[IGSREPORT-17174] Wk 1519 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 5 06:17:35 PST 2009
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IGS Electronic Report 05 Mar 06:17:37 PST 2009 Message Number 17174
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1519 (Feb 15, 2009 - Feb 21, 2009)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
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:
igs1519[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1519[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1519[0-6].cls IGS GPS clock combination summary report.
igs15197.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15197.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, 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.
Starting week 1478, a new solution from CNES/GRGS (GRG) is included for
evaluation and 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 | COD | 26 26
0 | EMR | HARB DAEJ HARB MIZU
0 | ESA | MAW1
0 | GFZ | 3 7 13 14 15 26 29 DAEJ FAA1 IRKT NRIL OHI2 SCH2
0 | GRG | NLIB NRIL
0 | JPL | HARB UNSA
0 | MIT | DAEJ DAEJ
1 | COD | 3 3 26
1 | EMR | HARB DAEJ HARB MIZU
1 | ESA | 3 6 26 SCH2 UNSA
1 | GFZ | 6 7 13 14 15 23 29 IRKT SUTM
1 | GRG | NLIB
1 | JPL | 3 HARB ZWE2
1 | MIT | 6 DAEJ ONSA
2 | COD | 3 3 USNO USNO
2 | EMR | HARB HARB WILL
2 | ESA | 3 7 26 SCH2
2 | GFZ | 7 29 IRKT MATE
2 | GRG | NLIB
2 | JPL | 7 HARB
2 | MIT | IENG ALIC IENG PRDS SCH2
3 | COD | 3 3 26
3 | EMR | 6 MIZU
3 | ESA | 3 26
3 | GFZ | 7 13 14 29 FAA1 HARB MATE ONSA REYK SCH2 VESL
3 | GRG | NLIB
3 | JPL | THU3 ZWE2
3 | MIT | HARB DAV1 HARB
4 | COD | 3 6 3 6 26 DAEJ SYDN
4 | EMR | HARB HARB MIZU
4 | ESA | 3 6 26 RAMO SCH2
4 | GFZ | 7 13 14 15 23 29 IRKT KOUR
4 | GRG | NLIB
4 | JPL | SCH2 ZWE2
5 | COD | 3 6 26 3 6 26
5 | EMR | SYOG MIZU
5 | ESA | 3 6 26 MAL2 MAS1 TOW2
5 | GFZ | 7 15 29 DAEJ DAV1 IRKT MATE SCH2
5 | GRG | NLIB REYK
5 | MIT | 30 30 MAS1 ALIC DARW DAV1 HOB2 MAS1 MAW1
6 | COD | 3 6 3 6 RCMN
6 | ESA | 3 6 26 MDVJ
6 | GFZ | 7 13 23 29 DAEJ
6 | GRG | GRAS NLIB REYK YSSK
6 | MIT | DARW
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
----+--------+---------------
2 | NGS | 5
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 G03 | | | | | | | 1 |
PRN G06 | | | | 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 | .5 .5 .6 -24 -7 -15 .25
EMR | 13.3 -8.9 -6.5 10 43 59 .35
ESA | 8.9 2.8 .8 -1 -113 29 .27
GFZ | .8 .7 1.3 22 -5 21 -.13
GRG | 6.2 -2.6 -6.3 -19 -16 21 .09
JPL | 9.1 2.5 2.8 -27 -43 37 .38
MIT | 11.4 -3.8 -.4 -15 2 -12 .09
NGS | 8.8 -2.6 -3.2 -42 -148 6 .24
SIO | 5.3 -2.7 -7.2 -51 -106 21 .51
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 1.1519.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1519.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 2.1519.[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 3.1519.[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 5.1519.0-6).
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 1519 summary. (Feb 15, 2009 - Feb 21, 2009)
Table 1.1519.a GPS week: 1519 MJD: 54877.000-54883.000
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 236| 0 0 2 12 -67 -48 -.10 9 8 | -224 -617 15 123
| 0 0 1 10 12 41 .02 | 615 891
emr 75| 1 -1 5 -59 -196 -74 .50 19 19 | 358 679 19 183
| 1 1 1 23 18 18 .02 | 871 687
esa 130| 0 0 -2 -42 91 -6 .32 9 9 | 218 -493 22 151
| 1 0 1 36 29 27 .02 | 1210 1269
gfz 196| 0 -1 -5 -69 -73 126 -.11 10 10 | -448 -42 24 138
| 1 0 1 16 16 51 .02 | 1308 615
grg 76| 1 0 0 -16 -61 -45 1.16 42 41 | -142971 603047 92 236
| 1 1 1 17 23 181 .15 | 377913 1595921
igr n/a| 0 0 0 -34 -66 -50 .05 5 5 | 5178 589 21 76
| 0 0 0 14 15 40 .04 | 906 676
jpl 132| 0 0 5 10 9 -11 .47 18 17 | 927 707 21 111
| 0 1 1 16 14 38 .03 | 1091 694
mit 257| 1 0 -1 11 -102 -26 -.30 10 9 | -316 43 21 140
| 0 0 1 25 23 14 .03 | 343 667
ngs 218| 0 0 0 92 196 -11 -.29 10 7 | 95044 -143441 2393 4160
| 0 0 1 19 37 27 .02 | 252055 377707
sio 257| -1 1 0 61 111 25 -.11 20 20 | --- --- --- ---
| 0 2 1 27 29 21 .02 | --- ---
Table 1.1519.b GPS week : 1519 MJD: 54877.000-54883.000
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
------+------------------------------------+------------------------------------------
2 | 5 5 6 6 6 6 6 |
3 | 6 7 5 6 6 6 6 |
4 | 4 4 4 4 4 4 5 |
5 | 4 4 6 4 4 4 4 |
6 | 5 5 5 7 7 7 6 |
7 | 5 5 5 5 5 6 6 |
8 | 4 3 4 3 3 4 4 |
9 | 3 3 4 3 4 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 5 4 4 5 5 5 4 |
12 | 5 5 5 5 5 6 5 |
13 | 4 4 4 4 4 5 5 |
14 | 4 4 4 4 4 5 4 |
15 | 5 5 5 5 6 5 6 |
16 | 5 5 5 5 5 5 6 |
17 | 4 4 5 4 6 5 5 |
18 | 5 5 4 5 5 6 6 |
19 | 5 5 5 5 5 5 5 |
20 | 5 5 5 5 6 6 6 |
21 | 5 4 4 4 5 5 5 |
22 | 5 4 4 5 5 5 5 |
23 | 5 5 4 5 5 5 5 |
24 | 3 3 3 4 4 4 4 |
25 | 3 3 4 3 4 4 4 |
26 | 6 5 5 6 6 6 6 |
27 | 3 4 3 3 4 3 4 |
28 | 4 4 4 4 4 4 4 |
29 | 4 5 4 5 5 6 6 |
30 | 4 3 4 3 4 4 4 |
31 | 5 4 5 5 5 5 5 |
32 | 4 4 4 4 5 4 5 |
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 2.1519.0 GPS week: 1519 Day: 0 MJD: 54877.000
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 236| 0 0 1 0 -52 -39 -.10 8 7 | 132 -1109 11 100
| 52 -26 |
emr 75| 1 0 5 -62 -193 -44 .50 19 19 | -1269 1904 19 175
| 54 35 |
esa 130| -1 0 0 -74 81 23 .31 7 7 | -723 377 20 140
| 34 14 |
gfz 196| 1 -1 -7 -82 -79 94 -.14 11 11 | -135 201 22 139
| 39 -23 |
grg 76| 1 -1 1 -36 -72 42 1.09 38 37 | -364 230 89 203
| 85 3 |
igr n/a| 0 0 0 -27 -63 -84 .13 6 5 | 3618 1554 19 83
| 16 9 |
jpl 132| -1 1 5 5 -7 -9 .44 19 18 | -850 1747 18 90
| -3 17 |
mit 257| 2 -1 0 55 -131 -23 -.26 10 9 | -694 649 19 149
| -25 47 |
ngs 218| 0 0 0 91 217 -23 -.31 10 7 | 49 -991 2154 3805
| -48 -23 |
sio 257| -1 0 0 106 100 11 -.09 21 21 | --- --- --- ---
| -22 -17 |
Table 2.1519.1 GPS week: 1519 Day: 1 MJD: 54878.000
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 236| 0 0 2 22 -53 -48 -.08 8 8 | 516 -1646 13 144
| 10 -12 |
emr 75| 0 -3 3 -28 -185 -70 .52 19 19 | 439 79 17 228
| 30 33 |
esa 130| 0 1 0 -80 69 -10 .35 9 9 | 519 -2662 22 156
| 25 -8 |
gfz 196| 0 0 -3 -74 -59 158 -.11 9 9 | 351 -449 23 144
| -13 -24 |
grg 76| 1 0 3 -3 -48 91 1.16 40 40 | 256 -634 91 232
| -11 3 |
igr n/a| -1 0 1 -20 -70 -72 .03 5 5 | 5022 173 23 90
| 23 8 |
jpl 132| 0 0 5 37 -2 -14 .48 18 17 | 692 166 22 113
| 1 13 |
mit 257| 1 -1 0 -19 -117 -15 -.29 9 8 | 135 -426 18 135
| -1 34 |
ngs 218| 0 0 -1 122 226 -46 -.28 10 7 | 379 -1481 2336 4105
| -75 36 |
sio 257| 0 0 0 31 76 29 -.13 19 18 | --- --- --- ---
| -13 3 |
Table 2.1519.2 GPS week: 1519 Day: 2 MJD: 54879.000
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 236| -1 0 3 5 -65 -5 -.10 9 9 | -333 -167 24 147
| 37 13 |
emr 75| 3 -3 5 -41 -171 -92 .48 19 19 | -332 686 23 200
| 28 39 |
esa 130| 0 0 -3 -67 53 -37 .31 7 7 | 2500 -790 26 148
| 30 8 |
gfz 196| 0 -1 -6 -62 -52 187 -.09 10 10 | -242 787 30 151
| -19 -19 |
grg 76| 2 -2 0 -28 -80 204 1.21 43 43 | -999999 4222256 87 270
| 83 21 |
igr n/a| -1 0 0 -57 -46 -89 -.01 6 6 | 4416 814 24 80
| 58 15 |
jpl 132| 1 2 5 10 30 -33 .44 18 17 | -190 1288 25 135
| 23 -16 |
mit 257| 1 0 0 26 -95 -34 -.30 8 8 | -765 332 25 174
| -8 41 |
ngs 218| -2 0 1 97 223 -34 -.27 11 8 | 666651 -999999 2518 4258
| 10 43 |
sio 257| -2 0 2 78 113 0 -.14 19 19 | --- --- --- ---
| -14 3 |
Table 2.1519.3 GPS week: 1519 Day: 3 MJD: 54880.000
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 236| 0 0 4 22 -70 -124 -.08 10 8 | 354 -1490 14 128
| 24 14 |
emr 75| 1 0 4 -42 -201 -73 .51 20 20 | 721 1225 19 203
| 44 76 |
esa 130| 1 0 -4 -59 116 -5 .33 9 9 | 415 -887 22 139
| 22 -40 |
gfz 196| 0 0 -4 -66 -95 151 -.10 10 10 | -35 350 24 136
| 8 9 |
grg 76| 2 1 0 -12 -63 -78 1.32 39 37 | -414 789 86 205
| 25 64 |
igr n/a| 0 1 0 -37 -70 -45 .04 5 4 | 5616 1345 19 82
| 24 50 |
jpl 132| 0 0 3 -8 3 63 .49 18 17 | 1689 1081 20 107
| -14 17 |
mit 257| 0 0 0 3 -109 -24 -.29 9 7 | -452 850 22 122
| -7 41 |
ngs 218| 0 0 2 106 200 12 -.30 10 8 | 384 -1547 2312 3855
| -38 48 |
sio 257| -2 1 1 55 124 18 -.12 19 20 | --- --- --- ---
| 1 -10 |
Table 2.1519.4 GPS week: 1519 Day: 4 MJD: 54881.000
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 236| 0 0 2 14 -89 -2 -.10 9 8 | -759 -420 12 136
| 22 60 |
emr 75| 0 0 8 -61 -230 -102 .50 19 19 | 988 57 15 187
| 72 62 |
esa 130| 0 0 -4 -27 139 -45 .32 10 10 | -342 -535 22 160
| 15 -50 |
gfz 196| -1 -2 -3 -88 -59 159 -.10 9 9 | 172 -974 23 133
| 13 31 |
grg 76| 0 -2 -2 -4 -54 -147 1.35 43 41 | -74 -773 88 235
| 30 136 |
igr n/a| 0 0 0 -43 -77 -67 .06 5 5 | 6033 -180 20 72
| 51 -14 |
jpl 132| 0 0 5 7 1 -53 .48 19 18 | 1852 -102 21 135
| 15 -18 |
mit 257| 2 0 -1 16 -55 -51 -.32 12 10 | 14 -1019 18 148
| -7 16 |
ngs 218| 0 0 0 94 116 -28 -.31 10 7 | -732 -462 2735 4345
| -6 84 |
sio 257| 0 1 1 63 162 14 -.11 19 19 | --- --- --- ---
| -10 -17 |
Table 2.1519.5 GPS week: 1519 Day: 5 MJD: 54882.000
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 236| 1 1 3 0 -68 -75 -.12 10 8 | -1207 940 14 100
| 52 0 |
emr 75| 1 0 6 -90 -194 -70 .48 18 18 | 1228 139 17 126
| 74 53 |
esa 130| 0 -1 -3 2 84 4 .32 9 9 | -1270 1497 23 151
| 3 11 |
gfz 196| 0 -1 -5 -39 -90 85 -.10 11 11 | -3382 299 24 127
| -4 0 |
grg 76| 2 2 0 -38 -19 -355 1.06 44 43 | -243 101 110 258
| 70 1 |
igr n/a| 0 0 0 -42 -49 -10 .05 5 5 | 6137 -54 21 61
| 21 -19 |
jpl 132| 0 0 5 -5 23 -37 .45 18 18 | 1969 82 23 94
| 11 -22 |
mit 257| 2 0 -1 7 -110 -7 -.34 13 11 | -324 284 26 126
| -20 5 |
ngs 218| -1 0 1 61 204 20 -.28 10 7 | -1175 868 2353 4310
| 80 -34 |
sio 257| -1 3 1 70 78 43 -.10 20 21 | --- --- --- ---
| -9 -2 |
Table 2.1519.6 GPS week: 1519 Day: 6 MJD: 54883.000
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 236| 0 0 2 22 -73 -45 -.12 10 9 | -272 -428 19 108
| 38 58 |
emr 75| 1 -1 5 -86 -195 -70 .48 19 19 | 731 664 24 163
| 83 71 |
esa 130| 2 0 0 5 97 24 .30 10 9 | 433 -453 22 166
| -3 -3 |
gfz 196| -2 0 -5 -74 -76 45 -.14 11 11 | 132 -512 25 142
| -8 24 |
grg 76| -1 0 0 4 -89 -71 .94 46 46 | 35 -639 99 251
| 37 105 |
igr n/a| 0 0 0 -16 -90 19 .05 5 4 | 5404 477 21 67
| -21 51 |
jpl 132| 0 0 6 28 16 6 .52 18 17 | 1329 693 22 103
| -29 -67 |
mit 257| 1 0 -2 -12 -101 -31 -.33 11 10 | -131 -364 22 131
| -16 22 |
ngs 218| 0 0 0 75 188 19 -.27 11 8 | -245 -481 2347 4447
| 40 -13 |
sio 257| -3 4 0 25 125 63 -.07 21 20 | --- --- --- ---
| 20 -29 |
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 3.1519.0 GPS week: 1519 Day: 0 MJD: 54877.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 6 15 7 17 58 6 20 8 6 40 5 | 19 27 26 29 51 21 29 17 23 34 21
3E | 12 22 10 21 23 14 18 14 12 18 5 | 99 101 97 100 121 103 100 97 98 103 98
4 | 7 10 5 13 55 4 13 10 8 22 3 | 34 40 42 45 37 39 37 37 40 33 38
5 | 9 11 5 8 23 3 12 12 9 18 3 | 14 18 16 14 38 14 12 20 16 15 15
6 | 8 23 9 9 32 8 16 10 10 25 4 | 42 51 49 47 43 47 45 51 46 43 46
7 | 8 23 8 17 36 5 21 10 6 24 5 | 19 33 26 30 35 22 29 25 24 25 23
8 | 9 10 7 11 20 5 14 10 8 16 3 | 40 42 39 41 41 39 39 40 36 34 37
9 | 6 11 8 7 22 5 10 7 10 13 3 | 18 18 21 17 25 19 19 18 20 20 18
10 | 6 12 8 14 27 5 11 7 7 23 3 | 18 23 24 24 27 19 22 19 21 24 20
11 | 8 21 6 10 78 6 20 12 6 19 4 | 31 39 34 34 52 31 34 37 31 28 31
12 | 7 25 6 13 26 5 24 13 8 18 5 | 21 36 24 19 35 22 33 19 23 17 22
13E | 7 14 8 9 33 5 20 9 8 16 4 | 16 27 17 14 34 17 24 19 16 20 15
14E | 8 23 7 10 28 6 18 7 7 21 4 | 19 30 25 16 42 21 30 18 22 20 21
15E | 7 23 7 12 28 6 23 13 13 25 5 | 26 32 29 26 35 24 31 26 24 27 25
16 | 9 24 8 9 29 7 23 12 13 15 5 | 26 38 30 21 35 28 38 26 25 24 26
17 | 8 20 7 8 46 5 21 8 9 15 4 | 23 34 30 21 54 26 33 21 21 25 24
18 | 6 22 7 10 29 5 23 7 8 28 4 | 19 31 21 20 33 19 31 19 24 25 20
19 | 8 29 8 12 32 7 23 9 8 11 4 | 25 43 34 24 54 30 39 26 28 26 27
20 | 7 22 6 11 62 5 22 9 9 31 5 | 22 33 24 25 51 22 31 25 22 30 22
21 | 8 16 7 11 55 5 18 6 11 29 4 | 23 24 24 25 43 22 25 24 25 30 23
22 | 6 25 5 10 42 8 22 10 9 27 4 | 23 34 26 25 42 22 33 25 24 26 23
23E | 7 16 6 12 36 5 21 12 12 18 4 | 19 26 21 21 30 20 26 22 24 24 19
24 | 8 9 7 9 33 4 11 6 6 16 3 | 29 35 37 37 24 32 34 34 34 37 34
25 | 6 12 6 7 35 5 13 10 7 12 3 | 16 22 19 17 25 18 21 20 22 17 18
26E | 9 24 12 9 40 7 17 11 21 12 5 | 17 35 25 18 38 21 31 15 31 20 19
27 | 7 10 8 9 12 5 11 6 8 12 3 | 20 26 22 20 29 22 24 21 21 21 19
28 | 8 20 9 10 44 5 19 9 8 16 4 | 17 33 22 16 42 19 26 19 19 18 17
29 | 8 20 7 6 21 6 19 9 11 21 4 | 22 29 22 18 37 22 27 24 24 27 21
30 | 8 14 6 8 17 3 14 9 11 17 3 | 16 22 17 13 24 16 19 19 18 17 15
31 | 5 21 9 10 37 8 21 9 12 23 4 | 20 32 24 23 39 22 29 22 23 26 21
32 | 6 18 7 9 36 5 20 6 7 24 4 | 15 20 19 16 25 17 22 17 20 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 7 11 38 6 19 10 10 21 |T 24 33 28 26 40 26 31 26 27 27 25
WRMS | 7 19 7 11 37 5 18 9 7 21 |NE 22 30 25 24 36 23 28 24 24 24 22
MEDI | 8 20 7 10 33 5 19 9 8 18 |MD 20 32 24 21 37 22 30 22 24 25 21
Table 3.1519.1 GPS week: 1519 Day: 1 MJD: 54878.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 9 17 8 14 52 5 19 6 6 39 5 | 14 24 22 21 40 15 24 12 18 32 15
3E | 14 30 10 18 52 8 19 13 18 19 6 | 88 100 92 90 87 90 94 91 84 95 89
4 | 7 9 6 9 46 7 11 8 7 24 3 | 30 34 35 36 27 32 32 31 32 33 32
X5 | 9 12 6 7 68 5 --- 10 8 16 3 | 12 18 11 13 65 12 --- 17 25 13 12
6 | 8 26 10 7 22 7 18 10 15 24 5 | 36 47 38 39 45 36 40 39 35 39 37
7 | 11 22 9 14 31 4 21 9 6 24 5 | 16 29 26 25 32 18 24 21 27 20 20
8 | 6 11 6 6 14 4 10 8 7 13 3 | 39 38 35 38 30 38 37 38 40 37 37
9 | 8 11 7 7 33 3 10 7 7 13 3 | 15 22 16 17 28 14 17 15 20 21 16
10 | 9 12 11 6 31 5 11 8 9 16 3 | 10 15 21 16 25 12 15 13 16 19 13
11 | 10 18 10 7 80 4 19 10 7 15 4 | 21 31 20 25 48 23 29 25 24 22 22
12 | 12 23 8 12 27 4 20 11 7 19 5 | 19 32 24 16 34 16 29 14 24 13 18
13E | 7 18 7 6 32 5 17 9 10 13 3 | 16 25 19 11 31 17 22 17 23 16 16
14E | 8 17 7 9 31 4 18 8 6 17 4 | 15 26 18 13 30 15 26 14 19 12 15
15E | 8 24 11 11 28 6 24 11 10 14 5 | 23 30 29 24 38 22 32 25 27 22 24
16 | 8 22 11 8 20 4 25 14 8 18 5 | 16 30 19 14 35 17 31 17 25 16 17
17 | 8 18 6 9 43 4 19 7 9 14 4 | 14 26 19 16 44 15 26 13 17 20 16
18 | 9 21 7 10 40 4 24 6 8 22 4 | 13 28 15 13 38 11 26 12 18 16 13
19 | 7 27 8 10 31 5 21 8 6 11 4 | 22 37 28 23 48 21 32 23 24 25 23
20 | 9 17 6 10 57 5 20 10 7 25 4 | 16 26 17 19 44 18 27 17 20 19 16
21 | 6 13 8 7 67 5 17 6 7 26 4 | 17 25 17 20 38 16 21 19 21 23 18
22 | 7 19 7 7 57 6 20 9 7 22 4 | 17 30 20 19 42 16 30 20 18 20 18
23E | 8 18 10 9 34 5 22 9 10 20 4 | 18 25 23 17 32 20 25 18 25 24 19
24 | 8 10 6 6 32 3 12 7 9 11 3 | 20 24 26 23 31 19 23 22 25 22 22
25 | 7 12 7 5 32 5 11 7 7 12 3 | 15 21 20 18 23 17 19 18 24 16 18
26E | 12 19 11 7 53 4 16 10 21 14 5 | 11 27 20 14 44 14 27 13 28 18 14
27 | 8 14 7 7 12 6 9 10 11 12 3 | 13 25 19 17 26 16 20 17 22 18 17
28 | 6 16 10 8 36 4 13 8 13 12 4 | 14 25 22 15 41 15 21 16 21 13 16
29 | 8 17 16 10 35 6 17 10 6 23 4 | 17 26 18 20 37 18 21 20 21 24 17
30 | 7 14 5 7 16 4 12 8 7 17 3 | 11 20 12 13 22 13 18 15 18 13 12
31 | 6 20 6 9 33 9 21 8 9 19 4 | 16 32 20 18 39 19 31 16 27 20 18
32 | 9 19 8 6 30 6 15 7 7 18 4 | 13 22 17 12 31 14 21 12 18 15 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 9 9 40 5 18 9 10 19 |T 19 29 23 21 37 20 28 21 25 23 21
WRMS | 8 19 9 9 40 5 17 8 7 18 |NE 17 26 21 19 35 17 25 18 23 20 18
MEDI | 8 18 8 8 33 5 18 8 7 17 |MD 16 26 20 18 37 17 26 17 24 20 17
Table 3.1519.2 GPS week: 1519 Day: 2 MJD: 54879.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 11 16 10 14 78 7 22 9 11 39 5 | 14 25 24 25 58 17 23 15 22 30 17
3E | 12 19 8 15 69 7 17 11 13 25 5 | 64 70 68 71 84 70 70 68 70 69 67
4 | 8 8 6 12 37 9 11 7 12 23 4 | 21 29 30 32 37 28 29 27 29 30 26
X5 | 12 16 8 10 97 11 --- 13 100 --- 5 | 10 15 14 12 80 11 --- 19 92 --- 11
6 | 15 20 9 11 29 5 18 10 12 26 5 | 77 85 87 85 88 85 83 88 90 81 84
7 | 10 26 6 11 30 7 19 8 11 23 5 | 15 31 22 21 34 20 27 23 26 18 19
8 | 9 13 7 8 24 6 12 10 7 13 3 | 20 25 25 20 29 27 27 27 28 26 24
9 | 7 16 9 7 44 6 10 5 11 12 3 | 12 20 15 16 34 12 15 12 19 15 13
10 | 8 13 7 12 31 7 10 6 10 19 3 | 13 22 21 24 27 17 20 16 16 20 16
11 | 8 22 6 6 87 5 19 9 9 16 4 | 21 32 24 22 57 24 29 27 26 22 22
12 | 7 22 10 12 32 5 22 10 11 16 4 | 18 30 18 22 41 18 30 15 20 18 17
13E | 7 16 5 9 35 6 19 8 10 13 3 | 14 24 15 17 34 13 23 17 17 19 14
14E | 8 20 9 11 36 4 19 7 12 15 4 | 18 23 24 24 41 20 28 19 29 20 20
15E | 8 23 9 12 29 6 25 8 13 20 5 | 14 26 21 22 25 17 28 16 18 23 17
16 | 10 23 7 9 21 5 22 10 10 17 4 | 17 30 25 16 34 19 30 19 18 19 19
17 | 10 20 8 8 45 8 17 6 17 15 4 | 15 29 22 17 48 18 25 16 21 23 16
18 | 7 22 5 9 33 5 22 5 8 21 4 | 13 29 18 18 34 14 28 16 22 20 16
19 | 9 25 7 10 29 4 21 9 10 9 4 | 19 32 24 19 49 19 29 18 21 22 19
20 | 7 21 8 9 63 6 21 8 9 25 4 | 14 28 16 18 52 14 26 16 22 16 14
21 | 8 17 6 7 68 7 19 9 8 23 4 | 18 24 19 21 46 22 21 22 25 23 19
22 | 6 21 5 8 50 4 20 5 7 19 4 | 13 29 20 20 39 16 27 19 21 23 17
23E | 8 18 5 12 33 7 22 10 7 14 4 | 15 24 19 20 32 14 21 15 17 19 15
24 | 7 13 6 8 40 5 12 7 8 15 3 | 22 29 31 33 23 26 32 28 32 31 28
25 | 9 17 5 5 28 8 14 8 12 13 3 | 12 21 17 14 27 17 20 17 22 16 14
26E | 9 19 7 9 48 6 16 10 19 12 4 | 13 28 20 18 55 17 28 12 27 14 15
27 | 11 14 5 9 20 5 11 6 6 10 3 | 13 25 18 18 28 17 20 16 20 16 15
28 | 9 19 7 9 34 4 17 7 12 15 4 | 14 27 18 18 39 17 25 16 21 14 15
29 | 8 24 7 8 35 5 18 7 8 19 4 | 18 30 23 18 41 20 26 22 24 24 20
30 | 8 17 7 7 34 5 13 7 7 16 3 | 11 21 15 14 23 13 18 17 17 14 13
31 | 8 21 8 9 29 6 20 11 10 18 4 | 17 28 20 21 38 21 29 20 26 21 19
32 | 8 23 8 9 29 5 16 6 9 18 4 | 9 20 15 14 27 11 18 10 22 15 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 7 10 43 6 18 8 11 19 |T 18 29 24 23 42 21 28 22 28 24 21
WRMS | 9 19 7 10 43 6 16 8 8 19 |NE 15 26 20 19 38 18 24 18 25 20 17
MEDI | 8 19 7 9 34 6 18 8 10 16 |MD 15 28 20 20 38 17 27 17 22 20 17
Table 3.1519.3 GPS week: 1519 Day: 3 MJD: 54880.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 9 18 9 11 41 4 18 8 16 36 5 | 14 24 27 23 42 18 28 18 24 30 18
3E | 12 21 12 18 41 6 14 10 10 24 5 | 71 72 66 67 64 67 70 65 68 73 67
4 | 9 13 9 10 34 5 11 9 13 21 4 | 30 31 37 38 44 29 33 33 30 35 31
X5 | 6 11 7 9 36 5 --- 11 9 15 4 | 11 15 16 14 51 11 --- 18 24 15 11
6E | 27 26 13 16 36 9 17 13 9 36 7 | 107 117 109 113 144 116 114 115 117 133 112
7 | 11 25 9 17 24 5 23 8 8 21 5 | 14 31 24 29 34 19 26 25 22 21 20
8 | 7 12 6 8 24 4 11 9 6 13 3 | 46 43 44 46 47 46 44 48 49 45 46
9 | 5 11 8 7 44 4 10 5 13 12 3 | 23 24 23 19 30 21 27 23 27 20 21
10 | 7 21 7 6 28 3 11 5 8 11 3 | 12 27 22 19 30 16 17 15 21 16 15
11 | 7 20 8 7 86 4 20 11 9 23 4 | 27 39 41 36 56 32 38 36 31 30 32
12 | 12 25 8 11 28 5 22 11 10 19 5 | 20 34 25 22 42 20 33 19 23 15 20
13E | 9 16 6 11 35 4 19 10 9 18 4 | 14 23 17 20 40 14 25 20 22 20 16
14E | 7 19 11 9 33 5 17 9 8 14 4 | 16 25 23 16 39 15 26 22 23 18 19
15E | 7 25 12 9 25 4 24 10 12 13 5 | 20 33 27 20 34 20 30 23 26 23 21
16 | 10 25 10 7 22 5 24 12 9 16 5 | 21 37 31 25 37 27 39 25 25 24 26
17 | 8 19 6 6 50 5 16 9 10 15 4 | 18 27 22 17 45 18 25 16 18 20 16
18 | 7 21 8 9 25 5 24 6 9 22 4 | 16 27 17 17 33 12 25 16 18 20 14
19 | 9 25 9 14 32 6 22 9 7 14 4 | 23 36 29 24 40 24 33 26 25 23 24
20 | 7 21 8 10 59 4 20 11 11 26 5 | 20 30 23 25 49 22 29 23 21 21 19
21 | 8 19 7 6 48 5 19 8 8 21 4 | 19 28 21 25 36 20 26 25 23 23 21
22 | 6 21 7 10 46 5 24 6 13 17 4 | 20 29 21 24 41 16 27 19 18 20 18
23E | 9 17 11 14 36 4 22 10 8 17 4 | 18 27 26 24 41 20 28 21 23 24 20
24 | 8 12 9 6 54 5 13 8 11 16 3 | 20 27 30 28 28 26 29 27 34 30 27
25 | 8 16 8 6 25 4 11 7 5 12 3 | 13 18 15 17 25 13 16 16 19 17 13
26E | 11 20 12 10 40 4 19 9 23 12 5 | 16 29 19 21 43 16 28 14 30 12 15
27 | 8 11 5 6 22 4 10 7 9 15 3 | 15 21 18 16 29 16 19 18 15 16 15
28 | 6 18 8 9 38 3 18 9 8 13 4 | 16 26 17 17 43 14 25 14 20 13 14
29 | 10 24 10 8 38 7 14 6 13 19 4 | 17 28 23 20 46 20 25 18 26 23 19
30 | 7 14 6 8 19 4 10 8 8 15 3 | 16 21 16 15 22 12 16 17 19 12 14
31 | 10 21 8 9 34 5 21 7 8 16 4 | 21 31 21 20 39 18 30 18 26 22 20
32 | 7 18 8 7 34 3 19 8 8 20 4 | 13 21 19 17 34 15 22 17 17 16 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 9 10 39 5 18 9 10 19 |T 23 32 28 26 42 24 31 26 28 26 24
WRMS | 8 20 9 10 37 4 17 7 8 20 |NE 19 28 24 23 37 20 27 22 24 22 20
MEDI | 8 19 8 9 35 5 18 9 9 16 |MD 18 28 23 21 40 19 27 20 23 21 19
Table 3.1519.4 GPS week: 1519 Day: 4 MJD: 54881.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 8 19 8 15 50 6 22 10 8 39 6 | 17 30 26 27 44 23 28 20 21 27 19
3E | 16 13 12 12 68 5 14 16 13 25 5 | 54 58 52 59 64 58 60 57 63 64 56
4 | 8 13 8 12 36 5 12 12 7 21 4 | 27 32 36 37 39 34 34 30 34 33 31
X5 | 8 13 7 7 26 4 --- 12 5 12 3 | 12 19 14 13 34 15 --- 17 23 17 12
6E | 18 21 16 12 80 9 20 18 10 27 6 | 92 96 97 96 91 95 96 89 89 90 92
7 | 8 23 8 13 23 4 20 14 11 21 5 | 19 35 21 25 37 23 28 27 26 20 20
8 | 6 12 7 7 19 5 9 8 8 15 3 | 45 51 46 48 50 46 47 47 40 46 45
9 | 6 11 10 8 33 3 9 9 13 11 3 | 16 22 20 19 23 20 22 17 26 17 18
10 | 7 12 9 9 41 3 11 7 10 12 3 | 17 22 23 24 31 22 23 20 25 20 19
11 | 8 16 7 5 75 4 21 12 10 21 4 | 23 33 28 26 46 28 34 30 27 25 25
12 | 10 24 9 9 22 4 22 12 6 17 5 | 16 31 22 17 32 19 29 18 16 18 16
13E | 8 18 8 7 23 4 19 12 9 13 4 | 14 31 19 16 32 20 27 22 22 20 17
14E | 8 19 11 8 27 5 19 10 7 13 4 | 16 28 25 19 40 21 28 20 19 21 19
15E | 11 22 13 10 37 5 28 23 12 22 6 | 22 31 26 28 38 26 31 39 26 42 25
16 | 9 22 10 7 24 6 25 14 8 18 5 | 17 34 23 17 41 21 36 21 21 25 20
17 | 8 27 9 8 44 5 20 15 12 22 5 | 20 37 29 22 56 26 33 21 22 30 22
18 | 9 21 8 9 31 5 23 8 9 26 5 | 14 32 20 21 36 19 30 19 25 27 19
19 | 9 27 11 10 38 5 22 10 10 15 5 | 22 38 28 18 42 23 34 21 18 23 20
20 | 9 19 12 9 62 6 22 16 10 25 5 | 20 34 23 22 46 25 31 25 21 21 19
21 | 6 20 11 7 66 5 19 9 8 24 4 | 17 24 23 21 43 20 24 22 23 22 18
22 | 8 19 10 8 49 5 21 9 13 18 4 | 16 34 27 24 39 22 33 21 29 26 23
23E | 8 17 8 10 28 4 24 11 7 13 4 | 15 27 20 18 30 20 26 21 22 19 17
24 | 8 13 9 6 44 4 13 10 10 9 3 | 22 24 29 27 29 25 26 28 28 26 24
25 | 6 12 8 5 32 4 12 10 9 15 3 | 18 26 18 18 26 20 22 19 21 23 17
26E | 11 20 9 8 49 5 18 17 23 14 5 | 15 32 23 16 50 22 30 17 34 16 17
27 | 8 12 6 7 30 4 9 9 8 18 3 | 17 28 20 23 28 21 28 20 21 25 19
28 | 6 19 10 8 37 4 18 10 9 12 4 | 16 32 22 19 44 22 29 18 20 21 18
29 | 10 23 13 7 34 4 16 10 8 15 4 | 19 28 28 19 40 19 25 19 24 21 20
30 | 6 13 7 6 20 4 12 11 7 15 3 | 16 23 18 17 25 20 20 20 20 19 16
31 | 7 18 10 6 33 6 20 11 10 18 4 | 20 34 22 22 44 22 30 24 21 23 20
32 | 11 18 11 7 38 5 19 12 10 18 4 | 16 28 21 19 25 22 26 21 21 17 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 10 9 43 5 19 12 10 19 |T 22 33 27 25 40 26 32 26 27 27 23
WRMS | 8 19 10 9 41 5 18 10 7 19 |NE 19 30 24 22 36 23 29 22 23 23 20
MEDI | 8 19 9 8 36 5 19 11 9 18 |MD 17 31 23 21 39 22 29 21 23 23 19
Table 3.1519.5 GPS week: 1519 Day: 5 MJD: 54882.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 7 16 5 13 60 5 21 12 9 39 5 | 15 24 21 23 43 18 27 19 20 29 18
3E | 19 17 10 16 58 8 15 12 12 22 5 | 101 98 101 103 99 99 98 100 98 97 100
4 | 7 13 7 10 35 5 13 14 9 23 4 | 28 33 33 33 30 32 31 34 35 38 32
5 | 6 14 9 6 20 4 8 15 7 9 3 | 13 17 11 11 26 10 13 15 16 13 11
6E | 14 17 12 27 73 12 17 21 10 28 7 | 90 92 91 99 93 95 95 91 91 96 92
7 | 8 23 8 13 32 4 21 19 11 24 5 | 14 30 16 18 37 15 24 26 21 15 16
8 | 8 11 9 7 41 9 10 12 11 24 4 | 80 85 82 83 61 82 83 84 80 84 81
9 | 6 11 9 6 26 4 9 9 9 14 3 | 17 21 17 15 26 15 19 14 19 15 16
10 | 6 15 7 6 57 4 9 10 6 16 3 | 14 16 20 19 33 16 18 17 19 15 17
11 | 8 17 8 7 69 5 22 14 12 21 4 | 16 29 26 22 46 19 28 24 24 20 20
12 | 9 24 11 10 26 4 19 15 11 22 5 | 16 29 15 16 32 15 24 13 21 16 16
13E | 9 16 8 10 32 4 21 14 13 13 4 | 13 23 18 15 34 14 23 18 19 18 14
14E | 7 21 10 9 33 5 19 11 9 13 4 | 15 24 19 17 40 17 23 14 16 16 16
15E | 7 25 12 9 35 3 27 12 10 10 5 | 31 38 34 31 41 29 32 33 32 33 30
16 | 9 22 9 12 28 4 25 14 9 18 5 | 18 33 25 19 38 21 34 18 24 24 22
17E | 10 22 10 8 51 5 20 14 7 27 5 | 19 33 28 23 46 25 31 24 25 28 23
18 | 8 21 8 13 35 4 25 12 10 28 5 | 17 29 19 21 34 16 28 16 20 25 18
19 | 7 25 11 11 47 4 23 10 8 14 5 | 17 28 17 16 38 15 28 13 17 16 15
20 | 8 20 10 10 78 5 24 16 9 25 5 | 15 27 20 18 52 16 26 17 21 16 15
21 | 9 18 10 15 56 6 22 9 8 22 5 | 19 20 22 28 26 21 23 23 25 21 20
22 | 9 18 7 10 49 5 22 10 7 18 4 | 19 30 23 22 36 20 31 20 24 24 21
23E | 9 15 9 7 35 3 25 11 8 12 4 | 19 23 25 21 28 18 25 20 23 21 19
24 | 6 12 8 8 35 6 9 12 11 10 3 | 20 20 25 26 21 21 19 25 26 20 22
25 | 7 13 8 7 28 3 11 12 9 15 3 | 10 19 15 12 28 13 17 15 19 16 12
26E | 9 19 12 12 48 4 18 10 20 20 5 | 13 25 20 14 45 15 27 13 28 20 14
27 | 7 9 7 5 28 4 8 7 7 16 3 | 16 22 18 18 29 18 21 19 21 22 17
28 | 7 18 9 9 45 4 15 12 8 13 4 | 13 25 15 16 44 14 22 16 19 16 15
29 | 21 22 11 11 33 7 18 12 11 19 5 | 52 67 64 69 68 62 65 64 63 62 62
30 | 9 14 9 7 18 4 11 14 4 19 4 | 16 21 17 16 21 15 20 19 19 14 16
31 | 11 20 8 11 34 5 20 12 8 18 4 | 13 29 18 19 43 17 26 15 21 18 17
32 | 7 17 10 4 37 4 16 13 10 20 4 | 11 19 18 12 33 12 18 12 21 12 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 9 11 44 5 18 13 10 20 |T 24 33 28 28 41 26 32 27 29 28 26
WRMS | 8 18 9 11 43 5 18 11 7 21 |NE 18 27 22 21 35 20 26 21 24 22 20
MEDI | 8 17 9 10 35 4 19 12 9 19 |MD 16 27 20 19 37 17 26 19 21 20 17
Table 3.1519.6 GPS week: 1519 Day: 6 MJD: 54883.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
2 | 9 17 9 12 49 4 22 11 8 42 6 | 17 26 23 28 45 19 26 22 20 35 18
3E | 22 16 12 14 60 9 15 13 11 23 6 | 88 91 93 94 99 93 94 90 93 95 92
4 | 8 14 11 10 39 6 9 11 12 22 4 | 32 36 40 43 29 38 34 39 35 43 36
5 | 6 13 7 10 28 3 9 10 8 16 3 | 13 18 14 15 29 13 11 17 16 16 12
6E | 14 17 16 15 78 4 15 18 13 25 6 | 84 92 84 82 90 85 88 85 86 90 84
7 | 8 24 9 16 37 4 20 18 9 22 5 | 19 31 20 26 38 19 28 30 25 17 20
8 | 8 12 6 7 24 3 11 11 8 16 3 | 36 37 32 36 40 35 34 38 34 30 33
9 | 7 11 9 8 36 5 10 12 7 15 3 | 18 25 20 21 32 20 21 20 20 19 18
10 | 8 22 10 8 59 4 10 8 10 15 4 | 18 24 24 26 41 20 20 23 20 21 19
11 | 10 17 7 5 82 5 20 10 6 19 4 | 29 36 32 31 54 29 33 34 34 24 30
12 | 10 20 10 13 39 4 22 13 9 18 5 | 18 30 20 20 45 20 32 23 20 21 19
13E | 7 19 7 13 33 4 23 10 10 11 4 | 15 29 21 18 33 17 28 21 20 18 17
14E | 8 17 7 7 43 4 19 11 12 14 4 | 20 27 24 17 46 20 27 22 21 20 20
15E | 13 22 9 8 39 5 27 12 9 20 5 | 50 59 53 56 48 54 60 62 52 61 54
16 | 11 30 12 10 36 4 27 16 11 25 6 | 21 39 22 21 40 22 38 23 23 28 23
17E | 7 24 9 17 37 6 20 9 10 18 5 | 19 29 24 27 34 20 26 24 25 30 21
18 | 8 20 8 14 44 5 21 9 9 39 5 | 19 28 19 23 38 17 27 20 26 29 19
19 | 11 25 16 9 30 4 18 10 12 13 5 | 26 37 32 24 36 26 34 23 25 30 26
20 | 9 22 13 10 65 3 22 18 11 27 6 | 22 30 23 21 54 21 31 21 25 21 20
21 | 7 19 11 11 86 6 19 6 12 23 5 | 24 25 27 31 60 23 24 29 24 30 24
22 | 10 18 6 12 52 4 19 9 10 26 5 | 21 29 23 27 37 19 29 22 26 25 22
23E | 10 22 10 10 31 4 24 9 10 15 5 | 19 28 25 18 31 17 26 20 19 18 18
24 | 8 12 10 10 38 4 11 9 13 11 4 | 27 28 33 38 21 29 28 34 29 28 30
25 | 8 14 7 7 32 3 11 10 9 18 3 | 14 22 17 15 32 15 18 17 19 22 14
26E | 10 19 9 11 42 6 18 10 21 25 5 | 16 27 22 17 43 18 28 17 28 23 16
27 | 7 9 5 5 26 5 11 7 9 22 3 | 18 22 20 18 33 17 21 22 20 22 18
28 | 6 21 9 8 35 4 18 9 9 12 4 | 19 30 20 17 46 16 27 22 20 20 18
29E | 14 21 13 17 33 4 18 10 12 16 5 | 39 52 56 58 56 48 53 52 49 49 49
30 | 8 13 7 9 28 4 11 11 8 22 4 | 18 22 17 15 26 16 18 19 21 18 16
31 | 10 23 7 10 43 5 22 11 14 18 5 | 23 32 22 25 43 23 29 21 24 22 21
32 | 10 20 10 6 43 3 20 12 12 21 5 | 14 21 18 15 28 15 22 15 25 15 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 10 11 46 5 18 11 11 21 |T 26 34 29 29 42 27 32 29 29 30 27
WRMS | 9 19 9 11 46 4 17 10 8 20 |NE 21 28 23 24 38 21 26 24 24 24 21
MEDI | 8 19 9 10 39 4 19 10 10 19 |MD 19 29 23 24 40 20 28 22 25 23 20
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 4.1519 GPS week: 1519 MJD: 54877.0-54883.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 |U 6 6 15 |U 13 23 45 |U 6 6 14 |
emr | emr 2966 | 8 9 24 | 17 25 53 | 8 7 16 |
esa | esa 2976 | 7 6 19 |U 13 21 44 | 6 6 16 |
gfz | gfz 2949 |U 7 7 20 |U 16 22 71 | 8 7 17 |
grg | grg 2976 | 9 9 24 |U 16 24 53 | 8 7 18 |
igr | igr 2955 | 7 6 19 | 15 22 49 | 6 6 14 |
igs | igs 2958 | 6 6 19 | 15 22 48 | 6 6 15 |
jpl | jpl 2909 |U 8 8 26 |U 14 21 50 |U 8 6 15 |
mit | mit 2976 |U 9 10 30 |U 16 22 51 |U 7 6 20 |
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 5.1519.0 GPS week: 1519 Day: 0 MJD: 54877.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 15 | 13 17 43 | 5 6 14 |
emr | emr 2972 | 7 10 24 | 15 21 50 | 7 7 18 |
esa | esa 2976 | 6 7 15 | 13 17 42 | 6 6 17 |
gfz | gfz 2953 | 7 8 17 | 14 13 60 | 8 7 20 |
grg | grg 2976 | 6 7 19 | 15 19 54 | 7 6 19 |
igr | igr 2955 | 6 6 18 | 14 18 49 | 5 6 16 |
igs | igs 2965 | 6 7 17 | 14 16 42 | 6 6 18 |
jpl | jpl 2972 | 7 9 20 | 13 16 43 | 6 6 16 |
mit | mit 2976 | 7 7 20 | 14 15 47 | 5 5 18 |
Table 5.1519.1 GPS week: 1519 Day: 1 MJD: 54878.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 13 | 21 18 68 | 6 7 14 |
emr | emr 2968 | 6 10 20 | 22 20 78 | 9 8 16 |
esa | esa 2976 | 6 6 15 | 19 19 70 | 7 7 15 |
gfz | gfz 2953 | 9 8 20 | 21 24 87 | 8 8 17 |
grg | grg 2976 | 6 6 18 | 20 19 70 | 10 10 18 |
igr | igr 2958 | 8 6 16 | 19 21 69 | 7 9 15 |
igs | igs 2969 | 5 6 13 | 21 18 70 | 6 7 14 |
jpl | jpl 2869 | 8 9 20 | 21 17 64 | 9 8 16 |
mit | mit 2976 | 8 5 17 | 21 19 71 | 6 8 17 |
Table 5.1519.2 GPS week: 1519 Day: 2 MJD: 54879.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 4 13 | 10 13 40 | 6 6 12 |
emr | emr 2968 | 8 9 19 | 12 13 51 | 9 7 18 |
esa | esa 2976 | 6 4 14 | 10 13 38 | ---- ---- ---- |
gfz | gfz 2948 | 6 7 14 | 12 11 71 | 10 9 16 |
grg | grg 2976 | 9 14 43 | 13 13 49 | 11 10 14 |
igr | igr 2928 | 6 4 12 | 11 12 42 | 6 6 13 |
igs | igs 2909 | 6 5 14 | 10 12 43 | 7 6 13 |
jpl | jpl 2870 | 7 8 19 | 10 12 46 | 8 6 15 |
mit | mit 2976 | 5 4 13 | 10 15 39 | ---- ---- ---- |
Table 5.1519.3 GPS week: 1519 Day: 3 MJD: 54880.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 7 17 | 10 16 36 | 7 8 17 |
emr | emr 2968 | 8 9 26 | 16 20 48 | 7 9 17 |
esa | esa 2976 | 8 7 19 | 10 16 39 | 6 7 16 |
gfz | gfz 2950 | 8 7 16 | 12 19 58 | 8 9 17 |
grg | grg 2976 | 8 8 23 | 10 26 54 | 9 11 21 |
igr | igr 2965 | 8 7 17 | 11 17 35 | 5 6 17 |
igs | igs 2968 | 7 7 20 | 10 16 37 | 6 7 18 |
jpl | jpl 2870 | 8 9 25 | 9 19 36 | 6 8 20 |
mit | mit 2976 | 8 8 25 | 11 15 44 | 9 10 27 |
Table 5.1519.4 GPS week: 1519 Day: 4 MJD: 54881.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 17 | 10 16 32 | 6 5 17 |
emr | emr 2964 | 8 10 22 | 15 17 40 | 6 6 15 |
esa | esa 2976 | 7 5 18 | 9 14 29 | 6 7 21 |
gfz | gfz 2949 | 6 6 17 | 17 17 61 | 8 6 17 |
grg | grg 2976 | 9 7 16 | 12 13 41 | 5 4 21 |
igr | igr 2962 | 7 5 17 | 14 17 42 | 6 4 16 |
igs | igs 2966 | 6 5 17 | 14 16 43 | 5 4 16 |
jpl | jpl 2865 | 8 8 22 | 12 14 44 | 6 5 16 |
mit | mit 2976 | 6 4 17 | 16 14 53 | 6 4 19 |
Table 5.1519.5 GPS week: 1519 Day: 5 MJD: 54882.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 4 19 | 14 65 50 | 8 7 12 |
emr | emr 2964 | 8 6 35 | 20 68 59 | 9 9 15 |
esa | esa 2976 | 9 6 37 | 13 58 52 | 7 6 12 |
gfz | gfz 2948 | 8 6 33 | 16 58 90 | 8 7 13 |
grg | grg 2976 | 10 8 20 | 22 64 58 | 9 6 17 |
igr | igr 2962 | 7 4 33 | 14 56 58 | 7 6 10 |
igs | igs 2964 | 7 4 32 | 16 59 55 | 7 7 10 |
jpl | jpl 2961 | 10 8 56 | 15 59 66 | 9 8 14 |
mit | mit 2976 | 21 35 101 | 16 57 59 | 10 7 25 |
Table 5.1519.6 GPS week: 1519 Day: 6 MJD: 54883.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 14 | 17 14 43 | 5 4 13 |
emr | emr 2964 | 9 8 21 | 20 16 49 | 7 5 14 |
esa | esa 2976 | 6 8 17 | 18 13 41 | 6 3 15 |
gfz | gfz 2944 | 8 7 20 | 22 15 70 | 7 6 18 |
grg | grg 2976 | 14 14 27 | 20 13 46 | 7 5 14 |
igr | igr 2956 | 7 7 17 | 21 14 47 | 6 4 14 |
igs | igs 2967 | 7 7 18 | 20 14 46 | 5 3 14 |
jpl | jpl 2960 | 8 6 22 | 19 13 48 | 9 5 12 |
mit | mit 2976 | 8 7 19 | 23 15 47 | 6 5 14 |
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 6.1519 GPS week: 1519 MJD: 54877.500-54883.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -5 -28 42 101 6 | 0 19
| 33 11 114 97 11 | 3
emr uuuuu | -42 -49 -90 87 -17 | 50 54
| 19 17 99 138 11 | 5
esa uuuuu | 20 -12 142 21 13 | -8 28
| 31 21 100 118 8 | 3
gfz uuuuu | 11 4 4 39 3 | 1 18
| 24 21 63 65 5 | 5
grg xxxxx | -37 -40 37 121 24 | 14 66
| 53 30 76 111 74 | 16
igr xxxxx | -4 -19 47 8 9 | -7 23
| 28 27 82 78 7 | 1
irf xxxxx | 10 6 -29 10 -5 | 6 17
| 7 9 32 17 5 | 3
jpl uuuuu | 21 5 43 185 -4 | -18 32
| 28 18 98 88 19 | 6
mit uuuuu | -19 18 -180 -76 -5 | 13 21
| 13 16 122 46 6 | 3
ngs uuuuu | -10 11 22 -113 0 | -2 19
| 37 45 74 68 9 | 2
sio uuxxu | 20 13 89 -43 -9 | 22 27
| 13 16 98 49 5 | 3
Table 7.1519.0 GPS week: 1519 Day: 0 MJD: 54877.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 34 -48 -33 -84 -4 | -4 14
emr uuuuu | -27 -50 -161 130 5 | 44 47
esa uuuuu | -6 -30 21 39 18 | -14 21
gfz uuuuu | 31 -35 47 -81 1 | -6 12
grg xxxxx | 5 -81 86 209 45 | -8 60
igr xxxxx | -1 -12 -39 105 2 | -8 21
irf xxxxx | 8 4 -19 21 3 | 1 7
jpl uuuuu | -9 7 107 321 -24 | -15 32
mit uuuuu | -39 29 -99 -98 4 | 8 12
ngs uuuuu | 31 52 60 -88 -13 | -5 16
sio uuxxu | 25 26 178 -102 -1 | 17 20
Table 7.1519.1 GPS week: 1519 Day: 1 MJD: 54878.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 24 -20 189 131 4 | -2 15
emr uuuuu | -21 -40 -175 105 -9 | 48 52
esa uuuuu | 20 -35 98 -12 24 | -11 23
gfz uuuuu | 36 3 52 138 7 | -4 15
grg xxxxx | 9 1 146 43 16 | 1 64
igr xxxxx | 4 -33 -17 -91 -1 | -8 21
irf xxxxx | 12 -10 -6 20 -1 | 4 13
jpl uuuuu | -1 -11 89 190 -22 | -14 31
mit uuuuu | -22 -9 -113 -34 -3 | 11 17
ngs uuuuu | -24 65 2 -213 -7 | -3 16
sio uuxxu | 9 3 132 -45 -7 | 19 23
Table 7.1519.2 GPS week: 1519 Day: 2 MJD: 54879.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 3 -30 44 221 -6 | 3 20
emr uuuuu | -23 -21 -185 284 -18 | 54 57
esa uuuuu | 8 -23 9 -84 13 | -6 28
gfz uuuuu | 35 26 84 35 9 | 2 19
grg xxxxx | -5 -76 28 166 89 | 8 66
igr xxxxx | 1 -51 107 -1 9 | -6 23
irf xxxxx | 16 7 22 34 -8 | 8 18
jpl uuuuu | 32 -16 94 222 -18 | -11 30
mit uuuuu | -25 15 -24 -23 -10 | 15 22
ngs uuuuu | -27 -3 -36 -126 6 | 0 18
sio uuxxu | 13 21 137 -91 -11 | 24 28
Table 7.1519.3 GPS week: 1519 Day: 3 MJD: 54880.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 2 -24 105 91 4 | 2 20
emr uuuuu | -60 -44 -116 216 -25 | 54 57
esa uuuuu | 56 -22 197 -158 12 | -6 28
gfz uuuuu | 7 -8 -68 34 7 | 4 18
grg xxxxx | -48 -25 -29 257 89 | 8 65
igr xxxxx | -34 -24 -56 -3 6 | -7 23
irf xxxxx | 16 0 -33 17 -2 | 8 18
jpl uuuuu | -1 14 -115 220 -6 | -14 32
mit uuuuu | -25 7 -128 -35 0 | 15 22
ngs uuuuu | -32 38 94 -2 -6 | -1 18
sio uuxxu | 26 -1 130 -57 -6 | 24 28
Table 7.1519.4 GPS week: 1519 Day: 4 MJD: 54881.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -42 -11 15 177 17 | 3 20
emr uuuuu | -44 -61 -79 -98 -24 | 54 57
esa uuuuu | 68 -4 211 200 5 | -4 29
gfz uuuuu | -13 -2 -15 50 1 | 7 19
grg xxxxx | -118 -19 29 -18 73 | 28 67
igr xxxxx | 32 -40 142 -90 21 | -6 23
irf xxxxx | 18 11 -70 -14 -9 | 10 19
jpl uuuuu | 36 -4 47 31 11 | -18 31
mit uuuuu | 2 18 -297 -86 -7 | 17 24
ngs uuuuu | -66 17 75 -158 5 | 0 19
sio uuxxu | 35 21 38 -7 -11 | 26 30
Table 7.1519.5 GPS week: 1519 Day: 5 MJD: 54882.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -1 -32 -155 97 5 | 1 20
emr uuuuu | -54 -54 16 -41 -21 | 49 55
esa uuuuu | -12 17 191 75 1 | -6 30
gfz uuuuu | -1 24 -83 26 2 | 5 20
grg xxxxx | -2 -50 82 191 -38 | 34 71
igr xxxxx | 18 -1 114 59 11 | -7 24
irf xxxxx | -1 20 -63 -3 -9 | 7 21
jpl uuuuu | 21 9 150 147 2 | -24 32
mit uuuuu | -6 40 -368 -112 -9 | 15 25
ngs uuuuu | 33 -60 69 -70 12 | -3 20
sio uuxxu | 1 29 -112 -41 -12 | 23 30
Table 7.1519.6 GPS week: 1519 Day: 6 MJD: 54883.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -55 -30 127 75 23 | -2 22
emr uuuuu | -68 -75 70 14 -24 | 43 52
esa uuuuu | 6 11 268 87 18 | -8 32
gfz uuuuu | -21 16 9 72 -5 | 2 22
grg xxxxx | -102 -29 -81 -4 -109 | 29 72
igr xxxxx | -48 29 80 74 14 | -9 25
irf xxxxx | 3 8 -31 -6 -8 | 4 24
jpl uuuuu | 70 37 -71 162 27 | -29 36
mit uuuuu | -19 24 -229 -144 -11 | 12 26
ngs uuuuu | 16 -32 -112 -134 6 | -6 22
sio uuxxu | 32 -12 118 40 -15 | 20 30
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