[IGSREPORT-18750] Wk 1589 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jul 8 04:00:59 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1589 (Jun 20, 2010 - Jun 26, 2010)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
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:
igs1589[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1589[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1589[0-6].cls IGS GPS clock combination summary report.
igs15897.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15897.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 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
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 | DGAR IISC
0 | EMR | WTZR WTZR
0 | ESA | DGAR IRKJ KOKB YAKT
0 | GFZ | KOKB METS STJO SUTH
0 | GRG | DGAR IRKJ ONSA
1 | COD | 1 1 DGAR
1 | EMR | 30 WTZR WTZR
1 | ESA | 1 1 DGAR IRKJ KOKB
1 | GFZ | KOKB MDVJ METS NYA1 SUTH
1 | GRG | DGAR IRKJ ONSA
1 | JPL | 30
1 | MIT | 30 CAS1 CAS1
2 | COD | DGAR SUTH
2 | EMR | WTZR WTZR
2 | ESA | DGAR DRAO KERG KOKB
2 | GFZ | DAV1 FAA1 IRKJ KOKB MDVJ METS
2 | GRG | DGAR IRKJ ONSA
2 | JPL | 30
2 | MIT | DAV1 DAV1 GODE
3 | COD | DGAR
3 | EMR | 30 30 WTZR WTZR
3 | ESA | KOKB DGAR IRKJ KOKB
3 | GFZ | HARB KOKB MDVJ METS SUTH UNSA
3 | GRG | DGAR IRKJ ONSA
3 | JPL | 21 CHUR
3 | MIT | 1 23 30 1 23 30 MDVJ
4 | COD | DGAR
4 | EMR | 30 WTZR WTZR
4 | ESA | 6 6 WHIT DGAR KOKB UNSA WHIT
4 | GFZ | KOKB MDVJ METS RESO SUTH
4 | GRG | DGAR ONSA
4 | MIT | 25 25 30 MAW1 BAKO CAS1 MAW1
5 | COD | DGAR SOFI
5 | EMR | WTZR HARB WTZR YAKT
5 | ESA | DGAR IRKJ KOKB UNSA
5 | GFZ | KOKB MDVJ METS MIZU SUTH
5 | GRG | DGAR IRKJ ONSA
5 | JPL | 21
5 | MIT | 7 20 23 25 30 32 7 20 23 25 30 32 USNO USNO
6 | COD | DGAR
6 | EMR | WTZR CHUR WTZR
6 | ESA | 26 26 KOKB DGAR KOKB
6 | GFZ | KOKB MDVJ METS SUTH
6 | GRG | DGAR ONSA
6 | JPL | 27 30 AREQ CHUR
6 | MIT | 10 20 25 27 30 32 10 20 25 27 30 32
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | EMR | 1
1 | GRG | 25
4 | ESA | 6
4 | GRG | 25
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 all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | 1.2 .6 1.9 -12 -9 -5 -.24
EMR | 3.5 -4.4 -.4 21 1 5 .21
ESA | 4.8 -.7 6.1 1 38 -76 -.16
GFZ | -.5 2.1 .4 9 36 -102 .07
GRG | 7.5 7.7 11.8 -30 38 -32 .07
JPL | 4.4 -3.1 -4.9 -19 -79 -89 -.20
MIT | 5.6 -1.0 11.2 9 -8 -28 -.07
NGS | 4.9 -2.9 11.5 -61 -36 19 -.11
SIO | 1.7 .3 -13.5 35 -73 -5 .22
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 IGN. For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
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 1.1589.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1589.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 2.1589.[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 3.1589.[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 5.1589.0-6).
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 1589 summary. (Jun 20, 2010 - Jun 26, 2010)
Table 1.1589.a GPS week: 1589 MJD: 55367.000-55373.000
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 243| 0 0 0 7 18 -26 -.20 9 8 | -441 -246 15 72
| 0 0 1 18 9 22 .02 | 191 416
emr 103| 0 -1 -5 -72 29 11 .39 18 18 | -30 -322 17 92
| 2 1 1 18 22 20 .05 | 818 1094
esa 146| 1 0 0 -42 -91 -39 .29 15 9 | -556 300 13 102
| 1 1 1 31 19 17 .03 | 597 797
gfz 199| 0 0 1 -24 -84 8 -.14 10 10 | 83 31 21 106
| 0 0 0 62 82 13 .04 | 352 531
grg 125| 1 1 5 29 -69 8 .65 16 14 | -1875 5684 50 208
| 0 1 1 39 30 8 .04 | 5288 15676
igr n/a| 0 0 -1 -12 0 0 .01 5 5 | 6400 -731 18 64
| 0 0 1 45 27 19 .04 | 1277 1123
jpl 111| 0 0 -8 18 156 49 .53 17 16 | 1834 -263 17 95
| 1 0 1 25 8 19 .03 | 770 1083
mit 258| 0 0 1 -22 -11 24 -.33 10 8 | -220 76 20 162
| 0 1 1 27 20 14 .03 | 511 819
ngs 215| 0 0 0 130 60 -12 -.18 12 8 | 357778 -309627 2326 3925
| 0 0 1 50 34 23 .04 | 615106 472843
sio 265| -2 2 0 -41 120 26 -.33 16 18 | --- --- --- ---
| 0 0 1 31 24 16 .03 | --- ---
Table 1.1589.b GPS week : 1589 MJD: 55367.000-55373.000
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 | 16 10 0 13 0 0 0 |
2 | 5 5 5 5 5 5 4 |
3 | 4 4 4 3 4 4 3 |
4 | 4 3 4 3 4 5 4 |
5 | 4 4 4 5 5 5 5 |
6 | 4 3 3 3 4 3 3 |
7 | 5 4 4 5 4 5 5 |
8 | 4 3 3 3 3 3 3 |
9 | 4 4 3 4 5 4 4 |
10 | 5 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 4 5 5 5 5 5 |
13 | 6 5 5 5 5 5 5 |
14 | 4 4 4 4 4 4 4 |
15 | 4 5 5 5 5 5 6 |
16 | 4 4 4 4 7 5 5 |
17 | 5 5 5 5 5 5 4 |
18 | 5 4 4 4 4 4 4 |
19 | 5 5 4 5 5 5 5 |
20 | 5 4 4 4 4 4 5 |
21 | 5 4 4 4 5 6 4 |
22 | 4 4 3 3 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 3 3 3 3 4 3 4 |
25 | 0 0 0 0 18 24 13 |
26 | 4 4 3 4 4 4 4 |
27 | 4 4 3 4 4 4 4 |
28 | 5 4 4 4 4 4 4 |
29 | 5 5 4 4 5 5 5 |
30 | 6 7 6 7 7 7 7 |
31 | 4 4 4 4 4 4 4 |
32 | 5 4 5 4 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 2.1589.0 GPS week: 1589 Day: 0 MJD: 55367.000
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 243| 0 -1 -1 35 10 -21 -.20 9 9 | -347 -620 16 82
| 22 -12 |
emr 103| 1 -2 -8 -75 -8 18 .30 19 19 | 378 -1312 14 80
| 28 -11 |
esa 146| 1 0 1 -4 -91 -40 .31 8 8 | -489 984 11 90
| -15 57 |
gfz 199| 0 -1 2 -129 -6 10 -.13 9 9 | -497 697 22 116
| -34 -7 |
grg 125| 0 1 7 89 -127 10 .62 17 14 | -71 -219 51 205
| 11 137 |
igr n/a| 0 0 0 55 -51 -1 -.01 6 6 | 7612 -1308 17 53
| -18 10 |
jpl 111| 1 0 -10 37 152 42 .50 16 15 | 2070 -1182 17 98
| 5 -60 |
mit 258| 0 0 0 -25 20 46 -.39 11 9 | -22 -232 20 143
| 11 9 |
ngs 215| 0 -1 0 212 45 -37 -.23 14 12 | 1257013 -999999 2852 4624
| -42 58 |
sio 265| -3 2 -2 -52 149 5 -.38 18 20 | --- --- --- ---
| -30 -36 |
Table 2.1589.1 GPS week: 1589 Day: 1 MJD: 55368.000
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 243| 0 -1 -2 4 5 -34 -.18 8 8 | -473 216 18 70
| 67 -17 |
emr 103| -1 -3 -6 -88 30 4 .40 18 18 | -895 680 15 89
| 18 -35 |
esa 146| 1 1 3 -67 -63 -40 .29 8 8 | -1443 1190 13 103
| 37 51 |
gfz 199| 0 0 0 -40 -33 30 -.10 9 9 | -96 430 20 104
| -41 25 |
grg 125| 1 1 5 0 -54 20 .64 15 13 | -263 673 46 246
| 98 -7 |
igr n/a| 0 0 0 -28 21 42 -.03 5 5 | 6461 342 17 72
| 29 -13 |
jpl 111| 0 0 -4 -24 158 28 .54 17 16 | 1011 725 17 98
| 48 -13 |
mit 258| 0 0 0 -1 -17 35 -.35 11 8 | -373 569 25 190
| 6 5 |
ngs 215| 0 0 0 141 16 -20 -.19 10 7 | -465 243 2150 3429
| -11 30 |
sio 265| -2 2 -1 -3 117 24 -.31 16 17 | --- --- --- ---
| -48 -42 |
Table 2.1589.2 GPS week: 1589 Day: 2 MJD: 55369.000
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 243| 0 -1 -1 15 8 13 -.18 8 8 | -226 -706 12 66
| -11 -13 |
emr 103| 1 -1 -6 -59 40 -21 .44 18 18 | -109 871 16 95
| 4 -40 |
esa 146| 0 0 0 -3 -106 -55 .31 8 8 | -728 837 11 94
| -19 81 |
gfz 199| -1 0 0 -44 -21 2 -.12 9 9 | 488 -732 23 101
| -37 1 |
grg 125| 2 -1 3 52 -84 16 .61 15 14 | 320 -676 68 222
| 71 -16 |
igr n/a| -1 0 -1 -18 -18 -5 -.00 5 5 | 6992 483 18 69
| -8 -26 |
jpl 111| 0 -1 -9 28 154 73 .50 16 15 | 1790 886 17 95
| 20 -23 |
mit 258| 0 1 1 -55 4 23 -.34 8 7 | 315 -578 19 156
| 12 4 |
ngs 215| 0 0 2 128 22 -28 -.16 11 7 | -238 -712 2485 3650
| 26 44 |
sio 265| -2 3 0 -76 153 10 -.32 15 16 | --- --- --- ---
| -31 -48 |
Table 2.1589.3 GPS week: 1589 Day: 3 MJD: 55370.000
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 243| 0 0 0 -27 21 -44 -.20 9 8 | -352 -467 14 70
| 84 -28 |
emr 103| 2 -2 -3 -94 42 -6 .37 18 18 | 1408 -1850 18 91
| 45 -58 |
esa 146| 0 0 0 -69 -110 -6 .30 8 7 | 296 -882 13 97
| 5 26 |
gfz 199| -1 0 0 81 -68 8 -.14 10 10 | 31 234 21 104
| -20 -24 |
grg 125| 2 1 4 -23 -56 -7 .64 15 15 | 496 -1066 48 187
| 169 -51 |
igr n/a| 0 0 -2 -25 -4 -21 -.00 5 5 | 7961 -2506 18 59
| -17 -36 |
jpl 111| 1 0 -9 -11 160 50 .51 18 17 | 3252 -1815 18 96
| 64 -59 |
mit 258| 0 0 1 24 -27 27 -.32 9 8 | 485 -1031 21 150
| 1 21 |
ngs 215| 0 0 1 53 83 -34 -.17 11 6 | 1259366 -999999 2073 3925
| 56 -17 |
sio 265| -2 3 0 9 124 43 -.31 15 17 | --- --- --- ---
| -51 -34 |
Table 2.1589.4 GPS week: 1589 Day: 4 MJD: 55371.000
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 243| 0 0 0 11 21 -26 -.17 9 8 | -564 -118 17 72
| -8 -53 |
emr 103| 1 -2 -2 -83 57 39 .46 17 17 | -276 746 19 98
| 5 -77 |
esa 146| 0 -1 -1 -52 -96 -57 .32 58 14 | -958 -77 21 124
| 45 82 |
gfz 199| 0 0 0 -9 -240 12 -.10 12 12 | -102 336 23 102
| -22 -16 |
grg 125| 1 3 5 44 -53 4 .70 18 16 | -13853 41213 45 196
| 70 -106 |
igr n/a| -1 0 -2 -55 12 -10 .10 6 6 | 5677 277 20 68
| -27 -18 |
jpl 111| 2 1 -7 36 172 29 .58 17 16 | 1554 826 17 96
| -37 -87 |
mit 258| 1 0 1 -41 -41 -1 -.30 8 8 | -925 1370 21 170
| 7 24 |
ngs 215| -2 0 0 91 105 8 -.11 10 8 | 2034 -8863 1955 3872
| 31 -55 |
sio 265| -2 3 1 -56 86 25 -.32 16 20 | --- --- --- ---
| -49 -17 |
Table 2.1589.5 GPS week: 1589 Day: 5 MJD: 55372.000
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 243| 0 0 0 1 31 -13 -.22 9 9 | -328 -404 17 82
| 34 -25 |
emr 103| -3 0 -6 -46 34 26 .38 16 16 | 254 -805 19 85
| -29 -36 |
esa 146| 2 0 2 -23 -64 -50 .25 10 9 | -670 560 16 119
| -25 21 |
gfz 199| 0 0 1 -1 -146 -15 -.16 10 10 | 352 -217 21 103
| -49 -15 |
grg 125| 1 0 6 0 -79 8 .70 16 14 | 320 -231 50 202
| 127 -34 |
igr n/a| 0 0 -2 -58 30 -2 -.01 4 4 | 5875 -1258 16 54
| -25 -22 |
jpl 111| 0 0 -10 30 156 42 .51 16 16 | 2137 -730 17 90
| -2 -32 |
mit 258| 0 -1 1 -39 -17 18 -.31 10 9 | -343 -187 20 170
| 17 20 |
ngs 215| 0 -1 1 122 92 17 -.19 13 9 | -6473 -79984 2082 3949
| -33 -87 |
sio 265| -3 3 0 -61 101 21 -.34 16 17 | --- --- --- ---
| -30 -22 |
Table 2.1589.6 GPS week: 1589 Day: 6 MJD: 55373.000
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 243| 0 0 0 8 26 -56 -.22 8 8 | -798 376 14 66
| 47 -14 |
emr 103| 0 0 -5 -56 9 18 .36 17 17 | -973 -587 21 107
| -24 -15 |
esa 146| 2 0 0 -73 -104 -26 .25 7 7 | 94 -510 11 93
| 11 44 |
gfz 199| 0 0 1 -25 -76 8 -.22 11 11 | 405 -527 22 116
| -52 1 |
grg 125| 1 2 8 43 -33 8 .65 16 14 | -80 97 48 198
| 74 -81 |
igr n/a| 0 0 -3 45 2 0 .01 6 5 | 4225 -1150 21 75
| -18 49 |
jpl 111| -1 0 -9 30 143 77 .56 16 15 | 1030 -554 19 97
| 21 -18 |
mit 258| 0 -1 3 -16 -3 21 -.33 10 9 | -678 623 20 158
| 7 1 |
ngs 215| -1 -1 -1 162 59 8 -.21 13 9 | -6786 -78076 2686 4026
| 4 4 |
sio 265| -3 1 3 -49 109 50 -.34 18 17 | --- --- --- ---
| -28 -24 |
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 3.1589.0 GPS week: 1589 Day: 0 MJD: 55367.000
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 | 21 97 --- --- --- 30 --- 13 35 --- 16 | 53 82 --- --- --- 57 --- 15 35 --- 50
2 | 8 16 6 7 16 5 14 7 15 34 4 | 20 22 23 23 24 20 27 19 21 20 19
3 | 8 14 6 7 13 5 9 8 10 21 3 | 18 26 26 22 32 23 22 22 26 27 22
4 | 9 12 5 6 15 5 11 8 12 19 3 | 31 27 27 31 29 26 21 29 28 35 27
5 | 6 17 8 9 21 6 15 7 12 18 4 | 11 18 15 15 31 12 20 12 13 20 11
6 | 8 14 5 7 13 5 10 9 12 18 3 | 24 31 43 29 36 29 27 28 32 29 29
7 | 15 19 9 9 23 5 20 14 10 16 5 | 15 25 14 16 28 13 22 15 13 16 11
8 | 7 23 6 5 18 5 13 8 9 12 3 | 14 24 14 15 20 12 17 13 11 13 12
9 | 8 17 7 9 13 5 13 9 16 19 4 | 20 25 19 16 21 21 26 19 23 14 18
10 | 12 18 7 9 11 6 13 16 11 21 4 | 13 26 16 20 23 15 26 23 15 24 16
11 | 10 18 8 8 8 6 13 12 10 18 4 | 36 46 43 42 45 40 42 38 41 37 39
12E | 10 26 9 8 19 5 22 9 14 17 4 | 26 33 28 24 33 28 34 27 32 28 27
13 | 9 17 11 11 25 5 21 18 14 18 5 | 16 27 23 20 33 18 27 22 19 24 17
14 | 7 22 6 6 16 6 13 9 14 10 3 | 15 26 21 17 26 18 25 19 21 21 17
15 | 9 19 5 12 18 6 16 12 12 15 4 | 16 25 18 21 30 17 24 21 17 22 17
16E | 7 19 7 12 17 5 21 8 14 11 4 | 20 27 19 17 22 20 27 22 29 18 18
17 | 9 21 7 10 17 6 22 13 12 21 4 | 16 35 23 20 28 19 31 20 22 18 18
18 | 10 26 9 10 13 6 18 12 16 18 4 | 26 36 29 24 34 26 29 19 31 22 24
19 | 10 15 8 4 12 4 20 16 11 21 4 | 23 32 32 25 31 25 33 23 23 23 24
20 | 9 23 11 7 16 9 16 19 10 17 5 | 15 27 16 16 24 17 21 19 12 18 13
21 | 11 17 11 10 11 7 16 9 14 30 4 | 26 23 25 29 20 23 24 29 26 22 23
22 | 9 20 8 6 13 5 13 7 10 16 3 | 13 25 18 12 26 15 22 15 17 22 14
23 | 9 19 10 10 18 4 22 12 14 15 4 | 18 30 24 19 27 20 28 18 21 18 18
24 | 6 13 6 6 11 6 8 6 14 20 3 | 22 24 23 24 30 25 23 23 27 29 23
X25E | 4 --- --- --- --- 78 --- --- --- --- 0 | 17 --- --- --- --- 29 --- --- --- --- 16
26 | 9 15 6 10 10 6 12 9 14 15 3 | 15 17 16 18 17 16 21 18 17 21 14
X27 | 6 16 5 9 12 6 --- 9 15 16 3 | 17 20 15 14 19 18 --- 15 19 14 14
28E | 9 28 9 10 13 5 20 12 11 15 4 | 15 35 18 21 24 16 25 15 20 21 16
X29 | 10 18 7 6 14 6 19 14 14 --- 4 | 17 29 21 18 23 18 27 26 19 --- 19
30E | 13 25 11 12 29 8 18 12 32 12 6 | 59 64 57 58 64 58 63 63 69 58 59
31 | 8 17 8 9 20 6 16 7 17 12 4 | 12 23 19 21 30 15 27 13 18 13 14
X32E | 13 --- 9 8 18 10 17 17 17 19 5 | 36 --- 33 32 49 39 37 31 40 31 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 8 9 17 6 16 11 14 18 |T 21 30 23 22 29 23 27 22 24 23 21
WRMS | 9 19 8 9 14 6 15 9 12 20 |NE 18 26 22 21 27 20 25 20 21 21 18
MEDI | 9 18 7 9 15 6 16 9 14 18 |MD 17 26 21 20 28 20 26 20 21 22 18
Table 3.1589.1 GPS week: 1589 Day: 1 MJD: 55368.000
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 | 24 33 17 --- --- 19 --- 18 13 --- 10 | 55 32 4 --- --- 56 --- 27 23 --- 46
2 | 6 14 7 9 16 4 17 9 10 32 4 | 12 19 18 16 19 13 22 15 16 18 12
3 | 8 16 6 8 11 5 14 6 6 18 3 | 15 21 19 15 21 18 23 16 16 24 16
4 | 6 11 8 6 15 6 9 9 7 18 3 | 17 18 19 20 18 18 17 22 19 28 17
5 | 8 23 8 12 20 6 16 8 6 18 4 | 9 22 16 15 31 11 19 13 10 19 9
6 | 7 15 5 7 11 4 13 6 7 15 3 | 18 23 39 19 25 21 27 20 21 24 20
7 | 12 18 8 10 21 7 18 12 5 15 4 | 12 23 14 14 26 11 22 12 13 14 10
8 | 6 14 7 7 13 4 16 7 6 9 3 | 11 18 14 9 18 9 18 12 12 9 10
9 | 7 18 6 9 15 4 12 10 9 14 3 | 13 23 15 14 20 10 21 11 13 9 11
10 | 12 13 8 10 11 7 14 15 8 16 4 | 11 19 16 18 22 12 23 22 18 23 14
11 | 6 15 6 7 9 6 15 13 10 18 3 | 22 31 26 24 31 24 32 24 26 23 24
12E | 7 25 10 9 13 4 22 10 9 12 4 | 13 27 16 18 22 12 22 12 14 16 13
13 | 9 20 10 10 23 5 22 15 11 16 5 | 15 28 20 19 29 16 27 18 22 18 15
14 | 6 20 10 8 14 3 19 10 10 12 4 | 12 25 20 15 24 13 21 15 16 17 13
15 | 10 19 7 12 21 6 18 14 8 14 4 | 15 24 18 18 29 12 22 17 15 19 14
16E | 7 15 7 10 13 5 23 6 7 12 3 | 12 22 15 14 18 13 24 11 11 18 11
17 | 9 23 9 11 18 6 20 11 7 19 4 | 10 28 17 16 26 14 27 13 17 11 12
X18 | 7 24 6 8 14 6 --- 8 7 18 4 | 16 28 20 16 23 18 --- 16 19 18 15
19 | 8 19 8 11 10 7 20 16 7 20 4 | 17 29 26 21 27 20 31 17 18 18 19
20 | 8 22 7 6 14 6 18 13 5 10 3 | 15 22 13 10 23 12 20 17 14 16 12
21 | 9 14 9 7 12 7 14 7 7 25 3 | 19 16 17 17 12 18 18 20 19 15 15
22 | 7 17 8 8 13 4 12 8 8 15 3 | 10 21 16 12 23 11 17 13 12 15 10
23 | 10 26 10 9 17 4 25 9 8 15 4 | 13 30 18 15 25 14 28 15 15 15 13
24 | 6 12 6 7 10 4 10 7 6 19 3 | 15 17 17 15 16 16 20 17 18 19 15
X25E | 3 --- --- --- >>>> 716 --- --- --- --- 0 | 1 --- --- --- 1 1 --- --- --- --- 1
26 | 7 14 9 7 11 6 13 11 8 13 3 | 12 16 15 11 18 8 19 14 11 16 10
27 | 6 17 7 7 14 4 13 8 10 14 3 | 11 23 14 13 22 10 22 10 12 10 11
28E | 8 20 9 12 15 6 19 9 6 12 4 | 25 33 28 27 38 28 31 27 25 28 26
X29 | 8 21 7 8 10 7 22 15 9 --- 4 | 12 23 15 10 20 12 24 21 12 --- 12
30E | 10 22 10 16 21 3 21 12 31 11 6 | 65 66 63 65 64 63 68 66 73 68 64
31 | 5 17 6 10 16 5 18 8 7 13 3 | 9 26 15 12 29 11 25 11 12 11 11
32E | 11 21 5 10 16 4 18 15 8 14 4 | 22 26 26 24 33 24 30 22 23 20 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 9 15 5 17 11 10 16 |T 16 25 19 17 24 17 24 18 18 19 16
WRMS | 8 18 8 9 13 5 16 8 7 17 |NE 13 22 18 15 23 14 22 16 15 17 13
MEDI | 7 18 8 9 14 5 18 10 8 15 |MD 13 23 17 15 23 13 22 16 16 18 13
Table 3.1589.2 GPS week: 1589 Day: 2 MJD: 55369.000
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 --- --- --- --- 105 --- --- --- --- 0 | 37 --- --- --- --- 68 --- --- --- --- 38
2 | 8 14 8 6 13 7 14 6 11 33 4 | 14 21 21 18 26 16 22 16 19 18 15
3 | 8 13 10 10 10 4 11 5 8 17 3 | 14 21 19 19 24 17 21 14 17 22 16
4 | 9 14 11 4 9 6 10 7 8 16 3 | 23 20 23 23 22 22 15 25 24 31 22
5 | 8 21 8 12 20 4 16 8 6 16 4 | 12 22 13 13 32 13 20 15 13 18 11
6 | 7 11 9 9 9 3 10 5 9 13 3 | 18 23 40 23 27 20 24 19 23 23 20
7 | 10 19 6 10 18 5 20 8 10 12 4 | 13 25 17 16 27 14 24 12 17 13 12
8 | 6 14 8 9 15 4 16 6 9 7 3 | 12 18 16 12 25 11 18 12 12 9 11
9 | 9 17 6 8 10 3 11 8 8 14 3 | 14 22 15 16 20 14 21 11 16 10 13
10 | 11 13 6 7 8 7 14 9 8 12 3 | 13 22 19 18 24 15 24 19 16 19 16
11 | 9 13 6 9 11 6 14 9 7 17 3 | 25 34 29 30 39 29 35 30 33 28 29
12E | 7 28 10 9 20 4 21 9 9 11 4 | 12 31 18 15 27 15 24 14 17 16 15
13 | 8 22 7 10 24 8 20 10 10 10 4 | 16 28 22 19 35 19 27 20 22 20 18
14 | 6 22 7 6 14 5 18 7 10 11 3 | 14 29 21 15 27 17 24 17 23 20 17
15 | 10 19 8 14 19 5 19 11 10 14 4 | 16 27 22 19 30 15 23 17 21 20 16
16E | 9 19 10 12 14 5 23 6 12 11 4 | 12 24 19 14 26 12 27 12 25 13 14
17 | 9 22 10 12 20 5 21 10 7 20 4 | 15 27 20 18 26 17 29 16 17 12 15
X18 | 11 21 7 9 17 3 --- 9 7 15 4 | 11 24 15 14 25 13 --- 14 15 18 11
19 | 8 17 10 10 10 4 18 10 9 20 4 | 19 28 26 21 28 21 32 17 17 18 19
20 | 7 20 7 7 18 5 17 9 7 7 3 | 12 20 15 14 27 14 21 15 15 16 13
21 | 10 14 8 8 11 5 16 8 8 24 4 | 20 19 15 19 14 18 21 21 21 16 16
22 | 7 15 9 6 17 4 12 5 7 11 3 | 10 18 14 9 25 13 18 12 17 15 11
23 | 8 27 9 11 18 7 23 7 11 13 4 | 17 33 23 19 28 19 28 17 23 17 18
24 | 6 10 4 5 13 5 8 7 7 14 2 | 16 19 21 20 22 19 18 20 23 20 18
X25E | 3 --- --- --- --- 32 --- --- --- --- 0 | 1 --- --- --- --- 1 --- --- --- --- 1
26 | 7 14 5 7 11 5 12 6 8 13 3 | 11 20 13 11 19 10 20 13 14 15 11
27 | 6 15 5 6 11 3 10 7 7 13 3 | 11 20 13 13 21 11 20 9 13 9 11
28E | 9 20 7 9 15 5 19 8 6 10 3 | 18 29 22 22 27 21 28 23 27 23 22
X29 | 8 19 8 7 12 5 22 11 9 --- 4 | 13 25 17 17 21 15 29 19 17 --- 15
30E | 12 21 9 12 21 5 20 10 34 11 6 | 32 35 36 37 36 31 36 33 49 34 32
31 | 5 22 9 9 16 5 16 5 7 14 3 | 11 28 18 15 31 14 26 11 16 14 13
32E | 11 22 10 12 13 7 16 10 11 13 4 | 20 27 25 24 28 22 27 20 24 19 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 9 15 5 16 8 11 15 |T 15 24 20 18 26 18 24 17 20 18 16
WRMS | 8 18 8 9 14 5 15 7 7 16 |NE 14 23 19 17 25 16 23 16 18 17 15
MEDI | 8 19 8 9 14 5 16 8 8 13 |MD 14 24 19 18 26 15 24 16 17 18 15
Table 3.1589.3 GPS week: 1589 Day: 3 MJD: 55370.000
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 | 12 31 --- --- --- 31 --- 23 24 --- 12 | 63 28 --- --- --- 59 --- 25 22 --- 64
2 | 8 14 6 8 11 5 19 8 8 33 4 | 15 21 22 17 23 19 27 19 20 19 17
3 | 8 17 6 7 12 3 14 4 6 16 3 | 13 25 22 20 25 17 22 17 15 25 18
4 | 7 12 5 6 13 6 11 7 8 16 3 | 26 22 24 26 27 22 18 25 22 31 22
5 | 7 22 7 12 20 5 18 13 7 16 4 | 11 24 20 15 30 13 22 19 10 22 13
6 | 7 15 6 7 12 3 13 4 6 12 3 | 19 28 88 25 31 22 25 23 22 24 23
7 | 17 20 6 13 20 5 18 9 10 13 4 | 14 25 19 20 28 13 25 12 16 13 12
8 | 4 15 7 9 14 5 15 8 7 9 3 | 13 19 20 17 20 13 17 12 14 10 12
9 | 6 14 6 8 10 4 14 12 10 14 3 | 15 18 19 16 18 14 21 17 11 13 13
10 | 12 16 6 6 14 7 12 8 8 11 3 | 14 27 24 20 22 16 25 19 17 21 16
11 | 11 16 7 9 10 6 19 6 7 16 3 | 31 42 38 38 42 32 39 36 29 33 34
12E | 8 24 10 11 21 5 25 11 12 8 4 | 13 26 17 18 22 14 24 15 15 17 13
13 | 8 23 8 11 21 6 20 10 7 13 4 | 17 30 26 26 32 21 27 21 21 20 20
14 | 4 20 8 7 15 4 19 9 10 11 3 | 14 26 22 17 28 15 24 15 17 18 16
15 | 10 17 6 14 17 6 21 15 9 19 4 | 20 27 27 20 30 18 26 25 22 30 21
16E | 7 16 10 11 16 6 22 7 9 10 4 | 10 23 21 15 20 13 24 11 11 16 12
17 | 8 20 14 11 16 6 23 11 8 16 4 | 14 26 22 20 25 17 28 17 17 13 15
X18 | 8 22 4 8 16 4 --- 11 9 16 4 | 11 25 14 9 23 10 --- 14 12 17 11
19 | 9 19 8 10 13 4 24 13 9 21 4 | 20 31 28 23 28 23 36 21 20 23 22
20 | 10 22 8 10 16 5 17 6 10 9 4 | 19 25 24 21 27 17 26 19 21 21 19
21 | 7 13 6 6 10 6 13 8 7 24 3 | 21 21 18 20 22 19 22 23 21 19 18
22 | 6 14 7 5 13 4 12 8 6 11 3 | 8 18 16 10 23 9 18 12 11 14 10
23 | 9 28 7 14 18 5 22 8 11 17 4 | 16 33 23 24 28 19 29 19 20 20 18
24 | 6 12 5 5 13 4 11 7 9 15 3 | 14 20 17 19 21 15 17 18 17 19 17
X25E | 4 --- --- --- --- 138 --- --- --- --- 0 | 1 --- --- --- --- 1 --- --- --- --- 1
26 | 7 14 6 8 12 6 13 13 8 13 3 | 14 20 20 14 20 13 21 19 12 21 14
27 | 5 14 7 15 11 4 13 11 9 13 3 | 16 20 20 24 22 16 20 18 12 16 16
28E | 7 16 8 9 16 5 22 10 10 11 4 | 22 26 19 21 28 22 27 20 25 21 20
X29 | 8 19 6 7 12 6 24 11 10 --- 4 | 12 27 20 14 20 15 29 18 15 --- 15
30E | 13 22 10 13 23 4 26 11 37 16 7 | 75 75 76 73 73 73 76 77 83 75 75
31 | 6 20 8 10 16 6 18 6 9 13 3 | 11 30 21 15 31 15 27 11 16 13 15
32E | 12 22 9 11 14 5 16 10 8 11 4 | 19 30 25 24 23 19 27 20 19 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 8 10 15 5 18 9 11 15 |T 18 27 25 21 27 19 26 20 19 21 19
WRMS | 8 18 7 10 15 5 17 8 6 17 |NE 15 25 24 19 25 16 24 18 17 19 17
MEDI | 8 17 7 9 14 5 18 9 9 13 |MD 14 26 21 20 25 16 25 19 17 19 16
Table 3.1589.4 GPS week: 1589 Day: 4 MJD: 55371.000
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 --- --- --- --- 109 --- --- --- --- 0 | 42 --- --- --- --- 99 --- --- --- --- 44
2 | 10 16 9 10 12 7 13 9 6 34 4 | 17 24 22 20 22 21 27 21 20 19 18
3 | 9 14 13 10 13 4 13 5 9 16 3 | 14 23 25 17 24 18 22 17 25 23 19
4 | 9 10 10 10 12 7 11 11 10 20 4 | 24 22 27 26 21 20 22 23 22 32 22
5 | 5 18 11 20 20 5 17 9 10 16 4 | 12 22 16 25 33 16 23 18 21 20 14
6 | 13 12 302 10 13 3 11 6 10 13 4 | 21 27 220 21 28 22 27 21 27 21 23
7 | 13 17 11 11 17 5 19 8 5 13 4 | 18 27 19 19 28 15 26 15 17 17 15
8 | 5 14 7 10 12 4 13 6 6 8 3 | 11 20 18 21 18 14 21 15 14 12 12
9 | 7 15 25 8 14 3 14 8 9 12 4 | 15 20 34 17 21 16 21 17 21 16 17
10 | 9 14 10 9 11 6 13 6 5 14 3 | 15 25 20 26 19 18 26 16 14 21 16
11 | 9 16 10 11 15 8 14 7 7 18 4 | 26 38 35 34 39 30 35 30 30 29 30
12E | 8 21 12 12 32 6 25 9 7 10 5 | 15 24 23 20 28 17 24 18 22 17 18
13 | 7 20 11 13 24 5 20 8 7 10 4 | 17 29 23 28 31 18 27 18 21 20 18
14 | 5 19 17 11 21 6 19 7 6 13 4 | 14 26 23 19 29 16 24 16 19 17 16
15 | 8 20 12 17 21 5 21 11 8 21 5 | 14 28 23 28 30 19 26 20 17 33 18
X16E | 8 26 --- 26 22 20 --- 11 10 17 6 | 13 32 --- 30 21 20 --- 15 21 18 16
17 | 7 21 14 12 19 7 20 11 7 13 4 | 17 28 22 20 27 21 29 21 19 20 18
18 | 9 19 11 8 16 6 16 6 8 14 4 | 18 27 25 13 24 18 27 18 21 21 18
19 | 11 19 17 11 14 6 18 11 11 20 5 | 18 32 31 22 27 24 33 21 25 19 22
20 | 5 17 10 17 20 5 18 8 5 9 4 | 15 22 23 16 23 18 21 18 18 21 15
21 | 12 11 14 10 14 5 13 7 12 26 4 | 22 26 29 24 22 22 28 24 28 23 24
22 | 7 18 10 8 18 6 14 6 7 11 3 | 14 23 23 15 26 15 24 17 20 18 16
23 | 9 24 12 14 20 5 24 7 8 14 4 | 15 33 24 26 23 17 29 16 19 19 17
24 | 7 13 10 8 15 6 10 9 6 16 3 | 14 21 21 15 17 18 21 17 18 16 16
X25E | 27 --- 40 --- 9962 29 --- 30 32 --- 18 | 1 --- 94 --- 1 1 --- 86 92 --- 1
26 | 5 14 9 12 13 5 15 6 8 11 3 | 13 17 21 25 20 17 23 19 18 23 15
27 | 6 14 19 9 15 4 13 8 9 12 4 | 15 19 28 21 22 17 23 18 22 18 17
28E | 8 16 12 11 16 8 21 11 7 8 4 | 12 20 23 17 22 18 22 16 17 17 14
X29 | 7 20 9 9 10 5 23 11 6 --- 4 | 14 26 18 15 21 15 28 17 18 --- 16
30E | 11 21 14 20 24 6 23 12 33 17 7 | 61 63 61 67 65 59 64 62 71 68 62
31 | 5 20 15 14 19 6 19 6 7 13 4 | 13 29 23 18 31 16 29 10 16 11 15
32E | 11 22 8 12 19 6 18 11 8 11 4 | 20 34 27 26 23 23 29 22 22 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 58 12 18 6 17 8 10 16 |T 17 26 34 23 25 21 26 22 24 21 19
WRMS | 8 17 14 12 16 6 16 8 8 20 |NE 16 25 31 21 25 18 25 18 20 20 17
MEDI | 8 17 11 11 16 6 17 8 8 13 |MD 15 26 23 21 23 18 26 18 21 20 17
Table 3.1589.5 GPS week: 1589 Day: 5 MJD: 55372.000
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 | 4 --- --- --- --- 41 --- --- --- --- 0 | 77 --- --- --- --- 97 --- --- --- --- 78
2 | 9 13 8 7 16 5 16 8 13 32 4 | 15 23 20 19 26 18 25 19 20 19 16
3 | 9 11 8 9 14 3 11 5 9 16 3 | 17 21 25 20 27 19 24 19 20 27 21
4 | 10 12 11 12 13 6 11 11 18 19 4 | 20 16 25 20 19 16 17 21 20 30 18
5 | 6 17 7 13 23 3 18 11 10 16 4 | 12 24 18 22 35 14 23 17 14 21 14
6 | 8 9 10 10 11 3 12 7 8 13 3 | 15 21 90 21 26 19 24 18 19 24 20
7 | 12 18 10 13 16 4 18 13 12 18 5 | 15 24 18 20 27 13 24 17 16 18 14
8 | 6 13 5 7 11 4 11 9 8 11 3 | 10 17 13 16 20 10 17 12 15 11 11
9 | 6 14 8 11 11 5 11 11 14 12 3 | 14 20 17 17 20 13 22 14 16 13 13
10 | 10 16 5 9 11 4 11 9 12 19 4 | 16 29 20 26 23 18 28 16 21 23 18
11 | 10 16 9 11 15 6 14 9 7 16 4 | 25 40 37 35 42 28 38 27 25 27 31
12E | 10 19 10 10 20 4 23 12 14 8 5 | 14 24 19 18 22 14 24 17 17 17 15
13 | 10 19 13 12 22 5 20 9 9 16 5 | 17 31 26 25 35 20 27 20 23 22 19
14 | 5 19 7 8 15 4 18 8 10 9 3 | 14 29 19 16 26 17 24 17 19 19 16
15 | 10 17 7 13 14 4 19 12 14 24 5 | 18 26 20 25 31 17 26 20 19 33 18
X16E | 12 17 8 14 15 5 --- 11 9 --- 5 | 14 23 20 20 27 14 --- 17 17 --- 15
17 | 10 17 7 12 16 3 21 12 9 13 4 | 14 22 17 18 26 14 26 16 18 16 14
18 | 9 17 8 10 16 2 14 10 10 14 4 | 16 23 14 16 23 13 22 15 12 22 12
19 | 9 17 10 10 13 3 24 9 12 20 4 | 18 29 30 22 31 23 34 19 24 21 22
20 | 7 20 8 6 17 4 17 9 14 9 4 | 17 26 20 23 31 18 26 21 18 23 18
21 | 14 13 22 11 11 5 14 6 11 29 5 | 21 18 29 24 15 18 22 20 21 22 17
22 | 8 16 7 8 18 4 11 8 6 10 3 | 13 19 12 13 27 13 19 13 11 17 11
23 | 10 23 13 13 15 4 24 7 9 17 5 | 14 34 25 24 28 19 29 17 21 20 18
24 | 7 10 6 7 11 4 7 11 9 15 3 | 16 19 16 17 19 16 18 18 18 20 16
X25E | 36 --- 29 --- --- 40 --- 52 42 --- 23 | 1 --- 113 --- --- 1 --- 100 120 --- 1
26 | 8 15 8 8 14 3 13 12 12 14 4 | 13 21 16 19 22 12 22 15 13 19 13
27 | 5 13 9 8 10 3 12 11 13 12 3 | 15 22 19 16 23 14 23 15 15 16 15
28E | 5 16 9 11 22 4 17 10 8 8 4 | 20 26 20 19 26 21 26 22 22 22 19
X29 | 9 20 9 8 14 3 21 8 9 --- 4 | 14 25 17 15 20 14 26 14 13 --- 13
30E | 12 21 11 10 26 8 21 17 42 11 7 | 99 101 95 101 98 98 103 99 99 97 97
31 | 6 18 9 10 13 5 17 5 7 13 3 | 14 30 25 19 31 19 29 15 19 16 18
32E | 10 21 11 11 15 4 18 13 12 13 4 | 20 30 25 27 28 21 31 22 24 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 10 10 16 4 16 10 13 16 |T 19 27 28 23 28 21 27 22 24 23 20
WRMS | 9 16 9 10 14 4 16 9 9 17 |NE 15 24 23 20 26 16 24 17 18 20 16
MEDI | 9 17 9 10 15 4 17 10 10 14 |MD 15 24 20 20 26 17 24 17 19 21 16
Table 3.1589.6 GPS week: 1589 Day: 6 MJD: 55373.000
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 | 5 --- --- --- --- 86 --- --- --- --- 0 | 108 --- --- --- --- 85 --- --- --- --- 109
2 | 7 13 4 10 11 4 14 11 8 33 4 | 22 25 26 23 24 23 28 26 24 27 22
3 | 6 12 7 9 15 5 12 6 6 19 3 | 18 22 21 21 30 19 26 19 21 26 20
4 | 8 13 5 9 14 4 7 8 11 20 3 | 31 28 31 31 35 28 24 31 30 39 29
5 | 8 22 8 13 21 4 17 11 10 19 4 | 16 29 20 22 34 16 26 20 20 24 17
6 | 5 11 6 7 12 5 11 7 5 14 3 | 20 25 50 25 34 22 26 24 25 25 24
7 | 13 19 7 10 19 6 16 16 10 22 5 | 18 26 22 23 28 19 26 29 27 29 20
8 | 6 14 6 8 11 6 12 10 8 13 3 | 15 19 18 17 22 15 23 20 24 16 16
9 | 8 16 4 11 13 5 13 10 12 15 3 | 16 20 14 17 21 12 20 14 19 13 13
10 | 9 15 4 9 11 6 10 9 7 21 3 | 17 26 21 24 25 16 25 20 22 25 19
11 | 10 13 5 12 17 6 12 7 7 17 3 | 38 48 44 47 56 40 46 41 40 38 41
12E | 9 23 9 9 18 6 23 12 10 9 4 | 14 24 17 17 26 13 21 14 18 14 14
13 | 9 20 11 12 17 6 15 9 16 15 4 | 19 35 27 26 35 20 27 23 22 26 22
14 | 6 17 5 9 16 4 17 10 12 10 3 | 16 25 19 20 27 18 24 19 27 21 18
15 | 9 17 12 12 20 6 20 14 12 34 5 | 16 25 26 23 32 16 26 21 18 39 19
16E | 5 16 9 8 22 6 22 9 15 11 4 | 16 26 18 21 21 18 27 15 24 18 17
17 | 9 19 7 11 16 5 19 11 9 16 4 | 20 26 21 25 26 22 28 24 26 25 20
18 | 7 21 6 7 18 4 19 10 9 18 4 | 17 27 16 16 25 15 27 18 17 24 15
19 | 7 18 8 13 11 6 21 11 10 21 4 | 24 31 27 24 34 25 35 22 26 22 24
20 | 10 21 11 14 19 8 17 8 15 11 4 | 20 33 26 25 31 26 31 26 26 26 23
21 | 12 10 6 10 12 7 12 7 10 31 4 | 28 24 28 31 26 26 28 27 28 24 25
22 | 6 13 5 8 18 6 11 9 9 13 3 | 16 21 16 18 26 15 24 18 17 21 15
23 | 9 26 10 14 13 5 20 7 14 17 4 | 18 38 26 23 28 19 29 19 21 22 20
24 | 6 10 6 7 12 5 8 11 12 19 3 | 21 20 21 20 25 20 20 20 22 22 20
X25E | 23 --- 13 --- --- 22 --- 20 34 --- 13 | 1 --- 118 --- --- 1 --- 123 125 --- 1
26 | 5 15 10 8 17 5 12 12 7 14 3 | 14 20 18 16 23 13 20 15 15 17 13
27 | 6 15 5 10 12 5 12 10 11 16 3 | 15 21 14 18 20 11 21 14 16 14 13
28E | 8 17 8 12 20 7 19 10 9 10 4 | 27 33 27 32 34 30 34 33 37 33 29
X29 | 10 25 9 8 15 5 23 12 13 --- 5 | 17 28 20 17 27 16 30 16 17 --- 16
30E | 10 21 11 16 18 7 22 10 39 16 6 | 98 97 102 94 99 96 101 96 110 103 99
31 | 5 17 6 12 14 5 18 8 12 13 3 | 15 29 19 18 32 15 30 14 22 13 16
32E | 12 23 7 16 13 7 18 12 15 14 5 | 22 35 24 30 28 23 33 26 23 24 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 7 11 16 6 16 10 13 18 |T 24 29 28 25 31 23 29 27 29 26 24
WRMS | 8 17 7 11 14 5 15 9 9 17 |NE 19 26 23 22 29 19 26 21 22 24 20
MEDI | 8 17 7 10 15 6 16 10 10 16 |MD 18 26 21 23 27 19 26 20 23 24 20
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 4.1589 GPS week: 1589 MJD: 55367.0-55373.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 |U 7 9 24 |U 6 8 22 |U 8 8 23 |
emr | emr 2900 | 11 10 31 |U 8 9 24 | 9 11 26 |
esa | esa 2921 | 8 9 27 |U 8 9 22 | 8 8 24 |
gfz | gfz 2870 |U 8 8 25 |U 8 10 20 |U 9 9 27 |
grg | grg 2907 | 16 14 46 |U 45 81 395 | 13 20 38 |
igr | igr 2926 | 8 9 25 | 8 8 22 | 8 10 24 |
igs | igs 2925 | 9 11 28 | 6 7 23 | 8 9 24 |
jpl | jpl 2791 |U 11 11 32 | 9 10 27 |U 8 10 26 |
mit | mit 2962 |U 15 12 45 |U 8 9 24 |U 15 18 38 |
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 5.1589.0 GPS week: 1589 Day: 0 MJD: 55367.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 | 7 9 31 | 9 12 28 | 8 8 21 |
emr | emr 2872 | 10 11 37 | 9 12 25 | 10 11 21 |
esa | esa 2880 | 8 9 33 | 8 12 26 | 9 9 22 |
gfz | gfz 2872 | 8 9 32 | 8 12 27 | 11 9 28 |
grg | grg 2880 | 8 9 34 | 11 15 30 | 10 9 26 |
igr | igr 2903 | 8 10 33 | 9 12 27 | 9 11 21 |
igs | igs 2880 | 8 9 32 | 8 12 30 | 8 9 20 |
jpl | jpl 2780 | 8 11 41 | 10 13 32 | 8 11 18 |
mit | mit 2976 | 7 8 31 | 8 11 31 | 13 10 28 |
Table 5.1589.1 GPS week: 1589 Day: 1 MJD: 55368.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2970 | 8 10 24 | 4 6 22 | 7 6 21 |
emr | emr 2972 | 9 10 25 | 6 8 20 | 7 6 25 |
esa | esa 2976 | 7 9 21 | 4 6 16 | 7 5 22 |
gfz | gfz 2876 | 7 8 19 | 5 7 16 | 7 6 23 |
grg | grg 2976 | 39 35 98 | 10 9 21 | 23 36 45 |
igr | igr 2878 | 7 8 22 | 5 5 17 | 8 7 24 |
igs | igs 2925 | 7 9 22 | 4 5 17 | 7 5 22 |
jpl | jpl 2778 | 9 9 24 | 6 9 27 | 8 6 25 |
mit | mit 2976 | 7 9 21 | 5 5 20 | 8 6 23 |
Table 5.1589.2 GPS week: 1589 Day: 2 MJD: 55369.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2959 | 9 11 23 | 6 6 16 | 9 10 31 |
emr | emr 2876 | 9 13 30 | 6 6 22 | 9 14 36 |
esa | esa 2880 | 8 12 26 | 5 5 18 | 9 11 35 |
gfz | gfz 2876 | 9 12 28 | 5 5 18 | 9 11 33 |
grg | grg 2880 | 8 10 26 | 8 5 21 | 11 12 40 |
igr | igr 2908 | 8 13 27 | 6 5 21 | 10 12 36 |
igs | igs 2878 | 8 10 24 | 6 5 18 | 9 11 33 |
jpl | jpl 2774 | 9 13 26 | 7 6 22 | 8 12 33 |
mit | mit 2880 | 7 12 26 | 5 5 19 | 9 13 34 |
Table 5.1589.3 GPS week: 1589 Day: 3 MJD: 55370.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 | 8 9 29 | 5 8 18 | 6 8 21 |
emr | emr 2972 | 11 9 32 | 8 7 21 | 9 15 21 |
esa | esa 2880 | 7 9 31 | 5 8 21 | 6 10 20 |
gfz | gfz 2876 | 8 8 30 | 6 10 18 | 6 10 20 |
grg | grg 2880 | 8 11 34 | 7 8 20 | 8 10 22 |
igr | igr 2869 | 8 10 30 | 6 7 20 | 6 10 19 |
igs | igs 2909 | 8 8 29 | 5 7 19 | 7 12 20 |
jpl | jpl 2778 | 10 11 34 | 5 8 25 | 7 12 20 |
mit | mit 2976 | 10 13 29 | 6 5 27 | 17 40 35 |
Table 5.1589.4 GPS week: 1589 Day: 4 MJD: 55371.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 7 6 25 | 6 6 21 | 8 9 23 |
emr | emr 2858 | 14 10 36 | 7 6 22 | 11 13 21 |
esa | esa 2880 | 10 8 34 | 7 7 25 | 10 8 21 |
gfz | gfz 2844 | 8 6 28 | 5 7 17 | 10 11 31 |
grg | grg 2976 | 17 9 75 | 253 512 2611 | 17 60 74 |
igr | igr 2930 | 9 9 26 | 5 5 20 | 9 10 21 |
igs | igs 2941 | 14 25 47 | 5 6 23 | 9 9 23 |
jpl | jpl 2774 | 20 11 45 | 7 8 23 | 9 10 21 |
mit | mit 2976 | 59 29 166 | 5 6 24 | 9 8 23 |
Table 5.1589.5 GPS week: 1589 Day: 5 MJD: 55372.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 7 8 18 | 5 9 19 | 10 8 23 |
emr | emr 2876 | 12 10 30 | 8 7 20 | 12 10 34 |
esa | esa 2976 | 9 9 23 | 5 6 17 | 11 8 28 |
gfz | gfz 2874 | 8 7 19 | 5 9 18 | 11 8 29 |
grg | grg 2880 | 11 8 23 | 8 6 24 | 12 9 29 |
igr | igr 2973 | 8 8 21 | 5 6 19 | 12 11 28 |
igs | igs 2973 | 10 8 22 | 5 8 20 | 10 8 27 |
jpl | jpl 2779 | 12 11 30 | 7 12 26 | 14 13 39 |
mit | mit 2976 | 10 8 20 | 6 6 21 | 13 14 33 |
Table 5.1589.6 GPS week: 1589 Day: 6 MJD: 55373.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 | 6 8 18 | 10 11 31 | 6 6 23 |
emr | emr 2875 | 10 7 29 | 13 14 37 | 9 9 23 |
esa | esa 2976 | 7 7 20 | 21 16 31 | 7 6 23 |
gfz | gfz 2877 | 7 6 19 | 25 23 27 | 7 7 23 |
grg | grg 2880 | 17 15 34 | 20 13 39 | 8 7 26 |
igr | igr 3027 | 7 6 18 | 20 16 30 | 6 7 22 |
igs | igs 2973 | 6 7 18 | 10 10 32 | 6 6 22 |
jpl | jpl 2875 | 11 9 26 | 19 14 35 | 7 7 22 |
mit | mit 2976 | 8 8 19 | 21 22 25 | 37 39 93 |
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 6.1589 GPS week: 1589 MJD: 55367.500-55373.500
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 | 23 -30 -12 65 -3 | 5 12
| 10 32 82 96 5 | 1
emr uuuxu | 39 -3 96 385 -6 | 31 35
| 16 23 172 84 9 | 2
esa uuuuu | -52 -2 19 -51 -5 | 17 22
| 25 24 92 38 7 | 2
gfz uuuuu | 5 40 -76 -11 0 | 9 17
| 13 11 45 63 5 | 4
grg uuuux | 22 -85 69 -17 9 | -1 24
| 67 43 97 181 30 | 2
igr xxxxx | 8 16 -7 73 -1 | 7 15
| 29 20 74 64 5 | 2
irf xxxxx | 0 4 1 -20 -5 | 9 21
| 17 12 42 30 9 | 6
jpl uuuuu | 41 -13 125 56 3 | 12 15
| 25 29 143 121 6 | 1
mit uuuuu | -12 -5 -8 -147 2 | 7 15
| 25 17 65 40 5 | 1
ngs uuuuu | 3 -1 -68 239 -2 | 7 14
| 38 26 120 148 4 | 3
sio uuuuu | 32 42 -87 -5 2 | 14 19
| 27 21 61 63 3 | 1
Table 7.1589.0 GPS week: 1589 Day: 0 MJD: 55367.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 33 -33 -105 258 3 | 4 12
emr uuuxu | 32 -39 452 218 -20 | 30 34
esa uuuuu | -36 4 90 -2 5 | 15 22
gfz uuuuu | 28 23 -86 10 7 | 6 17
grg uuuux | -116 -22 116 -335 45 | -4 22
igr xxxxx | 11 7 -84 40 6 | 5 15
irf xxxxx | 21 -11 9 -9 -18 | 19 34
jpl uuuuu | 81 -16 -88 67 1 | 11 15
mit uuuuu | 12 -22 -15 -136 -4 | 8 16
ngs uuuuu | -37 31 -282 414 -1 | 5 13
sio uuuuu | 57 19 -44 24 -1 | 14 20
Table 7.1589.1 GPS week: 1589 Day: 1 MJD: 55368.500
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 | 31 -58 45 70 4 | 4 13
emr uuuxu | 49 -9 6 434 2 | 30 34
esa uuuuu | -37 -28 -20 -69 -2 | 16 23
gfz uuuuu | -11 50 -13 39 -1 | 7 17
grg uuuux | 21 -89 46 -120 -3 | -2 24
igr xxxxx | 27 -20 72 -27 5 | 6 15
irf xxxxx | 14 9 7 -34 -15 | 16 33
jpl uuuuu | 27 -39 264 58 2 | 12 15
mit uuuuu | 9 3 10 -174 -4 | 8 16
ngs uuuuu | -16 20 -65 255 4 | 5 13
sio uuuuu | 56 57 -109 -75 -3 | 15 20
Table 7.1589.2 GPS week: 1589 Day: 2 MJD: 55369.500
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 | 26 13 -10 105 -8 | 4 12
emr uuuxu | 53 -2 125 403 -9 | 31 35
esa uuuuu | -68 21 -22 -30 -1 | 15 22
gfz uuuuu | 12 39 -85 12 4 | 7 17
grg uuuux | 29 -69 47 13 -16 | -1 24
igr xxxxx | 39 10 27 80 1 | 6 15
irf xxxxx | 13 2 46 5 -6 | 10 26
jpl uuuuu | 36 -18 121 -62 -4 | 11 15
mit uuuuu | 9 -10 24 -123 0 | 6 15
ngs uuuuu | -31 -24 -27 180 2 | 5 14
sio uuuuu | 61 33 -53 67 1 | 13 18
Table 7.1589.3 GPS week: 1589 Day: 3 MJD: 55370.500
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 | 16 -60 -104 -15 -1 | 3 11
emr uuuxu | 46 -21 65 394 -15 | 30 35
esa uuuuu | -38 19 27 -95 -6 | 15 22
gfz uuuuu | 12 44 -27 -47 -1 | 8 17
grg uuuux | 39 -145 195 -5 -4 | -2 24
igr xxxxx | 24 41 104 98 -3 | 5 15
irf xxxxx | -12 24 -79 -55 3 | 3 13
jpl uuuuu | 47 -40 337 -66 0 | 10 12
mit uuuuu | -33 23 -136 -172 6 | 6 14
ngs uuuuu | 5 -32 -37 414 -4 | 6 14
sio uuuuu | 22 75 -182 -78 5 | 13 18
Table 7.1589.4 GPS week: 1589 Day: 4 MJD: 55371.500
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 | 32 16 -55 42 -6 | 5 9
emr uuuxu | 56 3 111 485 0 | 32 35
esa uuuuu | -103 -37 -139 -102 -5 | 19 21
gfz uuuuu | -5 30 -143 -60 -4 | 12 15
grg uuuux | 85 -62 -115 114 -33 | 0 23
igr xxxxx | -3 35 -67 181 -7 | 8 14
irf xxxxx | -21 8 13 32 -1 | 5 12
jpl uuuuu | 66 45 136 276 5 | 11 13
mit uuuuu | -45 1 44 -72 4 | 8 15
ngs uuuuu | 34 -23 71 -12 -3 | 9 12
sio uuuuu | -4 57 -17 68 1 | 15 19
Table 7.1589.5 GPS week: 1589 Day: 5 MJD: 55372.500
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 -42 30 19 -2 | 7 12
emr uuuxu | 19 21 -13 357 3 | 34 38
esa uuuuu | -38 17 146 -18 -14 | 21 24
gfz uuuuu | -2 41 -107 77 1 | 15 18
grg uuuux | 17 -135 64 -26 32 | -1 24
igr xxxxx | 5 17 -38 47 -4 | 11 15
irf xxxxx | -17 -8 37 -38 1 | 7 14
jpl uuuuu | 15 -6 26 -12 6 | 14 17
mit uuuuu | -37 -25 55 -180 6 | 9 17
ngs uuuuu | 70 25 -164 242 -8 | 12 15
sio uuuuu | 5 22 -56 -47 7 | 16 21
Table 7.1589.6 GPS week: 1589 Day: 6 MJD: 55373.500
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 | 15 -46 116 -24 -9 | 6 12
emr uuuxu | 16 25 -77 403 -5 | 32 35
esa uuuuu | -43 -10 52 -40 -14 | 18 22
gfz uuuuu | 0 53 -69 -106 -7 | 13 17
grg uuuux | 82 -73 128 239 41 | 1 24
igr xxxxx | -48 19 -61 90 -4 | 10 15
irf xxxxx | 1 1 -25 -37 1 | 4 13
jpl uuuuu | 19 -20 77 130 14 | 13 17
mit uuuuu | 0 -6 -39 -174 5 | 7 15
ngs uuuuu | -3 -3 30 178 -5 | 10 15
sio uuuuu | 25 29 -150 9 2 | 14 19
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