[IGSREPORT-18646] Wk 1584 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jun 3 04:37:39 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1584 (May 16, 2010 - May 22, 2010)
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 (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 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:
igs1584[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1584[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1584[0-6].cls IGS GPS clock combination summary report.
igs15847.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15847.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 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations. The SIO solution for
week 1582 has been manually excluded due to applying unremovable over-
constraints.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | DGAR SANT
0 | EMR | 8 9 27 8 9 27
0 | ESA | DGAR IRKJ KOKB
0 | GFZ | KOKB METS SUTH
0 | GRG | DGAR IRKJ SPT0
0 | JPL | 8 9 27 UNSA
0 | MIT | 8 9 8 9 NNOR NNOR
0 | NGS | 1
1 | ALL | 1 24 1
1 | COD | DGAR
1 | EMR | 8 9 8 9 WTZR WTZR
1 | ESA | 24 USNO DGAR IRKJ UNSA USNO
1 | GFZ | FAA1 LPGS MDVJ SUTH
1 | GRG | DGAR IRKJ ONSA
1 | JPL | 8 9 10 DAEJ
1 | MIT | 8 9 27 31 8 9 24 27 31 USNO SOFI USNO
2 | ALL | 1 1
2 | COD | DGAR
2 | EMR | 10 8 10 WTZR
2 | ESA | DGAR UNSA YAKT
2 | GFZ | MDVJ SUTH YAKT
2 | GRG | DGAR ONSA SANT YAKT
2 | JPL | 8 10
2 | MIT | 10 8 10 MDVJ MDVJ
3 | COD | DGAR NRIL NTUS
3 | EMR | 8 10 8 10 WTZR WTZR
3 | ESA | DGAR KOKB
3 | GFZ | KOKB METS NKLG SUTH
3 | GRG | DGAR ONSA
3 | JPL | 8 10 BOR1 UNSA
3 | MIT | 8 10 8 10 BOR1
4 | COD | ALIC ALIC DGAR
4 | EMR | 8 10 8 10
4 | ESA | DGAR
4 | GFZ | SUTH UNSA YAKT
4 | GRG | DGAR NRIL ONSA
4 | JPL | 8 10
4 | MIT | 3 8 10 32 3 8 10 32
5 | COD | DGAR
5 | EMR | 8 10 8 10 WTZR WTZR
5 | ESA | DGAR KOKB
5 | GFZ | KOKB METS SUTH UNSA
5 | GRG | DGAR ONSA
5 | JPL | 8 10
5 | MIT | 3 8 10 16 3 8 10 16 MAW1 ADE1 ALIC KOUC MAW1
6 | ALL | 1 1
6 | COD | WROC DGAR WROC
6 | EMR | 8 8 10 WTZR WTZR
6 | ESA | DGAR KOKB METS UNSA
6 | GFZ | KOKB MATE MDVJ METS SUTH
6 | GRG | DGAR ONSA ULAB
6 | JPL | 8 10
6 | MIT | 8 10 8 10
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 | GRG | 7
5 | GRG | 32
6. 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.
7. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. 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 | .3 .6 1.0 -9 -2 -6 -.09
EMR | 6.4 4.3 -1.4 51 8 -2 .30
ESA | 5.2 1.8 9.9 23 24 -91 .15
GFZ | -.1 1.9 .2 6 24 -87 .34
GRG | 7.8 2.8 8.2 -11 2 -9 .30
JPL | 8.6 -1.2 3.0 9 -45 -11 .33
MIT | 5.0 -1.4 5.1 -5 -7 -23 .06
NGS | 5.8 -1.2 6.6 -17 -66 10 .23
SIO | .9 3.6 -5.5 33 362 -578 .32
8. 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.
9. 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 IGN. 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.
10. 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 1.1584.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1584.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 2.1584.[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 3.1584.[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 5.1584.0-6).
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 1584 summary. (May 16, 2010 - May 22, 2010)
Table 1.1584.a GPS week: 1584 MJD: 55332.000-55338.000
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 244| 0 0 0 10 -27 -7 -.28 9 8 | -415 -443 15 64
| 0 0 1 13 10 25 .02 | 306 520
emr 91| 0 1 -3 -89 -33 25 .28 17 17 | -4659 844 16 108
| 1 1 1 16 24 8 .02 | 2817 723
esa 131| 0 0 0 -34 -21 -45 .30 7 7 | -311 -647 11 86
| 0 0 1 14 22 9 .04 | 941 1406
gfz 198| 0 0 1 10 -46 -2 -.15 11 11 | 122 -133 20 115
| 0 1 1 46 48 17 .03 | 245 887
grg 127| 1 0 11 6 -29 0 .51 19 17 | 1428490 -124 50 204
| 2 1 1 31 18 9 .03 | 3779680 677
igr n/a| -1 0 0 3 -23 8 -.02 5 5 | -6812 1774 16 65
| 0 0 0 24 27 17 .04 | 5149 1059
jpl 125| 0 1 -5 -8 81 54 .38 19 17 | -1841 649 16 105
| 0 1 1 11 14 45 .04 | 2644 925
mit 271| 0 -2 -3 10 -10 28 -.35 11 10 | -15679 -381 19 149
| 0 0 1 13 21 11 .06 | 622 1115
ngs 214| 0 0 0 51 90 10 -.20 9 7 | 43653 93691 2105 3652
| 0 1 0 21 22 18 .03 | 659220 780920
sio 269| -4 2 2 -45 -745 -547 -.19 22 21 | --- --- --- ---
| 0 1 2 15 29 19 .03 | --- ---
Table 1.1584.b GPS week : 1584 MJD: 55332.000-55338.000
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 | 16 25 21 18 21 15 17 |
2 | 5 5 5 5 5 5 5 |
3 | 3 4 5 3 3 3 4 |
4 | 3 3 3 3 4 3 3 |
5 | 5 5 4 5 5 5 5 |
6 | 4 4 4 4 4 3 4 |
7 | 4 4 4 4 4 5 6 |
8 | 5 4 5 5 5 7 6 |
9 | 6 5 6 6 5 5 4 |
10 | 6 6 5 6 5 5 5 |
11 | 4 4 4 4 4 4 4 |
12 | 5 6 5 5 5 5 5 |
13 | 6 6 5 4 5 5 5 |
14 | 5 5 5 4 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 4 5 5 5 |
17 | 4 4 3 4 4 4 4 |
18 | 6 6 5 4 4 5 5 |
19 | 4 4 4 4 4 4 4 |
20 | 6 4 5 5 5 5 5 |
21 | 4 5 5 4 4 5 5 |
22 | 5 5 4 4 5 5 5 |
23 | 5 5 4 4 4 5 5 |
24 | 3 4 4 4 4 3 4 |
26 | 4 3 3 3 3 3 3 |
27 | 7 7 5 4 4 4 4 |
28 | 5 4 5 5 5 5 5 |
29 | 3 4 4 4 4 4 5 |
30 | 4 4 3 4 4 4 4 |
31 | 6 5 5 4 5 5 5 |
32 | 4 4 5 5 5 0 --- |
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 2.1584.0 GPS week: 1584 Day: 0 MJD: 55332.000
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 244| 0 0 0 22 -27 18 -.26 9 8 | -458 -282 14 62
| -5 10 |
emr 91| 0 0 -1 -61 -60 15 .28 17 17 | -6974 -333 17 97
| -49 58 |
esa 131| -1 1 0 -10 -35 -46 .25 7 7 | 495 -1767 11 90
| -36 31 |
gfz 198| -1 0 3 -61 5 -20 -.15 11 11 | 325 -1769 22 109
| -80 -21 |
grg 128| -1 0 10 -17 -16 -6 .55 23 20 | -447 412 49 212
| 110 68 |
igr n/a| 0 0 0 42 2 -1 .02 6 5 | -11825 29 16 62
| -41 13 |
jpl 125| 0 1 -4 11 69 19 .41 19 16 | -3607 -730 16 109
| -16 -3 |
mit 271| 0 -2 -1 0 10 31 -.27 11 10 | -14501 -2121 20 123
| 25 9 |
ngs 214| 1 0 0 85 66 18 -.23 10 8 | 13837 -1878 1964 3553
| -106 13 |
sio 269| -3 4 1 -70 -718 -523 -.16 23 22 | --- --- --- ---
| -11 368 |
Table 2.1584.1 GPS week: 1584 Day: 1 MJD: 55333.000
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 244| 1 0 1 13 -15 -28 -.28 10 8 | 0 -1157 14 52
| 21 -28 |
emr 91| -1 0 -2 -82 -56 27 .28 18 18 | -7581 496 17 93
| -32 42 |
esa 131| 0 0 -1 -23 -56 -27 .36 9 9 | -1267 384 13 88
| 7 23 |
gfz 198| 0 0 0 -23 18 0 -.15 10 10 | 377 -516 21 110
| -60 -26 |
grg 128| 0 1 14 -6 -43 -3 .52 18 19 | 9999999 -585 51 211
| 42 74 |
igr n/a| -1 1 0 23 -33 -2 -.02 5 5 | -12101 1433 19 77
| -39 20 |
jpl 125| -1 -1 -3 -10 67 101 .38 20 18 | -4550 255 16 107
| 39 -79 |
mit 271| 0 -2 -3 25 -22 14 -.28 10 9 | -16311 812 19 146
| -2 10 |
ngs 214| 0 0 0 52 73 6 -.17 8 7 | 1272940 -999999 2139 3296
| 73 20 |
sio 269| -4 3 1 -42 -748 -543 -.15 22 21 | --- --- --- ---
| -34 378 |
Table 2.1584.2 GPS week: 1584 Day: 2 MJD: 55334.000
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 244| 0 0 0 -4 -24 23 -.30 11 9 | -509 -78 13 57
| 42 14 |
emr 91| 0 0 -4 -88 -57 12 .28 17 17 | -7027 1519 17 125
| -46 24 |
esa 131| 1 0 2 -43 -5 -46 .31 7 7 | 521 -979 11 89
| 4 -8 |
gfz 198| 0 0 0 60 -34 0 -.17 10 10 | 13 93 20 119
| -72 5 |
grg 128| 2 0 9 -21 -54 4 .49 27 18 | -100 65 52 195
| 99 45 |
igr n/a| -1 1 -1 14 -39 31 -.01 5 5 | -10787 2944 16 62
| -40 9 |
jpl 125| 0 2 -5 -14 75 30 .34 19 17 | -4436 1638 16 99
| -6 -67 |
mit 271| 0 -1 -4 23 -4 24 -.32 10 10 | -15430 -224 18 151
| 1 2 |
ngs 214| 0 -1 0 22 71 -3 -.18 9 8 | -443 -344 2175 3896
| 75 25 |
sio 269| -4 3 0 -35 -749 -556 -.19 24 23 | --- --- --- ---
| -36 376 |
Table 2.1584.3 GPS week: 1584 Day: 3 MJD: 55335.000
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 244| 0 0 1 0 -12 -37 -.26 7 6 | -542 -506 17 60
| 31 -28 |
emr 91| 0 2 -1 -114 -28 27 .27 19 18 | -5065 1637 17 113
| -17 13 |
esa 131| 0 0 0 -47 6 -47 .32 8 8 | -1310 1562 11 89
| 26 -3 |
gfz 198| 0 0 0 66 -74 14 -.10 8 8 | 373 -273 21 119
| -82 -38 |
grg 128| 3 0 9 -14 -20 11 .54 17 16 | -151 117 44 197
| 68 7 |
igr n/a| -1 0 -1 -8 14 25 .00 5 5 | -7533 3132 17 73
| -41 -23 |
jpl 125| 0 2 -5 -6 112 97 .43 19 16 | -2498 1864 17 130
| 2 -17 |
mit 271| 0 -2 -3 0 -34 45 -.35 11 10 | -16034 243 17 153
| 2 -4 |
ngs 214| 0 0 0 33 110 -8 -.23 10 7 | -517 -723 1875 3825
| 117 31 |
sio 269| -4 0 2 -44 -795 -532 -.20 21 21 | --- --- --- ---
| -49 384 |
Table 2.1584.4 GPS week: 1584 Day: 4 MJD: 55336.000
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 244| 0 0 0 35 -34 10 -.30 7 7 | -299 -607 15 69
| -1 28 |
emr 91| 1 1 -3 -100 -20 28 .25 17 17 | -3813 659 15 97
| -9 -1 |
esa 131| 0 0 0 -40 -14 -46 .25 6 6 | 436 -1141 11 88
| 21 15 |
gfz 198| 0 -2 0 -9 -40 17 -.18 11 11 | -120 1133 20 135
| -61 -4 |
grg 128| 2 0 12 33 -16 7 .49 16 15 | 436 -821 52 201
| 36 9 |
igr n/a| -1 0 0 -2 -29 16 -.09 4 4 | -4612 1694 15 65
| -11 -14 |
jpl 125| 0 2 -7 -2 77 17 .31 19 17 | -821 353 19 104
| 3 -14 |
mit 271| -1 -2 -4 16 20 38 -.42 12 11 | -15587 -1046 17 155
| -7 -13 |
ngs 214| -1 0 1 67 84 -6 -.17 12 8 | -999999 1649365 2472 3509
| 177 82 |
sio 269| -4 1 1 -48 -705 -541 -.24 23 21 | --- --- --- ---
| -47 362 |
Table 2.1584.5 GPS week: 1584 Day: 5 MJD: 55337.000
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 244| 0 0 -1 2 -38 -3 -.27 7 7 | -151 -886 15 68
| 52 -22 |
emr 91| 2 3 -5 -87 -13 30 .30 17 17 | -1974 474 18 123
| -46 -21 |
esa 131| 1 0 1 -28 -5 -60 .31 7 7 | 315 -2614 13 82
| -4 -8 |
gfz 198| -2 0 1 30 -78 0 -.17 12 12 | 112 122 20 106
| -53 -21 |
grg 128| 2 2 11 7 -44 0 .50 17 14 | 413 -940 50 220
| 52 35 |
igr n/a| 0 0 0 -16 -66 -17 -.05 4 4 | -1622 1215 18 66
| -53 -9 |
jpl 125| -1 2 -4 -12 84 5 .38 18 16 | 879 64 18 100
| -14 -88 |
mit 271| -1 -2 -3 18 -32 30 -.40 12 12 | -15630 -1185 20 157
| 7 -1 |
ngs 214| 0 -2 0 38 100 37 -.22 8 5 | 11738 2011 2154 3871
| 3 86 |
sio 269| -4 0 2 -19 -758 -550 -.19 20 20 | --- --- --- ---
| -50 378 |
Table 2.1584.6 GPS week: 1584 Day: 6 MJD: 55338.000
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 244| 0 -1 1 9 -36 -34 -.26 10 9 | -946 411 20 83
| 32 -37 |
emr 91| 0 4 -3 -93 2 37 .31 17 17 | -182 1456 14 113
| -60 -44 |
esa 131| 0 0 -1 -48 -42 -41 .32 8 8 | -1369 21 11 80
| 27 -2 |
gfz 198| -1 0 0 7 -119 -31 -.14 10 10 | -225 274 20 111
| -55 2 |
grg 128| 0 0 10 62 -6 -15 .48 18 16 | -718 881 52 197
| -11 -61 |
igr n/a| 0 0 0 -26 -14 5 -.03 5 5 | 796 1977 14 54
| -40 9 |
jpl 125| 0 1 -4 -25 85 108 .40 19 16 | 2146 1100 15 90
| 23 14 |
mit 271| 0 0 0 -9 -7 12 -.39 11 10 | -16263 851 22 161
| 6 5 |
ngs 214| 0 -1 0 59 127 31 -.20 8 7 | 8016 7407 1960 3619
| -27 0 |
sio 269| -2 1 7 -55 -741 -584 -.18 21 20 | --- --- --- ---
| -41 369 |
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 3.1584.0 GPS week: 1584 Day: 0 MJD: 55332.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 23 --- --- --- --- 28 --- 22 20 --- 15 | 31 --- --- --- --- 32 --- 28 17 --- 20
2 | 8 18 9 12 20 6 22 8 13 25 4 | 27 32 21 25 22 24 33 27 27 32 23
3 | 9 10 5 8 20 5 8 8 8 26 3 | 15 18 16 20 32 18 15 20 20 18 17
4 | 5 9 6 6 14 6 11 9 8 18 3 | 19 19 19 22 21 19 15 20 20 21 17
5E | 8 16 8 20 18 5 18 9 7 13 4 | 11 21 15 24 22 12 23 16 16 21 13
X6 | 7 9 6 --- 16 5 10 8 12 22 3 | 28 28 25 --- 35 29 23 30 33 25 27
7E | 9 13 6 12 24 4 17 8 9 14 4 | 20 23 20 21 29 17 26 18 18 21 18
8E | 11 20 4 12 23 5 17 9 8 18 4 | 21 30 19 26 29 18 28 22 21 25 20
9E | 9 20 6 9 30 7 19 19 13 17 5 | 88 91 92 89 98 92 96 94 89 99 91
10E | 20 19 8 13 40 6 16 11 9 17 6 | 75 75 71 71 73 73 74 72 72 73 72
11 | 5 14 7 7 19 9 18 12 10 20 4 | 19 25 21 22 37 20 27 20 16 26 18
12 | 10 19 9 12 24 4 24 15 8 21 5 | 14 27 20 20 30 15 29 17 14 18 16
X13 | 6 18 9 --- 24 5 22 12 12 23 5 | 15 27 20 --- 35 16 30 20 17 12 17
14 | 9 21 9 11 25 6 24 11 7 21 5 | 16 24 18 23 28 16 25 22 15 19 16
15 | 9 19 7 10 18 3 19 10 10 19 4 | 9 23 11 16 26 11 23 14 14 16 10
16 | 8 23 6 11 21 7 25 15 8 26 5 | 17 33 21 19 26 19 32 19 18 17 18
17 | 9 9 7 4 14 4 12 10 9 33 3 | 26 27 27 33 32 29 27 33 31 38 27
18E | 13 22 7 16 23 4 25 16 11 15 5 | 30 45 38 36 39 34 45 34 35 41 34
19 | 5 14 7 6 13 6 14 8 10 31 3 | 27 27 29 26 29 26 30 26 25 28 26
20E | 10 20 8 12 45 7 21 13 11 26 6 | 19 26 19 20 39 18 27 19 13 20 17
21 | 7 19 6 10 18 3 19 8 6 19 4 | 35 37 31 33 33 32 36 37 36 41 33
X22E | 8 21 6 11 --- 4 25 11 13 12 5 | 19 32 21 21 --- 20 28 20 20 24 19
23 | 6 18 8 9 20 5 25 13 11 32 4 | 15 27 20 18 30 16 29 17 14 21 16
24 | 7 12 5 8 19 3 10 10 7 16 3 | 12 19 15 17 18 13 16 18 15 16 12
26 | 8 13 9 7 11 5 11 12 11 21 3 | 14 17 12 14 16 11 16 13 16 17 11
27E | 9 24 8 24 26 9 20 19 14 33 6 | 86 84 84 89 87 81 85 80 81 82 82
28 | 8 17 7 9 24 5 20 8 12 25 4 | 20 30 22 26 34 23 31 25 23 31 22
29 | 7 10 4 6 21 5 15 7 8 --- 3 | 23 24 25 24 27 24 24 24 24 --- 23
30 | 8 14 5 9 20 6 13 7 6 30 3 | 20 23 24 23 32 20 23 21 17 26 21
31E | 9 17 9 13 27 9 23 16 12 27 5 | 34 36 33 31 38 32 38 38 35 46 33
32 | 9 18 7 10 18 3 21 7 10 20 4 | 28 28 26 26 214 27 26 30 24 21 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 7 11 23 6 19 11 10 23 |T 26 32 27 29 41 27 32 28 26 30 26
WRMS | 8 17 7 11 20 5 16 10 8 22 |NE 20 25 20 22 28 20 25 22 20 23 19
MEDI | 8 18 7 10 20 5 19 10 10 21 |MD 20 27 21 23 32 20 27 22 20 24 20
Table 3.1584.1 GPS week: 1584 Day: 1 MJD: 55333.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 23 --- --- --- --- 27 --- 25 --- --- 24 | 24 --- --- --- --- 25 --- 25 --- --- 22
2 | 6 20 8 10 20 4 25 8 8 24 4 | 23 28 12 21 18 19 29 19 20 28 16
3 | 10 7 8 7 15 6 10 7 10 23 3 | 15 15 18 16 25 16 18 15 22 15 15
4 | 5 11 8 6 10 4 12 8 11 18 3 | 14 15 12 13 14 13 17 15 19 18 12
5E | 9 18 7 16 15 3 22 8 9 12 4 | 12 23 21 18 24 13 27 14 16 17 14
X6 | 7 7 7 --- 13 5 11 7 8 17 3 | 28 26 28 --- 29 28 24 27 30 24 25
7E | 8 16 11 8 20 3 17 10 8 13 4 | 20 23 19 15 31 16 28 18 22 17 17
8E | 10 18 7 12 15 5 17 8 7 18 4 | 20 28 23 27 30 22 32 22 22 26 22
9E | 12 21 7 10 20 5 23 17 9 26 5 | 73 79 73 74 82 74 80 80 73 76 74
10E | 16 18 10 16 24 4 21 14 13 18 6 | 86 80 85 85 81 80 81 78 81 82 81
11 | 6 15 10 8 18 5 19 12 9 22 4 | 15 25 18 16 31 15 27 18 19 25 14
12 | 11 23 10 9 24 6 24 14 10 22 5 | 12 28 17 17 30 14 29 14 15 14 13
X13 | 6 19 14 --- 20 5 27 12 8 19 5 | 15 27 22 --- 33 15 32 18 18 14 16
14 | 8 21 7 8 21 5 26 8 7 20 4 | 13 27 20 21 27 16 27 15 19 12 16
15 | 8 22 9 8 17 6 22 9 9 19 4 | 12 29 16 14 24 11 26 14 14 16 12
16 | 8 24 9 8 19 3 27 12 9 27 5 | 13 28 17 16 22 14 30 13 17 15 13
17 | 10 11 8 9 14 6 13 8 7 28 3 | 17 19 19 24 18 19 18 23 18 31 17
18E | 15 21 6 19 17 4 26 7 5 14 5 | 19 35 26 33 32 25 34 26 30 27 24
19 | 6 13 12 8 14 6 16 8 10 30 4 | 18 22 31 20 19 22 27 19 25 20 20
20E | 6 22 8 8 14 5 20 13 6 15 4 | 24 38 30 32 32 26 32 34 29 37 28
21 | 14 22 8 10 25 6 20 14 7 22 5 | 65 64 60 61 49 63 58 64 62 70 60
22E | 10 18 7 14 21 4 27 10 5 11 5 | 18 29 25 29 23 19 29 19 23 22 21
23 | 6 21 12 7 18 6 30 10 7 32 5 | 19 32 27 22 29 21 35 23 24 27 21
24 | 7 11 12 7 16 4 12 13 8 17 4 | 15 17 27 14 18 14 19 16 18 18 15
26 | 10 7 6 5 11 2 12 11 7 22 3 | 27 25 25 25 21 23 25 24 28 28 24
27E | 20 26 7 19 24 7 21 16 8 30 6 | 48 51 45 46 52 45 53 37 42 48 43
28 | 8 19 7 6 20 8 19 7 9 23 4 | 16 30 17 16 28 20 27 18 24 23 16
29 | 7 12 5 8 19 3 14 5 9 --- 3 | 15 20 25 21 20 18 20 15 20 --- 18
30 | 8 12 8 6 16 3 11 9 7 28 3 | 26 30 28 24 33 23 30 24 27 28 26
31E | 9 21 8 8 18 6 20 10 8 20 4 | 24 35 26 28 32 26 33 29 29 35 26
32 | 11 18 10 9 18 5 19 6 5 19 4 | 40 32 26 30 214 35 25 30 25 27 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 9 10 18 5 20 10 8 22 |T 25 32 27 27 37 25 32 26 27 28 25
WRMS | 8 18 9 10 19 5 18 9 7 21 |NE 20 26 23 21 25 20 27 20 23 23 19
MEDI | 8 18 8 8 18 5 20 10 8 20 |MD 19 28 25 21 29 20 28 19 22 25 20
Table 3.1584.2 GPS week: 1584 Day: 2 MJD: 55334.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 19 --- --- --- --- 24 --- 21 --- --- 20 | 20 --- --- --- --- 19 --- 18 --- --- 16
2 | 6 22 7 12 20 4 21 10 9 23 4 | 23 32 14 22 18 21 27 22 22 29 18
3 | 8 11 7 9 38 4 10 8 9 23 4 | 13 15 15 15 36 11 12 15 15 13 13
4 | 7 10 5 7 13 6 11 8 8 19 3 | 14 17 18 15 14 16 16 16 14 23 13
5E | 8 16 6 12 14 4 22 8 9 14 4 | 12 25 18 17 23 18 27 17 20 24 16
X6 | 8 10 6 --- 24 5 12 8 8 17 4 | 24 25 26 --- 33 23 24 28 27 26 25
7E | 7 13 5 14 109 5 17 5 6 16 4 | 21 25 22 22 92 20 27 21 22 23 20
8E | 13 19 6 12 23 6 23 12 14 20 5 | 17 25 22 27 22 19 28 24 27 26 20
9E | 22 20 8 10 20 5 23 17 11 55 6 | 81 88 83 82 90 83 88 88 82 89 83
10E | 16 18 8 15 21 9 18 12 10 16 5 | 53 58 53 58 53 58 55 50 49 59 52
11 | 5 15 6 7 18 6 17 11 8 22 3 | 13 24 18 18 27 15 24 18 13 25 14
12 | 8 20 8 9 20 3 23 14 11 25 5 | 12 27 18 15 28 14 26 15 17 16 14
X13 | 6 18 9 --- 20 6 23 15 8 21 5 | 15 30 20 --- 32 19 32 20 17 17 17
14 | 5 20 10 7 15 3 23 9 9 20 4 | 12 27 17 16 26 15 24 15 16 13 14
15 | 8 19 8 9 19 7 23 11 10 22 4 | 8 25 14 16 23 14 26 13 14 17 11
16 | 9 19 6 8 19 4 24 11 8 24 4 | 15 28 17 15 22 15 29 13 13 15 14
17 | 9 11 5 6 12 6 12 8 10 29 3 | 23 20 23 20 19 21 21 22 19 28 20
18E | 13 17 6 11 19 4 23 13 6 14 4 | 21 28 22 26 29 20 30 26 28 24 22
19 | 8 14 7 8 15 4 14 12 7 30 3 | 22 22 25 22 21 20 24 20 22 21 21
20E | 7 25 8 10 17 5 18 11 8 22 4 | 19 31 22 20 23 20 29 23 24 26 20
21 | 16 19 8 8 16 3 23 6 9 18 4 | 36 36 28 32 31 30 36 33 34 34 30
22E | 9 14 6 7 17 3 24 10 8 12 4 | 17 27 20 16 24 17 27 19 22 20 18
23 | 6 18 8 9 17 5 22 10 8 33 4 | 18 30 22 22 25 20 29 22 15 27 19
24 | 8 14 3 7 12 3 11 10 10 17 3 | 9 16 12 12 15 11 15 14 17 17 10
26 | 7 7 5 7 11 4 13 8 8 19 3 | 13 16 13 11 17 11 17 15 14 20 12
27 | 15 15 6 12 12 4 16 10 9 18 4 | 64 81 72 72 75 71 76 68 70 70 70
28 | 12 17 9 9 23 4 22 10 10 23 5 | 15 28 21 19 32 19 29 15 22 21 17
29 | 7 10 7 10 21 4 14 7 6 --- 3 | 18 20 24 22 19 20 18 16 16 --- 18
30 | 8 12 6 5 14 3 13 10 8 28 3 | 19 21 20 19 28 18 23 21 19 27 18
31E | 8 20 8 11 19 7 20 9 9 20 4 | 21 33 25 22 26 22 30 24 21 27 22
32E | 18 18 9 11 15 7 18 9 8 33 4 | 39 40 35 37 157 45 45 41 39 43 46
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 7 10 27 5 19 10 9 24 |T 22 30 25 25 36 24 30 24 25 28 23
WRMS | 9 17 7 10 18 5 17 10 8 23 |NE 17 24 19 18 24 17 23 18 18 21 16
MEDI | 8 17 7 9 18 4 18 10 8 21 |MD 18 27 21 20 26 19 27 20 20 24 18
Table 3.1584.3 GPS week: 1584 Day: 3 MJD: 55335.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 13 --- --- --- --- 20 --- 23 --- --- 17 | 21 --- --- --- --- 23 --- 24 --- --- 20
2 | 7 20 9 10 18 2 22 10 9 23 4 | 23 27 20 22 20 21 30 23 24 28 20
3 | 6 11 4 6 14 5 9 10 13 22 3 | 12 17 14 13 16 13 11 15 20 13 12
4 | 5 14 7 5 9 5 11 10 5 20 3 | 13 19 13 11 14 14 15 19 16 23 13
5E | 6 20 10 13 17 3 18 12 13 16 4 | 13 26 19 23 25 18 25 14 20 18 16
X6 | 8 10 6 --- 14 6 12 10 11 16 4 | 31 34 36 --- 37 34 33 38 36 37 33
7E | 8 13 7 13 22 4 16 7 10 13 4 | 16 25 21 23 39 18 26 15 21 21 18
8E | 10 24 7 14 15 5 19 14 13 20 5 | 23 33 27 34 34 26 34 29 33 32 27
9 | 18 37 10 10 16 3 17 14 9 19 6 | 72 85 76 77 81 75 83 77 72 77 74
10E | 9 16 8 13 26 5 14 21 13 19 5 | 73 68 71 75 70 70 68 71 72 73 70
11 | 5 16 5 6 14 4 17 10 6 20 3 | 14 25 18 17 28 14 25 16 21 23 15
12 | 6 21 10 8 20 5 25 12 12 21 4 | 14 27 21 16 27 16 28 17 18 16 15
13 | 5 17 9 5 21 5 23 10 5 20 4 | 12 26 19 11 34 17 29 15 16 13 15
14 | 6 22 8 8 14 5 22 10 9 17 4 | 12 28 21 20 27 20 28 19 27 17 17
15 | 4 21 8 8 17 4 21 12 13 17 4 | 9 24 12 13 24 11 24 15 15 16 10
16 | 6 21 8 6 16 4 25 11 5 25 4 | 15 29 18 17 23 19 30 18 21 15 17
17 | 7 9 7 5 13 5 13 13 7 30 3 | 22 25 24 24 25 24 26 27 25 31 22
18E | 8 19 6 10 16 4 22 11 7 14 4 | 15 31 21 18 24 17 29 18 18 23 18
19 | 5 13 7 7 16 5 15 12 10 32 3 | 19 24 28 24 20 23 25 20 26 22 22
20E | 7 28 10 8 20 6 21 12 13 15 5 | 8 29 17 13 21 11 20 13 19 14 11
21 | 5 21 7 7 15 4 21 8 8 19 4 | 41 49 40 45 39 42 48 45 46 48 42
22E | 6 18 7 6 18 6 23 13 9 12 4 | 13 30 22 20 24 18 27 20 18 23 18
23 | 4 18 10 6 15 5 23 7 7 32 4 | 17 29 22 22 30 19 29 16 19 25 18
24 | 7 14 5 8 11 4 10 12 10 16 3 | 11 20 17 15 15 13 19 16 17 19 13
26 | 6 11 7 5 12 4 12 9 9 20 3 | 11 17 13 12 15 11 19 13 17 19 11
27 | 6 20 7 7 13 2 16 9 11 16 3 | 57 65 60 60 66 60 66 57 63 56 59
28 | 8 19 9 8 19 5 21 16 7 23 4 | 14 28 23 20 30 19 31 21 24 25 17
29 | 7 11 8 8 16 5 15 8 12 --- 3 | 19 23 23 19 21 20 24 17 22 --- 19
30 | 7 14 9 6 12 4 12 10 14 23 3 | 27 30 30 26 30 25 28 26 26 29 27
31E | 5 21 6 9 15 5 24 7 8 19 4 | 32 41 33 29 35 32 41 33 34 38 32
32E | 10 23 9 9 19 5 19 8 13 37 4 | 78 52 49 48 274 76 46 54 47 50 82
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 8 8 17 5 19 11 10 21 |T 24 32 27 26 38 26 32 26 28 29 25
WRMS | 6 18 8 8 16 5 16 10 7 21 |NE 17 26 21 19 25 19 26 21 22 23 18
MEDI | 6 18 7 8 16 5 18 10 9 20 |MD 16 28 21 20 27 19 28 19 21 23 18
Table 3.1584.4 GPS week: 1584 Day: 4 MJD: 55336.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 14 --- --- --- --- 19 --- 29 --- --- 20 | 26 --- --- --- --- 21 --- 17 --- --- 20
2 | 6 20 9 13 16 3 23 11 11 24 4 | 22 28 17 21 18 19 28 23 26 28 17
3 | 7 10 3 8 10 5 10 12 13 23 3 | 12 15 15 17 21 16 12 17 22 18 13
4 | 6 11 6 8 10 4 12 12 11 24 3 | 12 12 9 12 14 10 10 13 23 18 8
5E | 7 21 6 21 19 3 18 9 9 15 5 | 8 25 17 21 24 13 22 12 22 14 12
6 | 7 10 4 8 16 4 10 13 12 17 3 | 59 56 55 9 57 55 53 57 61 52 55
7E | 6 13 7 14 20 4 17 7 6 13 4 | 28 31 29 32 32 27 31 32 36 30 28
8E | 11 22 8 16 20 4 20 14 13 21 5 | 23 31 22 26 29 22 33 22 26 24 21
9 | 8 19 6 13 20 3 20 13 8 20 4 | 53 65 56 57 70 55 66 57 57 50 56
10E | 10 15 6 15 24 5 14 19 13 20 5 | 34 37 38 37 47 35 41 39 40 39 35
11 | 4 15 6 7 16 3 21 10 7 22 3 | 15 25 19 17 30 15 27 14 26 22 15
12 | 7 21 9 10 16 3 24 12 13 22 4 | 12 26 17 17 27 14 28 15 21 14 14
13 | 5 18 6 10 22 3 23 9 9 19 4 | 12 28 17 13 33 15 30 14 22 12 15
14 | 7 20 5 10 17 4 23 11 15 18 4 | 13 26 18 20 25 14 25 20 28 16 15
15 | 6 18 7 7 16 4 19 17 9 20 4 | 11 24 13 14 24 10 22 19 20 18 10
16 | 8 23 5 10 15 5 27 13 12 22 5 | 11 28 16 17 22 13 30 13 22 18 14
17 | 10 10 4 10 7 2 12 16 11 26 3 | 16 18 17 23 19 18 17 25 29 30 16
18E | 7 19 4 9 13 5 23 12 11 15 4 | 19 31 23 22 24 19 29 22 28 23 20
19 | 7 11 7 10 13 3 14 17 10 34 4 | 15 18 21 17 16 17 19 21 21 21 16
20E | 7 19 6 14 17 4 21 10 14 17 4 | 10 20 13 17 16 9 20 14 26 17 10
21 | 6 18 5 10 15 3 21 10 12 19 4 | 27 29 24 24 18 25 27 27 35 33 24
22E | 7 13 4 11 20 6 25 12 12 13 4 | 14 24 21 22 23 18 26 19 26 20 18
23 | 6 17 6 12 16 4 23 10 10 31 4 | 11 26 16 13 26 12 27 12 23 21 13
24 | 8 10 4 10 11 5 11 10 17 17 3 | 8 11 11 10 14 8 14 11 21 14 7
26 | 5 9 3 10 11 3 11 9 8 19 2 | 10 16 9 12 15 10 16 12 19 18 9
27 | 6 16 5 11 16 4 16 12 9 18 4 | 30 41 36 35 43 33 43 33 37 34 34
28 | 7 19 6 12 20 5 21 17 11 25 4 | 15 28 18 16 29 16 28 19 27 22 15
29 | 7 9 4 13 15 3 13 8 18 --- 4 | 14 19 23 24 20 19 19 15 27 --- 18
30 | 8 13 5 7 12 2 11 12 7 23 3 | 13 22 21 20 23 17 20 18 21 22 17
31E | 6 19 5 14 17 5 22 8 10 16 4 | 33 39 35 34 42 34 40 34 41 36 34
32E | 11 24 6 10 14 8 19 15 18 54 5 | 67 54 53 51 253 65 55 56 64 65 68
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 6 11 16 4 19 12 12 23 |T 21 28 23 22 35 21 28 23 29 25 21
WRMS | 7 17 6 11 15 4 17 11 8 21 |NE 16 23 18 16 23 17 23 19 26 22 16
MEDI | 7 17 6 10 16 4 19 12 11 20 |MD 15 26 18 20 24 17 27 19 26 22 16
Table 3.1584.5 GPS week: 1584 Day: 5 MJD: 55337.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 21 --- --- --- --- 25 --- 19 20 --- 14 | 24 --- --- --- --- 28 --- 20 29 --- 21
2 | 8 18 8 13 13 3 23 8 10 24 4 | 23 25 14 23 14 19 28 21 22 30 18
3 | 8 8 5 6 12 5 8 13 7 22 3 | 11 14 12 14 14 11 10 12 19 12 11
4 | 6 11 6 10 10 4 10 10 5 20 3 | 11 16 11 16 16 14 14 16 16 19 11
5E | 7 19 8 14 20 5 20 9 9 13 4 | 12 23 17 19 25 15 22 14 19 16 14
6 | 8 8 5 8 11 5 9 14 6 17 3 | 48 48 50 9 46 51 48 49 52 48 48
7E | 7 13 8 20 17 3 16 16 11 17 5 | 19 25 21 29 28 21 28 26 25 22 20
8E | 12 26 9 28 26 4 22 13 12 19 6 | 27 38 27 39 32 26 36 26 26 30 26
9 | 7 19 9 14 14 5 17 14 8 18 4 | 34 47 40 40 45 37 46 35 43 39 39
10E | 9 16 7 14 19 4 13 16 13 17 4 | 67 64 62 66 63 64 62 64 67 66 64
11 | 6 16 6 12 17 5 19 9 11 22 4 | 13 23 15 15 25 12 24 15 19 24 13
12 | 9 20 10 9 22 4 23 11 6 21 4 | 12 26 18 18 28 15 25 16 18 16 14
13 | 5 17 6 10 22 5 21 12 10 19 4 | 12 27 17 10 33 15 29 15 15 16 14
14 | 7 20 7 10 15 3 24 11 5 16 4 | 10 27 16 16 23 12 25 18 15 15 12
15 | 6 21 8 8 15 5 21 19 9 19 4 | 11 27 17 17 24 13 23 23 18 18 13
X16 | 8 23 8 11 18 7 --- 10 13 --- 5 | 13 27 16 17 22 13 --- 14 20 --- 13
17 | 11 9 6 13 11 4 12 13 9 25 4 | 15 21 18 24 21 19 20 23 26 30 18
18E | 8 15 7 13 15 2 24 13 7 13 4 | 15 24 19 20 24 15 27 18 22 20 17
19 | 6 9 8 8 14 6 14 17 6 34 3 | 13 19 22 17 14 15 17 19 17 18 15
20E | 7 21 8 12 17 5 22 14 12 20 5 | 11 23 17 16 16 12 21 15 19 19 12
21 | 8 21 9 9 16 3 21 10 6 21 4 | 34 40 33 31 31 34 38 35 35 38 32
22E | 7 17 8 8 22 5 26 12 6 11 4 | 12 26 20 13 23 13 26 18 19 20 15
23 | 6 19 6 9 19 5 23 13 7 30 4 | 15 30 19 17 28 18 30 18 19 27 17
24 | 8 10 4 8 13 2 12 10 8 15 3 | 10 17 16 11 16 13 18 14 16 17 11
26 | 4 9 5 8 10 3 11 7 5 20 2 | 8 13 11 10 14 10 15 12 11 20 8
27 | 7 18 9 12 14 4 15 13 7 17 4 | 39 49 42 43 47 41 47 41 43 43 41
28 | 6 18 9 11 17 5 23 11 9 24 4 | 15 30 18 17 33 17 30 18 19 23 17
29 | 7 12 9 10 18 4 16 8 4 --- 3 | 17 19 27 19 15 19 19 12 19 --- 17
30 | 7 14 9 6 12 2 12 10 7 20 3 | 15 20 18 15 23 16 21 19 18 23 15
31E | 8 22 7 10 18 5 21 10 8 16 4 | 36 43 39 40 41 40 44 37 41 35 38
X32E | 4 --- --- --- 2280 42 --- --- --- --- 0 | 47 --- --- --- 936 41 --- --- --- --- 46
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 7 12 17 4 18 12 8 20 |T 20 28 23 22 57 22 28 22 24 26 21
WRMS | 7 17 7 12 14 4 16 12 5 20 |NE 16 24 19 16 23 18 24 19 21 23 16
MEDI | 7 17 8 10 16 5 19 12 8 19 |MD 15 26 18 17 24 16 25 18 19 22 17
Table 3.1584.6 GPS week: 1584 Day: 6 MJD: 55338.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 28 --- --- --- --- 23 --- 23 19 --- 16 | 32 --- --- --- --- 23 --- 21 27 --- 24
2 | 8 21 9 13 18 3 22 8 8 26 4 | 26 31 17 22 17 22 32 26 24 37 21
3 | 11 10 6 10 13 5 10 7 8 24 3 | 15 19 16 18 25 15 14 17 19 16 15
4 | 8 12 4 8 11 5 10 8 6 19 3 | 14 15 9 13 17 10 11 14 11 17 9
5E | 8 20 8 12 20 4 23 7 10 12 4 | 10 24 19 20 26 16 25 14 16 17 14
6 | 10 7 7 9 9 5 11 10 8 18 3 | 42 44 46 8 51 45 40 44 43 46 43
7E | 21 14 11 13 19 6 16 15 10 17 5 | 26 35 32 32 36 28 35 37 30 35 29
8E | 16 27 7 11 23 5 19 11 11 20 5 | 46 46 38 44 48 40 46 45 44 41 41
9 | 9 19 8 10 13 4 16 12 8 18 4 | 52 58 50 49 56 49 58 52 46 52 50
10E | 11 13 6 10 25 5 12 12 8 19 4 | 70 76 73 78 73 73 70 70 73 72 72
11 | 8 14 7 6 16 6 19 11 9 21 4 | 17 24 18 19 31 16 25 20 20 30 17
12 | 9 20 10 9 23 6 22 12 11 21 5 | 20 28 25 20 29 17 31 22 23 21 21
13 | 6 17 11 11 25 4 21 12 9 19 5 | 14 26 20 14 32 15 29 20 12 18 15
14 | 8 23 8 10 14 5 27 10 7 17 4 | 17 29 23 23 31 19 30 26 20 19 21
15 | 7 19 9 8 16 5 20 17 9 20 4 | 14 26 14 16 23 14 24 23 17 19 14
16 | 9 23 8 12 17 5 26 13 5 20 5 | 16 30 16 16 24 14 30 20 16 18 15
17 | 11 9 7 7 9 3 11 12 6 25 3 | 23 27 25 24 29 22 25 27 26 33 23
18E | 10 17 10 13 23 3 23 10 7 14 5 | 17 31 24 24 25 21 29 24 19 25 20
19 | 8 9 8 11 15 6 14 15 6 34 4 | 25 26 27 25 27 24 29 24 25 23 25
20E | 7 19 11 11 16 5 21 14 8 23 4 | 15 21 15 15 18 11 21 17 16 21 12
21 | 9 18 11 11 16 3 22 11 7 20 4 | 33 34 29 34 34 29 37 35 34 33 30
22E | 9 18 7 11 27 5 26 10 8 13 5 | 11 24 19 17 25 14 23 19 16 18 14
23 | 4 17 11 12 23 4 22 17 9 30 5 | 18 27 21 19 25 16 28 19 15 28 15
24 | 10 10 5 8 11 3 11 10 9 16 3 | 14 16 17 15 22 10 17 14 17 23 13
26 | 5 10 8 8 12 3 12 8 6 20 3 | 12 17 16 12 19 12 20 16 17 22 14
27 | 9 19 9 7 11 4 15 11 8 15 4 | 54 59 54 53 61 54 59 55 52 54 54
28 | 9 18 9 10 18 5 20 9 6 24 4 | 16 31 21 20 33 16 30 17 17 21 17
29 | 19 12 4 12 17 7 15 9 7 --- 4 | 31 23 26 26 28 23 24 22 20 --- 23
30 | 10 17 6 6 13 3 13 8 8 23 3 | 23 28 26 25 31 21 27 24 25 28 24
31 | 6 26 7 11 23 6 20 13 11 14 5 | 74 76 74 73 78 74 77 72 76 73 73
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 8 10 18 5 19 11 8 21 |T 26 32 27 26 33 25 32 28 27 30 25
WRMS | 9 17 8 10 16 5 16 10 7 20 |NE 21 26 21 19 27 19 26 22 21 25 19
MEDI | 9 17 8 10 16 5 19 11 8 20 |MD 18 28 23 20 29 19 29 22 20 23 21
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 4.1584 GPS week: 1584 MJD: 55332.0-55338.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2930 |U 8 7 21 |U 7 9 29 |U 8 7 19 |
emr | emr 2842 | 10 9 26 |U 11 14 41 | 9 8 24 |
esa | esa 2852 | 20 14 28 |U 7 8 27 | 8 7 22 |
gfz | gfz 2743 |U 7 8 23 |U 7 9 32 |U 8 5 19 |
grg | grg 2852 | 8 9 26 |U 8 11 34 | 10 7 24 |
igr | igr 2882 | 7 8 22 | 7 8 27 | 8 7 20 |
igs | igs 2845 | 7 7 22 | 7 8 28 | 8 6 19 |
jpl | jpl 2826 |U 8 8 25 | 13 23 54 |U 9 8 21 |
mit | mit 2948 |U 7 7 22 |U 13 22 47 |U 9 7 21 |
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 5.1584.0 GPS week: 1584 Day: 0 MJD: 55332.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2960 | 10 12 26 | ---- ---- ---- | 6 4 17 |
emr | emr 2870 | 10 11 32 | ---- ---- ---- | 7 5 25 |
esa | esa 2880 | 9 12 28 | ---- ---- ---- | 6 5 20 |
gfz | gfz 2673 | 9 13 28 | ---- ---- ---- | 6 4 19 |
grg | grg 2784 | 10 13 29 | ---- ---- ---- | 8 7 21 |
igr | igr 2909 | 9 12 26 | ---- ---- ---- | 6 5 20 |
igs | igs 2887 | 9 11 28 | ---- ---- ---- | 7 5 18 |
jpl | jpl 2866 | 10 12 28 | ---- ---- ---- | 6 5 17 |
mit | mit 2976 | 9 11 29 | ---- ---- ---- | 7 6 20 |
Table 5.1584.1 GPS week: 1584 Day: 1 MJD: 55333.0
CENT| CLK EPO | BRUS | WILL |
----+----------+-------------------+-------------------+
cod | cod 2942 | 10 8 29 | 7 5 16 |
emr | emr 2870 | 11 8 35 | 8 7 28 |
esa | esa 2880 | 96 49 71 | 7 5 21 |
gfz | gfz 2673 | 9 8 28 | 7 5 15 |
igr | igr 2927 | 9 9 29 | 7 6 20 |
igs | igs 2848 | 9 8 30 | 7 5 18 |
jpl | jpl 2869 | 10 7 33 | 8 7 20 |
mit | mit 2976 | 11 10 32 | 12 6 29 |
Table 5.1584.2 GPS week: 1584 Day: 2 MJD: 55334.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2959 | 7 5 22 | 4 7 19 | 8 5 17 |
emr | emr 2872 | 11 6 26 | 13 14 44 | 10 8 23 |
esa | esa 2880 | 7 5 21 | 4 6 15 | 8 5 18 |
gfz | gfz 2672 | 7 6 23 | 5 8 26 | 7 4 18 |
grg | grg 2880 | 8 6 25 | 5 8 22 | 9 6 23 |
igr | igr 2936 | 7 5 23 | 4 6 16 | 8 5 16 |
igs | igs 2849 | 7 5 22 | 4 6 17 | 8 5 17 |
jpl | jpl 2870 | 8 5 23 | 10 17 41 | 10 8 22 |
mit | mit 2976 | 6 5 23 | 10 18 39 | 10 9 18 |
Table 5.1584.3 GPS week: 1584 Day: 3 MJD: 55335.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2960 | 6 6 14 | 6 11 17 | 8 7 14 |
emr | emr 2872 | 10 10 19 | 13 18 36 | 10 10 25 |
esa | esa 2880 | 6 6 16 | 6 8 18 | 9 9 19 |
gfz | gfz 2768 | 6 6 16 | 6 11 20 | 8 8 16 |
grg | grg 2880 | 8 8 24 | 8 14 30 | 11 9 23 |
igr | igr 2913 | 6 6 16 | 6 9 17 | 9 8 15 |
igs | igs 2898 | 6 6 15 | 6 9 19 | 8 8 15 |
jpl | jpl 2872 | 6 8 16 | 11 21 38 | 10 11 19 |
mit | mit 2976 | 6 6 15 | 12 21 36 | 8 7 15 |
Table 5.1584.4 GPS week: 1584 Day: 4 MJD: 55336.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2961 | 6 5 15 | 10 12 52 | 9 9 22 |
emr | emr 2868 | 9 7 23 | 11 18 54 | 11 8 21 |
esa | esa 2880 | 6 5 18 | 10 12 46 | 9 7 23 |
gfz | gfz 2868 | 6 5 16 | 10 13 53 | 8 7 20 |
grg | grg 2880 | 7 6 20 | 12 15 59 | 11 9 27 |
igr | igr 2905 | 6 5 17 | 11 12 48 | 10 8 22 |
igs | igs 2894 | 6 4 18 | 10 10 51 | 10 9 21 |
jpl | jpl 2867 | 7 5 22 | 12 24 61 | 10 7 21 |
mit | mit 2976 | 6 5 14 | 20 29 87 | 10 8 21 |
Table 5.1584.5 GPS week: 1584 Day: 5 MJD: 55337.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2878 | 6 6 22 | 9 8 33 | 11 10 27 |
emr | emr 2771 | 8 9 26 | 10 11 38 | 9 9 26 |
esa | esa 2784 | 6 10 25 | 8 7 31 | 9 10 29 |
gfz | gfz 2771 | 6 10 26 | 8 9 29 | 10 8 27 |
grg | grg 2880 | 10 14 34 | ---- ---- ---- | ---- ---- ---- |
igr | igr 2805 | 7 10 25 | 9 8 30 | 10 11 27 |
igs | igs 2775 | 6 9 25 | 8 7 29 | 9 8 26 |
jpl | jpl 2674 | 8 13 34 | 19 34 74 | 11 12 25 |
mit | mit 2880 | 6 10 24 | 12 24 33 | 7 7 20 |
Table 5.1584.6 GPS week: 1584 Day: 6 MJD: 55338.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2855 | 7 8 18 | 6 7 24 | 6 6 18 |
emr | emr 2776 | 9 10 20 | 9 8 31 | 8 6 22 |
esa | esa 2784 | 8 9 20 | 7 7 26 | 7 5 22 |
gfz | gfz 2776 | 7 8 21 | 8 5 31 | 7 3 20 |
grg | grg 2784 | 6 8 23 | 9 9 24 | 10 4 28 |
igr | igr 2782 | 8 9 21 | 7 6 22 | 7 4 21 |
igs | igs 2765 | 7 8 20 | 7 6 24 | 7 4 19 |
jpl | jpl 2769 | 8 8 24 | 14 19 57 | 8 5 21 |
mit | mit 2880 | 6 5 21 | 12 18 40 | 6 5 26 |
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 6.1584 GPS week: 1584 MJD: 55332.500-55338.500
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 | 15 -26 92 -7 -1 | -5 14
| 21 28 77 64 6 | 3
emr uuuuu | -4 36 -22 46 -3 | 36 38
| 31 13 85 96 5 | 2
esa uuuuu | -1 -8 36 93 1 | 5 14
| 11 15 90 86 7 | 3
gfz uuuuu | 21 65 94 -104 -2 | 8 16
| 19 22 81 77 5 | 4
grg uuuux | -19 -58 293 -5 -7 | 0 10
| 40 51 92 106 20 | 2
igr xxxxx | 5 37 5 -7 -1 | 4 12
| 16 17 58 55 5 | 2
irf xxxxx | 6 -1 -40 -9 -1 | 0 18
| 9 21 60 50 10 | 6
jpl uuuuu | 42 -6 17 108 -1 | 2 15
| 44 23 111 97 8 | 3
mit uuuuu | 5 -6 -134 -37 -2 | 3 21
| 12 30 114 49 15 | 6
ngs uuuuu | -31 -46 -124 -62 2 | 1 10
| 32 75 94 86 6 | 3
sio xxxxx | -368 37 -433 128 -4 | 39 42
| 14 32 115 79 10 | 5
Table 7.1584.0 GPS week: 1584 Day: 0 MJD: 55332.500
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 | 8 -33 128 45 -10 | -5 14
emr uuuuu | -40 11 -91 -63 -9 | 39 43
esa uuuuu | -13 -2 -20 103 -12 | 4 14
gfz uuuuu | 39 42 -19 -74 -6 | 7 15
grg uuuux | -50 -148 452 176 -24 | 3 10
igr xxxxx | 5 3 -79 -88 6 | 2 11
irf xxxxx | 18 -38 -29 23 15 | -7 21
jpl uuuuu | 21 -22 -139 12 9 | 1 17
mit uuuuu | 9 -63 -8 -12 21 | -5 22
ngs uuuuu | 5 68 28 -99 2 | -1 11
sio xxxxx | -350 -27 -425 216 12 | 34 39
Table 7.1584.1 GPS week: 1584 Day: 1 MJD: 55333.500
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 | 37 -12 141 -19 -7 | -7 14
emr uuuuu | -33 41 -65 -51 -4 | 36 38
esa uuuuu | -14 2 -26 254 1 | 2 12
gfz uuuuu | 35 69 137 -49 -10 | 5 14
grg uuuux | -65 -33 323 -59 -9 | 0 11
igr xxxxx | -11 48 81 -10 -2 | 2 11
irf xxxxx | 9 9 17 79 6 | -6 21
jpl uuuuu | 88 -30 77 -25 4 | -1 15
mit uuuuu | -1 11 -9 47 11 | -4 23
ngs uuuuu | -11 -64 -201 -187 1 | -2 9
sio xxxxx | -369 43 -344 212 5 | 34 38
Table 7.1584.2 GPS week: 1584 Day: 2 MJD: 55334.500
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 | -10 -38 18 79 -3 | -9 15
emr uuuuu | -20 50 -60 84 -2 | 34 36
esa uuuuu | 12 0 -63 110 2 | 2 12
gfz uuuuu | -1 76 160 -78 4 | 3 13
grg uuuux | -41 -95 368 -42 -25 | -1 12
igr xxxxx | -5 44 60 -30 1 | 1 11
irf xxxxx | 4 4 -62 12 3 | -5 21
jpl uuuuu | 71 10 137 44 -2 | -1 15
mit uuuuu | 2 3 -163 -14 3 | -2 23
ngs uuuuu | -21 -71 -89 -107 -3 | -2 9
sio xxxxx | -372 40 -495 165 1 | 35 39
Table 7.1584.3 GPS week: 1584 Day: 3 MJD: 55335.500
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 -18 -37 -61 0 | -7 15
emr uuuuu | -17 30 163 -49 2 | 34 35
esa uuuuu | -1 -13 127 79 4 | 4 14
gfz uuuuu | 34 95 -18 11 5 | 7 16
grg uuuux | -11 -55 248 -23 -9 | -4 9
igr xxxxx | 19 54 -37 97 -1 | 3 13
irf xxxxx | -4 13 -122 -45 -2 | -1 21
jpl uuuuu | 13 11 -94 232 7 | 0 16
mit uuuuu | 0 11 -255 -98 -2 | 2 23
ngs uuuuu | -35 -104 -90 -103 -7 | 0 10
sio xxxxx | -388 62 -563 38 -4 | 38 42
Table 7.1584.4 GPS week: 1584 Day: 4 MJD: 55336.500
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 | -14 26 124 45 1 | -4 13
emr uuuuu | 15 34 -48 134 -9 | 37 38
esa uuuuu | -1 4 91 13 -7 | 7 15
gfz uuuuu | 18 86 114 -194 -5 | 10 18
grg uuuux | 5 -11 231 -43 25 | -2 8
igr xxxxx | 28 36 -38 5 -9 | 5 14
irf xxxxx | 14 25 -108 -22 -12 | 4 17
jpl uuuuu | 28 22 -46 182 -15 | 5 14
mit uuuuu | 27 32 -295 -47 -14 | 8 20
ngs uuuuu | -68 -152 -122 35 13 | 2 9
sio xxxxx | -348 72 -569 160 -15 | 43 45
Table 7.1584.5 GPS week: 1584 Day: 5 MJD: 55337.500
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 | 30 -60 86 -90 4 | -2 12
emr uuuuu | 29 38 -21 147 4 | 37 39
esa uuuuu | 16 -4 -24 110 8 | 8 15
gfz uuuuu | 29 45 182 -171 -1 | 12 17
grg uuuux | -27 -60 202 -141 14 | -1 11
igr xxxxx | 17 45 35 -16 2 | 6 13
irf xxxxx | 8 -8 -13 -62 -11 | 6 15
jpl uuuuu | 96 6 139 161 -1 | 5 14
mit uuuuu | 9 -15 -143 -79 -17 | 9 18
ngs uuuuu | -78 -11 -123 -26 3 | 5 10
sio xxxxx | -370 42 -371 49 -14 | 44 46
Table 7.1584.6 GPS week: 1584 Day: 6 MJD: 55338.500
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 | 30 -45 186 -50 6 | -1 11
emr uuuuu | 37 47 -35 118 0 | 38 39
esa uuuuu | -5 -40 167 -15 8 | 10 16
gfz uuuuu | -9 42 103 -174 0 | 13 18
grg uuuux | 54 -2 225 98 -22 | 2 11
igr xxxxx | -16 27 13 -5 -1 | 7 13
irf xxxxx | -7 -13 34 -50 -8 | 7 14
jpl uuuuu | -21 -36 42 147 -5 | 6 14
mit uuuuu | -12 -19 -62 -59 -16 | 10 17
ngs uuuuu | -7 14 -270 51 5 | 6 10
sio xxxxx | -376 28 -266 55 -12 | 44 46
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