[IGSREPORT-24928] Wk 1924 IGS Final Orbits
acc at igs.org
acc at igs.org
Fri Dec 9 09:49:08 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1924 (Nov 20, 2016 - Nov 26, 2016)
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:
igs1924[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1924[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1924[0-6].cls IGS GPS clock combination summary report.
igs19247.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19247.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 | ALL | 4
0 | COD | MAL2 NRMD CEDU MAL2 NRMD
0 | EMR | BJNM HERS
0 | ESA | RBAY RBAY
0 | GFZ | FAA1 GMSD GODE FAA1 GMSD GODE
0 | GRG | 13 13 GLSV MAL2 RABT SYOG GLSV MAL2 RABT SYOG
0 | JPL | TUVA
1 | ALL | 4
1 | COD | BJFS FAA1 HYDE INVK KARR MAW1 NANO NIST SSIA SYOG
1 | COD | BJFS FAA1 HYDE INVK KARR MAW1 NANO NIST SSIA SYOG
1 | ESA | BJNM BJNM
1 | GFZ | BJNM FAA1 HERS HOB2 REUN BJNM CEDU FAA1 HERS HOB2
1 | GFZ | REUN
1 | GRG | 11 24 11 24 GLSV SYOG GLSV SYOG
1 | JPL | TUVA
1 | MIT | SYOG SYOG
2 | ALL | 4
2 | ESA | NRIL SYOG NRIL SYOG TIXI
2 | GFZ | 13 13 BJNM CHTI CRO1 GMSD GODE CHTI CRO1 GMSD GODE
2 | GFZ | NKLG
2 | GRG | 13 13 CHTI MCM4 NKLG NRIL NRMD SYOG CHTI DGAR GLSV
2 | GRG | NRIL NRMD SYOG
2 | JPL | TUVA
3 | ALL | 4
3 | COD | LAMA LAMA URUM
3 | GFZ | BJNM FAA1 GMSD GODE BJNM FAA1 GMSD GODE
3 | GRG | GLSV MAW1 NKLG NRMD SYOG TLSE GLSV MAW1 NRMD SYOG
3 | JPL | TUVA
4 | ALL | 4
4 | COD | SYOG SYOG
4 | EMR | STJO WHIT
4 | ESA | FAA1 NRIL WHIT FAA1 NRIL WHIT
4 | GFZ | FAA1 GMSD GODE GUAT FAA1 GMSD GODE GUAT
4 | GRG | MAL2 MAW1 NKLG MAL2 MAW1
4 | JPL | DGAV MAC1
4 | MIT | REUN
5 | ALL | 4
5 | COD | MAW1 MAW1 TRO1
5 | ESA | TRO1
5 | GFZ | GODE GODE
5 | GRG | GLSV KARR LPGS MAL2 MAW1 MCM4 PIMO SYOG TLSE GLSV
5 | GRG | LPGS MAL2 MAW1 MCM4 PIMO SYOG TLSE
5 | JPL | PIMO TUVA
6 | ALL | 4
6 | COD | BJNM MAL2 NRMD MAL2 MDVJ NRMD SYOG
6 | EMR | 8 27 8 27 HERS
6 | ESA | TRO1 BJNM RBAY
6 | GFZ | BJNM MAL2 TRO1 BJNM MAL2
6 | GRG | GLSV SYOG TLSE GLSV SYOG
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
----+--------+---------------
1 | GRG | 24
6 | COD | 4 8
6 | GRG | 8
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 G08 | | | | | | 4 | 4 |
PRN G24 | 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.
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 | -.4 -.7 -2.1 -23 4 9 .68
EMR | 0 | 2.9 7.2 11.6 75 -18 23 .78
ESA | 0 | -.5 -.2 -.6 8 -36 9 .30
GFZ | 0 | 1.2 -.7 -.8 -48 -122 -28 .62
GRG | 0 | 5.0 3.0 30.7 13 -23 19 .46
JPL | 0 | 3.9 2.3 4.1 -49 -21 -16 .71
MIT | 0 | 4.0 1.8 1.5 48 2 -70 .74
NGS | 0 | .1 2.4 6.9 0 -34 -13 .74
SIO | 0 | .4 2.9 -3.9 -5 -3 -13 .51
COD | 1 | -.5 -1.3 -1.2 -39 -20 31 .69
EMR | 1 | 4.6 11.9 11.2 79 -35 9 .47
ESA | 1 | -.3 .1 -1.2 9 -30 7 .29
GFZ | 1 | 1.5 .1 -1.2 -25 -113 -69 .83
GRG | 1 | 4.7 7.7 20.1 9 -14 48 .12
JPL | 1 | 7.6 .7 9.6 -13 18 -12 .61
MIT | 1 | 3.7 1.4 2.9 19 -6 -58 .81
NGS | 1 | -1.0 4.4 -2.0 57 -14 12 .61
SIO | 1 | -.5 -2.6 -11.9 4 -16 4 .45
COD | 2 | -.8 -1.4 -2.2 3 10 58 .88
EMR | 2 | 3.2 8.6 14.0 89 -57 3 .59
ESA | 2 | -.4 -.1 -.8 16 -39 14 .14
GFZ | 2 | 1.1 -.4 .0 -42 -131 -21 .77
GRG | 2 | 10.7 3.0 9.9 21 -46 9 .40
JPL | 2 | 5.2 .8 4.7 -51 17 3 .48
MIT | 2 | 4.2 4.8 2.0 46 1 -16 .69
NGS | 2 | 5.4 -1.4 1.7 13 -45 26 .72
SIO | 2 | 4.3 2.4 -14.7 15 -13 22 .55
COD | 3 | -1.1 -1.5 -3.0 -19 23 2 .76
EMR | 3 | 4.0 7.8 11.6 75 -19 22 .63
ESA | 3 | -.9 -1.0 -.8 -22 -15 36 .33
GFZ | 3 | 1.0 .0 -1.1 -25 -117 -2 .74
GRG | 3 | 8.6 4.8 17.2 31 -53 35 .17
JPL | 3 | 1.3 2.3 3.0 -21 59 -14 .65
MIT | 3 | 6.6 5.9 1.7 37 -21 -24 .85
NGS | 3 | 2.2 -1.1 -.5 14 -39 -1 .83
SIO | 3 | 4.5 5.7 -18.0 30 0 -20 .53
COD | 4 | -.7 -.6 -1.9 -6 16 19 .59
EMR | 4 | 5.8 1.2 14.1 61 -42 -11 .67
ESA | 4 | -.5 -.5 -.8 -21 -3 42 .19
GFZ | 4 | .6 .2 -.9 -34 -133 9 .64
GRG | 4 | 7.9 3.6 21.3 -8 -28 15 .01
JPL | 4 | 2.2 3.5 6.9 -67 64 2 .55
MIT | 4 | 7.7 3.5 6.0 19 -27 -65 .62
NGS | 4 | 3.6 .6 1.9 16 -43 4 .72
SIO | 4 | 7.4 -.8 -14.9 3 -1 -10 .34
COD | 5 | -.7 -1.2 -2.3 8 10 -11 .89
EMR | 5 | 3.6 2.1 21.6 53 -32 -22 .59
ESA | 5 | -.2 -.1 -.6 -6 -29 26 .07
GFZ | 5 | 2.3 -.3 -.7 -29 -140 -24 .74
GRG | 5 | 7.6 2.6 32.1 -7 -46 69 .30
JPL | 5 | 4.3 7.6 5.4 -22 35 29 .55
MIT | 5 | 5.2 3.4 2.2 3 -21 -67 .71
NGS | 5 | -3.5 3.7 7.9 -12 -29 -18 .72
SIO | 5 | .2 5.1 -15.8 -18 7 -46 .53
COD | 6 | -.2 .1 -1.1 -11 3 19 .66
EMR | 6 | .2 35.8 16.5 66 -46 -7 .63
ESA | 6 | -.7 -.1 -.8 11 -40 6 -.04
GFZ | 6 | .5 1.0 -1.1 -28 -109 -45 .63
GRG | 6 | 5.2 1.1 35.0 3 -41 22 .16
JPL | 6 | -.1 4.8 3.4 -36 19 -8 .16
MIT | 6 | 2.5 4.0 -1.4 21 -15 -68 .60
NGS | 6 | -2.6 5.1 2.3 23 -18 -47 .73
SIO | 6 | 1.8 11.5 -12.9 10 -21 -19 .58
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.
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 1.1924.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1924.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 2.1924.[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 3.1924.[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 5.1924.0-6). 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 1924 summary. (Nov 20, 2016 - Nov 26, 2016)
Table 1.1924.a GPS week: 1924 MJD: 57712.000-57718.000
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 238| 0 0 1 -6 -7 2 .15 9 9 | -988 -245 14 130
| 0 1 1 17 16 19 .03 | 259 395
emr 80| 0 3 2 -6 -3 -14 .30 10 10 | 2134 42 13 108
| 0 8 0 7 21 17 .07 | 651 930
esa 150| 0 0 0 5 4 32 -.46 7 7 | -1134 12 7 114
| 0 0 0 16 18 10 .02 | 713 1107
gfz 197| 0 -1 -8 -7 -22 6 .24 11 10 | -224 -60 10 91
| 0 1 0 11 15 14 .01 | 245 636
grg 118| 1 -1 14 9 21 14 -.29 14 11 | -31 115 17 171
| 0 1 6 15 18 22 .02 | 112 373
igr n/a| 0 0 -2 -3 14 0 .03 5 4 | -1421 764 15 76
| 0 1 1 7 16 13 .03 | 1524 1042
jpl 80| 0 0 3 -6 27 -44 .29 9 9 | 1824 55 14 101
| 0 1 1 20 28 26 .03 | 649 931
mit 346| 0 0 -7 -7 -24 -3 -.00 13 12 | -25 -134 53 348
| 0 1 1 33 37 35 .03 | 333 326
sio 285| 0 0 -6 17 -9 2 -.04 15 14 | --- --- --- ---
| 0 0 1 27 34 29 .05 | --- ---
Table 1.1924.b GPS week : 1924 MJD: 57712.000-57718.000
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 3 4 4 |
2 | 4 5 4 5 5 5 5 |
3 | 3 3 3 3 3 4 4 |
4 | 18 19 18 15 12 17 0 |
5 | 4 4 4 4 4 4 4 |
6 | 3 3 3 3 3 3 3 |
7 | 4 4 4 4 4 5 4 |
8 | 3 4 4 4 4 5 16 |
9 | 3 4 3 4 3 4 4 |
10 | 3 3 3 3 3 4 4 |
11 | 4 4 4 4 5 5 5 |
12 | 5 5 4 4 5 5 5 |
13 | 4 4 4 5 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 5 5 5 5 |
16 | 4 5 5 5 5 5 4 |
17 | 4 4 4 4 4 4 5 |
18 | 5 5 5 5 4 5 5 |
19 | 4 4 4 4 4 4 6 |
20 | 3 3 3 4 4 4 4 |
21 | 5 5 5 5 5 5 5 |
22 | 4 4 4 4 3 4 4 |
23 | 4 4 5 4 4 5 5 |
24 | 3 10 3 4 4 4 5 |
25 | 4 4 3 4 3 4 4 |
26 | 3 3 3 4 3 4 4 |
27 | 3 4 4 4 4 4 10 |
28 | 4 4 4 4 4 4 4 |
29 | 5 6 5 5 5 5 6 |
30 | 3 3 3 3 3 4 4 |
31 | 3 4 3 3 3 4 3 |
32 | 4 3 3 3 3 4 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 2.1924.0 GPS week: 1924 Day: 0 MJD: 57712.000
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 237| 0 0 0 10 -26 -14 .15 8 8 | -898 -613 14 128
emr 80| -1 0 1 -3 36 14 .26 9 9 | 3003 -1105 15 115
esa 150| 0 0 0 3 -12 35 -.47 7 7 | -575 943 7 117
gfz 199| 0 1 -9 1 -20 -1 .23 12 10 | -1 60 10 94
grg 121| 2 -1 17 14 35 22 -.27 12 11 | 92 141 16 174
igr n/a| 0 0 0 6 2 7 .04 4 4 | -2063 -717 13 87
jpl 80| 0 0 3 -11 -4 -56 .33 8 8 | 2875 -1021 13 100
mit 347| 0 -1 -7 -18 -15 9 .01 14 12 | 154 -114 52 337
sio 291| 0 0 -6 -11 22 -32 -.11 14 14 | --- --- --- ---
Table 2.1924.1 GPS week: 1924 Day: 1 MJD: 57713.000
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 241| 0 0 2 -1 -29 4 .11 9 9 | -1345 -133 17 134
emr 80| 0 2 2 -1 13 -27 .25 11 10 | 1601 -257 12 94
esa 150| 0 0 0 21 -5 40 -.47 8 7 | -2138 -614 8 130
gfz 198| 0 0 -7 -13 0 -7 .23 12 11 | -14 -649 11 90
grg 114| 0 -2 7 -10 28 48 -.31 23 12 | -8 -176 18 187
igr n/a| 0 -1 -1 0 -10 -4 .00 5 4 | -3108 489 15 79
jpl 80| 0 0 4 -16 -10 -69 .31 9 9 | 1471 -144 13 99
mit 347| 0 -1 -7 -6 14 20 -.02 14 13 | 327 -283 53 364
sio 283| -2 0 -5 2 -2 25 -.01 14 14 | --- --- --- ---
Table 2.1924.2 GPS week: 1924 Day: 2 MJD: 57714.000
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 239| 0 0 3 -17 6 17 .17 8 8 | -708 -624 15 133
emr 80| -2 1 2 -22 -16 -20 .30 9 9 | 1473 1382 13 102
esa 150| 0 0 0 23 1 31 -.46 7 7 | -704 1734 8 116
gfz 197| 0 -1 -8 -19 -23 2 .26 11 10 | -686 1261 9 90
grg 116| 0 -1 7 3 36 -11 -.31 11 11 | -212 861 17 179
igr n/a| 0 0 -1 -8 12 -27 -.01 4 4 | -2659 2047 14 83
jpl 80| 1 1 2 6 48 -80 .29 8 8 | 1294 1472 14 107
mit 346| 0 0 -7 -2 -25 51 -.02 13 12 | 301 547 50 381
sio 291| 0 -1 -2 5 -51 38 -.08 14 13 | --- --- --- ---
Table 2.1924.3 GPS week: 1924 Day: 3 MJD: 57715.000
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 239| 0 1 1 -35 -8 -19 .17 9 9 | -1161 -166 13 132
emr 80| 0 1 2 -7 -5 -7 .29 9 9 | 1899 222 12 115
esa 150| 0 0 0 -17 10 36 -.43 7 6 | -1883 -927 7 118
gfz 198| -1 0 -8 -12 -44 20 .25 11 10 | -194 -413 10 107
grg 119| 2 -1 13 38 -12 10 -.27 13 11 | 1 -116 18 174
igr n/a| 0 0 -2 -13 8 1 .05 5 5 | -1635 434 16 73
jpl 80| 1 -1 4 21 55 -48 .30 9 9 | 1754 -161 14 108
mit 346| 0 0 -7 4 -21 11 -.02 13 12 | -363 -382 49 288
sio 283| 0 -1 -5 28 -7 -27 -.07 14 14 | --- --- --- ---
Table 2.1924.4 GPS week: 1924 Day: 4 MJD: 57716.000
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 238| 0 0 1 -8 -12 -8 .12 9 9 | -1208 303 14 132
emr 80| 0 0 3 -1 -22 -38 .27 9 9 | 2147 -544 13 107
esa 150| 0 0 0 -12 42 47 -.47 6 6 | -1604 -998 6 96
gfz 195| -1 0 -7 14 -23 30 .22 10 10 | -286 -330 10 88
grg 118| 0 0 14 -1 6 -5 -.27 13 11 | 91 -242 17 164
igr n/a| 0 0 -3 0 23 -1 .01 4 4 | -1103 96 15 61
jpl 80| 0 0 2 -33 58 -25 .26 9 9 | 1711 -672 16 102
mit 347| 0 0 -6 10 -58 -43 -.04 12 11 | 32 -380 55 317
sio 287| 1 -1 -7 59 -60 30 .05 16 16 | --- --- --- ---
Table 2.1924.5 GPS week: 1924 Day: 5 MJD: 57717.000
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 237| 0 0 1 17 9 1 .12 11 11 | -658 -656 15 123
emr 80| 0 -2 4 -2 -17 -17 .28 10 10 | 1750 1160 14 117
esa 150| 0 1 0 19 -9 19 -.47 7 7 | -448 -810 8 125
gfz 197| -1 -1 -8 -7 -36 12 .26 11 10 | -351 45 11 79
grg 121| 0 0 15 11 21 35 -.30 13 11 | -138 99 17 163
igr n/a| 0 0 -3 4 33 10 .07 5 5 | -920 2195 17 79
jpl 80| 1 -1 4 12 13 -11 .25 10 10 | 1126 1197 14 88
mit 346| 1 1 -7 -73 19 -40 .04 13 12 | -560 -47 50 386
sio 283| 0 0 -8 -9 27 3 -.01 14 13 | --- --- --- ---
Table 2.1924.6 GPS week: 1924 Day: 6 MJD: 57718.000
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 237| 0 -2 -1 -9 7 35 .19 10 10 | -943 170 14 132
emr 80| 0 21 2 -8 -11 -6 .46 16 16 | 3065 -561 15 110
esa 150| 0 1 0 2 4 16 -.45 6 6 | -587 757 7 99
gfz 197| 0 -4 -7 -16 -6 -7 .25 12 11 | -40 -396 12 92
grg 121| 0 -3 26 6 37 1 -.29 15 13 | -44 240 17 160
igr n/a| 0 -2 -3 -10 31 12 .06 5 5 | 1537 806 17 70
jpl 80| 0 -2 0 -22 30 -18 .28 8 8 | 2541 -286 14 106
mit 346| 1 -2 -10 36 -83 -30 .02 13 12 | -66 -282 64 364
sio 283| 0 0 -6 44 3 -19 -.07 16 14 | --- --- --- ---
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 3.1924.0 GPS week: 1924 Day: 0 MJD: 57712.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit sio IGS | cod emr esa gfz grg igr jpl mit sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 7 10 6 7 8 3 8 12 8 3 | 25 26 18 24 18 22 29 21 25 21
2 | 11 8 8 14 10 4 6 15 19 4 | 36 40 36 45 32 37 37 39 45 37
3 | 6 9 5 8 9 3 9 6 7 3 | 37 42 32 37 32 36 44 35 39 35
X4E | 17 --- --- --- --- 28 17 --- --- 17 | 100 --- --- --- --- 109 98 --- --- 98
5 | 6 6 8 15 11 4 8 16 17 4 | 42 45 42 42 43 42 46 39 40 41
6 | 7 8 6 7 7 2 9 10 14 3 | 22 25 20 23 17 22 26 25 24 21
7 | 6 11 8 13 13 4 8 12 13 4 | 24 28 20 24 19 20 24 19 17 20
8E | 7 12 6 8 13 2 7 11 6 3 | 113 114 110 114 113 112 27 107 109 111
9 | 6 10 6 7 14 3 9 8 7 3 | 19 20 14 21 20 18 24 22 19 17
10 | 7 7 4 7 8 3 7 10 12 2 | 37 43 37 41 34 38 40 45 42 38
11 | 10 9 14 13 10 3 8 11 13 4 | 37 38 32 42 32 37 42 36 34 34
12 | 10 8 6 14 14 5 7 18 20 4 | 28 28 22 27 26 25 29 28 23 24
13E | 8 7 6 11 20 4 8 15 15 4 | 30 30 29 31 34 29 31 32 30 29
14E | 10 10 6 10 21 6 9 14 14 4 | 43 47 41 46 43 43 44 44 46 42
15 | 7 10 5 12 18 4 9 15 16 4 | 27 31 21 27 31 24 30 25 17 24
16 | 10 10 6 14 8 4 8 14 16 4 | 30 24 21 27 23 24 25 22 23 22
17E | 8 12 5 10 13 4 10 15 14 4 | 26 29 18 27 25 24 29 23 27 23
18 | 8 11 5 24 7 3 7 14 18 4 | 26 32 28 46 27 29 28 31 28 28
19E | 15 6 6 13 13 4 6 15 14 4 | 24 23 17 23 25 20 26 20 19 19
20 | 5 7 7 10 9 4 7 12 15 3 | 32 34 32 36 31 33 32 37 36 32
21 | 8 7 8 16 11 4 7 19 19 4 | 31 32 34 40 30 32 33 41 37 32
22 | 5 8 9 11 10 5 6 20 10 3 | 32 34 32 34 26 34 36 33 29 30
23 | 6 10 6 14 20 4 10 13 14 4 | 26 26 19 25 32 23 30 23 18 22
24 | 8 10 4 7 9 4 9 13 11 3 | 200 198 197 196 197 198 199 202 198 198
25 | 9 7 5 7 7 5 9 16 14 3 | 22 26 17 22 21 21 27 25 29 22
26 | 8 9 5 6 8 4 8 7 13 3 | 25 22 19 23 20 22 25 22 27 21
27E | 7 10 6 7 15 3 8 9 8 3 | 25 21 15 25 19 21 26 23 19 19
28 | 7 10 7 11 9 3 8 14 15 3 | 27 27 19 24 23 23 28 24 15 22
29E | 15 9 7 15 15 3 11 23 19 5 | 39 31 29 38 35 33 33 36 33 31
30 | 5 7 7 9 10 3 10 9 7 3 | 28 28 23 28 23 26 29 24 26 25
31 | 8 8 5 10 10 4 8 12 11 3 | 28 29 19 22 22 24 28 25 20 23
32 | 7 11 4 7 15 4 7 10 11 3 | 28 28 23 25 28 25 30 22 23 24
------+---------------------------------------------------+----------------------------------------------------
RMS | 8 9 7 12 12 4 8 14 14 |T 39 38 33 38 35 38 38 37 36 37
WRMS | 8 9 7 10 11 4 8 12 14 |NE 36 37 32 37 33 34 38 36 34 33
MEDI | 7 9 6 10 10 4 8 13 14 |MD 28 29 23 27 27 25 29 25 27 24
Table 3.1924.1 GPS week: 1924 Day: 1 MJD: 57713.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit sio IGS | cod emr esa gfz grg igr jpl mit sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 8 7 6 7 7 4 7 9 8 2 | 21 25 19 21 19 22 27 22 25 21
2 | 14 8 9 16 13 5 7 16 20 4 | 30 30 25 30 27 27 28 28 33 27
3 | 5 9 6 7 9 5 8 9 11 3 | 25 33 23 26 25 27 32 27 29 26
X4E | 20 --- --- --- --- 24 17 --- --- 18 | 60 --- --- --- --- 66 68 --- --- 61
5 | 7 9 8 12 11 4 8 14 16 4 | 27 28 26 21 23 25 29 21 22 24
6 | 7 6 5 8 9 3 7 10 10 3 | 22 26 25 20 23 23 26 23 26 23
7 | 7 10 7 14 14 5 8 14 14 4 | 21 25 16 22 20 17 23 18 16 18
8E | 8 12 7 7 16 4 7 12 9 3 | 85 86 82 86 90 84 26 86 87 84
9 | 7 15 6 6 14 4 7 8 9 3 | 21 23 15 20 18 19 22 19 23 18
10 | 6 7 3 6 10 3 6 11 11 2 | 26 29 27 27 25 28 27 31 28 27
11 | 9 9 14 9 12 3 8 9 14 4 | 28 32 26 30 28 28 33 29 28 28
12 | 13 11 7 16 9 5 8 20 22 5 | 23 26 19 21 17 20 26 19 14 19
13E | 10 11 6 11 18 4 7 11 11 4 | 28 25 22 25 24 24 27 24 24 24
14 | 8 7 6 10 16 5 8 12 10 3 | 26 27 24 28 23 26 26 25 25 24
15 | 7 10 6 11 15 3 10 14 16 4 | 26 26 21 21 21 23 28 24 18 22
16 | 7 8 6 16 14 5 9 13 21 4 | 23 24 19 23 24 22 26 19 21 20
17E | 8 12 5 11 16 4 10 13 13 4 | 21 26 17 22 17 19 25 20 24 19
18 | 9 10 6 21 11 5 8 13 18 4 | 22 21 20 34 21 21 21 22 18 19
19E | 10 8 5 12 19 4 7 18 12 4 | 19 24 16 19 23 18 26 21 21 19
20 | 4 6 9 8 10 3 6 13 15 3 | 23 23 22 22 21 21 23 25 21 21
21 | 9 7 10 15 14 4 9 20 21 4 | 27 27 28 27 27 24 26 28 26 24
22 | 10 6 8 9 8 5 5 17 10 3 | 25 27 25 25 21 26 28 29 24 24
23 | 7 15 6 13 16 6 8 11 14 4 | 22 25 18 22 23 20 26 17 15 19
24 | 16 31 17 18 106 18 29 22 24 9 | 385 383 385 380 339 380 382 387 381 383
25 | 9 8 6 7 10 4 9 15 11 3 | 19 23 13 17 19 19 24 17 20 17
26 | 9 6 7 9 8 3 8 8 12 3 | 23 23 14 18 18 20 25 19 26 19
27E | 9 8 6 7 20 4 7 10 12 3 | 26 21 15 22 27 22 25 23 20 20
28 | 8 9 7 13 14 4 6 14 17 4 | 23 28 19 21 25 19 26 18 14 20
29E | 16 10 9 15 22 6 11 20 16 5 | 29 29 25 30 26 27 28 28 26 25
30 | 6 9 7 7 12 5 6 9 7 3 | 23 23 16 21 21 19 24 19 21 19
31 | 9 9 6 10 12 4 9 13 10 3 | 25 26 19 23 17 22 24 21 18 20
32 | 10 8 4 5 12 4 6 12 9 3 | 25 24 16 19 17 18 22 18 22 19
------+---------------------------------------------------+----------------------------------------------------
RMS | 9 11 8 12 23 5 9 14 14 |T 38 39 34 36 34 36 38 36 36 36
WRMS | 9 10 7 11 12 4 9 12 14 |NE 38 40 35 37 34 37 40 37 37 36
MEDI | 8 9 6 10 13 4 8 13 12 |MD 25 26 20 22 23 22 26 22 23 21
Table 3.1924.2 GPS week: 1924 Day: 2 MJD: 57714.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit sio IGS | cod emr esa gfz grg igr jpl mit sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 9 7 6 6 6 3 7 14 7 3 | 25 29 20 26 23 23 27 23 25 22
2 | 11 7 8 13 11 5 7 15 22 4 | 31 31 30 34 26 29 31 34 36 29
3 | 7 8 6 9 7 4 9 10 11 3 | 26 32 25 28 26 27 32 27 29 26
X4 | 16 --- --- --- --- 18 19 --- --- 17 | 102 --- --- --- --- 102 102 --- --- 102
5 | 8 8 7 10 8 5 7 14 18 3 | 34 35 33 32 33 33 35 30 29 32
6 | 5 9 6 6 8 5 6 8 13 2 | 23 25 19 24 18 22 26 23 22 21
7 | 10 11 5 13 12 4 8 14 14 4 | 24 27 18 24 21 20 24 20 17 19
8E | 9 12 8 9 14 4 8 10 14 4 | 105 103 100 103 104 100 27 97 95 99
9 | 6 12 4 6 12 4 9 9 9 3 | 17 20 14 18 17 17 21 18 20 15
10 | 8 7 5 8 7 3 7 10 8 3 | 31 33 28 31 29 29 30 35 30 29
11 | 9 9 14 8 10 4 8 10 13 4 | 29 35 31 34 30 31 33 32 29 30
12 | 10 7 6 14 11 5 7 17 21 4 | 26 27 20 25 21 22 25 23 20 21
13E | 10 8 4 12 19 6 9 12 11 4 | 33 36 32 33 37 32 33 36 33 32
14 | 8 8 6 8 12 4 8 10 14 3 | 23 27 21 22 21 22 24 22 20 20
15 | 8 8 6 11 16 3 9 16 19 4 | 22 25 21 22 23 19 24 21 19 19
16 | 7 12 8 15 13 5 10 14 21 4 | 26 27 20 25 23 21 24 18 19 20
17E | 9 10 5 8 11 4 10 15 14 3 | 24 29 19 24 21 22 27 24 24 22
18 | 9 9 6 25 8 5 8 15 16 4 | 24 25 24 39 25 23 23 26 23 23
19E | 15 5 5 12 13 5 7 15 13 4 | 25 26 19 24 21 20 26 23 22 21
20 | 6 6 7 9 10 3 6 12 14 3 | 23 27 25 28 24 23 24 27 26 23
21 | 9 7 7 16 14 3 7 17 20 4 | 25 28 27 30 26 24 27 31 28 25
22 | 5 6 11 9 9 4 9 17 12 3 | 25 28 29 26 24 27 30 28 22 25
23 | 7 12 5 14 19 4 9 13 17 4 | 25 26 19 26 29 21 28 20 21 21
24 | 7 11 4 10 9 5 10 10 10 3 | 200 201 201 197 203 200 199 205 204 201
25 | 7 8 4 6 9 4 9 10 11 3 | 21 25 14 18 16 18 23 19 21 18
26 | 7 7 7 9 8 5 6 8 17 3 | 25 26 18 21 20 21 23 19 27 20
27E | 7 10 7 9 9 4 9 9 12 3 | 25 26 19 25 21 22 25 24 20 21
28 | 7 8 8 10 10 4 7 13 16 3 | 26 28 22 23 22 21 26 20 17 21
29E | 9 10 7 11 15 5 12 19 15 4 | 29 27 24 28 24 24 27 28 26 24
30 | 7 8 5 6 10 4 8 7 7 2 | 24 25 20 26 21 23 26 22 21 22
31 | 5 8 6 10 9 3 9 11 10 3 | 28 28 21 25 21 23 26 21 20 22
32 | 7 8 5 6 10 2 7 7 10 2 | 26 29 22 21 22 21 26 21 24 22
------+---------------------------------------------------+----------------------------------------------------
RMS | 8 9 7 11 11 4 8 13 14 |T 36 36 30 34 32 33 34 32 31 33
WRMS | 8 9 7 10 11 4 8 12 13 |NE 32 35 30 33 30 30 33 31 31 30
MEDI | 8 8 6 9 10 4 8 12 14 |MD 25 27 21 26 23 23 26 23 23 22
Table 3.1924.3 GPS week: 1924 Day: 3 MJD: 57715.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit sio IGS | cod emr esa gfz grg igr jpl mit sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 7 9 6 8 7 4 9 11 9 3 | 21 23 18 20 17 19 26 22 22 19
2 | 11 9 9 14 9 5 8 15 21 4 | 30 32 28 35 25 29 29 34 38 29
3 | 8 9 6 7 9 4 10 9 12 3 | 33 34 28 30 25 29 35 31 31 30
X4 | 15 --- --- --- --- 38 14 --- --- 14 | 90 --- --- --- --- 99 94 --- --- 92
5 | 9 8 8 12 8 4 7 13 14 3 | 39 40 38 34 39 36 38 36 35 36
6 | 6 7 5 5 6 5 7 9 13 2 | 23 25 22 23 20 22 27 25 26 22
7 | 10 11 5 14 11 5 8 14 14 4 | 24 25 18 22 19 18 22 19 18 19
8E | 12 8 8 12 18 5 8 10 10 4 | 110 107 108 109 106 108 24 106 108 106
9 | 8 13 5 8 14 5 9 10 8 3 | 18 22 12 16 19 16 20 18 19 15
10 | 7 7 5 6 11 4 7 11 13 3 | 33 35 30 34 28 34 33 39 39 32
11 | 9 9 13 12 10 4 9 12 13 4 | 34 37 31 37 27 31 37 32 30 31
12 | 11 10 7 14 8 5 7 16 20 4 | 29 28 22 24 23 22 28 25 21 23
13 | 9 9 6 12 24 5 8 15 14 4 | 30 30 28 33 32 28 32 31 33 29
14 | 8 10 5 8 17 5 9 11 12 3 | 20 24 14 20 22 15 19 19 14 16
15 | 8 9 7 12 19 6 8 16 18 4 | 23 24 19 22 25 19 23 21 19 19
16 | 7 11 7 15 13 4 10 14 19 4 | 24 27 23 23 22 22 27 21 26 22
17E | 9 9 4 9 12 4 13 12 15 4 | 25 27 22 27 29 22 28 25 30 24
18 | 9 10 7 21 8 4 8 13 17 4 | 28 26 25 37 21 25 24 29 28 25
19E | 14 7 6 12 14 4 10 13 13 4 | 23 22 17 22 23 17 22 19 19 18
20 | 5 8 6 11 9 4 7 11 16 3 | 28 26 27 31 24 27 26 32 33 26
21 | 11 7 8 16 15 6 8 18 21 4 | 32 30 32 33 26 29 29 34 34 29
22 | 7 7 10 10 8 5 7 12 14 3 | 30 29 30 27 22 27 30 28 27 27
23 | 7 14 6 12 17 6 10 13 15 4 | 22 27 19 20 30 19 27 21 19 20
24 | 9 11 4 10 12 4 10 10 13 3 | 230 229 231 228 220 231 230 230 231 230
25 | 8 10 7 7 7 3 9 12 13 3 | 22 27 16 21 18 18 24 22 22 20
26 | 14 8 7 8 9 3 8 8 14 3 | 20 28 21 21 18 21 26 22 26 21
27E | 9 10 5 8 12 5 9 10 12 3 | 24 23 17 24 24 20 23 24 20 20
28 | 9 7 8 10 11 3 9 14 16 4 | 24 24 21 23 23 20 27 21 21 21
29E | 16 11 6 14 17 6 10 18 16 5 | 33 29 28 31 28 25 30 29 30 28
30 | 9 8 5 7 11 3 8 8 9 3 | 27 24 21 24 20 23 23 22 24 22
31 | 7 8 5 9 10 4 9 13 11 3 | 26 30 20 26 18 22 25 25 18 22
32 | 9 8 5 7 15 3 10 8 8 3 | 24 28 20 22 26 20 26 19 21 21
------+---------------------------------------------------+----------------------------------------------------
RMS | 9 9 7 11 13 5 9 13 14 |T 37 36 32 35 32 34 35 34 34 34
WRMS | 9 9 6 10 11 5 9 12 14 |NE 35 36 32 34 31 32 35 34 34 32
MEDI | 9 9 6 10 11 4 9 12 14 |MD 26 27 22 24 24 22 27 25 26 22
Table 3.1924.4 GPS week: 1924 Day: 4 MJD: 57716.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit sio IGS | cod emr esa gfz grg igr jpl mit sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 7 8 5 6 7 4 9 8 15 3 | 21 25 19 21 17 20 25 22 30 20
2 | 10 9 8 15 9 5 11 16 22 4 | 31 29 31 30 25 28 29 32 37 28
3 | 6 8 5 6 8 5 8 7 13 2 | 32 35 32 30 30 31 34 33 36 31
X4 | 13 --- --- --- --- 13 11 --- --- 12 | 61 --- --- --- --- 59 60 --- --- 60
5 | 6 7 7 12 10 5 9 14 15 3 | 34 39 36 29 34 32 37 34 34 34
6 | 5 7 5 6 6 5 9 9 13 2 | 26 26 24 22 22 22 25 24 31 24
7 | 9 13 7 14 11 5 9 16 15 4 | 22 28 19 24 22 20 25 21 20 21
8E | 10 10 7 9 19 5 11 13 15 4 | 114 115 111 114 115 113 21 114 116 113
9 | 9 9 6 8 11 4 9 9 11 3 | 19 22 16 19 19 18 22 19 25 18
10 | 6 8 4 5 12 3 8 10 15 3 | 35 37 35 36 33 35 37 38 41 35
11 | 9 12 13 10 13 4 11 10 18 4 | 34 42 34 39 30 35 39 37 36 35
12 | 12 8 7 15 12 5 10 16 22 4 | 26 28 21 29 25 22 29 27 25 24
13 | 10 8 6 12 15 4 10 12 17 4 | 20 23 19 22 20 19 24 20 28 20
14 | 6 8 5 9 15 4 7 11 14 3 | 21 26 19 24 25 20 22 19 21 20
15 | 12 6 8 12 18 5 8 15 22 4 | 25 25 23 21 28 20 25 20 23 21
16 | 11 9 7 13 13 5 9 16 22 4 | 30 25 21 24 26 22 26 23 25 22
17E | 11 11 5 7 13 3 11 10 13 3 | 25 30 24 25 25 24 30 25 29 25
18 | 10 8 6 17 7 4 7 13 19 4 | 24 24 25 32 24 22 23 24 28 23
19E | 11 7 6 10 13 3 11 13 13 4 | 21 24 19 21 24 19 25 20 23 20
20 | 8 6 7 11 8 4 8 12 16 3 | 30 28 28 32 26 26 28 32 35 28
21 | 9 7 8 14 12 5 9 16 23 4 | 32 33 33 38 29 32 34 36 39 32
22 | 5 4 9 9 10 5 5 9 13 3 | 28 27 29 27 22 28 29 28 28 26
23 | 5 9 5 12 20 5 9 13 19 4 | 25 29 24 28 32 25 29 24 29 25
24 | 13 13 5 9 8 5 8 9 15 3 | 101 102 107 104 100 102 103 103 107 103
25 | 9 9 4 7 7 4 9 10 12 3 | 24 27 18 25 21 21 26 24 25 22
26 | 9 8 5 7 9 4 9 7 16 3 | 27 27 19 24 23 24 27 21 28 23
27E | 9 8 6 9 23 5 8 11 13 4 | 24 22 16 23 22 20 22 22 23 19
28 | 9 9 6 10 10 4 7 13 15 3 | 26 28 22 22 23 20 27 22 23 22
29E | 14 11 8 15 17 5 11 19 19 5 | 31 23 21 29 28 22 25 27 29 23
30 | 9 9 6 6 10 3 10 7 9 3 | 24 25 20 22 21 22 25 22 24 22
31 | 9 8 5 8 11 4 8 10 13 3 | 30 31 23 28 25 25 28 27 25 26
32 | 6 10 4 6 13 3 8 8 10 3 | 26 29 25 24 28 23 27 22 26 24
------+---------------------------------------------------+----------------------------------------------------
RMS | 9 9 6 10 13 4 9 12 16 |T 32 33 29 31 30 30 30 31 33 30
WRMS | 9 9 6 10 11 4 9 11 16 |NE 30 32 28 30 28 28 31 29 32 28
MEDI | 9 8 6 9 11 4 9 11 15 |MD 26 28 23 25 25 22 27 24 28 24
Table 3.1924.5 GPS week: 1924 Day: 5 MJD: 57717.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit sio IGS | cod emr esa gfz grg igr jpl mit sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 7 10 7 9 11 5 10 8 11 3 | 24 30 22 25 17 23 31 24 28 24
2 | 11 10 8 14 9 6 11 16 21 4 | 29 27 26 29 23 25 27 27 28 25
3 | 12 10 6 8 9 4 11 8 10 3 | 29 31 24 24 19 25 33 26 28 25
X4 | 18 --- --- --- --- 20 16 --- --- 17 | 76 --- --- --- --- 62 63 --- --- 60
5 | 7 9 8 10 10 5 12 13 15 4 | 33 37 35 28 31 31 35 30 31 32
6 | 9 8 6 6 8 4 8 8 8 2 | 30 31 26 26 25 27 32 28 28 28
7 | 11 8 6 15 11 5 10 18 12 4 | 27 25 16 24 18 19 25 23 19 19
8E | 15 15 7 11 14 5 13 15 10 4 | 184 169 167 165 172 168 27 164 169 168
9 | 15 8 7 7 18 5 10 10 8 4 | 27 19 16 19 19 18 23 18 18 17
10 | 10 9 5 9 10 4 8 12 11 3 | 28 31 24 31 25 25 28 28 30 27
11 | 13 7 14 11 13 7 12 11 12 4 | 33 36 30 33 24 29 36 35 31 31
12 | 12 13 7 14 12 4 8 17 16 4 | 25 26 18 24 20 20 26 20 16 19
13 | 11 8 7 12 17 4 9 12 15 4 | 22 23 21 20 19 19 25 21 20 20
14 | 11 10 7 10 15 5 8 14 15 4 | 23 23 19 25 21 19 22 19 21 18
15 | 10 12 7 12 16 5 11 13 17 4 | 23 23 17 19 21 16 23 19 15 17
16 | 11 9 7 11 15 5 10 15 17 4 | 25 26 19 22 23 19 25 18 19 20
17E | 9 10 7 10 11 4 13 12 14 4 | 22 25 22 24 16 21 26 22 29 21
18 | 13 9 8 18 7 4 9 14 17 4 | 23 19 21 32 16 18 17 20 21 19
19E | 16 8 7 10 14 4 12 14 13 4 | 23 23 21 22 19 19 25 20 23 20
20 | 8 8 7 9 6 4 7 11 14 3 | 24 25 25 25 22 24 24 26 27 24
21 | 9 8 8 15 14 5 7 15 20 4 | 31 30 31 29 26 28 30 28 28 28
22 | 8 5 10 9 11 6 8 9 11 3 | 27 28 28 24 19 27 31 26 28 26
23 | 14 11 8 11 23 6 11 12 18 5 | 35 32 29 29 33 29 36 21 25 28
24 | 9 11 6 9 9 5 10 11 10 3 | 166 169 171 169 163 168 170 169 172 169
25 | 10 11 6 8 9 3 9 10 12 3 | 21 23 12 21 16 16 22 17 19 17
26 | 10 9 7 8 9 4 13 7 10 3 | 25 27 16 22 16 20 27 20 24 21
27E | 15 8 7 7 21 5 9 10 14 4 | 30 26 19 23 23 23 25 26 23 22
28 | 9 9 10 10 12 5 11 15 16 4 | 24 30 19 20 22 18 29 20 14 20
29E | 13 12 6 12 17 4 11 19 15 5 | 27 23 19 25 27 21 22 26 25 21
30 | 15 9 7 9 12 4 11 6 9 3 | 26 21 15 20 16 20 22 21 22 18
31 | 11 8 4 10 13 4 10 11 10 3 | 23 24 15 23 15 18 22 16 11 16
32 | 7 12 6 8 12 4 10 15 7 3 | 22 26 18 23 21 19 25 17 19 19
------+---------------------------------------------------+----------------------------------------------------
RMS | 11 10 7 11 13 5 10 13 14 |T 37 35 31 33 30 32 32 32 32 32
WRMS | 11 10 7 10 11 5 10 12 13 |NE 32 33 28 30 27 28 33 29 29 28
MEDI | 11 9 7 10 12 5 10 12 13 |MD 26 26 21 24 21 21 26 22 24 21
Table 3.1924.6 GPS week: 1924 Day: 6 MJD: 57718.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit sio IGS | cod emr esa gfz grg igr jpl mit sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 7 15 6 10 13 4 8 8 11 3 | 25 41 23 28 21 24 28 25 31 24
2 | 12 12 7 15 11 5 7 16 24 4 | 31 34 27 36 26 27 28 31 36 28
3 | 10 11 5 11 11 6 8 8 11 3 | 43 49 39 42 33 40 44 43 44 40
X4 | 210 --- --- --- --- 24 5 --- --- 0 | 211 --- --- --- --- 94 88 --- --- 90
5 | 9 13 6 12 10 4 7 15 14 4 | 44 50 46 45 49 44 49 42 45 45
6 | 8 15 5 5 8 3 6 8 8 3 | 25 30 20 26 26 22 28 23 24 22
7 | 8 17 5 15 13 5 9 16 12 4 | 29 38 24 32 26 28 31 28 30 27
X8E | 119 34 18 40 87 23 --- 41 37 16 | 447 450 448 451 453 445 --- 451 456 449
9 | 9 16 6 8 18 5 7 13 11 4 | 22 29 14 24 26 20 24 17 25 18
10 | 7 15 5 10 10 5 9 10 17 3 | 44 56 43 45 39 44 47 48 48 44
11 | 9 17 12 15 14 6 9 15 22 5 | 38 53 35 44 31 38 42 45 43 37
12 | 10 18 7 13 11 5 7 16 17 4 | 23 33 18 26 20 20 23 22 20 20
13 | 7 13 5 12 18 5 9 12 18 4 | 27 32 23 30 28 28 29 26 26 25
14 | 7 15 6 8 20 4 7 13 20 4 | 28 41 28 31 36 28 28 22 26 26
15 | 8 16 6 12 22 5 6 14 22 4 | 20 33 21 24 30 20 22 21 19 19
16 | 11 17 5 12 13 6 8 14 18 4 | 26 32 19 23 27 19 23 17 22 19
17E | 12 20 6 10 21 6 9 15 15 4 | 22 39 19 26 28 22 25 24 27 21
18 | 10 13 7 15 11 4 8 16 17 4 | 24 31 23 35 22 24 21 26 25 22
19E | 21 15 8 12 25 6 7 15 16 5 | 28 34 17 23 32 18 21 20 22 18
20 | 6 14 7 10 11 4 6 13 17 3 | 31 31 32 39 28 31 29 34 36 31
21 | 13 13 6 15 14 5 8 14 23 4 | 34 40 34 38 28 32 32 36 36 32
22 | 11 12 11 13 11 6 5 10 15 4 | 34 41 37 34 26 34 34 36 32 33
23 | 8 20 6 14 21 6 11 18 19 5 | 50 58 45 49 51 47 47 49 49 46
24 | 15 29 4 10 13 5 7 10 8 4 | 171 171 168 171 162 170 170 170 170 170
25 | 11 19 5 8 10 4 9 10 8 3 | 19 36 14 22 18 18 23 18 19 18
26 | 12 12 5 10 9 3 8 6 10 3 | 25 33 15 21 18 20 25 19 27 20
X27E | 8 24 9 13 53 9 --- 13 --- 9 | 34 45 29 35 65 35 --- 33 --- 31
28 | 6 16 7 11 13 5 7 17 14 4 | 24 35 22 21 19 19 25 24 17 21
29E | 15 13 7 14 25 3 10 23 16 5 | 24 28 18 29 30 20 19 27 29 20
30 | 7 16 6 7 13 4 9 10 8 3 | 25 34 22 25 20 23 26 23 26 22
31 | 10 13 4 10 12 4 8 9 8 3 | 35 47 29 34 32 30 31 27 29 30
32 | 6 16 4 7 16 4 7 10 12 3 | 34 46 30 34 39 31 35 26 30 32
------+---------------------------------------------------+----------------------------------------------------
RMS | 10 16 6 12 15 5 8 13 16 |T 53 56 44 49 48 47 36 46 48 46
WRMS | 10 16 6 11 13 5 8 12 14 |NE 36 45 33 38 34 34 36 35 36 34
MEDI | 9 15 6 12 13 5 8 13 15 |MD 28 38 24 32 28 28 28 26 29 26
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 4.1924 GPS week: 1924 MJD: 57712.0-57718.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 5 5 12 |U 7 9 22 |U 7 7 16 |
emr | emr 2976 | 7 7 18 |U 8 9 23 | 7 5 16 |
esa | esa 2976 | 6 7 15 |U 7 10 25 | 8 7 17 |
gfz | gfz 2974 |U 5 6 13 |U 7 9 24 |U 6 6 16 |
grg | grg 2974 |U 6 7 14 |U 7 10 25 | 8 9 22 |
igr | igr 2976 | 6 6 13 | 7 9 25 | 7 6 16 |
igs | igs 2976 | 6 6 14 | 7 9 23 | 7 6 16 |
jpl | jpl 3043 | 6 7 16 |U 7 9 24 | 7 7 19 |
mit | mit 2976 | 6 7 16 |U 8 12 28 |U 8 7 18 |
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 5.1924.0 GPS week: 1924 Day: 0 MJD: 57712.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 8 6 15 | 9 11 23 | 7 8 17 |
emr | emr 2976 | 10 8 18 | 9 11 24 | 6 4 16 |
esa | esa 2976 | 8 8 18 | 8 13 27 | 7 7 16 |
gfz | gfz 2971 | 7 6 15 | 8 13 24 | 6 7 14 |
grg | grg 2972 | 8 7 16 | 9 13 29 | 7 9 18 |
igr | igr 2976 | 8 7 16 | 8 12 24 | 6 8 15 |
igs | igs 2976 | 8 7 16 | 8 12 23 | 6 6 14 |
jpl | jpl 3067 | 9 7 18 | 8 12 27 | 7 6 17 |
mit | mit 2976 | 7 7 16 | 9 12 24 | 6 8 16 |
Table 5.1924.1 GPS week: 1924 Day: 1 MJD: 57713.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 9 16 | 7 9 22 | 7 7 17 |
emr | emr 2976 | 8 10 21 | 10 8 24 | 6 5 18 |
esa | esa 2976 | 8 12 21 | 8 9 24 | 7 8 18 |
gfz | gfz 2973 | 8 10 19 | 8 9 24 | 7 7 18 |
grg | grg 2971 | 7 10 18 | 9 11 27 | 7 9 26 |
igr | igr 2976 | 8 11 19 | 8 8 24 | 6 8 17 |
igs | igs 2976 | 7 11 19 | 8 9 23 | 6 7 18 |
jpl | jpl 3072 | 7 11 21 | 9 8 22 | 7 7 20 |
mit | mit 2976 | 7 9 20 | 8 10 24 | 6 7 18 |
Table 5.1924.2 GPS week: 1924 Day: 2 MJD: 57714.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 4 6 12 | 6 11 21 | 5 6 13 |
emr | emr 2976 | 7 8 19 | 7 11 20 | 5 5 13 |
esa | esa 2976 | 6 8 15 | 6 11 23 | 6 6 14 |
gfz | gfz 2975 | 5 5 14 | 5 10 23 | 5 6 12 |
grg | grg 2975 | 6 8 14 | 6 10 20 | 7 6 15 |
igr | igr 2976 | 5 7 15 | 6 10 22 | 5 6 12 |
igs | igs 2976 | 5 7 14 | 6 10 21 | 5 6 12 |
jpl | jpl 3072 | 6 8 17 | 6 11 23 | 5 5 15 |
mit | mit 2976 | 4 5 17 | 7 12 26 | 6 7 13 |
Table 5.1924.3 GPS week: 1924 Day: 3 MJD: 57715.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 3 4 12 | 5 7 18 | 8 6 19 |
emr | emr 2976 | 6 5 18 | 6 7 22 | 7 5 22 |
esa | esa 2976 | 5 5 16 | 5 7 26 | 8 7 22 |
gfz | gfz 2976 | 4 4 13 | 6 5 22 | 7 6 20 |
grg | grg 2976 | 5 6 14 | 5 8 23 | 7 7 22 |
igr | igr 2976 | 4 4 13 | 5 6 25 | 7 6 20 |
igs | igs 2976 | 4 4 13 | 5 6 23 | 7 6 20 |
jpl | jpl 3072 | 5 5 16 | 6 6 24 | 7 6 20 |
mit | mit 2976 | 5 5 14 | 5 6 27 | 9 8 18 |
Table 5.1924.4 GPS week: 1924 Day: 4 MJD: 57716.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 5 9 | 7 10 23 | 9 7 17 |
emr | emr 2976 | 6 8 14 | 8 10 20 | 8 6 15 |
esa | esa 2976 | 6 7 11 | 6 10 24 | 9 7 18 |
gfz | gfz 2976 | 5 6 7 | 6 11 26 | 8 6 17 |
grg | grg 2976 | 5 8 9 | 6 9 25 | 11 12 26 |
igr | igr 2976 | 5 6 8 | 6 10 24 | 8 7 16 |
igs | igs 2976 | 5 6 8 | 6 10 23 | 8 7 16 |
jpl | jpl 3072 | 6 6 12 | 7 10 24 | 8 6 18 |
mit | mit 2976 | 7 9 16 | 7 15 23 | 9 6 15 |
Table 5.1924.5 GPS week: 1924 Day: 5 MJD: 57717.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 5 5 11 | 6 7 24 | 7 6 16 |
emr | emr 2976 | 6 5 17 | 6 5 23 | 7 6 19 |
esa | esa 2976 | 5 4 12 | 6 7 26 | 8 8 21 |
gfz | gfz 2976 | 5 4 11 | 6 6 25 | 7 6 19 |
grg | grg 2976 | 5 5 12 | 7 6 23 | 10 11 26 |
igr | igr 2976 | 5 3 11 | 6 6 24 | 7 5 17 |
igs | igs 2976 | 5 4 12 | 6 6 24 | 7 6 19 |
jpl | jpl 3072 | 5 3 15 | 6 7 23 | 6 7 20 |
mit | mit 2976 | 9 7 17 | 8 12 35 | 10 9 27 |
Table 5.1924.6 GPS week: 1924 Day: 6 MJD: 57718.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 4 4 10 | 9 11 25 | 7 5 12 |
emr | emr 2976 | 8 5 22 | 11 11 27 | 9 6 13 |
esa | esa 2976 | 6 6 16 | 9 11 23 | 8 5 14 |
gfz | gfz 2976 | 6 5 13 | 8 11 26 | 7 6 15 |
grg | grg 2976 | 6 5 18 | 8 11 28 | 10 8 22 |
igr | igr 2976 | 6 4 13 | 9 11 29 | 7 5 13 |
igs | igs 2976 | 6 5 14 | 9 11 24 | 8 6 13 |
jpl | jpl 2880 | 7 6 17 | 9 11 26 | 9 12 20 |
mit | mit 2976 | 7 5 13 | 12 17 35 | 8 7 16 |
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 6.1924 GPS week: 1924 MJD: 57712.500-57718.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 6 90 -11 6 | 7 17
| 19 18 38 82 5 | 3
emr uuuux | 10 12 -109 21 1 | 12 25
| 51 20 59 55 30 | 8
esa uuuuu | -3 -15 129 22 7 | -1 15
| 17 10 46 44 4 | 3
gfz uuuuu | -2 11 -47 -158 -4 | 14 21
| 16 15 57 92 5 | 4
grg uuuuu | 3 -20 10 147 -2 | -1 14
| 23 14 56 50 4 | 2
igr xxxxx | -21 0 54 17 0 | -7 16
| 18 11 52 53 6 | 4
irf xxxxx | 34 -3 2 26 2 | -10 18
| 13 8 45 28 8 | 4
jpl uuuuu | -27 -6 -11 -29 -10 | 14 22
| 27 17 107 49 9 | 6
mit uuuuu | 31 14 -19 58 -13 | 24 31
| 23 19 76 84 7 | 8
sio uuuux | 19 5 -239 -19 -5 | 28 32
| 25 17 52 66 11 | 6
Table 7.1924.0 GPS week: 1924 Day: 0 MJD: 57712.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 22 -4 57 -3 -1 | 11 18
emr uuuux | -44 43 -160 -68 -30 | 24 31
esa uuuuu | 10 -7 145 69 2 | 3 13
gfz uuuuu | -15 7 5 -124 -7 | 20 22
grg uuuuu | -13 -25 106 161 3 | 0 11
igr xxxxx | -13 3 29 -42 -4 | -2 10
irf xxxxx | 29 -13 64 -5 -6 | -4 13
jpl uuuuu | -9 -17 -120 -39 -4 | 20 25
mit uuuuu | 22 -15 92 -35 -15 | 36 39
sio uuuux | 33 14 -227 37 0 | 35 38
Table 7.1924.1 GPS week: 1924 Day: 1 MJD: 57713.500
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 | 20 -7 58 -59 4 | 9 18
emr uuuux | -28 10 -103 18 -16 | 18 30
esa uuuuu | -7 -17 89 72 6 | 1 14
gfz uuuuu | -20 9 36 2 -6 | 18 22
grg uuuuu | -36 1 -50 178 -1 | 0 12
igr xxxxx | 5 -1 104 65 5 | -4 13
irf xxxxx | 21 -12 37 -9 -8 | -6 16
jpl uuuuu | 13 1 -35 -52 -1 | 18 24
mit uuuuu | 36 19 48 -68 -25 | 32 37
sio uuuux | 25 1 -139 -103 -20 | 33 36
Table 7.1924.2 GPS week: 1924 Day: 2 MJD: 57714.500
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 | -18 6 99 -68 12 | 9 17
emr uuuux | 6 13 -54 -33 -6 | 16 28
esa uuuuu | -4 -29 169 6 5 | 1 15
gfz uuuuu | 16 31 -119 -153 -6 | 18 22
grg uuuuu | 7 -9 40 179 -1 | 2 12
igr xxxxx | -21 18 9 3 -8 | -3 14
irf xxxxx | 25 5 0 25 -4 | -7 16
jpl uuuuu | -12 1 -57 61 -18 | 19 26
mit uuuuu | 14 -6 -34 59 -17 | 29 34
sio uuuux | 9 13 -284 0 -2 | 31 34
Table 7.1924.3 GPS week: 1924 Day: 3 MJD: 57715.500
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 43 65 138 6 | 7 15
emr uuuux | -6 12 -25 36 -2 | 11 22
esa uuuuu | -11 -2 187 -26 7 | -1 12
gfz uuuuu | 4 13 -51 -283 -3 | 15 19
grg uuuuu | 15 -45 -20 157 -5 | 0 12
igr xxxxx | -13 1 110 79 0 | -6 14
irf xxxxx | 49 -8 -16 23 2 | -11 16
jpl uuuuu | -52 -23 -87 -25 -2 | 14 21
mit uuuuu | 62 4 -55 89 -15 | 24 28
sio uuuux | 34 -25 -268 -64 -6 | 29 31
Table 7.1924.4 GPS week: 1924 Day: 4 MJD: 57716.500
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 | 0 -3 94 -109 0 | 6 17
emr uuuux | 10 2 -94 62 -3 | 8 23
esa uuuuu | -33 -6 142 -8 6 | -3 15
gfz uuuuu | 6 -17 -26 -171 -3 | 11 20
grg uuuuu | 37 -26 38 194 3 | -3 17
igr xxxxx | -16 -18 100 66 -7 | -8 19
irf xxxxx | 57 1 -11 73 9 | -13 20
jpl uuuuu | -46 24 -48 -4 -13 | 12 22
mit uuuuu | 62 31 -72 170 -7 | 20 29
sio uuuux | 20 -10 -255 -83 -15 | 26 31
Table 7.1924.5 GPS week: 1924 Day: 5 MJD: 57717.500
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 | -26 -7 165 39 8 | 3 16
emr uuuux | 16 24 -136 39 -1 | 3 21
esa uuuuu | 5 -23 114 -21 8 | -5 16
gfz uuuuu | 16 16 -67 -133 7 | 9 19
grg uuuuu | 10 -16 2 111 -5 | -5 18
igr xxxxx | -42 -9 46 -4 10 | -12 21
irf xxxxx | 26 0 19 43 11 | -15 21
jpl uuuuu | -21 -23 81 -98 -25 | 7 21
mit uuuuu | 22 28 18 120 -7 | 16 27
sio uuuux | -31 18 -287 4 -5 | 21 28
Table 7.1924.6 GPS week: 1924 Day: 6 MJD: 57718.500
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 | -20 11 92 -14 12 | 5 19
emr uuuux | 113 -22 -192 93 64 | 3 21
esa uuuuu | 19 -20 55 60 13 | -3 18
gfz uuuuu | -22 19 -107 -247 -10 | 10 21
grg uuuuu | 4 -21 -49 51 -7 | -4 18
igr xxxxx | -48 2 -21 -49 1 | -10 22
irf xxxxx | 32 6 -78 28 12 | -13 22
jpl uuuuu | -64 -4 185 -44 -9 | 6 20
mit uuuuu | 1 33 -128 71 -6 | 15 25
sio uuuux | 44 20 -216 74 13 | 20 26
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