[IGSREPORT-27555] Wk 2127 IGS Final Orbits
acc
acc at igs.org
Thu Oct 29 21:01:10 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2127 (Oct 11, 2020 - Oct 17, 2020)
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:
igs2127[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2127[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2127[0-6].cls IGS GPS clock combination summary report.
igs21277.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21277.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 | MAYG SCH2 SGOC TIXI SCH2 TIXI
0 | EMR | HARB
0 | ESA | CPVG DJIG PTBB CPVG DJIG PTBB
0 | GFZ | ANKR
0 | GRG | 13 CCJ2 CPVG CPVG SCOR SGOC
1 | COD | HOB2 LHAZ TIXI HOB2 LHAZ TIXI
1 | ESA | GMSD PTBB GMSD PTBB
1 | GRG | 21 SVTL SVTL
2 | COD | HOB2 TIXI HOB2 TIXI
2 | ESA | PTBB STHL PTBB
2 | GRG | 13 22 SVTL
3 | COD | CCJ2 SGOC TIXI TIXI
3 | EMR | SFER
3 | ESA | PTBB SFER PTBB SFER
3 | GFZ | SFER SFER
3 | GRG | 13 CCJ2 SVTL CCJ2 SVTL
4 | COD | 21 DAV1 SGOC TIXI YELL DAV1 SGOC TIXI YELL
4 | ESA | CCJ2 PTBB PTBB
4 | GFZ | YELL
4 | GRG | 21 21 CCJ2
4 | JPL | SVTL
5 | COD | NOVM TIXI TIXI
5 | EMR | SVTL SVTL
5 | ESA | PTBB NOVM PTBB
5 | GFZ | NYA2 NYA2
5 | GRG | 1
5 | MIT | SPT0 SPT0
6 | COD | TIXI TIXI
6 | ESA | PTBB PTBB
6 | GRG | 13 13 DJIG SVTL BRFT DJIG LHAZ SVTL
6 | JPL | SVTL
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 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
----+--------+---------------
3 | SIO | ALL (high Transformation - See Table 2)
3 | COD | 30
3 | GFZ | 30
3 | JPL | 30
3 | NGS | 30
3 | SIO | 30
7. 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 G30 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .5 -.0 1.1 1 0 -2 -.63
EMR | 0 | 7.5 3.8 20.4 -9 9 1 -.42
ESA | 0 | -.9 -1.1 .8 -7 -14 6 -.49
GFZ | 0 | .2 -.0 .8 0 -3 6 -.45
GRG | 0 | 6.5 3.8 7.0 5 -27 -22 -.21
JPL | 0 | 10.1 6.1 15.1 7 -2 -7 -.37
MIT | 0 | 6.3 4.6 8.3 11 -9 -8 -.21
NGS | 0 | 5.8 7.6 8.0 36 -58 31 -.34
SIO | 0 | 6.5 8.5 24.7 239 -130 -23 -.38
COD | 1 | .4 -.2 .9 -1 0 5 -.67
EMR | 1 | 2.9 5.4 21.0 -1 13 6 -.47
ESA | 1 | -.4 -.8 1.7 -9 5 -11 -.76
GFZ | 1 | .4 -.2 .9 -2 -10 6 -.59
GRG | 1 | 2.6 3.5 12.8 2 -66 41 -.06
JPL | 1 | 6.8 1.5 16.1 -7 -18 -4 -.53
MIT | 1 | 4.3 6.7 9.5 19 15 25 -.26
NGS | 1 | .2 9.0 18.4 69 -81 42 -.31
SIO | 1 | .7 12.2 21.5 317 19 13 -.45
COD | 2 | .4 .0 1.4 0 4 -1 -.69
EMR | 2 | 5.7 4.4 24.4 -5 15 22 -.50
ESA | 2 | -.1 -1.1 1.2 -9 -2 9 -.65
GFZ | 2 | .4 .1 .6 3 -9 10 -.54
GRG | 2 | 1.5 5.6 7.1 -1 -52 14 -.06
JPL | 2 | 11.8 2.7 20.0 3 -8 -1 -.39
MIT | 2 | 3.9 6.0 14.3 11 -35 -41 -.37
NGS | 2 | -4.5 -.1 21.5 -18 -18 28 -.19
SIO | 2 | 2.0 11.7 26.4 329 -38 12 -.44
COD | 3 | .7 .0 1.0 1 2 5 -.62
EMR | 3 | 7.6 .7 25.0 4 11 8 -.31
ESA | 3 | -.5 -.3 1.9 -22 9 -19 -.68
GFZ | 3 | .4 .3 .9 -1 -11 -2 -.45
GRG | 3 | 5.8 5.6 5.3 -8 -34 11 -.11
JPL | 3 | 4.0 3.7 16.9 17 -4 -12 -.35
MIT | 3 | 5.0 7.6 11.9 42 -17 1 -.30
NGS | 3 | .1 3.4 19.0 28 -44 5 -.28
SIO | 3 | -12.0 13.7 36.9 398 247 102 -.14
COD | 4 | .5 -.1 .9 2 -1 14 -.58
EMR | 4 | 5.1 9.4 27.1 -14 26 17 -.31
ESA | 4 | -.8 -.6 1.1 -18 -1 17 -.58
GFZ | 4 | .2 .3 1.0 3 -1 7 -.45
GRG | 4 | 7.7 7.5 3.2 -3 -21 13 -.18
JPL | 4 | 12.8 2.1 19.3 14 3 -2 -.27
MIT | 4 | 4.9 5.9 18.0 -20 -8 75 -.30
NGS | 4 | 2.0 5.0 28.9 26 -105 60 -.29
SIO | 4 | 6.7 7.9 29.1 227 -139 13 -.48
COD | 5 | .5 .1 .8 2 0 5 -.51
EMR | 5 | 11.2 5.4 22.8 -8 25 17 -.09
ESA | 5 | .1 -1.5 .9 -16 -4 13 -.55
GFZ | 5 | .5 .1 .4 7 -3 11 -.41
GRG | 5 | 6.7 4.2 5.9 -3 -50 27 .01
JPL | 5 | 16.6 -4.8 15.5 5 -8 6 -.39
MIT | 5 | 7.0 6.6 16.6 -13 -11 10 -.21
NGS | 5 | 7.7 .1 17.0 -2 -65 71 -.25
SIO | 5 | 7.5 6.7 34.4 225 -200 65 -.31
COD | 6 | .5 .1 .7 -1 0 3 -.48
EMR | 6 | 7.8 5.2 29.6 -8 26 14 -.12
ESA | 6 | -.5 -1.3 .3 -30 -2 9 -.50
GFZ | 6 | .1 .1 .5 6 -5 3 -.27
GRG | 6 | 5.3 3.8 .4 -3 -56 25 -.19
JPL | 6 | 8.1 2.4 14.9 16 9 -13 -.71
MIT | 6 | 4.9 2.9 19.3 -32 1 42 -.13
NGS | 6 | 6.7 -.0 27.4 36 -76 21 -.21
SIO | 6 | 6.0 6.5 31.5 243 -116 93 -.52
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://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 1.2127.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2127.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 2.2127.[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 3.2127.[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 5.2127.0-6). 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 2127 summary. (Oct 11, 2020 - Oct 17, 2020)
Table 1.2127.a GPS week: 2127 MJD: 59133.000-59139.000
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 754| -1 0 -3 -9 -3 11 -.08 7 7 | -558 -105 5 109
| 0 0 1 15 16 11 .02 | 292 462
emr 79| 1 -2 14 -9 -2 7 .13 13 13 | 207022 -184 13 160
| 1 1 1 11 14 9 .02 | 601 856
esa 149| -1 0 2 2 -4 -8 -.01 10 10 | -786 -507 8 85
| 0 0 1 8 13 11 .02 | 399 700
gfz 178| 0 -2 -6 -1 -3 -12 .15 10 10 | -202 24 82 660
| 0 0 2 26 18 8 .02 | 348 463
grg 99| 1 1 -4 0 -7 25 -.07 11 10 | -31 -8 9 137
| 0 0 4 12 16 15 .03 | 230 437
igr n/a| -1 0 -3 -5 -14 -13 .04 4 4 | 5567 -396 11 90
| 0 0 0 10 14 11 .02 | 1205 1027
jpl 80| 0 0 5 12 -6 -16 .16 9 9 | -267 -403 10 76
| 0 1 1 7 10 16 .01 | 1118 970
mit 368| 0 0 -1 -6 -9 10 -.05 6 6 | 4614 -456 20 1148
| 0 0 1 25 24 32 .01 | 1617 1015
ngs 146| 0 0 4 7 41 -21 -.07 10 10 | -522 -156 919 2106
| 0 0 3 23 40 22 .02 | 245 355
sio 358| 0 0 -4 31 41 4 -.07 12 10 | --- --- --- ---
| 1 0 1 54 139 33 .02 | --- ---
Table 1.2127.b GPS week : 2127 MJD: 59133.000-59139.000
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 3 3 4 10 4 |
2 | 3 3 3 3 3 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 4 4 4 4 4 4 4 |
5 | 3 2 2 3 3 3 3 |
6 | 3 3 3 3 3 3 3 |
7 | 4 3 3 4 3 3 4 |
8 | 4 5 4 5 4 4 4 |
9 | 4 4 4 4 4 3 4 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 4 3 3 4 3 3 3 |
13 | 3 3 4 3 3 3 3 |
15 | 3 3 3 3 3 3 3 |
16 | 3 3 3 4 3 3 3 |
17 | 3 3 3 4 3 3 3 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 4 3 |
20 | 3 3 3 3 3 3 3 |
21 | 3 4 3 3 3 3 4 |
22 | 3 3 3 4 3 2 3 |
23 | 3 3 3 4 4 4 4 |
24 | 4 4 5 5 5 5 4 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 3 3 3 |
27 | 4 4 4 4 4 4 4 |
28 | 2 3 3 3 3 3 3 |
29 | 5 4 4 4 4 4 4 |
30 | 4 4 4 26 4 5 5 |
31 | 4 3 3 4 4 4 4 |
32 | 3 3 3 3 3 3 4 |
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 2.2127.0 GPS week: 2127 Day: 0 MJD: 59133.000
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 755| 0 0 -2 -9 19 15 -.10 7 7 | -998 545 5 101
emr 80| 0 -3 14 -6 -10 19 .12 13 13 | 207856 -288 15 175
esa 149| 0 0 4 12 -5 0 -.03 11 11 | -1091 5 8 88
gfz 177| 0 -1 -7 -20 -32 -2 .17 11 11 | 67 -124 82 653
grg 106| 1 1 0 9 -13 22 -.01 10 9 | -349 674 9 129
igr n/a| -1 0 -2 8 -2 1 .03 4 4 | 7425 -302 11 83
jpl 80| 0 0 6 21 7 0 .16 9 9 | 1397 -376 9 61
mit 368| 0 1 -3 -19 -9 28 -.06 6 6 | 6886 -326 19 1486
ngs 150| 0 0 1 37 -9 -62 -.06 10 10 | -654 123 608 2010
sio 363| -1 0 -2 -12 38 -37 -.05 10 9 | --- --- --- ---
Table 2.2127.1 GPS week: 2127 Day: 1 MJD: 59134.000
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 754| -1 0 -1 -22 -18 4 -.08 7 7 | -570 -113 5 109
emr 80| 0 -1 15 -27 -12 14 .14 14 14 | 207552 -953 14 183
esa 149| 0 0 4 -1 -23 -9 -.04 11 10 | -1341 424 7 75
gfz 173| 0 -3 -6 -37 -22 -11 .14 11 12 | -384 237 83 685
grg 83| 1 0 0 -18 -16 2 -.06 12 11 | -78 177 10 157
igr n/a| -1 0 -2 -15 -38 -16 .03 4 4 | 6929 -1419 11 85
jpl 80| 0 -1 3 17 -20 -33 .16 9 9 | 846 -1212 9 78
mit 368| 0 0 -3 33 -1 21 -.04 5 5 | 6033 -1488 18 929
ngs 149| 0 1 4 -7 0 -6 -.05 9 9 | -583 -105 1057 2255
sio 365| 0 0 -4 30 103 15 -.05 10 9 | --- --- --- ---
Table 2.2127.2 GPS week: 2127 Day: 2 MJD: 59135.000
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 756| -1 0 -1 -19 -7 7 -.06 7 7 | -472 -224 6 109
emr 80| 0 0 13 -7 12 16 .15 13 13 | 206392 65 12 149
esa 149| 0 0 2 -11 20 9 -.02 10 9 | -885 -528 8 79
gfz 179| 0 -2 -10 -16 8 0 .18 11 10 | -193 -207 83 675
grg 85| 1 2 0 0 8 31 -.11 13 11 | 60 -237 11 145
igr n/a| 0 0 -2 -6 -3 2 .06 3 3 | 5443 -400 11 92
jpl 80| 0 -2 5 4 -13 4 .17 9 9 | -613 -293 11 78
mit 368| 0 1 -2 -5 -57 -32 -.04 6 5 | 4577 -499 20 1084
ngs 148| -1 0 7 44 94 -18 -.06 10 10 | -473 -208 1027 2063
sio 359| 1 0 -5 33 9 17 -.07 10 8 | --- --- --- ---
Table 2.2127.3 GPS week: 2127 Day: 3 MJD: 59136.000
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 758| -1 1 -4 -22 18 11 -.10 7 7 | -51 -859 7 118
emr 80| 3 -2 12 -12 -18 2 .15 12 12 | 206808 -220 11 171
esa 149| -2 1 3 3 -7 -12 .00 9 9 | -149 -1823 10 99
gfz 182| -1 -2 -4 31 -8 -19 .11 10 10 | 58 -510 89 651
grg 108| 1 1 -6 -11 -5 14 -.09 11 9 | 190 -350 9 122
igr n/a| 0 0 -3 -8 -20 -18 .02 4 4 | 5409 -1051 11 100
jpl 80| 0 -2 3 14 -13 -20 .17 9 9 | -541 -685 8 60
mit 368| 0 1 -2 16 -1 17 -.05 7 7 | 4889 -1088 23 1158
ngs 149| -1 0 5 -6 19 -2 -.08 9 9 | -52 -819 789 1907
sio 358| -3 -2 -4 75 323 33 -.07 18 14 | --- --- --- ---
Table 2.2127.4 GPS week: 2127 Day: 4 MJD: 59137.000
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 757| -1 0 -3 -6 -8 2 -.07 7 7 | -756 376 5 109
emr 79| 0 0 13 -7 21 -6 .14 12 12 | 207353 -706 13 174
esa 149| -1 0 2 1 1 -19 .03 10 10 | -800 -345 8 91
gfz 182| 0 -3 -8 6 5 -10 .16 11 11 | 264 -316 79 650
grg 100| 1 1 -7 11 12 18 -.06 10 9 | 292 -396 9 136
igr n/a| -1 -1 -4 -1 -15 -30 .03 5 4 | 5117 -793 12 94
jpl 80| 1 0 5 17 -3 -39 .16 10 10 | -132 -1043 12 90
mit 368| 0 0 0 0 -23 63 -.05 6 6 | 4541 -793 22 1475
ngs 147| 0 0 8 2 58 -42 -.11 10 10 | -645 159 1215 2352
sio 363| 0 0 -4 -20 -43 -50 -.09 12 10 | --- --- --- ---
Table 2.2127.5 GPS week: 2127 Day: 5 MJD: 59138.000
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 753| 0 0 -3 -6 -11 5 -.08 7 7 | -445 -320 6 112
emr 80| 1 -2 15 9 3 -1 .12 13 13 | 206970 -770 13 151
esa 149| -1 0 1 12 -11 -7 .01 10 10 | -411 -750 8 79
gfz 178| -1 -1 -7 33 8 -23 .18 10 11 | -614 214 79 656
grg 110| 1 1 -5 14 -5 41 -.08 11 10 | -73 -366 9 135
igr n/a| -1 0 -4 6 1 -17 .06 5 4 | 4528 -571 11 98
jpl 80| 1 0 5 12 -8 -13 .15 10 10 | -843 -880 13 83
mit 368| 0 0 1 -27 2 -3 -.06 6 5 | 1977 -676 21 927
ngs 138| 0 0 0 -2 86 -11 -.07 12 11 | -428 -384 873 2251
sio 357| 0 -1 -5 -12 -64 28 -.06 12 10 | --- --- --- ---
Table 2.2127.6 GPS week: 2127 Day: 6 MJD: 59139.000
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 747| -1 0 -3 22 -17 34 -.09 8 8 | -616 -144 5 108
emr 80| 1 -2 15 -16 -11 5 .08 13 13 | 206223 1582 14 120
esa 149| 0 0 0 2 -5 -23 .01 11 10 | -828 -538 9 86
gfz 179| -1 -1 -2 -5 16 -16 .15 8 8 | -614 878 80 652
grg 103| 2 0 -11 -1 -34 47 -.06 11 10 | -259 441 10 138
igr n/a| 0 0 -4 -18 -22 -13 .03 4 4 | 4119 1764 11 83
jpl 80| 0 0 5 1 4 -13 .18 10 10 | -1986 1663 10 85
mit 368| 0 0 0 -40 21 -18 -.05 6 5 | 3398 1676 21 983
ngs 146| 0 0 6 -17 43 -6 -.08 10 9 | -825 136 869 1910
sio 346| 1 0 -4 127 -78 24 -.09 13 12 | --- --- --- ---
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 3.2127.0 GPS week: 2127 Day: 0 MJD: 59133.000
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 11 13 8 11 2 6 4 7 10 3 | 120 120 121 123 119 121 122 121 120 123 120
2 | 8 9 8 9 11 4 9 6 10 8 3 | 25 27 24 25 24 23 22 23 25 29 23
3 | 6 10 7 7 7 3 8 6 6 8 2 | 21 31 26 28 21 22 28 21 25 32 23
4 | 12 16 14 10 12 4 11 5 13 8 4 | 73 63 67 70 70 68 67 66 67 66 67
5 | 6 12 8 9 6 3 7 5 6 6 2 | 30 36 35 33 31 32 39 32 35 36 33
6 | 6 9 10 9 12 4 7 5 13 6 3 | 32 35 35 30 31 31 32 30 28 34 29
7 | 10 11 8 12 15 3 8 5 15 9 3 | 27 25 23 31 21 25 25 27 28 36 24
8 | 6 14 17 13 14 3 13 5 10 9 4 | 29 31 29 29 27 29 32 30 30 39 28
9 | 7 11 14 7 18 4 7 6 8 8 3 | 38 40 41 37 38 38 40 35 35 38 36
10 | 4 11 8 7 5 3 8 5 8 7 2 | 29 36 33 31 28 31 34 29 33 32 31
11E | 10 9 11 7 11 5 9 7 11 11 3 | 20 26 23 26 23 22 24 24 24 33 22
12 | 9 17 11 13 10 4 8 4 7 16 3 | 41 44 43 45 38 43 42 42 41 47 42
13 | 6 12 7 15 6 6 8 4 8 12 3 | 31 37 29 29 30 30 34 32 31 36 30
15 | 8 12 8 14 6 4 5 7 7 8 3 | 32 39 33 27 34 31 35 32 34 33 32
16 | 7 18 8 9 8 2 6 5 8 9 3 | 28 28 28 29 27 27 27 27 26 34 27
17E | 6 12 9 8 12 5 9 8 13 7 3 | 53 56 54 54 58 55 54 56 56 63 54
18 | 8 14 20 15 8 4 10 5 13 11 4 | 54 51 50 64 55 55 56 56 56 62 55
19E | 11 14 9 12 9 4 5 6 10 20 3 | 33 31 30 31 32 30 29 31 31 38 30
20 | 5 7 10 10 6 5 5 4 9 7 2 | 22 24 24 24 21 24 24 25 26 30 23
21 | 10 15 6 8 11 4 7 8 9 8 3 | 22 31 26 24 19 24 26 24 26 32 23
22 | 5 8 7 11 7 3 6 4 4 8 2 | 46 47 48 44 48 44 45 45 46 53 45
23 | 6 14 11 9 7 4 15 6 8 7 3 | 50 49 50 52 50 50 49 50 49 55 50
24 | 11 21 17 8 10 3 12 7 9 14 4 | 28 31 32 32 26 29 30 28 26 36 27
25 | 7 10 12 10 6 4 8 4 10 9 3 | 30 31 33 33 27 31 33 29 29 34 30
26 | 3 10 10 8 6 3 7 6 9 7 2 | 28 30 31 32 29 29 31 27 27 35 28
27 | 4 16 19 12 8 3 11 4 6 9 3 | 25 35 26 29 27 27 31 27 28 36 27
28 | 5 9 6 7 8 3 7 4 8 7 2 | 23 24 24 24 20 23 25 21 26 29 22
29E | 8 19 9 27 17 6 9 7 11 10 4 | 53 52 52 58 57 54 54 52 54 55 53
30 | 8 14 14 13 12 4 11 10 13 11 4 | 995 730 993 995 700 995 996 998 997 994 996
31 | 7 13 7 11 9 3 8 7 11 14 3 | 28 27 26 32 27 28 28 28 27 39 27
32 | 5 12 13 6 6 3 8 5 11 8 3 | 38 44 40 39 40 39 42 36 43 38 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 11 11 10 4 9 6 10 10 |T 67 61 68 69 58 68 69 67 68 73 67
WRMS | 7 13 11 11 9 4 9 6 10 9 |NE 80 70 81 82 66 80 82 80 81 85 80
MEDI | 7 12 10 9 9 4 8 5 9 8 |MD 30 35 33 32 30 31 33 30 31 36 30
Table 3.2127.1 GPS week: 2127 Day: 1 MJD: 59134.000
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 15 8 12 3 8 4 6 11 3 | 118 118 117 117 118 118 119 115 114 119 117
2 | 7 12 5 11 12 4 8 5 9 8 3 | 23 25 22 27 24 24 22 21 26 29 22
3 | 6 14 7 6 10 3 7 6 11 14 3 | 19 28 21 25 17 20 26 18 21 31 20
4 | 12 17 12 11 12 4 10 5 10 8 3 | 56 51 56 56 52 54 52 54 52 58 53
5 | 6 11 6 6 8 3 7 4 6 9 2 | 21 26 21 22 18 22 25 19 20 24 20
6 | 6 12 11 6 14 2 9 4 7 9 3 | 31 33 32 32 29 31 31 28 33 35 30
7 | 8 15 8 10 17 4 9 5 9 8 3 | 29 29 27 33 25 28 26 29 30 34 28
8 | 6 15 18 14 27 3 13 6 11 11 4 | 31 30 30 32 33 31 31 29 32 39 29
9 | 5 14 14 10 21 4 9 5 8 9 3 | 36 40 40 40 38 37 39 37 35 40 37
10 | 4 12 6 5 7 3 9 5 9 5 2 | 23 30 26 23 22 24 30 22 22 27 23
11E | 9 14 13 14 15 4 8 7 9 14 3 | 22 27 26 27 23 25 26 26 27 38 24
12 | 8 16 6 11 8 4 8 4 9 11 3 | 29 34 30 33 29 31 34 29 31 37 31
13 | 5 11 7 12 8 6 8 5 9 8 2 | 32 41 35 31 32 33 37 33 35 40 34
15 | 6 9 7 11 9 3 7 5 6 5 2 | 30 38 32 25 33 30 32 32 29 33 30
16 | 7 22 7 10 9 5 7 7 9 10 3 | 27 27 26 29 25 25 25 25 28 32 26
17 | 5 11 9 10 10 5 8 6 7 7 2 | 53 54 53 56 54 53 56 53 58 52 53
18 | 8 13 19 12 10 5 12 6 8 15 4 | 41 42 42 46 42 42 43 43 41 55 42
19E | 10 14 7 12 9 4 9 7 12 11 3 | 28 27 26 31 27 26 25 27 27 32 26
20 | 5 9 9 8 7 3 6 5 12 7 2 | 18 21 21 16 16 18 21 18 21 27 18
21 | 8 12 10 10 25 4 7 6 11 10 3 | 21 26 25 25 19 24 25 22 27 33 22
22 | 5 10 10 7 10 4 7 6 10 13 3 | 58 59 60 59 56 58 58 58 61 62 58
23 | 4 13 10 8 7 3 17 5 12 7 3 | 27 26 29 30 27 27 26 27 28 34 26
24 | 7 30 13 13 10 5 14 4 9 8 4 | 30 39 33 33 30 31 32 29 36 42 31
25 | 6 12 8 9 6 3 7 3 10 12 2 | 25 30 29 28 24 27 31 24 25 32 26
26 | 5 11 7 10 9 5 7 4 6 11 2 | 22 25 23 25 22 22 27 20 25 29 22
27 | 5 16 18 13 11 5 12 4 7 8 3 | 24 28 24 26 25 25 26 24 28 32 24
28 | 4 9 7 11 7 3 7 5 6 8 2 | 19 24 20 23 17 20 24 20 21 25 20
29E | 8 17 9 20 11 5 9 6 14 9 4 | 45 49 46 46 50 47 48 49 55 55 48
30 | 6 14 15 14 14 4 11 9 9 10 4 | 9999 794 9999 9999 784 9999 9999 9999 9999 9999 9999
31 | 8 15 6 9 11 3 7 6 8 12 3 | 30 33 30 34 31 32 32 30 36 42 31
32 | 5 13 11 8 8 3 7 5 10 10 3 | 38 45 41 39 40 40 44 40 41 44 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 11 11 12 4 9 5 9 10 |T 33 61 34 35 57 34 35 33 35 40 33
WRMS | 7 14 10 12 11 4 9 5 9 9 |NE 33 71 34 35 67 34 35 33 35 40 33
MEDI | 6 13 9 10 10 4 8 5 9 9 |MD 29 30 29 31 29 28 31 28 29 34 28
Table 3.2127.2 GPS week: 2127 Day: 2 MJD: 59135.000
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 13 9 13 3 7 5 13 10 3 | 105 104 104 107 105 106 105 107 109 102 105
2 | 6 9 8 9 10 4 9 7 13 7 3 | 26 26 24 27 27 26 25 26 30 31 25
3 | 6 11 7 10 12 3 7 5 8 9 2 | 23 33 27 28 21 25 30 23 25 30 24
4 | 9 15 12 12 15 5 11 5 9 10 3 | 56 54 57 62 60 55 53 54 52 60 55
5 | 4 11 6 8 7 3 6 4 10 5 2 | 28 32 29 33 28 30 34 26 33 33 29
6 | 5 11 10 10 11 3 8 5 9 5 2 | 30 32 33 28 30 30 31 29 30 33 29
7 | 6 12 7 11 17 2 8 5 11 6 3 | 30 31 27 36 26 30 31 29 33 34 28
8 | 6 14 17 11 15 4 13 6 8 8 3 | 34 36 35 36 37 34 36 34 36 43 34
9 | 5 12 13 11 24 3 9 5 9 5 3 | 32 38 37 37 40 35 39 35 37 40 35
10 | 6 10 7 7 6 3 8 6 11 9 2 | 24 31 25 25 23 26 30 21 31 27 24
11E | 9 9 10 13 12 5 8 8 5 14 3 | 21 25 24 25 22 23 25 23 21 35 21
12 | 8 14 8 9 10 3 8 7 13 9 3 | 36 38 37 38 34 38 40 36 44 37 37
13 | 6 10 7 11 28 4 8 4 12 10 3 | 30 36 31 32 41 31 35 31 39 37 31
15 | 6 9 6 10 9 2 7 7 11 7 2 | 35 42 36 40 38 36 38 36 46 40 37
16 | 6 20 5 7 11 3 7 6 7 11 3 | 28 32 29 32 28 30 31 28 31 36 28
17 | 7 10 8 10 16 3 8 7 8 7 3 | 42 44 42 44 46 44 45 43 45 45 42
18 | 8 15 19 15 8 4 11 6 13 8 4 | 46 49 48 53 46 48 51 50 50 57 48
19E | 8 11 10 14 9 4 9 7 10 18 3 | 32 29 29 32 30 30 28 31 32 44 30
20 | 6 8 6 12 8 4 7 6 9 10 2 | 21 22 20 20 20 21 22 20 25 27 20
21 | 9 11 7 8 12 4 7 6 10 9 3 | 24 29 25 25 26 25 28 26 23 35 24
22 | 8 9 8 9 19 4 7 7 10 8 3 | 33 41 38 40 42 38 40 39 41 40 37
23 | 6 14 8 8 10 3 16 6 9 8 3 | 28 24 27 31 28 28 24 27 32 33 26
24 | 8 28 13 18 12 3 13 5 15 14 4 | 35 39 37 39 33 36 37 35 36 41 34
25 | 8 11 10 8 7 3 8 4 9 11 3 | 33 35 37 37 34 36 38 34 37 39 34
26 | 7 11 7 13 8 3 7 4 9 8 2 | 27 30 26 30 26 26 29 24 25 34 25
27 | 5 15 17 11 8 2 12 3 6 10 3 | 30 32 33 33 32 32 35 30 29 38 30
28 | 5 10 6 10 8 4 6 5 10 8 2 | 23 27 26 27 23 25 28 23 27 30 24
29 | 9 18 9 16 18 3 8 8 13 10 4 | 52 50 53 51 47 53 52 51 56 49 51
X30 | 5 15 14 18 --- 4 12 10 10 8 4 | 818 546 810 813 --- 814 816 817 820 807 815
31 | 9 12 7 8 9 3 8 5 15 13 3 | 32 33 31 35 30 33 34 32 32 39 31
32 | 5 10 11 7 7 3 7 6 10 14 3 | 33 36 34 33 35 34 34 33 33 42 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 10 11 13 3 9 6 10 10 |T 59 53 60 62 35 60 62 59 62 65 59
WRMS | 7 13 9 10 11 3 9 5 10 8 |NE 70 61 71 73 36 71 73 70 73 75 70
MEDI | 6 11 8 10 10 3 8 6 10 9 |MD 32 33 33 33 30 32 34 31 33 38 31
Table 3.2127.3 GPS week: 2127 Day: 3 MJD: 59136.000
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 8 12 10 11 4 6 6 8 17 3 | 96 92 92 93 97 96 96 95 94 95 95
2 | 6 10 7 8 9 5 10 8 8 15 3 | 23 27 25 25 22 23 23 21 24 31 23
3 | 4 11 5 11 9 4 9 6 8 14 3 | 20 28 22 26 21 22 28 18 20 37 21
4 | 9 14 11 9 14 4 9 7 7 15 3 | 55 45 50 50 56 50 49 51 50 57 50
5 | 5 11 9 8 8 3 7 8 7 14 3 | 26 31 31 32 25 27 32 26 28 32 28
6 | 5 10 11 9 11 4 6 8 11 13 3 | 25 29 30 28 25 26 28 24 27 39 26
7 | 7 13 8 9 15 4 8 6 9 33 3 | 29 29 26 33 28 29 29 31 30 39 28
8 | 5 14 15 14 14 3 11 8 13 21 4 | 25 30 27 29 25 28 32 27 31 41 27
9 | 3 17 13 12 20 3 7 5 10 18 4 | 24 29 26 27 32 25 28 24 22 36 25
10 | 6 11 6 8 7 3 10 6 6 11 2 | 20 31 23 24 21 23 30 19 19 26 22
11E | 9 7 8 14 10 3 7 7 10 24 3 | 23 30 28 32 27 29 30 30 27 46 27
12 | 8 13 6 10 11 2 8 7 11 13 3 | 35 36 32 35 30 34 34 33 32 39 33
13 | 6 9 8 6 11 4 7 5 11 31 3 | 24 31 24 29 28 26 27 24 27 46 25
15 | 5 10 8 8 8 3 9 5 11 17 3 | 31 37 30 34 31 31 31 31 32 47 31
16 | 8 19 5 6 8 4 7 10 9 14 3 | 22 26 23 25 23 24 26 25 23 33 23
17 | 8 10 7 15 16 3 10 8 10 16 4 | 30 32 30 33 29 29 31 27 33 43 29
18 | 8 13 17 12 8 4 10 9 7 10 4 | 35 36 33 38 38 35 38 37 31 47 35
19E | 10 11 8 10 9 3 9 8 12 21 3 | 29 27 25 25 27 25 25 27 27 41 26
20 | 6 8 7 7 7 3 7 5 8 14 2 | 15 21 17 16 16 17 21 17 17 24 16
21 | 8 12 6 10 8 4 8 7 8 18 3 | 23 29 26 24 21 24 28 26 23 38 24
22 | 8 10 6 8 11 5 8 11 10 15 3 | 93 95 95 95 91 95 94 98 90 100 94
23 | 7 14 9 8 10 3 17 6 7 13 3 | 29 29 30 32 32 29 30 31 28 39 29
24 | 7 25 13 17 11 4 12 7 12 25 4 | 24 30 25 30 23 25 26 23 23 36 23
25 | 7 10 7 8 7 3 7 6 10 17 3 | 23 28 27 27 22 25 26 23 23 34 24
26 | 6 10 7 8 5 4 8 7 7 11 2 | 31 34 34 33 32 32 36 31 30 40 32
27 | 6 13 16 9 9 4 11 7 9 13 4 | 24 33 27 28 26 28 33 27 31 36 27
28 | 6 9 7 9 9 5 6 6 12 20 3 | 19 25 23 24 19 22 27 22 24 36 22
29 | 10 15 8 11 15 4 8 8 11 14 4 | 34 38 38 36 38 35 37 37 38 43 36
X30 | 119 --- 29 71 --- 42 124 23 113 133 26 | 9999 --- 9999 9999 --- 9999 9999 9999 9999 9999 9999
31 | 10 14 7 10 10 4 8 10 10 16 3 | 31 31 27 31 31 30 30 31 31 41 29
32 | 6 9 12 11 7 3 7 6 8 16 3 | 24 31 27 24 24 24 27 24 27 36 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 9 10 11 4 9 7 9 18 |T 31 35 32 33 32 32 34 32 32 42 31
WRMS | 7 12 9 10 9 4 9 7 9 14 |NE 33 36 34 35 33 34 36 33 33 44 33
MEDI | 7 11 8 9 9 4 8 7 10 16 |MD 25 30 27 29 27 27 30 27 27 39 27
Table 3.2127.4 GPS week: 2127 Day: 4 MJD: 59137.000
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 12 16 11 11 4 8 6 7 11 3 | 119 117 117 121 119 122 118 115 116 117 120
2 | 7 12 7 13 11 5 11 6 12 8 3 | 23 26 24 27 24 24 26 25 29 29 23
3 | 6 11 7 9 7 3 9 4 13 10 3 | 15 28 19 17 17 18 26 15 24 27 17
4 | 10 15 13 13 12 6 10 6 12 10 3 | 53 46 51 59 55 52 47 48 51 57 50
5 | 5 10 6 8 9 4 8 5 8 9 2 | 25 29 26 30 24 26 30 23 29 27 25
6 | 4 10 12 8 11 4 9 4 8 8 2 | 26 30 29 26 26 27 30 25 26 29 25
7 | 8 10 8 12 13 3 6 5 8 12 3 | 27 25 22 32 26 24 25 23 28 30 23
8 | 5 13 13 16 11 4 14 6 13 11 4 | 26 29 28 27 25 26 28 25 30 31 25
9 | 5 15 13 16 17 3 7 4 8 9 3 | 26 32 30 29 33 28 32 27 30 31 27
10 | 8 10 6 6 7 3 9 5 7 10 2 | 19 30 24 26 21 22 30 20 22 23 22
11E | 9 9 11 15 12 7 7 11 12 21 4 | 28 31 28 30 31 28 30 33 32 39 29
12 | 7 14 6 9 11 4 8 7 7 9 3 | 34 38 35 36 35 35 37 34 38 38 34
13 | 5 9 8 8 11 4 8 5 8 10 2 | 23 30 25 26 26 25 32 23 31 32 25
15 | 5 9 6 8 8 3 7 6 7 11 2 | 31 38 32 35 32 31 33 31 33 37 32
16 | 8 18 6 9 8 5 7 7 9 14 3 | 21 24 25 28 23 24 22 23 27 26 22
17 | 7 12 8 8 14 4 11 6 10 7 3 | 24 28 23 24 23 24 28 24 28 29 23
18 | 9 16 18 9 9 4 10 8 12 12 4 | 44 45 45 47 49 45 48 47 49 52 46
19E | 9 13 10 10 8 6 18 6 13 11 3 | 42 44 39 40 42 42 44 43 45 49 41
20 | 9 8 8 9 6 4 7 5 10 10 2 | 14 20 18 18 15 17 20 17 22 24 16
21 | 8 10 7 8 10 4 10 6 10 13 3 | 20 22 22 22 20 20 24 23 24 29 20
22 | 6 8 9 7 7 6 6 6 9 11 2 | 30 34 32 37 34 35 36 31 38 38 32
23 | 7 14 9 10 8 3 17 5 12 8 3 | 24 25 28 30 28 25 24 27 27 32 25
24 | 6 23 13 23 11 6 11 5 13 16 4 | 29 32 35 40 28 33 34 28 30 34 29
25 | 8 10 10 8 8 5 9 7 7 10 3 | 29 32 34 30 29 31 34 28 35 35 29
26 | 7 10 9 9 6 5 7 5 8 11 2 | 26 29 28 28 28 27 29 25 26 30 26
27 | 6 14 15 13 8 5 14 5 10 7 3 | 22 29 26 25 22 24 26 24 31 28 23
28 | 7 11 7 10 8 4 7 4 11 16 3 | 17 21 20 21 16 18 21 17 19 26 17
29 | 7 16 9 13 12 5 9 8 14 12 3 | 30 33 34 34 32 32 35 32 44 38 32
30 | 6 13 12 18 12 7 12 10 11 15 4 | 668 9999 670 671 9999 672 669 667 668 668 668
31 | 10 16 6 10 9 5 8 6 11 14 3 | 27 31 27 32 31 30 30 30 33 37 28
32 | 6 9 11 8 6 3 7 6 9 11 2 | 32 36 35 36 35 34 36 32 37 37 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 10 11 10 5 10 6 10 12 |T 50 33 52 54 31 52 54 51 54 56 51
WRMS | 7 12 10 11 9 4 10 6 10 10 |NE 59 34 61 63 32 61 63 59 63 65 60
MEDI | 7 12 9 9 9 4 9 6 10 11 |MD 26 30 28 30 28 27 30 27 30 32 26
Table 3.2127.5 GPS week: 2127 Day: 5 MJD: 59138.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 9 --- --- --- 19 16 13 --- --- --- 9 | 52 --- --- --- 55 55 53 --- --- --- 52
2 | 8 12 6 8 10 6 9 6 11 11 3 | 17 22 19 19 19 18 19 20 20 25 18
3 | 5 10 6 8 10 3 9 5 6 9 2 | 24 32 26 24 22 25 30 25 24 33 25
4 | 11 15 11 10 14 7 8 6 11 11 3 | 57 51 58 56 59 55 53 54 56 62 55
5 | 4 9 7 7 8 5 8 5 10 8 2 | 22 26 24 25 23 23 28 22 26 28 23
6 | 5 9 11 7 9 4 6 3 12 12 2 | 22 27 26 23 24 23 26 23 26 29 23
7 | 8 12 8 16 12 3 7 5 9 10 3 | 29 29 27 38 28 28 28 29 34 33 28
8 | 5 12 16 13 9 4 14 6 12 9 3 | 21 24 23 25 21 22 25 19 23 27 21
9 | 6 12 13 12 18 4 5 2 8 6 3 | 33 37 37 39 36 35 35 34 32 36 34
10M | 6 9 7 8 9 3 9 6 10 8 2 | 27 35 32 34 30 32 34 28 29 33 29
11E | 7 7 12 10 13 7 8 9 17 18 4 | 32 31 29 33 35 30 32 33 35 45 32
12 | 5 16 8 8 9 5 10 5 13 10 3 | 23 25 23 25 22 26 29 24 26 29 24
13 | 6 10 6 7 8 3 8 7 11 15 3 | 30 36 30 32 32 30 36 31 34 36 31
15 | 6 14 7 10 9 4 10 6 13 13 3 | 35 44 36 37 38 35 41 36 35 40 36
16 | 5 19 7 8 8 3 8 6 11 12 3 | 17 17 18 23 19 19 18 18 20 24 17
17 | 6 12 6 10 11 3 8 7 9 7 3 | 25 26 23 25 25 25 28 26 31 28 25
18 | 8 15 17 10 11 7 11 6 13 9 4 | 28 29 34 30 35 29 32 31 38 34 30
19 | 9 16 7 9 13 9 6 9 20 14 4 | 73 71 73 74 72 70 70 69 73 66 70
20 | 6 8 8 7 8 4 8 6 8 9 2 | 18 20 20 21 20 20 20 19 22 26 18
21 | 7 9 10 9 12 5 6 9 8 13 3 | 17 21 19 20 20 19 19 21 19 28 18
22 | 5 6 7 8 9 3 5 5 9 7 2 | 56 56 56 56 55 56 55 57 53 62 55
23M | 7 16 9 14 11 4 20 5 9 8 4 | 32 30 33 37 36 34 31 34 32 37 32
24 | 9 22 15 17 23 5 11 5 17 20 5 | 22 25 25 28 23 22 23 20 22 31 19
25 | 6 11 10 9 7 5 9 4 9 7 2 | 19 25 25 23 20 23 27 21 19 27 21
26 | 7 9 11 7 6 3 8 4 13 8 2 | 26 28 28 28 28 28 29 28 28 32 27
27 | 6 13 17 10 7 4 13 4 8 7 3 | 19 24 22 23 20 21 25 21 24 27 21
28 | 8 14 9 7 8 4 7 5 14 12 3 | 18 26 24 21 16 20 25 22 24 27 20
29 | 5 17 8 12 10 5 9 7 12 10 3 | 29 27 29 32 29 30 28 28 33 32 28
30 | 8 13 15 17 12 5 11 10 12 17 4 | 889 547 889 890 529 890 887 893 887 889 890
31M | 11 11 9 9 10 5 10 6 12 18 3 | 29 30 26 30 28 29 30 31 33 37 28
32M | 6 10 12 8 9 3 11 6 10 12 3 | 28 35 32 32 32 30 34 30 35 28 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 10 10 11 5 10 6 12 11 |T 57 48 58 60 46 58 59 58 59 63 57
WRMS | 7 13 10 11 10 4 10 5 11 10 |NE 66 54 69 70 51 68 70 68 70 74 67
MEDI | 6 12 9 9 10 4 9 6 11 10 |MD 27 28 26 28 28 28 29 28 29 32 28
Table 3.2127.6 GPS week: 2127 Day: 6 MJD: 59139.000
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 8 17 8 13 6 6 8 7 12 3 | 64 76 78 76 69 67 69 77 77 74 68
2 | 7 11 7 8 11 5 11 6 8 15 3 | 23 28 24 26 25 23 23 24 26 28 23
3 | 8 11 6 8 8 3 9 3 7 13 2 | 22 33 27 23 22 24 32 25 24 29 25
4 | 13 13 11 8 14 6 11 6 8 12 3 | 85 74 79 80 83 80 78 79 78 81 79
5 | 4 11 7 6 7 4 10 5 8 13 2 | 32 39 38 34 32 33 40 33 37 30 34
6 | 5 11 12 6 12 4 7 4 8 15 3 | 38 41 42 35 38 37 40 40 39 45 39
7 | 8 14 8 8 16 5 10 8 10 10 3 | 31 31 28 35 30 31 34 33 34 33 31
8 | 7 12 18 9 10 3 12 6 7 14 3 | 34 36 38 39 37 36 38 37 36 41 36
9 | 8 12 14 6 23 3 8 4 7 8 3 | 49 53 56 51 51 52 54 53 50 51 51
10 | 7 10 7 4 7 3 10 4 7 12 2 | 27 35 32 32 28 31 34 28 28 30 29
11E | 8 10 11 13 13 6 8 11 11 21 4 | 26 34 31 30 30 29 31 32 33 36 29
12 | 5 15 7 6 8 4 8 6 10 14 3 | 39 41 40 41 39 40 42 39 39 40 39
13 | 8 10 6 10 9 4 8 9 13 11 3 | 43 51 45 42 45 43 47 48 49 46 45
15 | 6 10 7 9 9 4 9 6 10 8 2 | 38 49 42 39 41 38 43 41 39 40 40
16 | 7 21 8 8 8 5 8 5 7 12 3 | 21 22 22 25 20 22 21 20 25 21 20
17 | 7 12 7 8 12 4 10 6 10 6 3 | 33 37 33 34 33 33 36 36 35 35 34
18 | 9 16 17 11 9 4 11 6 12 11 4 | 55 51 54 62 57 55 53 57 58 58 55
19 | 8 12 8 6 9 5 10 8 12 10 3 | 44 44 40 44 40 41 40 44 41 48 42
20 | 7 8 6 6 9 3 8 4 8 7 2 | 22 24 23 25 22 23 24 22 24 23 22
21 | 7 12 9 9 11 4 8 9 10 15 3 | 22 28 26 27 25 25 27 27 25 31 24
22 | 8 7 8 6 10 3 5 4 9 14 2 | 39 43 42 41 37 42 42 41 36 39 40
23 | 7 16 8 11 9 4 20 5 7 8 3 | 43 41 44 47 46 44 44 44 42 48 43
24E | 7 26 15 8 10 5 11 6 13 17 4 | 33 42 36 35 32 34 36 35 33 37 33
25 | 7 10 9 7 7 3 9 4 7 12 2 | 29 30 32 30 28 29 34 28 30 28 29
26 | 6 9 10 6 6 6 8 5 11 8 2 | 30 30 34 33 33 33 32 29 32 33 30
27 | 7 16 19 9 7 4 12 5 5 11 3 | 25 33 28 30 26 29 32 30 32 29 28
28 | 6 11 8 9 8 3 6 5 9 12 2 | 20 26 26 27 22 24 26 23 23 23 23
29 | 8 19 7 11 10 5 8 7 13 16 3 | 37 37 38 39 40 37 40 38 41 42 38
30 | 9 18 15 13 15 6 12 12 9 14 4 | 602 416 602 605 409 603 601 606 604 603 603
31 | 10 14 5 11 12 6 9 5 13 15 3 | 31 35 33 37 35 34 36 36 36 36 33
32 | 8 9 12 6 9 3 10 6 11 18 3 | 48 53 50 48 49 49 51 52 47 52 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 11 8 11 4 10 6 10 13 |T 54 52 56 57 49 55 57 56 56 57 55
WRMS | 8 13 10 8 10 4 10 5 9 12 |NE 61 57 64 64 54 63 65 64 64 64 62
MEDI | 7 12 8 8 9 4 9 6 9 12 |MD 33 37 38 35 35 34 38 36 36 37 34
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2127 GPS week: 2127 MJD: 59133.0-59139.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 |U 9 12 23 |U 9 17 45 |U 12 11 25 |
emr | emr 2948 |U 19 20 40 |U 12 17 52 |U 15 18 38 |
esa | esa 2962 | 10 10 31 |U 9 16 44 | 12 9 28 |
gfz | gfz 2960 |U 11 13 28 |U 9 14 42 |U 12 10 25 |
grg | grg 2944 |U 19 16 30 | 9 13 46 | 13 12 25 |
igr | igr 2962 | 9 11 22 | 8 14 42 | 10 9 23 |
igs | igs 2973 | 10 12 23 | 8 13 42 | 10 10 24 |
jpl | jpl 2976 | 15 19 39 | 13 27 68 | 12 14 32 |
mit | mit 2962 |U 10 11 20 |U 9 14 42 |U 12 10 26 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.2127.0 GPS week: 2127 Day: 0 MJD: 59133.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 8 11 22 | 7 12 34 | 12 7 20 |
emr | emr 2976 | 16 17 39 | 11 18 49 | 13 12 38 |
esa | esa 2976 | 10 9 32 | 8 13 35 | 11 7 26 |
gfz | gfz 2976 | 13 14 23 | 8 10 32 | 14 12 34 |
grg | grg 2976 | 9 13 22 | 8 10 34 | 12 10 22 |
igr | igr 2976 | 9 10 23 | 7 13 36 | 10 7 22 |
igs | igs 2976 | 9 10 22 | 7 11 35 | 10 7 21 |
jpl | jpl 2976 | 15 17 38 | 10 14 55 | 12 11 33 |
mit | mit 2976 | 9 9 22 | 7 10 32 | 12 7 21 |
Table 5.2127.1 GPS week: 2127 Day: 1 MJD: 59134.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 8 22 | 7 13 49 | 12 9 22 |
emr | emr 2976 | 20 20 53 | 12 19 48 | 14 22 36 |
esa | esa 2976 | 12 9 35 | 7 17 49 | 11 8 26 |
gfz | gfz 2976 | 10 10 22 | 7 14 51 | 12 7 23 |
grg | grg 2976 | 10 10 20 | 7 13 53 | 13 12 24 |
igr | igr 2976 | 10 10 27 | 6 14 45 | 10 8 20 |
igs | igs 2976 | 10 9 25 | 7 14 47 | 11 9 22 |
jpl | jpl 2976 | 15 15 41 | 9 17 58 | 12 11 29 |
mit | mit 2976 | 11 9 22 | 6 12 48 | 11 8 22 |
Table 5.2127.2 GPS week: 2127 Day: 2 MJD: 59135.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 10 18 | 9 12 44 | 12 13 23 |
emr | emr 2976 | 14 19 33 | 10 16 50 | 14 17 36 |
esa | esa 2976 | 9 10 27 | 9 15 47 | 11 10 26 |
gfz | gfz 2976 | 15 18 37 | 10 12 42 | 12 10 21 |
grg | grg 2879 | 9 14 20 | 10 14 60 | 13 15 21 |
igr | igr 2976 | 9 12 19 | 9 13 46 | 10 11 20 |
igs | igs 2976 | 8 11 18 | 9 12 45 | 11 12 21 |
jpl | jpl 2976 | 12 16 31 | 13 16 65 | 12 15 31 |
mit | mit 2976 | 10 11 16 | 10 11 44 | 12 11 23 |
Table 5.2127.3 GPS week: 2127 Day: 3 MJD: 59136.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 21 27 49 | 12 42 79 | 13 19 31 |
emr | emr 2880 | 21 24 38 | 11 20 76 | 16 19 31 |
esa | esa 2976 | 15 13 39 | 9 19 60 | 12 12 25 |
gfz | gfz 2965 | 12 13 54 | 7 15 54 | 12 11 16 |
grg | grg 2867 | 9 15 27 | 7 14 56 | 14 12 21 |
igr | igr 2976 | 11 13 25 | 8 15 54 | 10 11 20 |
igs | igs 2976 | 17 16 34 | 8 15 57 | 10 12 22 |
jpl | jpl 2976 | 20 22 44 | 24 85 122 | 15 25 37 |
mit | mit 2976 | 16 15 25 | 10 21 62 | 11 12 27 |
Table 5.2127.4 GPS week: 2127 Day: 4 MJD: 59137.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 6 12 13 | 9 13 34 | 12 12 26 |
emr | emr 2976 | 19 21 39 | 11 17 51 | 18 24 38 |
esa | esa 2976 | 9 12 29 | 9 18 39 | 11 10 30 |
gfz | gfz 2976 | 9 11 16 | 9 14 35 | 11 12 26 |
grg | grg 2976 | 7 13 18 | 9 13 36 | 12 15 28 |
igr | igr 2976 | 8 12 18 | 8 15 35 | 10 10 25 |
igs | igs 2976 | 8 13 19 | 9 13 34 | 10 11 25 |
jpl | jpl 2976 | 16 21 40 | 12 16 57 | 13 11 32 |
mit | mit 2976 | 9 12 18 | 9 13 35 | 12 12 28 |
Table 5.2127.5 GPS week: 2127 Day: 5 MJD: 59138.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 | 7 9 22 | 10 12 33 | 11 8 29 |
emr | emr 2880 | 17 16 45 | 13 16 45 | 16 15 44 |
esa | esa 2880 | 8 7 33 | 10 15 33 | 13 9 31 |
gfz | gfz 2880 | 6 9 25 | 9 14 32 | 11 9 31 |
grg | grg 2965 | 7 11 24 | 10 13 37 | 14 12 34 |
igr | igr 2880 | 7 10 25 | 9 13 31 | 10 8 29 |
igs | igs 2956 | 8 11 25 | 10 12 32 | 11 8 29 |
jpl | jpl 2976 | 15 21 46 | ---- ---- ---- | 12 12 31 |
mit | mit 2880 | 8 11 22 | 9 12 32 | 13 11 33 |
Table 5.2127.6 GPS week: 2127 Day: 6 MJD: 59139.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 10 15 | 11 15 43 | 11 12 27 |
emr | emr 2976 | 24 21 37 | 14 14 48 | 13 13 46 |
esa | esa 2976 | 8 11 25 | 11 17 46 | 12 9 31 |
gfz | gfz 2976 | 12 17 21 | 10 17 47 | 11 11 22 |
grg | grg 2974 | 79 37 79 | 10 16 47 | 12 12 25 |
igr | igr 2976 | 6 11 17 | 10 17 44 | 10 11 26 |
igs | igs 2976 | 7 12 17 | 11 15 43 | 10 11 26 |
jpl | jpl 2976 | 15 18 37 | 13 16 51 | 9 14 34 |
mit | mit 2976 | 8 12 15 | 10 16 42 | 12 11 29 |
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 6.2127 GPS week: 2127 MJD: 59133.500-59139.500
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 8 27 2 -1 | 8 19
| 11 19 52 62 2 | 1
emr uuuuu | 2 -15 134 124 -4 | 43 49
| 15 18 96 59 13 | 4
esa uuuuu | 9 -2 -8 10 6 | 28 33
| 13 8 76 74 6 | 2
gfz uuuuu | -17 -13 56 -71 6 | 26 31
| 27 32 126 99 1 | 1
grg uuuuu | 8 2 11 -53 -3 | -2 16
| 15 11 44 36 4 | 1
igr xxxxx | 11 5 47 -16 2 | -2 17
| 11 7 29 20 5 | 1
irf xxxxx | 3 14 -39 17 1 | -1 17
| 7 6 13 13 3 | 1
jpl uuuuu | -2 -27 69 -54 -15 | 42 46
| 21 13 31 61 7 | 4
mit uuuuu | 25 24 -139 24 -1 | 17 24
| 17 13 19 28 5 | 1
ngs uuuuu | -56 -10 -3 51 6 | 8 21
| 43 58 140 188 4 | 2
sio xxxxx | 65 -252 -134 -164 1 | 36 40
| 157 54 97 179 7 | 1
Table 7.2127.0 GPS week: 2127 Day: 0 MJD: 59133.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -9 22 85 81 -2 | 7 17
emr uuuuu | 23 -13 -28 183 -14 | 51 58
esa uuuuu | 17 -1 -65 70 -1 | 28 32
gfz uuuuu | 23 35 -172 -110 4 | 26 29
grg uuuuu | 0 4 -11 -70 2 | -2 14
igr xxxxx | -1 -6 32 -5 1 | -2 15
irf xxxxx | 2 15 -53 14 3 | -2 14
jpl uuuuu | -20 -21 60 55 -9 | 48 50
mit uuuuu | 10 27 -101 19 1 | 17 21
ngs uuuuu | -36 -88 245 -253 0 | 8 18
sio xxxxx | 129 -205 -20 -243 4 | 37 40
Table 7.2127.1 GPS week: 2127 Day: 1 MJD: 59134.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 6 16 -34 38 -3 | 6 17
emr uuuuu | -2 -3 147 106 11 | 46 53
esa uuuuu | 20 -17 98 60 -3 | 27 31
gfz uuuuu | -14 18 15 -79 6 | 25 29
grg uuuuu | 11 2 -42 -21 -5 | -2 14
igr xxxxx | 22 4 28 -22 -4 | -3 16
irf xxxxx | 10 14 -55 12 6 | -2 15
jpl uuuuu | 7 -38 66 -18 -18 | 46 48
mit uuuuu | 6 23 -134 -11 4 | 16 21
ngs uuuuu | -44 -29 117 -52 9 | 6 18
sio xxxxx | -11 -305 -279 -8 4 | 36 39
Table 7.2127.2 GPS week: 2127 Day: 2 MJD: 59135.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 13 62 -32 0 | 6 17
emr uuuuu | 2 7 71 139 -5 | 44 50
esa uuuuu | -17 -5 70 -1 6 | 26 31
gfz uuuuu | -19 -4 -15 -22 6 | 25 28
grg uuuuu | 0 3 -12 -37 -8 | -2 14
igr xxxxx | 9 2 89 13 -3 | -3 16
irf xxxxx | -9 12 -22 42 4 | -2 15
jpl uuuuu | 17 -5 91 -70 -24 | 44 47
mit uuuuu | 50 25 -142 39 4 | 16 21
ngs uuuuu | -119 -79 -15 3 9 | 6 18
sio xxxxx | 63 -311 -94 41 6 | 36 39
Table 7.2127.3 GPS week: 2127 Day: 3 MJD: 59136.500
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 21 59 61 1 | 8 20
emr uuuuu | 9 -11 227 64 7 | 42 48
esa uuuuu | 1 10 -75 -123 8 | 28 34
gfz uuuuu | 4 -54 149 81 6 | 26 32
grg uuuuu | 2 22 1 -117 -8 | -1 16
igr xxxxx | 17 14 91 -27 3 | -2 17
irf xxxxx | 12 25 -37 12 0 | 0 18
jpl uuuuu | 7 -18 9 -87 -16 | 44 47
mit uuuuu | 35 -1 -155 69 3 | 18 25
ngs uuuuu | -56 18 -77 26 8 | 9 22
sio xxxxx | -242 -313 -243 -451 -15 | 38 42
Table 7.2127.4 GPS week: 2127 Day: 4 MJD: 59137.500
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 | 10 -11 43 -34 0 | 9 20
emr uuuuu | -25 -23 193 93 3 | 40 46
esa uuuuu | 13 3 47 18 10 | 28 34
gfz uuuuu | -14 -16 68 3 5 | 27 32
grg uuuuu | -6 -15 62 -69 -1 | -3 16
igr xxxxx | 21 4 39 -31 5 | -2 17
irf xxxxx | -1 13 -24 1 -2 | -1 18
jpl uuuuu | 12 -29 83 -25 -24 | 41 44
mit uuuuu | 34 41 -154 -3 -6 | 18 25
ngs uuuuu | -82 4 -161 71 6 | 9 22
sio xxxxx | 171 -204 -41 -119 2 | 35 40
Table 7.2127.5 GPS week: 2127 Day: 5 MJD: 59138.500
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 21 30 -3 1 | 8 20
emr uuuuu | -1 -50 238 67 -2 | 39 45
esa uuuuu | 13 -4 -48 -41 12 | 28 34
gfz uuuuu | -48 -43 167 -170 5 | 26 31
grg uuuuu | 8 2 -4 -13 -1 | -4 17
igr xxxxx | -7 5 28 -42 6 | -3 18
irf xxxxx | 0 7 -48 14 -1 | -2 18
jpl uuuuu | 4 -40 73 -113 -10 | 37 42
mit uuuuu | 27 21 -151 45 -6 | 17 25
ngs uuuuu | -73 56 -106 259 2 | 9 22
sio xxxxx | 243 -213 -118 -52 7 | 34 39
Table 7.2127.6 GPS week: 2127 Day: 6 MJD: 59139.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 16 -27 -55 -97 -3 | 10 23
emr uuuuu | 6 -10 90 219 -26 | 40 46
esa uuuuu | 12 -2 -81 88 9 | 31 38
gfz uuuuu | -55 -27 181 -200 7 | 29 35
grg uuuuu | 40 -1 82 -40 2 | -2 18
igr xxxxx | 18 11 25 3 9 | -1 20
irf xxxxx | 3 10 -37 28 -3 | 0 20
jpl uuuuu | -43 -40 104 -116 -5 | 37 41
mit uuuuu | 9 35 -136 11 -8 | 18 26
ngs uuuuu | 19 51 -26 302 8 | 11 24
sio xxxxx | 102 -210 -142 -317 1 | 36 42
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