[IGSREPORT-16973] Wk 1510 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jan 1 04:28:38 PST 2009
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IGS Electronic Report 01 Jan 04:28:40 PST 2009 Message Number 16973
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1510 (Dec 14, 2008 - Dec 20, 2008)
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:
igs1510[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1510[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1510[0-6].cls IGS GPS clock combination summary report.
igs15107.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15107.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.
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 21 GUAT RCMN WHIT
0 | GFZ | 7 29 31 SUTM
0 | JPL | ZWE2
0 | MIT | 31 DARW HARB
1 | ESA | 32
1 | GFZ | 7 29 CHUR IRKT KERG
1 | JPL | GUAT
1 | MIT | CHUR
2 | COD | HARB
2 | EMR | MIZU
2 | ESA | 32 CRO1 MCM4
2 | GFZ | 7 21 29 CHUR DAEJ IRKT THTI WSRT
2 | MIT | CHUR DAEJ WSRT
3 | COD | MATE WROC
3 | EMR | 32 HARB MIZU OPMT
3 | ESA | 32
3 | GFZ | 7 29 CHUR
3 | JPL | BOR1 HARB
3 | MIT | BOR1 CHUR
4 | COD | RCMN WTZR
4 | EMR | HARB MIZU WTZR
4 | ESA | 32 UNSA
4 | GFZ | 7 20 29 CHUR IRKT REYK
4 | JPL | GUAT HARB
4 | MIT | 17 IENG
5 | COD | WROC
5 | ESA | 5 21 32
5 | GFZ | 5 7 20 29 GODE HARB
5 | JPL | 5
5 | MIT | 27 BOR1 HARB
6 | COD | RCMN
6 | EMR | 10 MIZU
6 | ESA | 32 DARW
6 | GFZ | 7 20 HARB IRKT
6 | MIT | 4 22 HARB HOB2 SANT
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
----+------------+----------
G14 | 2008_12_19 | 2008147
6. 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.
7. 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 | .1 .0 .5 -23 -10 -9 .14
EMR | 10.9 2.7 3.2 121 -10 65 .35
ESA | 6.6 3.0 -5.2 11 -129 33 .19
GFZ | .8 .5 1.3 18 -32 18 -.22
GRG | 7.7 -.8 -.2 -25 -15 7 -.01
JPL | 4.4 5.7 9.6 -16 -32 -3 .19
MIT | 4.5 -2.7 -5.2 1 -8 -2 -.06
NGS | 9.1 -8.3 -3.8 -106 -169 78 .06
SIO | 2.8 2.2 -.1 32 -85 19 .28
8. 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.
9. 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.
10. 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 1.1510.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1510.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 2.1510.[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 3.1510.[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 5.1510.0-6).
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 1510 summary. (Dec 14, 2008 - Dec 20, 2008)
Table 1.1510.a GPS week: 1510 MJD: 54814.000-54820.000
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 247| 0 1 1 30 -66 -60 -.17 10 9 | -457 258 15 115
| 0 0 0 10 13 27 .04 | 500 629
emr 77| 1 0 6 -224 -106 -62 .41 19 19 | -141851 882 19 209
| 0 1 2 27 22 37 .05 | 378411 1813
esa 130| 1 0 -1 -18 36 -30 .30 8 8 | 422 -1164 20 110
| 1 0 1 19 21 22 .04 | 1197 2948
gfz 201| 0 0 -4 -50 -29 208 -.13 10 10 | 122 -160 25 130
| 0 0 1 11 11 88 .03 | 458 773
grg 83| 3 2 11 68 -65 -59 1.16 46 44 | -459 229 108 1672
| 2 3 4 32 32 64 .07 | 499 628
igr n/a| 0 0 -1 -13 -98 -70 .01 6 6 | 12799 1559 23 85
| 0 0 1 15 18 17 .05 | 4296 1283
jpl 141| -1 0 7 8 -30 -17 .52 18 16 | 12389 64205 20 110
| 1 1 2 15 20 43 .06 | 20887 168753
mit 265| -1 0 -1 6 -98 -36 -.31 13 11 | 39 -571 21 144
| 1 0 1 39 30 17 .03 | 267 920
ngs 248| 0 -1 0 198 238 -72 -.23 12 9 | -817 1564 2192 3788
| 1 0 2 32 27 24 .07 | 1293 3624
sio 110| -3 1 0 -76 57 16 -.16 23 22 | --- --- --- ---
| 1 1 1 18 22 8 .09 | --- ---
Table 1.1510.b GPS week : 1510 MJD: 54814.000-54820.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 0 0 0 0 0 0 0 |
2 | 6 6 6 6 6 6 6 |
3 | 5 5 5 4 4 5 4 |
4 | 4 4 4 4 5 5 5 |
5 | 5 4 4 4 4 5 5 |
6 | 4 5 4 4 4 4 4 |
7 | 5 5 6 5 5 5 6 |
8 | 7 6 6 5 5 5 5 |
9 | 5 5 5 4 5 4 5 |
10 | 7 6 6 7 6 8 8 |
11 | 5 5 5 4 4 4 5 |
12 | 5 5 5 5 5 5 5 |
13 | 5 4 4 5 4 4 5 |
14 | 6 5 5 5 6 0 5 |
15 | 6 6 6 6 5 5 5 |
16 | 5 5 6 5 6 5 6 |
17 | 7 6 6 6 6 6 6 |
18 | 5 5 5 5 4 5 6 |
19 | 5 4 4 4 4 4 4 |
20 | 5 4 4 5 5 5 5 |
21 | 5 5 5 5 5 5 5 |
22 | 5 6 5 4 4 5 4 |
23 | 5 5 4 5 5 5 5 |
24 | 5 4 3 3 3 4 3 |
25 | 5 5 4 4 4 4 4 |
26 | 5 5 4 4 4 4 4 |
27 | 5 5 5 5 5 5 5 |
28 | 6 5 5 5 5 5 5 |
29 | 5 4 5 4 5 5 4 |
30 | 4 4 4 4 4 5 4 |
31 | 6 6 6 5 5 5 4 |
32 | 7 6 6 6 5 5 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 2.1510.0 GPS week: 1510 Day: 0 MJD: 54814.000
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 247| 0 1 2 47 -54 -17 -.23 11 11 | 52 -91 13 84
| 28 -59 |
emr 77| 1 0 7 -241 -135 -104 .36 21 21 | -489 -1221 21 198
| 8 -22 |
esa 130| 1 0 0 -15 17 -45 .30 8 8 | 251 210 20 110
| -27 67 |
gfz 201| 0 0 -5 -45 -28 185 -.12 9 9 | 388 -741 23 121
| 15 -46 |
grg 83| 0 3 18 75 -16 -50 1.02 46 46 | 39 -112 112 353
| 65 -7 |
igr n/a| 0 0 0 -23 -84 -88 .08 6 6 | 8064 -162 25 92
| -17 -8 |
jpl 141| -2 1 4 -21 -42 -59 .46 20 19 | 24 -1465 20 97
| 9 -18 |
mit 265| 0 -1 -1 35 -126 -49 -.34 18 17 | 14 -460 21 114
| -29 0 |
ngs 248| 0 -1 0 169 217 -88 -.24 13 9 | 193 -196 2059 3863
| 15 0 |
sio 110| -1 1 0 -100 67 22 -.23 23 24 | --- --- --- ---
| 149 -38 |
Table 2.1510.1 GPS week: 1510 Day: 1 MJD: 54815.000
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 247| 0 0 0 20 -48 -79 -.19 11 10 | -811 1052 14 122
| 1 -48 |
emr 77| 1 -1 3 -173 -127 -86 .40 19 19 | -1612 1372 26 264
| -29 10 |
esa 130| 0 0 0 -14 17 -36 .30 8 8 | -645 -498 20 118
| 1 79 |
gfz 201| 1 0 -5 -53 -13 258 -.14 9 9 | 205 -208 26 122
| 0 -47 |
grg 83| 2 6 10 110 -79 -44 1.23 45 43 | -818 1024 106 423
| -26 -35 |
igr n/a| 0 0 1 12 -119 -72 .07 5 5 | 7823 2106 23 90
| -32 53 |
jpl 141| -1 0 6 18 -57 -84 .49 19 17 | -1579 737 21 95
| -43 -78 |
mit 265| 0 0 -2 -64 -92 -41 -.28 13 11 | -162 178 18 101
| 25 -2 |
ngs 248| -1 -2 3 245 258 -84 -.19 13 9 | -815 1022 2082 3280
| -62 -12 |
sio 110| -2 2 0 -75 38 26 -.26 23 22 | --- --- --- ---
| 103 -22 |
Table 2.1510.2 GPS week: 1510 Day: 2 MJD: 54816.000
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 247| 0 2 1 19 -67 -60 -.20 10 10 | 129 -329 17 115
| -5 -18 |
emr 77| 0 3 6 -217 -77 2 .36 21 21 | -999999 4118 19 213
| -27 -45 |
esa 130| 2 -2 -1 -33 12 -51 .31 8 8 | 173 863 21 109
| 5 33 |
gfz 201| -2 0 -4 -52 -23 233 -.15 10 10 | 624 -1019 27 146
| -8 -27 |
grg 83| 2 5 11 22 -76 -11 1.17 45 42 | 130 -367 112 390
| 26 21 |
igr n/a| 0 -1 -1 -7 -126 -64 -.00 5 5 | 10290 3101 22 100
| -26 55 |
jpl 141| -1 2 6 0 -40 -16 .50 17 16 | 55306 446889 21 110
| 3 -19 |
mit 265| 0 0 0 -21 -85 -43 -.30 12 10 | 319 -734 24 143
| 6 26 |
ngs 248| 0 -1 -1 244 239 -80 -.14 13 10 | 144 -384 2570 4268
| -20 44 |
sio 110| -2 3 1 -48 95 11 -.23 22 25 | --- --- --- ---
| 100 -23 |
Table 2.1510.3 GPS week: 1510 Day: 3 MJD: 54817.000
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 247| 0 1 0 23 -84 -52 -.12 10 9 | -794 117 22 114
| -12 -11 |
emr 77| 2 0 7 -256 -85 -45 .46 18 18 | 988 1967 23 209
| 37 -15 |
esa 130| 1 -1 0 -1 36 -36 .37 8 8 | -94 120 21 109
| -22 8 |
gfz 201| 0 0 -4 -71 -32 237 -.09 10 10 | -782 1174 27 130
| 12 -15 |
grg 83| 1 -4 12 25 -117 -200 1.12 47 44 | -791 94 114 9459
| 68 59 |
igr n/a| 0 0 -2 -31 -104 -80 .01 5 5 | 12673 3181 22 79
| 2 23 |
jpl 141| -1 -1 6 27 -6 3 .50 18 17 | 24620 3121 20 98
| -24 -54 |
mit 265| 0 0 0 0 -84 -26 -.30 11 10 | 112 -1941 23 154
| 22 19 |
ngs 248| 0 0 -3 187 207 -100 -.35 12 7 | -3525 9665 2235 4123
| 5 23 |
sio 110| -3 2 1 -56 74 20 -.19 22 21 | --- --- --- ---
| 109 -21 |
Table 2.1510.4 GPS week: 1510 Day: 4 MJD: 54818.000
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 247| 0 0 1 33 -81 -104 -.12 9 9 | -163 -165 16 129
| 3 -2 |
emr 77| 0 1 3 -246 -99 -87 .45 18 18 | 1831 -712 16 183
| 37 9 |
esa 130| 3 0 0 -28 62 -39 .25 8 8 | 2906 -7732 19 103
| -15 35 |
gfz 201| 0 0 -1 -38 -50 337 -.10 10 10 | 352 -799 26 133
| -9 -20 |
grg 83| 6 1 13 79 -39 -16 1.14 47 48 | -160 -197 104 369
| 40 42 |
igr n/a| 0 0 -1 -18 -86 -81 .02 6 5 | 14889 458 21 72
| -14 32 |
jpl 141| -3 0 6 7 -3 -12 .50 17 16 | 1808 -616 20 115
| 18 -10 |
mit 265| 0 0 -2 23 -89 -46 -.31 10 9 | 403 -1625 21 146
| 14 6 |
ngs 248| 0 -1 -2 188 243 -67 -.21 11 9 | -161 -194 2203 3878
| -38 -21 |
sio 110| -5 1 1 -82 52 -1 -.11 22 18 | --- --- --- ---
| 125 5 |
Table 2.1510.5 GPS week: 1510 Day: 5 MJD: 54819.000
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 247| 0 1 2 33 -56 -46 -.17 9 8 | -406 -34 16 119
| 1 -5 |
emr 77| 2 1 7 -225 -98 -81 .39 19 19 | 3224 -33 16 168
| 24 -9 |
esa 130| 2 0 -4 11 49 -15 .32 9 9 | 828 -867 20 103
| -28 13 |
gfz 201| 0 -1 -4 -38 -26 146 -.13 9 9 | 187 165 25 129
| -4 -32 |
grg 83| 5 -1 5 78 -72 -54 1.18 46 42 | -403 -60 103 368
| 50 66 |
igr n/a| 1 0 -2 -1 -91 -73 -.01 6 6 | 17551 1035 24 76
| -9 10 |
jpl 141| -2 -1 9 16 -20 -4 .58 17 15 | 3438 155 21 117
| 17 6 |
mit 265| -2 0 0 21 -61 -45 -.35 13 10 | -40 216 23 173
| 25 -2 |
ngs 248| 2 0 -1 180 218 -59 -.20 14 10 | -377 -84 2021 3606
| 72 -60 |
sio 110| -5 2 1 -85 41 17 -.06 23 21 | --- --- --- ---
| 129 26 |
Table 2.1510.6 GPS week: 1510 Day: 6 MJD: 54820.000
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 247| 0 1 2 37 -69 -61 -.13 8 7 | -1212 1258 13 125
| 6 -13 |
emr 77| 1 0 6 -212 -123 -34 .46 18 18 | 3097 683 14 229
| -15 27 |
esa 130| 0 0 -3 -47 60 14 .25 8 8 | -459 -246 21 118
| -11 18 |
gfz 201| 0 -2 -3 -49 -32 61 -.18 10 10 | -116 305 21 133
| 14 -25 |
grg 83| 5 5 8 87 -52 -40 1.22 48 43 | -1213 1221 109 348
| 36 -44 |
igr n/a| 1 -1 -1 -22 -77 -35 -.07 7 7 | 18303 1194 24 92
| -4 -11 |
jpl 141| 0 0 10 10 -39 50 .63 17 15 | 3106 616 22 141
| -39 -41 |
mit 265| -3 0 -1 53 -151 -1 -.29 15 11 | -368 365 22 181
| 4 20 |
ngs 248| 1 0 -1 171 287 -26 -.29 12 10 | -1183 1125 2178 3503
| 24 -59 |
sio 110| -4 0 -1 -84 33 14 -.06 24 22 | --- --- --- ---
| 139 -6 |
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 3.1510.0 GPS week: 1510 Day: 0 MJD: 54814.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 --- --- --- --- 179 --- --- --- --- 0 | 29 --- --- --- --- 153 --- --- --- --- 31
2 | 12 22 8 6 50 6 25 16 15 35 6 | 14 28 20 17 45 19 31 19 22 31 18
3 | 9 16 6 7 49 5 15 15 12 29 4 | 25 25 22 21 38 21 24 26 28 31 23
4 | 10 15 4 8 52 4 15 15 10 21 4 | 29 30 29 34 35 31 28 28 32 37 28
5 | 12 16 7 9 21 5 13 14 8 28 4 | 22 29 28 26 39 25 19 24 26 30 25
6 | 7 13 6 5 51 6 14 12 9 31 4 | 31 30 27 27 34 27 29 31 32 23 27
7E | 9 24 6 11 34 8 18 14 8 20 4 | 34 47 46 46 53 42 42 38 43 32 41
8E | 18 20 10 15 34 6 20 23 16 36 6 | 109 102 109 107 111 108 111 101 110 96 105
9 | 11 22 5 9 38 9 19 15 12 21 4 | 13 29 19 13 37 14 23 15 20 21 16
10E | 18 20 9 10 34 5 21 19 25 23 6 | 30 38 37 35 49 33 40 35 45 45 35
11 | 10 18 6 8 87 7 21 14 11 22 4 | 33 43 38 36 59 32 40 35 29 31 34
12 | 10 23 10 10 27 6 25 15 10 21 5 | 20 35 22 20 48 23 36 24 25 26 22
13 | 10 26 7 8 36 5 18 13 10 17 4 | 18 34 22 20 46 21 29 16 18 13 18
14 | 15 23 9 8 40 7 26 21 13 23 6 | 14 31 25 20 34 20 24 20 26 17 22
15 | 12 29 9 13 25 8 24 18 10 24 6 | 18 32 23 23 38 18 27 19 19 17 20
16 | 9 24 7 6 45 5 22 12 13 21 5 | 17 35 19 15 56 17 30 16 19 20 16
17 | 13 15 8 15 54 9 24 18 12 45 6 | 33 35 35 41 40 32 33 37 32 50 33
18E | 10 25 9 9 35 6 25 20 10 15 5 | 18 34 28 22 44 21 33 17 28 21 24
19 | 12 17 7 5 88 7 15 27 11 25 5 | 37 34 38 35 79 34 32 39 39 36 36
20E | 8 17 9 5 22 5 20 17 12 14 4 | 35 41 40 35 51 36 39 35 33 39 36
21 | 12 22 7 8 52 4 23 15 9 19 5 | 19 33 24 18 54 21 34 15 21 19 21
22E | 11 21 8 9 36 5 19 19 13 12 5 | 15 29 26 18 45 19 28 16 28 20 22
23 | 7 29 6 8 32 5 20 17 14 15 5 | 16 37 23 21 44 21 29 18 18 19 18
24 | 10 15 9 7 42 10 14 17 13 15 4 | 24 31 35 29 33 33 34 26 35 27 31
25 | 9 21 5 11 32 5 15 20 11 15 4 | 12 25 16 19 30 14 25 22 17 17 12
26 | 9 18 9 9 23 6 15 23 11 17 5 | 18 23 24 18 31 17 17 19 23 19 20
27 | 14 20 6 10 35 5 18 16 10 19 5 | 13 28 16 16 30 14 23 22 16 23 15
28 | 10 27 8 8 40 8 25 17 14 20 5 | 23 41 27 25 47 25 35 26 24 30 25
29 | 11 11 9 8 56 5 13 16 11 29 4 | 30 35 40 36 38 35 33 34 33 29 34
30 | 10 14 7 8 28 7 12 12 8 21 4 | 14 25 21 19 35 21 24 18 18 23 18
31E | 14 19 6 10 46 6 20 31 13 21 6 | 52 57 55 53 67 51 53 57 49 50 52
32E | 13 22 9 7 76 6 15 28 27 23 6 | 28 36 36 30 52 32 36 27 42 25 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 21 8 9 46 6 20 18 13 23 |T 26 35 31 28 46 32 33 28 30 29 28
WRMS | 11 21 8 9 46 6 19 17 9 24 |NE 21 31 25 23 42 28 28 23 24 25 23
MEDI | 10 20 7 8 38 6 19 17 11 21 |MD 22 34 27 23 44 23 31 24 28 26 24
Table 3.1510.1 GPS week: 1510 Day: 1 MJD: 54815.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 --- --- --- --- 51 --- --- --- --- 0 | 22 --- --- --- --- 65 --- --- --- --- 26
2 | 14 22 10 10 37 5 25 14 11 28 5 | 11 29 22 16 40 16 30 15 21 27 17
3 | 7 15 9 7 83 3 12 8 12 34 4 | 22 23 19 19 43 18 19 20 26 30 21
4 | 8 15 8 8 45 4 12 9 10 20 4 | 23 29 23 24 32 20 21 25 27 29 23
5 | 12 12 5 6 26 5 12 8 12 24 4 | 31 37 42 40 52 36 18 36 44 33 38
6 | 9 12 8 8 67 4 14 9 12 30 4 | 25 26 22 22 33 24 23 23 31 25 24
7E | 9 18 7 13 40 4 16 10 11 28 5 | 19 26 26 23 46 22 24 18 26 22 21
8E | 16 17 9 14 33 5 18 16 14 28 5 | 88 91 89 90 70 90 86 91 94 96 90
9 | 12 21 6 8 45 8 16 12 9 20 4 | 12 25 12 15 52 11 21 14 21 17 13
10E | 16 20 10 10 44 5 20 12 23 23 6 | 25 34 30 28 54 27 36 27 39 33 27
11 | 9 18 5 10 80 6 19 12 13 18 4 | 23 33 25 24 48 21 32 24 28 27 24
12 | 15 24 8 9 32 6 24 9 11 19 5 | 20 30 21 17 50 19 32 15 28 19 19
13 | 9 18 7 8 32 2 19 7 7 19 4 | 15 31 22 19 46 18 28 13 23 13 17
14 | 12 20 10 7 49 7 25 13 10 20 5 | 13 26 22 16 35 16 23 17 27 17 19
15 | 11 26 10 12 32 4 22 14 11 29 5 | 13 28 17 20 43 16 25 17 22 23 17
16 | 10 24 7 8 37 5 23 10 15 21 5 | 15 33 21 17 47 18 27 18 28 20 20
17 | 13 16 9 12 70 9 17 14 9 45 6 | 19 20 18 23 30 17 17 23 20 42 19
18E | 9 21 11 11 30 4 22 14 13 14 5 | 18 31 24 24 41 22 27 19 30 25 23
19 | 8 14 6 7 52 5 13 12 7 26 4 | 22 21 24 21 25 20 19 23 27 24 23
20E | 9 14 6 6 38 4 23 12 12 12 4 | 32 39 37 36 51 34 37 31 33 40 34
21 | 12 24 7 8 38 5 22 11 8 17 5 | 21 33 25 20 47 23 31 16 28 19 23
22E | 10 26 9 11 40 5 25 14 17 14 5 | 15 28 24 18 48 17 27 17 27 24 20
23 | 8 24 7 10 24 4 22 10 10 16 4 | 15 33 22 20 43 18 27 14 22 16 17
24 | 8 15 6 8 35 5 9 10 9 14 3 | 17 25 27 24 31 23 24 21 32 26 24
25 | 10 20 7 9 35 4 15 17 15 17 5 | 9 24 17 15 32 12 22 17 22 13 12
26 | 9 13 10 8 24 5 11 20 13 15 4 | 19 22 24 24 36 21 23 26 23 23 21
27 | 13 16 7 12 30 4 15 13 13 18 4 | 11 22 14 17 29 12 21 16 17 17 12
28 | 11 20 8 8 35 5 21 13 14 17 5 | 21 31 24 22 41 22 31 25 26 27 22
29 | 8 11 7 7 39 6 12 9 11 26 4 | 16 23 23 21 27 21 22 20 29 21 22
30 | 8 15 5 6 17 6 12 7 12 18 3 | 12 25 18 14 34 16 21 15 27 21 17
31 | 13 20 9 13 35 8 21 19 13 21 5 | 67 73 72 71 88 66 70 77 73 65 72
32E | 12 21 9 11 80 6 18 16 24 19 6 | 25 30 33 29 55 28 34 23 42 27 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 8 9 45 5 19 13 13 23 |T 22 31 27 25 43 25 28 24 31 27 25
WRMS | 10 19 8 9 43 5 17 11 9 22 |NE 17 27 21 20 38 20 24 19 26 23 20
MEDI | 10 18 8 8 37 5 18 12 12 20 |MD 19 29 23 21 43 20 25 20 27 24 21
Table 3.1510.2 GPS week: 1510 Day: 2 MJD: 54816.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 --- --- --- --- 48 --- --- --- --- 0 | 20 --- --- --- --- 48 --- --- --- --- 23
2 | 12 23 9 10 44 5 22 15 10 26 5 | 10 32 17 19 42 15 31 13 15 24 14
3 | 7 17 9 5 77 6 11 12 12 37 4 | 21 20 23 21 36 21 20 22 29 36 22
4 | 9 12 7 11 38 7 9 14 9 19 4 | 23 26 23 27 46 22 24 22 25 26 21
X5 | 8 15 6 8 30 3 --- 6 10 23 4 | 23 30 22 24 31 26 --- 26 26 26 22
6 | 6 12 9 9 65 5 8 11 11 29 4 | 22 24 27 22 28 24 21 24 30 28 24
7 | 15 27 8 17 46 4 20 9 9 21 5 | 30 47 43 46 67 41 39 37 41 33 37
8E | 13 19 9 13 38 5 16 14 16 27 5 | 89 83 87 87 69 86 87 88 86 84 85
9 | 11 20 6 7 32 3 16 12 13 20 4 | 15 27 12 15 28 13 22 13 21 17 12
10E | 17 21 8 11 37 7 19 9 29 13 6 | 25 38 27 31 50 25 36 23 42 27 25
11 | 8 21 8 10 70 7 17 8 11 20 4 | 27 39 30 32 45 26 34 26 30 29 28
12 | 7 20 11 11 27 4 24 9 9 21 5 | 19 31 19 18 48 18 33 18 20 21 17
13 | 7 27 8 9 27 4 17 6 7 19 4 | 17 36 23 23 52 19 29 16 22 15 18
14 | 11 26 7 7 48 5 19 14 9 23 5 | 13 28 19 19 33 14 21 19 25 17 17
15 | 10 26 6 10 30 5 20 12 13 29 5 | 13 28 17 19 40 14 27 19 23 24 15
16 | 9 30 9 8 32 6 24 10 18 21 5 | 16 37 23 17 44 17 30 19 29 21 18
17 | 13 15 7 16 71 5 16 17 9 42 6 | 22 27 24 33 35 25 24 26 28 43 25
18E | 9 20 9 10 31 4 22 10 11 18 4 | 17 32 24 22 42 19 28 18 29 25 21
19 | 8 14 5 10 66 5 11 7 12 27 4 | 28 28 28 30 49 28 26 27 33 28 27
20E | 7 20 7 5 32 5 21 9 8 22 4 | 38 47 40 38 58 39 44 35 44 42 39
21 | 10 23 6 7 40 6 22 11 12 18 4 | 16 35 22 17 48 20 32 14 27 20 19
22E | 9 23 7 9 31 3 20 11 15 18 5 | 14 28 21 16 47 16 26 14 28 20 18
23 | 7 28 7 8 31 5 19 7 8 14 4 | 16 33 22 18 43 18 28 14 19 17 15
24 | 8 15 4 6 40 6 8 11 9 11 3 | 18 27 25 24 28 22 27 20 29 23 22
25 | 8 19 9 8 29 3 14 13 12 13 4 | 13 26 19 17 27 13 24 17 22 14 12
26 | 11 17 5 9 22 2 9 14 13 17 4 | 21 24 20 20 32 19 22 22 33 25 22
27 | 11 17 9 13 38 5 14 14 15 16 5 | 12 22 16 19 33 14 21 18 20 16 11
28 | 11 23 8 11 49 5 20 14 12 17 5 | 24 39 25 27 47 25 36 23 29 29 25
29 | 7 12 10 7 38 7 12 9 13 30 4 | 22 30 32 24 35 25 24 25 33 22 25
30 | 7 14 6 8 26 5 11 6 10 19 3 | 14 27 16 16 30 15 22 13 22 20 15
31 | 14 23 12 10 43 7 17 24 13 20 6 | 40 45 42 34 35 36 41 39 39 36 36
32E | 9 25 9 10 68 6 15 14 22 19 5 | 22 30 29 26 40 26 34 22 40 24 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 21 8 10 45 5 17 12 13 22 |T 22 33 26 25 41 24 30 23 30 26 23
WRMS | 10 21 8 10 42 5 16 10 10 25 |NE 18 29 21 21 38 20 26 19 25 23 19
MEDI | 9 20 8 9 38 5 17 11 12 20 |MD 20 30 23 22 42 21 27 22 29 24 22
Table 3.1510.3 GPS week: 1510 Day: 3 MJD: 54817.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 --- --- --- --- 68 --- --- --- --- 0 | 21 --- --- --- --- 73 --- --- --- --- 23
2 | 11 21 8 12 37 5 24 15 15 25 5 | 19 32 18 21 38 18 32 15 18 24 17
3 | 6 12 6 4 61 6 14 11 10 33 4 | 24 22 23 24 32 23 26 23 25 30 22
4 | 8 9 4 10 28 5 11 15 11 24 4 | 31 29 31 30 30 32 29 30 34 35 29
X5 | 12 16 7 8 23 6 --- 7 6 --- 4 | 40 46 47 44 67 46 --- 43 47 --- 44
6 | 6 11 8 7 58 5 13 8 8 27 3 | 28 27 27 29 34 27 30 27 28 25 26
7 | 8 21 6 11 31 7 19 7 10 23 4 | 26 39 30 28 49 29 29 23 25 20 24
8 | 15 16 7 10 38 5 16 11 8 23 4 | 85 90 91 88 96 89 90 92 92 91 88
9 | 11 18 6 9 40 7 14 9 13 18 4 | 19 26 19 16 46 15 23 15 19 16 14
10E | 17 22 11 10 35 6 22 9 30 18 6 | 32 37 34 31 50 29 39 27 44 36 30
11 | 9 16 6 10 88 7 17 8 9 15 4 | 33 40 34 32 59 34 39 31 34 28 32
12 | 9 18 7 13 34 5 23 13 10 18 5 | 22 31 23 18 52 21 33 21 16 23 19
13 | 8 22 8 10 36 4 19 6 8 19 4 | 20 35 25 21 50 21 30 18 21 18 19
X14 | 12 25 9 8 44 5 --- 6 9 23 5 | 12 29 19 12 39 14 --- 13 23 15 16
15 | 11 27 9 13 40 6 25 10 7 24 5 | 19 33 20 19 46 19 30 19 24 29 18
16 | 8 25 10 8 32 4 20 11 9 20 4 | 22 41 25 22 44 22 33 20 24 27 22
17 | 13 17 8 15 58 4 17 14 8 44 6 | 26 28 34 35 33 31 26 31 31 44 29
18E | 7 17 10 9 40 3 22 11 8 21 4 | 17 25 24 16 42 18 28 18 27 25 20
19 | 7 10 8 7 102 5 12 4 5 26 3 | 32 30 32 31 88 31 32 32 31 31 30
20E | 10 13 9 10 33 4 23 12 12 20 4 | 41 47 44 40 56 42 49 41 46 44 42
21 | 8 22 10 10 34 6 21 10 7 22 4 | 21 34 27 18 51 23 32 17 21 21 20
22E | 8 15 8 11 36 5 20 8 6 15 4 | 16 24 25 18 42 18 28 19 25 22 20
23 | 6 29 9 11 33 5 21 7 9 14 4 | 19 41 24 22 46 21 30 19 21 21 20
24 | 5 10 9 9 33 6 9 9 7 11 3 | 25 30 34 30 32 30 28 25 29 24 28
25 | 9 16 8 10 30 5 15 12 9 15 4 | 15 25 19 13 37 16 23 19 20 14 14
26 | 10 17 9 9 26 3 10 13 9 17 4 | 29 35 29 30 56 30 29 30 36 35 29
27 | 12 17 8 9 33 4 15 12 13 15 4 | 17 27 20 17 37 17 23 22 20 18 15
28 | 12 22 11 11 47 4 21 10 10 16 5 | 22 35 28 24 40 22 30 24 18 23 20
29 | 7 10 8 8 37 6 12 9 8 29 4 | 28 30 34 29 30 30 29 28 29 24 27
30 | 7 16 10 6 18 5 13 8 8 14 3 | 18 26 23 15 34 18 24 13 20 20 16
31 | 8 21 10 9 41 7 19 17 14 18 5 | 33 42 39 36 54 34 34 34 33 29 33
32E | 10 20 9 10 81 4 17 13 24 19 5 | 23 33 28 24 42 23 32 20 33 23 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 8 10 47 5 18 11 12 22 |T 26 34 30 26 46 28 32 26 29 27 25
WRMS | 9 18 8 10 44 5 17 10 7 21 |NE 23 31 26 24 44 26 29 23 25 24 22
MEDI | 8 17 8 10 36 5 17 10 9 19 |MD 22 32 27 24 44 23 30 23 25 24 22
Table 3.1510.4 GPS week: 1510 Day: 4 MJD: 54818.000
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 | 8 --- --- --- --- 24 --- --- --- --- 0 | 26 --- --- --- --- 31 --- --- --- --- 27
2 | 10 23 11 12 28 5 23 14 11 22 5 | 23 34 25 23 39 25 37 23 28 33 24
3 | 9 12 7 9 66 5 12 9 11 28 4 | 25 24 23 22 34 23 21 26 28 31 23
4 | 9 11 8 13 34 7 13 16 9 29 5 | 30 27 33 28 26 30 29 32 32 39 29
X5 | 10 16 7 6 39 6 --- 6 8 20 4 | 41 45 41 34 41 39 --- 35 37 56 38
6 | 8 11 7 7 55 4 12 8 7 24 3 | 25 27 25 24 24 24 24 26 24 25 23
7 | 8 21 10 17 49 6 16 7 10 24 5 | 25 38 29 32 53 28 30 25 27 24 25
8 | 12 14 8 12 34 5 17 13 10 25 5 | 64 67 66 67 73 65 69 66 68 66 65
9 | 12 17 6 10 50 8 15 11 8 25 4 | 29 35 25 20 37 24 30 25 25 28 24
10E | 15 22 10 9 37 10 19 12 22 21 6 | 26 34 26 27 49 26 35 22 38 26 26
11 | 7 16 8 9 87 4 18 7 11 18 4 | 31 41 37 29 52 32 38 32 32 27 32
12 | 14 20 9 10 27 6 21 13 7 21 5 | 33 34 30 23 45 28 36 27 28 29 28
13 | 6 20 10 10 30 6 18 6 7 18 4 | 23 36 28 24 45 24 32 24 21 23 23
X14 | 13 26 8 13 --- 5 --- 9 7 --- 5 | 12 31 22 22 --- 17 --- 18 20 --- 18
X15 | 8 22 9 9 35 5 23 10 11 --- 5 | 26 36 28 26 48 26 33 27 26 --- 26
16 | 10 27 12 8 32 4 22 10 12 21 5 | 24 37 27 18 50 25 33 25 31 26 24
17 | 10 16 8 14 85 7 16 8 10 44 5 | 26 30 30 33 49 28 28 30 29 43 28
18E | 8 15 9 11 28 4 21 7 9 18 4 | 24 31 27 22 34 24 30 22 26 27 24
19 | 8 12 6 8 68 4 9 5 10 27 3 | 31 34 36 27 58 31 29 32 35 27 31
20E | 9 14 9 9 41 5 23 10 12 14 4 | 61 69 66 62 64 63 69 60 60 67 62
21 | 10 18 7 10 45 5 20 9 10 21 4 | 28 38 28 19 50 26 36 25 26 30 26
22E | 7 18 7 9 30 6 20 8 10 14 4 | 26 33 26 19 46 25 31 24 28 28 24
23 | 6 27 10 10 38 5 22 7 12 13 5 | 23 41 29 21 45 25 34 23 22 23 23
24 | 8 11 5 8 38 5 8 10 10 8 3 | 27 36 31 27 41 27 31 29 27 28 28
25 | 9 14 7 11 32 6 14 12 10 13 4 | 21 30 22 20 32 22 29 22 23 21 19
26 | 7 15 6 7 18 5 8 9 9 18 3 | 30 36 31 30 34 30 30 34 30 34 30
27 | 10 13 10 11 24 5 15 14 11 16 4 | 20 26 17 19 31 18 26 26 18 20 17
28 | 9 21 8 11 61 6 20 11 16 19 5 | 23 35 26 19 46 23 33 23 18 25 21
29 | 8 10 9 7 33 7 11 13 10 28 4 | 27 31 28 24 36 26 27 31 24 23 26
30 | 9 14 6 7 25 6 12 10 8 16 3 | 25 32 23 16 31 24 28 22 25 23 22
31 | 8 22 10 7 36 7 17 8 12 18 4 | 26 35 29 24 40 26 29 23 30 23 25
32E | 11 23 7 9 73 6 16 10 20 21 5 | 25 38 34 23 43 27 34 23 34 27 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 8 10 47 6 17 10 11 22 |T 28 36 30 26 43 28 33 28 29 31 27
WRMS | 9 18 8 10 48 5 16 9 9 18 |NE 26 33 28 23 40 26 30 26 26 29 25
MEDI | 9 16 8 9 36 5 17 10 10 21 |MD 26 35 28 24 43 26 31 25 28 27 25
Table 3.1510.5 GPS week: 1510 Day: 5 MJD: 54819.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 5 --- --- --- --- 121 --- --- --- --- 0 | 28 --- --- --- --- 80 --- --- --- --- 31
2 | 10 23 11 8 26 4 23 17 16 23 5 | 13 30 15 16 37 13 31 14 15 23 14
3 | 6 15 11 9 61 5 11 9 12 29 4 | 19 21 16 22 23 17 18 22 19 26 16
4 | 11 9 8 7 46 6 8 17 13 26 4 | 25 23 29 27 30 28 24 26 32 31 25
5 | 19 16 8 8 42 5 14 14 9 17 5 | 67 72 71 68 70 67 56 73 71 67 70
6 | 4 12 10 9 60 6 10 8 11 24 4 | 17 22 19 20 22 18 19 21 19 18 16
7 | 8 21 10 15 42 9 12 6 13 21 4 | 25 37 27 28 42 28 28 22 29 24 23
8 | 12 18 9 7 33 6 15 15 14 26 5 | 29 40 32 30 43 30 35 30 30 31 29
9 | 10 17 6 7 35 6 15 12 7 25 4 | 12 26 16 15 24 13 23 20 15 19 13
10E | 14 23 15 10 25 11 20 32 29 30 8 | 26 37 33 33 37 30 36 41 39 40 29
11 | 7 18 8 6 79 4 16 10 13 18 4 | 29 33 30 27 46 28 32 27 33 23 27
12 | 9 21 13 9 26 4 21 17 9 21 5 | 15 30 16 15 41 14 29 19 16 17 15
13 | 5 21 9 6 31 5 18 7 12 19 4 | 16 34 20 20 45 20 28 16 21 19 17
X14 | 5 --- --- --- --- 27 --- --- --- --- 0 | 9 --- --- --- --- 19 --- --- --- --- 9
15 | 7 22 10 8 39 4 22 13 11 27 5 | 17 31 22 20 48 18 30 24 19 30 19
16 | 8 24 8 7 31 4 23 12 12 22 5 | 17 33 17 17 34 19 30 15 20 18 15
17 | 9 14 11 14 94 5 13 10 13 43 5 | 24 28 29 30 42 27 24 27 33 40 25
18E | 7 24 9 10 43 4 23 8 14 12 5 | 16 28 18 20 34 15 25 19 23 23 17
19 | 5 17 8 9 77 7 13 9 10 28 4 | 21 24 25 25 51 23 18 23 26 22 22
20E | 10 14 8 5 38 3 24 11 14 13 4 | 56 62 57 59 67 60 64 56 59 63 57
21 | 8 20 7 10 42 4 20 7 14 23 4 | 18 34 21 17 42 16 35 16 15 21 17
22E | 9 17 7 12 21 6 23 7 12 15 4 | 16 24 19 20 34 13 25 15 19 20 16
23 | 7 26 10 8 41 5 23 9 14 15 5 | 17 37 21 21 46 20 29 15 22 18 17
24 | 6 14 5 8 39 5 5 14 9 11 3 | 18 27 24 20 36 21 24 23 23 20 21
25 | 8 15 5 9 29 7 14 12 9 19 4 | 14 26 17 19 23 17 23 17 19 20 13
26 | 5 10 8 6 28 4 8 11 12 17 3 | 26 27 25 23 36 24 25 27 27 32 23
27 | 11 17 9 7 31 6 13 17 13 16 4 | 12 26 15 18 32 14 21 22 14 18 12
28 | 9 20 8 8 49 4 18 10 15 23 4 | 16 34 22 22 44 18 31 19 21 23 18
29 | 7 14 6 9 38 5 11 15 9 31 4 | 18 24 26 25 26 21 22 27 24 18 21
30 | 8 16 8 9 27 6 12 16 15 15 4 | 11 25 18 15 29 14 26 18 16 16 14
31 | 7 19 7 10 37 6 18 9 16 20 4 | 30 39 29 31 40 31 33 29 33 26 29
32E | 9 24 11 8 67 8 16 11 22 19 5 | 24 31 31 26 42 25 33 21 36 25 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 9 9 46 6 17 13 14 23 |T 21 32 25 24 38 25 29 24 26 26 22
WRMS | 8 19 9 9 42 6 15 10 10 21 |NE 19 30 23 22 37 23 27 23 23 24 20
MEDI | 8 17 8 8 38 5 15 11 13 21 |MD 18 30 22 21 37 20 28 22 22 23 18
Table 3.1510.6 GPS week: 1510 Day: 6 MJD: 54820.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 --- --- --- --- 110 --- --- --- --- 0 | 29 --- --- --- --- 91 --- --- --- --- 29
2 | 9 21 10 11 29 8 24 20 14 25 5 | 23 35 26 23 41 24 36 24 25 31 23
3 | 6 10 5 8 71 7 10 10 9 29 3 | 27 29 28 29 51 31 25 31 34 36 29
4 | 8 12 6 10 46 8 12 21 9 24 4 | 36 34 38 38 31 39 34 36 44 41 37
5 | 9 16 9 9 31 10 13 15 9 22 4 | 49 52 53 51 41 56 28 48 53 44 50
6 | 4 9 5 7 80 6 10 9 12 30 3 | 29 32 31 32 51 33 29 32 34 30 30
7 | 6 27 9 20 40 6 17 9 11 24 5 | 29 38 28 35 43 27 33 24 33 26 29
8 | 10 17 10 9 55 5 15 18 10 26 5 | 67 67 65 62 63 64 68 65 65 62 64
9 | 9 23 9 8 33 5 17 15 10 25 5 | 24 37 29 23 25 27 28 30 32 27 26
10E | 15 26 10 11 44 15 24 36 17 30 7 | 31 39 36 31 40 34 41 38 39 37 31
11 | 6 16 7 11 88 7 15 12 13 23 4 | 39 43 40 39 60 39 40 41 40 32 37
12 | 6 19 9 11 32 7 23 17 9 20 5 | 30 38 31 24 46 30 41 31 33 33 30
13 | 6 22 7 12 25 7 17 10 12 21 4 | 24 36 26 29 46 27 33 25 27 24 25
X14 | 9 24 10 8 38 8 21 11 13 --- 5 | 8 22 7 4 15 10 19 6 9 --- 11
15 | 7 23 9 9 31 6 22 14 9 29 5 | 28 36 28 24 44 28 33 30 29 27 27
16 | 6 25 6 10 25 5 24 14 14 27 5 | 27 41 28 23 49 28 38 28 36 32 28
17 | 8 12 10 10 87 4 14 10 13 46 5 | 34 37 39 38 53 37 34 38 41 47 37
18E | 10 15 9 10 39 6 24 20 12 19 5 | 35 38 37 31 48 32 37 27 33 29 34
19 | 4 11 5 8 83 6 11 8 10 27 3 | 39 41 40 40 82 41 35 45 37 40 39
20E | 8 20 7 8 39 6 22 9 16 13 4 | 56 61 56 56 70 56 62 57 58 62 57
21 | 8 19 8 11 32 7 21 9 10 26 4 | 24 37 28 23 39 24 36 23 22 27 24
22E | 9 17 6 8 30 6 24 6 8 15 4 | 24 29 27 21 36 26 31 26 27 28 25
23 | 6 25 8 13 24 8 20 9 13 15 5 | 23 38 25 28 42 27 33 25 27 26 25
24 | 5 15 6 8 41 7 7 12 7 11 3 | 30 37 40 34 32 35 33 32 36 29 34
25 | 7 15 6 11 34 7 13 17 11 16 4 | 22 31 23 25 34 24 30 27 28 25 24
26 | 6 12 8 10 19 4 12 12 11 23 4 | 31 31 32 29 35 32 28 34 38 28 31
27 | 9 16 10 9 32 5 14 21 11 18 5 | 20 29 18 20 29 20 26 30 23 23 20
28 | 9 20 10 8 44 6 19 11 10 27 5 | 23 35 25 18 42 22 31 21 18 29 21
29 | 7 12 5 7 36 5 11 16 9 29 4 | 31 34 34 33 35 34 31 35 32 28 31
30 | 5 16 7 8 21 8 13 19 10 17 4 | 20 31 24 18 34 23 28 22 26 23 21
31 | 9 18 6 8 26 6 15 14 11 16 4 | 29 40 33 30 40 31 35 34 32 27 31
32E | 9 26 10 10 84 7 13 12 23 21 5 | 25 31 29 20 41 26 32 25 33 25 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 10 48 7 17 15 12 24 |T 30 37 32 30 43 33 34 31 33 32 30
WRMS | 7 18 8 10 43 7 15 11 10 22 |NE 27 35 30 28 41 32 31 30 31 31 28
MEDI | 7 17 8 9 36 6 15 12 11 23 |MD 29 37 29 29 41 30 33 30 33 29 29
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 4.1510 GPS week: 1510 MJD: 54814.0-54820.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 |U 8 8 21 |U 57 61 286 |U 11 9 20 |
emr | emr 2953 | 11 10 24 | 54 53 244 | 16 12 27 |
esa | esa 2962 | 9 9 22 |U 54 52 252 | 12 9 22 |
gfz | gfz 2938 |U 11 10 23 |U 52 55 249 | 18 11 31 |
igr | igr 2954 | 9 9 21 | 53 51 248 | 12 9 23 |
igs | igs 2943 | 9 8 20 | 55 53 257 | 13 9 26 |
jpl | jpl 2882 |U 12 10 23 |U 37 49 143 | 13 11 28 |
mit | mit 2962 |U 9 10 23 |U 51 55 257 |U 16 10 27 |
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 5.1510.0 GPS week: 1510 Day: 0 MJD: 54814.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 8 8 19 | 16 14 70 | 10 8 25 |
emr | emr 2964 | 14 10 24 | 20 15 75 | 11 10 31 |
esa | esa 2976 | 10 6 20 | 15 13 73 | 11 8 27 |
gfz | gfz 2945 | 14 9 21 | 15 17 76 | 22 9 39 |
igr | igr 2946 | 9 7 19 | 15 13 72 | 12 8 33 |
igs | igs 2880 | 11 6 18 | 15 14 71 | 10 8 31 |
jpl | jpl 2961 | 14 9 20 | 16 17 79 | 11 7 30 |
mit | mit 2976 | 12 8 19 | 17 16 74 | 12 9 31 |
Table 5.1510.1 GPS week: 1510 Day: 1 MJD: 54815.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 7 25 | ---- ---- ---- | 10 9 23 |
emr | emr 2964 | 12 10 27 | ---- ---- ---- | 15 11 27 |
esa | esa 2976 | 11 10 25 | ---- ---- ---- | 12 9 24 |
gfz | gfz 2947 | 14 12 29 | ---- ---- ---- | 19 10 31 |
igr | igr 2959 | 11 10 26 | ---- ---- ---- | 11 9 23 |
igs | igs 2973 | 9 8 22 | ---- ---- ---- | 12 8 26 |
jpl | jpl 2962 | 12 7 24 | ---- ---- ---- | 13 10 26 |
mit | mit 2976 | 9 9 19 | ---- ---- ---- | 13 8 26 |
Table 5.1510.2 GPS week: 1510 Day: 2 MJD: 54816.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 9 9 20 | 12 17 42 | 11 9 19 |
emr | emr 2968 | 14 13 32 | 15 19 54 | 17 11 22 |
esa | esa 2976 | 10 11 20 | 12 18 37 | 13 9 19 |
gfz | gfz 2952 | 13 15 27 | 11 22 39 | 17 10 28 |
igr | igr 2974 | 10 11 20 | 12 20 40 | 12 7 21 |
igs | igs 2969 | 10 11 21 | 14 18 38 | 13 9 23 |
jpl | jpl 2869 | 12 12 27 | 14 21 46 | 13 10 23 |
mit | mit 2976 | 10 12 22 | 12 18 43 | 24 13 32 |
Table 5.1510.3 GPS week: 1510 Day: 3 MJD: 54817.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 7 23 | 230 238 1223 | 12 12 19 |
emr | emr 2968 | 12 11 25 | 249 233 1203 | 18 14 21 |
esa | esa 2976 | 8 9 23 | 258 239 1292 | 13 11 21 |
gfz | gfz 2952 | 10 10 20 | 245 255 1221 | 18 12 30 |
igr | igr 2976 | 8 8 24 | 251 237 1258 | 13 11 19 |
igs | igs 2973 | 8 8 26 | 262 241 1314 | 17 11 26 |
jpl | jpl 2774 | 11 13 25 | 150 209 600 | 15 16 29 |
mit | mit 2976 | 8 10 28 | 238 248 1286 | 24 14 31 |
Table 5.1510.4 GPS week: 1510 Day: 4 MJD: 54818.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 | 7 6 16 | 11 12 45 | 11 10 19 |
emr | emr 2968 | 9 6 19 | 12 14 46 | 16 13 30 |
esa | esa 2976 | 7 5 16 | 12 10 41 | 13 9 22 |
gfz | gfz 2958 | 7 6 19 | 14 9 58 | 15 11 30 |
igr | igr 2974 | 7 5 16 | 11 11 41 | 12 9 21 |
igs | igs 2974 | 7 4 15 | 11 11 47 | 11 9 26 |
jpl | jpl 2775 | 10 11 19 | 11 14 41 | 14 11 33 |
mit | mit 2976 | 7 5 23 | 11 12 44 | 12 11 27 |
Table 5.1510.5 GPS week: 1510 Day: 5 MJD: 54819.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
emr | emr 2872 | 12 11 22 | 10 15 29 | 18 12 41 |
esa | esa 2880 | 10 10 25 | 10 13 24 | 13 8 23 |
gfz | gfz 2860 | 11 10 25 | 9 12 36 | 17 11 34 |
igr | igr 2878 | 11 13 24 | 9 12 27 | 12 8 23 |
igs | igs 2863 | 10 8 18 | 9 12 25 | 13 7 31 |
jpl | jpl 2869 | 12 9 21 | 10 14 30 | 12 10 31 |
mit | mit 2880 | 12 13 28 | 9 13 31 | 12 6 27 |
Table 5.1510.6 GPS week: 1510 Day: 6 MJD: 54820.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 9 21 | 17 22 49 | 13 9 19 |
emr | emr 2968 | 8 10 21 | 20 19 56 | 15 12 19 |
esa | esa 2976 | 7 10 24 | 17 17 48 | 12 9 20 |
gfz | gfz 2957 | 7 11 21 | 18 19 62 | 15 12 24 |
igr | igr 2974 | 7 10 20 | 18 16 53 | 12 9 19 |
igs | igs 2973 | 7 9 20 | 18 19 48 | 13 10 20 |
jpl | jpl 2966 | 11 11 25 | 19 19 64 | 14 13 25 |
mit | mit 2976 | 7 11 21 | 18 22 65 | 14 12 19 |
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 6.1510 GPS week: 1510 MJD: 54814.500-54820.500
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 | 21 3 15 168 3 | -4 19
| 25 15 111 112 10 | 3
emr uuuuu | 5 1 -180 -76 -1 | 39 45
| 28 25 132 134 13 | 3
esa uuuuu | -37 20 -15 -116 1 | -15 25
| 25 19 66 50 11 | 2
gfz uuuuu | 29 3 61 95 -5 | -1 19
| 14 12 78 110 8 | 3
grg xxxxx | -16 -31 51 221 -6 | -3 30
| 45 27 86 141 45 | 2
igr xxxxx | -23 21 71 19 -5 | -3 16
| 23 8 88 79 7 | 3
irf xxxxx | -1 6 15 27 8 | -9 21
| 6 7 53 29 10 | 2
jpl uuuuu | 29 15 97 187 -3 | 8 21
| 31 24 196 128 9 | 2
mit uuuuu | -11 -3 -73 -101 -1 | -3 22
| 12 20 139 197 16 | 2
ngs uuuuu | 11 7 52 71 8 | -3 20
| 33 38 133 94 19 | 3
sio uuxxu | 10 -116 39 179 1 | -8 26
| 26 17 106 112 18 | 2
Table 7.1510.0 GPS week: 1510 Day: 0 MJD: 54814.500
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 | 61 -22 -102 268 12 | -8 20
emr uuuuu | 24 -2 -208 -304 -16 | 42 48
esa uuuuu | -65 33 -4 -125 16 | -13 24
gfz uuuuu | 48 -9 -34 209 10 | -2 21
grg xxxxx | 9 -59 161 475 -86 | 1 14
igr xxxxx | 10 23 208 96 8 | -2 16
irf xxxxx | 2 6 -86 -13 -5 | -10 21
jpl uuuuu | 20 -3 416 291 -6 | 6 21
mit uuuuu | 2 35 -374 -322 -23 | -1 19
ngs uuuuu | 2 -9 191 116 23 | -7 18
sio uuxxu | 40 -143 18 341 -25 | -7 26
Table 7.1510.1 GPS week: 1510 Day: 1 MJD: 54815.500
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 | 49 -6 186 283 9 | -7 19
emr uuuuu | -9 24 -310 -197 -17 | 41 47
esa uuuuu | -78 -6 -90 -127 -6 | -13 24
gfz uuuuu | 48 -5 173 208 1 | 0 20
grg xxxxx | 36 21 61 283 32 | -7 33
igr xxxxx | -52 27 8 7 -9 | -2 16
irf xxxxx | 1 -5 69 19 -4 | -10 21
jpl uuuuu | 79 38 204 304 0 | 6 21
mit uuuuu | 3 -30 1 -257 -21 | -2 21
ngs uuuuu | 13 57 -38 140 31 | -6 19
sio uuxxu | 23 -108 147 275 -19 | -8 27
Table 7.1510.2 GPS week: 1510 Day: 2 MJD: 54816.500
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 | 25 7 125 254 4 | -5 19
emr uuuuu | 52 29 -223 -108 -2 | 39 45
esa uuuuu | -26 -3 21 -70 -11 | -14 25
gfz uuuuu | 34 10 150 130 -8 | 0 20
grg xxxxx | -14 -24 -24 171 10 | -3 33
igr xxxxx | -48 28 -59 -21 -12 | -2 17
irf xxxxx | 7 2 59 0 4 | -11 21
jpl uuuuu | 26 -1 -109 113 0 | 7 21
mit uuuuu | -19 -4 27 -255 -9 | -4 22
ngs uuuuu | -37 22 -87 211 28 | -3 20
sio uuxxu | 30 -98 177 262 -9 | -9 28
Table 7.1510.3 GPS week: 1510 Day: 3 MJD: 54817.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 10 22 -12 192 15 | -3 17
emr uuuuu | 14 -27 79 -14 20 | 39 46
esa uuuuu | -9 32 15 -134 4 | -15 25
gfz uuuuu | 14 -2 72 119 -9 | 1 19
grg xxxxx | -60 -58 -25 202 -23 | -2 33
igr xxxxx | -24 8 110 45 -2 | -2 16
irf xxxxx | -1 10 27 23 18 | -9 20
jpl uuuuu | 53 34 -65 340 -3 | 10 20
mit uuuuu | -20 -12 -36 -153 16 | -4 22
ngs uuuuu | -24 5 -70 46 -18 | 2 20
sio uuxxu | 20 -99 -113 133 17 | -7 26
Table 7.1510.4 GPS week: 1510 Day: 4 MJD: 54818.500
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 | 4 1 -65 19 2 | 2 19
emr uuuuu | -7 -33 -158 -13 1 | 41 49
esa uuuuu | -33 19 92 -44 10 | -14 25
gfz uuuuu | 22 13 58 -13 -4 | 2 19
grg xxxxx | -40 -36 -16 157 27 | -4 33
igr xxxxx | -30 18 88 110 -10 | -1 16
irf xxxxx | 2 4 36 45 16 | -5 22
jpl uuuuu | 12 -14 -57 183 -21 | 12 22
mit uuuuu | -4 -10 -41 -31 7 | 0 24
ngs uuuuu | 23 42 -10 15 2 | 2 20
sio uuxxu | -3 -121 -2 83 15 | -4 27
Table 7.1510.5 GPS week: 1510 Day: 5 MJD: 54819.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -6 18 56 138 -11 | -2 17
emr uuuuu | -2 -5 -137 37 3 | 36 41
esa uuuuu | -24 47 -55 -200 3 | -17 25
gfz uuuuu | 21 23 -7 97 -12 | -3 14
grg xxxxx | -77 -31 21 13 35 | -3 33
igr xxxxx | -21 28 21 22 -7 | -6 15
irf xxxxx | -11 19 15 40 14 | -8 20
jpl uuuuu | -17 2 44 14 8 | 6 19
mit uuuuu | -9 -6 9 140 9 | -5 21
ngs uuuuu | 49 -53 148 -79 -7 | -1 19
sio uuxxu | -37 -110 -51 59 15 | -9 23
Table 7.1510.6 GPS week: 1510 Day: 6 MJD: 54820.500
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 | 4 1 -83 22 -8 | -5 21
emr uuuuu | -36 22 -307 62 9 | 33 39
esa uuuuu | -27 18 -87 -114 -11 | -18 26
gfz uuuuu | 16 -7 14 -88 -15 | -7 19
grg xxxxx | 35 -29 176 244 -36 | -1 33
igr xxxxx | 2 11 121 -125 -6 | -8 19
irf xxxxx | -9 7 -18 72 12 | -8 20
jpl uuuuu | 32 46 246 62 3 | 7 19
mit uuuuu | -29 3 -100 166 13 | -6 22
ngs uuuuu | 50 -17 230 43 -4 | -3 21
sio uuxxu | -3 -132 94 96 13 | -10 24
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