[IGSREPORT-20552] Wk 1672 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Feb 9 05:56:31 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1672 (Jan 22, 2012 - Jan 28, 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:
igs1672[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1672[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1672[0-6].cls IGS GPS clock combination summary report.
igs16727.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16727.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 | MOBS MOBS
0 | EMR | 3 3
0 | ESA | KOUR TIXI
0 | GFZ | 3 6 19 26 BRFT DAV1 DGAR HOLB IRKT KIRU SYOG
0 | GRG | KOUR USN3
0 | JPL | 3 6 26
0 | MIT | 3 6 26 3 6 26
1 | COD | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
1 | COD | 21 22 23 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7 8
1 | COD | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 25 26
1 | COD | 27 28 29 30 31 32
1 | ESA | 6 26 UNSA
1 | GFZ | 5 6 19 29 BRFT CEDU COCO DGAR KOUR OHI2
1 | GRG | USN3
1 | JPL | 21 AREQ
1 | MIT | GRAZ NICO NYAL
2 | COD | REUN SOFI XMIS
2 | EMR | 3 6 3 6 26 WUHN NYAL WUHN
2 | ESA | UNSA
2 | GFZ | 3 6 17 19 29 BRFT DGAR HOLB IRKT KIRU OHI2 PDEL REUN
2 | GRG | KOUR LPGS USN3
2 | JPL | 3 6 AREQ
2 | MIT | 3 6 26 3 6 26 CHUR DAV1 HYDE CHUR GODE
3 | COD | NICO XMIS
3 | EMR | 6 21 26 6 21 26 SCH2 YELL SCH2 YELL
3 | ESA | KOUR TIXI
3 | GFZ | 5 6 17 19 26 29 BRFT DGAR HOLB KIRU OHI2 PDEL
3 | GRG | AMC2 KIT3 KOUR
3 | JPL | 6 26 AREQ YELL
3 | MIT | 3 6 26 3 6 26 MAW1 MAW1 NICO NYAL
4 | COD | MOBS MOBS XMIS
4 | EMR | 6 3 6 YELL TLSE YELL
4 | ESA | UNSA
4 | GFZ | 5 6 17 19 29 BOGT BRFT DGAR MANA OHI2 REUN STJO YELL
4 | GRG | AMC2 STJO USNO
4 | JPL | 3
4 | MIT | 3 6 3 6 MAW1 MAW1 SOFI STJO
5 | COD | MOBS HRAO MOBS SUTM XMIS
5 | EMR | 3 6 3 6 YELL YELL
5 | ESA | MATE HYDE UNSA
5 | GFZ | 5 6 17 19 26 29 BRFT KIRU MATE
5 | GRG | AMC2 TIXI
5 | JPL | 3 6 AREQ
5 | MIT | 1 3 6 1 3 6 MAW1 TIXI IRKJ MAW1 TIXI
6 | COD | WUHN OHI3 WUHN XMIS
6 | EMR | 3 3
6 | ESA | UNSA
6 | GFZ | 17 19 29 BRFT BRUS IISC KIRU
6 | GRG | USN3
6 | JPL | 3 6 AREQ
6 | MIT | 3 6 15 16 19 26 28 3 6 11 15 16 19 26 28 HRAO HYDE
6 | MIT | KHAJ MAC1 MOBS TOW2 TOW2 WUHN
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
----+--------+---------------
1 | NGS | 3
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 | -1.0 -.2 -1.1 -46 -10 7 .15
EMR | 1.6 .2 17.7 18 -9 9 .42
ESA | 7.2 4.7 -1.5 79 -175 62 .14
GFZ | -1.9 .4 -1.4 -65 27 -2 .21
GRG | 4.7 -1.6 -3.0 -30 40 -29 .17
JPL | -.2 4.4 11.0 -66 36 -33 .20
MIT | 7.5 .2 .1 -31 18 -51 .30
NGS | 5.2 2.1 -6.8 30 -35 35 .47
SIO | 6.1 1.9 11.5 4 -107 26 .18
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 1.1672.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1672.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 2.1672.[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 3.1672.[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 5.1672.0-6).
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 1672 summary. (Jan 22, 2012 - Jan 28, 2012)
Table 1.1672.a GPS week: 1672 MJD: 55948.000-55954.000
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 251| 0 0 5 57 -23 3 -.36 10 9 | -434 -97 420 475
| 0 0 2 14 9 10 .02 | 287 1026
emr 96| -1 0 15 -71 -36 -34 .26 19 19 | 180879 256 15 106
| 1 1 1 16 25 20 .03 | 306662 570
esa 130| 1 0 0 -97 175 8 .10 7 7 | 1024 -1127 13 128
| 0 0 1 15 21 6 .01 | 1216 1444
gfz 191| -1 -1 -9 108 -116 -9 .47 13 12 | 97 -231 33 110
| 0 1 0 46 33 12 .04 | 280 797
grg 123| 1 0 -6 26 -122 2 .53 16 15 | -10 -14 52 244
| 1 0 2 15 16 17 .05 | 292 605
igr n/a| 0 0 -1 -26 -47 1 -.10 5 5 | -5084 -363 20 84
| 0 0 0 21 22 14 .02 | 1952 676
jpl 174| 0 -1 2 92 -139 -3 .36 14 14 | 2500 142 17 81
| 0 1 1 20 11 72 .04 | 969 620
mit 262| 0 0 -3 54 -89 -7 -.38 11 10 | -71 -33 21 169
| 0 0 1 36 32 15 .01 | 290 726
ngs 220| 0 0 -3 -82 13 -4 -.26 13 8 | -114084 790592 2016 3737
| 0 1 0 29 33 15 .06 | 300529 2091652
sio 246| 0 0 4 -10 166 23 -.23 18 17 | --- --- --- ---
| 1 0 1 34 24 14 .01 | --- ---
Table 1.1672.b GPS week : 1672 MJD: 55948.000-55954.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 5 5 4 4 4 4 4 |
2 | 5 5 5 4 5 4 4 |
3 | 8 12 8 9 8 8 8 |
4 | 4 3 3 3 3 3 3 |
5 | 5 5 4 5 5 6 4 |
6 | 6 7 7 6 6 6 6 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 4 3 3 4 4 |
9 | 4 4 4 3 4 4 4 |
10 | 4 3 3 3 3 3 4 |
11 | 4 5 4 4 4 4 4 |
12 | 5 5 5 4 4 4 4 |
13 | 5 4 4 5 4 4 5 |
14 | 4 4 3 4 4 4 4 |
15 | 5 4 4 4 4 4 4 |
16 | 5 5 5 4 4 4 5 |
17 | 4 4 5 4 4 4 4 |
18 | 5 5 5 4 5 5 5 |
19 | 5 5 4 5 4 4 4 |
20 | 5 5 4 4 4 4 4 |
21 | 4 6 4 4 5 5 5 |
22 | 5 4 4 4 4 4 4 |
23 | 6 5 5 5 5 4 5 |
25 | 4 4 4 4 4 4 3 |
26 | 5 5 6 6 6 5 4 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 4 5 5 4 |
30 | 5 4 4 4 3 4 4 |
31 | 5 4 4 4 4 4 4 |
32 | 4 4 4 4 4 4 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1672.0 GPS week: 1672 Day: 0 MJD: 55948.000
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 251| 0 1 10 66 -33 11 -.35 11 10 | -538 -540 21 74
| 20 -6 |
emr 96| -2 2 13 -89 -8 -72 .27 20 20 | 629920 -107 21 100
| 22 -97 |
esa 130| 0 1 -2 -115 139 6 .12 7 7 | 304 -1404 15 126
| 54 24 |
gfz 191| 0 -3 -8 200 -73 -16 .51 16 15 | 630 -1861 39 101
| -49 67 |
grg 123| 1 0 -8 4 -92 4 .52 20 19 | 112 -718 70 269
| 50 -26 |
igr n/a| 0 0 0 -55 -84 -19 -.08 6 6 | -3415 -241 19 69
| 18 41 |
jpl 174| 0 -3 2 57 -153 -34 .41 15 15 | 3638 -174 19 65
| 13 2 |
mit 262| 0 0 -1 125 -65 2 -.39 11 11 | 7 -715 25 167
| -29 7 |
ngs 220| 0 1 -3 -120 -35 13 -.20 11 9 | -508 -639 2141 3935
| 28 66 |
sio 246| 0 -1 6 45 184 32 -.23 19 16 | --- --- --- ---
| -10 -103 |
Table 2.1672.1 GPS week: 1672 Day: 1 MJD: 55949.000
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 251| 1 0 5 67 -7 5 -.34 10 9 | -228 -593 2836 2848
| -19 -76 |
emr 96| -3 0 13 -56 -6 -41 .31 20 20 | 629655 -442 19 125
| 0 -46 |
esa 130| 0 0 1 -87 158 9 .11 7 6 | 1687 -1506 11 114
| 0 9 |
gfz 191| 0 -1 -9 115 -154 -13 .52 15 15 | -213 521 35 116
| -32 1 |
grg 123| 2 1 -6 51 -115 4 .53 16 15 | 358 -65 50 255
| -1 -46 |
igr n/a| 0 0 -1 -13 -50 2 -.08 5 4 | -3102 -615 25 102
| -42 42 |
jpl 174| 0 -1 1 119 -119 -35 .35 14 13 | 3609 -505 19 99
| -74 71 |
mit 262| 0 0 -5 32 -155 5 -.37 10 9 | 355 431 24 172
| 3 45 |
ngs 220| 0 0 -4 -109 73 3 -.23 12 10 | -795620 5534014 1918 3749
| 24 -37 |
sio 246| -1 0 4 -41 115 41 -.24 17 14 | --- --- --- ---
| 14 -67 |
Table 2.1672.2 GPS week: 1672 Day: 2 MJD: 55950.000
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 251| 0 1 6 49 -31 -4 -.35 11 9 | -121 -631 13 74
| 9 -14 |
emr 96| 0 0 13 -58 -15 -43 .28 19 19 | 1462 103 16 116
| 5 -54 |
esa 130| 1 1 0 -78 178 17 .09 7 6 | 565 -711 14 137
| 4 5 |
gfz 191| 0 -3 -9 84 -136 -20 .45 12 11 | 72 202 34 127
| -45 31 |
grg 123| 0 0 -1 14 -136 -25 .46 17 14 | 58 109 49 264
| 18 -44 |
igr n/a| 0 0 -2 -24 -57 4 -.11 5 4 | -4136 0 22 86
| 18 27 |
jpl 174| 0 0 0 82 -149 44 .38 15 15 | 2342 264 18 87
| 33 34 |
mit 262| -1 0 -3 49 -86 -6 -.37 10 9 | 7 48 18 182
| 14 43 |
ngs 220| 1 0 -4 -70 17 -23 -.24 13 8 | -184 -555 2006 3787
| 19 22 |
sio 246| -1 -1 5 -11 168 30 -.21 17 14 | --- --- --- ---
| 13 -75 |
Table 2.1672.3 GPS week: 1672 Day: 3 MJD: 55951.000
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 251| 0 1 6 54 -21 4 -.38 9 8 | -250 -699 18 80
| 18 -15 |
emr 96| -2 -3 15 -69 -55 -13 .24 20 20 | 1337 -237 17 111
| -22 -2 |
esa 130| 0 0 0 -95 205 16 .10 7 7 | 3337 -3385 14 139
| -16 -8 |
gfz 191| -1 -2 -10 127 -147 10 .44 12 14 | 201 -619 32 108
| -41 12 |
grg 123| 2 1 -3 24 -119 9 .48 14 12 | 280 -812 52 215
| 19 -31 |
igr n/a| 0 0 -2 -30 -20 25 -.11 4 4 | -4191 -1715 20 90
| -25 11 |
jpl 174| -1 -1 3 92 -129 -57 .35 15 14 | 2649 -651 19 78
| -35 6 |
mit 262| 0 0 -2 39 -87 0 -.37 11 9 | 172 -899 18 152
| 16 40 |
ngs 220| 1 0 -4 -91 30 -15 -.21 13 8 | -197 -805 2163 4033
| 50 -3 |
sio 246| -1 -1 4 -21 162 27 -.21 17 16 | --- --- --- ---
| 10 -78 |
Table 2.1672.4 GPS week: 1672 Day: 4 MJD: 55952.000
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 251| 0 0 6 65 -15 11 -.38 10 9 | -815 166 18 82
| -17 -48 |
emr 96| -1 1 14 -51 -54 -19 .23 18 18 | 1627 719 13 104
| -19 2 |
esa 130| 1 0 0 -81 169 3 .10 6 6 | 1337 -1174 16 147
| 25 -15 |
gfz 191| 0 0 -8 60 -118 1 .44 12 11 | -94 167 32 104
| -10 -12 |
grg 123| 0 0 -7 26 -129 16 .51 16 15 | -338 661 45 225
| 7 -20 |
igr n/a| 0 0 0 -1 -43 4 -.12 5 5 | -5420 -408 19 89
| -19 23 |
jpl 174| 0 -2 4 106 -142 -55 .32 14 13 | 2715 361 19 82
| 3 -32 |
mit 262| -1 0 -3 22 -97 -2 -.39 11 9 | -457 709 19 176
| -5 33 |
ngs 220| 0 0 -2 -44 7 12 -.26 13 9 | -693 14 2002 3566
| -27 74 |
sio 246| 0 0 3 -44 162 21 -.23 17 17 | --- --- --- ---
| 18 -72 |
Table 2.1672.5 GPS week: 1672 Day: 5 MJD: 55953.000
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 251| 0 0 3 29 -20 12 -.35 8 8 | -278 -519 21 88
| 30 -31 |
emr 96| 0 0 17 -93 -70 -20 .25 19 19 | 1332 1068 11 94
| 24 25 |
esa 130| 2 0 1 -105 181 0 .09 7 7 | -160 1521 13 118
| 57 7 |
gfz 191| -2 0 -8 84 -110 -3 .43 12 10 | 180 -15 30 111
| 15 20 |
grg 123| 2 0 -6 25 -127 22 .60 15 14 | -142 757 51 235
| 8 -8 |
igr n/a| 0 0 0 -54 -21 4 -.10 4 4 | -6942 353 18 85
| 16 35 |
jpl 174| 0 0 1 81 -140 -28 .32 14 13 | 1372 1066 15 84
| 0 18 |
mit 262| 0 0 -3 81 -53 -11 -.38 11 10 | -358 851 22 164
| -25 5 |
ngs 220| 0 0 -4 -91 8 0 -.30 13 8 | -490 -206 1798 3281
| 17 -52 |
sio 246| 0 0 3 26 180 6 -.24 17 16 | --- --- --- ---
| -1 -64 |
Table 2.1672.6 GPS week: 1672 Day: 6 MJD: 55954.000
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 251| -1 0 1 68 -33 -15 -.37 8 8 | -808 2137 19 80
| 2 -11 |
emr 96| 0 0 17 -79 -46 -27 .27 19 19 | 821 693 12 94
| 67 -15 |
esa 130| 1 1 2 -117 193 3 .12 7 7 | 99 -1230 13 118
| 25 -6 |
gfz 191| -1 0 -8 84 -71 -22 .49 11 10 | -92 -14 29 103
| -59 -3 |
grg 123| 1 0 -8 36 -139 -14 .59 16 15 | -398 -33 50 251
| -1 -9 |
igr n/a| 0 0 -1 -6 -53 -13 -.10 5 4 | -8385 79 17 70
| 10 6 |
jpl 174| 0 0 6 110 -141 140 .38 14 14 | 1179 636 16 77
| 5 48 |
mit 262| 0 -2 -4 32 -78 -41 -.40 12 10 | -225 -661 21 171
| 5 10 |
ngs 220| 0 -1 -3 -47 -8 -23 -.36 12 8 | -897 2325 2088 3808
| 25 44 |
sio 246| 1 -1 1 -27 191 1 -.23 19 24 | --- --- --- ---
| 15 -81 |
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 3.1672.0 GPS week: 1672 Day: 0 MJD: 55948.000
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 | 18 18 4 16 10 6 13 9 13 23 4 | 39 40 37 41 42 36 41 44 39 38 37
2 | 10 23 5 20 10 5 17 10 10 27 4 | 23 35 23 33 23 22 32 23 24 27 22
3E | 17 24 8 19 54 6 17 15 22 31 7 | 31 33 23 22 58 29 26 26 46 29 25
4 | 9 12 4 17 15 6 10 9 8 13 3 | 25 31 29 34 34 30 31 32 27 28 27
5 | 11 17 5 16 11 8 19 10 10 24 4 | 22 31 24 28 28 25 32 25 25 27 23
6E | 22 21 8 19 26 12 17 13 18 25 6 | 112 127 116 121 130 114 125 120 118 120 119
7 | 6 22 6 12 19 7 13 14 10 18 4 | 35 45 36 37 46 37 44 32 35 32 34
8 | 9 15 5 12 14 8 12 14 12 16 4 | 19 26 21 27 23 21 25 15 22 17 18
9 | 11 17 9 12 13 3 10 11 7 11 3 | 16 25 23 23 24 19 23 20 21 16 17
10 | 12 15 5 17 11 5 11 9 7 17 3 | 26 29 32 38 34 32 34 33 31 29 29
11 | 9 21 5 16 16 6 13 10 9 14 4 | 19 31 23 26 34 21 30 30 25 23 22
12 | 10 23 7 14 22 4 17 12 9 16 4 | 20 34 20 25 33 22 31 19 22 17 19
13E | 9 15 7 15 30 6 11 9 11 11 4 | 19 27 18 20 29 18 24 20 20 20 17
14E | 10 15 8 17 14 4 8 6 8 16 3 | 19 28 25 22 25 21 24 23 20 28 22
15 | 12 23 7 17 16 4 14 11 10 13 4 | 15 29 17 24 19 17 24 19 20 22 15
16 | 10 29 6 12 21 4 18 17 10 18 5 | 17 36 16 16 27 17 28 15 16 12 15
17E | 8 18 7 18 16 6 18 11 11 10 4 | 20 33 23 30 31 21 30 17 21 20 21
18 | 12 21 6 20 14 3 13 10 9 30 5 | 24 32 26 39 29 28 32 28 27 26 25
19E | 8 22 7 18 18 7 14 13 10 13 4 | 24 37 21 20 26 24 27 24 25 24 22
20 | 8 17 7 15 14 7 14 13 7 30 4 | 17 23 19 22 26 18 26 26 21 21 19
21 | 7 20 7 13 14 6 16 7 9 27 4 | 25 33 26 27 24 27 31 27 24 37 24
22 | 10 18 7 22 16 5 12 13 7 18 4 | 24 31 29 37 39 27 33 30 28 30 28
23E | 9 25 13 17 16 6 15 21 13 20 5 | 38 47 47 49 45 41 47 30 41 31 39
25 | 11 15 6 17 20 6 14 10 12 10 4 | 16 26 21 22 30 21 30 17 23 18 18
26E | 13 17 10 15 14 6 21 13 14 22 5 | 61 64 60 63 64 63 64 66 64 65 61
X27 | 11 20 7 11 14 4 11 7 9 --- 4 | 16 29 22 24 23 20 24 21 24 --- 19
28 | 7 18 6 15 21 6 13 7 7 12 3 | 18 32 21 21 33 20 28 18 21 14 18
29E | 11 28 10 19 18 5 22 10 9 11 5 | 49 53 52 54 52 50 53 47 49 51 48
30 | 9 17 7 15 16 5 12 11 14 21 4 | 14 26 19 18 25 18 22 18 19 25 17
31 | 10 17 11 15 24 6 14 9 11 15 4 | 14 29 21 24 36 19 26 15 20 17 18
32 | 7 21 6 15 16 6 11 10 8 13 3 | 16 18 18 23 27 17 20 24 18 18 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 20 7 16 20 6 15 11 11 19 |T 26 36 29 32 36 28 34 29 30 29 27
WRMS | 10 20 7 15 19 6 15 11 9 16 |NE 20 30 23 26 29 22 29 23 23 22 21
MEDI | 10 18 7 16 16 6 14 10 10 16 |MD 20 31 23 26 30 22 30 24 24 25 22
Table 3.1672.1 GPS week: 1672 Day: 1 MJD: 55949.000
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 | 17 13 6 18 11 4 17 10 12 16 4 | 33 26 29 30 29 28 29 34 29 24 28
2 | 7 22 6 16 13 4 15 10 13 27 4 | 15 27 19 28 19 16 22 18 17 20 16
X3E | 15 22 --- --- --- 18 --- 16 152 --- 12 | 23 23 --- --- --- 29 --- 25 124 --- 23
4 | 8 11 4 12 12 3 8 7 12 11 3 | 17 23 22 29 26 20 23 20 23 19 21
5 | 9 14 6 23 16 7 14 9 11 21 4 | 15 21 18 28 23 18 23 19 20 17 17
6E | 23 23 15 19 21 9 19 18 27 28 7 | 87 97 100 104 108 97 102 101 96 103 97
7 | 6 25 5 10 17 4 12 8 9 13 3 | 16 31 20 21 28 16 21 18 20 17 19
8 | 10 14 7 11 15 5 11 10 10 12 3 | 19 22 21 26 19 18 24 15 19 13 18
9 | 8 16 6 15 9 4 11 10 9 7 3 | 13 20 14 21 20 12 17 17 16 14 13
10 | 8 12 5 11 11 5 7 9 6 15 3 | 21 24 26 27 27 24 26 21 23 22 24
11 | 11 20 4 15 17 6 12 8 20 13 4 | 21 28 20 22 31 22 25 26 29 20 22
12 | 13 23 6 14 19 6 17 10 11 15 4 | 16 31 20 29 26 18 26 18 21 20 18
13E | 7 14 7 15 11 2 11 9 8 10 3 | 13 20 17 18 19 13 19 18 18 16 14
14E | 8 18 5 15 14 3 10 9 10 13 3 | 17 25 22 22 22 17 19 23 20 23 19
15 | 8 23 6 16 16 3 19 8 11 12 4 | 12 27 14 22 19 14 23 17 18 19 13
16 | 7 24 10 12 18 5 16 11 11 17 4 | 15 28 16 22 24 16 26 18 16 16 15
17E | 7 18 7 15 13 4 20 9 11 10 4 | 22 32 25 32 33 24 30 24 24 27 25
18M | 11 18 6 19 18 4 13 13 9 22 4 | 29 34 31 39 30 30 34 38 30 30 31
19E | 10 24 7 16 20 4 12 15 16 15 5 | 12 28 19 21 20 14 19 21 18 22 16
20 | 9 16 6 26 8 5 12 7 14 27 4 | 14 21 18 26 15 16 21 19 18 17 17
21M | 8 23 6 16 19 5 24 11 11 30 5 | 20 27 24 23 27 22 24 20 27 26 20
22M | 7 18 4 17 15 4 13 6 10 19 3 | 17 28 24 27 29 21 28 20 23 19 21
23 | 8 24 7 16 21 4 15 12 8 12 4 | 19 27 20 26 28 16 24 21 18 15 18
25 | 10 16 6 16 21 5 13 9 10 9 4 | 12 22 24 24 27 16 24 16 20 17 17
26E | 15 16 9 14 19 7 17 10 17 22 5 | 64 66 65 60 62 67 64 69 69 56 64
27 | 9 20 5 13 14 3 12 8 13 11 3 | 15 26 18 23 21 17 22 19 21 16 16
28 | 8 24 6 10 17 4 11 7 11 12 3 | 18 34 21 26 30 18 23 18 20 13 18
29E | 9 27 6 14 26 4 18 10 9 17 5 | 65 67 69 67 61 68 67 67 63 70 66
X30 | 9 15 8 15 15 6 12 11 8 --- 4 | 10 23 17 20 19 13 20 16 18 --- 13
31 | 8 20 6 13 20 5 14 9 11 16 4 | 13 27 17 22 33 16 23 16 19 21 17
32 | 8 16 5 14 13 4 14 9 13 13 3 | 11 14 12 14 15 11 14 16 14 12 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 7 15 16 5 14 10 12 17 |T 22 30 26 29 29 24 28 26 29 24 24
WRMS | 9 20 6 15 15 4 13 9 10 14 |NE 16 25 19 24 23 17 22 19 20 17 17
MEDI | 8 18 6 15 16 4 13 9 11 15 |MD 17 27 20 26 26 18 23 19 20 19 18
Table 3.1672.2 GPS week: 1672 Day: 2 MJD: 55950.000
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 11 6 11 15 4 13 8 9 13 3 | 29 29 31 35 33 31 35 35 30 28 30
2 | 10 23 7 12 11 3 17 10 11 25 4 | 19 29 18 23 21 17 27 21 20 22 17
3E | 18 23 9 17 28 10 20 12 41 31 7 | 34 34 33 35 31 28 32 30 61 33 27
4 | 9 9 4 10 11 4 8 6 7 10 2 | 18 19 19 27 25 22 25 23 23 18 20
5 | 9 15 7 8 14 6 19 11 10 17 4 | 14 22 17 26 23 17 29 16 17 18 15
6E | 27 18 13 18 16 8 21 13 28 22 7 | 93 105 103 110 109 100 111 106 101 111 103
7 | 7 19 5 9 20 3 12 9 7 12 3 | 15 25 19 22 34 16 23 16 15 15 16
8 | 9 18 6 14 11 6 9 8 10 10 3 | 15 23 18 30 26 17 23 16 18 14 16
9 | 8 14 5 10 13 5 14 12 8 13 3 | 13 23 16 22 21 15 20 22 17 20 15
10 | 9 9 5 9 10 4 10 8 6 14 3 | 20 21 22 31 25 23 29 26 20 22 22
11 | 8 17 6 10 18 5 12 7 8 8 3 | 16 25 18 20 28 17 25 23 17 18 17
12 | 13 26 6 12 23 3 21 10 11 16 5 | 17 31 17 24 25 16 28 16 17 16 14
13E | 7 16 6 11 14 5 12 8 11 10 3 | 27 32 27 27 36 23 30 29 27 28 26
14E | 11 13 5 11 11 3 7 8 10 11 3 | 25 31 30 30 30 26 29 30 31 28 27
15 | 8 24 6 11 15 4 19 8 8 13 4 | 11 26 12 22 20 11 23 15 12 16 10
16 | 9 27 10 8 19 5 16 10 10 18 4 | 13 31 22 18 26 13 26 16 15 15 15
17E | 7 23 8 12 27 4 22 13 11 14 5 | 21 30 25 26 34 20 27 17 20 18 19
18 | 11 18 6 19 14 3 12 9 9 21 4 | 20 29 23 41 25 22 28 24 21 23 22
19E | 8 20 7 12 14 5 11 14 11 13 4 | 20 25 17 20 22 17 21 22 23 22 17
20 | 8 14 5 16 8 4 11 7 8 24 3 | 17 23 19 24 21 19 26 23 19 23 18
21 | 8 17 5 11 12 5 16 8 11 27 4 | 19 27 20 26 24 18 28 19 18 25 17
22 | 9 16 5 12 13 4 10 10 13 14 3 | 22 27 26 32 32 23 29 22 28 23 23
23 | 7 23 7 13 17 4 16 17 11 12 4 | 16 28 20 21 24 16 24 14 18 13 14
25 | 9 14 6 13 23 3 15 7 11 11 4 | 12 19 15 18 25 12 25 14 11 11 11
26E | 18 20 9 13 18 6 24 10 13 25 5 | 60 68 66 66 68 65 64 71 65 73 66
X27 | 10 16 4 10 15 7 14 8 11 --- 3 | 13 23 16 21 21 17 24 18 22 --- 15
28 | 6 24 6 12 20 4 15 6 11 12 4 | 19 35 20 25 33 19 29 18 17 14 18
29E | 10 23 8 11 15 5 20 11 12 11 4 | 33 39 34 44 39 36 37 30 40 35 34
30 | 9 12 6 12 18 6 13 6 9 15 3 | 12 19 19 18 27 15 22 16 19 22 15
31 | 7 17 6 11 24 4 14 10 8 17 4 | 13 21 15 22 35 13 24 11 16 17 14
32 | 7 15 6 12 9 3 14 8 6 14 3 | 13 16 15 21 18 15 22 21 15 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 7 12 17 5 15 10 13 17 |T 22 30 24 29 31 23 30 25 25 25 22
WRMS | 9 19 6 11 14 4 15 9 8 14 |NE 15 24 18 23 25 17 25 19 17 18 16
MEDI | 9 17 6 12 15 4 14 9 10 14 |MD 18 27 19 25 26 17 27 21 19 20 17
Table 3.1672.3 GPS week: 1672 Day: 3 MJD: 55951.000
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 13 7 12 11 2 15 11 10 14 3 | 28 26 27 33 33 27 32 34 28 25 27
2 | 8 22 5 13 13 4 16 11 6 24 4 | 19 29 18 22 21 16 25 19 18 20 17
3E | 16 26 13 12 20 9 23 17 45 39 8 | 26 31 21 21 24 21 27 18 48 30 18
4 | 8 10 7 11 11 3 10 5 9 11 3 | 15 17 21 32 27 22 22 22 25 18 20
5 | 9 15 7 30 8 5 16 9 8 19 5 | 18 24 21 34 24 19 28 20 20 21 19
6E | 12 30 12 16 20 9 20 11 26 17 6 | 75 92 85 91 92 81 91 87 81 91 85
7 | 5 18 5 11 18 4 13 6 8 13 3 | 13 24 18 19 29 12 22 14 15 13 15
8 | 11 13 6 7 11 3 11 7 8 11 3 | 20 30 26 27 26 22 32 22 23 19 22
9 | 8 15 7 10 9 4 9 8 8 15 3 | 17 25 20 25 21 19 21 21 22 20 18
10 | 9 13 8 10 10 3 9 7 8 13 3 | 18 20 27 34 27 23 25 25 23 24 24
11 | 10 16 5 7 17 5 12 9 13 8 3 | 21 26 27 29 32 23 28 30 28 24 24
12 | 8 22 5 10 20 4 17 8 9 14 4 | 16 29 20 26 26 19 28 19 21 20 18
13E | 9 20 7 12 13 6 12 24 11 12 5 | 26 31 25 28 32 23 27 29 29 26 24
14E | 13 19 7 9 12 4 9 11 9 24 4 | 58 67 65 62 66 61 62 63 65 63 63
15 | 6 22 5 13 17 3 17 7 10 15 4 | 8 27 11 20 19 9 20 14 14 17 9
16 | 7 25 9 11 15 4 14 7 9 15 4 | 14 29 17 20 21 15 24 14 14 14 14
17E | 8 18 7 11 12 3 18 10 9 10 4 | 18 25 19 27 26 17 27 16 18 18 18
18 | 9 16 6 15 10 3 14 8 9 21 4 | 21 30 25 39 26 23 27 24 22 25 23
19E | 8 26 7 11 19 4 11 15 17 12 4 | 12 29 14 19 21 13 19 16 17 14 11
20 | 6 15 4 10 10 4 11 8 7 22 3 | 18 22 21 25 21 18 23 22 20 21 19
21 | 6 18 6 11 10 4 15 11 9 28 4 | 18 25 19 24 24 17 23 19 20 25 17
22 | 7 16 6 9 9 3 10 10 10 16 3 | 20 30 25 32 29 23 30 26 27 25 24
23 | 8 27 7 13 16 3 16 13 9 10 4 | 21 30 23 25 28 21 26 23 25 20 21
25 | 10 15 6 10 17 4 14 9 7 11 3 | 12 22 21 24 27 16 27 20 17 17 17
26E | 12 24 10 16 17 5 25 16 14 24 5 | 108 115 112 111 109 113 112 114 111 110 110
X27 | 10 18 7 11 11 4 10 8 9 --- 3 | 15 25 20 25 21 19 24 20 22 --- 18
28 | 6 20 5 11 15 4 13 7 8 11 3 | 13 30 19 19 27 14 24 14 15 11 15
29E | 7 24 7 10 10 3 19 13 9 11 4 | 75 77 78 80 78 76 79 77 77 75 77
30 | 7 15 6 12 17 4 9 6 9 17 3 | 10 21 14 17 18 12 19 12 14 21 12
31 | 7 19 8 11 20 3 11 7 11 13 4 | 11 25 16 22 32 12 19 11 18 14 14
32 | 7 18 7 8 10 3 16 9 11 16 3 | 13 17 17 22 21 15 19 22 17 17 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 7 12 14 4 15 11 13 17 |T 25 33 28 33 33 26 32 28 29 28 26
WRMS | 8 20 7 14 12 4 14 9 8 16 |NE 15 24 20 25 24 17 24 19 19 18 17
MEDI | 8 18 7 11 13 4 14 9 9 14 |MD 18 27 21 25 26 19 26 21 22 20 18
Table 3.1672.4 GPS week: 1672 Day: 4 MJD: 55952.000
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 12 4 10 13 3 15 10 10 18 3 | 24 24 28 31 32 24 29 33 29 30 27
2 | 9 23 7 13 12 6 16 9 8 24 4 | 16 27 17 23 20 16 25 18 15 19 16
3E | 16 22 8 12 24 8 18 25 45 23 7 | 29 35 27 32 27 30 32 37 58 26 29
4 | 7 10 4 10 15 6 8 6 10 12 3 | 19 21 24 26 29 22 25 25 25 21 23
5 | 10 14 6 29 11 8 15 6 9 21 4 | 16 21 19 33 24 18 25 20 23 22 18
6E | 14 21 8 15 20 12 18 16 22 20 5 | 75 79 81 88 96 78 90 89 79 93 84
7 | 7 17 6 10 19 4 13 5 11 12 3 | 11 22 17 18 27 12 21 11 18 11 14
8 | 10 10 5 8 14 5 10 10 9 9 3 | 14 20 18 20 17 15 20 15 21 12 15
9 | 8 14 7 9 10 4 9 11 10 13 3 | 9 17 13 16 14 9 17 14 16 14 11
10 | 11 14 5 9 13 4 9 5 9 14 3 | 18 19 21 30 25 20 24 23 24 22 21
11 | 13 18 5 8 21 5 11 10 11 9 4 | 18 25 22 26 32 19 25 28 27 23 21
12 | 9 22 6 11 16 4 19 9 11 14 4 | 16 30 20 26 27 17 30 20 21 20 19
13E | 8 21 5 10 19 3 11 9 14 12 4 | 22 31 21 28 28 22 27 25 20 26 21
14 | 12 19 5 7 17 4 11 9 7 15 3 | 30 38 39 41 43 35 37 36 34 33 35
15 | 7 22 6 10 19 3 19 10 8 13 4 | 10 26 14 18 22 11 21 14 16 15 11
16 | 7 26 8 10 14 5 16 7 7 17 4 | 12 31 16 21 20 14 25 14 16 13 14
17E | 7 17 5 12 15 3 17 9 7 13 3 | 15 23 20 26 25 15 25 16 15 19 17
18 | 10 15 8 23 16 3 13 11 11 20 4 | 18 24 21 42 27 20 26 23 18 23 20
19E | 7 20 6 10 14 4 13 10 9 10 3 | 11 21 16 17 15 10 16 14 14 10 12
20 | 9 14 5 14 8 5 11 5 10 21 3 | 18 20 19 23 19 18 24 20 19 20 18
21 | 8 18 7 9 15 3 17 11 11 28 4 | 16 27 21 24 30 18 27 19 22 26 18
22 | 9 15 5 8 13 5 12 7 9 16 3 | 17 27 26 33 33 21 28 26 23 26 24
23 | 9 28 7 12 21 3 15 8 13 9 4 | 13 29 16 19 24 14 22 16 16 12 14
25 | 10 14 6 10 17 3 15 9 9 12 3 | 13 20 19 17 25 13 27 18 19 16 15
26E | 18 16 9 16 16 9 20 17 16 33 6 | 93 97 90 94 91 89 98 97 90 94 92
27 | 11 18 6 10 14 5 10 9 11 13 3 | 10 22 15 18 17 12 22 16 17 13 13
28 | 7 18 8 12 15 4 12 9 10 11 3 | 16 28 20 26 28 16 26 17 19 15 17
29E | 10 24 8 13 11 4 17 14 12 11 4 | 46 55 48 47 50 43 49 47 49 47 47
30 | 7 13 4 9 14 6 11 8 8 12 3 | 9 19 14 18 13 10 21 14 14 13 12
31 | 7 17 6 8 20 4 14 8 8 15 3 | 8 24 16 21 31 12 22 12 11 15 14
32 | 9 16 5 12 8 4 16 13 14 17 4 | 14 13 15 19 19 13 19 22 16 19 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 12 16 5 14 11 13 17 |T 21 29 24 29 30 22 29 25 25 24 23
WRMS | 9 18 6 11 15 5 13 9 9 17 |NE 14 22 18 22 23 15 23 18 19 17 16
MEDI | 9 17 6 10 15 4 14 9 10 14 |MD 16 24 20 26 27 17 25 20 19 20 18
Table 3.1672.5 GPS week: 1672 Day: 5 MJD: 55953.000
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 15 9 8 12 3 15 10 13 18 4 | 25 22 24 23 24 22 24 28 30 25 22
2 | 7 23 8 11 11 4 16 10 6 23 4 | 13 25 12 19 20 11 21 15 16 18 12
3E | 12 20 10 13 25 5 17 23 45 25 7 | 26 30 22 24 27 24 24 31 53 26 23
4 | 6 11 5 9 13 2 8 8 8 10 2 | 16 17 17 25 24 19 20 20 19 18 18
5 | 8 16 11 31 13 5 15 9 10 25 5 | 13 23 18 30 22 15 23 16 18 16 14
6E | 13 19 10 14 13 10 18 24 21 26 6 | 72 79 78 86 90 76 87 87 74 88 80
7 | 6 21 8 9 15 3 13 8 8 13 3 | 13 24 16 19 25 14 19 11 11 13 12
8 | 9 12 6 9 12 4 13 13 10 11 3 | 17 24 23 25 22 18 26 21 21 18 19
9 | 7 15 8 11 11 4 12 10 9 15 3 | 16 24 20 21 19 17 23 19 20 20 17
10 | 9 12 6 8 11 3 8 5 8 15 3 | 14 15 20 27 23 17 20 19 18 19 18
11 | 8 22 4 8 19 4 11 9 12 11 4 | 20 28 19 25 30 19 23 25 25 23 20
12 | 7 24 6 11 14 5 17 7 7 15 4 | 15 28 14 23 22 14 23 13 18 13 13
13E | 10 19 7 10 12 4 9 12 7 11 3 | 35 41 37 40 47 33 38 32 34 33 34
14 | 5 17 6 5 22 2 7 10 9 12 3 | 20 27 24 29 36 23 26 22 25 20 22
15 | 5 24 6 9 20 3 17 7 10 12 4 | 8 27 14 18 24 9 18 13 13 13 9
16 | 6 22 7 10 12 5 15 6 6 19 3 | 14 28 16 22 22 17 25 15 15 19 15
17E | 6 18 4 10 15 4 14 10 9 13 3 | 17 25 21 28 26 17 25 18 17 22 19
18 | 9 19 7 18 17 3 13 11 15 23 4 | 17 30 20 39 24 21 25 21 24 24 20
19E | 6 20 8 15 20 3 13 7 10 8 4 | 15 26 17 25 26 16 21 16 20 17 15
20 | 9 15 4 11 8 5 12 8 10 19 3 | 18 21 15 18 21 14 22 19 19 20 15
21 | 7 19 7 8 14 3 15 12 12 28 4 | 13 24 15 19 24 15 21 17 23 25 14
22 | 7 15 6 8 12 3 13 9 8 23 3 | 16 25 20 28 27 17 25 20 19 24 19
23 | 7 24 6 9 22 2 12 8 10 8 4 | 20 29 20 22 32 18 22 17 20 18 18
25 | 8 12 7 8 14 4 13 11 10 12 3 | 12 17 17 18 22 12 24 15 17 12 13
26 | 8 17 7 10 13 6 19 11 11 24 4 | 121 124 125 124 122 121 124 123 118 119 122
X27 | 9 19 4 9 13 3 14 9 11 --- 4 | 14 25 19 22 17 17 25 19 21 --- 16
28 | 6 18 6 13 14 3 12 10 8 11 3 | 13 28 19 22 29 15 23 12 18 11 15
29E | 7 24 8 9 17 4 18 13 12 12 4 | 60 64 64 64 59 62 62 64 64 65 62
30 | 8 17 7 11 13 5 15 6 6 12 3 | 9 23 16 21 17 15 21 12 15 17 14
31 | 6 19 6 10 17 5 16 10 8 13 3 | 9 26 17 22 32 17 25 11 15 14 15
32 | 10 17 5 6 9 6 13 18 13 18 4 | 15 13 14 15 20 15 16 26 17 22 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 7 12 15 4 14 11 13 17 |T 22 31 25 30 31 23 29 25 27 26 23
WRMS | 8 19 7 10 14 4 13 10 8 16 |NE 14 23 17 21 22 15 22 17 18 17 15
MEDI | 7 19 7 10 13 4 13 10 10 13 |MD 16 25 19 23 24 17 23 19 19 19 17
Table 3.1672.6 GPS week: 1672 Day: 6 MJD: 55954.000
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 6 9 15 4 13 12 9 20 4 | 32 30 32 38 40 31 34 41 34 36 33
2 | 6 21 5 10 11 5 15 6 6 24 3 | 18 30 18 24 23 17 24 18 19 22 17
3E | 13 27 8 12 16 8 17 23 40 25 7 | 32 39 28 33 33 33 31 33 62 35 31
4 | 7 12 6 12 16 4 8 8 10 11 3 | 25 23 29 38 39 28 30 32 31 27 29
5 | 6 13 6 12 12 4 15 8 8 30 4 | 19 25 23 33 32 23 28 24 23 34 23
6E | 10 22 6 15 14 12 18 18 20 26 5 | 79 88 90 96 101 85 94 94 82 98 89
7 | 6 21 6 11 16 4 13 7 7 13 3 | 14 25 18 22 25 14 21 10 13 13 13
8 | 9 15 6 10 13 5 12 13 10 12 3 | 15 21 17 25 20 16 25 20 17 15 16
9 | 8 14 11 10 12 3 9 9 9 16 3 | 11 23 17 22 16 13 22 12 16 13 12
10 | 7 9 7 9 15 4 8 7 11 18 3 | 22 21 26 38 38 26 27 29 28 27 27
11 | 8 19 9 11 20 5 10 15 10 15 4 | 23 29 26 34 36 23 29 33 25 27 25
12 | 7 22 7 12 17 6 20 9 7 16 4 | 20 30 21 23 25 19 31 17 22 18 19
13 | 9 25 9 12 27 3 13 9 12 11 4 | 27 30 24 32 39 27 34 27 27 28 26
14 | 6 15 6 7 19 4 8 13 10 18 3 | 30 33 36 43 43 33 32 32 34 27 33
15 | 6 26 6 10 19 4 18 7 12 14 4 | 10 31 10 20 23 10 21 14 14 15 10
16 | 10 25 8 13 14 4 14 11 8 20 4 | 17 33 17 23 23 18 28 19 16 20 17
17E | 9 19 7 10 15 5 17 11 8 15 4 | 17 25 25 31 26 21 27 20 20 23 21
18 | 8 17 5 22 14 4 13 10 10 30 4 | 20 29 23 48 28 23 27 26 21 35 24
19E | 7 17 10 12 13 5 11 12 10 19 4 | 12 22 18 22 18 10 17 14 13 16 12
20 | 10 17 6 13 9 5 14 10 9 19 4 | 26 28 25 28 29 26 29 26 26 27 24
21 | 6 21 7 9 13 4 17 12 9 27 4 | 18 27 20 25 27 18 24 20 21 27 18
22 | 8 16 7 9 11 7 9 9 10 32 4 | 26 31 30 36 40 26 33 32 26 36 29
23 | 8 24 9 9 23 3 13 12 10 12 4 | 20 32 21 23 28 18 28 18 23 21 19
25 | 6 12 5 10 13 4 13 8 10 11 3 | 14 17 19 18 23 16 25 14 17 16 15
26 | 9 19 8 7 12 6 18 9 13 24 4 | 105 106 109 110 112 110 106 110 111 114 109
X27 | 10 18 7 9 13 5 10 12 11 --- 4 | 12 25 18 22 19 16 23 16 20 --- 15
28 | 7 18 8 9 18 4 13 11 7 13 3 | 17 29 20 21 30 17 26 16 16 15 17
29E | 7 24 6 8 14 4 16 13 5 9 3 | 52 56 56 59 55 54 57 55 55 53 54
30 | 8 20 7 9 18 5 11 7 8 17 3 | 8 26 13 18 18 11 19 10 13 17 10
31 | 7 21 8 13 17 4 14 11 9 15 4 | 12 25 18 23 32 12 22 10 18 12 14
32 | 11 16 6 18 14 4 17 22 11 22 5 | 16 16 15 31 26 17 19 30 21 25 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 7 11 16 5 14 12 12 19 |T 24 32 27 34 34 26 32 28 28 29 26
WRMS | 8 19 7 10 15 4 14 10 8 24 |NE 17 25 20 26 27 18 25 20 20 21 18
MEDI | 8 19 7 10 14 4 13 11 10 17 |MD 19 29 21 28 28 19 27 20 21 25 19
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1672 GPS week: 1672 MJD: 55948.0-55954.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 |U 6 6 18 |U 12 14 40 |U 35 27 107 |
emr | emr 2965 | 10 12 25 |U 14 16 49 | 38 29 127 |
esa | esa 2962 | 7 7 20 |U 11 13 39 | 33 27 109 |
gfz | gfz 2950 |U 10 9 24 |U 19 18 54 |U 42 29 136 |
grg | grg 2961 | 9 11 28 |U 15 17 57 | 38 31 92 |
igr | igr 2968 | 6 7 18 | 12 13 39 | 35 27 109 |
igs | igs 2943 | 7 8 20 | 12 13 37 | 41 30 125 |
jpl | jpl 2950 |U 9 12 24 |U 13 16 50 | 41 29 100 |
mit | mit 2976 |U 7 10 24 |U 16 16 53 |U 45 44 129 |
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 5.1672.0 GPS week: 1672 Day: 0 MJD: 55948.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 20 | 14 14 34 | 11 12 11 |
emr | emr 2964 | 12 11 29 | 14 14 41 | 11 14 22 |
esa | esa 2976 | 7 9 25 | 15 12 37 | 5 11 13 |
gfz | gfz 2962 | 8 10 29 | 16 12 43 | 13 12 20 |
grg | grg 2976 | 9 12 33 | 18 11 45 | 19 10 23 |
igr | igr 2976 | 7 7 22 | 15 12 34 | 11 11 13 |
igs | igs 2949 | 7 9 25 | 15 13 36 | 10 11 12 |
jpl | jpl 2964 | 9 12 28 | 15 14 42 | 11 12 19 |
mit | mit 2976 | 8 10 31 | 17 13 48 | 22 34 19 |
Table 5.1672.1 GPS week: 1672 Day: 1 MJD: 55949.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 8 7 18 | 15 18 49 | 29 24 210 |
emr | emr 2963 | 12 15 33 | 17 15 51 | 31 19 204 |
esa | esa 2880 | 8 10 21 | 14 18 53 | 45 26 220 |
gfz | gfz 2870 | 8 11 24 | 25 17 66 | 49 25 224 |
grg | grg 2880 | 9 12 27 | 15 16 61 | 50 28 48 |
igr | igr 2944 | 8 8 20 | 15 17 47 | 42 24 218 |
igs | igs 2913 | 10 13 26 | 16 18 56 | 44 23 221 |
jpl | jpl 2872 | 11 15 30 | 16 17 66 | 52 28 38 |
mit | mit 2976 | 9 13 28 | 16 18 57 | 59 61 310 |
Table 5.1672.2 GPS week: 1672 Day: 2 MJD: 55950.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 7 15 | 17 18 46 | 60 55 154 |
emr | emr 2964 | 10 13 28 | 23 24 69 | 56 54 148 |
esa | esa 2976 | 6 7 19 | 17 18 43 | 48 54 162 |
gfz | gfz 2963 | 6 8 22 | 21 22 51 | 54 52 172 |
grg | grg 2976 | 12 24 40 | 21 30 88 | 50 59 159 |
igr | igr 2976 | 5 7 16 | 17 18 45 | 51 53 160 |
igs | igs 2939 | 5 8 18 | 17 19 43 | 58 54 151 |
jpl | jpl 2955 | 6 12 23 | 20 23 74 | 50 52 160 |
mit | mit 2976 | 7 11 32 | 24 26 95 | 74 58 137 |
Table 5.1672.3 GPS week: 1672 Day: 3 MJD: 55951.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 19 | 8 8 31 | 66 16 166 |
emr | emr 2966 | 12 14 20 | 9 12 34 | 64 20 166 |
esa | esa 2976 | 6 7 19 | 8 7 27 | 58 15 152 |
gfz | gfz 2964 | 7 7 22 | 16 20 45 | 65 13 181 |
grg | grg 2976 | 8 9 25 | 14 10 42 | 60 19 149 |
igr | igr 2976 | 6 7 20 | 8 7 32 | 61 14 159 |
igs | igs 2946 | 6 7 20 | 8 8 29 | 62 13 163 |
jpl | jpl 2966 | 9 15 24 | 8 9 26 | 60 15 174 |
mit | mit 2976 | 7 12 20 | 15 11 44 | 77 57 188 |
Table 5.1672.4 GPS week: 1672 Day: 4 MJD: 55952.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 17 | 8 13 47 | 64 66 178 |
emr | emr 2968 | 8 11 25 | 10 22 72 | 61 59 203 |
esa | esa 2976 | 7 9 19 | 7 14 43 | 60 67 186 |
gfz | gfz 2965 | 8 13 23 | 17 16 54 | 64 67 199 |
grg | grg 2975 | 8 9 31 | 12 25 83 | 68 75 199 |
igr | igr 2976 | 7 9 19 | 8 14 45 | 62 66 182 |
igs | igs 2937 | 6 9 18 | 7 9 29 | 65 70 188 |
jpl | jpl 2968 | 9 13 23 | 11 22 73 | 64 62 193 |
mit | mit 2976 | 6 12 19 | 10 17 53 | 71 79 197 |
Table 5.1672.5 GPS week: 1672 Day: 5 MJD: 55953.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 5 20 | 9 9 31 | 6 6 12 |
emr | emr 2968 | 9 7 21 | 14 10 40 | 8 7 20 |
esa | esa 2976 | 7 5 20 | 9 10 31 | 6 7 13 |
gfz | gfz 2964 | 15 6 30 | 20 16 46 | 10 8 20 |
grg | grg 2973 | 7 6 20 | 14 10 41 | 7 8 20 |
igr | igr 2975 | 7 5 16 | 9 9 30 | 5 7 12 |
igs | igs 2968 | 7 5 19 | 10 9 30 | 6 7 13 |
jpl | jpl 2961 | 8 5 17 | 10 9 35 | 6 7 18 |
mit | mit 2976 | 8 5 20 | 14 11 42 | 7 6 17 |
Table 5.1672.6 GPS week: 1672 Day: 6 MJD: 55954.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 16 | 10 16 45 | 7 8 16 |
emr | emr 2968 | 10 11 21 | 10 14 35 | ---- ---- ---- |
esa | esa 2976 | 6 5 17 | 9 14 39 | 8 9 18 |
gfz | gfz 2967 | 17 8 21 | 19 22 73 | ---- ---- ---- |
grg | grg 2976 | 8 7 21 | 11 16 40 | 15 18 43 |
igr | igr 2953 | 6 5 17 | 9 14 41 | 11 11 20 |
igs | igs 2953 | 7 6 16 | 9 14 37 | ---- ---- ---- |
jpl | jpl 2968 | 8 11 24 | 12 14 32 | ---- ---- ---- |
mit | mit 2976 | 7 7 18 | 13 14 33 | 8 12 32 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1672 GPS week: 1672 MJD: 55948.500-55954.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 31 0 15 101 0 | 7 15
| 24 14 89 105 4 | 1
emr uuuxu | 29 -5 -10 27 -12 | 25 30
| 46 27 83 231 6 | 5
esa uuuuu | 0 -15 66 -10 2 | -7 15
| 11 20 73 64 4 | 1
gfz uuuuu | -15 38 -29 -7 0 | 10 16
| 24 25 41 103 5 | 1
grg uuuux | 28 -8 1 -43 -13 | 25 44
| 17 16 49 74 23 | 4
igr xxxxx | -24 9 50 37 -3 | 1 15
| 14 17 52 56 3 | 1
irf xxxxx | 2 6 -3 2 3 | 0 12
| 5 9 35 37 6 | 1
jpl uuuuu | -19 14 -82 -122 -11 | 1 19
| 33 30 85 91 8 | 5
mit uuuuu | -24 9 -83 1 2 | 13 17
| 19 25 92 57 2 | 1
ngs uuuuu | -14 -13 53 78 5 | -2 12
| 47 25 109 108 7 | 3
sio uuuuu | 79 -2 14 118 -2 | 20 25
| 16 17 111 102 12 | 5
Table 7.1672.0 GPS week: 1672 Day: 0 MJD: 55948.500
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 | 15 -4 -160 257 -1 | 5 14
emr uuuxu | 106 -6 -19 428 -4 | 29 32
esa uuuuu | -15 -38 71 -42 1 | -8 16
gfz uuuuu | -58 65 -59 -114 0 | 9 15
grg uuuux | 35 -34 73 75 -38 | 29 44
igr xxxxx | -32 -2 150 10 3 | 0 14
irf xxxxx | 9 16 -70 74 4 | -2 12
jpl uuuuu | 7 3 91 -150 -8 | 6 18
mit uuuuu | 2 45 -271 66 1 | 11 16
ngs uuuuu | -57 -12 206 120 7 | -6 13
sio uuuuu | 112 26 -220 49 -22 | 28 32
Table 7.1672.1 GPS week: 1672 Day: 1 MJD: 55949.500
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 | 79 13 68 26 -3 | 7 15
emr uuuxu | 49 -6 -105 222 -11 | 29 33
esa uuuuu | -6 -6 124 -73 0 | -7 16
gfz uuuuu | 2 26 -52 -43 9 | 10 17
grg uuuux | 49 -5 -76 -3 -12 | 28 44
igr xxxxx | -39 36 42 52 -3 | 1 15
irf xxxxx | 3 -6 -19 -44 7 | -1 13
jpl uuuuu | -68 68 -94 15 -18 | 6 18
mit uuuuu | -42 -9 -100 -25 0 | 13 18
ngs uuuuu | 40 -30 66 264 10 | -4 14
sio uuuuu | 70 -20 40 -59 -17 | 26 31
Table 7.1672.2 GPS week: 1672 Day: 2 MJD: 55950.500
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 | 20 -2 31 175 6 | 8 15
emr uuuxu | 60 2 23 91 -10 | 29 33
esa uuuuu | 1 3 -12 46 2 | -5 14
gfz uuuuu | -25 52 -26 -162 -1 | 12 17
grg uuuux | 50 -11 8 -44 -37 | 26 43
igr xxxxx | -21 -11 74 139 1 | 2 15
irf xxxxx | 6 7 9 -5 5 | 0 13
jpl uuuuu | -28 -26 -91 -247 -11 | 5 18
mit uuuuu | -37 -7 -46 37 1 | 14 18
ngs uuuuu | -16 -12 128 145 6 | -2 12
sio uuuuu | 81 -6 68 108 -4 | 23 29
Table 7.1672.3 GPS week: 1672 Day: 3 MJD: 55951.500
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 | 13 -20 -52 -13 -1 | 7 15
emr uuuxu | 0 20 -77 -197 -22 | 27 31
esa uuuuu | 6 14 142 -3 1 | -6 14
gfz uuuuu | -14 39 -40 8 -3 | 11 17
grg uuuux | 29 -21 -34 -30 -30 | 22 43
igr xxxxx | -13 23 0 33 -6 | 2 15
irf xxxxx | -2 -2 15 0 9 | -1 12
jpl uuuuu | -8 33 -161 -200 -17 | 2 18
mit uuuuu | -42 -18 -26 38 2 | 14 18
ngs uuuuu | 1 -52 -39 53 10 | -1 12
sio uuuuu | 76 -12 54 134 3 | 19 24
Table 7.1672.4 GPS week: 1672 Day: 4 MJD: 55952.500
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 | 46 20 75 160 2 | 6 15
emr uuuxu | -4 22 -37 -114 -16 | 23 29
esa uuuuu | 13 -22 35 17 -3 | -7 16
gfz uuuuu | 10 13 -4 82 -7 | 9 17
grg uuuux | 18 -4 -16 -117 1 | 20 43
igr xxxxx | -25 22 -1 47 -3 | 0 16
irf xxxxx | -2 3 43 7 8 | -1 12
jpl uuuuu | 30 0 -164 -130 -11 | -2 21
mit uuuuu | -35 8 20 15 0 | 12 17
ngs uuuuu | -76 30 -16 -52 10 | -1 12
sio uuuuu | 70 -15 123 147 6 | 16 21
Table 7.1672.5 GPS week: 1672 Day: 5 MJD: 55953.500
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 | 28 -13 78 119 -1 | 6 15
emr uuuxu | -28 -7 -8 -167 -11 | 21 28
esa uuuuu | -10 -40 -35 79 6 | -7 16
gfz uuuuu | -23 2 48 78 2 | 9 16
grg uuuux | 5 9 28 -152 24 | 21 44
igr xxxxx | -38 1 48 23 -6 | 0 16
irf xxxxx | -3 17 12 -25 -2 | 1 12
jpl uuuuu | -21 17 -70 -111 -16 | -3 21
mit uuuuu | -8 42 -70 -104 2 | 13 18
ngs uuuuu | 49 0 129 -21 -1 | 1 12
sio uuuuu | 61 18 46 192 7 | 16 20
Table 7.1672.6 GPS week: 1672 Day: 6 MJD: 55954.500
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 | 15 7 65 -17 -6 | 6 14
emr uuuxu | 19 -58 151 -76 -8 | 17 25
esa uuuuu | 10 -16 140 -97 8 | -7 16
gfz uuuuu | 7 68 -72 100 -2 | 8 16
grg uuuux | 13 10 27 -30 -1 | 26 46
igr xxxxx | -2 -1 34 -48 -6 | -2 16
irf xxxxx | 4 9 -10 9 -8 | 2 11
jpl uuuuu | -44 4 -85 -31 6 | -7 20
mit uuuuu | -6 4 -87 -22 7 | 12 17
ngs uuuuu | -40 -16 -100 34 -10 | 2 12
sio uuuuu | 85 -6 -14 257 9 | 15 19
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