[IGSREPORT-18093] Wk 1560 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 17 14:34:11 PST 2009
******************************************************************************
IGS Electronic Report 17 Dec 14:34:35 PST 2009 Message Number 18093
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1560 (Nov 29, 2009 - Dec 05, 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:
igs1560[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1560[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1560[0-6].cls IGS GPS clock combination summary report.
igs15607.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15607.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 | 24 24
0 | ESA | 21 UNSA
0 | GFZ | 4 5 14 22 ALIC CEDU CHAT CONZ DARW GODE GUAT HARB
0 | GFZ | ISPA KIRU LPGS MAS1 MCM4 ONSA STJO SUTM SYOG THTI
0 | GFZ | WTZR YAKT
0 | GRG | SPT0
0 | JPL | 32 DGAR KERG
0 | MIT | HARB
1 | ALL | 1 1
1 | ESA | 32 CEDU NYAL
1 | GFZ | 10 28 32 BAKO BRUS DARW GRAZ HARB KARR NRC1 ONSA
1 | GFZ | PDEL PERT PRDS QAQ1 REUN SCH2 STJO TOW2 UNSA WSRT
1 | GFZ | YKRO
1 | GRG | ONSA
1 | JPL | 10
2 | ALL | 1 24 1
2 | EMR | WTZR
2 | ESA | 32 CRO1
2 | GFZ | 14 21 26 28 BRUS CHPI CONZ CRO1 DAEJ DARW GRAZ GUAT
2 | GFZ | HOLM HYDE IRKT KARR KERG KIRU LPGS MCM4 PERT PIE1
2 | GFZ | PIMO RIOP SEY1 SFER SUTH SUWN TSKB TWTF UNSA VILL
2 | GFZ | WSRT
2 | GRG | NRC1
2 | JPL | 32
2 | MIT | BRAZ
3 | EMR | HARB
3 | ESA | 32 UNSA
3 | GFZ | 32 ALGO AREQ CEDU CHPI GUAT HOFN KERG KIRU MCM4 METS
3 | GFZ | RIOP SFER STJO SUTH SYOG THTI
3 | JPL | 32 DGAR
3 | MIT | KOUR
3 | NGS | 1
4 | ESA | 32
4 | GFZ | 4 7 ALGO DAEJ DARW GUAM GUAT LPGS NRC1 ONSA PIMO
4 | GFZ | SFER STJO THU3 VILL WSRT YELL
4 | GRG | WTZR
4 | JPL | 32 DGAR
4 | NGS | 1
5 | EMR | HARB
5 | ESA | 21 32
5 | GFZ | AMC2 BAKO DARW DUBO GODE GUAT KIRU MAS1 MDO1 MIZU
5 | GFZ | NTUS NYAL ONSA REUN SFER SHAO STJO SUWN TEHN THU3
5 | GFZ | TSKB WTZR
5 | GRG | AMC2
5 | JPL | 32 DGAR UNSA
5 | NGS | 1
6 | EMR | WTZR
6 | ESA | 32 KOKB
6 | GFZ | 14 ABPO ALGO ARTU BAKO BRUS CONZ DAEJ DAV1 FLIN GODE
6 | GFZ | GUAT IISC MAS1 NRC1 NTUS NYAL ONSA QAQ1 STJO SYOG
6 | GFZ | TSKB UNSA VESL VILL YELL ZECK
6 | GRG | ONSA
6 | JPL | 32 DGAR
5. 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.
6. 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]
-------+---------------------------------------------------
EMR | 3.9 .0 3.3 39 7 33 .25
ESA | 3.5 -1.5 -5.5 38 -36 113 -.04
GFZ | .9 1.2 1.4 7 -25 -1 -.20
GRG | 2.1 5.3 -1.3 3 22 -91 .55
JPL | -.2 3.4 13.1 -3 -37 -41 .18
MIT | -.3 -4.4 -7.5 2 11 -35 -.15
NGS | 2.8 -6.4 -7.2 -92 -66 25 .03
SIO | 1.0 -.4 -1.6 -21 -7 42 .14
7. 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.
8. 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.
9. 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 1.1560.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1560.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 2.1560.[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 3.1560.[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 5.1560.0-6).
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 1560 summary. (Nov 29, 2009 - Dec 05, 2009)
Table 1.1560.a GPS week: 1560 MJD: 55164.000-55170.000
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]
--------+----------------------------------------------------+------------------------------
emr 89| 1 2 5 -92 -75 -19 .42 18 18 | 817 -222 21 124
| 2 2 2 23 17 28 .03 | 1138 825
esa 129| 1 0 -1 -81 -4 31 .21 11 10 | -1382 1106 24 124
| 2 1 1 15 18 15 .03 | 1027 1626
gfz 195| 0 0 -3 -42 30 -21 -.14 10 10 | 358 -691 40 144
| 1 1 1 44 56 13 .04 | 190 821
grg 110| 0 0 2 -49 -61 -14 1.00 23 22 | 1516232 -165581 64 217
| 1 1 5 30 55 25 .03 | 3744643 372683
igr n/a| 0 0 0 13 -58 -81 -.03 7 6 | 2393 -374 26 91
| 0 0 1 27 31 19 .04 | 1610 937
jpl 137| 0 2 4 -16 60 0 .45 17 16 | 2165 -370 22 100
| 1 1 1 28 24 38 .03 | 1401 852
mit 260| -1 -1 -3 -32 -96 14 -.36 13 12 | -15628 -103 24 142
| 0 0 1 22 27 11 .02 | 532 1262
ngs 220| 0 -1 0 186 71 -35 -.21 12 9 | -208948 421960 2164 3708
| 0 1 0 42 52 11 .03 | 328557 753107
sio 262| -1 3 6 43 -30 54 .03 20 20 | --- --- --- ---
| 1 1 1 18 18 7 .02 | --- ---
Table 1.1560.b GPS week : 1560 MJD: 55164.000-55170.000
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 | 24 17 15 18 15 17 22 |
2 | 6 6 6 7 7 7 6 |
3 | 5 5 5 5 5 5 5 |
4 | 5 5 5 4 4 4 4 |
5 | 5 6 6 6 7 8 6 |
6 | 5 5 5 5 5 5 5 |
7 | 6 6 5 5 5 6 5 |
8 | 9 8 7 6 6 7 5 |
9 | 6 6 5 6 5 6 6 |
10 | 7 8 8 7 7 7 8 |
11 | 5 5 4 5 4 5 4 |
12 | 6 6 6 6 6 6 6 |
13 | 6 7 6 6 5 6 5 |
14 | 6 5 6 6 6 6 6 |
15 | 6 6 6 6 6 6 6 |
16 | 7 7 7 7 6 7 6 |
17 | 7 7 8 8 8 7 6 |
18 | 6 6 6 6 7 7 6 |
19 | 5 6 6 6 5 5 4 |
20 | 5 5 5 6 5 6 6 |
21 | 5 5 5 5 5 6 5 |
22 | 5 5 5 6 5 5 5 |
23 | 6 6 6 6 6 6 6 |
24 | 11 16 14 19 --- --- --- |
25 | 7 6 6 6 5 5 5 |
26 | 5 5 5 5 5 5 4 |
27 | 6 6 5 6 5 6 5 |
28 | 5 6 5 5 5 5 5 |
29 | 5 5 5 4 5 5 4 |
30 | 4 4 5 5 5 5 4 |
31 | 6 6 6 6 6 6 6 |
32 | 7 7 7 7 7 6 6 |
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 2.1560.0 GPS week: 1560 Day: 0 MJD: 55164.000
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]
--------+----------------------------------------------------+------------------------------
emr 89| 4 -1 3 -133 -70 -36 .46 19 19 | 2849 -978 21 114
| 22 -24 |
esa 129| 0 0 -1 -84 -18 22 .24 9 9 | -13 1100 24 118
| 8 26 |
gfz 195| -2 0 -4 4 -16 -33 -.11 10 10 | 507 -172 39 124
| -41 -75 |
grg 110| 0 1 3 -62 -8 -36 .95 24 23 | -241 1200 64 229
| 65 -110 |
igr n/a| 0 0 0 -41 -32 -61 .02 6 6 | 5635 -1335 24 85
| -39 -72 |
jpl 137| 2 0 4 -12 83 -5 .46 18 17 | 4857 -1066 22 93
| -16 -45 |
mit 260| 0 0 -1 2 -111 3 -.39 13 12 | -15961 923 23 138
| -9 74 |
ngs 220| 0 0 0 136 121 -16 -.24 11 9 | -781497 737735 2213 3566
| 97 -86 |
sio 262| 0 1 9 58 -4 58 .03 21 19 | --- --- --- ---
| -101 7 |
Table 2.1560.1 GPS week: 1560 Day: 1 MJD: 55165.000
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]
--------+----------------------------------------------------+------------------------------
emr 89| 4 1 2 -81 -46 -12 .41 20 20 | 605 -281 24 191
| -8 -7 |
esa 129| 0 0 0 -76 4 43 .24 10 10 | -1464 2601 33 139
| 31 24 |
gfz 195| 0 -2 -1 -75 -65 -35 -.07 10 10 | 711 -2027 50 158
| -74 -71 |
grg 110| -3 2 11 -17 16 -13 .97 24 24 | 9999999 465 64 241
| 8 -130 |
igr n/a| 0 0 2 24 -11 -114 -.02 6 6 | 3203 -1204 33 112
| -58 -68 |
jpl 137| 0 2 2 7 102 -14 .40 18 16 | 2791 -811 30 121
| -39 -49 |
mit 260| -3 -2 -3 -24 -123 0 -.38 13 12 | -16305 1550 27 205
| -2 70 |
ngs 220| 1 0 -1 197 149 -36 -.23 12 9 | 16688 -736 2293 4430
| 25 -118 |
sio 262| -2 1 8 32 -50 70 .03 21 19 | --- --- --- ---
| -87 38 |
Table 2.1560.2 GPS week: 1560 Day: 2 MJD: 55166.000
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]
--------+----------------------------------------------------+------------------------------
emr 89| 0 6 3 -71 -62 -58 .43 18 18 | -527 766 18 98
| -10 -31 |
esa 129| 0 0 -2 -79 26 27 .19 11 10 | -1281 2724 24 132
| -13 8 |
gfz 195| 0 -1 -2 -91 31 -23 -.18 10 10 | 165 -2 35 126
| -45 -53 |
grg 110| 0 1 3 -55 -39 -39 1.03 23 21 | 446328 -999999 76 201
| 55 -37 |
igr n/a| 0 0 -1 44 -49 -87 -.01 6 6 | 1196 302 27 92
| -52 -36 |
jpl 137| 1 1 2 26 63 44 .48 18 16 | 1106 612 23 103
| -28 -91 |
mit 260| 0 -1 -2 -41 -127 10 -.35 12 11 | -15885 251 19 109
| 13 56 |
ngs 220| 0 -1 0 242 90 -29 -.23 13 8 | -558162 2016005 2134 3708
| -7 -34 |
sio 262| 0 3 8 34 -39 52 .06 19 18 | --- --- --- ---
| -74 11 |
Table 2.1560.3 GPS week: 1560 Day: 3 MJD: 55167.000
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]
--------+----------------------------------------------------+------------------------------
emr 89| 2 3 6 -68 -86 -39 .42 18 18 | 653 104 24 121
| -16 -14 |
esa 129| 0 -1 -1 -93 8 23 .21 11 10 | -1570 -184 22 128
| 6 -35 |
gfz 195| 1 -1 -5 -75 84 -32 -.17 12 12 | 281 357 39 142
| -52 -20 |
grg 110| 0 0 0 -15 -110 -42 1.01 23 19 | 296 -145 60 217
| 21 18 |
igr n/a| 0 0 -2 11 -81 -84 -.09 6 6 | 1549 -304 24 94
| -23 4 |
jpl 137| 0 2 5 -19 42 62 .44 17 15 | 1749 -251 21 108
| 7 -37 |
mit 260| -1 -1 -4 -64 -108 13 -.37 13 12 | -15416 240 26 140
| 10 43 |
ngs 220| 0 -1 1 227 44 -45 -.24 11 8 | 16713 67 2507 3722
| -37 0 |
sio 262| -2 2 5 31 -38 47 .03 19 19 | --- --- --- ---
| -92 7 |
Table 2.1560.4 GPS week: 1560 Day: 4 MJD: 55168.000
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]
--------+----------------------------------------------------+------------------------------
emr 89| 3 3 7 -104 -102 -8 .43 18 18 | 1747 -1623 20 116
| 8 10 |
esa 129| 0 -1 0 -106 -18 38 .15 11 11 | -478 -1654 22 121
| -27 -51 |
gfz 195| 0 0 -1 -59 89 -16 -.19 10 10 | 250 -1227 35 133
| 5 14 |
grg 110| -1 -1 0 -91 -102 1 1.03 23 22 | 784 -1251 67 219
| 113 2 |
igr n/a| 0 0 0 7 -98 -68 -.01 6 7 | 2466 -1400 22 84
| -40 -3 |
jpl 137| 0 1 3 -19 35 -19 .45 17 15 | 2580 -1690 20 90
| 2 -55 |
mit 260| -1 -1 -4 -14 -80 25 -.36 13 12 | -14625 -2304 24 144
| 5 38 |
ngs 220| 0 -1 0 194 16 -43 -.19 11 9 | 17404 -1575 2145 3711
| 71 38 |
sio 262| -1 2 5 78 -35 56 .03 20 21 | --- --- --- ---
| -109 6 |
Table 2.1560.5 GPS week: 1560 Day: 5 MJD: 55169.000
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]
--------+----------------------------------------------------+------------------------------
emr 89| 0 3 8 -81 -83 -5 .38 18 18 | 461 408 25 128
| -9 -20 |
esa 129| 6 1 -3 -58 -7 56 .22 13 12 | -1606 776 21 116
| -44 -6 |
gfz 195| 0 -1 -2 -22 63 2 -.12 10 10 | 358 -1064 43 160
| -17 1 |
grg 110| 2 3 0 -24 -134 19 1.03 22 22 | 166380 -158985 59 211
| 61 25 |
igr n/a| 0 0 0 35 -84 -93 -.02 7 7 | 1563 660 23 87
| -37 -31 |
jpl 137| -2 4 5 -38 47 -40 .41 17 16 | 1306 445 23 86
| 14 -78 |
mit 260| -1 -2 -3 -48 -56 16 -.36 12 11 | -15516 -652 26 142
| 10 19 |
ngs 220| -1 -3 0 172 9 -49 -.18 13 11 | -173703 202111 1801 3501
| 66 38 |
sio 262| -2 3 6 30 -41 48 .00 22 21 | --- --- --- ---
| -98 14 |
Table 2.1560.6 GPS week: 1560 Day: 6 MJD: 55170.000
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]
--------+----------------------------------------------------+------------------------------
emr 89| 0 0 8 -109 -73 26 .43 18 18 | -67 47 20 104
| 0 -16 |
esa 129| 1 0 0 -71 -26 10 .21 10 10 | -3264 2381 24 116
| -61 69 |
gfz 195| 0 0 -4 23 24 -14 -.18 8 8 | 234 -708 40 171
| -33 -39 |
grg 110| 0 0 -5 -78 -52 7 1.01 22 20 | 84 -355 58 203
| 90 -78 |
igr n/a| 0 1 0 10 -53 -61 -.07 8 7 | 1145 662 31 88
| -69 -47 |
jpl 137| -1 4 4 -61 48 -23 .47 17 15 | 771 171 21 99
| 0 -60 |
mit 260| 0 -1 -3 -38 -68 30 -.34 12 11 | -15692 -731 24 122
| 27 19 |
ngs 220| 0 -2 0 132 65 -30 -.16 11 8 | -85 118 2060 3324
| 29 -38 |
sio 262| -1 5 5 39 -3 50 .05 21 22 | --- --- --- ---
| -91 9 |
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 3.1560.0 GPS week: 1560 Day: 0 MJD: 55164.000
Weighted Average Orbit Dynamics (7 days)
PRN | emr esa gfz grg igr jpl mit ngs sio IGS | emr esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
X1 | --- --- --- --- 27 --- 25 22 --- 23 | --- --- --- --- 30 --- 27 30 --- 25
2 | 18 10 9 22 7 22 11 10 30 6 | 38 32 26 46 29 39 21 22 20 25
3 | 12 6 10 16 6 12 14 11 22 5 | 29 28 25 28 23 28 26 24 24 23
4 | 14 6 6 33 7 13 13 9 24 4 | 27 26 25 38 26 26 23 25 23 23
5E | 21 9 14 17 6 19 9 8 11 5 | 52 47 48 49 50 49 46 45 48 46
6 | 11 5 8 15 5 11 15 12 21 4 | 32 29 28 28 26 31 33 25 28 27
7E | 20 9 8 16 8 13 19 12 15 5 | 40 36 34 44 35 34 33 37 33 33
8E | 24 18 13 22 8 21 28 20 24 8 | 126 126 124 138 123 128 118 130 129 124
9 | 22 11 12 23 8 17 11 9 23 5 | 38 22 29 38 24 34 23 27 28 24
10E | 20 12 10 18 7 19 10 23 16 6 | 28 28 24 30 20 25 23 38 29 24
11 | 12 7 12 28 5 15 9 10 17 4 | 38 28 29 45 27 34 30 25 30 27
12 | 18 10 9 29 5 25 13 9 20 5 | 31 23 21 42 20 33 20 17 24 21
13 | 18 12 9 26 7 17 17 11 23 6 | 32 25 17 42 22 26 20 23 23 19
14 | 18 8 12 27 4 22 11 9 18 5 | 26 23 21 33 19 26 23 19 19 20
15 | 24 8 11 24 7 25 12 9 20 6 | 28 21 19 37 17 26 18 20 18 16
16 | 23 9 9 27 8 25 18 9 28 6 | 41 33 26 48 30 41 24 35 27 29
17 | 15 7 9 22 6 18 11 11 42 6 | 40 38 43 39 39 39 41 39 48 39
18E | 26 10 13 18 5 23 10 6 13 5 | 65 56 57 57 56 65 57 68 58 59
19 | 12 5 8 17 6 13 17 10 16 4 | 44 44 40 42 38 39 37 36 37 38
20E | 14 9 10 13 6 20 12 8 13 5 | 26 21 16 26 18 22 18 18 22 16
21 | 18 8 10 41 6 20 8 7 17 4 | 27 18 10 42 15 27 13 14 13 14
22E | 20 9 11 29 8 19 11 9 12 5 | 32 26 21 30 24 27 22 21 23 21
23 | 21 10 10 21 7 19 12 9 21 5 | 35 28 25 37 23 32 25 25 29 25
X24 | 19 --- --- --- 20 --- 11 15 --- 10 | 16 --- --- --- 35 --- 16 20 --- 15
X25 | 16 8 11 --- 5 16 23 12 --- 6 | 23 13 14 --- 16 24 29 16 --- 14
26 | 12 6 8 22 5 16 11 8 24 4 | 24 20 20 20 18 24 22 18 33 20
27 | 22 9 11 23 7 16 12 8 20 5 | 28 12 19 25 14 21 18 12 19 13
28 | 16 10 9 25 6 19 12 12 17 5 | 32 30 31 42 28 34 31 33 29 29
29 | 12 9 9 19 7 13 18 8 20 5 | 34 36 36 32 33 32 41 35 35 35
30 | 11 9 10 15 5 11 9 9 15 4 | 24 20 22 25 20 22 21 17 21 18
31E | 19 9 10 29 6 18 9 11 24 5 | 44 40 44 46 40 41 40 43 39 40
32E | 26 10 11 29 6 18 13 22 20 7 | 34 30 28 51 27 38 32 38 40 30
------+---------------------------------------------------+----------------------------------------------------
RMS | 19 9 10 24 6 18 13 11 21 |T 36 31 30 41 30 35 30 31 32 29
WRMS | 19 9 10 23 6 17 12 9 19 |NE 31 26 25 36 24 30 25 24 26 23
MEDI | 18 9 10 22 6 18 12 9 20 |MD 32 28 25 39 26 32 24 25 28 24
Table 3.1560.1 GPS week: 1560 Day: 1 MJD: 55165.000
Weighted Average Orbit Dynamics (7 days)
PRN | emr esa gfz grg igr jpl mit ngs sio IGS | emr esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
X1 | 34 --- --- --- 23 --- 20 21 --- 17 | 39 --- --- --- 25 --- 28 28 --- 22
2 | 22 10 10 25 7 22 10 9 29 6 | 37 33 32 48 24 34 21 25 23 25
3 | 12 6 8 18 7 12 14 13 22 5 | 19 22 18 24 15 21 23 20 22 18
4 | 15 9 4 31 8 10 9 8 22 4 | 22 22 24 27 18 21 22 23 25 21
5E | 22 10 14 17 4 19 11 10 12 5 | 52 48 50 59 46 47 47 48 50 47
6 | 10 7 6 15 7 10 12 10 21 4 | 21 21 17 24 18 23 24 21 24 19
7E | 16 11 11 20 6 17 18 9 13 5 | 32 29 27 35 27 29 32 29 31 28
8E | 25 18 14 22 7 18 27 14 22 8 | 120 116 110 128 113 118 113 116 120 114
9 | 24 11 10 29 7 18 11 10 19 5 | 29 17 22 30 12 25 20 17 21 15
10E | 24 16 10 25 4 20 11 26 18 7 | 35 26 24 39 22 29 23 36 26 23
11 | 14 12 6 28 6 16 9 13 17 5 | 30 23 22 43 18 30 22 20 25 19
12 | 21 8 10 32 3 24 11 10 18 5 | 32 26 25 43 21 33 22 24 25 24
13 | 20 14 12 28 6 18 17 11 22 6 | 32 21 23 46 16 27 16 19 18 17
14 | 19 9 8 30 5 21 10 8 19 5 | 27 19 19 34 16 26 19 19 18 17
15 | 22 8 11 24 4 21 11 8 20 5 | 28 17 18 38 13 25 17 15 16 14
16 | 26 11 7 29 6 24 16 8 26 6 | 40 31 28 46 27 38 30 32 33 29
17 | 17 9 13 23 6 18 11 14 41 7 | 30 26 35 24 23 24 26 22 39 24
18E | 26 11 12 16 5 24 12 11 15 6 | 61 56 61 62 56 58 56 50 55 55
19 | 10 8 12 19 5 13 20 13 17 5 | 33 39 35 37 30 32 31 26 31 31
20E | 19 11 8 16 5 19 7 10 15 5 | 24 19 17 26 14 23 14 19 16 15
21 | 22 9 10 26 2 20 8 8 16 5 | 34 18 18 37 15 29 15 21 14 18
22E | 19 9 11 25 6 18 11 8 11 5 | 25 18 16 21 13 25 17 19 18 17
23 | 27 12 11 25 8 20 12 10 18 6 | 40 28 32 45 27 33 22 26 23 25
X24 | 27 --- --- --- 30 --- 22 20 --- 16 | 22 --- --- --- 28 --- 16 28 --- 18
X25 | 18 10 9 --- 4 15 21 11 --- 6 | 23 13 13 --- 12 22 22 18 --- 12
26 | 14 10 9 20 4 13 13 9 23 5 | 21 20 16 20 13 22 19 19 31 17
27 | 24 12 9 28 5 16 11 9 19 5 | 28 14 17 27 10 21 18 16 16 13
28 | 18 10 13 29 4 22 15 7 21 6 | 49 43 50 38 45 46 47 45 49 44
29 | 13 9 9 19 6 13 15 13 18 5 | 23 19 22 21 18 20 22 21 21 20
30 | 13 7 8 20 3 11 8 11 13 4 | 21 16 16 28 12 21 17 17 16 15
31E | 18 7 10 24 7 20 14 10 23 5 | 50 39 43 45 38 41 43 33 30 37
32E | 24 8 10 24 6 19 14 22 19 6 | 35 34 31 51 30 38 30 42 40 32
------+---------------------------------------------------+----------------------------------------------------
RMS | 20 10 10 24 6 18 13 12 21 |T 34 29 29 39 25 32 27 28 30 26
WRMS | 20 10 10 24 6 16 12 9 19 |NE 29 23 23 34 19 27 22 22 24 20
MEDI | 19 10 10 24 6 18 12 10 19 |MD 30 22 23 37 18 27 22 22 25 20
Table 3.1560.2 GPS week: 1560 Day: 2 MJD: 55166.000
Weighted Average Orbit Dynamics (7 days)
PRN | emr esa gfz grg igr jpl mit ngs sio IGS | emr esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
X1 | 27 --- --- --- 17 --- 14 21 --- 14 | 41 --- --- --- 24 --- 24 26 --- 25
2 | 19 11 11 21 6 20 12 11 29 6 | 34 22 26 39 22 31 22 25 22 21
3 | 10 7 7 15 6 11 12 12 21 4 | 22 21 21 22 18 21 22 17 20 18
4 | 15 7 8 34 6 9 10 15 19 4 | 25 21 24 30 23 23 25 25 22 21
5E | 19 12 11 20 7 20 12 13 13 5 | 55 53 56 58 53 53 52 57 56 53
6 | 8 9 9 14 5 12 12 11 20 4 | 26 20 26 26 22 26 27 19 22 21
7 | 16 12 9 17 6 14 13 12 16 5 | 51 57 51 58 53 52 46 64 45 52
8E | 22 14 12 23 9 18 20 13 21 7 | 91 82 88 89 83 90 89 82 89 85
9 | 21 9 8 20 7 15 13 8 18 5 | 29 16 20 30 14 25 20 18 20 16
10E | 20 19 13 25 8 19 13 30 15 7 | 25 22 20 36 17 22 17 36 13 15
11 | 14 7 6 26 4 15 9 8 14 4 | 33 25 23 41 24 30 25 23 26 23
12 | 19 12 9 26 6 20 11 8 17 5 | 31 26 30 38 23 30 24 21 23 23
13 | 18 15 8 24 6 17 13 12 20 6 | 30 25 20 43 19 28 13 23 14 17
14 | 20 10 8 37 6 23 10 9 19 5 | 34 25 25 48 21 28 25 26 23 23
15 | 22 9 7 26 4 21 10 10 20 5 | 32 23 23 40 19 28 19 24 18 18
16 | 25 11 11 28 7 25 12 12 22 6 | 37 22 32 43 21 32 25 27 31 24
17 | 16 11 12 22 7 20 11 18 41 7 | 34 34 36 33 33 29 36 35 43 31
18E | 18 10 13 18 4 23 11 8 12 5 | 41 37 34 41 35 44 36 46 32 37
19 | 12 7 7 19 8 12 21 11 17 5 | 30 27 29 30 28 28 37 25 33 27
20E | 18 11 9 13 6 21 9 8 16 5 | 23 19 19 27 19 23 24 19 28 17
21 | 22 11 8 24 4 19 7 9 14 5 | 30 17 20 33 18 29 20 28 15 19
22E | 17 8 12 23 6 19 12 10 11 5 | 25 16 16 21 15 22 16 23 16 16
23 | 22 13 11 20 6 21 9 13 18 6 | 38 34 30 46 31 37 25 31 27 28
X24 | 27 --- --- --- 23 --- 14 18 --- 13 | 20 --- --- --- 34 --- 14 15 --- 10
X25 | 18 10 8 --- 4 13 16 11 --- 5 | 24 14 12 --- 15 23 20 23 --- 13
26 | 13 8 4 18 4 13 12 8 22 4 | 27 20 19 22 16 22 22 21 31 18
27 | 22 9 8 20 6 15 12 9 16 5 | 31 14 21 29 14 23 21 21 18 16
28 | 12 11 8 24 3 19 10 8 17 5 | 24 21 22 32 21 22 24 27 22 20
29 | 12 10 8 17 7 10 11 14 18 4 | 35 34 36 35 35 33 35 38 31 33
30 | 20 8 9 13 5 9 9 8 14 4 | 28 19 18 25 14 20 15 18 16 15
31 | 20 15 14 30 6 23 10 12 16 6 | 49 48 56 51 46 46 48 48 49 48
32E | 22 10 8 17 5 20 14 23 17 6 | 35 35 31 44 33 40 33 45 40 33
------+---------------------------------------------------+----------------------------------------------------
RMS | 18 11 10 23 6 18 12 13 19 |T 34 28 29 38 26 32 28 30 29 26
WRMS | 18 10 10 21 6 16 11 8 18 |NE 30 22 24 34 22 27 23 24 23 20
MEDI | 19 10 8 21 6 19 12 11 17 |MD 31 22 24 36 22 28 24 25 23 21
Table 3.1560.3 GPS week: 1560 Day: 3 MJD: 55167.000
Weighted Average Orbit Dynamics (7 days)
PRN | emr esa gfz grg igr jpl mit ngs sio IGS | emr esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
X1 | 29 --- --- --- 24 --- 23 22 --- 17 | 31 --- --- --- 27 --- 29 29 --- 24
2 | 21 12 14 21 6 19 11 10 31 6 | 37 34 31 45 26 38 27 28 26 28
3 | 13 11 7 15 5 10 12 9 23 5 | 26 23 20 26 21 20 24 20 21 20
4 | 12 11 8 34 5 7 11 6 14 4 | 20 22 23 33 22 20 22 19 18 18
5E | 22 11 13 14 10 19 16 8 15 6 | 41 38 37 47 37 36 39 35 39 34
6 | 11 10 7 13 5 10 12 7 21 4 | 29 24 24 29 25 25 30 23 25 24
7 | 17 10 10 28 9 14 13 11 14 5 | 40 41 38 51 38 37 31 43 34 36
8E | 23 10 11 20 8 14 16 13 23 6 | 138 133 132 138 132 137 130 134 136 133
9 | 20 10 13 19 5 15 14 9 18 5 | 29 18 21 29 14 25 16 15 21 14
10E | 20 14 12 25 8 20 11 26 17 7 | 33 28 24 43 26 30 26 40 31 25
11 | 14 10 10 21 5 16 12 9 17 5 | 35 27 26 44 26 32 28 23 31 25
12 | 20 12 12 28 6 20 10 13 16 6 | 39 32 27 50 27 38 25 29 29 28
13 | 17 13 9 26 9 17 11 12 14 5 | 32 28 19 44 23 28 17 28 16 21
14 | 17 10 11 27 5 22 11 9 19 5 | 25 18 21 34 17 27 18 24 18 17
15 | 19 10 8 22 6 17 13 8 19 5 | 29 20 14 37 17 26 21 15 22 16
16 | 28 12 11 26 6 26 12 11 22 7 | 47 34 30 43 34 43 29 37 31 33
17 | 17 13 27 24 6 18 13 10 38 8 | 33 38 45 35 33 30 36 32 43 33
18E | 18 12 10 13 5 21 16 9 15 6 | 49 45 46 55 45 49 45 43 48 43
19 | 14 8 7 18 5 13 22 10 18 5 | 44 44 43 43 39 38 43 36 41 40
20E | 18 12 8 17 6 21 15 10 19 6 | 32 32 26 40 26 29 28 26 38 25
21 | 17 8 12 24 6 19 9 7 15 5 | 30 23 23 37 18 29 21 21 22 21
22E | 17 11 12 25 5 20 14 9 8 5 | 27 22 24 32 19 27 19 22 22 20
23 | 23 10 10 19 9 19 11 11 18 5 | 37 29 27 39 28 33 26 29 24 26
X24 | --- --- --- --- 24 --- 17 19 --- 18 | --- --- --- --- 71 --- 12 20 --- 15
X25 | 18 10 8 --- 5 14 15 9 --- 5 | 27 18 15 --- 17 26 22 22 --- 16
26 | 10 9 10 17 5 11 13 7 22 4 | 22 16 20 22 18 23 21 23 29 18
27 | 20 11 9 16 5 15 14 10 15 5 | 28 16 19 28 15 23 17 14 18 13
28 | 16 12 13 23 7 17 10 8 15 5 | 34 26 34 35 29 33 33 34 33 30
29 | 10 7 10 18 7 13 10 9 17 4 | 29 34 32 32 28 30 35 32 30 32
30 | 15 7 12 12 6 11 8 11 13 4 | 27 18 22 24 15 22 18 16 19 16
31 | 18 11 14 34 4 18 16 12 14 6 | 42 37 39 44 37 38 37 42 34 36
32E | 25 15 12 30 5 13 14 19 15 6 | 37 35 28 58 32 39 33 40 36 31
------+---------------------------------------------------+----------------------------------------------------
RMS | 18 11 12 23 6 17 13 11 19 |T 36 31 31 41 30 34 29 31 32 28
WRMS | 18 10 12 19 6 15 12 8 19 |NE 31 25 25 35 25 29 24 24 25 22
MEDI | 18 11 10 21 6 17 13 10 17 |MD 32 28 26 39 26 30 26 28 29 25
Table 3.1560.4 GPS week: 1560 Day: 4 MJD: 55168.000
Weighted Average Orbit Dynamics (7 days)
PRN | emr esa gfz grg igr jpl mit ngs sio IGS | emr esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
X1 | 24 --- --- --- 23 --- 22 19 --- 15 | 32 --- --- --- 26 --- 25 23 --- 21
2 | 21 12 10 20 8 19 11 10 31 6 | 35 25 19 37 20 34 19 17 23 19
3 | 12 9 7 14 5 13 11 12 23 5 | 22 21 17 22 16 23 18 24 18 18
4 | 11 9 5 28 7 7 13 8 15 4 | 20 19 16 30 19 20 20 23 16 16
5E | 18 12 10 20 6 19 19 7 30 6 | 33 30 27 35 29 30 33 27 47 27
6 | 9 11 7 14 6 12 12 9 22 4 | 25 29 23 26 22 30 25 27 21 24
7 | 18 9 9 28 9 11 13 9 14 4 | 30 23 25 40 22 25 15 25 21 20
8E | 24 9 10 17 9 15 14 12 25 6 | 91 88 83 97 86 93 85 92 95 87
9 | 22 8 8 18 6 16 15 9 15 5 | 31 20 16 31 19 29 19 19 21 16
10E | 18 13 11 21 7 19 13 25 14 6 | 28 21 21 31 23 25 20 39 23 20
11 | 16 7 7 22 5 13 12 8 13 4 | 34 29 21 41 26 33 27 25 26 24
12 | 21 12 11 25 6 21 12 15 16 6 | 35 26 26 39 23 32 23 27 21 23
13 | 19 12 8 26 7 16 11 11 16 5 | 31 24 19 42 22 27 15 25 14 18
14 | 19 13 7 30 5 19 13 8 18 5 | 28 20 18 36 18 28 20 21 18 17
15 | 22 11 5 25 7 20 13 11 19 5 | 32 24 18 39 20 27 20 17 20 17
16 | 21 13 9 23 7 21 12 9 23 6 | 34 21 19 37 20 30 16 22 19 18
17 | 18 11 26 25 8 18 15 12 38 8 | 27 26 36 26 23 26 28 25 36 24
18E | 21 14 12 16 7 21 15 14 27 7 | 43 35 40 38 32 44 35 40 29 36
19 | 13 9 8 19 6 10 19 12 19 5 | 30 33 28 31 26 31 29 27 28 27
20E | 13 10 6 26 4 19 12 7 17 4 | 25 24 15 23 21 27 21 24 28 19
21 | 16 9 8 27 6 17 9 9 17 4 | 26 20 14 34 15 26 14 15 13 14
22E | 17 12 10 28 5 18 14 9 9 5 | 24 15 15 39 13 23 14 15 15 12
23 | 23 11 8 22 6 18 11 9 20 5 | 34 25 19 38 20 27 17 20 15 17
X25 | 15 8 7 --- 7 13 15 10 --- 5 | 24 17 15 --- 15 22 17 20 --- 12
26 | 11 10 7 20 6 8 13 7 22 4 | 18 18 17 21 16 18 18 18 29 15
27 | 21 7 8 19 6 14 14 12 15 5 | 28 17 14 30 15 23 16 16 17 12
28 | 17 8 11 32 5 19 10 7 15 5 | 33 28 28 32 28 27 30 26 31 25
29 | 12 11 9 19 8 14 10 11 18 5 | 31 29 28 30 29 26 28 30 26 27
30 | 14 8 13 14 6 12 8 11 12 4 | 21 24 19 28 17 22 20 18 19 16
31 | 16 16 7 32 8 20 13 9 17 5 | 29 25 16 37 19 26 20 23 17 18
32E | 19 14 10 18 5 16 14 20 15 6 | 31 33 26 45 29 38 28 37 33 28
------+---------------------------------------------------+----------------------------------------------------
RMS | 18 11 10 23 6 17 13 11 20 |T 31 26 23 35 32 29 23 26 25 22
WRMS | 18 11 10 22 7 15 12 9 21 |NE 28 23 20 32 33 26 21 22 21 19
MEDI | 18 11 8 22 6 16 13 10 17 |MD 30 24 19 35 21 27 20 24 21 19
Table 3.1560.5 GPS week: 1560 Day: 5 MJD: 55169.000
Weighted Average Orbit Dynamics (7 days)
PRN | emr esa gfz grg igr jpl mit ngs sio IGS | emr esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
X1 | 26 --- --- --- 30 --- 20 24 --- 16 | 32 --- --- --- 43 --- 21 36 --- 25
2 | 21 13 12 21 5 23 11 9 30 6 | 29 21 20 37 19 31 18 18 22 16
3 | 13 10 9 17 5 10 12 12 24 5 | 21 24 20 24 18 20 17 22 11 18
4 | 10 9 5 28 6 8 7 11 12 3 | 18 21 18 29 17 18 17 17 14 15
5E | 20 19 12 23 13 21 23 10 38 8 | 30 26 27 37 22 27 45 27 58 29
6 | 10 11 8 15 6 10 12 12 23 5 | 23 23 23 26 21 23 22 23 15 21
7 | 16 13 11 24 9 17 14 12 13 5 | 31 28 27 39 28 26 20 31 24 23
8 | 27 14 10 19 9 16 13 11 25 6 | 135 131 131 130 130 133 126 131 133 130
9 | 22 11 9 15 5 18 14 9 18 5 | 30 14 16 28 16 27 15 17 19 14
10E | 18 13 11 27 10 17 12 25 17 6 | 29 27 25 39 28 28 25 43 30 26
11 | 15 9 6 24 5 15 8 12 16 4 | 31 29 21 41 24 32 23 25 27 24
12 | 20 13 8 22 6 20 12 11 15 5 | 31 21 20 38 19 29 17 20 17 18
13 | 18 12 10 29 8 19 9 15 14 5 | 27 17 18 43 21 28 17 29 14 17
14 | 17 13 9 25 7 21 13 14 20 6 | 28 19 18 33 16 27 18 22 17 16
15 | 21 14 9 20 8 22 12 10 19 6 | 30 21 14 40 19 28 19 21 20 17
16 | 22 14 9 27 9 22 14 14 24 6 | 35 25 21 41 22 30 21 29 24 21
17 | 15 13 9 25 8 16 12 16 40 7 | 25 32 24 24 23 23 29 24 34 23
18E | 19 14 14 14 5 21 15 11 35 7 | 51 46 51 52 42 50 46 46 58 46
19 | 13 10 11 22 6 12 11 12 18 5 | 23 32 30 27 24 23 20 24 19 23
20E | 14 13 7 18 6 23 11 12 21 5 | 24 26 21 32 24 29 24 28 30 23
21 | 21 14 11 23 7 19 11 9 16 5 | 26 14 15 33 13 24 14 19 14 12
22E | 18 9 11 20 9 18 10 12 9 5 | 24 19 19 28 16 23 16 23 15 17
23 | 21 13 9 23 8 19 9 11 20 5 | 33 26 23 42 27 32 21 28 21 23
X25 | 18 11 7 --- 7 13 13 11 --- 5 | 24 16 13 --- 17 24 17 24 --- 13
26 | 9 10 9 19 7 11 13 11 24 5 | 21 18 16 20 17 22 21 24 28 16
27 | 24 11 9 14 5 16 14 9 17 5 | 31 13 17 29 18 25 13 19 19 14
28 | 12 12 8 30 7 20 10 9 16 5 | 30 27 25 37 28 30 30 32 32 26
29 | 12 15 8 20 6 12 8 10 17 4 | 20 27 23 24 22 20 22 25 20 20
30 | 19 10 12 12 4 13 6 9 11 4 | 29 17 17 27 16 23 17 16 19 14
31 | 15 14 11 23 10 19 16 14 19 6 | 33 26 26 39 26 33 27 32 26 26
32E | 21 15 9 18 6 14 10 20 15 6 | 29 35 28 50 30 36 27 40 32 30
------+---------------------------------------------------+----------------------------------------------------
RMS | 18 13 10 22 7 17 12 13 22 |T 31 27 25 37 28 30 25 29 28 24
WRMS | 18 12 10 22 7 16 11 11 21 |NE 27 21 19 32 24 25 19 23 20 18
MEDI | 18 13 9 22 7 17 12 11 18 |MD 29 24 21 37 22 27 21 24 21 21
Table 3.1560.6 GPS week: 1560 Day: 6 MJD: 55170.000
Weighted Average Orbit Dynamics (7 days)
PRN | emr esa gfz grg igr jpl mit ngs sio IGS | emr esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
X1 | 27 --- --- --- 71 --- 18 --- --- 22 | 31 --- --- --- 64 --- 27 --- --- 26
2 | 23 11 8 20 6 19 12 8 30 6 | 37 20 22 39 23 33 23 21 29 21
3 | 9 8 8 15 4 10 12 9 27 4 | 28 27 27 31 25 30 27 24 23 25
4 | 11 11 5 31 7 7 8 8 13 3 | 24 24 29 30 28 25 28 30 23 24
5E | 19 13 10 16 8 20 12 8 23 5 | 29 27 21 26 20 27 25 19 36 21
6 | 8 7 9 14 4 9 9 11 28 4 | 34 34 34 37 32 36 36 30 30 32
7 | 22 11 9 21 8 16 11 5 12 5 | 30 25 25 39 24 24 19 24 21 22
8 | 16 10 7 18 7 15 11 10 25 5 | 127 127 128 121 125 128 126 123 129 126
9 | 19 8 8 17 7 17 16 9 21 5 | 28 18 17 27 14 24 17 20 18 15
10E | 20 10 11 16 15 18 17 28 33 8 | 32 32 26 34 31 35 34 41 50 29
11 | 15 9 5 24 4 13 9 10 16 4 | 38 35 32 47 31 37 34 31 32 32
12 | 24 12 8 23 7 22 16 10 15 6 | 38 24 21 41 26 35 22 27 23 23
13 | 21 10 7 25 6 16 9 8 15 4 | 35 29 27 46 26 29 22 25 21 23
14 | 23 10 7 29 9 19 13 8 19 5 | 31 25 22 32 20 28 24 22 23 21
15 | 23 15 8 28 7 21 12 10 24 6 | 30 26 19 42 21 29 22 20 26 20
16 | 21 8 8 26 7 19 12 9 24 5 | 37 26 24 39 25 33 27 26 31 25
17 | 12 10 11 22 9 14 13 7 41 6 | 43 42 38 42 42 38 48 39 46 39
18E | 17 11 10 20 11 24 10 9 17 5 | 41 33 33 41 28 38 34 39 42 35
19 | 12 9 7 21 4 10 7 10 20 4 | 41 46 42 44 41 40 41 41 40 41
20E | 15 12 8 15 5 20 18 8 16 5 | 35 31 28 32 28 33 27 29 32 27
21 | 18 9 7 26 7 19 10 8 19 5 | 25 13 15 33 13 24 17 19 19 14
22E | 14 9 8 27 7 20 9 9 8 4 | 25 22 20 26 18 27 22 19 23 21
23 | 26 13 8 20 5 19 8 7 21 5 | 40 30 25 43 26 31 21 23 24 23
X25 | 16 9 6 --- 6 12 11 9 --- 4 | 24 16 15 --- 19 24 19 21 --- 15
26 | 11 7 6 20 7 12 13 9 21 4 | 20 22 18 21 18 20 26 21 28 19
27 | 19 9 7 18 11 17 17 8 19 5 | 27 17 16 28 15 23 20 19 19 15
28 | 14 9 8 29 7 15 10 9 16 4 | 31 25 29 40 28 29 31 28 33 27
29 | 12 9 6 17 6 11 9 6 17 4 | 34 31 34 35 31 30 33 36 30 32
30 | 11 11 6 16 6 13 9 8 9 4 | 18 16 13 26 14 21 16 15 17 13
31 | 18 9 9 27 8 19 14 12 19 5 | 35 32 31 34 28 33 31 28 29 29
32E | 20 9 10 19 7 14 12 24 15 6 | 30 32 26 45 26 36 28 36 31 28
------+---------------------------------------------------+----------------------------------------------------
RMS | 18 10 8 22 8 17 12 11 21 |T 34 30 28 38 33 33 29 29 32 27
WRMS | 18 10 8 20 7 15 11 8 22 |NE 31 26 24 36 32 29 26 25 26 23
MEDI | 18 9 8 20 7 16 12 9 19 |MD 31 26 25 37 26 30 27 25 29 24
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 4.1560 GPS week: 1560 MJD: 55164.0-55170.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2984 | 15 9 33 |U 12 12 36 | 9 9 22 |
esa | esa 2879 | 9 7 23 |U 9 11 32 | 7 8 18 |
gfz | gfz 2817 |U 14 13 31 |U 12 18 55 | 15 13 33 |
grg | grg 2784 | 11 8 34 |U 9 11 37 | 9 9 19 |
igr | igr 2908 | 10 7 25 | 9 11 34 | 7 7 19 |
igs | igs 2912 | 10 7 27 | 9 10 33 | 7 8 19 |
jpl | jpl 2867 |U 13 9 33 |U 9 10 34 |U 8 8 17 |
mit | mit 3030 |U 10 8 30 |U 37 21 114 |U 7 9 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 5.1560.0 GPS week: 1560 Day: 0 MJD: 55164.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2946 | 18 10 43 | 16 22 49 | 8 6 23 |
esa | esa 2880 | 12 8 32 | 13 18 39 | 6 7 18 |
gfz | gfz 2822 | 12 10 35 | 15 27 77 | 11 8 34 |
grg | grg 2784 | 13 11 43 | 12 16 54 | 11 11 25 |
igr | igr 2967 | 11 8 30 | 13 18 40 | 7 6 22 |
igs | igs 2879 | 15 10 40 | 13 18 40 | 6 7 21 |
jpl | jpl 2865 | 17 11 41 | 13 18 42 | 8 8 16 |
mit | mit 3072 | 12 10 33 | 13 20 40 | 6 6 23 |
Table 5.1560.1 GPS week: 1560 Day: 1 MJD: 55165.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 3043 | 20 11 29 | 12 12 35 | 9 11 23 |
esa | esa 2880 | 8 8 23 | 10 12 40 | 8 11 24 |
gfz | gfz 2815 | 24 34 46 | 14 16 61 | 15 9 32 |
grg | grg 2784 | 14 13 33 | 11 12 34 | 8 10 19 |
igr | igr 2972 | 8 8 21 | 9 12 41 | 8 10 16 |
igs | igs 2937 | 10 9 27 | 12 10 45 | 8 10 20 |
jpl | jpl 2867 | 16 13 32 | 10 10 36 | 8 11 15 |
mit | mit 3072 | 10 11 25 | 13 10 46 | 7 9 22 |
Table 5.1560.2 GPS week: 1560 Day: 2 MJD: 55166.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 3046 | 8 7 40 | 9 13 34 | 9 10 23 |
esa | esa 2880 | 7 6 25 | 7 13 34 | 8 10 17 |
gfz | gfz 2809 | 9 6 20 | 12 27 75 | 17 15 34 |
grg | grg 2784 | 11 7 49 | 9 16 48 | 7 12 20 |
igr | igr 2933 | 6 5 33 | 7 14 38 | 7 8 25 |
igs | igs 2906 | 6 5 27 | 7 12 36 | 7 9 25 |
jpl | jpl 2864 | 10 8 51 | 7 12 34 | 9 11 17 |
mit | mit 3072 | 6 7 41 | 200 74 564 | 8 13 24 |
Table 5.1560.3 GPS week: 1560 Day: 3 MJD: 55167.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2967 | 15 10 38 | 12 11 35 | 7 6 12 |
esa | esa 2880 | 12 8 26 | 7 9 30 | 6 5 14 |
gfz | gfz 2817 | 11 8 26 | 12 13 47 | 10 9 34 |
grg | grg 2784 | 11 8 41 | 9 10 31 | 8 7 18 |
igr | igr 2878 | 11 8 26 | 8 9 29 | 5 5 14 |
igs | igs 2898 | 11 8 32 | 8 9 30 | 5 4 15 |
jpl | jpl 2869 | 14 9 43 | 8 10 30 | 6 5 13 |
mit | mit 3072 | 11 8 35 | 11 19 54 | 6 5 13 |
Table 5.1560.4 GPS week: 1560 Day: 4 MJD: 55168.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2965 | 13 7 22 | 10 9 33 | 7 6 19 |
esa | esa 2879 | 9 6 20 | 9 7 34 | 7 7 13 |
gfz | gfz 2826 | 14 10 26 | 16 17 49 | 17 22 33 |
grg | grg 2784 | 9 5 25 | 9 9 37 | 8 9 13 |
igr | igr 2870 | 10 6 21 | 9 7 35 | 7 8 17 |
igs | igs 2942 | 11 6 18 | 9 6 32 | 6 8 16 |
jpl | jpl 2870 | 15 8 20 | 9 6 37 | 7 6 19 |
mit | mit 2976 | 10 7 30 | 9 7 35 | 8 12 16 |
Table 5.1560.5 GPS week: 1560 Day: 5 MJD: 55169.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2961 | 16 10 32 | 15 12 39 | 10 10 23 |
esa | esa 2880 | 6 5 17 | 9 9 29 | 9 9 20 |
gfz | gfz 2816 | 15 9 30 | 10 10 35 | 21 16 41 |
grg | grg 2784 | 10 6 25 | 9 10 32 | 10 7 21 |
igr | igr 2867 | 9 6 20 | 9 10 32 | 8 8 18 |
igs | igs 2952 | 11 7 26 | 10 9 33 | 9 10 21 |
jpl | jpl 2865 | 10 7 26 | 10 9 33 | 8 7 18 |
mit | mit 2976 | 10 6 25 | 9 9 35 | 8 6 23 |
Table 5.1560.6 GPS week: 1560 Day: 6 MJD: 55170.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2966 | 13 10 31 | 12 7 29 | 13 15 31 |
esa | esa 2880 | 8 8 21 | 6 7 19 | 8 10 18 |
gfz | gfz 2820 | 13 10 32 | 9 13 37 | 16 12 26 |
grg | grg 2784 | 7 7 24 | 7 8 27 | 9 11 20 |
igr | igr 2870 | 12 9 25 | 8 7 21 | 8 7 18 |
igs | igs 2875 | 10 8 21 | 8 7 18 | 9 10 16 |
jpl | jpl 2869 | 10 8 20 | 8 8 25 | 8 9 18 |
mit | mit 2976 | 10 7 21 | 7 9 22 | 7 9 18 |
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 6.1560 GPS week: 1560 MJD: 55164.500-55170.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 5 -8 -65 -70 4 | 46 48
| 12 7 167 87 7 | 1
esa uuuuu | -15 4 191 -53 -12 | -4 16
| 45 35 194 161 10 | 5
gfz uuuuu | 25 27 -57 11 2 | 8 10
| 26 20 82 46 6 | 2
grg --xxx | -- -- 151 175 11 | 11 20
| -- -- 99 113 22 | 2
igr xxxxx | 26 35 111 -24 -11 | 7 12
| 24 17 101 72 5 | 4
irf xxxxx | -10 -10 -13 5 -6 | 3 9
| 9 10 34 60 7 | 2
jpl uuuuu | 50 -2 -32 173 8 | 7 15
| 22 20 71 125 13 | 1
mit uuuuu | -55 -18 -148 -131 -10 | 6 12
| 30 19 72 101 9 | 2
ngs uuuuu | 19 -45 124 42 10 | -11 15
| 51 37 86 108 11 | 2
sio uuuuu | -23 83 -85 152 2 | 18 20
| 17 21 92 125 14 | 3
Table 7.1560.0 GPS week: 1560 Day: 0 MJD: 55164.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 6 -19 137 -147 -5 | 48 49
esa uuuuu | -44 -5 -19 -184 -19 | 4 14
gfz uuuuu | 57 44 -142 29 6 | 4 11
grg --xxx | -- -- 164 317 25 | 12 23
igr xxxxx | 54 42 156 -30 -10 | 11 14
irf xxxxx | -18 3 -56 89 3 | 2 10
jpl uuuuu | 27 19 69 330 -5 | 8 17
mit uuuuu | -92 12 -111 -23 0 | 6 13
ngs uuuuu | 68 -94 174 -30 -1 | -12 15
sio uuuuu | -25 104 -52 326 21 | 14 17
Table 7.1560.1 GPS week: 1560 Day: 1 MJD: 55165.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | -14 -8 206 31 6 | 46 48
esa uuuuu | -45 -47 11 -253 -24 | 2 15
gfz uuuuu | 50 58 -173 71 11 | 5 11
grg --xxx | -- -- 101 320 -15 | 13 25
igr xxxxx | 47 42 -18 -53 -8 | 10 14
irf xxxxx | -21 -16 -36 73 1 | 2 10
jpl uuuuu | 28 23 -74 350 -7 | 6 16
mit uuuuu | -91 -14 -68 21 -1 | 6 12
ngs uuuuu | 97 -41 160 -170 -2 | -12 15
sio uuuuu | -59 71 49 270 15 | 15 18
Table 7.1560.2 GPS week: 1560 Day: 2 MJD: 55166.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 15 -10 -132 -121 -5 | 48 49
esa uuuuu | -24 -7 147 -159 -10 | -1 18
gfz uuuuu | 37 25 -61 27 2 | 8 9
grg --xxx | -- -- 207 152 -5 | 11 24
igr xxxxx | 20 32 26 -157 -18 | 10 14
irf xxxxx | -16 -20 -8 35 -2 | 4 7
jpl uuuuu | 75 8 -107 170 -1 | 7 16
mit uuuuu | -72 -33 -128 -95 -3 | 7 11
ngs uuuuu | 18 -13 274 122 2 | -12 15
sio uuuuu | -27 54 -93 184 10 | 18 20
Table 7.1560.3 GPS week: 1560 Day: 3 MJD: 55167.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 6 -6 -152 66 3 | 47 48
esa uuuuu | 27 -28 313 -58 5 | -5 15
gfz uuuuu | 12 30 -46 -41 -4 | 10 10
grg --xxx | -- -- 69 179 1 | 6 18
igr xxxxx | -12 1 144 -15 -10 | 7 13
irf xxxxx | -8 -22 -11 -67 -9 | 4 7
jpl uuuuu | 29 -29 -77 110 14 | 6 14
mit uuuuu | -51 -32 -206 -206 -12 | 8 11
ngs uuuuu | -8 15 95 96 14 | -11 15
sio uuuuu | -15 70 -115 142 -3 | 21 22
Table 7.1560.4 GPS week: 1560 Day: 4 MJD: 55168.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | -8 -6 -138 -62 11 | 46 47
esa uuuuu | 53 29 393 19 -6 | -6 14
gfz uuuuu | -12 -3 31 -45 -4 | 10 10
grg --xxx | -- -- 194 105 1 | 10 17
igr xxxxx | 5 42 225 -19 -9 | 5 10
irf xxxxx | 2 2 -37 -28 -10 | 4 7
jpl uuuuu | 57 0 -62 100 26 | 5 13
mit uuuuu | -36 -3 -274 -173 -17 | 8 11
ngs uuuuu | -36 -69 46 123 20 | -10 15
sio uuuuu | -4 111 -226 86 -7 | 21 22
Table 7.1560.5 GPS week: 1560 Day: 5 MJD: 55169.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 20 5 -237 -97 12 | 45 46
esa uuuuu | 6 40 454 50 -9 | -8 15
gfz uuuuu | -1 13 -59 -19 5 | 9 10
grg --xxx | -- -- 11 5 23 | 11 17
igr xxxxx | 31 33 225 46 -4 | 3 8
irf xxxxx | 0 -4 45 -42 -14 | 3 7
jpl uuuuu | 78 -18 -40 147 23 | 7 15
mit uuuuu | -19 -14 -163 -193 -22 | 6 11
ngs uuuuu | -38 -70 98 107 24 | -10 15
sio uuuuu | -14 94 -153 107 -16 | 20 22
Table 7.1560.6 GPS week: 1560 Day: 6 MJD: 55170.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 9 -14 -141 -157 7 | 45 46
esa uuuuu | -76 47 37 215 -18 | -11 19
gfz uuuuu | 32 19 50 56 -3 | 8 10
grg --xxx | -- -- 310 150 50 | 12 17
igr xxxxx | 40 55 19 63 -19 | 0 12
irf xxxxx | -7 -14 10 -22 -11 | -1 13
jpl uuuuu | 53 -14 65 7 7 | 7 15
mit uuuuu | -26 -41 -88 -248 -14 | 2 17
ngs uuuuu | 31 -43 20 45 16 | -8 12
sio uuuuu | -16 77 -5 -54 -8 | 17 22
More information about the IGSREPORT
mailing list