[IGSREPORT-20299] Wk 1659 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Nov 10 06:02:43 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1659 (Oct 23, 2011 - Oct 29, 2011)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1659[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1659[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1659[0-6].cls IGS GPS clock combination summary report.
igs16597.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16597.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 of poorer consistency (GRG),
they provide broadcast clocks (NGS), or clock corrections are not provided
(SIO). The clock information not used is still compared to combination for
completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
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 | EMR | 8
0 | ESA | CEDU CEDU KOUR
0 | GFZ | MDVJ SFER
0 | GRG | KOUR NRC1
0 | JPL | 3 8 CAS1
0 | MIT | 20 21 27 20 21 27 DAV1 NNOR
1 | EMR | 8 8
1 | GFZ | SFER WSRT
1 | GRG | AMC2
1 | JPL | 8
1 | MIT | 27 3 27 MAW1
2 | COD | MAC1
2 | EMR | 8 8 KERG YELL KERG YELL
2 | ESA | NICO NICO
2 | GFZ | 19 CHUR MCM4 PERT
2 | GRG | AMC2
2 | JPL | 8 YELL
2 | MIT | 1 19 27 1 19 27
3 | COD | WROC SOFI WROC
3 | EMR | 8 8
3 | ESA | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
3 | ESA | 21 22 23 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7 8
3 | ESA | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 25 26
3 | ESA | 27 28 29 30 31 32 KOUR
3 | GFZ | HARB MDVJ
3 | GRG | AMC2 KOUR NKLG
3 | JPL | 8 BRUS
3 | MIT | 14 27 14 27 DAV1 GUAT KOSG
4 | ESA | RAMO
4 | GFZ | MDVJ WAB2
4 | GRG | AMC2 SANT
4 | MIT | 27 27 KOSG KOSG KOUR
5 | COD | 21
5 | EMR | 21
5 | GFZ | 8 KOSG MDVJ
5 | GRG | SANT USN3
5 | JPL | 8
5 | MIT | 27 27 GUAT GUAT
6 | COD | 27
6 | EMR | 8
6 | GFZ | 30 KOSG KOUR MDVJ SYOG
6 | GRG | USN3
6 | MIT | 27 27 CAS1 BOR1 GUAT KOSG KOUR
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
----+--------+---------------
0 | SIO | ALL (high Transformation - See Table 2)
1 | SIO | ALL (high Transformation - See Table 2)
3 | SIO | ALL (high Transformation - See Table 2)
4 | SIO | ALL (high Transformation - See Table 2)
5 | SIO | ALL (high Transformation - See Table 2)
6 | SIO | ALL (high Transformation - See Table 2)
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) 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. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
7. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | -.1 .4 -.1 -39 -2 23 .08
EMR | 6.5 6.0 6.4 -19 27 -26 .29
ESA | 6.0 3.2 -1.0 90 -198 179 .03
GFZ | -.7 1.0 -.1 -27 0 4 .05
GRG | 6.6 1.7 14.4 -18 29 -2 .14
JPL | 1.2 6.3 17.4 40 -49 50 .35
MIT | 5.9 3.7 8.2 -28 12 -28 .16
NGS | 6.7 -.1 5.7 -19 -34 31 .44
SIO | 8.4 5.1 -5.6 86 -201 26 .09
8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
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 1.1659.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1659.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 2.1659.[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 3.1659.[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 5.1659.0-6).
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 1659 summary. (Oct 23, 2011 - Oct 29, 2011)
Table 1.1659.a GPS week: 1659 MJD: 55857.000-55863.000
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 256| 0 0 1 80 -39 -9 -.30 10 9 | -80 -500 20 90
| 0 0 1 14 11 14 .02 | 491 1125
emr 92| 2 1 0 28 -117 -11 .42 20 20 | 3169 -288 14 140
| 1 1 2 30 15 10 .04 | 1147 1110
esa 146| 0 0 3 -96 163 40 .18 9 9 | -1649 1032 21 194
| 0 0 1 13 7 16 .03 | 790 1722
gfz 199| -1 0 -3 -8 -78 0 -.23 11 11 | 234 -53 22 101
| 0 1 1 38 58 9 .05 | 262 181
grg 129| 2 1 3 15 -79 -16 .55 19 18 | 1428593 -274 50 235
| 0 0 1 10 18 13 .08 | 3779634 435
igr n/a| 0 0 0 -6 -45 -62 -.16 5 5 | -6862 -1382 18 85
| 0 0 0 23 17 11 .03 | 2590 951
jpl 142| 0 0 0 -95 64 20 .57 15 15 | 3641 -299 19 95
| 0 1 0 15 15 11 .02 | 934 1079
mit 257| 0 -1 -4 10 -95 -54 -.37 15 13 | -260 -56 22 199
| 0 0 0 14 25 13 .07 | 217 581
ngs 222| 1 0 0 55 2 -7 -.19 11 9 | 55063 19932 1775 3620
| 0 1 1 32 18 13 .03 | 145928 54133
sio 253| -1 1 -6 -170 354 -12 -.34 22 21 | --- --- --- ---
| 1 1 1 25 46 5 .03 | --- ---
Table 1.1659.b GPS week : 1659 MJD: 55857.000-55863.000
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 | 5 6 5 6 5 5 5 |
2 | 5 5 5 5 5 4 4 |
3 | 4 4 5 5 4 4 3 |
4 | 5 5 4 4 4 4 4 |
5 | 5 5 4 6 6 6 6 |
6 | 4 4 4 4 4 4 3 |
7 | 5 5 4 6 5 5 5 |
8 | 6 7 6 7 8 7 6 |
9 | 5 6 5 5 5 5 5 |
10 | 5 5 4 5 5 5 4 |
11 | 5 4 4 5 5 5 4 |
12 | 5 5 5 5 5 6 5 |
13 | 4 5 5 5 5 5 5 |
14 | 5 5 4 5 5 5 5 |
15 | 5 5 4 5 5 5 4 |
16 | 6 5 5 5 6 5 4 |
17 | 5 5 5 5 5 5 5 |
18 | 6 6 5 7 6 6 5 |
19 | 4 4 4 5 4 4 4 |
20 | 5 5 4 5 5 5 4 |
21 | 5 5 4 5 5 5 4 |
22 | 5 5 4 5 5 6 4 |
23 | 5 5 5 5 5 5 5 |
25 | 5 5 4 5 4 5 4 |
26 | 4 4 5 4 4 4 4 |
27 | 9 8 8 10 11 13 12 |
28 | 5 5 4 6 5 5 5 |
29 | 4 5 5 5 5 5 5 |
30 | 5 5 4 6 5 5 5 |
31 | 5 5 5 6 7 6 5 |
32 | 5 5 5 5 5 6 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 2.1659.0 GPS week: 1659 Day: 0 MJD: 55857.000
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 256| 0 0 0 67 -49 -4 -.32 9 9 | -266 -80 22 81
| 27 -24 |
emr 92| 1 3 0 35 -119 -4 .47 20 20 | 2963 -810 14 150
| -39 -13 |
esa 146| 1 0 3 -104 165 42 .23 10 10 | -2974 3821 17 173
| 55 31 |
gfz 199| -1 0 -3 0 13 2 -.23 10 10 | -44 256 23 99
| 29 16 |
grg 129| 2 0 1 9 -79 -7 .62 15 14 | 9999999 210 38 256
| 38 -49 |
igr n/a| 0 -1 0 -4 -19 -72 -.14 5 5 | -2980 -2032 18 67
| -38 -4 |
jpl 142| 0 -1 0 -110 48 34 .60 17 16 | 3601 -754 18 89
| 74 -22 |
mit 257| 0 -2 -4 19 -54 -67 -.47 14 13 | -511 768 20 189
| -16 14 |
ngs 222| 0 0 0 21 -31 -14 -.19 12 9 | 385997 142673 1691 3900
| -42 41 |
sio 253| -2 0 -8 -194 386 -20 -.32 22 21 | --- --- --- ---
| 74 -191 |
Table 2.1659.1 GPS week: 1659 Day: 1 MJD: 55858.000
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 256| 0 1 -1 87 -34 -2 -.32 10 9 | 1014 -3017 20 102
| 27 -39 |
emr 92| 2 0 0 59 -111 0 .46 21 21 | 1751 -163 12 144
| -5 -18 |
esa 146| 0 0 3 -119 151 43 .14 9 9 | -1119 -1027 15 184
| 50 19 |
gfz 199| -2 0 -2 -25 -74 8 -.26 10 11 | 641 -13 25 112
| -3 3 |
grg 129| 1 1 2 26 -68 -11 .65 15 15 | -57 -863 43 216
| 0 -81 |
igr n/a| 0 0 -1 22 -53 -72 -.19 5 5 | -5298 -1376 18 75
| -18 25 |
jpl 142| 0 0 0 -82 80 6 .58 16 16 | 2526 -37 18 93
| 75 -38 |
mit 257| 0 -1 -2 -1 -97 -69 -.44 14 13 | -101 -1093 32 233
| 14 26 |
ngs 222| 1 0 0 87 11 -14 -.21 11 8 | 867 -2828 1815 4068
| -64 -14 |
sio 253| -2 1 -7 -201 338 -12 -.37 22 20 | --- --- --- ---
| 76 -176 |
Table 2.1659.2 GPS week: 1659 Day: 2 MJD: 55859.000
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 256| 0 2 1 108 -54 -29 -.30 10 9 | -357 105 19 85
| 63 -36 |
emr 92| 0 2 0 70 -113 -13 .44 19 19 | 1922 2140 12 129
| 12 -50 |
esa 146| 0 0 3 -102 171 62 .19 7 7 | -1942 1648 14 171
| 53 15 |
gfz 199| -2 0 -1 -51 -160 -1 -.26 9 9 | 128 -277 21 110
| 33 26 |
grg 129| 1 0 1 22 -117 -18 .60 16 15 | -469 237 52 219
| 18 -83 |
igr n/a| 0 0 0 26 -46 -71 -.12 5 5 | -6469 351 17 82
| -5 12 |
jpl 142| -1 0 0 -86 44 18 .60 15 15 | 2795 1994 20 112
| 103 -66 |
mit 257| 1 -1 -4 36 -115 -50 -.39 14 13 | -553 170 24 184
| 19 27 |
ngs 222| 1 -2 -1 110 26 -25 -.22 10 8 | -393 118 1932 3481
| -91 24 |
sio 253| 0 0 -7 -131 292 -8 -.37 21 19 | --- --- --- ---
| 52 -175 |
Table 2.1659.3 GPS week: 1659 Day: 3 MJD: 55860.000
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 256| 0 0 1 81 -44 10 -.32 10 9 | -132 -170 30 98
| -12 -54 |
emr 92| 3 0 0 35 -92 -19 .39 19 19 | 4791 -993 14 115
| 11 -67 |
esa 146| -1 -1 2 -80 169 44 .19 9 9 | -1212 1621 54 128
| 40 37 |
gfz 199| 0 2 -2 -41 -102 -10 -.29 13 13 | 262 -24 23 94
| 34 39 |
grg 129| 1 0 3 24 -86 -29 .48 20 19 | 512 -789 56 264
| 17 -94 |
igr n/a| 0 0 -1 -10 -53 -50 -.15 5 5 | -5664 -2595 23 112
| -6 14 |
jpl 142| 0 3 1 -75 61 23 .55 15 14 | 5204 -1319 24 99
| 67 -67 |
mit 257| 0 -1 -3 -4 -120 -50 -.34 15 13 | 51 -310 19 169
| 17 42 |
ngs 222| 0 -1 -1 51 14 -9 -.16 12 9 | -189 -89 1658 3429
| -51 -8 |
sio 253| 0 1 -6 -183 320 -11 -.35 23 23 | --- --- --- ---
| 44 -185 |
Table 2.1659.4 GPS week: 1659 Day: 4 MJD: 55861.000
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 256| 0 0 1 70 -45 -1 -.29 9 8 | -385 -15 15 89
| 20 -80 |
emr 92| 3 2 0 -11 -111 -30 .37 19 19 | 4399 -489 17 151
| 9 -37 |
esa 146| 0 0 5 -90 160 53 .16 10 9 | -2134 1877 18 250
| 46 46 |
gfz 199| -2 1 -5 27 -38 -10 -.22 12 11 | -19 1 22 98
| -18 29 |
grg 129| 3 1 5 10 -65 -37 .54 21 19 | 53 -171 54 238
| 41 -96 |
igr n/a| 0 0 0 -27 -72 -69 -.14 4 4 | -7587 -1582 18 91
| 3 -4 |
jpl 142| -1 -2 0 -103 59 23 .55 15 14 | 4497 -657 18 93
| 65 -159 |
mit 257| 1 -2 -4 -1 -122 -63 -.32 17 15 | -192 224 22 192
| 14 42 |
ngs 222| 1 0 -2 31 -4 0 -.14 12 9 | -404 -7 1723 3483
| -22 -11 |
sio 253| -2 1 -5 -152 327 -8 -.37 23 22 | --- --- --- ---
| 41 -215 |
Table 2.1659.5 GPS week: 1659 Day: 5 MJD: 55862.000
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 256| 0 0 1 84 -27 -10 -.28 10 9 | -283 112 21 88
| 25 -25 |
emr 92| 1 0 1 1 -133 -4 .42 18 18 | 3446 -1011 18 153
| 54 -12 |
esa 146| 0 0 2 -87 155 11 .17 11 10 | -1607 137 17 215
| 27 82 |
gfz 199| -3 1 -3 -21 -58 14 -.16 12 12 | 526 -268 22 94
| 7 40 |
grg 129| 4 0 3 -2 -68 1 .43 24 21 | 24 -376 54 242
| 54 -67 |
igr n/a| 0 0 0 -34 -44 -53 -.15 5 5 | -9425 -1694 17 68
| 32 10 |
jpl 142| 0 0 0 -91 77 29 .56 14 13 | 3539 -778 17 91
| 114 -39 |
mit 257| 0 -2 -4 11 -81 -47 -.30 14 12 | -319 -275 19 215
| 22 28 |
ngs 222| 1 1 0 53 4 0 -.21 11 8 | -302 106 1898 3641
| -52 42 |
sio 253| 0 2 -6 -155 418 -6 -.32 22 20 | --- --- --- ---
| 48 -244 |
Table 2.1659.6 GPS week: 1659 Day: 6 MJD: 55863.000
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 256| 0 0 2 65 -23 -27 -.28 9 9 | -155 -441 17 93
| 59 -67 |
emr 92| 3 3 5 9 -138 -10 .41 20 20 | 2913 -691 16 144
| 19 13 |
esa 146| 0 0 0 -88 168 27 .20 8 8 | -555 -849 18 240
| 60 35 |
gfz 199| -1 2 -4 54 -129 3 -.19 9 9 | 144 -48 21 102
| -18 43 |
grg 129| 2 1 5 18 -70 -14 .49 24 21 | 89 -171 53 216
| 20 -61 |
igr n/a| 0 0 0 -15 -29 -46 -.19 5 5 | -10613 -747 20 100
| 4 17 |
jpl 142| 0 0 0 -116 79 3 .55 14 13 | 3329 -546 19 88
| 98 -91 |
mit 257| 0 -2 -4 16 -75 -30 -.32 13 11 | -198 120 21 214
| -1 27 |
ngs 222| 1 0 0 34 -3 14 -.18 11 8 | -131 -443 1710 3339
| 36 11 |
sio 253| -2 2 -6 -172 397 -18 -.30 20 18 | --- --- --- ---
| 44 -228 |
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 3.1659.0 GPS week: 1659 Day: 0 MJD: 55857.000
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 | 9 18 9 8 --- 7 18 17 14 14 5 | 63 68 64 62 --- 64 67 63 65 59 63
2 | 8 21 6 9 17 5 16 13 7 32 4 | 25 40 34 26 41 30 39 30 31 32 30
3 | 10 11 10 7 11 5 12 13 12 33 4 | 18 22 20 15 26 14 26 16 15 29 16
4 | 12 20 6 7 12 6 10 20 9 20 4 | 17 26 13 16 19 16 18 15 12 16 12
5 | 8 18 10 6 20 5 20 10 10 12 4 | 16 27 21 18 36 17 29 18 18 19 18
6 | 8 12 11 10 11 4 12 13 12 24 4 | 22 26 26 22 31 21 31 21 22 27 23
7E | 8 20 10 10 14 7 21 12 11 12 4 | 25 32 24 27 36 24 33 25 23 23 24
8E | 15 19 12 9 19 6 19 19 23 27 6 | 26 28 24 25 29 22 29 26 33 32 22
9E | 11 19 14 11 15 9 16 15 13 22 5 | 35 43 40 35 43 36 41 35 34 31 34
10 | 12 16 7 10 15 5 16 13 10 26 4 | 27 30 20 24 29 23 28 26 25 29 22
11 | 7 15 11 12 19 6 12 9 16 21 4 | 17 25 21 18 33 16 25 18 17 23 16
12 | 10 27 11 10 13 5 18 18 9 25 5 | 23 35 23 25 27 23 30 25 23 23 21
13 | 6 21 7 9 17 5 13 10 11 21 4 | 18 30 21 24 34 19 28 18 21 19 19
14 | 10 22 11 11 14 4 16 14 12 17 5 | 22 34 30 31 34 26 32 28 26 24 25
15 | 9 23 11 8 12 4 20 10 13 13 5 | 15 28 25 17 29 17 25 19 22 17 18
16 | 10 27 9 9 14 5 17 19 13 17 5 | 18 33 18 17 29 14 24 19 17 18 15
17 | 11 13 6 14 12 4 17 12 11 34 4 | 51 54 53 57 54 51 56 51 50 61 52
18 | 8 27 20 14 17 7 18 13 8 17 6 | 66 75 66 68 74 65 71 68 69 69 67
19 | 7 13 10 9 11 3 14 8 13 32 4 | 30 37 34 30 35 30 38 29 31 31 30
20 | 7 22 9 8 20 5 18 13 8 17 4 | 21 29 19 22 27 18 22 26 18 27 18
21 | 8 24 11 8 18 6 17 14 7 18 5 | 25 36 25 23 32 25 31 27 22 24 23
22 | 7 25 10 10 18 5 17 21 9 16 5 | 18 31 20 15 34 18 28 26 19 27 18
23 | 8 26 9 13 14 6 16 13 9 21 5 | 13 32 18 22 26 16 26 16 20 19 15
25 | 8 15 12 9 13 7 13 17 9 14 4 | 21 24 17 18 24 16 25 18 18 18 14
26 | 9 12 9 7 11 6 16 9 12 12 4 | 18 22 18 15 21 12 18 18 21 19 15
X27 | 22 22 19 20 --- 25 21 16 --- --- 9 | 15 34 32 27 --- 21 33 34 --- --- 21
28 | 12 18 8 10 17 5 20 15 13 15 5 | 28 34 33 38 39 28 34 32 28 30 30
29 | 8 18 8 12 11 4 17 11 10 29 4 | 35 40 37 36 36 33 39 35 32 40 34
X30 | 10 15 11 10 11 4 --- 15 14 23 5 | 27 29 23 21 27 22 --- 26 22 22 22
31E | 8 22 11 11 16 4 22 11 11 16 5 | 28 36 27 28 35 25 34 25 26 27 25
32 | 12 18 7 7 13 6 15 17 10 20 4 | 28 28 28 29 24 24 27 35 27 31 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 10 10 15 5 17 14 12 22 |T 26 34 28 27 33 25 32 28 26 28 25
WRMS | 9 20 10 10 14 5 16 13 9 21 |NE 24 34 26 26 32 24 31 28 25 27 23
MEDI | 9 19 10 10 14 5 17 13 11 20 |MD 23 32 24 24 32 22 29 26 22 27 22
Table 3.1659.1 GPS week: 1659 Day: 1 MJD: 55858.000
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 | 11 18 8 14 --- 7 17 19 12 15 5 | 39 46 41 42 --- 39 47 39 41 37 40
2 | 10 20 8 13 16 4 14 16 11 36 5 | 27 36 37 33 42 30 36 30 33 32 31
3 | 9 15 5 12 15 5 15 12 9 33 4 | 17 26 21 20 27 17 27 21 16 30 18
4 | 10 17 10 12 11 6 9 16 9 22 4 | 16 23 21 14 19 15 18 19 17 21 14
5 | 9 27 8 12 16 4 21 13 11 16 5 | 16 35 23 22 36 17 28 19 17 18 19
6 | 8 14 4 10 15 4 13 13 10 21 4 | 24 29 25 25 32 23 29 27 22 30 24
7E | 9 20 11 7 13 4 17 12 14 17 4 | 27 37 29 32 36 31 36 34 38 35 31
8E | 18 19 12 11 19 5 18 20 22 30 6 | 17 29 17 20 22 16 25 25 27 29 15
9 | 16 20 8 8 16 9 17 15 15 24 5 | 31 39 36 38 38 38 40 38 42 41 35
10 | 15 19 7 13 14 7 14 15 10 27 5 | 25 28 27 22 23 19 26 25 24 31 21
11 | 7 15 6 9 18 4 14 11 13 19 4 | 16 28 21 18 35 17 26 18 20 23 18
12 | 10 22 11 11 15 6 18 16 13 24 5 | 21 32 24 25 28 20 28 24 23 23 21
13 | 7 22 10 9 18 4 13 14 11 20 4 | 18 32 22 23 35 18 30 20 21 19 20
14 | 9 22 9 10 15 3 16 14 11 18 4 | 23 33 26 24 31 22 31 27 23 24 23
15 | 5 26 9 8 14 5 18 10 7 13 4 | 16 32 21 21 28 17 25 17 19 19 18
16 | 9 29 6 9 14 4 18 19 7 19 5 | 16 34 20 20 29 17 26 22 17 21 17
17 | 12 13 8 14 12 5 16 16 7 33 4 | 28 35 31 34 32 29 34 28 31 33 29
18 | 8 33 12 11 17 6 17 14 8 14 5 | 83 90 79 82 83 79 87 83 81 82 81
19 | 9 13 6 13 11 7 15 10 11 26 4 | 21 30 25 20 31 20 30 22 23 21 22
20 | 8 24 6 9 15 5 17 11 9 14 4 | 19 27 17 17 18 15 21 18 18 18 15
21 | 10 19 9 6 21 5 14 12 11 16 4 | 22 29 18 20 28 18 25 23 21 23 18
22 | 7 26 9 12 19 5 13 20 9 14 5 | 23 35 25 22 34 19 30 26 18 27 22
23 | 9 27 10 11 15 6 15 13 10 21 5 | 18 37 21 23 29 17 28 18 19 20 18
25 | 11 17 8 10 15 7 13 16 9 15 4 | 16 23 17 18 23 13 26 17 16 14 13
26 | 7 14 8 7 14 5 12 8 8 14 3 | 17 20 18 15 19 14 19 18 15 18 15
X27 | 21 20 16 15 --- 19 14 15 --- --- 7 | 16 22 16 25 --- 21 20 23 --- --- 12
28 | 11 17 7 10 17 3 18 15 6 17 4 | 29 36 32 32 37 29 34 29 30 28 30
29 | 7 16 10 11 9 4 16 13 15 29 4 | 21 26 20 22 20 19 25 21 21 27 19
X30 | 11 19 9 13 12 6 --- 16 10 21 5 | 36 38 33 32 31 30 --- 33 29 35 31
31E | 11 22 12 11 11 6 21 10 9 15 5 | 44 45 38 40 44 40 48 43 38 45 40
32 | 12 20 7 8 17 5 17 19 13 22 5 | 36 45 43 41 39 38 46 48 37 47 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 21 9 10 15 5 16 14 11 22 |T 25 34 27 27 32 24 31 27 26 29 24
WRMS | 9 21 9 11 15 5 16 13 8 20 |NE 27 37 29 29 34 26 33 30 27 31 26
MEDI | 9 20 8 11 15 5 16 14 10 19 |MD 21 32 24 23 31 19 28 24 22 27 21
Table 3.1659.2 GPS week: 1659 Day: 2 MJD: 55859.000
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 | 9 16 8 8 --- 8 17 20 11 15 4 | 51 55 55 51 --- 53 57 52 50 52 51
2 | 9 18 8 9 17 5 14 12 11 30 4 | 24 31 32 23 35 24 36 27 28 31 26
3 | 15 11 7 8 12 6 11 14 8 30 4 | 25 21 19 15 22 14 23 20 17 29 15
4 | 8 23 6 7 10 5 10 14 8 19 3 | 15 29 11 15 19 11 17 19 17 19 12
5 | 6 18 7 7 21 3 17 12 10 12 4 | 18 25 24 17 37 18 27 21 23 19 21
6 | 8 10 7 7 10 6 12 13 9 20 3 | 20 22 19 19 22 16 24 24 18 28 16
7E | 7 19 6 7 20 4 17 12 7 18 4 | 30 32 28 27 34 28 31 29 32 34 29
8E | 16 22 8 14 20 4 20 20 20 29 6 | 27 36 29 31 36 28 33 35 37 38 29
9 | 12 17 8 11 16 7 17 14 12 22 4 | 19 28 23 23 30 21 30 27 24 27 22
10 | 10 19 6 9 12 3 12 16 8 24 4 | 17 24 16 19 20 15 18 21 20 23 15
11 | 9 17 6 7 18 5 12 11 11 14 3 | 16 28 16 17 32 15 26 18 21 18 16
12 | 8 24 8 8 16 5 18 15 11 24 4 | 27 34 23 22 28 21 30 27 25 27 22
13 | 9 20 8 6 22 4 14 14 9 17 4 | 18 30 20 19 33 17 27 18 21 15 19
14 | 8 21 7 10 14 4 16 13 9 16 4 | 17 28 22 20 27 19 29 20 17 15 19
15 | 7 22 8 9 16 6 17 11 10 14 4 | 13 26 17 17 28 15 26 16 20 16 17
16 | 12 25 5 10 14 6 18 19 10 21 4 | 16 30 19 21 26 15 24 24 18 27 17
17 | 9 13 8 11 13 5 16 15 8 31 4 | 35 36 32 37 40 32 36 35 33 42 33
18 | 12 29 12 11 17 5 13 13 11 13 5 | 56 60 51 47 50 50 55 52 53 53 52
19 | 7 13 7 12 9 6 14 13 9 23 4 | 24 30 24 24 26 21 31 23 23 23 22
20 | 6 21 6 7 18 6 15 11 11 12 4 | 17 26 15 18 16 13 20 19 14 18 13
21 | 8 18 7 6 17 4 13 16 12 17 4 | 27 33 27 24 28 25 28 22 26 29 24
22 | 7 19 7 8 18 5 14 14 7 13 4 | 24 30 26 16 32 20 34 23 21 24 23
23 | 10 27 9 8 18 5 15 11 8 20 4 | 14 33 19 16 23 14 24 16 17 17 15
25 | 9 16 5 9 16 3 15 16 12 18 4 | 19 25 15 17 23 13 27 18 20 16 14
26 | 21 13 7 11 14 3 14 11 12 15 4 | 23 17 14 16 19 10 16 16 20 18 12
X27 | 20 22 13 23 --- 17 14 18 --- --- 8 | 13 29 22 31 --- 20 26 31 --- --- 18
28 | 10 17 7 11 15 4 16 13 9 17 4 | 23 30 23 31 35 23 24 28 24 28 24
29 | 9 15 6 9 13 4 18 18 9 27 4 | 26 31 27 26 27 24 35 24 26 31 25
X30 | 7 15 5 11 14 4 --- 15 10 18 4 | 27 33 28 33 30 28 --- 30 29 34 28
31E | 14 20 9 9 12 5 17 19 11 18 4 | 57 65 60 59 60 59 62 55 60 60 59
32 | 12 20 6 8 14 5 18 15 12 24 4 | 19 31 26 27 31 21 32 26 20 32 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 7 9 16 5 15 14 10 21 |T 24 31 25 25 29 22 30 26 25 28 23
WRMS | 9 19 7 9 15 5 15 13 8 19 |NE 21 32 23 24 29 21 28 25 23 26 22
MEDI | 9 19 7 9 16 5 15 14 10 18 |MD 23 30 23 22 28 20 27 24 21 27 22
Table 3.1659.3 GPS week: 1659 Day: 3 MJD: 55860.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1M | 10 18 7 12 --- 6 17 19 11 13 5 | 46 52 44 47 --- 46 53 43 47 43 45
2M | 10 18 8 17 20 5 14 11 13 33 5 | 36 39 41 33 42 36 36 37 46 42 37
3M | 8 12 12 10 14 5 12 14 12 33 4 | 20 26 22 17 27 17 26 21 18 30 18
4 | 9 18 10 9 14 6 10 11 9 19 4 | 13 25 15 13 19 12 17 17 14 18 12
5M | 9 22 9 13 31 5 19 13 10 16 5 | 18 30 25 24 41 20 27 22 19 22 21
6M | 6 12 10 13 12 4 10 13 11 22 4 | 24 31 27 27 31 23 32 28 23 32 25
7 | 15 19 10 14 23 5 17 11 11 21 5 | 41 45 47 46 46 39 48 42 44 37 43
8E | 17 18 13 15 18 7 22 21 21 30 7 | 30 36 33 34 31 31 36 38 32 37 29
9 | 9 16 9 16 20 4 13 13 14 24 5 | 14 25 20 21 27 14 23 22 17 27 15
10 | 11 18 7 13 19 5 13 16 10 25 4 | 18 27 21 22 27 16 25 24 20 25 18
11M | 11 15 8 10 24 6 13 15 13 15 5 | 18 30 22 20 38 20 28 19 22 24 20
12 | 9 23 9 16 16 6 14 13 10 21 5 | 35 43 37 33 39 34 38 34 37 37 34
13 | 8 18 9 10 22 3 12 14 11 18 4 | 19 30 20 22 38 18 27 17 16 16 18
14 | 10 22 9 14 21 5 15 17 9 17 5 | 24 35 29 32 35 24 33 31 31 26 27
15M | 9 25 10 15 22 5 14 11 8 15 5 | 15 30 23 23 34 16 25 23 17 23 19
16 | 10 26 9 11 17 4 18 18 7 25 5 | 16 33 23 20 29 16 28 22 17 26 19
17M | 11 13 8 18 13 5 15 16 10 33 4 | 51 55 54 57 55 50 55 55 51 62 52
18 | 12 29 10 15 29 7 14 32 10 32 7 | 116 124 117 122 119 116 122 125 121 122 119
19M | 8 15 7 10 19 6 11 16 12 24 4 | 27 32 26 26 32 25 32 27 24 26 25
20 | 7 24 9 11 27 4 15 13 10 14 5 | 19 31 17 20 26 17 21 21 21 22 16
21 | 8 20 9 12 21 4 13 13 11 19 4 | 19 31 23 24 26 20 27 22 22 26 21
22 | 7 19 9 13 26 5 12 16 11 13 5 | 23 32 27 24 40 23 31 25 26 28 25
23 | 7 22 9 11 19 4 15 13 12 21 4 | 18 32 19 19 34 16 25 17 18 18 16
25 | 8 13 9 13 17 6 17 12 15 21 4 | 23 29 27 21 31 20 33 23 25 23 22
26M | 6 12 10 15 19 5 11 9 9 19 4 | 13 20 16 17 25 12 18 19 14 19 14
X27 | 23 20 23 32 --- 28 16 17 --- --- 10 | 10 25 32 33 --- 33 20 27 --- --- 16
28M | 10 20 10 16 21 4 19 15 11 19 5 | 36 43 41 43 45 38 40 42 48 34 40
29M | 6 15 9 15 15 4 16 15 15 30 5 | 30 36 32 34 31 30 36 32 31 48 31
X30 | 6 18 8 14 13 6 --- 20 17 28 5 | 39 43 41 39 39 33 --- 40 33 40 37
31 | 18 20 10 15 14 8 23 12 14 20 6 | 90 90 93 94 93 84 97 88 91 82 91
32 | 12 19 9 11 19 4 16 18 10 27 5 | 23 28 23 21 26 22 26 25 25 29 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 9 13 20 5 15 15 12 23 |T 29 38 33 33 38 29 36 33 32 34 30
WRMS | 9 19 9 13 19 5 14 13 9 23 |NE 28 38 32 32 39 29 34 32 31 34 29
MEDI | 9 18 9 13 19 5 14 14 11 21 |MD 23 32 27 24 34 23 28 25 24 27 22
Table 3.1659.4 GPS week: 1659 Day: 4 MJD: 55861.000
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 | 8 16 8 8 --- 4 16 21 14 14 5 | 42 47 44 38 --- 41 48 35 43 38 40
2 | 7 19 11 14 21 4 16 11 8 29 4 | 18 27 26 19 31 20 31 21 18 26 21
3 | 7 13 6 14 16 4 11 14 8 33 4 | 17 22 17 15 26 15 26 17 17 26 16
4 | 7 14 8 8 15 5 9 15 11 21 4 | 13 18 10 13 17 13 18 15 13 18 8
5 | 8 22 8 14 30 4 20 13 8 15 5 | 15 31 20 21 39 18 33 16 16 14 18
6 | 8 11 7 14 13 4 11 14 10 22 4 | 20 24 19 19 24 17 26 21 20 22 19
7 | 6 17 7 10 25 5 20 14 9 15 4 | 30 39 32 35 41 34 38 31 33 30 31
8E | 17 24 13 19 23 9 18 28 26 30 7 | 71 71 75 73 72 70 70 72 79 73 72
9 | 9 18 8 14 21 4 13 17 15 22 5 | 17 27 17 20 29 20 28 25 30 28 19
10 | 10 18 9 11 22 4 14 19 9 26 5 | 18 26 15 20 27 16 27 19 16 22 13
11 | 8 16 8 9 22 3 13 19 10 13 4 | 32 38 30 33 39 32 41 37 30 33 29
12M | 8 22 12 14 17 8 16 18 9 18 5 | 50 57 50 48 50 49 58 61 49 59 50
13 | 5 20 10 10 26 4 13 14 12 20 4 | 21 32 22 22 37 20 29 19 24 15 19
14 | 9 20 11 12 19 3 15 22 11 19 5 | 17 28 21 22 31 19 28 26 20 21 17
15 | 7 22 9 11 23 3 14 13 7 16 4 | 13 27 18 16 33 15 23 18 15 20 14
16 | 8 26 10 11 17 4 19 19 13 27 5 | 16 33 19 14 27 15 26 19 18 25 15
17 | 9 13 8 13 16 2 14 21 15 35 5 | 24 27 26 29 24 25 28 24 29 28 25
18 | 8 25 13 14 25 4 12 15 13 14 5 | 46 52 45 49 56 46 44 44 48 45 44
19 | 9 15 6 10 16 3 13 22 6 31 4 | 29 33 28 22 29 25 33 24 26 21 26
20 | 6 19 10 9 22 4 16 16 12 18 5 | 21 28 21 19 25 20 29 21 22 20 18
21 | 7 19 9 10 19 3 11 13 15 19 4 | 18 25 20 19 23 16 20 18 13 25 15
22 | 5 23 11 12 24 3 10 18 9 13 5 | 13 28 18 14 34 13 21 15 15 19 14
23 | 7 28 12 9 21 4 15 12 11 22 5 | 21 38 20 17 31 17 29 18 18 17 16
25M | 8 14 12 10 17 6 13 12 11 18 4 | 37 38 32 35 34 35 44 40 36 39 34
26 | 6 11 6 13 19 4 9 12 11 19 4 | 17 22 16 17 26 16 21 20 18 21 15
X27 | 22 21 32 27 --- 25 15 17 --- --- 11 | 12 24 48 25 --- 29 26 29 --- --- 20
28 | 12 20 7 16 19 3 16 18 9 20 5 | 20 31 22 25 28 19 29 22 22 23 20
29 | 10 16 11 7 15 4 16 13 11 30 4 | 22 29 23 25 28 24 31 21 24 27 22
X30 | 8 17 9 10 14 5 --- 18 14 25 5 | 20 31 22 23 23 19 --- 21 19 21 19
31 | 13 20 13 11 23 4 22 28 15 19 6 | 56 57 57 53 61 54 57 47 55 49 53
32 | 9 16 9 9 17 4 15 24 13 28 5 | 17 22 16 17 22 14 27 21 14 23 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 10 12 21 4 15 17 12 23 |T 25 33 27 26 33 25 32 27 26 28 24
WRMS | 8 19 9 11 19 4 14 15 9 22 |NE 19 29 23 21 29 19 26 22 19 22 17
MEDI | 8 19 9 11 19 4 14 17 11 20 |MD 20 29 22 22 29 20 29 21 20 23 19
Table 3.1659.5 GPS week: 1659 Day: 5 MJD: 55862.000
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 16 8 9 --- 5 13 19 11 12 5 | 46 51 47 40 --- 44 54 39 43 43 44
2 | 9 17 9 13 24 4 11 9 6 30 4 | 23 30 26 27 33 23 28 25 24 34 24
3 | 8 12 11 9 17 2 10 9 11 33 4 | 16 21 16 14 18 14 22 14 16 28 14
4 | 9 17 9 8 19 4 8 10 9 19 4 | 15 20 13 17 19 13 16 18 15 18 13
5 | 9 21 9 11 36 5 19 11 8 11 5 | 14 29 21 22 43 17 30 18 18 19 19
6 | 7 9 12 12 14 2 9 10 14 21 4 | 16 22 15 20 19 15 21 17 20 23 14
7 | 7 17 9 11 31 5 18 11 10 14 5 | 16 27 16 18 30 15 24 17 19 16 14
8E | 17 18 15 15 24 5 17 24 16 28 6 | 72 74 69 72 71 72 70 74 75 75 71
9 | 12 20 9 12 24 5 12 12 10 22 5 | 16 30 19 19 30 16 24 21 17 21 16
10 | 12 15 5 11 26 6 12 11 9 24 4 | 18 26 18 24 31 17 23 25 21 24 19
11 | 9 14 6 10 24 6 11 17 12 14 4 | 25 36 30 24 39 24 34 28 23 24 26
12 | 9 23 14 12 21 5 15 14 12 20 5 | 41 51 46 43 45 41 44 47 42 46 43
13 | 7 20 11 10 28 4 12 9 8 18 4 | 16 29 21 18 33 16 25 13 15 11 15
14 | 8 18 13 12 23 5 14 15 13 19 5 | 16 28 24 22 30 16 27 22 17 20 18
15 | 11 19 11 11 25 5 13 11 11 13 5 | 10 27 18 19 34 12 25 14 15 14 14
16 | 9 22 11 9 20 3 15 11 10 25 4 | 15 28 18 15 24 12 22 14 13 20 13
17 | 11 13 10 22 15 4 15 13 10 31 5 | 28 29 28 38 29 27 30 29 29 28 28
18 | 9 28 13 13 34 5 15 10 10 16 5 | 67 76 70 71 76 69 71 71 72 71 70
19 | 7 15 8 9 17 4 12 18 8 29 4 | 21 29 24 19 23 19 27 23 19 21 21
20E | 8 19 12 8 26 5 13 9 10 16 4 | 24 31 21 25 30 23 26 23 23 23 21
21 | 9 20 10 10 22 8 10 15 13 23 4 | 18 29 18 21 24 19 21 28 18 27 18
22 | 8 19 13 14 34 4 12 19 8 16 5 | 17 26 25 21 39 16 27 19 15 17 18
23 | 8 24 10 12 25 4 14 9 9 23 5 | 15 31 19 16 27 13 24 15 14 12 13
25 | 10 16 14 9 22 5 13 13 15 20 5 | 27 34 31 31 34 26 36 33 28 31 29
26 | 9 13 7 11 20 4 10 10 8 13 4 | 13 22 13 17 25 11 17 15 14 11 12
X27 | 28 23 25 27 --- 16 --- 16 --- --- 12 | 11 27 31 29 --- 25 --- 22 --- --- 17
28 | 11 18 7 15 21 3 13 14 8 19 4 | 29 33 24 29 33 26 30 30 27 23 26
29 | 8 13 11 9 18 5 14 14 13 31 4 | 22 26 25 23 26 21 25 24 22 31 21
X30 | 9 14 10 10 21 6 --- 16 13 26 5 | 21 25 19 23 21 18 --- 22 23 25 19
31 | 10 16 14 11 33 7 22 16 14 18 6 | 21 26 24 23 37 21 32 16 23 19 19
32 | 12 18 8 9 24 5 15 22 12 27 5 | 20 24 22 17 29 17 28 22 21 25 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 11 12 24 5 14 14 11 22 |T 23 32 26 26 32 23 30 25 24 26 23
WRMS | 9 18 10 12 21 5 13 12 8 20 |NE 20 30 24 24 32 20 28 24 22 24 20
MEDI | 9 18 10 11 24 5 13 13 10 20 |MD 18 29 22 22 30 18 27 22 20 23 19
Table 3.1659.6 GPS week: 1659 Day: 6 MJD: 55863.000
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 | 10 15 8 11 --- 5 15 17 10 13 4 | 50 58 53 55 --- 52 58 47 50 58 53
2 | 8 21 8 9 20 4 13 12 9 29 4 | 25 33 27 21 34 21 29 24 26 33 23
3 | 7 12 7 6 18 5 7 8 8 33 3 | 18 22 19 15 25 16 24 18 18 30 17
4 | 8 18 7 7 15 3 13 10 7 15 3 | 10 19 9 14 15 9 16 14 12 17 9
5 | 10 26 8 5 38 4 21 15 9 12 5 | 19 32 22 20 44 18 28 19 19 20 19
6 | 5 10 6 9 16 2 9 8 10 20 3 | 21 24 21 22 27 19 27 23 20 27 20
7 | 9 22 8 10 29 5 19 12 7 12 5 | 30 35 32 32 38 30 36 26 31 27 29
8E | 17 20 10 13 26 8 17 24 13 24 6 | 94 93 92 94 93 89 97 96 93 97 91
9 | 10 20 11 10 23 6 14 12 13 25 4 | 14 28 18 21 28 15 26 17 20 23 17
10 | 10 16 5 9 23 6 12 10 10 24 4 | 16 24 16 22 26 13 18 20 22 21 15
11 | 8 15 6 7 21 5 13 14 12 10 4 | 25 39 31 31 44 27 41 27 27 32 30
12 | 7 27 11 9 21 9 16 13 15 15 5 | 32 39 36 33 41 33 35 28 33 31 31
13 | 8 21 8 13 29 5 14 8 9 17 4 | 21 29 24 26 38 21 28 19 27 14 21
14 | 9 20 8 6 25 4 13 14 14 20 4 | 17 25 27 22 31 19 24 25 21 20 21
15 | 9 21 8 5 24 4 12 8 8 14 4 | 14 25 21 17 36 16 23 17 17 16 17
16 | 8 27 7 8 19 4 14 11 6 20 4 | 15 30 17 16 23 15 22 17 17 18 15
17 | 11 13 8 15 16 8 13 15 13 30 4 | 46 47 46 49 48 45 46 48 46 49 46
18 | 6 28 7 6 39 5 14 10 7 16 4 | 54 61 53 52 48 52 55 55 58 55 53
19 | 7 15 4 7 14 4 10 16 9 29 3 | 31 37 32 29 33 31 35 30 30 27 31
20E | 9 22 9 10 22 5 11 9 8 12 4 | 20 25 22 21 22 17 20 22 22 19 19
21 | 7 21 7 6 23 5 11 17 11 18 4 | 18 28 16 16 28 15 22 23 14 26 17
22 | 7 20 7 4 36 6 9 11 7 11 4 | 29 35 29 26 40 24 31 30 29 28 27
23 | 8 27 9 13 26 5 17 10 8 21 5 | 19 34 21 23 31 16 29 19 21 15 18
25 | 9 17 7 6 23 7 14 10 14 15 4 | 21 27 24 20 32 20 32 18 25 20 21
26 | 9 15 7 6 20 5 11 9 11 8 3 | 18 25 21 18 31 16 26 19 17 15 18
X27 | 26 24 24 22 --- 17 --- 18 --- --- 11 | 10 25 30 28 --- 18 --- 19 --- --- 18
28 | 11 20 7 10 21 4 15 13 11 18 4 | 25 30 22 31 32 24 28 29 25 24 25
29 | 8 15 8 7 18 5 15 15 15 31 4 | 33 37 34 33 35 32 37 33 29 41 31
X30 | 8 16 8 11 19 5 --- 17 14 27 5 | 16 23 18 25 19 16 --- 23 15 25 17
31 | 8 15 8 10 33 5 19 22 10 14 5 | 44 46 48 44 56 44 50 46 45 41 44
32 | 12 20 7 9 24 8 18 19 12 26 5 | 20 29 21 24 28 22 29 21 23 33 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 8 9 24 5 14 13 11 20 |T 26 34 29 29 35 25 33 28 28 30 26
WRMS | 9 20 8 9 21 5 13 11 8 18 |NE 20 30 23 24 29 20 27 23 23 24 20
MEDI | 8 20 8 9 23 5 14 12 10 18 |MD 21 30 24 24 32 20 29 23 23 26 21
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1659 GPS week: 1659 MJD: 55857.0-55863.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 |U 15 20 43 |U 6 10 23 |U 7 8 19 |
emr | emr 2972 |U 17 21 49 |U 7 9 24 | 9 12 21 |
esa | esa 2976 | 19 20 46 |U 5 9 20 | 8 9 20 |
gfz | gfz 2971 |U 17 21 45 |U 6 9 21 |U 7 8 17 |
grg | grg 2779 | 24 22 72 |U 7 10 30 | 12 11 24 |
igr | igr 2962 | 16 20 45 | 6 9 22 | 9 8 19 |
igs | igs 2975 | 19 20 45 | 6 9 21 | 7 9 20 |
jpl | jpl 2842 |U 25 26 48 |U 6 9 24 | 9 12 22 |
mit | mit 2976 |U 94 44 171 |U 9 12 30 |U 12 15 34 |
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 5.1659.0 GPS week: 1659 Day: 0 MJD: 55857.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 7 7 21 | 5 9 23 | 4 7 20 |
emr | emr 2971 | 8 7 22 | 6 7 21 | 7 11 21 |
esa | esa 2976 | 7 6 22 | 5 8 24 | 6 9 18 |
gfz | gfz 2968 | 8 6 26 | 6 8 20 | 11 11 18 |
grg | grg 2755 | 9 8 24 | 5 9 25 | 10 11 16 |
igr | igr 2975 | 7 6 22 | 6 8 23 | 6 8 16 |
igs | igs 2976 | 8 6 23 | 5 7 22 | 7 8 17 |
jpl | jpl 2863 | 10 7 24 | 6 8 23 | 8 9 18 |
mit | mit 2976 | 19 22 47 | 11 24 40 | 10 17 29 |
Table 5.1659.1 GPS week: 1659 Day: 1 MJD: 55858.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2965 | 10 8 27 | 6 9 24 | 5 7 19 |
emr | emr 2972 | 12 9 31 | 6 9 23 | 6 8 14 |
esa | esa 2976 | 12 9 28 | 6 9 20 | 6 8 18 |
gfz | gfz 2972 | 11 8 28 | 7 11 24 | 5 7 18 |
grg | grg 2784 | 16 15 40 | 7 12 25 | 9 9 23 |
igr | igr 2975 | 12 8 28 | 6 11 23 | 5 6 18 |
igs | igs 2976 | 11 9 27 | 6 9 22 | 6 7 18 |
jpl | jpl 2865 | 14 9 32 | 6 9 25 | 7 8 26 |
mit | mit 2976 | 49 20 82 | 17 15 57 | 19 29 36 |
Table 5.1659.2 GPS week: 1659 Day: 2 MJD: 55859.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 16 25 41 | 6 8 21 | 6 7 13 |
emr | emr 2972 | 17 23 40 | 7 11 26 | 8 11 19 |
esa | esa 2976 | 17 25 37 | 5 9 20 | 6 7 12 |
gfz | gfz 2972 | 16 27 41 | 6 9 21 | 6 8 13 |
grg | grg 2784 | 23 27 50 | 7 12 28 | 10 10 20 |
igr | igr 2960 | 18 28 42 | 5 8 21 | 7 8 12 |
igs | igs 2976 | 16 25 40 | 5 9 21 | 6 8 14 |
jpl | jpl 2871 | 28 32 56 | 6 10 26 | 7 10 12 |
mit | mit 2976 | 33 46 80 | 6 9 24 | 7 7 15 |
Table 5.1659.3 GPS week: 1659 Day: 3 MJD: 55860.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 47 76 145 | 6 12 26 | 9 9 21 |
emr | emr 2972 | 45 73 147 | 7 10 26 | 10 11 23 |
esa | esa 2976 | 57 69 148 | 5 11 21 | 12 8 23 |
gfz | gfz 2971 | 46 74 143 | 6 11 21 | 6 6 17 |
grg | grg 2784 | 63 65 148 | 8 12 30 | 18 11 43 |
igr | igr 2951 | 47 75 144 | 6 11 23 | 20 8 27 |
igs | igs 2970 | 56 67 146 | 6 11 24 | 8 9 23 |
jpl | jpl 2871 | 63 98 111 | 6 12 27 | 10 12 25 |
mit | mit 2976 | 480 123 816 | 6 13 23 | 19 13 29 |
Table 5.1659.4 GPS week: 1659 Day: 4 MJD: 55861.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2969 | 12 10 34 | 6 9 22 | 7 8 22 |
emr | emr 2972 | 15 12 46 | 8 11 21 | 8 11 22 |
esa | esa 2976 | 11 10 37 | 5 9 18 | 7 10 21 |
gfz | gfz 2973 | 11 10 33 | 5 9 17 | 6 9 17 |
grg | grg 2784 | 41 18 195 | ---- ---- ---- | ---- ---- ---- |
igr | igr 2973 | 11 10 37 | 5 9 18 | 6 8 18 |
igs | igs 2976 | 11 11 35 | 5 9 17 | 7 9 19 |
jpl | jpl 2867 | 19 16 55 | 5 10 19 | 9 13 23 |
mit | mit 2976 | 14 40 36 | 7 7 21 | 10 11 71 |
Table 5.1659.5 GPS week: 1659 Day: 5 MJD: 55862.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 7 6 17 | 6 13 20 | 9 12 20 |
emr | emr 2972 | 13 12 33 | 8 10 24 | 12 15 22 |
esa | esa 2976 | 21 16 27 | 6 9 18 | 8 11 23 |
gfz | gfz 2972 | 22 17 27 | 8 10 21 | 7 10 21 |
grg | grg 2784 | 9 11 22 | 8 8 29 | 11 12 20 |
igr | igr 2959 | 8 6 18 | 7 10 21 | 7 11 21 |
igs | igs 2976 | 21 17 26 | 7 10 19 | 8 13 22 |
jpl | jpl 2780 | 31 18 39 | 7 10 22 | 13 15 20 |
mit | mit 2976 | 41 22 39 | 7 9 22 | 9 11 23 |
Table 5.1659.6 GPS week: 1659 Day: 6 MJD: 55863.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 6 5 19 | 6 7 27 | ---- ---- ---- |
emr | emr 2974 | 9 8 22 | 9 6 28 | 13 16 28 |
esa | esa 2976 | 7 7 23 | 5 6 22 | 8 11 26 |
gfz | gfz 2971 | 7 7 19 | 6 8 24 | ---- ---- ---- |
grg | grg 2784 | 10 8 25 | 8 8 40 | ---- ---- ---- |
igr | igr 2942 | 7 6 23 | 6 7 25 | ---- ---- ---- |
igs | igs 2976 | 7 6 21 | 6 6 23 | 9 12 25 |
jpl | jpl 2782 | 9 7 18 | 5 6 26 | 11 15 27 |
mit | mit 2976 | 20 37 94 | 7 7 24 | ---- ---- ---- |
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 6.1659 GPS week: 1659 MJD: 55857.500-55863.500
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 | 49 -9 -73 176 -7 | 2 14
| 18 23 85 45 5 | 3
emr uuuuu | 28 12 -35 -80 -8 | 49 51
| 23 24 40 144 4 | 2
esa uuuxu | -36 -27 -17 -433 -11 | 5 17
| 17 13 61 83 7 | 2
gfz uuuuu | -26 11 -47 -97 -1 | -7 14
| 15 26 70 116 3 | 2
grg uuuxx | 78 -6 -5 240 -28 | -45 75
| 12 17 83 108 63 | 9
igr xxxxx | -8 25 -28 -56 2 | -4 16
| 17 18 56 53 7 | 3
irf xxxxx | 2 21 -16 -63 0 | 0 14
| 13 7 19 77 3 | 2
jpl uuuuu | 71 -65 28 155 -16 | 48 50
| 40 16 75 59 7 | 7
mit uuuxu | -27 11 -14 -372 4 | 2 13
| 20 15 43 103 7 | 2
ngs uuuuu | -10 61 89 8 4 | 5 13
| 15 36 106 74 5 | 2
sio xuuuu | 204 -34 -268 49 -8 | 5 14
| 37 20 100 122 5 | 3
Table 7.1659.0 GPS week: 1659 Day: 0 MJD: 55857.500
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 -11 -182 175 -15 | 7 17
emr uuuuu | 22 55 -41 -100 -14 | 54 56
esa uuuxu | -22 -39 -61 -359 -4 | 10 21
gfz uuuuu | -7 -13 7 13 0 | -5 16
grg uuuxx | 58 -22 10 130 41 | -40 70
igr xxxxx | 13 54 -31 22 9 | -7 18
irf xxxxx | 9 16 5 -56 -5 | 1 16
jpl uuuuu | 31 -58 71 271 -22 | 60 63
mit uuuxu | -5 32 -7 -383 -8 | 4 17
ngs uuuuu | -32 58 41 -137 10 | 4 14
sio xxxxx | 200 -58 -165 163 -17 | 12 22
Table 7.1659.1 GPS week: 1659 Day: 1 MJD: 55858.500
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 | 31 -17 -118 139 -9 | 3 15
emr uuuuu | 10 15 -76 -148 -8 | 50 52
esa uuuxu | -27 -40 62 -533 -13 | 6 18
gfz uuuuu | -11 13 21 -45 1 | -9 15
grg uuuxx | 73 10 -115 113 33 | -40 70
igr xxxxx | -33 28 -35 -44 6 | -8 17
irf xxxxx | -8 10 2 -163 -1 | -2 15
jpl uuuuu | 30 -65 81 150 -22 | 53 56
mit uuuxu | -34 -4 -15 -422 -1 | 0 14
ngs uuuuu | 6 74 -44 10 8 | 3 13
sio xxxxx | 168 -66 -186 -74 -8 | 6 17
Table 7.1659.2 GPS week: 1659 Day: 2 MJD: 55859.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 34 -41 -107 158 -4 | 2 14
emr uuuuu | 48 10 -84 49 -11 | 49 51
esa uuuxu | -17 -31 -13 -325 -4 | 4 16
gfz uuuuu | -28 -11 -58 -136 4 | -9 15
grg uuuxx | 81 4 -3 135 31 | -39 70
igr xxxxx | -14 27 -120 -85 9 | -7 18
irf xxxxx | -2 22 -9 -85 4 | -3 15
jpl uuuuu | 64 -81 103 165 -19 | 49 50
mit uuuxu | -29 3 -26 -394 4 | -1 13
ngs uuuuu | -26 113 157 2 -1 | 3 13
sio xuuuu | 173 -30 -210 76 -1 | 4 14
Table 7.1659.3 GPS week: 1659 Day: 3 MJD: 55860.500
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 | 50 31 86 199 -3 | 1 14
emr uuuuu | 63 8 -13 103 -10 | 48 50
esa uuuxu | -41 -21 -9 -529 -10 | 5 16
gfz uuuuu | -43 -15 -73 -294 -3 | -8 14
grg uuuxx | 90 2 -15 310 -43 | -38 70
igr xxxxx | -18 25 -28 -121 6 | -4 17
irf xxxxx | -4 19 -6 -84 1 | -1 15
jpl uuuuu | 63 -48 -100 144 -20 | 47 49
mit uuuxu | -46 2 74 -389 6 | 0 13
ngs uuuuu | 4 70 100 60 6 | 4 14
sio xxxxx | 181 -25 -301 88 -5 | 3 14
Table 7.1659.4 GPS week: 1659 Day: 4 MJD: 55861.500
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 | 66 -2 -103 110 -14 | 2 13
emr uuuuu | 23 9 -21 26 -2 | 49 50
esa uuuxu | -60 -28 -109 -463 -24 | 5 16
gfz uuuuu | -43 36 -151 -189 1 | -7 13
grg uuuxx | 82 -23 125 351 -50 | -45 75
igr xxxxx | -10 15 -22 -58 -3 | -1 13
irf xxxxx | -14 18 -41 -119 -1 | 1 12
jpl uuuuu | 145 -47 -47 98 -19 | 45 48
mit uuuxu | -56 4 -25 -504 8 | 3 11
ngs uuuuu | -3 40 283 83 5 | 6 13
sio xxxxx | 201 -23 -408 -133 -6 | 5 12
Table 7.1659.5 GPS week: 1659 Day: 5 MJD: 55862.500
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 | 50 0 -42 205 -2 | 0 14
emr uuuuu | 37 -29 32 -286 -3 | 48 49
esa uuuxu | -57 -2 55 -453 -15 | 3 17
gfz uuuuu | -15 18 -110 -56 -3 | -6 12
grg uuuxx | 92 -29 57 345 -110 | -51 80
igr xxxxx | 15 -7 73 -105 -9 | 0 13
irf xxxxx | 25 25 -42 71 1 | 2 11
jpl uuuuu | 64 -89 23 168 -5 | 41 44
mit uuuxu | -3 3 -58 -166 11 | 4 11
ngs uuuuu | -17 77 33 57 -1 | 7 13
sio xxxxx | 269 -23 -395 203 -10 | 4 12
Table 7.1659.6 GPS week: 1659 Day: 6 MJD: 55863.500
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 | 77 -27 -48 245 -4 | -1 12
emr uuuuu | -3 13 -46 -205 -8 | 46 47
esa uuuxu | -25 -28 -43 -370 -6 | 2 16
gfz uuuuu | -33 50 33 25 -3 | -6 12
grg uuuxx | 71 12 -97 294 -96 | -62 92
igr xxxxx | -7 28 -32 0 -2 | -1 12
irf xxxxx | 10 32 -20 -7 2 | 2 12
jpl uuuuu | 101 -66 67 92 -7 | 39 41
mit uuuxu | -17 33 -45 -349 9 | 5 13
ngs uuuuu | -1 -4 52 -18 0 | 7 13
sio xxxxx | 238 -12 -214 17 -7 | 3 10
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