[IGSREPORT-19611] Wk 1627 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Mar 31 05:00:08 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1627 (Mar 13, 2011 - Mar 19, 2011)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1627[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1627[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1627[0-6].cls IGS GPS clock combination summary report.
igs16277.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16277.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 they either 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 | USNO IISC NRC1 USNO
0 | EMR | 9 9 WTZR WTZR
0 | ESA | ALIC
0 | GFZ | 9 11 20 FAA1 HARB MDVJ OUS2 RAMO
0 | GRG | ADIS ALIC
0 | JPL | 25 27 FAA1
0 | MIT | HRAO HARB HRAO
1 | COD | MDVJ PIE1
1 | EMR | MATE WTZR WTZR
1 | ESA | MDVJ
1 | GFZ | 6 11 30 ALIC ALRT STJO
1 | GRG | ZECK
1 | JPL | 25
1 | MIT | 23 23 ALRT DAV1 ALRT DAV1 KOUC MAW1 MDVJ SFER
2 | EMR | WTZR WTZR
2 | ESA | 27 27 MATE UNSA
2 | GFZ | 11 DAV1 MDVJ WES2
2 | GRG | AMC2 MATE ZECK
2 | JPL | 25
2 | MIT | 9 9 MDVJ
3 | COD | 4
3 | EMR | 4 4 WTZR WTZR
3 | ESA | UNSA
3 | GFZ | 4 11 MATE MDVJ
3 | GRG | AMC2 QAQ1
3 | JPL | 4 9
3 | MIT | 25 25 BAKO
4 | EMR | WTZR WTZR
4 | ESA | UNSA
4 | GFZ | 11 24 ALIC COCO MDVJ SALU
4 | GRG | AMC2 SANT
4 | MIT | 19 27 19 27 HARB MAW1 HARB MAW1
5 | ALL | 1 1
5 | COD | WROC RAMO WROC
5 | EMR | 4 4 WTZR WTZR
5 | ESA | UNSA
5 | GFZ | 11 BRMU HARB MDVJ
5 | GRG | ADIS AMC2 SANT
5 | JPL | 4 25 IISC
5 | MIT | 4 9 27 4 9 27 BRMU OUS2
6 | COD | 26 26 RAMO
6 | EMR | 4 4 WTZR WTZR
6 | ESA | ALIC
6 | GFZ | MDVJ SCUB
6 | GRG | AMC2
6 | JPL | 4 21 25
6 | MIT | 4 9 11 4 9 11 CAS1
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | COD | 25
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G25 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) 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.
8. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | -.7 .8 .8 -13 10 -18 .20
EMR | -2.6 5.0 8.0 27 -9 39 .41
ESA | 3.0 6.4 -8.9 125 -56 21 .18
GFZ | -4.7 -5.3 .1 49 -25 356 .48
GRG | -2.4 3.8 4.8 41 32 -78 .41
JPL | 1.1 4.8 5.8 52 -38 52 .14
MIT | 5.0 -3.4 -3.7 -3 -25 -35 .34
NGS | -.4 -2.5 -1.3 -33 -2 18 .28
SIO | 2.8 6.3 .4 124 -81 17 .58
9. 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.
10. 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.
11. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna
model is introduced (IGSMAIL #5272). The antenna phase center offsets and
phase center variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
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 1.1627.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1627.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 2.1627.[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 3.1627.[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 5.1627.0-6).
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 1627 summary. (Mar 13, 2011 - Mar 19, 2011)
Table 1.1627.a GPS week: 1627 MJD: 55633.000-55639.000
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 240| 0 0 3 74 -45 2 -.21 10 9 | -284 -570 17 72
| 0 0 1 15 18 17 .03 | 362 588
emr 94| 0 1 4 12 16 27 .44 21 21 | -1439 -374 18 90
| 0 3 1 30 39 19 .03 | 738 1191
esa 137| 1 1 -1 -137 -33 2 .23 9 9 | -357 408 14 131
| 0 1 1 20 20 14 .02 | 1016 1453
gfz 196| 0 -3 -2 -36 34 0 -.20 11 12 | 307 -265 24 99
| 1 1 1 60 31 11 .02 | 255 442
grg 131| 0 1 0 -25 -71 -16 .63 16 15 | 27 -45 47 211
| 1 0 1 42 22 9 .03 | 227 366
igr n/a| 0 0 0 63 -19 -10 -.04 5 5 | -1965 -851 18 62
| 0 0 1 11 25 33 .02 | 1469 1129
jpl 137| 1 1 4 -55 78 48 .51 22 22 | 2192 -461 20 92
| 1 0 1 23 10 49 .03 | 865 1200
mit 258| 1 -1 -6 92 46 -1 -.33 13 12 | -252 350 23 153
| 1 1 0 35 16 7 .03 | 135 225
ngs 213| -1 0 -1 138 -46 -28 -.21 10 8 | -294 -576 2258 3998
| 1 0 0 29 25 10 .03 | 350 590
sio 257| 1 2 8 -182 160 15 -.12 20 20 | --- --- --- ---
| 1 0 1 32 15 12 .02 | --- ---
Table 1.1627.b GPS week : 1627 MJD: 55633.000-55639.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 0 0 0 0 0 20 0 |
2 | 4 4 5 5 5 5 6 |
3 | 3 3 3 4 4 4 4 |
4 | 4 4 5 5 7 7 5 |
5 | 6 6 6 5 5 5 5 |
6 | 4 3 4 4 4 4 4 |
7 | 5 4 4 5 4 4 5 |
8 | 4 5 5 5 5 5 5 |
9 | 5 5 6 6 6 6 6 |
10 | 3 3 3 4 4 4 4 |
11 | 4 4 5 5 5 5 5 |
12 | 5 5 6 6 5 5 5 |
13 | 4 4 4 4 4 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 5 5 6 6 6 |
19 | 5 5 5 5 5 5 6 |
20 | 6 5 5 5 5 5 6 |
21 | 5 4 5 5 5 5 5 |
22 | 5 5 5 5 6 5 5 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 5 4 5 6 8 |
25 | 5 5 6 22 4 5 5 |
26 | 4 4 4 4 4 4 5 |
27 | 7 7 8 7 7 7 7 |
28 | 5 5 5 5 5 5 5 |
29 | 5 4 5 5 5 5 5 |
30 | 4 3 3 4 5 4 4 |
31 | 5 4 5 5 5 4 5 |
32 | 5 4 4 4 4 5 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1627.0 GPS week: 1627 Day: 0 MJD: 55633.000
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 240| 0 0 4 84 -22 -3 -.18 9 9 | -812 298 16 67
| 37 8 |
emr 94| 0 -4 3 34 1 24 .42 21 21 | -119 -2289 17 80
| -58 40 |
esa 137| 0 2 -4 -142 -28 2 .26 10 9 | 1333 1150 12 112
| 14 70 |
gfz 196| 1 -2 -3 -131 10 3 -.18 12 11 | 69 241 24 99
| -60 -30 |
grg 131| 1 1 0 30 -62 -23 .65 15 14 | 321 -485 38 200
| -32 -46 |
igr n/a| 0 0 -2 64 13 -23 -.03 5 5 | 453 -2637 18 54
| -29 41 |
jpl 137| 2 1 4 -48 81 13 .50 22 22 | 3621 -2373 21 90
| 3 17 |
mit 258| 0 0 -5 54 14 0 -.38 13 12 | -65 336 22 153
| 13 8 |
ngs 213| -1 -1 -1 159 -13 -19 -.22 9 7 | -831 304 2653 4331
| -2 -2 |
sio 257| 0 2 9 -208 138 33 -.11 21 17 | --- --- --- ---
| 63 -16 |
Table 2.1627.1 GPS week: 1627 Day: 1 MJD: 55634.000
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 240| 0 0 4 104 -36 8 -.20 10 10 | 30 -789 16 78
| 5 35 |
emr 94| 0 1 6 52 -5 13 .40 21 21 | -1878 1552 17 80
| -58 33 |
esa 137| 1 1 -2 -100 -51 -12 .23 8 8 | -1005 -379 13 123
| 19 115 |
gfz 196| 1 -3 -1 -102 64 0 -.22 9 10 | 580 -901 22 92
| -68 6 |
grg 131| 0 1 -1 14 -58 -24 .66 14 14 | 24 87 48 204
| -4 -19 |
igr n/a| 0 -1 0 83 -22 -64 -.05 5 5 | -1642 1084 16 57
| -61 78 |
jpl 137| 2 1 5 -28 83 133 .50 21 21 | 1783 1594 19 93
| 27 -27 |
mit 258| 0 0 -5 43 64 -7 -.35 11 10 | -336 410 22 160
| 13 -2 |
ngs 213| -1 0 -1 165 -72 -44 -.24 9 8 | 7 -783 2254 3792
| 72 52 |
sio 257| 0 2 9 -213 175 27 -.12 20 19 | --- --- --- ---
| 61 -23 |
Table 2.1627.2 GPS week: 1627 Day: 2 MJD: 55635.000
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 240| 0 0 4 56 -25 -6 -.18 9 9 | 134 -1488 15 63
| 131 15 |
emr 94| 1 -2 0 -29 -20 68 .47 21 21 | -795 -969 18 97
| -14 51 |
esa 137| 2 1 0 -153 -32 -11 .23 9 9 | -1439 694 13 129
| 37 106 |
gfz 196| 0 -2 -4 16 59 17 -.18 9 10 | 358 -425 24 98
| -3 12 |
grg 131| -1 1 -2 -83 -89 0 .63 17 16 | 33 -372 45 190
| 127 -8 |
igr n/a| 0 0 0 48 -14 -39 -.01 5 5 | -901 -1477 16 59
| 3 35 |
jpl 137| 1 1 5 -95 63 -25 .52 22 22 | 3021 -1164 23 89
| -31 -37 |
mit 258| 0 -1 -7 141 42 10 -.33 13 12 | -310 183 20 151
| 1 -6 |
ngs 213| -1 0 -2 117 -69 -16 -.18 10 8 | 110 -1477 2334 3812
| 23 54 |
sio 257| 0 2 7 -127 154 13 -.08 18 20 | --- --- --- ---
| 62 -23 |
Table 2.1627.3 GPS week: 1627 Day: 3 MJD: 55636.000
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 240| 0 0 4 66 -40 12 -.20 10 9 | -734 28 18 74
| 35 28 |
emr 94| 2 0 3 37 -20 13 .46 21 21 | -1409 -769 20 95
| -45 46 |
esa 137| 1 1 0 -129 -64 -4 .21 8 9 | 362 -1862 13 110
| 58 120 |
gfz 196| 0 -5 -2 -53 63 -20 -.22 12 14 | -82 205 26 98
| 3 7 |
grg 131| -2 0 -2 -23 -30 -9 .61 17 17 | -419 340 44 276
| 56 -72 |
igr n/a| 0 0 0 57 -2 -5 -.05 5 5 | -1922 -1017 18 60
| -10 78 |
jpl 137| 1 2 3 -34 71 50 .54 21 21 | 2261 -486 19 94
| -7 19 |
mit 258| 0 0 -6 73 52 6 -.31 11 10 | -471 417 23 134
| -3 -6 |
ngs 213| 0 -1 -3 168 -51 -32 -.18 10 9 | -688 18 2246 4098
| 32 22 |
sio 257| 0 3 7 -200 158 9 -.13 19 19 | --- --- --- ---
| 64 -9 |
Table 2.1627.4 GPS week: 1627 Day: 4 MJD: 55637.000
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 240| 0 0 1 71 -58 -28 -.22 9 9 | -268 -516 16 70
| 95 52 |
emr 94| 0 4 4 -5 27 27 .42 22 22 | -2081 -466 19 91
| 4 15 |
esa 137| 2 2 0 -166 -39 17 .23 10 9 | -289 -717 16 132
| 21 86 |
gfz 196| 0 -3 -1 -17 50 0 -.20 11 11 | 512 -472 23 98
| -27 35 |
grg 131| 0 2 0 -67 -83 -19 .60 16 16 | 30 40 49 215
| 85 39 |
igr n/a| 0 0 0 72 -62 24 -.01 5 5 | -2748 -823 17 70
| -28 86 |
jpl 137| 0 0 4 -45 92 75 .45 23 23 | 1830 -310 21 97
| 5 -92 |
mit 258| 1 -3 -6 111 46 1 -.31 15 13 | -189 298 23 159
| 5 -11 |
ngs 213| -2 -1 -2 152 -66 -36 -.19 10 8 | -321 -497 2020 3969
| 32 52 |
sio 257| 2 3 8 -152 177 22 -.12 19 20 | --- --- --- ---
| 56 1 |
Table 2.1627.5 GPS week: 1627 Day: 5 MJD: 55638.000
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 240| -1 1 1 66 -57 2 -.23 10 9 | -227 -762 21 71
| 60 50 |
emr 94| 0 4 5 13 86 24 .41 23 23 | -1687 325 19 85
| 2 -52 |
esa 137| 0 0 0 -131 -9 27 .20 10 8 | -1422 1939 19 140
| 13 91 |
gfz 196| 0 -2 -4 9 -7 1 -.23 13 13 | 187 83 25 94
| -23 31 |
grg 131| 1 0 0 -43 -83 -23 .67 15 13 | 18 435 47 196
| 80 -4 |
igr n/a| 0 0 -1 58 -44 10 -.07 6 5 | -2978 -311 20 58
| -67 50 |
jpl 137| 1 0 6 -57 86 59 .53 23 23 | 1776 35 22 86
| 38 9 |
mit 258| 3 -2 -6 100 43 -12 -.33 14 13 | -257 765 23 131
| 8 -6 |
ngs 213| -4 0 0 114 -27 -31 -.24 10 8 | -223 -786 2080 4048
| 28 -47 |
sio 257| 3 3 6 -197 146 9 -.14 20 21 | --- --- --- ---
| 58 10 |
Table 2.1627.6 GPS week: 1627 Day: 6 MJD: 55639.000
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 240| 0 0 1 71 -74 29 -.27 11 9 | -116 -762 20 82
| 59 45 |
emr 94| 1 2 6 -16 48 17 .46 23 23 | -2108 -7 21 104
| 25 -31 |
esa 137| 0 2 -1 -139 -12 0 .23 9 8 | -43 2037 17 172
| 67 71 |
gfz 196| -2 -3 -1 20 2 -8 -.19 14 13 | 528 -587 28 114
| 26 12 |
grg 131| 1 0 -2 -5 -92 -19 .61 17 13 | 186 -366 61 197
| 63 21 |
igr n/a| -1 0 0 59 -5 23 -.05 6 6 | -4021 -781 21 79
| 2 47 |
jpl 137| 0 0 6 -75 67 30 .48 23 23 | 1058 -525 20 95
| 52 -11 |
mit 258| 4 -2 -6 119 62 -5 -.28 13 12 | -138 43 30 188
| -7 -1 |
ngs 213| -2 -1 0 92 -19 -17 -.22 10 9 | -115 -815 2224 3938
| 41 8 |
sio 257| 2 2 7 -175 177 -4 -.13 22 22 | --- --- --- ---
| 51 5 |
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 3.1627.0 GPS week: 1627 Day: 0 MJD: 55633.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 --- --- --- --- 382 --- --- --- --- 0 | 71 --- --- --- --- 254 --- --- --- --- 69
2 | 9 21 7 10 14 6 24 13 9 12 4 | 20 24 20 22 24 19 21 23 24 22 18
3 | 6 12 5 7 16 4 15 11 5 8 3 | 14 19 13 14 16 13 16 15 16 12 10
4 | 8 20 9 8 14 4 15 12 11 13 4 | 28 35 28 28 35 30 37 31 32 30 27
5 | 10 19 8 8 13 6 25 10 7 49 5 | 18 23 22 28 27 20 22 26 22 54 19
X6 | 7 12 5 7 14 4 --- 12 7 16 3 | 15 18 12 17 15 14 --- 17 18 16 12
7 | 10 21 9 10 20 6 21 16 11 18 5 | 42 45 43 35 48 39 45 38 45 37 38
8 | 11 18 11 9 12 5 15 9 10 22 4 | 18 25 17 15 25 15 24 15 20 25 15
9E | 13 23 13 10 18 6 18 15 9 21 5 | 29 34 28 33 25 27 28 33 32 28 27
10 | 8 14 6 6 10 3 12 9 6 11 3 | 33 33 37 37 41 34 36 39 39 29 34
11E | 6 19 10 11 11 5 25 13 9 10 4 | 24 33 26 24 31 23 31 26 23 23 22
12 | 11 23 8 10 14 5 26 10 11 32 5 | 16 28 20 24 30 17 29 16 19 25 17
13 | 7 20 7 11 18 5 22 8 7 15 4 | 20 36 26 24 40 22 34 21 23 21 22
14 | 8 23 9 10 14 7 24 11 9 16 4 | 23 25 23 23 31 19 28 22 25 23 20
15 | 10 23 13 11 17 3 29 13 6 22 5 | 14 27 23 21 28 16 29 21 16 23 16
16 | 8 21 7 11 12 5 28 9 6 26 4 | 20 27 13 21 18 14 26 18 15 19 13
17 | 8 20 11 14 18 5 25 14 12 17 5 | 21 34 24 23 31 24 37 22 27 25 22
18 | 10 23 13 15 11 6 28 13 9 25 5 | 18 28 25 30 30 19 30 24 21 22 20
19 | 11 25 10 11 17 3 29 12 10 20 5 | 23 36 20 23 19 24 37 22 28 28 21
20 | 12 18 11 29 13 7 24 15 9 24 6 | 21 29 28 37 27 21 27 26 25 20 21
21 | 8 20 9 8 18 4 26 10 10 11 4 | 36 42 40 37 53 39 42 39 36 37 38
22 | 10 21 12 8 11 5 26 12 10 30 5 | 25 30 30 31 33 23 27 31 29 33 25
23 | 8 21 5 10 14 5 23 12 9 19 4 | 22 37 26 25 33 23 33 21 24 26 23
24 | 8 17 10 12 12 3 20 12 8 19 4 | 26 38 27 30 29 25 37 23 23 33 25
X25 | 9 17 7 9 11 3 27 15 8 --- 4 | 225 8 228 225 6 225 8 224 6 --- 226
26 | 10 15 9 11 9 5 11 15 7 20 4 | 12 19 13 19 16 10 19 15 12 18 9
27E | 15 29 15 14 20 6 20 22 16 16 6 | 33 43 33 33 41 34 24 45 37 40 32
X28 | 8 --- 11 10 14 6 23 10 8 25 4 | 23 --- 22 25 30 21 30 25 24 24 22
29 | 9 25 6 10 16 4 24 12 9 15 4 | 19 37 25 22 30 24 36 24 26 18 21
30 | 8 12 9 10 14 3 18 10 11 14 4 | 26 26 19 27 28 22 22 27 25 25 22
31 | 6 23 9 10 21 4 16 12 8 14 4 | 37 41 32 30 34 34 38 33 39 34 31
32 | 9 18 10 10 12 7 19 16 8 19 4 | 22 25 27 29 29 22 23 29 24 21 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 21 10 12 15 5 22 13 9 21 |T 31 30 31 32 29 36 29 31 25 26 30
WRMS | 9 21 9 11 14 5 22 12 7 17 |NE 31 27 31 33 26 38 27 31 22 24 30
MEDI | 8 20 9 10 14 5 23 12 9 18 |MD 22 29 25 25 30 22 29 24 24 25 22
Table 3.1627.1 GPS week: 1627 Day: 1 MJD: 55634.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 7 --- --- --- --- 130 --- --- --- --- 0 | 43 --- --- --- --- 197 --- --- --- --- 43
2 | 7 22 6 9 16 6 23 10 9 12 4 | 22 25 20 26 28 22 28 26 32 21 22
3 | 8 14 4 7 13 3 14 9 7 8 3 | 13 16 13 15 18 11 13 14 19 13 12
4 | 9 21 8 8 14 6 14 9 11 20 4 | 25 33 25 29 28 22 34 29 31 21 26
5 | 9 20 8 13 13 7 22 10 10 45 5 | 17 23 20 25 25 17 25 22 26 46 18
6 | 9 14 4 8 12 4 13 10 6 15 3 | 16 18 15 18 19 14 14 17 23 17 14
7E | 16 17 7 11 14 6 16 10 8 12 4 | 46 51 48 44 48 40 47 44 52 44 46
8 | 14 23 8 6 13 5 13 10 11 25 4 | 17 32 22 15 23 15 27 17 25 26 16
9E | 16 20 11 10 17 6 16 16 14 24 5 | 31 35 30 34 26 30 34 40 37 32 30
10 | 10 13 6 7 10 4 10 7 9 10 3 | 25 25 29 26 30 26 28 29 33 22 26
11E | 8 20 10 7 13 2 24 13 10 12 4 | 15 29 19 20 27 18 27 18 24 20 17
12 | 11 24 6 10 16 6 25 8 8 32 5 | 17 29 21 23 26 20 31 18 25 26 19
13 | 6 20 7 8 22 5 21 7 9 15 4 | 19 29 24 17 39 18 31 19 28 17 20
14 | 10 26 6 8 14 4 29 14 9 17 4 | 20 29 21 20 30 19 29 22 21 19 19
15 | 12 25 10 8 18 6 24 16 12 21 5 | 17 28 21 18 27 15 27 26 21 23 17
16 | 8 26 6 10 12 5 27 8 9 27 4 | 15 25 13 17 22 14 24 14 20 16 12
17 | 11 20 8 12 19 4 22 8 12 16 4 | 26 33 26 19 32 21 32 23 28 20 21
18 | 13 20 9 13 11 5 26 11 9 21 5 | 15 30 23 25 27 21 28 22 22 23 20
19 | 9 27 11 8 15 3 27 11 9 22 5 | 19 30 16 19 17 18 29 19 24 24 16
20 | 9 23 8 10 10 4 21 13 9 22 4 | 19 28 22 22 24 19 28 25 32 21 20
21 | 9 17 11 9 17 4 26 8 9 7 4 | 34 38 36 38 51 33 39 35 42 34 36
22 | 12 19 8 11 11 5 26 11 8 24 4 | 18 28 23 26 28 22 28 26 25 31 22
23 | 8 27 6 6 15 5 26 10 11 19 4 | 22 32 23 19 30 19 33 23 30 19 20
24 | 7 21 7 8 13 4 14 12 8 17 4 | 25 41 27 27 30 24 36 22 29 30 26
X25 | 11 15 5 8 16 5 26 14 10 --- 4 | 91 7 93 96 7 94 9 93 9 --- 94
26 | 9 16 8 8 11 6 15 11 8 17 3 | 15 20 16 15 18 12 22 16 19 16 12
X27E | 15 25 13 12 21 7 --- 24 19 31 7 | 18 31 22 23 32 19 --- 34 35 29 20
28 | 12 21 6 9 14 3 20 10 9 22 4 | 19 32 23 20 31 16 31 18 25 17 19
29 | 9 22 6 9 14 3 25 10 9 16 4 | 21 33 25 25 30 22 35 24 26 18 23
30 | 8 11 5 8 13 4 16 8 8 12 3 | 21 18 17 23 24 20 17 20 26 19 18
31 | 15 21 5 8 15 5 21 11 10 13 4 | 37 47 39 43 43 39 39 39 37 39 39
32 | 9 20 6 8 16 4 21 12 9 17 4 | 18 24 18 22 23 19 20 25 31 18 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 21 8 9 14 5 21 11 9 20 |T 24 29 25 26 27 28 28 26 27 24 24
WRMS | 10 21 8 10 14 5 21 10 8 19 |NE 22 25 23 23 25 29 25 24 24 21 22
MEDI | 9 20 7 8 14 5 21 10 9 17 |MD 19 29 22 23 27 19 28 23 26 21 20
Table 3.1627.2 GPS week: 1627 Day: 2 MJD: 55635.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 5 --- --- --- --- 157 --- --- --- --- 0 | 51 --- --- --- --- 150 --- --- --- --- 50
2 | 10 25 10 10 16 5 23 15 12 14 5 | 19 32 24 26 23 24 30 27 31 21 25
3 | 8 12 6 8 14 5 12 11 8 8 3 | 7 15 12 10 15 9 18 12 10 12 10
4 | 9 22 16 12 17 5 16 15 9 16 5 | 37 46 37 39 41 39 46 38 40 41 39
5 | 9 21 9 9 14 7 23 13 15 38 5 | 12 27 20 22 26 15 28 22 20 39 17
6 | 8 13 7 8 15 4 13 12 9 16 3 | 10 16 15 13 16 10 18 15 13 18 11
7E | 9 13 7 11 15 4 21 9 8 9 3 | 26 37 29 29 37 28 39 30 28 31 29
8 | 11 26 7 6 14 4 13 13 10 20 4 | 14 34 19 13 24 15 29 14 16 27 17
9E | 15 21 10 12 19 4 18 20 15 18 5 | 28 32 26 27 19 28 31 38 32 21 26
10 | 9 12 9 6 11 4 10 10 7 11 3 | 22 28 30 28 33 24 31 30 25 22 26
11E | 7 19 8 10 15 6 26 15 10 11 4 | 16 24 17 12 24 13 28 16 19 14 15
12 | 12 24 9 10 20 6 24 9 10 33 5 | 13 28 20 15 27 16 27 13 19 24 17
13 | 7 18 9 9 21 6 27 10 7 12 4 | 17 31 23 19 38 19 36 18 19 17 19
14 | 9 28 8 8 19 4 29 14 9 17 5 | 16 27 22 19 32 18 33 22 20 17 20
15 | 11 22 10 11 20 5 26 12 11 18 5 | 13 27 21 18 27 16 30 19 16 18 17
16 | 8 23 8 10 12 6 24 11 10 24 4 | 11 25 16 17 19 11 27 14 13 15 14
17 | 8 21 11 11 19 6 25 13 11 17 5 | 18 32 17 18 29 17 35 21 23 22 18
18 | 11 23 9 11 19 6 28 11 9 21 5 | 19 35 28 27 32 25 36 26 22 21 25
19 | 9 24 11 9 16 5 23 15 9 20 5 | 20 32 22 21 16 22 34 20 25 25 21
20 | 8 19 11 11 13 6 24 12 10 24 4 | 15 26 19 25 22 17 24 21 22 25 17
21 | 9 23 5 9 20 8 26 12 10 9 4 | 36 44 41 39 48 40 42 38 35 38 39
22 | 10 21 12 8 16 6 27 13 6 21 5 | 18 30 25 23 31 22 32 25 23 24 23
23 | 7 25 8 8 17 4 29 11 8 18 4 | 16 29 20 17 27 17 33 19 19 18 16
24 | 8 17 8 10 17 6 18 16 11 14 4 | 23 35 25 28 29 23 36 21 26 30 26
X25 | 20 19 7 8 19 8 26 15 13 --- 6 | 323 11 327 324 9 326 16 325 6 --- 326
26 | 6 16 8 9 11 4 17 11 11 17 3 | 12 21 14 14 17 13 23 14 15 15 14
X27E | 15 21 16 11 26 6 --- 32 18 --- 8 | 17 29 23 19 34 19 --- 32 30 --- 22
28 | 8 21 11 11 17 4 23 14 10 22 5 | 21 32 26 21 32 21 33 21 24 18 23
29 | 9 25 8 9 18 5 23 11 7 15 4 | 18 37 21 19 25 20 33 20 20 16 21
30 | 8 13 10 7 11 6 12 10 8 7 3 | 26 24 24 27 28 24 29 28 22 25 25
31E | 6 23 9 11 23 5 19 10 8 13 4 | 31 45 37 33 42 35 40 33 36 33 35
32 | 9 20 10 7 15 5 17 9 9 17 4 | 18 23 21 22 27 20 25 25 19 20 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 21 9 9 17 5 22 13 10 18 |T 29 29 32 31 27 34 30 32 22 23 31
WRMS | 9 21 9 10 16 5 22 12 8 20 |NE 30 26 34 33 25 36 28 33 18 20 33
MEDI | 9 21 9 9 17 5 23 12 10 17 |MD 18 29 22 21 27 20 31 21 22 21 21
Table 3.1627.3 GPS week: 1627 Day: 3 MJD: 55636.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 --- --- --- --- 190 --- --- --- --- 0 | 72 --- --- --- --- 195 --- --- --- --- 72
2E | 10 21 10 10 18 4 21 8 12 13 4 | 30 33 30 35 36 32 34 34 37 29 30
3 | 7 13 5 8 21 4 13 8 10 8 3 | 10 17 12 12 20 10 16 13 16 13 11
4E | 17 22 6 10 19 6 16 11 12 20 5 | 68 75 72 68 75 69 74 77 73 81 70
5 | 10 20 9 12 16 5 22 10 11 31 5 | 17 24 24 25 30 19 25 25 21 34 20
6 | 9 13 5 9 19 6 13 9 10 15 3 | 15 17 16 14 22 15 14 18 18 20 14
7E | 8 26 8 14 14 3 21 13 8 9 4 | 23 35 26 23 33 23 31 23 31 22 23
8 | 13 19 6 10 16 5 14 13 11 22 4 | 17 31 22 21 24 18 29 21 24 28 19
9E | 17 18 11 14 24 5 17 19 13 18 5 | 32 34 31 34 28 31 33 40 35 28 29
10 | 9 11 7 21 13 5 12 9 11 12 4 | 27 30 35 30 37 29 29 34 30 27 29
11E | 7 21 9 11 11 3 27 13 9 12 4 | 14 27 20 17 26 14 25 17 19 17 16
12 | 9 21 8 19 15 3 24 12 9 32 5 | 16 26 22 34 28 19 29 18 21 28 19
13 | 6 19 7 10 22 4 24 8 8 13 4 | 22 35 26 22 41 22 36 23 27 23 23
14 | 9 28 7 13 16 5 28 15 11 17 5 | 19 29 23 24 33 19 28 24 24 19 21
15 | 10 20 9 12 23 6 24 9 7 20 4 | 17 26 22 21 30 17 27 23 21 23 19
16 | 9 24 6 12 15 7 24 8 11 27 5 | 16 25 19 19 23 15 26 17 17 17 15
17 | 7 17 8 15 20 3 24 9 11 18 4 | 24 31 23 18 31 23 33 25 30 29 23
18 | 14 23 8 17 16 5 27 11 7 22 5 | 16 31 28 33 36 22 30 29 23 21 24
19 | 9 24 12 10 18 6 26 11 10 20 5 | 21 35 17 21 19 21 32 20 25 26 19
20 | 8 21 11 11 13 6 24 9 10 25 4 | 20 30 29 27 29 20 27 23 30 27 22
21 | 10 25 5 10 23 4 18 9 11 12 4 | 32 47 43 43 53 38 40 39 40 39 40
22 | 10 22 8 13 14 6 26 12 10 21 5 | 19 29 26 32 38 22 26 31 24 26 25
23 | 9 24 6 11 16 8 27 10 7 18 4 | 22 37 24 25 33 22 36 26 26 28 24
24 | 6 19 9 12 13 5 17 13 9 16 4 | 20 34 23 26 30 21 33 20 24 27 22
X25 | 120 --- 27 28 --- 13 --- 37 --- --- 21 | 671 --- 685 693 --- 688 --- 694 --- --- 689
26 | 8 15 7 8 15 4 13 8 9 17 3 | 12 20 15 17 20 12 19 18 14 16 13
X27E | 16 21 7 13 29 4 --- 22 18 19 6 | 21 30 21 24 40 22 --- 34 34 27 23
28 | 9 22 10 12 16 3 19 15 9 21 5 | 18 30 27 25 32 20 29 21 20 19 22
29 | 9 24 13 14 17 6 24 9 13 16 5 | 19 32 19 25 24 19 33 22 21 23 19
30 | 9 12 5 11 16 6 11 9 9 12 3 | 24 27 26 31 34 24 24 29 29 27 27
31E | 8 25 7 10 20 5 17 14 12 14 4 | 19 31 19 18 29 21 28 26 24 21 18
32 | 10 20 7 11 13 8 20 6 10 17 4 | 20 23 25 28 29 20 22 26 29 21 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 21 8 12 17 5 21 11 10 19 |T 43 31 46 47 32 48 29 48 26 26 45
WRMS | 9 21 9 14 17 5 21 10 9 19 |NE 49 27 52 54 29 56 27 53 23 23 51
MEDI | 9 21 8 12 16 5 21 10 10 17 |MD 20 30 24 25 30 21 29 24 24 26 22
Table 3.1627.4 GPS week: 1627 Day: 4 MJD: 55637.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 --- --- --- --- 129 --- --- --- --- 0 | 53 --- --- --- --- 120 --- --- --- --- 49
2E | 8 24 14 12 19 4 23 11 13 13 5 | 19 23 18 21 23 16 25 19 27 12 16
3 | 9 17 7 9 14 6 14 9 10 11 3 | 11 16 14 12 14 10 14 11 14 12 11
4E | 16 23 14 9 20 8 19 13 20 36 6 | 101 106 108 105 102 109 106 106 108 115 105
5 | 7 20 10 11 15 5 23 11 12 26 4 | 17 25 23 25 22 18 26 24 20 30 18
6 | 8 17 6 8 12 6 17 12 9 16 3 | 12 18 13 14 12 12 15 13 15 15 12
7E | 7 18 8 13 18 4 21 11 5 12 4 | 19 23 19 19 29 16 25 21 22 21 15
8 | 11 19 7 9 18 5 14 19 9 22 4 | 20 29 24 20 28 21 32 21 27 29 21
9E | 15 21 13 12 17 5 18 22 16 18 5 | 32 33 32 29 29 30 33 39 37 24 30
10 | 8 16 8 16 11 4 14 12 12 14 4 | 23 28 30 25 26 25 29 29 27 23 24
11E | 7 23 8 10 11 5 23 18 9 11 4 | 17 29 18 18 24 16 25 21 21 18 16
12 | 10 23 8 7 20 5 21 11 11 33 5 | 21 28 23 21 29 20 30 22 29 28 22
13 | 4 21 7 7 20 5 24 9 9 13 4 | 21 36 28 20 40 20 36 23 23 23 23
14 | 10 28 11 16 14 6 27 14 10 15 5 | 21 28 28 27 32 23 31 26 25 20 22
15 | 11 25 11 12 15 7 26 12 7 18 5 | 19 32 28 25 27 23 31 25 23 23 23
16 | 8 27 7 9 13 3 28 9 9 27 5 | 16 27 20 19 21 15 28 17 17 18 15
17 | 6 21 11 11 15 6 25 14 10 19 4 | 20 33 24 19 27 19 36 21 20 24 19
18 | 12 25 10 15 19 5 31 14 8 25 5 | 16 31 29 30 32 22 33 26 25 17 23
19 | 9 26 9 11 18 3 28 15 9 19 5 | 24 35 20 20 18 20 35 23 26 27 22
20 | 7 22 11 7 10 5 25 12 6 26 4 | 25 28 27 25 26 21 27 25 26 25 22
21E | 7 21 10 11 16 6 24 15 6 9 4 | 52 51 52 52 53 50 53 53 55 51 51
22 | 11 24 13 10 15 7 35 15 9 23 5 | 23 29 32 31 37 25 30 30 30 26 28
23 | 7 26 8 10 14 5 26 13 6 17 4 | 22 36 22 20 30 19 32 24 23 23 20
24 | 7 33 9 13 16 5 18 18 9 16 5 | 31 47 28 29 33 28 36 27 29 31 29
X25 | 8 18 6 7 17 5 --- 11 6 --- 4 | 786 10 800 804 6 800 --- 802 6 --- 800
26 | 6 18 7 9 12 5 13 13 7 18 3 | 18 23 20 19 17 16 21 19 17 22 17
27E | 15 21 13 10 23 5 18 28 21 18 6 | 18 27 20 21 31 19 20 37 35 21 20
28 | 7 23 8 10 13 5 25 16 10 21 4 | 22 32 25 21 32 23 33 24 21 20 21
29 | 8 25 8 10 19 5 21 13 7 16 4 | 21 33 17 19 27 20 35 23 28 19 19
30 | 12 15 7 10 19 5 18 19 8 11 4 | 71 72 72 74 66 69 74 74 73 69 71
31E | 8 21 7 8 21 3 20 15 9 12 4 | 16 26 19 17 28 16 25 19 21 18 18
32 | 9 20 10 8 11 6 20 9 8 19 4 | 24 26 28 28 30 26 29 32 30 22 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 22 10 11 16 5 22 15 10 19 |T 50 32 53 52 30 52 33 54 29 27 50
WRMS | 9 22 9 11 16 5 22 13 8 20 |NE 56 29 61 59 27 60 31 60 24 24 57
MEDI | 8 21 8 10 16 5 21 13 9 18 |MD 21 29 24 21 28 20 30 24 25 23 22
Table 3.1627.5 GPS week: 1627 Day: 5 MJD: 55638.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 26 --- --- --- --- 43 --- 19 35 --- 20 | 39 --- --- --- --- 65 --- 4 5 --- 52
2E | 6 23 8 13 12 6 28 11 8 13 4 | 22 27 21 24 23 19 29 28 24 24 21
3 | 8 16 7 12 16 6 17 8 11 12 4 | 11 15 13 12 18 12 18 13 19 15 11
4E | 18 25 24 16 29 16 17 13 14 16 7 | 90 91 93 93 80 98 87 92 96 91 91
5 | 6 20 8 18 11 6 25 8 6 23 4 | 16 22 16 27 18 16 22 21 16 26 15
6 | 8 14 6 13 11 4 16 9 12 16 4 | 12 15 14 15 16 13 16 16 22 18 13
7E | 9 20 7 14 12 6 23 9 9 13 4 | 15 24 20 18 27 16 25 18 21 17 15
8 | 12 24 8 14 19 7 15 15 8 23 5 | 16 29 16 19 23 15 24 18 22 30 15
9E | 15 22 11 11 16 4 19 20 15 19 5 | 29 32 24 30 23 28 27 41 37 24 26
10 | 8 17 9 14 10 6 17 8 8 18 4 | 23 26 28 31 23 25 25 27 27 23 24
11E | 11 20 8 15 19 5 25 19 12 15 5 | 14 25 16 14 26 13 25 20 18 20 13
12 | 9 23 6 9 14 8 24 12 9 31 5 | 17 27 21 20 24 19 29 21 23 30 19
13 | 7 27 7 12 17 3 26 9 8 14 4 | 17 35 23 20 36 17 35 19 21 20 19
14 | 8 28 9 15 14 2 26 15 10 19 5 | 18 26 22 23 29 19 27 23 19 16 18
15 | 8 24 8 12 18 5 27 13 7 21 5 | 16 29 21 20 26 18 27 24 20 19 18
16 | 8 24 7 15 10 4 25 11 10 27 5 | 15 24 15 16 21 12 24 15 16 13 13
17 | 6 25 10 15 14 4 28 13 8 19 5 | 18 33 20 17 28 18 32 17 20 21 17
18 | 10 30 9 18 13 5 31 15 7 26 5 | 14 31 22 29 28 19 30 22 22 17 19
19 | 8 27 12 14 16 5 30 11 8 18 5 | 21 32 19 21 20 21 32 21 22 29 19
20 | 9 21 9 11 13 4 22 13 10 31 5 | 21 24 24 23 21 16 24 21 20 25 18
21E | 9 24 6 16 13 4 23 14 8 10 4 | 30 38 32 32 36 29 36 34 30 32 30
22 | 10 24 8 11 12 5 28 12 10 25 5 | 20 28 26 25 30 22 28 26 29 21 22
23 | 9 29 7 13 12 4 29 12 7 18 5 | 19 32 23 20 27 16 32 22 18 21 17
24 | 14 22 13 16 17 4 20 18 12 20 5 | 39 46 42 42 44 40 48 39 32 45 39
X25 | 9 18 6 12 12 4 25 15 10 --- 4 | 318 8 322 322 7 322 8 324 5 --- 323
26 | 6 17 7 12 11 4 19 14 7 17 4 | 11 17 14 13 15 11 18 17 15 13 11
27E | 14 20 11 13 25 4 19 27 18 19 6 | 16 26 18 21 36 19 22 38 31 24 20
28 | 8 23 8 13 12 5 22 14 7 21 4 | 16 32 23 20 30 18 29 19 25 17 18
29 | 9 25 8 10 13 5 25 14 11 16 4 | 16 28 19 18 24 16 28 22 24 20 16
30 | 12 12 6 11 9 4 15 12 10 14 4 | 47 45 46 47 44 43 46 46 42 43 44
31E | 7 21 8 9 18 4 21 10 11 11 4 | 14 27 20 16 27 17 25 20 17 16 17
32 | 9 20 13 11 11 4 21 11 9 23 4 | 23 22 31 27 21 21 18 26 23 20 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 23 10 13 15 6 23 14 10 20 |T 31 29 34 34 27 32 28 34 24 25 32
WRMS | 9 23 8 13 13 5 23 13 8 21 |NE 32 26 35 35 24 33 26 34 20 21 33
MEDI | 9 23 8 13 13 4 23 13 9 18 |MD 17 27 21 21 26 18 27 21 22 21 18
Table 3.1627.6 GPS week: 1627 Day: 6 MJD: 55639.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 7 --- --- --- --- 121 --- --- --- --- 0 | 47 --- --- --- --- 101 --- --- --- --- 50
2E | 8 31 7 13 26 4 28 12 11 12 5 | 17 28 14 18 26 15 25 23 22 16 16
3 | 9 13 8 11 14 5 17 10 8 13 3 | 11 17 15 13 17 11 19 13 14 15 12
4E | 10 17 9 14 18 5 15 13 10 22 4 | 100 100 98 94 102 97 96 96 99 104 94
5 | 8 22 7 12 15 5 25 10 9 22 4 | 21 27 22 29 30 23 24 28 24 29 21
6 | 8 13 5 13 13 6 18 11 6 17 3 | 11 18 14 16 18 11 16 15 15 18 12
7E | 9 16 7 15 17 4 24 11 12 15 4 | 21 28 23 23 26 21 27 26 28 26 21
8 | 11 27 8 11 20 5 19 11 11 27 5 | 15 29 17 18 25 18 27 17 21 35 17
9E | 16 24 13 15 16 5 18 21 19 18 6 | 34 38 31 30 30 31 33 40 36 31 30
10 | 8 15 3 12 11 5 16 10 11 14 3 | 36 40 43 38 45 39 40 44 39 39 38
11E | 8 20 9 15 20 6 26 14 9 16 5 | 17 29 20 18 27 18 29 21 21 21 20
12 | 10 23 6 11 15 7 23 15 8 32 5 | 20 28 23 23 28 21 27 22 21 34 20
13 | 7 21 10 13 22 4 25 14 8 16 5 | 23 34 27 25 38 23 35 25 27 22 23
14 | 10 27 10 12 14 5 26 12 8 21 5 | 22 33 31 29 35 24 32 30 21 27 26
15 | 7 26 8 13 18 6 29 11 8 24 5 | 21 31 26 26 31 22 32 27 23 27 24
16 | 10 26 7 16 13 6 25 10 9 32 5 | 21 30 24 27 31 21 29 24 23 23 23
17 | 6 25 8 12 16 3 27 9 10 15 4 | 27 40 30 25 34 26 43 24 24 28 26
18 | 10 26 11 16 15 6 31 10 11 32 5 | 18 32 28 34 35 23 31 30 23 31 25
X19 | 11 27 11 12 --- 6 28 13 10 19 5 | 26 40 20 22 --- 26 39 25 29 32 26
20 | 7 22 10 18 11 7 22 16 8 35 5 | 27 28 34 35 29 27 25 31 31 32 27
21E | 9 28 7 14 14 6 28 9 8 12 4 | 40 48 44 46 48 42 43 45 41 46 44
22 | 8 25 10 12 10 6 27 13 8 29 5 | 28 35 38 38 40 31 32 40 31 32 33
23 | 8 30 8 12 14 4 28 14 8 22 5 | 23 35 27 26 31 21 33 26 24 24 22
24E | 35 18 13 18 31 15 21 16 11 24 7 | 52 55 56 57 57 51 56 55 46 55 53
X25 | 12 16 8 11 16 5 24 14 8 --- 4 | 326 8 331 330 6 329 9 330 4 --- 331
26 | 6 18 6 15 12 5 21 19 9 21 4 | 15 23 17 18 19 16 25 21 18 25 16
X27E | 13 25 12 15 23 5 --- 26 20 19 7 | 26 32 27 28 46 28 --- 41 38 30 31
28 | 8 23 9 10 11 7 23 13 9 23 4 | 21 33 28 27 34 23 34 27 26 26 25
29 | 8 24 8 9 16 6 25 20 7 16 4 | 22 35 21 21 25 22 35 24 25 22 22
30 | 10 14 8 14 13 5 16 11 5 17 4 | 59 64 65 64 66 60 64 66 61 63 64
31E | 11 22 10 14 22 5 18 11 9 11 4 | 20 31 24 22 32 23 29 24 25 24 23
32 | 9 18 7 13 9 6 18 12 7 20 4 | 32 31 39 38 38 33 28 40 36 29 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 22 9 14 17 6 23 13 10 22 |T 37 34 40 40 34 39 33 41 29 32 39
WRMS | 9 22 8 13 13 6 23 12 9 22 |NE 37 31 41 41 31 41 30 42 25 29 39
MEDI | 9 23 8 13 15 5 24 12 9 19 |MD 22 32 27 27 31 23 31 27 25 28 25
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 4.1627 GPS week: 1627 MJD: 55633.0-55639.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 |U 11 10 28 |U 9 9 35 |U 9 10 45 |
emr | emr 2939 |U 14 11 28 |U 11 10 34 | 10 11 49 |
esa | esa 2976 | 10 9 26 |U 9 8 35 | 9 9 45 |
gfz | gfz 2966 |U 9 9 21 |U 11 9 42 |U 9 11 43 |
grg | grg 2948 | 18 18 34 |U 10 9 43 | 9 9 56 |
igr | igr 2969 | 14 11 41 | 9 9 35 | 8 9 44 |
igs | igs 2964 | 8 8 20 | 9 9 34 | 8 9 46 |
jpl | jpl 2869 |U 11 10 31 |U 9 10 34 |U 10 10 47 |
mit | mit 2989 |U 14 12 38 |U 10 10 37 |U 9 10 49 |
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 5.1627.0 GPS week: 1627 Day: 0 MJD: 55633.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 | 7 8 18 | ---- ---- ---- | 7 7 19 |
emr | emr 2876 | 11 9 21 | ---- ---- ---- | 12 11 29 |
esa | esa 2976 | 9 8 17 | ---- ---- ---- | 6 6 18 |
gfz | gfz 2968 | 10 9 21 | ---- ---- ---- | 6 5 16 |
grg | grg 2976 | 10 9 21 | ---- ---- ---- | 7 6 19 |
igr | igr 2976 | 9 8 19 | ---- ---- ---- | 6 5 19 |
igs | igs 2976 | 9 8 17 | ---- ---- ---- | 6 5 18 |
jpl | jpl 2866 | 12 9 21 | ---- ---- ---- | 8 6 17 |
mit | mit 2976 | 7 7 19 | ---- ---- ---- | 7 6 22 |
Table 5.1627.1 GPS week: 1627 Day: 1 MJD: 55634.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 8 9 20 | ---- ---- ---- | 19 27 218 |
emr | emr 2968 | 10 12 29 | ---- ---- ---- | 19 25 222 |
esa | esa 2976 | 8 6 15 | ---- ---- ---- | 18 22 202 |
gfz | gfz 2968 | 9 9 20 | ---- ---- ---- | 19 26 196 |
grg | grg 2976 | 9 5 15 | ---- ---- ---- | 15 22 273 |
igr | igr 2976 | 7 7 16 | ---- ---- ---- | 18 25 209 |
igs | igs 2976 | 8 8 15 | ---- ---- ---- | 18 26 215 |
jpl | jpl 2876 | 12 11 39 | ---- ---- ---- | 22 23 203 |
mit | mit 2976 | 10 8 19 | ---- ---- ---- | 20 30 221 |
Table 5.1627.2 GPS week: 1627 Day: 2 MJD: 55635.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3038 | 6 7 12 | 12 11 32 | 7 6 15 |
emr | emr 2967 | 15 7 38 | 14 10 33 | 9 7 18 |
esa | esa 2976 | 16 15 28 | 11 10 38 | 7 5 17 |
gfz | gfz 2968 | 8 8 21 | 12 9 51 | 7 5 15 |
grg | grg 2975 | 20 21 40 | 11 9 41 | 7 5 17 |
igr | igr 2961 | 7 5 16 | 12 10 37 | 7 5 14 |
igs | igs 2975 | 7 5 15 | 12 10 35 | 7 5 15 |
jpl | jpl 2874 | 14 8 38 | 12 11 36 | 9 7 14 |
mit | mit 2976 | 7 7 15 | 12 11 39 | 8 6 17 |
Table 5.1627.3 GPS week: 1627 Day: 3 MJD: 55636.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 14 10 47 | 9 7 44 | 10 11 16 |
emr | emr 2871 | 21 15 38 | 11 9 38 | 7 9 18 |
esa | esa 2976 | 19 15 53 | 8 8 40 | 9 7 17 |
gfz | gfz 2968 | 21 17 34 | 12 9 47 | 9 8 20 |
grg | grg 2880 | 21 18 38 | 9 9 55 | 7 6 20 |
igr | igr 2959 | 33 15 137 | 7 8 40 | 8 7 16 |
igs | igs 2925 | 12 10 27 | 9 8 41 | 7 6 17 |
jpl | jpl 2779 | 11 13 30 | 8 11 38 | 8 9 26 |
mit | mit 2976 | 32 19 61 | 9 9 40 | 6 4 16 |
Table 5.1627.4 GPS week: 1627 Day: 4 MJD: 55637.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 12 10 52 | 9 10 33 | 5 5 17 |
emr | emr 2966 | 9 8 18 | 9 10 34 | 9 8 19 |
esa | esa 2976 | 7 8 26 | 9 11 33 | 7 8 22 |
gfz | gfz 2964 | 6 6 17 | 11 13 39 | 10 14 20 |
grg | grg 2976 | 7 10 24 | 10 10 43 | 8 8 24 |
igr | igr 2974 | 7 8 28 | 8 10 34 | 6 6 19 |
igs | igs 2974 | 7 7 24 | 9 10 34 | 6 6 19 |
jpl | jpl 2863 | 11 10 37 | 9 10 37 | 7 7 26 |
mit | mit 2976 | 10 9 49 | 10 10 37 | 9 8 23 |
Table 5.1627.5 GPS week: 1627 Day: 5 MJD: 55638.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 19 23 38 | 8 7 27 | 8 8 19 |
emr | emr 2964 | 23 21 41 | 10 8 28 | 9 10 20 |
esa | esa 2976 | 7 6 25 | 8 7 30 | 12 10 24 |
gfz | gfz 2965 | 7 7 23 | 9 7 35 | 9 9 18 |
grg | grg 2976 | 51 54 83 | 8 9 32 | 10 8 21 |
igr | igr 2974 | 26 31 52 | 8 6 29 | 8 8 19 |
igs | igs 2968 | 7 8 28 | 8 6 29 | 9 9 22 |
jpl | jpl 2958 | 11 11 35 | 8 7 23 | 9 9 20 |
mit | mit 3072 | 22 27 70 | 8 8 33 | 7 6 19 |
Table 5.1627.6 GPS week: 1627 Day: 6 MJD: 55639.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3018 | 8 7 13 | 9 8 39 | 6 5 14 |
emr | emr 2964 | 7 8 14 | 9 13 37 | 7 9 18 |
esa | esa 2976 | 7 7 20 | 9 7 33 | 5 6 16 |
gfz | gfz 2965 | 6 6 14 | 10 7 38 | 6 7 16 |
grg | grg 2880 | 9 7 20 | 9 9 43 | 9 8 17 |
igr | igr 2967 | 6 6 17 | 9 9 35 | 5 6 16 |
igs | igs 2960 | 6 7 16 | 9 9 34 | 5 6 14 |
jpl | jpl 2868 | 9 8 15 | 8 11 35 | 10 9 23 |
mit | mit 2976 | 8 9 33 | 11 14 39 | 9 9 23 |
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 6.1627 GPS week: 1627 MJD: 55633.500-55639.500
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 | -10 -42 137 168 2 | 8 18
| 19 39 66 103 4 | 3
emr uuuuu | 8 39 -91 223 -3 | 52 53
| 36 23 43 145 4 | 3
esa uuuuu | -71 -14 88 -176 -6 | 7 17
| 15 15 77 63 4 | 3
gfz uuuuu | 12 40 20 -98 1 | 8 17
| 20 21 66 116 3 | 3
grg uuuux | 36 -35 9 102 11 | -2 25
| 38 45 111 111 19 | 1
igr xxxxx | -36 46 69 22 -13 | 9 19
| 17 26 33 81 5 | 4
irf xxxxx | 23 19 -78 48 -1 | 8 18
| 11 15 51 38 3 | 3
jpl uuuuu | 40 6 127 267 2 | 16 24
| 46 28 90 176 9 | 4
mit uuuuu | 26 14 -197 126 1 | 18 24
| 15 22 86 80 3 | 3
ngs uuuuu | 3 -14 -20 -78 -1 | 1 12
| 28 23 88 95 4 | 2
sio uuuuu | 31 -41 71 55 19 | 30 38
| 21 19 70 41 8 | 9
Table 7.1627.0 GPS week: 1627 Day: 0 MJD: 55633.500
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 -46 140 207 10 | 4 16
emr uuuuu | -33 49 -120 264 -5 | 49 51
esa uuuuu | -63 -23 183 -264 0 | 3 17
gfz uuuuu | 37 51 12 -16 0 | 3 15
grg uuuux | 53 23 -67 230 5 | -3 24
igr xxxxx | -34 20 87 -8 -15 | 12 20
irf xxxxx | 7 -9 -153 4 -3 | 5 18
jpl uuuuu | -10 -12 114 500 -3 | 11 20
mit uuuuu | -1 -22 -325 13 0 | 13 22
ngs uuuuu | 9 -7 80 -130 -4 | 0 11
sio uuuuu | 23 -72 8 30 32 | 15 26
Table 7.1627.1 GPS week: 1627 Day: 1 MJD: 55634.500
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 3 189 287 2 | 6 18
emr uuuuu | 0 66 -136 65 -5 | 50 52
esa uuuuu | -82 -11 131 -197 -7 | 5 18
gfz uuuuu | 27 76 -20 13 6 | 4 17
grg uuuux | 52 12 -2 192 29 | -4 23
igr xxxxx | -45 69 78 -72 -6 | 10 18
irf xxxxx | 33 8 -77 32 -3 | 6 19
jpl uuuuu | 60 -19 87 87 10 | 12 21
mit uuuuu | 35 -5 -211 56 0 | 15 24
ngs uuuuu | -19 -64 31 17 -7 | 1 12
sio uuuuu | 56 -53 39 89 28 | 21 33
Table 7.1627.2 GPS week: 1627 Day: 2 MJD: 55635.500
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 -108 54 308 1 | 9 19
emr uuuuu | -21 37 -140 138 -8 | 52 54
esa uuuuu | -76 -14 64 -72 -14 | 7 18
gfz uuuuu | 18 26 114 5 -1 | 8 17
grg uuuux | 38 -104 236 56 -14 | 0 25
igr xxxxx | -5 20 91 -43 -6 | 11 18
irf xxxxx | 30 23 -121 84 -2 | 9 19
jpl uuuuu | 67 54 206 20 14 | 15 23
mit uuuuu | 36 22 -265 151 1 | 19 25
ngs uuuuu | -24 0 -103 -180 1 | 2 11
sio uuuuu | 53 -39 -37 130 19 | 28 37
Table 7.1627.3 GPS week: 1627 Day: 3 MJD: 55636.500
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 -11 237 107 -2 | 12 19
emr uuuuu | -16 69 -23 31 0 | 55 56
esa uuuuu | -90 -34 122 -123 -3 | 10 16
gfz uuuuu | 23 21 -2 -50 2 | 11 17
grg uuuux | 102 -32 -21 173 -10 | 0 25
igr xxxxx | -48 34 87 44 -15 | 12 19
irf xxxxx | 30 24 -1 65 -3 | 12 19
jpl uuuuu | 11 31 18 193 10 | 20 26
mit uuuuu | 36 27 -72 205 -2 | 23 26
ngs uuuuu | 8 -8 -141 -195 -2 | 4 12
sio uuuuu | 39 -40 138 56 17 | 36 41
Table 7.1627.4 GPS week: 1627 Day: 4 MJD: 55637.500
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 | -22 -75 101 62 0 | 11 18
emr uuuuu | 15 16 -77 322 -4 | 54 55
esa uuuuu | -56 -1 73 -167 -4 | 10 16
gfz uuuuu | -5 47 106 -145 0 | 11 17
grg uuuux | -9 -65 10 -69 34 | -3 25
igr xxxxx | -56 48 95 -13 -19 | 10 17
irf xxxxx | 30 20 -81 20 -2 | 11 18
jpl uuuuu | 122 15 74 286 -8 | 20 26
mit uuuuu | 41 15 -216 88 0 | 22 25
ngs uuuuu | -22 -12 -76 43 3 | 2 11
sio uuuuu | 29 -36 102 43 13 | 38 43
Table 7.1627.5 GPS week: 1627 Day: 5 MJD: 55638.500
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 | -40 -37 168 54 4 | 9 18
emr uuuuu | 62 21 -80 404 -3 | 52 54
esa uuuuu | -81 10 -63 -192 -6 | 8 16
gfz uuuuu | -21 46 -11 -279 -3 | 9 17
grg uuuux | 14 -57 23 -4 18 | -1 25
igr xxxxx | -40 90 8 81 -14 | 6 19
irf xxxxx | 10 23 -28 23 1 | 8 17
jpl uuuuu | 1 -15 101 409 2 | 19 26
mit uuuuu | 16 15 -111 135 4 | 19 24
ngs uuuuu | 57 -5 73 -18 2 | 1 12
sio uuuuu | 0 -35 154 33 11 | 38 43
Table 7.1627.6 GPS week: 1627 Day: 6 MJD: 55639.500
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 | -26 -18 72 150 -2 | 7 18
emr uuuuu | 50 16 -63 337 3 | 48 50
esa uuuuu | -52 -26 104 -219 -6 | 4 16
gfz uuuuu | 7 15 -61 -214 6 | 6 17
grg uuuux | -2 -22 -114 137 17 | -2 25
igr xxxxx | -28 39 40 165 -17 | 1 20
irf xxxxx | 19 41 -88 105 3 | 4 16
jpl uuuuu | 30 -11 286 376 -10 | 16 25
mit uuuuu | 20 48 -178 235 5 | 16 22
ngs uuuuu | 11 0 -6 -84 0 | -1 13
sio uuuuu | 14 -10 93 7 15 | 37 42
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