[IGSREPORT-15751] Wk 1455 IGS Final Orbits [Resubmission]
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Dec 13 01:23:21 PST 2007
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IGS Electronic Report 13 Dec 01:23:25 PST 2007 Message Number 15751
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
Final IGS Orbit Combination - Week 1455 (Nov 25, 2007 - Dec 01, 2007)
Contacts: G. Gendt (gendt at gfz-potsdam.de),
Th. Nischan ( nisn at gfz-potsdam.de)
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. 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, no satellite L1/L2 delay calibration should be
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. 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 (weights are those from the orbit combination).
Pole rate combination uses only centres providing estimated pole rates.
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 3 weeks (21 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:
igs1455[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1455[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1455[0-6].cls IGS GPS clock combination summary report.
igs14557.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs14557.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ and JPL. The
other centres are excluded because they either provide broadcast clocks (NGS)
or clock corrections are not provided (SIO). The clock information not
used is still compared to combination for completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics 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.
Day | Centre | PRN/STA list
----+--------+---------------
0 | EMR | ONSA
0 | ESA | YELL
0 | GFZ | 15 DAV1
0 | MIT | 1 6 7 12 14 20 31 TIDB
1 | COD | CHUR
1 | ESA | 9 HARB NTUS YELL
1 | GFZ | 15
1 | MIT | DAEJ TIDB
2 | ESA | LPGS
2 | GFZ | 15 VILL
2 | MIT | 1 11 NTUS
3 | EMR | ONSA
3 | ESA | 9 15 24 NTUS
3 | MIT | 11 BOR1 DRAO NTUS
4 | COD | MCM4 NRIL
4 | EMR | ONSA
4 | GFZ | 21 24
5 | ALL | 32
5 | EMR | MCM4 ONSA SPT0
5 | ESA | BILI
5 | GFZ | JPLM
5 | MIT | 30 GRAZ SANT
6 | EMR | MAR6 TWTF
6 | ESA | NTUS SUTM
6 | GFZ | 4 20 22 NPLD NTUS THTI
6 | MIT | 9 12 30 31 IRKT NTUS SYOG
5. 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)
4 | SIO | ALL (high Transformation - See Table 2)
5 | SIO | ALL (high Transformation - See Table 2)
5 | ESA | 31
6 | SIO | ALL (high Transformation - See Table 2)
6. 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 G24 | | | | | 1 | | |
7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) 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.
8. Small rotations were applied to the all AC orbit and ERP values in order
to align them to the IGS05. These rotations were estimated in the process
of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based
on the common stations between the individual AC SINEX solutions and the
IGS05.snx SINEX. 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 | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .0 .5 .3 -3 0 0 .06
EMR | -1.6 -2.2 4.5 10 3 10 .17
ESA | 4.7 2.6 6.0 6 -19 29 -1.07
GFZ | .4 .0 .5 -4 -12 4 -.16
JPL | -1.5 1.0 14.0 -1 -10 -12 .18
MIT | 4.6 2.8 16.7 11 12 -6 -.24
NGS | 2.6 1.5 -4.0 28 -58 9 -.81
SIO | 2.4 7.0 39.5 48 20 -12 .36
9. 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 navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by NRCan. For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model
is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five 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 1.1455.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1455.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 2.1455.[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 3.1455.[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 and final
part, Table 5, is similar to Table 4 and contains daily precise navigation
statistics (tables 5.1455.0-6).
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 1455 summary. (Nov 25, 2007 - Dec 01, 2007)
Table 1.1455.a GPS week: 1455 MJD: 54429.000-54435.000
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 179| 0 0 1 11 -10 -12 -.27 16 14 | -100 -326 54 89
| 1 0 1 23 15 28 .03 | 217 388
emr 65| -1 -1 0 6 -33 -4 .29 15 15 | 1782 -499 64 101
| 1 0 1 24 20 13 .03 | 1611 1755
esa 66| 1 0 0 33 -32 -11 .23 22 20 | 1828 -527 55 156
| 0 1 3 71 53 50 .05 | 1613 1727
gfz 179| -1 1 1 -2 6 -60 -.08 13 13 | 353 -483 32 109
| 0 0 1 21 17 27 .05 | 538 592
igr n/a| 0 0 -2 5 -9 15 -.00 7 7 | -4176 -625 29 85
| 0 0 0 23 10 20 .03 | 1815 1889
jpl 123| 0 0 0 28 -25 30 .41 11 11 | 5142 -617 28 67
| 0 1 0 21 23 21 .05 | 1581 1753
mit 263| 1 0 -1 12 -4 7 -.43 17 16 | -43 -406 58 128
| 0 0 1 33 43 36 .06 | 269 706
ngs 200| 0 0 -3 -78 89 48 -.34 16 13 | 18345 59293 2392 3905
| 1 1 0 21 34 26 .05 | 48503 158096
sio 97| 4 0 -3 -69 774 -39 .05 28 26 | --- --- --- ---
| 1 1 1 62 727 34 .07 | --- ---
Table 1.1455.b GPS week : 1455 MJD: 54429.000-54435.000
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 | 6 5 5 5 6 6 6 |
2E | 6 6 7 6 6 6 7 |
3 | 6 5 5 5 5 5 5 |
4E | 6 7 9 6 6 6 6 |
5 | 6 5 5 5 4 5 5 |
6 | 5 5 4 4 4 5 4 |
7 | 6 5 5 4 4 4 5 |
8E | 7 7 6 7 7 6 7 |
9E | 7 7 8 8 8 8 8 |
10 | 6 5 5 5 5 6 6 |
11 | 7 8 8 7 8 7 6 |
12 | 6 6 6 6 6 7 6 |
13 | 7 7 7 7 7 7 7 |
14 | 7 6 7 6 6 6 7 |
15 | 10 7 7 10 7 7 7 |
16 | 7 7 7 6 6 6 6 |
17 | 9 6 6 6 7 6 6 |
18 | 6 6 6 6 6 6 6 |
19 | 7 7 7 9 6 6 6 |
20 | 7 6 7 7 6 7 6 |
21E | 6 6 5 5 6 5 5 |
22 | 7 6 6 6 6 6 6 |
23 | 7 7 8 8 7 7 6 |
24E | 8 7 7 9 8 9 6 |
25E | 7 7 7 6 5 6 6 |
26 | 7 6 6 6 5 5 6 |
27E | 6 7 8 7 6 6 7 |
28 | 8 7 8 7 7 7 8 |
30 | 5 5 5 5 4 5 5 |
31E | 7 6 6 6 6 7 6 |
32 | 14 10 13 14 22 14 12 |
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
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1455.0 GPS week: 1455 Day: 0 MJD: 54429.000
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 179| 0 1 1 34 -3 0 -.34 15 14 | -400 42 55 79
| -25 24 |
emr 65| -2 -1 0 -8 -14 -2 .26 18 16 | 1842 391 77 103
| 13 -36 |
esa 66| 1 0 0 61 28 -50 .24 21 21 | 1938 292 62 156
| -34 53 |
gfz 179| -1 1 1 -1 12 -71 -.04 14 14 | 169 -1006 41 120
| 15 45 |
igr n/a| 1 0 -1 3 -1 -2 -.03 7 7 | -4177 550 32 95
| 37 -45 |
jpl 123| 0 -1 0 36 -60 18 .49 13 13 | 5454 149 34 69
| 0 0 |
mit 263| 1 0 0 -14 53 38 -.40 19 18 | -114 -543 96 187
| 39 -50 |
ngs 200| 2 2 -3 -69 44 76 -.34 18 15 | -258 -15 2700 3903
| 94 59 |
sio 97| 2 0 -1 -69 -30 18 .10 27 25 | --- --- --- ---
| -14 64 |
Table 2.1455.1 GPS week: 1455 Day: 1 MJD: 54430.000
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 179| 0 1 0 50 13 15 -.27 15 13 | 114 -520 55 82
| -5 -8 |
emr 65| -1 -1 0 -4 -65 -21 .25 16 16 | 2504 640 65 92
| -26 60 |
esa 66| 1 0 2 -85 30 18 .17 20 20 | 2721 441 61 157
| 19 38 |
gfz 179| -3 1 1 35 -6 -71 -.03 15 15 | -174 179 31 92
| -5 30 |
igr n/a| 0 0 -1 38 -3 52 -.04 6 6 | -3413 774 28 85
| -19 -19 |
jpl 123| 0 0 0 31 -28 15 .40 12 12 | 5876 398 29 71
| 0 0 |
mit 263| 1 -1 0 52 -33 6 -.36 16 14 | -360 311 48 88
| -31 -10 |
ngs 200| 1 0 -3 -96 98 57 -.27 14 12 | 163 -599 2424 4058
| 86 8 |
sio 97| 1 -1 -2 -137 -24 -47 .17 26 25 | --- --- --- ---
| 98 29 |
Table 2.1455.2 GPS week: 1455 Day: 2 MJD: 54431.000
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 179| -2 1 0 14 -25 -37 -.24 14 12 | -145 -219 56 90
| 7 27 |
emr 65| -1 -1 0 31 -50 9 .28 17 17 | 3358 185 64 94
| -15 18 |
esa 66| 1 0 0 136 -113 -71 .26 24 24 | 3388 150 63 177
| 49 77 |
gfz 179| -2 1 3 -28 11 -109 -.03 14 14 | 83 -184 34 101
| -1 5 |
igr n/a| 0 0 -1 37 -29 2 .03 6 6 | -2393 -11 28 80
| -1 3 |
jpl 123| 1 1 0 46 -23 48 .43 12 12 | 6515 68 32 74
| 0 0 |
mit 263| 0 -1 -1 -37 -64 68 -.36 15 13 | 93 -18 52 109
| 10 -29 |
ngs 200| 1 0 -2 -46 120 42 -.30 14 13 | 128341 417821 2509 4004
| 71 -22 |
sio 97| 5 -2 -4 -140 272 -29 .08 28 27 | --- --- --- ---
| 64 73 |
Table 2.1455.3 GPS week: 1455 Day: 3 MJD: 54432.000
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 179| -2 0 2 -14 -18 29 -.24 17 15 | -250 -874 58 96
| 19 62 |
emr 65| 0 -1 2 47 -16 -2 .30 15 15 | 3100 -2274 58 99
| -82 20 |
esa 66| 2 -1 -1 3 -49 15 .26 22 20 | 3072 -2230 43 139
| 8 90 |
gfz 179| -1 1 0 -11 17 -38 -.12 12 12 | 320 -1149 25 86
| -16 41 |
igr n/a| 0 0 -3 1 -8 26 .01 7 7 | -2751 -2371 27 63
| -33 8 |
jpl 123| 0 0 0 -4 -46 29 .45 12 12 | 6138 -1955 25 63
| 0 0 |
mit 263| 0 -2 0 43 34 -35 -.42 16 14 | -80 -1579 49 107
| -12 -55 |
ngs 200| 0 1 -2 -74 88 19 -.30 16 11 | -147 -987 2553 4134
| 62 73 |
sio 97| 7 -1 -5 -115 825 -21 .00 28 27 | --- --- --- ---
| 74 31 |
Table 2.1455.4 GPS week: 1455 Day: 4 MJD: 54433.000
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 179| 0 0 2 -8 -22 -45 -.26 16 14 | -217 239 50 98
| 14 26 |
emr 65| 0 0 1 5 -10 -6 .31 13 13 | 1523 -479 63 119
| -7 -15 |
esa 66| 1 -3 1 0 -54 22 .16 19 19 | 1542 -520 54 147
| 27 35 |
gfz 179| -2 1 0 -19 4 -61 -.10 11 11 | 102 290 26 94
| 20 41 |
igr n/a| 0 0 -2 -12 3 -6 -.00 7 7 | -4274 -686 26 81
| 42 -30 |
jpl 123| 0 0 0 44 2 59 .40 9 9 | 5012 -476 22 59
| 0 0 |
mit 263| 0 -1 -1 17 12 12 -.53 18 19 | -55 274 51 150
| -16 -43 |
ngs 200| 0 0 -4 -83 53 10 -.40 16 12 | -7 -131 2198 3832
| 76 93 |
sio 97| 3 0 -2 -27 1144 -91 -.02 28 23 | --- --- --- ---
| 72 60 |
Table 2.1455.5 GPS week: 1455 Day: 5 MJD: 54434.000
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 179| 0 0 4 2 -22 -16 -.27 18 16 | 221 -645 55 97
| 3 42 |
emr 65| 0 -1 0 -18 -33 14 .33 13 13 | 1645 -3461 61 107
| -10 7 |
esa 66| 0 1 -4 88 -1 -67 .21 26 20 | 1582 -3427 53 154
| 13 8 |
gfz 179| 0 1 2 16 29 -49 -.16 13 13 | 492 -998 32 125
| -51 26 |
igr n/a| 0 0 -3 -16 -14 21 -.02 9 9 | -4313 -3933 33 94
| 13 4 |
jpl 123| 0 0 0 0 -22 43 .37 10 10 | 5247 -3876 25 77
| 0 0 |
mit 263| 1 0 -2 36 4 -11 -.47 17 16 | 470 -1070 51 136
| -17 -28 |
ngs 200| -1 0 -4 -113 77 49 -.36 18 15 | 315 -695 2106 3746
| 82 32 |
sio 97| 5 1 -5 -1 1434 -50 .03 31 28 | --- --- --- ---
| 93 91 |
Table 2.1455.6 GPS week: 1455 Day: 6 MJD: 54435.000
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 179| 0 0 0 0 4 -30 -.25 15 15 | -23 -310 52 86
| -3 19 |
emr 65| -1 -1 0 -10 -41 -20 .32 14 14 | -1498 1503 62 99
| 22 47 |
esa 66| 2 0 6 26 -66 55 .31 19 19 | -1441 1600 53 166
| -44 39 |
gfz 179| -1 0 2 -7 -23 -22 -.08 11 11 | 1482 -516 35 145
| -59 49 |
igr n/a| 1 0 -2 -12 -10 13 .03 9 8 | -7913 1299 34 101
| 33 23 |
jpl 123| 0 0 0 43 2 -2 .34 10 10 | 1756 1368 32 60
| 0 0 |
mit 263| 1 0 -3 -9 -41 -24 -.46 17 16 | -257 -223 62 120
| 2 -8 |
ngs 200| -1 2 -3 -67 140 79 -.40 17 15 | 11 -339 2254 3658
| 54 11 |
sio 97| 3 2 -4 3 1804 -54 -.02 30 28 | --- --- --- ---
| 84 45 |
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 3.1455.0 GPS week: 1455 Day: 0 MJD: 54429.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 10 13 20 11 6 11 21 17 23 5 | 15 25 27 20 18 26 18 14 27 17
2E | 15 16 19 15 7 12 18 16 27 6 | 31 42 29 40 33 35 31 31 39 33
3 | 10 12 22 13 5 11 17 20 20 5 | 25 31 27 25 28 30 18 29 27 25
4E | 18 17 20 11 6 10 15 17 24 6 | 107 106 90 108 108 111 108 107 108 108
5 | 8 15 17 13 5 12 14 16 26 5 | 33 44 38 34 37 38 37 35 46 36
6 | 9 14 19 10 8 7 17 18 25 5 | 26 34 39 29 30 28 28 34 34 28
7 | 11 15 15 10 8 8 18 13 30 5 | 29 36 30 30 32 28 27 32 35 28
8 | 20 9 27 16 8 14 23 17 29 7 | 77 86 81 86 83 91 88 80 98 84
9E | 20 18 20 16 8 12 20 16 30 7 | 51 52 44 53 47 47 41 47 52 47
10 | 11 10 29 9 7 10 19 16 18 5 | 18 23 30 23 20 26 18 20 25 19
11 | 15 20 23 15 9 12 13 21 21 6 | 16 37 31 27 24 26 19 26 18 21
12 | 10 15 15 12 8 14 14 21 32 6 | 28 37 35 33 29 34 26 26 40 30
13 | 20 19 18 15 6 15 17 22 27 7 | 19 33 29 25 20 27 18 15 31 19
14 | 13 19 18 14 4 12 19 20 33 6 | 17 35 27 24 19 28 21 19 32 20
X15 | 20 15 47 21 10 12 26 18 --- 9 | 30 34 49 33 28 36 20 24 --- 29
16 | 15 14 16 12 6 15 29 20 32 7 | 19 31 29 27 23 32 26 26 31 24
17 | 18 46 23 14 10 15 21 18 28 9 | 27 59 34 36 30 32 28 33 34 31
18 | 17 17 14 12 5 15 19 18 21 6 | 26 36 32 31 25 34 19 23 31 26
19 | 17 15 23 18 7 16 18 23 31 7 | 23 39 35 39 30 42 21 27 27 30
20 | 16 17 26 12 7 16 16 15 36 7 | 22 34 35 32 28 33 23 25 37 27
21E | 13 17 16 14 6 12 12 14 19 5 | 22 32 31 30 26 29 26 26 25 26
22 | 19 15 17 13 5 17 16 22 27 6 | 19 32 32 27 23 30 19 24 35 22
23 | 17 20 18 9 7 17 15 22 28 6 | 17 35 30 23 21 29 18 19 23 20
24E | 20 16 28 21 8 14 25 16 27 7 | 85 95 97 94 91 92 93 92 84 90
25E | 16 20 18 13 7 11 19 16 30 6 | 25 30 28 23 22 27 24 28 40 23
26 | 14 12 30 15 7 10 20 13 25 6 | 22 26 31 24 22 26 24 17 31 21
27E | 21 9 17 11 7 12 23 16 22 6 | 33 31 35 33 30 27 36 38 26 30
28 | 18 17 22 15 7 17 22 17 38 7 | 35 36 34 36 33 34 37 34 49 32
30 | 9 15 15 17 6 9 12 18 19 5 | 60 70 58 62 61 63 64 59 63 62
31E | 11 18 21 15 7 15 21 20 30 6 | 18 31 34 27 20 27 18 19 35 21
X32 | 13 --- --- --- 13 --- --- 16 --- 14 | 17 --- --- --- 23 --- --- 26 --- 22
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 18 21 14 7 13 19 18 27 |T 32 42 39 37 34 38 33 34 40 33
WRMS | 14 16 21 14 7 13 18 15 25 |NE 26 38 36 33 29 35 28 29 36 29
MEDI | 15 15 19 13 7 12 18 17 27 |MD 25 35 32 30 28 30 24 26 34 27
Table 3.1455.1 GPS week: 1455 Day: 1 MJD: 54430.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 10 17 24 14 4 10 10 11 21 5 | 16 29 34 25 17 25 16 15 25 19
2E | 15 17 12 13 5 13 19 15 22 6 | 34 42 41 35 34 39 35 37 40 35
3 | 11 14 11 12 5 13 15 15 18 5 | 20 26 26 26 23 27 16 22 21 21
4E | 18 16 21 14 5 11 20 15 23 6 | 109 117 87 112 109 112 119 116 126 113
5 | 8 14 19 15 4 6 8 10 21 4 | 27 31 26 25 27 26 28 30 33 26
6 | 8 13 18 11 5 7 10 13 35 5 | 23 27 35 23 23 24 24 31 42 24
7 | 8 14 12 10 5 7 9 11 42 5 | 23 26 30 22 21 22 25 26 52 24
8E | 23 13 25 21 9 14 18 15 28 7 | 52 52 48 54 52 54 51 53 65 52
9E | 23 17 23 14 9 11 16 13 27 6 | 53 55 51 53 51 49 47 54 52 50
10 | 11 13 24 12 5 8 13 12 20 5 | 17 22 30 20 16 19 16 17 25 17
X11 | 14 22 34 19 14 --- 11 12 21 7 | 16 32 33 25 21 --- 18 19 23 18
12 | 11 15 14 15 6 10 11 16 27 5 | 20 31 33 30 22 28 21 24 26 24
13 | 20 20 18 16 6 15 21 12 30 7 | 22 38 35 28 23 29 26 23 29 24
14 | 11 19 16 20 6 11 17 12 29 6 | 16 35 33 25 20 25 18 21 23 20
X15 | 17 16 24 17 10 12 19 16 --- 7 | 26 37 42 31 25 33 23 27 --- 28
16 | 16 12 17 14 6 15 24 18 29 6 | 18 28 33 24 19 30 16 20 22 20
17 | 14 15 20 15 8 12 16 12 28 6 | 23 32 32 33 23 27 27 30 28 25
18 | 17 19 19 12 4 13 18 13 21 6 | 25 37 37 30 23 33 20 24 26 25
19 | 16 16 16 13 11 16 18 21 35 7 | 21 35 33 30 29 36 16 28 40 26
20 | 16 20 17 13 6 15 14 14 23 6 | 25 40 34 32 29 32 29 30 39 30
21E | 11 17 22 17 5 8 12 11 24 5 | 19 28 33 30 21 23 26 24 31 23
22 | 13 15 24 15 7 13 14 14 25 6 | 16 33 37 24 20 28 20 20 30 22
X23 | 14 25 15 15 6 --- 15 14 24 7 | 19 40 31 27 24 --- 23 25 24 24
24E | 18 17 25 15 6 13 20 14 25 6 | 78 83 82 82 77 80 87 80 80 80
25E | 15 23 19 15 6 10 14 15 30 6 | 16 31 26 23 16 24 21 20 35 18
26 | 16 11 31 14 6 9 12 14 21 6 | 24 29 43 23 21 26 24 23 34 24
X27E | 21 13 20 17 6 --- 13 11 28 7 | 28 30 32 31 25 --- 34 32 23 27
28 | 18 17 18 17 6 19 20 13 31 7 | 25 34 33 29 24 29 30 26 32 26
30 | 7 12 18 21 3 6 8 11 16 4 | 42 44 39 43 39 40 39 42 39 39
31E | 11 16 19 19 7 14 13 16 20 6 | 15 28 33 30 23 26 16 25 31 21
X32 | 8 --- --- --- 9 --- --- 11 --- 10 | 14 --- --- --- 15 --- --- 15 --- 14
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 16 20 15 6 12 16 14 26 |T 28 38 38 34 29 35 30 31 37 30
WRMS | 13 16 20 15 6 12 14 12 25 |NE 21 32 33 27 22 28 22 24 30 23
MEDI | 14 16 19 15 6 12 14 13 25 |MD 23 32 33 29 23 28 24 25 31 24
Table 3.1455.2 GPS week: 1455 Day: 2 MJD: 54431.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 9 15 26 14 3 9 8 15 22 5 | 12 21 36 23 14 23 16 16 37 15
2E | 13 19 38 11 6 12 17 13 22 6 | 73 74 95 73 69 69 76 75 86 75
3 | 9 14 15 14 5 10 11 11 23 4 | 19 25 30 22 22 23 21 25 28 20
X4E | 18 21 --- 26 18 16 16 19 32 8 | 124 130 --- 126 124 130 128 128 118 125
5 | 7 14 26 11 5 8 9 13 22 4 | 19 28 24 20 22 24 21 28 40 21
6 | 8 14 14 11 4 6 9 12 18 4 | 18 28 18 25 22 24 24 26 43 23
7 | 7 15 17 17 7 7 8 12 24 4 | 21 26 23 28 24 24 24 30 51 24
8E | 17 14 29 12 5 13 13 13 27 6 | 50 52 56 53 51 53 55 49 69 52
9E | 29 17 29 21 9 12 18 18 34 8 | 43 44 42 48 41 37 36 46 49 38
10 | 12 13 26 12 4 8 13 13 23 5 | 16 24 31 23 18 20 20 23 38 19
X11 | 15 21 34 19 7 --- 11 12 --- 8 | 11 33 34 24 18 --- 19 16 --- 17
12 | 11 14 28 15 7 12 12 16 30 6 | 22 33 36 32 25 33 26 28 42 26
13 | 17 21 23 18 5 17 16 12 24 6 | 15 36 33 25 21 31 20 16 35 20
14 | 11 16 26 17 7 11 18 18 38 6 | 16 30 37 27 18 25 19 24 39 19
X15 | 17 16 32 14 7 14 17 15 --- 7 | 21 32 38 30 22 32 21 23 --- 23
16 | 13 17 18 13 7 15 21 15 42 7 | 19 30 35 24 22 29 22 23 37 22
17 | 12 16 25 13 10 15 12 16 29 6 | 19 30 30 31 26 27 21 27 32 22
18 | 15 21 27 12 5 13 18 14 25 6 | 27 37 30 31 24 33 21 25 48 26
19 | 15 19 20 14 6 18 18 18 28 6 | 16 36 31 28 23 32 19 19 38 22
20 | 14 21 27 14 7 16 11 17 29 6 | 19 36 36 26 27 31 25 20 31 23
21E | 10 17 28 12 4 11 11 11 19 5 | 23 33 46 31 26 30 29 32 36 28
22 | 13 16 25 15 4 12 15 15 31 6 | 17 31 29 27 20 30 19 19 36 21
X23 | 14 25 22 14 7 --- 13 13 --- 7 | 13 39 34 25 23 --- 20 22 --- 21
24E | 21 21 19 14 6 15 17 12 24 6 | 66 75 67 72 71 74 79 71 79 71
25E | 13 13 28 15 6 11 12 15 43 6 | 17 25 34 21 17 27 18 21 48 18
X26 | 14 14 --- 15 5 9 11 13 24 5 | 18 24 --- 24 17 23 20 20 39 19
X27E | 19 14 37 17 5 --- 11 14 --- 8 | 29 27 44 29 26 --- 28 33 --- 26
28 | 19 16 22 17 7 17 22 16 33 7 | 22 28 34 30 22 29 30 20 36 21
30 | 4 12 19 14 4 8 11 12 15 4 | 43 50 42 42 45 48 46 48 58 45
31E | 11 17 14 14 6 11 17 16 18 5 | 19 28 34 28 22 28 22 24 45 23
X32 | 14 --- --- --- 23 --- 12 25 --- 12 | 14 --- --- --- 18 --- 12 12 --- 13
------+---------------------------------------------------+----------------------------------------------------
RMS | 14 17 24 14 6 12 15 14 28 |T 27 38 37 34 30 36 30 31 47 30
WRMS | 12 17 24 14 6 12 13 13 27 |NE 18 31 32 27 22 28 22 23 39 21
MEDI | 13 16 26 14 6 12 13 14 24 |MD 19 31 34 28 22 30 21 24 39 22
Table 3.1455.3 GPS week: 1455 Day: 3 MJD: 54432.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 12 12 20 9 7 10 12 11 25 5 | 13 25 32 20 14 24 14 14 52 16
2 | 14 20 17 8 6 8 22 16 32 6 | 36 47 44 42 42 43 41 42 73 40
3 | 10 12 13 10 6 10 10 17 23 4 | 23 31 24 23 28 30 23 23 60 25
4 | 19 18 21 13 6 8 15 14 32 6 | 68 74 104 74 72 74 75 71 88 73
5 | 7 10 19 12 7 8 10 12 21 4 | 22 27 30 21 25 25 23 27 61 22
6 | 9 11 15 11 5 6 9 9 24 4 | 20 26 27 25 25 24 23 26 69 22
7 | 9 14 9 11 5 6 8 7 29 3 | 23 29 28 27 27 26 22 27 74 24
X8E | 16 14 --- 12 6 14 13 18 27 6 | 62 72 --- 63 67 70 70 68 76 67
9E | 30 11 25 13 7 10 23 19 29 7 | 48 45 46 51 46 41 39 51 68 44
10 | 11 16 20 8 10 8 13 16 25 5 | 12 26 26 18 17 20 17 21 58 16
X11 | 12 16 26 13 6 --- 12 13 --- 7 | 9 27 30 21 16 --- 12 12 --- 14
12 | 13 11 16 13 9 10 20 18 30 6 | 19 30 30 27 23 30 21 21 56 22
13 | 19 18 20 13 6 14 18 18 23 7 | 15 36 33 22 22 29 19 19 56 21
14 | 14 15 20 15 6 9 20 15 34 6 | 15 32 28 24 19 26 19 18 50 19
15 | 21 17 61 12 7 12 21 16 --- 9 | 23 35 70 28 25 32 21 25 --- 27
16 | 18 14 13 11 6 13 18 15 35 6 | 15 29 25 23 19 27 15 20 49 19
17 | 15 12 21 13 6 12 15 13 30 5 | 24 30 37 32 28 29 26 27 53 26
18 | 15 14 21 9 6 11 16 17 33 6 | 21 31 35 28 26 30 16 25 74 22
19 | 20 17 18 10 8 30 22 22 37 8 | 14 32 32 25 25 42 19 19 66 23
20 | 18 17 23 11 7 12 16 16 29 6 | 17 34 34 26 24 31 20 18 46 24
21E | 10 19 13 9 6 7 10 11 22 4 | 24 34 28 26 25 25 27 27 59 24
22 | 15 14 21 12 5 11 18 19 33 6 | 16 32 32 24 20 28 15 23 60 20
X23 | 16 24 18 11 3 --- 17 15 27 7 | 15 40 32 25 24 --- 20 20 50 23
24E | 39 22 24 14 11 18 21 16 30 9 | 130 149 151 145 141 148 149 143 144 144
25E | 13 12 18 13 6 12 12 20 31 6 | 14 23 25 17 15 26 15 25 54 15
26 | 12 13 25 13 6 8 11 17 21 5 | 15 22 32 21 17 22 14 21 57 17
X27E | 19 13 19 12 10 --- 14 15 37 6 | 25 24 25 28 23 --- 25 24 52 21
28 | 20 20 16 9 6 15 24 18 33 7 | 23 30 26 25 24 29 28 24 54 21
30 | 8 10 13 16 5 7 8 11 17 4 | 41 44 42 39 42 44 40 40 64 40
31E | 12 13 16 15 7 12 14 11 17 5 | 17 31 31 22 21 29 14 16 54 19
X32 | 17 --- --- --- 20 --- 13 25 --- 13 | 13 --- --- --- 28 --- 12 29 --- 13
------+---------------------------------------------------+----------------------------------------------------
RMS | 17 15 22 12 7 12 16 16 28 |T 26 38 39 33 31 37 28 31 63 29
WRMS | 15 15 20 12 7 12 14 11 27 |NE 21 33 36 27 26 31 23 25 60 24
MEDI | 15 14 19 12 6 10 15 16 29 |MD 20 31 32 25 25 29 21 24 58 22
Table 3.1455.4 GPS week: 1455 Day: 4 MJD: 54433.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 10 10 33 11 6 10 13 11 25 5 | 13 19 29 20 14 19 15 15 73 13
2 | 14 17 12 8 6 8 20 15 26 5 | 26 40 32 31 29 32 34 28 83 29
3 | 11 14 21 12 8 8 7 10 29 4 | 20 26 21 22 22 24 20 24 82 20
4 | 15 13 18 12 5 10 21 15 29 6 | 60 67 53 65 62 63 68 60 96 62
5 | 5 10 17 10 6 4 9 12 22 4 | 25 31 27 28 28 28 33 25 75 27
6 | 7 9 14 10 4 3 9 12 21 3 | 20 26 32 26 25 25 21 27 81 23
7 | 8 10 13 10 5 5 10 12 24 4 | 18 25 21 23 22 21 21 22 78 20
8E | 16 14 30 10 7 10 13 19 21 6 | 43 45 61 43 45 45 41 49 87 42
9E | 27 14 19 15 9 10 24 21 31 7 | 50 48 51 51 45 44 41 49 86 45
10 | 11 10 20 8 4 7 16 18 20 5 | 14 19 26 17 13 19 15 14 76 15
X11 | 18 15 28 15 6 --- 15 13 --- 7 | 9 26 35 21 18 --- 15 13 --- 14
12 | 14 12 18 12 6 8 16 18 34 5 | 18 29 35 28 22 29 23 18 73 23
13 | 18 17 22 13 5 12 20 16 25 6 | 18 35 37 23 23 26 20 18 82 21
14 | 14 13 20 13 4 7 17 15 38 5 | 13 30 30 25 18 23 15 17 68 18
15 | 19 11 18 11 7 11 30 20 --- 7 | 28 34 33 32 27 32 22 26 --- 27
16 | 17 11 16 11 6 11 20 16 30 5 | 14 27 26 23 18 24 16 15 78 18
17 | 15 12 14 12 9 8 34 16 30 6 | 20 30 30 28 25 26 36 24 69 24
18 | 17 15 14 9 8 10 16 16 36 5 | 20 33 29 27 24 31 19 22 96 23
19 | 16 14 12 10 8 11 17 13 31 5 | 16 31 32 26 23 31 14 15 79 22
20 | 17 14 17 9 9 12 17 18 31 6 | 17 32 35 25 23 28 21 16 68 23
21 | 18 18 23 8 8 7 15 13 35 5 | 50 56 67 52 50 55 54 52 88 53
22 | 15 14 12 11 6 10 15 17 34 5 | 14 30 27 23 19 26 15 22 82 19
23 | 19 19 19 9 7 11 23 16 34 6 | 16 37 33 24 22 28 21 19 82 22
24E | 21 16 25 12 12 13 26 19 29 7 | 87 89 88 83 84 83 84 85 97 84
25E | 12 11 16 11 7 9 12 19 22 5 | 12 25 25 19 16 26 18 23 75 17
26 | 12 8 20 10 6 7 16 18 25 5 | 19 22 29 19 16 21 12 16 79 17
27E | 18 12 20 12 7 11 13 18 24 6 | 19 27 33 27 23 25 29 30 68 23
28 | 21 12 21 12 5 13 27 14 39 7 | 17 27 30 25 22 25 33 20 66 21
30 | 8 9 13 12 6 6 9 11 21 4 | 36 43 41 40 39 41 38 37 71 39
31E | 12 15 25 12 5 10 16 13 15 6 | 11 28 33 20 16 23 12 12 72 16
X32 | 19 --- --- --- 47 --- 27 43 --- 22 | 13 --- --- --- 38 --- 13 37 --- 14
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 13 19 11 7 9 18 16 28 |T 24 34 36 30 28 31 27 27 78 26
WRMS | 14 13 19 11 7 9 19 12 23 |NE 21 32 32 28 25 29 24 24 78 24
MEDI | 15 13 18 11 6 10 16 16 29 |MD 18 30 32 25 23 26 21 22 78 22
Table 3.1455.5 GPS week: 1455 Day: 5 MJD: 54434.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 11 10 32 11 9 8 15 15 38 6 | 11 20 33 17 14 19 15 13 89 15
2 | 16 16 17 13 8 7 16 16 24 5 | 22 37 34 31 27 29 26 26 102 28
X3 | 10 9 --- 11 11 8 11 11 28 4 | 15 21 --- 19 20 19 16 18 96 17
4 | 15 17 21 13 8 7 14 15 25 5 | 41 49 48 47 45 49 37 44 111 45
5 | 8 10 17 15 7 5 10 12 27 4 | 32 33 35 34 35 33 32 30 90 32
6 | 11 10 18 10 8 5 11 17 25 4 | 18 24 26 21 24 23 18 23 103 19
7 | 10 11 11 11 7 5 12 14 33 4 | 21 24 29 24 25 24 21 23 108 21
8E | 14 10 26 10 10 10 16 17 27 5 | 49 50 47 48 46 48 51 48 109 47
9E | 28 16 18 15 10 12 21 24 26 7 | 50 48 50 53 46 45 41 53 102 46
10 | 12 11 27 9 5 8 14 15 22 5 | 16 23 32 21 17 21 16 20 98 18
X11 | 13 14 22 15 11 --- 13 16 31 6 | 9 29 32 22 20 --- 15 16 96 17
12 | 19 12 17 20 10 8 19 18 31 6 | 19 29 28 32 21 27 24 19 96 22
13 | 20 17 20 13 10 12 20 19 29 6 | 18 37 34 25 24 28 21 22 99 23
14 | 15 13 18 17 6 7 16 19 41 6 | 13 29 29 23 18 23 18 20 88 19
15 | 20 14 18 12 8 12 21 21 --- 6 | 22 33 29 28 21 30 15 28 --- 24
16 | 17 13 13 11 11 11 20 20 31 6 | 14 27 26 23 20 27 18 20 97 19
17 | 15 13 27 13 11 8 18 15 29 6 | 16 26 39 27 20 23 23 21 96 21
18 | 18 14 19 11 5 10 16 16 28 6 | 21 29 32 26 21 27 22 20 109 21
19 | 16 9 17 9 9 13 16 18 36 5 | 15 31 30 26 22 29 12 19 102 21
20 | 19 16 13 11 12 14 17 22 34 6 | 17 33 28 26 24 28 20 21 89 23
21 | 15 15 17 11 6 8 13 13 31 5 | 24 32 36 26 25 27 25 25 103 25
22 | 16 14 16 15 7 9 15 19 29 6 | 15 29 29 24 18 23 17 25 101 19
23 | 20 18 16 10 9 14 21 20 33 7 | 17 40 33 26 23 30 24 20 86 24
24 | 44 14 21 11 18 12 25 21 36 9 | 91 112 120 114 114 113 117 110 133 110
25E | 12 13 23 10 11 9 14 19 33 5 | 14 24 31 19 16 24 18 19 94 17
26 | 13 11 20 12 7 8 13 17 27 5 | 18 25 23 22 18 21 12 23 97 18
27E | 14 13 24 10 11 10 16 18 38 6 | 26 29 32 32 25 25 32 32 90 26
28 | 21 12 18 13 7 17 24 18 40 7 | 17 27 27 25 19 25 29 23 89 19
30 | 7 11 19 15 6 6 8 13 22 4 | 27 33 38 26 31 30 28 28 99 27
31E | 12 15 90 17 11 9 16 15 17 6 | 16 29 62 25 21 25 12 15 93 18
X32 | 14 --- --- --- 40 --- 15 28 --- 14 | 11 --- --- --- 39 --- 15 28 --- 15
------+---------------------------------------------------+----------------------------------------------------
RMS | 18 13 26 13 9 10 17 18 31 |T 23 33 36 30 27 30 25 27 98 26
WRMS | 16 13 20 13 9 10 16 15 28 |NE 21 33 35 29 27 30 24 26 99 25
MEDI | 15 13 18 11 9 9 16 17 29 |MD 18 29 32 26 22 27 21 23 97 21
Table 3.1455.6 GPS week: 1455 Day: 6 MJD: 54435.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 12 14 27 10 7 9 12 16 32 5 | 18 26 32 24 19 21 21 23 119 18
2 | 17 21 29 11 8 9 14 18 29 6 | 25 35 42 26 27 28 27 29 127 27
3 | 10 11 16 13 6 8 12 14 25 5 | 23 27 22 25 26 24 24 29 114 22
4 | 14 12 25 11 12 7 16 17 31 5 | 43 45 51 47 44 48 43 44 128 45
5 | 7 11 13 10 9 8 14 12 24 4 | 38 42 39 35 38 40 42 43 128 36
6 | 8 11 15 10 7 6 10 14 26 4 | 26 31 38 33 34 32 25 38 132 28
7 | 8 11 12 11 8 8 14 12 32 4 | 26 29 33 33 33 31 22 34 136 25
8E | 15 12 26 9 8 13 18 19 27 6 | 73 73 68 71 73 73 73 74 144 71
9E | 19 15 20 12 8 13 26 29 31 7 | 46 50 52 54 50 49 49 59 117 48
10 | 12 11 25 9 7 9 13 17 20 5 | 15 21 25 20 17 18 16 29 126 16
11 | 14 15 20 14 8 9 13 18 26 6 | 11 26 28 22 17 18 14 17 114 15
12 | 17 12 13 11 10 10 22 16 32 6 | 19 29 29 29 20 27 27 24 120 23
13 | 17 18 24 14 8 11 21 15 24 7 | 17 37 39 26 22 25 23 19 121 21
14 | 15 23 22 12 7 8 16 16 42 6 | 19 38 31 28 22 25 22 24 115 22
15 | 21 16 17 8 9 13 20 17 41 6 | 27 32 31 29 24 29 21 29 86 24
16 | 17 12 14 11 6 12 18 21 30 6 | 19 28 29 26 19 28 18 19 113 20
17 | 14 16 13 10 10 9 22 18 31 6 | 24 33 37 36 30 32 34 34 116 29
18 | 17 17 18 8 7 11 17 15 22 6 | 27 36 37 33 29 31 25 28 129 26
19 | 14 11 17 9 11 10 16 18 34 5 | 18 31 28 28 25 30 15 22 115 23
20 | 15 16 11 11 9 11 17 18 28 5 | 16 33 28 28 22 27 19 23 114 23
21 | 12 16 17 6 7 8 14 13 36 5 | 29 34 36 35 33 32 30 34 136 30
22 | 16 14 16 10 7 9 14 20 29 5 | 21 32 33 30 24 25 21 27 126 22
23 | 17 18 13 8 7 14 19 16 30 6 | 17 37 34 27 20 29 20 18 117 22
24 | 16 13 16 8 14 11 22 14 44 6 | 78 91 89 94 87 90 92 88 150 88
25E | 15 12 22 11 7 11 16 13 28 5 | 15 21 24 20 16 23 20 21 122 15
26 | 15 12 21 11 8 9 17 20 29 6 | 21 23 30 23 17 18 15 25 115 17
27E | 16 12 33 14 10 12 16 18 28 7 | 22 25 42 31 21 22 31 29 115 23
28 | 21 14 19 12 10 15 26 21 36 7 | 21 26 32 26 20 26 33 24 111 21
30 | 7 12 16 12 8 8 10 14 25 4 | 31 38 35 28 34 33 34 36 117 30
31E | 13 13 13 9 7 14 17 18 18 5 | 15 27 31 19 18 27 13 18 121 18
X32 | 17 --- --- --- 17 --- 12 20 --- 12 | 19 --- --- --- 34 --- 22 43 --- 22
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 14 19 11 9 10 17 17 30 |T 26 35 36 32 29 32 28 32 121 28
WRMS | 15 14 19 11 8 10 16 15 28 |NE 24 34 35 31 28 30 27 30 121 26
MEDI | 15 13 17 11 8 9 16 17 29 |MD 21 32 33 28 24 28 23 29 119 23
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 4.1455 GPS week: 1455 MJD: 54429.0-54435.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 |U 9 10 24 |U 15 12 52 |U 6 7 18 |
emr | emr 2860 |U 21 20 49 |U 19 14 67 | 11 11 28 |
esa | esa 2824 |U 12 12 31 |U 15 12 53 | 8 8 21 |
gfz | gfz 2849 |U 21 19 47 |U 18 14 68 |U 11 9 28 |
igr | igr 2878 | 13 15 37 | 15 17 61 | 10 10 25 |
igs | igs 2912 | 18 19 100 | 16 14 60 | 15 17 41 |
jpl | jpl 2711 |U 22 23 85 |U 18 16 69 |U 10 10 27 |
mit | mit 2948 |U 21 23 48 |U 21 16 88 |U 9 9 22 |
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 5.1455.0 GPS week: 1455 Day: 0 MJD: 54429.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 8 7 25 | 12 10 46 | 5 6 15 |
emr | emr 2854 | 19 17 36 | 17 14 83 | 10 9 28 |
esa | esa 2876 | 11 9 23 | 11 12 45 | 7 9 20 |
gfz | gfz 2842 | 18 19 35 | 12 13 64 | 10 9 27 |
igr | igr 2870 | 9 11 37 | 12 23 63 | 11 17 28 |
igs | igs 2876 | 23 25 156 | 11 14 46 | 12 14 29 |
jpl | jpl 2854 | 15 15 25 | 15 16 58 | 7 12 26 |
mit | mit 2880 | 27 23 57 | 31 30 168 | 15 10 29 |
Table 5.1455.1 GPS week: 1455 Day: 1 MJD: 54430.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2959 | 15 20 32 | 13 16 41 | 12 17 40 |
emr | emr 2860 | 15 18 36 | 21 15 87 | 20 31 47 |
esa | esa 2880 | 16 22 43 | 14 12 44 | 10 10 20 |
gfz | gfz 2844 | 12 20 37 | 16 14 78 | 11 14 32 |
igr | igr 2880 | 13 18 31 | 13 17 51 | 11 12 24 |
igs | igs 2880 | 17 16 56 | 17 14 62 | 52 65 145 |
jpl | jpl 2576 | 12 27 33 | 19 22 96 | 13 11 37 |
mit | mit 2880 | 11 12 28 | 17 15 91 | 9 9 24 |
Table 5.1455.2 GPS week: 1455 Day: 2 MJD: 54431.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2965 | 11 6 16 | 20 9 59 | 6 5 18 |
emr | emr 2858 | 20 13 97 | 20 9 62 | 9 7 26 |
esa | esa 2688 | 13 7 25 | 16 9 47 | 8 7 24 |
gfz | gfz 2844 | 22 10 90 | 22 9 84 | 10 7 25 |
igr | igr 2880 | 18 11 23 | 17 13 61 | 10 9 25 |
igs | igs 2941 | 20 12 63 | 17 10 70 | 11 10 26 |
jpl | jpl 2574 | 28 16 237 | 19 13 74 | 13 13 36 |
mit | mit 2976 | 26 27 67 | 21 11 73 | 7 8 21 |
Table 5.1455.3 GPS week: 1455 Day: 3 MJD: 54432.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 6 7 17 | 13 10 55 | 6 7 18 |
emr | emr 2860 | 26 23 33 | 21 11 50 | 9 9 22 |
esa | esa 2784 | 11 14 25 | 13 9 57 | 7 9 22 |
gfz | gfz 2844 | 33 16 26 | 18 12 61 | 12 10 35 |
igr | igr 2879 | 14 10 38 | 14 11 54 | 13 14 36 |
igs | igs 2944 | 18 23 201 | 16 16 67 | 9 7 22 |
jpl | jpl 2576 | 23 18 129 | 19 14 60 | 13 11 33 |
mit | mit 2976 | 21 19 39 | 19 11 69 | 11 6 27 |
Table 5.1455.4 GPS week: 1455 Day: 4 MJD: 54433.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2961 | 9 14 25 | 15 11 46 | 6 5 15 |
emr | emr 2864 | 24 31 57 | 16 12 48 | 9 9 25 |
esa | esa 2880 | 15 16 36 | 15 12 53 | 9 6 20 |
gfz | gfz 2855 | 22 30 51 | 19 11 53 | 11 9 29 |
igr | igr 2880 | 15 26 63 | 16 15 54 | 11 7 28 |
igs | igs 2915 | 19 25 141 | 16 13 58 | 11 12 33 |
jpl | jpl 2768 | 25 33 65 | 16 12 51 | 8 8 23 |
mit | mit 2976 | 20 33 56 | 17 11 77 | 7 8 20 |
Table 5.1455.5 GPS week: 1455 Day: 5 MJD: 54434.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 8 5 29 | 11 10 65 | 5 8 10 |
emr | emr 2864 | 22 24 50 | 12 10 62 | 10 7 24 |
esa | esa 2784 | 13 11 39 | 12 10 58 | 10 10 21 |
gfz | gfz 2856 | 25 23 55 | 14 13 62 | 10 10 22 |
igr | igr 2879 | 12 15 34 | 10 14 61 | 11 6 20 |
igs | igs 2880 | 12 19 39 | 10 13 60 | 8 5 16 |
jpl | jpl 2768 | 31 31 64 | 13 14 66 | 9 7 20 |
mit | mit 2976 | 19 23 48 | 12 14 66 | 7 7 17 |
Table 5.1455.6 GPS week: 1455 Day: 6 MJD: 54435.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2965 | 8 8 23 | 24 16 53 | 5 5 12 |
emr | emr 2864 | 19 18 33 | 25 26 78 | 8 6 24 |
esa | esa 2880 | 9 10 27 | 23 18 69 | 8 7 20 |
gfz | gfz 2862 | 17 18 37 | 24 27 78 | 11 8 25 |
igr | igr 2880 | 10 12 32 | 25 24 85 | 7 4 17 |
igs | igs 2953 | 18 16 43 | 27 19 61 | 7 7 17 |
jpl | jpl 2864 | 21 20 40 | 24 22 78 | 8 8 16 |
mit | mit 2976 | 19 22 39 | 30 23 73 | 8 10 17 |
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 : 21-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 6.1455 GPS week: 1455 MJD: 54429.500-54435.500
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 6 -2 -23 1 | 9 19
| 19 20 77 81 8 | 2
emr uuuuu | 7 22 -83 -208 -1 | 50 52
| 33 34 137 154 15 | 2
esa uuuux | -28 2 -20 -13 1 | 55 64
| 26 28 105 115 25 | 5
gfz uuuuu | -13 21 -8 79 5 | 1 14
| 10 21 55 87 4 | 2
igr xxxxx | 29 -3 93 -7 -5 | 6 15
| 23 30 52 87 11 | 2
irf xxxxx | 21 7 10 153 -4 | -3 13
| 9 12 58 109 9 | 2
mit uuuuu | 53 11 -127 159 -7 | 8 17
| 23 24 92 128 13 | 3
ngs uuuuu | -15 -68 231 -4 1 | 2 12
| 36 12 148 147 12 | 2
sio uuuuu | -35 -60 17 -55 -4 | 15 21
| 29 44 133 99 20 | 4
Table 7.1455.0 GPS week: 1455 Day: 0 MJD: 54429.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 39 9 123 12 | 5 18
emr uuuuu | 55 1 -149 -313 -6 | 48 51
esa uuuux | -34 48 -41 170 54 | 51 59
gfz uuuuu | -26 -1 0 -33 7 | -4 15
igr xxxxx | 64 -23 144 -148 7 | 3 15
irf xxxxx | 19 14 -68 112 -2 | -4 14
mit uuuuu | 69 -25 -309 369 1 | 7 17
ngs uuuuu | -40 -80 428 -167 -5 | 0 10
sio uuuuu | -45 28 171 -216 -15 | 20 23
Table 7.1455.1 GPS week: 1455 Day: 1 MJD: 54430.500
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 | 25 18 -86 -40 -8 | 10 20
emr uuuuu | -43 39 -63 -405 -25 | 53 55
esa uuuux | -21 -6 -73 -152 5 | 62 70
gfz uuuuu | -13 18 36 194 5 | 1 15
igr xxxxx | 36 32 88 87 -2 | 7 17
irf xxxxx | 17 13 84 126 -18 | 0 11
mit uuuuu | 27 44 -151 186 -27 | 12 16
ngs uuuuu | 9 -73 369 73 20 | 1 11
sio uuuuu | -12 -85 -199 82 -31 | 21 24
Table 7.1455.2 GPS week: 1455 Day: 2 MJD: 54431.500
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 | -17 14 54 -26 0 | 10 20
emr uuuuu | -8 36 -186 -377 -15 | 51 54
esa uuuux | -67 -28 34 50 -20 | 60 69
gfz uuuuu | 5 22 -8 132 3 | 2 15
igr xxxxx | 7 22 11 -35 -9 | 8 16
irf xxxxx | 10 21 1 30 -10 | -1 12
mit uuuuu | 39 11 -61 1 -17 | 10 17
ngs uuuuu | 32 -50 82 187 12 | 3 12
sio uuuuu | -63 -43 176 -42 -17 | 17 23
Table 7.1455.3 GPS week: 1455 Day: 3 MJD: 54432.500
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 | -27 -24 65 5 10 | 10 20
emr uuuuu | 15 77 -236 -121 6 | 50 53
esa uuuux | -55 -13 128 33 -14 | 58 67
gfz uuuuu | -6 11 67 68 -3 | 4 15
igr xxxxx | 27 28 139 90 1 | 8 16
irf xxxxx | 35 -5 85 75 -9 | -2 13
mit uuuuu | 90 7 -20 55 -15 | 9 17
ngs uuuuu | -38 -67 18 -55 7 | 5 14
sio xxxxx | 4 -79 44 43 -13 | 14 21
Table 7.1455.4 GPS week: 1455 Day: 4 MJD: 54433.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -2 4 61 -19 2 | 8 17
emr uuuuu | 39 25 -150 -62 16 | 48 50
esa uuuux | -11 -9 36 -94 -2 | 53 63
gfz uuuuu | -17 -2 3 67 11 | 1 13
igr xxxxx | 54 -24 142 -17 4 | 6 14
irf xxxxx | 24 18 -3 130 2 | -5 13
mit uuuuu | 67 34 -113 58 -4 | 6 17
ngs uuuuu | -69 -58 184 8 -10 | 4 13
sio xxxxx | -36 -54 -65 -60 14 | 10 18
Table 7.1455.5 GPS week: 1455 Day: 5 MJD: 54434.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -28 -5 -130 -56 1 | 8 17
emr uuuuu | 7 8 72 -151 11 | 49 51
esa uuuux | 6 -15 -19 23 -10 | 51 61
gfz uuuuu | -12 49 -95 152 6 | 2 13
igr xxxxx | 10 -15 84 42 -14 | 5 14
irf xxxxx | 14 -2 10 249 4 | -6 14
mit uuuuu | 42 15 -91 214 2 | 5 17
ngs uuuuu | -18 -84 285 -204 -8 | 1 13
sio xxxxx | -77 -95 27 -68 20 | 11 18
Table 7.1455.6 GPS week: 1455 Day: 6 MJD: 54435.500
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 -6 14 -149 -8 | 9 18
emr uuuuu | -19 -31 130 -30 5 | 50 53
esa uuuux | -11 35 -205 -123 -7 | 49 60
gfz uuuuu | -21 50 -62 -25 8 | 3 14
igr xxxxx | 5 -42 46 -68 -23 | 5 14
irf xxxxx | 28 -9 -40 349 7 | -5 14
mit uuuuu | 36 -11 -141 230 11 | 6 18
ngs uuuuu | 17 -63 254 131 -8 | 2 13
sio xxxxx | -17 -93 -35 -123 15 | 13 22
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