[IGSREPORT-15210] Wk 1430 IGS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Jun 21 06:13:49 PDT 2007
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IGS Electronic Report 21 Jun 06:13:58 PDT 2007 Message Number 15210
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
Final IGS Orbit Combination - Week 1430 (Jun 03, 2007 - Jun 09, 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:
igs1430[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1430[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1430[0-6].cls IGS GPS clock combination summary report.
igs14307.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs14307.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 | ESA | ARTU
0 | GFZ | VILL
0 | JPL | 2 18 YIBL
0 | MIT | GLPS KOUR VILL
1 | GFZ | MAS1
1 | JPL | 2 18
1 | MIT | 32 BAHR GRAS MAS1 VILL
2 | ESA | THTI
2 | MIT | 8 KOUR
3 | EMR | NISU
3 | ESA | KOUR SCUB
3 | GFZ | DAV1 GRAZ NISU
3 | JPL | 2 18 21
3 | MIT | 25 GRAZ IISC KOUR
4 | ESA | BILI
4 | GFZ | BAN2 KOUR
4 | JPL | 13 18 21
4 | MIT | KOUR MBAR MKEA
5 | ESA | YAKT
5 | GFZ | BAN2
5 | JPL | WAB2
5 | MIT | GUAM KOUR
6 | ESA | BILI
6 | GFZ | BAN2
6 | JPL | WAB2 YAR2
6 | MIT | 29 GRAS
5. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G30 | 2007_06_05 | 2007075
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 | MIT | 32
2 | COD | 32
2 | JPL | 32
4 | NGS | 32
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 G29 | 4 | 1 | | | | | 2 |
PRN G32 | | | 4 | | | | |
8. 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.
9. 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 | .2 .1 .6 -5 4 1 -.32
EMR | 3.8 -8.5 -1.1 -1 19 3 .19
ESA | 2.8 -4.3 -15.6 -13 -4 9 -1.02
GFZ | .3 -.2 .5 -16 -8 -12 -.36
JPL | 9.9 -2.8 16.3 151 -5 124 .07
MIT | -1.0 -4.5 1.5 0 5 2 .06
NGS | 9.1 -2.0 .3 -21 -125 38 -1.07
SIO | -2.9 1.4 -14.1 46 -27 48 .16
10. 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.
11. 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.
12. 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 1.1430.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1430.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 2.1430.[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 3.1430.[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 5.1430.0-6).
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 1430 summary. (Jun 03, 2007 - Jun 09, 2007)
Table 1.1430.a GPS week: 1430 MJD: 54254.000-54260.000
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 171| 1 -1 -3 -6 -61 2 -.24 14 14 | -362 -272 49 88
| 1 0 0 9 5 24 .03 | 738 1322
emr 64| 1 0 2 16 -29 53 .33 20 19 | 5295 -852 54 100
| 1 1 2 18 20 27 .02 | 1173 1189
esa 67| -1 0 13 46 -79 46 .19 20 20 | 5269 -618 54 127
| 1 1 1 37 41 39 .05 | 1189 1150
gfz 185| 0 0 -7 39 -28 -151 -.10 14 14 | 165 -21 31 107
| 0 1 1 21 21 95 .03 | 298 635
igr n/a| 0 0 0 -26 -40 34 .02 8 8 | -6562 154 30 64
| 0 0 0 9 14 40 .03 | 937 1268
jpl n/a| -1 -6 -14 -117 -65 177 -.01 40 40 | 4232 -828 92 135
| 8 3 5 24 27 26 .04 | 1287 1371
mit 170| -2 -1 6 -8 -74 12 -.07 24 23 | 58 -355 74 140
| 1 1 0 29 23 33 .03 | 298 486
ngs 202| -1 0 0 14 221 32 .02 14 12 | -364 -265 2438 4168
| 1 1 2 29 29 40 .03 | 667 1207
sio 98| 3 1 5 -143 -26 60 -.22 24 22 | --- --- --- ---
| 1 1 2 33 20 30 .04 | --- ---
Table 1.1430.b GPS week : 1430 MJD: 54254.000-54260.000
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 6 6 6 7 6 5 |
2 | 8 8 8 8 7 8 8 |
3 | 6 6 6 6 6 6 6 |
4 | 7 7 7 7 6 6 7 |
5 | 6 6 6 6 6 6 5 |
6 | 6 7 7 7 7 7 7 |
7 | 7 7 7 7 7 6 6 |
8E | 7 7 7 7 7 7 7 |
9E | 7 7 6 6 7 6 6 |
10 | 6 6 6 6 6 6 6 |
11 | 8 9 8 8 8 9 8 |
12 | 9 8 8 8 8 7 8 |
13 | 8 7 7 7 8 7 8 |
14 | 8 13 8 8 8 8 8 |
16 | 8 8 8 8 9 9 8 |
17 | 9 9 9 8 9 9 8 |
18 | 9 8 8 8 8 8 8 |
19 | 8 8 8 8 8 8 9 |
20 | 8 7 7 7 7 8 7 |
21 | 8 8 7 8 8 7 8 |
22 | 9 9 8 9 8 8 7 |
23 | 8 8 8 7 8 8 14 |
24E | 8 7 7 7 7 6 7 |
25E | 7 7 6 7 6 6 6 |
26 | 6 6 6 6 7 6 6 |
27E | 8 7 7 7 6 6 7 |
28 | 9 8 8 8 9 8 8 |
29 | 8 7 7 7 7 7 16 |
30 | 6 7 0 6 6 6 6 |
31E | 7 7 7 7 7 7 7 |
32 | 13 22 0 16 29 17 17 |
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 2.1430.0 GPS week: 1430 Day: 0 MJD: 54254.000
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 171| 0 -1 -4 -9 -60 -32 -.29 15 14 | -1022 462 45 89
| 41 28 |
emr 64| 3 1 2 42 -26 11 .31 18 18 | 6969 -2261 58 102
| -3 -39 |
esa 67| -2 -1 15 -26 -6 33 .17 21 20 | 6830 -1715 60 134
| 193 -64 |
gfz 185| 0 2 -7 5 -19 -10 -.12 15 15 | -88 -37 32 123
| 46 -4 |
igr n/a| 0 2 0 -41 -36 0 .01 8 8 | -7612 -1275 28 65
| 51 -50 |
jpl n/a| 0 -4 -20 -76 -88 150 -.00 39 39 | 6198 -2365 90 141
| -47 5 |
mit 170| 0 -1 6 17 -88 -40 -.02 24 21 | -206 31 70 169
| -31 11 |
ngs 202| -3 0 0 39 216 -15 .06 16 14 | -937 409 2553 4190
| 30 -63 |
sio 98| 2 0 3 -106 -24 36 -.19 25 23 | --- --- --- ---
| 34 7 |
Table 2.1430.1 GPS week: 1430 Day: 1 MJD: 54255.000
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 171| 1 0 -4 1 -53 -7 -.23 15 14 | 650 -1569 46 94
| 33 37 |
emr 64| 0 2 1 6 -41 36 .33 23 23 | 6068 -148 59 99
| -29 -20 |
esa 67| 0 0 12 30 -108 27 .13 19 19 | 6125 28 52 118
| 34 -55 |
gfz 185| -1 3 -7 61 -13 -54 -.11 15 15 | 650 -581 30 100
| 6 -22 |
igr n/a| -1 1 1 -19 -12 25 .07 8 8 | -7635 623 25 64
| -12 -78 |
jpl n/a| 1 -5 -11 -117 -46 145 .01 40 40 | 5034 -402 83 143
| -74 -5 |
mit 170| -2 -1 7 20 -100 -11 -.04 24 21 | 700 -941 75 120
| -3 13 |
ngs 202| -1 -2 0 -37 220 13 .03 14 12 | 522 -1341 2434 4241
| 11 -108 |
sio 98| 5 1 7 -103 -35 5 -.18 24 23 | --- --- --- ---
| 58 18 |
Table 2.1430.2 GPS week: 1430 Day: 2 MJD: 54256.000
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 171| 0 -1 -5 -16 -64 -4 -.28 15 14 | -819 641 50 84
| 2 37 |
emr 64| 1 0 -3 10 -22 30 .32 18 18 | 6293 -1067 53 88
| 27 -14 |
esa 67| -1 0 14 74 -97 -15 .13 19 19 | 6416 -1073 53 130
| 25 2 |
gfz 185| 0 -1 -8 46 -66 -100 -.08 16 16 | 315 -249 29 98
| -12 5 |
igr n/a| 0 0 1 -21 -36 -27 .03 7 7 | -6568 -378 33 69
| 0 -52 |
jpl n/a| -3 -12 -16 -148 -27 160 .03 41 41 | 5151 -1225 97 137
| -38 7 |
mit 170| -2 1 4 -43 -99 20 -.11 22 21 | -25 200 73 136
| 53 15 |
ngs 202| -1 0 3 49 247 -2 .03 13 12 | -726 514 2252 3952
| 0 -117 |
sio 98| 3 2 2 -174 -49 99 -.20 22 20 | --- --- --- ---
| 65 -21 |
Table 2.1430.3 GPS week: 1430 Day: 3 MJD: 54257.000
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 171| 1 -1 -3 -9 -66 -11 -.23 15 14 | -502 432 42 85
| 17 51 |
emr 64| 0 0 0 42 -38 78 .32 16 16 | 5061 -855 55 96
| -61 0 |
esa 67| 0 2 12 56 -94 25 .20 21 21 | 5007 -685 54 120
| -5 35 |
gfz 185| 0 0 -5 58 -21 -186 -.11 14 14 | 114 15 30 113
| -26 16 |
igr n/a| 0 1 0 -25 -49 60 .03 8 8 | -7009 249 33 64
| -49 13 |
jpl n/a| 3 -6 -15 -109 -65 179 .05 41 41 | 3946 -860 87 118
| -81 38 |
mit 170| -2 0 6 -56 -78 56 -.09 21 21 | 69 33 74 133
| 41 -15 |
ngs 202| -3 1 -1 26 262 50 -.02 15 13 | -450 348 2267 4107
| -78 -115 |
sio 98| 1 0 7 -193 -27 64 -.21 24 23 | --- --- --- ---
| 62 -27 |
Table 2.1430.4 GPS week: 1430 Day: 4 MJD: 54258.000
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 171| 3 -2 -3 -7 -57 28 -.22 14 13 | -1287 1397 47 84
| 29 59 |
emr 64| 0 -1 4 -3 -28 82 .34 20 20 | 4698 -1182 53 97
| 49 -33 |
esa 67| 0 0 12 84 -95 97 .21 19 19 | 4599 -937 54 118
| -49 28 |
gfz 185| -1 1 -7 23 -5 -217 -.12 14 14 | -268 941 32 119
| 21 -5 |
igr n/a| 0 0 2 -36 -50 23 -.00 7 7 | -6198 -76 28 62
| 37 -24 |
jpl n/a| -13 -3 -21 -115 -90 203 -.03 43 43 | 3714 -1148 97 142
| 15 38 |
mit 170| -2 -1 6 0 -62 10 -.07 22 23 | -32 -377 72 151
| 8 -32 |
ngs 202| -1 2 -1 7 234 14 .02 15 13 | -1287 1322 2561 4676
| 104 -49 |
sio 98| 6 3 7 -136 -33 75 -.21 23 20 | --- --- --- ---
| 33 0 |
Table 2.1430.5 GPS week: 1430 Day: 5 MJD: 54259.000
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 171| 3 -1 -3 10 -61 39 -.22 15 15 | 372 -2107 57 95
| 39 35 |
emr 64| 0 -2 5 7 -58 65 .35 17 17 | 4160 -1820 53 103
| -13 8 |
esa 67| 0 1 13 39 -37 83 .20 20 20 | 4101 -1581 54 146
| -33 26 |
gfz 185| 0 1 -6 59 -25 -245 -.12 13 13 | 122 -864 37 111
| -15 16 |
igr n/a| 0 0 0 -13 -51 78 .01 7 7 | -5809 -722 31 62
| -10 4 |
jpl n/a| -8 -2 -9 -107 -98 213 -.02 41 41 | 3019 -1736 99 136
| -64 76 |
mit 170| -3 -1 7 0 -47 4 -.08 24 24 | 44 -1039 74 128
| 6 -26 |
ngs 202| 0 0 -2 -6 179 74 .05 13 11 | 258 -1953 2566 4356
| 54 -29 |
sio 98| 4 2 6 -157 -29 75 -.29 24 21 | --- --- --- ---
| 25 -14 |
Table 2.1430.6 GPS week: 1430 Day: 6 MJD: 54260.000
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 171| 1 0 -2 -15 -68 5 -.20 14 13 | 71 -1164 59 91
| 41 57 |
emr 64| 2 -2 2 7 7 72 .36 25 20 | 3821 1364 53 119
| 20 -81 |
esa 67| -2 2 9 68 -115 75 .27 20 20 | 3811 1636 51 127
| -9 5 |
gfz 185| -1 -1 -5 25 -47 -246 -.04 14 14 | 312 626 31 90
| 10 40 |
igr n/a| 0 0 1 -24 -49 81 -.00 8 8 | -5104 2659 33 62
| 28 -40 |
jpl n/a| 10 -10 -7 -143 -40 189 -.07 39 39 | 2568 1938 92 133
| -46 31 |
mit 170| -4 -4 6 0 -43 47 -.09 32 28 | -138 -394 81 148
| 14 -31 |
ngs 202| 0 0 0 20 189 93 -.01 13 11 | 68 -1155 2439 3657
| 59 6 |
sio 98| 2 3 3 -130 16 69 -.27 29 22 | --- --- --- ---
| 29 -43 |
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 3.1430.0 GPS week: 1430 Day: 0 MJD: 54254.000
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 15 20 13 9 18 17 13 12 5 | 20 29 28 24 23 24 25 25 20 23
2 | 15 20 22 9 9 57 27 20 19 8 | 14 31 30 22 21 47 22 24 18 19
3 | 10 18 11 16 6 19 25 14 17 6 | 21 26 30 23 24 27 32 28 27 23
4 | 12 18 24 15 7 16 26 15 29 7 | 10 22 27 22 16 20 22 17 20 15
5 | 11 16 17 13 8 15 21 14 21 6 | 20 32 29 28 31 26 37 35 28 28
6 | 10 16 17 13 7 12 30 11 23 6 | 26 33 35 23 31 27 40 35 39 30
7 | 12 17 19 13 7 10 32 12 26 6 | 31 36 28 28 33 31 32 35 38 31
8E | 18 20 18 14 9 23 27 13 15 6 | 50 47 58 53 47 47 42 52 47 48
9E | 16 13 16 18 7 18 17 16 21 6 | 28 32 34 31 28 34 21 33 34 29
10 | 12 16 16 13 8 15 17 14 29 6 | 19 24 29 25 18 20 20 24 21 20
11 | 12 21 22 16 9 55 19 15 27 8 | 16 32 41 28 25 41 17 26 28 23
12 | 16 20 19 15 8 49 35 18 26 8 | 26 37 38 36 31 55 39 32 36 31
13 | 14 19 21 18 6 52 19 14 17 7 | 15 33 36 23 19 37 18 17 19 19
14 | 22 20 19 19 11 53 19 16 22 8 | 23 35 24 26 19 35 17 18 19 18
16 | 16 20 17 18 5 48 29 15 21 8 | 17 30 27 27 23 40 32 25 28 22
17 | 14 16 20 14 9 55 33 15 43 9 | 23 28 32 25 26 43 36 28 39 24
18 | 15 22 23 13 8 52 25 20 28 8 | 19 33 30 24 21 39 24 21 29 21
19 | 14 19 12 19 10 53 29 19 25 8 | 27 37 38 38 30 54 35 31 31 31
20 | 14 19 19 18 8 48 15 19 18 7 | 17 34 30 25 24 33 20 26 20 22
21 | 21 20 20 12 7 50 25 16 23 8 | 53 49 54 45 44 51 45 49 45 47
22 | 18 21 21 15 8 53 17 22 32 8 | 22 34 29 24 21 38 22 22 26 21
23 | 15 19 19 14 7 50 19 18 23 7 | 15 37 33 25 21 40 20 21 15 19
24E | 19 19 26 14 9 17 31 12 26 7 | 48 52 62 50 50 53 43 53 57 51
25E | 15 19 19 14 7 26 16 14 23 6 | 59 59 68 59 56 61 59 59 53 58
26 | 10 12 26 11 8 18 19 15 25 6 | 16 23 25 24 16 25 16 23 22 19
27E | 25 27 28 18 7 20 18 15 18 8 | 15 29 35 22 14 21 17 17 14 16
28 | 14 18 23 16 10 57 26 20 32 8 | 23 31 30 31 24 35 26 29 22 23
29 | 10 13 39 13 11 18 28 21 27 8 | 251 256 253 248 251 257 259 254 158 253
30 | 8 13 23 15 6 13 19 14 22 6 | 7 12 15 9 8 8 12 17 4 9
31E | 11 17 17 12 7 53 14 14 27 7 | 14 29 20 16 14 34 14 18 18 15
X32 | 15 --- --- --- 18 35 --- 15 --- 13 | 20 --- --- --- 44 31 --- 45 --- 48
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 18 21 15 8 39 24 16 25 |T 31 40 41 36 33 43 35 36 32 34
WRMS | 14 18 20 15 8 39 21 14 23 |NE 30 40 40 35 33 43 36 36 31 33
MEDI | 14 19 19 14 8 35 21 15 23 |MD 20 32 30 25 24 35 24 26 27 23
Table 3.1430.1 GPS week: 1430 Day: 1 MJD: 54255.000
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 16 19 14 7 16 17 13 17 5 | 23 34 28 27 27 29 31 27 25 26
2 | 12 22 22 10 6 59 23 14 17 7 | 19 34 27 26 26 41 29 28 23 24
3 | 11 18 17 15 7 18 17 15 24 6 | 19 23 23 21 20 24 24 27 17 20
4 | 13 19 29 13 7 13 20 10 24 6 | 17 27 29 25 26 27 30 27 25 22
5 | 11 22 15 15 7 13 23 13 14 6 | 22 32 25 20 27 27 37 32 28 27
6 | 11 17 18 15 9 13 33 11 28 7 | 24 25 27 22 26 25 37 29 32 26
7 | 11 19 12 13 7 13 39 11 18 6 | 37 36 40 33 37 36 42 39 48 38
8E | 16 23 22 17 11 24 17 15 15 7 | 41 44 47 46 41 42 43 38 45 41
9E | 21 18 18 18 9 15 17 12 25 7 | 28 35 40 31 30 34 29 28 38 29
10 | 11 17 22 11 6 14 22 8 26 6 | 21 28 27 26 24 24 20 24 35 23
11 | 17 23 26 18 8 49 24 15 23 8 | 20 38 41 30 27 38 22 30 25 26
12 | 15 23 14 15 6 48 39 14 23 8 | 24 39 32 30 31 43 39 29 37 30
13 | 13 20 23 13 9 52 17 13 19 7 | 14 36 31 24 22 36 22 24 26 22
14 | 22 68 20 18 10 49 18 18 43 12 | 22 80 28 27 26 36 19 27 31 26
16 | 17 19 15 18 5 47 28 16 22 8 | 19 30 28 25 21 36 21 22 20 22
17 | 12 19 20 17 6 54 32 11 39 8 | 20 26 27 21 20 30 34 24 33 21
18 | 14 21 23 13 9 57 22 18 22 8 | 23 33 30 23 20 35 26 20 24 23
19 | 15 15 13 18 9 53 26 18 23 7 | 24 33 28 28 26 41 19 29 24 25
20 | 13 16 16 15 6 49 15 16 15 6 | 19 34 29 24 23 34 21 29 21 22
21 | 20 20 21 10 8 54 23 12 27 8 | 30 31 31 25 27 39 33 25 32 27
22 | 17 19 25 14 10 53 21 19 34 8 | 23 35 28 24 21 35 24 19 41 23
23 | 13 20 20 16 7 46 28 17 23 7 | 16 38 28 25 21 38 26 22 22 21
24E | 17 20 20 14 7 16 28 14 24 7 | 51 54 59 52 51 53 44 52 59 51
25E | 15 22 15 16 6 24 17 14 17 6 | 52 59 55 56 52 55 59 54 61 55
26 | 7 16 17 14 5 16 21 12 22 5 | 17 27 27 23 22 25 21 24 25 20
27E | 20 20 20 17 8 22 14 17 18 7 | 17 25 29 24 18 24 17 24 17 19
28 | 13 17 18 16 10 59 25 16 33 8 | 20 34 26 28 24 32 25 26 28 22
X29 | 10 17 28 14 8 25 24 12 --- 7 | 56 64 67 60 58 70 68 59 --- 61
X30 | 9 18 17 18 6 13 18 14 --- 6 | 12 14 15 11 12 13 10 17 --- 15
31E | 11 19 14 13 10 52 17 16 19 6 | 18 32 21 20 24 36 21 21 21 21
X32 | 27 --- --- --- 25 53 149 28 --- 22 | 36 --- --- --- 32 28 10 43 --- 38
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 23 19 15 8 40 24 14 24 |T 25 36 32 28 27 35 29 29 30 27
WRMS | 14 23 19 15 8 40 21 12 23 |NE 23 34 30 26 25 33 27 28 28 26
MEDI | 13 19 19 15 7 46 22 14 23 |MD 22 34 28 25 26 35 26 27 26 24
Table 3.1430.2 GPS week: 1430 Day: 2 MJD: 54256.000
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 | 13 15 18 16 6 20 18 11 14 5 | 18 29 28 24 20 27 26 26 17 22
2 | 14 21 19 13 7 59 24 12 21 7 | 16 33 26 22 21 38 26 22 22 21
3 | 16 17 14 17 6 18 16 12 20 6 | 24 34 39 26 28 34 27 31 26 30
4 | 13 19 20 16 6 13 23 14 25 6 | 13 25 29 25 20 22 28 27 22 20
5 | 10 18 14 15 7 16 19 11 16 5 | 20 30 23 22 28 27 37 32 27 26
6 | 13 15 17 14 7 11 30 15 23 6 | 22 28 34 25 29 25 41 36 34 29
7 | 14 15 17 14 5 12 33 11 25 6 | 18 25 27 20 22 20 35 24 32 21
8E | 18 20 18 15 8 25 15 12 18 6 | 30 31 30 33 29 33 23 28 30 27
9E | 19 15 22 17 7 15 17 9 19 6 | 26 34 33 32 28 33 26 34 32 28
10 | 11 14 18 14 7 19 17 11 23 5 | 17 23 23 21 20 22 17 24 28 19
11 | 14 27 24 17 6 52 15 13 22 8 | 19 44 40 26 25 41 20 24 25 25
12 | 14 21 16 18 6 52 29 11 26 7 | 24 37 33 27 27 40 35 27 36 28
13 | 13 17 23 15 6 51 20 11 16 7 | 15 32 38 23 21 40 20 23 21 22
14 | 22 20 16 22 9 53 18 16 18 8 | 27 41 26 28 22 36 16 22 22 24
16 | 17 21 14 23 9 51 29 15 21 8 | 22 36 27 27 24 37 25 28 26 26
17 | 13 20 16 15 8 52 30 13 38 8 | 23 29 30 24 27 37 33 32 36 26
18 | 15 21 17 13 7 58 19 14 20 7 | 23 36 27 26 22 36 28 23 28 26
19 | 14 17 17 19 8 54 21 12 22 7 | 27 32 34 32 27 44 25 31 30 29
20 | 13 15 23 14 6 51 14 13 18 6 | 17 31 27 25 21 36 17 24 16 21
21 | 18 20 18 12 5 54 19 12 21 7 | 23 34 31 27 24 34 23 27 29 25
22 | 16 21 21 15 10 56 15 16 27 8 | 24 38 30 26 20 37 26 26 26 25
23 | 15 19 23 17 5 47 25 15 18 7 | 16 37 33 24 19 39 21 17 17 20
24 | 14 15 20 13 7 17 28 9 31 6 | 61 64 70 64 62 67 53 64 73 63
25E | 14 20 21 18 6 23 12 10 21 6 | 29 38 31 35 29 37 31 31 38 32
26 | 9 13 23 14 6 18 19 11 18 5 | 19 25 26 25 22 25 22 29 25 22
27E | 21 19 26 15 7 23 15 14 21 7 | 19 27 32 22 17 27 19 21 19 20
28 | 13 18 14 19 8 56 25 17 32 8 | 17 30 29 27 20 33 25 25 25 21
X29 | 10 12 23 14 8 15 27 10 --- 6 | 45 48 48 44 48 52 57 51 --- 47
X30 | 6 --- --- --- 21 --- --- --- --- 0 | 31 --- --- --- 31 --- --- --- --- 34
31E | 12 17 23 12 8 53 16 11 19 6 | 18 30 26 19 17 29 21 22 22 21
X32 | 369 --- --- --- 75 402 --- 15 --- 0 | 13 --- --- --- 267 32 --- 279 --- 244
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 18 19 16 7 41 21 13 22 |T 23 33 32 27 33 34 27 37 28 33
WRMS | 14 18 19 16 7 41 21 12 20 |NE 22 34 32 27 35 35 28 38 27 35
MEDI | 14 18 18 15 7 47 19 12 21 |MD 22 32 30 26 24 34 26 27 26 25
Table 3.1430.3 GPS week: 1430 Day: 3 MJD: 54257.000
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 | 13 13 23 14 8 20 21 13 17 6 | 20 29 28 23 22 30 24 28 26 23
2 | 15 17 30 11 7 55 23 16 19 7 | 11 25 32 19 16 39 22 19 19 14
3 | 13 17 13 10 9 18 11 13 25 5 | 17 24 22 18 19 17 21 26 22 20
4 | 13 16 22 12 7 17 21 16 25 6 | 11 24 34 21 18 22 18 22 21 16
5 | 11 13 17 10 9 13 22 14 17 5 | 22 29 29 23 29 25 37 31 28 26
6 | 14 15 23 15 8 13 29 13 24 7 | 28 33 23 28 33 28 43 36 38 30
7 | 13 13 16 13 7 13 32 11 25 6 | 36 40 32 36 41 36 46 40 46 38
8E | 15 17 21 14 8 21 19 13 20 6 | 48 54 57 56 49 51 52 46 57 51
9E | 15 14 19 15 10 17 19 11 17 5 | 26 32 32 29 26 31 22 26 28 25
10 | 13 12 18 14 4 17 16 12 23 5 | 15 19 23 19 13 15 17 16 21 14
11 | 13 18 25 13 7 52 16 15 30 7 | 16 33 40 25 23 34 13 25 35 21
12 | 16 17 19 13 7 50 26 15 26 7 | 23 33 32 25 27 42 32 30 32 26
13 | 14 14 22 13 6 51 16 14 21 7 | 16 33 38 24 22 35 20 24 22 21
14 | 22 20 21 16 7 55 14 18 22 8 | 24 37 25 25 21 31 19 24 19 20
16 | 17 16 16 20 9 52 26 18 24 8 | 18 30 31 28 22 41 27 25 27 24
17 | 11 14 18 14 8 46 29 13 35 7 | 20 23 26 23 20 31 27 21 38 20
18 | 14 20 24 12 9 60 20 17 22 8 | 23 34 30 27 25 35 28 28 24 26
19 | 15 15 15 12 12 59 28 11 26 7 | 21 30 26 32 24 41 17 27 24 24
20 | 12 15 16 13 8 52 19 14 14 6 | 17 30 30 23 20 34 17 21 17 19
21 | 18 19 23 11 7 59 21 19 27 8 | 29 34 28 26 28 38 24 29 31 26
22 | 15 19 25 15 10 53 17 20 36 8 | 21 33 34 26 22 34 23 26 34 22
23 | 14 15 17 15 6 49 17 17 28 7 | 16 33 29 24 18 32 18 18 18 18
24 | 17 15 23 13 5 14 28 11 30 7 | 32 38 44 34 34 34 26 34 37 32
25E | 14 20 26 12 6 22 18 12 24 6 | 55 62 68 58 58 60 54 58 61 58
26 | 11 14 23 14 6 21 19 12 17 6 | 15 21 25 21 18 24 16 21 21 17
27E | 21 19 21 13 7 20 17 11 19 6 | 18 28 23 23 17 25 16 16 16 17
28 | 14 15 15 18 11 57 22 17 27 7 | 21 28 31 29 23 32 21 22 23 21
X29 | 11 14 20 14 11 19 25 12 --- 6 | 45 48 45 44 44 51 52 47 --- 45
X30 | 10 11 --- 13 9 10 17 15 --- 6 | 18 27 --- 19 21 22 26 28 --- 22
31E | 11 15 15 18 8 54 13 18 17 7 | 18 29 22 21 20 29 18 26 19 19
X32 | 21 --- --- --- 19 40 --- 20 --- 16 | 14 --- --- --- 285 39 --- 265 --- 154
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 16 21 14 8 41 21 15 24 |T 23 32 32 27 34 33 26 35 28 29
WRMS | 14 16 21 14 8 41 21 13 23 |NE 21 30 30 25 34 32 25 35 27 28
MEDI | 14 15 21 13 8 40 19 14 24 |MD 20 30 30 25 22 34 22 26 24 22
Table 3.1430.4 GPS week: 1430 Day: 4 MJD: 54258.000
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 18 17 13 8 50 19 13 11 6 | 13 24 27 19 15 45 25 20 14 17
2 | 14 19 15 13 7 59 23 13 15 7 | 13 28 25 24 18 41 27 19 19 18
3 | 11 17 13 15 6 19 12 14 27 6 | 19 22 18 21 23 20 26 23 24 18
4 | 12 17 22 13 7 13 16 16 22 6 | 12 23 30 25 23 26 24 24 21 19
5 | 11 22 22 14 7 16 23 11 13 6 | 19 37 27 20 23 24 31 26 25 23
6 | 10 20 14 16 9 10 32 12 26 6 | 21 25 23 18 26 19 38 26 40 24
7 | 9 20 13 15 9 10 35 15 22 6 | 24 28 23 20 27 20 32 28 39 25
8E | 17 24 24 17 6 25 18 15 18 7 | 38 41 38 39 35 40 34 35 40 36
9E | 17 16 19 15 8 21 21 18 19 6 | 25 27 34 27 23 32 27 23 28 23
10 | 12 15 25 12 6 15 14 11 19 5 | 15 20 17 18 17 22 17 21 23 14
11 | 11 20 23 14 9 52 20 20 24 7 | 20 32 36 23 24 28 24 28 29 21
12 | 16 28 17 17 8 51 25 13 25 8 | 25 37 27 26 25 44 27 27 31 25
13 | 14 20 20 14 8 57 20 17 16 7 | 17 35 38 24 22 37 22 22 18 21
14 | 17 22 17 17 10 60 20 21 20 8 | 18 32 24 25 17 32 15 26 22 17
16 | 18 20 17 19 7 58 27 18 25 8 | 16 28 29 26 22 40 21 24 25 20
17 | 12 17 21 14 7 46 28 18 44 8 | 20 27 31 24 20 36 34 26 44 22
18 | 15 23 16 12 8 63 19 16 27 8 | 21 34 26 20 21 30 23 18 20 20
19 | 14 17 17 17 8 58 25 16 25 8 | 18 31 29 24 21 38 23 24 23 21
20 | 14 18 19 11 7 52 26 14 16 7 | 19 32 35 24 24 36 25 27 22 21
21 | 15 20 19 11 7 59 21 17 19 7 | 19 30 26 19 16 33 23 20 23 18
22 | 15 20 17 15 8 59 17 16 21 7 | 19 31 25 23 20 31 19 20 27 19
23 | 14 22 22 14 6 51 16 14 27 7 | 16 34 32 22 18 32 19 16 21 17
24 | 16 17 24 14 6 12 26 14 30 7 | 26 35 34 33 32 33 25 34 44 30
25E | 14 17 17 14 7 22 16 13 23 6 | 30 41 40 35 34 41 38 40 37 34
26 | 10 20 24 13 5 18 20 18 22 6 | 16 26 26 21 17 28 24 28 23 18
27E | 20 18 20 13 8 21 18 11 15 6 | 15 23 24 18 13 23 20 14 21 13
28 | 14 30 19 15 8 55 23 17 33 8 | 16 34 31 27 22 39 21 22 25 19
29 | 10 13 24 14 6 16 27 18 23 6 | 42 46 43 43 44 51 51 48 55 44
X30 | 8 16 --- 15 8 14 20 14 18 6 | 20 27 --- 20 23 26 28 24 16 24
31E | 13 15 14 13 6 51 19 15 19 6 | 18 29 26 21 21 34 31 24 18 21
X32 | 17 --- --- --- 1104 58 --- 1055 --- 28 | 36 --- --- --- 926 58 --- 910 --- 57
------+---------------------------------------------------+----------------------------------------------------
RMS | 14 20 19 14 7 43 22 15 23 |T 20 30 29 24 52 33 26 53 27 23
WRMS | 13 20 19 14 7 43 23 13 20 |NE 20 30 28 23 57 33 25 58 26 22
MEDI | 14 19 19 14 7 50 20 15 22 |MD 19 30 27 23 22 33 25 24 23 21
Table 3.1430.5 GPS week: 1430 Day: 5 MJD: 54259.000
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 13 25 13 8 17 16 11 14 5 | 17 27 31 23 20 22 30 27 27 23
2 | 16 20 21 14 9 55 25 13 23 7 | 9 28 23 18 15 34 27 16 25 15
3 | 14 14 16 13 8 19 16 15 25 6 | 15 25 23 16 19 24 23 24 22 18
4 | 13 16 26 12 6 17 20 12 21 6 | 11 23 31 24 19 24 25 21 21 19
5 | 9 16 21 15 7 14 18 9 16 5 | 23 34 35 27 30 31 35 32 31 29
6 | 11 15 21 15 8 12 35 10 26 7 | 23 30 27 24 27 28 48 28 40 27
7 | 11 15 12 13 8 11 36 11 21 6 | 30 35 28 31 32 33 54 29 43 32
8E | 16 19 19 14 9 22 25 14 18 6 | 27 31 36 35 27 32 34 27 38 29
9E | 15 13 23 15 5 16 24 12 17 6 | 26 30 35 25 25 33 29 32 30 26
10 | 12 17 22 10 7 18 19 10 15 5 | 14 22 20 19 16 21 23 17 21 16
11 | 18 20 23 16 9 54 36 13 23 8 | 20 33 37 25 23 30 28 25 24 22
12 | 17 17 16 15 5 48 24 11 26 7 | 25 36 33 24 28 36 29 30 36 27
13 | 16 16 22 13 6 54 13 14 20 7 | 16 35 38 23 22 35 28 21 27 22
14 | 19 25 17 18 5 54 18 15 29 8 | 14 40 32 29 19 34 21 19 25 21
16 | 19 16 25 16 9 52 32 16 26 8 | 13 27 29 23 21 30 29 24 25 19
17 | 13 17 18 11 6 51 29 14 50 8 | 16 20 30 20 20 27 30 25 45 19
18 | 16 21 19 12 6 62 20 15 23 7 | 19 33 28 26 19 31 24 20 18 21
19 | 18 16 17 15 8 56 32 14 27 8 | 21 33 31 29 28 36 27 27 27 25
20 | 14 26 20 12 8 54 18 13 21 7 | 16 34 27 23 22 35 24 22 24 20
21 | 16 15 17 11 6 58 17 12 19 6 | 18 26 25 19 17 30 21 18 28 18
22 | 16 24 18 12 6 54 18 17 22 7 | 17 39 26 23 19 30 23 19 28 20
23 | 15 20 24 13 5 52 22 13 24 7 | 15 36 32 22 20 33 22 16 26 18
24 | 13 14 20 11 5 14 27 10 25 6 | 31 38 39 36 34 36 30 36 46 34
25E | 15 17 16 11 7 20 22 13 19 6 | 59 67 70 65 62 68 67 62 69 64
26 | 13 12 22 11 8 21 15 11 21 5 | 15 23 22 21 17 23 19 18 20 17
27E | 20 18 16 12 9 21 15 15 19 6 | 14 23 23 20 18 21 17 20 23 15
28 | 14 18 17 13 8 57 24 14 30 7 | 20 35 29 28 23 32 26 24 34 24
29 | 10 13 24 12 7 20 28 14 26 6 | 48 51 53 49 49 54 61 51 54 50
X30 | 8 17 --- 14 7 12 16 10 16 5 | 19 25 --- 18 22 23 27 23 18 23
31E | 11 14 21 12 9 51 22 16 26 7 | 15 28 22 24 22 33 20 24 36 21
X32 | 24 --- --- --- 21 37 --- 20 --- 17 | 23 --- --- --- 267 39 --- 256 --- 57
------+---------------------------------------------------+----------------------------------------------------
RMS | 15 17 20 13 7 41 24 13 24 |T 20 32 31 26 32 32 30 33 31 25
WRMS | 15 17 20 13 7 41 24 11 21 |NE 19 31 30 24 32 31 29 33 29 24
MEDI | 15 16 20 13 7 37 22 13 22 |MD 18 31 30 24 22 32 27 24 27 22
Table 3.1430.6 GPS week: 1430 Day: 6 MJD: 54260.000
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 14 18 12 6 16 24 11 12 5 | 17 28 27 21 21 28 27 20 21 19
2 | 16 18 18 11 6 59 25 12 23 7 | 11 27 22 24 15 38 30 19 32 18
3 | 10 21 16 13 7 13 20 15 24 6 | 22 27 26 19 23 28 32 29 28 24
4 | 14 23 27 11 7 14 27 15 20 7 | 9 26 29 22 14 23 28 17 17 14
5 | 9 16 17 9 6 15 18 9 19 5 | 18 32 26 20 25 26 34 28 26 23
6 | 10 17 28 12 5 10 37 12 26 7 | 28 38 32 29 37 37 52 42 46 33
7 | 9 18 17 11 7 11 37 9 20 6 | 28 38 31 34 36 35 56 35 40 33
8E | 13 30 18 15 11 18 27 17 17 7 | 34 43 33 36 32 39 35 37 40 34
9E | 15 13 22 13 6 17 22 10 20 6 | 24 33 37 33 28 31 27 29 25 27
10 | 11 19 26 12 9 14 21 13 21 6 | 15 20 25 19 18 16 25 22 29 16
11 | 13 19 21 17 6 50 21 14 23 7 | 18 34 38 27 23 35 18 24 22 21
12 | 16 17 18 14 6 50 26 14 36 8 | 24 33 31 26 24 45 30 24 33 24
13 | 18 17 16 16 9 54 24 13 29 8 | 15 32 34 24 20 35 23 19 29 19
14 | 17 22 16 18 6 59 19 14 26 8 | 21 32 25 28 18 34 19 20 27 19
16 | 17 20 18 17 7 51 32 19 22 8 | 20 32 29 30 23 44 32 24 24 23
17 | 10 16 18 12 10 48 33 13 41 8 | 21 23 25 25 24 40 32 26 42 22
18 | 13 21 19 13 7 57 18 14 31 7 | 24 37 36 31 26 39 29 26 34 28
19 | 14 18 12 17 11 49 42 16 29 8 | 23 35 25 33 28 50 33 26 29 25
20 | 13 16 16 12 6 53 21 12 20 6 | 18 32 30 28 22 36 22 22 23 22
21 | 16 21 16 11 7 54 20 14 31 7 | 21 27 30 24 20 34 21 21 26 20
22 | 14 21 19 12 6 52 15 16 22 7 | 20 36 32 28 24 37 23 23 29 24
23 | 17 87 15 19 14 49 23 17 30 13 | 13 63 27 23 21 31 19 17 26 17
24 | 13 19 24 11 5 14 29 9 26 6 | 32 39 48 38 35 40 30 38 47 36
25E | 12 19 21 14 8 19 24 10 23 6 | 68 72 74 74 64 70 62 68 79 70
26 | 9 16 19 9 6 17 19 9 28 5 | 16 22 29 23 20 25 18 22 29 19
27E | 17 17 27 14 8 20 15 11 17 6 | 16 30 31 25 20 29 20 27 21 20
28 | 13 23 14 16 8 51 28 15 28 8 | 24 36 33 28 25 41 21 26 36 25
29 | 23 23 27 23 17 23 111 15 81 16 | 63 64 63 66 59 65 57 60 68 62
30 | 7 15 22 12 5 15 21 9 19 5 | 19 25 5 15 21 23 27 23 14 22
31E | 10 19 18 12 6 51 20 14 11 6 | 18 32 23 22 19 31 28 24 21 20
X32 | 21 --- --- --- 14 54 --- 15 --- 17 | 29 --- --- --- 124 40 --- 129 --- 47
------+---------------------------------------------------+----------------------------------------------------
RMS | 14 25 20 14 8 39 32 13 29 |T 23 34 31 29 29 36 30 31 32 26
WRMS | 13 20 20 14 8 39 28 11 22 |NE 21 33 30 27 28 35 29 30 31 25
MEDI | 13 19 18 12 7 48 23 14 23 |MD 21 32 30 26 23 35 28 24 29 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 4.1430 GPS week: 1430 MJD: 54254.0-54260.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2943 |U 17 11 30 |U 19 29 66 |U 21 26 43 |
emr | emr 2866 |U 18 13 32 |U 19 28 62 | 24 29 49 |
esa | esa 2729 |U 22 14 33 |U 19 28 67 | 20 27 41 |
gfz | gfz 2845 |U 17 13 35 |U 17 25 63 |U 20 25 41 |
igr | igr 2917 | 22 14 34 | 19 27 67 | 22 27 46 |
igs | igs 2916 | 19 13 34 | 19 25 68 | 23 28 45 |
jpl | jpl 2931 | 22 15 37 | 19 33 68 | 27 35 53 |
mit | mit 2880 |U 17 10 31 |U 17 28 59 |U 19 25 38 |
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 5.1430.0 GPS week: 1430 Day: 0 MJD: 54254.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2934 | 14 11 27 | 15 24 53 | 19 22 34 |
emr | emr 2880 | 12 8 29 | 19 27 57 | 21 21 39 |
esa | esa 2784 | 21 13 32 | 17 24 60 | 19 20 39 |
gfz | gfz 2853 | 10 8 29 | 14 22 52 | 21 19 37 |
igr | igr 2918 | 15 11 29 | 16 23 64 | 20 23 38 |
igs | igs 2907 | 10 9 24 | 16 20 64 | 22 21 40 |
jpl | jpl 2944 | 12 9 27 | 15 28 65 | 25 36 43 |
mit | mit 2880 | 11 7 22 | 13 23 51 | 20 22 33 |
Table 5.1430.1 GPS week: 1430 Day: 1 MJD: 54255.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2946 | 11 11 24 | 18 27 58 | 19 27 47 |
emr | emr 2879 | 10 26 25 | 20 29 51 | 24 23 46 |
esa | esa 2784 | 17 18 26 | 19 27 65 | 21 27 42 |
gfz | gfz 2855 | 10 20 42 | 16 22 57 | 22 23 41 |
igr | igr 2932 | 16 19 26 | 19 24 61 | 23 19 44 |
igs | igs 2926 | 13 14 27 | 19 26 68 | 23 23 45 |
jpl | jpl 2945 | 15 25 36 | 16 28 57 | 27 35 51 |
mit | mit 2976 | 11 8 31 | 17 25 55 | 20 23 39 |
Table 5.1430.2 GPS week: 1430 Day: 2 MJD: 54256.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2946 | 15 9 35 | 24 36 91 | 33 35 81 |
emr | emr 2784 | 15 8 36 | 17 29 52 | 26 33 69 |
esa | esa 2688 | 28 18 46 | 16 24 63 | 20 31 51 |
gfz | gfz 2765 | 17 11 40 | 16 22 58 | 21 28 56 |
igr | igr 2843 | 25 13 36 | 18 23 63 | 23 29 54 |
igs | igs 2848 | 18 12 38 | 19 20 68 | 23 26 55 |
jpl | jpl 2851 | 23 14 34 | 16 28 57 | 28 38 69 |
mit | mit 2784 | 17 10 35 | 13 23 53 | 19 27 53 |
Table 5.1430.3 GPS week: 1430 Day: 3 MJD: 54257.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2951 | 17 9 28 | 21 30 75 | 19 28 38 |
emr | emr 2880 | 19 9 30 | 22 32 82 | 22 25 44 |
esa | esa 2688 | 15 8 20 | 23 33 74 | 18 30 36 |
gfz | gfz 2861 | 17 10 26 | 21 29 75 | 18 28 39 |
igr | igr 2927 | 17 11 28 | 20 32 77 | 18 30 39 |
igs | igs 2917 | 20 13 34 | 22 31 64 | 25 41 51 |
jpl | jpl 2946 | 19 6 37 | 22 38 90 | 25 36 55 |
mit | mit 2880 | 15 9 28 | 20 36 68 | 18 28 39 |
Table 5.1430.4 GPS week: 1430 Day: 4 MJD: 54258.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2947 | 9 9 26 | 21 33 67 | 18 24 32 |
emr | emr 2880 | 11 9 28 | 22 31 73 | 21 28 41 |
esa | esa 2688 | 14 10 25 | 21 35 71 | 19 30 34 |
gfz | gfz 2861 | 10 9 28 | 19 31 67 | 19 26 38 |
igr | igr 2946 | 11 13 40 | 20 30 70 | 20 30 42 |
igs | igs 2946 | 10 10 38 | 22 29 88 | 19 25 39 |
jpl | jpl 2949 | 16 11 31 | 22 41 85 | 28 36 50 |
mit | mit 2880 | 12 7 27 | 21 32 71 | 17 23 30 |
Table 5.1430.5 GPS week: 1430 Day: 5 MJD: 54259.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2947 | 15 7 30 | 20 28 60 | 19 24 35 |
emr | emr 2880 | 22 13 39 | 19 24 64 | 23 29 44 |
esa | esa 2688 | 17 7 31 | 18 26 70 | 20 27 43 |
gfz | gfz 2861 | 15 9 35 | 17 24 70 | 19 26 38 |
igr | igr 2929 | 21 9 35 | 19 28 65 | 20 28 39 |
igs | igs 2944 | 18 9 42 | 18 25 64 | 22 28 41 |
jpl | jpl 2941 | 20 9 35 | 19 33 74 | 27 37 50 |
mit | mit 2880 | 16 7 30 | 18 26 61 | 19 25 34 |
Table 5.1430.6 GPS week: 1430 Day: 6 MJD: 54260.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2930 | 40 24 42 | 17 26 55 | 19 22 32 |
emr | emr 2880 | 38 20 38 | 17 23 57 | 27 46 58 |
esa | esa 2784 | 39 25 48 | 18 25 63 | 22 28 42 |
gfz | gfz 2859 | 42 25 44 | 17 24 60 | 21 25 40 |
igr | igr 2928 | 48 24 42 | 21 27 67 | 30 31 65 |
igs | igs 2929 | 43 23 38 | 18 26 61 | 25 30 40 |
jpl | jpl 2943 | 50 31 57 | 24 38 52 | 27 30 52 |
mit | mit 2880 | 38 23 41 | 19 31 50 | 20 25 36 |
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 6.1430 GPS week: 1430 MJD: 54254.500-54260.500
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 | -51 -13 63 -51 0 | 5 18
| 12 18 41 35 7 | 2
emr uuuxu | 18 17 -92 626 5 | 50 55
| 35 26 95 80 7 | 3
esa uuuuu | -5 -7 72 -11 4 | 51 57
| 33 74 88 129 14 | 3
gfz uuuuu | -15 11 -67 -44 8 | -2 21
| 13 11 35 41 4 | 4
igr xxxxx | 24 9 -29 -17 9 | -1 20
| 26 16 92 114 15 | 5
irf xxxxx | -8 16 65 -51 10 | 3 25
| 13 19 34 30 11 | 6
jpl uuuuu | -35 64 -173 125 -9 | -3 20
| 18 25 145 140 15 | 2
mit uuuux | 1 3 81 -60 36 | 31 44
| 34 43 60 67 18 | 15
ngs uuxuu | 60 -10 85 129 -2 | 17 19
| 38 44 264 116 11 | 1
sio uuuuu | 3 -28 67 -55 6 | 23 34
| 30 32 62 41 8 | 4
Table 7.1430.0 GPS week: 1430 Day: 0 MJD: 54254.500
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 | -45 0 96 -55 -3 | 7 20
emr uuuxu | 22 44 -166 612 11 | 49 54
esa uuuuu | 47 -152 155 204 28 | 45 53
gfz uuuuu | -13 -5 -32 -98 4 | -5 20
igr xxxxx | 33 -10 -133 -203 15 | -5 19
irf xxxxx | -17 41 46 -35 24 | -5 23
jpl uuuuu | -22 88 -319 108 -13 | 0 21
mit uuuux | -28 72 114 -37 59 | 11 23
ngs uuxuu | 46 11 -324 78 -1 | 18 20
sio uuuuu | -24 7 -18 -101 11 | 18 30
Table 7.1430.1 GPS week: 1430 Day: 1 MJD: 54255.500
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 | -62 -21 -11 -38 -2 | 6 19
emr uuuxu | -5 41 106 742 14 | 47 53
esa uuuuu | 30 -22 -69 7 16 | 49 56
gfz uuuuu | -3 6 -32 1 14 | -7 20
igr xxxxx | 53 24 128 87 16 | -6 18
irf xxxxx | -25 12 62 -82 26 | -4 24
jpl uuuuu | -20 86 -117 272 -4 | -3 22
mit uuuux | -38 15 -10 -135 57 | 16 30
ngs uuxuu | 83 1 461 66 -22 | 18 20
sio uuuuu | -43 -46 104 -63 22 | 18 30
Table 7.1430.2 GPS week: 1430 Day: 2 MJD: 54256.500
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 | -56 12 85 -78 -11 | 6 19
emr uuuxu | -5 -13 -76 600 9 | 48 54
esa uuuuu | -21 -11 29 -168 5 | 52 60
gfz uuuuu | -24 26 -105 -26 11 | -5 21
igr xxxxx | 33 14 -98 -22 22 | -5 20
irf xxxxx | -19 14 63 -70 11 | 0 26
jpl uuuuu | -26 52 -292 318 5 | -4 21
mit uuuux | -34 -39 131 -129 40 | 25 41
ngs uuxuu | 98 14 90 227 -5 | 18 20
sio uuuuu | 2 -51 97 -103 4 | 21 33
Table 7.1430.3 GPS week: 1430 Day: 3 MJD: 54257.500
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 | -59 -37 84 -76 -6 | 4 18
emr uuuxu | -8 41 -106 573 0 | 50 56
esa uuuuu | -43 -15 100 104 -3 | 56 63
gfz uuuuu | -24 6 -124 -59 3 | -2 22
igr xxxxx | -21 29 -82 -53 27 | -1 23
irf xxxxx | -8 -20 128 -34 6 | 3 28
jpl uuuuu | -46 61 -129 183 9 | -4 21
mit uuuux | 7 -61 121 50 35 | 32 48
ngs uuxuu | 107 58 216 3 -3 | 17 19
sio uuuuu | 19 -82 108 5 3 | 24 36
Table 7.1430.4 GPS week: 1430 Day: 4 MJD: 54258.500
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 | -59 2 97 -43 5 | 2 18
emr uuuxu | 33 -18 -177 625 1 | 48 55
esa uuuuu | -28 80 115 -110 2 | 50 55
gfz uuuuu | 5 10 -60 -88 8 | -3 23
igr xxxxx | 24 -6 4 -107 -9 | 1 23
irf xxxxx | 0 31 16 -87 5 | 4 27
jpl uuuuu | -38 16 -53 10 -12 | -4 20
mit uuuux | 32 23 57 -105 30 | 36 51
ngs uuxuu | 49 -73 182 325 -2 | 16 18
sio uuuuu | 0 -2 -19 -68 2 | 23 35
Table 7.1430.5 GPS week: 1430 Day: 5 MJD: 54259.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -29 -30 64 -84 6 | 5 17
emr uuuxu | -2 22 -94 513 2 | 54 58
esa uuuuu | -20 42 2 -28 -11 | 53 58
gfz uuuuu | -10 24 -54 -45 4 | 2 20
igr xxxxx | 2 19 44 103 1 | 5 19
irf xxxxx | 6 9 68 -40 -4 | 10 25
jpl uuuuu | -70 73 38 -66 -14 | -1 17
mit uuuux | 32 3 15 -19 15 | 46 56
ngs uuxuu | 35 -45 161 166 7 | 17 19
sio uuuuu | 20 -16 131 -43 -5 | 28 37
Table 7.1430.6 GPS week: 1430 Day: 6 MJD: 54260.500
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 | -50 -17 26 16 10 | 5 17
emr uuuxu | 88 4 -130 717 -4 | 56 59
esa uuuuu | 2 33 172 -85 -12 | 52 57
gfz uuuuu | -33 14 -59 9 12 | 3 19
igr xxxxx | 47 -4 -63 77 -10 | 6 19
irf xxxxx | 7 24 74 -6 1 | 11 24
jpl uuuuu | -24 70 -336 48 -37 | -3 19
mit uuuux | 38 10 138 -42 16 | 50 58
ngs uuxuu | 1 -35 -191 39 13 | 17 19
sio uuuuu | 50 -5 70 -12 3 | 29 37
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