[IGSREPORT-19904] Wk 1640 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Fri Jul 1 04:41:00 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1640 (Jun 12, 2011 - Jun 18, 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:
igs1640[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1640[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1640[0-6].cls IGS GPS clock combination summary report.
igs16407.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16407.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 | ALL | 30
0 | COD | HRAO HRAO
0 | EMR | 30 YELL YELL
0 | ESA | IRKJ
0 | GFZ | MDVJ SFER
0 | GRG | IRKJ
0 | JPL | 25 COCO
0 | MIT | 30
1 | COD | WILL WROC
1 | EMR | 30
1 | ESA | IRKJ UNSA
1 | GFZ | 15 ISPA MDVJ
1 | GRG | IRKJ
1 | JPL | 15 25
1 | MIT | 23 30 23 30 MDVJ
2 | COD | 30 30
2 | EMR | YELL
2 | ESA | ALIC IRKJ UNSA
2 | GFZ | 30 MDVJ
2 | GRG | IRKJ NKLG
2 | JPL | 25 COCO
2 | MIT | CAS1 MAW1 CAS1 MAW1
3 | COD | 30 30
3 | GFZ | 30 GOLD MDVJ YAR2
3 | GRG | IRKJ SANT
3 | JPL | 25
3 | MIT | 30 30
4 | EMR | 30
4 | ESA | IRKJ UNSA
4 | GFZ | 30 CHUR MDVJ
4 | GRG | USN3
4 | JPL | 25
4 | MIT | 30
5 | ESA | 30 ALIC NICO UNSA
5 | GFZ | 25 30 MDVJ REUN
5 | GRG | ADIS AMC2 REUN SANT
5 | JPL | 25 AREQ
5 | MIT | 30 30 MAW1
6 | COD | BRMU
6 | EMR | 30
6 | ESA | IRKJ UNSA
6 | GFZ | 12 25 30 MDVJ
6 | GRG | USN3
6 | JPL | 25 WHIT
6 | MIT | 12 30 12 30 DAV1 DAV1 MDVJ
5. 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.
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 | -.5 .4 .2 -19 -4 -9 .17
EMR | 4.4 -3.7 6.4 26 3 -13 .36
ESA | 2.7 -5.0 11.7 -45 -51 53 .17
GFZ | -2.9 .4 -.5 -3 40 3 .14
GRG | 2.1 -.7 21.9 -8 15 -26 .15
JPL | 2.1 -3.8 1.4 -5 27 81 -1.03
MIT | 3.6 -4.3 15.4 -14 7 -26 .14
NGS | 3.4 -4.5 16.8 -49 12 0 .17
SIO | .1 -4.8 -4.8 -100 -74 -3 .15
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 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 does not yet use IGS08/igs08.atx, which causes their RMS
clock residuals to be higher than for the other centres; for the same
reason, 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 1.1640.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1640.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 2.1640.[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 3.1640.[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 5.1640.0-6).
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 1640 summary. (Jun 12, 2011 - Jun 18, 2011)
Table 1.1640.a GPS week: 1640 MJD: 55724.000-55730.000
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 249| 0 0 -2 -13 12 -11 -.21 7 7 | -672 -54 15 91
| 0 0 0 15 6 27 .02 | 413 438
emr 108| 0 -1 -3 -108 25 -8 .39 18 17 | 1068 -241 17 117
| 1 1 1 5 31 18 .03 | 1224 1396
esa 128| 0 0 2 22 67 8 .27 7 7 | -436 -392 15 128
| 0 0 1 9 14 17 .01 | 907 620
gfz 193| -1 0 0 -57 -119 10 -.11 10 10 | -122 276 23 142
| 0 1 1 30 51 7 .03 | 649 965
grg 133| 2 1 6 -51 -1 0 .48 18 16 | -101 -29 49 262
| 0 1 1 28 30 27 .13 | 404 707
igr n/a| 0 0 -1 -19 6 -18 -.07 5 5 | 20136 236 20 108
| 0 0 1 8 12 10 .02 | 2141 1311
jpl 139| -1 0 -5 -42 -51 0 .57 17 16 | 562 -81 19 333
| 0 1 1 18 13 21 .02 | 1632 1493
mit 257| 0 0 1 -27 -33 -23 -.35 11 10 | -254 3 20 164
| 0 0 0 21 19 19 .03 | 714 972
ngs 226| 0 0 1 70 -27 2 -.20 9 7 | -692 -48 2006 3863
| 0 0 1 15 21 20 .02 | 417 452
sio 251| -2 0 -1 182 128 23 -.15 18 18 | --- --- --- ---
| 0 0 1 26 19 13 .03 | --- ---
Table 1.1640.b GPS week : 1640 MJD: 55724.000-55730.000
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 | 0 0 0 0 0 0 0 |
2 | 4 5 5 5 5 5 6 |
3 | 3 3 3 3 3 3 4 |
4 | 3 4 4 3 4 4 5 |
5 | 4 5 4 4 4 5 5 |
6 | 3 3 3 3 3 3 4 |
7 | 4 4 4 4 5 5 5 |
8 | 4 3 3 3 3 4 5 |
9 | 4 3 4 3 4 3 4 |
10 | 3 3 3 3 4 4 4 |
11 | 3 4 3 4 3 4 4 |
12 | 5 4 5 5 4 5 5 |
13 | 5 4 4 4 4 4 5 |
14 | 4 4 4 4 4 5 4 |
15 | 4 5 4 4 5 4 5 |
16 | 4 4 4 4 4 4 5 |
17 | 5 5 5 4 4 4 5 |
18 | 4 4 4 4 4 4 5 |
19 | 4 4 4 5 4 5 5 |
20 | 4 4 4 4 3 4 4 |
21 | 4 4 4 3 4 4 5 |
22 | 4 3 3 3 3 4 4 |
23 | 5 4 4 4 5 5 5 |
24 | 4 4 3 4 3 4 4 |
25 | 4 4 4 5 5 7 11 |
26 | 4 4 4 4 5 5 5 |
27 | 3 3 3 3 4 4 4 |
28 | 4 4 4 4 4 5 4 |
29 | 5 5 4 4 4 4 5 |
30 | 15 12 12 13 9 10 8 |
31 | 4 4 4 4 5 5 5 |
32 | 4 4 4 4 4 4 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 2.1640.0 GPS week: 1640 Day: 0 MJD: 55724.000
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 249| 0 0 -1 9 10 -21 -.21 6 6 | -836 513 13 87
| 8 -9 |
emr 108| 1 1 -4 -104 67 -11 .38 18 18 | 764 -411 15 102
| 9 -110 |
esa 128| 1 0 1 30 76 9 .24 6 6 | -606 -644 14 126
| 6 8 |
gfz 193| -3 -1 0 -102 -167 17 -.15 10 9 | -1196 1908 23 145
| -14 101 |
grg 133| 1 0 8 -49 -56 -7 .60 14 13 | -648 438 41 247
| 78 11 |
igr n/a| 0 0 -1 -11 7 -24 -.07 5 5 | 17640 90 21 112
| -27 43 |
jpl 139| 0 1 -7 -15 -68 18 .56 17 16 | -290 -805 18 324
| -41 78 |
mit 269| 0 0 0 -34 -7 1 -.38 11 9 | -639 467 20 140
| 0 20 |
ngs 226| 0 0 1 85 0 0 -.20 9 8 | -853 560 2046 4107
| -24 -29 |
sio 251| -4 0 -2 169 160 28 -.16 19 19 | --- --- --- ---
| -136 -102 |
Table 2.1640.1 GPS week: 1640 Day: 1 MJD: 55725.000
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 249| 0 0 -2 -5 8 8 -.23 6 6 | -213 -624 15 92
| 27 4 |
emr 108| 0 -1 -4 -117 66 -35 .38 17 17 | 1544 -62 16 121
| 9 -99 |
esa 128| 0 0 2 26 54 -12 .27 7 7 | 479 -733 15 136
| 29 24 |
gfz 193| -2 0 -1 -76 -140 16 -.11 11 10 | 632 -754 23 144
| -47 66 |
grg 133| 1 0 7 -74 -11 -28 .56 14 12 | 308 227 47 241
| 68 -89 |
igr n/a| 0 0 -1 -17 14 -34 -.09 5 5 | 19067 425 20 97
| -10 24 |
jpl 139| -1 0 -4 -61 -62 -28 .53 17 16 | 24 8 19 360
| -36 12 |
mit 269| 0 0 0 1 -22 -11 -.39 11 9 | -173 537 23 179
| 1 22 |
ngs 226| 0 0 1 66 -24 16 -.19 8 8 | -232 -633 2072 4487
| 7 -47 |
sio 251| -2 1 -2 189 136 21 -.17 17 15 | --- --- --- ---
| -142 -88 |
Table 2.1640.2 GPS week: 1640 Day: 2 MJD: 55726.000
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 249| 0 0 -2 3 23 -45 -.23 6 6 | -496 -478 16 90
| -15 -58 |
emr 108| 0 0 -4 -109 4 -14 .38 18 18 | 1811 -3018 15 114
| -9 -31 |
esa 128| 0 0 0 37 86 18 .27 7 6 | -2118 -1046 16 120
| 14 2 |
gfz 193| -2 0 1 -75 -191 16 -.16 9 9 | 141 -358 24 133
| -64 56 |
grg 133| 2 0 7 -43 26 7 .57 15 14 | 121 -494 58 244
| 37 -123 |
igr n/a| 0 0 0 -33 15 -7 -.09 4 4 | 19818 -1975 19 112
| -17 9 |
jpl 139| 0 1 -6 -26 -41 29 .60 17 16 | 476 -2611 20 322
| -1 -91 |
mit 269| 0 0 0 -67 -62 -2 -.35 10 9 | 258 -856 21 179
| 18 21 |
ngs 226| 1 -1 3 72 1 7 -.18 8 7 | -513 -478 2194 3872
| -27 -46 |
sio 251| -2 1 -1 141 105 40 -.13 16 16 | --- --- --- ---
| -142 -90 |
Table 2.1640.3 GPS week: 1640 Day: 3 MJD: 55727.000
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 249| 0 0 -2 -22 20 4 -.17 6 6 | -137 -316 14 83
| 22 -1 |
emr 108| 2 -1 -2 -113 26 -18 .39 17 17 | -1064 768 19 116
| -6 -65 |
esa 128| 0 0 2 14 50 18 .27 8 7 | 576 -248 18 126
| 56 40 |
gfz 193| -1 0 -2 -23 -105 12 -.07 10 10 | 535 -728 22 152
| -20 83 |
grg 133| 2 0 4 -62 5 -10 .54 16 14 | 380 -1430 43 263
| 71 -94 |
igr n/a| 0 0 0 -29 11 -12 -.07 5 5 | 18207 1556 21 133
| -4 20 |
jpl 139| -1 2 -3 -46 -54 8 .60 16 14 | -1793 1463 20 331
| -10 -35 |
mit 269| 0 0 2 -15 -21 -38 -.32 9 8 | 493 -1407 21 181
| -18 8 |
ngs 226| 1 0 2 46 -31 10 -.22 8 6 | -148 -321 2071 3841
| -7 -50 |
sio 251| -3 0 -1 199 145 3 -.11 16 21 | --- --- --- ---
| -167 -88 |
Table 2.1640.4 GPS week: 1640 Day: 4 MJD: 55728.000
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 249| 0 0 -3 -31 8 -28 -.20 7 7 | -1036 418 18 100
| -4 -28 |
emr 108| -2 -3 0 -106 -13 0 .42 17 17 | 120 1388 18 128
| -6 -20 |
esa 128| 0 1 2 9 78 17 .27 6 6 | -686 505 14 123
| 52 13 |
gfz 193| 0 1 -1 -22 -110 6 -.09 12 11 | -674 877 24 143
| 14 68 |
grg 133| 3 2 7 -32 32 -12 .43 20 16 | -578 543 49 318
| 68 -150 |
igr n/a| 0 0 -1 -13 16 -20 -.06 6 5 | 20324 1890 19 101
| -9 14 |
jpl 139| -2 -2 -3 -66 -44 -1 .57 18 16 | 171 1794 20 331
| 171 14 |
mit 269| 0 0 0 -16 -41 -28 -.33 9 9 | 220 -528 19 165
| -4 8 |
ngs 226| 0 -2 1 59 -47 24 -.22 9 7 | -1055 420 2007 3706
| -13 -27 |
sio 251| -3 1 -2 202 121 31 -.15 18 18 | --- --- --- ---
| -166 -83 |
Table 2.1640.5 GPS week: 1640 Day: 5 MJD: 55729.000
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 249| 0 0 0 -25 9 33 -.20 8 7 | -1248 135 16 91
| 9 -19 |
emr 108| -1 -3 -5 -99 5 -1 .43 17 17 | 1744 172 22 121
| -10 -52 |
esa 128| 1 0 0 20 74 27 .27 7 7 | -623 365 19 123
| 29 9 |
gfz 193| -1 0 0 -40 -40 2 -.09 10 10 | -99 544 23 142
| 23 51 |
grg 133| 2 1 7 -91 -19 -2 .22 24 21 | -121 88 58 252
| 103 -93 |
igr n/a| 0 0 -2 -15 -17 -24 -.05 6 5 | 22467 375 24 105
| 2 59 |
jpl 139| -2 0 -5 -32 -55 -23 .56 18 17 | 2271 302 22 339
| -17 -96 |
mit 269| 0 0 1 -25 -54 -45 -.33 10 10 | -1617 1423 19 155
| -9 17 |
ngs 226| 0 0 0 69 -54 -38 -.18 9 7 | -1278 147 1798 3148
| 34 20 |
sio 251| -2 1 1 216 116 6 -.15 20 20 | --- --- --- ---
| -176 -84 |
Table 2.1640.6 GPS week: 1640 Day: 6 MJD: 55730.000
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 249| 1 -1 -1 -19 5 -30 -.25 12 11 | -744 -31 19 97
| 7 -44 |
emr 108| 1 -2 -3 -110 20 25 .35 18 17 | 2558 -530 18 119
| -5 -32 |
esa 128| 0 0 4 17 55 -17 .27 8 7 | -77 -944 15 144
| 36 39 |
gfz 193| 0 1 -2 -63 -79 -1 -.12 10 10 | -196 444 23 139
| -10 93 |
grg 133| 2 5 4 -4 13 56 .43 22 20 | -169 419 51 275
| -41 -79 |
igr n/a| 0 0 -3 -14 -3 -4 -.08 6 6 | 23431 -703 21 100
| 17 6 |
jpl 139| 0 0 -7 -48 -30 -1 .55 18 17 | 3081 -721 20 326
| -4 57 |
mit 269| 0 0 1 -33 -27 -40 -.35 15 11 | -325 388 17 155
| 1 -11 |
ngs 226| 0 0 -1 93 -34 -6 -.21 10 7 | -768 -32 1860 3883
| -52 4 |
sio 251| -2 0 1 157 111 33 -.22 22 19 | --- --- --- ---
| -140 -97 |
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 3.1640.0 GPS week: 1640 Day: 0 MJD: 55724.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 3 --- --- --- --- 142 --- --- --- --- 0 | 43 --- --- --- --- 62 --- --- --- --- 44
2 | 6 15 7 8 14 5 17 7 9 36 4 | 25 26 27 27 26 26 27 25 26 24 24
3 | 5 13 4 8 11 3 9 7 8 16 3 | 14 23 17 19 25 15 19 15 20 20 17
4 | 6 12 5 7 12 5 12 10 11 20 3 | 32 31 33 35 34 34 25 38 34 39 32
5 | 4 25 9 13 18 5 20 9 8 15 4 | 15 27 16 16 26 13 24 15 18 18 14
6 | 4 12 5 8 10 2 9 7 7 14 2 | 21 26 22 25 30 21 22 22 26 22 23
7 | 6 20 6 9 19 6 18 10 7 16 4 | 16 26 13 18 24 14 22 13 16 19 13
8 | 4 16 7 6 13 6 11 16 9 13 3 | 13 20 13 14 15 13 17 20 15 14 12
9 | 6 14 5 10 10 4 15 12 12 15 3 | 17 24 19 20 23 17 27 17 22 13 18
10 | 7 15 6 9 11 5 11 7 7 21 3 | 15 20 15 17 17 13 17 17 19 21 14
11 | 7 15 6 13 7 5 13 6 7 16 3 | 39 48 41 47 53 39 45 39 43 40 42
12E | 7 19 9 8 19 4 26 12 11 13 4 | 32 37 37 29 36 33 38 34 35 32 33
13 | 7 22 8 11 21 4 21 12 8 18 4 | 18 31 19 17 33 16 27 18 23 17 18
14 | 5 22 8 10 16 4 15 12 10 17 4 | 15 29 18 17 24 15 20 17 16 18 15
15 | 5 19 6 11 20 5 19 9 10 17 4 | 17 26 19 24 29 17 25 21 20 18 18
X16E | 6 17 6 13 --- 5 20 12 10 11 4 | 18 23 19 20 --- 16 24 19 19 17 17
17 | 6 22 6 9 13 6 21 14 12 26 4 | 19 27 23 23 22 21 29 24 23 25 19
18 | 6 18 5 11 15 6 20 8 12 18 4 | 26 31 22 18 25 21 34 24 28 27 23
19 | 6 16 7 10 12 5 21 11 7 32 4 | 20 30 26 24 31 21 34 21 20 29 22
20 | 5 21 5 8 16 5 16 9 9 13 3 | 21 27 21 18 26 19 23 19 23 21 19
21 | 4 11 3 10 10 5 13 8 9 29 3 | 33 31 31 35 27 31 34 35 34 32 31
22 | 4 15 6 10 14 6 12 10 11 15 3 | 20 24 19 18 23 17 23 22 20 23 18
23 | 8 28 7 14 16 4 22 10 7 16 4 | 15 33 21 13 27 15 30 16 20 14 16
24 | 5 18 6 17 11 5 10 8 6 15 3 | 21 26 24 31 28 21 23 20 23 21 22
25E | 4 25 7 8 12 5 16 11 10 10 3 | 43 50 42 41 42 39 47 44 41 41 41
26 | 6 14 6 8 13 7 12 13 8 18 3 | 37 35 36 29 36 35 37 33 34 29 34
27 | 5 13 6 8 13 4 14 9 10 14 3 | 14 20 17 17 21 15 23 12 19 13 14
28E | 6 15 7 9 12 4 20 12 6 18 3 | 19 20 17 17 20 17 22 17 19 21 17
29 | 10 19 7 9 15 5 22 14 10 18 4 | 21 29 25 20 25 23 30 24 24 20 22
X30E | 29 27 14 21 29 16 --- 60 --- --- 14 | 46 60 59 63 56 54 --- 71 --- --- 51
31 | 6 19 6 13 19 6 19 10 9 17 4 | 12 28 17 18 32 14 26 12 14 12 14
32 | 8 21 6 11 11 4 16 12 8 15 3 | 23 29 23 21 24 18 28 23 24 26 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 18 6 10 14 5 17 11 9 19 |T 23 29 24 24 28 23 27 24 23 22 23
WRMS | 6 18 6 9 13 5 16 9 8 19 |NE 20 27 22 22 27 20 26 21 23 22 20
MEDI | 6 18 6 10 13 5 16 10 9 16 |MD 20 27 21 20 26 18 25 21 22 21 19
Table 3.1640.1 GPS week: 1640 Day: 1 MJD: 55725.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 4 --- --- --- --- 35 --- --- --- --- 0 | 26 --- --- --- --- 35 --- --- --- --- 28
2 | 5 13 10 8 9 7 17 9 9 35 4 | 17 18 21 19 21 19 23 18 19 25 17
3 | 5 13 5 10 13 3 11 7 6 16 3 | 16 22 19 18 22 17 20 18 20 21 17
4 | 5 14 6 10 10 5 12 9 9 18 3 | 23 27 26 32 24 28 21 32 25 36 25
5 | 4 23 9 13 19 6 20 10 9 16 4 | 13 24 15 16 27 12 23 14 15 18 11
6 | 5 12 8 7 11 3 11 7 7 14 3 | 18 21 23 19 25 20 20 21 22 19 20
7 | 5 18 7 10 17 5 17 6 6 14 3 | 15 26 21 19 26 14 24 16 16 19 15
8 | 4 12 8 8 11 7 13 14 8 10 3 | 15 19 20 15 17 14 20 19 18 17 15
9 | 5 13 5 9 9 4 14 12 10 11 3 | 12 19 18 17 20 13 24 16 15 16 14
10 | 8 12 7 8 9 4 10 8 6 19 3 | 14 20 17 19 18 15 20 19 17 19 14
11 | 8 14 6 15 7 5 14 7 9 14 3 | 22 35 32 36 37 26 35 25 27 25 28
12E | 8 16 9 10 14 4 26 15 10 9 4 | 25 29 28 25 27 24 32 24 24 24 24
13 | 6 17 8 8 22 4 20 11 7 13 4 | 16 28 25 21 32 18 28 21 23 19 19
14 | 4 19 5 11 15 4 19 10 9 16 3 | 15 26 19 18 24 18 24 19 19 19 16
15 | 6 24 6 23 22 4 20 13 8 11 5 | 17 32 23 33 26 19 27 21 21 22 19
16E | 5 14 5 13 17 4 19 13 5 10 3 | 18 24 22 23 28 21 27 24 22 20 20
17 | 7 22 8 11 12 4 22 14 8 23 4 | 16 28 20 23 21 18 26 22 17 20 16
18 | 7 19 7 10 14 4 19 7 9 17 4 | 17 27 21 19 24 18 27 20 21 23 18
19 | 5 16 7 10 9 4 19 11 7 28 4 | 16 28 21 20 27 17 30 19 18 25 18
20 | 7 21 8 10 15 4 17 9 6 12 3 | 22 29 22 21 26 20 25 21 20 22 20
21 | 5 14 5 10 8 4 14 7 7 27 3 | 22 22 22 28 22 23 22 27 26 21 21
22 | 4 15 7 7 15 4 13 7 8 14 3 | 14 23 16 19 21 16 19 20 18 21 15
23 | 7 22 7 10 15 4 21 11 10 16 4 | 12 29 21 16 28 14 29 17 20 16 16
24 | 5 16 7 20 12 5 13 10 9 15 4 | 17 21 20 31 23 19 20 18 20 22 19
25E | 6 25 5 11 15 4 18 11 8 6 4 | 28 41 35 35 33 28 39 30 30 30 30
26 | 7 16 7 10 14 6 13 12 9 11 3 | 39 40 36 41 37 38 38 42 43 41 38
27 | 4 12 5 9 13 3 13 10 9 11 3 | 12 18 16 16 21 12 21 13 14 14 13
28E | 7 13 9 12 12 5 24 10 7 15 4 | 14 19 17 19 21 15 21 18 18 18 14
29 | 8 22 8 6 12 5 22 16 9 17 4 | 19 33 27 23 28 23 31 21 25 23 22
X30E | 22 30 12 17 24 17 --- 46 --- --- 11 | 33 43 41 39 41 39 --- 60 --- --- 36
31 | 5 20 4 13 17 5 18 9 8 16 3 | 16 28 18 19 30 17 27 15 18 15 16
32 | 10 19 5 12 13 5 15 12 10 12 4 | 22 29 23 21 24 19 29 20 23 24 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 17 7 11 14 5 17 11 8 17 |T 18 26 22 23 25 20 25 22 21 21 19
WRMS | 6 17 7 10 12 5 16 9 8 15 |NE 17 25 21 22 25 18 25 20 20 21 18
MEDI | 5 16 7 10 13 4 17 10 8 14 |MD 17 27 21 20 25 18 24 20 20 21 18
Table 3.1640.2 GPS week: 1640 Day: 2 MJD: 55726.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 4 --- --- --- --- 46 --- --- --- --- 0 | 25 --- --- --- --- 44 --- --- --- --- 27
2 | 6 15 7 7 10 6 16 9 8 37 4 | 19 20 21 19 22 19 24 19 18 19 17
3 | 6 12 3 10 11 2 11 9 7 15 3 | 22 23 27 22 27 24 23 21 30 22 25
4 | 6 13 9 6 11 5 13 12 8 20 3 | 24 23 26 26 24 25 20 29 27 32 24
5 | 7 26 7 9 18 5 21 7 7 14 4 | 14 25 14 14 26 13 24 14 12 16 12
6 | 4 12 4 9 10 3 11 9 7 13 2 | 22 22 25 25 25 23 24 21 26 21 24
7 | 5 18 8 7 19 4 20 7 6 14 3 | 13 27 21 17 30 14 25 16 15 17 16
8 | 5 16 7 7 12 6 12 7 7 9 3 | 14 22 17 15 21 14 22 17 13 15 14
9 | 7 16 6 7 14 3 12 11 11 11 3 | 13 21 19 15 24 14 23 14 18 11 15
10 | 9 15 6 7 10 5 9 7 6 15 3 | 13 22 16 18 15 15 23 17 19 19 14
11 | 6 13 4 11 10 4 14 8 8 12 3 | 33 39 34 38 42 34 41 32 31 31 35
12E | 8 23 10 9 19 6 27 13 10 9 4 | 24 32 32 28 27 26 33 26 26 25 25
13 | 5 22 7 9 22 3 23 10 5 12 4 | 16 31 20 20 34 18 30 18 22 18 19
14 | 5 19 6 9 19 4 16 10 7 13 3 | 13 25 18 17 26 15 24 17 15 18 16
15 | 6 17 8 10 23 4 22 13 11 11 4 | 13 23 18 16 27 14 23 19 17 21 14
16E | 6 13 5 11 15 3 22 11 6 9 3 | 15 22 21 21 22 17 24 18 17 18 17
17 | 6 23 9 11 11 4 21 14 9 21 4 | 12 25 17 19 18 13 25 17 14 15 12
18 | 5 20 6 10 13 4 16 7 10 16 3 | 18 27 22 12 23 16 27 17 21 22 18
19 | 6 17 6 11 13 3 19 14 10 25 4 | 21 27 26 20 29 20 32 21 19 21 22
20 | 5 20 6 9 15 5 17 9 8 11 3 | 18 26 20 17 27 16 27 18 19 17 18
21 | 5 11 4 10 12 5 13 8 9 27 3 | 19 21 20 22 19 19 24 21 23 25 19
22 | 4 18 7 6 14 4 13 9 10 12 3 | 15 23 19 11 21 15 23 16 19 19 16
23 | 5 22 6 8 17 3 24 8 6 16 4 | 12 26 19 17 28 14 30 15 18 14 15
24 | 4 13 6 14 15 4 12 9 6 12 3 | 19 21 25 27 25 22 25 20 18 18 21
25E | 7 23 5 10 18 4 18 12 11 7 4 | 39 47 38 41 38 36 43 39 37 38 37
26 | 9 16 6 11 17 5 13 10 7 11 3 | 23 27 21 34 19 25 23 29 27 31 22
27 | 5 13 6 10 15 4 11 9 9 11 3 | 12 18 18 17 24 15 22 13 17 11 15
28E | 7 14 7 9 17 4 20 17 4 12 4 | 13 19 18 11 21 13 23 21 17 17 14
29 | 10 23 7 8 12 6 20 10 8 17 4 | 17 31 23 18 25 20 29 16 20 18 19
X30E | 24 28 17 17 32 14 --- 43 --- --- 12 | 27 38 36 35 40 32 --- 57 --- --- 31
31 | 6 17 7 8 20 6 16 7 11 13 3 | 14 26 18 18 33 17 27 14 20 14 16
32 | 9 17 7 14 15 6 19 12 9 11 4 | 19 26 22 20 23 17 31 19 19 23 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 18 7 9 15 4 17 10 8 16 |T 18 25 22 20 25 19 26 21 20 20 19
WRMS | 6 18 6 9 14 4 16 9 7 16 |NE 17 24 21 19 25 18 25 18 19 19 18
MEDI | 6 17 6 9 15 4 16 9 8 12 |MD 17 25 21 19 25 17 24 18 19 18 18
Table 3.1640.3 GPS week: 1640 Day: 3 MJD: 55727.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 3 --- --- --- --- 29 --- --- --- --- 0 | 26 --- --- --- --- 37 --- --- --- --- 26
2 | 7 13 5 12 10 6 13 8 7 38 4 | 26 28 27 29 26 25 29 26 29 24 25
3 | 6 14 7 10 10 4 11 11 6 15 3 | 17 27 17 18 23 17 26 24 17 26 18
4 | 5 12 7 5 11 5 9 11 5 18 3 | 30 31 28 29 29 29 27 35 32 36 29
5 | 7 22 8 11 19 6 19 7 6 15 4 | 18 28 17 20 28 17 26 18 20 19 17
6 | 4 11 6 10 9 5 10 9 7 13 3 | 17 23 18 20 23 16 24 21 16 24 17
7 | 5 17 12 7 21 6 15 9 9 19 4 | 20 30 24 21 32 20 27 20 24 21 20
8 | 4 13 6 6 15 6 11 6 7 9 2 | 19 26 21 19 22 18 23 19 23 20 19
9 | 6 13 8 8 15 5 10 8 5 9 3 | 17 22 20 19 26 16 24 16 16 17 17
10 | 7 12 6 8 11 5 10 5 7 15 3 | 20 24 22 20 21 19 23 22 26 21 20
11 | 7 16 7 11 9 4 11 10 10 13 3 | 33 44 38 42 43 35 42 37 34 38 36
12E | 8 17 12 10 17 5 24 12 9 8 4 | 23 32 32 27 30 25 32 25 26 24 25
13 | 6 22 7 8 25 4 19 8 4 10 3 | 21 34 24 19 36 18 29 21 23 21 20
14 | 6 18 5 15 22 5 18 7 6 12 4 | 16 24 19 19 27 16 24 17 17 17 15
15 | 6 21 7 9 25 6 20 9 8 11 4 | 18 29 21 22 34 19 29 22 20 25 19
16E | 4 18 6 10 13 4 22 7 8 11 3 | 25 29 26 24 24 25 31 23 26 23 24
17 | 8 19 9 10 15 6 17 9 6 21 4 | 21 27 22 25 27 21 27 24 28 19 21
18 | 5 21 8 9 16 5 16 5 8 14 3 | 25 28 22 18 25 20 28 19 22 24 20
19 | 5 18 7 11 11 3 20 15 6 26 4 | 19 32 26 23 30 21 34 26 20 23 22
20 | 5 20 7 7 14 4 15 7 8 12 3 | 24 27 23 20 24 20 28 24 23 23 21
21 | 5 12 5 8 10 6 11 6 6 27 3 | 30 29 28 27 26 28 30 28 29 31 27
22 | 5 16 7 12 16 3 13 7 6 12 3 | 21 24 21 22 24 18 23 19 20 22 18
23 | 7 25 5 5 20 5 23 7 10 15 4 | 15 32 21 17 31 16 31 16 17 16 17
24 | 6 17 9 13 12 5 9 9 8 11 3 | 20 28 24 28 25 22 25 22 24 22 22
25E | 7 24 6 19 21 5 18 10 12 10 4 | 40 46 38 42 40 37 47 41 43 40 39
26 | 7 14 10 8 17 6 12 11 9 15 3 | 50 53 55 51 51 51 52 54 55 54 52
27 | 7 12 5 6 18 4 11 8 7 10 3 | 15 20 17 18 25 15 23 15 15 18 15
28E | 6 13 10 9 14 6 20 8 6 14 3 | 16 22 16 17 20 15 22 17 23 18 15
29 | 9 20 8 10 13 5 21 8 8 17 4 | 23 32 26 22 29 22 31 22 22 23 22
X30E | 24 26 18 20 43 15 --- 43 --- --- 12 | 30 37 25 30 41 26 --- 52 --- --- 26
31 | 5 19 6 8 23 6 18 10 10 16 4 | 17 28 21 20 35 19 29 18 16 16 17
32 | 9 21 7 12 11 4 17 10 11 11 4 | 24 26 25 21 22 20 31 22 23 25 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 17 7 10 16 5 16 9 8 16 |T 23 29 24 24 29 22 29 24 24 24 22
WRMS | 6 17 7 10 14 5 14 8 6 21 |NE 22 29 24 23 28 21 28 23 23 24 21
MEDI | 6 17 7 10 15 5 15 8 7 13 |MD 21 28 23 21 27 20 28 22 23 23 20
Table 3.1640.4 GPS week: 1640 Day: 4 MJD: 55728.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 4 --- --- --- --- 90 --- --- --- --- 0 | 33 --- --- --- --- 77 --- --- --- --- 35
2 | 7 12 5 10 12 5 12 12 10 39 4 | 19 24 20 21 20 19 19 21 22 23 18
3 | 6 13 4 12 14 4 14 9 7 18 3 | 23 28 25 28 30 25 29 28 27 27 25
4 | 9 20 5 12 10 4 9 10 11 21 4 | 29 37 31 28 29 29 30 33 33 39 29
5 | 7 20 6 13 18 7 22 10 9 17 4 | 16 26 17 15 20 15 23 17 22 20 14
6 | 6 11 4 10 14 4 15 9 8 15 3 | 23 26 26 28 31 23 26 27 27 25 25
7 | 7 17 7 11 29 5 17 12 6 24 4 | 16 28 16 18 33 15 27 18 17 24 15
8 | 5 13 6 8 21 4 11 12 8 12 3 | 17 23 16 14 24 15 24 18 23 19 16
9 | 6 12 8 11 19 6 13 9 9 12 3 | 15 20 21 18 27 14 26 16 17 17 16
10 | 8 16 5 10 15 22 12 8 13 16 3 | 19 27 17 19 16 23 23 20 26 22 17
11 | 7 12 4 10 9 6 16 7 7 15 3 | 32 45 35 38 45 33 43 35 36 36 35
12E | 8 15 10 7 15 4 28 11 10 10 4 | 22 29 29 23 33 24 32 23 23 23 23
13 | 5 20 5 11 33 3 22 10 7 12 4 | 16 32 18 20 41 16 31 18 21 20 17
14 | 5 18 5 11 30 5 16 5 8 9 3 | 12 26 17 16 32 14 23 15 17 18 14
15 | 5 20 6 11 36 2 19 8 10 13 4 | 15 26 18 17 39 16 21 18 19 22 15
16E | 6 16 7 9 26 4 23 8 8 13 4 | 17 25 22 20 32 20 25 18 19 19 18
17 | 7 18 9 12 14 7 19 7 6 26 4 | 16 25 18 22 20 18 26 19 20 25 17
18 | 6 19 6 10 17 5 19 6 8 16 3 | 20 27 20 16 18 18 28 18 18 22 17
19 | 7 16 5 11 16 2 21 14 5 27 4 | 18 31 25 23 26 21 33 24 22 21 21
20 | 6 18 5 9 14 3 16 8 7 13 3 | 18 24 19 21 20 16 23 19 20 23 17
21 | 5 10 6 10 10 9 12 7 5 29 3 | 22 20 21 22 18 19 22 24 21 25 20
22 | 5 17 5 8 17 4 14 6 9 13 3 | 15 24 14 13 21 15 23 17 18 20 14
23 | 6 23 5 12 27 3 23 8 9 17 4 | 11 30 17 16 35 12 31 14 18 14 14
24 | 5 17 5 13 13 7 15 8 7 10 3 | 19 27 22 28 24 20 28 21 24 20 21
25E | 11 18 6 20 19 6 21 9 10 15 4 | 65 67 67 69 64 65 69 70 60 69 65
26 | 10 15 5 10 23 4 14 14 14 19 4 | 31 31 29 28 38 29 35 35 31 34 30
27 | 6 12 6 9 22 4 13 10 11 12 3 | 13 20 17 16 28 12 24 12 17 14 13
28E | 4 12 8 9 15 5 20 11 10 17 3 | 17 21 18 17 19 17 29 19 25 23 17
29 | 9 19 8 10 12 6 21 8 9 19 4 | 18 29 22 21 24 18 28 19 20 21 19
X30E | 18 27 10 15 27 11 --- 31 --- --- 9 | 23 42 26 24 34 27 --- 38 --- --- 24
31 | 8 20 8 23 29 8 20 8 13 15 5 | 13 30 18 25 36 15 28 11 17 13 13
32 | 9 22 5 11 14 5 19 10 10 12 4 | 19 28 21 23 18 17 31 19 22 24 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 6 12 20 6 18 9 9 18 |T 20 28 22 22 28 22 28 22 23 24 21
WRMS | 7 17 6 11 16 5 16 9 7 18 |NE 18 27 20 21 27 18 27 20 22 22 18
MEDI | 6 17 6 11 17 5 16 9 9 15 |MD 18 27 20 21 28 18 27 19 21 22 17
Table 3.1640.5 GPS week: 1640 Day: 5 MJD: 55729.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 4 --- --- --- --- 66 --- --- --- --- 0 | 30 --- --- --- --- 80 --- --- --- --- 32
2 | 5 12 6 9 12 7 17 16 8 43 5 | 19 24 23 22 23 21 27 25 22 24 19
3 | 7 13 6 10 15 4 13 7 8 18 3 | 16 24 19 18 22 17 26 18 20 20 17
4 | 7 10 7 6 17 6 11 11 10 25 3 | 24 26 22 26 28 25 23 31 28 39 24
5 | 8 27 7 12 21 6 20 10 8 17 4 | 13 33 16 17 23 14 31 19 17 21 15
6 | 7 13 6 9 15 4 12 6 9 14 3 | 16 22 19 20 24 17 27 19 22 19 18
7 | 7 16 8 12 38 6 16 12 7 24 4 | 21 31 21 22 40 21 32 24 25 28 21
8 | 3 14 6 10 31 5 9 16 9 11 4 | 22 28 22 23 32 21 30 27 26 25 22
9 | 5 14 6 8 24 4 11 7 7 15 3 | 17 24 19 19 36 19 28 18 23 18 18
10 | 7 12 7 9 21 8 10 10 6 18 3 | 20 26 22 20 24 18 31 25 24 27 21
11 | 9 12 5 10 8 4 15 11 7 14 3 | 23 37 29 31 38 26 39 31 25 29 28
12E | 12 18 9 7 25 7 29 6 11 12 4 | 20 27 26 21 30 21 30 20 23 21 21
X13 | 6 21 6 12 --- 4 19 9 7 11 4 | 20 36 23 21 --- 20 30 21 26 24 21
14 | 6 19 7 9 38 4 22 8 12 10 4 | 14 27 20 18 39 17 30 19 23 19 17
X15 | 5 18 6 10 --- 7 17 7 9 12 3 | 16 30 19 22 --- 18 30 21 22 27 19
16E | 6 18 6 7 30 5 24 7 9 13 4 | 22 28 25 21 34 24 30 21 26 19 22
17 | 6 21 8 9 17 5 21 8 9 24 4 | 18 30 21 24 27 22 32 24 25 29 21
18 | 7 20 6 12 18 4 17 8 6 15 3 | 21 32 25 18 26 22 31 23 24 25 21
19 | 9 17 7 14 18 3 24 15 6 31 5 | 18 31 23 21 27 19 37 24 17 19 20
20 | 7 19 7 8 19 3 19 8 10 10 3 | 21 30 24 20 29 21 31 23 25 25 22
21 | 10 12 6 9 10 7 11 6 9 28 3 | 18 26 24 22 23 21 25 24 21 32 20
22 | 6 20 5 9 17 4 16 7 7 12 3 | 16 29 19 18 23 19 27 20 19 23 17
23 | 7 21 7 9 37 5 21 8 6 15 4 | 13 29 21 16 41 16 31 16 20 16 16
24 | 8 15 5 15 13 7 13 9 8 12 3 | 17 23 21 30 25 21 29 24 22 21 21
25E | 22 20 11 15 25 10 28 19 19 19 6 | 61 60 57 48 57 54 67 45 50 50 52
26 | 14 16 5 8 31 5 15 10 10 33 5 | 79 83 76 78 76 77 83 84 78 95 78
27 | 4 13 5 9 27 4 9 8 8 17 3 | 14 22 18 19 36 17 27 16 22 17 17
28E | 6 20 11 9 22 5 22 16 10 23 4 | 17 28 18 21 29 17 29 22 22 26 18
29 | 9 23 6 7 14 7 24 8 10 19 4 | 18 34 25 19 27 20 33 21 25 23 21
X30E | 15 30 11 19 27 18 --- 31 --- --- 9 | 22 43 27 21 28 20 --- 35 --- --- 21
31 | 6 20 9 6 36 5 26 10 15 12 4 | 11 27 17 11 43 14 28 14 20 13 13
32 | 9 20 6 9 18 4 17 10 8 15 4 | 22 36 24 23 23 21 34 23 24 30 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 7 10 24 6 18 10 9 20 |T 21 31 24 23 32 24 32 25 25 26 23
WRMS | 7 17 7 10 21 5 17 10 7 20 |NE 20 30 23 23 31 21 32 24 24 26 21
MEDI | 7 18 6 9 21 5 17 9 8 15 |MD 18 29 22 21 28 20 30 23 23 24 21
Table 3.1640.6 GPS week: 1640 Day: 6 MJD: 55730.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 4 --- --- --- --- 92 --- --- --- --- 0 | 41 --- --- --- --- 60 --- --- --- --- 43
2 | 8 12 8 11 15 5 15 14 10 48 5 | 27 28 29 30 28 26 26 29 28 30 25
3 | 13 12 6 10 16 6 12 11 8 21 4 | 15 18 17 15 23 14 20 12 17 19 14
4 | 16 12 7 9 17 5 9 12 11 35 5 | 27 32 33 28 34 31 25 40 29 51 30
5 | 11 22 10 8 19 6 18 10 10 17 4 | 14 24 17 13 21 15 23 21 19 26 14
6 | 10 12 6 7 14 5 12 10 7 17 3 | 18 21 23 21 28 18 21 19 22 22 19
7 | 10 18 7 9 31 8 18 14 6 27 5 | 17 28 19 18 38 16 26 18 16 25 17
8 | 10 14 5 8 21 7 11 22 8 12 4 | 17 22 14 15 30 15 23 18 15 15 14
9 | 16 12 5 8 21 5 12 9 7 20 4 | 19 20 18 14 27 13 21 11 15 13 14
10 | 13 16 6 11 17 8 10 11 8 18 4 | 16 23 17 13 17 13 19 21 19 23 14
11 | 9 12 6 9 15 5 14 9 8 16 3 | 40 47 48 47 55 42 47 45 40 45 44
12E | 13 17 7 10 23 6 30 13 8 15 5 | 24 29 28 27 26 23 30 28 21 25 24
13 | 9 25 6 12 33 4 20 8 8 12 5 | 17 34 24 18 44 18 28 17 17 20 18
14 | 7 18 5 11 29 3 18 6 7 11 4 | 16 26 22 18 31 16 25 15 20 17 17
X15 | 11 20 6 10 --- 4 21 10 10 13 4 | 21 28 20 17 --- 19 27 19 22 24 19
16E | 9 17 5 7 20 5 28 11 8 12 4 | 27 29 29 29 30 27 35 27 24 27 26
17 | 10 19 9 10 21 6 20 13 11 31 5 | 18 25 18 17 28 16 25 20 19 24 15
18 | 9 24 8 10 17 6 18 12 8 19 4 | 22 31 19 15 23 16 27 17 14 22 16
19 | 10 18 8 10 19 5 22 8 11 37 5 | 22 32 27 21 29 22 35 21 25 21 23
20 | 8 18 6 11 18 5 18 7 7 14 4 | 25 28 24 20 28 22 30 21 23 22 22
21 | 15 11 5 11 14 7 13 12 9 32 4 | 31 29 25 26 27 26 29 29 26 35 25
22 | 8 16 7 11 19 6 15 11 6 16 4 | 17 24 16 14 24 13 24 15 14 20 14
23 | 8 24 7 11 25 4 25 10 7 15 4 | 14 29 21 14 33 14 29 15 15 14 15
24 | 17 13 7 15 19 7 12 9 9 12 4 | 27 24 30 34 33 27 25 26 21 22 26
25E | 24 33 21 21 37 17 29 53 30 27 11 | 97 120 118 118 118 107 113 133 103 115 112
26 | 13 15 10 10 24 5 12 12 9 23 4 | 31 29 29 26 34 27 28 28 28 28 27
27 | 12 13 5 8 19 4 11 10 8 17 3 | 15 19 14 12 25 11 19 11 11 12 11
28E | 10 15 8 8 20 6 21 14 7 12 4 | 20 21 20 13 25 15 25 16 16 22 15
29 | 12 22 10 10 16 8 23 7 7 20 4 | 24 36 28 24 30 24 35 22 24 26 24
X30E | 17 20 9 15 17 7 --- 23 --- --- 7 | 32 45 38 28 38 33 --- 37 --- --- 33
31 | 10 17 10 10 28 4 20 14 13 13 5 | 15 29 21 20 35 16 26 13 14 14 15
32 | 11 22 7 8 19 5 21 10 9 15 4 | 23 31 24 18 25 19 30 20 21 28 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 18 8 10 22 6 18 15 10 22 |T 24 31 26 23 32 24 29 25 23 26 23
WRMS | 11 17 7 10 20 6 17 11 7 19 |NE 21 27 22 20 30 19 26 20 20 23 19
MEDI | 10 17 7 10 19 5 18 11 8 17 |MD 21 28 23 18 28 18 26 20 20 22 19
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 4.1640 GPS week: 1640 MJD: 55724.0-55730.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 |U 7 8 21 |U 6 7 19 |U 9 10 22 |
emr | emr 2971 |U 13 11 30 |U 9 8 21 | 9 10 23 |
esa | esa 2976 | 9 9 23 |U 5 6 16 | 8 10 24 |
gfz | gfz 2968 |U 8 8 22 |U 5 7 19 |U 10 12 27 |
grg | grg 2921 | 8 9 25 |U 6 7 20 | 10 11 27 |
igr | igr 2964 | 9 8 23 | 5 6 16 | 8 9 23 |
igs | igs 2945 | 10 9 24 | 5 5 16 | 8 10 23 |
jpl | jpl 2878 | 13 11 33 |U 5 7 21 | 9 13 24 |
mit | mit 2976 |U 11 9 26 |U 6 7 20 |U 9 9 24 |
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 5.1640.0 GPS week: 1640 Day: 0 MJD: 55724.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 7 8 16 | ---- ---- ---- | 8 9 25 |
emr | emr 2972 | 9 8 25 | ---- ---- ---- | 8 9 20 |
esa | esa 2976 | 7 7 15 | ---- ---- ---- | 9 10 29 |
gfz | gfz 2971 | 7 7 17 | ---- ---- ---- | 9 11 26 |
grg | grg 2880 | 7 6 16 | ---- ---- ---- | 12 11 27 |
igr | igr 2971 | 7 7 15 | ---- ---- ---- | 8 10 27 |
igs | igs 2880 | 9 7 16 | ---- ---- ---- | 10 11 27 |
jpl | jpl 2879 | 11 8 20 | ---- ---- ---- | 9 13 25 |
mit | mit 2976 | 9 6 16 | ---- ---- ---- | 9 11 31 |
Table 5.1640.1 GPS week: 1640 Day: 1 MJD: 55725.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 6 8 20 | ---- ---- ---- | 14 18 42 |
emr | emr 2972 | 9 10 25 | ---- ---- ---- | 13 15 36 |
esa | esa 2976 | 6 8 19 | ---- ---- ---- | 14 21 44 |
gfz | gfz 2971 | 6 9 21 | ---- ---- ---- | 12 18 42 |
grg | grg 2976 | 6 9 22 | ---- ---- ---- | 12 18 46 |
igr | igr 2974 | 6 8 19 | ---- ---- ---- | 12 18 45 |
igs | igs 2972 | 6 9 20 | ---- ---- ---- | 13 20 45 |
jpl | jpl 2880 | 12 13 33 | ---- ---- ---- | 14 34 43 |
mit | mit 2976 | 6 8 21 | ---- ---- ---- | 12 15 37 |
Table 5.1640.2 GPS week: 1640 Day: 2 MJD: 55726.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3049 | 7 5 20 | 6 6 21 | 6 9 19 |
emr | emr 2972 | 10 7 24 | 8 8 21 | 9 11 26 |
esa | esa 2976 | 7 6 18 | 5 7 17 | 7 11 20 |
gfz | gfz 2964 | 6 5 16 | 5 8 18 | 9 12 23 |
grg | grg 2976 | 7 6 20 | 5 7 19 | 7 10 22 |
igr | igr 2958 | 7 5 17 | 5 7 15 | 7 9 19 |
igs | igs 2961 | 6 6 18 | 5 6 16 | 7 10 19 |
jpl | jpl 2880 | 12 7 25 | 6 8 23 | 11 11 26 |
mit | mit 2976 | 7 6 19 | 6 8 24 | 8 8 17 |
Table 5.1640.3 GPS week: 1640 Day: 3 MJD: 55727.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 7 9 18 | 8 5 20 | 7 7 19 |
emr | emr 2971 | 10 13 23 | 10 7 24 | 9 12 20 |
esa | esa 2976 | 7 8 18 | 6 8 19 | 8 8 23 |
gfz | gfz 2966 | 7 7 17 | 6 7 19 | 8 9 27 |
grg | grg 2976 | 7 8 19 | 7 7 21 | 9 11 26 |
igr | igr 2959 | 8 8 18 | 5 6 18 | 9 10 26 |
igs | igs 2931 | 8 9 19 | 6 6 17 | 7 8 22 |
jpl | jpl 2880 | 10 9 22 | 6 7 20 | 8 11 19 |
mit | mit 2976 | 7 8 17 | 8 8 25 | 9 9 28 |
Table 5.1640.4 GPS week: 1640 Day: 4 MJD: 55728.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 8 10 25 | 4 11 19 | 9 9 21 |
emr | emr 2972 | 10 11 27 | 9 9 24 | 9 6 22 |
esa | esa 2976 | 9 10 27 | 4 6 14 | 8 7 21 |
gfz | gfz 2966 | 8 10 25 | 5 9 25 | 10 11 26 |
grg | grg 2976 | 9 9 29 | 4 6 14 | 9 7 24 |
igr | igr 2972 | 8 10 25 | 4 6 18 | 8 6 19 |
igs | igs 2953 | 8 9 26 | 4 6 15 | 8 7 21 |
jpl | jpl 2880 | 14 11 35 | 4 6 20 | 7 6 23 |
mit | mit 2976 | 9 9 25 | 5 6 16 | 9 7 23 |
Table 5.1640.5 GPS week: 1640 Day: 5 MJD: 55729.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 8 10 26 | 6 6 17 | 6 6 16 |
emr | emr 2972 | 13 12 41 | 9 8 20 | 8 7 21 |
esa | esa 2976 | 9 11 31 | 5 6 17 | 6 5 17 |
gfz | gfz 2972 | 9 10 30 | 6 7 17 | 8 9 21 |
grg | grg 2784 | 10 12 33 | 8 7 27 | 8 8 22 |
igr | igr 2944 | 8 10 29 | 5 7 15 | 6 4 14 |
igs | igs 2969 | 9 11 32 | 5 5 16 | 6 5 17 |
jpl | jpl 2872 | 11 10 39 | 5 8 21 | 7 5 20 |
mit | mit 2976 | 12 16 42 | 6 8 19 | 8 5 19 |
Table 5.1640.6 GPS week: 1640 Day: 6 MJD: 55730.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 10 9 26 | 8 7 18 | 9 13 15 |
emr | emr 2972 | 29 16 44 | 7 6 18 | 8 12 15 |
esa | esa 2976 | 17 12 33 | 5 4 13 | 7 10 14 |
gfz | gfz 2971 | 11 11 27 | 5 6 15 | 11 13 22 |
grg | grg 2880 | 13 13 36 | 7 7 21 | 10 15 23 |
igr | igr 2976 | 22 11 35 | 5 6 14 | 7 10 14 |
igs | igs 2954 | 24 12 39 | 5 4 15 | 8 11 14 |
jpl | jpl 2880 | 20 16 56 | 5 7 22 | 8 10 16 |
mit | mit 2976 | 24 13 39 | 5 5 16 | 8 11 14 |
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 6.1640 GPS week: 1640 MJD: 55724.500-55730.500
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 | 19 -11 82 -4 -4 | 3 13
| 25 18 70 59 7 | 2
emr uuuuu | 55 -1 111 260 -2 | 33 36
| 38 15 91 57 9 | 2
esa uuuuu | -23 -35 -23 45 -2 | 8 13
| 16 16 84 63 2 | 2
gfz uuuuu | -78 13 31 -33 2 | 8 12
| 13 24 134 43 6 | 2
grg uuuux | 85 -59 55 -123 -67 | -14 36
| 44 41 147 117 65 | 16
igr xxxxx | -29 3 48 -13 -2 | 0 11
| 21 18 53 47 6 | 3
irf xxxxx | -4 -4 -4 -39 -3 | 6 12
| 12 12 12 23 3 | 2
jpl uuuuu | 5 -13 115 15 2 | 16 22
| 60 65 87 79 8 | 3
mit uuuuu | -16 -2 -72 -132 -6 | 20 23
| 21 20 46 15 5 | 2
ngs uuuuu | 21 8 41 3 0 | 8 13
| 22 23 86 88 8 | 1
sio uuuuu | 87 149 -233 38 3 | 29 31
| 17 26 82 53 6 | 2
Table 7.1640.0 GPS week: 1640 Day: 0 MJD: 55724.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 18 -16 66 29 7 | 5 11
emr uuuuu | 119 -17 70 333 7 | 35 36
esa uuuuu | 1 -14 -11 -19 0 | 9 13
gfz uuuuu | -92 6 -56 -29 -4 | 9 12
grg uuuux | -2 -86 255 -238 27 | -2 19
igr xxxxx | -34 19 -11 39 1 | 3 10
irf xxxxx | 9 -8 1 -25 3 | 7 11
jpl uuuuu | -69 33 61 17 -2 | 19 23
mit uuuuu | -11 -8 -67 -106 5 | 21 22
ngs uuuuu | 38 16 -22 114 3 | 9 12
sio uuuuu | 111 128 -135 74 2 | 30 31
Table 7.1640.1 GPS week: 1640 Day: 1 MJD: 55725.500
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 | -16 -31 0 35 -10 | 6 12
emr uuuuu | 87 -13 258 242 -9 | 37 39
esa uuuuu | -36 -33 -195 37 2 | 9 13
gfz uuuuu | -78 43 -13 -26 -3 | 10 12
grg uuuux | 77 -72 71 -93 -16 | -1 21
igr xxxxx | -36 6 44 -32 6 | 3 11
irf xxxxx | -12 -4 -12 -34 -4 | 8 12
jpl uuuuu | -24 32 272 -10 -15 | 20 24
mit uuuuu | -34 -5 -53 -133 -6 | 23 24
ngs uuuuu | 35 -11 147 3 9 | 9 13
sio uuuuu | 76 138 -202 69 1 | 30 32
Table 7.1640.2 GPS week: 1640 Day: 2 MJD: 55726.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 37 -2 68 -56 -7 | 2 12
emr uuuuu | 10 -8 165 264 -17 | 34 36
esa uuuuu | -23 -31 37 23 -4 | 7 12
gfz uuuuu | -77 47 -155 -37 0 | 7 10
grg uuuux | 102 -54 -78 -79 -35 | -3 23
igr xxxxx | -30 0 22 -37 -5 | 1 9
irf xxxxx | -21 -17 20 -86 -4 | 5 11
jpl uuuuu | 70 -16 28 -98 0 | 15 21
mit uuuuu | -42 -35 4 -139 -10 | 20 23
ngs uuuuu | 25 10 108 105 8 | 8 12
sio uuuuu | 69 125 -169 -48 5 | 27 29
Table 7.1640.3 GPS week: 1640 Day: 3 MJD: 55727.500
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 -27 42 92 -5 | 0 14
emr uuuuu | 58 1 156 264 -5 | 31 34
esa uuuuu | -47 -61 -34 91 -4 | 5 12
gfz uuuuu | -90 15 -56 -42 8 | 5 10
grg uuuux | 87 -76 49 -129 -62 | -8 29
igr xxxxx | -27 -1 15 -55 -9 | -1 11
irf xxxxx | -7 -5 -3 -11 -3 | 4 12
jpl uuuuu | 28 5 59 -59 6 | 13 20
mit uuuuu | -15 13 -66 -142 -8 | 19 23
ngs uuuuu | 43 2 112 14 -9 | 8 12
sio uuuuu | 81 162 -171 71 9 | 27 28
Table 7.1640.4 GPS week: 1640 Day: 4 MJD: 55728.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 23 21 66 -6 0 | 0 14
emr uuuuu | 15 23 105 148 0 | 30 34
esa uuuuu | -18 -35 65 55 -5 | 6 12
gfz uuuuu | -73 3 151 42 10 | 6 11
grg uuuux | 145 -51 62 -51 -115 | -12 36
igr xxxxx | -19 26 25 59 -6 | -3 11
irf xxxxx | -5 17 -17 -36 -2 | 3 12
jpl uuuuu | -19 -154 197 85 7 | 13 20
mit uuuuu | -13 21 -147 -117 -9 | 18 22
ngs uuuuu | 22 30 -86 -86 -11 | 7 12
sio uuuuu | 78 183 -322 6 11 | 27 29
Table 7.1640.5 GPS week: 1640 Day: 5 MJD: 55729.500
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 | 17 -2 106 -65 1 | 2 14
emr uuuuu | 50 17 34 281 8 | 32 36
esa uuuuu | -11 -22 -30 154 -2 | 8 13
gfz uuuuu | -53 -16 153 -28 7 | 9 14
grg uuuux | 91 -96 197 -309 -162 | -25 51
igr xxxxx | -61 5 108 -5 4 | -3 11
irf xxxxx | -2 7 -8 -39 -3 | 5 13
jpl uuuuu | 94 24 100 37 5 | 16 22
mit uuuuu | -19 16 -76 -151 -7 | 18 23
ngs uuuuu | -22 -27 -16 -121 -5 | 8 13
sio uuuuu | 82 183 -309 -3 3 | 30 33
Table 7.1640.6 GPS week: 1640 Day: 6 MJD: 55730.500
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 | 57 -21 223 -56 -15 | 4 15
emr uuuuu | 45 -9 -14 287 4 | 34 38
esa uuuuu | -26 -50 5 -25 -1 | 9 14
gfz uuuuu | -80 -4 196 -107 -5 | 11 17
grg uuuux | 92 27 -171 39 -107 | -44 74
igr xxxxx | 7 -31 133 -62 -5 | -1 12
irf xxxxx | 13 -14 -12 -43 -7 | 6 14
jpl uuuuu | -44 -10 87 132 11 | 18 24
mit uuuuu | 24 -15 -100 -138 -6 | 19 23
ngs uuuuu | 9 38 43 -9 3 | 9 14
sio uuuuu | 110 126 -321 96 -8 | 33 36
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