[IGSREPORT-20322] Wk 1660 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Nov 17 13:20:05 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1660 (Oct 30, 2011 - Nov 05, 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:
igs1660[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1660[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1660[0-6].cls IGS GPS clock combination summary report.
igs16607.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16607.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because of poorer consistency (GRG),
they provide broadcast clocks (NGS), or clock corrections are not provided
(SIO). The clock information not used is still compared to combination for
completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | EMR | 21 21 KHAJ KHAJ
0 | ESA | KOUR
0 | GFZ | 30 HARB MDVJ
0 | GRG | KOUR NTUS USN3
0 | JPL | 21 22 27 TIXI
0 | MIT | 27 27 GUAT GUAT
1 | COD | MOBS
1 | ESA | YAKT TIXI ZECK
1 | GFZ | COCO
1 | MIT | 27 27 DAV1 DAV1
2 | COD | NKLG STHL ZECK
2 | EMR | 4 4 CHUR CHUR
2 | GFZ | 4 30 MAC1 MDVJ NTUS
2 | GRG | SANT
2 | JPL | CAS1
2 | MIT | 27 27 CAS1 MAC1 NTUS CAS1 MAC1 NTUS
3 | COD | WROC SOFI STHL WROC
3 | ESA | WHIT WHIT ZECK
3 | GFZ | 2 BAN2 BJCO CHUR MDVJ WHIT
3 | JPL | 10 22 HARB QIKI
3 | MIT | 27 27
4 | COD | WROC DUBO GUAT SOFI TLSE WROC
4 | EMR | MCM4
4 | ESA | REUN KOUR REUN URUM
4 | GFZ | HOLM MDVJ OPMT TLSE WHIT
4 | GRG | KOUR
4 | JPL | STHL
4 | MIT | 27 27 KHAJ NICO GUAT KHAJ NICO
5 | COD | KOSG GOPE KOSG
5 | EMR | WTZR
5 | ESA | HARB REUN SCH2 HARB REUN
5 | GFZ | MDVJ SCH2 YELL
5 | GRG | KOUR SANT WTZR
5 | JPL | HARB
5 | MIT | 25 27 25 27 KOSG NICO
6 | COD | CAS1
6 | GFZ | MDVJ SUTM
6 | JPL | 10
6 | MIT | 27 27 CAS1
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | SIO | ALL (high Transformation - See Table 2)
1 | SIO | ALL (high Transformation - See Table 2)
2 | SIO | ALL (high Transformation - See Table 2)
3 | SIO | ALL (high Transformation - See Table 2)
4 | SIO | ALL (high Transformation - See Table 2)
5 | SIO | ALL (high Transformation - See Table 2)
6 | SIO | ALL (high Transformation - See Table 2)
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
7. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | -.1 .4 -.5 -43 3 16 .08
EMR | 3.2 7.0 6.5 -3 15 -11 .40
ESA | 6.0 3.2 -11.1 79 -200 95 .17
GFZ | -.6 1.1 -.4 -27 3 -2 .20
GRG | 5.3 .8 6.7 -16 28 8 .19
JPL | .5 7.2 15.8 56 -39 18 .61
MIT | 5.9 2.7 10.6 -31 16 -40 .16
NGS | 6.6 -.7 5.1 -23 -34 32 .50
SIO | 7.2 7.7 -14.8 129 -223 6 .20
8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1660.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1660.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 2.1660.[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 3.1660.[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 5.1660.0-6).
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 1660 summary. (Oct 30, 2011 - Nov 05, 2011)
Table 1.1660.a GPS week: 1660 MJD: 55864.000-55870.000
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 257| 0 0 0 77 -62 5 -.27 9 9 | -597 241 19 90
| 0 0 1 12 10 10 .02 | 482 635
emr 98| 0 1 4 4 -83 35 .39 20 20 | 124138 -3841 16 132
| 1 1 2 32 10 18 .05 | 585748 11262
esa 138| 0 0 1 -88 193 -27 .21 7 7 | -1133 1451 17 235
| 1 0 0 23 23 18 .02 | 758 828
gfz 202| -1 0 -3 51 -83 8 -.19 11 11 | 99 -180 24 103
| 0 0 1 74 59 6 .02 | 196 336
grg 131| 1 1 -1 27 -108 14 .50 18 17 | -218 229 51 240
| 0 1 3 15 10 27 .11 | 320 432
igr n/a| 0 0 0 -18 -62 -64 -.10 5 5 | -11946 830 18 76
| 0 0 0 21 16 18 .02 | 1658 1174
jpl 152| -1 0 1 -117 48 27 .54 15 14 | 689 169 20 106
| 1 1 1 7 5 35 .03 | 855 801
mit 260| 1 -2 -1 46 -134 -15 -.41 13 11 | -442 214 19 193
| 0 1 0 25 28 14 .02 | 265 377
ngs 226| 0 0 0 34 11 0 -.27 11 9 | -589 203 1861 3490
| 1 1 0 47 21 15 .03 | 418 551
sio 254| -1 2 -9 -223 390 -31 -.28 22 20 | --- --- --- ---
| 2 0 0 27 22 28 .04 | --- ---
Table 1.1660.b GPS week : 1660 MJD: 55864.000-55870.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 5 5 4 5 5 5 4 |
2 | 4 4 4 5 5 5 5 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 4 4 4 5 4 |
5 | 6 5 5 5 5 5 4 |
6 | 3 4 4 4 4 4 4 |
7 | 5 5 5 5 5 5 5 |
8 | 5 5 5 5 5 5 5 |
9 | 4 5 5 5 5 4 4 |
10 | 5 6 5 5 6 7 6 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 4 4 4 5 5 |
14 | 5 5 4 5 5 4 4 |
15 | 4 5 4 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 4 5 5 5 4 4 |
18 | 5 5 5 5 5 5 4 |
19 | 3 3 3 4 4 4 4 |
20 | 5 5 5 5 4 5 4 |
21 | 4 4 4 5 4 5 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
25 | 4 5 4 5 5 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 10 11 9 11 11 8 9 |
28 | 5 5 5 5 5 5 4 |
29 | 4 5 4 4 5 5 4 |
30 | 4 5 5 5 5 5 5 |
31 | 6 5 5 5 5 5 5 |
32 | 5 5 5 5 5 6 8 |
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 2.1660.0 GPS week: 1660 Day: 0 MJD: 55864.000
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 257| 0 0 0 67 -50 14 -.28 10 9 | -434 548 21 95
| 20 -17 |
emr 98| 0 3 2 25 -95 33 .37 20 20 | -999999 -29327 17 136
| -38 -28 |
esa 138| -1 0 2 -109 173 -37 .18 7 7 | -744 629 16 202
| 55 29 |
gfz 202| 0 0 -2 104 -107 0 -.23 11 11 | 42 -32 24 99
| 6 7 |
grg 131| 1 1 -4 32 -100 -4 .62 16 15 | -131 -326 39 229
| -7 -66 |
igr n/a| 0 0 1 -29 -37 -76 -.11 5 5 | -12064 -1047 19 75
| -15 19 |
jpl 152| 0 0 0 -110 48 30 .51 15 14 | 1885 -1070 20 108
| 78 -73 |
mit 260| 1 0 -1 11 -102 -11 -.43 12 11 | -296 -3 22 209
| 12 42 |
ngs 226| 2 -1 1 26 34 2 -.23 9 8 | -474 519 1615 3457
| 14 -9 |
sio 254| 0 1 -10 -265 411 -74 -.26 22 21 | --- --- --- ---
| 96 -222 |
Table 2.1660.1 GPS week: 1660 Day: 1 MJD: 55865.000
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 257| 0 0 0 67 -78 0 -.29 8 7 | -1348 1196 18 92
| 13 -8 |
emr 98| -1 1 3 -1 -68 25 .33 20 20 | 624686 -648 16 139
| -12 -58 |
esa 138| 0 -1 1 -114 179 -6 .20 7 7 | -2055 1357 15 230
| 64 29 |
gfz 202| -1 1 -5 74 -76 0 -.20 14 13 | -35 148 24 102
| 33 48 |
grg 131| 1 2 -6 28 -102 33 .59 16 14 | -455 423 56 246
| 21 -60 |
igr n/a| 0 1 0 -26 -74 -41 -.13 5 5 | -12755 -241 18 66
| 9 28 |
jpl 152| 0 1 3 -127 46 -27 .50 14 13 | 1068 -430 20 105
| 97 -58 |
mit 260| 1 0 0 61 -101 -10 -.42 12 11 | -721 675 21 241
| -18 17 |
ngs 226| 1 2 0 28 25 2 -.25 11 9 | -1098 825 1904 4078
| 35 -23 |
sio 254| 0 1 -8 -214 410 -54 -.27 20 17 | --- --- --- ---
| 77 -231 |
Table 2.1660.2 GPS week: 1660 Day: 2 MJD: 55866.000
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 257| 0 0 0 65 -63 16 -.26 9 8 | -629 188 20 86
| 9 -21 |
emr 98| 0 1 6 -42 -80 14 .41 19 19 | 623493 -101 17 120
| 23 -71 |
esa 138| 0 0 0 -105 171 -62 .21 8 8 | -713 1331 22 255
| 65 13 |
gfz 202| -1 0 -3 143 8 17 -.19 11 11 | 174 -199 25 106
| -8 54 |
grg 131| 1 1 -4 -2 -97 -1 .63 15 15 | -116 -167 39 227
| 65 -66 |
igr n/a| 0 -1 0 -38 -69 -76 -.10 5 5 | -13425 584 19 86
| 18 41 |
jpl 152| -3 2 2 -117 56 70 .57 15 14 | 123 -56 24 103
| 68 -79 |
mit 260| 1 -1 -1 45 -113 7 -.41 11 10 | -187 -304 18 182
| -13 28 |
ngs 226| 1 -2 0 -1 4 -7 -.28 10 8 | -697 288 1813 3637
| 30 -3 |
sio 254| -3 2 -8 -226 416 -30 -.27 21 20 | --- --- --- ---
| 75 -228 |
Table 2.1660.3 GPS week: 1660 Day: 3 MJD: 55867.000
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 257| -1 0 1 93 -74 3 -.24 10 10 | 121 -858 24 100
| 3 -46 |
emr 98| 2 3 4 -26 -96 15 .47 20 20 | 622498 524 17 147
| 31 -69 |
esa 138| 0 0 1 -94 176 -14 .22 7 7 | -936 988 15 229
| 37 25 |
gfz 202| 0 0 -2 88 -23 14 -.19 11 11 | 487 -815 26 118
| 25 -6 |
grg 131| 0 0 -1 18 -109 -19 .47 22 20 | 111 236 63 256
| 64 -69 |
igr n/a| 0 0 0 -32 -78 -46 -.07 5 5 | -13030 1362 19 80
| 2 16 |
jpl 152| 0 3 0 -115 41 22 .56 16 15 | 108 594 22 106
| 87 -37 |
mit 260| 0 -2 -1 91 -163 -18 -.38 12 12 | -41 -11 19 198
| -23 28 |
ngs 226| 0 0 0 -30 -5 21 -.28 9 8 | 94 -854 2239 3282
| 68 54 |
sio 254| -3 2 -8 -179 376 -49 -.23 22 20 | --- --- --- ---
| 74 -229 |
Table 2.1660.4 GPS week: 1660 Day: 4 MJD: 55868.000
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 257| -1 0 -2 71 -61 9 -.27 10 9 | -583 538 18 81
| 32 -37 |
emr 98| 0 1 6 -3 -84 60 .42 19 19 | -1417 1195 21 127
| 2 -54 |
esa 138| 2 0 0 -72 222 -25 .24 7 7 | -844 2119 20 244
| 46 5 |
gfz 202| 0 1 -1 44 -111 6 -.17 10 10 | -127 103 25 102
| -36 -10 |
grg 131| 1 0 2 38 -103 57 .34 22 20 | -742 843 57 257
| 13 -75 |
igr n/a| 0 0 0 -24 -41 -48 -.11 6 6 | -12677 2013 20 73
| -23 5 |
jpl 152| -3 1 2 -108 48 7 .54 15 15 | -343 964 20 104
| 56 -33 |
mit 260| 0 -3 -1 48 -169 -41 -.42 13 12 | -680 434 18 156
| 6 46 |
ngs 226| 1 0 0 24 -13 0 -.30 12 9 | -594 523 1819 3406
| 41 13 |
sio 254| -3 3 -9 -234 366 -13 -.26 22 20 | --- --- --- ---
| 113 -189 |
Table 2.1660.5 GPS week: 1660 Day: 5 MJD: 55869.000
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 257| -1 0 0 82 -52 10 -.27 10 9 | -1030 175 21 94
| 37 -44 |
emr 98| 0 0 8 33 -87 49 .39 20 20 | -979 1468 12 127
| -34 -38 |
esa 138| 1 0 0 -77 226 -31 .22 7 7 | -2342 2966 17 257
| 50 -23 |
gfz 202| -1 1 -5 -26 -168 13 -.18 10 10 | 43 -57 23 102
| -15 3 |
grg 131| 1 1 1 43 -122 35 .41 19 16 | -353 638 51 218
| 25 -60 |
igr n/a| 0 1 0 4 -69 -89 -.08 5 5 | -11065 2192 18 79
| -19 37 |
jpl 152| -1 -1 1 -113 55 13 .55 15 14 | 315 1201 16 107
| 132 -65 |
mit 260| 1 -2 -1 44 -155 -16 -.41 13 11 | -610 48 18 184
| 18 37 |
ngs 226| 0 0 -1 84 39 3 -.28 11 9 | -1056 248 1802 3421
| -37 -70 |
sio 254| -1 3 -9 -204 362 0 -.28 22 20 | --- --- --- ---
| 112 -195 |
Table 2.1660.6 GPS week: 1660 Day: 6 MJD: 55870.000
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 257| 0 0 1 96 -55 -13 -.29 8 8 | -281 -100 17 87
| 19 -26 |
emr 98| 1 2 2 46 -72 48 .36 19 19 | 685 -3 18 134
| -24 -68 |
esa 138| 0 1 0 -50 203 -17 .23 7 7 | -303 768 18 230
| 29 -2 |
gfz 202| -1 0 -3 -66 -107 8 -.17 9 9 | 114 -409 23 94
| -31 -9 |
grg 131| 1 2 -1 30 -123 2 .43 19 17 | 159 -42 57 247
| 24 -63 |
igr n/a| 0 0 0 17 -70 -69 -.10 5 5 | -8606 950 17 74
| -14 29 |
jpl 152| -1 0 0 -125 41 71 .55 14 13 | 1667 -15 21 109
| 139 -112 |
mit 260| 2 -1 -1 23 -138 -15 -.43 16 12 | -563 660 21 186
| 18 42 |
ngs 226| 0 0 0 106 -1 -28 -.29 13 10 | -302 -127 1835 3154
| -136 -44 |
sio 254| 1 2 -8 -240 392 0 -.35 24 19 | --- --- --- ---
| 144 -205 |
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 3.1660.0 GPS week: 1660 Day: 0 MJD: 55864.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 11 14 8 9 --- 7 16 14 10 22 4 | 29 42 32 31 --- 34 43 27 28 32 30
2 | 8 23 6 10 16 5 16 10 7 22 4 | 17 32 20 17 24 17 28 21 18 26 19
3 | 10 10 6 10 15 4 9 8 11 32 3 | 16 20 20 23 29 17 24 19 20 25 19
4 | 6 19 6 10 13 5 12 11 9 19 3 | 19 29 19 24 23 20 23 25 23 24 19
5 | 17 23 8 15 10 7 24 13 8 26 5 | 79 87 81 82 81 79 84 78 82 84 82
6 | 6 10 6 11 12 2 8 10 9 28 3 | 19 23 24 28 31 22 24 26 22 27 23
7 | 6 22 7 11 17 3 20 9 7 12 4 | 12 27 14 15 24 12 26 12 16 12 13
8E | 15 19 7 11 19 6 15 17 13 21 5 | 32 42 37 36 43 36 41 42 37 34 36
9 | 10 18 7 14 12 7 14 12 6 20 4 | 12 24 12 21 22 14 21 15 15 20 12
10 | 13 18 5 10 19 5 17 13 7 17 4 | 64 64 61 65 63 64 61 63 60 62 60
11 | 7 16 6 9 19 5 12 8 8 17 3 | 17 33 26 24 42 20 32 23 21 27 23
12 | 7 26 6 10 18 5 17 12 10 17 4 | 15 31 18 19 28 17 27 21 16 19 17
13 | 9 23 8 12 24 5 14 6 5 14 4 | 16 32 23 23 39 20 29 18 20 15 20
14 | 8 24 7 11 19 4 14 16 7 18 4 | 18 28 25 27 32 24 28 25 22 17 23
15 | 9 21 6 8 16 5 14 11 11 18 4 | 17 28 22 18 29 19 24 18 23 15 20
16 | 8 25 9 12 16 4 17 10 6 17 4 | 15 28 17 16 24 13 22 14 13 15 14
17 | 9 14 7 18 14 6 15 14 13 35 4 | 28 30 30 38 35 29 32 32 32 37 30
18E | 12 25 11 11 15 4 14 11 11 21 5 | 36 44 41 39 37 38 43 34 38 32 38
19 | 6 14 4 7 12 4 9 13 8 30 3 | 27 29 28 28 30 28 30 33 28 29 28
20E | 7 21 6 12 16 5 17 15 5 15 4 | 13 26 18 17 19 16 21 15 17 20 14
21 | 8 18 10 8 13 4 13 9 10 20 4 | 23 33 27 22 35 21 30 19 22 14 24
22E | 15 18 8 8 14 4 10 11 9 26 4 | 37 46 44 41 38 41 45 41 44 37 42
23 | 9 26 8 12 17 4 17 7 8 21 4 | 12 31 17 17 26 14 26 17 14 13 14
25 | 9 17 7 9 16 4 16 9 9 15 4 | 21 26 23 23 30 24 33 23 24 25 22
26 | 13 13 7 7 11 4 13 13 7 12 4 | 18 19 16 14 17 14 16 20 16 15 15
X27 | 21 24 24 21 --- 13 23 22 --- --- 10 | 17 29 19 35 --- 21 21 18 --- --- 17
28 | 10 17 6 12 18 5 14 15 9 17 4 | 17 26 15 25 33 17 23 26 19 21 18
29 | 7 12 8 12 13 5 16 13 8 31 4 | 23 30 28 29 29 26 32 29 29 25 27
X30 | 8 14 6 10 13 5 --- 15 8 27 4 | 15 21 17 18 21 18 --- 20 19 30 16
31 | 10 19 8 9 22 5 19 21 13 11 5 | 15 26 17 15 29 14 28 19 18 14 16
32 | 10 22 6 10 15 6 18 17 9 26 4 | 32 38 33 32 36 32 40 39 36 42 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 7 11 16 5 15 12 9 22 |T 23 33 26 27 32 25 31 26 26 26 25
WRMS | 9 20 7 11 15 5 14 11 8 21 |NE 18 28 21 22 28 19 27 21 20 21 19
MEDI | 9 19 7 10 16 5 15 12 8 20 |MD 18 29 23 24 30 20 28 23 22 25 20
Table 3.1660.1 GPS week: 1660 Day: 1 MJD: 55865.000
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 15 6 12 --- 5 14 17 11 18 4 | 23 35 29 23 --- 24 38 23 24 28 24
2 | 7 24 8 16 16 4 14 9 6 20 4 | 18 31 21 13 22 17 25 22 18 25 18
3 | 5 12 6 12 15 4 10 10 12 27 3 | 16 18 14 16 22 14 18 13 16 17 13
4 | 5 17 5 13 13 4 9 9 8 22 3 | 23 26 22 21 21 21 24 23 24 25 21
5E | 11 19 7 10 16 4 21 11 8 19 4 | 24 39 30 35 36 31 40 34 33 36 30
6 | 5 11 6 16 11 4 9 11 11 22 3 | 17 20 17 22 21 16 21 19 16 19 16
7 | 7 17 7 15 19 4 16 10 9 13 4 | 21 28 19 17 26 17 28 17 21 17 18
8 | 14 24 7 12 20 7 17 14 10 20 5 | 42 54 46 48 50 43 51 52 46 49 44
9 | 7 20 8 15 10 7 15 15 17 17 4 | 17 29 14 20 23 18 26 19 22 22 16
10E | 12 20 8 16 20 6 17 15 12 18 5 | 65 68 63 64 60 62 62 70 68 63 63
11 | 7 19 6 10 16 5 13 9 10 16 4 | 18 31 21 19 35 18 29 19 15 24 18
12 | 7 25 7 13 15 7 19 13 13 19 5 | 15 28 16 14 26 13 25 19 15 18 14
13 | 6 23 8 15 22 3 14 6 7 14 4 | 17 32 18 18 37 17 30 19 15 16 17
14 | 7 20 9 16 14 4 13 12 12 17 4 | 12 28 20 20 28 16 26 18 18 13 17
15 | 7 25 7 11 14 3 15 10 14 17 4 | 18 33 24 21 31 21 25 22 28 18 21
16 | 4 26 11 16 15 5 17 13 10 16 5 | 10 28 18 14 23 10 22 15 12 14 12
17 | 6 15 5 19 12 4 13 12 10 35 4 | 17 24 22 27 23 20 24 21 22 27 20
18E | 7 28 10 15 17 7 13 13 11 15 5 | 25 39 33 33 41 29 38 31 34 33 31
19 | 6 14 5 10 9 4 11 9 10 31 3 | 17 19 17 18 19 15 19 17 19 16 15
20E | 8 23 7 15 17 3 14 14 9 12 4 | 18 29 24 18 23 16 24 17 19 19 17
21 | 5 20 8 10 15 3 13 13 13 18 4 | 21 31 21 20 36 20 32 16 22 15 21
22E | 7 20 8 14 14 6 9 9 11 14 4 | 17 26 22 23 28 20 25 21 22 22 20
23 | 7 28 8 17 18 4 17 8 8 21 5 | 16 35 18 16 25 15 28 19 12 16 15
25 | 9 18 7 15 15 6 14 7 14 14 4 | 23 27 19 15 30 15 31 17 15 21 17
26 | 6 15 8 15 13 3 9 12 13 13 4 | 15 22 20 17 20 16 20 22 16 20 15
X27 | 20 37 17 21 --- 13 --- 20 --- --- 10 | 19 36 22 23 --- 22 --- 22 --- --- 16
28 | 8 21 7 14 19 5 14 14 8 17 4 | 16 29 20 21 29 15 25 23 21 21 17
29 | 9 15 6 16 11 4 17 11 13 30 4 | 18 26 20 21 19 19 23 20 21 15 18
X30 | 8 18 7 18 11 5 --- 17 11 25 5 | 16 28 16 20 18 14 --- 17 15 26 14
31 | 9 18 8 14 18 5 17 21 8 8 5 | 16 25 15 17 29 13 25 20 16 14 14
32 | 9 22 8 14 15 4 18 16 10 29 5 | 26 33 29 32 35 28 36 35 30 42 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 7 14 16 5 14 12 11 20 |T 20 30 22 22 28 20 28 23 22 23 20
WRMS | 7 20 7 13 14 5 13 11 9 17 |NE 17 27 19 18 25 16 25 19 18 19 16
MEDI | 7 20 7 15 15 4 14 12 10 18 |MD 18 29 20 20 26 17 25 20 19 20 17
Table 3.1660.2 GPS week: 1660 Day: 2 MJD: 55866.000
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 15 8 10 --- 5 16 11 9 18 4 | 26 39 29 24 --- 28 40 26 26 28 26
2 | 7 22 7 12 15 6 16 7 12 20 4 | 18 29 18 16 23 17 27 21 24 25 17
3 | 9 11 6 17 16 5 9 11 12 29 4 | 20 22 15 17 24 16 24 17 20 19 15
4 | 7 16 6 8 14 5 13 9 9 24 3 | 18 23 19 16 26 19 20 21 17 23 16
5E | 11 22 8 12 14 6 21 10 7 12 4 | 34 43 36 31 35 30 42 31 33 37 31
6 | 6 10 8 16 13 4 8 12 10 20 4 | 17 22 16 19 25 15 22 22 17 21 16
7 | 7 21 11 8 19 3 17 12 11 13 4 | 20 33 25 16 29 20 28 20 24 18 20
8 | 12 22 11 12 19 6 18 11 11 25 5 | 37 41 34 34 45 36 40 38 39 33 35
9 | 9 17 9 15 16 5 13 11 15 18 4 | 20 28 19 20 28 18 28 20 20 22 16
10E | 11 18 8 10 13 7 15 14 13 17 4 | 49 53 51 55 49 52 47 55 58 48 50
11 | 7 17 9 8 17 4 16 7 11 14 4 | 21 34 28 20 40 22 33 24 25 27 23
12 | 9 28 9 13 13 6 18 13 13 20 5 | 17 35 18 18 29 17 27 23 22 20 17
13 | 7 20 6 10 22 5 12 7 10 16 4 | 18 34 20 18 39 19 31 21 19 17 19
14 | 8 22 8 14 12 5 12 10 9 18 4 | 18 30 20 22 32 20 29 20 19 16 18
15 | 7 24 8 10 16 4 14 9 7 16 4 | 25 36 25 24 37 23 33 32 24 27 25
16 | 7 22 7 11 16 8 16 14 13 17 4 | 17 32 17 13 26 17 25 15 20 16 14
17 | 12 16 7 16 13 5 17 10 8 34 4 | 24 29 27 30 28 24 30 24 26 31 23
18E | 8 26 9 12 17 4 16 13 9 19 5 | 29 42 34 30 43 30 42 35 33 32 32
19 | 7 12 6 7 10 4 11 8 10 27 3 | 21 26 21 22 26 18 26 25 23 20 20
20E | 8 22 8 10 17 4 12 11 10 15 4 | 17 31 18 17 26 19 23 21 21 22 17
21 | 7 20 6 9 14 4 12 13 10 21 4 | 23 39 21 19 34 20 32 16 21 16 21
22E | 7 18 7 10 17 5 9 11 9 17 4 | 20 28 21 17 34 18 26 22 23 25 20
23 | 9 25 9 9 17 4 15 8 10 20 4 | 17 35 18 12 30 15 28 21 14 16 15
25 | 11 16 8 13 15 7 14 8 10 15 4 | 18 31 22 20 33 20 33 21 23 24 20
26 | 5 14 6 11 14 5 11 11 7 15 3 | 20 27 17 19 24 18 30 28 20 28 19
X27 | 22 18 10 22 --- 12 --- 9 --- --- 8 | 23 28 30 23 --- 20 --- 23 --- --- 20
28 | 10 21 6 12 16 5 15 13 7 18 4 | 19 32 20 22 31 16 26 24 22 21 18
29 | 7 13 9 11 12 4 14 12 15 29 4 | 21 29 23 24 24 20 27 25 23 24 21
X30 | 8 17 7 14 14 3 --- 13 10 24 4 | 18 29 18 20 21 14 --- 12 15 24 15
31 | 11 15 10 11 18 5 18 17 8 8 5 | 16 25 15 14 30 13 27 19 16 16 13
32 | 9 18 9 9 18 5 18 13 11 37 4 | 35 42 34 36 41 36 44 42 39 54 36
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 8 11 15 5 15 11 10 21 |T 22 32 23 22 31 21 30 24 24 25 21
WRMS | 8 19 8 11 15 5 14 10 8 20 |NE 19 30 20 19 29 18 28 21 20 21 18
MEDI | 8 18 8 11 16 5 15 11 10 18 |MD 20 31 21 20 30 19 28 22 22 23 20
Table 3.1660.3 GPS week: 1660 Day: 3 MJD: 55867.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 9 17 5 9 --- 4 18 13 12 21 4 | 29 40 29 29 --- 28 38 25 30 31 28
2 | 11 20 7 24 18 6 16 14 6 26 5 | 25 34 24 28 29 23 27 25 23 26 22
3 | 6 11 4 9 20 3 13 9 8 25 3 | 15 21 18 17 27 14 24 18 15 19 15
4 | 12 14 5 8 16 5 12 11 8 27 3 | 20 25 24 22 31 24 27 22 22 28 22
5E | 6 21 8 9 20 6 21 12 9 13 4 | 19 32 20 22 25 19 28 22 23 23 19
6 | 6 9 4 12 17 3 12 9 9 15 3 | 21 26 22 25 30 22 26 26 23 24 22
7 | 9 19 6 8 24 4 19 8 10 11 4 | 20 31 21 19 30 22 30 21 24 17 20
8 | 14 19 5 9 21 6 19 13 11 23 4 | 21 29 21 21 28 24 28 30 21 23 20
9 | 12 21 8 9 21 7 18 13 11 19 5 | 20 25 17 14 27 16 22 18 17 19 14
10E | 14 22 7 11 20 7 19 13 12 17 5 | 52 55 51 52 47 54 52 56 55 49 51
11 | 7 19 5 7 24 3 17 8 10 24 4 | 16 31 18 15 36 16 30 18 14 26 16
12 | 9 27 10 9 17 4 17 19 10 19 5 | 17 33 20 17 27 18 22 20 17 17 16
13 | 9 20 5 6 26 5 14 9 8 15 4 | 21 35 23 18 40 23 29 23 22 17 21
14 | 8 21 5 10 22 5 16 11 11 18 4 | 18 30 23 22 32 21 26 20 18 16 20
15 | 10 26 8 8 23 4 16 13 7 16 4 | 16 27 19 15 33 17 22 22 19 18 16
16 | 6 25 8 11 21 5 17 17 9 18 5 | 15 31 15 15 24 13 20 15 13 15 12
17 | 15 14 7 18 15 4 18 12 10 34 5 | 20 27 26 35 28 26 29 28 25 36 25
18E | 7 31 10 10 19 5 15 15 9 18 5 | 27 40 35 33 34 32 36 28 31 33 30
19 | 9 12 5 9 18 4 13 8 10 26 3 | 25 28 22 23 29 24 26 28 24 24 22
20E | 7 18 5 9 36 4 16 14 6 19 4 | 13 26 17 13 27 13 19 19 17 17 13
21 | 7 25 7 7 20 5 11 15 10 22 4 | 23 38 21 21 36 22 30 19 25 19 22
22E | 6 21 8 9 20 4 13 9 6 15 4 | 13 24 16 15 20 16 21 17 17 23 15
23 | 10 23 6 8 25 5 15 10 9 20 4 | 16 35 18 17 30 17 25 20 19 14 15
25 | 9 22 8 12 18 5 14 12 8 15 4 | 20 30 23 21 31 21 27 18 18 23 18
26 | 7 16 5 10 17 6 13 14 9 16 4 | 20 24 21 16 25 19 22 26 20 22 18
X27 | 28 23 27 25 --- 34 26 17 --- --- 11 | 15 23 39 29 --- 33 22 23 --- --- 20
28 | 12 20 8 12 21 4 15 13 8 19 4 | 17 29 19 21 33 18 25 23 20 19 18
29 | 10 14 8 10 16 5 16 13 12 31 4 | 23 30 28 23 27 25 29 27 28 26 25
X30 | 9 16 7 13 20 4 --- 15 11 25 4 | 18 32 24 23 23 20 --- 21 20 27 19
31 | 10 18 7 11 31 5 21 13 10 14 5 | 18 30 18 19 33 18 29 21 16 24 16
32 | 11 21 6 7 29 4 14 13 9 42 4 | 24 35 27 27 41 25 33 31 30 38 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 7 11 22 5 16 12 9 22 |T 20 30 23 22 30 22 27 23 22 23 20
WRMS | 10 20 7 11 20 5 15 12 8 20 |NE 19 29 22 21 30 20 26 21 20 22 19
MEDI | 9 20 7 9 20 5 16 13 9 19 |MD 20 30 21 21 30 21 27 22 20 23 20
Table 3.1660.4 GPS week: 1660 Day: 4 MJD: 55868.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 9 14 7 10 --- 6 17 16 13 23 4 | 28 38 31 31 --- 29 41 23 31 28 29
2 | 9 19 7 9 17 6 14 14 11 29 4 | 19 31 23 20 29 20 28 27 25 29 20
3 | 10 9 5 10 18 3 10 11 10 21 3 | 16 16 18 20 20 13 18 17 16 19 13
4 | 11 13 6 9 17 6 10 19 8 24 4 | 16 21 19 15 22 17 20 32 21 31 16
5E | 6 20 7 13 22 5 22 14 9 14 5 | 19 29 21 22 26 19 32 25 19 23 20
6 | 8 9 4 10 15 4 9 15 12 16 3 | 26 25 24 28 28 21 28 28 25 29 22
7 | 7 21 7 7 32 6 18 9 9 12 4 | 17 30 21 20 35 21 27 21 20 23 19
8 | 16 22 6 9 24 8 14 11 11 20 5 | 27 37 30 31 36 29 34 36 31 35 29
9 | 9 18 8 7 25 6 18 14 9 20 4 | 19 28 20 23 32 18 29 24 20 23 18
10E | 15 17 9 13 17 6 16 16 15 19 5 | 43 42 38 41 40 40 40 47 43 42 39
11 | 8 16 6 8 23 6 14 10 14 22 4 | 12 26 17 13 29 11 26 14 12 15 13
12 | 10 21 8 7 19 5 22 19 10 17 5 | 14 24 19 16 23 12 24 20 13 17 14
13 | 6 21 7 6 32 6 12 9 9 16 4 | 19 35 25 19 43 21 33 22 20 17 22
14 | 11 21 7 10 26 5 18 9 15 21 5 | 14 28 23 24 34 21 28 21 23 18 20
15 | 9 26 7 9 24 7 18 15 13 18 5 | 14 29 19 20 37 17 27 24 17 20 17
16 | 11 23 8 9 23 5 14 15 10 16 5 | 14 25 17 17 25 10 18 15 15 19 11
17 | 10 13 6 16 14 5 16 12 13 33 4 | 25 26 24 29 25 23 30 30 27 32 25
18E | 7 27 9 12 17 7 15 13 10 13 4 | 24 33 27 24 28 22 30 18 28 21 24
19 | 10 14 5 7 16 4 12 12 12 26 3 | 23 23 20 21 20 19 22 25 22 23 19
20E | 7 19 6 7 24 6 13 11 14 17 4 | 13 23 22 15 19 15 20 17 23 17 16
21 | 7 21 5 8 19 5 13 13 13 20 4 | 23 37 25 27 37 22 37 25 22 23 25
22E | 7 18 7 9 20 7 10 11 11 20 4 | 16 22 19 20 22 17 19 17 20 18 15
23 | 7 24 7 8 29 7 14 10 12 22 4 | 13 31 20 16 32 14 25 18 16 17 15
25 | 9 18 6 10 19 4 12 15 13 15 4 | 17 25 18 19 24 13 28 15 14 20 14
26 | 7 16 8 9 18 5 14 14 10 17 4 | 21 27 21 24 31 19 28 29 22 25 21
X27 | 29 28 24 22 --- 12 22 16 --- --- 10 | 21 28 34 37 --- 27 20 25 --- --- 22
28 | 10 19 5 9 20 4 17 12 9 19 4 | 18 27 19 22 30 17 23 24 16 19 17
29 | 8 17 9 13 17 6 17 18 13 31 5 | 25 28 36 26 25 27 32 33 30 28 28
X30 | 10 17 6 13 21 5 --- 17 13 23 5 | 23 30 21 27 23 21 --- 16 22 29 19
31 | 12 14 8 9 37 5 19 12 12 15 5 | 22 25 19 17 37 18 28 21 21 27 17
32E | 12 26 8 7 18 6 16 12 11 43 4 | 57 66 62 61 59 59 65 63 65 72 61
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 7 10 22 6 15 13 12 22 |T 21 29 24 24 30 21 28 24 23 25 21
WRMS | 9 19 7 10 20 6 15 12 9 20 |NE 19 27 22 22 29 18 26 22 20 23 19
MEDI | 9 19 7 9 20 6 14 13 11 20 |MD 19 28 21 22 29 19 28 24 21 23 19
Table 3.1660.5 GPS week: 1660 Day: 5 MJD: 55869.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 9 14 7 10 --- 7 15 16 15 18 4 | 28 38 33 23 --- 26 44 22 27 30 28
2 | 10 24 7 11 14 5 17 17 10 33 5 | 15 30 17 15 24 15 25 27 14 34 16
3 | 10 13 5 10 15 4 10 10 8 21 3 | 12 17 17 15 17 13 20 16 13 20 13
4 | 10 15 6 8 13 3 12 20 12 25 4 | 22 25 24 22 28 21 27 32 26 32 23
5E | 6 18 6 10 14 4 23 11 11 16 4 | 21 31 23 25 29 22 31 25 26 26 22
6 | 10 9 4 12 13 5 9 11 10 18 3 | 12 14 18 17 19 15 21 19 17 21 15
7 | 9 20 6 11 27 4 16 7 7 15 4 | 18 26 20 15 31 16 25 19 18 18 16
8 | 17 18 7 10 20 7 12 14 10 22 5 | 22 30 25 25 30 21 29 31 27 30 23
9 | 12 17 6 11 16 5 14 13 9 18 4 | 16 23 18 23 24 15 24 23 16 20 15
10E | 17 22 12 14 21 9 20 22 16 18 6 | 49 49 48 54 46 50 43 55 51 48 46
11 | 6 17 6 6 18 3 12 9 14 17 4 | 15 29 20 16 32 15 30 17 17 17 17
12 | 6 28 8 10 17 4 19 15 10 17 5 | 14 29 17 19 25 12 23 19 15 17 14
13 | 8 19 6 9 29 6 13 10 7 20 4 | 20 31 21 18 38 17 31 17 18 15 18
14 | 9 21 7 9 21 5 13 10 10 22 4 | 15 26 22 19 30 18 26 19 21 17 19
15 | 7 24 5 7 21 5 14 13 12 18 4 | 13 27 16 17 34 13 25 20 16 18 14
16 | 11 22 7 11 16 4 14 14 12 24 4 | 13 26 17 17 22 13 23 16 19 22 13
17 | 7 11 6 15 14 6 14 8 9 36 4 | 21 19 22 30 21 21 25 22 24 29 21
18E | 8 28 9 9 13 6 12 11 7 16 4 | 28 38 35 33 35 32 36 31 27 30 32
19 | 13 13 4 9 12 5 12 12 10 25 4 | 18 20 18 18 15 15 21 20 18 19 15
20E | 9 19 8 8 20 4 15 9 14 15 4 | 17 25 23 17 23 16 24 18 20 21 17
21 | 8 22 7 8 15 5 16 14 9 25 4 | 21 35 24 19 33 21 39 23 21 20 23
22E | 8 21 7 6 15 3 12 9 9 17 4 | 20 26 22 20 26 19 30 20 23 23 21
23 | 10 26 8 11 24 5 15 9 12 22 5 | 17 34 21 17 30 15 28 16 15 13 15
25 | 8 17 7 10 17 3 13 13 12 18 4 | 14 22 21 20 28 15 28 16 19 22 16
26 | 7 12 5 9 17 5 9 13 11 17 3 | 20 21 17 21 27 16 21 24 19 19 16
X27 | 17 20 10 18 --- 20 --- 16 --- 36 7 | 16 26 21 30 --- 19 --- 25 --- 15 17
28 | 8 22 7 11 19 5 15 10 11 21 4 | 16 29 15 20 27 16 25 20 22 19 15
29 | 9 17 9 12 15 5 20 13 18 32 5 | 21 26 33 25 23 25 28 26 28 26 25
X30 | 10 17 7 9 15 5 --- 15 9 27 4 | 19 26 19 23 21 17 --- 19 19 33 18
31 | 6 22 6 13 30 4 17 14 10 22 5 | 16 29 16 21 32 15 27 22 17 27 16
32E | 19 30 12 10 22 5 17 15 17 30 6 | 55 58 53 54 55 52 58 54 53 59 52
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 7 10 19 5 15 13 11 22 |T 20 28 23 22 28 19 28 23 22 24 20
WRMS | 9 20 7 10 16 5 14 11 9 20 |NE 17 26 20 20 26 16 26 20 19 21 17
MEDI | 9 19 7 10 17 5 14 13 10 21 |MD 18 26 21 20 28 16 27 20 19 21 17
Table 3.1660.6 GPS week: 1660 Day: 6 MJD: 55870.000
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 | 7 12 7 8 --- 7 13 15 16 22 4 | 33 43 38 39 --- 36 48 29 37 34 36
2 | 6 22 9 10 15 6 15 17 13 36 4 | 25 39 26 26 32 25 35 33 26 41 26
3 | 8 13 4 7 13 4 10 11 11 24 3 | 14 23 20 24 26 17 24 22 19 29 18
4 | 6 14 6 5 14 6 12 21 13 18 4 | 15 23 20 20 22 18 24 21 18 22 18
5E | 6 16 5 8 15 5 17 11 11 17 4 | 23 28 23 24 25 23 26 25 22 26 22
6 | 9 12 5 10 14 3 9 12 7 26 3 | 20 26 26 31 31 23 27 30 23 37 23
7 | 5 18 7 8 28 4 15 9 12 14 4 | 24 32 24 21 38 23 32 24 27 24 22
8 | 14 16 6 8 18 7 13 17 10 21 4 | 26 33 28 29 31 26 33 36 31 33 27
9 | 10 17 6 7 16 4 12 13 16 19 4 | 20 27 21 26 27 19 29 22 23 21 20
10E | 14 20 8 10 16 5 18 25 18 18 5 | 57 55 52 52 51 52 53 59 55 50 51
11 | 7 17 5 6 18 6 12 15 14 11 4 | 14 30 17 21 32 15 30 21 12 17 15
12 | 5 23 9 9 15 5 19 17 14 15 4 | 14 27 20 23 24 14 23 19 21 16 16
13 | 7 20 6 7 29 4 12 11 12 18 4 | 24 35 27 25 44 25 35 23 25 19 25
14 | 7 21 8 10 22 3 13 9 9 21 4 | 20 29 31 29 35 24 30 28 25 20 25
15 | 7 24 6 14 22 4 16 11 15 19 5 | 14 25 20 24 35 15 24 19 18 16 17
16 | 9 25 10 9 18 3 18 15 9 28 5 | 12 28 17 16 22 12 23 18 12 25 13
17 | 8 10 5 13 16 4 16 14 13 36 4 | 34 35 35 41 37 34 36 39 38 41 35
18E | 5 22 9 7 13 5 13 12 12 15 4 | 23 29 27 24 28 23 29 23 22 22 23
19 | 9 15 4 7 11 4 11 16 14 29 3 | 30 33 28 33 30 30 32 35 31 35 29
20E | 7 17 5 6 20 5 11 14 14 15 4 | 17 25 22 22 25 18 25 19 20 15 17
21 | 7 19 7 8 17 3 13 15 8 22 4 | 30 41 30 29 39 29 42 27 30 26 30
22E | 7 19 10 8 13 4 11 10 11 15 4 | 18 25 19 24 25 19 25 22 20 17 19
23 | 7 25 6 10 28 5 14 11 14 23 5 | 20 33 23 22 36 17 27 17 17 19 18
25 | 6 16 7 7 15 4 13 13 13 16 4 | 13 21 20 16 26 12 28 12 13 19 13
26 | 5 12 4 11 13 3 8 13 12 13 3 | 23 26 24 26 29 22 28 26 24 22 23
X27 | 20 17 12 20 --- 18 --- 17 --- 18 8 | 20 29 28 38 --- 34 --- 25 --- 14 23
28 | 9 20 4 7 20 4 14 9 11 19 4 | 18 28 21 25 33 18 23 21 22 21 19
29 | 6 13 8 14 14 6 15 13 13 31 4 | 31 34 36 41 32 33 39 33 38 36 33
X30 | 9 16 5 10 15 4 --- 16 11 35 4 | 21 29 21 20 23 16 --- 20 20 33 18
31 | 6 16 7 12 29 4 16 12 11 23 4 | 23 31 24 25 36 21 33 27 26 30 22
32E | 17 27 9 8 26 6 17 41 22 63 7 | 92 96 94 88 93 90 98 102 93 113 91
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 7 9 19 5 14 16 13 24 |T 24 32 27 29 33 25 33 28 26 28 25
WRMS | 8 19 7 9 17 5 13 12 10 19 |NE 21 30 24 26 31 22 30 24 23 25 22
MEDI | 7 17 6 8 16 4 13 13 12 19 |MD 21 29 24 25 31 23 29 24 23 24 22
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 4.1660 GPS week: 1660 MJD: 55864.0-55870.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 |U 14 8 27 |U 7 10 21 |U 9 11 19 |
emr | emr 2971 |U 16 10 31 |U 9 9 26 | 12 14 23 |
esa | esa 2976 | 14 8 28 |U 7 9 21 | 9 11 22 |
gfz | gfz 2969 |U 16 9 30 |U 7 10 22 |U 9 10 22 |
grg | grg 2784 | 17 14 34 |U 9 10 32 | 14 14 28 |
igr | igr 2972 | 14 8 27 | 7 9 22 | 9 9 20 |
igs | igs 2975 | 14 8 27 | 7 9 21 | 10 11 21 |
jpl | jpl 2816 |U 18 10 35 |U 8 10 27 | 11 12 24 |
mit | mit 2976 |U 31 21 102 |U 7 10 23 |U 12 11 28 |
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 5.1660.0 GPS week: 1660 Day: 0 MJD: 55864.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2969 | 10 7 28 | 6 9 21 | 8 13 20 |
emr | emr 2976 | 11 11 30 | 8 7 24 | 10 12 25 |
esa | esa 2976 | 9 7 28 | 6 7 20 | 10 12 22 |
gfz | gfz 2970 | 10 7 29 | 6 8 19 | 10 12 23 |
grg | grg 2784 | 15 11 31 | 7 8 28 | 12 14 27 |
igr | igr 2976 | 9 7 29 | 6 7 20 | 9 12 22 |
igs | igs 2975 | 9 7 28 | 6 7 19 | 9 12 21 |
jpl | jpl 2865 | 13 8 30 | 8 8 24 | 12 14 22 |
mit | mit 2976 | 8 9 26 | 6 7 18 | 9 12 30 |
Table 5.1660.1 GPS week: 1660 Day: 1 MJD: 55865.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 | 8 10 25 | 8 10 23 | 12 13 18 |
emr | emr 2976 | 9 10 27 | 11 9 27 | 18 27 23 |
esa | esa 2976 | 9 11 26 | 7 10 23 | 12 13 20 |
gfz | gfz 2971 | 9 11 27 | 8 12 29 | 13 13 21 |
grg | grg 2784 | 10 13 30 | 9 9 35 | 15 13 30 |
igr | igr 2975 | 8 11 25 | 7 10 24 | 13 12 19 |
igs | igs 2976 | 8 9 24 | 8 9 25 | 14 16 19 |
jpl | jpl 2784 | 12 13 32 | 8 9 30 | 15 14 21 |
mit | mit 2976 | 14 25 154 | 7 8 25 | 16 14 39 |
Table 5.1660.2 GPS week: 1660 Day: 2 MJD: 55866.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2972 | 47 13 50 | 7 8 18 | 6 9 15 |
emr | emr 2972 | 47 15 53 | 8 6 23 | 10 13 21 |
esa | esa 2976 | 47 13 50 | 6 7 17 | 8 12 19 |
gfz | gfz 2971 | 46 14 49 | 6 8 19 | 8 12 17 |
grg | grg 2784 | 47 16 54 | 7 9 25 | 12 17 28 |
igr | igr 2975 | 47 14 50 | 6 8 19 | 7 12 18 |
igs | igs 2976 | 47 15 50 | 6 7 17 | 8 11 17 |
jpl | jpl 2780 | 48 13 51 | 7 10 26 | 10 14 19 |
mit | mit 2976 | 16 33 106 | 7 9 21 | 9 11 22 |
Table 5.1660.3 GPS week: 1660 Day: 3 MJD: 55867.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 7 6 18 | 8 9 22 | 9 13 23 |
emr | emr 2971 | 10 9 25 | 10 9 26 | ---- ---- ---- |
esa | esa 2976 | 8 6 20 | 7 7 19 | ---- ---- ---- |
gfz | gfz 2972 | 9 6 19 | 8 9 21 | 8 7 26 |
grg | grg 2784 | 9 10 24 | 9 11 25 | ---- ---- ---- |
igr | igr 2972 | 8 6 19 | 7 8 21 | 8 6 24 |
igs | igs 2976 | 8 6 19 | 8 8 20 | ---- ---- ---- |
jpl | jpl 2871 | 13 6 23 | 8 9 23 | 11 14 31 |
mit | mit 2976 | 16 17 114 | 7 10 24 | ---- ---- ---- |
Table 5.1660.4 GPS week: 1660 Day: 4 MJD: 55868.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2960 | 8 7 22 | 8 6 20 | 11 10 22 |
emr | emr 2972 | 11 9 28 | 7 7 23 | 12 13 24 |
esa | esa 2976 | 6 6 21 | 7 7 21 | 9 11 24 |
gfz | gfz 2968 | 9 7 24 | 7 7 22 | 10 12 22 |
grg | grg 2784 | 13 15 38 | 10 10 42 | 13 17 25 |
igr | igr 2957 | 8 7 20 | 7 6 22 | 9 10 21 |
igs | igs 2976 | 7 5 21 | 7 6 20 | 10 11 23 |
jpl | jpl 2861 | 9 7 33 | 7 7 26 | 11 12 25 |
mit | mit 2976 | 40 21 80 | 8 9 22 | 11 10 26 |
Table 5.1660.5 GPS week: 1660 Day: 5 MJD: 55869.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2964 | 10 8 27 | 8 14 21 | 8 10 16 |
emr | emr 2970 | 13 7 29 | 7 13 27 | 16 9 29 |
esa | esa 2976 | 10 8 29 | 7 13 21 | 8 10 27 |
gfz | gfz 2967 | 15 9 30 | 8 14 20 | 11 9 28 |
grg | grg 2784 | 13 21 39 | 9 10 37 | 27 14 37 |
igr | igr 2976 | 10 8 29 | 7 12 22 | 9 8 23 |
igs | igs 2976 | 10 7 27 | 7 13 21 | 13 9 29 |
jpl | jpl 2778 | 14 8 36 | 8 11 24 | 12 10 32 |
mit | mit 2976 | 29 13 53 | 8 14 22 | 18 11 29 |
Table 5.1660.6 GPS week: 1660 Day: 6 MJD: 55870.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 10 8 21 | 8 13 24 | 7 7 20 |
emr | emr 2966 | 9 11 24 | 8 12 36 | 8 10 19 |
esa | esa 2976 | 8 7 21 | 6 12 26 | 6 7 19 |
gfz | gfz 2969 | 13 10 36 | 7 12 26 | 5 8 16 |
grg | grg 2784 | 9 10 24 | 10 17 33 | 8 12 22 |
igr | igr 2975 | 7 6 19 | 7 11 25 | 5 7 15 |
igs | igs 2975 | 8 8 21 | 7 12 26 | 6 6 18 |
jpl | jpl 2776 | 16 14 41 | 8 12 36 | 7 9 19 |
mit | mit 2976 | 91 27 179 | 8 13 28 | 8 8 22 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1660 GPS week: 1660 MJD: 55864.500-55870.500
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 7 -29 210 -1 | -2 9
| 19 21 66 140 7 | 2
emr uuuuu | 46 34 -16 117 -1 | 44 45
| 22 23 103 180 7 | 2
esa uuuuu | -20 -23 32 -149 -3 | -3 13
| 12 11 75 71 5 | 5
gfz uuuuu | -22 30 -25 11 8 | -4 9
| 28 18 60 73 3 | 1
grg uuuux | 56 -3 -4 242 -27 | -69 97
| 16 23 120 68 79 | 20
igr xxxxx | -34 32 -17 117 0 | 0 7
| 22 11 41 91 3 | 1
irf xxxxx | -9 26 5 31 -1 | 2 9
| 12 12 42 23 4 | 2
jpl uuuuu | 56 -68 13 270 -6 | 33 34
| 20 38 113 55 4 | 4
mit uuuuu | -44 26 -62 -155 0 | 9 13
| 19 28 89 25 3 | 1
ngs uuuxu | 2 24 59 52 -9 | 7 11
| 29 59 163 259 6 | 3
sio xxxxx | 205 -72 132 109 11 | 3 12
| 27 38 73 96 13 | 3
Table 7.1660.0 GPS week: 1660 Day: 0 MJD: 55864.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 14 5 -135 378 0 | 0 11
emr uuuuu | 25 63 -103 150 -2 | 46 47
esa uuuuu | -32 -30 75 -166 -7 | 3 15
gfz uuuuu | -10 19 63 69 2 | -4 9
grg uuuux | 63 32 -197 227 53 | -66 99
igr xxxxx | -22 40 -82 207 3 | 0 10
irf xxxxx | -3 25 56 26 -7 | 4 11
jpl uuuuu | 70 -53 -111 231 -5 | 38 40
mit uuuuu | -45 13 96 -161 2 | 8 13
ngs uuuxu | 6 11 -30 -2 0 | 9 13
sio xxxxx | 219 -71 232 20 -9 | 3 10
Table 7.1660.1 GPS week: 1660 Day: 1 MJD: 55865.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 2 24 -2 235 4 | 1 11
emr uuuuu | 52 49 -36 412 0 | 46 47
esa uuuuu | -35 -27 180 -246 -7 | 2 15
gfz uuuuu | -54 4 29 -23 7 | -4 9
grg uuuux | 54 16 -124 348 33 | -55 91
igr xxxxx | -34 28 -37 173 0 | 2 8
irf xxxxx | -6 37 46 65 -3 | 4 11
jpl uuuuu | 52 -60 -90 254 -7 | 38 40
mit uuuuu | -23 55 -32 -184 0 | 10 13
ngs uuuxu | 17 2 -105 489 -10 | 11 12
sio xxxxx | 225 -40 136 33 7 | 2 10
Table 7.1660.2 GPS week: 1660 Day: 2 MJD: 55866.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 14 24 -56 424 -3 | -1 10
emr uuuuu | 64 10 98 267 1 | 44 45
esa uuuuu | -20 -32 -4 -202 -9 | -1 15
gfz uuuuu | -61 41 -6 -81 7 | -4 9
grg uuuux | 59 -32 104 246 46 | -47 84
igr xxxxx | -48 15 36 140 -1 | 2 9
irf xxxxx | -7 33 43 33 -2 | 2 10
jpl uuuuu | 72 -35 -49 294 -11 | 35 37
mit uuuuu | -35 46 -2 -131 -3 | 8 13
ngs uuuxu | -4 3 -50 277 -4 | 9 12
sio xxxxx | 221 -42 182 38 17 | 0 9
Table 7.1660.3 GPS week: 1660 Day: 3 MJD: 55867.500
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 | 54 36 -74 129 9 | -4 9
emr uuuuu | 77 8 62 -33 11 | 42 42
esa uuuuu | -17 2 -37 -124 -1 | -7 11
gfz uuuuu | 14 14 -8 50 10 | -6 8
grg uuuux | 77 -25 143 291 -78 | -55 81
igr xxxxx | -8 37 24 176 -3 | -1 6
irf xxxxx | 8 39 -37 52 4 | -1 8
jpl uuuuu | 45 -48 213 338 -10 | 30 32
mit uuuuu | -20 62 -158 -156 5 | 6 12
ngs uuuxu | -46 -29 -2 10 -20 | 7 11
sio xxxxx | 237 -35 17 65 29 | -1 8
Table 7.1660.4 GPS week: 1660 Day: 4 MJD: 55868.500
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 | 32 -12 -8 84 0 | -2 8
emr uuuuu | 49 18 92 -110 -2 | 44 45
esa uuuuu | -10 -26 -15 -186 3 | -6 11
gfz uuuuu | 5 56 -95 122 7 | -3 8
grg uuuux | 70 7 27 262 -164 | -67 90
igr xxxxx | -10 43 -39 145 3 | 0 6
irf xxxxx | -5 20 -28 31 0 | 2 8
jpl uuuuu | 28 -36 80 327 -5 | 30 31
mit uuuuu | -51 14 -113 -121 -3 | 9 12
ngs uuuxu | -18 -21 130 -315 -13 | 6 11
sio xxxxx | 184 -93 157 150 21 | 4 13
Table 7.1660.5 GPS week: 1660 Day: 5 MJD: 55869.500
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 -13 68 105 -13 | -2 8
emr uuuuu | 12 58 -57 13 -8 | 44 45
esa uuuuu | -3 -26 37 -44 -2 | -7 11
gfz uuuuu | -29 39 -82 -61 10 | -2 9
grg uuuux | 34 -1 11 147 -30 | -90 115
igr xxxxx | -63 43 -27 -30 3 | -1 6
irf xxxxx | -26 24 -9 -8 -2 | 2 8
jpl uuuuu | 39 -108 55 266 0 | 29 30
mit uuuuu | -63 6 -90 -146 -4 | 9 13
ngs uuuxu | 44 61 88 -17 -6 | 3 8
sio xxxxx | 169 -88 144 190 6 | 6 16
Table 7.1660.6 GPS week: 1660 Day: 6 MJD: 55870.500
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 -14 4 113 -4 | -4 9
emr uuuuu | 41 29 -170 122 -8 | 43 44
esa uuuuu | -25 -24 -9 -78 4 | -8 11
gfz uuuuu | -18 36 -73 -1 9 | -2 9
grg uuuux | 36 -19 9 173 -47 | -102 121
igr xxxxx | -56 19 6 8 -4 | -1 5
irf xxxxx | -27 5 -38 20 0 | 1 7
jpl uuuuu | 85 -134 -5 180 -2 | 28 29
mit uuuuu | -69 -13 -136 -188 1 | 9 12
ngs uuuxu | 17 141 379 -81 -9 | 2 8
sio xxxxx | 178 -139 58 269 4 | 6 16
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