[IGSREPORT-18114] Wk 1561 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 24 05:40:22 PST 2009
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IGS Electronic Report 24 Dec 05:40:25 PST 2009 Message Number 18114
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1561 (Dec 06, 2009 - Dec 12, 2009)
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:
igs1561[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1561[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1561[0-6].cls IGS GPS clock combination summary report.
igs15617.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15617.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 | ALL | 1 1
0 | COD | 32
0 | EMR | WTZR WTZR
0 | ESA | 32 UNSA
0 | GFZ | 14 27 ALIC ALRT AMC2 ARTU BAKO BOR1 CEDU CONZ CRO1
0 | GFZ | DAEJ DARW DAV1 DGAR EIL1 FAA1 FAIR GRAZ GUAT HARB
0 | GFZ | HOB2 KARR KERG KOUR MAS1 MDO1 MIZU NRC1 ONSA PRDS
0 | GFZ | RIOP SANT SFER THTI THU3 TIDB TOW2 TSKB TWTF USUD
0 | GFZ | WSRT YAKT
0 | GRG | WTZR
0 | JPL | 32 DGAR
0 | MIT | GUAT HARB IRKT
1 | COD | 1 32 1 32 CHUR DAV1 FLIN
1 | EMR | 10 10 WTZR WTZR
1 | ESA | 5 32 SUTH UNSA
1 | GFZ | 3 5 10 13 17 29 ADE1 ALIC AREQ BJFS BRFT CAS1 DAEJ
1 | GFZ | DGAR GUAT HARB ISPA KIRU MAL2 MAS1 MBAR MDO1 NYA1
1 | GFZ | NYAL ONSA PIE1 REUN SANT SEY1 SFER SHAO TOW2 YAKT
1 | GFZ | YELL YKRO
1 | GRG | MCM4 TLSE WTZR
1 | JPL | 32 DGAR FLIN
1 | MIT | 5 24 5 24 HARB
2 | COD | 32 10 32 HARB
2 | EMR | WTZR
2 | ESA | 10 32
2 | GFZ | 3 5 11 13 14 18 22 27 28 32 ALIC AMC2 AREQ BAKO BOR1
2 | GFZ | BUE1 CHAT CONZ DARW FAA1 GUAT HARB HOB2 HOLM HRAO
2 | GFZ | HRM1 ISPA KARR LPGS MAS1 MBAR MCM4 MDO1 NICO NTUS
2 | GFZ | ONSA OUS2 PERT PRE1 SANT SCH2 SFER SUTH TIDB TOW2
2 | GFZ | TSKB TWTF UNSA WSRT YAR2 YKRO ZECK ZIMM
2 | GRG | WTZR
2 | JPL | 18 32 DGAR
2 | MIT | 24 24
2 | NGS | 1
3 | COD | 32 10 32
3 | EMR | WTZR WTZR
3 | ESA | 10 32
3 | GFZ | 5 18 19 20 ALIC AMC2 BAKO BOR1 BRUS CAS1 CHAT COCO
3 | GFZ | CRO1 DARW DAV1 DGAR FAA1 HRM1 KARR MAS1 MBAR MDO1
3 | GFZ | METS NANO NYA1 ONSA OUS2 PRE1 RABT SANT SCH2 SFER
3 | GFZ | SUTH TSKB VILL WHIT WSRT WTZR YAR2 ZECK
3 | GRG | TLSE WTZR
3 | JPL | 32 DGAR GUAT
3 | MIT | 1 1 DARW GUAT
3 | NGS | 1
4 | COD | 10 10 WTZR DUBO
4 | EMR | MCM4 WTZR
4 | ESA | 10 UNSA
4 | GFZ | 5 10 13 18 19 20 32 ADE1 ALIC AREQ AUCK BRFT BRUS
4 | GFZ | CAS1 CEDU CONZ DARW DAV1 DGAR FAA1 GODE HOB2 HOLM
4 | GFZ | KIRU LPGS MAC1 MATE MDO1 METS MIZU NRMD NYAL ONSA
4 | GFZ | OUS2 PDEL QAQ1 REUN SANT SFER THTI TIDB TWTF WSRT
4 | GFZ | WTZR YELL
4 | GRG | ONSA POTS TLSE
4 | JPL | 32 DGAR
4 | MIT | 1 6 24 1 6 24 DARW WTZR
4 | NGS | 1
5 | ALL | 8
5 | COD | 1 10 1 10
5 | EMR | 32 32 WTZR WTZR
5 | ESA | 10 32
5 | GFZ | 5 10 16 17 18 19 20 32 AMC2 AREQ AUCK BAKO BJFS BRAZ
5 | GFZ | CONZ DAEJ DGAR DUBO FAA1 FAIR GLSV GODE GRAZ GUAM
5 | GFZ | HARB HOFN HYDE KIRU KIT3 MBAR MCM4 MDO1 MIZU NANO
5 | GFZ | NYAL ONSA PRDS PRE1 QAQ1 RIOP SFER SHAO SUTH THTI
5 | GFZ | THU3 TRO1 TWTF VESL WTZR YELL ZIMM
5 | GRG | USUD
5 | JPL | 10 32 DGAR
5 | MIT | 24 24 DARW DARW HARB
6 | ALL | 1
6 | COD | 10 32 1 10 32
6 | EMR | WTZR
6 | ESA | 10 32 DARW FAA1 UNSA
6 | GFZ | 3 5 18 ALGO BOR1 BRAZ CAS1 CHAT DAV1 FAIR HOLM KARR
6 | GFZ | KIRU KIT3 MAS1 MCM4 MDO1 METS MIZU NICO NRMD NYA1
6 | GFZ | ONSA OUS2 PERT QAQ1 RABT REUN SCH2 TIDB TRO1 TSKB
6 | GFZ | VILL WHIT WSRT
6 | GRG | ALGO ONSA ZECK
6 | JPL | 32 CEDU DGAR FLIN
6 | MIT | 24 24 CEDU FLIN HARB
6 | NGS | 1
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
----+------------+----------
G07 | 2009_12_09 | 2009124
G08 | 2009_12_11 | 2009125
6. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
1 | ESA | 5
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 the all AC orbit and ERP values in order
to align them to the IGS05. These rotations were estimated in the process
of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based
on the common stations between the individual AC SINEX solutions and the
IGS05.snx SINEX. 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 1.0 .7 -29 -7 -17 .14
EMR | 6.4 -3.3 12.1 57 -25 1 .56
ESA | 10.2 -3.4 -2.2 26 -80 89 .19
GFZ | .6 1.4 1.0 10 -8 -11 .14
GRG | 13.6 11.3 3.1 204 -14 -522 .88
JPL | 4.9 1.7 19.5 14 -30 -18 .55
MIT | 2.8 -2.6 -4.5 22 -4 2 .13
NGS | 7.3 -7.4 -4.1 -81 -113 24 .28
SIO | 5.1 -1.4 -8.1 -35 -92 44 .51
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 NRCan. 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 1.1561.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1561.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 2.1561.[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 3.1561.[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 5.1561.0-6).
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 1561 summary. (Dec 06, 2009 - Dec 12, 2009)
Table 1.1561.a GPS week: 1561 MJD: 55171.000-55177.000
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 238| 0 0 0 36 -52 -4 -.15 8 8 | -406 128 16 69
| 0 0 0 20 19 18 .03 | 422 736
emr 89| 0 0 8 -128 -15 11 .51 19 19 | 384 273 22 90
| 2 2 1 21 26 16 .04 | 1104 1168
esa 121| 1 0 -2 -79 -12 17 .26 10 10 | -468 518 19 124
| 1 1 1 14 22 23 .02 | 560 1397
gfz 195| 0 -1 -3 -24 -53 -12 -.13 10 10 | 40 888 35 143
| 0 0 0 37 47 9 .06 | 696 2324
grg 110| 0 3 0 -425 -64 16 1.02 23 22 | 7 12 60 222
| 1 1 2 35 22 25 .03 | 261 642
igr n/a| 0 0 0 -10 -79 -71 .02 6 6 | 3172 570 24 86
| 0 0 0 15 22 20 .03 | 1507 1229
jpl 133| 0 1 7 -68 2 19 .57 17 15 | 1743 495 19 99
| 1 0 1 17 22 36 .04 | 1329 1373
mit 255| 0 0 -3 -29 -79 13 -.37 13 12 | -15620 234 20 118
| 1 0 0 27 22 15 .04 | 488 1708
ngs 217| 0 0 -1 138 153 -30 -.17 10 8 | -503176 529768 3039 26695
| 0 1 1 25 34 19 .03 | 492427 517191
sio 262| -2 3 3 84 87 12 .16 21 20 | --- --- --- ---
| 0 0 0 27 33 15 .03 | --- ---
Table 1.1561.b GPS week : 1561 MJD: 55171.000-55177.000
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 | 13 10 11 9 10 9 10 |
2 | 6 6 6 6 6 6 6 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 5 5 4 4 4 |
5 | 8 12 5 5 5 5 5 |
6 | 5 4 4 4 4 4 4 |
7 | 4 4 4 0 5 4 4 |
8 | 5 5 6 5 5 10 5 |
9 | 4 5 5 5 5 5 4 |
10 | 7 6 7 6 6 6 6 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 5 5 5 4 4 |
14 | 5 5 5 5 5 4 5 |
15 | 5 5 5 5 5 5 6 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 6 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 4 4 4 4 5 4 5 |
20 | 5 5 5 4 4 4 4 |
21 | 5 6 6 5 5 5 6 |
22 | 4 5 5 5 5 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 13 17 12 17 13 16 10 |
25 | 5 5 5 5 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 5 5 5 5 5 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 6 5 5 |
30 | 4 4 4 5 4 4 5 |
31 | 5 4 4 4 4 4 4 |
32 | 7 7 6 6 6 6 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 2.1561.0 GPS week: 1561 Day: 0 MJD: 55171.000
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 238| 0 0 0 29 -40 11 -.18 10 9 | -430 98 18 72
| -22 21 |
emr 89| -2 4 8 -155 -7 2 .45 20 20 | 111 613 23 73
| 2 -31 |
esa 121| 1 0 -2 -68 -43 10 .26 9 9 | -944 1790 17 106
| -24 33 |
gfz 195| 0 0 -2 6 -88 -6 -.05 11 11 | 323 -1387 40 168
| -30 -34 |
grg 110| 0 3 2 -423 -33 34 1.01 23 22 | -94 100 64 202
| 44 -20 |
igr n/a| 0 0 0 2 -88 -55 .03 6 6 | 1989 881 33 147
| -58 -18 |
jpl 133| -3 2 5 -57 6 66 .54 18 16 | 1165 967 15 86
| 17 -22 |
mit 255| 1 0 -3 -52 -36 -14 -.33 12 10 | -15473 -698 22 97
| -4 24 |
ngs 217| 0 -1 0 140 139 -20 -.19 10 7 | -999999 1097440 2050 3379
| 24 -5 |
sio 262| -1 2 4 70 141 -16 .14 22 19 | --- --- --- ---
| -106 -61 |
Table 2.1561.1 GPS week: 1561 Day: 1 MJD: 55172.000
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 238| 0 0 0 6 -29 -5 -.10 8 8 | -342 415 13 59
| 14 -46 |
emr 89| 1 -2 8 -117 34 0 .54 20 20 | 1702 -920 21 87
| -44 -61 |
esa 121| 1 1 -1 -81 7 -12 .25 12 12 | 160 -92 20 132
| -5 12 |
gfz 195| 0 -1 -4 -47 -104 -3 -.09 9 9 | 436 798 36 134
| -42 4 |
grg 110| 0 2 1 -464 -46 31 1.03 22 21 | 83 387 54 212
| 77 6 |
igr n/a| -1 1 0 0 -87 -55 .05 6 6 | 3635 -682 24 73
| -40 -25 |
jpl 133| -2 1 7 -75 40 59 .64 18 16 | 2536 -911 19 103
| 13 -85 |
mit 255| 1 0 -3 -1 -85 11 -.31 11 9 | -15687 241 21 116
| -29 32 |
ngs 217| 0 0 0 155 194 -30 -.18 11 8 | -999999 1123073 5116 84279
| 105 -35 |
sio 262| -1 3 3 106 96 14 .17 20 20 | --- --- --- ---
| -123 -41 |
Table 2.1561.2 GPS week: 1561 Day: 2 MJD: 55173.000
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 238| 0 1 0 66 -89 5 -.17 10 9 | 127 -690 22 82
| -52 17 |
emr 89| -3 0 8 -96 -29 15 .51 19 19 | 156 -292 55 128
| -35 -53 |
esa 121| 2 -3 -2 -83 -40 16 .27 12 12 | -616 -290 25 139
| -24 -4 |
gfz 195| 0 -1 -3 -88 9 -14 -.10 10 10 | 454 2102 37 172
| -48 -30 |
grg 110| 1 5 3 -387 -96 -2 .97 23 22 | 315 -734 60 225
| 12 54 |
igr n/a| 0 0 0 -2 -120 -97 .04 6 6 | 2332 -96 29 99
| -39 -14 |
jpl 133| 0 1 5 -38 -18 32 .57 16 14 | 994 -234 36 115
| 25 -34 |
mit 255| 0 0 -4 -46 -61 13 -.36 13 12 | -15345 331 31 144
| 7 12 |
ngs 217| 0 0 0 180 122 -43 -.20 10 7 | 13704 509 2265 3509
| -10 21 |
sio 262| -2 3 3 33 109 13 .12 20 18 | --- --- --- ---
| -87 -43 |
Table 2.1561.3 GPS week: 1561 Day: 3 MJD: 55174.000
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 238| 0 0 0 38 -46 21 -.15 8 7 | -2 -976 17 77
| 16 -35 |
emr 89| 0 2 7 -156 -4 12 .51 17 17 | 144 -996 16 81
| 9 -30 |
esa 121| 0 0 -2 -98 -10 12 .25 11 11 | 118 -989 18 125
| -16 -9 |
gfz 195| 0 -2 -4 -16 -78 -25 -.20 9 9 | 409 -982 37 140
| -39 0 |
grg 110| 0 4 0 -383 -52 47 1.04 23 22 | 387 -869 63 257
| -11 -14 |
igr n/a| 0 0 -1 0 -48 -101 .02 6 6 | 2712 -661 20 74
| -32 -33 |
jpl 133| 0 2 8 -92 20 27 .57 17 15 | 1296 -1005 17 104
| 13 -38 |
mit 255| -1 0 -4 12 -84 16 -.37 14 14 | -15580 -1007 18 110
| -20 28 |
ngs 217| 1 -2 -1 130 188 -61 -.15 10 8 | 16850 -1660 2356 3781
| 102 -84 |
sio 262| -3 4 3 113 39 12 .17 21 20 | --- --- --- ---
| -113 -8 |
Table 2.1561.4 GPS week: 1561 Day: 4 MJD: 55175.000
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 238| 0 0 1 53 -51 -21 -.16 8 7 | -309 197 14 77
| -34 -18 |
emr 89| 1 -3 6 -122 -19 -5 .52 19 19 | -1075 2361 16 91
| -16 -20 |
esa 121| 0 1 -2 -95 -2 28 .25 11 10 | -744 1208 20 126
| -19 -13 |
gfz 195| 0 0 -3 -33 -80 -3 -.10 10 10 | -1097 3086 34 141
| -19 -22 |
grg 110| 1 3 -1 -433 -74 29 1.04 22 20 | -282 650 66 232
| 39 18 |
igr n/a| 0 0 0 -13 -75 -73 -.02 6 6 | 1893 2824 24 72
| -20 -2 |
jpl 133| 0 0 7 -81 1 -3 .54 17 15 | 252 2886 18 96
| 8 -26 |
mit 255| -2 0 -3 -34 -98 37 -.39 14 13 | -15743 672 17 134
| -12 21 |
ngs 217| 0 0 -3 138 185 -37 -.16 10 7 | 13157 3316 2237 3925
| 95 -42 |
sio 262| -3 3 1 89 58 36 .12 20 22 | --- --- --- ---
| -108 -21 |
Table 2.1561.5 GPS week: 1561 Day: 5 MJD: 55176.000
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 238| 0 0 0 42 -65 -8 -.15 7 7 | -1067 981 14 54
| 9 -34 |
emr 89| 0 0 9 -120 -48 10 .56 19 19 | -375 275 12 70
| -19 1 |
esa 121| 1 0 -1 -58 11 2 .29 9 8 | -4 -713 18 116
| -68 -44 |
gfz 195| 0 -1 -4 -16 13 -7 -.20 10 10 | -838 4223 32 122
| -31 -42 |
grg 110| 0 1 0 -408 -84 -4 1.05 23 24 | -221 -199 60 224
| 37 50 |
igr n/a| 0 1 0 -39 -67 -54 -.01 5 5 | 3404 555 20 68
| -15 -31 |
jpl 133| 0 0 8 -69 -6 -11 .56 17 16 | 1641 485 15 95
| -12 -37 |
mit 255| -1 -1 -3 -61 -98 18 -.41 13 11 | -14960 -1556 19 96
| 8 18 |
ngs 217| 0 0 -2 122 113 -7 -.13 9 8 | -798350 752100 5022 84324
| 38 15 |
sio 262| -1 3 3 77 83 18 .19 21 19 | --- --- --- ---
| -84 -34 |
Table 2.1561.6 GPS week: 1561 Day: 6 MJD: 55177.000
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 238| 1 0 0 21 -42 -32 -.17 8 7 | -823 871 14 67
| 48 -25 |
emr 89| 2 2 11 -133 -32 46 .46 18 18 | 2026 875 17 101
| -32 -30 |
esa 121| -1 -1 -6 -70 -7 63 .27 10 10 | -1248 2712 20 125
| -56 12 |
gfz 195| 0 -1 -3 25 -43 -24 -.16 10 10 | 593 -1623 35 126
| -39 -13 |
grg 110| -2 0 -2 -476 -63 -19 1.00 22 21 | -135 750 59 202
| 101 4 |
igr n/a| 0 0 -1 -20 -70 -61 .01 5 5 | 6241 1170 20 72
| -48 -46 |
jpl 133| 0 0 7 -66 -23 -30 .59 16 15 | 4322 1278 18 95
| -20 -24 |
mit 255| -1 0 -2 -21 -89 8 -.41 14 13 | -16557 3655 18 134
| -5 9 |
ngs 217| 0 0 -1 98 130 -9 -.19 9 7 | -767601 733601 2230 3669
| 111 -36 |
sio 262| -1 3 3 101 81 11 .18 22 21 | --- --- --- ---
| -93 -52 |
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 3.1561.0 GPS week: 1561 Day: 0 MJD: 55171.000
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 | 11 49 --- --- --- 17 --- 18 16 --- 13 | 26 51 --- --- --- 35 --- 31 31 --- 30
2 | 11 23 8 12 20 7 22 15 12 23 5 | 14 33 17 21 35 20 32 18 18 19 16
3 | 7 14 9 11 18 6 10 12 8 25 4 | 15 20 24 23 20 19 21 17 18 17 17
4 | 10 12 6 8 28 5 9 8 5 27 3 | 33 29 35 31 40 30 30 34 31 39 31
5E | 13 25 10 15 16 9 26 32 9 36 7 | 40 45 81 40 46 43 42 57 39 60 41
6 | 8 11 11 10 15 5 11 14 8 25 4 | 21 22 27 25 21 21 22 26 21 23 22
7 | 8 21 10 9 27 5 16 7 8 12 4 | 10 24 17 11 15 15 19 11 14 11 12
8 | 11 22 7 8 17 8 14 13 8 17 4 | 8 24 17 12 28 11 20 16 14 17 11
9 | 10 21 6 10 16 6 14 8 6 25 4 | 20 30 23 22 29 18 25 19 21 31 19
10E | 16 21 8 12 20 11 23 7 26 21 6 | 29 38 37 32 44 32 39 34 42 40 31
11 | 7 17 10 8 25 5 15 6 8 18 4 | 36 40 39 36 44 32 37 37 38 31 36
12 | 10 24 9 10 26 6 22 13 7 18 5 | 26 38 29 22 44 27 36 23 26 24 25
13 | 6 22 9 10 28 4 17 10 8 14 4 | 18 33 23 21 46 20 29 19 20 17 19
14 | 11 20 7 12 27 7 19 9 9 16 4 | 19 33 24 23 37 20 29 22 23 18 21
15 | 10 23 8 7 23 5 24 9 9 23 5 | 23 32 24 22 39 22 29 21 27 23 22
16 | 8 27 11 7 29 7 22 10 7 16 4 | 25 41 24 21 43 23 36 22 25 24 23
17 | 11 13 8 13 19 7 14 13 8 30 4 | 24 26 30 31 33 25 25 27 25 41 26
18E | 7 19 9 12 15 6 21 14 8 17 4 | 41 44 43 44 53 43 43 46 40 46 41
19 | 9 17 9 8 23 6 10 7 8 28 4 | 24 22 30 28 27 25 19 27 23 25 24
20E | 10 17 12 10 20 5 21 9 8 16 4 | 20 29 25 23 33 23 31 22 28 26 23
21 | 14 18 7 11 28 7 19 10 10 29 5 | 22 35 26 19 46 22 36 20 24 19 23
22E | 9 17 9 11 30 7 19 9 8 14 4 | 37 38 36 41 45 37 38 36 37 37 35
23 | 7 28 9 11 25 6 19 8 6 18 4 | 20 39 24 24 40 23 29 19 22 20 20
X24 | 16 --- --- --- --- 48 --- 14 22 --- 12 | 27 --- --- --- --- 39 --- 30 27 --- 27
X25 | 8 18 11 8 --- 7 14 13 8 --- 4 | 15 22 20 17 --- 17 23 19 18 --- 15
26 | 9 10 7 9 19 6 14 9 9 26 4 | 19 22 20 14 28 15 26 19 22 35 19
27 | 10 20 7 11 17 6 14 9 8 25 4 | 13 26 20 19 27 15 19 16 18 27 14
28 | 10 17 9 11 37 4 18 8 8 12 4 | 20 31 22 18 48 21 30 16 21 18 18
29 | 7 16 10 10 21 6 13 9 7 35 4 | 21 27 28 23 30 23 23 27 23 30 22
30 | 6 14 6 10 10 5 12 8 7 18 3 | 55 61 59 55 64 56 63 57 57 67 58
31 | 7 19 8 9 33 7 19 14 10 13 4 | 12 29 15 15 39 12 24 13 13 12 12
32E | 14 24 12 13 17 6 15 21 20 15 6 | 44 47 45 40 54 41 48 42 53 41 43
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 9 10 23 6 18 12 10 22 |T 24 33 29 25 37 25 30 26 26 28 24
WRMS | 9 20 9 10 22 6 16 10 7 19 |NE 21 31 25 23 35 23 28 23 23 25 22
MEDI | 10 19 9 10 21 6 16 9 8 18 |MD 21 32 24 23 39 23 29 22 23 25 22
Table 3.1561.1 GPS week: 1561 Day: 1 MJD: 55172.000
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 28 --- --- --- 18 --- 16 14 --- 9 | 20 34 --- --- --- 34 --- 29 35 --- 26
2 | 10 26 10 12 20 7 23 15 12 21 5 | 11 31 14 16 34 14 30 11 18 13 12
3 | 7 12 12 7 14 5 10 12 9 22 4 | 11 16 14 12 17 11 15 14 18 15 11
4 | 9 13 6 9 25 6 7 8 8 28 4 | 19 19 21 19 30 19 21 18 23 27 18
X5E | 15 28 221 15 22 12 --- 38 9 --- 11 | 21 29 157 23 27 21 --- 26 24 --- 17
6 | 7 10 15 7 16 5 8 14 10 20 4 | 14 16 16 15 15 13 14 18 20 16 13
7 | 7 22 10 10 26 5 17 7 5 12 4 | 9 25 14 12 17 11 19 10 14 10 10
8 | 11 21 11 10 21 5 13 16 11 19 5 | 8 24 12 14 30 10 20 17 20 16 9
9 | 8 21 8 10 14 4 13 10 14 25 4 | 18 27 20 18 27 19 23 19 26 28 17
10E | 9 23 12 10 15 15 21 18 23 11 6 | 23 33 34 29 40 29 35 31 40 30 28
11 | 6 19 10 7 22 3 15 4 7 17 3 | 24 30 25 24 39 23 29 24 29 22 23
12 | 8 27 11 8 22 4 24 12 7 17 5 | 20 36 21 21 34 21 31 21 25 22 20
13 | 6 20 11 8 30 8 18 10 8 13 4 | 14 29 17 16 45 17 28 16 21 15 16
14 | 8 20 13 7 27 6 19 8 12 15 4 | 13 29 21 17 36 17 25 18 27 17 18
15 | 7 25 14 9 26 9 24 8 14 23 5 | 17 31 23 18 39 22 27 16 21 22 16
16 | 8 24 13 8 25 5 24 9 10 15 4 | 18 33 20 18 38 19 33 17 26 20 20
17 | 8 14 9 10 21 8 13 11 11 32 4 | 16 25 21 25 35 18 25 18 26 38 21
18E | 9 19 13 8 18 5 24 11 8 12 4 | 38 38 36 37 33 37 42 37 44 41 38
19 | 6 14 9 6 17 5 10 5 9 25 3 | 14 13 17 14 19 12 12 17 20 14 13
20E | 7 19 13 8 12 5 23 8 10 14 4 | 18 21 21 21 27 18 25 15 22 23 16
21 | 9 19 15 9 27 6 22 13 8 31 5 | 19 32 28 20 46 22 35 21 26 19 21
22E | 9 14 11 10 22 6 23 7 10 11 4 | 37 37 36 41 42 38 43 43 45 41 40
23 | 8 28 13 9 20 7 20 8 6 19 4 | 17 33 19 16 36 16 27 18 23 21 17
X24 | 22 24 --- --- --- 22 --- 16 49 --- 17 | 18 25 --- --- --- 28 --- 26 32 --- 22
X25 | 9 17 13 6 --- 6 13 14 7 --- 4 | 11 22 16 12 --- 14 21 21 21 --- 12
26 | 8 14 14 8 14 6 11 10 9 24 4 | 12 26 23 17 28 17 23 17 23 33 17
27 | 7 20 10 10 16 5 13 8 13 24 4 | 10 24 19 18 26 15 17 17 22 26 14
28 | 9 15 12 7 33 4 16 8 8 14 4 | 17 27 20 17 46 20 27 17 27 18 18
29 | 6 18 17 7 18 5 15 8 9 33 5 | 18 28 32 22 27 20 23 23 24 26 21
30 | 6 15 12 7 11 6 12 7 10 16 3 | 71 77 79 76 76 75 76 71 77 76 74
31 | 7 20 11 6 31 5 17 6 7 12 3 | 10 25 15 14 37 14 23 13 23 14 14
32E | 12 27 15 10 20 8 16 19 25 16 6 | 43 45 45 40 59 42 49 42 52 44 42
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 12 9 22 6 18 11 11 20 |T 19 29 28 22 34 22 28 22 27 25 21
WRMS | 8 20 12 9 21 6 16 9 8 20 |NE 17 28 21 19 33 20 26 20 25 22 18
MEDI | 8 20 12 8 21 6 16 10 9 17 |MD 17 28 21 18 34 19 25 18 24 22 17
Table 3.1561.2 GPS week: 1561 Day: 2 MJD: 55173.000
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 --- --- --- --- 14 --- 21 11 --- 11 | 21 --- --- --- --- 24 --- 27 22 --- 22
2 | 10 23 7 12 27 6 18 18 11 21 5 | 17 31 20 18 36 19 29 19 16 14 16
3 | 9 12 9 8 14 6 8 12 9 23 4 | 15 17 16 17 18 16 16 17 20 19 15
4 | 11 11 9 9 25 7 7 13 10 27 4 | 28 22 33 25 31 27 25 28 24 35 25
5E | 10 19 13 9 19 4 20 12 8 10 4 | 22 27 58 18 26 21 28 23 21 23 19
6 | 8 11 9 6 20 5 7 13 8 21 3 | 18 18 17 17 21 18 17 22 20 20 18
7 | 8 21 9 11 --- 5 16 9 7 12 4 | 13 25 15 10 --- 15 21 13 13 12 11
8 | 12 25 11 10 19 7 14 20 7 20 5 | 12 26 16 15 32 15 22 25 17 20 13
9 | 9 24 11 8 17 7 15 12 11 22 5 | 13 29 19 19 27 18 23 19 22 27 15
10E | 9 22 23 8 27 9 22 13 23 11 6 | 22 32 34 25 36 24 37 21 29 26 22
11 | 7 17 9 6 23 5 13 9 8 17 4 | 31 32 29 28 41 31 32 30 32 27 28
12 | 10 21 15 11 23 4 18 15 9 17 5 | 24 31 24 20 35 24 29 21 25 23 21
13 | 7 21 15 13 31 7 16 15 7 12 5 | 19 32 21 19 47 19 29 23 22 18 19
14 | 10 20 14 8 27 5 16 8 9 17 4 | 17 30 25 21 35 19 28 19 23 23 20
15 | 8 21 14 9 22 8 18 12 10 22 5 | 19 30 23 17 40 19 27 20 21 23 17
16 | 10 21 13 8 24 6 19 11 6 16 4 | 22 37 28 23 40 23 33 20 23 25 23
17 | 9 14 9 16 21 7 14 11 10 30 5 | 21 25 27 35 27 23 25 21 19 38 23
18E | 10 16 12 12 34 7 23 16 9 14 5 | 38 39 38 37 49 37 42 36 35 38 36
19 | 7 14 8 8 19 5 9 6 9 26 4 | 21 19 17 21 20 21 17 25 22 23 20
20E | 7 13 12 12 15 5 20 16 8 13 4 | 22 25 23 19 27 22 28 28 24 24 21
21 | 14 20 8 12 26 5 19 12 8 29 5 | 21 31 24 20 38 19 33 20 18 20 19
22E | 13 16 13 11 23 5 20 12 9 10 5 | 31 32 32 33 33 31 34 34 34 33 32
23 | 8 26 12 11 23 7 19 12 6 17 5 | 20 35 20 18 38 20 29 24 24 21 20
X24 | 9 27 --- --- --- 10 --- 16 --- --- 11 | 23 23 --- --- --- 35 --- 28 --- --- 21
X25 | 7 17 11 6 --- 4 11 17 7 --- 4 | 16 22 18 19 --- 19 22 27 21 --- 17
26 | 9 14 12 8 15 5 9 9 8 25 4 | 22 30 27 25 33 25 28 26 28 41 25
27 | 10 22 10 8 16 6 16 13 9 22 5 | 13 28 19 19 30 18 20 21 18 28 14
28 | 8 15 10 6 34 5 12 6 7 13 3 | 17 30 21 17 44 19 27 17 20 18 18
29 | 10 14 14 8 19 6 15 13 7 34 5 | 20 21 28 19 22 21 23 21 21 25 18
30 | 9 16 9 7 15 6 13 11 8 16 4 | 47 49 49 48 47 46 49 45 44 48 45
31 | 6 16 14 7 28 5 16 8 7 13 4 | 12 24 17 15 35 14 21 14 17 18 13
32E | 14 25 15 10 20 6 13 17 21 16 6 | 49 49 50 45 52 45 51 51 50 45 47
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 12 10 23 6 16 13 10 20 |T 22 29 26 22 34 23 28 24 24 26 21
WRMS | 9 19 12 10 22 6 14 12 7 18 |NE 20 27 23 21 33 21 26 22 22 24 19
MEDI | 9 19 11 8 22 6 16 12 8 17 |MD 21 30 23 19 35 21 28 22 22 23 20
Table 3.1561.3 GPS week: 1561 Day: 3 MJD: 55174.000
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 | 12 19 --- --- --- 14 --- 20 14 --- 9 | 23 39 --- --- --- 27 --- 35 37 --- 29
2 | 9 21 11 11 28 6 20 19 7 24 5 | 17 31 18 18 38 17 31 19 20 21 17
3 | 4 11 12 9 15 7 10 13 8 22 4 | 14 21 17 18 27 16 19 19 19 18 15
4 | 10 9 11 6 21 4 8 16 9 26 4 | 28 25 30 27 39 26 26 29 29 30 27
5E | 9 17 9 7 23 3 21 13 11 13 4 | 21 31 25 27 36 24 30 24 25 29 24
6 | 4 8 10 6 14 7 10 12 8 21 3 | 18 21 21 22 26 20 20 24 24 20 19
X7 | 4 --- --- --- --- 20 --- --- --- --- 0 | 9 --- --- --- --- 16 --- --- --- --- 10
8 | 12 23 8 8 14 5 16 18 10 22 5 | 11 28 18 14 30 13 24 21 15 20 14
9 | 9 21 8 9 16 5 17 14 10 23 5 | 24 33 27 27 33 26 29 28 28 38 24
10E | 9 19 20 12 16 6 19 14 21 12 6 | 21 36 37 29 38 26 36 24 27 30 25
11 | 6 18 9 8 25 5 15 13 11 18 4 | 31 35 37 33 41 30 32 32 34 29 31
12 | 7 19 10 9 23 5 20 14 7 18 4 | 25 37 26 24 39 25 34 28 25 30 25
13 | 5 19 11 7 26 4 17 16 9 14 4 | 22 36 28 25 48 24 31 24 26 22 24
14 | 8 20 12 8 26 3 21 11 7 17 4 | 16 29 23 21 36 20 28 21 24 24 20
15 | 6 21 10 9 23 7 21 15 7 22 5 | 19 32 25 23 41 23 29 22 23 27 21
16 | 6 22 9 7 23 6 22 15 6 19 4 | 25 40 28 24 43 25 36 24 30 27 26
17 | 10 14 14 18 21 8 16 11 13 31 5 | 22 26 30 35 29 23 25 21 27 37 26
18E | 6 12 9 9 30 7 22 15 11 7 4 | 30 34 34 34 44 31 34 30 34 31 30
19 | 7 10 10 6 21 6 11 10 9 26 4 | 21 23 25 24 28 23 19 27 27 24 22
20E | 6 15 9 10 13 4 18 12 7 11 4 | 23 25 24 27 30 25 29 25 24 24 23
21 | 8 19 9 9 24 6 19 10 7 27 4 | 24 36 30 23 47 28 38 25 31 24 27
22E | 9 15 12 7 46 7 22 14 12 10 4 | 31 35 37 33 43 30 32 29 32 30 31
23 | 8 26 11 11 20 6 19 14 7 19 5 | 25 42 26 27 40 27 33 26 26 26 25
X24 | 11 --- --- --- --- 71 --- 24 --- --- 17 | 30 --- --- --- --- 62 --- 41 --- --- 33
X25 | 7 19 8 8 --- 4 11 18 9 --- 4 | 19 28 22 22 --- 22 25 25 24 --- 20
26 | 6 14 10 8 21 5 12 12 5 25 4 | 18 29 24 23 33 23 26 25 25 39 23
27 | 8 19 7 7 14 4 14 14 9 23 4 | 17 26 22 22 28 20 19 24 24 34 19
28 | 8 16 9 6 30 5 15 12 9 15 4 | 22 30 23 21 45 21 28 18 20 22 20
29 | 7 14 9 10 15 9 12 20 7 34 5 | 24 26 25 26 30 24 24 32 26 33 25
30 | 6 16 8 10 15 11 14 15 8 29 4 | 123 124 126 125 124 123 123 123 124 130 123
31 | 4 16 12 6 23 4 13 10 13 12 4 | 14 29 19 19 39 20 25 18 22 21 17
32E | 10 22 10 12 35 7 13 14 19 13 5 | 62 63 66 61 73 63 65 62 70 65 63
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 11 9 23 6 17 14 10 21 |T 25 35 30 29 41 28 32 29 30 32 27
WRMS | 7 17 11 9 22 6 15 14 8 20 |NE 24 34 29 27 40 27 31 29 29 31 26
MEDI | 7 18 10 8 21 6 16 14 9 19 |MD 22 31 25 24 38 24 29 25 26 27 24
Table 3.1561.4 GPS week: 1561 Day: 4 MJD: 55175.000
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 | 15 26 --- --- --- 19 --- 17 13 --- 9 | 20 37 --- --- --- 28 --- 28 31 --- 25
2 | 10 22 10 11 23 5 21 20 12 24 5 | 13 28 20 19 36 15 29 13 19 17 15
3 | 4 10 11 9 12 6 10 11 9 23 4 | 11 16 11 17 20 11 14 16 14 17 10
4 | 8 10 8 9 20 5 8 15 12 21 4 | 21 25 27 25 33 24 22 27 28 27 24
5E | 7 17 9 11 19 2 20 14 9 12 4 | 16 22 20 21 29 18 24 17 24 21 18
6 | 4 10 12 7 21 5 8 12 10 22 4 | 14 17 11 18 20 14 14 21 18 17 13
7 | 6 20 12 17 18 11 19 11 8 16 5 | 8 24 12 15 24 10 19 12 15 12 10
8 | 12 17 9 10 19 7 13 19 8 20 5 | 12 22 15 15 27 12 19 21 17 20 13
9 | 8 21 10 10 18 5 13 12 8 23 4 | 14 25 13 13 27 11 18 18 16 29 11
10E | 9 17 17 9 14 7 17 16 17 13 5 | 28 39 42 32 44 33 42 32 35 36 32
11 | 5 17 8 10 22 3 15 13 7 18 4 | 26 33 28 23 37 23 26 28 26 23 24
12 | 6 22 10 9 24 4 20 13 10 18 4 | 19 32 19 13 38 18 28 20 21 22 18
13 | 6 18 15 11 26 8 19 16 11 14 5 | 15 30 20 20 45 16 26 15 21 12 15
14 | 8 18 12 8 22 4 18 12 9 17 4 | 12 27 20 15 36 15 24 17 22 22 17
15 | 5 24 9 9 24 7 18 15 9 19 4 | 16 32 19 17 35 17 24 20 23 23 17
16 | 8 28 9 8 27 6 24 15 7 17 5 | 21 38 19 17 38 16 33 18 22 20 19
17 | 9 12 11 12 20 7 15 9 15 31 5 | 20 25 25 28 32 24 24 21 31 37 24
18E | 7 17 14 10 24 5 23 13 6 7 4 | 25 31 34 30 29 28 33 30 30 32 28
19 | 6 13 7 10 18 5 12 14 8 27 4 | 16 22 18 21 24 18 16 26 18 22 16
20E | 5 16 8 12 10 6 18 14 8 14 4 | 16 27 24 24 31 17 24 17 19 24 18
21 | 11 18 10 7 24 5 19 11 7 28 5 | 19 29 19 12 39 17 31 15 21 17 17
22E | 9 19 13 7 49 5 22 14 7 10 4 | 18 27 25 21 40 21 26 21 24 22 20
23 | 7 24 12 11 19 9 19 14 9 18 5 | 15 33 22 19 37 16 25 16 18 15 15
X24 | 12 21 --- --- --- 15 --- 24 --- --- 13 | 20 24 --- --- --- 32 --- 27 --- --- 20
X25 | 5 18 9 8 --- 7 13 17 7 --- 4 | 8 20 13 14 --- 10 18 15 16 --- 8
26 | 7 13 11 9 18 4 11 11 7 25 4 | 14 27 18 17 32 15 24 20 21 38 18
27 | 7 22 9 11 16 5 13 14 9 24 4 | 10 26 11 13 26 11 16 19 14 29 10
28 | 6 18 10 9 29 4 15 10 6 11 3 | 18 31 25 19 47 20 29 21 20 20 20
29 | 8 16 13 9 17 6 15 20 9 35 5 | 14 21 23 17 23 14 18 27 21 23 17
30 | 7 19 7 9 19 5 13 10 9 16 4 | 48 54 50 44 50 47 53 49 54 53 50
31 | 5 16 9 11 24 6 16 11 10 13 4 | 11 23 16 12 37 11 20 15 16 17 12
32E | 13 31 12 16 18 9 12 14 16 15 6 | 53 62 62 55 74 49 59 54 49 50 53
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 11 10 22 6 17 14 10 20 |T 18 29 22 20 34 19 25 22 23 24 19
WRMS | 7 19 10 10 20 6 15 13 7 22 |NE 16 27 19 18 33 17 23 20 21 23 17
MEDI | 7 18 10 9 20 5 15 14 9 18 |MD 16 27 20 18 35 17 24 20 21 22 17
Table 3.1561.5 GPS week: 1561 Day: 5 MJD: 55176.000
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 | 12 20 --- --- --- 17 --- 18 12 --- 8 | 18 32 --- --- --- 19 --- 26 20 --- 20
2 | 10 21 11 10 26 6 21 21 9 25 5 | 14 26 19 17 34 16 27 15 14 19 13
3 | 5 14 8 9 11 8 11 7 7 23 3 | 12 19 14 15 22 15 18 15 14 15 11
4 | 7 11 9 6 23 5 10 13 6 19 3 | 21 22 25 22 35 24 22 26 24 25 21
5E | 7 22 11 9 21 4 20 13 8 9 4 | 12 21 26 16 29 13 20 14 14 15 12
6 | 8 11 7 5 22 5 11 10 7 22 3 | 17 16 16 16 23 17 18 20 15 16 13
7 | 6 22 6 12 20 7 19 8 5 17 4 | 11 27 14 11 25 9 22 9 7 8 9
X8 | 7 --- 12 --- --- 31 --- --- --- --- 10 | 7 --- 22 --- --- 27 --- --- --- --- 5
9 | 10 20 7 11 18 3 13 11 8 24 4 | 19 28 17 18 29 16 22 20 19 29 16
10E | 12 23 19 11 23 7 17 15 15 14 5 | 34 42 45 35 53 33 43 33 38 38 36
11 | 6 19 4 9 24 6 19 11 10 18 4 | 27 30 27 27 39 26 27 31 30 25 25
12 | 6 24 9 10 24 3 19 10 7 18 4 | 16 30 16 14 35 17 26 18 15 21 14
13 | 6 19 8 8 27 6 19 10 7 15 4 | 16 30 24 17 46 19 28 15 18 16 16
14 | 8 17 9 6 27 6 19 12 9 17 4 | 13 27 27 17 39 16 26 18 15 22 16
15 | 5 18 6 13 26 5 18 15 9 24 4 | 16 28 18 18 37 16 25 20 18 23 15
16 | 7 26 7 7 26 5 22 16 9 18 5 | 18 34 17 15 35 15 28 18 16 18 15
17 | 7 12 9 14 19 3 17 7 8 31 4 | 19 26 26 27 31 24 25 21 25 38 22
18E | 7 14 10 9 25 6 21 15 10 10 4 | 18 25 22 19 31 17 25 17 25 17 20
19 | 7 16 6 6 18 5 11 15 5 30 4 | 18 23 20 21 25 22 19 28 20 23 18
20E | 5 19 7 9 12 5 17 12 9 10 4 | 19 24 19 17 24 18 24 19 21 20 16
21 | 10 19 9 10 29 4 19 9 6 34 5 | 18 30 21 14 39 17 30 15 18 20 17
22E | 9 19 6 8 38 7 18 13 9 13 4 | 20 25 18 18 39 16 24 21 23 20 18
23 | 6 25 8 8 21 6 21 14 8 19 4 | 20 34 25 19 36 21 29 20 20 20 19
X24 | 18 47 --- --- --- 45 --- 19 30 --- 15 | 24 56 --- --- --- 53 --- 28 26 --- 27
X25 | 5 15 7 9 --- 5 12 12 6 --- 3 | 14 18 17 16 --- 16 20 16 16 --- 12
26 | 6 15 7 9 20 5 10 10 8 25 4 | 14 27 21 17 30 16 23 17 16 37 15
27 | 8 21 6 9 17 3 12 12 8 25 4 | 12 26 14 17 28 13 18 18 15 28 12
28 | 6 17 8 8 27 4 16 7 7 15 3 | 19 32 22 20 48 21 32 18 22 20 20
29 | 6 13 14 10 20 5 12 18 8 35 5 | 19 20 25 19 28 18 21 27 22 26 19
30 | 7 17 9 12 16 5 15 14 8 16 4 | 72 75 72 75 72 74 75 72 73 73 72
31 | 5 17 8 10 27 6 17 11 12 13 4 | 11 24 16 15 37 11 22 16 10 16 10
32E | 9 27 7 16 16 8 17 11 17 13 5 | 66 70 71 64 77 64 71 66 61 70 65
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 9 10 23 5 17 13 9 21 |T 20 30 24 21 36 22 27 23 22 25 19
WRMS | 7 19 8 10 24 5 16 11 8 19 |NE 18 29 22 20 35 21 26 21 20 24 18
MEDI | 7 19 8 9 22 5 17 12 8 18 |MD 18 27 21 17 35 17 25 19 19 20 16
Table 3.1561.6 GPS week: 1561 Day: 6 MJD: 55177.000
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 | 12 33 --- --- --- 14 --- 18 13 --- 10 | 25 41 --- --- --- 31 --- 28 33 --- 27
2 | 9 20 11 11 31 5 21 22 12 28 6 | 19 31 22 21 38 19 32 17 17 23 17
3 | 8 10 7 8 15 5 10 10 9 25 3 | 14 17 18 18 21 13 18 20 17 19 15
4 | 9 10 9 6 25 3 10 17 6 20 4 | 30 29 36 30 34 30 29 32 33 28 30
5E | 9 20 11 8 17 4 18 14 9 10 4 | 16 26 26 16 29 18 25 17 18 20 15
6 | 8 10 8 9 21 6 10 10 8 23 3 | 21 19 21 22 21 18 19 26 21 20 19
7 | 5 17 11 8 22 4 15 13 8 18 4 | 11 22 10 11 25 10 18 11 13 11 10
X8 | 10 --- 11 9 --- 6 16 15 9 24 5 | 7 --- 6 5 --- 10 10 5 7 5 6
9 | 8 17 7 9 19 4 13 12 7 24 4 | 14 26 20 18 28 16 20 19 18 27 15
10E | 11 19 18 16 13 6 13 16 15 13 5 | 34 43 50 35 51 40 48 39 38 40 37
11 | 6 19 7 7 21 5 15 14 10 17 4 | 33 35 35 33 41 31 32 36 34 29 30
12 | 7 27 10 11 22 4 19 11 6 20 5 | 26 42 25 21 35 25 33 27 24 28 25
13 | 5 16 10 8 29 4 15 13 6 16 4 | 17 28 19 17 44 17 28 15 19 14 17
14 | 9 23 7 6 30 6 20 11 10 19 4 | 15 29 21 17 38 16 27 19 22 24 18
15 | 6 23 17 12 27 5 22 16 9 21 5 | 19 29 26 18 41 19 27 22 21 23 17
16 | 6 27 10 9 26 5 21 15 11 22 5 | 26 43 25 23 42 26 37 23 29 26 25
17 | 8 10 10 15 22 4 14 7 7 33 4 | 24 26 31 34 33 29 26 25 26 41 26
18E | 8 17 13 12 --- 5 19 15 9 9 4 | 19 29 31 22 --- 22 29 24 23 27 22
19 | 8 12 11 7 18 4 12 17 10 28 4 | 23 21 27 25 25 22 20 33 26 23 23
20E | 6 18 8 8 17 5 13 12 6 12 3 | 13 23 19 13 24 13 19 15 15 17 13
21 | 11 20 11 10 25 6 20 11 7 37 5 | 19 33 23 15 38 17 33 13 20 21 18
22E | 8 14 6 7 19 5 17 11 7 13 3 | 23 29 25 27 37 24 31 23 27 27 25
23 | 7 24 11 11 22 5 17 18 8 20 5 | 18 32 20 20 35 18 26 21 21 19 18
X24 | 14 16 --- --- --- 34 --- 14 21 --- 9 | 30 30 --- --- --- 56 --- 33 36 --- 32
X25 | 5 16 8 7 --- 5 14 14 8 --- 4 | 14 21 18 15 --- 15 22 19 19 --- 15
26 | 7 13 7 9 17 4 10 11 5 27 4 | 13 21 18 16 27 14 22 16 20 35 16
27 | 7 18 7 8 20 4 13 13 7 26 4 | 9 23 18 18 28 15 17 20 17 29 13
28 | 7 19 7 9 27 4 16 11 11 19 4 | 26 36 30 21 44 26 32 21 19 25 24
29 | 6 13 11 10 18 4 14 20 7 37 5 | 21 24 31 23 29 22 23 27 23 30 22
30 | 8 15 8 13 18 3 16 15 8 17 4 | 61 64 63 64 60 62 61 60 57 64 60
31 | 6 17 9 10 32 4 15 10 8 15 4 | 12 25 13 17 39 14 25 16 17 18 13
32E | 11 23 10 12 18 6 15 13 11 16 5 | 70 71 71 72 70 69 73 74 77 76 71
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 10 10 22 5 16 14 9 22 |T 22 31 26 23 36 24 28 24 25 27 22
WRMS | 7 18 10 10 21 5 15 13 7 21 |NE 21 29 24 21 34 22 26 23 23 25 21
MEDI | 8 17 10 9 21 5 15 13 8 20 |MD 19 29 23 20 35 19 26 21 21 25 18
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 4.1561 GPS week: 1561 MJD: 55171.0-55177.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 |U 7 8 23 |U 38 39 142 |U 9 11 22 |
emr | emr 2975 | 18 12 45 |U 40 40 143 | 10 11 22 |
esa | esa 2852 | 8 9 25 |U 34 31 99 | 9 10 21 |
gfz | gfz 2798 |U 21 15 56 |U 39 41 97 | 19 21 44 |
grg | grg 2715 | 10 10 31 |U 38 44 136 | 10 11 23 |
igr | igr 2845 | 12 13 31 | 39 37 120 | 10 14 28 |
igs | igs 2948 | 13 10 33 | 38 41 143 | 9 12 23 |
jpl | jpl 2828 |U 14 12 37 |U 23 30 122 |U 9 12 24 |
mit | mit 3044 |U 13 10 33 |U 34 42 121 |U 10 13 24 |
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 5.1561.0 GPS week: 1561 Day: 0 MJD: 55171.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 | 7 7 17 | 9 12 28 | 9 12 17 |
emr | emr 2968 | 12 15 24 | 9 10 34 | 9 9 21 |
esa | esa 2880 | 8 11 21 | 9 12 31 | 8 10 17 |
gfz | gfz 2829 | 14 11 43 | 12 16 45 | 18 18 35 |
grg | grg 2784 | 8 10 23 | 9 14 35 | 9 8 19 |
igr | igr 2848 | 19 24 35 | 15 17 46 | 15 18 51 |
igs | igs 2935 | 9 10 19 | 9 12 28 | 8 9 17 |
jpl | jpl 2870 | 10 13 24 | 10 12 34 | 8 9 19 |
mit | mit 3072 | 10 11 23 | 10 14 36 | 9 9 18 |
Table 5.1561.1 GPS week: 1561 Day: 1 MJD: 55172.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 | 6 7 26 | 221 217 831 | 7 8 19 |
emr | emr 3059 | 11 8 31 | 225 225 795 | 11 11 20 |
esa | esa 2880 | 7 8 28 | 192 164 524 | 9 10 18 |
gfz | gfz 2826 | 17 16 33 | 201 202 387 | 20 25 42 |
grg | grg 2784 | 7 8 31 | 204 241 746 | 10 9 22 |
igr | igr 2771 | 10 7 32 | 212 198 633 | 9 10 19 |
igs | igs 3009 | 7 6 29 | 223 234 831 | 8 9 19 |
jpl | jpl 2771 | 11 10 45 | 113 150 666 | 9 9 19 |
mit | mit 3072 | 8 7 23 | 190 239 658 | 9 9 23 |
Table 5.1561.2 GPS week: 1561 Day: 2 MJD: 55173.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 7 5 24 | 6 10 25 | 8 11 25 |
emr | emr 2960 | 12 6 22 | 8 8 29 | 10 12 26 |
esa | esa 2880 | 8 6 23 | 6 7 23 | 9 12 22 |
gfz | gfz 2824 | 16 12 69 | 14 15 45 | 15 15 43 |
grg | grg 2688 | 10 12 29 | 9 10 33 | 11 16 28 |
igr | igr 2770 | 14 17 30 | 12 11 31 | 14 21 36 |
igs | igs 3011 | 10 6 24 | 8 10 28 | 11 15 33 |
jpl | jpl 2869 | 11 7 28 | 7 7 26 | 9 11 23 |
mit | mit 3072 | 11 7 32 | 7 7 23 | 12 15 28 |
Table 5.1561.3 GPS week: 1561 Day: 3 MJD: 55174.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 7 11 29 | 6 9 21 | 9 13 21 |
emr | emr 2871 | 13 12 34 | 6 9 32 | 11 14 25 |
esa | esa 2784 | 8 10 28 | 6 8 24 | 8 9 18 |
gfz | gfz 2729 | 14 17 50 | 14 14 47 | 16 20 36 |
grg | grg 2688 | 10 10 33 | 10 9 38 | 12 13 22 |
igr | igr 2808 | 14 16 32 | 7 7 23 | 8 13 22 |
igs | igs 2850 | 15 16 31 | 6 7 23 | 9 14 28 |
jpl | jpl 2775 | 16 16 37 | 6 9 31 | 11 16 30 |
mit | mit 2976 | 13 13 32 | 7 7 26 | 10 17 33 |
Table 5.1561.4 GPS week: 1561 Day: 4 MJD: 55175.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 8 9 25 | 7 7 24 | 8 11 24 |
emr | emr 3060 | 11 12 41 | 9 9 32 | 8 9 16 |
esa | esa 2880 | 9 9 23 | 7 7 27 | 8 9 20 |
gfz | gfz 2824 | 46 22 86 | 13 13 72 | 25 19 61 |
grg | grg 2784 | 10 12 29 | 10 10 26 | 8 13 19 |
igr | igr 2929 | 12 12 31 | 8 7 29 | 8 12 20 |
igs | igs 3022 | 11 11 33 | 7 7 26 | 8 11 22 |
jpl | jpl 2869 | 13 12 30 | 9 9 33 | 8 11 26 |
mit | mit 3072 | 10 10 24 | 8 9 36 | 9 12 19 |
Table 5.1561.5 GPS week: 1561 Day: 5 MJD: 55176.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 9 7 28 | 7 11 29 | 8 8 23 |
emr | emr 2958 | 32 16 83 | 10 11 38 | 10 12 24 |
esa | esa 2784 | 10 9 34 | 6 9 29 | 10 12 26 |
gfz | gfz 2730 | 32 21 86 | 10 13 39 | 23 32 62 |
grg | grg 2688 | 13 12 43 | 9 10 38 | 11 13 28 |
igr | igr 2843 | 9 7 38 | 8 9 32 | 11 16 27 |
igs | igs 2849 | 30 13 78 | 8 8 32 | 10 13 25 |
jpl | jpl 2775 | 31 14 78 | 8 9 34 | 12 13 33 |
mit | mit 2976 | 30 14 77 | 8 9 35 | 12 15 26 |
Table 5.1561.6 GPS week: 1561 Day: 6 MJD: 55177.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 7 8 16 | 9 10 37 | 10 11 23 |
emr | emr 2950 | 32 14 80 | 11 12 39 | 10 12 24 |
esa | esa 2880 | 7 8 20 | 8 11 34 | 9 11 23 |
gfz | gfz 2830 | 11 9 26 | 11 13 42 | 15 19 31 |
grg | grg 2592 | 12 9 27 | 11 11 35 | 9 8 22 |
igr | igr 2950 | 8 9 17 | 9 12 44 | 7 11 18 |
igs | igs 2960 | 8 9 16 | 8 10 32 | 10 13 19 |
jpl | jpl 2871 | 9 9 19 | 10 11 33 | 9 13 20 |
mit | mit 3072 | 6 7 17 | 9 10 33 | 11 16 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 6.1561 GPS week: 1561 MJD: 55171.500-55177.500
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 | 3 -6 -60 66 3 | 1 16
| 23 33 97 98 5 | 5
emr uuuuu | 18 11 -239 -175 3 | 48 49
| 23 18 93 90 6 | 2
esa uuuuu | -12 22 183 -126 10 | -16 23
| 21 21 81 39 10 | 1
gfz uuuuu | 5 27 31 -5 -12 | 1 15
| 20 9 35 47 7 | 5
grg --xxx | -- -- 38 81 -6 | 12 23
| -- -- 169 20 29 | 2
igr xxxxx | 10 27 4 -14 4 | -7 15
| 14 17 93 68 5 | 2
irf xxxxx | -14 -9 -5 23 6 | -6 16
| 6 9 53 17 6 | 2
jpl uuuuu | 24 -15 -65 45 2 | 12 18
| 22 19 104 84 9 | 2
mit uuuuu | -35 -1 -138 167 10 | -3 18
| 10 20 141 140 8 | 1
ngs uuuuu | 9 -75 5 2 -3 | -7 13
| 34 42 97 64 7 | 1
sio uuuuu | 23 93 111 128 10 | 16 23
| 23 21 125 115 10 | 2
Table 7.1561.0 GPS week: 1561 Day: 0 MJD: 55171.500
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 | -24 11 -82 250 8 | -4 8
emr uuuuu | 28 -13 -249 -149 10 | 46 46
esa uuuuu | -36 13 208 -139 5 | -16 22
gfz uuuuu | 31 19 -10 24 3 | 6 10
grg --xxx | -- -- -138 72 -39 | 15 24
igr xxxxx | 15 47 -44 67 -3 | -4 13
irf xxxxx | -3 -11 39 8 -7 | -3 14
jpl uuuuu | 19 -28 -93 170 6 | 8 14
mit uuuuu | -27 -7 34 1 -3 | -1 17
ngs uuuuu | 2 -35 -181 80 -6 | -7 11
sio uuuuu | 58 95 281 67 -10 | 16 21
Table 7.1561.1 GPS week: 1561 Day: 1 MJD: 55172.500
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 | 33 -22 40 -58 5 | -3 10
emr uuuuu | 48 36 -393 0 3 | 47 48
esa uuuuu | -25 -3 152 -85 15 | -17 22
gfz uuuuu | -17 34 42 23 -16 | 7 10
grg --xxx | -- -- -70 76 2 | 11 23
igr xxxxx | 12 32 -62 19 12 | -5 12
irf xxxxx | -13 -8 69 28 7 | -5 13
jpl uuuuu | 72 -21 -236 144 18 | 9 15
mit uuuuu | -45 21 58 -62 16 | -3 16
ngs uuuuu | 22 -113 -42 62 -7 | -6 11
sio uuuuu | 28 115 261 -69 12 | 15 20
Table 7.1561.2 GPS week: 1561 Day: 2 MJD: 55173.500
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 31 -24 122 9 | -4 11
emr uuuuu | 41 14 -324 -257 8 | 47 47
esa uuuuu | -8 3 294 -186 10 | -18 22
gfz uuuuu | 18 27 23 8 -15 | 3 13
grg --xxx | -- -- -119 74 -20 | 9 23
igr xxxxx | 2 18 -140 5 5 | -7 12
irf xxxxx | -12 -21 27 1 11 | -7 14
jpl uuuuu | 22 -46 -98 -6 3 | 11 15
mit uuuuu | -24 -28 -116 174 16 | -4 16
ngs uuuuu | -33 -11 4 24 -10 | -8 14
sio uuuuu | 31 66 142 169 14 | 14 20
Table 7.1561.3 GPS week: 1561 Day: 3 MJD: 55174.500
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 -16 -248 44 -6 | 10 24
emr uuuuu | 9 -9 -154 -267 5 | 50 52
esa uuuuu | -12 16 191 -134 -1 | -14 23
gfz uuuuu | -21 39 15 16 -16 | 4 14
grg --xxx | -- -- 47 127 16 | 12 24
igr xxxxx | 12 32 100 -139 4 | -5 15
irf xxxxx | -21 0 -65 42 12 | -4 17
jpl uuuuu | 17 -13 48 20 -4 | 14 20
mit uuuuu | -49 20 -277 255 19 | -2 20
ngs uuuuu | 63 -102 41 21 3 | -6 14
sio uuuuu | -13 113 58 67 22 | 18 27
Table 7.1561.4 GPS week: 1561 Day: 4 MJD: 55175.500
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 36 20 18 1 | 5 21
emr uuuuu | 2 18 -161 -173 -8 | 50 52
esa uuuuu | -5 21 261 -157 -3 | -16 24
gfz uuuuu | 4 21 -4 -60 -12 | 1 16
grg --xxx | -- -- 49 72 35 | 10 22
igr xxxxx | -16 22 20 -20 -1 | -6 16
irf xxxxx | -18 2 -19 47 8 | -5 18
jpl uuuuu | 8 -6 -22 55 -10 | 14 20
mit uuuuu | -39 14 -187 280 13 | -2 20
ngs uuuuu | 24 -93 21 -33 5 | -6 14
sio uuuuu | 3 110 -40 163 15 | 18 26
Table 7.1561.5 GPS week: 1561 Day: 5 MJD: 55176.500
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 -28 -24 15 5 | 1 20
emr uuuuu | -18 0 -237 -222 4 | 48 50
esa uuuuu | 27 49 105 -93 14 | -16 25
gfz uuuuu | 25 12 85 40 -19 | -3 18
grg --xxx | -- -- 160 71 10 | 13 23
igr xxxxx | 14 -4 127 27 5 | -9 18
irf xxxxx | -17 -19 -12 10 6 | -6 18
jpl uuuuu | 20 -7 -118 -57 -4 | 13 20
mit uuuuu | -35 -27 -177 267 7 | -3 20
ngs uuuuu | -32 -57 75 -107 2 | -6 14
sio uuuuu | 17 65 90 235 9 | 17 25
Table 7.1561.6 GPS week: 1561 Day: 6 MJD: 55177.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 9 -53 -105 73 2 | 0 18
emr uuuuu | 14 27 -153 -158 -3 | 47 50
esa uuuuu | -28 51 69 -86 26 | -17 25
gfz uuuuu | -3 34 64 -83 -11 | -8 21
grg --xxx | -- -- 335 77 -43 | 13 23
igr xxxxx | 30 43 24 -60 7 | -9 18
irf xxxxx | -16 -5 -72 22 6 | -8 18
jpl uuuuu | 8 15 62 -10 3 | 12 20
mit uuuuu | -25 0 -302 253 5 | -4 20
ngs uuuuu | 20 -116 119 -32 -11 | -7 15
sio uuuuu | 36 88 -13 266 8 | 15 24
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