[IGSREPORT-21096] Wk 1700 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Aug 23 10:50:22 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1700 (Aug 05, 2012 - Aug 11, 2012)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi 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:
igs1700[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1700[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1700[0-6].cls IGS GPS clock combination summary report.
igs17007.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17007.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 | COD | KOUC
0 | EMR | 6
0 | ESA | 21 NNOR
0 | GFZ | 23 29 30 AMC2 BRAZ BRFT DGAR GMSD MAL2 OHI2 PDEL
0 | GFZ | VILL
0 | JPL | 6 CHUM
0 | MIT | 6 6 NICO NICO TWTF
1 | COD | 32 32 KOUC
1 | ESA | IRKJ
1 | GFZ | 23 BRFT
1 | GRG | IRKJ
1 | JPL | CHUM
1 | MIT | 32 6 32 TLSE USNO TLSE USNO
2 | COD | CHUR
2 | EMR | TLSE
2 | ESA | NNOR ONSA
2 | GFZ | 23 SUTM
2 | JPL | 6
2 | MIT | 6 18 28 6 18 28 GMAS MDVJ
3 | COD | KOUC
3 | ESA | IRKJ NNOR TLSE
3 | GFZ | 23 SFER VILL
3 | GRG | IRKJ
3 | JPL | 1 CHUM
3 | MIT | 28 30 28 30 TLSE TLSE
4 | COD | KOUC ONSA KOUC ONSA TLSE
4 | EMR | TLSE
4 | ESA | TLSE IRKJ NNOR TLSE
4 | GFZ | 23 29 HOB2
4 | GRG | IRKJ
4 | JPL | ONSA
4 | MIT | 26 SYOG TLSE HNPT SYOG
5 | COD | KOUC FLRS KOUC
5 | EMR | HERS HERS
5 | ESA | IRKJ NNOR
5 | GFZ | 23 NYAL VILL
5 | GRG | IRKJ
5 | JPL | DRAG
5 | MIT | 30 30
6 | COD | 4 JOZ2 KOUC JOZ2 KOUC TLSE
6 | EMR | 27 27 HERS HERS
6 | ESA | IRKJ NNOR
6 | GFZ | 4 23 27 MCM4 NTUS
6 | GRG | IRKJ
6 | JPL | 4 27
6 | MIT | 8 28 8 28
5. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G29 | 2012_08_08 | 2012050
6. 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
----+--------+---------------
3 | SIO | 6
7. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G06 | | | | 1 | | | |
PRN G24 | | | | | 2 | | |
8. 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.
9. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the current IGS reference frame. These rotations were
estimated in the IGS SINEX combination process, performed by the IGS Reference
Frame Coordinator at the Institut Geographique National (IGN). 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 | .4 .8 .6 -34 -13 15 -.31
EMR | -3.0 -4.4 -5.5 -6 -1 4 -.02
ESA | -2.3 -1.2 20.5 7 76 96 -.11
GFZ | -1.0 .7 -.2 -35 -9 -21 -.42
GRG | -1.7 -5.1 16.2 -48 35 -12 -.19
JPL | -5.6 2.9 -6.9 -40 11 35 -.01
MIT | 1.0 -.2 14.2 -11 14 -41 -.25
NGS | -1.2 3.0 16.2 -62 25 -14 -.12
SIO | -7.7 5.1 -2.6 63 71 11 -.28
10. 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.
11. 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.
12. 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 1.1700.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1700.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 2.1700.[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 3.1700.[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 5.1700.0-6).
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 1700 summary. (Aug 05, 2012 - Aug 11, 2012)
Table 1.1700.a GPS week: 1700 MJD: 56144.000-56150.000
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 263| 0 0 2 13 27 1 -.26 9 8 | -528 102 16 60
| 0 0 0 14 7 15 .03 | 305 508
emr 91| -1 -5 -13 -16 4 -5 .40 15 15 | 978 -166 19 107
| 1 2 1 17 16 7 .03 | 1064 937
esa 176| 0 0 2 -70 -26 19 .31 8 8 | -507 -294 16 132
| 0 0 1 13 10 11 .03 | 998 1671
gfz 196| 0 2 -1 35 59 -22 -.22 9 9 | 250 98 30 147
| 0 1 1 41 27 9 .01 | 622 667
grg 126| 1 0 9 59 -25 12 .57 16 15 | 162 -168 52 204
| 0 0 1 12 10 14 .05 | 271 391
igr n/a| 0 0 0 -26 13 -26 -.06 4 4 | 9619 -577 20 79
| 0 0 1 18 9 13 .02 | 1435 880
jpl 140| 2 0 -6 32 -1 28 .57 14 13 | 2364 -187 21 96
| 1 0 1 18 9 24 .03 | 948 799
mit 255| 2 0 0 -28 3 -13 -.33 9 8 | -12 -90 22 155
| 0 0 0 15 17 10 .01 | 353 508
ngs 255| 0 0 2 100 -32 -14 -.23 10 8 | -518 36 2034 3647
| 0 1 2 39 36 15 .03 | 299 498
sio 245| -2 2 -2 -173 -97 3 -.33 21 20 | --- --- --- ---
| 0 0 0 18 11 15 .02 | --- ---
Table 1.1700.b GPS week : 1700 MJD: 56144.000-56150.000
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 | 4 4 4 4 4 4 5 |
2 | 4 4 5 4 4 4 4 |
3 | 5 4 4 4 3 3 4 |
4 | 3 3 4 3 3 3 4 |
5 | 4 4 4 5 5 4 5 |
6 | 4 4 5 6 4 4 4 |
7 | 4 4 4 4 4 4 5 |
8 | 4 3 4 3 3 3 3 |
9 | 4 4 4 4 4 4 5 |
10 | 4 3 4 3 4 3 4 |
11 | 4 4 4 4 4 3 4 |
12 | 5 4 4 4 4 4 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 5 4 4 4 4 4 |
16 | 6 5 5 5 5 5 6 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 5 4 4 4 4 4 4 |
22 | 4 4 3 4 4 3 4 |
23 | 4 5 4 4 4 4 4 |
24 | --- --- --- --- 0 0 0 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 4 4 4 6 5 6 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 0 5 5 5 |
30 | 3 3 3 3 3 3 4 |
31 | 4 4 4 4 4 4 4 |
32 | 3 4 4 4 4 3 4 |
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 2.1700.0 GPS week: 1700 Day: 0 MJD: 56144.000
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 263| 0 0 3 15 19 -2 -.29 9 8 | -544 159 14 62
| 20 -7 |
emr 91| -3 -5 -11 4 8 -7 .40 15 15 | 2156 -574 20 105
| -15 -8 |
esa 176| 0 0 3 -60 -12 -3 .29 7 7 | 508 -1443 14 114
| 27 -9 |
gfz 196| 0 0 -3 -13 23 -20 -.23 11 10 | 977 -1003 33 164
| -1 -11 |
grg 126| 2 0 9 67 -22 3 .49 17 15 | 356 -450 52 212
| -48 -20 |
igr n/a| 0 0 0 -9 6 -51 -.06 4 4 | 12139 -1078 20 71
| 9 13 |
jpl 140| 0 0 -6 63 -9 43 .55 13 12 | 3591 -821 20 89
| -9 3 |
mit 255| 2 0 1 -52 -2 -24 -.33 10 9 | 143 -435 23 142
| 35 -33 |
ngs 255| 0 0 0 113 11 0 -.20 10 8 | -526 130 1992 3936
| -30 7 |
sio 245| -3 2 -2 -200 -110 -8 -.35 22 21 | --- --- --- ---
| 78 46 |
Table 2.1700.1 GPS week: 1700 Day: 1 MJD: 56145.000
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 263| -1 0 3 15 31 -10 -.30 8 8 | -589 137 17 58
| 50 21 |
emr 91| 0 -3 -13 -30 14 -1 .37 15 15 | 1089 -1123 22 113
| 25 -3 |
esa 176| 0 0 2 -84 -33 15 .28 6 6 | 128 -1640 19 140
| 44 -13 |
gfz 196| 0 1 -3 50 64 -9 -.21 10 11 | 12 113 36 151
| 6 11 |
grg 126| 2 0 11 74 -24 4 .53 16 15 | 216 -597 70 258
| -45 -8 |
igr n/a| 0 0 0 -10 14 -30 -.10 4 4 | 10567 -1740 22 78
| 8 -6 |
jpl 140| 4 0 -2 33 -11 2 .52 14 13 | 2260 -981 25 92
| 29 22 |
mit 255| 1 0 0 -9 40 -7 -.35 10 10 | 90 -407 24 148
| 26 -55 |
ngs 255| 0 1 0 102 -40 -18 -.21 9 8 | -627 30 1719 3021
| -4 63 |
sio 245| -3 1 -3 -156 -84 18 -.36 20 20 | --- --- --- ---
| 61 32 |
Table 2.1700.2 GPS week: 1700 Day: 2 MJD: 56146.000
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 263| 0 -1 2 6 27 1 -.24 8 8 | -443 128 15 60
| 58 5 |
emr 91| 0 -3 -13 -35 -9 -4 .41 15 15 | 854 -657 20 106
| 9 12 |
esa 176| 0 0 2 -73 -16 28 .36 8 8 | -158 -1344 19 127
| 25 -12 |
gfz 196| 0 1 0 37 81 -13 -.20 9 9 | 331 626 32 151
| 1 -3 |
grg 126| 1 0 9 71 -25 6 .56 16 15 | -42 0 50 190
| -42 -1 |
igr n/a| 1 0 1 -43 7 -16 -.05 5 5 | 9785 -952 21 77
| -1 30 |
jpl 140| 4 -1 -5 21 -3 0 .57 15 14 | 2201 -411 22 96
| -28 66 |
mit 255| 1 0 0 -16 2 -21 -.32 8 6 | -71 -15 21 141
| 32 -41 |
ngs 255| 0 2 2 103 -59 4 -.22 10 8 | -501 154 2237 3682
| 4 62 |
sio 245| -2 1 -2 -157 -102 -17 -.33 20 21 | --- --- --- ---
| 60 33 |
Table 2.1700.3 GPS week: 1700 Day: 3 MJD: 56147.000
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 263| 0 0 2 41 19 14 -.23 9 8 | -224 -343 18 64
| 48 22 |
emr 91| -2 -10 -13 6 35 -12 .42 16 16 | -82 -252 22 111
| 1 -35 |
esa 176| 0 0 4 -53 -39 21 .31 8 8 | -1993 1161 16 142
| 32 -2 |
gfz 196| 0 3 0 -18 89 -29 -.20 9 8 | -47 -422 30 138
| -13 14 |
grg 126| 1 0 8 63 -19 -1 .56 16 16 | 40 -139 50 215
| -42 2 |
igr n/a| 0 1 2 -9 2 -28 -.05 4 4 | 8595 -538 20 80
| 14 22 |
jpl 140| 0 -1 -6 47 11 57 .58 13 13 | 1443 -183 21 86
| 23 -40 |
mit 255| 2 0 0 -43 2 -19 -.32 8 7 | -271 279 22 165
| 39 -43 |
ngs 255| -1 1 1 165 -89 -20 -.27 11 10 | -181 -448 2143 3711
| -94 94 |
sio 245| 0 3 -2 -200 -83 -8 -.36 24 20 | --- --- --- ---
| 83 24 |
Table 2.1700.4 GPS week: 1700 Day: 4 MJD: 56148.000
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 263| 0 0 2 15 26 8 -.24 11 9 | -524 243 16 54
| 42 14 |
emr 91| 0 -5 -12 -30 -11 -14 .36 15 15 | -427 1225 17 93
| 19 4 |
esa 176| 0 0 1 -67 -32 30 .33 8 8 | -1443 2493 16 115
| 26 -22 |
gfz 196| -1 3 0 28 85 -34 -.23 8 8 | -451 659 27 134
| -37 21 |
grg 126| 1 1 8 46 -39 8 .57 15 14 | 61 -171 48 190
| -15 -5 |
igr n/a| 0 0 1 -21 18 -18 -.07 5 4 | 7948 602 21 75
| 0 -8 |
jpl 140| 1 0 -9 30 5 56 .56 15 14 | 1210 1045 20 89
| 43 -56 |
mit 255| 2 0 1 -19 -5 -16 -.33 8 8 | -63 -143 24 164
| 31 -33 |
ngs 255| 0 0 3 112 -41 -18 -.25 10 8 | -550 245 2200 3945
| -26 54 |
sio 245| -1 2 -1 -168 -90 3 -.33 19 17 | --- --- --- ---
| 69 27 |
Table 2.1700.5 GPS week: 1700 Day: 5 MJD: 56149.000
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 263| 0 0 1 -3 40 21 -.24 8 8 | -1138 1006 14 55
| 43 0 |
emr 91| 0 -4 -13 -25 0 -2 .45 16 16 | 780 1074 17 109
| -15 13 |
esa 176| -1 -1 0 -62 -34 29 .28 7 7 | -1089 451 17 142
| 23 -18 |
gfz 196| -2 3 -2 98 32 -31 -.22 9 8 | -262 837 27 147
| -23 11 |
grg 126| 2 0 8 45 -37 31 .65 14 13 | -144 586 47 186
| -12 -2 |
igr n/a| 0 0 0 -50 14 -24 -.04 4 4 | 8515 599 20 87
| 2 29 |
jpl 140| 3 1 -7 3 8 19 .61 15 14 | 2197 778 20 117
| 15 14 |
mit 255| 1 -1 0 -28 -5 -11 -.32 8 7 | -521 802 19 156
| 40 -29 |
ngs 255| 0 0 5 34 11 -41 -.23 8 7 | -1064 844 2130 3515
| 1 42 |
sio 245| -2 2 -2 -172 -111 17 -.31 21 21 | --- --- --- ---
| 65 35 |
Table 2.1700.6 GPS week: 1700 Day: 6 MJD: 56150.000
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 263| -1 0 2 0 30 -24 -.26 9 9 | -240 -615 22 72
| 55 20 |
emr 91| -1 -4 -14 -6 -4 5 .37 15 15 | 2476 -855 21 113
| -18 16 |
esa 176| 0 0 2 -89 -18 16 .30 9 9 | 497 -1742 16 144
| 43 -17 |
gfz 196| 0 2 -1 66 37 -18 -.23 9 9 | 1195 -123 28 144
| -21 14 |
grg 126| 1 0 8 47 -9 33 .63 16 15 | 653 -406 49 181
| -15 -13 |
igr n/a| 1 0 0 -41 29 -12 -.07 5 5 | 9790 -936 21 87
| 5 21 |
jpl 140| 1 0 -6 27 -8 15 .61 14 13 | 3647 -737 21 105
| -15 50 |
mit 255| 1 -1 0 -30 -10 5 -.35 10 9 | 608 -716 24 171
| 22 -36 |
ngs 255| 0 0 4 75 -18 -10 -.22 10 8 | -179 -699 1821 3719
| 11 -19 |
sio 245| -1 3 -2 -160 -96 19 -.31 21 20 | --- --- --- ---
| 42 35 |
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 3.1700.0 GPS week: 1700 Day: 0 MJD: 56144.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 21 7 13 14 4 13 12 11 14 4 | 24 28 29 21 37 25 39 24 23 19 24
2 | 8 19 8 8 13 3 15 7 11 23 4 | 24 39 27 23 33 24 35 21 21 24 24
3E | 15 16 7 13 14 7 14 11 9 33 4 | 28 36 28 30 33 26 34 23 25 23 26
4 | 7 12 5 10 8 5 10 8 10 14 3 | 14 20 19 19 22 13 23 12 17 16 15
5 | 9 14 8 5 11 4 10 9 8 32 3 | 29 34 32 34 36 32 33 36 35 31 32
6E | 8 16 6 11 15 3 16 10 10 16 4 | 23 30 22 22 25 23 31 26 23 23 23
7 | 9 15 6 13 19 3 17 8 10 8 4 | 12 22 15 16 24 12 23 14 13 12 12
8 | 7 11 6 10 13 3 11 9 11 18 3 | 13 18 14 12 16 13 20 15 16 19 12
9 | 9 19 6 13 13 4 11 12 9 23 4 | 14 27 18 17 19 17 21 21 18 30 16
10 | 8 10 6 11 14 5 9 8 10 19 3 | 29 32 34 28 35 30 35 30 32 22 31
11 | 7 15 6 10 20 4 12 11 10 14 3 | 14 23 16 16 31 14 22 16 15 19 14
12 | 14 17 8 9 18 5 13 11 11 28 4 | 16 30 21 20 27 19 28 21 21 22 19
13 | 9 14 7 11 21 6 14 8 12 13 4 | 12 26 16 13 28 13 23 13 18 14 13
14 | 8 17 9 11 15 3 15 8 12 17 4 | 14 27 18 16 25 15 24 16 17 19 15
15 | 11 14 9 11 15 4 16 12 6 22 4 | 16 28 21 18 25 17 25 22 18 20 18
16 | 8 15 11 12 18 3 18 9 12 50 5 | 13 23 17 12 24 13 25 14 16 46 12
17E | 7 15 6 9 18 4 16 9 8 12 3 | 21 29 18 18 28 21 26 24 24 23 21
18 | 8 13 7 16 9 4 11 15 9 19 4 | 18 22 21 30 21 19 20 24 21 22 19
19E | 8 17 7 10 21 3 11 9 10 18 4 | 14 23 15 13 22 14 21 18 18 23 15
20 | 6 10 4 6 14 4 11 6 9 33 3 | 21 22 24 22 29 23 20 21 21 33 21
21 | 8 17 7 10 42 4 14 12 10 20 5 | 15 29 19 14 41 17 27 18 20 18 17
22 | 9 12 6 9 8 3 11 9 10 23 3 | 23 26 26 24 29 23 25 29 20 26 23
23 | 9 16 8 11 16 4 15 8 9 27 4 | 13 29 18 15 22 14 25 16 19 26 15
25 | 8 20 6 7 23 4 14 8 9 14 4 | 15 29 19 19 30 19 29 21 19 18 18
26 | 6 10 7 14 13 3 11 13 7 27 4 | 15 24 19 14 23 16 26 20 13 32 17
27 | 9 17 5 11 15 3 11 10 7 19 3 | 36 46 40 37 41 40 47 43 41 46 40
28 | 5 11 7 10 17 3 11 7 9 20 3 | 10 24 17 16 23 14 24 13 14 16 13
29E | 11 15 7 10 20 4 16 12 11 20 4 | 11 20 12 15 17 13 19 17 20 16 14
30 | 7 10 6 7 12 2 9 11 9 14 3 | 9 17 15 11 16 11 18 17 15 16 12
31 | 6 15 10 9 22 4 18 7 10 13 4 | 12 24 16 12 30 12 24 15 16 16 13
32 | 6 13 6 6 12 5 7 7 8 21 3 | 16 25 26 19 28 20 25 19 17 23 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 7 11 17 4 13 10 10 22 |T 17 26 21 19 27 18 26 20 20 23 18
WRMS | 8 15 7 10 15 4 12 9 8 21 |NE 16 25 20 18 26 17 25 19 19 22 17
MEDI | 8 15 7 10 15 4 13 9 10 19 |MD 15 26 19 18 27 17 25 20 19 22 17
Table 3.1700.1 GPS week: 1700 Day: 1 MJD: 56145.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 19 7 11 18 3 15 11 11 14 4 | 24 30 31 20 41 24 39 20 23 18 25
2 | 6 17 6 6 14 3 16 9 9 23 3 | 20 33 29 21 37 22 33 18 24 14 24
3 | 10 17 6 10 20 6 18 11 8 13 4 | 14 27 17 19 26 15 27 15 18 16 16
4 | 5 12 5 11 11 3 12 7 7 14 3 | 15 25 23 23 24 18 26 15 20 19 19
5 | 7 14 5 6 11 5 13 11 8 30 3 | 31 31 27 30 31 30 32 31 29 30 29
6E | 9 17 7 10 15 5 20 11 10 17 4 | 22 29 23 25 28 22 30 24 22 29 23
7 | 7 16 6 9 16 4 18 8 12 10 3 | 13 25 13 13 23 11 23 15 13 16 12
8 | 8 11 4 9 13 3 10 7 8 13 3 | 10 18 12 12 15 10 18 13 12 16 11
9 | 9 14 7 10 13 3 10 11 7 20 3 | 12 20 20 14 16 14 20 18 15 26 15
10 | 5 7 7 8 14 4 10 9 7 18 3 | 19 21 25 22 25 21 23 19 20 15 20
11 | 6 15 6 10 22 5 10 10 11 14 3 | 13 22 18 14 35 14 22 10 16 16 14
12 | 11 15 6 11 18 4 15 11 9 23 4 | 13 25 20 16 26 15 25 14 15 18 15
13 | 8 15 8 10 22 6 15 8 14 11 4 | 13 27 15 13 30 15 24 12 23 16 14
14 | 6 22 7 12 16 3 14 8 9 17 4 | 11 28 15 16 25 13 20 14 15 19 13
15 | 13 15 7 9 15 5 17 14 9 19 4 | 19 25 17 17 26 15 24 18 17 19 16
16 | 9 16 8 15 18 5 17 11 7 48 5 | 11 23 18 17 24 13 25 11 15 41 13
17E | 7 16 7 8 14 3 17 9 7 14 3 | 18 28 25 22 25 19 26 18 20 19 20
18 | 8 13 6 14 9 4 11 13 7 17 3 | 14 17 12 20 17 14 16 19 17 17 13
19E | 6 17 7 11 15 5 13 11 7 18 3 | 13 21 17 16 21 14 19 12 15 15 13
20 | 6 11 6 12 15 4 12 8 11 30 4 | 20 22 21 24 22 20 23 18 22 29 20
21 | 6 16 7 10 13 3 13 12 11 18 3 | 11 25 14 12 32 12 25 15 11 12 13
22 | 6 12 6 9 12 3 12 11 7 23 3 | 17 22 18 17 25 17 23 21 14 19 17
23 | 8 18 8 11 17 4 17 11 9 25 4 | 15 28 19 15 25 16 26 16 20 25 16
25 | 7 19 7 8 16 4 13 7 10 15 3 | 12 18 18 13 25 14 26 16 14 16 14
26 | 6 13 6 10 13 6 10 14 8 26 4 | 14 25 18 14 22 14 23 20 14 32 16
27 | 9 12 5 10 15 4 12 10 12 15 3 | 32 42 35 34 38 34 43 36 37 38 35
28 | 6 12 7 11 11 5 14 8 11 20 3 | 10 26 21 21 25 18 23 16 17 18 17
29E | 11 16 10 13 13 4 18 12 12 15 4 | 9 21 17 15 17 11 20 14 12 13 12
30 | 8 11 5 9 15 4 9 6 9 13 3 | 8 15 12 10 16 10 17 11 15 11 10
31 | 9 17 6 12 20 5 15 5 11 12 4 | 12 24 15 12 29 13 23 14 13 16 13
32 | 5 12 6 11 15 3 10 9 11 21 3 | 23 29 26 25 27 24 29 24 17 26 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 15 6 10 16 4 14 10 9 20 |T 15 24 19 18 25 16 24 17 17 20 17
WRMS | 8 15 6 11 15 4 13 10 8 20 |NE 15 24 19 17 25 16 24 16 17 20 16
MEDI | 7 15 6 10 15 4 13 10 9 17 |MD 14 25 18 17 25 15 24 16 17 18 16
Table 3.1700.2 GPS week: 1700 Day: 2 MJD: 56146.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 21 7 9 15 5 16 7 9 15 4 | 26 32 36 23 42 29 44 23 27 22 28
2 | 9 17 13 6 15 7 20 7 11 22 4 | 25 36 30 23 36 25 37 22 23 20 25
3 | 10 13 6 9 13 5 15 8 9 14 3 | 15 26 18 17 22 15 27 15 20 19 16
4 | 8 12 10 9 9 3 13 9 9 13 3 | 15 23 23 18 22 17 22 16 19 16 17
5 | 8 16 10 5 10 5 14 8 14 31 4 | 30 33 34 30 34 30 31 32 35 33 31
6E | 11 21 7 10 17 5 20 11 9 21 4 | 49 56 47 48 53 48 55 53 48 57 50
7 | 7 14 6 7 15 5 17 6 9 9 3 | 13 24 18 13 24 14 24 14 18 13 13
8 | 11 10 8 7 13 4 12 5 12 12 3 | 14 19 18 13 16 14 17 14 16 17 13
9 | 9 20 6 7 15 4 11 9 8 15 3 | 13 27 17 13 21 15 21 19 18 24 16
10 | 7 10 9 10 15 5 11 5 13 18 3 | 22 21 30 25 29 26 24 22 25 19 23
11 | 7 14 6 8 20 5 15 8 12 13 3 | 13 26 21 17 35 17 26 13 19 18 17
12 | 10 15 8 11 15 6 15 8 10 19 4 | 18 29 23 18 29 21 28 20 21 21 19
13 | 8 18 8 9 19 5 14 6 10 10 3 | 14 28 17 14 30 14 22 15 16 14 15
14 | 4 19 8 10 16 3 13 6 9 17 3 | 14 28 17 15 24 15 22 15 20 18 15
15 | 12 15 9 12 13 5 19 10 6 17 4 | 16 24 18 19 27 15 24 20 18 18 17
16 | 9 16 9 11 20 4 17 7 10 46 5 | 14 26 20 15 25 15 25 14 18 39 14
17E | 9 16 6 9 13 5 16 7 10 12 3 | 16 27 24 17 26 20 25 19 16 22 18
18 | 5 12 8 10 9 5 13 10 9 18 3 | 14 19 18 23 17 16 19 18 22 15 15
19E | 7 15 6 11 17 4 10 8 7 17 3 | 15 27 20 17 25 18 22 15 20 16 17
20 | 9 11 5 10 17 6 13 5 10 29 4 | 24 26 28 25 28 24 26 21 20 32 23
21 | 5 15 7 9 15 4 16 10 9 20 3 | 16 30 19 14 30 16 28 19 17 17 17
22 | 5 12 7 6 9 5 11 7 8 23 3 | 17 21 21 20 21 19 23 22 22 20 19
23 | 7 20 9 10 17 6 20 8 8 23 4 | 14 32 20 17 26 17 27 16 17 24 17
25 | 6 18 7 9 18 5 16 7 10 15 3 | 16 25 21 16 29 19 29 20 20 18 17
26 | 6 14 9 8 13 5 11 9 6 27 3 | 17 24 21 14 23 18 24 19 15 35 18
27 | 9 18 6 6 19 4 11 9 11 15 3 | 34 51 39 38 46 39 45 40 41 42 39
28 | 8 12 6 8 15 5 12 6 10 17 3 | 10 25 21 17 26 15 23 15 16 15 15
29E | 11 15 8 15 15 5 17 9 12 15 4 | 13 18 10 17 17 9 17 16 15 12 12
30 | 9 12 9 7 16 5 8 4 5 13 3 | 11 20 18 12 18 13 21 13 16 12 13
31 | 7 16 9 11 21 3 15 4 7 13 3 | 14 24 20 14 29 14 23 14 16 15 15
32 | 8 12 5 6 16 7 11 7 10 20 3 | 17 22 24 18 22 19 24 20 18 23 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 15 8 9 16 5 15 8 10 20 |T 18 27 22 19 27 19 26 19 21 22 19
WRMS | 8 15 8 9 15 5 14 6 8 21 |NE 16 25 22 17 26 18 25 18 19 20 18
MEDI | 8 15 8 9 15 5 14 7 9 17 |MD 15 26 21 17 26 17 24 19 19 19 17
Table 3.1700.3 GPS week: 1700 Day: 3 MJD: 56147.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 23 7 11 15 4 14 10 6 15 4 | 26 31 30 24 37 26 41 24 23 19 26
2 | 7 18 8 7 15 4 17 7 11 23 4 | 25 38 26 23 33 24 36 20 19 21 24
3 | 8 13 8 7 10 4 13 11 10 16 3 | 14 25 18 14 20 15 27 15 16 22 15
4 | 7 12 6 12 10 4 12 6 9 12 3 | 14 23 18 20 22 16 24 15 19 15 16
5 | 16 16 7 10 13 6 13 8 9 31 4 | 66 64 65 69 66 64 67 66 61 65 65
6E | 13 22 10 11 14 8 20 19 12 79 5 | 96 106 98 98 104 97 103 90 94 65 97
7 | 8 18 8 7 17 3 18 8 10 13 4 | 13 26 15 12 23 13 26 16 20 15 14
8 | 9 9 5 7 10 3 10 6 8 10 2 | 15 20 15 11 15 14 21 14 13 14 13
9 | 9 16 6 7 15 4 12 11 12 14 3 | 14 24 18 15 17 15 18 14 13 22 14
10 | 6 9 5 7 15 5 9 5 9 17 3 | 23 26 26 25 34 27 28 24 21 22 24
11 | 9 16 8 8 21 5 11 9 12 13 4 | 11 23 16 14 31 12 22 13 14 14 12
12 | 11 13 7 10 18 4 12 8 14 20 4 | 20 31 23 18 26 20 28 21 21 17 20
13 | 8 14 8 7 20 4 13 7 12 11 3 | 16 27 16 11 29 13 26 15 20 12 15
14 | 6 20 8 11 17 5 13 5 12 17 4 | 17 29 18 18 25 16 24 16 18 21 16
15 | 9 19 8 11 13 4 17 9 10 16 4 | 15 29 17 18 26 15 26 17 13 20 16
16 | 8 14 9 13 20 5 16 8 8 47 5 | 17 24 17 15 24 14 27 15 18 44 15
17E | 9 16 5 7 13 4 15 11 7 9 3 | 21 27 21 12 26 19 23 17 15 19 17
18 | 8 14 11 10 10 4 11 7 13 19 3 | 16 19 17 23 15 15 20 18 17 15 15
19E | 8 16 9 10 18 5 11 10 10 18 4 | 19 26 22 17 25 19 26 21 21 22 19
20 | 5 11 6 7 16 4 12 7 9 30 3 | 21 22 24 22 27 23 24 21 19 31 21
21 | 6 17 9 11 13 3 14 8 12 19 4 | 20 32 22 16 29 19 30 19 18 18 19
22 | 7 11 8 7 9 3 10 7 14 23 3 | 20 21 21 22 25 19 23 23 19 21 19
23 | 7 16 7 9 16 4 15 9 10 23 4 | 19 31 19 12 23 16 29 18 19 24 17
25 | 8 20 7 10 23 4 15 6 11 16 4 | 21 31 20 20 28 19 29 22 24 16 20
26 | 7 14 10 7 11 4 10 6 12 28 3 | 20 25 22 17 24 20 27 21 21 33 20
27 | 9 18 6 8 17 4 18 11 13 14 4 | 42 59 42 46 49 44 54 46 43 47 45
28 | 10 13 7 8 14 4 10 8 9 17 3 | 14 27 19 15 25 14 26 17 13 16 15
X29E | 4 --- --- --- --- 28 --- --- --- --- 0 | 25 --- --- --- --- 28 --- --- --- --- 21
30 | 7 11 8 9 13 5 9 4 8 12 3 | 17 21 19 18 21 16 23 17 18 15 17
31 | 7 15 7 11 20 4 14 6 9 11 3 | 18 28 19 18 33 16 27 15 19 18 18
32 | 10 13 6 7 17 5 11 7 12 23 3 | 39 43 40 36 38 37 41 38 35 37 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 8 9 16 4 13 8 11 24 |T 23 31 25 23 30 23 31 23 23 24 23
WRMS | 8 16 8 8 16 4 13 7 10 20 |NE 20 28 22 20 27 20 28 20 20 22 20
MEDI | 8 15 7 8 15 4 13 8 10 17 |MD 19 27 19 18 26 19 26 18 19 20 18
Table 3.1700.4 GPS week: 1700 Day: 4 MJD: 56148.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 14 20 7 9 15 5 14 8 7 16 4 | 28 30 34 25 41 27 43 22 24 21 27
2 | 7 17 7 5 14 3 19 8 12 22 4 | 24 35 28 23 38 24 36 24 22 21 25
3 | 8 12 7 5 9 5 16 7 10 14 3 | 15 25 21 19 21 16 30 18 23 22 18
4 | 6 14 6 9 9 3 13 6 10 11 3 | 16 26 21 22 24 18 25 17 21 21 19
5 | 17 16 8 8 10 4 16 7 17 32 4 | 58 64 62 67 61 61 63 61 59 63 61
6 | 14 20 9 7 12 8 16 8 6 18 4 | 64 70 65 66 69 65 76 63 65 53 65
7 | 9 17 8 7 15 4 16 8 9 12 3 | 13 25 16 15 23 12 25 18 16 19 15
8 | 8 8 6 7 10 4 12 6 10 10 3 | 15 19 15 15 16 14 17 14 16 15 14
9 | 10 15 9 9 13 5 11 10 13 12 4 | 15 20 16 13 17 15 21 13 18 19 13
10 | 8 9 6 8 14 4 10 6 12 19 3 | 19 27 24 25 29 25 25 24 27 21 23
11 | 7 12 6 7 22 6 12 8 9 12 3 | 13 23 18 16 34 13 25 14 15 16 15
12 | 12 15 7 10 16 5 15 9 10 19 4 | 19 27 22 17 28 18 26 19 18 18 18
13 | 8 15 8 8 20 5 13 7 10 11 3 | 16 27 16 14 31 14 24 16 18 15 15
14 | 7 16 7 10 16 5 13 7 12 17 4 | 17 28 19 20 27 16 26 16 17 21 16
15 | 10 16 8 10 14 6 19 9 7 16 4 | 16 25 17 19 26 14 26 16 14 18 16
16 | 10 15 10 11 14 5 17 7 7 46 5 | 16 27 20 18 25 15 28 16 16 39 16
17E | 8 16 5 10 14 4 19 7 6 15 3 | 18 26 22 23 25 18 29 21 19 21 19
18 | 8 13 8 9 8 4 12 8 10 21 3 | 18 17 14 20 17 15 16 18 19 19 14
19E | 7 14 6 9 20 4 13 6 6 13 3 | 16 24 19 17 23 15 24 17 18 19 17
20 | 7 13 7 8 15 4 14 8 13 29 4 | 16 24 22 23 24 19 23 22 21 30 20
21 | 7 16 8 5 14 5 18 8 10 19 3 | 15 29 18 15 30 14 30 18 15 17 17
22 | 8 12 7 6 8 4 12 8 8 23 3 | 23 24 21 23 26 20 23 23 20 21 20
23 | 8 18 8 7 15 4 18 8 10 24 4 | 16 28 18 15 24 14 28 14 15 23 15
X24 | 4 --- --- --- --- >>>> --- --- --- --- 0 | 150 --- --- --- --- 9999 --- --- --- --- 148
25 | 6 20 8 9 21 5 15 8 8 14 4 | 17 24 19 19 28 16 30 21 14 19 17
26 | 6 13 10 7 11 4 11 9 12 26 3 | 15 21 17 17 24 15 22 18 17 33 17
27 | 31 17 9 9 22 9 18 16 13 16 6 | 73 83 79 76 85 75 88 78 75 78 78
28 | 10 11 5 9 13 4 12 8 9 17 3 | 14 27 23 20 27 17 27 21 21 18 19
29E | 14 19 8 14 18 5 15 8 11 13 4 | 12 21 12 19 20 14 19 16 13 16 13
30 | 9 10 9 7 14 4 11 4 9 13 3 | 12 20 17 13 17 11 23 14 16 14 14
31 | 8 16 11 9 17 4 16 6 9 11 3 | 16 27 21 18 31 15 25 15 13 17 16
32 | 7 13 7 7 12 3 11 8 12 20 3 | 18 28 23 20 25 21 27 22 21 23 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 8 8 15 5 15 8 10 19 |T 25 29 24 23 30 21 30 22 22 24 26
WRMS | 9 15 8 8 14 4 14 8 8 17 |NE 23 26 21 20 27 18 27 19 19 22 24
MEDI | 8 15 8 8 14 4 14 8 10 16 |MD 16 26 20 19 26 16 26 18 18 21 17
Table 3.1700.5 GPS week: 1700 Day: 5 MJD: 56149.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 20 8 12 14 3 14 6 8 20 4 | 26 27 34 23 43 28 43 23 22 19 27
2 | 7 16 7 7 13 6 15 10 9 23 3 | 19 29 25 19 35 22 32 20 20 17 21
3 | 8 12 7 6 11 4 16 7 5 15 3 | 11 24 19 15 18 13 27 13 17 20 14
4 | 6 13 6 7 9 3 11 6 7 13 2 | 15 21 17 15 20 13 22 13 18 14 15
5 | 7 16 9 12 9 3 14 6 6 34 4 | 59 61 60 62 63 61 65 59 64 64 60
6 | 7 13 7 7 12 5 16 8 8 21 3 | 38 48 42 39 39 38 45 38 37 35 38
7 | 7 17 6 8 13 4 20 7 6 16 3 | 11 25 13 14 24 13 22 14 11 16 12
8 | 9 10 5 8 10 4 13 7 6 14 3 | 10 16 12 13 14 11 16 11 11 15 10
9 | 10 21 6 8 14 5 18 12 8 12 4 | 12 24 16 14 14 16 22 14 15 19 12
10 | 5 11 7 6 13 3 10 5 8 20 3 | 16 21 17 18 24 19 21 19 22 21 18
11 | 7 12 7 5 20 4 11 9 7 12 3 | 10 23 19 16 34 14 22 16 18 17 15
12 | 12 20 9 10 17 5 16 9 6 19 4 | 14 23 17 17 24 15 24 16 16 15 14
13 | 7 16 5 8 19 2 15 7 8 12 3 | 11 25 13 11 29 12 22 12 13 13 11
14 | 9 19 7 10 16 2 15 7 13 19 4 | 14 28 16 16 24 14 22 13 21 19 13
15 | 7 16 8 10 16 3 16 9 6 18 3 | 12 25 19 16 26 16 23 13 17 19 14
16 | 9 16 8 11 14 5 16 9 7 47 4 | 9 24 15 13 22 10 24 12 12 39 10
17E | 7 16 6 8 16 4 16 13 8 9 3 | 16 24 19 18 25 16 24 17 24 18 17
18 | 7 14 8 11 6 4 12 6 9 22 3 | 12 18 11 20 13 12 15 13 19 16 11
19E | 6 14 6 10 19 3 13 7 8 16 3 | 10 23 19 13 23 13 21 12 16 12 13
20 | 5 12 8 11 12 3 16 9 9 28 3 | 14 21 22 22 18 18 19 20 18 30 18
21 | 7 18 7 6 17 3 15 7 10 21 3 | 12 28 17 11 26 13 27 14 15 15 13
22 | 7 11 6 6 7 3 11 7 8 24 3 | 14 20 14 14 19 14 20 17 21 15 14
23 | 7 21 8 9 15 3 18 8 7 24 4 | 12 29 16 14 25 15 25 14 15 23 13
X24 | 4 --- --- --- --- 81 --- --- --- --- 0 | 133 --- --- --- --- 9999 --- --- --- --- 130
25 | 6 23 8 9 15 4 15 10 7 16 4 | 13 23 13 14 24 12 26 17 11 13 12
26 | 7 14 8 6 12 4 14 9 7 29 3 | 12 23 18 14 22 15 23 16 14 32 14
27E | 17 23 6 9 17 8 21 11 7 23 5 | 39 50 39 40 43 40 51 41 38 46 40
28 | 8 12 6 9 12 4 13 8 8 19 3 | 10 27 19 18 23 15 25 17 16 18 15
29E | 10 22 10 13 16 3 16 10 11 16 4 | 14 24 10 16 19 13 17 14 14 16 11
30 | 9 13 6 9 14 4 9 6 7 14 3 | 10 18 14 15 16 11 20 13 12 12 12
31 | 7 15 7 11 15 3 16 5 9 11 3 | 15 25 17 17 29 15 24 14 15 16 14
32 | 6 12 8 6 12 3 10 6 5 21 3 | 16 22 22 19 22 18 21 19 17 23 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 16 7 9 14 4 15 8 8 21 |T 19 26 20 18 25 17 26 18 19 21 20
WRMS | 8 16 7 8 13 4 14 7 7 21 |NE 19 25 19 17 25 16 25 17 18 20 20
MEDI | 7 16 7 9 14 4 15 7 8 19 |MD 13 24 17 16 24 15 23 14 17 18 14
Table 3.1700.6 GPS week: 1700 Day: 6 MJD: 56150.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 15 20 8 11 15 4 11 11 12 24 4 | 30 29 36 25 43 28 44 26 27 23 29
2 | 9 14 11 6 15 3 14 10 11 23 4 | 24 34 25 23 35 22 34 22 22 24 24
3 | 10 11 8 7 13 3 15 7 8 16 3 | 16 22 19 17 19 15 28 16 20 25 17
4 | 6 14 9 10 13 4 12 11 7 16 3 | 13 19 16 15 24 13 20 16 19 12 14
5 | 7 15 11 10 15 5 12 8 12 34 4 | 54 55 59 61 62 56 58 59 58 59 58
6 | 6 12 7 7 10 3 14 9 7 23 3 | 38 46 43 41 39 40 46 37 37 41 39
7 | 8 23 7 9 15 5 19 11 11 16 4 | 14 32 17 16 24 15 26 18 18 17 16
8 | 8 9 7 9 11 3 11 8 8 16 3 | 12 19 14 16 15 12 18 14 13 19 12
9 | 10 18 9 8 16 4 16 18 13 16 4 | 14 23 17 15 22 13 23 18 17 16 14
10 | 10 10 8 6 16 7 9 7 8 21 3 | 23 24 27 25 37 25 24 25 25 27 24
11 | 7 18 8 8 21 5 9 14 8 15 4 | 9 22 18 13 34 10 20 16 15 15 13
12 | 12 16 9 11 17 7 13 12 10 23 4 | 21 26 19 21 24 16 24 20 19 21 18
13 | 7 15 9 8 21 5 13 7 7 14 3 | 14 27 15 13 30 12 24 15 17 15 14
14 | 7 16 10 13 17 4 14 7 13 18 4 | 17 26 16 21 25 16 24 17 15 26 15
15 | 12 13 11 9 14 4 20 12 6 16 4 | 14 24 17 19 26 14 27 15 12 18 14
16 | 10 14 10 11 18 5 17 11 9 47 5 | 12 24 18 20 24 13 26 17 20 40 15
17E | 10 15 8 8 14 4 18 8 12 11 4 | 21 24 18 18 26 17 25 20 24 23 18
18 | 7 11 9 9 9 4 11 7 10 22 3 | 18 17 16 26 21 18 16 22 21 20 17
19E | 12 12 7 9 24 5 10 7 9 16 4 | 15 21 17 13 26 13 20 15 18 16 14
20 | 6 12 8 9 14 4 14 14 8 29 4 | 20 21 23 25 29 21 21 24 23 28 21
21 | 6 16 8 10 16 3 15 8 9 21 4 | 18 32 20 18 29 18 29 19 17 18 18
22 | 8 14 8 9 10 6 10 8 15 24 4 | 26 23 24 30 32 23 24 30 23 25 24
23 | 7 19 11 6 16 5 18 10 9 23 4 | 17 32 20 16 26 15 31 18 19 23 18
X24 | 4 --- --- --- --- 62 --- --- --- --- 0 | 92 --- --- --- --- 9999 --- --- --- --- 92
25 | 8 20 7 11 21 4 13 7 7 17 4 | 20 28 19 26 27 17 27 23 17 17 19
26 | 7 9 11 8 13 5 13 11 10 26 4 | 14 21 19 16 23 16 21 21 19 32 17
27E | 14 22 8 9 16 6 20 19 12 20 5 | 45 62 49 48 53 48 59 52 54 53 50
28 | 9 13 6 8 9 3 13 6 10 20 3 | 14 26 20 20 25 16 25 21 22 22 18
29E | 11 20 12 13 20 5 17 8 9 16 4 | 15 24 17 22 23 16 20 19 16 21 17
30 | 8 11 8 7 17 8 10 7 10 16 3 | 9 18 14 15 19 10 20 15 16 14 13
31 | 10 17 8 9 19 6 18 8 13 10 4 | 15 27 18 18 28 14 27 17 21 22 17
32 | 8 13 9 8 14 4 8 8 11 22 3 | 16 19 23 20 26 17 21 19 17 20 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 9 9 16 5 14 10 10 21 |T 21 27 22 22 28 19 27 22 21 24 22
WRMS | 9 15 9 9 15 5 13 9 8 20 |NE 21 25 21 21 28 18 26 21 20 22 22
MEDI | 8 14 8 9 15 4 13 8 10 20 |MD 16 24 19 20 26 16 24 19 19 22 17
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 4.1700 GPS week: 1700 MJD: 56144.0-56150.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2980 |U 7 7 16 |U 4 6 22 | ---- ---- ---- |
emr | emr 2960 | 8 9 20 |U 6 7 30 | ---- ---- ---- |
esa | esa 2962 | 7 6 17 |U 4 6 23 | ---- ---- ---- |
gfz | gfz 2957 |U 7 6 16 |U 5 6 25 | ---- ---- ---- |
grg | grg 2962 |U 10 12 26 |U 8 10 38 | ---- ---- ---- |
igr | igr 2948 | 7 6 16 | 4 6 24 | ---- ---- ---- |
igs | igs 2960 | 6 6 16 | 4 6 23 | ---- ---- ---- |
jpl | jpl 2960 | 7 7 18 |U 5 6 23 | ---- ---- ---- |
mit | mit 2962 | 6 6 17 |U 5 6 25 | ---- ---- ---- |
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 5.1700.0 GPS week: 1700 Day: 0 MJD: 56144.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 9 23 | 5 6 24 | ---- ---- ---- |
emr | emr 2972 | 9 11 25 | 6 7 24 | ---- ---- ---- |
esa | esa 2976 | 9 9 24 | 4 6 21 | ---- ---- ---- |
gfz | gfz 2966 | 10 9 24 | 5 6 25 | ---- ---- ---- |
grg | grg 2976 | 9 8 25 | 7 8 47 | ---- ---- ---- |
igr | igr 2976 | 9 9 23 | 5 6 26 | ---- ---- ---- |
igs | igs 2973 | 9 9 24 | 4 6 22 | ---- ---- ---- |
jpl | jpl 2972 | 10 10 24 | 5 6 21 | ---- ---- ---- |
mit | mit 2976 | 9 9 25 | 5 8 28 | ---- ---- ---- |
Table 5.1700.1 GPS week: 1700 Day: 1 MJD: 56145.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 5 4 13 | 6 8 26 | ---- ---- ---- |
emr | emr 2971 | 6 9 17 | 6 9 39 | ---- ---- ---- |
esa | esa 2976 | 5 5 15 | 6 10 25 | ---- ---- ---- |
gfz | gfz 2972 | 5 4 15 | 6 10 29 | ---- ---- ---- |
grg | grg 2975 | 12 21 31 | 11 14 49 | ---- ---- ---- |
igr | igr 2975 | 5 4 14 | 6 9 25 | ---- ---- ---- |
igs | igs 2975 | 5 4 15 | 5 9 25 | ---- ---- ---- |
jpl | jpl 2971 | 6 6 17 | 5 10 31 | ---- ---- ---- |
mit | mit 2976 | 6 5 19 | 8 10 26 | ---- ---- ---- |
Table 5.1700.2 GPS week: 1700 Day: 2 MJD: 56146.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 5 12 | 5 5 19 | ---- ---- ---- |
emr | emr 2974 | 8 9 17 | 5 5 28 | ---- ---- ---- |
esa | esa 2976 | 7 5 14 | 5 5 24 | ---- ---- ---- |
gfz | gfz 2971 | 7 5 13 | 5 5 25 | ---- ---- ---- |
grg | grg 2976 | 13 12 28 | 8 10 31 | ---- ---- ---- |
igr | igr 2975 | 7 5 13 | 5 5 22 | ---- ---- ---- |
igs | igs 2974 | 7 5 13 | 4 5 23 | ---- ---- ---- |
jpl | jpl 2974 | 8 7 16 | 5 5 22 | ---- ---- ---- |
mit | mit 2976 | 7 5 14 | 5 6 24 | ---- ---- ---- |
Table 5.1700.3 GPS week: 1700 Day: 3 MJD: 56147.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 10 11 23 | 4 6 20 | ---- ---- ---- |
emr | emr 2880 | 10 12 25 | 6 8 31 | ---- ---- ---- |
esa | esa 2880 | 10 11 23 | 4 6 21 | ---- ---- ---- |
gfz | gfz 2876 | 10 11 22 | 4 5 21 | ---- ---- ---- |
grg | grg 2880 | 10 12 22 | 6 9 37 | ---- ---- ---- |
igr | igr 2784 | 12 11 25 | 4 7 22 | ---- ---- ---- |
igs | igs 2880 | 9 11 22 | 4 5 21 | ---- ---- ---- |
jpl | jpl 2877 | 9 11 24 | 4 5 19 | ---- ---- ---- |
mit | mit 2880 | 10 10 21 | 4 6 25 | ---- ---- ---- |
Table 5.1700.4 GPS week: 1700 Day: 4 MJD: 56148.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2981 | 6 6 15 | 3 5 20 | ---- ---- ---- |
emr | emr 2976 | 7 9 24 | 5 7 27 | ---- ---- ---- |
esa | esa 2976 | 5 5 17 | 4 4 22 | ---- ---- ---- |
gfz | gfz 2972 | 7 5 19 | 4 4 23 | ---- ---- ---- |
grg | grg 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igr | igr 2976 | 5 5 16 | 4 4 23 | ---- ---- ---- |
igs | igs 2976 | 5 5 18 | 4 4 22 | ---- ---- ---- |
jpl | jpl 2976 | 7 6 17 | 5 4 21 | ---- ---- ---- |
mit | mit 2976 | 5 4 18 | 4 5 21 | ---- ---- ---- |
Table 5.1700.5 GPS week: 1700 Day: 5 MJD: 56149.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3044 | 6 6 14 | 4 5 21 | ---- ---- ---- |
emr | emr 2975 | 7 10 15 | 5 6 28 | ---- ---- ---- |
esa | esa 2976 | 4 4 10 | 4 6 23 | ---- ---- ---- |
gfz | gfz 2975 | 4 4 9 | 5 5 22 | ---- ---- ---- |
grg | grg 2975 | 6 9 23 | 6 9 25 | ---- ---- ---- |
igr | igr 2975 | 4 5 11 | 4 5 23 | ---- ---- ---- |
igs | igs 2975 | 4 4 10 | 4 5 23 | ---- ---- ---- |
jpl | jpl 2975 | 5 7 16 | 5 5 24 | ---- ---- ---- |
mit | mit 2976 | 5 4 12 | 4 5 24 | ---- ---- ---- |
Table 5.1700.6 GPS week: 1700 Day: 6 MJD: 56150.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 5 6 12 | 4 7 21 | ---- ---- ---- |
emr | emr 2976 | 7 7 17 | 7 6 32 | ---- ---- ---- |
esa | esa 2976 | 5 6 15 | 4 6 27 | ---- ---- ---- |
gfz | gfz 2971 | 5 5 12 | 7 6 31 | ---- ---- ---- |
grg | grg 2976 | 11 11 25 | 9 10 41 | ---- ---- ---- |
igr | igr 2976 | 4 5 13 | 4 6 26 | ---- ---- ---- |
igs | igs 2970 | 5 5 13 | 4 5 26 | ---- ---- ---- |
jpl | jpl 2976 | 6 5 15 | 7 5 26 | ---- ---- ---- |
mit | mit 2976 | 5 6 13 | 4 5 27 | ---- ---- ---- |
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 : 10-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 6.1700 GPS week: 1700 MJD: 56144.500-56150.500
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 | -11 -35 97 -99 5 | 5 16
| 12 12 56 94 7 | 1
emr uuuuu | 0 9 -18 -181 -8 | 34 41
| 17 15 102 73 14 | 2
esa uuuuu | 13 -22 80 192 2 | 17 23
| 9 8 48 46 4 | 2
gfz uuuuu | -9 22 46 -28 -1 | 8 17
| 12 14 42 60 3 | 1
grg uuuux | 6 41 -75 -135 1 | 19 41
| 6 18 53 40 22 | 5
igr xxxxx | -15 5 99 9 2 | 4 17
| 15 8 50 40 6 | 2
irf xxxxx | 0 10 5 -30 1 | 5 15
| 5 5 19 9 3 | 1
jpl uuuuu | -9 2 166 -109 9 | 36 40
| 42 25 56 46 4 | 4
mit uuuuu | 38 -22 -136 14 5 | 16 22
| 11 10 68 32 2 | 3
ngs uuuuu | -44 30 -73 -60 -3 | 11 17
| 36 34 43 121 3 | 2
sio uuuuu | -34 -56 87 76 -5 | 36 39
| 10 16 66 47 8 | 3
Table 7.1700.0 GPS week: 1700 Day: 0 MJD: 56144.500
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 -14 149 -71 -7 | 5 17
emr uuuuu | 0 21 -140 -209 14 | 31 39
esa uuuuu | 1 -21 51 152 2 | 16 22
gfz uuuuu | 3 7 58 -79 -4 | 6 18
grg uuuux | 12 54 -149 -195 -16 | 11 45
igr xxxxx | -21 -3 74 -3 5 | 1 17
irf xxxxx | -8 6 36 -40 -4 | 5 16
jpl uuuuu | -11 15 76 -111 12 | 29 36
mit uuuuu | 25 -29 -40 2 1 | 14 20
ngs uuuuu | -15 36 -47 77 -1 | 12 17
sio uuuuu | -54 -72 194 117 -19 | 40 42
Table 7.1700.1 GPS week: 1700 Day: 1 MJD: 56145.500
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 -30 96 -20 -2 | 6 17
emr uuuuu | 5 -5 40 -147 -3 | 35 42
esa uuuuu | 15 -24 73 131 3 | 18 24
gfz uuuuu | -9 14 103 -108 -3 | 9 17
grg uuuux | 10 65 -127 -172 0 | 17 40
igr xxxxx | 8 12 137 31 -1 | 4 17
irf xxxxx | 2 20 -27 -30 -1 | 7 15
jpl uuuuu | -20 -9 196 -137 6 | 34 39
mit uuuuu | 57 -6 -251 15 6 | 16 22
ngs uuuuu | -61 24 -39 83 -1 | 14 18
sio uuuuu | -30 -41 1 99 -10 | 40 42
Table 7.1700.2 GPS week: 1700 Day: 2 MJD: 56146.500
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 -47 69 -187 8 | 2 15
emr uuuuu | -6 2 116 -256 -10 | 33 40
esa uuuuu | 18 -14 73 182 6 | 15 21
gfz uuuuu | 9 10 23 59 0 | 6 16
grg uuuux | 7 53 -107 -134 -23 | 18 40
igr xxxxx | -24 12 109 24 4 | 1 16
irf xxxxx | 6 11 7 -28 1 | 3 14
jpl uuuuu | -60 39 228 -104 5 | 34 38
mit uuuuu | 47 -21 -123 -5 6 | 13 19
ngs uuuuu | -56 7 -121 -61 -6 | 11 16
sio uuuuu | -27 -49 65 87 -7 | 35 38
Table 7.1700.3 GPS week: 1700 Day: 3 MJD: 56147.500
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 -43 105 -74 10 | 4 15
emr uuuuu | 34 4 -26 -32 -7 | 34 41
esa uuuuu | 1 -27 80 182 2 | 17 23
gfz uuuuu | -15 18 82 -56 -1 | 8 16
grg uuuux | -3 47 -31 -93 -18 | 19 40
igr xxxxx | -23 -9 119 -39 1 | 4 16
irf xxxxx | -1 5 4 -16 5 | 5 14
jpl uuuuu | 39 -18 146 -36 6 | 36 40
mit uuuuu | 42 -34 -145 58 8 | 16 21
ngs uuuuu | -95 99 -96 -275 -5 | 12 16
sio uuuuu | -25 -78 44 89 0 | 35 38
Table 7.1700.4 GPS week: 1700 Day: 4 MJD: 56148.500
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 -33 109 42 12 | 5 17
emr uuuuu | -7 -10 48 -195 -16 | 36 42
esa uuuuu | 19 -17 71 267 5 | 19 24
gfz uuuuu | -24 46 49 -18 4 | 9 17
grg uuuux | 2 24 -66 -120 6 | 20 40
igr xxxxx | 5 9 145 -3 9 | 5 17
irf xxxxx | -3 9 9 -39 2 | 7 16
jpl uuuuu | 53 -34 183 -134 7 | 38 42
mit uuuuu | 30 -22 -130 -26 5 | 18 23
ngs uuuuu | -57 35 -131 -99 -7 | 12 17
sio uuuuu | -30 -60 118 84 -3 | 35 38
Table 7.1700.5 GPS week: 1700 Day: 5 MJD: 56149.500
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 | 4 -32 -8 -175 10 | 6 16
emr uuuuu | -9 26 0 -225 -7 | 36 42
esa uuuuu | 22 -12 32 222 -6 | 19 24
gfz uuuuu | -7 34 -26 -26 -1 | 9 17
grg uuuux | 6 23 -8 -144 34 | 22 41
igr xxxxx | -25 9 -2 -28 5 | 5 16
irf xxxxx | 4 11 11 -20 1 | 7 16
jpl uuuuu | -10 -4 219 -173 16 | 40 43
mit uuuuu | 33 -29 -84 57 6 | 19 24
ngs uuuuu | -38 10 -57 -74 0 | 10 17
sio uuuuu | -31 -54 137 85 -1 | 34 37
Table 7.1700.6 GPS week: 1700 Day: 6 MJD: 56150.500
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 -48 161 -208 6 | 5 16
emr uuuuu | -19 25 -165 -200 -31 | 34 41
esa uuuuu | 14 -36 181 210 0 | 17 24
gfz uuuuu | -17 28 36 35 0 | 7 17
grg uuuux | 10 22 -37 -85 24 | 26 42
igr xxxxx | -24 2 114 80 -10 | 5 17
irf xxxxx | -3 7 -4 -35 4 | 5 16
jpl uuuuu | -53 22 117 -66 10 | 40 43
mit uuuuu | 33 -15 -182 -1 5 | 19 23
ngs uuuuu | 16 -4 -22 -69 0 | 9 17
sio uuuuu | -38 -35 48 -27 4 | 32 36
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