[IGSREPORT-18300] Wk 1569 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Feb 18 05:22:47 PST 2010
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IGS Electronic Report 18 Feb 05:23:11 PST 2010 Message Number 18300
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1569 (Jan 31, 2010 - Feb 06, 2010)
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 (weights are those from the orbit combination).
Pole rate combination uses only centres providing estimated pole rates.
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:
igs1569[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1569[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1569[0-6].cls IGS GPS clock combination summary report.
igs15697.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15697.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 1478, a new solution from CNES/GRGS (GRG) is included for
evaluation and statistics only.
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 | EMR | WTZR WTZR
0 | ESA | UNSA
0 | GFZ | 14 15 16 23 26 ABPO ALIC AREQ ASPA BJFS CAS1 CHAT
0 | GFZ | CHUR DARW DAV1 DGAR GLSV GUAT HARB HOB2 HOLM KARR
0 | GFZ | MAC1 MAL2 PDEL PERT RABT RESO REUN SUTM SYOG THU3
0 | GFZ | TRO1 TWTF VILL WUHN YAR2 YELL
0 | GRG | ONSA ULAB
0 | JPL | 32
0 | MIT | 7 25 7 25 26 HARB
1 | ALL | 1
1 | COD | WROC WROC
1 | EMR | 26 12 15 16 19 25 26 28 29 WTZR WTZR
1 | GFZ | 5 6 14 15 16 26 AMC2 AUCK BAKO BRUS BUE1 CAS1 CEDU
1 | GFZ | COCO CONZ CRO1 DARW DAV1 GLSV GUAM GUAT HARB HOFN
1 | GFZ | HOLM HYDE KIRU KIT3 KOUR MAS1 MAW1 MCM4 MDO1 MIZU
1 | GFZ | NICO NRMD NTUS NYAL PERT PIE1 PIMO PRDS SANT SCUB
1 | GFZ | SYOG TLSE TRO1 TSKB TWTF UNSA WAB2 WSRT WUHN YAKT
1 | GFZ | YAR2 YELL
1 | GRG | NRC1
1 | JPL | 15 16 19 23 26 29 32
1 | MIT | 25 26 25 26
2 | COD | 25
2 | EMR | 25 26 26 KHAJ WTZR KHAJ WTZR
2 | ESA | 10 10 25 CEDU UNSA
2 | GFZ | 5 15 23 29 31 ALGO ALIC ALRT AREQ BOR1 BRFT BRUS
2 | GFZ | BUE1 CAS1 CEDU COCO CONZ DARW FAA1 GLSV GRAZ GUAM
2 | GFZ | GUAT HARB HOB2 HRAO KIRU KIT3 LPGS NRC1 NYAL ONSA
2 | GFZ | OUS2 PIMO PRDS QAQ1 RESO SUTH SUTM THTI THU3 TIDB
2 | GFZ | TOW2 TWTF ULAB WSRT WTZR YAKT YELL YKRO
2 | GRG | NRC1
2 | JPL | 32 BAKO GUAT
2 | MIT | 10 25 26 10 26 PTBB HARB PTBB TRO1
3 | COD | 26
3 | EMR | 26 HARB WTZR WTZR
3 | GFZ | 9 13 17 21 29 ABPO ADE1 ALGO ALIC ALRT AMC2 AREQ
3 | GFZ | ARTU ASPA AUCK BAKO BOGT BOR1 CAS1 CHUR COCO CONZ
3 | GFZ | DGAR DUBO GLSV GRAZ GUAM GUAT HARB HOB2 HOFN HRAO
3 | GFZ | HRM1 KIRU MAC1 MAL2 MAS1 MAW1 MCM4 MIZU NRC1 NTUS
3 | GFZ | NYAL PIE1 PIMO PRDS RABT RAMO RESO SANT SEY1 SFER
3 | GFZ | SHAO STJO SYOG THU3 TOW2 TSKB UNSA WAB2 WHIT WSRT
3 | GFZ | WTZR WUHN YAKT YAR2 YELL ZIMM
3 | GRG | ONSA
3 | JPL | 15 23 32 DGAR
3 | MIT | 25 25 CEDU CEDU
3 | NGS | 1
4 | COD | NRIL
4 | EMR | 3 3 26 WTZR WTZR
4 | ESA | MAL2
4 | GFZ | 3 5 14 17 ALRT ARTU AUCK BOR1 BRUS CAS1 DGAR GUAM
4 | GFZ | HARB MAC1 MAS1 NICO NRC1 NYA1 NYAL OHI2 OUS2 QIKI
4 | GFZ | RAMO STJO TEHN TIDB TLSE TOW2 TSKB WAB2 YKRO YSSK
4 | GRG | SPT0
4 | JPL | 3 26 32 DGAR
4 | MIT | 25 26 3 25 26 COCO HARB
5 | ALL | 1 1
5 | EMR | 3 25 26 3 25 26 WTZR WTZR
5 | GFZ | 3 9 14 15 22 23 24 28 ADE1 AREQ ASPA BAKO BOR1 BUE1
5 | GFZ | CEDU CHAT CHPI CONZ GRAZ GUAM HARB HOB2 HOLM HYDE
5 | GFZ | KIRU LPGS MAC1 MAL2 MATE MCM4 MDO1 MIZU NTUS OHI2
5 | GFZ | OUS2 PIMO QIKI RABT RAMO SCUB SHAO SUTH SUWN TSKB
5 | GFZ | VILL WAB2
5 | GRG | ONSA
5 | JPL | 3 32 DGAR
5 | MIT | 3 25 26 3 25 26
6 | ALL | 1 1
6 | EMR | 3 25 3 25 WTZR WTZR
6 | GFZ | 5 15 23 26 28 ADE1 AMC2 AREQ ASPA AUCK CHAT EIL1
6 | GFZ | FAA1 GLPS GOLD GUAT HARB KIT3 KOUC LPGS MCM4 MDO1
6 | GFZ | METS NRC1 OUS2 RESO SANT SCUB SFER UNSA WES2 WUHN
6 | GFZ | YAKT YELL YSSK
6 | GRG | ONSA
6 | JPL | 26 32 DGAR
6 | MIT | 3 25 3 25 26 MAW1 MAW1
5. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G17 | 2010_02_02 | 2010017
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 G03 | | | | | | 1 | |
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 | .0 1.6 .5 -18 -1 -27 -.07
EMR | -1.1 -3.4 5.8 24 -14 30 .47
ESA | 3.8 4.8 1.7 77 -25 15 -.04
GFZ | .5 1.3 1.3 5 2 -13 .04
GRG | 1.5 12.2 6.8 3 19 78 1.03
JPL | 2.7 -3.2 9.1 13 -40 -77 .44
MIT | 4.7 -5.9 -3.0 22 4 -19 .25
NGS | 7.5 -1.6 -10.1 -30 -137 -9 .36
SIO | 2.2 -3.0 9.9 -87 24 -10 .47
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 1.1569.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1569.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 2.1569.[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 3.1569.[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 5.1569.0-6).
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 1569 summary. (Jan 31, 2010 - Feb 06, 2010)
Table 1.1569.a GPS week: 1569 MJD: 55227.000-55233.000
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 242| 1 0 0 44 -34 -29 -.14 8 7 | -524 -10 18 73
| 0 0 1 18 13 8 .01 | 507 779
emr 91| -2 1 7 -48 -50 -19 .43 19 19 | 761 0 25 91
| 1 1 2 28 32 14 .03 | 827 1244
esa 130| 1 0 -1 -123 -7 32 .25 8 8 | -560 391 15 101
| 1 0 1 27 13 15 .02 | 871 1326
gfz 196| -1 -1 -5 -26 -34 8 -.11 10 10 | 85 -676 34 137
| 0 0 1 65 68 13 .03 | 315 867
grg 107| 0 0 6 36 -107 22 1.03 24 22 | 49197 -64135 65 229
| 1 0 2 39 33 18 .05 | 130283 169372
igr n/a| 0 0 -1 25 -36 -23 .04 5 5 | -7119 -28 19 65
| 0 0 0 22 20 15 .03 | 841 1388
jpl 130| 0 0 6 -46 42 -4 .44 19 18 | 2837 145 20 95
| 0 1 1 23 23 36 .03 | 1306 1495
mit 256| 0 0 -2 -2 -69 4 -.27 13 11 | -9200 1344 25 155
| 0 0 0 40 9 11 .04 | 8590 2007
ngs 219| -1 0 -4 100 213 -15 -.18 10 8 | 96252 -9069 2199 3689
| 0 0 1 37 32 14 .04 | 339422 269641
sio 261| -1 1 14 171 -100 21 -.08 19 18 | --- --- --- ---
| 0 1 0 38 14 10 .03 | --- ---
Table 1.1569.b GPS week : 1569 MJD: 55227.000-55233.000
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 13 0 12 0 19 17 |
2 | 6 6 5 5 4 5 5 |
3 | 6 5 5 8 6 6 5 |
4 | 4 3 4 3 4 4 4 |
5 | 5 5 5 5 5 5 5 |
6 | 5 5 4 5 4 4 7 |
7 | 5 5 5 6 5 5 5 |
8 | 4 3 3 5 3 3 3 |
9 | 3 3 3 4 3 3 4 |
10 | 5 6 4 4 4 5 4 |
11 | 5 4 4 5 4 5 4 |
12 | 4 4 4 5 4 5 5 |
13 | 5 4 4 4 4 4 4 |
14 | 4 4 4 4 4 5 5 |
15 | 5 5 5 6 5 5 5 |
16 | 6 5 4 5 5 5 5 |
17 | 4 4 0 4 4 4 4 |
18 | 4 4 5 5 5 5 5 |
19 | 5 5 5 5 5 5 5 |
20 | 6 5 5 5 5 5 5 |
21 | 5 4 5 5 4 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 5 5 5 5 |
24 | 4 4 3 4 3 4 4 |
25 | 6 7 8 10 9 8 11 |
26 | 6 6 6 6 6 6 6 |
27 | 4 4 4 5 4 5 5 |
28 | 5 4 5 5 5 5 4 |
29 | 6 5 5 5 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 5 4 5 5 4 5 5 |
32 | 4 4 4 4 4 4 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 2.1569.0 GPS week: 1569 Day: 0 MJD: 55227.000
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 242| 0 0 0 70 -41 -35 -.14 8 8 | -305 -360 22 75
| 1 -22 |
emr 91| -1 -1 7 -24 -2 -43 .38 19 19 | 670 100 19 78
| -25 -51 |
esa 130| 3 1 0 -162 15 38 .29 9 9 | -1100 2427 13 90
| 6 -47 |
gfz 196| -2 -2 -5 -87 -131 35 -.12 9 9 | 42 -351 31 120
| -83 -47 |
grg 107| 0 0 7 96 -48 25 .99 25 21 | 70 -271 56 206
| -154 -53 |
igr n/a| 0 0 -2 41 -44 -17 .05 5 5 | -7513 274 18 66
| -49 -51 |
jpl 130| 0 0 7 -87 17 9 .47 18 18 | 1564 767 18 109
| 91 -58 |
mit 256| 1 0 -2 -7 -79 1 -.25 14 12 | -25 -63 23 159
| -1 9 |
ngs 219| -2 0 -3 153 238 -18 -.13 9 7 | -306 -407 1826 3724
| -22 -42 |
sio 261| 0 0 14 180 -99 15 -.09 20 19 | --- --- --- ---
| -89 14 |
Table 2.1569.1 GPS week: 1569 Day: 1 MJD: 55228.000
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 242| 0 0 -1 54 -36 -29 -.15 7 7 | -239 -435 18 81
| 0 -7 |
emr 91| -2 0 8 -14 -32 -9 .43 20 20 | -52 555 42 109
| -25 5 |
esa 130| 1 0 0 -93 -6 53 .26 7 7 | -522 743 18 107
| -22 1 |
gfz 196| -1 0 -5 -56 -51 8 -.09 9 9 | 83 -531 37 166
| -60 -53 |
grg 107| 0 0 4 59 -133 44 .96 24 21 | 344652 -448235 56 256
| -81 63 |
igr n/a| 0 0 0 31 -41 -44 .04 4 4 | -7968 593 22 69
| -41 -31 |
jpl 130| 0 1 6 -42 33 0 .42 18 17 | 1336 980 31 90
| 31 -26 |
mit 256| 1 0 -1 -29 -50 -16 -.24 13 11 | -15925 885 29 146
| 5 15 |
ngs 219| 0 0 -4 118 231 -14 -.24 11 8 | -351840 502316 2654 4230
| 4 -3 |
sio 261| -1 0 14 155 -81 7 -.11 19 18 | --- --- --- ---
| -65 27 |
Table 2.1569.2 GPS week: 1569 Day: 2 MJD: 55229.000
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 242| 1 -1 0 18 -27 -14 -.14 7 7 | -716 426 16 55
| 56 7 |
emr 91| -1 1 8 -69 -23 0 .40 18 18 | 289 -1161 17 94
| 3 7 |
esa 130| 1 0 -2 -129 -12 5 .24 7 8 | 345 -869 12 99
| 26 -6 |
gfz 196| -2 0 -3 56 -42 10 -.11 10 10 | 383 -1747 33 138
| -47 -41 |
grg 107| 0 0 10 30 -95 34 1.02 21 21 | 4 -530 59 225
| 3 53 |
igr n/a| 0 1 0 -7 -14 -31 .05 5 5 | -7479 -1270 16 72
| 0 -42 |
jpl 130| 0 2 4 -62 53 -6 .41 18 17 | 2295 -936 15 81
| 53 -45 |
mit 256| 0 0 -2 43 -65 9 -.25 12 11 | 251 -756 19 172
| -16 15 |
ngs 219| -1 0 -4 44 227 -9 -.19 11 8 | -741 416 2645 3850
| 89 -15 |
sio 261| 0 0 15 215 -106 27 -.10 18 17 | --- --- --- ---
| -72 27 |
Table 2.1569.3 GPS week: 1569 Day: 3 MJD: 55230.000
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 242| 1 0 0 30 -16 -39 -.14 9 7 | 260 -1064 25 75
| 24 -17 |
emr 91| -4 2 3 -81 -50 -29 .43 19 19 | 57 1006 52 123
| 30 32 |
esa 130| 1 0 -1 -133 -20 44 .22 8 8 | -139 -10 27 113
| 51 11 |
gfz 196| -2 -1 -4 2 -43 -2 -.16 11 11 | 621 -2014 53 179
| -45 -26 |
grg 107| 3 1 2 3 -89 9 1.02 23 21 | 236 -555 90 238
| 37 86 |
igr n/a| 0 1 -1 14 -11 4 .03 6 5 | -7683 1183 23 76
| -48 -36 |
jpl 130| 0 1 4 -47 88 16 .47 21 20 | 2547 1438 37 107
| 35 -54 |
mit 256| 0 -1 -3 41 -71 4 -.23 12 10 | -15938 1602 34 153
| -19 7 |
ngs 219| -1 0 -1 68 241 -14 -.15 12 9 | 19119 -13156 2092 3423
| 79 -22 |
sio 261| -1 1 14 210 -87 18 -.10 18 18 | --- --- --- ---
| -84 16 |
Table 2.1569.4 GPS week: 1569 Day: 4 MJD: 55231.000
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 242| 1 0 1 63 -53 -20 -.14 7 7 | -815 317 15 75
| -7 -2 |
emr 91| -3 1 8 -17 -85 -26 .47 18 18 | 573 1778 18 74
| -24 50 |
esa 130| 2 0 -1 -86 -16 35 .27 8 8 | -824 1625 13 106
| -10 9 |
gfz 196| -1 -1 -7 -120 73 7 -.10 9 9 | -219 244 31 115
| -41 -59 |
grg 107| 0 0 7 39 -149 -10 1.06 25 23 | -340 216 72 253
| -76 128 |
igr n/a| 0 0 -1 61 -69 -30 .09 5 5 | -7182 1816 18 59
| -49 -13 |
jpl 130| 0 -1 10 -13 28 -8 .49 18 17 | 3073 1848 13 90
| 73 -78 |
mit 256| 0 -1 -3 -50 -69 6 -.28 12 10 | -282 158 26 155
| 14 -12 |
ngs 219| 0 0 -5 131 164 -23 -.21 10 7 | 226966 -130675 1991 3538
| -37 41 |
sio 261| -2 2 14 128 -114 15 -.09 17 17 | --- --- --- ---
| -63 26 |
Table 2.1569.5 GPS week: 1569 Day: 5 MJD: 55232.000
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 242| 0 1 2 39 -45 -30 -.12 7 6 | -1347 1349 15 73
| 38 -1 |
emr 91| -3 0 7 -62 -86 -11 .44 20 20 | 2129 -477 13 79
| -26 43 |
esa 130| 2 0 -1 -145 3 23 .24 8 8 | -2075 151 12 93
| 23 12 |
gfz 196| 0 -1 -6 -18 31 1 -.12 9 9 | -231 -380 27 127
| -16 -36 |
grg 107| 0 1 9 51 -128 37 1.11 25 22 | -377 907 60 242
| -69 110 |
igr n/a| 0 0 -1 19 -46 -15 .01 6 5 | -5535 -718 20 56
| -30 -17 |
jpl 130| 0 0 8 -40 28 39 .42 20 18 | 4875 -862 15 94
| 68 -12 |
mit 256| 0 0 -4 26 -78 2 -.29 13 11 | -16219 5225 23 144
| -11 -14 |
ngs 219| 0 0 -4 90 171 -37 -.18 11 8 | 761621 -408739 1999 3805
| 91 54 |
sio 261| -1 2 13 190 -122 30 -.02 18 16 | --- --- --- ---
| -86 17 |
Table 2.1569.6 GPS week: 1569 Day: 6 MJD: 55233.000
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 242| 0 0 4 35 -18 -34 -.14 9 8 | -508 -303 18 78
| -9 3 |
emr 91| -2 4 5 -68 -73 -15 .42 17 17 | 1666 -1795 19 81
| -15 72 |
esa 130| 0 0 -3 -115 -16 27 .25 9 9 | 392 -1328 13 101
| 4 44 |
gfz 196| 0 -2 -5 40 -79 -3 -.08 9 9 | -78 46 32 117
| -25 -18 |
grg 107| 0 0 5 -25 -109 19 1.03 24 22 | 137 -478 64 188
| 19 87 |
igr n/a| 0 1 -1 19 -24 -32 -.00 5 4 | -6477 -2077 19 61
| -53 -14 |
jpl 130| 1 1 6 -31 45 -79 .41 19 18 | 4169 -2218 16 100
| 21 10 |
mit 256| 0 -1 -3 -44 -73 23 -.33 13 12 | -16263 2361 21 160
| 15 -22 |
ngs 219| 0 0 -5 95 219 10 -.16 10 9 | 18947 -13238 2188 3253
| -13 21 |
sio 261| -2 1 14 119 -92 38 -.06 19 18 | --- --- --- ---
| -80 -2 |
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 3.1569.0 GPS week: 1569 Day: 0 MJD: 55227.000
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 --- --- --- --- 26 --- --- --- --- 0 | 22 --- --- --- --- 21 --- --- --- --- 22
2 | 9 19 10 15 21 4 22 9 6 34 5 | 22 29 28 35 33 24 30 24 25 28 23
3 | 8 26 10 13 24 7 16 20 11 18 5 | 37 51 38 46 40 38 39 40 44 42 40
4 | 7 11 7 9 18 5 12 12 7 21 3 | 33 32 37 38 39 35 34 35 39 29 35
5 | 5 20 8 8 35 4 24 11 7 32 5 | 24 35 28 30 47 27 35 23 31 31 26
6 | 6 17 10 12 21 6 16 21 10 15 5 | 25 39 30 34 37 27 39 27 28 40 29
7 | 8 21 11 7 26 4 22 22 9 17 5 | 26 34 29 31 42 25 31 29 25 28 25
8 | 7 13 9 7 15 4 12 13 6 15 3 | 51 55 57 57 59 53 54 52 52 50 50
9 | 6 12 9 5 17 3 10 12 8 11 3 | 27 31 26 32 35 28 30 32 29 25 27
10 | 7 16 6 6 19 6 13 12 9 32 4 | 36 37 39 44 41 40 36 37 40 32 36
11 | 14 19 7 6 29 6 18 17 13 22 5 | 39 42 42 40 46 41 43 46 45 40 41
12 | 7 18 8 8 23 4 16 10 6 16 4 | 23 33 26 27 38 25 35 23 31 26 25
13E | 6 17 9 9 25 5 20 14 11 17 4 | 20 31 23 18 41 19 28 19 22 19 20
14E | 8 25 8 8 19 3 17 8 9 17 4 | 18 29 24 22 29 19 28 20 27 23 21
15E | 9 19 5 10 28 6 26 11 11 20 4 | 70 74 74 83 71 75 75 74 76 78 73
16 | 7 22 12 7 21 3 23 22 10 20 5 | 21 32 24 21 40 22 34 31 27 27 24
17 | 7 18 9 9 40 4 16 10 9 10 4 | 12 20 8 13 28 11 18 9 18 9 12
18 | 6 18 8 8 26 3 22 7 7 19 4 | 27 37 31 31 42 29 39 29 32 35 30
19 | 8 24 10 9 31 5 21 12 10 13 4 | 24 35 29 22 42 22 33 21 27 28 24
20 | 9 22 9 19 28 5 22 10 8 26 5 | 27 35 30 32 43 27 36 28 31 32 28
21 | 7 12 7 8 21 4 20 7 7 32 4 | 24 30 26 28 34 24 29 26 29 27 26
22 | 6 16 5 9 26 5 21 7 7 18 3 | 28 38 33 33 46 29 40 31 31 29 31
23E | 6 17 10 7 17 6 22 10 10 16 4 | 25 33 32 25 36 24 30 22 29 26 27
24 | 10 13 7 8 17 4 10 12 7 16 3 | 43 47 49 50 44 47 47 46 50 48 48
X25 | 12 21 11 --- --- 16 --- 13 7 --- 6 | 33 35 41 --- --- 39 --- 34 34 --- 33
26E | 10 24 9 9 33 4 20 29 18 11 6 | 23 30 25 27 43 24 33 40 37 25 26
27 | 6 13 8 6 17 4 8 5 9 24 3 | 23 28 24 31 32 25 27 25 28 32 24
28 | 8 25 13 9 30 6 15 10 10 16 4 | 20 37 27 23 44 23 31 22 25 18 21
X29 | 9 27 10 10 24 4 22 14 10 --- 5 | 26 40 24 26 45 25 37 25 31 --- 26
30 | 8 20 8 8 14 5 16 10 6 20 4 | 23 35 22 23 33 23 33 27 28 33 23
31 | 9 20 7 9 25 4 20 16 10 16 4 | 24 38 31 28 43 27 33 28 29 31 27
32 | 5 17 9 9 33 5 17 15 8 13 4 | 23 26 28 24 38 23 28 27 31 25 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 9 9 25 5 18 14 9 20 |T 28 36 31 32 41 29 35 30 33 31 29
WRMS | 8 19 9 9 21 5 18 12 7 19 |NE 27 35 30 31 40 28 34 29 32 30 28
MEDI | 7 19 9 8 24 4 18 12 9 17 |MD 24 35 29 30 41 25 33 28 31 29 26
Table 3.1569.1 GPS week: 1569 Day: 1 MJD: 55228.000
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 | 13 --- --- --- --- 53 --- 17 26 --- 13 | 21 --- --- --- --- 40 --- 20 27 --- 19
2 | 9 21 8 20 23 6 18 9 11 33 5 | 19 30 25 33 30 22 26 20 25 25 22
3 | 7 26 9 12 19 4 16 19 11 20 5 | 50 59 51 54 51 50 51 51 54 52 50
4 | 5 11 5 10 18 2 8 8 9 21 3 | 20 21 22 25 26 21 22 21 22 22 20
5 | 6 20 8 12 36 5 21 9 11 25 4 | 13 28 17 15 39 14 30 13 18 23 15
6 | 7 17 8 12 14 4 16 22 12 15 4 | 22 38 30 30 34 27 36 26 31 34 26
7 | 7 25 7 6 27 4 24 16 6 15 4 | 19 31 26 20 38 19 28 24 21 24 20
8 | 7 14 3 8 14 3 10 11 9 12 3 | 53 56 57 52 62 54 56 55 56 56 54
9 | 4 13 6 8 18 4 8 11 9 11 3 | 20 19 20 19 31 18 19 18 23 18 18
10 | 7 18 6 10 22 6 12 27 14 38 6 | 62 61 60 57 54 59 60 63 59 60 59
11 | 8 18 6 7 28 5 17 12 7 16 4 | 28 35 25 28 41 28 32 32 33 27 28
12 | 6 26 6 6 28 4 19 9 6 16 4 | 20 31 18 16 37 15 26 16 20 18 17
13E | 5 18 6 8 22 3 20 9 9 12 3 | 14 27 18 15 33 14 24 13 19 14 14
14E | 6 18 7 8 29 3 18 10 13 10 4 | 19 27 24 22 42 20 28 19 30 19 21
15E | 7 20 6 7 25 5 25 12 9 17 4 | 66 64 64 60 64 62 63 66 65 69 64
16 | 7 27 8 14 24 5 24 16 9 18 5 | 16 30 16 22 32 16 29 22 24 18 17
17 | 7 19 7 7 24 5 15 7 8 9 3 | 13 20 9 8 25 11 17 10 19 11 11
18 | 7 23 7 6 22 4 22 9 9 16 4 | 17 28 19 18 34 16 29 16 15 18 16
19 | 8 26 7 8 24 5 22 11 13 12 4 | 20 34 24 18 34 20 30 19 30 25 22
20 | 8 21 9 13 29 6 22 7 10 23 4 | 20 31 23 23 36 21 31 21 27 21 21
21 | 6 15 5 7 19 4 15 9 10 32 4 | 20 26 23 21 30 17 22 18 18 23 18
22 | 6 16 6 7 26 5 18 10 10 14 3 | 20 29 24 23 39 20 31 22 23 16 21
23E | 5 14 6 8 23 5 23 9 10 12 3 | 23 33 29 25 35 24 31 22 29 23 25
24 | 8 15 5 5 20 4 9 8 11 19 3 | 33 33 35 35 34 31 33 32 31 31 32
X25 | 11 20 9 --- --- 25 --- 14 20 --- 7 | 29 44 42 --- --- 40 --- 39 43 --- 36
26E | 9 24 10 7 29 3 20 26 21 15 6 | 20 31 23 21 40 19 31 29 31 18 21
27 | 4 13 6 8 18 4 8 8 10 25 3 | 19 21 20 18 32 17 18 16 21 30 17
28 | 4 24 7 9 30 5 18 11 9 16 4 | 20 31 23 20 44 21 29 16 20 14 19
X29 | 9 31 6 8 20 4 23 9 12 --- 5 | 23 38 25 23 37 23 33 20 26 --- 24
30 | 7 19 5 5 18 4 13 8 11 22 4 | 16 27 19 19 29 19 22 17 21 24 17
31 | 6 18 7 7 29 5 21 11 11 15 4 | 19 30 23 22 42 21 31 18 23 20 21
32 | 6 18 8 8 29 6 15 15 11 13 4 | 17 24 22 18 36 17 23 18 27 17 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 20 7 9 24 4 18 13 11 19 |T 24 33 27 26 38 25 31 25 29 26 25
WRMS | 7 20 7 9 21 4 17 11 8 18 |NE 23 31 25 24 36 24 29 23 26 24 23
MEDI | 7 19 7 8 23 4 18 10 10 16 |MD 20 31 23 22 36 20 29 20 25 23 21
Table 3.1569.2 GPS week: 1569 Day: 2 MJD: 55229.000
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 --- --- --- --- 131 --- --- --- --- 0 | 17 --- --- --- --- 97 --- --- --- --- 18
2 | 6 16 6 15 21 10 18 8 10 29 4 | 20 28 27 29 33 23 26 20 26 20 22
3 | 9 19 9 13 24 6 15 13 10 16 4 | 55 64 59 60 63 59 66 60 60 65 59
4 | 7 11 4 12 18 6 8 7 10 19 3 | 30 30 31 33 32 32 29 31 34 30 31
5 | 6 22 10 11 21 6 23 10 14 23 5 | 21 34 27 25 38 24 33 19 27 23 23
6 | 7 14 6 10 16 7 16 14 10 16 4 | 23 34 27 28 36 25 35 25 27 34 26
7 | 6 21 6 9 23 4 22 13 9 15 4 | 20 30 24 23 39 21 28 25 21 23 21
8 | 7 10 6 8 16 4 11 11 6 11 3 | 24 27 29 28 36 27 31 26 32 28 28
9 | 6 13 7 9 13 5 9 9 7 12 3 | 17 23 20 21 29 19 20 20 23 19 19
10 | 7 16 6 8 19 5 12 10 10 28 4 | 29 35 33 34 32 31 30 27 30 30 30
11 | 10 17 6 9 28 6 17 13 11 14 4 | 30 35 34 36 40 32 34 38 32 32 32
12 | 7 21 5 8 23 4 20 13 11 15 4 | 21 31 26 22 37 22 33 20 32 21 23
13E | 6 17 6 9 21 5 20 10 12 14 4 | 13 26 19 14 35 15 25 15 14 16 14
14E | 6 19 8 8 22 4 18 11 9 11 4 | 16 25 23 19 35 19 25 19 21 20 18
15E | 8 21 8 9 20 7 27 16 10 14 5 | 59 64 63 63 61 62 64 62 66 64 62
16 | 6 20 8 8 22 5 21 13 9 15 4 | 17 26 19 17 33 18 28 21 22 20 18
X17 | 3 --- --- --- --- 23 --- --- --- --- 0 | 23 --- --- --- --- 24 --- --- --- --- 25
18 | 6 22 8 10 22 5 21 11 10 19 4 | 21 34 23 25 36 24 33 23 24 27 23
19 | 6 24 8 9 22 5 19 15 12 12 4 | 22 34 23 23 37 23 28 19 29 25 22
20 | 8 21 9 16 27 7 22 8 11 19 5 | 20 32 24 30 37 23 32 24 25 24 22
21 | 7 17 8 9 22 6 16 11 7 32 4 | 19 27 21 21 31 21 23 22 20 26 19
22 | 5 18 7 7 26 7 20 11 13 13 4 | 23 34 25 27 41 25 34 27 23 23 24
23E | 5 15 6 8 20 6 25 14 9 10 4 | 25 30 27 27 33 25 31 28 30 27 26
24 | 6 14 6 5 17 5 8 9 8 18 3 | 43 45 45 47 39 44 42 43 45 44 44
X25 | 12 29 11 --- --- 17 --- 15 15 --- 7 | 22 33 22 --- --- 28 --- 25 28 --- 22
26E | 9 25 11 9 18 5 20 27 21 14 6 | 21 34 28 25 39 25 33 33 31 26 24
27 | 6 14 8 8 13 4 8 8 11 25 4 | 17 22 20 20 27 17 19 17 21 29 18
28 | 4 22 11 11 24 4 20 10 11 16 4 | 18 34 24 18 39 21 31 20 25 18 20
X29 | 9 26 6 7 21 6 20 11 12 --- 5 | 18 35 21 17 35 21 28 24 22 --- 20
30 | 7 17 4 7 15 3 12 12 12 21 4 | 15 25 20 21 29 18 23 24 23 26 18
31 | 7 21 9 10 25 5 20 9 17 14 4 | 21 31 27 27 41 24 29 22 28 26 24
32 | 8 19 8 9 30 4 16 11 9 10 4 | 17 24 25 24 35 20 25 23 23 19 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 10 21 5 18 12 11 18 |T 23 32 27 27 37 28 31 26 28 28 25
WRMS | 7 18 8 10 21 5 17 11 8 17 |NE 21 30 25 25 35 27 29 24 26 25 23
MEDI | 6 19 7 9 21 5 19 11 10 15 |MD 21 31 25 25 36 24 30 24 26 26 22
Table 3.1569.3 GPS week: 1569 Day: 3 MJD: 55230.000
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 | 13 --- --- --- --- 15 --- 21 15 --- 11 | 26 --- --- --- --- 39 --- 20 32 --- 21
2 | 7 17 8 13 19 7 20 6 14 28 5 | 24 30 27 30 35 28 31 24 31 27 25
3E | 28 26 12 18 36 9 22 14 15 16 7 | 110 118 118 109 121 114 119 113 112 115 112
4 | 4 10 5 10 12 5 8 6 5 17 3 | 30 30 32 33 37 32 27 31 36 28 30
5 | 6 19 5 13 34 5 25 11 12 23 5 | 20 32 23 24 44 21 31 18 24 26 21
6 | 12 18 9 13 26 5 17 13 12 16 5 | 27 40 35 31 39 33 39 29 36 42 31
7 | 8 26 9 10 22 8 24 18 9 18 5 | 23 33 26 25 40 22 29 26 28 28 22
8 | 13 11 8 9 17 8 17 17 9 19 4 | 87 93 93 92 96 91 96 94 102 93 93
9 | 4 12 10 9 15 4 12 6 12 12 3 | 21 23 22 26 27 18 22 21 21 21 19
10 | 5 14 5 10 19 6 16 10 12 24 4 | 41 40 38 41 41 41 37 42 44 41 40
11 | 7 19 8 7 27 6 21 14 13 15 4 | 34 39 33 34 46 31 37 38 34 33 32
12 | 8 21 10 9 24 3 22 10 11 13 4 | 19 33 18 19 36 16 31 18 27 19 18
13E | 6 17 6 10 27 7 23 10 9 15 4 | 18 28 21 17 40 16 26 21 22 23 17
14E | 6 17 9 10 16 4 18 6 11 13 4 | 18 28 20 24 34 19 26 19 24 21 19
15E | 7 21 9 11 31 5 29 9 24 14 5 | 30 36 35 36 32 33 35 34 36 34 32
16 | 5 24 9 10 22 3 24 15 7 14 4 | 19 30 18 13 36 16 29 23 21 21 17
X17 | 7 --- 6 7 --- 6 19 8 9 --- 4 | 14 --- 17 14 --- 13 23 13 20 --- 14
18 | 6 23 9 10 20 4 27 7 7 16 4 | 22 36 25 24 37 23 35 22 23 22 22
19 | 6 24 8 8 24 4 22 12 9 12 4 | 26 38 25 24 43 24 33 22 30 26 25
20 | 8 21 7 14 25 5 22 10 15 20 5 | 24 29 22 25 34 21 30 27 32 25 22
21 | 7 14 9 10 21 6 24 12 10 31 5 | 19 25 25 21 32 17 25 22 22 26 19
22 | 4 14 7 10 26 4 21 9 8 13 3 | 24 33 28 28 44 25 34 26 26 22 25
23E | 6 16 6 10 30 7 26 16 6 13 4 | 30 39 31 29 41 31 39 34 36 34 30
24 | 8 13 7 9 13 4 15 10 9 19 4 | 37 39 38 41 39 37 42 41 44 40 39
X25 | 20 23 23 --- --- 10 --- 20 13 --- 10 | 31 36 45 --- --- 36 --- 35 45 --- 35
26E | 9 24 10 8 23 5 21 23 21 14 6 | 22 33 22 24 47 23 33 33 34 24 23
27 | 5 12 9 11 16 3 13 7 16 27 4 | 19 20 21 24 28 17 21 20 22 31 18
28 | 7 23 10 14 21 5 21 11 9 19 5 | 17 33 22 16 39 17 27 17 19 17 16
X29 | 7 21 7 9 19 4 25 14 9 --- 5 | 26 36 22 24 38 25 32 31 28 --- 25
30 | 6 15 6 9 17 5 12 12 12 23 4 | 20 26 21 19 29 19 22 26 26 31 20
31 | 5 20 9 9 24 5 26 10 12 14 4 | 21 33 25 24 39 22 31 22 22 26 22
32 | 4 16 8 7 28 5 19 11 11 12 4 | 21 25 20 20 35 17 23 23 23 21 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 8 11 23 6 21 12 12 18 |T 28 37 31 30 42 29 35 30 33 32 28
WRMS | 7 19 8 11 21 5 20 10 9 18 |NE 26 34 28 27 39 26 32 28 31 29 26
MEDI | 7 18 8 10 22 5 21 11 11 16 |MD 23 33 25 24 39 23 31 24 28 26 22
Table 3.1569.4 GPS week: 1569 Day: 4 MJD: 55231.000
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 --- --- --- --- 41 --- --- --- --- 0 | 29 --- --- --- --- 34 --- --- --- --- 29
2 | 5 12 8 11 22 8 18 5 10 27 4 | 19 25 24 26 31 22 27 20 23 22 19
3E | 20 19 9 15 32 10 16 13 15 26 6 | 114 125 117 125 132 116 120 122 117 130 119
4 | 6 10 7 9 19 6 10 8 11 17 3 | 24 24 30 28 29 27 24 26 29 24 25
5 | 6 19 12 11 33 4 22 15 11 23 5 | 20 30 24 23 40 22 31 21 25 24 20
6 | 8 17 6 10 25 6 15 14 10 15 4 | 24 39 26 31 36 26 37 24 27 37 27
7 | 6 25 7 10 24 3 23 10 9 16 4 | 20 32 23 22 38 20 30 22 20 25 19
8 | 10 9 7 9 15 4 10 7 8 11 3 | 40 43 43 39 53 43 46 44 41 45 40
9 | 5 13 8 6 20 6 8 7 9 12 3 | 18 21 18 17 29 17 20 19 22 20 17
10 | 5 13 9 9 18 5 11 14 8 23 4 | 31 25 29 28 25 29 27 35 33 28 28
11 | 8 18 9 7 27 4 19 10 9 15 4 | 27 32 31 30 40 28 33 32 31 29 27
12 | 7 22 8 8 28 3 20 11 7 12 4 | 18 30 19 17 37 19 31 19 20 19 18
13E | 6 16 6 10 23 4 18 10 12 11 4 | 26 30 24 20 41 26 32 27 30 28 24
14E | 6 19 8 9 25 5 22 10 5 13 4 | 21 25 23 21 34 22 33 21 23 19 20
15E | 8 15 7 9 23 6 24 13 8 21 4 | 36 35 34 32 37 34 35 36 33 37 32
16 | 6 24 6 10 25 4 21 13 7 14 4 | 19 33 20 19 34 21 32 22 20 21 20
17 | 5 19 7 6 25 4 18 7 9 7 3 | 16 19 15 13 21 17 25 12 18 12 16
18 | 6 23 9 9 27 6 23 8 9 17 4 | 22 31 23 21 39 21 33 21 22 19 20
19 | 8 25 11 9 24 6 23 13 8 11 5 | 25 36 23 23 43 24 39 23 26 25 24
20 | 7 18 9 13 25 5 19 9 12 20 4 | 21 28 20 24 32 24 31 25 18 23 19
X21 | 6 18 7 8 23 7 --- 11 8 --- 4 | 20 25 21 20 30 18 --- 20 19 --- 18
22 | 5 20 7 11 30 6 21 9 8 15 4 | 25 33 27 27 43 26 38 25 27 19 24
23E | 8 16 7 9 33 5 26 20 8 12 5 | 46 48 49 49 61 48 51 54 46 46 47
24 | 6 11 6 7 17 5 12 7 6 19 3 | 37 36 35 40 36 35 34 39 40 37 37
X25 | 12 23 16 --- --- 6 --- 17 21 --- 8 | 22 29 31 --- --- 22 --- 25 35 --- 23
26E | 8 26 9 5 27 6 20 23 20 13 6 | 22 33 25 23 44 25 37 33 32 19 24
27 | 5 13 8 8 21 6 9 11 11 28 4 | 18 20 17 18 30 17 20 20 20 32 16
28 | 7 23 11 14 27 4 17 9 8 15 4 | 17 33 18 18 40 19 28 17 15 16 15
X29 | 7 21 12 7 22 4 18 12 8 --- 4 | 23 33 25 21 36 23 32 26 25 --- 23
30 | 6 14 6 8 19 5 10 10 8 23 4 | 20 27 21 17 30 21 26 25 21 32 20
31 | 5 20 10 5 27 4 19 10 8 13 4 | 20 31 24 19 41 23 33 23 26 25 22
32 | 6 19 9 8 28 3 16 8 11 11 4 | 20 22 21 21 35 21 27 22 20 20 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 8 9 25 5 18 12 10 17 |T 26 33 28 27 39 27 34 29 29 29 26
WRMS | 7 18 8 9 23 5 17 10 7 17 |NE 22 29 24 23 35 23 30 24 24 24 22
MEDI | 6 19 8 9 25 5 18 10 9 15 |MD 22 31 24 22 36 23 32 24 25 24 22
Table 3.1569.5 GPS week: 1569 Day: 5 MJD: 55232.000
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 --- --- --- --- 48 --- 23 32 --- 19 | 41 --- --- --- --- 46 --- 22 27 --- 26
2 | 6 16 9 18 21 7 18 8 10 28 5 | 18 27 23 30 32 20 26 19 22 19 19
3E | 14 19 10 14 28 10 18 17 19 16 5 | 92 105 103 105 111 103 100 103 95 108 100
4 | 6 10 7 11 17 5 13 8 7 17 3 | 21 22 24 27 28 25 19 25 24 25 21
5 | 6 21 8 8 23 5 24 15 13 25 5 | 16 28 16 16 37 16 28 15 21 24 14
6 | 10 20 8 8 23 6 16 12 8 14 4 | 37 49 42 41 48 38 44 36 39 46 39
7 | 7 23 10 8 23 6 25 10 11 18 4 | 15 26 16 16 35 14 25 16 20 18 13
8 | 6 11 7 5 14 6 12 9 10 11 3 | 68 67 67 69 72 69 70 69 73 67 68
9 | 6 12 8 6 18 4 8 9 12 12 3 | 21 21 17 19 27 18 20 18 21 18 17
10 | 7 15 7 9 16 5 12 16 13 23 4 | 30 30 26 31 31 30 26 35 31 33 28
11 | 9 18 7 4 30 6 22 12 10 22 4 | 21 28 22 22 33 19 26 24 23 27 19
12 | 5 24 8 12 30 5 22 12 9 13 4 | 14 25 15 11 35 12 26 14 20 14 12
13E | 7 15 4 7 20 5 21 7 10 12 3 | 12 23 16 10 35 12 25 16 17 16 11
14E | 7 21 7 9 19 6 24 14 8 10 4 | 17 22 21 20 30 15 23 22 20 16 16
15E | 7 27 12 9 18 4 23 13 11 17 5 | 28 34 31 36 36 31 32 32 32 32 29
16 | 6 25 10 9 23 8 26 14 7 15 5 | 14 29 21 15 33 14 28 17 21 17 14
17 | 5 22 9 7 25 6 18 10 8 9 4 | 15 22 15 11 16 13 20 11 15 10 13
18 | 8 23 8 11 24 4 23 8 8 19 4 | 16 30 19 19 36 17 31 15 22 18 16
19 | 8 30 9 10 28 7 24 13 10 13 5 | 21 34 18 14 36 16 30 16 27 17 17
20 | 7 22 10 11 27 6 23 13 10 24 5 | 17 26 19 19 30 16 26 20 18 15 13
X21 | 6 22 10 7 22 5 --- 15 7 --- 4 | 19 26 20 16 27 17 --- 18 21 --- 17
22 | 6 21 7 8 27 6 21 8 11 17 4 | 20 32 23 20 41 19 32 21 25 17 20
23E | 7 19 7 10 20 4 27 14 6 12 4 | 42 53 46 44 62 45 51 50 43 46 44
24 | 5 15 7 7 16 5 10 10 8 19 3 | 26 26 26 26 21 25 21 27 30 20 24
X25 | 13 19 17 --- --- 14 --- 15 15 --- 7 | 28 42 34 --- --- 36 --- 33 37 --- 31
26E | 8 24 10 7 51 4 20 24 19 14 5 | 18 28 17 21 57 18 31 32 32 23 19
27 | 6 13 9 7 20 5 10 16 14 27 4 | 21 23 16 20 27 18 21 20 22 29 17
28 | 6 21 10 10 27 5 17 13 7 17 4 | 9 25 11 15 38 10 21 12 14 12 9
X29 | 7 23 11 8 18 4 18 15 8 --- 5 | 14 26 14 18 31 12 22 17 17 --- 13
30 | 6 16 7 6 23 4 12 12 10 26 4 | 14 17 12 16 26 11 18 17 18 30 12
31 | 7 24 8 8 27 5 22 12 10 13 4 | 15 29 21 15 40 15 26 19 21 23 16
32 | 4 18 9 7 31 6 15 11 9 11 3 | 13 17 18 14 29 11 16 14 16 15 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 20 8 9 25 6 20 13 11 18 |T 24 32 25 25 38 24 30 25 27 26 23
WRMS | 6 20 8 9 22 5 18 11 8 16 |NE 21 28 21 20 33 20 26 21 24 22 19
MEDI | 7 21 8 8 23 5 20 12 10 16 |MD 18 27 20 19 33 17 26 19 22 19 17
Table 3.1569.6 GPS week: 1569 Day: 6 MJD: 55233.000
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 | 21 --- --- --- --- 28 --- 30 21 --- 17 | 38 --- --- --- --- 29 --- 16 39 --- 30
2 | 7 15 8 14 21 5 18 10 7 27 4 | 24 31 31 34 36 27 33 26 31 28 27
3E | 9 14 8 13 34 4 14 13 13 15 4 | 99 102 105 102 110 103 108 105 104 100 102
4 | 8 11 8 10 14 5 10 14 9 18 4 | 28 32 37 36 35 33 32 38 35 32 32
5 | 6 19 11 9 35 3 23 15 7 29 5 | 24 32 31 29 43 25 34 24 27 35 26
6E | 30 18 13 17 26 12 18 15 12 23 7 | 37 42 43 42 47 35 41 30 38 42 36
7 | 10 25 9 11 22 4 21 12 9 18 5 | 25 35 31 30 39 26 29 29 30 35 27
8 | 7 11 5 9 12 5 11 6 8 10 3 | 63 64 64 63 62 62 62 62 69 64 63
9 | 6 11 7 4 17 3 8 15 8 15 3 | 31 31 29 30 35 29 28 35 38 30 30
10 | 5 9 7 10 16 3 12 13 4 23 3 | 39 37 40 42 41 38 38 39 41 45 39
11 | 9 17 6 7 29 3 20 10 9 20 4 | 35 35 36 37 41 35 34 40 37 36 34
12 | 9 20 10 9 27 4 22 16 8 12 4 | 25 33 24 22 38 23 33 24 33 23 25
13E | 7 16 9 11 22 6 20 9 11 12 4 | 23 32 27 23 39 23 30 25 23 25 23
14E | 7 16 8 9 14 4 20 19 10 12 4 | 24 31 26 28 31 27 30 29 29 24 26
15E | 7 21 8 12 26 4 27 14 11 14 5 | 35 37 38 42 40 38 38 41 38 38 36
16 | 8 17 7 10 23 5 24 16 9 15 4 | 21 29 25 22 36 23 31 27 27 26 23
17 | 6 18 7 9 28 4 17 12 9 9 4 | 14 22 13 10 20 13 19 12 15 11 14
18 | 6 18 10 8 22 3 22 8 8 21 4 | 25 35 27 29 39 26 35 26 30 28 26
19 | 9 24 12 12 29 5 24 11 10 13 5 | 30 43 31 30 46 29 41 28 35 31 31
20 | 7 19 9 10 27 5 23 14 11 26 5 | 25 31 27 31 33 28 30 33 31 28 26
21 | 8 16 7 8 22 3 18 15 9 30 5 | 24 27 27 25 32 23 26 28 27 29 25
22 | 6 16 9 7 26 4 20 9 9 18 4 | 26 37 32 33 43 28 36 31 31 28 29
23E | 9 13 9 11 27 6 27 11 13 14 4 | 51 57 55 58 55 54 57 55 60 50 53
24 | 8 11 8 5 17 4 12 9 10 19 3 | 31 32 35 36 30 32 28 35 37 29 33
X25 | 23 25 19 --- --- 16 --- 13 23 --- 10 | 39 41 50 --- --- 39 --- 44 45 --- 41
26E | 9 25 9 9 14 3 23 21 19 15 6 | 28 34 29 29 37 27 36 31 35 27 28
27 | 7 12 7 6 18 3 9 19 9 28 4 | 27 28 26 27 33 25 25 33 34 35 26
28 | 7 17 9 8 24 4 17 12 9 17 4 | 20 31 24 16 39 20 27 20 24 23 20
X29 | 10 21 10 6 21 4 21 13 11 --- 5 | 28 37 25 25 35 27 35 30 35 --- 28
30 | 7 14 9 6 18 3 15 11 8 26 4 | 25 28 27 23 30 23 26 27 33 35 25
31 | 8 17 9 6 27 6 20 12 11 15 4 | 25 36 29 26 42 26 31 28 31 31 26
32 | 8 17 9 5 31 4 18 12 7 16 4 | 24 26 25 29 35 25 23 30 29 28 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 9 9 24 5 19 13 10 19 |T 31 37 34 33 40 31 35 33 36 34 32
WRMS | 8 17 9 9 22 4 18 12 9 18 |NE 28 33 31 29 37 28 32 30 33 31 29
MEDI | 8 17 9 9 22 4 20 13 9 17 |MD 26 33 29 29 38 27 32 30 33 30 27
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 4.1569 GPS week: 1569 MJD: 55227.0-55233.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 |U 7 9 23 |U 15 17 52 |U 7 8 16 |
emr | emr 2926 | 12 12 31 |U 14 17 47 | 9 9 19 |
esa | esa 2962 | 9 9 27 |U 13 16 46 | 7 7 18 |
gfz | gfz 2817 |U 12 14 40 |U 15 17 65 | 11 13 29 |
grg | grg 2852 | 10 9 31 |U 14 17 48 | 9 12 21 |
igr | igr 2943 | 9 10 28 | 15 16 52 | 9 9 22 |
igs | igs 2944 | 9 11 30 | 14 17 51 | 8 8 18 |
jpl | jpl 2832 |U 10 12 32 |U 14 17 49 |U 8 7 19 |
mit | mit 3017 |U 9 11 32 |U 14 15 48 |U 8 8 20 |
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 5.1569.0 GPS week: 1569 Day: 0 MJD: 55227.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 | 6 8 18 | 10 9 41 | 8 10 14 |
emr | emr 2958 | 9 9 24 | 7 10 46 | 10 11 18 |
esa | esa 2976 | 7 7 22 | 7 8 35 | 7 7 15 |
gfz | gfz 2836 | 8 11 25 | 9 10 51 | 10 8 22 |
grg | grg 2880 | 6 7 14 | 12 14 52 | 9 14 15 |
igr | igr 2976 | 7 7 22 | 7 10 33 | 7 8 15 |
igs | igs 2974 | 7 7 19 | 8 9 38 | 7 8 14 |
jpl | jpl 2876 | 7 8 19 | 8 9 37 | 8 8 16 |
mit | mit 2976 | 8 8 26 | 8 8 34 | 6 6 18 |
Table 5.1569.1 GPS week: 1569 Day: 1 MJD: 55228.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 6 12 19 | 8 11 29 | 6 6 13 |
emr | emr 2957 | 9 14 26 | 9 9 26 | 9 11 20 |
esa | esa 2976 | 6 9 19 | 7 9 27 | 7 7 16 |
gfz | gfz 2829 | 13 15 35 | 10 16 46 | 10 14 26 |
grg | grg 2880 | 6 6 21 | 9 12 30 | 7 11 16 |
igr | igr 2972 | 8 11 28 | 9 13 33 | 11 14 23 |
igs | igs 2946 | 8 12 21 | 8 10 26 | 9 9 21 |
jpl | jpl 2876 | 10 13 31 | 8 10 28 | 7 8 17 |
mit | mit 3072 | 17 23 62 | 9 9 42 | 9 10 18 |
Table 5.1569.2 GPS week: 1569 Day: 2 MJD: 55229.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2859 | 9 15 28 | 8 10 31 | 11 9 17 |
esa | esa 2880 | 8 11 24 | 8 10 24 | 8 6 15 |
gfz | gfz 2735 | 7 16 45 | 11 10 67 | 11 13 36 |
grg | grg 2784 | 9 11 30 | 7 10 31 | 12 12 15 |
igr | igr 2858 | 8 12 24 | 7 10 25 | 8 7 15 |
igs | igs 2849 | 8 13 31 | 8 10 32 | 10 7 15 |
jpl | jpl 2779 | 8 13 26 | 7 10 30 | 10 7 15 |
mit | mit 2880 | 8 12 28 | 7 8 28 | 9 8 16 |
Table 5.1569.3 GPS week: 1569 Day: 3 MJD: 55230.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3051 | 7 10 23 | 13 13 35 | 6 7 17 |
emr | emr 2861 | 19 21 37 | 14 15 44 | 10 10 20 |
esa | esa 2976 | 9 11 26 | 12 13 34 | 7 8 17 |
gfz | gfz 2825 | 14 11 42 | 14 16 70 | 14 21 40 |
grg | grg 2784 | 14 11 31 | 13 14 41 | 8 11 25 |
igr | igr 2961 | 10 15 23 | 16 12 57 | 15 18 39 |
igs | igs 3021 | 10 14 30 | 12 15 42 | 7 9 24 |
jpl | jpl 2875 | 9 15 27 | 13 15 42 | 9 10 19 |
mit | mit 3072 | 8 10 22 | 13 14 33 | 8 6 26 |
Table 5.1569.4 GPS week: 1569 Day: 4 MJD: 55231.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 5 6 18 | 16 23 52 | 7 11 17 |
emr | emr 2945 | 8 8 24 | 17 29 58 | 8 8 21 |
esa | esa 2976 | 6 4 21 | 18 25 56 | 8 8 20 |
gfz | gfz 2828 | 10 8 29 | 16 27 62 | 10 11 23 |
grg | grg 2880 | 8 6 29 | 16 21 53 | 9 10 24 |
igr | igr 2954 | 5 5 18 | 18 27 58 | 7 7 20 |
igs | igs 2947 | 6 5 22 | 17 25 54 | 8 8 18 |
jpl | jpl 2775 | 7 7 21 | 18 28 61 | 7 8 21 |
mit | mit 2976 | 6 5 22 | 17 24 58 | 7 9 20 |
Table 5.1569.5 GPS week: 1569 Day: 5 MJD: 55232.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 8 5 22 | 24 26 106 | 9 10 17 |
emr | emr 2952 | 10 8 32 | 24 27 71 | 10 8 20 |
esa | esa 2976 | 9 7 28 | 23 27 98 | 8 9 22 |
gfz | gfz 2824 | 12 14 37 | 22 24 93 | 14 13 31 |
grg | grg 2880 | 11 7 36 | 22 28 81 | 11 13 29 |
igr | igr 2946 | 9 6 30 | 26 24 94 | 9 8 23 |
igs | igs 2943 | 9 8 32 | 26 27 112 | 8 8 18 |
jpl | jpl 2773 | 9 8 34 | 27 26 82 | 8 7 23 |
mit | mit 3072 | 8 7 27 | 23 21 76 | 10 10 19 |
Table 5.1569.6 GPS week: 1569 Day: 6 MJD: 55233.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 11 14 40 | 20 20 51 | 6 6 18 |
emr | emr 2953 | 19 14 46 | 19 20 53 | 8 7 20 |
esa | esa 2976 | 18 17 50 | 18 20 53 | 7 5 21 |
gfz | gfz 2843 | 17 23 67 | 23 16 67 | 10 11 27 |
grg | grg 2880 | 17 15 55 | 17 21 51 | 10 11 21 |
igr | igr 2937 | 18 17 52 | 19 20 62 | 7 6 18 |
igs | igs 2929 | 17 17 57 | 19 21 57 | 7 5 17 |
jpl | jpl 2870 | 18 18 63 | 19 22 67 | 7 5 19 |
mit | mit 3072 | 10 13 41 | 18 19 63 | 9 9 20 |
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 6.1569 GPS week: 1569 MJD: 55227.500-55233.500
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 | 0 -19 -3 66 -3 | 2 18
| 12 15 64 91 7 | 4
emr uuuuu | -28 7 -94 1 -3 | 21 29
| 25 16 90 108 8 | 2
esa uuuuu | -9 -16 130 39 0 | -6 20
| 12 14 76 42 4 | 3
gfz uuuuu | 34 41 -29 -57 1 | 6 21
| 15 18 44 57 8 | 3
grg --xxx | -- -- 96 -25 -15 | 14 30
| -- -- 151 109 23 | 3
igr xxxxx | 23 34 -5 -48 -3 | 0 16
| 9 16 67 63 6 | 2
irf xxxxx | -6 -4 -24 4 6 | 6 24
| 16 15 56 70 9 | 4
jpl uuuuu | 32 -58 8 106 -8 | -14 22
| 24 31 108 136 11 | 3
mit uuuuu | -5 -3 -83 26 14 | 7 26
| 28 27 125 144 14 | 7
ngs uuuuu | -11 -32 -33 -99 -5 | -7 16
| 26 43 40 125 9 | 2
sio uuuuu | -24 73 17 49 17 | 24 36
| 22 21 122 145 14 | 7
Table 7.1569.0 GPS week: 1569 Day: 0 MJD: 55227.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -13 -21 7 79 9 | -2 16
emr uuuuu | 16 5 -135 181 -14 | 24 30
esa uuuuu | 12 -26 201 -35 4 | -9 18
gfz uuuuu | 12 63 27 -8 0 | 4 17
grg --xxx | -- -- -214 160 -38 | 15 26
igr xxxxx | 16 29 5 -41 8 | -1 14
irf xxxxx | -35 -20 -61 -99 -7 | 4 19
jpl uuuuu | 23 -111 0 222 8 | -16 24
mit uuuuu | -44 -19 -183 -179 -6 | 2 17
ngs uuuuu | 7 2 -18 76 3 | -7 16
sio uuuuu | -49 69 -111 -227 -3 | 18 27
Table 7.1569.1 GPS week: 1569 Day: 1 MJD: 55228.500
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 -20 -14 107 4 | -4 17
emr uuuuu | -13 5 -248 48 -9 | 18 27
esa uuuuu | -9 2 80 65 4 | -12 19
gfz uuuuu | 45 40 -35 -22 7 | 1 17
grg --xxx | -- -- 140 -45 -22 | 9 29
igr xxxxx | 23 21 -10 -89 -3 | -4 13
irf xxxxx | -8 -20 66 -17 8 | -1 19
jpl uuuuu | 18 -51 -18 125 -13 | -19 26
mit uuuuu | -23 -25 64 -35 12 | -3 18
ngs uuuuu | -5 -24 -104 -139 -19 | -10 18
sio uuuuu | -35 45 188 -4 11 | 14 25
Table 7.1569.2 GPS week: 1569 Day: 2 MJD: 55229.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -17 -47 -29 171 -2 | 2 20
emr uuuuu | -17 6 -55 -4 -11 | 21 30
esa uuuuu | -4 -17 -10 77 -4 | -6 21
gfz uuuuu | 31 56 -97 -69 1 | 6 23
grg --xxx | -- -- 206 -52 9 | 11 30
igr xxxxx | 32 9 -80 -15 -2 | 1 17
irf xxxxx | -10 9 35 -17 14 | 4 24
jpl uuuuu | 35 -44 -43 95 -22 | -15 24
mit uuuuu | -25 25 91 -59 26 | 2 24
ngs uuuuu | 5 -80 13 -73 -4 | -8 18
sio uuuuu | -37 81 162 55 24 | 20 33
Table 7.1569.3 GPS week: 1569 Day: 3 MJD: 55230.500
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 | 14 -12 -20 -103 -9 | 7 18
emr uuuuu | -35 -18 47 61 -3 | 23 31
esa uuuuu | -14 -39 116 27 -8 | -2 19
gfz uuuuu | 23 57 -61 -68 -15 | 11 23
grg --xxx | -- -- 98 19 14 | 16 32
igr xxxxx | 33 60 -34 33 -12 | 4 16
irf xxxxx | -3 12 -43 -17 15 | 9 26
jpl uuuuu | 51 -23 -113 328 -6 | -11 17
mit uuuuu | -10 31 -70 -12 30 | 9 27
ngs uuuuu | 19 -67 -32 -170 2 | -5 15
sio uuuuu | -19 96 26 22 34 | 26 38
Table 7.1569.4 GPS week: 1569 Day: 4 MJD: 55231.500
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 -8 86 32 -8 | 5 18
emr uuuuu | -53 9 -107 -59 6 | 20 28
esa uuuuu | -12 -5 153 85 0 | -4 19
gfz uuuuu | 56 26 -44 -118 -1 | 8 22
grg --xxx | -- -- 35 -172 -36 | 16 32
igr xxxxx | 10 34 -38 -103 -4 | 2 16
irf xxxxx | -3 -15 -18 5 13 | 8 25
jpl uuuuu | 75 -88 -80 53 6 | -12 18
mit uuuuu | 9 -29 -66 91 25 | 10 29
ngs uuuuu | -44 22 6 -118 -16 | -6 15
sio uuuuu | -29 48 17 113 30 | 28 40
Table 7.1569.5 GPS week: 1569 Day: 5 MJD: 55232.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 7 -26 -110 140 -6 | 5 18
emr uuuuu | -37 38 -106 -155 7 | 20 28
esa uuuuu | -6 -11 209 41 0 | -4 20
gfz uuuuu | 42 28 1 -133 5 | 8 22
grg --xxx | -- -- 202 -118 3 | 16 32
igr xxxxx | 23 42 134 -135 -3 | 1 16
irf xxxxx | 6 12 -86 43 6 | 11 27
jpl uuuuu | 18 -56 143 -72 -17 | -12 18
mit uuuuu | 20 23 -196 111 14 | 14 33
ngs uuuuu | -48 -79 -57 30 2 | -6 15
sio uuuuu | -11 98 -123 162 19 | 32 44
Table 7.1569.6 GPS week: 1569 Day: 6 MJD: 55233.500
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 | 12 -1 61 36 -7 | 2 20
emr uuuuu | -57 5 -55 -65 1 | 18 28
esa uuuuu | -29 -14 161 14 3 | -6 22
gfz uuuuu | 33 15 10 21 11 | 5 22
grg --xxx | -- -- 203 32 -34 | 14 32
igr xxxxx | 29 43 -8 14 -6 | -1 18
irf xxxxx | 15 -10 -61 131 -7 | 9 28
jpl uuuuu | 5 -31 169 -9 -13 | -16 25
mit uuuuu | 37 -25 -217 267 -4 | 14 33
ngs uuuuu | -6 3 -41 -297 -2 | -9 18
sio uuuuu | 17 70 -42 221 4 | 31 44
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