[IGSREPORT-19121] Wk 1606 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Nov 4 05:19:09 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1606 (Oct 17, 2010 - Oct 23, 2010)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1606[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1606[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1606[0-6].cls IGS GPS clock combination summary report.
igs16067.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16067.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because they either provide broadcast
clocks (NGS) or clock corrections are not provided (SIO). The clock
information not used is still compared to combination for completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
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 | DGAR
0 | EMR | 27 9 27 WTZR WTZR
0 | ESA | KARR SUTH
0 | GFZ | 4 7 8 9 17 21 24 31 ARTU CHAT GODE KERG PIE1 SFER
0 | GFZ | UNSA
0 | GRG | DGAR ONSA SANT
0 | JPL | 4 9 24 27 32
0 | MIT | 24 27 4 8 9 24 27 MDVJ
1 | ALL | 1
1 | COD | 9 GLPS
1 | EMR | 9 27 27 WTZR WTZR
1 | ESA | 9
1 | GFZ | 4 7 8 9 21 31 DAV1 DGAR KERG MDVJ UNSA
1 | GRG | DGAR ONSA SANT
1 | JPL | 4 8 9 27 32 BOR1 HARB
1 | MIT | 9 8 27 FLIN
2 | ALL | 1
2 | COD | 27 HRAO
2 | EMR | 9 9 27 WTZR IRKT WTZR
2 | ESA | 27
2 | GFZ | 4 7 8 9 17 21 24 31 HARB RESO SFER UNSA
2 | GRG | ONSA SANT
2 | JPL | 4 9 24 27 32
2 | MIT | 4 8 9 21 24 4 8 9 21 24 27 SOFI TWTF
3 | ALL | 1
3 | COD | DGAR GLSV
3 | EMR | 8 WTZR WTZR
3 | ESA | KARR
3 | GFZ | 4 7 8 17 21 31 DAV1 DGAR GLPS IRKT KERG PERT SALU
3 | GFZ | UNSA
3 | GRG | DGAR ONSA SANT
3 | JPL | 4 8 9 27 31 32
3 | MIT | 3 6 8 9 22 3 4 6 8 9 22 24 27 DAV1 KHAJ DAV1 KHAJ
4 | COD | MCM4 CEDU DGAR MCM4
4 | EMR | 8 WTZR WTZR
4 | ESA | KERG
4 | GFZ | 4 7 8 24 31 AUCK MDVJ UNSA
4 | GRG | DGAR NRC1
4 | JPL | 4 8 9 24 27 31 32
4 | MIT | 6 8 24 4 6 7 8 9 24 27 DAV1 USNO DAV1 IRKJ IRKT USNO
5 | ALL | 1
5 | COD | DAV1 DAV1 DGAR GRAZ
5 | EMR | 8 9 27 8 9 27 WTZR WTZR
5 | ESA | IRKJ KERG UNSA
5 | GFZ | 4 8 21 27 GODE IISC MATE RABT SCH2
5 | GRG | DAV1 DGAR ONSA
5 | JPL | 8 9 27 32 HARB
5 | MIT | 8 9 27 28 8 9 27 28 MAW1 DAV1 MAW1
6 | ALL | 1
6 | COD | DGAR GUAT
6 | EMR | 8 WTZR WTZR
6 | ESA | KERG
6 | GFZ | DAV1 MDVJ SFER
6 | GRG | DGAR ONSA SANT
6 | JPL | 9 27 32
6 | MIT | 8 9 24 27 9 24 27 CHUR MAW1 CHUR
5. 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.
6. 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 | .6 1.2 .5 7 -26 -8 -.17
EMR | 3.7 3.5 3.2 27 -7 5 .13
ESA | 2.2 8.8 11.3 120 16 -76 -.03
GFZ | -.1 1.8 .2 30 -7 -39 .19
GRG | -1.1 15.5 14.5 34 85 -81 .18
JPL | -.3 10.3 7.2 0 -82 8 .24
MIT | -2.9 4.1 12.5 18 -3 -31 -.09
NGS | -.2 3.1 10.5 49 39 -6 -.15
SIO | 1.5 3.8 1.3 37 -4 -61 .13
7. 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.
8. 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.
9. 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 1.1606.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1606.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 2.1606.[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 3.1606.[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 5.1606.0-6).
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 1606 summary. (Oct 17, 2010 - Oct 23, 2010)
Table 1.1606.a GPS week: 1606 MJD: 55486.000-55492.000
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 227| 0 0 0 56 56 -2 -.22 8 7 | -254 -191 18 78
| 0 0 1 10 8 15 .03 | 300 352
emr 93| 0 0 1 27 14 43 .51 20 20 | 1802 -1331 21 81
| 1 1 1 32 13 15 .05 | 2613 1457
esa 143| 1 0 0 -132 7 -54 .24 8 8 | -516 -138 16 107
| 0 0 1 17 15 16 .02 | 615 840
gfz 195| 0 2 0 22 -7 26 -.20 12 12 | 121 -23 22 106
| 1 0 1 47 24 14 .03 | 173 326
grg 135| 2 2 1 2 -170 -19 .67 16 16 | -107 -2589 61 217
| 1 1 0 12 26 14 .03 | 437 6771
igr n/a| 0 0 0 76 -4 37 -.03 5 5 | 23153 -1176 18 61
| 0 0 0 20 18 19 .03 | 2434 1435
jpl 139| 1 0 1 74 178 52 .52 21 21 | 4832 -1440 18 112
| 0 1 1 18 19 41 .05 | 2687 1255
mit 261| -1 -2 -2 44 -11 5 -.47 13 10 | -4 -140 22 139
| 0 0 0 31 12 5 .02 | 422 814
ngs 221| -1 -1 0 -22 -63 35 -.23 12 8 | -199 -207 2000 3781
| 0 0 0 25 16 14 .04 | 294 480
sio 256| 0 1 -1 15 -1 -45 -.06 18 17 | --- --- --- ---
| 1 1 1 29 12 6 .02 | --- ---
Table 1.1606.b GPS week : 1606 MJD: 55486.000-55492.000
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 | 27 39 19 28 0 24 37 |
2 | 5 6 5 5 5 5 5 |
3 | 4 4 4 4 4 5 5 |
4 | 5 4 5 4 4 6 6 |
5 | 6 5 5 4 5 5 5 |
6 | 4 4 4 4 3 4 4 |
7 | 5 5 5 4 5 4 4 |
8 | 6 7 9 7 6 6 6 |
9 | 6 6 6 6 7 7 6 |
10 | 4 4 4 3 3 3 4 |
11 | 4 4 4 4 4 4 5 |
12 | 5 5 5 4 5 5 5 |
13 | 5 5 4 4 5 5 4 |
14 | 5 4 4 4 4 4 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 6 5 |
17 | 6 5 6 5 5 5 5 |
18 | 5 5 5 5 4 4 5 |
19 | 5 5 5 4 5 4 5 |
20 | 4 5 4 4 4 4 5 |
21 | 4 4 4 5 4 4 4 |
22 | 5 5 5 5 4 4 5 |
23 | 5 5 5 5 5 5 5 |
24 | 4 5 5 5 5 6 6 |
25 | 6 7 6 6 6 6 6 |
26 | 4 3 4 3 4 4 4 |
27 | 6 6 7 6 6 6 6 |
28 | 5 5 5 5 5 5 5 |
29 | 4 5 4 4 4 4 4 |
30 | 4 4 4 3 4 4 4 |
31 | 5 5 4 5 5 5 5 |
32 | 4 4 4 5 5 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 2.1606.0 GPS week: 1606 Day: 0 MJD: 55486.000
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 227| 0 1 0 48 50 5 -.18 8 8 | 5 -524 16 75
| 71 14 |
emr 93| 0 0 1 36 15 69 .61 20 20 | 3318 -66 21 77
| -43 -4 |
esa 143| 0 -1 2 -148 27 -60 .26 9 9 | -54 -303 14 93
| 40 -5 |
gfz 195| 2 1 -2 -21 35 46 -.16 13 14 | 221 -308 21 106
| 12 4 |
grg 135| 3 2 0 -13 -217 0 .62 18 17 | 260 -79 64 180
| 11 77 |
igr n/a| -1 -1 1 47 -27 24 -.02 6 5 | 24265 500 17 60
| -22 15 |
jpl 139| 2 0 1 69 168 5 .56 21 21 | 6925 -87 20 110
| 3 -36 |
mit 261| 0 0 -3 95 -3 12 -.48 13 10 | 226 -50 17 128
| 4 11 |
ngs 221| -2 -1 1 -26 -83 13 -.27 11 9 | -2 -438 1864 3377
| -49 51 |
sio 256| -1 0 -4 65 -18 -36 -.06 19 20 | --- --- --- ---
| -20 25 |
Table 2.1606.1 GPS week: 1606 Day: 1 MJD: 55487.000
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 227| -1 1 0 69 51 -16 -.23 8 7 | 32 -582 26 81
| 8 38 |
emr 93| 0 -1 -1 64 1 53 .53 20 20 | 3355 629 23 72
| -73 17 |
esa 143| 0 0 0 -121 12 -56 .20 8 7 | -1089 -428 21 109
| 21 -1 |
gfz 195| 1 2 1 22 -4 29 -.23 13 15 | 50 221 24 102
| -48 1 |
grg 135| 1 3 1 3 -196 -8 .64 16 15 | -297 403 67 203
| 19 23 |
igr n/a| 0 0 0 81 0 29 -.04 5 5 | 24825 654 18 60
| -36 17 |
jpl 139| 1 0 2 98 180 90 .54 21 21 | 6881 171 18 99
| 10 47 |
mit 261| 0 -2 -2 29 10 5 -.46 13 10 | -380 509 27 122
| 15 19 |
ngs 221| 0 -1 0 -27 -75 59 -.26 12 9 | 143 -781 2248 4079
| -137 1 |
sio 256| -1 0 -2 -22 7 -53 -.07 17 16 | --- --- --- ---
| -4 21 |
Table 2.1606.2 GPS week: 1606 Day: 2 MJD: 55488.000
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 227| 0 0 0 44 58 -8 -.20 8 7 | -162 -290 15 74
| 62 -17 |
emr 93| 3 0 0 27 1 29 .50 20 20 | 3769 -1201 16 77
| -41 45 |
esa 143| 1 0 0 -153 5 -67 .22 9 8 | -250 1495 14 120
| 51 12 |
gfz 195| 1 1 0 39 -27 43 -.18 13 12 | 131 -16 20 112
| -20 6 |
grg 135| 3 3 1 5 -161 -18 .68 16 14 | 294 -264 51 237
| 53 -28 |
igr n/a| 0 0 0 72 12 37 -.03 5 5 | 25158 -1287 21 60
| -8 -15 |
jpl 139| 1 0 1 63 201 83 .57 21 21 | 6752 -1539 19 118
| 23 -53 |
mit 261| -3 -1 -1 80 -12 -1 -.46 13 10 | 152 -151 20 142
| 6 20 |
ngs 221| -1 -1 0 -25 -39 37 -.27 13 9 | -108 -240 2267 3338
| -42 16 |
sio 256| -1 0 0 21 -17 -41 -.05 17 17 | --- --- --- ---
| -24 13 |
Table 2.1606.3 GPS week: 1606 Day: 3 MJD: 55489.000
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 227| 0 1 0 71 47 -21 -.21 9 8 | -272 -276 17 81
| -1 34 |
emr 93| 0 0 0 51 35 43 .48 20 20 | 2593 -793 25 93
| -44 -24 |
esa 143| 2 0 0 -116 6 -41 .25 8 7 | -1383 -24 16 104
| -12 12 |
gfz 195| 0 2 1 -20 0 15 -.17 12 11 | -16 -80 24 114
| -36 18 |
grg 135| 2 2 2 8 -161 -9 .65 17 16 | -224 -2 77 195
| 36 -12 |
igr n/a| 0 0 0 105 10 67 .01 5 4 | 23887 -875 24 64
| -47 9 |
jpl 139| 2 -2 2 96 166 103 .53 21 20 | 5267 -1049 19 99
| 17 -34 |
mit 261| -2 -1 -2 11 -13 12 -.44 11 9 | -728 874 22 146
| 29 24 |
ngs 221| -2 -1 0 22 -50 26 -.24 11 7 | -199 -393 1992 4162
| -93 -15 |
sio 256| 0 1 0 -8 6 -47 -.05 17 17 | --- --- --- ---
| -37 -1 |
Table 2.1606.4 GPS week: 1606 Day: 4 MJD: 55490.000
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 227| 0 0 0 54 52 25 -.23 8 8 | -384 -52 17 75
| 46 -6 |
emr 93| 0 -1 3 17 24 43 .51 19 19 | 2586 -1931 28 87
| -40 -7 |
esa 143| 1 -1 0 -111 10 -75 .21 8 8 | 215 -1301 19 113
| 41 31 |
gfz 195| 0 3 0 -17 -34 14 -.18 12 12 | -97 361 23 102
| 6 22 |
grg 135| 2 4 1 20 -161 -27 .68 15 15 | -948 -17937 58 226
| 8 -26 |
igr n/a| 0 0 0 71 -31 59 -.05 6 5 | 23787 -1742 17 65
| -28 24 |
jpl 139| 1 0 0 84 181 55 .46 20 20 | 5124 -1736 17 113
| 19 -57 |
mit 261| 0 -2 -1 34 -12 2 -.45 13 10 | 547 -1715 26 156
| 21 17 |
ngs 221| -1 -1 1 -6 -52 42 -.20 11 8 | -244 -258 1953 4009
| -115 -43 |
sio 256| 1 2 -1 7 -9 -48 -.06 17 16 | --- --- --- ---
| -42 3 |
Table 2.1606.5 GPS week: 1606 Day: 5 MJD: 55491.000
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 227| 0 1 -2 58 67 0 -.25 8 7 | -150 -82 13 79
| 28 -12 |
emr 93| 0 0 2 30 22 47 .47 20 20 | 660 -3756 14 72
| -33 -27 |
esa 143| 1 -1 2 -124 -24 -26 .27 8 8 | -95 -411 12 108
| 22 -15 |
gfz 195| 0 2 1 49 5 11 -.24 10 10 | 121 220 21 100
| -5 36 |
grg 135| 3 1 2 -14 -157 -43 .68 16 15 | 197 65 50 260
| 34 -45 |
igr n/a| 0 0 0 59 -1 20 -.07 4 4 | 22035 -3408 17 74
| -25 -20 |
jpl 139| 0 1 -1 58 203 18 .49 20 19 | 3415 -3367 16 128
| -20 -81 |
mit 261| -2 -2 -2 20 -26 1 -.49 14 11 | 156 -106 19 158
| 18 31 |
ngs 221| -1 -1 1 -37 -68 26 -.21 13 9 | -196 -116 1602 3424
| -63 34 |
sio 256| 0 1 -2 12 7 -39 -.11 18 17 | --- --- --- ---
| -52 -15 |
Table 2.1606.6 GPS week: 1606 Day: 6 MJD: 55492.000
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 227| 0 0 1 48 68 -3 -.26 9 8 | -852 466 22 83
| 55 1 |
emr 93| 2 -1 2 -37 1 21 .48 21 21 | -3661 -2202 22 92
| 15 -23 |
esa 143| 1 0 -1 -151 16 -54 .25 9 9 | -960 3 16 102
| 11 25 |
gfz 195| 0 1 0 105 -26 22 -.23 11 10 | 437 -560 27 109
| 7 21 |
grg 135| 1 0 0 5 -139 -27 .72 17 17 | -37 -310 62 222
| 18 -57 |
igr n/a| 0 0 0 96 9 22 -.04 5 5 | 18120 -2075 18 50
| -37 5 |
jpl 139| 0 0 0 52 147 8 .46 22 22 | -534 -2474 20 117
| -35 -67 |
mit 261| -1 -2 0 36 -20 7 -.48 15 13 | -1 -346 25 124
| 17 21 |
ngs 221| -1 -1 0 -57 -73 45 -.18 11 8 | -793 771 2079 4078
| -57 -27 |
sio 256| 1 2 0 36 11 -52 -.05 19 18 | --- --- --- ---
| -56 -15 |
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 3.1606.0 GPS week: 1606 Day: 0 MJD: 55486.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 19 --- --- 38 --- 189 --- --- --- --- 27 | 32 --- --- 26 --- 142 --- --- --- --- 28
2E | 6 27 9 12 15 8 21 13 10 26 5 | 18 31 19 17 25 17 24 20 21 26 17
3 | 6 14 7 14 18 4 9 6 14 19 4 | 20 22 22 29 29 21 20 26 17 22 21
4E | 11 18 11 10 14 5 16 17 10 23 5 | 148 149 151 149 147 148 148 142 149 151 149
5 | 8 21 6 14 18 6 23 19 16 24 5 | 31 41 32 35 45 30 39 19 35 21 29
6 | 5 12 6 12 15 4 10 6 13 19 3 | 23 27 26 28 32 24 25 28 19 27 24
7E | 8 20 6 9 14 4 23 13 11 16 4 | 32 42 34 31 37 31 40 33 30 30 32
8E | 14 21 14 11 20 8 15 25 22 17 6 | 102 111 108 107 112 105 109 108 111 106 107
9E | 12 19 11 12 24 8 20 27 18 17 6 | 71 79 77 76 76 76 80 71 76 75 72
10 | 5 16 6 9 12 6 11 14 9 13 3 | 19 26 22 23 27 18 22 21 19 20 19
11 | 7 13 7 7 23 4 14 11 8 16 4 | 19 23 15 19 25 17 19 21 17 27 17
12 | 6 21 11 11 16 5 23 15 9 23 5 | 23 26 27 30 24 24 28 28 26 26 23
13 | 7 22 8 13 20 6 25 10 9 20 4 | 28 38 34 37 39 33 38 29 32 23 30
14 | 8 17 8 16 18 5 23 5 8 22 4 | 20 33 31 36 36 26 29 24 31 22 27
15 | 9 23 9 12 21 7 29 11 11 15 5 | 23 32 28 30 31 24 30 28 27 24 24
16 | 8 25 10 15 15 3 27 12 10 24 5 | 20 33 27 29 30 24 30 27 24 26 22
17 | 9 18 8 26 14 5 26 10 9 25 5 | 18 29 23 23 25 17 33 16 21 18 18
18 | 6 25 9 15 18 6 28 7 9 14 4 | 18 37 23 18 32 20 38 18 20 20 20
19 | 8 22 7 11 21 5 24 8 14 25 5 | 20 30 17 18 19 17 32 20 19 21 17
20 | 8 25 8 9 20 3 21 6 9 13 4 | 16 31 20 15 29 16 27 17 17 17 16
21E | 5 16 8 12 16 5 17 9 8 9 3 | 21 26 20 24 32 24 26 22 25 22 21
22 | 7 23 10 14 20 4 22 7 11 15 4 | 19 36 29 24 36 23 34 20 25 22 23
23 | 9 27 12 15 17 6 26 7 7 19 5 | 19 34 29 31 31 22 33 20 21 19 21
24E | 10 21 8 11 17 5 19 8 11 13 4 | 61 62 64 64 65 63 61 67 66 63 63
X25 | 19 --- 8 13 16 6 --- 15 6 --- 6 | 23 --- 32 34 39 28 --- 40 31 --- 29
26 | 8 12 7 9 18 7 15 9 6 13 3 | 20 25 28 26 29 23 20 26 22 25 23
27E | 12 22 12 12 17 7 25 27 18 15 6 | 32 38 39 35 39 32 40 31 40 35 32
28 | 8 17 6 12 13 6 28 12 9 26 4 | 28 34 31 37 34 28 32 29 27 28 29
X29 | 6 20 8 11 14 4 23 8 9 --- 4 | 17 32 21 18 25 19 30 20 17 --- 18
30 | 6 18 5 11 13 9 15 10 5 11 3 | 32 32 30 33 35 34 28 37 33 32 31
31E | 5 19 9 10 18 5 27 11 11 13 4 | 37 43 38 34 45 36 43 36 31 34 35
32 | 10 20 9 11 18 3 13 14 5 15 4 | 18 20 22 22 27 17 20 25 19 21 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 9 13 18 6 21 13 11 19 |T 32 40 36 36 40 36 39 34 34 34 32
WRMS | 8 20 9 14 17 5 21 10 9 20 |NE 22 30 25 27 30 28 28 24 23 23 22
MEDI | 8 20 8 12 17 5 22 11 9 17 |MD 21 32 28 29 32 24 30 26 25 25 23
Table 3.1606.1 GPS week: 1606 Day: 1 MJD: 55487.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 26 --- --- 57 --- 78 --- --- --- --- 39 | 17 --- --- 46 --- 59 --- --- --- --- 22
2E | 8 30 9 15 15 9 24 14 11 24 5 | 18 34 16 16 23 17 26 19 18 25 16
3 | 4 13 5 25 17 4 13 8 8 15 4 | 17 21 15 31 23 17 20 21 17 17 17
4E | 10 15 7 14 11 6 16 13 14 15 4 | 114 117 115 112 120 113 118 112 109 114 113
5 | 6 20 7 13 19 5 24 11 14 18 4 | 11 25 17 16 33 12 27 14 17 16 13
6 | 5 13 5 13 15 5 12 7 11 15 3 | 16 25 17 22 23 18 21 19 16 19 17
7E | 9 21 6 10 15 4 25 14 12 16 4 | 24 38 30 30 36 28 38 29 34 29 28
8E | 17 21 17 15 22 9 17 29 26 17 7 | 90 96 95 89 93 93 96 94 91 95 90
9E | 13 18 11 12 16 6 19 23 15 19 5 | 59 63 61 62 61 61 64 69 65 60 61
10 | 6 15 6 10 13 4 10 12 9 14 3 | 16 21 21 20 26 16 20 18 20 16 17
11 | 7 14 8 9 18 6 17 9 9 17 4 | 20 22 19 20 20 20 23 25 19 28 17
12 | 9 20 8 11 13 6 21 14 9 23 4 | 16 26 19 20 21 17 26 23 20 18 15
13 | 5 19 8 13 21 3 22 10 9 21 4 | 15 28 20 22 34 17 31 17 16 15 15
14 | 6 18 5 15 15 6 22 8 10 16 4 | 17 28 23 26 29 17 29 18 21 18 20
15 | 7 22 8 11 19 5 26 8 11 15 4 | 19 29 23 22 31 19 30 21 20 21 20
16 | 6 22 6 15 14 6 26 13 9 23 5 | 17 28 19 23 27 17 30 21 18 20 18
17 | 9 18 8 12 9 5 22 11 14 21 4 | 14 26 16 19 22 12 30 11 19 12 13
18 | 6 25 6 14 17 5 24 7 11 14 4 | 13 30 20 15 28 16 31 14 22 15 16
19 | 6 23 6 8 17 6 22 8 10 23 4 | 15 28 18 17 14 14 29 18 19 20 15
20 | 9 21 7 21 16 4 24 7 10 11 4 | 14 25 15 23 27 12 25 13 13 13 12
21E | 6 18 8 9 19 5 16 6 14 9 4 | 19 26 22 21 24 20 25 20 24 20 19
22 | 7 24 7 13 20 6 26 9 8 15 4 | 14 35 22 18 36 17 29 15 17 19 18
23 | 7 23 9 14 18 3 26 8 9 18 4 | 13 29 19 23 27 16 32 14 17 13 14
24E | 11 23 9 10 23 5 20 10 15 13 5 | 59 58 60 58 59 58 57 63 58 58 57
X25 | 22 --- 9 11 15 6 --- 19 8 --- 7 | 16 --- 22 24 30 20 --- 26 22 --- 18
26 | 7 11 7 9 11 5 15 7 10 13 3 | 17 20 22 21 25 19 19 23 20 23 19
27E | 14 23 7 9 16 5 23 22 19 21 5 | 33 42 39 39 41 38 41 49 51 39 39
28 | 7 16 8 13 13 4 23 10 9 24 4 | 21 30 22 26 29 20 29 21 24 19 22
X29 | 8 18 7 11 12 5 25 11 13 --- 4 | 12 22 16 18 17 16 27 22 20 --- 15
30 | 8 14 4 12 9 6 14 11 9 10 3 | 22 28 24 29 28 22 25 28 24 24 23
31E | 4 26 6 11 13 5 24 12 15 10 4 | 27 39 28 29 35 29 38 28 36 31 29
32 | 8 19 6 11 15 3 18 11 7 15 4 | 16 22 16 21 23 16 24 22 18 22 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 8 13 16 5 21 13 12 17 |T 25 35 28 30 34 27 35 29 29 28 26
WRMS | 7 20 7 15 15 5 21 10 9 16 |NE 16 26 19 22 26 18 26 19 19 18 17
MEDI | 7 19 7 12 15 5 22 11 10 16 |MD 17 28 21 22 28 17 29 21 20 20 18
Table 3.1606.2 GPS week: 1606 Day: 2 MJD: 55488.000
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 | 32 --- --- 41 --- 39 --- 24 33 --- 19 | 26 --- --- 25 --- 48 --- 30 28 --- 24
2E | 7 26 9 12 13 7 21 14 15 21 5 | 15 31 18 13 22 14 25 14 17 19 14
3 | 8 15 5 9 12 4 13 8 10 15 3 | 14 21 19 18 22 14 18 17 15 18 15
4E | 10 18 7 8 18 4 13 11 16 17 4 | 85 88 88 86 92 87 89 90 84 87 86
5 | 7 25 5 10 18 4 23 10 11 17 4 | 15 31 16 15 30 12 26 14 14 14 14
6 | 5 14 6 11 13 5 13 7 14 11 3 | 18 21 25 19 26 18 22 20 17 21 19
7E | 8 18 6 11 18 3 26 13 9 15 4 | 19 28 20 19 28 19 29 24 22 22 20
8E | 17 21 24 13 25 5 19 32 32 23 8 | 105 106 104 101 109 101 107 106 107 107 103
9E | 11 19 10 14 28 6 22 21 16 26 6 | 57 58 58 56 59 57 56 67 60 54 58
10 | 7 14 7 9 11 4 11 11 8 11 3 | 14 19 16 13 20 12 19 17 14 14 14
11 | 6 17 11 10 20 5 15 10 12 15 4 | 16 21 16 14 19 14 16 19 22 24 14
12 | 7 21 9 22 15 6 24 12 13 20 5 | 17 25 24 36 20 19 25 23 25 19 21
13 | 6 20 7 7 20 5 21 9 10 17 4 | 17 28 23 22 32 19 28 19 19 17 18
14 | 7 17 9 12 13 4 24 7 9 12 4 | 15 26 24 25 29 18 26 18 22 17 20
15 | 5 26 6 12 17 5 29 11 9 16 4 | 17 30 18 22 29 17 26 22 18 19 18
16 | 7 23 9 14 13 6 25 12 13 22 5 | 15 28 22 21 25 17 27 21 21 20 17
17 | 8 16 10 28 12 4 19 11 13 21 5 | 11 23 17 27 20 13 26 12 18 12 14
18 | 6 23 9 13 14 4 28 7 12 15 4 | 14 29 21 15 26 15 32 14 20 15 16
19 | 8 21 11 8 11 4 23 7 7 22 4 | 15 26 13 13 15 11 27 16 17 18 14
20 | 8 22 9 8 14 6 25 8 7 10 4 | 10 25 14 11 24 10 24 10 15 12 11
21E | 6 20 9 7 15 5 19 9 13 10 4 | 23 26 19 27 27 25 27 25 34 23 22
22 | 6 23 9 12 16 5 29 8 10 14 4 | 13 33 20 17 33 16 31 14 18 20 18
23 | 7 24 10 9 17 4 25 8 7 19 4 | 14 32 23 22 28 18 29 16 16 14 17
24E | 12 20 9 13 19 5 16 10 11 12 4 | 46 43 41 50 40 44 39 51 44 42 42
X25 | 16 --- 8 9 15 6 --- 16 10 --- 6 | 14 --- 23 23 27 21 --- 26 27 --- 20
26 | 6 14 5 9 14 4 13 11 10 14 3 | 14 21 19 16 25 14 15 21 18 19 17
27E | 11 25 9 11 16 6 24 28 22 19 6 | 21 30 24 21 28 19 32 31 28 23 20
28 | 8 18 7 17 13 4 25 10 11 25 5 | 22 32 28 34 33 24 31 23 24 22 26
X29 | 7 17 7 12 9 6 21 8 10 --- 4 | 10 24 12 13 16 10 24 13 14 --- 11
30 | 6 14 7 11 11 3 14 11 6 11 3 | 25 25 29 25 31 24 22 29 23 25 24
31E | 5 20 8 11 13 5 25 12 14 12 4 | 22 31 23 27 28 24 32 25 28 24 24
32 | 10 18 6 8 13 7 18 11 5 19 4 | 16 19 17 19 23 17 19 20 18 27 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 9 13 16 5 21 13 13 17 |T 23 32 26 27 31 24 31 27 27 26 24
WRMS | 7 20 8 12 14 5 21 10 9 17 |NE 15 25 19 20 25 17 24 18 19 18 17
MEDI | 7 20 9 11 14 5 21 11 11 16 |MD 16 28 21 21 27 18 26 20 20 20 18
Table 3.1606.3 GPS week: 1606 Day: 3 MJD: 55489.000
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 | 35 --- --- 48 --- 39 --- 41 65 --- 27 | 18 --- --- 27 --- 46 --- 31 46 --- 24
2E | 6 24 8 12 13 8 23 8 9 20 4 | 18 31 24 18 30 19 29 21 20 23 19
3 | 8 15 6 10 19 4 15 7 11 14 3 | 17 22 22 26 28 20 21 23 23 19 20
4E | 10 18 9 13 16 2 15 9 10 18 4 | 105 108 109 108 107 105 108 105 108 106 106
5 | 5 21 4 13 17 3 25 7 10 14 4 | 11 26 15 17 31 14 27 13 12 13 12
6 | 8 14 6 9 15 5 15 6 13 12 3 | 20 24 26 26 30 23 23 26 25 22 23
7E | 10 17 7 9 15 3 24 9 12 14 4 | 25 34 29 27 31 27 35 30 33 30 28
8E | 16 25 15 14 15 6 17 24 25 19 6 | 86 92 90 84 92 86 89 87 85 88 87
9E | 14 21 7 12 21 5 21 23 15 23 6 | 39 45 36 42 39 39 48 52 41 41 39
10 | 8 13 6 9 14 4 12 8 8 13 3 | 20 24 27 24 28 21 23 21 23 19 22
11 | 6 17 6 8 23 4 13 8 8 14 3 | 17 25 18 16 21 16 20 23 22 25 17
12 | 6 18 8 11 14 5 23 12 9 20 4 | 21 28 28 28 26 23 30 27 26 23 23
13 | 6 20 7 10 23 3 20 8 9 18 4 | 19 30 21 25 36 21 30 18 22 15 19
14 | 8 20 6 16 16 4 26 7 8 14 4 | 16 30 23 31 31 18 28 20 21 18 20
15 | 6 25 7 13 16 4 26 10 8 16 4 | 23 30 23 28 32 23 29 24 24 22 22
16 | 10 26 6 11 15 5 26 13 10 22 5 | 19 31 22 25 25 21 31 27 22 22 20
17 | 7 18 6 21 12 6 19 9 10 19 4 | 14 23 17 23 22 13 27 14 14 13 14
18 | 5 25 8 16 18 4 27 6 9 16 4 | 14 29 17 15 24 14 31 12 14 13 12
19 | 6 20 7 9 17 3 24 7 10 21 4 | 16 26 18 16 19 15 29 19 19 16 15
20 | 10 21 5 9 18 4 20 9 6 10 4 | 13 25 13 12 26 11 23 12 14 12 11
21E | 7 20 9 16 21 3 20 8 13 8 4 | 20 25 22 27 40 19 27 24 23 24 21
22 | 5 23 8 13 17 4 29 7 9 16 4 | 13 32 19 18 33 17 29 15 14 18 15
23 | 9 23 7 11 20 3 24 7 8 19 4 | 16 32 22 25 31 20 31 16 19 14 17
24E | 14 21 12 11 19 4 17 10 18 15 5 | 72 67 71 70 70 67 65 74 65 65 68
X25 | 19 --- 8 10 16 8 --- 17 7 --- 6 | 21 --- 29 33 37 28 --- 37 29 --- 28
26 | 6 12 6 9 13 3 13 8 10 14 3 | 21 23 25 22 27 23 22 24 26 23 22
27E | 10 22 7 14 19 6 23 23 19 15 5 | 25 30 31 25 36 27 35 41 42 30 30
28 | 7 16 7 16 13 6 23 9 10 24 4 | 23 30 24 33 34 25 30 27 23 24 24
X29 | 6 18 6 10 13 5 20 7 9 --- 3 | 15 26 17 16 18 15 26 20 14 --- 14
30 | 7 11 6 12 15 4 14 9 8 10 3 | 29 31 30 30 33 31 28 34 33 29 30
31E | 6 20 7 9 15 3 24 12 10 22 4 | 21 30 23 19 31 23 32 26 26 31 22
32 | 12 20 8 9 18 8 19 10 6 20 4 | 13 19 14 19 23 17 22 19 14 24 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 8 12 17 5 21 11 11 17 |T 25 34 29 29 35 27 34 30 29 28 26
WRMS | 8 20 7 11 16 4 20 9 7 17 |NE 17 26 21 23 27 20 26 21 21 19 19
MEDI | 7 20 7 11 16 4 20 9 10 16 |MD 19 30 23 25 31 21 29 24 23 23 21
Table 3.1606.4 GPS week: 1606 Day: 4 MJD: 55490.000
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 | 6 --- --- --- --- 1646 --- --- --- --- 0 | 16 --- --- --- --- 9999 --- --- --- --- 21
2E | 8 20 10 11 13 7 20 10 13 19 4 | 14 24 21 14 20 13 21 14 22 19 13
3 | 9 14 7 11 14 4 14 11 6 15 3 | 14 18 20 24 23 17 17 26 21 20 17
4E | 8 20 9 12 16 5 17 8 11 18 4 | 68 70 68 68 67 67 68 66 74 76 70
5 | 6 22 8 13 14 5 23 8 10 16 4 | 12 27 19 17 32 11 25 11 14 11 13
6 | 8 13 4 10 11 4 13 8 8 12 3 | 16 21 21 21 24 17 20 24 17 21 17
7E | 9 18 7 11 15 3 23 12 9 20 4 | 50 53 50 49 51 48 55 46 48 41 47
8E | 11 19 13 12 15 7 15 21 23 20 6 | 70 75 75 72 79 73 76 75 73 72 73
9E | 14 19 10 11 18 7 20 31 16 19 6 | 33 39 35 35 40 36 39 44 39 36 33
10 | 5 12 7 8 14 5 9 7 10 13 3 | 14 22 17 18 25 15 21 16 20 15 14
11 | 6 14 7 7 21 7 15 8 8 15 3 | 16 21 15 14 19 15 17 20 18 24 13
12 | 6 20 8 11 11 7 23 11 11 21 4 | 21 27 24 27 27 23 27 25 27 22 22
13 | 8 20 8 10 19 3 24 8 7 17 4 | 20 31 24 23 35 20 29 19 23 15 20
14 | 8 17 8 12 14 5 24 11 8 12 4 | 15 29 23 23 27 18 27 22 22 18 19
15 | 5 24 8 15 13 5 23 13 9 16 4 | 16 28 22 25 30 17 26 23 18 20 18
16 | 10 22 9 15 15 4 27 15 9 22 5 | 17 27 20 23 25 19 28 27 18 21 18
17 | 9 15 8 19 12 7 17 9 11 20 4 | 12 24 18 23 22 15 26 15 23 12 15
18 | 7 23 7 12 16 4 24 6 9 16 4 | 13 31 19 14 29 14 31 14 12 18 15
19 | 8 20 12 11 13 5 23 8 8 20 4 | 16 25 15 15 17 13 25 18 18 14 13
20 | 6 19 5 11 18 6 18 7 10 13 4 | 13 24 17 14 29 14 22 13 23 13 15
21E | 8 20 7 7 13 6 15 6 8 9 3 | 27 31 26 27 28 29 31 28 30 26 25
22 | 5 20 8 13 15 5 23 9 7 15 4 | 12 30 22 16 32 16 29 14 17 18 16
23 | 9 25 8 14 17 3 28 8 10 21 5 | 16 34 23 24 28 19 30 17 23 16 18
24E | 14 20 12 16 18 6 20 9 13 15 5 | 61 59 58 63 60 62 56 66 67 60 61
X25 | 17 --- 9 10 15 8 --- 18 9 --- 6 | 15 --- 27 30 36 21 --- 35 22 --- 24
26 | 6 12 8 9 10 7 11 11 10 12 3 | 14 22 21 18 25 16 17 22 17 18 17
27E | 9 18 7 10 21 9 22 28 20 16 6 | 23 29 24 22 27 27 29 45 35 32 26
28 | 6 16 8 15 11 5 24 10 11 25 4 | 22 28 26 30 32 21 30 23 28 22 23
X29 | 6 17 6 12 12 6 19 7 8 --- 3 | 13 24 14 14 17 11 25 13 11 --- 10
30 | 6 12 7 8 13 7 12 13 7 11 3 | 26 29 30 29 33 28 27 33 30 27 29
31E | 10 19 9 11 15 4 25 11 14 17 4 | 24 33 29 24 30 25 34 26 27 27 23
32 | 9 21 7 22 19 5 17 9 7 19 5 | 12 19 12 24 21 12 17 14 15 22 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 12 15 6 20 13 11 17 |T 22 31 26 27 31 24 30 27 27 26 24
WRMS | 8 19 8 12 15 5 20 10 8 16 |NE 15 25 20 21 26 16 24 20 19 18 17
MEDI | 8 19 8 11 15 5 20 9 9 16 |MD 16 28 22 23 28 18 27 23 22 21 18
Table 3.1606.5 GPS week: 1606 Day: 5 MJD: 55491.000
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 --- --- 27 --- 159 --- --- --- --- 23 | 18 --- --- 17 --- 447 --- --- --- --- 18
2E | 10 24 7 11 21 3 20 13 13 23 5 | 27 35 26 25 33 23 28 25 22 31 22
3 | 8 14 9 10 9 3 14 19 12 19 4 | 15 22 16 22 21 17 21 29 18 24 17
4E | 10 21 9 16 20 3 16 16 12 25 5 | 117 123 121 118 121 118 119 121 120 120 118
5 | 8 22 4 14 17 4 22 9 10 16 4 | 11 25 14 15 31 11 24 11 12 11 12
6 | 7 13 8 9 8 4 15 14 12 16 3 | 16 20 16 19 20 17 22 25 15 23 16
7E | 10 20 6 8 15 4 24 10 12 14 4 | 39 47 45 42 48 40 48 42 44 41 42
8E | 11 23 15 12 15 5 15 23 23 15 6 | 45 51 55 45 59 47 55 47 52 45 47
9E | 14 20 12 9 13 5 21 31 20 19 6 | 35 40 35 39 32 37 39 54 45 34 37
10 | 7 15 6 9 12 3 11 9 10 12 3 | 11 23 17 17 22 14 20 17 19 14 15
11 | 6 16 8 7 22 4 16 10 11 15 4 | 15 22 16 16 20 17 17 22 23 25 14
12 | 8 19 9 10 12 4 22 7 10 27 4 | 18 25 25 26 25 22 26 23 25 25 21
13 | 7 19 8 10 19 3 24 10 7 18 4 | 16 27 21 19 33 16 26 16 19 13 16
14 | 9 18 6 11 15 5 24 13 8 12 4 | 14 27 22 21 27 15 26 22 21 16 17
15 | 6 23 7 13 13 6 26 13 13 16 4 | 16 25 20 19 28 15 24 25 17 20 17
16 | 8 26 7 13 10 4 24 20 15 24 5 | 17 30 19 24 26 19 28 30 21 21 20
17 | 8 17 7 11 16 4 17 8 17 19 4 | 10 24 22 20 22 14 24 13 24 14 16
18 | 5 21 7 9 15 4 25 9 10 15 4 | 11 27 19 15 29 13 29 13 15 14 14
19 | 7 21 7 6 12 4 21 12 11 21 4 | 15 27 17 17 20 17 24 20 20 12 16
20 | 8 23 9 7 19 4 22 7 8 14 4 | 13 28 23 11 26 15 25 14 21 16 16
21E | 5 18 10 8 14 4 15 9 9 10 3 | 21 30 22 23 29 22 25 26 28 25 21
22 | 5 22 9 10 14 5 24 9 9 14 4 | 12 28 19 16 33 14 29 12 14 16 15
23 | 9 25 7 12 16 4 27 10 11 25 5 | 11 31 21 19 28 17 29 14 20 16 15
24E | 13 23 9 12 19 5 20 12 21 20 5 | 85 82 84 82 82 82 77 82 83 76 81
X25 | 16 --- 9 9 15 6 --- 11 10 --- 5 | 19 --- 26 27 31 21 --- 28 28 --- 24
26 | 5 12 6 9 11 6 12 10 14 11 3 | 14 22 21 17 24 17 17 21 23 18 18
27E | 12 18 9 7 21 7 18 25 20 15 5 | 27 34 33 28 35 34 36 48 41 36 32
28 | 9 19 8 15 10 5 21 10 14 24 4 | 19 27 21 25 29 19 28 21 22 20 19
X29 | 8 18 7 13 12 5 20 7 13 --- 4 | 10 24 17 14 19 12 23 16 21 --- 12
30 | 5 18 5 9 12 4 13 11 11 12 3 | 23 22 23 24 27 21 26 26 25 18 22
31E | 8 22 6 12 17 5 29 17 13 12 5 | 17 29 25 26 30 21 32 31 31 34 26
32 | 8 19 7 7 21 4 17 13 9 20 4 | 11 18 16 14 22 14 18 15 16 25 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 8 10 16 4 20 14 13 18 |T 23 33 28 26 33 38 32 29 29 27 25
WRMS | 7 20 8 10 15 4 19 11 9 17 |NE 14 24 19 18 25 34 24 19 19 18 16
MEDI | 8 19 7 10 15 4 20 11 12 16 |MD 16 27 21 20 28 17 26 23 22 21 17
Table 3.1606.6 GPS week: 1606 Day: 6 MJD: 55492.000
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 | 31 --- --- 44 --- 94 --- --- --- --- 37 | 25 --- --- 25 --- 216 --- --- --- --- 20
2 | 7 21 8 8 22 5 23 13 11 29 5 | 23 33 27 22 24 24 32 25 35 30 26
3 | 10 17 7 7 17 7 13 16 12 23 4 | 18 21 25 23 33 20 22 25 21 27 20
4 | 9 21 8 21 18 9 14 14 14 21 5 | 83 83 83 79 79 77 77 86 78 80 80
5 | 8 21 8 15 18 5 25 12 11 17 4 | 12 28 18 17 32 11 26 14 16 15 15
6 | 8 15 8 7 15 5 13 13 12 20 4 | 22 25 27 24 34 22 26 28 22 30 24
7E | 6 21 11 9 13 4 25 10 11 9 4 | 36 45 37 33 43 36 45 39 36 36 38
8E | 12 23 15 10 15 4 18 24 22 17 6 | 50 57 58 50 60 52 57 54 56 53 53
9E | 15 21 10 12 21 4 19 31 17 17 6 | 38 44 34 36 37 37 44 57 44 35 38
10 | 7 15 8 10 15 4 14 10 13 12 4 | 16 29 24 23 28 17 26 22 21 23 21
11 | 7 16 11 7 22 4 19 14 8 17 4 | 16 24 19 18 24 17 21 24 25 27 17
12 | 9 19 8 10 16 7 25 8 12 28 5 | 26 29 34 32 35 25 30 28 30 29 29
13 | 6 20 6 10 19 3 22 9 9 19 4 | 22 29 23 26 34 21 28 20 26 18 21
14 | 11 23 8 14 18 6 25 16 6 14 5 | 19 31 28 32 35 20 29 28 27 22 24
15 | 8 24 8 12 14 6 27 13 9 15 4 | 21 32 26 29 38 23 29 30 27 25 24
16 | 7 30 7 10 16 4 26 16 9 24 5 | 22 36 28 25 32 23 31 27 24 25 23
17 | 8 20 12 14 12 4 22 11 9 21 4 | 16 27 25 17 24 17 30 18 28 22 20
18 | 6 27 7 12 15 5 26 10 9 16 4 | 16 32 22 17 26 16 32 13 19 16 16
19 | 8 20 8 8 15 4 23 14 9 24 4 | 22 31 20 18 23 20 32 22 27 17 20
20 | 9 22 11 8 16 5 22 13 9 16 4 | 12 25 17 13 27 12 26 14 18 13 13
21E | 12 18 9 10 14 6 18 10 11 9 4 | 31 39 35 39 39 35 40 35 38 37 34
22 | 6 25 7 13 17 4 26 10 6 13 4 | 15 34 26 21 32 18 30 14 18 18 19
23 | 10 24 8 12 21 4 26 9 8 25 5 | 18 30 25 26 30 19 29 16 24 18 20
24E | 16 24 11 10 21 6 23 18 14 23 6 | 108 102 101 107 100 101 96 114 103 94 102
X25 | 15 --- 7 11 18 6 --- 12 8 --- 5 | 27 --- 37 35 43 31 --- 42 39 --- 36
26 | 5 16 8 10 14 5 15 12 10 12 3 | 19 28 28 26 31 23 24 30 23 25 24
27E | 11 20 7 11 20 5 19 22 19 17 5 | 27 33 28 30 38 27 37 35 36 29 28
28 | 7 19 8 17 11 4 27 13 8 23 5 | 28 33 32 36 38 29 32 31 31 29 30
X29 | 9 18 6 11 16 7 20 8 8 --- 4 | 14 24 18 17 18 14 26 19 21 --- 15
30 | 9 19 6 9 16 4 13 11 8 12 3 | 32 28 31 30 37 30 29 38 34 29 32
31E | 8 22 9 10 21 5 28 17 10 15 5 | 18 30 21 22 28 19 30 25 27 25 21
32 | 9 21 12 9 16 5 18 18 7 21 4 | 15 24 21 18 24 18 25 17 23 28 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 21 9 11 17 5 22 15 11 19 |T 27 35 31 30 36 33 34 31 32 30 28
WRMS | 8 21 9 10 17 5 22 12 8 18 |NE 19 28 25 23 30 28 27 23 24 22 21
MEDI | 8 21 8 10 16 5 22 13 9 17 |MD 22 30 27 25 33 22 30 27 27 27 23
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 4.1606 GPS week: 1606 MJD: 55486.0-55492.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 |U 8 8 20 |U 9 12 28 |U 7 7 18 |
emr | emr 2861 |U 12 11 33 |U 14 15 40 | 8 6 22 |
esa | esa 2976 | 9 9 21 |U 8 11 28 | 7 7 15 |
gfz | gfz 3027 |U 15 13 30 |U 23 20 48 |U 10 7 18 |
grg | grg 2976 | 19 14 84 |U 9 12 29 | 8 8 20 |
igr | igr 2950 | 9 9 25 | 10 12 31 | 7 6 16 |
igs | igs 2920 | 8 8 23 | 10 12 27 | 8 6 16 |
jpl | jpl 2858 |U 14 12 44 | 17 17 41 |U 7 6 20 |
mit | mit 3003 |U 15 11 66 |U 15 16 46 |U 11 9 20 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1606.0 GPS week: 1606 Day: 0 MJD: 55486.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 | 6 7 23 | 9 18 37 | 6 5 16 |
emr | emr 2860 | 9 8 36 | 19 25 62 | 10 7 24 |
esa | esa 2976 | 6 6 15 | 10 16 39 | 7 6 14 |
gfz | gfz 3036 | 15 14 30 | 27 22 47 | 12 9 25 |
grg | grg 2976 | 20 15 32 | 11 17 44 | 12 10 24 |
igr | igr 2964 | 7 8 34 | 11 16 37 | 6 6 12 |
igs | igs 2936 | 7 6 30 | 11 16 33 | 6 5 18 |
jpl | jpl 2856 | 13 11 42 | 17 23 51 | 7 5 20 |
mit | mit 2976 | 7 8 29 | 15 21 41 | 12 6 18 |
Table 5.1606.1 GPS week: 1606 Day: 1 MJD: 55487.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3049 | 9 10 18 | 10 13 24 | 8 8 24 |
emr | emr 2860 | 11 12 29 | 20 17 34 | 10 6 28 |
esa | esa 2976 | 8 8 23 | 8 10 22 | 7 8 16 |
gfz | gfz 3033 | 18 17 35 | 22 18 55 | 11 8 18 |
grg | grg 2976 | 12 13 25 | 9 12 23 | 8 9 25 |
igr | igr 2982 | 10 10 26 | 11 14 33 | 7 7 15 |
igs | igs 2949 | 9 10 23 | 12 12 26 | 11 7 19 |
jpl | jpl 2858 | 10 13 33 | 17 18 37 | 7 5 25 |
mit | mit 2976 | 9 9 24 | 21 17 50 | 11 8 16 |
Table 5.1606.2 GPS week: 1606 Day: 2 MJD: 55488.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 | 9 7 19 | 8 8 24 | 8 7 15 |
emr | emr 2860 | 14 10 44 | 10 7 30 | 8 8 19 |
esa | esa 2976 | 11 7 21 | 7 7 23 | 8 8 12 |
gfz | gfz 3045 | 19 17 35 | 22 20 48 | 12 7 16 |
grg | grg 2976 | 64 28 443 | 8 8 19 | ---- ---- ---- |
igr | igr 2968 | 12 6 27 | 7 10 22 | 7 8 11 |
igs | igs 2930 | 10 6 21 | 7 8 20 | 6 5 13 |
jpl | jpl 2857 | 17 14 61 | 18 12 43 | 6 7 19 |
mit | mit 3072 | 11 10 38 | 12 13 45 | 8 7 13 |
Table 5.1606.3 GPS week: 1606 Day: 3 MJD: 55489.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 7 8 23 | 9 13 34 | 7 8 13 |
emr | emr 2860 | 12 12 33 | 9 11 35 | 9 8 20 |
esa | esa 2976 | 9 11 26 | 8 11 29 | 10 8 17 |
gfz | gfz 3040 | 17 14 30 | 21 21 56 | 13 8 19 |
grg | grg 2976 | 8 10 25 | 9 11 31 | 8 7 17 |
igr | igr 2987 | 10 9 19 | 10 14 34 | 9 7 19 |
igs | igs 2974 | 8 8 26 | 9 13 33 | 9 7 13 |
jpl | jpl 2857 | 10 10 38 | 12 12 40 | 9 9 21 |
mit | mit 3072 | 8 7 21 | 13 14 46 | 8 11 15 |
Table 5.1606.4 GPS week: 1606 Day: 4 MJD: 55490.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 8 7 14 | 9 10 23 | 7 6 18 |
emr | emr 2860 | 11 12 30 | 15 13 38 | 6 4 19 |
esa | esa 2976 | 9 13 19 | 9 9 26 | 7 6 16 |
gfz | gfz 2958 | 11 10 25 | 23 17 38 | 9 7 19 |
grg | grg 2976 | 8 12 18 | 10 11 27 | 7 6 17 |
igr | igr 2854 | 9 13 23 | 10 9 29 | 7 6 17 |
igs | igs 2956 | 7 9 18 | 10 9 24 | 7 6 15 |
jpl | jpl 2858 | 18 16 42 | 19 17 37 | 6 5 19 |
mit | mit 2976 | 44 25 270 | 17 15 48 | 27 22 39 |
Table 5.1606.5 GPS week: 1606 Day: 5 MJD: 55491.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 8 8 20 | ---- ---- ---- | 7 7 20 |
emr | emr 2864 | 16 12 35 | ---- ---- ---- | 8 6 24 |
esa | esa 2976 | 10 6 22 | ---- ---- ---- | 7 7 19 |
gfz | gfz 3044 | 15 9 28 | ---- ---- ---- | 8 7 19 |
grg | grg 2976 | 10 8 25 | ---- ---- ---- | 8 8 22 |
igr | igr 2944 | 9 8 21 | ---- ---- ---- | 7 6 19 |
igs | igs 2820 | 10 7 21 | ---- ---- ---- | 7 6 19 |
jpl | jpl 2862 | 19 10 51 | ---- ---- ---- | 7 7 20 |
mit | mit 2976 | 16 13 57 | ---- ---- ---- | 8 7 20 |
Table 5.1606.6 GPS week: 1606 Day: 6 MJD: 55492.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3008 | 9 10 23 | ---- ---- ---- | 7 7 19 |
emr | emr 2863 | 14 13 27 | ---- ---- ---- | 5 6 19 |
esa | esa 2976 | 9 11 23 | ---- ---- ---- | 6 4 13 |
gfz | gfz 3035 | 11 8 29 | ---- ---- ---- | 6 5 14 |
grg | grg 2976 | 8 8 20 | ---- ---- ---- | 7 5 17 |
igr | igr 2954 | 9 12 22 | ---- ---- ---- | 7 5 16 |
igs | igs 2876 | 7 11 21 | ---- ---- ---- | 8 5 18 |
jpl | jpl 2864 | 13 9 41 | ---- ---- ---- | 7 6 19 |
mit | mit 2976 | 8 8 24 | ---- ---- ---- | 6 4 18 |
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 6.1606 GPS week: 1606 MJD: 55486.500-55492.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -3 -47 -45 -7 -1 | 14 22
| 20 20 85 92 5 | 3
emr uuuuu | 7 29 -6 -150 -13 | 75 78
| 23 25 139 36 16 | 4
esa uuuuu | -4 -33 -24 46 1 | 17 24
| 21 16 46 71 5 | 2
gfz uuuuu | -11 4 -46 -41 -3 | 11 21
| 19 19 54 56 6 | 3
grg uuuux | 14 -34 -26 -1 12 | -3 19
| 39 16 75 168 25 | 3
igr xxxxx | -1 21 39 -48 1 | -5 18
| 16 6 72 92 2 | 2
irf xxxxx | 4 -8 -19 15 -2 | 4 16
| 7 9 75 46 8 | 3
jpl uuuuu | 44 -11 26 49 -14 | 27 35
| 37 24 71 58 11 | 4
mit uuuuu | -16 -24 0 54 1 | 25 30
| 12 16 108 71 10 | 3
ngs uuuuu | 2 71 116 -30 1 | 6 14
| 30 29 67 106 9 | 3
sio uuuuu | 0 25 -48 -20 -6 | 54 56
| 9 22 100 90 11 | 3
Table 7.1606.0 GPS week: 1606 Day: 0 MJD: 55486.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 1 -72 22 -134 5 | 9 20
emr uuuuu | 19 42 -106 -194 20 | 70 73
esa uuuuu | 20 -41 -76 162 9 | 13 20
gfz uuuuu | 11 -13 34 43 4 | 7 18
grg uuuux | -62 -12 -39 -331 -34 | -4 26
igr xxxxx | 0 21 99 44 1 | -7 18
irf xxxxx | 15 -1 38 55 7 | -1 14
jpl uuuuu | 51 -4 56 13 -5 | 26 34
mit uuuuu | 4 -5 54 110 9 | 20 24
ngs uuuuu | -36 48 43 -123 -16 | 9 18
sio uuuuu | -10 19 52 11 5 | 48 51
Table 7.1606.1 GPS week: 1606 Day: 1 MJD: 55487.500
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 -28 -27 -57 5 | 13 23
emr uuuuu | -5 53 -180 -98 -4 | 76 80
esa uuuuu | 13 -41 -48 67 0 | 16 24
gfz uuuuu | 11 28 -21 -81 4 | 11 22
grg uuuux | -11 -39 -46 -67 -7 | -7 26
igr xxxxx | -5 16 -4 -99 4 | -5 19
irf xxxxx | 12 -20 57 58 4 | 2 18
jpl uuuuu | -35 -30 -114 25 -2 | 29 36
mit uuuuu | -7 -35 121 102 9 | 23 29
ngs uuuuu | 11 117 139 -150 -5 | 8 17
sio uuuuu | -9 -16 19 103 3 | 51 55
Table 7.1606.2 GPS week: 1606 Day: 2 MJD: 55488.500
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 -57 -134 -87 -6 | 18 23
emr uuuuu | -38 46 8 -153 -18 | 81 83
esa uuuuu | -5 -46 -6 2 -2 | 19 25
gfz uuuuu | 1 25 -103 -111 -2 | 15 22
grg uuuux | 35 -48 -176 -41 17 | -6 25
igr xxxxx | 22 13 -99 -89 -1 | -2 17
irf xxxxx | 7 5 20 47 1 | 6 16
jpl uuuuu | 60 -18 -10 78 -20 | 33 37
mit uuuuu | -13 -1 68 106 6 | 27 31
ngs uuuuu | -9 47 164 38 5 | 9 17
sio uuuuu | -6 29 -3 38 0 | 55 58
Table 7.1606.3 GPS week: 1606 Day: 3 MJD: 55489.500
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 44 -8 0 | 15 22
emr uuuuu | 27 26 -85 -185 -21 | 78 81
esa uuuuu | -9 -6 -41 -34 4 | 17 24
gfz uuuuu | -15 18 6 -81 -1 | 12 21
grg uuuux | 15 -54 -9 157 10 | -1 16
igr xxxxx | -6 29 73 -106 -3 | -5 18
irf xxxxx | 3 -18 18 14 4 | 3 17
jpl uuuuu | 37 -35 71 57 -16 | 29 36
mit uuuuu | -21 -47 50 64 9 | 25 30
ngs uuuuu | 18 75 15 18 0 | 5 14
sio uuuuu | 4 19 -1 15 0 | 54 57
Table 7.1606.4 GPS week: 1606 Day: 4 MJD: 55490.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 5 -55 -58 62 -8 | 16 23
emr uuuuu | 6 31 -31 -153 -30 | 77 80
esa uuuuu | -32 -50 50 -7 -8 | 18 25
gfz uuuuu | -23 -15 -52 -48 -4 | 13 22
grg uuuux | 25 -17 11 48 22 | -3 11
igr xxxxx | -25 19 108 -148 1 | -6 18
irf xxxxx | -1 -9 -76 26 -5 | 5 17
jpl uuuuu | 56 -28 22 -12 -34 | 28 36
mit uuuuu | -18 -30 -88 80 0 | 27 32
ngs uuuuu | 42 106 129 36 8 | 3 12
sio uuuuu | -4 33 -117 -36 -9 | 56 59
Table 7.1606.5 GPS week: 1606 Day: 5 MJD: 55491.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 10 -34 22 126 -6 | 16 23
emr uuuuu | 25 27 209 -105 -18 | 74 78
esa uuuuu | 13 -28 -62 21 1 | 19 25
gfz uuuuu | -38 -1 -96 -22 -9 | 13 22
grg uuuux | 43 -40 21 110 35 | -2 12
igr xxxxx | 18 19 39 -45 2 | -5 18
irf xxxxx | -2 -6 -31 -55 -8 | 7 16
jpl uuuuu | 79 14 59 20 -10 | 26 35
mit uuuuu | -33 -24 -12 -76 -6 | 29 33
ngs uuuuu | -36 57 114 116 5 | 3 12
sio uuuuu | 13 46 -44 -109 -17 | 58 59
Table 7.1606.6 GPS week: 1606 Day: 6 MJD: 55492.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -6 -63 -180 49 2 | 14 21
emr uuuuu | 18 -23 142 -159 -17 | 70 74
esa uuuuu | -30 -19 19 110 2 | 17 24
gfz uuuuu | -26 -15 -88 15 -11 | 10 19
grg uuuux | 52 -26 57 121 39 | 0 14
igr xxxxx | -10 29 60 107 3 | -7 18
irf xxxxx | -5 -8 -155 -41 -16 | 4 16
jpl uuuuu | 62 27 98 162 -9 | 20 30
mit uuuuu | -26 -25 -193 -10 -18 | 27 31
ngs uuuuu | 22 49 207 -141 8 | 2 11
sio uuuuu | 10 48 -239 -161 -22 | 55 57
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