[IGSREPORT-20872] Wk 1688 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu May 31 10:11:26 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1688 (May 13, 2012 - May 19, 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:
igs1688[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1688[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1688[0-6].cls IGS GPS clock combination summary report.
igs16887.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16887.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because of poorer consistency (GRG),
they provide broadcast clocks (NGS), or clock corrections are not provided
(SIO). The clock information not used is still compared to combination for
completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | ALL | 24
0 | COD | CHUR QAQ1 CHUR KOUC QAQ1
0 | EMR | 30 30 HERS HERS
0 | ESA | NNOR UNSA
0 | GFZ | 32
0 | JPL | 32 CHUM IISC IRKJ RAMO
0 | MIT | 30 30 32 REUN
1 | COD | KOUC KOUC XMIS
1 | EMR | DRAO DRAO
1 | ESA | IRKJ NNOR
1 | GFZ | BRFT BRMU MATE
1 | GRG | IRKJ
1 | MIT | 28 28 30 32 DAV1 GODE NICO DAV1 GODE NICO
2 | ALL | 24
2 | COD | KOUC KOUC RCMN
2 | EMR | 30 30 HERS HERS MCM4 WTZR
2 | ESA | IRKJ NNOR UNSA
2 | GFZ | 32 CHAN FAIR MAG0 SSIA
2 | GRG | IRKJ
2 | JPL | 30 32 CHUM
2 | MIT | 30 32 30 32 GODE GODE
3 | ALL | 24
3 | COD | KOUC KOUC
3 | EMR | 30 HERS
3 | ESA | IRKJ NNOR
3 | GFZ | BOR1 DAV1
3 | GRG | IRKJ
3 | JPL | 30
3 | MIT | 1 6 23 26 31 32 1 6 23 26 30 31 32 CAS1 GODE MDVJ
4 | COD | KOUC KOUC WILL
4 | ESA | NNOR SOFI UNSA
4 | GFZ | 32 DAV1 THTI TWTF
4 | JPL | 32
4 | MIT | 1 30 1 30 32 MDVJ
5 | ALL | 24
5 | COD | KOUC KOUC
5 | ESA | IRKJ NNOR UNSA
5 | GFZ | 32 BOR1 BRFT DAV1
5 | GRG | IRKJ
5 | JPL | IRKJ
5 | MIT | 23 30 32 15 23 30 32 CAS1 DAV1 GODE CAS1 DAV1
6 | ALL | 24
6 | COD | KOUC FLRS KOUC
6 | EMR | 30 30 HERS
6 | ESA | IRKJ NICO
6 | GFZ | 30 BRFT DAV1
6 | GRG | IRKJ IRKJ
6 | MIT | 30 30 31
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 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 | .0 -.3 -1.7 -59 -24 34 .42
EMR | 5.1 -6.2 7.3 8 8 -12 .60
ESA | 1.2 -1.6 20.9 -67 35 79 .33
GFZ | -.5 .8 -.6 -42 16 -15 .27
GRG | 3.6 .2 19.2 -45 20 -3 .19
JPL | 2.6 -1.2 11.1 -27 17 1 .57
MIT | 2.1 -4.6 19.1 -46 32 -68 .33
NGS | 9.6 -5.8 14.7 -75 -29 47 .46
SIO | 3.1 -2.8 -4.7 -57 -185 124 .41
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 1.1688.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1688.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 2.1688.[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 3.1688.[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 5.1688.0-6).
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 1688 summary. (May 13, 2012 - May 19, 2012)
Table 1.1688.a GPS week: 1688 MJD: 56060.000-56066.000
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 259| 0 0 -2 20 46 27 -.25 8 8 | -457 -424 18 77
| 0 0 1 13 14 6 .02 | 579 949
emr 93| 2 0 -5 -105 51 -21 .33 17 17 | 4581 -30 19 108
| 2 1 1 13 27 15 .03 | 652 1339
esa 176| 0 0 1 1 11 -13 .23 8 8 | -25 -539 14 123
| 0 0 1 22 22 12 .02 | 1139 1954
gfz 194| 0 0 1 -24 -62 -5 -.23 10 10 | 104 50 28 107
| 0 0 1 54 67 9 .03 | 305 750
grg 125| 0 2 7 -11 -35 -6 .60 13 12 | -89 123 46 183
| 1 1 3 8 10 9 .03 | 293 578
igr n/a| 0 0 -2 -73 -6 -5 -.10 5 4 | 3119 -605 18 70
| 0 0 1 18 12 14 .02 | 1211 1269
jpl 172| -1 1 -4 -53 -40 37 .43 15 14 | 5063 -264 18 82
| 1 1 1 13 15 24 .02 | 799 1265
mit 320| 0 -1 0 7 -69 -29 -.47 12 11 | -396 314 25 160
| 1 0 1 17 19 17 .01 | 398 577
ngs 222| 0 -1 0 85 74 -8 -.24 11 9 | 150439 -143277 2052 3682
| 0 0 2 24 41 11 .05 | 399077 377779
sio 238| 0 0 -4 38 377 135 -.38 20 21 | --- --- --- ---
| 1 1 1 13 15 19 .02 | --- ---
Table 1.1688.b GPS week : 1688 MJD: 56060.000-56066.000
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 4 |
2 | 5 4 4 4 4 4 4 |
3 | 4 3 4 3 4 4 4 |
4 | 5 4 3 3 4 4 4 |
5 | 5 5 5 5 5 5 5 |
6 | 4 3 4 3 4 3 3 |
7 | 5 5 4 4 4 4 4 |
8 | 4 3 3 4 4 4 3 |
9 | 4 5 4 4 4 4 4 |
10 | 8 7 6 6 6 6 7 |
11 | 4 5 4 4 4 4 4 |
12 | 6 8 6 5 6 6 6 |
13 | 5 5 5 5 5 5 5 |
14 | 4 5 4 4 5 4 5 |
15 | 5 4 4 4 5 5 5 |
16 | 5 5 5 4 5 5 4 |
17 | 5 4 4 4 5 5 4 |
18 | 4 4 4 4 5 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 5 5 4 4 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 4 4 4 4 3 |
23 | 5 5 5 4 4 5 4 |
24 | 15 0 13 10 0 12 10 |
25 | 4 4 4 4 6 4 4 |
26 | 4 3 4 4 4 4 4 |
27 | 4 4 4 4 4 4 4 |
28 | 5 4 5 5 4 4 4 |
29 | 5 4 4 4 4 4 5 |
30 | 6 6 6 6 7 8 8 |
31 | 5 5 5 4 5 5 5 |
32 | 5 5 5 5 5 5 6 |
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 2.1688.0 GPS week: 1688 Day: 0 MJD: 56060.000
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 259| 0 0 -5 16 21 18 -.24 9 9 | -125 -800 18 75
| 32 15 |
emr 93| 4 -2 -7 -96 74 -13 .28 17 17 | 3471 1397 17 82
| -14 -111 |
esa 176| 0 0 1 -11 -18 -9 .23 8 8 | -337 -515 12 115
| -6 -21 |
gfz 194| 0 0 0 12 33 -13 -.21 12 12 | -167 681 28 105
| -11 18 |
grg 125| 0 2 12 0 -56 -8 .57 13 13 | -11 9 40 170
| -11 3 |
igr n/a| 0 0 -3 -91 -28 -7 -.11 5 5 | 3604 499 19 67
| 3 9 |
jpl 172| -3 1 -6 -50 -39 43 .42 15 14 | 4603 794 18 92
| 23 6 |
mit 320| 0 0 -2 14 -33 6 -.47 14 13 | -216 79 29 147
| -44 15 |
ngs 222| 0 -2 3 67 22 -29 -.34 11 8 | -198 -712 2078 3731
| -18 35 |
sio 238| 0 0 -6 28 398 170 -.38 21 20 | --- --- --- ---
| -107 -198 |
Table 2.1688.1 GPS week: 1688 Day: 1 MJD: 56061.000
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 259| 0 0 -3 11 32 22 -.24 8 7 | -719 54 18 86
| 29 3 |
emr 93| 1 -3 -6 -126 55 -31 .31 18 18 | 4599 1958 21 130
| -11 -78 |
esa 176| 1 0 3 -35 18 -32 .25 8 8 | -1607 1402 15 148
| -18 -31 |
gfz 194| 0 0 1 63 -4 -11 -.26 10 10 | -277 1171 28 121
| -54 37 |
grg 125| 1 1 9 -18 -40 -14 .62 14 12 | -576 1126 42 203
| 0 -9 |
igr n/a| 0 0 -3 -95 -13 18 -.08 5 5 | 3869 1156 20 74
| -38 -1 |
jpl 172| -3 0 -6 -52 -20 58 .42 15 14 | 5106 1548 19 82
| -14 -29 |
mit 320| -2 -1 0 28 -89 -21 -.47 14 12 | -654 886 23 132
| -30 46 |
ngs 222| 0 0 0 58 22 8 -.26 11 8 | -676 -19 1819 3809
| -41 8 |
sio 238| -3 0 -6 38 360 149 -.41 21 24 | --- --- --- ---
| -95 -184 |
Table 2.1688.2 GPS week: 1688 Day: 2 MJD: 56062.000
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 259| 1 0 -3 26 46 33 -.24 9 7 | -452 -170 18 71
| 0 -16 |
emr 93| 3 0 -5 -83 22 -26 .35 18 18 | 5327 406 18 76
| -23 -53 |
esa 176| 0 0 1 5 20 -18 .26 8 8 | 1273 2465 14 109
| -25 -27 |
gfz 194| 0 -1 3 -37 -51 -1 -.24 10 9 | 265 493 26 105
| -18 1 |
grg 125| 1 0 7 -17 -30 -6 .62 13 12 | -371 689 44 172
| -7 -16 |
igr n/a| 0 0 -2 -76 -10 -8 -.09 4 4 | 4247 154 19 67
| -14 10 |
jpl 172| -2 2 -5 -47 -44 55 .46 16 15 | 5920 494 17 83
| -13 18 |
mit 320| -1 0 0 3 -74 -34 -.46 11 10 | -519 835 21 139
| -19 39 |
ngs 222| -1 0 0 86 71 -13 -.25 11 8 | -345 -314 2167 3663
| -51 -32 |
sio 238| -2 0 -4 49 384 126 -.37 20 22 | --- --- --- ---
| -83 -208 |
Table 2.1688.3 GPS week: 1688 Day: 3 MJD: 56063.000
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 259| 0 0 -2 18 53 31 -.22 9 7 | -1333 909 17 77
| 13 -28 |
emr 93| 5 0 -4 -99 71 -21 .36 17 17 | 5114 -587 19 84
| -17 -74 |
esa 176| 1 0 0 0 49 -25 .24 8 8 | -138 -1084 13 113
| -2 -30 |
gfz 194| 0 0 1 -47 -129 0 -.25 9 9 | 521 -956 29 100
| -26 7 |
grg 125| 0 2 6 -3 -36 13 .63 14 13 | -53 4 42 197
| -30 -36 |
igr n/a| 0 0 -2 -75 5 -14 -.10 4 4 | 3873 -1190 18 63
| 5 -4 |
jpl 172| -2 2 -4 -53 -44 52 .46 14 13 | 5900 -916 19 90
| 26 16 |
mit 320| -1 0 0 -10 -87 -33 -.44 9 9 | -431 544 23 171
| -23 57 |
ngs 222| 0 -2 0 118 120 -8 -.21 11 9 | -1164 600 2114 3580
| -75 -106 |
sio 238| -2 0 -4 28 364 133 -.35 19 21 | --- --- --- ---
| -78 -187 |
Table 2.1688.4 GPS week: 1688 Day: 4 MJD: 56064.000
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 259| 0 0 -2 1 60 22 -.27 9 8 | 255 -1453 20 81
| 55 -24 |
emr 93| 0 1 -4 -111 88 -11 .32 17 17 | 5082 -1794 21 142
| -14 -111 |
esa 176| 0 0 0 -3 19 -10 .25 9 9 | 1473 -2496 14 129
| -22 -22 |
gfz 194| 0 -1 2 -17 -157 11 -.17 11 11 | 315 -296 30 119
| -33 47 |
grg 125| 1 2 3 -6 -31 -9 .58 14 13 | 301 -210 54 191
| -8 -44 |
igr n/a| 0 0 0 -67 7 -20 -.12 4 4 | 3397 -2557 17 72
| -17 7 |
jpl 172| -2 3 -3 -72 -68 16 .41 15 14 | 5638 -2170 20 84
| 30 -1 |
mit 320| 0 -3 0 19 -76 -38 -.49 12 11 | 163 -405 34 250
| -19 37 |
ngs 222| 0 -2 1 94 128 0 -.25 11 9 | 1055462 -999999 2144 3886
| -91 -100 |
sio 238| 0 0 -5 44 364 123 -.36 19 21 | --- --- --- ---
| -79 -198 |
Table 2.1688.5 GPS week: 1688 Day: 5 MJD: 56065.000
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 259| 0 0 -2 43 52 33 -.27 8 8 | 114 -1735 20 82
| 16 -14 |
emr 93| -1 -1 -3 -105 32 -45 .32 17 17 | 4240 -811 19 150
| 4 -39 |
esa 176| 0 0 1 38 -12 3 .22 8 8 | 259 -2989 13 139
| -25 -16 |
gfz 194| 0 0 0 -111 -44 -17 -.22 9 9 | 246 -515 29 109
| -15 34 |
grg 125| 0 2 3 -19 -23 -11 .57 13 12 | -11 -232 55 176
| -12 -20 |
igr n/a| 0 0 -1 -39 0 -15 -.09 4 4 | 1837 -1245 19 77
| -6 21 |
jpl 172| 0 1 -3 -31 -41 43 .40 15 14 | 4402 -835 18 74
| 55 -21 |
mit 320| 1 -2 0 -19 -55 -49 -.47 12 11 | -73 -467 20 139
| -16 37 |
ngs 222| 0 0 1 113 76 -7 -.22 11 9 | 125 -1774 1828 3652
| -97 -49 |
sio 238| 0 1 -3 23 394 111 -.40 19 22 | --- --- --- ---
| -77 -200 |
Table 2.1688.6 GPS week: 1688 Day: 6 MJD: 56066.000
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 259| 0 0 0 25 59 26 -.25 8 7 | -941 226 21 72
| 51 -20 |
emr 93| 2 0 -2 -113 18 1 .37 17 17 | 4239 -779 22 94
| 1 -28 |
esa 176| -1 0 0 13 5 0 .18 7 7 | -1103 -558 17 112
| -6 -2 |
gfz 194| 0 0 1 -36 -86 -8 -.25 11 11 | -174 -227 30 96
| -35 35 |
grg 125| 0 2 5 -15 -30 -3 .62 14 12 | 98 -522 48 176
| -7 -21 |
igr n/a| 0 0 -2 -66 -5 8 -.08 4 4 | 1011 -1058 19 76
| 3 22 |
jpl 172| 1 0 -1 -67 -27 -8 .44 15 14 | 3872 -763 18 72
| -2 40 |
mit 320| 1 -1 1 14 -69 -34 -.47 14 11 | -1045 726 27 146
| -40 29 |
ngs 222| 0 0 -4 62 77 -8 -.17 11 9 | -127 -721 2220 3459
| -33 -69 |
sio 238| 2 3 -3 59 377 136 -.40 20 20 | --- --- --- ---
| -90 -208 |
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 3.1688.0 GPS week: 1688 Day: 0 MJD: 56060.000
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 | 9 12 8 14 11 4 13 13 9 11 4 | 42 41 45 53 43 42 38 42 46 39 43
2 | 9 20 8 12 11 4 16 10 8 34 4 | 16 26 18 17 20 14 26 18 15 24 15
3 | 9 11 7 15 9 3 8 10 11 15 3 | 13 15 16 22 21 13 14 16 15 14 15
4 | 11 11 7 9 10 5 9 25 10 35 4 | 23 26 31 30 33 23 27 36 27 40 27
5E | 6 17 6 11 13 4 21 13 8 16 4 | 14 26 21 21 23 17 27 18 17 19 17
6 | 6 10 6 13 9 3 10 11 11 13 3 | 18 17 21 25 25 17 16 21 16 17 19
7 | 11 16 9 16 14 6 12 9 14 16 4 | 9 22 14 14 23 10 18 12 14 16 11
8 | 7 15 7 10 10 5 15 10 10 18 4 | 11 22 15 14 13 11 21 15 16 17 13
9 | 8 17 6 14 9 6 13 16 7 26 4 | 13 23 16 17 20 16 20 23 18 27 16
10E | 15 19 14 13 17 11 20 32 25 24 7 | 52 57 57 58 65 54 62 64 62 62 56
11 | 11 12 9 13 11 5 10 11 10 19 4 | 25 29 31 32 36 25 30 22 25 21 27
12 | 9 25 7 9 18 4 29 16 10 19 5 | 51 54 47 50 51 47 57 52 48 54 50
13 | 9 16 10 14 18 5 13 15 10 22 4 | 20 27 20 21 31 17 25 20 20 19 19
14 | 8 23 8 10 12 4 15 11 5 21 4 | 19 30 23 20 26 17 23 19 18 24 18
15 | 12 19 9 12 14 5 18 13 8 23 4 | 16 30 20 22 27 20 29 21 23 22 19
16 | 6 24 7 14 14 4 20 11 7 27 4 | 25 32 29 33 36 27 30 27 28 29 27
17 | 7 13 7 17 12 8 16 14 11 22 4 | 20 26 22 25 25 21 26 26 24 19 21
18E | 8 19 9 10 11 6 16 13 5 17 4 | 18 25 20 18 19 16 24 24 18 22 18
19 | 8 12 8 14 10 3 11 15 8 25 4 | 17 22 21 22 23 19 20 18 17 12 18
20E | 8 23 6 13 18 6 13 11 10 19 4 | 26 35 25 24 25 25 26 30 29 38 25
21 | 7 17 6 9 11 5 15 15 9 26 4 | 25 26 18 23 17 23 26 33 28 38 22
22E | 6 14 6 9 11 5 14 11 10 18 3 | 19 26 22 18 26 20 23 21 21 21 19
23 | 9 19 11 13 15 5 12 14 10 19 4 | 24 31 24 21 26 20 25 22 25 18 22
X24 | 11 --- --- --- --- 17 21 --- --- --- 15 | 31 --- --- --- --- 30 29 --- --- --- 31
25E | 9 19 6 11 14 5 13 13 7 16 4 | 37 37 35 32 34 35 36 30 35 28 33
26 | 8 11 10 9 13 3 11 12 8 16 3 | 28 23 21 24 24 24 27 30 22 25 23
27 | 8 15 6 13 11 5 12 13 8 18 4 | 12 19 13 19 20 12 20 20 15 24 14
28 | 6 14 7 12 22 6 13 13 11 11 4 | 24 33 27 26 39 26 30 29 30 29 26
29 | 11 13 8 12 13 4 18 13 7 28 4 | 19 23 21 23 24 20 25 26 21 26 20
30E | 12 15 11 14 15 7 16 15 22 21 5 | 19 25 23 27 23 19 18 22 30 17 21
31 | 7 21 7 10 16 3 14 11 11 15 4 | 14 24 15 15 31 12 22 12 11 14 13
32E | 10 18 5 11 12 6 15 16 18 23 5 | 29 28 26 29 22 30 24 29 42 44 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 8 12 13 5 15 14 11 21 |T 22 28 24 25 28 22 27 25 25 26 23
WRMS | 9 17 8 12 13 5 14 13 8 20 |NE 19 25 21 22 25 19 24 22 20 22 20
MEDI | 8 16 7 12 12 5 14 13 10 19 |MD 19 26 21 23 25 20 25 22 22 24 20
Table 3.1688.1 GPS week: 1688 Day: 1 MJD: 56061.000
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 15 5 14 9 5 14 9 12 12 4 | 32 25 26 39 28 28 24 30 29 30 28
2 | 7 20 9 10 11 6 18 10 7 33 4 | 16 27 17 16 21 17 25 14 15 22 15
3 | 5 15 7 11 9 3 10 9 8 16 3 | 13 15 17 16 19 13 14 15 13 14 13
4 | 9 11 6 7 8 5 9 17 9 32 3 | 17 19 22 15 23 18 21 21 13 32 16
5E | 5 20 9 14 15 5 22 11 9 16 4 | 17 30 22 21 28 18 26 18 19 19 19
6 | 5 14 8 10 9 3 9 8 6 14 3 | 14 14 19 17 18 14 15 17 15 16 15
7 | 8 18 12 11 16 4 12 12 12 15 4 | 13 24 18 14 27 13 22 18 17 17 16
8 | 6 15 8 6 8 4 12 7 10 13 3 | 14 22 17 16 19 15 24 18 17 16 16
9 | 9 19 6 9 16 4 16 15 10 25 4 | 16 24 16 19 21 16 22 22 18 26 16
10E | 16 17 9 10 19 6 16 26 22 23 6 | 44 50 50 46 56 45 56 50 49 50 47
11 | 10 13 10 12 11 6 12 11 14 19 4 | 19 24 24 25 30 18 28 17 20 18 21
12 | 23 24 10 13 23 8 30 21 14 27 7 | 84 82 83 82 83 76 85 80 80 85 81
13 | 5 16 11 9 17 6 14 18 8 20 4 | 16 27 20 19 30 16 24 20 20 22 18
14 | 7 24 8 9 13 6 16 14 7 20 4 | 17 29 23 19 25 18 23 20 19 23 17
15 | 5 19 8 6 14 3 18 14 10 22 4 | 14 28 18 18 24 17 23 20 19 21 16
16 | 4 22 9 12 18 3 18 10 8 27 4 | 19 24 20 20 30 17 23 17 17 18 19
17 | 7 15 10 11 10 4 17 14 11 21 4 | 15 22 21 19 21 18 23 20 22 16 16
18E | 7 20 8 8 13 7 11 13 5 16 3 | 17 25 21 18 21 18 21 19 16 19 17
19 | 5 14 10 11 8 3 10 15 11 25 4 | 12 20 21 19 20 17 20 14 17 13 15
20E | 6 27 8 13 18 6 11 12 10 20 4 | 33 44 34 29 40 32 36 37 34 41 33
21 | 7 18 7 8 11 6 15 11 10 25 4 | 20 24 16 18 11 18 20 27 25 35 17
22E | 6 15 6 9 14 5 10 11 7 17 3 | 15 26 23 16 23 18 23 15 19 17 18
23 | 7 21 10 11 13 7 14 16 7 19 4 | 16 30 20 21 26 17 23 20 20 17 19
X24 | 4 --- --- --- --- 28 --- --- --- --- 0 | 31 --- --- --- --- 31 --- --- --- --- 29
25E | 6 18 8 9 13 5 11 12 6 11 3 | 21 26 24 19 25 22 26 23 21 20 20
26 | 6 13 6 5 11 3 11 15 7 18 3 | 21 20 19 19 25 17 21 18 18 16 19
27 | 5 16 6 8 12 5 12 13 10 16 3 | 12 22 17 15 19 15 19 14 17 14 13
28 | 6 16 9 6 19 4 12 15 9 13 4 | 26 29 28 26 33 25 29 29 29 26 27
29 | 8 15 9 8 11 5 17 13 7 30 4 | 12 21 14 12 13 14 21 18 15 16 12
30E | 9 17 10 12 14 4 16 20 24 23 5 | 15 25 22 21 20 17 19 15 32 17 17
31 | 8 24 7 9 16 4 14 11 9 15 4 | 16 30 20 17 33 17 25 16 19 17 17
32E | 9 18 8 13 10 7 13 15 21 23 5 | 33 32 29 29 28 29 29 30 37 39 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 10 14 5 15 14 11 21 |T 21 27 23 22 27 21 26 22 23 24 21
WRMS | 7 18 8 10 12 5 14 12 8 24 |NE 16 23 19 18 22 17 21 18 18 20 17
MEDI | 7 17 8 10 13 5 14 13 9 20 |MD 16 25 21 19 25 17 23 19 19 19 17
Table 3.1688.2 GPS week: 1688 Day: 2 MJD: 56062.000
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 | 7 14 4 12 9 2 14 8 10 12 3 | 31 27 24 40 27 28 27 31 32 29 29
2 | 7 19 10 9 8 4 16 7 9 32 4 | 12 24 13 10 18 10 24 12 10 19 11
3 | 7 14 7 10 10 3 12 7 11 18 3 | 18 19 17 22 21 15 15 18 15 17 17
4 | 6 11 7 9 9 5 10 12 8 30 3 | 16 17 22 22 22 16 18 23 16 31 18
5E | 6 23 8 11 12 4 22 12 11 20 4 | 14 31 19 15 25 15 28 18 17 14 17
6 | 8 13 7 9 9 3 12 7 9 17 3 | 20 19 18 21 22 17 18 20 16 17 19
7 | 7 17 8 10 13 5 12 11 11 15 4 | 9 21 13 15 23 12 18 14 17 14 14
8 | 7 16 6 7 10 3 12 7 6 12 3 | 11 20 16 18 14 13 19 14 16 15 15
9 | 9 16 7 10 13 4 14 10 10 24 4 | 10 24 22 21 22 18 21 21 24 28 19
10E | 15 19 8 11 14 7 19 20 21 18 6 | 45 50 50 49 59 46 57 49 54 50 49
11 | 9 13 8 9 10 4 12 7 9 17 3 | 18 22 21 24 28 17 24 17 18 16 19
12E | 14 23 10 10 18 6 28 10 9 11 5 | 68 74 72 72 74 67 76 74 66 75 71
13 | 6 20 9 10 17 3 12 16 13 17 4 | 15 28 18 18 28 14 22 18 20 19 16
14 | 6 21 7 9 12 5 18 10 5 19 4 | 16 27 20 19 25 17 24 17 16 23 18
15 | 6 20 6 8 14 3 19 13 10 20 4 | 14 29 16 16 23 13 23 17 19 18 16
16 | 11 27 6 11 12 3 18 9 8 26 4 | 75 76 75 79 79 74 73 73 73 75 75
17 | 9 17 8 14 11 3 19 9 7 21 4 | 13 22 19 26 15 16 24 20 19 16 17
18E | 7 17 9 11 15 5 11 10 6 12 4 | 14 23 19 21 22 15 18 18 17 16 18
19 | 7 14 9 13 9 3 14 9 13 25 4 | 14 19 19 18 18 12 19 13 14 6 14
20E | 6 22 6 8 14 4 12 10 8 19 4 | 18 30 21 18 26 19 23 19 20 22 20
21 | 8 18 9 10 11 5 17 10 8 25 4 | 22 25 16 19 12 19 22 27 22 32 19
22E | 6 14 7 8 16 4 11 10 6 13 3 | 18 28 25 19 24 20 25 20 19 20 20
23 | 6 22 9 10 14 4 12 12 12 18 4 | 17 30 22 20 25 17 22 19 20 20 19
X24 | 7 --- --- --- --- 23 20 --- --- --- 12 | 31 --- --- --- --- 29 34 --- --- --- 32
25E | 7 19 6 8 14 4 12 11 7 11 3 | 29 32 25 24 27 24 28 26 28 25 25
26 | 7 11 9 8 12 4 15 15 10 14 4 | 16 16 15 17 17 14 20 22 18 19 16
27 | 6 14 8 9 11 4 15 9 7 13 3 | 10 19 15 18 17 11 17 13 15 15 14
28 | 15 17 7 10 13 5 16 14 6 13 4 | 60 66 65 68 70 67 68 68 68 68 66
29 | 9 14 8 8 12 5 18 10 8 28 4 | 15 21 20 16 17 18 23 22 19 21 18
30E | 11 19 10 11 19 6 18 16 26 25 6 | 15 25 17 18 22 13 20 15 29 15 16
31 | 7 23 8 9 16 4 16 11 12 15 4 | 12 25 16 14 31 11 22 13 17 13 15
32E | 10 18 8 11 15 4 14 15 22 21 5 | 27 25 24 29 24 26 21 27 36 35 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 8 10 13 4 16 11 11 20 |T 22 29 24 26 28 22 27 25 25 25 24
WRMS | 7 18 8 9 12 4 15 10 8 22 |NE 16 22 18 19 21 16 21 18 18 19 17
MEDI | 7 17 8 10 12 4 14 10 9 18 |MD 16 25 19 19 23 17 22 19 19 19 18
Table 3.1688.3 GPS week: 1688 Day: 3 MJD: 56063.000
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 | 6 12 8 9 12 3 13 8 8 14 3 | 32 29 31 38 35 30 28 33 32 28 31
2 | 8 19 10 9 9 4 14 6 7 33 3 | 18 27 18 14 19 16 26 17 17 18 17
3 | 6 11 4 9 9 4 9 8 9 19 3 | 15 16 16 16 21 13 18 14 15 13 15
4 | 7 13 7 7 13 4 7 10 5 30 3 | 19 22 22 20 25 17 18 21 18 32 20
5E | 6 20 7 10 10 3 23 11 8 19 4 | 16 26 18 16 27 15 25 16 17 18 17
6 | 6 11 5 10 9 3 9 8 8 18 3 | 17 18 18 17 24 16 19 18 17 16 18
7 | 6 18 9 9 12 4 11 9 9 15 3 | 13 24 16 13 24 12 20 17 15 17 15
8 | 7 16 7 7 13 4 15 8 10 11 3 | 14 22 17 15 15 13 23 14 16 11 15
9 | 7 15 6 10 12 5 13 11 9 23 3 | 18 23 19 18 20 18 23 19 20 22 19
10E | 15 20 10 12 16 5 17 14 18 16 5 | 42 52 48 47 51 44 55 45 48 48 46
11 | 6 11 12 8 12 4 11 8 13 18 4 | 20 26 22 24 31 20 26 19 20 17 21
12E | 11 22 7 9 24 5 24 9 8 13 5 | 43 50 45 44 50 45 49 44 47 44 45
13 | 7 18 8 10 18 4 12 12 13 15 4 | 14 26 16 19 28 14 21 20 22 18 17
14 | 6 20 8 10 11 5 13 9 7 18 3 | 17 27 21 20 25 17 23 18 17 19 19
15 | 7 18 6 7 16 3 19 8 9 15 4 | 15 26 17 14 23 15 23 17 20 17 16
16E | 7 20 7 11 12 7 16 9 11 17 4 | 48 52 46 46 48 44 51 46 47 47 47
17 | 8 15 11 12 10 4 17 9 8 20 4 | 20 23 20 24 21 19 23 22 22 19 19
18E | 9 18 8 9 18 4 9 8 9 12 4 | 19 28 23 20 25 20 24 21 23 19 21
19 | 5 14 9 9 12 3 11 10 12 25 3 | 15 19 19 18 23 14 20 16 16 13 17
20E | 8 19 7 9 19 3 10 8 8 18 4 | 33 39 37 32 39 34 35 38 38 41 35
21 | 5 14 7 8 11 3 14 8 10 25 3 | 24 26 23 22 15 23 25 28 26 34 23
22E | 7 13 6 7 16 5 9 8 11 12 3 | 13 24 22 14 25 15 23 13 15 16 16
23 | 8 21 8 13 13 3 14 7 12 17 4 | 12 27 17 19 21 11 21 15 17 15 15
X24 | 7 --- --- --- --- 32 12 --- --- --- 9 | 42 --- --- --- --- 51 39 --- --- --- 39
25E | 6 14 7 10 13 4 11 11 7 10 3 | 21 24 23 17 24 17 24 18 17 14 18
26 | 9 13 7 6 13 3 11 10 11 12 3 | 15 16 15 14 18 11 17 16 12 13 14
27 | 7 16 5 8 16 4 11 7 7 12 3 | 13 21 15 17 17 13 20 15 16 15 15
28E | 22 15 11 7 14 5 14 7 10 11 5 | 71 70 63 68 73 66 69 68 71 66 67
29 | 11 17 7 7 10 3 17 10 9 27 4 | 16 23 17 16 14 15 21 19 16 18 15
30E | 11 19 12 11 12 6 15 14 22 24 5 | 16 23 22 16 18 17 19 15 28 14 17
31 | 6 20 7 10 15 5 15 8 11 16 4 | 15 25 18 17 31 15 25 15 21 13 17
32E | 11 18 8 10 16 5 13 12 19 17 5 | 31 32 29 34 29 30 27 33 42 38 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 8 9 14 4 14 9 11 19 |T 23 28 24 23 27 22 27 23 24 23 23
WRMS | 7 17 8 9 13 4 13 9 9 21 |NE 18 23 18 18 22 17 22 18 18 18 18
MEDI | 7 17 7 9 13 4 13 9 9 17 |MD 17 26 20 18 24 17 23 18 20 18 18
Table 3.1688.4 GPS week: 1688 Day: 4 MJD: 56064.000
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 12 9 9 9 3 13 10 8 14 3 | 32 27 31 34 27 29 28 33 32 28 30
2 | 7 19 8 9 9 4 17 10 7 33 4 | 19 29 24 20 25 19 29 19 23 23 20
3 | 6 11 7 12 10 4 8 9 10 22 3 | 23 21 25 22 25 21 20 25 22 24 23
4 | 8 11 7 7 12 6 11 14 11 32 3 | 15 22 20 22 22 18 21 21 18 32 18
5E | 7 20 6 12 11 5 23 10 11 20 4 | 18 29 22 20 28 19 29 19 27 21 21
6 | 6 11 7 11 9 3 8 10 10 21 3 | 23 20 24 23 25 22 19 26 22 24 23
7 | 7 17 9 10 13 4 15 7 8 15 4 | 14 25 18 16 25 15 23 17 18 17 16
8 | 7 14 9 8 11 4 13 8 11 10 3 | 13 23 19 19 15 17 21 17 20 16 17
9 | 8 17 7 8 12 4 13 16 6 23 4 | 14 23 15 16 14 13 19 19 14 20 15
10E | 14 21 9 13 13 7 17 13 19 15 5 | 36 49 44 44 50 41 51 38 43 41 41
11 | 8 12 8 13 10 5 10 10 10 20 4 | 21 26 24 27 29 21 28 18 20 18 22
12E | 15 22 9 8 24 5 27 13 6 12 6 | 24 37 30 25 37 26 36 28 29 29 28
13 | 7 17 12 12 16 4 16 10 8 16 4 | 14 25 18 21 28 14 22 18 12 18 15
14 | 8 20 11 9 12 5 14 11 13 17 4 | 19 29 27 19 29 19 23 19 21 21 20
15 | 9 21 9 7 16 6 21 13 6 14 4 | 17 29 17 20 22 16 25 21 19 20 17
16E | 6 21 13 12 16 4 17 13 8 21 5 | 29 34 34 29 35 27 29 32 29 35 30
17 | 7 16 9 14 9 3 17 13 9 21 4 | 18 23 21 26 23 19 24 22 25 18 18
18E | 8 17 10 10 18 5 11 11 11 12 4 | 25 31 30 24 29 25 28 28 26 28 25
19 | 6 14 9 11 8 4 12 12 9 25 3 | 14 18 18 20 20 14 19 15 14 10 15
20E | 9 21 7 11 17 4 12 9 8 19 4 | 32 41 37 36 38 35 36 36 34 37 34
21 | 9 20 9 9 10 4 13 9 13 26 4 | 26 30 22 22 17 22 25 28 24 35 23
22E | 8 13 7 7 20 4 9 11 9 14 4 | 20 27 28 19 38 21 26 19 20 19 23
23 | 6 19 9 13 13 3 15 8 11 19 4 | 15 26 19 21 20 15 21 18 16 21 15
X24 | 5 --- --- --- --- 25 --- --- --- --- 0 | 37 --- --- --- --- 34 --- --- --- --- 37
25E | 9 20 8 24 12 3 13 14 13 12 5 | 16 25 23 27 23 17 23 19 21 15 18
26 | 10 12 7 9 10 3 12 11 9 12 3 | 16 20 15 17 19 13 19 20 19 21 16
27 | 8 19 7 8 13 5 12 13 6 12 4 | 17 26 16 19 19 15 20 18 16 17 16
28E | 8 15 9 8 14 3 12 12 10 7 4 | 28 29 29 29 30 27 28 27 34 27 29
29 | 8 16 7 8 12 4 18 12 8 28 4 | 14 22 14 19 16 14 22 19 19 17 14
30E | 11 22 9 10 28 8 16 17 23 26 6 | 20 27 17 19 34 16 18 16 28 15 19
31 | 9 22 10 9 16 3 16 9 8 15 4 | 19 29 22 19 34 17 29 16 18 14 19
32E | 8 18 9 10 11 6 14 15 20 20 5 | 34 32 30 37 31 32 29 34 40 39 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 9 11 14 4 15 12 11 19 |T 21 27 23 23 26 21 25 22 23 23 22
WRMS | 8 17 9 11 13 4 14 11 9 21 |NE 19 24 20 21 22 18 22 20 19 20 19
MEDI | 8 17 9 10 12 4 13 11 9 19 |MD 19 27 22 21 25 19 24 19 21 21 20
Table 3.1688.5 GPS week: 1688 Day: 5 MJD: 56065.000
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 13 6 9 8 4 14 11 10 17 3 | 32 29 26 32 26 30 27 32 34 25 29
2 | 8 17 10 8 8 3 17 10 9 33 4 | 16 23 20 18 23 15 26 16 20 16 18
3 | 7 12 6 11 11 4 9 8 11 24 3 | 18 17 16 16 14 15 17 18 14 20 16
4 | 10 12 10 5 11 4 10 20 11 34 4 | 15 19 20 14 20 16 20 24 22 32 18
5E | 7 21 8 11 15 4 23 12 11 20 5 | 13 31 21 19 31 16 25 18 14 16 17
6 | 5 12 5 9 11 3 9 8 10 22 3 | 20 18 17 17 17 17 20 20 15 20 18
7 | 8 20 8 9 14 4 14 7 8 16 4 | 16 26 18 15 23 13 23 18 16 15 17
8 | 6 18 7 7 12 4 11 6 10 10 3 | 14 24 17 14 14 15 24 14 17 12 17
9 | 7 15 6 8 11 4 13 19 5 22 4 | 16 24 19 18 19 17 24 26 20 25 20
10E | 16 17 8 13 16 8 16 16 14 15 5 | 46 55 54 50 58 48 59 45 49 46 50
11 | 8 13 8 13 10 5 11 9 9 20 3 | 20 28 18 22 27 20 29 15 20 16 19
12E | 12 21 8 8 13 4 26 19 9 13 5 | 20 29 24 24 29 22 33 30 25 28 24
13 | 8 16 8 11 17 4 15 9 13 15 4 | 16 27 17 18 28 15 24 17 18 17 17
14 | 5 23 8 10 12 3 14 9 13 14 4 | 15 26 20 16 25 14 22 15 15 16 16
15 | 8 21 5 6 14 5 21 14 8 12 4 | 18 29 19 18 27 18 26 21 21 20 19
16E | 5 18 7 16 19 5 15 10 6 19 4 | 24 27 23 23 28 24 25 26 24 28 23
17 | 9 16 9 14 10 3 18 11 10 20 4 | 21 22 20 23 17 18 30 23 22 18 20
18E | 7 15 8 9 14 4 11 10 7 12 3 | 23 26 26 20 25 22 26 26 22 23 23
19 | 7 15 8 10 13 4 15 11 13 25 4 | 16 19 15 12 18 13 20 15 11 7 14
20E | 11 21 9 8 15 4 11 8 8 21 4 | 32 40 39 39 37 36 35 39 36 44 35
21 | 5 15 9 7 9 2 14 8 9 25 3 | 24 21 22 20 13 22 24 25 22 32 22
22E | 7 13 7 7 14 6 10 9 12 10 3 | 17 26 24 16 29 18 27 19 16 16 20
23 | 9 20 8 11 13 3 17 10 11 19 4 | 16 29 20 18 22 16 25 20 19 20 18
X24 | 7 --- --- --- --- 12 17 --- --- --- 11 | 33 --- --- --- --- 32 26 --- --- --- 31
25E | 8 16 9 8 14 3 12 15 8 10 4 | 18 20 22 16 22 17 25 23 22 19 19
26 | 7 11 7 8 10 4 12 11 12 13 3 | 21 22 21 20 23 19 22 20 23 17 21
27 | 8 14 4 7 13 4 11 12 6 12 3 | 13 20 16 15 18 13 24 17 15 15 16
28E | 5 14 8 8 11 4 11 11 7 12 3 | 20 26 20 21 22 20 24 24 21 20 20
29 | 8 16 6 7 10 4 16 14 8 28 4 | 15 19 10 12 14 12 22 18 12 14 13
X30E | 11 24 11 --- 14 7 --- 20 27 --- 8 | 20 28 18 --- 22 16 --- 19 29 --- 17
31 | 7 21 8 7 15 5 13 12 19 15 4 | 13 26 18 14 31 14 26 13 20 10 16
32E | 11 17 8 8 11 5 15 13 21 19 5 | 30 26 23 27 24 28 25 29 38 30 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 8 9 13 4 15 12 11 19 |T 20 25 21 20 24 19 25 22 21 21 20
WRMS | 8 17 8 9 12 4 14 11 9 22 |NE 18 23 18 17 20 17 23 19 18 18 18
MEDI | 8 16 8 8 13 4 14 11 10 17 |MD 18 26 20 18 23 17 25 20 20 19 19
Table 3.1688.6 GPS week: 1688 Day: 6 MJD: 56066.000
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 | 11 11 6 12 9 3 15 10 9 15 4 | 31 32 33 36 36 31 35 35 32 29 32
2 | 7 15 7 11 10 4 17 13 9 33 4 | 24 32 24 20 28 24 34 24 27 20 24
3 | 7 13 5 12 14 3 9 8 8 23 3 | 20 21 21 24 27 19 22 20 18 18 20
4 | 10 11 10 7 10 6 9 21 8 35 4 | 18 25 25 24 27 19 24 31 24 40 23
5E | 8 19 6 10 13 5 21 13 11 20 4 | 27 34 26 23 36 23 31 21 27 22 26
6 | 6 12 5 9 13 4 8 9 9 19 3 | 21 23 22 25 29 21 25 23 22 21 22
7 | 8 17 10 8 17 4 14 10 9 20 4 | 19 29 19 20 26 18 25 21 23 22 19
8 | 5 15 7 7 12 4 11 7 8 10 3 | 17 26 17 18 17 18 22 18 23 16 18
9 | 5 16 4 11 10 4 12 18 9 21 4 | 15 25 16 15 17 14 22 17 14 22 15
10E | 14 18 9 11 17 6 17 40 15 23 7 | 54 60 59 56 64 55 65 69 59 56 58
11 | 9 11 9 15 10 3 12 8 13 20 4 | 23 32 30 30 39 25 33 22 25 19 26
12E | 11 23 9 12 19 5 29 19 11 14 6 | 34 45 38 38 42 36 45 42 39 44 37
13 | 7 19 11 11 20 6 16 9 10 17 4 | 16 30 21 24 30 17 24 21 16 22 18
14 | 7 21 6 13 12 3 17 9 15 14 4 | 20 30 22 26 30 21 25 21 20 22 20
15 | 8 20 6 11 15 4 22 14 13 11 5 | 20 28 19 16 26 18 27 17 23 17 19
16E | 6 19 7 15 16 3 13 9 11 20 4 | 32 38 33 33 36 30 36 34 27 35 30
17 | 5 16 7 12 8 5 17 12 13 22 4 | 23 25 24 28 24 22 26 29 26 23 23
18E | 6 17 7 10 12 4 12 10 9 13 3 | 31 37 32 29 29 31 34 33 30 34 30
19 | 6 14 4 12 10 3 13 12 11 25 3 | 18 23 22 23 26 17 25 19 17 14 19
20 | 8 21 9 9 14 4 12 7 8 22 4 | 23 33 26 22 29 22 27 24 25 28 25
21 | 6 13 8 8 9 4 14 8 9 25 3 | 27 27 26 28 20 25 30 28 25 37 25
22E | 6 11 5 11 14 4 9 8 9 9 3 | 23 31 30 24 33 26 29 23 22 24 25
23 | 7 19 8 13 16 5 14 9 10 20 4 | 15 27 18 23 24 15 23 20 16 21 16
X24 | 7 --- --- --- --- 20 14 --- --- --- 10 | 33 --- --- --- --- 30 28 --- --- --- 31
25E | 6 22 8 9 12 3 13 16 10 9 4 | 16 26 19 16 20 12 22 17 15 13 13
26 | 7 12 6 11 13 3 12 10 8 12 3 | 21 21 19 18 23 17 22 18 21 16 19
27 | 6 15 4 13 14 4 12 13 10 12 4 | 16 22 17 18 19 15 21 17 17 19 16
28E | 5 15 8 10 16 5 11 12 8 11 3 | 22 28 22 22 25 21 26 26 25 25 22
29 | 9 17 11 8 12 4 17 13 11 28 4 | 17 23 17 18 20 15 24 20 15 22 15
X30E | 12 21 12 12 15 7 --- 21 31 --- 7 | 20 28 26 21 24 19 --- 22 34 --- 19
31 | 7 19 6 9 16 3 15 13 13 15 4 | 19 29 22 22 35 19 30 19 21 16 21
32E | 11 20 8 11 16 7 15 15 23 16 5 | 41 39 38 41 39 39 36 41 53 43 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 7 11 14 4 15 14 11 19 |T 23 29 25 25 29 22 28 25 25 25 23
WRMS | 7 17 7 11 12 4 14 11 9 20 |NE 20 26 21 22 26 20 26 22 21 21 21
MEDI | 7 17 7 11 13 4 14 12 10 19 |MD 21 28 22 23 27 21 26 22 23 22 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 4.1688 GPS week: 1688 MJD: 56060.0-56066.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 |U 6 5 13 |U 6 8 23 |U 30 25 48 |
emr | emr 2963 | 7 7 19 |U 9 9 35 | 29 27 53 |
esa | esa 2976 | 5 5 14 |U 6 7 22 | 29 24 48 |
gfz | gfz 2949 |U 5 5 14 |U 7 8 27 |U 29 25 50 |
grg | grg 2976 |U 8 9 24 |U 8 9 30 | 32 29 53 |
igr | igr 2975 | 6 5 15 | 6 8 23 | 29 25 48 |
igs | igs 2973 | 5 5 15 | 7 6 24 | 32 25 54 |
jpl | jpl 3005 | 7 6 17 |U 8 9 29 | 30 25 52 |
mit | mit 2976 | 6 6 17 |U 28 30 126 |U 25 30 48 |
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 5.1688.0 GPS week: 1688 Day: 0 MJD: 56060.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 5 5 11 | 6 11 18 | 63 41 147 |
emr | emr 2964 | 7 5 12 | 9 8 30 | 66 42 151 |
esa | esa 2976 | 5 5 11 | 7 7 17 | 60 39 154 |
gfz | gfz 2963 | 5 5 11 | 7 8 22 | 62 51 159 |
grg | grg 2976 | 7 7 22 | 9 8 27 | 58 46 134 |
igr | igr 2976 | 5 5 12 | 7 10 19 | 60 41 147 |
igs | igs 2970 | 4 4 12 | 6 8 16 | 60 41 146 |
jpl | jpl 3058 | 6 5 17 | 9 11 27 | 67 45 160 |
mit | mit 2976 | 5 5 13 | 10 12 49 | 57 45 135 |
Table 5.1688.1 GPS week: 1688 Day: 1 MJD: 56061.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 5 4 13 | 9 8 32 | 15 14 25 |
emr | emr 2964 | 7 7 20 | 9 6 37 | 17 17 35 |
esa | esa 2976 | 5 5 15 | 8 7 26 | 13 13 25 |
gfz | gfz 2962 | 5 5 15 | 8 8 30 | 13 11 26 |
grg | grg 2976 | 8 9 30 | 9 9 39 | 13 19 29 |
igr | igr 2976 | 5 5 15 | 8 7 27 | 17 12 25 |
igs | igs 2976 | 4 4 15 | 8 5 33 | 13 13 25 |
jpl | jpl 2963 | 5 4 17 | 9 7 41 | 16 13 27 |
mit | mit 2976 | 5 4 17 | 11 13 45 | 14 13 23 |
Table 5.1688.2 GPS week: 1688 Day: 2 MJD: 56062.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 5 8 17 | 5 8 23 | 26 36 60 |
emr | emr 2962 | 6 6 21 | 6 12 29 | 26 27 62 |
esa | esa 2976 | 5 7 14 | 5 8 21 | 25 30 54 |
gfz | gfz 2962 | 5 8 17 | 10 6 39 | 28 33 59 |
grg | grg 2976 | 6 7 25 | 6 8 27 | 24 32 51 |
igr | igr 2976 | 5 7 15 | 5 7 24 | 26 32 58 |
igs | igs 2971 | 5 7 17 | 5 7 21 | 25 31 58 |
jpl | jpl 3060 | 9 11 19 | 8 9 30 | 25 24 57 |
mit | mit 2976 | 5 8 19 | 11 11 58 | 27 34 64 |
Table 5.1688.3 GPS week: 1688 Day: 3 MJD: 56063.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 6 4 13 | 6 8 22 | 45 38 17 |
emr | emr 2964 | 7 5 19 | 9 8 38 | 41 37 27 |
esa | esa 2976 | 6 4 15 | 6 7 22 | 45 35 22 |
gfz | gfz 2963 | 6 4 15 | 6 7 23 | 45 35 21 |
grg | grg 2976 | 10 8 28 | 7 9 30 | 46 39 49 |
igr | igr 2973 | 6 5 18 | 6 8 22 | 45 38 22 |
igs | igs 2974 | 6 4 16 | 6 6 26 | 44 36 25 |
jpl | jpl 3060 | 6 5 19 | 8 13 27 | 45 38 26 |
mit | mit 2976 | 6 4 18 | 9 12 28 | 25 62 19 |
Table 5.1688.4 GPS week: 1688 Day: 4 MJD: 56064.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 5 4 11 | 8 8 23 | 7 9 18 |
emr | emr 2963 | 7 6 19 | 10 9 29 | 11 16 20 |
esa | esa 2976 | 5 4 13 | 8 8 23 | 7 9 19 |
gfz | gfz 2964 | 5 3 13 | 7 10 25 | 8 8 17 |
grg | grg 2976 | 8 9 18 | 8 9 32 | 8 10 27 |
igr | igr 2976 | 6 4 14 | 8 8 23 | 7 9 18 |
igs | igs 2969 | 5 3 13 | 8 6 21 | 8 10 17 |
jpl | jpl 2964 | 6 5 15 | 9 7 34 | 9 10 19 |
mit | mit 2976 | 6 7 18 | 138 138 602 | 8 9 23 |
Table 5.1688.5 GPS week: 1688 Day: 5 MJD: 56065.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3056 | 6 5 12 | 5 5 20 | 37 31 37 |
emr | emr 2963 | 8 9 20 | 7 7 36 | 32 37 40 |
esa | esa 2976 | 6 5 14 | 5 5 20 | 40 30 35 |
gfz | gfz 2872 | 5 5 13 | 5 6 22 | 35 28 40 |
grg | grg 2976 | 9 9 26 | 8 9 26 | 50 42 53 |
igr | igr 2976 | 5 4 15 | 4 6 19 | 38 32 42 |
igs | igs 2975 | 5 5 13 | 5 6 23 | 58 33 77 |
jpl | jpl 2968 | 6 5 17 | 5 5 22 | 38 32 46 |
mit | mit 2976 | 10 9 19 | 9 12 49 | 36 32 41 |
Table 5.1688.6 GPS week: 1688 Day: 6 MJD: 56066.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 | 7 7 16 | 5 8 26 | 16 10 30 |
emr | emr 2964 | 8 9 22 | 11 14 44 | 13 13 32 |
esa | esa 2976 | 6 8 16 | 5 9 22 | 17 10 25 |
gfz | gfz 2963 | 8 8 16 | 5 9 25 | 12 9 29 |
grg | grg 2976 | 6 13 16 | 6 10 29 | 23 13 29 |
igr | igr 2975 | 7 8 16 | 5 9 25 | 13 11 26 |
igs | igs 2976 | 7 8 17 | 9 7 24 | 14 11 28 |
jpl | jpl 2968 | 8 7 20 | 6 9 25 | 12 11 31 |
mit | mit 2976 | 6 9 15 | 11 16 52 | 11 13 31 |
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 6.1688 GPS week: 1688 MJD: 56060.500-56066.500
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 -49 33 -82 4 | 0 20
| 12 21 65 89 7 | 2
emr uuuuu | 61 -10 39 202 6 | 24 33
| 30 10 80 77 6 | 2
esa uuuuu | 11 -6 -45 204 2 | 4 19
| 10 8 73 31 6 | 2
gfz uuuuu | -36 6 -8 -107 2 | 4 22
| 19 12 70 60 4 | 4
grg uuuux | 10 -10 65 -226 35 | -17 34
| 10 12 81 57 13 | 5
igr xxxxx | -19 -12 35 -53 2 | -1 19
| 9 12 74 40 3 | 3
irf xxxxx | -10 -21 7 -56 -1 | 2 20
| 8 5 25 26 2 | 3
jpl uuuuu | -14 -36 84 -6 -2 | 9 23
| 25 25 52 51 5 | 4
mit uuuuu | -47 6 -43 -233 -6 | 16 26
| 18 15 47 75 3 | 4
ngs uuuuu | 35 37 -10 64 -1 | 10 20
| 47 28 144 73 4 | 3
sio xxxxx | 188 66 -91 -149 0 | 44 48
| 14 15 33 96 6 | 3
Table 7.1688.0 GPS week: 1688 Day: 0 MJD: 56060.500
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 -43 38 -84 17 | 1 17
emr uuuuu | 107 3 -29 125 -1 | 23 31
esa uuuuu | 17 -5 43 214 7 | 6 17
gfz uuuuu | -22 0 30 -171 2 | 9 19
grg uuuux | -7 0 96 -198 26 | -25 41
igr xxxxx | -13 -14 96 -111 4 | 2 16
irf xxxxx | -4 -11 33 -81 1 | 5 17
jpl uuuuu | -10 -34 87 -68 -8 | 14 22
mit uuuuu | -19 33 -55 -288 -2 | 20 26
ngs uuuuu | -39 7 -157 128 -3 | 13 19
sio xxxxx | 194 96 -109 -168 11 | 46 49
Table 7.1688.1 GPS week: 1688 Day: 1 MJD: 56061.500
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 | -8 -55 38 -12 7 | 2 18
emr uuuuu | 73 -15 -72 235 -3 | 24 32
esa uuuuu | 26 -8 60 214 9 | 7 17
gfz uuuuu | -42 28 1 -120 -6 | 9 19
grg uuuux | 4 -26 143 -196 53 | -21 39
igr xxxxx | -4 12 152 -30 4 | 2 16
irf xxxxx | -5 -26 38 -84 0 | 6 17
jpl uuuuu | 24 -12 35 21 -5 | 13 21
mit uuuuu | -51 4 -35 -318 -2 | 20 26
ngs uuuuu | -13 15 -153 63 2 | 14 20
sio xxxxx | 179 69 -101 -335 2 | 47 50
Table 7.1688.2 GPS week: 1688 Day: 2 MJD: 56062.500
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 | 7 -23 93 -227 6 | 0 21
emr uuuuu | 44 0 58 137 8 | 23 32
esa uuuuu | 18 2 -96 228 3 | 4 20
gfz uuuuu | -10 -5 40 -49 5 | 5 24
grg uuuux | 7 -16 163 -333 22 | -15 32
igr xxxxx | -19 -9 78 -42 8 | -1 20
irf xxxxx | -9 -23 -11 -42 -2 | 3 21
jpl uuuuu | -27 -10 129 66 3 | 10 24
mit uuuuu | -48 -4 -110 -198 -10 | 18 27
ngs uuuuu | 23 28 -25 45 -8 | 12 21
sio xxxxx | 199 60 -124 -129 -4 | 45 49
Table 7.1688.3 GPS week: 1688 Day: 3 MJD: 56063.500
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 | 9 -34 54 -19 4 | 2 21
emr uuuuu | 55 -4 72 240 7 | 26 35
esa uuuuu | 11 -19 -56 230 2 | 6 20
gfz uuuuu | -26 5 84 -177 2 | 5 24
grg uuuux | 17 9 -65 -271 54 | -16 32
igr xxxxx | -15 -26 -1 -104 1 | 0 21
irf xxxxx | -19 -21 6 -39 -2 | 4 21
jpl uuuuu | -35 -47 84 -5 -8 | 10 24
mit uuuuu | -76 2 19 -97 -8 | 19 28
ngs uuuuu | 87 54 -92 35 5 | 11 21
sio xxxxx | 168 57 -43 -33 -2 | 46 50
Table 7.1688.4 GPS week: 1688 Day: 4 MJD: 56064.500
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 -82 -20 -167 2 | 0 23
emr uuuuu | 88 -13 16 280 7 | 24 34
esa uuuuu | -1 -5 -42 201 -2 | 3 22
gfz uuuuu | -70 6 -14 -141 5 | 2 25
grg uuuux | 21 -19 -4 -164 25 | -15 32
igr xxxxx | -30 -10 -39 -43 1 | -3 23
irf xxxxx | -23 -27 17 -85 -3 | 0 23
jpl uuuuu | -22 -57 125 -28 2 | 5 24
mit uuuuu | -60 -8 -18 -285 -9 | 14 28
ngs uuuuu | 77 64 -10 119 -1 | 8 21
sio xxxxx | 175 52 -57 -177 -4 | 42 48
Table 7.1688.5 GPS week: 1688 Day: 5 MJD: 56065.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 6 -36 110 -90 -4 | -4 21
emr uuuuu | 31 -24 49 291 12 | 21 31
esa uuuuu | 8 5 -85 204 4 | 0 20
gfz uuuuu | -42 -5 -88 -58 -1 | -2 22
grg uuuux | 12 -8 37 -217 31 | -16 31
igr xxxxx | -29 -14 -27 0 -1 | -7 21
irf xxxxx | -8 -20 -4 -19 0 | -4 21
jpl uuuuu | 13 -75 -6 40 -2 | 2 23
mit uuuuu | -45 -4 -5 -208 -7 | 10 23
ngs uuuuu | 41 77 196 -74 -1 | 4 17
sio xxxxx | 192 57 -76 -119 -4 | 38 43
Table 7.1688.6 GPS week: 1688 Day: 6 MJD: 56066.500
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 -69 -80 21 -5 | 1 18
emr uuuuu | 26 -19 178 107 14 | 27 35
esa uuuuu | 0 -12 -140 139 -8 | 5 19
gfz uuuuu | -37 17 -112 -33 7 | 3 20
grg uuuux | 19 -11 83 -201 32 | -10 32
igr xxxxx | -24 -21 -16 -39 -1 | -2 18
irf xxxxx | -2 -18 -33 -45 -3 | 1 19
jpl uuuuu | -42 -16 131 -66 3 | 7 22
mit uuuuu | -31 22 -94 -236 -4 | 13 24
ngs uuuuu | 67 15 174 131 -2 | 7 18
sio xxxxx | 206 72 -129 -84 -1 | 42 46
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