[IGSREPORT-19541] Wk 1624 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Mar 10 05:31:57 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1624 (Feb 20, 2011 - Feb 26, 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:
igs1624[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1624[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1624[0-6].cls IGS GPS clock combination summary report.
igs16247.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16247.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 | 24 26 24 26
0 | EMR | WTZR YELL WTZR YELL
0 | ESA | 21 21 MDVJ UNSA
0 | GFZ | 26 ALIC CHUR MDVJ
0 | GRG | ADIS SANT
0 | JPL | 6 25
0 | MIT | 21 26 21 26 CHUR DAV1 MDVJ
1 | COD | MATE
1 | EMR | WTZR HARB WTZR
1 | ESA | 27 27 UNSA
1 | GFZ | 27 QIKI
1 | GRG | ADIS AMC2 GUAT SANT
1 | JPL | 25 ADIS
2 | COD | RAMO SOFI
2 | EMR | WTZR WTZR
2 | ESA | ALIC MATE UNSA
2 | GRG | ADIS AMC2 SANT
2 | JPL | 25 ADIS
2 | MIT | NICO BRUS CAS1 HARB MATE NICO SCH2
3 | ALL | 6 6
3 | COD | AREQ
3 | EMR | WTZR WTZR
3 | ESA | UNSA
3 | GFZ | FAA1 IRKT MDVJ SHAO WUHN
3 | GRG | ADIS LHAZ SANT USN3
3 | JPL | 25 ADIS ALIC
3 | MIT | 7 7
4 | EMR | WTZR WTZR
4 | ESA | MATE MATE NRC1
4 | GFZ | 12 BRUS MATE MDVJ RAMO RESO ZECK
4 | GRG | ADIS AMC2 SANT
4 | JPL | 25 ADIS CAS1 DAV1
4 | MIT | CAS1 CAS1 DAV1
5 | COD | ALRT HARB
5 | EMR | HARB WTZR WTZR
5 | ESA | UNSA
5 | GFZ | CEDU HARB MAC1 TIDB
5 | GRG | AMC2 SANT
5 | JPL | 25
5 | MIT | 4 4 CHUR CHUR HARB WES2
6 | EMR | WTZR WTZR
6 | ESA | UNSA
6 | GFZ | 6 ALRT ARTU HARB
6 | GRG | ADIS SANT
6 | JPL | 25 ADIS
6 | MIT | DAV1 HARB
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 | GRG | 6
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 G06 | 2 | | | | | | |
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 | -.2 .7 .1 -3 14 -15 .26
EMR | 3.3 5.9 6.3 62 -33 13 .59
ESA | 6.7 6.1 -2.8 107 -52 -28 .22
GFZ | -1.1 .5 .3 -3 28 -36 .43
GRG | 6.0 9.9 2.1 34 52 -87 .50
JPL | 3.6 5.0 13.2 28 -31 52 .11
MIT | 7.5 -1.0 6.4 10 -10 -18 .24
NGS | 5.4 -.6 1.8 -3 -85 20 .22
SIO | 7.1 -2.0 15.5 -44 -70 -3 .34
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 1.1624.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1624.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 2.1624.[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 3.1624.[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 5.1624.0-6).
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 1624 summary. (Feb 20, 2011 - Feb 26, 2011)
Table 1.1624.a GPS week: 1624 MJD: 55612.000-55618.000
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 233| 0 1 2 33 -29 0 -.23 9 8 | -30 -630 19 88
| 0 0 0 19 14 21 .02 | 434 685
emr 89| 0 3 6 -70 47 15 .47 19 19 | -1538 29 14 96
| 1 2 0 28 9 24 .04 | 809 1242
esa 130| 0 0 -3 -122 -20 -28 .19 9 9 | -902 118 13 122
| 1 1 1 12 31 16 .02 | 1364 1762
gfz 196| 0 -1 -2 55 -80 17 -.17 10 10 | 293 -229 22 102
| 1 1 1 33 58 15 .02 | 427 632
grg 136| 2 1 -5 -38 -109 -37 .65 16 15 | 59 45 46 219
| 1 0 1 20 20 9 .02 | 150 388
igr n/a| 0 0 -2 40 8 4 -.04 5 5 | 4664 -520 17 67
| 0 0 0 26 36 22 .02 | 1633 1226
jpl 142| 0 0 6 -33 61 15 .47 18 18 | 2519 -69 18 99
| 1 1 2 18 13 61 .02 | 855 1249
mit 256| 0 -1 -1 25 -16 23 -.32 12 11 | -447 864 20 154
| 0 1 1 27 26 10 .04 | 663 1392
ngs 216| 0 0 -1 54 136 -18 -.22 11 10 | -141698 162417 2343 3824
| 1 1 1 31 34 21 .03 | 275659 405074
sio 258| -2 0 6 119 116 21 -.28 21 21 | --- --- --- ---
| 0 0 1 40 25 17 .02 | --- ---
Table 1.1624.b GPS week : 1624 MJD: 55612.000-55618.000
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 0 0 |
2 | 5 5 5 4 5 5 5 |
3 | 7 5 4 4 4 4 4 |
4 | 4 4 4 3 4 4 4 |
5 | 5 5 5 5 5 5 5 |
6 | 7 7 5 19 6 5 5 |
7 | 4 5 4 4 4 4 4 |
8 | 4 5 4 4 4 4 4 |
9 | 4 4 4 4 5 4 5 |
10 | 4 4 4 3 4 3 4 |
11 | 5 4 5 5 5 5 5 |
12 | 5 5 5 5 6 5 5 |
13 | 5 5 5 5 5 5 5 |
14 | 5 5 5 5 4 5 5 |
15 | 5 6 6 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 4 4 5 6 5 |
18 | 5 5 5 4 5 5 5 |
19 | 5 5 5 5 5 5 5 |
20 | 5 5 5 5 5 5 5 |
21 | 5 5 5 5 5 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 6 5 5 5 5 5 5 |
24 | 4 4 5 5 4 4 5 |
25 | 5 5 5 4 4 5 5 |
26 | 5 5 5 5 5 5 5 |
27 | 4 4 5 5 5 4 5 |
28 | 4 4 4 4 5 5 5 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 3 4 4 |
31 | 5 4 5 5 4 5 5 |
32 | 4 5 5 5 5 5 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 2.1624.0 GPS week: 1624 Day: 0 MJD: 55612.000
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 233| 0 1 3 70 -17 10 -.24 10 8 | -441 -188 20 99
| -7 -60 |
emr 89| 0 1 5 -93 51 -9 .49 18 18 | -431 35 16 99
| 29 -9 |
esa 130| 3 0 -2 -116 -13 -18 .16 8 8 | -1411 1075 14 111
| 51 89 |
gfz 196| 0 -1 0 23 -95 16 -.19 13 12 | -111 291 22 94
| -116 75 |
grg 136| 1 1 -6 -27 -101 -26 .68 17 16 | -141 614 52 213
| 61 -74 |
igr n/a| 0 0 -3 55 -55 8 -.04 6 6 | 6943 -449 18 78
| -18 22 |
jpl 142| 0 1 5 -58 55 67 .47 20 19 | 3362 63 19 98
| -20 29 |
mit 256| 0 -2 0 -3 -29 17 -.27 12 11 | -502 1172 27 175
| 8 38 |
ngs 216| -2 -1 -4 106 123 -42 -.25 11 9 | -488 -138 2291 3852
| 24 79 |
sio 258| -1 0 4 101 113 8 -.29 21 21 | --- --- --- ---
| -56 -29 |
Table 2.1624.1 GPS week: 1624 Day: 1 MJD: 55613.000
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 233| 0 1 2 27 -43 11 -.24 9 8 | -142 -680 25 106
| 89 21 |
emr 89| 3 4 6 -79 41 21 .47 18 18 | -1270 -985 15 91
| 29 -10 |
esa 130| 0 0 -5 -136 -29 -34 .19 9 9 | 9 -1986 13 121
| 64 85 |
gfz 196| -1 -1 -1 46 7 28 -.16 11 11 | 41 -70 21 97
| -44 13 |
grg 136| 1 0 -6 -71 -111 -33 .62 16 15 | 7 -62 46 191
| 112 -46 |
igr n/a| 0 0 -3 74 -18 39 -.05 8 7 | 5737 -1251 17 68
| -36 18 |
jpl 142| 0 -2 8 -33 49 -19 .46 18 17 | 2585 -872 19 94
| -60 -36 |
mit 256| 0 -3 0 64 7 29 -.29 10 10 | -139 156 19 132
| 5 39 |
ngs 216| 1 1 0 41 74 -50 -.25 13 12 | -724588 1079584 2221 3718
| 1 81 |
sio 258| -2 0 7 179 152 18 -.28 21 20 | --- --- --- ---
| -70 -14 |
Table 2.1624.2 GPS week: 1624 Day: 2 MJD: 55614.000
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 233| 0 0 1 8 -14 8 -.23 8 8 | -42 -89 15 78
| 46 -4 |
emr 89| 0 5 7 -108 42 -24 .49 19 19 | -2382 948 14 80
| 24 11 |
esa 130| 0 1 -5 -102 -40 -33 .23 10 10 | -2905 203 13 123
| 65 76 |
gfz 196| 0 -2 -1 63 -53 -13 -.17 11 10 | 321 -366 21 101
| -24 56 |
grg 136| 1 0 -5 -61 -96 -46 .66 15 13 | 211 -654 52 218
| 101 -44 |
igr n/a| 0 0 -1 48 2 -13 -.01 6 6 | 4731 355 17 67
| -38 11 |
jpl 142| 1 0 8 -28 64 90 .46 18 17 | 2047 844 18 97
| 71 12 |
mit 256| 0 -2 -1 39 3 8 -.28 10 10 | 110 -533 20 131
| 5 31 |
ngs 216| 0 1 -2 31 122 -7 -.26 14 14 | -108 7 2281 3783
| 8 54 |
sio 258| -3 -1 5 134 131 2 -.30 21 20 | --- --- --- ---
| -64 2 |
Table 2.1624.3 GPS week: 1624 Day: 3 MJD: 55615.000
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 233| 0 1 0 34 -38 -3 -.20 8 8 | -254 -410 21 87
| 59 -3 |
emr 89| 0 0 6 -84 49 37 .52 20 20 | -656 -2009 13 85
| 17 1 |
esa 130| 0 0 -1 -133 15 -52 .19 7 7 | -1487 3410 13 121
| 30 36 |
gfz 196| 1 -1 -5 107 -130 32 -.15 10 10 | -112 503 23 105
| -53 42 |
grg 136| 2 1 -4 -32 -100 -30 .66 15 15 | 276 -81 37 196
| 63 -58 |
igr n/a| 0 1 -1 57 50 20 -.05 5 5 | 6035 -2723 16 70
| -42 -17 |
jpl 142| -4 -1 8 -40 64 68 .47 19 18 | 4000 -2275 17 104
| 102 -159 |
mit 256| 0 -2 -2 36 -26 18 -.32 11 9 | -1893 3786 20 162
| 7 32 |
ngs 216| 1 0 0 41 176 -7 -.23 11 10 | -267301 60501 2451 3798
| 24 -35 |
sio 258| -2 -1 8 119 102 21 -.28 20 20 | --- --- --- ---
| -54 16 |
Table 2.1624.4 GPS week: 1624 Day: 4 MJD: 55616.000
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 233| 0 1 1 39 -11 -14 -.20 9 8 | 805 -1899 19 85
| 19 -27 |
emr 89| 0 3 6 -58 40 41 .48 20 20 | -2529 1200 14 103
| -12 29 |
esa 130| 1 0 -1 -115 26 -8 .18 9 9 | 1283 -526 14 125
| 40 55 |
gfz 196| -1 -2 -2 35 -141 15 -.21 10 10 | 877 -980 26 107
| -68 5 |
grg 136| 3 0 -3 -32 -100 -55 .66 17 14 | 109 58 42 225
| 28 -72 |
igr n/a| -1 0 -1 24 31 13 -.05 4 4 | 3368 206 18 64
| -45 4 |
jpl 142| 0 0 4 -26 72 -70 .47 19 18 | 1810 580 18 101
| -59 -41 |
mit 256| 0 -1 -2 -12 -57 40 -.32 13 12 | -200 342 21 155
| 14 25 |
ngs 216| 0 1 -2 87 150 -24 -.19 10 9 | 784 -1896 2297 3558
| -43 -43 |
sio 258| -2 0 6 68 71 56 -.24 20 19 | --- --- --- ---
| -50 16 |
Table 2.1624.5 GPS week: 1624 Day: 5 MJD: 55617.000
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 233| 1 1 1 40 -32 28 -.24 11 9 | -386 3 17 89
| 40 20 |
emr 89| -1 4 5 -33 38 20 .40 18 18 | -1940 -334 16 131
| -35 28 |
esa 130| 0 -1 -4 -123 -52 -40 .17 9 9 | -1593 -1301 16 149
| 46 105 |
gfz 196| -2 0 0 21 -126 12 -.15 9 9 | 159 159 23 109
| -60 83 |
grg 136| 3 1 -7 -23 -102 -33 .62 16 15 | -82 173 48 234
| 14 -51 |
igr n/a| -1 0 -1 27 12 -12 -.06 5 5 | 3003 -772 18 75
| -36 39 |
jpl 142| 1 0 7 0 44 -35 .52 18 17 | 1795 -340 17 104
| 8 3 |
mit 256| 0 0 -3 10 17 27 -.36 13 12 | -198 338 21 166
| 0 14 |
ngs 216| 0 -2 -2 58 172 -5 -.20 10 7 | -403 3 2090 3553
| -10 -33 |
sio 258| -1 0 6 76 130 19 -.27 21 21 | --- --- --- ---
| -42 12 |
Table 2.1624.6 GPS week: 1624 Day: 6 MJD: 55618.000
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 233| 0 1 3 17 -46 -36 -.24 9 9 | 245 -1149 16 76
| 79 4 |
emr 89| -1 4 5 -39 65 21 .46 20 20 | -1561 1348 16 85
| -55 -4 |
esa 130| 0 0 -4 -128 -48 -10 .20 8 8 | -212 -46 13 105
| 80 86 |
gfz 196| 0 -3 -2 91 -20 30 -.19 10 10 | 881 -1144 23 107
| -47 64 |
grg 136| 3 2 -4 -17 -154 -36 .63 16 14 | 39 267 45 258
| 57 39 |
igr n/a| 0 0 -2 -6 39 -23 -.04 5 5 | 2835 990 16 48
| -27 38 |
jpl 142| 0 -1 2 -46 81 7 .46 18 18 | 2034 1516 19 99
| 11 17 |
mit 256| 1 0 -1 43 -34 26 -.37 14 13 | -311 790 17 161
| 0 21 |
ngs 216| 0 0 0 15 137 7 -.18 10 8 | 212 -1138 2772 4506
| 14 -104 |
sio 258| 0 -1 8 154 112 21 -.31 22 21 | --- --- --- ---
| -66 -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 3.1624.0 GPS week: 1624 Day: 0 MJD: 55612.000
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 --- --- --- --- 38 --- --- --- --- 0 | 33 --- --- --- --- 33 --- --- --- --- 30
2 | 8 20 9 13 14 6 24 15 10 22 5 | 28 39 31 26 36 29 42 30 32 29 28
3 | 30 18 12 14 19 10 15 14 18 33 7 | 59 68 59 61 66 56 64 53 53 50 56
4 | 7 12 7 12 12 7 7 14 9 18 3 | 16 21 18 17 24 14 19 17 20 14 15
5 | 8 16 9 16 11 7 18 9 9 31 4 | 20 30 29 32 33 26 28 26 25 24 23
6E | 15 20 11 14 21 7 18 21 16 34 6 | 117 125 112 121 125 122 90 120 121 114 120
7 | 6 18 10 9 20 6 18 8 10 19 4 | 22 29 25 22 35 22 27 19 27 21 21
8 | 10 15 9 12 13 7 11 10 9 18 4 | 20 24 21 22 28 19 20 20 19 21 18
9 | 10 15 6 13 11 6 12 13 9 14 4 | 14 25 20 24 20 17 21 18 21 19 17
10 | 11 14 9 11 12 3 12 8 9 22 4 | 36 31 37 33 39 36 32 37 41 37 34
11 | 10 14 8 15 23 5 19 9 9 14 4 | 17 28 21 25 38 19 29 18 20 16 18
12 | 9 22 8 8 16 5 23 9 9 21 4 | 12 27 18 16 25 12 28 15 14 16 13
13 | 6 16 8 10 25 7 24 8 8 19 4 | 12 22 16 12 33 14 24 13 22 13 10
14 | 8 15 9 10 20 5 18 11 12 19 4 | 13 24 17 15 29 15 21 17 21 15 13
15 | 11 24 6 14 18 5 24 15 12 17 5 | 12 28 17 18 28 12 24 16 17 18 12
16 | 8 25 9 15 18 6 27 10 10 25 5 | 12 27 17 19 27 14 30 19 20 17 13
17E | 8 16 8 16 17 6 21 12 9 18 4 | 22 34 27 24 32 24 37 29 28 34 26
18 | 11 15 8 16 13 5 21 12 9 24 4 | 15 24 22 29 31 21 24 27 24 26 21
19E | 7 17 9 13 12 5 23 12 11 18 4 | 17 31 22 24 28 19 30 22 24 22 20
20 | 5 19 8 20 11 6 18 12 15 24 5 | 28 29 32 38 35 29 26 29 31 27 27
21 | 8 22 8 10 17 5 28 9 9 21 4 | 19 32 20 19 24 20 34 18 26 31 18
22 | 9 13 7 9 13 6 21 11 9 23 4 | 26 30 31 31 40 29 30 34 29 33 29
23 | 7 26 9 10 18 6 29 19 12 17 5 | 16 30 18 15 29 17 32 21 26 18 14
24 | 5 13 10 11 16 6 13 12 12 25 4 | 17 19 18 18 22 15 20 22 19 26 15
X25 | 10 16 8 13 16 6 23 20 9 --- 5 | 21 28 21 22 31 18 31 27 22 --- 19
26 | 8 13 6 9 19 4 15 10 14 29 4 | 12 19 18 17 24 15 22 14 20 30 13
27 | 9 19 5 14 11 5 13 10 10 16 4 | 12 26 16 24 22 17 24 17 20 19 16
28 | 7 17 7 10 17 7 21 7 11 20 4 | 18 30 22 23 33 19 29 20 20 18 19
29E | 9 22 10 9 17 6 28 11 7 15 4 | 15 21 21 15 25 15 24 12 19 15 14
30 | 6 12 7 9 15 4 13 11 11 13 3 | 21 20 22 23 30 19 21 26 22 25 21
31 | 7 25 8 13 22 4 22 11 11 14 5 | 18 33 23 19 37 19 30 19 24 16 19
32 | 7 15 7 12 15 6 17 9 11 21 4 | 14 19 25 20 28 15 20 17 23 17 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 8 13 17 6 20 12 11 21 |T 22 31 26 26 34 24 30 25 27 26 23
WRMS | 8 18 8 12 16 6 19 11 9 21 |NE 20 28 23 23 31 21 27 22 24 22 20
MEDI | 8 16 8 12 16 6 19 11 10 19 |MD 17 28 21 22 30 19 28 20 22 21 18
Table 3.1624.1 GPS week: 1624 Day: 1 MJD: 55613.000
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 --- --- --- --- 53 --- --- --- --- 0 | 32 --- --- --- --- 47 --- --- --- --- 33
2 | 8 21 8 11 12 7 21 12 15 22 4 | 16 32 20 16 29 19 30 21 19 21 18
3 | 12 16 8 10 23 10 12 6 10 23 4 | 21 30 24 22 36 21 31 20 22 31 23
4 | 6 12 7 10 12 6 9 9 13 15 3 | 16 19 17 17 22 17 18 18 19 18 16
5 | 9 16 12 13 8 7 18 10 14 30 4 | 12 26 20 20 26 17 25 15 17 15 16
6E | 24 19 11 14 19 15 16 15 15 32 6 | 91 93 87 95 87 94 74 96 93 90 93
7 | 6 17 11 8 21 8 18 9 12 18 4 | 16 23 18 15 31 15 23 13 17 15 13
8 | 10 22 9 7 13 8 11 12 14 18 4 | 13 27 17 13 22 15 23 16 17 18 14
9 | 10 14 7 8 11 7 10 9 15 13 3 | 14 22 20 20 23 17 25 19 22 19 18
10 | 9 14 12 12 8 6 9 9 15 19 4 | 12 19 23 19 20 14 19 17 17 15 15
11 | 8 17 10 9 23 8 16 7 9 14 4 | 15 25 21 19 36 17 27 17 21 17 18
12 | 7 21 8 9 18 7 22 9 12 23 4 | 12 27 16 14 26 13 27 15 13 16 14
13 | 7 18 8 11 25 10 19 7 17 16 4 | 14 23 17 16 32 15 22 14 21 14 13
14 | 7 18 11 9 19 7 16 12 16 16 4 | 10 24 12 12 27 10 18 10 13 12 9
15 | 11 25 10 14 16 5 24 12 14 17 5 | 12 30 14 16 26 11 26 14 11 14 12
16 | 7 23 8 14 16 6 25 10 11 25 5 | 12 27 13 17 26 14 30 17 13 17 13
17E | 7 21 10 10 19 5 19 10 17 21 4 | 31 42 35 33 44 33 44 33 32 33 33
18 | 10 15 7 14 15 6 18 11 15 25 4 | 13 19 15 18 22 13 20 16 15 19 14
19E | 8 17 9 14 18 7 20 8 9 17 4 | 16 24 21 24 34 18 28 22 21 18 19
20 | 7 15 5 17 10 11 18 7 16 22 4 | 22 25 23 33 23 21 28 25 21 28 22
21 | 8 21 7 5 16 5 25 8 14 22 4 | 17 30 20 19 21 18 29 18 21 33 17
22 | 8 12 8 7 10 6 17 9 13 22 4 | 19 24 22 20 29 19 23 20 17 23 19
23 | 6 23 8 11 17 9 24 13 15 16 5 | 16 26 16 17 27 15 27 17 16 17 13
24 | 7 13 12 8 14 10 13 12 13 22 4 | 17 17 17 18 20 14 21 21 18 24 16
X25 | 7 12 6 11 17 5 22 21 12 --- 5 | 16 20 16 17 28 14 33 25 14 --- 15
26 | 7 15 10 11 15 7 14 10 13 31 4 | 12 21 18 16 21 13 25 13 12 31 13
27 | 11 16 7 9 14 7 12 7 13 14 4 | 11 23 19 19 25 18 25 19 20 19 17
28 | 5 21 9 6 17 6 18 6 11 22 4 | 13 30 14 12 27 14 29 13 16 19 13
29E | 8 23 12 12 21 5 22 15 13 13 5 | 19 28 26 21 31 20 29 23 21 22 20
30 | 6 12 6 10 15 6 12 10 10 13 3 | 13 18 15 16 26 13 20 19 12 20 15
31 | 7 19 7 9 22 7 18 9 11 14 4 | 12 26 16 18 37 16 25 15 17 15 15
32 | 8 12 7 11 10 10 16 12 15 27 4 | 16 22 23 21 25 16 21 22 13 25 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 9 11 16 8 18 10 13 21 |T 18 27 21 21 29 19 27 20 20 22 19
WRMS | 8 18 9 11 15 7 17 10 12 20 |NE 15 24 18 17 26 16 24 17 16 19 16
MEDI | 7 17 8 10 16 7 18 10 13 19 |MD 15 25 18 18 26 16 25 18 17 19 16
Table 3.1624.2 GPS week: 1624 Day: 2 MJD: 55614.000
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 | 3 --- --- --- --- 104 --- --- --- --- 0 | 27 --- --- --- --- 72 --- --- --- --- 27
2 | 7 23 8 12 13 7 22 9 16 21 4 | 18 36 20 19 27 20 34 19 17 22 18
3 | 8 15 13 9 13 6 13 10 11 22 4 | 14 25 18 16 25 15 22 15 16 26 14
4 | 5 12 19 8 12 6 9 9 16 11 4 | 13 17 24 15 17 12 13 15 15 12 11
5 | 9 15 13 12 8 5 18 11 15 30 4 | 16 26 22 24 27 20 25 20 21 17 19
X6E | 10 19 11 11 18 13 --- 10 13 28 5 | 85 87 97 96 95 85 --- 87 80 97 86
7 | 6 19 10 9 19 5 15 9 11 16 4 | 17 26 21 17 31 16 20 16 19 18 15
8 | 9 18 8 8 14 6 12 10 13 20 4 | 13 23 16 16 22 14 19 17 15 18 14
9 | 11 17 10 9 12 6 13 8 17 14 4 | 9 23 18 19 20 15 20 17 20 17 15
10 | 5 12 10 12 8 3 10 10 13 18 3 | 17 18 22 21 23 17 17 20 20 18 18
11 | 8 14 10 11 22 6 15 11 11 17 4 | 13 24 19 23 37 17 26 16 19 13 16
12 | 8 26 6 9 15 7 22 10 15 23 5 | 11 31 13 15 24 12 26 15 10 14 13
13 | 7 17 8 8 23 7 19 8 16 18 4 | 11 23 17 11 32 11 20 13 14 13 11
14 | 7 24 11 10 18 4 20 10 17 15 4 | 11 28 18 16 27 15 19 14 22 14 14
15 | 13 26 13 14 15 5 24 10 13 17 5 | 9 30 17 17 26 13 24 13 15 13 12
16 | 7 25 10 12 12 5 23 11 13 25 5 | 9 25 16 15 23 11 25 13 14 17 10
17E | 7 20 9 11 15 5 18 9 11 17 4 | 24 38 31 24 34 26 36 24 25 26 25
18 | 11 18 9 15 15 5 18 10 13 25 5 | 13 23 19 27 26 17 19 21 22 22 18
19E | 8 20 10 11 23 6 22 11 12 16 5 | 14 25 18 21 34 15 23 16 20 16 16
20 | 6 16 11 14 11 8 17 13 18 28 5 | 17 20 24 27 24 15 21 22 20 25 17
21 | 9 22 9 11 14 6 24 6 11 23 4 | 18 30 16 20 20 18 28 20 21 30 16
22 | 9 15 11 9 9 5 18 9 10 23 4 | 19 26 24 26 31 22 21 25 23 27 22
23 | 7 24 8 9 16 6 24 11 14 17 4 | 9 27 18 14 27 12 24 13 16 15 11
24 | 5 17 12 9 12 7 13 15 15 23 4 | 11 15 15 15 17 11 17 17 18 18 10
X25 | 8 14 6 11 16 4 24 12 12 --- 4 | 14 23 18 19 28 18 32 22 16 --- 15
26 | 7 14 10 11 15 6 15 10 15 31 4 | 11 20 16 19 19 15 21 13 24 32 13
X27 | 11 20 8 7 14 6 --- 11 18 15 4 | 9 24 18 19 21 15 --- 19 22 19 15
28 | 6 20 10 8 16 5 16 5 12 22 4 | 13 28 17 20 26 16 24 14 16 21 15
29E | 8 24 10 10 21 6 22 10 15 17 5 | 25 32 24 27 32 23 33 24 22 22 23
30 | 5 12 6 10 9 4 9 10 18 14 3 | 15 20 17 18 21 13 19 19 18 22 15
31 | 7 24 8 13 20 6 19 8 12 17 4 | 15 29 21 16 35 16 27 16 21 17 16
32 | 9 15 9 6 10 6 17 17 16 30 4 | 17 19 20 18 21 15 18 26 16 29 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 10 11 15 6 18 10 14 21 |T 16 27 21 21 28 19 23 20 20 22 18
WRMS | 8 19 10 10 13 6 17 10 14 20 |NE 13 24 18 18 25 17 22 17 18 19 15
MEDI | 7 18 10 10 15 6 18 10 13 18 |MD 14 25 18 19 26 15 22 17 19 18 15
Table 3.1624.3 GPS week: 1624 Day: 3 MJD: 55615.000
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 | 4 --- --- --- --- 104 --- --- --- --- 0 | 22 --- --- --- --- 103 --- --- --- --- 23
2 | 7 23 5 12 14 5 21 9 10 21 4 | 17 32 21 19 27 20 32 17 23 20 19
3 | 10 17 6 9 12 4 13 10 9 20 3 | 14 30 19 17 22 15 28 17 16 30 17
4 | 7 13 7 9 15 4 11 10 7 10 3 | 11 13 12 14 19 10 16 15 10 14 9
5 | 9 17 8 13 11 5 17 9 13 28 4 | 16 27 23 29 30 21 24 24 22 19 21
X6 | 30 31 --- 47 108 22 --- 17 52 --- 18 | 68 90 --- 81 98 78 --- 75 94 --- 73
7 | 9 19 7 8 19 5 18 9 12 14 4 | 16 23 16 13 30 15 22 14 21 17 14
8 | 9 19 5 7 13 3 13 11 12 18 3 | 13 22 13 11 18 11 17 14 12 19 11
9 | 10 21 5 8 14 4 12 12 13 12 4 | 14 25 15 21 21 17 24 22 23 20 16
10 | 6 12 5 10 10 5 9 7 9 17 3 | 16 18 22 25 22 17 21 22 18 17 18
11 | 6 20 7 8 21 3 16 11 16 18 4 | 15 30 21 19 38 18 28 19 19 20 18
12 | 6 21 5 9 15 4 20 10 16 23 4 | 10 27 14 18 22 13 27 16 19 13 13
13 | 7 16 6 10 25 5 21 10 11 14 4 | 12 24 13 17 32 12 24 15 16 16 12
14 | 8 21 7 10 16 2 22 6 14 15 4 | 12 24 15 17 27 14 22 12 17 14 13
15 | 9 24 11 10 17 4 27 13 8 17 5 | 13 29 16 15 26 11 27 17 17 17 12
16 | 7 23 8 11 16 6 25 12 15 23 5 | 9 25 18 12 21 15 27 17 21 21 12
17E | 7 17 6 10 12 3 23 8 10 15 4 | 23 36 29 26 33 27 38 27 30 29 27
18 | 9 17 7 15 7 5 19 8 12 22 4 | 14 24 19 28 26 20 24 21 23 21 19
19E | 7 24 9 11 13 4 23 12 9 13 4 | 14 29 20 19 26 17 26 19 15 17 16
20 | 8 15 10 16 10 5 20 15 7 32 5 | 24 28 25 33 29 24 29 30 23 33 24
21 | 6 24 6 9 16 5 23 7 13 21 4 | 15 29 16 15 19 16 26 16 20 29 15
22 | 9 14 5 9 6 4 19 8 9 21 3 | 21 29 27 32 33 26 26 28 27 27 25
23 | 6 24 7 10 17 5 29 6 10 16 4 | 14 31 16 18 28 16 32 15 17 21 14
24 | 6 20 9 6 12 5 14 18 13 18 4 | 13 22 16 17 18 15 22 23 20 22 15
X25 | 7 14 6 12 14 4 23 9 11 --- 4 | 13 22 16 18 26 15 33 17 18 --- 13
26 | 8 20 10 12 11 5 14 17 11 31 5 | 14 24 16 18 22 13 23 18 15 30 13
27 | 10 23 6 9 16 4 11 16 10 15 4 | 9 27 12 19 20 14 22 23 18 19 13
28 | 7 16 6 8 21 3 17 7 8 21 4 | 10 25 14 15 25 12 25 12 13 22 12
29E | 7 26 8 10 22 4 22 12 11 15 4 | 19 35 28 25 26 24 32 21 23 24 23
30 | 5 15 5 8 15 5 11 10 13 13 3 | 14 25 19 17 24 17 20 20 20 23 16
31 | 7 20 8 12 21 7 20 6 15 14 4 | 16 27 17 13 36 18 26 14 20 16 15
32 | 11 15 10 8 10 5 20 20 8 31 5 | 14 21 22 18 21 15 19 21 15 21 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 7 10 15 5 19 11 11 20 |T 16 28 18 21 27 21 25 20 21 21 18
WRMS | 8 20 7 10 15 5 18 9 10 20 |NE 14 25 17 18 25 19 24 18 18 20 15
MEDI | 7 20 7 10 15 5 19 10 11 18 |MD 14 27 16 18 26 16 25 18 19 20 15
Table 3.1624.4 GPS week: 1624 Day: 4 MJD: 55616.000
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 | 4 --- --- --- --- 59 --- --- --- --- 0 | 20 --- --- --- --- 61 --- --- --- --- 19
2 | 8 25 9 8 17 4 20 12 11 22 4 | 16 34 23 18 30 20 31 16 23 19 19
3 | 10 16 7 9 19 3 14 13 10 22 4 | 18 29 20 19 25 18 26 22 21 33 19
4 | 8 15 7 11 15 3 9 15 9 15 4 | 10 14 15 13 17 12 17 17 15 20 11
5 | 8 16 8 11 9 6 16 11 11 28 4 | 16 29 23 27 27 21 26 21 17 19 18
6 | 9 17 7 9 35 4 13 15 9 34 5 | 47 48 54 45 68 49 68 47 57 58 47
7 | 7 21 9 7 19 4 21 9 9 14 4 | 15 28 19 12 29 15 23 14 18 17 14
8 | 10 18 7 8 10 3 14 10 9 17 3 | 12 25 17 16 18 13 18 12 17 19 13
9 | 10 23 7 10 12 4 13 15 14 11 4 | 13 29 18 16 16 13 20 23 18 17 14
10 | 7 12 6 13 11 5 8 10 11 18 3 | 16 19 17 25 21 17 18 20 19 16 16
11 | 7 25 13 7 23 4 16 12 9 15 4 | 12 29 21 18 37 17 23 18 18 19 15
12 | 9 24 8 19 16 6 23 12 13 22 5 | 12 29 19 23 21 16 27 20 17 16 14
13 | 8 17 8 7 25 4 17 11 11 16 4 | 13 23 17 16 32 12 21 18 18 18 13
14 | 8 20 6 10 17 3 22 8 9 17 4 | 12 23 16 18 26 12 20 11 15 16 11
15 | 12 22 10 11 18 2 25 18 9 18 5 | 12 28 15 18 27 9 24 18 9 14 10
16 | 6 22 6 8 15 4 26 13 8 23 4 | 12 28 18 15 22 18 31 18 20 22 16
17E | 13 20 11 7 14 6 29 12 9 15 5 | 28 44 34 34 38 34 47 33 37 39 34
18 | 11 18 8 13 12 5 19 9 10 25 4 | 14 24 15 21 23 15 20 20 14 22 14
19E | 6 21 12 11 14 5 22 12 12 13 4 | 16 26 22 22 27 20 25 19 25 21 19
20 | 9 16 12 16 15 5 17 17 11 31 5 | 20 23 20 34 23 21 22 28 22 30 21
21 | 9 23 9 10 19 5 21 7 11 22 4 | 16 31 19 18 17 18 25 17 23 30 16
22 | 9 15 7 9 10 5 18 9 11 20 4 | 19 27 22 24 29 22 25 24 21 23 20
23 | 8 24 6 8 17 5 26 9 9 17 4 | 15 31 16 15 27 14 28 15 19 20 14
24 | 7 16 13 8 15 3 14 17 12 13 4 | 12 18 13 21 18 16 18 22 21 20 14
X25 | 6 13 8 11 12 5 23 9 11 --- 4 | 16 24 24 18 26 17 31 17 17 --- 17
26 | 9 17 8 8 10 4 14 16 12 30 4 | 12 24 13 15 19 10 21 14 11 29 11
27 | 10 22 9 9 10 3 14 20 9 15 4 | 10 26 16 16 18 12 20 23 17 17 13
28 | 6 21 7 10 22 4 19 9 13 18 4 | 14 27 18 20 27 15 27 16 20 22 15
29E | 10 20 7 10 16 5 22 9 12 15 4 | 22 29 27 24 23 23 32 22 24 24 22
30 | 6 14 6 6 15 4 12 12 7 12 3 | 16 22 19 16 21 18 19 20 21 23 17
31 | 6 24 8 8 19 6 19 9 7 14 4 | 15 31 20 14 33 18 26 16 18 18 16
32 | 9 15 11 10 13 5 17 20 12 30 5 | 14 17 20 22 22 15 18 22 20 21 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 9 10 17 4 19 13 10 20 |T 16 27 20 20 26 19 25 20 20 22 17
WRMS | 8 20 9 10 14 4 18 12 9 19 |NE 14 25 18 18 24 17 23 18 18 20 15
MEDI | 8 20 8 9 15 4 18 12 11 17 |MD 15 27 19 18 25 17 24 19 19 20 16
Table 3.1624.5 GPS week: 1624 Day: 5 MJD: 55617.000
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 --- --- --- --- 125 --- --- --- --- 0 | 23 --- --- --- --- 96 --- --- --- --- 24
2 | 9 23 9 9 16 4 23 14 10 23 5 | 17 32 22 17 29 18 32 17 24 19 19
3 | 11 14 7 9 14 5 12 14 12 22 4 | 15 27 24 20 25 18 28 20 20 34 19
4 | 6 15 12 6 14 6 9 15 9 11 3 | 8 17 13 12 16 10 18 14 11 18 9
5 | 9 15 13 8 11 5 18 12 8 29 4 | 14 26 21 23 28 19 26 20 19 18 17
6 | 10 15 8 8 16 5 13 16 10 32 4 | 33 43 30 35 40 39 34 37 41 39 35
7 | 8 20 11 8 16 5 16 12 9 17 4 | 14 27 17 13 27 13 24 14 17 17 13
8 | 12 18 7 5 10 5 10 11 9 17 3 | 13 22 15 11 15 11 19 12 14 17 11
9 | 11 16 12 7 11 5 11 15 9 13 4 | 14 25 21 18 22 16 22 21 22 16 16
10 | 8 11 8 9 9 3 10 9 7 18 3 | 13 17 19 19 20 15 16 18 15 14 15
11 | 8 16 8 8 22 7 16 12 12 17 4 | 17 30 23 22 40 21 27 21 24 19 20
12 | 11 23 7 10 16 6 21 12 6 23 4 | 11 28 19 18 23 17 28 17 15 15 15
13 | 7 18 8 10 25 6 18 12 10 15 4 | 14 26 14 15 33 12 23 18 17 18 13
14 | 11 18 5 9 19 7 23 9 10 16 4 | 12 22 15 16 28 14 23 13 14 16 12
15 | 12 23 10 11 17 5 24 15 7 19 5 | 12 25 16 16 28 11 22 15 11 16 11
16 | 9 22 11 9 14 4 22 15 13 22 5 | 10 26 16 17 25 14 28 15 18 20 13
17E | 30 15 10 12 15 9 20 15 9 17 6 | 82 84 84 77 87 73 82 78 75 75 79
18 | 11 17 9 18 14 5 17 12 11 26 5 | 14 21 20 29 23 15 20 22 17 22 16
19E | 11 26 10 12 19 5 17 13 11 14 5 | 14 29 22 22 29 18 24 18 21 20 18
20 | 8 17 8 13 14 5 17 16 11 32 5 | 22 29 23 29 28 22 28 26 22 29 23
21 | 9 21 12 7 15 4 23 10 10 26 5 | 13 24 18 14 22 14 24 16 19 30 13
22 | 9 13 7 9 10 5 16 11 8 23 4 | 18 23 25 24 29 19 25 25 19 24 21
23 | 7 24 10 7 17 5 28 14 10 18 5 | 15 31 19 17 27 17 31 19 17 21 15
24 | 7 13 6 8 14 4 13 15 10 13 3 | 14 19 17 18 19 14 21 20 19 18 16
X25 | 10 17 9 10 17 5 23 17 8 --- 5 | 18 26 25 23 27 21 37 21 19 --- 19
26 | 9 17 10 7 13 3 10 17 7 30 4 | 12 22 15 16 20 10 19 12 12 32 12
27 | 12 20 9 7 11 5 12 20 7 13 4 | 10 25 17 17 21 12 20 21 15 15 13
28 | 7 19 11 7 22 5 22 11 9 18 4 | 12 25 17 13 26 11 28 14 14 18 12
29E | 11 19 10 9 16 5 25 10 6 18 4 | 14 24 23 17 27 17 26 16 17 17 16
30 | 9 13 10 7 15 6 11 15 10 13 4 | 15 23 21 21 24 17 21 21 21 21 17
31 | 7 25 10 11 22 5 18 8 9 13 4 | 14 30 18 17 36 15 23 13 15 17 14
32 | 8 16 7 8 17 4 16 15 10 27 4 | 11 17 15 13 21 11 19 16 17 17 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 9 9 16 5 18 13 10 21 |T 16 27 21 20 27 20 26 20 20 22 18
WRMS | 9 18 9 9 15 5 17 12 7 21 |NE 14 24 18 18 25 17 24 17 17 20 15
MEDI | 9 17 9 9 15 5 17 14 9 18 |MD 14 25 19 17 27 15 24 18 17 18 15
Table 3.1624.6 GPS week: 1624 Day: 6 MJD: 55618.000
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 --- --- --- --- 156 --- --- --- --- 0 | 28 --- --- --- --- 93 --- --- --- --- 28
2 | 9 27 10 11 14 6 19 15 9 22 5 | 21 35 23 16 29 20 32 20 22 25 22
3 | 9 16 7 9 16 6 11 14 10 26 4 | 17 29 20 23 23 22 29 21 21 35 21
4 | 8 18 6 8 14 6 10 13 10 12 3 | 20 24 22 21 20 20 22 24 18 24 20
5 | 9 18 10 12 10 4 16 13 7 30 4 | 20 33 30 31 33 26 28 28 26 24 25
6 | 9 16 7 9 14 5 11 16 14 36 4 | 66 68 61 66 74 66 62 65 69 64 67
7 | 7 22 10 8 18 5 19 14 6 16 4 | 17 26 19 18 30 15 23 16 17 18 16
8 | 11 17 7 7 11 5 12 14 6 18 3 | 14 21 16 15 20 11 20 15 15 20 13
9 | 11 22 8 7 14 3 13 17 12 16 4 | 13 29 20 18 22 17 23 18 23 19 17
10 | 10 16 6 8 11 4 10 12 7 22 3 | 18 25 27 28 28 24 24 26 28 18 24
11 | 7 20 11 9 20 5 18 13 11 17 4 | 14 28 23 20 39 18 23 19 17 17 16
12 | 10 24 9 10 17 6 22 9 10 24 5 | 16 32 21 21 24 20 29 18 15 17 18
13 | 9 20 7 11 24 4 22 13 7 17 4 | 13 28 19 18 32 13 24 22 17 22 16
14 | 9 25 8 9 18 3 24 12 8 16 4 | 12 25 15 15 28 14 23 16 10 20 11
15 | 12 23 10 10 17 4 24 15 11 20 5 | 11 28 17 16 27 14 25 15 14 21 14
16 | 8 22 9 11 14 4 25 15 10 24 5 | 13 30 19 20 24 20 33 22 23 25 18
17 | 20 22 8 10 16 6 17 15 13 16 5 | 76 101 97 90 93 91 98 99 94 86 93
18 | 10 17 7 15 12 4 18 12 11 25 4 | 16 24 22 26 31 20 22 26 16 27 19
19E | 10 25 9 11 17 5 21 15 11 16 5 | 15 31 21 18 31 18 25 18 18 22 17
20 | 7 17 6 16 12 4 18 17 13 31 5 | 24 28 28 33 33 27 28 29 31 25 27
21 | 9 18 10 6 17 6 20 12 10 24 4 | 18 30 22 21 21 22 29 20 21 33 19
22 | 8 16 8 8 10 4 18 12 11 22 4 | 26 31 33 33 40 29 26 35 29 35 30
23 | 8 25 7 11 16 6 30 14 8 19 5 | 15 32 19 19 28 18 33 18 16 23 17
24 | 7 15 13 9 11 5 14 17 13 18 4 | 13 18 17 17 19 16 19 20 20 19 14
X25 | 9 14 7 9 16 4 22 14 12 --- 4 | 20 28 23 21 29 20 34 19 15 --- 20
26 | 7 20 8 6 15 5 13 13 8 32 4 | 11 22 17 15 19 13 21 12 16 33 14
X27 | 11 24 7 7 12 4 --- 21 8 --- 5 | 10 30 17 17 21 15 --- 21 17 --- 14
28 | 9 19 7 8 19 4 19 12 12 17 4 | 18 28 19 21 26 19 29 22 24 26 19
29E | 10 23 8 7 16 6 24 12 11 15 4 | 16 33 24 23 29 24 32 20 23 24 23
30 | 7 11 6 8 13 4 9 16 8 14 3 | 19 26 24 27 26 23 25 27 24 24 22
31 | 8 20 10 9 21 6 17 10 11 15 4 | 15 25 20 17 35 17 25 18 20 21 18
32 | 8 17 8 9 13 5 18 15 8 25 4 | 14 20 21 21 27 16 20 20 24 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 8 10 16 5 18 14 10 22 |T 19 31 25 24 31 25 29 24 23 27 22
WRMS | 9 20 8 10 14 5 18 13 8 21 |NE 16 27 21 21 27 21 25 21 19 23 18
MEDI | 9 20 8 9 15 5 18 14 10 19 |MD 16 28 21 21 28 20 25 20 20 24 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 4.1624 GPS week: 1624 MJD: 55612.0-55618.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 |U 7 10 25 |U 12 12 39 |U 6 6 13 |
emr | emr 2972 |U 10 12 28 |U 15 13 39 | 7 7 15 |
esa | esa 2962 | 7 9 25 |U 12 12 37 | 6 6 13 |
gfz | gfz 2965 |U 7 9 27 |U 12 12 38 |U 6 5 13 |
grg | grg 2972 | 8 11 25 |U 12 14 39 | 8 6 18 |
igr | igr 2971 | 7 9 25 | 12 12 36 | 6 6 11 |
igs | igs 2962 | 7 9 25 | 13 12 38 | 6 5 12 |
jpl | jpl 2917 |U 9 11 27 |U 14 13 37 | 7 7 17 |
mit | mit 2976 |U 19 15 48 |U 35 39 527 |U 6 6 14 |
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 5.1624.0 GPS week: 1624 Day: 0 MJD: 55612.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3019 | 7 13 29 | ---- ---- ---- | 7 9 16 |
emr | emr 2972 | 8 7 24 | ---- ---- ---- | 7 9 15 |
esa | esa 2976 | 6 7 24 | ---- ---- ---- | 7 8 12 |
gfz | gfz 2968 | 6 5 20 | ---- ---- ---- | 7 8 12 |
grg | grg 2976 | 6 10 16 | ---- ---- ---- | 8 8 20 |
igr | igr 2976 | 6 7 26 | ---- ---- ---- | 7 8 10 |
igs | igs 2975 | 6 8 25 | ---- ---- ---- | 6 8 11 |
jpl | jpl 2971 | 8 7 24 | ---- ---- ---- | 6 9 16 |
mit | mit 2976 | 7 6 23 | ---- ---- ---- | 7 11 14 |
Table 5.1624.1 GPS week: 1624 Day: 1 MJD: 55613.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 6 9 14 | 6 7 36 | 8 4 11 |
emr | emr 2972 | 8 11 22 | 6 6 34 | 7 5 11 |
esa | esa 2976 | 6 7 15 | 5 7 33 | 7 4 13 |
gfz | gfz 2972 | 5 7 16 | 6 7 37 | 5 3 13 |
grg | grg 2976 | 6 11 14 | 7 7 38 | 8 6 23 |
igr | igr 2976 | 6 7 16 | 5 7 34 | 5 4 11 |
igs | igs 2976 | 6 7 16 | 5 6 33 | 6 4 12 |
jpl | jpl 2967 | 8 12 22 | 5 8 42 | 7 6 16 |
mit | mit 2976 | 84 54 170 | 6 8 38 | ---- ---- ---- |
Table 5.1624.2 GPS week: 1624 Day: 2 MJD: 55614.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 11 10 26 | 27 21 52 | 6 3 10 |
emr | emr 2976 | 13 16 29 | 28 22 52 | 7 6 11 |
esa | esa 2976 | 11 13 29 | 25 20 48 | 6 5 12 |
gfz | gfz 2973 | 11 12 29 | 26 19 48 | 6 5 11 |
grg | grg 2976 | 12 15 30 | 24 22 50 | 8 5 19 |
igr | igr 2976 | 11 12 28 | 25 19 45 | 6 6 10 |
igs | igs 2976 | 11 12 28 | 26 20 47 | 6 4 10 |
jpl | jpl 2781 | 11 14 27 | 29 20 48 | 8 6 13 |
mit | mit 2976 | 11 11 26 | 26 18 46 | 6 4 11 |
Table 5.1624.3 GPS week: 1624 Day: 3 MJD: 55615.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3008 | 6 9 16 | 13 12 31 | 8 7 12 |
emr | emr 2958 | 9 14 24 | 16 13 29 | 8 7 17 |
esa | esa 2880 | 6 9 18 | 13 14 32 | 6 7 10 |
gfz | gfz 2920 | 6 8 18 | 13 13 31 | 6 7 12 |
grg | grg 2948 | 6 10 17 | 15 16 35 | 8 6 16 |
igr | igr 2947 | 6 8 20 | 14 13 28 | 6 7 10 |
igs | igs 2880 | 6 9 18 | 16 13 35 | 6 7 11 |
jpl | jpl 2874 | 8 12 25 | 15 12 28 | 7 8 15 |
mit | mit 2976 | 6 8 20 | 152 176 2965 | 6 6 10 |
Table 5.1624.4 GPS week: 1624 Day: 4 MJD: 55616.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 9 10 27 | 12 12 50 | 6 5 14 |
emr | emr 2976 | 9 10 25 | 15 13 47 | 6 7 16 |
esa | esa 2976 | 7 8 19 | 11 11 43 | 5 4 15 |
gfz | gfz 2976 | 6 7 20 | 12 12 44 | 5 4 13 |
grg | grg 2976 | 6 7 22 | 12 12 43 | 7 5 15 |
igr | igr 2976 | 7 8 21 | 12 11 45 | 5 4 13 |
igs | igs 2976 | 7 7 21 | 12 11 47 | 5 4 13 |
jpl | jpl 2972 | 8 10 23 | 13 12 42 | 7 6 21 |
mit | mit 2976 | 9 7 25 | 12 12 50 | 6 6 18 |
Table 5.1624.5 GPS week: 1624 Day: 5 MJD: 55617.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 6 9 36 | 10 10 33 | 4 5 13 |
emr | emr 2976 | 11 12 45 | 13 14 40 | 6 6 17 |
esa | esa 2976 | 8 7 43 | 10 11 33 | 6 6 16 |
gfz | gfz 2976 | 8 8 44 | 10 12 39 | 6 5 13 |
grg | grg 2976 | 8 8 50 | 9 11 35 | 7 5 16 |
igr | igr 2976 | 8 8 40 | 10 10 32 | 6 6 12 |
igs | igs 2976 | 7 8 43 | 10 11 32 | 6 5 14 |
jpl | jpl 2975 | 9 10 44 | 11 13 30 | 6 7 19 |
mit | mit 2976 | 8 8 46 | 10 12 33 | 6 6 14 |
Table 5.1624.6 GPS week: 1624 Day: 6 MJD: 55618.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 8 12 25 | 7 11 34 | 5 6 14 |
emr | emr 2976 | 10 14 26 | 11 11 35 | 8 9 18 |
esa | esa 2976 | 7 13 25 | 7 11 31 | 6 6 14 |
gfz | gfz 2976 | 9 13 40 | 7 11 32 | 6 5 15 |
grg | grg 2976 | 8 14 27 | 7 14 35 | 8 6 14 |
igr | igr 2976 | 7 11 23 | 7 10 31 | 6 6 13 |
igs | igs 2976 | 7 13 24 | 7 11 31 | 6 5 13 |
jpl | jpl 2880 | 8 11 26 | 9 12 31 | 7 10 21 |
mit | mit 2976 | 7 11 25 | 7 11 33 | 6 6 16 |
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 6.1624 GPS week: 1624 MJD: 55612.500-55618.500
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 | 29 -40 122 280 -8 | -3 19
| 34 30 84 56 5 | 1
emr uuuuu | 15 7 134 81 15 | 11 27
| 26 31 79 114 8 | 10
esa uuuuu | -54 -47 -120 -164 -8 | -15 25
| 14 17 107 106 10 | 1
gfz uuuuu | -26 65 -27 88 -5 | -7 22
| 25 25 86 63 8 | 1
grg uuuux | 66 -56 84 219 -15 | 4 20
| 42 26 49 69 19 | 2
igr xxxxx | 5 41 1 -35 -3 | -6 17
| 16 15 52 88 8 | 2
irf xxxxx | 22 6 -50 39 2 | -3 24
| 16 14 83 90 18 | 7
jpl uuuuu | 47 -1 44 204 -10 | -18 24
| 53 54 34 110 11 | 2
mit uuuuu | -7 1 -64 -33 4 | 8 26
| 16 16 143 104 19 | 8
ngs uuuuu | 22 4 -26 -258 -6 | -13 19
| 63 16 62 179 16 | 0
sio uuuuu | 22 64 225 210 4 | 1 25
| 30 22 92 116 17 | 6
Table 7.1624.0 GPS week: 1624 Day: 0 MJD: 55612.500
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 | 101 12 198 240 -14 | -4 19
emr uuuuu | 50 -24 180 -39 24 | -3 16
esa uuuuu | -48 -46 -144 -85 -22 | -13 24
gfz uuuuu | -34 121 -177 56 -16 | -6 22
grg uuuux | 115 -56 142 223 9 | 2 18
igr xxxxx | 19 23 2 -39 -5 | -9 18
irf xxxxx | 41 5 6 60 12 | -14 22
jpl uuuuu | 12 25 104 137 -14 | -22 28
mit uuuuu | 3 -3 32 6 11 | -2 17
ngs uuuuu | -38 -19 -37 -176 -21 | -12 18
sio uuuuu | 70 61 291 207 6 | -6 20
Table 7.1624.1 GPS week: 1624 Day: 1 MJD: 55613.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 6 -79 21 258 -13 | -5 19
emr uuuuu | 37 -19 232 16 15 | 1 20
esa uuuuu | -58 -54 -315 -28 -19 | -15 25
gfz uuuuu | 14 54 -101 82 -11 | -8 22
grg uuuux | 73 -102 101 105 -53 | 4 20
igr xxxxx | 9 46 -25 -189 -19 | -9 18
irf xxxxx | 27 10 46 112 21 | -12 22
jpl uuuuu | 63 70 66 26 -26 | -20 27
mit uuuuu | -12 5 96 49 23 | -1 18
ngs uuuuu | -54 9 30 -405 -24 | -14 19
sio uuuuu | 41 80 341 291 20 | -5 20
Table 7.1624.2 GPS week: 1624 Day: 2 MJD: 55614.500
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 | 37 -21 104 287 -10 | -2 20
emr uuuuu | 22 1 69 126 16 | 7 26
esa uuuuu | -43 -40 -177 -273 -10 | -14 24
gfz uuuuu | -23 49 9 99 -13 | -6 23
grg uuuux | 77 -76 68 154 -12 | 3 20
igr xxxxx | 22 63 -14 -98 -6 | -7 18
irf xxxxx | 33 25 28 180 16 | -6 26
jpl uuuuu | 21 -46 47 175 -1 | -17 24
mit uuuuu | 2 20 55 111 19 | 6 26
ngs uuuuu | -21 17 -140 -511 -14 | -13 19
sio uuuuu | 31 89 312 409 18 | -1 25
Table 7.1624.3 GPS week: 1624 Day: 3 MJD: 55615.500
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 -43 1 206 -7 | -2 19
emr uuuuu | -2 -1 60 14 23 | 12 26
esa uuuuu | -37 -14 -48 -123 -6 | -14 24
gfz uuuuu | -43 69 -33 5 -7 | -6 23
grg uuuux | 57 -47 36 256 -4 | 2 20
igr xxxxx | 16 58 -33 19 -1 | -6 17
irf xxxxx | -1 16 -33 55 13 | -1 24
jpl uuuuu | 158 -86 48 313 -17 | -15 22
mit uuuuu | -33 9 0 12 18 | 10 27
ngs uuuuu | 34 -8 -58 -264 -10 | -13 19
sio uuuuu | -17 70 213 244 18 | 2 26
Table 7.1624.4 GPS week: 1624 Day: 4 MJD: 55616.500
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 | 30 -34 142 264 0 | -2 19
emr uuuuu | -26 -3 55 8 16 | 16 30
esa uuuuu | -52 -55 -36 -105 -5 | -15 25
gfz uuuuu | -2 53 78 211 0 | -8 22
grg uuuux | 75 -43 43 290 -22 | 5 20
igr xxxxx | -1 30 40 77 -1 | -5 17
irf xxxxx | 3 -15 -114 -28 -3 | 2 25
jpl uuuuu | 44 44 19 321 -16 | -16 23
mit uuuuu | -22 -29 -173 -106 -1 | 14 30
ngs uuuuu | 46 28 -12 -351 6 | -13 19
sio uuuuu | -13 35 139 122 3 | 5 28
Table 7.1624.5 GPS week: 1624 Day: 5 MJD: 55617.500
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 -47 209 341 -5 | -2 19
emr uuuuu | 2 28 111 155 9 | 21 34
esa uuuuu | -75 -53 -120 -313 -3 | -15 25
gfz uuuuu | -53 53 24 97 5 | -8 22
grg uuuux | 81 -21 155 287 -12 | 5 20
igr xxxxx | -9 29 -60 -37 6 | -4 17
irf xxxxx | 30 -7 -119 -51 -21 | 4 25
jpl uuuuu | 27 -15 4 158 8 | -17 23
mit uuuuu | 16 -7 -204 -135 -22 | 16 31
ngs uuuuu | 63 3 48 -4 7 | -12 20
sio uuuuu | 18 35 173 91 -18 | 8 29
Table 7.1624.6 GPS week: 1624 Day: 6 MJD: 55618.500
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 -69 180 365 -8 | -3 19
emr uuuuu | 23 65 228 286 1 | 25 35
esa uuuuu | -67 -70 0 -220 6 | -18 25
gfz uuuuu | -45 57 9 62 4 | -9 22
grg uuuux | -20 -47 44 220 -9 | 7 19
igr xxxxx | -19 37 94 21 2 | -5 17
irf xxxxx | 19 10 -165 -59 -21 | 3 26
jpl uuuuu | 2 -1 22 296 -7 | -15 21
mit uuuuu | -2 10 -257 -169 -23 | 16 31
ngs uuuuu | 123 -4 -10 -93 18 | -13 20
sio uuuuu | 24 76 103 106 -21 | 7 29
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