[IGSREPORT-17945] Wk 1553 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Oct 29 11:39:01 PDT 2009
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IGS Electronic Report 29 Oct 11:39:25 PDT 2009 Message Number 17945
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1553 (Oct 11, 2009 - Oct 17, 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:
igs1553[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1553[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1553[0-6].cls IGS GPS clock combination summary report.
igs15537.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15537.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
0 | COD | MIZU
0 | EMR | 24 MIZU
0 | ESA | 4 MAS1 UNSA WTZR
0 | GFZ | 1 2 24 DARW DAV1 DGAR FAA1 FLIN KERG ONSA PERT SFER
0 | GRG | ONSA TWTF
0 | JPL | 32 DGAR KARR
0 | MIT | 24 MAS1 MAS1 MIZU
0 | NGS | 1
1 | ALL | 1
1 | COD | 4 4
1 | EMR | 25 25 WTZR
1 | ESA | 4 CEDU
1 | GFZ | 2 5 8 11 24 25 AUCK CHAT DARW HOB2 IRKT KARR KIRU
1 | GFZ | MCM4 NRMD OUS2 PERT PIMO SFER SYOG YAR2
1 | GRG | ONSA TWTF
1 | JPL | 4 25 32 DGAR
1 | MIT | 24 24
2 | ALL | 1
2 | COD | 4 25 4 25 TOW2
2 | EMR | 21 21
2 | ESA | 4 25 ALGO TOW2 UNSA
2 | GFZ | 2 8 11 21 24 25 ADE1 AMC2 AUCK CEDU CHAT DARW DAV1
2 | GFZ | DUBO FAA1 GODE GUAT HOB2 KIRU KOUC MDO1 NRMD OUS2
2 | GFZ | PIE1 STJO TIDB TOW2 TRO1 YAR2 YELL
2 | GRG | ONSA
2 | JPL | 32 DGAR
2 | MIT | 24 24 ALGO ALGO
3 | COD | 24 24
3 | EMR | NRC1
3 | ESA | NRC1 UNSA
3 | GFZ | 27 KERG MAW1
3 | GRG | ONSA TRO1 TWTF
3 | JPL | 32 DGAR
3 | MIT | HARB DAV1 HARB MATE
4 | COD | 24 24
4 | EMR | KHAJ
4 | ESA | 27 KOKB UNSA
4 | GFZ | 4 11 21 24 CEDU FAA1 HOB2 HRAO MAC1 MIZU ONSA TOW2
4 | GFZ | TSKB TWTF WSRT
4 | JPL | 32
4 | MIT | MIZU KERG MIZU
4 | NGS | 1
5 | ALL | 1 24
5 | COD | 4 25 MIZU
5 | EMR | 9 9
5 | ESA | 4 25 CEDU UNSA
5 | GFZ | 2 4 9 11 21 27 BAKO DAV1 DUBO FLIN WTZR
5 | GRG | KHAJ WTZR
5 | JPL | 9 27 32 AREQ
5 | MIT | 8 24 8 27
6 | ALL | 1 1
6 | COD | 4 9 25
6 | ESA | 4 9 25
6 | GFZ | 2 27 ALGO DUBO FAA1 GUAM HARB MAS1 MATE MAW1 ONSA
6 | GFZ | ZECK ZIMM
6 | GRG | WTZR
6 | JPL | 27
6 | MIT | 8 24 8 21 24 27 HARB KHAJ
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
----+--------+---------------
4 | ALL | 8
5 | MIT | 8
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 | .3 1.0 1.1 -4 -4 -5 -.12
EMR | .2 -1.9 1.5 56 16 55 .45
ESA | 6.0 7.9 9.3 101 -24 50 -.09
GFZ | .0 1.1 1.1 17 -10 6 -.02
GRG | 6.4 5.0 6.1 -13 -17 23 -.05
JPL | .0 6.4 5.9 3 -9 3 .47
MIT | 3.4 1.5 15.5 4 7 -22 -.16
NGS | 4.3 .1 10.3 13 8 -13 -.06
SIO | 7.6 3.4 3.3 64 -89 8 .23
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 1.1553.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1553.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 2.1553.[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 3.1553.[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 5.1553.0-6).
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 1553 summary. (Oct 11, 2009 - Oct 17, 2009)
Table 1.1553.a GPS week: 1553 MJD: 55115.000-55121.000
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 226| 1 0 0 56 -5 0 -.14 8 7 | -575 181 22 84
| 0 0 0 20 17 25 .03 | 783 999
emr 86| -1 0 0 -59 -95 31 .61 20 20 | 716 -969 19 87
| 1 2 1 31 55 10 .02 | 3526 1557
esa 120| 0 -3 0 -114 47 -31 .33 10 10 | 201 -51 21 123
| 1 1 0 28 41 13 .03 | 1949 1217
gfz 185| 0 0 -1 14 5 -12 -.18 11 11 | 51 -283 28 121
| 0 0 1 61 98 17 .05 | 330 826
grg 112| 3 2 1 64 13 30 1.06 35 34 | -78482 172087 82 233
| 2 2 2 28 23 51 .03 | 167316 435629
igr n/a| 0 0 0 49 -20 -24 .06 6 5 | -6902 -499 19 68
| 0 0 1 19 29 20 .04 | 2527 1600
jpl 120| -1 0 -2 25 -12 42 .57 20 19 | 1571 -732 18 91
| 2 1 1 22 18 14 .02 | 2791 1543
mit 266| -1 0 0 69 -31 11 -.35 13 12 | -14111 -368 23 131
| 0 0 0 20 20 15 .02 | 2293 2090
ngs 219| 0 0 0 18 -23 -1 -.18 10 7 | 8900 5517 2233 15688
| 0 0 1 42 65 20 .01 | 6085 2454
sio 252| 1 2 2 -91 142 6 -.07 22 22 | --- --- --- ---
| 0 0 0 16 28 18 .04 | --- ---
Table 1.1553.b GPS week : 1553 MJD: 55115.000-55121.000
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 | 10 8 12 12 9 8 11 |
2 | 4 4 4 5 5 6 6 |
3 | 4 4 4 4 5 4 5 |
4 | 6 6 6 6 7 6 6 |
5 | 6 6 5 5 6 6 6 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 5 5 5 |
8 | 5 6 5 6 --- 16 26 |
9 | 5 5 5 6 8 7 6 |
10 | 4 4 4 4 4 4 5 |
11 | 4 4 4 4 5 4 4 |
12 | 4 4 4 5 5 5 5 |
13 | 5 5 4 5 5 5 5 |
14 | 5 4 4 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 6 6 6 |
17 | 5 5 5 5 6 6 5 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 5 5 5 |
20 | 5 5 5 5 6 5 5 |
21 | 5 6 4 5 5 5 4 |
22 | 5 5 4 5 6 6 5 |
23 | 5 5 5 5 6 6 6 |
24 | 10 9 10 9 10 12 11 |
25 | 7 6 6 6 6 6 6 |
26 | 4 4 4 5 5 4 4 |
27 | 5 5 6 6 6 6 5 |
28 | 4 5 5 5 6 5 5 |
29 | 5 5 5 6 6 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 4 5 4 5 5 5 6 |
32 | 5 5 5 6 6 5 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1553.0 GPS week: 1553 Day: 0 MJD: 55115.000
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 226| 1 0 0 50 0 -9 -.11 8 7 | -526 458 23 99
| 6 33 |
emr 86| 0 0 -3 -54 -44 37 .62 19 19 | 4118 1381 19 87
| -22 -11 |
esa 120| 0 -1 0 -126 15 -46 .32 9 9 | -176 484 19 114
| 26 33 |
gfz 185| 0 1 0 62 -47 -14 -.18 10 10 | 299 -213 27 117
| -26 -65 |
grg 112| 4 2 -1 64 11 35 1.12 33 30 | 616 -48 81 237
| 93 41 |
igr n/a| 0 1 -1 39 -7 1 .06 5 5 | -4706 1321 18 67
| -13 18 |
jpl 120| 1 1 -4 15 -20 59 .60 19 18 | 4233 1141 17 74
| 20 1 |
mit 266| 0 -1 2 85 -39 -16 -.39 12 11 | -15017 -692 21 123
| -24 -14 |
ngs 219| -1 0 0 -7 25 28 -.18 8 6 | 11013 5636 1846 3650
| 50 -76 |
sio 252| 1 1 2 -79 123 5 -.13 22 20 | --- --- --- ---
| 5 -52 |
Table 2.1553.1 GPS week: 1553 Day: 1 MJD: 55116.000
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 226| 0 1 0 57 -8 44 -.14 8 7 | -692 283 16 69
| -24 40 |
emr 86| -2 0 -2 -63 -40 12 .60 20 20 | 5347 -2769 15 77
| 6 -16 |
esa 120| 0 -1 0 -116 6 -49 .33 8 8 | 3635 -1554 21 130
| 47 52 |
gfz 185| 0 0 0 34 -66 -33 -.16 11 11 | 122 -352 27 117
| -37 -36 |
grg 112| 2 0 2 91 -13 0 1.05 33 31 | 683 -895 78 222
| 59 52 |
igr n/a| 0 0 0 37 -2 -7 .04 5 5 | -3282 -2595 20 71
| 30 29 |
jpl 120| -4 0 -3 6 -26 28 .56 20 19 | 5554 -2934 17 95
| 20 58 |
mit 266| 0 -1 0 78 -6 0 -.38 13 12 | -13855 -2490 17 111
| -32 -18 |
ngs 219| 0 0 0 22 31 13 -.21 10 7 | 7985 8887 2211 3986
| 39 -25 |
sio 252| 2 2 2 -91 147 -14 -.09 21 21 | --- --- --- ---
| 6 -67 |
Table 2.1553.2 GPS week: 1553 Day: 2 MJD: 55117.000
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 226| 1 1 0 61 13 -5 -.10 9 8 | -388 543 18 83
| 7 -2 |
emr 86| -1 2 0 -50 -52 42 .64 21 21 | 3289 -2066 14 105
| -15 10 |
esa 120| 0 -3 0 -167 51 -25 .36 9 9 | 686 -535 21 124
| 83 20 |
gfz 185| 0 0 -1 -37 -95 -9 -.15 10 10 | 79 -688 28 120
| -21 -52 |
grg 112| 6 0 4 50 21 114 1.05 34 33 | 131 778 84 240
| 24 36 |
igr n/a| 0 0 0 65 -4 -23 .10 5 5 | -4984 -1717 19 71
| -16 31 |
jpl 120| -4 0 -3 10 13 46 .59 20 19 | 3516 -2039 17 85
| 48 22 |
mit 266| -1 0 1 91 -56 7 -.34 10 9 | -15479 149 22 152
| -19 10 |
ngs 219| 0 0 -1 52 45 -12 -.18 8 6 | 11408 5562 2234 4216
| -39 -94 |
sio 252| 1 2 3 -69 103 9 -.07 21 19 | --- --- --- ---
| -2 -55 |
Table 2.1553.3 GPS week: 1553 Day: 3 MJD: 55118.000
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 226| 1 0 0 96 -16 -28 -.14 9 8 | -1552 1655 34 104
| -58 -4 |
emr 86| -1 0 0 -3 -124 25 .59 20 20 | 20 -1191 27 94
| -33 67 |
esa 120| 1 -3 1 -119 127 -21 .36 10 9 | -1424 1682 26 123
| 87 -75 |
gfz 185| 0 1 0 -101 -1 9 -.13 10 10 | -606 947 34 119
| -28 14 |
grg 112| 3 3 2 108 6 64 1.01 37 37 | -34 389 82 213
| -97 110 |
igr n/a| 0 0 -1 74 -56 -47 .07 6 6 | -7835 -878 21 71
| -22 98 |
jpl 120| -2 1 -3 60 -7 34 .56 20 20 | 370 -865 22 84
| 25 16 |
mit 266| -1 0 0 35 -49 24 -.35 11 11 | -15963 285 34 154
| -8 6 |
ngs 219| 0 0 0 91 -51 14 -.19 10 7 | -3977 5030 2987 86805
| -62 20 |
sio 252| 2 1 1 -116 134 -13 -.06 21 19 | --- --- --- ---
| 4 -81 |
Table 2.1553.4 GPS week: 1553 Day: 4 MJD: 55119.000
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 226| 1 0 0 34 -36 4 -.14 9 8 | -1401 379 34 102
| 27 50 |
emr 86| 0 -1 0 -102 -192 42 .64 21 21 | -1499 -2161 22 89
| 23 126 |
esa 120| 2 -3 1 -75 59 -38 .34 13 13 | -2374 907 25 133
| 31 -71 |
gfz 185| 0 0 -4 46 198 -27 -.15 12 12 | 365 -1669 32 111
| 26 -4 |
grg 112| 3 6 1 68 -9 41 1.05 36 38 | -447419 1159656 92 251
| 90 200 |
igr n/a| 0 -1 0 25 -68 -45 .06 6 6 | -8852 -1406 21 61
| -19 26 |
jpl 120| 0 -2 -1 2 -40 61 .54 20 20 | -524 -1458 22 91
| 66 54 |
mit 266| -1 0 1 79 -2 24 -.35 13 11 | -14627 -2002 31 126
| -8 -5 |
ngs 219| -1 1 0 -26 -132 -14 -.18 11 8 | 10548 5504 2406 3629
| -50 39 |
sio 252| 2 2 1 -78 195 3 -.01 22 21 | --- --- --- ---
| 5 -102 |
Table 2.1553.5 GPS week: 1553 Day: 5 MJD: 55120.000
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 226| 1 0 0 35 4 16 -.15 8 7 | 807 -1602 18 66
| 1 -18 |
emr 86| -4 -1 0 -85 -120 24 .59 20 20 | -3059 -762 16 76
| 4 70 |
esa 120| 3 -4 0 -97 58 -22 .33 11 11 | 1290 -1516 19 122
| 26 -17 |
gfz 185| 0 0 -2 69 54 -25 -.19 11 11 | 224 -412 29 164
| 10 -27 |
grg 112| 0 2 2 34 55 0 1.08 36 33 | -104402 30549 73 236
| 45 42 |
igr n/a| 0 0 0 35 1 -43 .11 6 6 | -9685 67 17 68
| -8 -13 |
jpl 120| 0 0 -1 35 3 44 .55 20 19 | -1384 -22 16 87
| -19 1 |
mit 266| 0 0 1 62 -40 16 -.33 14 13 | -14705 -1562 17 108
| -25 -27 |
ngs 219| -1 0 3 -22 -77 -15 -.18 10 7 | 15285 844 1905 3854
| 87 91 |
sio 252| 0 3 2 -99 142 18 -.04 24 25 | --- --- --- ---
| -23 -96 |
Table 2.1553.6 GPS week: 1553 Day: 6 MJD: 55121.000
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 226| 1 1 0 59 6 -24 -.20 8 7 | -277 -444 17 65
| 13 16 |
emr 86| -3 -5 0 -54 -93 33 .59 19 19 | -3201 785 20 85
| 0 43 |
esa 120| 0 -2 0 -99 13 -16 .28 9 8 | -224 172 20 115
| 35 1 |
gfz 185| 1 2 -1 23 -5 11 -.29 11 11 | -121 405 22 104
| -17 -22 |
grg 112| 0 1 -2 33 23 -46 1.04 36 34 | 1049 14185 84 234
| 16 57 |
igr n/a| 0 0 1 66 -3 -6 .00 5 5 | -8975 1713 19 72
| -59 9 |
jpl 120| 1 0 -1 48 -7 23 .57 19 18 | -767 1049 20 123
| 11 32 |
mit 266| -1 0 0 50 -24 23 -.34 17 15 | -9136 3734 22 144
| -6 -23 |
ngs 219| -1 0 0 19 -7 -25 -.19 10 7 | 10039 7156 2046 3681
| 8 9 |
sio 252| 0 2 1 -105 152 39 -.07 25 25 | --- --- --- ---
| -22 -78 |
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 3.1553.0 GPS week: 1553 Day: 0 MJD: 55115.000
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 --- --- 17 --- 21 --- 14 14 --- 10 | 19 --- --- 33 --- 36 --- 21 31 --- 23
2E | 7 17 8 9 29 4 17 13 8 14 4 | 15 24 18 16 31 16 22 13 17 21 15
3 | 6 12 9 11 23 4 14 12 7 24 4 | 19 22 25 30 18 21 22 21 20 25 20
4E | 11 21 13 10 69 7 18 20 20 19 6 | 34 48 39 34 58 36 45 36 41 37 36
5 | 7 22 8 14 32 5 26 14 10 33 5 | 28 41 29 29 44 28 39 25 29 36 28
6 | 5 11 8 9 21 4 12 13 5 25 3 | 20 22 23 29 23 22 21 23 23 24 20
7 | 8 16 11 10 41 5 16 9 6 14 4 | 18 28 23 16 41 18 25 16 19 17 18
8 | 13 13 8 12 20 5 13 11 5 25 4 | 43 42 42 39 48 49 36 75 40 40 41
9 | 8 21 9 12 28 4 17 13 8 18 4 | 40 54 45 40 55 43 56 45 41 40 42
10 | 7 10 9 12 29 5 11 13 8 11 3 | 21 22 21 24 21 18 17 22 18 20 19
11E | 9 15 7 5 30 5 22 10 7 14 4 | 25 38 34 31 35 31 37 29 31 32 30
12 | 4 12 5 7 39 5 14 10 7 21 3 | 21 26 21 22 38 19 26 20 19 24 21
13 | 9 20 7 9 37 5 22 11 7 19 4 | 15 29 23 19 43 17 27 19 19 19 17
14 | 6 17 9 9 24 3 20 16 6 18 4 | 19 27 25 22 34 20 25 14 18 22 19
15 | 8 21 13 12 26 6 25 14 10 10 5 | 16 26 21 20 30 16 24 17 16 17 15
16 | 5 18 9 10 41 4 16 9 7 32 4 | 14 24 18 20 32 14 21 14 17 14 14
17 | 9 18 6 8 28 5 21 9 10 25 4 | 18 37 29 27 51 25 38 20 24 18 23
18 | 5 21 9 10 38 6 23 8 7 21 4 | 24 37 33 24 42 25 36 23 22 25 25
19 | 5 20 11 12 40 4 23 9 6 21 4 | 14 28 13 16 39 12 28 17 14 21 14
20 | 7 22 6 12 32 5 24 13 7 21 4 | 26 37 32 31 40 28 36 27 30 27 28
21E | 6 22 9 13 44 4 25 8 7 9 4 | 18 29 25 17 40 20 29 17 17 20 18
22 | 6 21 9 9 30 4 22 9 5 28 4 | 24 35 31 25 42 25 33 24 25 31 25
23 | 8 24 8 12 32 5 23 12 6 18 4 | 17 34 29 26 38 21 31 21 23 24 21
X24E | 19 26 17 29 --- 17 --- 22 20 --- 9 | 44 43 35 48 --- 40 --- 39 48 --- 39
25E | 17 26 13 14 --- 9 22 14 17 25 6 | 53 58 57 60 --- 54 59 57 58 66 55
26 | 9 20 8 11 25 3 12 13 7 19 4 | 20 30 21 17 27 18 21 21 14 29 18
27 | 7 21 9 10 22 5 19 13 9 17 4 | 92 96 95 95 97 93 94 94 92 92 94
28 | 7 14 10 7 33 4 16 6 6 30 4 | 29 36 34 33 31 29 34 29 27 29 30
29 | 6 19 8 7 32 3 22 13 6 19 4 | 20 36 30 21 50 24 37 23 23 19 23
30 | 6 11 8 7 22 5 9 14 4 18 3 | 25 27 25 25 33 23 25 24 25 17 23
31 | 5 18 7 7 29 5 16 9 7 16 3 | 22 32 25 22 44 23 28 22 25 27 24
32 | 7 19 7 11 24 5 15 8 6 38 4 | 14 19 21 23 24 16 18 14 15 41 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 9 10 33 5 19 12 8 22 |T 25 35 30 29 39 27 33 27 27 29 26
WRMS | 7 19 9 10 30 5 18 11 6 20 |NE 21 30 25 24 35 22 28 23 22 24 21
MEDI | 7 19 9 10 30 5 18 12 7 19 |MD 20 32 25 25 39 23 28 22 23 24 23
Table 3.1553.1 GPS week: 1553 Day: 1 MJD: 55116.000
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 --- --- 15 --- 15 --- 14 16 --- 8 | 15 --- --- 16 --- 22 --- 17 21 --- 13
2E | 7 19 7 9 34 3 20 16 7 11 4 | 11 24 17 16 28 12 20 14 13 19 14
3 | 7 13 9 12 23 3 15 11 6 22 4 | 11 16 15 20 15 11 14 18 17 17 12
4E | 9 24 13 10 44 6 17 15 25 14 6 | 30 46 36 32 56 31 42 29 32 33 31
5 | 7 23 10 12 27 6 26 15 9 31 5 | 24 39 24 26 41 24 38 23 25 32 23
6 | 5 11 7 10 23 4 14 12 7 23 4 | 14 18 15 19 18 13 18 21 17 20 14
7 | 7 21 9 10 44 5 20 9 8 11 4 | 13 26 18 16 39 13 23 14 12 16 13
8 | 10 18 6 14 48 10 20 14 11 34 5 | 84 90 60 76 62 57 51 138 62 54 83
9 | 6 24 6 12 26 5 17 16 8 15 4 | 38 51 37 40 41 39 49 42 37 41 39
10 | 6 11 8 8 26 5 12 15 8 11 3 | 17 21 17 23 21 16 20 20 19 20 18
11E | 8 17 6 5 47 4 22 11 7 13 4 | 21 27 20 20 37 21 25 20 20 20 19
12 | 7 13 6 7 36 5 15 11 6 21 3 | 12 23 15 18 27 14 22 14 14 17 13
13 | 6 21 7 12 41 6 24 11 6 19 4 | 12 28 17 17 42 13 26 14 13 18 13
14 | 4 16 11 6 25 2 19 11 10 17 4 | 18 27 24 19 35 16 25 14 21 17 19
15 | 8 21 8 9 29 5 25 15 11 11 5 | 16 30 18 23 32 18 29 15 22 17 18
16 | 7 20 9 12 32 4 19 10 8 31 5 | 9 23 15 17 26 10 20 9 12 8 9
17 | 8 24 8 10 30 5 22 10 9 25 5 | 20 42 31 27 52 25 39 20 22 13 24
18 | 6 23 10 12 29 4 26 12 10 20 5 | 20 36 29 21 39 21 36 20 22 21 22
19 | 7 19 8 12 38 3 26 9 7 20 4 | 12 23 13 12 33 10 25 16 15 16 11
20 | 7 23 9 13 28 6 24 13 10 21 5 | 16 31 23 20 36 19 30 17 20 19 18
21E | 6 29 10 14 38 7 29 21 8 10 5 | 20 35 25 26 48 24 32 24 21 19 19
22 | 6 19 8 8 22 4 22 11 7 25 4 | 21 31 26 21 41 21 33 20 22 23 22
23 | 8 27 9 15 33 6 25 10 7 20 5 | 16 31 23 21 34 17 26 14 18 18 16
X24E | 18 27 26 15 --- 10 --- 21 19 --- 9 | 41 42 46 50 --- 41 --- 34 46 --- 38
25E | 18 20 10 15 --- 6 20 14 16 24 6 | 56 54 58 55 --- 54 53 53 56 64 55
26 | 9 15 8 8 28 5 11 13 10 17 4 | 18 25 20 18 29 15 22 21 19 26 18
27 | 12 26 7 10 21 7 19 15 11 16 5 | 104 118 112 109 120 108 113 108 110 110 109
28 | 7 17 8 12 44 5 19 7 14 31 5 | 17 30 23 27 31 19 27 19 22 23 20
29 | 8 20 9 11 43 6 24 10 11 19 4 | 18 31 24 18 47 19 34 17 16 14 18
30 | 8 10 4 5 22 4 9 13 8 14 3 | 14 20 17 19 31 16 21 20 17 12 15
31 | 6 25 7 8 32 6 20 10 11 14 4 | 21 37 25 21 43 20 31 20 27 23 23
32 | 9 22 9 11 18 5 13 8 7 37 5 | 9 18 16 15 22 11 17 10 10 39 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 8 11 33 5 20 13 10 21 |T 24 35 27 27 38 24 32 26 25 26 24
WRMS | 7 20 8 11 31 5 19 12 7 21 |NE 18 29 21 22 34 18 27 22 19 20 19
MEDI | 7 20 8 11 30 5 20 12 8 19 |MD 17 30 23 20 36 19 26 20 20 19 18
Table 3.1553.2 GPS week: 1553 Day: 2 MJD: 55117.000
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 | 20 --- --- 25 --- 16 --- 14 24 --- 12 | 14 --- --- 31 --- 26 --- 20 27 --- 19
2E | 7 21 7 8 32 3 21 9 8 14 4 | 13 24 20 15 30 15 22 13 15 16 13
3 | 7 16 9 14 26 5 13 8 6 23 4 | 15 19 18 24 15 17 19 18 19 17 16
4E | 10 23 12 10 48 7 18 9 23 15 5 | 31 47 36 36 54 33 45 32 31 36 32
5 | 7 23 8 12 36 7 26 10 9 29 5 | 20 40 25 27 44 22 37 22 23 27 22
6 | 6 14 9 10 28 4 13 7 4 24 3 | 16 19 22 22 25 18 20 17 19 21 17
7 | 7 18 8 11 48 7 17 8 8 12 4 | 15 29 18 16 41 16 24 15 16 18 15
X8 | 10 18 7 15 32 7 --- 8 6 27 5 | 49 50 35 48 61 54 --- 62 35 27 48
9 | 7 22 7 12 25 4 19 14 7 17 4 | 37 43 37 37 45 35 45 37 36 37 36
10 | 5 13 6 9 28 7 13 11 8 9 3 | 12 23 17 21 19 16 16 17 18 16 15
11E | 8 15 8 10 41 6 17 6 6 12 3 | 18 26 20 19 40 19 23 18 20 19 17
12 | 10 15 9 8 45 4 15 8 6 20 4 | 15 24 20 24 28 16 23 14 20 16 16
13 | 6 21 8 10 39 5 22 8 5 19 4 | 13 28 19 20 40 15 25 15 12 20 13
14 | 6 18 10 9 27 5 22 9 9 16 4 | 13 25 18 20 36 15 24 14 18 17 16
15 | 12 24 7 10 39 8 26 10 6 9 4 | 18 27 20 22 32 19 26 17 16 18 17
16 | 8 21 11 12 27 4 17 9 7 29 4 | 12 25 17 20 27 11 20 13 14 14 12
17 | 8 20 8 8 38 4 22 11 10 26 5 | 22 42 30 30 55 28 40 25 25 19 25
18 | 6 22 9 12 24 5 25 7 7 19 4 | 20 38 27 25 44 21 35 20 18 16 21
19 | 6 23 10 14 40 3 24 9 7 20 4 | 12 27 12 11 34 11 26 17 12 14 10
20 | 7 21 8 11 26 7 22 9 7 21 4 | 19 32 26 22 38 22 29 20 21 23 21
21E | 7 24 12 9 38 6 23 6 6 8 4 | 18 29 28 19 49 20 30 16 19 20 19
22 | 7 22 9 6 24 5 21 9 6 21 4 | 20 36 26 23 45 21 34 22 22 20 22
23 | 7 30 11 11 31 6 26 8 7 19 5 | 15 32 22 20 34 16 26 16 18 19 16
X24E | 16 36 14 23 --- 16 --- 24 23 --- 9 | 39 42 37 50 --- 38 --- 31 54 --- 37
25E | 13 23 10 13 --- 4 18 12 12 25 5 | 41 53 45 48 --- 43 47 42 43 56 44
26 | 11 14 8 9 25 6 12 13 6 16 4 | 17 21 19 17 26 17 22 22 15 25 17
27E | 19 29 8 11 28 7 26 18 7 20 6 | 64 77 67 65 80 70 75 74 67 64 66
28 | 7 17 10 10 37 4 18 9 10 35 5 | 19 30 29 29 32 21 31 23 16 23 21
29 | 10 19 11 9 33 4 21 8 7 19 4 | 18 31 24 24 46 20 34 20 18 16 19
30 | 9 13 7 7 22 4 9 11 7 18 3 | 19 21 24 26 33 21 22 23 23 19 20
31 | 7 23 11 7 35 5 17 9 8 13 4 | 15 31 16 17 40 16 25 15 19 17 15
32 | 8 21 9 8 23 7 13 5 8 37 4 | 9 19 20 18 29 13 16 12 14 39 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 21 9 10 34 5 20 10 8 21 |T 21 32 25 26 38 23 29 23 23 23 22
WRMS | 8 21 9 10 33 5 19 9 6 19 |NE 17 29 22 23 35 19 26 20 19 20 18
MEDI | 7 21 9 10 32 5 19 9 7 19 |MD 18 29 22 22 38 19 26 18 19 19 17
Table 3.1553.3 GPS week: 1553 Day: 3 MJD: 55118.000
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 --- --- 14 --- 28 --- 12 30 --- 12 | 16 --- --- 19 --- 43 --- 21 44 --- 21
2E | 9 17 8 9 41 5 19 11 10 14 4 | 18 28 24 25 40 20 27 19 22 26 20
3 | 5 13 6 10 28 5 12 8 7 21 3 | 18 19 16 19 18 15 20 18 20 17 14
4E | 9 22 15 9 62 5 17 11 22 14 5 | 32 41 38 31 52 32 43 31 34 36 32
5 | 6 24 6 7 43 5 22 13 10 28 5 | 28 41 34 31 44 28 39 29 28 32 28
6 | 7 12 6 9 29 5 11 7 8 23 3 | 21 20 19 22 16 18 23 20 24 22 18
7 | 7 21 8 9 48 3 16 8 9 14 4 | 14 28 22 20 41 18 26 16 19 21 16
X8 | 8 25 7 14 28 7 --- 10 16 --- 5 | 39 43 20 49 29 79 --- 140 25 --- 38
9 | 20 26 9 11 29 9 18 17 11 19 6 | 62 83 70 72 77 72 84 73 72 75 70
10 | 6 12 8 4 34 3 9 10 12 8 3 | 22 24 26 23 22 20 23 24 22 19 21
11E | 9 17 11 7 48 4 19 8 6 10 4 | 17 24 22 18 47 18 23 16 17 17 16
12 | 7 16 12 10 50 6 17 15 8 20 4 | 17 27 21 22 39 18 28 23 18 20 18
13 | 7 18 7 10 44 3 22 10 8 20 4 | 13 27 19 20 45 15 26 13 17 18 13
14 | 6 13 10 12 37 4 21 12 11 21 4 | 16 24 23 21 40 17 25 18 19 15 16
15 | 10 24 9 8 35 6 23 11 7 13 4 | 16 27 18 20 31 16 26 17 13 19 15
16 | 8 21 9 12 23 6 22 8 8 30 5 | 13 24 22 17 32 15 24 16 18 15 14
17 | 7 25 14 10 43 6 26 9 7 23 5 | 24 41 34 28 58 27 38 23 23 19 25
18 | 6 20 12 13 25 6 24 8 11 20 5 | 21 38 31 25 44 25 37 24 26 23 24
19 | 5 20 8 11 39 8 22 10 9 18 4 | 13 29 14 14 39 11 29 18 15 16 12
20 | 8 18 8 11 30 5 25 12 7 18 4 | 20 30 26 24 40 21 30 18 21 19 19
21E | 6 22 9 11 34 6 22 7 10 9 4 | 14 27 23 15 41 20 28 15 21 19 16
22 | 8 20 9 8 26 5 23 15 8 21 5 | 22 36 30 27 46 25 33 26 25 21 24
23 | 7 24 10 11 35 4 27 11 7 19 5 | 13 30 22 22 34 15 28 13 13 16 13
X24E | 20 32 13 23 --- 8 --- 18 21 --- 9 | 38 38 36 42 --- 38 --- 33 47 --- 35
25E | 14 21 9 13 --- 6 18 16 9 24 5 | 52 58 57 54 --- 53 56 53 53 65 54
26 | 11 16 8 12 29 6 14 17 12 17 5 | 19 25 21 20 34 17 21 26 17 25 17
27E | 11 31 12 12 32 8 25 14 15 23 6 | 134 146 140 135 158 138 145 138 136 135 137
28 | 5 15 10 9 43 7 19 9 12 34 5 | 21 33 27 27 33 24 31 26 18 26 23
29 | 11 21 13 13 41 6 25 8 14 20 5 | 20 36 31 22 43 24 40 27 26 19 24
30 | 8 11 7 8 25 6 11 9 9 15 3 | 20 25 25 23 30 21 26 26 22 23 21
31 | 5 23 5 11 38 5 21 11 9 12 4 | 18 32 21 22 44 19 31 18 23 20 19
32 | 11 18 11 11 18 6 20 7 6 36 5 | 14 19 21 16 23 12 20 15 15 39 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 10 10 37 6 20 11 10 20 |T 25 36 30 29 42 29 35 31 28 28 26
WRMS | 8 20 9 10 37 6 20 11 7 19 |NE 19 29 23 23 35 22 28 25 21 21 19
MEDI | 8 20 9 11 35 6 21 10 9 20 |MD 19 29 23 22 40 20 28 21 22 20 19
Table 3.1553.4 GPS week: 1553 Day: 4 MJD: 55119.000
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 | 12 --- --- 18 --- 20 --- 16 17 --- 9 | 15 --- --- 27 --- 31 --- 22 27 --- 19
2E | 8 18 15 10 31 6 20 16 15 14 5 | 16 27 21 21 29 23 23 21 28 23 19
3 | 7 16 9 15 29 5 14 8 9 23 4 | 16 21 20 24 18 22 17 19 29 19 19
4E | 13 23 14 10 45 5 16 20 27 12 6 | 33 48 37 35 57 37 43 34 38 37 34
5 | 8 25 10 13 40 6 25 12 14 29 6 | 18 37 24 21 44 22 34 19 26 26 20
6 | 6 14 11 12 27 5 12 7 6 23 4 | 19 23 25 25 20 24 20 21 28 23 21
7 | 7 25 11 8 50 5 16 13 7 14 4 | 20 38 26 20 42 26 28 20 27 26 22
9E | 23 27 15 20 27 10 24 19 9 25 7 | 65 75 74 71 80 72 77 75 74 71 69
10 | 6 13 12 8 27 7 11 10 14 12 4 | 15 21 22 18 17 21 19 19 25 20 19
11E | 7 18 13 9 32 6 16 12 8 16 4 | 17 29 20 17 35 23 24 17 27 22 19
12 | 7 18 11 9 49 8 20 12 7 24 4 | 15 28 26 22 35 20 26 20 29 15 20
13 | 5 21 13 15 48 4 24 12 9 20 5 | 15 31 22 16 46 21 26 12 25 23 17
14 | 8 20 16 9 37 7 22 13 7 20 5 | 14 29 19 20 40 18 26 21 23 16 18
15 | 10 20 14 12 36 7 24 12 9 14 5 | 22 31 26 25 33 25 29 20 29 25 23
16 | 8 21 14 18 32 5 20 10 12 32 6 | 13 27 17 24 26 19 22 21 27 16 17
17 | 8 20 11 11 31 6 21 11 14 25 5 | 24 42 34 30 47 31 40 23 34 18 27
18 | 6 24 13 14 25 7 23 9 7 23 5 | 17 36 26 21 40 22 33 20 23 17 20
19 | 6 23 10 11 44 5 23 9 6 20 4 | 17 30 19 10 40 21 28 20 26 19 18
20 | 7 24 13 14 25 6 24 12 8 21 5 | 21 37 28 21 37 26 31 21 28 23 23
21E | 7 23 13 12 29 9 21 10 12 9 5 | 18 30 26 22 33 25 29 18 25 20 18
22 | 7 21 14 10 36 6 22 18 8 25 5 | 18 34 25 21 44 22 30 26 26 16 21
23 | 7 29 15 14 40 5 28 12 7 20 6 | 13 35 22 15 37 19 29 12 20 18 15
X24E | 21 29 11 18 --- 11 --- 22 27 --- 9 | 34 36 31 44 --- 37 --- 32 49 --- 32
25E | 13 23 11 16 --- 5 19 18 12 25 6 | 45 56 53 51 --- 50 53 46 50 61 49
26 | 10 17 14 10 30 6 14 15 6 18 4 | 19 29 22 20 32 22 23 26 26 26 21
27E | 12 29 11 13 51 8 24 15 11 19 6 | 81 94 86 85 90 86 91 84 88 89 86
28 | 8 13 14 10 56 6 17 10 13 36 5 | 22 33 26 25 37 26 32 25 30 27 24
29 | 8 22 17 14 37 6 22 9 13 25 5 | 22 37 30 24 47 28 38 25 30 22 24
30 | 7 16 12 7 27 5 12 9 10 21 4 | 20 32 31 25 29 26 27 27 30 24 25
31 | 7 26 15 11 23 5 20 10 8 17 5 | 20 38 26 18 40 21 29 22 32 21 23
32 | 10 23 14 10 21 5 17 9 7 37 5 | 19 29 25 16 23 22 24 19 25 43 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 21 13 12 36 6 20 13 11 22 |T 23 36 29 26 39 41 32 26 32 27 25
WRMS | 8 21 13 12 38 6 20 11 8 21 |NE 17 31 24 21 35 41 27 20 26 22 20
MEDI | 8 21 13 12 32 6 20 12 9 21 |MD 19 32 26 22 37 23 29 21 28 23 21
Table 3.1553.5 GPS week: 1553 Day: 5 MJD: 55120.000
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 --- --- 15 --- 20 --- 12 14 --- 8 | 20 --- --- 23 --- 26 --- 23 25 --- 20
2E | 7 19 13 11 25 8 21 19 12 19 5 | 21 28 26 23 34 23 26 31 28 27 22
3 | 6 13 9 11 22 5 13 8 8 26 4 | 15 15 13 20 19 15 17 20 16 22 14
4E | 10 21 13 11 55 7 15 18 23 15 6 | 32 46 37 32 60 34 43 34 36 39 33
5 | 9 26 11 12 34 8 25 12 11 31 6 | 27 43 31 27 46 27 39 26 29 31 27
6 | 5 13 9 10 21 5 13 10 8 26 4 | 16 18 14 21 19 16 19 20 18 28 15
7 | 9 24 9 13 47 5 22 13 6 14 5 | 17 33 21 19 42 19 29 17 18 24 18
X8 | 10 26 --- --- 73 56 --- 389 --- --- 16 | 39 51 --- --- 47 129 --- 217 --- --- 42
9E | 11 23 11 21 34 6 21 18 15 24 6 | 58 71 60 62 63 58 70 61 55 66 61
10 | 6 14 8 9 22 8 10 14 11 12 4 | 19 24 23 20 29 18 20 23 20 24 19
11E | 7 17 12 11 36 5 17 10 6 17 4 | 18 25 19 21 30 18 23 21 16 19 17
12 | 7 15 11 9 52 7 15 17 7 26 4 | 20 26 24 18 35 19 25 22 19 19 19
13 | 7 21 13 10 48 4 21 14 7 23 5 | 14 31 23 17 44 17 27 14 16 25 16
14 | 5 18 14 10 28 6 22 15 10 22 5 | 16 30 21 19 33 18 28 23 14 19 18
15 | 8 21 12 9 39 9 23 15 12 14 5 | 18 28 20 17 32 18 26 23 19 26 19
16 | 8 20 14 13 36 5 22 14 7 29 5 | 14 25 16 18 29 14 23 21 12 17 14
17 | 8 22 12 11 27 5 22 13 13 29 5 | 21 44 31 29 49 27 40 22 27 15 26
18 | 6 19 11 13 21 5 22 8 7 27 5 | 20 37 28 23 41 23 35 22 20 26 22
19 | 6 21 9 13 43 4 25 10 9 22 5 | 12 26 11 12 38 13 28 17 16 16 12
20 | 7 24 11 11 26 6 26 11 7 23 5 | 19 33 26 24 38 22 30 20 25 22 22
21E | 7 26 12 12 24 6 21 10 10 12 5 | 17 33 22 21 36 19 27 18 18 22 17
22 | 7 22 12 10 23 6 23 19 8 29 5 | 18 36 26 21 40 23 33 26 21 21 21
23 | 6 28 14 12 35 4 26 12 6 22 5 | 15 31 23 18 35 17 27 15 17 21 17
X24E | 15 27 20 25 149 22 --- 20 42 --- 11 | 35 35 28 48 9999 33 --- 30 63 --- 34
25E | 11 22 10 13 --- 5 19 20 11 26 5 | 53 57 58 56 --- 53 55 54 54 63 54
26 | 8 17 11 7 27 8 11 12 8 25 4 | 15 31 19 17 27 19 23 23 13 27 17
27E | 9 24 9 16 54 10 23 18 11 21 5 | 124 136 130 125 136 127 134 127 125 131 127
28 | 7 16 8 9 43 6 17 10 11 36 5 | 19 31 25 26 35 23 30 22 22 23 21
29 | 9 19 9 12 49 6 22 11 8 22 5 | 20 35 27 21 51 24 38 24 21 18 22
30 | 8 12 8 10 33 5 10 12 7 19 3 | 21 24 22 19 27 18 22 23 20 18 19
31 | 9 25 13 8 32 7 24 14 9 15 5 | 23 37 22 22 45 22 32 24 23 25 23
32 | 9 21 12 10 20 5 12 10 6 37 5 | 12 18 18 16 24 14 18 14 15 41 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 11 11 36 6 20 14 10 24 |T 25 36 28 27 40 29 34 33 27 30 26
WRMS | 7 20 11 11 33 6 19 13 7 25 |NE 18 30 22 20 35 24 27 29 19 23 19
MEDI | 8 21 11 11 34 6 21 13 9 23 |MD 19 31 23 21 36 19 28 23 20 24 19
Table 3.1553.6 GPS week: 1553 Day: 6 MJD: 55121.000
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 --- --- 23 --- 23 --- 16 22 --- 11 | 20 --- --- 23 --- 34 --- 27 34 --- 23
2E | 7 19 7 9 29 5 23 27 9 15 5 | 18 29 22 21 32 21 27 28 23 23 20
3 | 7 13 8 10 18 3 12 15 11 29 4 | 18 18 18 26 19 20 17 26 23 24 17
4E | 11 22 9 11 49 5 15 24 21 14 6 | 30 43 34 33 53 31 42 31 37 36 32
5 | 6 24 9 17 30 7 24 14 9 33 6 | 23 39 27 28 45 24 38 23 26 30 24
6 | 6 14 6 10 18 3 12 16 9 28 4 | 20 18 18 26 21 20 18 26 22 27 18
7 | 11 20 9 11 42 4 17 18 7 16 5 | 23 30 22 18 35 19 29 19 23 22 20
X8 | 29 55 --- 65 31 43 --- 27 --- --- 26 | 44 58 --- 51 40 82 --- 103 --- --- 35
9E | 13 24 9 14 54 11 20 19 14 21 6 | 83 91 82 81 89 78 91 84 80 84 81
10 | 8 11 5 8 22 6 11 25 9 17 4 | 18 19 18 19 22 15 17 26 18 19 15
11E | 9 15 5 12 40 5 14 13 7 18 4 | 23 25 22 28 38 22 23 26 23 21 20
12 | 7 16 9 10 41 6 17 12 8 28 4 | 20 27 24 25 32 20 26 27 19 24 22
13 | 7 18 9 13 46 3 20 13 7 26 4 | 14 29 21 19 46 16 26 16 16 27 16
14 | 5 17 9 11 28 4 22 17 7 23 4 | 17 28 21 22 36 17 27 19 16 19 18
15 | 6 21 10 10 47 5 24 17 8 16 5 | 16 25 19 22 39 18 24 23 18 25 17
16 | 8 18 10 14 38 5 21 19 12 30 5 | 15 21 17 20 30 14 23 25 14 17 13
17 | 7 22 9 11 34 6 22 15 7 26 5 | 21 40 28 27 51 25 39 21 22 18 24
18 | 6 20 7 10 24 2 22 8 10 29 5 | 19 33 26 22 40 21 33 22 22 25 21
19 | 7 20 7 11 37 4 26 12 10 29 5 | 17 28 14 13 42 15 30 23 20 19 15
20 | 7 21 10 12 29 5 25 12 7 22 5 | 21 29 24 23 37 21 31 21 22 22 20
21E | 7 18 9 10 44 6 23 8 8 12 4 | 19 27 22 20 56 18 28 17 17 20 17
22 | 6 19 8 10 23 3 22 16 8 30 5 | 20 32 27 23 40 21 32 24 20 21 22
23 | 7 24 12 12 41 4 23 13 8 25 5 | 14 29 22 19 35 17 28 14 19 21 16
X24E | 19 32 19 26 >>>> 16 --- 21 31 --- 11 | 42 53 45 49 912 46 --- 40 62 --- 43
25E | 12 19 9 15 --- 4 14 24 10 27 5 | 67 67 68 73 --- 70 67 69 67 77 69
26 | 8 14 8 6 23 3 10 12 8 32 4 | 18 26 21 18 26 18 22 20 17 28 18
27E | 8 19 7 14 60 6 18 20 13 19 5 | 123 132 125 116 130 122 133 125 124 120 122
28 | 8 17 8 10 30 5 17 11 6 36 5 | 24 32 31 32 37 25 29 25 24 27 26
29 | 8 18 9 8 30 7 22 11 10 25 5 | 24 36 28 22 46 27 41 27 25 25 25
30 | 8 16 8 8 33 6 11 14 6 21 4 | 25 26 24 26 28 22 25 30 25 23 24
31E | 15 19 12 9 33 7 20 20 10 15 5 | 46 48 49 42 61 39 48 38 39 39 41
32 | 7 18 8 8 22 5 14 13 8 39 5 | 11 18 16 14 20 12 19 12 12 40 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 9 11 36 5 19 17 10 25 |T 28 37 31 31 71 30 35 33 29 31 28
WRMS | 7 19 8 11 34 5 18 15 7 25 |NE 20 29 22 23 34 22 27 26 20 23 20
MEDI | 7 19 9 11 33 5 20 15 9 25 |MD 20 29 22 23 38 21 28 25 22 24 20
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1553 GPS week: 1553 MJD: 55115.0-55121.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 |U 9 9 25 |U 7 10 24 |U 7 8 19 |
emr | emr 2934 | 16 15 39 |U 11 11 35 | 8 9 21 |
esa | esa 2934 | 12 12 32 |U 7 9 24 | 6 6 18 |
gfz | gfz 2984 |U 18 18 38 |U 16 21 40 | 9 9 23 |
grg | grg 2811 | 14 13 38 |U 10 12 31 | 8 7 21 |
igr | igr 3000 | 12 12 36 | 9 10 26 | 7 8 19 |
igs | igs 2957 | 13 13 33 | 10 12 29 | 7 8 19 |
jpl | jpl 2799 | 15 16 40 |U 12 12 31 |U 8 8 21 |
mit | mit 3058 |U 12 12 37 |U 12 12 38 |U 16 12 35 |
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 5.1553.0 GPS week: 1553 Day: 0 MJD: 55115.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 10 9 31 | 8 12 32 | 6 8 21 |
emr | emr 2954 | 14 12 40 | 11 9 35 | 7 9 22 |
esa | esa 2976 | 11 10 35 | 8 11 30 | 8 8 23 |
gfz | gfz 3047 | 11 11 29 | 14 11 30 | 9 17 37 |
grg | grg 2784 | 10 12 36 | 9 12 34 | 7 10 27 |
igr | igr 3032 | 11 10 33 | 11 10 31 | 6 7 20 |
igs | igs 3023 | 12 10 33 | 11 12 31 | 6 7 20 |
jpl | jpl 2875 | 12 11 39 | 13 11 36 | 7 7 23 |
mit | mit 3072 | 10 10 41 | 11 12 43 | 7 8 18 |
Table 5.1553.1 GPS week: 1553 Day: 1 MJD: 55116.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 | 8 6 26 | 5 9 23 | 6 7 20 |
emr | emr 2953 | 9 9 30 | 9 7 34 | 7 7 22 |
esa | esa 2976 | 8 7 26 | 5 8 23 | 5 5 16 |
gfz | gfz 3044 | 11 10 35 | 13 18 32 | 7 6 16 |
grg | grg 2784 | 9 9 32 | 12 11 32 | 7 5 20 |
igr | igr 3057 | 8 9 26 | 5 7 19 | 5 6 16 |
igs | igs 2959 | 8 6 27 | 10 10 33 | 6 7 17 |
jpl | jpl 2872 | 9 10 27 | 7 9 34 | 7 6 18 |
mit | mit 3072 | 10 9 34 | 10 10 40 | 8 6 15 |
Table 5.1553.2 GPS week: 1553 Day: 2 MJD: 55117.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 9 12 18 | 9 8 26 | 6 9 18 |
emr | emr 2951 | 14 15 33 | 11 14 39 | 9 9 21 |
esa | esa 2976 | 11 15 25 | 9 7 25 | 6 6 17 |
gfz | gfz 2846 | 24 26 47 | 22 46 65 | 8 6 17 |
grg | grg 2784 | 14 14 53 | 12 19 37 | 8 5 19 |
igr | igr 3025 | 11 12 48 | 10 11 31 | 5 6 16 |
igs | igs 2959 | 8 12 30 | 10 14 31 | 7 7 18 |
jpl | jpl 2775 | 14 22 43 | 10 11 28 | 8 8 22 |
mit | mit 3072 | 12 17 38 | 10 14 33 | 8 9 14 |
Table 5.1553.3 GPS week: 1553 Day: 3 MJD: 55118.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 9 10 25 | 9 11 25 | 7 7 19 |
emr | emr 2962 | 15 12 33 | 10 13 35 | 9 14 20 |
esa | esa 2976 | 10 12 27 | 9 13 26 | 6 7 15 |
gfz | gfz 3031 | 17 18 39 | 16 17 38 | 9 8 19 |
grg | grg 2784 | 9 9 32 | 12 16 33 | 8 9 19 |
igr | igr 2966 | 11 15 39 | 13 14 30 | 7 8 16 |
igs | igs 3067 | 10 10 37 | 11 13 26 | 7 8 16 |
jpl | jpl 2772 | 15 16 48 | 14 15 33 | 9 10 20 |
mit | mit 3072 | 15 13 47 | 14 17 34 | 7 8 16 |
Table 5.1553.4 GPS week: 1553 Day: 4 MJD: 55119.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2943 | 8 6 16 | 6 10 18 | 6 4 16 |
emr | emr 2850 | 16 14 36 | 10 12 33 | 8 8 18 |
esa | esa 2880 | 10 10 25 | 5 9 15 | 6 4 19 |
gfz | gfz 2954 | 16 19 35 | 14 10 24 | 8 8 26 |
grg | grg 2784 | 13 14 23 | 8 8 20 | ---- ---- ---- |
igr | igr 2957 | 9 8 21 | 5 8 12 | 7 10 20 |
igs | igs 2930 | 13 15 22 | 8 10 18 | 8 11 24 |
jpl | jpl 2769 | 12 13 27 | 11 10 17 | 6 7 18 |
mit | mit 2976 | 14 14 33 | 12 10 34 | 8 10 23 |
Table 5.1553.5 GPS week: 1553 Day: 5 MJD: 55120.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 | 10 7 30 | 5 7 17 | 7 9 21 |
emr | emr 2941 | 16 15 42 | 10 9 30 | 9 9 24 |
esa | esa 2880 | 12 11 40 | 5 6 16 | 7 9 24 |
gfz | gfz 2949 | 20 19 37 | 17 13 33 | 10 11 29 |
grg | grg 2880 | 12 11 39 | 6 8 23 | ---- ---- ---- |
igr | igr 2949 | 11 9 39 | 8 8 25 | 8 7 22 |
igs | igs 2842 | 12 11 35 | 9 8 24 | 8 10 23 |
jpl | jpl 2770 | 14 12 43 | 13 12 34 | 8 9 23 |
mit | mit 3072 | 13 8 37 | 9 9 32 | 62 33 139 |
Table 5.1553.6 GPS week: 1553 Day: 6 MJD: 55121.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 12 13 28 | 9 15 29 | 11 12 17 |
emr | emr 2927 | 29 29 58 | 16 16 39 | 10 10 21 |
esa | esa 2880 | 26 21 49 | 10 12 32 | 6 6 16 |
gfz | gfz 3020 | 27 26 47 | 17 32 55 | 10 8 20 |
grg | grg 2880 | 32 24 52 | 11 11 40 | ---- ---- ---- |
igr | igr 3016 | 25 22 47 | 12 13 35 | 12 15 24 |
igs | igs 2920 | 27 23 51 | 14 16 40 | 8 7 16 |
jpl | jpl 2760 | 28 25 51 | 14 14 35 | 9 9 21 |
mit | mit 3072 | 11 10 32 | 15 13 48 | 12 9 22 |
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 6.1553 GPS week: 1553 MJD: 55115.500-55121.500
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 11 67 -62 -6 | 13 18
| 29 27 91 115 3 | 2
emr uuuuu | -48 12 89 -252 8 | 59 61
| 43 17 63 136 7 | 4
esa uuuuu | 1 -41 70 178 15 | 10 25
| 58 32 171 128 9 | 3
gfz uuuuu | 20 20 -43 12 -1 | 2 12
| 20 21 38 48 6 | 2
grg xxxxx | -84 -26 93 -58 -10 | 1 26
| 55 61 112 116 27 | 7
igr xxxxx | -35 22 90 -19 -2 | -3 12
| 39 25 105 86 9 | 1
irf xxxxx | -7 7 -25 35 1 | -5 14
| 14 6 31 27 2 | 2
jpl uuuuu | -33 -18 164 -114 -11 | 23 26
| 22 32 167 169 11 | 2
mit uuuuu | 3 24 -228 181 -6 | 10 16
| 24 15 88 79 4 | 3
ngs uuuuu | -2 2 135 -56 0 | 1 11
| 52 51 60 37 4 | 1
sio uuuuu | 69 11 -242 -292 11 | 28 33
| 32 17 97 78 3 | 3
Table 7.1553.0 GPS week: 1553 Day: 0 MJD: 55115.500
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 | -61 3 78 -230 -2 | 16 20
emr uuuuu | -17 31 65 -96 16 | 58 60
esa uuuuu | -61 -17 -27 140 -3 | 9 24
gfz uuuuu | 37 35 -8 -17 2 | 0 10
grg xxxxx | -69 -84 169 -159 -42 | 12 29
igr xxxxx | -46 22 15 23 -8 | -1 10
irf xxxxx | -28 9 -32 -8 -1 | -3 13
jpl uuuuu | -29 -11 200 24 -2 | 26 28
mit uuuuu | -14 33 -230 55 -5 | 15 20
ngs uuuuu | 48 -41 139 -17 -1 | 3 11
sio uuuuu | 24 4 -188 -392 10 | 30 35
Table 7.1553.1 GPS week: 1553 Day: 1 MJD: 55116.500
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 | -43 34 125 -93 -4 | 13 19
emr uuuuu | 13 4 108 -122 15 | 55 57
esa uuuuu | -55 -37 -55 54 15 | 8 24
gfz uuuuu | 33 47 7 -71 5 | -1 11
grg xxxxx | -55 -49 149 -153 -7 | 6 32
igr xxxxx | -32 -20 75 -16 -6 | -3 12
irf xxxxx | -3 10 -24 52 -2 | -6 14
jpl uuuuu | -61 -10 365 64 -8 | 25 27
mit uuuuu | 15 42 -214 167 -12 | 12 18
ngs uuuuu | 22 -29 102 -32 -3 | 1 11
sio uuuuu | 64 4 -226 -224 7 | 27 31
Table 7.1553.2 GPS week: 1553 Day: 2 MJD: 55117.500
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 | -23 -5 87 -165 -7 | 13 19
emr uuuuu | -35 17 200 -200 12 | 56 58
esa uuuuu | -45 -81 -106 38 19 | 8 25
gfz uuuuu | 27 23 -78 61 4 | 1 11
grg xxxxx | -61 -22 111 27 -24 | 4 31
igr xxxxx | -56 18 38 39 -16 | -3 12
irf xxxxx | -25 2 -4 3 3 | -6 14
jpl uuuuu | -47 -46 304 33 -23 | 26 27
mit uuuuu | -35 21 -93 105 -7 | 10 17
ngs uuuuu | 69 41 75 -22 -3 | 1 11
sio uuuuu | 30 4 -95 -321 13 | 26 30
Table 7.1553.3 GPS week: 1553 Day: 3 MJD: 55118.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -2 56 140 -20 -2 | 11 16
emr uuuuu | -73 31 107 -366 11 | 57 58
esa uuuuu | 69 -89 195 189 24 | 6 21
gfz uuuuu | -20 26 -50 39 0 | 1 11
grg xxxxx | -116 95 -136 -97 -11 | -2 27
igr xxxxx | -104 20 -6 -194 -2 | -6 12
irf xxxxx | -6 -2 19 56 4 | -8 14
jpl uuuuu | -22 -27 -147 -302 -17 | 23 25
mit uuuuu | -12 6 -135 264 -4 | 8 14
ngs uuuuu | -26 60 68 -97 -3 | 0 10
sio uuuuu | 75 -6 -180 -213 15 | 25 29
Table 7.1553.4 GPS week: 1553 Day: 4 MJD: 55119.500
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 | -45 -21 -92 126 -8 | 13 18
emr uuuuu | -121 -17 76 -430 6 | 60 62
esa uuuuu | 76 -25 366 391 21 | 10 25
gfz uuuuu | 9 -20 -92 37 1 | 3 12
grg xxxxx | -195 -84 36 -77 14 | -8 20
igr xxxxx | -21 25 234 -60 1 | -4 12
irf xxxxx | 5 6 -24 57 1 | -5 14
jpl uuuuu | -49 -60 88 -357 -24 | 23 25
mit uuuuu | 10 14 -289 268 -7 | 9 15
ngs uuuuu | -34 56 140 -108 2 | 1 11
sio uuuuu | 107 1 -353 -202 8 | 28 33
Table 7.1553.5 GPS week: 1553 Day: 5 MJD: 55120.500
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 | 26 17 -22 -44 -7 | 14 18
emr uuuuu | -62 14 -9 -378 -1 | 64 66
esa uuuuu | 25 -8 146 299 19 | 15 29
gfz uuuuu | 35 8 -64 50 -5 | 5 13
grg xxxxx | -34 -27 136 166 34 | -4 21
igr xxxxx | 21 26 246 45 15 | -2 12
irf xxxxx | 8 18 -32 31 1 | -3 14
jpl uuuuu | 7 37 213 -171 -12 | 22 25
mit uuuuu | 35 43 -310 190 -4 | 10 16
ngs uuuuu | -83 -69 185 -76 4 | 3 12
sio uuuuu | 104 41 -350 -321 10 | 31 36
Table 7.1553.6 GPS week: 1553 Day: 6 MJD: 55121.500
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 -7 155 -9 -10 | 11 16
emr uuuuu | -45 6 77 -172 -2 | 64 66
esa uuuuu | -3 -29 -33 135 8 | 14 28
gfz uuuuu | 20 23 -17 -16 -13 | 4 13
grg xxxxx | -59 -10 184 -110 -33 | 0 21
igr xxxxx | -11 65 28 31 -1 | -3 12
irf xxxxx | -2 6 -81 51 1 | -5 14
jpl uuuuu | -34 -5 125 -89 7 | 19 23
mit uuuuu | 21 12 -324 218 -1 | 7 14
ngs uuuuu | -11 -2 236 -42 5 | 1 10
sio uuuuu | 76 28 -305 -369 12 | 32 36
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