[IGSREPORT-17641] Wk 1540 IGS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 30 04:50:37 PDT 2009
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IGS Electronic Report 30 Jul 04:51:00 PDT 2009 Message Number 17641
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Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1540 (Jul 12, 2009 - Jul 18, 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:
igs1540[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1540[0-6].clk IGS GPS satellite and station clocks in SP3 format.
igs1540[0-6].cls IGS GPS clock combination summary report.
igs15407.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15407.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 | COD | 30 30 ONSA SCH2
0 | EMR | MIZU NLIB WTZR WUHN
0 | ESA | 21 UNSA
0 | GFZ | 12 30 PERT TWTF YELL
0 | GRG | POTS USNO
0 | MIT | TWTF TWTF
1 | EMR | TWTF WTZR TWTF WTZR
1 | ESA | 30 ALGO
1 | GFZ | 16 29 ALGO BOGT CONZ NYA1 RIO2 UNSA WHIT
1 | GRG | ONSA
1 | JPL | 32 TWTF
1 | MIT | USNO MAW1 TWTF USNO
1 | NGS | 1
2 | ALL | 1 1
2 | EMR | 16 WTZR KERG WTZR
2 | ESA | 30 KERG STJO
2 | GFZ | 12 CHUR FAA1 IRKT NLIB NYAL UNSA VILL
2 | GRG | USNO
2 | JPL | 32
3 | COD | 30 WTZR
3 | EMR | MIZU
3 | ESA | 30 RAMO
3 | GFZ | ANKR CHUR NANO NISU NYAL UNSA
3 | GRG | DAV1 ONSA
3 | JPL | 32
3 | MIT | TWTF NISU TWTF
3 | NGS | 1
4 | COD | 30 30
4 | EMR | WTZR WTZR
4 | ESA | 30
4 | GFZ | 16 HARB KOUR MDO1 NYA1
4 | GRG | ONSA
4 | JPL | 32
4 | MIT | GODE KHAJ
4 | NGS | 1
5 | COD | 30 30
5 | EMR | WTZR
5 | ESA | 30
5 | GFZ | 12 NYA1 SFER
5 | GRG | ONSA SYOG
5 | JPL | 32
5 | MIT | TSKB
6 | COD | 30 30 RCMN
6 | EMR | MIZU WTZR
6 | ESA | 30
6 | GFZ | 12 16 BRFT CHUR FAA1 MAS1 NYA1
6 | GRG | ONSA
6 | JPL | 32 DAV1
6 | MIT | IRKT
6 | NGS | 1
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
6 | MIT | ~00:00 | ~ -0.40 ns
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 | .4 .7 1.3 5 -8 5 -.32
EMR | 8.5 -12.8 -7.4 72 -6 41 -.15
ESA | 5.6 .5 2.7 71 -87 24 .11
GFZ | .1 .7 1.6 16 -5 7 -.36
GRG | 6.2 1.3 3.7 -7 14 8 .05
JPL | 4.5 -1.8 1.2 -11 2 -13 -.01
MIT | 7.0 -6.0 7.1 4 20 -2 -.23
NGS | 11.5 -3.3 7.7 -26 -136 -35 -.36
SIO | 2.9 -6.5 -16.4 -118 -103 6 .08
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 1.1540.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1540.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 2.1540.[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 3.1540.[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 5.1540.0-6).
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 1540 summary. (Jul 12, 2009 - Jul 18, 2009)
Table 1.1540.a GPS week: 1540 MJD: 55024.000-55030.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -1 16 -46 -3 -.12 7 7 | -422 -267 15 66
| 0 0 1 23 15 22 .01 | 581 782
emr 79| 1 -2 -2 -140 -6 -20 .39 17 17 | 1865 -184 17 91
| 0 1 1 40 12 10 .04 | 1079 1603
esa 129| 0 0 4 -83 45 36 .37 9 9 | -1731 1823 17 101
| 1 0 0 17 32 28 .03 | 1148 2606
gfz 184| 0 0 1 -36 -66 -15 -.06 8 8 | 36 331 22 118
| 0 0 1 49 51 5 .03 | 389 716
grg 107| 4 -1 -2 18 -32 -36 1.12 32 31 | 173 -80 78 220
| 1 0 1 25 25 54 .04 | 301 536
igr n/a| 0 0 0 24 -48 -60 .06 5 5 | 29460 93 17 66
| 0 1 0 29 16 14 .01 | 1285 1677
jpl 124| 0 0 -8 40 -66 31 .57 17 16 | 990 -237 17 94
| 1 1 2 31 14 30 .03 | 1209 1659
mit 257| 0 0 0 -9 -112 6 -.28 11 9 | -13056 -247 20 141
| 0 0 1 31 41 14 .02 | 5680 548
ngs 217| 0 0 0 95 228 -22 -.28 10 9 | 11932 1433 2153 3854
| 0 0 1 49 51 18 .02 | 5839 2231
sio 251| -3 1 -1 257 131 -21 -.18 22 21 | --- --- --- ---
| 1 1 2 26 27 19 .04 | --- ---
Table 1.1540.b GPS week : 1540 MJD: 55024.000-55030.000
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 | 11 10 16 13 18 0 16 |
2 | 4 4 4 4 4 4 4 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 4 4 4 4 5 |
6 | 3 3 4 3 3 3 4 |
7 | 5 5 5 5 6 5 6 |
8 | 4 3 4 3 3 4 3 |
9 | 3 3 4 4 4 4 3 |
10 | 4 4 5 4 4 4 4 |
11 | 5 5 5 5 5 5 5 |
12 | 5 5 5 5 5 4 5 |
13 | 4 4 5 5 5 5 5 |
14 | 4 4 4 4 4 3 4 |
15 | 4 5 4 4 5 5 6 |
16 | 4 4 5 5 5 5 5 |
17 | 5 5 6 5 5 6 6 |
18 | 4 4 5 4 5 4 4 |
19 | 5 4 5 5 4 4 4 |
20 | 4 4 4 4 4 4 5 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 3 3 4 3 3 3 4 |
25 | 4 3 4 4 4 4 4 |
26 | 4 4 5 4 4 4 4 |
27 | 3 3 4 4 4 4 3 |
28 | 5 4 5 5 6 5 5 |
29 | 5 5 6 4 5 5 5 |
30 | 9 7 6 5 5 5 5 |
31 | 5 4 5 5 5 5 5 |
32 | 5 5 5 5 5 5 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1540.0 GPS week: 1540 Day: 0 MJD: 55024.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -1 13 -40 -19 -.14 7 7 | -691 -92 13 66
| 33 -24 |
emr 79| 0 0 -3 -143 -7 -14 .41 17 17 | 3953 -2828 23 103
| 28 -46 |
esa 129| 0 0 4 -85 88 78 .36 9 9 | -1692 933 21 111
| 46 26 |
gfz 184| 0 1 1 -38 -83 -18 -.04 8 8 | -322 1557 23 144
| -28 -68 |
grg 107| 2 0 0 -5 -51 -14 1.15 29 29 | 289 -543 83 254
| 61 -4 |
igr n/a| 0 1 0 33 -45 -49 .05 5 5 | 31082 -2771 20 78
| 3 -24 |
jpl 124| 1 0 -10 23 -57 -3 .57 18 17 | 3346 -3069 19 114
| 49 71 |
mit 257| 0 0 2 8 -162 -7 -.26 13 10 | -14412 -923 22 158
| 23 32 |
ngs 217| 0 0 1 96 220 -10 -.27 9 8 | 13569 2680 2563 4026
| -87 -81 |
sio 251| -4 0 -5 268 86 -27 -.22 24 22 | --- --- --- ---
| -149 -66 |
Table 2.1540.1 GPS week: 1540 Day: 1 MJD: 55025.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -1 28 -60 -6 -.11 7 7 | -1291 1007 15 54
| -31 -13 |
emr 79| 1 -4 -3 -126 0 -35 .45 16 16 | 991 1581 18 86
| 4 -53 |
esa 129| 1 0 4 -104 78 31 .35 8 8 | -3916 6515 17 99
| 21 -11 |
gfz 184| -1 1 0 -37 -24 -19 -.04 8 8 | -379 617 21 89
| -31 -48 |
grg 107| 4 0 -2 39 -50 -12 1.05 32 32 | -316 710 82 213
| -2 48 |
igr n/a| 0 0 0 48 -65 -46 .05 5 5 | 28194 1433 16 59
| -5 1 |
jpl 124| 0 -1 -10 79 -59 81 .61 19 17 | 208 1336 16 90
| -30 -21 |
mit 257| 0 -1 1 -34 -144 0 -.29 10 8 | -15814 44 21 122
| 25 32 |
ngs 217| 0 0 1 119 171 -8 -.28 8 6 | 12416 3622 1933 3782
| -67 -28 |
sio 251| -4 0 -3 228 121 -53 -.24 22 20 | --- --- --- ---
| -135 -84 |
Table 2.1540.2 GPS week: 1540 Day: 2 MJD: 55026.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 1 0 -1 1 -73 34 -.12 8 7 | -158 -556 14 61
| 31 17 |
emr 79| 1 -4 -1 -141 -5 -20 .40 17 17 | 1894 -1302 16 84
| -1 -69 |
esa 129| -1 1 4 -96 47 -8 .39 10 10 | -2006 1826 18 104
| 8 -3 |
gfz 184| 0 0 3 -12 26 -7 -.11 9 9 | -159 574 24 163
| 8 -61 |
grg 107| 4 0 -2 -15 -24 -24 1.12 33 33 | 222 -149 81 231
| 54 80 |
igr n/a| 0 2 0 5 -73 -86 .07 5 5 | 28989 -1219 18 71
| -18 6 |
jpl 124| 0 -1 -8 20 -91 15 .60 18 18 | 993 -1462 18 92
| -25 -23 |
mit 257| 0 0 0 29 -122 -12 -.28 11 10 | -15773 -115 18 126
| 10 10 |
ngs 217| 0 0 0 42 162 -8 -.24 11 9 | 12497 3832 2075 3973
| -44 2 |
sio 251| -3 1 -3 286 112 -35 -.19 22 22 | --- --- --- ---
| -147 -71 |
Table 2.1540.3 GPS week: 1540 Day: 3 MJD: 55027.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -2 44 -48 -27 -.14 7 6 | -342 -635 18 94
| -37 -12 |
emr 79| 0 -1 -2 -159 -14 -15 .37 17 17 | 1328 202 17 84
| 35 -48 |
esa 129| -1 0 3 -59 50 20 .35 7 7 | -1727 2816 16 99
| 8 42 |
gfz 184| 1 0 2 -76 -86 -12 -.05 8 8 | 110 232 24 136
| -2 -55 |
grg 107| 3 -2 -1 27 -1 -66 1.08 32 32 | 302 -144 77 204
| -50 -34 |
igr n/a| 0 0 0 41 -29 -64 .05 5 5 | 28454 530 18 70
| -17 -41 |
jpl 124| 0 -1 -8 75 -49 58 .57 17 15 | 308 57 17 98
| -29 68 |
mit 257| 0 0 0 -41 -137 14 -.30 10 8 | -15275 -40 23 164
| 13 22 |
ngs 217| 0 1 3 113 275 -13 -.27 11 10 | 14927 -575 2007 3655
| 1 -56 |
sio 251| -4 0 -2 231 139 -9 -.16 20 21 | --- --- --- ---
| -153 -84 |
Table 2.1540.4 GPS week: 1540 Day: 4 MJD: 55028.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 0 -18 -37 14 -.11 8 8 | 465 -1309 14 59
| 50 12 |
emr 79| 2 -4 0 -205 9 -25 .33 18 18 | 1175 243 19 89
| 47 -76 |
esa 129| 1 0 2 -86 -4 40 .41 9 9 | -1251 -636 17 108
| 15 67 |
gfz 184| 0 0 0 42 -105 -24 -.10 9 9 | 780 -800 23 103
| -27 -52 |
grg 107| 7 -1 -1 8 -70 -138 1.14 34 32 | 420 -459 73 211
| 108 16 |
igr n/a| 0 0 0 -16 -47 -49 .06 5 5 | 28709 869 18 62
| 19 -2 |
jpl 124| -3 2 -5 -5 -80 6 .54 17 15 | 72 391 18 98
| 32 22 |
mit 257| 0 0 0 22 -88 13 -.30 11 9 | -15382 -556 21 132
| 3 14 |
ngs 217| -1 0 -2 35 258 -17 -.29 10 9 | 16796 -2059 2371 3779
| 5 -84 |
sio 251| -2 2 -1 288 145 -27 -.16 21 20 | --- --- --- ---
| -162 -74 |
Table 2.1540.5 GPS week: 1540 Day: 5 MJD: 55029.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 1 -1 0 2 -31 3 -.12 7 7 | -877 442 15 65
| 9 -9 |
emr 79| 0 0 -2 -136 2 -30 .36 17 17 | 1113 1642 16 95
| -8 -40 |
esa 129| 0 0 2 -91 33 27 .34 9 9 | -70 -1368 19 101
| 62 45 |
gfz 184| 0 0 3 -15 -127 -13 -.03 9 9 | 140 149 24 101
| -14 -54 |
grg 107| 2 0 -5 17 -6 38 1.11 33 31 | -176 610 78 222
| 29 -8 |
igr n/a| -1 0 1 -1 -45 -54 .08 5 5 | 29371 2142 18 64
| 9 8 |
jpl 124| -1 2 -6 30 -65 22 .58 17 15 | 193 1734 18 87
| -15 28 |
mit 257| 0 0 -1 -1 -91 15 -.27 9 8 | -236 651 17 140
| 13 23 |
ngs 217| 0 0 0 83 297 -39 -.29 11 10 | -861 400 2191 4170
| -67 -69 |
sio 251| -1 2 0 271 146 0 -.14 21 19 | --- --- --- ---
| -163 -78 |
Table 2.1540.6 GPS week: 1540 Day: 6 MJD: 55030.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 0 42 -36 -20 -.11 7 7 | -62 -726 16 67
| -6 -6 |
emr 79| 1 -2 -2 -69 -27 -4 .39 16 16 | 2602 -828 16 96
| -40 -25 |
esa 129| 0 2 4 -61 22 64 .37 10 10 | -1457 2679 16 91
| 31 49 |
gfz 184| 0 0 2 -114 -67 -14 -.06 8 8 | 88 -9 21 94
| -6 -30 |
grg 107| 4 -2 -2 57 -26 -35 1.18 31 28 | 474 -588 72 205
| -59 19 |
igr n/a| -1 -1 0 64 -30 -72 .06 6 6 | 31427 -328 17 59
| -15 -15 |
jpl 124| 0 0 -6 55 -60 36 .56 17 15 | 1812 -652 16 85
| -20 -5 |
mit 257| 0 0 -1 -49 -40 25 -.28 10 9 | -14506 -796 24 149
| 39 12 |
ngs 217| 0 0 0 180 216 -56 -.29 11 10 | 14183 2133 1937 3596
| -112 -41 |
sio 251| -1 2 1 231 170 0 -.17 23 20 | --- --- --- ---
| -131 -74 |
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 3.1540.0 GPS week: 1540 Day: 0 MJD: 55024.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 13 --- --- --- --- 10 --- 20 11 --- 10 | 39 --- --- --- --- 34 --- 28 38 --- 37
2 | 6 13 10 7 25 5 13 11 10 33 4 | 31 34 35 31 37 32 33 29 33 28 31
3 | 6 11 7 6 26 3 10 12 9 25 3 | 23 24 29 22 27 21 25 18 27 30 24
4 | 7 10 4 8 41 6 9 10 8 31 3 | 29 32 35 30 26 31 30 31 29 29 29
6 | 5 11 8 8 29 5 10 10 6 19 3 | 26 28 33 27 29 26 28 25 29 27 28
7 | 7 17 9 12 35 7 17 11 9 36 5 | 17 28 21 20 49 20 30 13 22 35 19
8 | 5 12 9 6 24 4 13 9 9 19 3 | 13 20 20 16 27 13 21 10 13 21 15
9 | 6 13 6 4 20 4 13 7 8 16 3 | 16 18 16 17 23 13 18 16 18 13 15
10 | 7 23 9 9 15 4 10 8 10 27 4 | 15 32 17 23 27 19 22 19 23 34 18
11 | 10 12 9 8 35 5 12 8 7 40 4 | 42 44 44 43 30 42 40 43 44 48 41
12E | 10 15 9 6 25 4 27 10 10 14 4 | 52 53 53 52 54 50 51 46 53 51 51
13 | 5 20 9 8 29 5 20 10 7 19 4 | 15 29 21 17 44 15 27 17 14 18 16
14 | 7 19 11 7 20 7 19 11 7 18 4 | 16 27 26 18 39 19 26 18 20 26 20
15 | 6 19 11 9 32 3 18 10 10 15 4 | 17 25 19 18 30 17 22 17 19 18 16
16E | 6 16 9 7 28 4 26 9 10 12 4 | 37 45 47 40 56 39 44 37 43 39 41
17 | 8 18 8 7 47 5 23 12 9 33 4 | 22 36 27 20 54 23 41 22 21 20 23
18 | 6 19 7 7 24 3 20 8 7 24 4 | 19 27 24 17 39 18 32 17 16 22 18
19 | 8 19 8 9 39 5 22 12 9 23 4 | 20 30 26 20 36 19 34 15 23 18 22
20 | 6 17 9 7 21 5 19 8 11 14 4 | 16 21 15 13 33 16 24 15 21 16 14
21 | 6 14 10 6 36 5 16 9 6 28 4 | 29 30 27 29 44 27 31 28 30 37 28
22 | 5 16 8 6 23 5 15 14 7 19 3 | 12 23 23 13 40 14 26 15 15 17 15
23 | 6 24 8 7 31 3 22 10 10 21 4 | 13 34 19 15 37 15 28 17 20 19 17
24 | 6 11 6 4 25 6 11 8 8 24 3 | 26 26 26 28 33 25 20 28 28 24 26
25 | 5 12 8 6 --- 3 12 11 7 21 3 | 17 22 28 20 --- 16 24 14 20 20 20
26 | 7 16 5 9 13 3 13 10 7 26 4 | 16 22 19 22 25 16 19 20 18 27 17
27 | 5 14 7 6 24 4 13 9 7 14 3 | 13 19 16 18 27 13 19 17 18 14 14
28E | 6 17 7 9 23 5 24 12 10 21 4 | 48 57 52 48 61 49 54 48 47 49 49
29 | 8 19 9 6 33 5 25 9 9 32 5 | 21 38 30 24 45 22 42 20 22 29 24
30E | 13 26 12 14 35 7 24 45 15 22 8 | 30 38 33 30 44 30 42 47 39 35 31
31 | 6 24 11 8 29 8 20 8 11 22 4 | 11 33 21 16 41 15 30 11 14 19 15
32 | 8 20 9 13 30 4 20 13 11 25 5 | 12 26 13 20 26 12 23 15 16 22 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 9 8 29 5 18 13 9 24 |T 23 30 27 24 37 23 30 23 25 26 24
WRMS | 7 17 9 8 29 5 17 10 8 22 |NE 19 28 24 21 34 19 27 19 22 24 20
MEDI | 6 16 9 7 28 5 17 10 9 22 |MD 19 28 26 20 37 19 28 18 22 24 20
Table 3.1540.1 GPS week: 1540 Day: 1 MJD: 55025.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 10 --- --- --- --- 13 --- 14 17 --- 10 | 24 --- --- --- --- 30 --- 25 29 --- 23
2 | 5 14 8 6 25 5 18 5 8 30 3 | 21 24 20 22 29 20 21 17 21 16 17
3 | 6 12 6 8 33 4 13 7 7 23 3 | 18 23 19 19 27 19 22 19 19 25 18
4 | 7 8 8 9 37 4 10 7 10 26 3 | 25 25 26 25 29 24 28 24 24 27 23
6 | 5 10 7 6 31 4 13 7 7 18 3 | 23 27 25 26 35 25 24 26 24 27 24
7 | 8 16 11 11 31 5 19 8 9 37 5 | 13 26 17 15 34 14 26 15 14 38 11
8 | 5 14 8 6 25 4 12 9 7 19 3 | 14 21 17 14 24 14 23 14 16 22 12
9 | 5 15 3 5 24 4 11 7 9 14 3 | 15 22 16 18 25 15 18 16 19 15 15
10 | 8 15 7 7 20 6 12 7 11 22 3 | 15 26 18 16 23 15 23 17 15 28 14
11 | 11 10 8 5 37 5 16 9 7 40 4 | 24 29 30 26 23 26 27 25 28 36 25
12E | 14 18 11 9 35 11 28 7 7 13 4 | 43 44 49 45 46 51 51 45 43 45 44
13 | 6 19 7 7 36 2 20 12 6 14 4 | 16 30 18 16 41 16 27 16 17 18 14
14 | 8 18 9 5 24 5 15 10 11 17 4 | 11 25 20 15 36 13 23 14 15 19 13
15 | 9 15 9 15 33 6 20 7 11 15 4 | 19 25 22 25 32 19 24 19 19 20 18
16E | 6 13 9 7 35 4 27 8 8 7 4 | 29 35 39 34 49 33 36 33 31 31 32
17 | 7 19 8 7 41 6 23 13 11 32 5 | 22 36 26 23 56 23 40 21 21 16 22
18 | 6 21 8 9 24 5 21 6 6 22 4 | 18 31 22 19 39 20 31 19 19 21 19
19 | 6 17 7 7 39 4 23 8 10 22 4 | 16 25 19 14 34 14 29 13 15 15 14
20 | 8 17 11 8 19 4 18 10 8 12 4 | 12 21 17 16 27 14 23 13 15 17 12
21 | 5 12 8 5 25 5 16 6 7 28 3 | 18 23 18 21 26 17 22 18 21 25 18
22 | 6 18 7 7 28 5 18 8 6 17 3 | 12 25 21 14 38 15 28 16 12 14 14
23 | 7 25 9 7 42 4 24 11 7 16 4 | 14 30 18 12 35 14 28 14 14 16 13
24 | 5 7 5 7 28 6 11 8 8 18 3 | 19 18 18 24 27 18 13 19 25 17 19
25 | 6 13 7 5 --- 4 11 6 7 21 3 | 15 18 15 14 --- 15 18 18 14 18 12
26 | 5 16 7 5 18 4 11 8 6 26 3 | 25 29 30 25 41 26 30 28 25 35 27
27 | 5 13 4 4 30 4 10 7 9 14 3 | 17 22 17 21 30 16 21 18 19 17 17
28E | 6 15 7 7 26 5 26 10 8 20 4 | 50 52 52 50 62 51 59 52 51 55 51
29 | 8 18 7 12 31 3 26 6 6 27 4 | 16 30 21 20 41 18 35 15 17 21 18
30E | 12 20 9 14 59 6 25 31 12 20 7 | 22 32 28 29 47 24 37 35 27 31 25
31 | 5 18 8 12 42 4 18 10 7 21 4 | 11 28 17 13 47 15 29 10 14 17 13
32 | 9 19 9 11 31 3 21 11 8 25 4 | 18 25 19 22 26 19 27 20 18 28 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 16 8 8 32 5 19 10 8 22 |T 19 27 23 21 35 21 28 21 21 24 19
WRMS | 7 16 8 8 32 5 17 8 6 20 |NE 17 25 20 19 33 17 25 17 18 21 16
MEDI | 6 15 8 7 31 4 18 8 8 20 |MD 18 25 19 20 34 18 27 18 19 21 18
Table 3.1540.2 GPS week: 1540 Day: 2 MJD: 55026.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 20 --- --- --- --- 23 --- 19 30 --- 16 | 21 --- --- --- --- 31 --- 38 38 --- 26
2 | 7 10 12 4 33 6 14 10 14 27 4 | 24 26 34 25 33 26 26 23 24 23 23
3 | 4 11 7 6 30 4 14 8 10 23 3 | 22 27 24 24 27 24 32 24 23 34 23
4 | 7 11 8 4 27 6 11 9 12 25 3 | 20 27 30 21 25 24 25 23 22 28 21
6 | 6 11 7 7 25 5 14 9 9 18 3 | 19 26 24 24 32 22 32 19 21 31 21
7 | 9 17 10 8 38 4 16 9 10 38 5 | 10 25 16 15 38 13 24 13 12 37 10
8 | 5 12 11 6 25 4 10 11 11 17 3 | 12 20 22 15 28 15 21 13 13 17 13
9 | 7 16 9 11 23 4 11 8 12 15 4 | 12 25 16 14 27 13 18 15 19 12 12
10 | 10 20 8 11 17 5 10 10 14 18 4 | 15 25 22 15 27 17 25 18 16 26 14
11 | 11 12 8 6 37 7 17 13 12 36 5 | 33 37 35 35 25 34 36 36 39 40 33
12E | 9 14 13 11 33 4 24 15 14 17 5 | 39 42 45 39 51 39 42 47 44 44 40
13 | 8 23 12 8 40 5 18 16 12 17 5 | 17 33 23 17 41 17 25 18 18 20 15
14 | 6 15 8 8 26 6 19 11 9 17 4 | 13 25 18 15 39 15 25 16 16 19 14
15 | 7 15 9 10 35 5 14 12 10 14 4 | 16 24 22 22 35 17 20 17 16 20 15
16E | 10 16 11 9 52 6 27 10 10 10 4 | 29 33 34 31 53 29 34 33 33 32 30
17 | 9 18 12 11 28 7 23 12 13 32 5 | 21 35 26 19 45 20 37 22 19 17 20
18 | 6 21 10 10 21 3 20 9 8 21 4 | 12 28 20 15 32 14 27 15 15 20 14
19 | 7 21 8 6 29 5 24 11 11 23 4 | 21 33 25 23 37 22 37 23 25 31 22
20 | 5 22 10 6 22 6 18 10 10 13 4 | 17 27 21 18 31 18 26 17 23 16 16
21 | 6 11 9 6 21 4 15 7 10 28 4 | 20 23 20 21 27 21 24 23 25 31 20
22 | 5 16 8 7 27 4 17 8 8 15 3 | 9 26 18 13 38 13 26 14 11 12 12
23 | 8 24 14 10 36 4 22 14 9 21 5 | 15 31 20 17 31 15 27 17 14 21 14
24 | 7 8 7 7 28 5 11 11 11 17 3 | 21 22 23 26 18 22 19 25 24 20 22
25 | 7 12 9 6 --- 3 11 7 14 21 3 | 14 18 16 14 --- 13 20 14 15 14 11
26 | 9 16 9 9 21 4 13 10 9 27 4 | 46 50 47 49 51 46 50 43 47 56 47
27 | 8 17 9 12 30 6 11 10 12 13 4 | 11 23 17 15 35 13 19 14 16 10 12
28E | 10 24 11 7 23 6 24 10 10 22 5 | 28 35 28 29 32 30 36 26 25 33 26
29 | 8 22 16 9 34 5 27 9 15 25 5 | 15 33 21 16 32 18 36 19 22 23 17
30E | 10 22 10 13 70 5 22 25 15 20 6 | 24 37 31 29 60 24 40 28 31 35 27
31 | 7 20 10 11 45 11 21 11 9 24 5 | 12 33 23 18 50 19 31 13 17 18 16
32 | 8 18 9 12 34 5 20 13 10 24 5 | 16 21 19 18 28 15 26 16 16 24 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 10 9 33 5 18 11 11 22 |T 19 29 24 21 35 21 28 22 22 25 19
WRMS | 7 17 10 9 33 5 18 10 9 22 |NE 17 27 23 20 33 19 27 19 20 23 18
MEDI | 7 16 9 8 29 5 17 10 11 21 |MD 17 27 22 18 32 19 26 19 21 23 17
Table 3.1540.3 GPS week: 1540 Day: 3 MJD: 55027.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 15 --- --- --- --- 24 --- 14 26 --- 13 | 17 --- --- --- --- 36 --- 20 41 --- 24
2 | 6 11 8 7 47 5 11 7 9 26 3 | 30 34 35 31 51 31 34 29 33 29 31
3 | 5 12 8 6 26 5 10 10 12 21 3 | 28 29 29 30 35 28 32 27 31 35 29
4 | 7 9 4 7 32 5 9 6 11 27 3 | 24 29 30 27 25 27 30 25 34 33 27
6 | 4 11 7 7 26 5 9 9 8 14 3 | 29 30 30 32 41 31 33 32 35 33 31
7 | 7 19 9 7 35 3 16 8 13 36 4 | 9 25 17 14 43 11 24 10 19 36 12
8 | 5 14 5 5 24 3 11 5 9 14 3 | 9 16 13 15 30 10 20 10 14 14 11
9 | 6 17 6 9 27 7 11 6 14 14 3 | 14 23 18 15 30 14 20 13 23 12 15
10 | 8 18 7 9 21 6 10 9 10 17 4 | 16 28 19 17 27 17 24 20 17 27 17
11 | 10 15 8 5 25 6 12 9 12 33 4 | 33 35 35 35 31 33 34 36 39 42 33
12E | 9 14 7 11 30 3 24 10 10 9 4 | 18 25 24 21 34 20 27 21 25 21 20
13 | 6 20 9 7 31 4 18 16 13 14 4 | 12 29 18 13 40 14 26 18 22 19 14
14 | 5 16 4 7 20 4 18 9 12 13 3 | 13 26 21 14 37 16 25 14 25 17 17
15 | 5 19 10 12 38 5 19 8 10 16 4 | 17 29 19 19 40 16 25 17 23 20 17
16E | 8 22 8 12 36 8 24 10 9 13 4 | 27 39 34 32 43 29 37 28 28 26 29
17 | 7 21 9 10 30 5 22 12 11 30 5 | 20 36 29 23 46 22 38 20 24 18 22
18 | 6 19 5 9 26 5 21 10 11 20 4 | 15 24 17 13 35 15 30 15 21 20 15
19 | 8 19 10 6 33 3 21 9 11 19 4 | 25 35 33 28 39 26 40 25 27 27 28
20 | 6 20 8 7 28 6 18 11 12 12 4 | 12 23 15 12 33 15 25 16 20 18 13
21 | 4 13 6 5 22 4 12 6 9 28 3 | 23 25 26 23 29 22 28 25 28 35 25
22 | 6 17 7 6 22 4 14 7 9 12 3 | 11 21 19 13 34 12 27 11 18 12 13
23 | 7 24 10 7 35 4 22 13 10 18 4 | 14 32 17 15 30 15 30 17 22 21 15
24 | 6 8 6 8 28 5 10 8 9 14 3 | 22 25 24 26 17 24 21 27 31 20 25
25 | 6 12 7 6 --- 4 11 6 12 18 3 | 10 16 17 13 --- 9 16 11 20 14 12
26 | 9 19 5 7 21 5 13 8 11 23 4 | 21 23 19 22 34 18 24 23 22 28 19
27 | 5 14 8 10 43 5 11 7 15 13 3 | 16 22 19 18 47 17 22 16 25 17 17
28E | 8 20 8 6 26 6 22 13 9 22 4 | 52 56 56 50 63 52 60 51 55 56 53
29 | 6 21 9 6 38 5 21 7 6 20 4 | 18 32 22 16 41 19 36 18 21 16 19
30E | 8 20 6 9 56 5 18 20 11 20 5 | 26 40 31 27 53 27 40 29 28 39 29
31 | 6 20 7 10 39 7 19 8 13 21 4 | 11 28 18 14 45 14 30 11 20 18 14
32 | 8 19 7 12 23 6 19 12 11 23 4 | 18 24 21 23 28 20 30 21 27 28 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 7 8 32 5 17 10 11 20 |T 19 28 24 21 37 21 29 21 26 25 21
WRMS | 6 17 7 8 32 5 15 8 10 21 |NE 18 26 22 20 35 19 27 19 24 23 19
MEDI | 6 18 7 7 28 5 16 9 11 18 |MD 18 28 21 19 35 19 28 20 25 21 19
Table 3.1540.4 GPS week: 1540 Day: 4 MJD: 55028.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 22 --- --- --- --- 23 --- 15 33 --- 17 | 26 --- --- --- --- 33 --- 26 45 --- 32
2 | 6 15 8 6 46 6 13 9 9 24 4 | 22 30 29 25 44 24 27 23 26 25 25
3 | 7 14 7 6 30 6 10 12 10 21 3 | 19 24 24 19 28 18 24 26 23 25 21
4 | 6 16 8 5 49 4 7 7 9 26 3 | 26 33 30 27 33 25 29 25 24 30 25
6 | 7 14 5 5 37 6 11 9 8 14 3 | 18 23 22 17 37 15 23 20 18 17 19
7 | 12 19 7 9 44 4 16 9 15 37 5 | 13 28 20 19 43 15 25 16 20 38 16
8 | 4 15 9 5 27 5 11 9 7 15 3 | 15 21 21 18 30 17 20 18 14 21 16
9 | 6 14 8 10 25 7 12 7 11 15 3 | 16 22 21 22 27 17 21 18 26 15 17
10 | 9 19 7 9 21 5 12 9 6 16 3 | 17 26 20 22 28 18 25 19 18 25 18
11 | 13 11 10 9 52 7 12 9 10 33 5 | 30 35 32 29 28 27 31 31 28 40 28
12E | 11 14 8 12 29 4 24 8 7 11 4 | 15 28 27 26 36 21 25 19 25 19 21
13 | 8 23 10 8 38 5 17 17 12 14 5 | 16 34 22 21 47 16 27 22 21 22 18
14 | 8 19 9 7 30 5 19 12 6 13 4 | 15 30 22 21 43 16 25 18 19 18 17
15 | 6 23 10 9 30 6 18 9 12 18 4 | 18 32 20 24 34 21 26 21 19 30 18
16E | 8 25 10 8 22 5 24 16 9 17 5 | 25 41 34 29 38 28 35 30 32 32 28
17 | 8 21 7 7 30 5 20 16 10 31 5 | 23 41 30 26 50 26 40 25 21 20 25
18 | 6 21 8 7 24 3 21 10 9 19 4 | 17 29 21 17 38 17 31 17 24 22 18
19 | 7 19 6 6 40 3 21 10 9 19 4 | 18 32 24 19 38 20 34 19 24 19 20
20 | 6 22 12 8 23 6 17 9 7 10 4 | 13 25 19 19 29 15 23 14 16 18 13
21 | 6 17 8 8 30 5 12 6 10 28 4 | 23 30 24 23 26 23 27 24 25 32 23
22 | 5 17 10 8 19 4 18 9 6 12 3 | 13 27 22 18 38 15 27 14 21 16 16
23 | 8 27 9 9 32 5 21 11 10 17 5 | 13 37 21 18 34 14 29 18 18 20 16
24 | 5 13 5 7 27 5 9 9 10 15 3 | 22 24 22 22 21 22 19 23 27 21 22
25 | 8 15 8 7 --- 3 9 7 14 19 4 | 12 23 18 17 --- 14 16 16 19 18 14
26 | 8 16 9 7 22 6 13 9 8 23 4 | 35 43 39 36 53 35 43 38 37 45 36
27 | 5 14 9 9 40 5 12 8 12 14 3 | 16 22 18 21 32 18 23 17 24 17 16
28E | 10 19 11 9 29 8 20 22 11 28 5 | 33 43 42 36 52 36 44 49 38 47 39
29 | 10 20 9 14 26 5 23 8 12 21 5 | 19 35 26 26 37 23 35 20 20 18 22
30E | 8 20 9 12 66 9 20 13 9 19 4 | 28 37 32 34 44 28 40 28 33 36 30
31 | 6 22 8 10 31 6 20 10 11 22 4 | 14 34 21 17 43 16 29 14 18 19 16
32 | 7 19 9 15 28 6 17 10 9 21 4 | 14 24 17 24 31 17 23 15 18 25 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 9 9 34 5 17 11 10 21 |T 19 30 24 23 36 20 28 22 23 25 21
WRMS | 8 18 9 9 32 5 15 9 9 20 |NE 18 29 23 21 35 19 27 20 21 23 19
MEDI | 7 19 8 8 30 5 17 9 10 19 |MD 18 30 22 22 37 18 27 20 23 21 19
Table 3.1540.5 GPS week: 1540 Day: 5 MJD: 55029.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 3 --- --- --- --- 33 --- --- --- --- 0 | 21 --- --- --- --- 24 --- --- --- --- 28
2 | 5 12 6 6 20 5 12 7 12 23 3 | 23 29 27 26 30 23 27 22 25 23 24
3 | 6 12 7 10 34 5 9 6 11 21 3 | 36 40 40 35 40 36 39 35 38 45 37
4 | 5 13 9 7 26 4 9 7 11 28 3 | 19 25 24 24 24 18 23 17 17 27 19
6 | 4 13 6 8 28 5 8 6 11 14 3 | 26 33 30 25 29 27 31 27 31 32 28
7 | 9 19 9 9 32 5 19 7 13 36 5 | 13 27 17 18 39 13 26 14 17 39 14
8 | 5 14 13 5 30 4 11 7 10 12 3 | 14 17 18 18 37 13 19 18 17 18 15
9 | 6 11 8 8 24 3 12 9 11 14 3 | 12 20 16 17 24 11 20 14 19 12 13
10 | 8 19 7 10 20 4 11 10 13 18 4 | 17 30 20 24 26 18 25 17 19 24 18
11 | 10 14 9 8 51 4 13 8 9 37 4 | 29 34 31 32 24 29 31 27 31 39 28
12E | 9 14 11 10 24 7 22 9 9 10 4 | 19 24 24 21 35 18 23 17 22 20 19
13 | 5 22 8 10 43 4 19 11 11 15 4 | 15 32 19 23 45 16 24 19 19 22 17
14 | 6 13 6 7 44 5 17 7 8 9 3 | 17 26 24 19 53 18 24 17 19 17 18
15 | 6 21 12 9 36 6 16 10 14 28 5 | 15 27 18 24 35 14 22 19 19 34 15
16E | 6 17 10 10 38 8 24 13 11 13 4 | 15 27 22 22 34 22 26 21 23 20 19
17 | 7 21 11 11 34 6 23 16 15 30 5 | 22 37 29 26 45 22 38 26 23 19 22
18 | 7 23 6 9 31 5 19 7 10 19 4 | 19 28 22 16 38 18 27 18 24 24 19
19 | 7 19 7 6 30 5 21 7 10 21 4 | 22 33 31 21 37 22 35 22 22 23 24
20 | 7 19 11 7 23 4 19 7 6 11 4 | 16 25 17 23 28 15 25 17 15 20 15
21 | 6 11 6 4 29 5 12 6 12 30 4 | 17 19 14 15 24 16 20 19 24 30 17
22 | 7 16 7 10 24 3 16 7 9 11 3 | 14 23 19 14 34 14 26 12 18 14 14
23 | 7 26 9 10 34 5 26 6 11 16 5 | 15 33 19 21 30 14 28 15 17 17 15
24 | 6 11 6 6 34 4 11 6 12 16 3 | 17 18 18 18 17 18 15 21 27 22 18
25 | 6 14 5 8 --- 3 10 6 11 18 3 | 12 19 12 19 --- 10 15 13 17 14 11
26 | 7 17 7 8 18 4 13 8 11 23 4 | 29 37 35 26 41 28 37 28 32 37 30
27 | 4 11 7 8 29 5 11 9 14 12 3 | 14 20 19 18 26 14 21 16 22 16 15
28E | 7 20 12 14 20 5 22 15 9 25 5 | 42 41 43 45 52 42 44 48 45 46 42
29 | 10 21 9 10 30 6 25 8 12 24 5 | 18 34 24 19 34 20 35 20 23 19 21
30E | 9 23 9 12 64 3 18 14 8 16 5 | 27 40 32 27 50 28 41 27 30 33 29
31 | 5 17 9 14 31 7 20 8 11 22 4 | 14 30 19 19 46 21 31 16 19 20 17
32 | 9 16 6 11 24 5 19 9 10 21 4 | 17 24 17 23 23 15 26 16 16 27 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 9 9 33 5 17 9 11 21 |T 19 28 23 22 34 19 27 20 23 25 20
WRMS | 7 17 9 9 31 5 15 8 10 19 |NE 18 27 22 21 33 18 26 19 21 24 19
MEDI | 6 16 8 9 30 5 16 7 11 18 |MD 17 27 20 21 34 18 26 18 22 22 18
Table 3.1540.6 GPS week: 1540 Day: 6 MJD: 55030.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 20 --- --- --- --- 27 --- 20 28 --- 16 | 27 --- --- --- --- 32 --- 24 28 --- 26
2 | 5 12 10 4 22 7 11 9 14 24 3 | 31 35 36 33 40 31 32 31 28 31 31
3 | 6 12 7 7 39 5 8 8 13 22 3 | 25 31 28 27 33 27 32 24 24 38 25
4 | 8 10 10 6 16 6 9 12 16 34 4 | 29 32 31 32 33 27 28 29 28 43 28
6 | 5 12 6 8 35 6 9 9 12 13 3 | 20 27 23 22 32 23 26 22 22 25 21
7 | 7 17 13 9 35 8 22 9 14 37 5 | 19 28 21 19 35 19 28 20 21 46 18
8 | 5 14 10 6 28 6 9 8 10 12 3 | 20 26 24 25 29 21 26 22 20 23 21
9 | 5 12 9 4 26 6 10 10 8 14 3 | 17 22 20 17 28 17 20 18 20 16 17
10 | 7 15 7 8 17 7 9 9 12 21 3 | 15 24 16 15 26 15 23 16 16 27 14
11 | 9 12 11 6 30 8 14 11 16 40 5 | 41 42 39 38 34 38 34 39 43 44 38
12E | 7 14 9 10 37 6 22 12 11 13 4 | 19 25 24 21 39 20 27 19 23 17 19
13 | 7 20 11 7 37 5 21 12 9 18 4 | 20 35 23 25 42 20 30 22 25 29 21
14 | 6 16 10 5 34 7 17 7 11 9 3 | 17 26 23 21 36 18 24 18 22 21 18
15 | 8 27 14 10 43 5 20 11 12 32 5 | 22 36 21 21 31 21 27 22 26 35 21
16E | 6 21 9 11 25 5 24 13 12 11 4 | 22 31 27 21 33 22 32 22 26 24 23
17 | 10 19 11 11 29 9 23 17 12 30 5 | 20 35 24 21 49 22 39 21 19 21 20
18 | 6 19 8 8 32 6 18 7 10 19 4 | 23 31 26 22 39 23 33 24 28 32 24
19 | 7 17 7 6 33 6 19 10 12 23 4 | 23 33 30 24 41 24 38 24 24 26 24
20 | 6 21 10 5 28 5 21 12 8 15 4 | 15 27 13 19 33 16 26 20 18 23 15
21 | 6 11 8 6 24 7 14 11 10 34 4 | 33 31 33 32 35 33 32 35 35 48 33
22 | 6 15 7 6 27 5 15 6 11 12 3 | 15 23 21 16 37 16 26 19 21 19 17
23 | 5 20 11 8 32 5 24 8 11 15 4 | 17 32 19 20 31 17 32 17 21 19 18
24 | 6 10 8 5 25 6 10 9 10 25 3 | 27 28 29 28 18 25 21 31 28 32 27
25 | 6 12 9 6 --- 6 11 10 9 19 3 | 17 22 19 20 --- 17 19 20 21 22 16
26 | 6 15 8 7 31 8 13 9 12 24 4 | 66 71 67 70 51 64 69 69 67 70 67
27 | 5 11 10 6 25 5 11 9 8 14 3 | 17 23 21 17 30 18 20 19 19 17 17
28E | 8 17 10 11 23 8 23 13 14 16 5 | 54 54 51 51 62 54 54 51 52 52 51
29 | 9 22 13 6 28 5 23 8 11 29 5 | 22 35 24 20 38 23 39 24 25 25 23
30E | 8 20 12 8 62 5 16 12 7 22 4 | 32 43 38 35 50 32 43 31 34 40 34
31 | 6 16 10 7 30 7 20 9 12 24 4 | 16 25 22 19 42 18 30 17 19 25 16
32 | 9 16 8 13 27 5 20 11 10 23 4 | 16 20 17 22 25 17 26 18 19 28 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 16 10 8 31 6 17 10 11 23 |T 24 31 27 25 36 24 31 25 26 30 24
WRMS | 7 16 10 8 28 6 15 9 10 20 |NE 23 30 25 24 34 23 30 24 25 30 23
MEDI | 6 15 10 7 29 6 16 10 11 21 |MD 20 31 24 21 35 22 28 22 24 26 21
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 4.1540 GPS week: 1540 MJD: 55024.0-55030.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2970 |U 8 11 26 |U 7 22 29 |U 8 8 22 |
emr | emr 2875 | 10 14 34 | 8 24 38 |U 10 12 26 |
esa | esa 2880 | 9 12 27 |U 7 23 27 | 8 7 22 |
gfz | gfz 2863 |U 8 11 26 |U 7 22 32 | 9 8 22 |
grg | grg 2784 | 9 12 30 |U 10 22 43 | 10 9 24 |
igr | igr 2868 | 9 12 27 | 8 16 28 | 8 7 21 |
igs | igs 2914 | 8 12 27 | 7 17 27 | 8 8 22 |
jpl | jpl 2872 | 9 11 31 |U 7 18 32 |U 8 8 22 |
mit | mit 2962 |U 8 11 26 |U 17 15 36 |U 10 11 24 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1540.0 GPS week: 1540 Day: 0 MJD: 55024.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2973 | 9 9 29 | 7 19 31 | 15 8 34 |
emr | emr 2876 | 11 9 36 | 10 23 34 | 16 12 32 |
esa | esa 2880 | 9 8 29 | 7 25 30 | 15 9 30 |
gfz | gfz 2864 | 9 9 28 | 8 26 33 | 14 8 31 |
grg | grg 2784 | 10 9 32 | 10 22 36 | 16 10 31 |
igr | igr 2872 | 10 9 28 | 10 12 34 | 15 9 30 |
igs | igs 2866 | 9 9 29 | 8 11 31 | 15 9 31 |
jpl | jpl 2873 | 10 9 32 | 10 19 36 | 15 11 32 |
mit | mit 2976 | 9 10 29 | 14 17 40 | 18 15 30 |
Table 5.1540.1 GPS week: 1540 Day: 1 MJD: 55025.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2969 | 10 20 40 | 7 13 31 | 8 8 23 |
emr | emr 2876 | 11 26 53 | 8 18 38 | 10 9 27 |
esa | esa 2880 | 10 22 43 | 7 13 28 | 8 6 22 |
gfz | gfz 2864 | 9 21 42 | 9 15 34 | 9 8 24 |
grg | grg 2784 | 11 25 48 | 10 16 40 | 10 7 27 |
igr | igr 2855 | 10 21 42 | 6 7 30 | 9 7 24 |
igs | igs 2928 | 10 23 46 | 7 10 29 | 8 7 24 |
jpl | jpl 2873 | 11 23 49 | 7 8 31 | 9 8 25 |
mit | mit 2976 | 9 19 40 | 8 7 31 | 9 8 24 |
Table 5.1540.2 GPS week: 1540 Day: 2 MJD: 55026.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 9 8 24 | 8 26 28 | 8 7 19 |
emr | emr 2875 | 11 8 30 | 9 30 39 | 14 21 34 |
esa | esa 2880 | 10 9 27 | 7 29 30 | 7 7 21 |
gfz | gfz 2863 | 9 8 25 | 8 28 40 | 8 7 21 |
grg | grg 2784 | 10 9 27 | 12 30 48 | 8 9 18 |
igr | igr 2876 | 9 9 26 | 7 25 30 | 7 8 18 |
igs | igs 2878 | 9 7 24 | 7 25 30 | 7 7 20 |
jpl | jpl 2875 | 11 8 29 | 7 24 33 | 7 8 18 |
mit | mit 2976 | 8 6 20 | 7 16 31 | 10 9 22 |
Table 5.1540.3 GPS week: 1540 Day: 3 MJD: 55027.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 8 11 20 | 8 20 28 | 8 6 18 |
emr | emr 2876 | 9 14 24 | 10 27 43 | 7 7 21 |
esa | esa 2880 | 9 12 21 | 8 26 27 | 7 7 17 |
gfz | gfz 2866 | 8 12 20 | 8 26 34 | 8 7 18 |
grg | grg 2784 | 10 14 25 | 11 25 42 | 9 9 26 |
igr | igr 2866 | 9 13 20 | 7 10 22 | 8 6 17 |
igs | igs 2955 | 8 12 20 | 8 24 29 | 7 6 16 |
jpl | jpl 2871 | 9 11 22 | 7 23 37 | 7 6 20 |
mit | mit 2976 | 8 11 22 | 8 21 34 | 9 6 16 |
Table 5.1540.4 GPS week: 1540 Day: 4 MJD: 55028.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 6 8 23 | 5 30 23 | 6 6 26 |
emr | emr 2876 | 9 11 31 | 9 26 46 | 8 12 26 |
esa | esa 2880 | 6 9 23 | 6 30 28 | 7 7 26 |
gfz | gfz 2864 | 6 8 21 | 6 22 33 | 7 7 26 |
grg | grg 2784 | 8 7 26 | 8 19 43 | 8 10 28 |
igr | igr 2869 | 7 9 22 | 7 21 27 | 6 6 22 |
igs | igs 2944 | 6 9 23 | 5 23 26 | 6 8 25 |
jpl | jpl 2871 | 7 8 28 | 6 18 31 | 7 8 24 |
mit | mit 2976 | 6 8 21 | 6 25 29 | 9 11 25 |
Table 5.1540.5 GPS week: 1540 Day: 5 MJD: 55029.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2967 | 8 10 26 | 10 27 36 | 6 10 17 |
emr | emr 2876 | 11 14 36 | 8 26 36 | 8 12 23 |
esa | esa 2880 | 8 10 26 | 7 22 27 | 6 8 20 |
gfz | gfz 2863 | 8 9 23 | 6 22 25 | 7 10 19 |
grg | grg 2784 | 9 9 30 | 8 24 49 | 9 11 22 |
igr | igr 2869 | 8 10 26 | 9 21 25 | 6 8 21 |
igs | igs 2876 | 8 10 25 | 7 17 25 | 6 9 19 |
jpl | jpl 2871 | 10 9 30 | 6 18 29 | 7 11 20 |
mit | mit 2880 | 8 10 26 | 8 6 28 | 8 10 20 |
Table 5.1540.6 GPS week: 1540 Day: 6 MJD: 55030.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2973 | 8 10 22 | 6 18 24 | 6 7 19 |
emr | emr 2876 | 9 14 26 | 7 18 30 | 8 12 22 |
esa | esa 2880 | 8 12 22 | 6 16 21 | 6 7 18 |
gfz | gfz 2863 | 7 12 21 | 6 12 24 | 7 7 17 |
grg | grg 2784 | 7 13 21 | 8 17 43 | 7 11 19 |
igr | igr 2874 | 7 12 21 | 6 15 26 | 6 8 17 |
igs | igs 2952 | 7 13 21 | 6 12 22 | 6 8 16 |
jpl | jpl 2872 | 8 12 24 | 6 13 31 | 6 8 17 |
mit | mit 2976 | 7 13 22 | 64 17 62 | 8 21 29 |
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 6.1540 GPS week: 1540 MJD: 55024.500-55030.500
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 | -11 -18 -1 24 5 | -5 12
| 18 32 69 116 3 | 1
emr uuuuu | 35 -20 196 -55 -17 | 14 22
| 14 26 101 162 12 | 4
esa uuuuu | -47 -38 -32 -60 16 | 5 14
| 25 22 89 79 12 | 4
gfz uuuuu | 36 3 20 45 1 | 8 15
| 10 16 61 67 6 | 1
grg xxxxx | -33 -31 -20 76 -4 | 2 20
| 43 59 92 97 21 | 2
igr xxxxx | -7 -7 -40 62 -3 | 5 16
| 22 13 81 36 9 | 3
irf xxxxx | -16 -11 -14 -25 -7 | 3 16
| 7 5 50 30 4 | 3
jpl uuuuu | -36 -5 93 87 -5 | 11 20
| 37 30 102 68 10 | 3
mit uuuuu | -37 -29 -93 -137 -13 | 8 19
| 12 16 155 91 4 | 4
ngs uuuuu | 35 42 -39 203 4 | 0 10
| 34 39 144 81 5 | 0
sio uuuuu | 59 138 -45 -153 -19 | 15 26
| 11 17 125 194 4 | 5
Table 7.1540.0 GPS week: 1540 Day: 0 MJD: 55024.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 3 -43 -37 -149 4 | -5 12
emr uuuuu | 25 -38 75 157 1 | 16 23
esa uuuuu | -47 -56 -25 -78 -3 | 2 10
gfz uuuuu | 47 18 61 136 -3 | 8 15
grg xxxxx | -17 -71 23 66 21 | 2 20
igr xxxxx | 3 -13 -47 114 -4 | 10 16
irf xxxxx | -21 -10 -59 -62 -11 | 6 15
jpl uuuuu | -92 -59 134 28 10 | 12 21
mit uuuuu | -53 -33 -163 -231 -11 | 11 20
ngs uuuuu | 60 77 15 145 9 | 0 11
sio uuuuu | 45 139 -56 -430 -21 | 20 27
Table 7.1540.1 GPS week: 1540 Day: 1 MJD: 55025.500
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 | -8 14 97 178 6 | -5 13
emr uuuuu | 32 -21 112 87 -7 | 16 23
esa uuuuu | -10 -38 106 -1 13 | 1 12
gfz uuuuu | 27 14 -98 70 5 | 8 15
grg xxxxx | -69 -15 -121 51 -17 | 1 20
igr xxxxx | -22 -12 -97 0 -16 | 8 17
irf xxxxx | -21 -17 12 -34 -9 | 6 16
jpl uuuuu | 0 13 -88 70 -5 | 13 20
mit uuuuu | -53 -42 -30 -186 -13 | 11 20
ngs uuuuu | 7 50 7 123 -3 | 0 9
sio uuuuu | 63 118 -44 -263 -17 | 19 27
Table 7.1540.2 GPS week: 1540 Day: 2 MJD: 55026.500
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 | -43 -44 -118 63 6 | -5 12
emr uuuuu | 43 -12 149 -56 -10 | 17 23
esa uuuuu | -23 -21 56 -37 15 | 2 12
gfz uuuuu | 35 -21 64 57 -9 | 8 15
grg xxxxx | -106 -67 92 150 25 | -2 21
igr xxxxx | -32 5 48 96 -7 | 6 17
irf xxxxx | -26 -13 -82 -18 -14 | 5 16
jpl uuuuu | -3 12 136 176 -7 | 14 20
mit uuuuu | -36 -23 -299 -179 -20 | 11 20
ngs uuuuu | -28 31 86 202 5 | 0 10
sio uuuuu | 45 134 -221 -279 -26 | 19 27
Table 7.1540.3 GPS week: 1540 Day: 3 MJD: 55027.500
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 32 31 -30 2 | -4 12
emr uuuuu | 40 -40 156 50 -21 | 17 23
esa uuuuu | -50 -13 -26 -102 10 | 3 12
gfz uuuuu | 47 -3 4 -12 1 | 8 16
grg xxxxx | 26 45 12 40 -1 | 3 20
igr xxxxx | 33 12 16 60 -6 | 5 17
irf xxxxx | -8 -5 -25 3 -4 | 3 17
jpl uuuuu | -76 24 128 60 -1 | 13 20
mit uuuuu | -30 -18 -152 -112 -13 | 9 20
ngs uuuuu | 48 -6 89 299 2 | -1 10
sio uuuuu | 76 148 -74 -119 -17 | 16 27
Table 7.1540.4 GPS week: 1540 Day: 4 MJD: 55028.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -30 -55 44 82 11 | -4 11
emr uuuuu | 58 -52 358 -122 -31 | 15 20
esa uuuuu | -85 -20 -111 75 38 | 5 15
gfz uuuuu | 34 22 40 -62 0 | 8 16
grg xxxxx | -34 -113 35 -85 -21 | 5 21
igr xxxxx | -16 -24 -38 57 2 | 4 16
irf xxxxx | -18 -5 -29 -56 -5 | 2 16
jpl uuuuu | -40 -37 229 8 -21 | 13 21
mit uuuuu | -32 -8 -174 -186 -14 | 7 19
ngs uuuuu | 66 -10 2 275 3 | 0 10
sio uuuuu | 56 157 -101 -135 -21 | 14 25
Table 7.1540.5 GPS week: 1540 Day: 5 MJD: 55029.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -3 -18 -30 -85 3 | -4 12
emr uuuuu | 28 -1 287 -269 -29 | 11 18
esa uuuuu | -57 -71 -83 -136 21 | 9 21
gfz uuuuu | 42 5 75 101 10 | 7 15
grg xxxxx | -4 -38 -9 228 -6 | 3 21
igr xxxxx | -20 -18 23 57 12 | 2 15
irf xxxxx | -12 -9 21 -31 -5 | 1 15
jpl uuuuu | -40 6 98 184 -12 | 10 18
mit uuuuu | -35 -22 -22 -114 -13 | 5 17
ngs uuuuu | 57 58 -174 273 12 | 0 10
sio uuuuu | 66 154 -13 -4 -18 | 11 23
Table 7.1540.6 GPS week: 1540 Day: 6 MJD: 55030.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -3 -12 3 111 3 | -5 13
emr uuuuu | 16 22 236 -233 -21 | 6 22
esa uuuuu | -58 -49 -140 -144 19 | 11 21
gfz uuuuu | 21 -12 -9 28 4 | 6 15
grg xxxxx | -28 41 -169 85 -33 | 3 20
igr xxxxx | 6 -3 -185 50 0 | 3 15
irf xxxxx | -9 -18 65 21 -1 | -2 17
jpl uuuuu | -4 2 12 85 -3 | 6 19
mit uuuuu | -21 -57 187 46 -9 | 1 19
ngs uuuuu | 32 94 -298 102 4 | 0 11
sio uuuuu | 65 113 195 159 -12 | 5 23
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