[IGSREPORT-17482] Wk 1533 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 11 05:06:21 PDT 2009
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IGS Electronic Report 11 Jun 05:06:43 PDT 2009 Message Number 17482
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1533 (May 24, 2009 - May 30, 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:
igs1533[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1533[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1533[0-6].cls IGS GPS clock combination summary report.
igs15337.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15337.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. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | ALL | 1 5 1 5
0 | COD | 9 25 27
0 | EMR | MIZU WTZR
0 | ESA | 8 9 25 27 UNSA
0 | GFZ | 31
0 | GRG | NLIB ZECK
0 | MIT | 8 HOB2
1 | COD | 8 9 25 27 8 9 25 27 MDO1 RCMN
1 | EMR | WTZR MIZU WTZR
1 | ESA | 8 9 25 27 METS
1 | GFZ | CHUR IRKT
1 | GRG | HOFN NLIB NOVM POTS REYK SCUB WUHN
1 | JPL | MDO1
1 | MIT | 5 5
1 | NGS | 1
2 | ALL | 1 1
2 | COD | 8 8 9 25 27 RCMN
2 | EMR | 5 MIZU WTZR
2 | ESA | 8 9 25 27 KERG METS
2 | GFZ | CHUR PARC
2 | GRG | NLIB
2 | JPL | 27
2 | MIT | KERG SANT
3 | COD | 8 9 25 27 5 8 9 25 27 RCMN
3 | EMR | WTZR
3 | ESA | 8 9 25 27
3 | GFZ | 31 CHUR HARB MIZU UNSA
3 | GRG | NLIB
3 | JPL | MBAR ZWE2
3 | MIT | KHAJ
3 | NGS | 1
4 | ALL | 1 1
4 | COD | 8 9 25 27 8 9 25 27 RCMN YAR2
4 | EMR | KERG MIZU WTZR
4 | ESA | 8 9 25 27 MIZU
4 | GFZ | 18 CHUR GOLD HARB SUWN
4 | GRG | NLIB
4 | JPL | HARB
4 | MIT | 5 5 USN3 ALIC GODE HOB2 MDVJ PIE1 USN3
5 | COD | 8 9 10 25 27 8 9 10 25 27
5 | ESA | 8 9 10 25 27 ALIC
5 | GFZ | CHUR RCMN
5 | GRG | NLIB
5 | JPL | 10
5 | MIT | 5 15 5 15
5 | NGS | 1
6 | ALL | 1 5 1 5
6 | COD | 8 9 10 27 8 9 10 27
6 | EMR | MIZU
6 | ESA | 8 9 10 27 MIZU
6 | GFZ | 25 ANKR BAN2 CHUR GOLD THTI
6 | GRG | NLIB
6 | JPL | 25
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
2 | GFZ | ~08:30 | ~ 0.05 ns
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 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 | .4 .3 .4 -19 -17 4 .05
EMR | -.3 -15.6 -3.1 63 12 93 .16
ESA | .1 -4.9 12.0 -14 -6 43 -.03
GFZ | .0 .2 1.7 4 -6 6 -.20
GRG | 6.1 -2.1 -1.4 -15 -15 6 .06
JPL | 2.2 -4.7 -3.0 26 -2 -5 .40
MIT | 2.8 -9.3 8.6 -43 23 -32 .01
NGS | 7.5 -11.3 3.3 -137 -106 55 .29
SIO | -5.1 -3.6 5.0 -56 119 -18 .45
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 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.
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 1.1533.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1533.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 2.1533.[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 3.1533.[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 5.1533.0-6).
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 1533 summary. (May 24, 2009 - May 30, 2009)
Table 1.1533.a GPS week: 1533 MJD: 54975.000-54981.000
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 235| 1 0 0 -22 2 -15 -.21 10 8 | -415 -191 15 66
| 0 0 1 13 17 19 .03 | 428 643
emr 85| -3 1 0 -127 -20 -18 .33 19 19 | 3432 -68 20 96
| 0 2 1 21 10 22 .05 | 1194 1557
esa 142| 0 0 1 -54 -6 -4 .34 10 9 | -434 -277 19 106
| 1 1 0 34 39 22 .02 | 1509 2432
gfz 190| 0 0 1 -64 -5 166 -.04 12 12 | -142871 12312 23 108
| 0 1 1 19 20 77 .05 | 377957 33840
grg 107| 2 -1 -9 -49 45 -89 .98 39 36 | -998 1277 91 1382
| 1 1 3 21 27 35 .05 | 2753 3887
igr n/a| 0 0 0 -42 -16 -46 .06 6 5 | 17730 90 21 65
| 0 0 0 8 17 25 .02 | 1197 1424
jpl 119| 0 1 -4 -106 -19 -1 .44 19 17 | 1292 -104 18 89
| 1 0 1 8 10 25 .04 | 1088 1483
mit 276| 0 -1 0 19 -54 -63 -.27 11 10 | -14352 -604 21 141
| 0 1 2 34 37 16 .03 | 833 612
ngs 216| 0 0 -1 225 189 -33 -.32 11 9 | 36813 3577 2092 3687
| 0 1 0 52 62 15 .05 | 437110 579173
sio 257| -3 0 5 73 -255 -41 .22 21 20 | --- --- --- ---
| 0 1 1 17 43 16 .03 | --- ---
Table 1.1533.b GPS week : 1533 MJD: 54975.000-54981.000
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 | 14 12 14 14 12 17 17 |
2 | 6 6 5 5 6 5 5 |
3 | 4 4 4 3 4 4 3 |
4 | 4 4 4 4 4 4 5 |
5 | 10 13 12 11 8 9 9 |
6 | 4 4 4 3 3 3 3 |
7 | 6 5 5 5 4 4 5 |
8 | 6 5 5 5 5 5 5 |
9 | 7 6 6 5 5 5 5 |
10 | 5 4 5 5 6 5 6 |
11 | 4 5 5 5 4 4 4 |
12 | 5 5 6 5 5 5 5 |
13 | 5 5 5 11 5 5 5 |
14 | 5 6 6 5 5 5 5 |
15 | 6 5 5 5 5 5 5 |
16 | 6 6 6 5 5 5 6 |
17 | 5 5 5 4 4 4 5 |
18 | 6 5 6 5 5 6 5 |
19 | 5 5 5 4 5 5 4 |
20 | 5 5 6 4 5 5 5 |
21 | 5 5 5 5 5 5 5 |
22 | 5 5 5 4 5 4 5 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 6 6 6 6 6 7 7 |
26 | 5 4 4 4 4 3 4 |
27 | 5 4 5 4 4 4 5 |
28 | 5 5 5 5 5 5 5 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 5 4 4 |
31 | 9 5 5 5 5 6 6 |
32 | 5 6 5 5 5 6 6 |
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 2.1533.0 GPS week: 1533 Day: 0 MJD: 54975.000
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 235| 2 0 -1 -23 4 2 -.19 9 8 | -826 521 14 57
| 22 32 |
emr 85| -2 -2 0 -156 -14 1 .35 19 19 | 2635 -622 20 97
| -14 -37 |
esa 142| -1 0 0 -16 -74 35 .34 10 10 | -599 3 17 103
| -29 51 |
gfz 190| 0 -1 2 -44 18 71 -.09 12 12 | 20 -2497 22 152
| -10 12 |
grg 107| 4 -1 -10 -27 36 -131 1.00 40 37 | -175 -65 90 211
| 57 -16 |
igr n/a| 0 0 0 -54 0 -88 .05 5 6 | 16607 -567 22 59
| -38 -31 |
jpl 119| 1 2 -2 -113 -23 22 .48 19 17 | 604 -613 20 104
| 38 44 |
mit 276| 0 0 4 56 -75 -57 -.26 16 13 | -14712 -223 21 127
| 15 28 |
ngs 216| 0 1 -2 144 227 -46 -.36 10 8 | 9578 5784 2409 4035
| 115 -20 |
sio 257| -2 2 2 78 -271 -36 .25 24 22 | --- --- --- ---
| -72 91 |
Table 2.1533.1 GPS week: 1533 Day: 1 MJD: 54976.000
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 235| 1 -1 0 -8 31 -8 -.25 9 9 | -854 505 20 62
| 0 -42 |
emr 85| -3 -1 -1 -150 -16 -4 .33 19 19 | 1831 2574 22 71
| -4 -13 |
esa 142| -1 0 0 -24 -26 12 .32 8 8 | -3114 4169 20 101
| -1 82 |
gfz 190| 0 0 0 -71 -27 102 -.06 11 11 | -454 554 24 96
| -4 2 |
grg 107| 0 -1 -14 -27 88 -139 .89 40 36 | -7227 10066 97 8347
| 18 -76 |
igr n/a| 0 0 -1 -34 9 -21 .06 5 5 | 15785 2656 19 55
| 7 4 |
jpl 119| 1 0 -3 -97 -18 31 .48 18 16 | -366 2553 21 83
| 14 25 |
mit 276| 1 0 1 45 -113 -75 -.33 12 11 | -14663 -887 20 90
| 4 30 |
ngs 216| 1 0 -2 187 301 -34 -.38 12 10 | 10550 4892 2071 3583
| 111 -83 |
sio 257| -3 2 5 79 -299 -64 .18 21 20 | --- --- --- ---
| -75 82 |
Table 2.1533.2 GPS week: 1533 Day: 2 MJD: 54977.000
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 235| 1 0 0 -32 7 -5 -.24 9 8 | -310 -186 15 57
| 20 55 |
emr 85| -4 -1 -2 -140 -27 -36 .33 18 18 | 4040 1549 20 89
| -15 7 |
esa 142| 1 1 0 -48 -23 -14 .35 10 10 | 281 -1591 19 106
| 8 38 |
gfz 190| 0 1 2 -34 8 274 .05 14 14 | 81 -142 25 89
| 15 23 |
grg 107| 3 0 -12 -37 62 -71 .95 41 39 | 23 237 96 226
| 61 71 |
igr n/a| 0 0 -1 -33 -38 -17 .04 5 5 | 17981 1421 24 72
| -4 39 |
jpl 119| 0 2 -4 -96 -38 -31 .40 19 17 | 1949 1230 19 77
| -21 82 |
mit 276| 1 -2 0 49 -2 -77 -.29 10 10 | -13228 -1283 23 106
| 8 4 |
ngs 216| 0 0 0 193 153 -48 -.34 12 10 | 7599 9918 1991 3895
| 87 117 |
sio 257| -3 0 5 94 -194 -59 .20 22 19 | --- --- --- ---
| -63 74 |
Table 2.1533.3 GPS week: 1533 Day: 3 MJD: 54978.000
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 235| 1 0 -1 -43 18 -27 -.18 9 8 | 258 -1214 13 71
| 22 -14 |
emr 85| -3 0 0 -115 -8 5 .40 20 20 | 5230 -1456 19 90
| -79 4 |
esa 142| 0 1 1 -123 -2 -17 .37 15 10 | 253 -1570 19 109
| 45 24 |
gfz 190| 0 0 3 -79 -3 176 -.02 12 12 | 382 -589 23 128
| 26 -3 |
grg 107| 2 0 -11 -47 53 -63 1.05 40 37 | 422 -630 92 222
| 61 32 |
igr n/a| 0 0 0 -36 -16 -41 .10 5 5 | 19150 -1006 22 67
| 14 28 |
jpl 119| 0 2 -3 -103 -13 12 .48 18 16 | 2760 -1354 17 73
| -26 21 |
mit 276| 0 -1 0 35 -79 -48 -.25 9 8 | -13544 -660 20 132
| 17 9 |
ngs 216| 0 0 0 227 214 -29 -.28 9 9 | 12712 3015 2096 4064
| 19 19 |
sio 257| -3 0 5 91 -313 -21 .25 20 20 | --- --- --- ---
| -87 104 |
Table 2.1533.4 GPS week: 1533 Day: 4 MJD: 54979.000
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 235| 2 0 0 -29 -11 7 -.22 10 9 | -140 -551 13 66
| 11 33 |
emr 85| -3 2 -2 -103 -14 -17 .35 19 19 | 4511 -1628 19 107
| -51 11 |
esa 142| 1 0 1 -52 45 -33 .35 8 8 | 57 -202 20 116
| 42 38 |
gfz 190| 0 -1 2 -55 -7 124 -.04 12 12 | 46 -133 20 85
| -5 33 |
grg 107| 3 -1 -4 -80 21 -41 .96 37 34 | 6 -148 91 213
| 40 60 |
igr n/a| 0 0 0 -51 -38 -33 .07 6 6 | 18923 -1278 18 57
| 29 45 |
jpl 119| -1 0 -4 -102 -20 3 .43 19 17 | 2289 -1611 16 77
| 20 37 |
mit 276| 0 -2 0 -13 -50 -41 -.27 9 8 | -14193 -809 22 166
| 29 -14 |
ngs 216| 0 0 -1 279 154 -2 -.29 11 9 | -772901 1075328 2091 3329
| -73 82 |
sio 257| -3 1 7 44 -257 -36 .22 21 20 | --- --- --- ---
| -60 94 |
Table 2.1533.5 GPS week: 1533 Day: 5 MJD: 54980.000
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 235| 2 0 2 -17 -13 -44 -.20 11 9 | -217 -605 16 80
| 3 53 |
emr 85| -3 3 1 -109 -22 -18 .29 20 20 | 2851 -453 21 95
| -67 25 |
esa 142| 1 2 1 -64 9 -1 .34 10 9 | 1590 -3592 21 109
| 50 6 |
gfz 190| 0 0 0 -88 12 154 .00 10 10 | -177 -31 23 104
| 5 15 |
grg 107| 1 -5 -9 -50 53 -96 1.04 39 36 | -168 -1 94 236
| 46 73 |
igr n/a| 0 0 0 -43 -13 -58 .08 6 6 | 17699 -192 21 71
| 12 -14 |
jpl 119| 0 1 -6 -115 -6 -8 .43 20 18 | 886 -396 21 120
| 0 46 |
mit 276| 0 -3 0 -19 -37 -57 -.26 9 8 | -15767 581 22 181
| 19 -3 |
ngs 216| -1 -1 0 266 122 -40 -.24 10 8 | 310851 -163039 2021 3557
| -15 111 |
sio 257| -4 -1 6 69 -214 -24 .19 20 20 | --- --- --- ---
| -77 84 |
Table 2.1533.6 GPS week: 1533 Day: 6 MJD: 54981.000
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 235| 0 0 0 -6 -15 -29 -.21 11 9 | -816 188 16 75
| 15 48 |
emr 85| -4 5 0 -118 -41 -56 .26 19 19 | 2927 -441 19 124
| -44 27 |
esa 142| 2 0 1 -50 26 -14 .31 8 7 | -1506 841 19 102
| 45 -15 |
gfz 190| 0 0 2 -77 -35 262 -.11 12 12 | -999999 89025 24 106
| -6 24 |
grg 107| 1 -2 -6 -73 5 -82 .99 38 33 | 130 -519 78 221
| 96 98 |
igr n/a| 0 0 0 -41 -16 -63 .04 6 6 | 17970 -399 22 74
| 33 14 |
jpl 119| 0 0 -4 -114 -12 -37 .37 18 16 | 924 -540 16 95
| 18 30 |
mit 276| -1 -2 -2 -16 -21 -86 -.24 12 11 | -14360 -948 20 189
| 15 -24 |
ngs 216| 0 -2 0 278 149 -35 -.34 11 9 | 679303 -910858 1968 3346
| -15 167 |
sio 257| -4 0 3 58 -238 -50 .24 22 23 | --- --- --- ---
| -74 79 |
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 3.1533.0 GPS week: 1533 Day: 0 MJD: 54975.000
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 | 15 --- --- --- 2938 43 --- 15 25 --- 13 | 26 --- --- --- 17 29 --- 22 34 --- 26
2 | 8 24 12 17 41 6 27 18 13 23 6 | 21 32 22 16 34 19 34 20 23 22 19
3M | 8 11 7 10 30 8 8 8 7 22 3 | 22 28 26 26 19 23 25 25 30 28 24
4 | 7 16 8 10 30 5 13 12 9 25 4 | 18 24 18 20 21 20 21 17 20 30 16
X5 | 10 24 --- --- --- 15 --- 21 18 --- 10 | 17 29 --- --- --- 26 --- 18 32 --- 20
6M | 7 12 8 11 39 7 9 7 10 23 3 | 24 27 28 28 22 23 24 26 30 29 24
7E | 9 19 13 15 28 5 21 18 7 17 5 | 16 27 23 22 30 17 23 22 24 26 19
8E | 16 20 13 8 65 6 22 17 12 22 6 | 28 36 31 31 59 30 42 35 38 30 31
9E | 14 22 12 16 55 6 20 19 14 43 7 | 64 73 62 57 70 59 73 52 60 52 59
10 | 8 17 13 10 21 5 14 11 14 20 4 | 37 40 40 34 42 35 39 38 41 35 37
11 | 7 20 9 7 44 4 17 11 9 15 4 | 19 31 24 22 51 21 32 18 24 20 20
12 | 10 24 7 12 27 6 23 12 11 21 5 | 20 40 31 25 38 25 37 22 27 26 24
13 | 8 20 10 13 34 5 21 16 9 19 5 | 13 31 23 22 43 17 28 21 20 18 17
14 | 8 19 10 14 40 6 21 11 7 22 5 | 20 33 31 31 42 27 30 27 29 25 25
15 | 8 21 12 11 29 5 22 11 16 19 5 | 20 28 20 20 40 17 28 19 24 18 18
16 | 10 21 11 10 42 5 23 14 10 24 5 | 21 36 27 20 36 21 35 22 24 29 22
17 | 6 17 8 13 36 7 14 13 13 25 4 | 29 31 28 32 32 30 28 28 31 19 26
18 | 11 28 15 17 38 4 22 13 9 21 6 | 35 44 36 41 54 34 38 38 40 38 35
19M | 7 13 7 13 36 8 13 9 7 30 4 | 31 34 38 39 45 34 37 32 33 44 33
20E | 8 16 8 16 41 5 17 14 11 20 5 | 24 29 30 27 44 23 27 28 22 31 24
21M | 6 20 11 11 28 5 20 12 7 30 5 | 23 35 22 19 33 21 33 19 26 30 20
22 | 6 19 10 10 36 7 22 11 7 12 4 | 26 33 34 32 39 25 29 33 30 27 29
23 | 6 20 10 14 29 4 24 13 8 23 5 | 17 30 20 22 40 16 31 17 19 17 16
24M | 8 13 10 7 25 4 11 18 8 20 4 | 27 32 30 31 39 29 32 21 25 27 24
25E | 8 19 13 13 60 5 17 18 12 28 5 | 64 64 66 65 73 63 66 70 65 73 64
26 | 14 21 7 9 35 3 14 15 12 18 5 | 67 72 72 67 48 72 72 75 72 75 70
27E | 11 21 9 11 78 4 18 12 10 13 4 | 40 46 40 37 53 35 47 33 39 33 36
28 | 7 20 8 11 36 5 19 13 8 24 4 | 19 28 18 22 37 20 27 19 24 24 18
29M | 5 9 8 9 41 6 13 14 9 37 4 | 27 31 30 30 48 28 32 27 32 41 28
30 | 6 10 10 8 13 3 11 11 11 22 4 | 23 24 25 25 28 21 25 26 27 30 23
31E | 11 17 10 18 36 8 23 52 13 31 8 | 25 34 29 25 33 24 32 55 32 53 28
32 | 9 18 6 11 35 4 15 18 11 22 4 | 27 35 30 26 34 25 31 29 22 40 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 10 12 40 5 19 16 10 24 |T 27 36 31 30 40 28 35 29 31 33 28
WRMS | 8 19 10 12 37 6 17 13 8 22 |NE 23 33 27 26 36 25 32 24 28 27 24
MEDI | 8 19 10 11 36 5 18 13 10 22 |MD 24 32 29 26 39 25 32 26 29 29 24
Table 3.1533.1 GPS week: 1533 Day: 1 MJD: 54976.000
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 --- --- --- --- 27 --- 15 23 --- 12 | 27 --- --- --- --- 22 --- 20 31 --- 25
2 | 9 21 9 17 32 4 23 11 11 22 5 | 21 33 24 20 34 22 32 20 25 25 20
3 | 9 12 5 7 39 5 8 7 9 18 3 | 23 23 24 21 23 23 22 24 31 17 22
4 | 9 16 9 10 26 7 12 9 9 21 4 | 15 21 18 15 18 15 21 12 19 26 13
X5 | 14 30 --- --- --- 35 --- 16 28 --- 12 | 16 23 --- --- --- 36 --- 18 32 --- 18
6 | 8 13 7 9 38 5 9 7 8 15 3 | 19 20 21 18 26 19 20 18 26 17 18
7E | 7 17 8 10 29 5 18 14 13 17 4 | 15 22 18 17 28 17 22 15 27 21 15
8E | 14 22 8 10 69 8 20 11 13 20 5 | 26 37 33 29 54 30 42 31 37 28 30
9E | 13 22 9 11 61 6 19 13 11 32 5 | 48 61 54 47 82 49 61 46 50 42 49
10 | 8 16 7 11 34 5 13 10 12 16 4 | 33 40 36 33 33 36 41 33 40 37 33
11 | 9 18 7 8 52 6 15 15 10 14 4 | 21 35 29 23 44 25 34 24 28 19 24
12 | 9 23 8 13 28 6 23 12 12 20 5 | 18 34 28 24 38 22 34 20 27 22 22
13 | 8 21 9 13 42 3 24 12 11 16 5 | 16 33 22 20 46 20 34 15 22 16 17
14 | 11 20 10 13 40 6 23 11 14 21 5 | 17 29 26 26 40 23 31 18 29 18 21
15 | 9 20 8 8 37 2 22 12 16 14 5 | 18 30 22 18 40 20 31 16 27 20 18
16 | 10 22 11 8 39 6 23 12 14 24 5 | 21 35 29 23 38 26 36 20 29 21 23
17 | 5 13 7 9 26 5 12 12 16 24 4 | 14 20 17 18 24 16 18 18 23 18 14
18 | 11 26 8 14 30 4 21 9 7 21 5 | 37 44 36 38 46 36 42 36 44 39 37
19 | 8 16 6 11 24 10 11 8 9 29 4 | 27 30 35 33 33 32 32 27 36 30 30
20E | 7 16 7 15 46 5 21 13 13 11 4 | 18 30 26 20 46 21 29 21 23 24 20
21 | 9 19 8 9 30 4 17 9 7 28 4 | 19 31 24 16 34 19 28 17 29 26 19
22 | 7 24 7 14 39 4 25 8 10 11 5 | 16 32 20 24 32 19 26 17 23 16 17
23 | 6 20 9 14 42 5 23 12 10 19 5 | 17 34 24 20 44 21 34 18 22 16 19
24 | 10 17 5 6 20 3 13 13 9 17 4 | 22 29 26 21 36 22 31 17 31 25 22
25E | 10 25 9 17 54 5 16 15 14 28 5 | 49 51 50 47 54 47 50 49 58 53 49
26 | 14 14 8 7 37 5 10 8 12 14 4 | 37 39 38 36 48 36 39 32 43 37 35
27E | 11 18 7 10 58 4 16 10 11 13 4 | 33 41 40 35 49 36 43 36 43 36 36
28 | 6 21 8 10 38 6 17 12 12 24 4 | 16 31 23 21 36 21 27 16 27 24 18
29 | 8 9 9 12 42 5 12 11 10 37 5 | 19 22 26 20 44 22 23 17 29 37 21
30 | 6 11 8 9 23 5 11 8 11 20 3 | 19 23 29 21 26 23 24 21 30 28 22
31E | 8 18 7 10 22 6 22 19 10 16 5 | 22 30 23 24 39 23 30 24 27 26 22
32 | 14 20 7 12 48 5 19 14 13 23 5 | 20 35 27 26 37 23 34 25 28 38 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 8 11 40 5 18 12 12 21 |T 23 32 28 25 39 25 32 23 31 26 24
WRMS | 9 19 8 11 36 5 16 11 10 20 |NE 19 30 25 21 36 23 30 19 27 22 20
MEDI | 9 19 8 10 38 5 17 12 11 20 |MD 19 31 26 21 38 22 31 20 29 25 22
Table 3.1533.2 GPS week: 1533 Day: 2 MJD: 54977.000
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 --- --- --- --- 25 --- 16 27 --- 13 | 18 --- --- --- --- 27 --- 15 36 --- 19
2 | 5 22 11 15 36 4 23 9 9 21 5 | 18 31 15 16 27 17 27 18 15 24 15
3 | 6 12 8 15 42 4 11 8 12 17 4 | 18 22 21 23 20 17 21 20 25 20 19
4 | 7 13 7 9 32 5 12 6 11 19 3 | 14 22 21 18 22 18 17 16 17 24 16
X5 | 19 33 --- --- --- 35 --- 13 16 --- 11 | 18 25 --- --- --- 24 --- 15 18 --- 15
6 | 7 12 8 17 42 3 11 5 10 14 4 | 17 21 21 29 21 17 19 19 25 20 19
7E | 8 16 10 12 24 6 18 12 9 12 4 | 16 27 21 18 27 19 22 20 26 24 19
8E | 15 20 7 12 62 7 19 10 10 25 5 | 27 39 31 30 52 29 42 31 30 30 28
9E | 10 20 11 21 47 5 22 12 11 31 6 | 45 58 50 48 72 46 58 42 47 40 46
10 | 14 16 9 9 32 3 13 8 12 16 4 | 42 50 49 44 45 46 50 46 48 50 45
11 | 6 20 12 9 77 4 17 14 18 17 5 | 15 33 22 23 57 19 27 21 23 19 19
12 | 11 25 9 11 33 6 23 14 17 23 5 | 16 34 25 20 38 19 32 18 23 21 18
13 | 7 20 5 11 39 5 23 11 8 16 4 | 14 34 23 17 44 18 31 19 17 21 18
14 | 8 21 13 14 29 5 25 9 18 21 5 | 16 30 24 23 36 19 26 17 23 17 17
15 | 7 22 12 9 32 5 24 11 13 18 5 | 13 30 21 14 35 17 28 14 21 19 15
16 | 7 20 14 15 29 5 24 8 13 21 5 | 15 31 20 22 37 19 31 16 20 20 17
17 | 6 15 7 14 21 7 13 9 11 27 4 | 22 27 21 26 22 22 23 25 20 20 21
18E | 11 21 10 15 43 5 23 8 9 28 5 | 53 60 59 59 70 53 59 58 62 59 57
19 | 5 15 7 16 40 4 14 7 11 29 4 | 19 24 28 32 45 22 26 22 24 28 23
20E | 9 14 9 25 52 6 19 13 10 18 5 | 16 31 29 38 56 21 26 20 17 25 21
21 | 9 20 10 12 30 3 21 7 8 27 5 | 18 31 19 15 32 17 29 18 25 28 18
22E | 7 17 10 16 51 4 24 9 12 13 5 | 36 45 43 43 39 38 41 39 41 37 38
23 | 8 21 8 12 46 7 26 13 9 19 5 | 16 37 24 18 43 21 32 23 20 24 21
24 | 8 18 8 9 21 3 14 10 10 16 4 | 14 27 21 18 35 16 24 15 23 24 16
25E | 14 21 10 9 59 6 19 14 11 26 5 | 42 38 44 40 51 43 43 48 52 48 43
26 | 6 15 10 9 25 5 13 10 12 17 4 | 26 32 28 28 41 27 33 28 30 34 27
27E | 9 16 9 16 58 8 18 12 13 19 5 | 16 29 21 25 32 21 30 21 27 26 20
28 | 7 19 12 13 30 7 17 9 11 21 4 | 17 28 21 24 34 19 27 19 21 21 18
29 | 5 11 7 16 40 4 13 7 11 37 4 | 17 22 23 21 39 20 22 17 24 34 19
30 | 9 11 9 10 24 5 12 8 13 23 4 | 19 23 22 21 31 18 23 20 22 27 19
31E | 8 17 10 13 24 7 20 12 11 17 4 | 16 25 19 18 30 17 25 25 28 28 18
32 | 11 21 9 11 44 5 17 14 12 22 5 | 24 36 30 24 40 24 32 26 28 38 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 10 14 41 5 19 10 12 22 |T 21 32 27 26 39 24 30 24 27 28 23
WRMS | 8 18 10 14 39 5 17 10 10 19 |NE 17 29 22 20 35 20 27 18 21 22 18
MEDI | 8 19 9 12 36 5 18 10 11 19 |MD 17 31 22 23 37 19 27 20 24 24 19
Table 3.1533.3 GPS week: 1533 Day: 3 MJD: 54978.000
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 | 17 --- --- --- --- 26 --- 11 26 --- 13 | 21 --- --- --- --- 32 --- 21 27 --- 20
2 | 7 22 9 15 40 4 20 7 8 20 4 | 23 30 25 22 34 20 30 22 22 26 21
3 | 7 12 7 9 36 3 7 6 9 17 3 | 22 24 23 29 21 22 21 24 24 24 23
4 | 5 17 8 8 37 5 11 8 7 16 3 | 23 27 27 22 29 21 22 25 23 31 22
X5 | 22 26 --- --- --- 22 --- 11 16 --- 10 | 19 26 --- --- --- 33 --- 22 30 --- 21
6 | 6 11 7 8 32 5 9 6 9 13 3 | 23 24 27 30 22 26 23 25 24 26 24
7E | 8 17 17 11 27 7 15 9 8 13 4 | 25 28 23 24 35 27 28 24 29 29 24
8E | 13 20 9 10 63 7 20 13 8 19 5 | 31 41 33 32 51 33 46 37 36 34 33
9E | 9 19 8 15 60 4 20 8 11 24 5 | 57 64 58 56 80 56 68 51 51 50 55
10E | 12 24 9 15 36 4 15 7 5 11 4 | 50 53 52 48 57 50 53 50 52 42 49
11 | 8 22 8 9 63 4 15 12 9 15 4 | 24 38 29 28 55 25 31 26 26 25 25
12 | 9 24 9 11 25 4 25 9 12 21 5 | 20 34 29 24 38 23 34 21 24 23 22
13 | 15 22 67 15 51 10 24 18 11 19 11 | 20 34 81 25 47 25 36 28 22 27 28
14 | 8 23 10 15 23 5 24 8 12 18 5 | 19 32 28 27 37 23 29 21 25 19 21
15 | 6 20 15 10 32 4 20 9 10 16 4 | 21 31 28 23 41 22 30 18 26 24 21
16 | 8 20 10 13 43 6 25 11 8 21 5 | 21 32 28 24 36 22 35 22 24 22 22
17 | 7 14 7 12 42 6 12 7 8 28 4 | 26 30 29 29 40 26 28 29 33 27 27
18E | 9 21 10 16 27 4 22 4 7 16 4 | 68 73 72 71 76 68 73 69 73 76 70
19 | 7 14 7 10 24 7 11 7 6 29 4 | 30 29 34 34 34 33 32 29 31 36 30
20E | 6 17 7 10 37 6 18 11 9 11 4 | 22 32 27 21 42 22 30 24 20 27 22
21 | 8 22 8 8 28 6 19 6 7 29 4 | 21 33 24 19 31 19 30 22 25 30 21
22E | 7 18 8 14 38 3 23 7 8 10 4 | 30 39 35 34 47 31 37 32 35 32 32
23 | 8 22 9 13 32 7 24 12 7 19 5 | 22 37 25 28 45 25 36 26 22 25 24
24 | 8 16 7 9 23 3 14 9 9 16 4 | 18 27 24 20 34 19 27 21 22 29 19
25E | 15 24 15 14 48 7 21 10 8 27 6 | 60 64 62 59 65 60 63 61 61 65 60
26 | 7 15 7 9 21 4 11 9 9 14 3 | 24 30 26 25 35 24 29 24 32 31 25
27E | 9 17 7 14 57 3 17 7 9 14 4 | 34 40 37 36 46 35 42 33 37 38 34
28 | 8 23 10 13 41 5 20 6 10 21 4 | 20 35 22 25 38 23 29 22 29 24 21
29 | 8 15 11 11 42 5 16 6 12 35 5 | 24 26 23 23 45 22 27 22 27 35 22
30 | 8 12 7 8 19 5 12 8 14 19 4 | 22 25 30 27 28 24 25 23 23 28 22
31E | 10 26 11 15 26 8 21 8 8 18 5 | 23 35 30 26 40 25 30 26 27 29 23
32 | 11 22 9 8 53 4 17 8 11 22 4 | 30 39 35 32 53 29 36 29 32 41 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 15 12 40 5 18 9 9 20 |T 27 35 34 30 42 29 35 29 31 32 28
WRMS | 8 19 10 12 37 5 16 8 9 20 |NE 21 31 31 25 38 24 30 23 25 25 22
MEDI | 8 20 9 11 36 5 18 8 9 18 |MD 23 32 28 27 40 25 30 24 27 29 23
Table 3.1533.4 GPS week: 1533 Day: 4 MJD: 54979.000
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 --- --- --- --- 20 --- 14 24 --- 12 | 23 --- --- --- --- 30 --- 22 29 --- 22
2 | 7 22 9 19 41 4 23 10 11 21 5 | 23 29 22 24 34 21 31 22 27 25 21
3 | 7 15 9 10 38 3 12 8 12 17 4 | 22 26 25 28 23 23 22 22 30 23 24
4 | 7 13 6 12 33 2 10 11 9 17 3 | 20 23 23 27 26 21 23 19 22 28 21
X5 | 14 21 --- --- --- 16 --- 11 14 --- 8 | 19 21 --- --- --- 28 --- 22 31 --- 21
6 | 6 13 8 10 28 6 10 7 7 13 3 | 21 23 26 29 25 24 22 20 27 23 22
7E | 11 17 8 10 21 6 15 8 10 11 4 | 24 27 29 29 29 24 27 24 24 24 25
8E | 14 21 7 10 52 6 18 10 10 23 5 | 30 42 36 36 51 35 46 35 35 34 34
9E | 10 18 7 10 45 6 19 6 8 26 4 | 52 61 57 56 70 53 66 49 53 49 53
10E | 12 22 12 21 44 7 19 10 11 15 5 | 60 64 63 66 67 60 63 61 61 62 61
11 | 8 18 6 12 66 7 18 8 8 14 4 | 22 34 30 35 51 26 32 23 25 24 26
12 | 11 24 9 11 26 6 23 10 11 22 5 | 21 35 29 27 44 24 34 22 24 26 23
13 | 9 20 10 10 36 6 25 16 9 16 5 | 21 34 30 27 47 24 35 27 23 25 24
14 | 6 22 9 14 28 6 24 6 14 19 5 | 23 30 29 32 38 25 35 25 30 23 26
15 | 9 21 10 8 44 5 21 10 14 18 5 | 21 32 26 27 40 24 32 22 20 24 22
16 | 8 21 7 10 30 6 26 9 9 26 5 | 22 34 32 30 38 25 38 23 30 22 26
17 | 7 14 10 9 34 6 12 7 9 29 4 | 23 25 28 28 25 23 24 25 30 26 25
18E | 12 22 8 13 25 4 24 6 9 17 4 | 48 52 49 47 54 48 51 49 49 50 47
19 | 8 17 8 16 21 6 15 7 10 29 4 | 26 33 36 42 35 33 34 31 31 35 32
20E | 6 17 12 10 31 6 20 8 13 13 4 | 23 34 35 31 39 26 32 25 24 27 26
21 | 9 22 6 10 33 3 20 6 7 29 4 | 22 33 25 23 42 21 31 22 27 29 23
22E | 8 20 8 17 34 4 23 6 8 12 4 | 20 27 25 29 38 22 26 23 27 23 22
23 | 8 22 8 11 32 6 25 10 8 19 4 | 21 34 28 29 40 24 34 24 21 26 24
24 | 9 17 7 6 19 3 14 9 12 13 4 | 19 28 27 24 35 22 29 20 23 33 22
25E | 21 25 8 12 43 7 20 11 13 27 6 | 38 43 41 43 43 36 41 41 39 45 38
26 | 9 14 9 7 28 5 12 8 9 17 3 | 21 29 29 26 35 24 29 22 26 29 24
27E | 10 16 7 13 65 6 18 7 11 17 4 | 28 36 32 36 49 30 39 30 35 34 30
28 | 8 18 8 12 43 7 18 11 10 21 4 | 20 28 26 25 40 24 30 26 29 27 24
29 | 8 16 8 12 24 4 16 6 15 37 5 | 23 27 28 28 31 23 29 22 27 38 25
30 | 12 14 9 8 17 7 13 12 13 21 4 | 21 22 30 24 34 24 24 27 27 30 24
31E | 9 23 5 12 24 7 24 12 9 16 5 | 20 30 26 26 36 23 30 27 26 33 24
32 | 13 22 9 8 43 5 17 7 10 24 4 | 33 43 37 36 52 33 39 30 32 44 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 8 12 37 6 19 9 11 21 |T 25 33 31 32 40 28 34 27 30 31 27
WRMS | 9 19 8 12 34 6 17 8 9 20 |NE 21 29 27 27 37 24 30 23 26 25 23
MEDI | 9 20 8 10 33 6 18 8 10 18 |MD 22 32 29 29 38 24 32 24 27 27 24
Table 3.1533.5 GPS week: 1533 Day: 5 MJD: 54980.000
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 | 24 --- --- --- --- 44 --- 17 31 --- 17 | 21 --- --- --- --- 36 --- 24 30 --- 20
2 | 8 21 11 8 36 7 25 11 10 20 5 | 18 25 16 19 31 16 25 17 20 20 15
3 | 5 11 13 6 33 6 11 6 11 18 3 | 16 15 15 15 21 13 11 17 23 15 14
4 | 5 17 8 8 31 4 11 9 8 16 3 | 14 23 16 18 21 16 17 16 15 22 13
X5 | 13 22 --- --- --- 27 --- 15 15 --- 9 | 12 20 --- --- --- 26 --- 16 22 --- 12
6 | 6 9 11 5 32 6 11 5 7 13 3 | 14 16 16 14 23 15 13 14 22 17 14
7E | 9 17 12 9 24 7 18 7 10 9 4 | 20 25 22 23 26 25 24 23 27 27 23
8E | 15 23 8 10 50 6 20 11 10 19 5 | 26 37 30 29 49 27 40 24 27 24 26
9E | 12 18 10 10 44 5 19 5 9 28 4 | 63 68 62 65 85 61 72 61 62 62 62
10E | 17 16 6 13 63 8 19 10 12 24 5 | 58 62 56 57 64 59 63 60 53 59 56
11 | 10 19 9 6 68 8 20 6 7 13 4 | 13 27 15 17 50 16 26 16 21 17 15
12 | 11 25 9 9 32 6 24 8 9 20 5 | 14 32 20 20 40 16 33 16 20 20 17
13 | 11 21 11 8 46 5 26 14 6 13 5 | 12 27 21 15 45 15 29 17 14 15 13
14 | 7 24 8 10 36 5 22 8 8 17 4 | 16 28 22 23 38 21 28 21 25 18 20
15 | 8 23 10 10 41 4 22 11 14 16 5 | 11 25 18 14 38 11 23 19 13 13 10
16 | 7 21 7 8 36 6 29 11 7 28 5 | 15 30 22 20 40 18 33 17 20 19 18
17 | 9 14 9 6 22 6 14 10 9 27 4 | 15 13 13 17 23 13 17 19 24 17 13
18E | 13 26 7 14 35 5 26 12 6 15 5 | 79 85 82 81 78 81 83 81 79 85 80
19 | 8 13 9 13 24 8 15 6 9 30 4 | 20 26 29 33 30 26 27 25 28 27 26
20E | 9 16 9 13 24 6 20 8 12 15 4 | 19 28 22 24 34 18 27 18 21 25 19
21 | 7 21 9 6 31 5 24 8 12 28 5 | 12 25 13 12 33 10 27 14 18 26 11
22E | 8 20 7 9 33 4 24 7 6 8 4 | 16 28 20 18 29 17 24 18 25 17 18
23 | 9 20 10 10 31 5 28 8 8 17 4 | 15 27 18 18 36 16 29 17 15 16 15
24 | 8 17 9 7 20 5 13 8 11 14 4 | 12 22 19 12 29 13 21 11 17 24 12
25E | 24 27 12 18 52 6 19 10 13 30 6 | 53 57 49 54 60 52 54 53 52 56 51
26 | 6 13 7 6 13 5 11 6 7 15 3 | 19 23 21 17 29 18 25 15 23 26 18
27E | 11 18 10 9 64 5 19 5 9 16 4 | 28 35 31 29 63 29 38 32 34 35 30
28 | 10 21 10 10 44 7 21 15 10 19 5 | 12 25 15 15 42 14 26 18 22 17 13
29 | 7 16 9 6 29 8 17 5 13 37 5 | 13 18 15 17 18 14 20 13 21 28 13
30 | 10 15 7 5 24 5 12 10 8 18 3 | 13 16 17 16 31 15 20 21 18 23 14
31E | 9 29 9 13 36 10 28 10 13 17 5 | 15 26 19 20 41 16 23 25 21 24 18
32 | 24 20 14 8 42 7 19 11 14 22 6 | 48 59 55 53 63 52 57 51 56 60 52
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 20 10 10 39 6 20 9 10 20 |T 22 31 26 26 40 24 31 25 27 28 23
WRMS | 9 20 9 10 36 6 18 8 8 20 |NE 14 24 18 17 35 17 25 17 20 18 15
MEDI | 9 20 9 9 33 6 19 8 9 17 |MD 15 26 20 18 36 16 26 18 22 23 17
Table 3.1533.6 GPS week: 1533 Day: 6 MJD: 54981.000
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 | 26 --- --- --- --- 39 --- 15 26 --- 16 | 28 --- --- --- --- 35 --- 27 26 --- 23
2 | 10 21 8 12 38 4 21 13 13 23 5 | 29 31 23 26 31 25 33 25 27 33 24
3 | 6 9 7 9 25 9 6 6 11 16 3 | 28 28 25 29 23 27 24 29 34 27 27
4 | 8 13 5 11 25 4 11 16 14 18 4 | 25 25 22 27 23 22 21 28 26 30 22
X5 | 13 21 --- --- --- 17 --- 11 18 --- 9 | 19 26 --- --- --- 22 --- 21 30 --- 20
6 | 9 8 5 10 24 8 7 7 11 13 3 | 28 27 27 29 26 27 24 27 36 25 27
7E | 7 17 10 21 29 5 18 8 12 17 5 | 26 29 28 34 35 24 28 28 29 34 26
8E | 12 19 8 12 57 6 20 10 11 23 5 | 33 44 40 41 59 38 50 35 38 35 37
9E | 9 17 5 10 45 5 20 13 11 28 5 | 64 74 68 66 77 64 76 58 65 69 66
10E | 14 16 7 14 79 8 16 12 10 32 5 | 73 72 74 77 90 71 71 76 80 85 75
11 | 7 18 9 7 70 8 17 13 7 13 4 | 27 34 29 31 60 27 30 29 34 29 27
12 | 11 25 8 8 30 5 21 14 10 18 5 | 22 37 27 25 40 24 34 24 29 27 24
13 | 6 19 7 12 51 5 21 12 11 15 4 | 23 36 31 29 46 27 35 27 28 27 26
14 | 8 23 9 14 30 6 25 10 9 17 5 | 26 32 28 32 38 26 31 30 31 27 27
15 | 8 24 6 14 37 4 22 15 14 16 5 | 25 36 29 30 37 27 34 30 29 29 26
16 | 9 23 7 10 29 6 24 10 11 31 5 | 26 35 29 27 40 27 36 24 36 25 27
17 | 8 11 7 9 30 4 12 16 14 30 5 | 34 34 33 36 33 32 30 36 44 34 33
18E | 14 21 8 14 25 3 22 11 8 20 5 | 54 58 55 57 55 55 60 56 63 61 56
19 | 6 10 7 9 24 6 13 10 10 29 4 | 30 31 31 30 33 31 35 32 37 35 31
20E | 8 19 12 10 31 6 18 10 16 15 5 | 28 39 38 34 41 31 35 35 27 33 31
21 | 8 21 7 10 27 5 19 11 9 30 5 | 24 35 23 22 37 22 33 25 30 35 23
22E | 11 20 7 14 32 5 23 13 6 9 4 | 20 27 20 25 32 20 25 24 29 22 21
23 | 7 19 8 13 31 5 23 11 12 20 5 | 27 35 29 31 38 28 35 28 28 31 27
24 | 10 14 6 6 16 5 10 11 8 12 3 | 20 26 22 21 30 19 25 20 24 27 19
25E | 28 26 7 14 42 8 23 12 11 32 7 | 74 74 75 72 74 72 71 77 76 75 73
26 | 8 18 5 11 21 5 12 10 11 12 4 | 27 32 28 29 33 28 30 30 36 32 27
27E | 11 20 6 20 45 4 21 11 11 18 5 | 40 49 44 50 59 42 48 41 45 47 43
28 | 8 19 9 12 41 5 20 16 8 23 5 | 24 33 28 30 45 26 33 27 30 26 26
29 | 8 14 8 8 26 8 14 9 9 35 4 | 29 31 28 29 37 26 33 28 29 35 27
30 | 10 11 6 7 17 4 10 13 10 16 3 | 24 28 28 27 34 26 28 29 27 31 25
31E | 11 28 10 12 31 4 23 10 11 15 5 | 23 35 23 24 37 22 30 25 32 31 23
32E | 15 25 14 12 37 11 16 14 17 22 6 | 64 78 74 74 73 65 69 70 65 68 68
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 8 12 38 6 18 12 11 22 |T 32 39 35 36 43 33 38 34 37 37 33
WRMS | 9 19 7 12 33 6 16 11 9 23 |NE 25 32 28 29 38 26 31 27 30 29 25
MEDI | 9 19 7 11 30 5 19 11 11 18 |MD 27 34 28 30 37 27 33 28 30 31 27
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 4.1533 GPS week: 1533 MJD: 54975.0-54981.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 |U 7 7 23 |U 7 8 20 |U 13 9 29 |
emr | emr 2952 | 10 9 26 | 8 9 28 |U 14 10 31 |
esa | esa 2880 | 8 8 23 |U 6 8 20 | 13 9 27 |
gfz | gfz 2846 |U 8 8 27 |U 9 11 40 | 12 8 27 |
grg | grg 2893 | 9 9 26 |U 9 10 29 | 16 10 39 |
igr | igr 2879 | 9 8 24 | 7 8 26 | 12 10 28 |
igs | igs 2925 | 8 7 24 | 7 8 21 | 12 9 28 |
jpl | jpl 2856 | 8 8 25 |U 8 8 23 |U 13 9 28 |
mit | mit 3072 |U 8 7 24 |U 7 11 28 |U 14 11 67 |
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 5.1533.0 GPS week: 1533 Day: 0 MJD: 54975.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 9 6 20 | 6 8 18 | 7 9 26 |
emr | emr 2956 | 12 9 26 | 6 8 28 | 9 8 26 |
esa | esa 2880 | 10 7 24 | 5 6 18 | 7 8 26 |
gfz | gfz 2857 | 10 6 24 | 6 7 24 | 6 8 26 |
grg | grg 2976 | 11 9 28 | 9 7 29 | ---- ---- ---- |
igr | igr 2954 | 10 6 27 | 6 7 21 | 7 8 25 |
igs | igs 2866 | 11 6 24 | 4 5 18 | 7 9 26 |
jpl | jpl 2858 | 11 8 24 | 6 6 21 | 8 9 22 |
mit | mit 3072 | 10 4 19 | 6 9 28 | 18 17 154 |
Table 5.1533.1 GPS week: 1533 Day: 1 MJD: 54976.0
CENT| CLK EPO | BRUS | WILL |
----+----------+-------------------+-------------------+
cod | cod 3053 | 9 12 26 | 8 8 21 |
emr | emr 2956 | 12 14 30 | 9 9 23 |
esa | esa 2880 | 10 13 28 | 7 7 19 |
gfz | gfz 2851 | 10 14 32 | 7 7 20 |
grg | grg 2880 | 11 15 31 | 14 9 29 |
igr | igr 2897 | 10 13 30 | 8 7 18 |
igs | igs 2950 | 10 12 28 | 7 8 21 |
jpl | jpl 2856 | 10 13 28 | 8 9 16 |
mit | mit 3072 | 10 12 26 | 8 9 22 |
Table 5.1533.2 GPS week: 1533 Day: 2 MJD: 54977.0
CENT| CLK EPO | BRUS | WILL |
----+----------+-------------------+-------------------+
cod | cod 3051 | 8 9 30 | 9 7 19 |
emr | emr 2952 | 12 8 29 | 10 9 25 |
esa | esa 2880 | 9 9 31 | 9 7 19 |
gfz | gfz 2854 | 8 9 33 | 8 6 20 |
grg | grg 2880 | 8 9 31 | 15 8 38 |
igr | igr 2805 | 15 13 25 | 9 16 22 |
igs | igs 2944 | 9 8 30 | 8 6 18 |
jpl | jpl 2856 | 9 8 31 | 9 8 21 |
mit | mit 3072 | 8 8 30 | 9 7 19 |
Table 5.1533.3 GPS week: 1533 Day: 3 MJD: 54978.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 5 5 14 | 10 8 22 | 41 12 79 |
emr | emr 2953 | 9 7 19 | 12 11 32 | 44 12 75 |
esa | esa 2880 | 5 6 14 | 10 12 29 | 40 14 74 |
gfz | gfz 2844 | 6 6 16 | 13 13 43 | 41 10 70 |
grg | grg 2880 | 8 7 15 | 11 12 30 | 32 12 76 |
igr | igr 2882 | 5 7 14 | 12 9 29 | 39 10 76 |
igs | igs 2944 | 5 5 14 | 12 9 23 | 38 11 74 |
jpl | jpl 2858 | 6 7 17 | 13 10 28 | 40 10 75 |
mit | mit 3072 | 6 5 15 | 12 13 27 | 31 13 69 |
Table 5.1533.4 GPS week: 1533 Day: 4 MJD: 54979.0
CENT| CLK EPO | BRUS | WILL |
----+----------+-------------------+-------------------+
cod | cod 3051 | 6 6 21 | 7 7 16 |
emr | emr 2957 | 9 6 24 | 8 9 21 |
esa | esa 2880 | 8 4 21 | 7 8 15 |
gfz | gfz 2839 | 7 7 26 | 6 7 14 |
grg | grg 2880 | 8 8 24 | 13 9 28 |
igr | igr 2883 | 7 6 23 | 7 8 15 |
igs | igs 2927 | 7 5 22 | 7 8 14 |
jpl | jpl 2853 | 5 7 23 | 8 9 19 |
mit | mit 3072 | 6 4 21 | 7 7 17 |
Table 5.1533.5 GPS week: 1533 Day: 5 MJD: 54980.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 7 7 27 | 5 8 14 | 9 10 21 |
emr | emr 2953 | 11 8 28 | 7 10 27 | 9 15 26 |
esa | esa 2880 | 9 9 25 | 5 7 15 | 9 11 19 |
gfz | gfz 2842 | 10 10 32 | 10 14 53 | 9 11 19 |
grg | grg 2880 | 11 9 26 | 7 11 36 | 10 13 32 |
igr | igr 2882 | 9 8 27 | 5 8 24 | 8 11 18 |
igs | igs 2980 | 9 8 27 | 5 10 21 | 8 10 21 |
jpl | jpl 2856 | 9 8 25 | 6 9 23 | 8 12 21 |
mit | mit 3072 | 12 12 34 | 6 11 31 | 17 20 166 |
Table 5.1533.6 GPS week: 1533 Day: 6 MJD: 54981.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 7 5 21 | 6 8 26 | 8 8 20 |
emr | emr 2943 | 8 9 25 | 7 8 25 | 9 8 23 |
esa | esa 2880 | 7 7 21 | 6 8 20 | 9 8 20 |
gfz | gfz 2840 | 7 7 24 | 8 12 40 | 9 7 21 |
grg | grg 2880 | 8 7 25 | 10 10 23 | 14 11 34 |
igr | igr 2853 | 6 6 21 | 6 8 32 | 9 7 21 |
igs | igs 2866 | 6 6 21 | 6 10 20 | 9 8 21 |
jpl | jpl 2857 | 7 9 23 | 6 7 22 | 9 8 21 |
mit | mit 3072 | 6 5 20 | 6 9 25 | 8 7 21 |
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 6.1533 GPS week: 1533 MJD: 54975.500-54981.500
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 | 6 -6 46 -145 -2 | -4 17
| 30 10 114 101 6 | 2
emr uuxux | 26 46 -44 143 11 | 24 35
| 18 23 330 87 28 | 7
esa uuuuu | -2 -16 -23 3 -9 | 5 12
| 37 37 117 117 11 | 2
gfz uuuuu | 14 4 54 -138 2 | 17 23
| 8 16 97 90 10 | 4
grg xxxxx | -5 -47 89 -174 12 | -7 39
| 54 26 110 115 37 | 2
igr xxxxx | 17 -1 -2 -49 2 | -9 19
| 25 30 62 55 7 | 2
irf xxxxx | 30 7 44 -31 7 | -9 23
| 10 7 48 31 19 | 6
jpl uuuuu | -11 1 -41 -28 10 | -11 31
| 14 23 143 110 20 | 4
mit uuuuu | 25 -8 65 -1 10 | 1 25
| 28 14 182 108 24 | 6
ngs uuuuu | -27 -26 11 -19 2 | -3 16
| 80 66 55 170 7 | 3
sio uuuuu | -57 80 -196 153 0 | 64 67
| 18 12 44 89 23 | 5
Table 7.1533.0 GPS week: 1533 Day: 0 MJD: 54975.500
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 | -12 -6 -186 -192 -3 | -6 13
emr uuxux | 57 30 395 12 12 | 17 24
esa uuuuu | -31 45 -121 194 -7 | 5 10
gfz uuuuu | 8 26 -143 -192 -4 | 14 17
grg xxxxx | 36 -41 115 -207 50 | -9 40
igr xxxxx | 51 54 65 -23 -4 | -7 18
irf xxxxx | 20 16 128 -75 12 | -16 19
jpl uuuuu | -24 -22 148 -128 16 | -14 28
mit uuuuu | -8 1 349 -137 12 | -5 16
ngs uuuuu | 40 -99 -41 88 1 | -4 14
sio uuuuu | -71 88 -159 39 5 | 58 59
Table 7.1533.1 GPS week: 1533 Day: 1 MJD: 54976.500
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 | 62 13 116 -254 2 | -8 14
emr uuxux | 33 17 358 118 33 | 14 19
esa uuuuu | -62 14 -89 -29 -17 | 4 11
gfz uuuuu | 18 17 148 -219 1 | 11 15
grg xxxxx | 96 -5 -118 -155 -45 | -6 42
igr xxxxx | 16 6 -80 -92 -4 | -12 18
irf xxxxx | 20 13 69 -19 22 | -18 19
jpl uuuuu | -5 -1 -50 -72 39 | -18 26
mit uuuuu | -10 9 156 20 29 | -8 14
ngs uuuuu | 103 -98 -40 187 -14 | -6 15
sio uuuuu | -62 88 -235 85 20 | 56 57
Table 7.1533.2 GPS week: 1533 Day: 2 MJD: 54977.500
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 -8 53 -102 2 | -5 17
emr uuxux | 38 27 58 172 41 | 19 30
esa uuuuu | 7 4 -136 122 -28 | 6 13
gfz uuuuu | 22 -3 38 -218 19 | 14 20
grg xxxxx | -26 -49 89 -251 -23 | -7 42
igr xxxxx | 6 16 -39 -144 0 | -10 19
irf xxxxx | 45 12 61 -36 29 | -13 23
jpl uuuuu | -37 33 -74 -195 17 | -14 31
mit uuuuu | 41 4 149 78 38 | -4 22
ngs uuuuu | -72 -75 60 -195 5 | -6 15
sio uuuuu | -29 75 -142 284 24 | 61 64
Table 7.1533.3 GPS week: 1533 Day: 3 MJD: 54978.500
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 | 33 -18 42 -295 4 | -3 18
emr uuxux | 15 83 -163 213 30 | 25 40
esa uuuuu | -5 -41 -93 -31 -13 | 7 13
gfz uuuuu | 22 -22 53 -134 6 | 19 27
grg xxxxx | -13 -57 60 -109 -1 | -11 41
igr xxxxx | -9 -10 -21 -47 -2 | -8 19
irf xxxxx | 19 4 33 -35 18 | -7 25
jpl uuuuu | -2 30 56 40 24 | -10 32
mit uuuuu | 10 -13 89 24 28 | 2 29
ngs uuuuu | 0 -15 -34 -61 4 | -2 16
sio uuuuu | -85 91 -165 131 13 | 67 71
Table 7.1533.4 GPS week: 1533 Day: 4 MJD: 54979.500
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 | 0 -14 184 -54 0 | -1 19
emr uuxux | 22 48 -420 270 15 | 30 45
esa uuuuu | -5 -45 24 -92 -4 | 6 12
gfz uuuuu | 0 2 94 -155 6 | 20 29
grg xxxxx | -27 -43 230 -138 23 | -5 36
igr xxxxx | -12 -32 -55 -40 16 | -7 19
irf xxxxx | 33 -3 31 15 4 | -3 26
jpl uuuuu | -4 -23 -266 124 8 | -7 33
mit uuuuu | 47 -32 32 146 9 | 6 32
ngs uuuuu | -49 70 63 -252 2 | 0 17
sio uuuuu | -61 57 -222 252 -2 | 69 74
Table 7.1533.5 GPS week: 1533 Day: 5 MJD: 54980.500
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 | -18 -2 54 -54 -12 | -3 19
emr uuxux | 10 68 -397 150 -21 | 31 45
esa uuuuu | 29 -49 170 -137 3 | 3 11
gfz uuuuu | 20 -4 139 31 -10 | 20 28
grg xxxxx | -38 -45 68 1 24 | -5 36
igr xxxxx | 49 -11 33 27 3 | -8 19
irf xxxxx | 35 1 -11 -5 -18 | -3 26
jpl uuuuu | -11 1 -164 39 -16 | -7 33
mit uuuuu | 38 -18 -132 13 -20 | 7 32
ngs uuuuu | -76 16 -13 -54 9 | -1 17
sio uuuuu | -49 78 -189 176 -28 | 68 73
Table 7.1533.6 GPS week: 1533 Day: 6 MJD: 54981.500
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 -11 60 -67 -7 | -5 20
emr uuxux | 7 48 -139 66 -34 | 30 45
esa uuuuu | 49 -41 85 -5 3 | 2 11
gfz uuuuu | 10 10 50 -79 -3 | 19 28
grg xxxxx | -64 -92 178 -363 54 | -5 36
igr xxxxx | 20 -29 82 -28 3 | -9 20
irf xxxxx | 34 4 -5 -63 -19 | -4 27
jpl uuuuu | 4 -14 63 -3 -16 | -9 34
mit uuuuu | 58 -11 -186 -150 -23 | 6 32
ngs uuuuu | -133 19 84 156 5 | 0 17
sio uuuuu | -45 78 -262 104 -33 | 66 72
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