- 86 80 50 81 --- --- 82
12 | 7 13 7 7 9 4 8 6 10 12 3 | 50 55 51 51 45 50 50 50 46 54 49
13 | 8 11 7 11 10 5 10 10 6 11 3 | 20 27 21 23 20 22 26 22 20 26 21
14 | 9 12 7 11 10 5 8 7 8 6 3 | 41 50 46 48 51 45 45 49 48 47 46
15 | 6 9 11 14 10 7 10 9 8 10 3 | 43 49 44 46 43 42 46 42 39 41 42
16 | 8 19 6 6 11 5 7 6 9 4 3 | 18 22 19 22 16 17 19 17 18 23 17
17 | 6 12 7 11 9 5 7 8 6 6 3 | 27 34 29 32 32 29 32 27 30 32 28
18 | 12 19 12 17 22 6 12 11 16 9 5 | 79 78 78 82 78 79 80 74 80 77 77
19 | 7 12 6 9 8 4 8 7 9 7 2 | 38 41 40 42 42 40 40 39 40 44 39
20 | 5 9 6 11 8 6 6 6 11 10 2 | 17 20 19 19 17 18 18 18 19 20 17
21 | 9 13 8 13 12 4 9 7 8 6 3 | 36 40 37 37 36 39 40 40 42 37 38
22 | 7 11 4 11 8 4 9 4 8 9 2 | 26 25 23 28 25 25 24 23 26 26 24
23 | 6 10 6 9 8 4 12 5 8 11 3 | 22 27 23 26 25 22 22 22 23 27 22
24E | 10 13 12 22 14 5 9 8 8 11 4 | 29 28 29 28 24 26 29 26 28 30 26
25 | 6 10 6 7 9 4 6 5 7 7 2 | 23 26 22 23 21 22 26 22 18 27 22
26 | 7 9 8 9 9 4 6 5 7 6 2 | 29 28 26 32 20 26 29 23 24 28 25
27 | 8 10 7 11 12 4 9 6 6 11 3 | 21 25 25 25 25 22 26 20 22 27 22
X28 | 7 12 3 11 7 5 10 6 15 --- 3 | 14 24 18 19 16 16 24 17 21 --- 17
29 | 11 17 5 9 16 4 9 5 10 7 3 | 40 39 39 40 40 39 42 38 40 44 39
30E | 9 13 7 18 11 4 10 5 7 14 3 | 25 32 28 28 27 27 28 26 29 33 26
31E | 10 10 8 8 14 10 7 5 8 9 3 | 26 27 24 28 29 27 27 26 27 30 25
32 | 7 9 7 10 7 4 7 5 8 12 2 | 28 29 29 28 29 28 30 27 28 36 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 8 11 11 5 9 7 9 9 |T 37 40 36 38 38 37 38 37 36 40 37
WRMS | 8 12 8 10 10 5 9 6 9 8 |NE 38 41 37 39 39 38 39 37 36 40 38
MEDI | 7 11 7 11 10 4 8 6 8 9 |MD 27 29 26 28 28 27 29 26 28 31 26
Table 3.2204.1 GPS week: 2204 Day: 1 MJD: 59673.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 14 6 7 11 3 9 5 11 11 3 | 161 164 163 165 167 162 163 162 164 160 162
2E | 6 14 10 9 12 7 10 12 11 11 3 | 58 66 58 63 64 59 62 57 63 61 60
3 | 6 10 9 9 7 4 8 6 6 12 3 | 17 25 22 20 16 19 24 15 15 18 18
4 | 12 15 5 10 10 4 8 8 8 8 3 | 55 53 53 54 51 53 54 53 54 54 53
5 | 5 10 8 11 9 4 7 7 11 8 3 | 35 33 33 38 32 34 38 36 32 39 34
6 | 6 10 6 13 8 5 9 6 13 8 3 | 29 30 27 28 31 26 28 26 25 27 26
7E | 10 15 8 15 15 3 10 6 12 11 3 | 23 26 21 26 22 21 24 25 29 28 22
8 | 8 11 7 9 10 3 10 7 12 8 3 | 21 23 22 21 21 20 24 18 20 25 20
9 | 7 9 8 8 10 3 8 6 8 8 2 | 20 21 20 17 21 18 22 17 19 19 18
10 | 5 12 6 9 8 4 8 8 12 8 3 | 18 23 19 20 17 18 25 17 18 21 18
X11 | 11 18 --- --- 15 7 10 8 --- --- 6 | 57 57 --- --- 55 54 31 55 --- --- 56
12 | 5 14 5 7 10 5 6 6 14 9 3 | 31 35 30 33 24 30 32 31 28 36 30
13 | 8 12 6 12 9 5 10 8 10 11 3 | 16 25 18 21 17 19 24 19 20 26 18
14 | 6 9 7 7 11 5 9 7 10 7 2 | 30 32 29 31 36 29 29 33 32 32 30
15 | 7 12 7 9 9 6 8 9 11 10 3 | 39 42 39 43 44 41 44 39 42 42 40
16 | 8 22 6 9 11 5 6 8 13 7 3 | 15 20 14 20 14 14 15 14 17 21 14
17 | 6 11 6 8 9 3 9 6 12 9 3 | 25 27 23 26 26 24 26 23 27 24 23
18 | 12 19 12 15 20 5 10 8 12 10 4 | 54 57 53 59 56 54 56 53 54 57 54
19 | 8 12 4 10 7 5 9 6 16 11 3 | 28 30 27 34 28 29 27 28 27 31 27
20 | 6 8 6 8 8 4 8 6 13 9 2 | 18 17 17 20 17 16 18 16 18 19 16
21E | 7 12 7 10 18 9 8 7 11 10 3 | 56 54 54 52 51 54 55 54 52 61 54
22 | 8 11 4 10 10 3 8 7 8 8 2 | 19 21 19 20 20 19 18 19 22 22 18
23 | 5 13 5 10 8 4 11 6 11 9 3 | 16 17 17 20 18 15 16 17 19 22 16
24E | 8 16 12 21 16 5 8 7 11 8 4 | 24 28 25 23 20 22 25 24 22 29 22
25 | 5 10 9 9 8 5 6 6 11 9 2 | 18 24 23 20 16 19 25 20 17 27 20
26 | 8 9 7 8 9 4 8 5 7 8 2 | 23 21 22 23 18 21 24 17 18 24 20
27 | 8 12 7 7 12 3 8 7 11 10 3 | 20 21 21 22 20 20 22 18 21 27 19
X28 | 7 13 6 13 8 5 9 7 13 --- 3 | 17 25 16 22 17 17 22 16 21 --- 17
29 | 12 17 6 10 14 5 8 5 15 10 3 | 30 32 31 31 28 30 31 30 31 36 29
30E | 11 21 7 17 14 5 9 7 10 9 4 | 22 31 25 24 27 24 28 26 26 25 24
31E | 10 11 7 9 16 5 6 4 8 5 3 | 27 29 26 28 32 27 28 26 27 30 26
32 | 10 9 6 8 9 3 7 5 8 8 2 | 27 30 28 30 28 27 30 27 25 31 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 7 11 11 5 8 7 11 9 |T 32 35 32 34 32 32 34 32 32 35 32
WRMS | 8 13 7 10 10 4 8 7 11 9 |NE 32 34 31 33 32 31 33 31 31 35 31
MEDI | 8 12 7 9 10 5 8 7 11 9 |MD 24 28 25 26 24 24 26 25 25 27 23
Table 3.2204.2 GPS week: 2204 Day: 2 MJD: 59674.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 22 26 11 16 101 8 25 10 13 22 6 | 461 463 459 457 457 458 460 459 458 457 459
2E | 7 12 11 9 19 5 11 9 7 8 3 | 34 36 30 34 45 32 36 32 34 35 33
3 | 6 13 8 12 8 4 8 6 7 12 3 | 27 34 30 22 28 27 32 24 28 26 26
4 | 8 16 9 10 11 4 9 8 12 7 3 | 57 54 52 62 52 55 53 55 62 55 55
5 | 6 8 8 8 6 4 9 6 9 9 2 | 26 27 26 26 25 25 27 25 24 29 25
6 | 5 9 7 14 10 4 10 5 10 7 3 | 28 28 29 29 31 27 30 27 26 28 27
7E | 14 13 7 6 10 3 9 7 8 9 3 | 35 34 30 31 33 31 31 33 34 34 31
8 | 8 10 9 12 10 4 9 6 7 8 3 | 26 28 29 25 27 26 28 23 25 29 25
9 | 7 8 8 8 9 6 8 6 8 5 2 | 23 25 24 20 24 22 26 21 19 22 21
10 | 7 11 9 11 8 3 9 9 7 9 3 | 26 30 28 29 28 27 31 26 24 30 27
X11 | 11 19 --- --- 13 7 10 6 9 --- 5 | 37 40 --- --- 40 36 27 39 48 --- 38
12 | 6 14 6 5 9 4 7 4 7 12 2 | 42 45 41 41 36 40 42 38 40 42 40
13 | 6 12 6 10 10 5 9 7 8 11 3 | 26 32 26 29 28 27 32 27 25 31 27
14 | 8 10 6 9 11 4 7 5 9 12 3 | 28 31 29 33 35 29 32 33 29 36 30
15 | 6 11 6 9 16 6 7 8 10 11 3 | 47 53 49 51 50 47 50 49 44 46 48
16 | 7 20 6 11 11 5 9 8 7 9 3 | 21 24 21 21 21 20 20 19 22 25 20
17 | 6 11 5 8 11 3 7 6 7 7 2 | 24 28 23 27 28 25 28 24 24 26 24
18 | 13 24 14 18 17 5 12 8 19 8 5 | 43 40 39 46 45 41 44 40 42 43 41
19 | 6 13 5 9 7 4 9 5 6 6 2 | 25 27 24 29 28 25 27 27 24 28 25
20 | 5 7 5 8 8 5 8 5 11 9 2 | 22 21 22 22 22 20 23 21 21 24 21
21E | 9 10 7 13 11 6 9 7 12 9 3 | 30 28 25 28 29 26 27 29 25 26 26
22 | 8 10 5 17 11 4 8 6 9 8 3 | 33 32 30 36 31 31 30 29 31 35 30
23 | 6 15 7 9 8 3 12 6 8 9 3 | 22 23 22 25 25 21 22 24 19 26 21
24E | 6 13 13 17 15 4 9 6 9 12 4 | 21 23 21 23 19 20 23 20 21 26 20
25 | 6 10 7 8 10 5 6 5 7 11 2 | 29 30 31 29 27 28 31 28 28 33 28
26 | 6 9 8 8 10 3 9 7 6 6 2 | 29 26 29 28 26 27 29 24 26 29 26
27 | 9 12 8 13 10 3 9 7 5 9 3 | 26 24 27 25 26 25 27 23 23 28 24
X28 | 6 12 7 15 7 5 7 7 9 --- 3 | 21 26 19 22 23 18 26 21 20 --- 20
29 | 12 16 5 8 14 4 8 4 9 12 3 | 36 33 33 36 34 33 36 33 35 36 33
30E | 14 12 6 10 18 5 9 5 7 9 3 | 24 26 24 24 21 24 26 24 23 26 22
31E | 7 12 9 12 18 4 7 4 8 5 3 | 25 28 26 27 30 26 28 25 26 30 25
32 | 7 8 7 13 9 3 7 6 9 8 2 | 21 22 22 24 20 21 23 19 22 20 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 11 22 4 10 6 9 10 |T 42 44 42 43 43 41 43 41 42 45 41
WRMS | 7 13 7 12 11 4 10 7 9 8 |NE 46 47 46 47 46 45 47 45 45 49 45
MEDI | 7 12 7 10 10 4 9 6 8 9 |MD 26 28 28 28 28 27 28 26 25 29 26
Table 3.2204.3 GPS week: 2204 Day: 3 MJD: 59675.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 13 6 13 12 6 8 7 7 7 3 | 241 239 240 237 242 240 241 240 241 241 240
2E | 7 13 11 10 15 5 11 8 7 8 3 | 40 44 39 44 50 39 43 38 44 43 41
3 | 6 10 7 11 8 5 7 6 9 8 3 | 23 30 25 24 22 23 29 20 26 22 23
4 | 10 13 6 9 9 6 9 7 8 10 3 | 58 51 54 58 49 53 50 52 55 48 52
5 | 6 9 8 10 6 5 9 7 5 10 2 | 24 26 23 28 22 24 29 25 25 25 24
6 | 7 10 8 9 11 6 7 6 9 8 3 | 27 29 28 25 32 27 31 26 27 26 26
7E | 14 14 6 10 13 3 10 8 8 8 3 | 27 28 24 29 25 25 25 26 27 25 25
8 | 10 10 6 9 10 4 9 5 9 8 3 | 21 26 24 23 25 22 25 21 25 25 22
9 | 7 9 8 11 9 4 8 6 9 6 2 | 24 25 25 23 22 23 26 22 24 23 22
10 | 8 10 7 8 7 3 8 9 8 8 3 | 19 23 20 20 20 19 26 18 21 21 19
X11 | 13 20 --- --- 18 8 11 9 12 --- 6 | 30 29 --- --- 35 29 28 30 41 --- 29
12 | 5 15 6 7 8 5 8 5 7 10 2 | 43 47 44 45 38 43 43 41 40 44 42
13 | 7 13 8 9 10 4 10 7 7 10 3 | 19 27 19 22 19 21 27 20 22 23 20
14 | 8 11 6 8 11 5 7 6 8 8 2 | 31 35 33 37 38 33 35 39 37 35 35
15 | 5 11 7 10 10 5 8 8 6 9 3 | 34 40 33 37 36 34 38 35 36 36 35
16 | 7 20 5 6 12 5 7 7 6 9 3 | 20 25 21 22 20 21 20 21 22 24 20
17 | 6 11 6 10 11 3 9 7 6 7 2 | 27 31 26 30 29 27 31 27 30 27 27
18 | 11 22 17 14 21 6 11 10 13 10 5 | 34 37 36 38 40 34 38 34 32 38 34
19 | 7 13 5 13 8 3 8 7 7 7 3 | 28 30 27 31 30 28 30 26 32 29 28
20 | 7 9 6 8 8 6 9 5 9 12 3 | 19 20 21 24 19 20 22 18 21 23 20
21E | 9 9 9 10 11 7 8 6 8 6 3 | 26 30 26 28 34 28 28 30 31 32 28
22 | 10 9 4 9 11 4 9 7 5 8 2 | 24 23 24 27 21 21 21 21 22 22 21
23 | 6 12 9 13 8 3 12 9 8 9 3 | 13 16 16 21 18 13 15 16 17 20 14
24E | 9 12 14 28 12 5 11 8 7 11 4 | 26 26 29 31 24 26 28 27 31 28 26
25 | 6 10 7 8 8 6 6 4 8 9 2 | 22 27 25 25 21 22 27 23 21 28 23
26 | 7 10 9 9 10 3 6 7 6 7 2 | 30 30 31 31 26 29 31 29 28 32 29
27 | 10 9 7 8 12 3 9 6 8 9 3 | 21 23 24 24 23 22 25 21 25 27 22
X28 | 10 14 6 11 7 5 10 7 7 --- 3 | 19 28 20 24 18 18 28 20 22 --- 20
29 | 10 16 7 9 13 4 8 5 8 10 3 | 23 23 20 26 24 23 24 23 27 29 23
30E | 13 12 7 16 15 7 9 6 7 9 3 | 23 26 26 24 24 26 27 26 26 26 24
31E | 9 10 7 9 16 4 6 6 8 6 3 | 21 23 20 22 22 20 23 21 23 24 20
32 | 10 13 6 5 9 5 6 4 8 6 2 | 19 24 20 21 20 19 22 18 21 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 8 11 11 5 9 7 8 9 |T 33 35 33 35 34 32 35 32 35 35 32
WRMS | 8 12 8 12 11 5 9 7 8 8 |NE 34 37 35 36 34 34 37 34 36 36 34
MEDI | 8 11 7 9 10 5 8 7 8 8 |MD 24 27 25 26 24 24 28 25 26 26 24
Table 3.2204.4 GPS week: 2204 Day: 4 MJD: 59676.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 13 7 9 11 5 11 8 9 12 3 | 300 299 299 295 305 298 298 299 297 299 299
2E | 8 13 10 12 13 5 11 8 10 8 3 | 35 37 30 37 40 31 37 32 34 34 33
3 | 6 8 10 12 8 5 9 6 5 11 3 | 25 29 28 27 23 25 30 23 25 23 25
4 | 9 15 7 9 9 5 8 8 10 7 3 | 56 53 52 58 54 53 54 54 58 56 54
5 | 5 9 7 10 7 5 9 6 6 10 2 | 23 22 19 20 20 21 26 22 20 22 21
6 | 7 10 7 12 8 4 8 5 9 5 2 | 26 25 26 22 26 23 26 23 23 24 23
7E | 14 13 8 10 16 4 11 7 7 8 3 | 37 35 31 34 35 33 35 34 36 33 33
8 | 8 10 7 12 11 4 9 7 8 11 3 | 24 23 25 24 24 21 23 20 21 22 21
9 | 7 10 8 13 8 5 8 7 7 7 3 | 22 21 22 20 21 20 27 19 19 22 20
10 | 9 9 8 11 5 4 10 11 7 8 3 | 26 26 25 27 24 24 30 24 22 26 24
X11 | 15 18 --- --- 19 10 13 8 --- --- 7 | 38 38 --- --- 44 41 44 41 --- --- 40
12 | 6 14 7 9 10 4 8 6 8 10 3 | 35 37 34 34 31 33 38 33 30 34 33
13 | 7 16 7 11 11 5 10 7 8 11 3 | 26 31 23 25 24 25 31 26 25 28 25
14 | 8 10 8 10 12 5 9 7 10 9 3 | 32 35 33 37 39 33 33 38 33 39 34
15 | 7 16 7 9 10 5 9 8 10 11 3 | 36 47 39 42 39 38 41 39 40 38 39
16 | 6 23 4 7 13 5 8 6 8 8 3 | 20 21 20 22 19 20 19 19 20 22 19
17 | 7 11 6 11 8 4 8 9 8 8 3 | 21 27 22 27 22 25 27 24 26 25 23
18 | 12 23 13 14 19 5 11 8 10 8 4 | 44 43 40 45 46 42 45 43 43 42 42
19 | 7 12 6 13 9 3 11 7 11 7 3 | 24 22 23 29 23 23 25 21 22 27 23
20 | 8 8 5 12 9 5 9 8 8 9 3 | 23 18 20 20 18 20 22 22 20 19 19
21E | 7 11 10 10 9 6 8 5 5 6 2 | 27 29 26 33 30 26 26 29 30 30 28
22 | 7 10 5 11 9 3 8 8 7 9 3 | 28 24 26 31 25 26 26 25 24 27 25
23 | 6 10 6 14 9 4 12 9 7 10 3 | 19 19 19 26 22 17 19 21 17 23 19
24E | 10 17 13 18 13 5 11 6 14 8 4 | 25 27 26 28 23 23 26 23 29 25 24
25 | 7 9 8 10 10 4 7 5 9 13 3 | 22 25 26 26 21 22 27 22 23 27 23
26 | 5 8 9 9 9 3 9 5 6 7 2 | 25 26 25 27 22 23 27 23 24 24 23
27 | 15 9 7 11 12 3 10 7 11 10 3 | 25 20 23 22 23 21 23 20 20 22 20
X28 | 8 12 8 14 12 7 11 8 12 --- 4 | 23 26 20 28 23 21 30 22 22 --- 22
29 | 9 17 6 11 13 4 8 5 9 8 3 | 32 27 28 31 29 29 31 28 30 31 29
30E | 13 15 8 11 12 6 9 7 7 8 3 | 22 26 21 28 22 23 24 24 24 24 22
31E | 8 10 8 11 13 6 8 6 7 6 3 | 23 25 24 25 25 24 26 24 25 26 23
32 | 7 10 7 8 8 3 11 4 5 8 2 | 23 24 24 28 21 23 25 20 22 24 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 8 11 11 5 9 7 8 9 |T 36 37 35 38 36 35 38 35 35 37 35
WRMS | 8 13 8 11 10 4 9 7 9 9 |NE 38 38 37 39 38 37 40 37 37 39 37
MEDI | 7 11 7 11 10 5 9 7 8 8 |MD 25 26 25 28 24 24 27 24 24 26 23
Table 3.2204.5 GPS week: 2204 Day: 5 MJD: 59677.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 10 9 16 9 4 9 9 8 14 3 | 255 252 255 255 258 255 255 254 255 248 254
2E | 7 16 9 9 18 5 9 9 7 9 3 | 37 40 32 34 46 33 34 32 36 36 34
3 | 7 12 9 10 9 3 8 5 7 11 3 | 18 27 22 19 16 20 27 18 19 18 19
4 | 9 14 8 8 8 5 9 8 8 9 3 | 63 62 59 63 62 62 63 65 63 67 62
5 | 6 8 7 10 8 4 8 8 5 10 2 | 22 25 22 25 21 24 25 24 24 25 23
6 | 7 8 7 9 11 4 8 6 10 6 2 | 30 33 32 29 30 29 31 28 27 29 28
7E | 16 13 7 12 12 5 12 6 8 11 3 | 29 28 28 34 30 27 28 29 29 31 28
8 | 11 11 7 11 11 3 8 6 10 10 3 | 22 26 23 23 25 21 25 20 22 25 21
9 | 8 11 9 10 7 5 8 7 6 7 2 | 24 26 26 23 23 24 28 23 23 23 23
10 | 8 10 6 13 7 4 7 9 7 8 3 | 20 26 21 24 19 20 27 19 19 21 20
X11 | 12 20 --- --- 17 10 --- 10 18 --- 7 | 60 61 --- --- 59 59 --- 60 41 --- 61
12 | 6 14 7 8 8 4 10 7 5 10 3 | 32 34 29 33 29 31 31 31 32 32 30
13 | 8 11 6 13 9 5 11 7 6 13 3 | 19 26 22 21 19 21 27 20 23 25 21
14 | 9 12 6 10 14 4 8 6 8 7 3 | 31 37 35 36 36 33 35 36 35 32 34
15 | 7 12 6 10 9 5 10 9 8 11 3 | 40 48 43 44 41 42 45 42 41 43 42
16 | 7 21 6 11 12 4 8 8 6 7 3 | 18 22 18 20 19 20 21 19 21 21 18
17 | 7 13 6 9 11 3 8 6 7 8 3 | 31 37 31 34 33 33 36 31 34 30 31
18 | 13 23 13 15 20 6 11 10 10 9 4 | 57 57 57 58 54 57 58 56 59 56 56
19 | 8 12 7 7 11 5 7 5 10 5 2 | 33 36 37 38 32 36 36 33 33 33 33
20 | 7 9 7 11 8 5 7 6 7 10 2 | 21 23 21 22 21 21 23 20 22 22 20
22 | 9 8 5 15 8 4 6 7 8 8 2 | 19 20 19 24 19 20 20 20 20 21 19
23 | 7 14 6 15 10 3 10 8 9 9 3 | 21 23 21 27 20 20 21 21 22 23 20
24E | 9 12 13 16 15 4 8 8 10 11 4 | 39 39 41 42 35 38 38 36 40 37 37
25 | 7 9 6 9 9 4 9 6 7 13 3 | 20 26 21 24 19 20 26 20 19 25 20
26 | 8 9 7 14 8 3 6 4 7 6 2 | 25 28 24 27 21 25 28 24 25 26 24
27 | 11 9 7 11 12 3 9 5 8 12 3 | 21 24 24 23 25 22 26 21 23 27 22
X28 | 10 12 6 13 11 5 8 5 6 --- 3 | 19 28 22 23 18 20 27 20 21 --- 21
29 | 9 16 7 9 12 4 7 5 11 10 3 | 31 31 30 29 29 30 32 31 30 35 30
30E | 16 14 8 20 14 7 9 7 9 9 4 | 28 36 30 40 29 31 34 32 33 30 30
31E | 8 11 8 9 14 4 5 5 11 11 3 | 24 27 24 26 26 24 26 24 26 29 24
32 | 8 9 7 8 7 3 6 3 7 7 2 | 28 31 29 28 26 29 32 26 25 31 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 12 11 4 8 7 8 10 |T 36 39 36 38 36 36 38 36 36 37 36
WRMS | 8 13 8 11 10 4 8 7 8 8 |NE 37 41 37 38 37 38 40 37 37 39 37
MEDI | 8 12 7 10 11 4 8 7 8 9 |MD 28 28 26 27 26 25 28 26 26 29 27
Table 3.2204.6 GPS week: 2204 Day: 6 MJD: 59678.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 9 10 10 3 9 7 8 13 3 | 276 274 276 275 281 276 276 278 276 276 276
2E | 8 16 10 12 16 4 9 8 7 8 3 | 36 35 28 35 43 30 30 30 29 33 31
3 | 9 9 7 10 7 4 8 6 8 11 3 | 23 29 25 23 22 23 28 19 23 20 22
4 | 11 13 11 9 8 5 9 7 11 8 3 | 78 73 70 76 73 73 73 76 80 75 75
5 | 7 10 7 8 7 3 7 6 6 7 2 | 29 27 26 29 26 27 29 28 26 31 27
6 | 6 12 8 14 11 6 10 7 12 6 3 | 33 35 32 35 37 31 30 31 29 33 31
7E | 17 13 8 11 12 4 12 5 11 8 3 | 30 29 26 28 31 27 27 28 31 28 27
8 | 10 11 8 13 7 3 8 6 9 9 3 | 23 25 25 24 24 23 26 20 24 27 22
9 | 8 8 8 10 5 3 7 6 10 8 2 | 21 22 22 19 22 21 25 20 22 20 20
10 | 8 9 8 9 5 4 9 9 7 9 3 | 24 28 24 24 24 23 30 22 22 23 23
X11 | 16 23 --- --- 14 14 --- 9 17 --- 7 | 87 84 --- --- 90 85 --- 86 52 --- 85
12 | 5 16 7 8 9 4 6 5 7 11 3 | 45 50 44 46 40 45 45 43 41 45 43
13 | 7 11 6 11 10 6 10 6 9 12 3 | 21 27 21 22 26 22 27 22 21 26 22
14 | 7 11 7 8 9 5 10 7 8 9 3 | 46 52 49 48 55 48 48 54 50 50 50
15 | 6 12 8 8 9 6 12 7 9 9 3 | 49 59 52 53 54 51 55 49 49 48 51
16 | 7 19 6 8 10 4 8 6 9 6 3 | 20 21 16 19 18 17 19 17 21 22 17
17 | 6 13 5 16 10 4 11 8 8 7 3 | 28 32 26 30 31 29 31 25 33 29 27
18 | 12 22 10 12 16 5 14 10 10 10 4 | 85 81 82 83 81 81 88 82 80 84 82
19 | 9 12 5 10 7 5 11 9 10 9 3 | 37 40 37 40 38 38 37 33 40 40 36
20 | 7 10 6 11 8 6 8 5 6 8 2 | 20 17 20 22 19 19 20 18 19 21 18
X21E | 9 11 9 21 12 11 6 10 7 --- 4 | 12 17 11 13 14 14 13 13 14 --- 12
22 | 7 8 4 10 6 4 7 5 6 9 2 | 25 26 23 30 27 25 24 24 27 26 24
23 | 7 13 5 10 7 4 12 6 7 7 3 | 27 28 26 29 28 24 28 27 22 28 26
24E | 10 15 14 12 21 7 10 8 11 8 4 | 40 40 38 41 35 38 41 37 41 39 38
25 | 6 10 6 8 8 5 7 4 8 6 2 | 22 24 22 23 19 20 26 21 19 25 21
26 | 6 8 6 10 6 3 6 8 7 6 2 | 29 27 26 31 24 27 29 24 28 28 26
27 | 10 10 8 9 13 3 7 6 7 10 3 | 23 24 26 23 24 23 27 20 25 28 23
X28 | 6 13 5 15 7 6 11 7 11 --- 3 | 18 22 18 22 19 18 23 19 21 --- 18
29 | 9 17 6 9 12 4 9 7 9 12 3 | 40 40 37 38 39 38 41 38 40 45 39
30E | 16 18 9 17 10 6 9 6 9 9 4 | 28 38 30 33 36 31 35 33 32 32 31
31E | 7 13 9 8 13 5 7 6 11 5 3 | 31 37 31 35 30 32 35 33 30 35 31
32 | 7 10 6 6 6 4 7 4 8 6 2 | 27 30 27 27 28 27 31 25 30 30 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 11 10 5 9 7 9 9 |T 41 43 39 41 42 40 41 40 40 43 40
WRMS | 8 13 8 10 10 5 9 6 9 8 |NE 44 46 42 43 44 43 44 43 43 45 43
MEDI | 7 12 7 10 9 4 9 6 8 8 |MD 28 29 26 30 28 27 30 27 29 30 27
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 4.2204 GPS week: 2204 MJD: 59672.0-59678.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 9 11 28 |U 11 13 35 |U 8 12 27 |
emr | emr 3058 |U 16 20 30 |U 12 23 56 |U 11 18 33 |
esa | esa 2962 | 13 11 27 |U 11 17 48 | 9 14 29 |
gfz | gfz 2961 |U 10 11 30 |U 9 12 35 |U 8 9 24 |
grg | grg 3057 |U 9 13 25 |U 11 14 36 | 9 10 25 |
igr | igr 3058 | 9 9 24 | 10 14 37 | 8 12 24 |
igs | igs 3058 | 9 9 23 | 10 14 36 | 7 11 24 |
jpl | jpl 3030 | 12 13 26 |U 12 21 45 | 10 17 30 |
mit | mit 3058 |U 9 11 25 |U 10 12 37 |U 8 10 23 |
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 5.2204.0 GPS week: 2204 Day: 0 MJD: 59672.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 11 26 | 10 13 28 | 8 14 24 |
emr | emr 3072 | 13 17 32 | 10 25 52 | 10 19 34 |
esa | esa 2976 | 12 9 27 | 11 18 53 | 8 15 26 |
gfz | gfz 2976 | 8 9 28 | 11 13 35 | 8 10 22 |
grg | grg 3072 | 8 12 21 | 12 18 34 | 10 10 21 |
igr | igr 3072 | 7 7 21 | 11 16 38 | 7 14 22 |
igs | igs 3072 | 7 7 22 | 10 15 35 | 7 13 21 |
jpl | jpl 3072 | 10 11 25 | 11 20 48 | 8 20 25 |
mit | mit 3072 | 6 9 23 | 10 15 37 | 8 11 21 |
Table 5.2204.1 GPS week: 2204 Day: 1 MJD: 59673.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 9 27 | 8 13 41 | 9 9 27 |
emr | emr 3072 | 12 17 36 | 12 23 57 | 12 16 33 |
esa | esa 2976 | 12 8 21 | 9 15 58 | 9 11 32 |
gfz | gfz 2975 | 10 9 26 | 7 10 37 | 7 7 24 |
grg | grg 3071 | 9 9 23 | 10 13 42 | 10 7 27 |
igr | igr 3072 | 9 7 22 | 8 12 42 | 8 8 24 |
igs | igs 3072 | 8 7 21 | 8 12 43 | 8 8 24 |
jpl | jpl 3072 | 10 9 25 | 10 18 56 | 10 13 31 |
mit | mit 3072 | 8 7 22 | 8 10 40 | 8 7 23 |
Table 5.2204.2 GPS week: 2204 Day: 2 MJD: 59674.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 11 30 | 10 12 38 | 10 13 26 |
emr | emr 3072 | 21 25 27 | 10 16 59 | 10 20 29 |
esa | esa 2976 | 10 10 29 | 9 14 46 | 8 15 24 |
gfz | gfz 2975 | 10 11 27 | 6 7 36 | 9 9 20 |
grg | grg 3070 | 9 13 27 | 7 16 37 | 9 13 24 |
igr | igr 3072 | 8 11 25 | 8 11 36 | 9 13 24 |
igs | igs 3072 | 8 11 22 | 8 10 35 | 8 13 23 |
jpl | jpl 3072 | 16 19 29 | 9 15 42 | 9 20 28 |
mit | mit 3072 | 8 13 27 | 8 12 39 | 9 10 22 |
Table 5.2204.3 GPS week: 2204 Day: 3 MJD: 59675.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 12 28 | 14 13 35 | 8 16 30 |
emr | emr 3072 | 13 18 28 | 15 21 54 | 9 20 32 |
esa | esa 2976 | 12 11 24 | 13 16 45 | 8 16 29 |
gfz | gfz 2975 | 9 13 29 | 12 11 28 | 9 11 23 |
grg | grg 3072 | 8 14 24 | 12 15 34 | 7 12 25 |
igr | igr 3072 | 9 10 24 | 13 12 36 | 8 14 26 |
igs | igs 3072 | 8 10 23 | 13 13 35 | 7 14 25 |
jpl | jpl 3072 | 11 13 23 | 13 20 45 | 8 23 31 |
mit | mit 3072 | 8 12 23 | 13 11 36 | 8 12 25 |
Table 5.2204.4 GPS week: 2204 Day: 4 MJD: 59676.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 11 32 | 12 12 39 | 7 10 28 |
emr | emr 3072 | 19 21 28 | 13 23 64 | 10 13 36 |
esa | esa 2976 | 15 11 30 | 11 16 52 | 8 13 33 |
gfz | gfz 2975 | 13 12 36 | 8 13 41 | 7 9 25 |
grg | grg 3072 | 12 15 27 | 11 13 42 | 7 9 25 |
igr | igr 3072 | 12 9 28 | 10 13 43 | 6 9 26 |
igs | igs 3072 | 12 9 28 | 11 13 42 | 6 9 26 |
jpl | jpl 3072 | 14 9 30 | 14 20 52 | 8 14 29 |
mit | mit 3072 | 11 11 27 | 10 12 41 | 7 9 24 |
Table 5.2204.5 GPS week: 2204 Day: 5 MJD: 59677.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 15 27 | 11 14 31 | 7 15 30 |
emr | emr 2976 | 18 21 32 | 11 27 51 | 15 20 34 |
esa | esa 2880 | 14 14 25 | 11 17 41 | 12 15 30 |
gfz | gfz 2879 | 12 15 30 | 10 11 35 | 8 12 29 |
grg | grg 2976 | 10 16 23 | 12 11 28 | 9 13 30 |
igr | igr 2976 | 10 12 23 | 10 14 31 | 8 13 29 |
igs | igs 2976 | 10 12 21 | 10 14 31 | 8 13 27 |
jpl | jpl 2880 | 11 12 23 | 11 22 35 | 10 18 33 |
mit | mit 2976 | 9 13 24 | 11 10 32 | 7 12 27 |
Table 5.2204.6 GPS week: 2204 Day: 6 MJD: 59678.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 9 30 | 13 17 33 | 9 9 23 |
emr | emr 3072 | 16 21 31 | 14 27 53 | 15 20 36 |
esa | esa 2976 | 13 12 31 | 13 22 40 | 10 13 29 |
gfz | gfz 2974 | 11 9 38 | 10 17 35 | 10 7 26 |
grg | grg 3071 | 11 12 30 | 12 16 36 | 9 7 22 |
igr | igr 3072 | 10 10 29 | 12 20 32 | 9 10 22 |
igs | igs 3072 | 9 9 28 | 12 19 33 | 9 9 22 |
jpl | jpl 2976 | 13 16 28 | 14 31 40 | 13 14 30 |
mit | mit 3072 | 10 10 29 | 12 17 35 | 9 9 22 |
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 6.2204 GPS week: 2204 MJD: 59672.500-59678.500
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 5 52 -46 -9 | 10 27
| 15 13 32 71 3 | 1
emr uuuuu | -44 -21 51 99 2 | 3 29
| 31 13 53 16 12 | 3
esa uuuuu | 31 0 40 205 -8 | 40 46
| 14 17 70 76 3 | 2
gfz uuuuu | 18 -11 152 140 2 | 30 40
| 10 19 149 126 6 | 4
grg uuuuu | 4 11 17 -29 -6 | 6 24
| 20 11 50 41 5 | 2
igr xxxxx | 3 8 23 -20 -2 | 1 24
| 8 11 65 55 4 | 2
irf xxxxx | 6 6 -38 -14 3 | 2 26
| 9 7 23 17 5 | 3
jpl uuuuu | 31 -19 93 15 15 | 32 39
| 26 9 41 39 6 | 6
mit uuuuu | -9 9 -131 -146 9 | 24 35
| 15 14 63 31 4 | 4
ngs uuuuu | -49 14 -149 -154 5 | 14 31
| 41 27 132 142 2 | 4
sio xxxxx | 35 -12 -441 -220 11 | 31 39
| 76 41 123 160 6 | 4
Table 7.2204.0 GPS week: 2204 Day: 0 MJD: 59672.500
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 14 43 -169 -13 | 11 27
emr uuuuu | -59 -4 69 96 3 | 3 29
esa uuuuu | 52 -3 22 270 -5 | 41 47
gfz uuuuu | 22 4 73 301 -1 | 27 38
grg uuuuu | 18 -8 -3 -50 -10 | 7 23
igr xxxxx | -3 -7 0 65 -11 | 3 26
irf xxxxx | -4 8 -47 -28 1 | 1 27
jpl uuuuu | 13 -23 51 -61 23 | 26 34
mit uuuuu | -30 24 -68 -158 7 | 22 33
ngs uuuuu | -10 -17 -129 -85 6 | 10 28
sio xxxxx | -63 63 -543 -482 11 | 30 39
Table 7.2204.1 GPS week: 2204 Day: 1 MJD: 59673.500
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 12 67 -85 -10 | 9 26
emr uuuuu | -37 -26 16 109 11 | 0 27
esa uuuuu | 20 3 -23 104 -6 | 39 45
gfz uuuuu | 13 17 -76 181 4 | 26 37
grg uuuuu | -5 10 -38 -15 -10 | 5 22
igr xxxxx | -3 14 8 -8 -5 | 0 24
irf xxxxx | 4 -7 -36 2 3 | -2 25
jpl uuuuu | 22 -11 105 1 6 | 25 32
mit uuuuu | -9 4 -82 -105 6 | 20 30
ngs uuuuu | -40 -28 44 -123 7 | 9 27
sio xxxxx | -86 5 -303 -349 4 | 27 34
Table 7.2204.2 GPS week: 2204 Day: 2 MJD: 59674.500
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 1 104 12 -10 | 11 27
emr uuuuu | -17 -16 8 115 8 | 2 29
esa uuuuu | 39 18 -71 194 -4 | 41 47
gfz uuuuu | 20 -20 52 22 -3 | 29 41
grg uuuuu | -19 16 -29 -56 -9 | 7 24
igr xxxxx | 1 25 19 -64 -1 | 1 25
irf xxxxx | 13 2 -31 -20 4 | 0 26
jpl uuuuu | 48 -22 82 42 18 | 30 37
mit uuuuu | -6 -18 -83 -126 11 | 22 34
ngs uuuuu | -100 42 -13 -146 3 | 13 31
sio xxxxx | 68 -16 -380 -171 9 | 29 37
Table 7.2204.3 GPS week: 2204 Day: 3 MJD: 59675.500
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 -17 3 -53 -5 | 10 27
emr uuuuu | -31 -44 57 111 -18 | 2 29
esa uuuuu | 46 22 47 124 -7 | 40 47
gfz uuuuu | 19 -31 120 50 9 | 29 41
grg uuuuu | -14 21 49 -90 -6 | 6 25
igr xxxxx | -7 6 90 -109 1 | 0 25
irf xxxxx | 17 8 -22 -35 10 | 0 26
jpl uuuuu | 71 -25 86 15 16 | 31 38
mit uuuuu | -5 9 -118 -128 17 | 23 34
ngs uuuuu | -93 37 -123 25 8 | 14 31
sio xxxxx | 79 -29 -625 -205 4 | 30 37
Table 7.2204.4 GPS week: 2204 Day: 4 MJD: 59676.500
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 | -14 -3 31 -25 -6 | 9 26
emr uuuuu | -10 -23 18 70 -3 | 0 30
esa uuuuu | 25 1 122 207 -12 | 38 45
gfz uuuuu | 14 -21 326 -25 9 | 29 40
grg uuuuu | -9 -1 35 -27 -7 | 4 24
igr xxxxx | 14 5 92 -26 1 | -1 24
irf xxxxx | 13 8 -37 -15 7 | 0 26
jpl uuuuu | 46 -9 108 60 15 | 32 39
mit uuuuu | 16 18 -193 -150 10 | 23 34
ngs uuuuu | -75 17 -268 -84 5 | 13 31
sio xxxxx | 100 1 -508 -125 16 | 29 37
Table 7.2204.5 GPS week: 2204 Day: 5 MJD: 59677.500
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 4 67 53 -12 | 10 28
emr uuuuu | -51 -14 31 87 17 | 1 31
esa uuuuu | 24 -14 107 220 -11 | 38 45
gfz uuuuu | 1 6 286 187 -5 | 31 44
grg uuuuu | 27 15 104 32 -4 | 5 25
igr xxxxx | 12 -1 47 -9 -2 | 0 26
irf xxxxx | -1 12 -9 -13 0 | 3 29
jpl uuuuu | -7 -12 46 33 9 | 37 45
mit uuuuu | -9 6 -140 -202 4 | 27 39
ngs uuuuu | 1 9 -293 -240 6 | 15 34
sio xxxxx | 67 -47 -428 -221 16 | 33 43
Table 7.2204.6 GPS week: 2204 Day: 6 MJD: 59678.500
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 | 29 20 48 -55 -7 | 13 26
emr uuuuu | -102 -18 159 108 -5 | 9 27
esa uuuuu | 14 -28 75 318 -11 | 42 46
gfz uuuuu | 34 -30 278 264 -1 | 37 44
grg uuuuu | 29 20 1 6 4 | 9 23
igr xxxxx | 7 16 -97 10 0 | 6 22
irf xxxxx | -2 12 -83 13 -4 | 9 23
jpl uuuuu | 25 -32 169 14 17 | 43 48
mit uuuuu | -22 17 -236 -149 6 | 33 39
ngs uuuuu | -24 35 -265 -421 3 | 23 32
sio xxxxx | 83 -64 -301 16 19 | 40 46
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