[IGSREPORT-18729] Wk 1588 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jul 1 05:32:19 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1588 (Jun 13, 2010 - Jun 19, 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:
igs1588[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1588[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1588[0-6].cls IGS GPS clock combination summary report.
igs15887.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15887.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 | ALL | 1
0 | COD | 1 DGAR
0 | EMR | 10 10 30 WTZR KERG WTZR
0 | ESA | DGAR KOKB METS
0 | GFZ | IRKJ KOKB MDVJ METS
0 | GRG | DGAR ONSA
0 | JPL | 10 32
0 | MIT | 9 32 9 32 CAS1 NNOR CAS1 IRKJ NNOR
1 | COD | DGAR SUTM
1 | EMR | 10 10 32 WTZR KERG
1 | ESA | DGAR KOKB METS
1 | GFZ | KOKB METS SUTH
1 | GRG | DGAR ONSA
1 | JPL | 32
1 | MIT | 8 25 32 8 25 32 HOB2 KARR MAW1 SYOG CEDU HOB2 MAW1
1 | MIT | NYA1 SYOG
2 | ALL | 1 1
2 | COD | USNO DGAR USNO
2 | EMR | WTZR THU3 WTZR WUHN
2 | ESA | HOB2 KARR DGAR HOB2 IRKJ KARR KOKB METS
2 | GFZ | KOKB METS SUTH UNSA
2 | GRG | DGAR IRKJ ONSA
2 | JPL | 32 IRKJ
2 | MIT | 25 32 SOFI
3 | COD | 27 MAW1 CHUR DGAR MAW1
3 | EMR | 21 21
3 | ESA | 1 1 KOKB WTZR DGAR IRKJ KOKB UNSA YAKT
3 | GFZ | 21 KOKB METS SUTH YAKT
3 | GRG | DGAR IRKJ USUD
3 | JPL | 27 32
3 | MIT | 21 25 21 25 MDVJ
4 | ALL | 27
4 | COD | DGAR
4 | EMR | 30 KERG WTZR
4 | ESA | DGAR KOKB
4 | GFZ | KOKB MDVJ METS SUTH
4 | GRG | DGAR IRKJ SPT0
4 | JPL | 30 32
4 | MIT | 25 25 30
5 | COD | DGAR
5 | EMR | 1 1 WTZR WTZR
5 | ESA | 27 27 KOKB DGAR IRKJ KERG UNSA YAKT
5 | GFZ | 30 ARTU MDVJ SUTH YAKT
5 | GRG | DGAR IRKJ TSKB ULAB USUD
5 | JPL | 30 32
5 | MIT | 27 30 27 30
6 | COD | 1 1 DGAR
6 | EMR | 30 30 WTZR MATE WTZR
6 | ESA | DGAR IRKJ KOKB
6 | GFZ | KOKB MDVJ METS SUTH UNSA
6 | GRG | DGAR IRKJ WTZR
6 | JPL | 30
6 | MIT | 30 30
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
----+--------+---------------
1 | COD | 25
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G10 | | | | 1 | | | |
PRN G25 | 2 | 1 | | | | 1 | |
7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products,
including the IGS combined orbits, are based on the IGS realization of the
ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447.
8. Small rotations were applied to 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 | .7 .4 1.6 -11 -8 0 -.24
EMR | 9.6 -1.2 -2.7 28 8 -4 .30
ESA | 6.7 .0 14.9 7 24 -56 -.12
GFZ | -.3 2.2 .0 7 28 -101 .24
GRG | 4.2 8.1 11.8 -8 25 -21 .16
JPL | 8.6 1.4 -8.5 -14 -56 -55 .06
MIT | 7.0 -1.6 7.3 10 3 -37 -.11
NGS | 10.5 -4.7 3.6 -78 -163 31 -.01
SIO | 4.0 -3.7 -10.9 -39 -91 9 .18
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by 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.
11. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna
model is introduced (IGSMAIL #5272). The antenna phase center offsets and
phase center variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1588.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1588.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 2.1588.[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 3.1588.[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 5.1588.0-6).
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 1588 summary. (Jun 13, 2010 - Jun 19, 2010)
Table 1.1588.a GPS week: 1588 MJD: 55360.000-55366.000
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 244| 0 0 -1 -12 -25 -41 -.21 10 9 | -337 -495 18 77
| 0 0 0 8 13 21 .02 | 484 684
emr 104| 1 0 -5 -41 3 38 .35 19 19 | -2587 325 19 88
| 0 1 1 26 19 22 .03 | 1742 808
esa 140| 1 0 0 -54 -70 -39 .28 8 8 | -499 -217 14 123
| 0 1 1 22 18 20 .01 | 983 1987
gfz 199| 0 0 3 -57 -124 1 -.19 10 10 | 182 -155 21 108
| 1 1 1 40 70 11 .05 | 299 615
grg 126| 0 0 10 -26 -89 21 .61 17 14 | 1428588 -13 47 200
| 1 1 2 22 18 14 .05 | 3779636 501
igr n/a| 0 0 -1 3 -20 8 -.03 5 5 | 4036 457 17 63
| 0 0 0 17 19 17 .02 | 2173 779
jpl 134| 0 0 -10 5 81 61 .48 17 16 | -500 175 18 99
| 1 1 1 11 11 41 .04 | 1565 719
mit 254| 0 -1 0 -27 -80 22 -.30 11 9 | -301 117 21 163
| 0 0 0 17 16 13 .03 | 352 543
ngs 215| 0 0 0 184 288 -6 -.20 11 8 | 463322 -338825 2126 3844
| 1 0 2 17 44 10 .03 | 368741 339543
sio 266| -4 0 1 62 119 25 -.35 18 18 | --- --- --- ---
| 1 0 1 17 26 13 .03 | --- ---
Table 1.1588.b GPS week : 1588 MJD: 55360.000-55366.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 13 9 11 11 11 13 18 |
2 | 5 5 5 5 5 5 6 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 3 3 4 4 4 |
5 | 4 5 5 5 4 4 5 |
6 | 4 4 4 3 3 4 4 |
7 | 5 5 5 4 4 5 6 |
8 | 4 4 4 4 4 4 4 |
9 | 4 4 5 4 4 4 4 |
10 | 6 6 6 5 6 5 5 |
11 | 4 4 4 3 4 4 4 |
12 | 5 6 5 5 5 5 6 |
13 | 5 4 5 5 5 5 6 |
14 | 4 4 4 4 4 4 4 |
15 | 5 5 4 4 4 5 5 |
16 | 5 5 5 5 4 6 5 |
17 | 5 5 5 5 5 5 6 |
18 | 6 5 5 5 4 5 5 |
19 | 4 4 5 5 5 4 5 |
20 | 4 4 3 4 4 4 4 |
21 | 4 5 4 4 4 5 5 |
22 | 3 4 4 4 5 4 4 |
23 | 5 4 5 5 5 5 6 |
24 | 3 3 3 3 3 4 4 |
25 | 0 25 15 21 27 0 24 |
26 | 4 4 3 3 3 3 4 |
27 | 4 4 4 4 3 4 4 |
28 | 5 5 6 5 4 5 4 |
29 | 4 5 5 5 4 5 5 |
30 | 6 6 6 6 7 7 7 |
31 | 4 4 4 4 5 4 4 |
32 | 7 5 5 6 6 6 6 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1588.0 GPS week: 1588 Day: 0 MJD: 55360.000
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 244| 0 0 -2 -2 -1 -32 -.21 9 8 | 364 -1319 16 79
| 23 -56 |
emr 104| 2 0 -5 -48 -8 30 .34 18 18 | -3954 206 17 86
| -25 -42 |
esa 140| 1 0 1 -70 -63 -66 .26 7 7 | -1361 1788 11 102
| -27 21 |
gfz 199| 0 0 3 -55 -211 15 -.23 10 10 | 737 -1514 22 109
| -89 16 |
grg 126| 1 -1 10 -41 -88 34 .71 20 17 | 223 -208 44 200
| 122 16 |
igr n/a| 0 0 -1 -23 -22 -10 -.02 6 5 | 2260 178 18 63
| -46 22 |
jpl 134| 2 -1 -11 1 87 52 .54 17 16 | -1620 31 17 115
| 32 -28 |
mit 254| 0 0 0 -24 -99 24 -.28 11 8 | -101 -552 22 180
| 4 36 |
ngs 215| 0 0 1 173 330 10 -.16 10 7 | 251307 -203787 2015 3896
| 22 -78 |
sio 266| -5 1 0 63 83 29 -.31 18 19 | --- --- --- ---
| -94 -42 |
Table 2.1588.1 GPS week: 1588 Day: 1 MJD: 55361.000
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 244| 0 0 -1 -6 -21 -55 -.20 10 9 | -1032 452 20 88
| 20 -38 |
emr 104| 0 3 -7 9 -15 68 .36 19 19 | -4187 85 18 102
| -66 -40 |
esa 140| 1 0 2 -70 -58 -59 .28 8 7 | -1493 2234 13 116
| -19 29 |
gfz 199| 1 0 2 -93 -102 15 -.21 11 11 | -36 57 21 106
| -78 9 |
grg 126| 0 1 5 -14 -79 23 .61 17 14 | -322 453 46 187
| 66 2 |
igr n/a| 0 0 -2 23 3 34 -.04 5 5 | 2040 126 16 55
| -34 22 |
jpl 134| 0 0 -10 22 80 83 .49 17 16 | -2056 46 19 101
| 6 -6 |
mit 254| -1 -2 0 -18 -83 27 -.28 10 8 | -817 592 22 173
| 7 30 |
ngs 215| 2 -1 1 182 273 -10 -.24 12 8 | 707366 -385910 2043 3705
| 48 -68 |
sio 266| -6 0 1 69 96 38 -.37 17 19 | --- --- --- ---
| -96 -48 |
Table 2.1588.2 GPS week: 1588 Day: 2 MJD: 55362.000
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 244| 0 0 0 -29 -44 -26 -.22 12 9 | -551 -468 18 71
| 66 -31 |
emr 104| 2 0 -5 -33 -18 46 .32 17 17 | -4707 2040 21 78
| -52 -16 |
esa 140| 2 0 -1 -58 -75 -42 .27 7 6 | -1191 343 14 124
| -17 41 |
gfz 199| 0 2 5 -42 -41 -16 -.19 11 11 | -72 274 22 107
| -48 22 |
grg 126| 0 0 8 -65 -68 19 .60 17 14 | -313 276 53 198
| 132 -11 |
igr n/a| 0 0 0 23 -29 24 -.03 5 5 | 1594 2100 19 58
| -31 27 |
jpl 134| -2 0 -10 3 77 100 .47 16 15 | -2353 1728 18 95
| -13 -2 |
mit 254| 0 -1 2 -3 -59 7 -.30 11 9 | -583 708 16 134
| -2 18 |
ngs 215| 0 -1 0 193 242 -20 -.22 12 9 | -350 -710 1956 3712
| -12 37 |
sio 266| -4 0 1 88 111 14 -.38 17 19 | --- --- --- ---
| -110 -53 |
Table 2.1588.3 GPS week: 1588 Day: 3 MJD: 55363.000
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 244| 0 0 -2 -16 -15 -51 -.20 10 8 | 114 -1356 22 88
| 35 -50 |
emr 104| 2 1 -6 -38 1 57 .36 19 19 | -2384 -133 24 89
| -60 -50 |
esa 140| 1 0 0 -67 -90 -23 .28 7 7 | 61 -1205 19 165
| 10 28 |
gfz 199| 0 1 3 -34 -52 -2 -.23 10 10 | 368 -119 22 123
| -41 31 |
grg 126| 0 0 11 -20 -70 21 .54 16 14 | 240 -735 47 222
| 119 -24 |
igr n/a| -1 0 0 3 -53 21 -.04 5 4 | 3927 222 19 84
| -24 -1 |
jpl 134| -2 0 -13 19 103 -24 .41 19 17 | -475 -232 22 99
| -17 -120 |
mit 254| 0 -1 1 -38 -84 34 -.29 10 9 | -80 -474 18 163
| 3 21 |
ngs 215| 0 0 0 201 246 -1 -.17 11 7 | 711451 -388521 2140 3857
| -10 39 |
sio 266| -4 0 3 42 109 27 -.37 17 18 | --- --- --- ---
| -110 -75 |
Table 2.1588.4 GPS week: 1588 Day: 4 MJD: 55364.000
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 244| 0 0 -2 -9 -29 -5 -.18 11 8 | -740 196 19 80
| 53 -16 |
emr 104| 1 1 -3 -77 20 5 .39 19 19 | -1405 74 19 93
| -32 -60 |
esa 140| 2 0 0 -60 -78 -28 .30 8 8 | -974 488 14 124
| 9 30 |
gfz 199| 0 0 4 -21 -88 -6 -.17 9 9 | -27 229 21 105
| -36 36 |
grg 126| 0 1 10 -30 -108 9 .62 16 14 | 9999999 691 45 198
| 135 49 |
igr n/a| 0 0 -1 -11 -6 -6 .00 5 5 | 5448 344 18 62
| -28 4 |
jpl 134| 0 0 -10 5 77 80 .45 18 18 | 615 -35 18 102
| 11 2 |
mit 254| 0 0 0 -23 -67 0 -.31 11 9 | -538 692 21 168
| 0 23 |
ngs 215| -1 -1 -3 154 264 -1 -.19 11 7 | 714576 -392369 2047 3597
| -46 -11 |
sio 266| -3 0 2 76 144 4 -.32 19 17 | --- --- --- ---
| -127 -84 |
Table 2.1588.5 GPS week: 1588 Day: 5 MJD: 55365.000
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 244| 0 0 -2 -11 -31 -65 -.19 9 9 | -327 -406 17 69
| 56 -24 |
emr 104| 1 -1 -6 -55 13 46 .37 19 19 | -1450 466 17 76
| -43 -48 |
esa 140| 1 2 0 -48 -38 -9 .27 9 9 | 606 -3165 15 123
| 21 18 |
gfz 199| -2 1 2 -25 -205 -2 -.18 10 10 | 16 29 21 103
| -59 12 |
grg 126| 3 0 12 -13 -116 -1 .59 16 15 | -71 -220 48 226
| 120 27 |
igr n/a| 0 0 -2 3 -6 -2 -.01 5 5 | 5724 595 17 63
| -32 16 |
jpl 134| 0 0 -8 -4 74 50 .48 16 15 | 635 188 18 96
| 86 19 |
mit 254| 0 -1 0 -24 -101 27 -.30 12 10 | -176 -63 22 161
| 17 38 |
ngs 215| 1 -1 0 177 360 -17 -.18 12 10 | -274 -481 2414 3828
| -33 -61 |
sio 266| -2 0 2 53 132 42 -.35 21 18 | --- --- --- ---
| -102 -83 |
Table 2.1588.6 GPS week: 1588 Day: 6 MJD: 55366.000
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 244| -1 0 -1 -13 -31 -55 -.24 10 10 | -190 -567 16 65
| 29 -19 |
emr 104| 1 0 -4 -46 31 18 .33 20 20 | -25 -460 17 96
| -52 -66 |
esa 140| 0 0 1 -5 -86 -42 .28 9 9 | 853 -2002 16 109
| -31 59 |
gfz 199| 0 -1 1 -130 -169 6 -.10 12 12 | 291 -43 24 109
| -63 -2 |
grg 126| 1 1 12 2 -93 39 .58 16 14 | 361 -350 46 169
| 57 -33 |
igr n/a| 0 -1 -1 7 -33 -3 -.04 5 5 | 7259 -364 17 59
| -17 24 |
jpl 134| 1 2 -10 -7 70 87 .49 18 17 | 1751 -496 16 88
| 6 -19 |
mit 254| 0 -1 0 -61 -69 34 -.37 13 10 | 188 -82 29 167
| 11 28 |
ngs 215| 0 0 -3 206 301 -3 -.19 11 9 | 859183 -999999 2272 4316
| -6 6 |
sio 266| -3 0 1 41 158 24 -.36 20 18 | --- --- --- ---
| -117 -87 |
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 3.1588.0 GPS week: 1588 Day: 0 MJD: 55360.000
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 | 14 30 --- --- --- 27 --- 19 28 --- 12 | 59 68 --- --- --- 74 --- 65 68 --- 60
2 | 9 18 5 11 17 6 18 9 9 34 4 | 21 30 23 24 23 25 32 28 27 37 24
3 | 9 15 7 7 18 3 11 5 13 19 3 | 21 21 23 24 25 21 23 22 30 29 22
4 | 7 13 6 7 20 6 10 10 13 9 3 | 24 21 21 27 26 23 19 27 26 27 23
5E | 10 21 7 14 21 5 16 7 9 12 4 | 29 35 30 38 42 30 33 27 37 30 30
6 | 8 12 10 6 17 3 11 5 13 17 3 | 21 21 28 27 27 22 23 24 31 28 25
7 | 10 19 8 9 27 3 17 12 8 17 4 | 20 28 21 16 36 17 30 25 26 25 20
8 | 7 15 6 9 23 4 16 10 9 13 4 | 19 24 23 24 36 19 29 23 28 26 21
9 | 7 17 7 13 13 6 15 19 6 13 4 | 16 23 20 21 22 16 22 20 24 17 17
10E | 18 23 12 14 26 8 16 22 15 18 6 | 66 76 72 79 83 72 77 78 74 81 73
11 | 5 15 7 8 12 4 19 9 6 20 3 | 24 36 28 31 37 25 37 24 30 21 26
12 | 14 27 10 10 22 9 25 9 8 19 5 | 41 51 42 43 46 44 49 46 45 50 43
13 | 6 22 5 13 23 5 21 12 10 16 4 | 14 30 17 18 37 15 29 17 18 15 14
14 | 6 22 8 9 13 5 20 7 6 14 3 | 14 27 19 20 25 16 24 15 21 18 15
15 | 7 19 10 11 18 6 24 12 10 11 4 | 13 26 17 17 29 14 27 17 21 19 14
16 | 10 22 5 11 17 7 21 4 13 17 4 | 38 44 36 43 40 40 44 39 44 43 39
17 | 11 15 6 11 21 6 17 12 12 26 4 | 24 27 23 28 26 25 28 26 31 31 24
18E | 15 22 6 9 30 6 23 16 8 22 5 | 25 33 25 25 31 23 34 29 34 32 26
19 | 6 14 6 9 16 4 17 10 8 24 4 | 24 26 22 21 24 22 28 21 27 22 22
20E | 9 18 7 10 14 6 12 6 10 14 3 | 41 48 46 43 47 44 46 43 45 41 43
21 | 10 15 5 9 9 4 18 7 12 24 4 | 20 25 18 13 23 18 32 17 19 20 18
22E | 8 14 5 7 17 5 12 6 7 17 3 | 19 28 23 22 29 22 30 23 28 29 23
23 | 7 23 6 13 20 8 22 10 7 18 4 | 12 31 17 19 26 15 28 16 19 15 13
24 | 6 13 5 7 17 4 9 5 4 16 3 | 24 23 26 26 29 27 21 24 34 27 26
X25E | 4 --- --- --- --- 89 --- --- --- --- 0 | 67 --- --- --- --- 63 --- --- --- --- 66
26 | 5 12 9 10 12 6 15 12 12 18 4 | 13 17 15 14 22 12 23 16 21 18 14
27 | 5 19 5 11 15 4 12 11 5 11 3 | 17 26 21 23 29 19 22 19 25 19 20
28 | 9 23 10 9 26 5 15 10 9 12 4 | 35 41 33 39 36 33 32 38 35 36 33
X29 | 7 15 8 11 17 7 19 9 10 --- 4 | 23 31 26 25 28 25 35 24 30 --- 25
30E | 13 23 10 11 19 8 18 14 14 27 5 | 50 58 46 48 52 47 55 54 57 40 50
31 | 6 15 7 12 27 8 16 9 8 16 4 | 17 24 18 18 32 18 28 19 23 17 17
X32E | 10 --- 9 24 32 8 16 13 21 13 6 | 40 --- 39 42 38 40 37 41 44 37 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 7 10 20 6 17 11 10 18 |T 27 33 27 28 33 28 32 29 32 29 28
WRMS | 8 18 7 10 17 5 16 8 7 19 |NE 19 25 21 21 28 19 27 21 25 22 20
MEDI | 8 18 7 10 18 6 16 10 9 17 |MD 23 28 23 24 29 23 29 24 30 27 24
Table 3.1588.1 GPS week: 1588 Day: 1 MJD: 55361.000
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 29 16 --- --- 19 --- 15 19 --- 8 | 29 34 26 --- --- 36 --- 25 35 --- 29
2 | 6 20 7 11 13 5 18 12 12 32 5 | 18 21 15 19 20 16 23 18 21 30 15
3 | 10 14 7 8 14 3 11 5 11 19 3 | 20 24 20 19 28 22 25 23 32 27 22
4 | 7 17 7 9 12 6 11 7 16 9 3 | 18 19 20 18 18 13 14 17 21 15 16
5E | 7 21 8 12 18 6 18 9 11 16 4 | 19 27 22 23 31 18 24 20 19 24 19
6 | 9 12 6 9 14 3 11 5 13 19 3 | 16 20 17 18 26 18 21 19 30 25 18
7 | 14 19 7 15 20 3 15 11 10 18 4 | 21 28 20 19 33 17 27 22 26 20 18
8 | 5 17 8 9 16 5 15 9 6 15 3 | 16 24 20 16 31 14 25 18 21 20 16
9 | 9 18 7 8 13 7 14 15 12 12 4 | 18 24 19 19 23 17 25 24 22 23 18
10E | 20 23 11 11 15 7 18 23 14 20 6 | 59 66 62 64 65 61 66 67 62 71 62
11 | 5 15 5 7 11 5 16 9 9 18 3 | 20 35 25 20 34 25 35 22 31 14 23
12E | 11 30 10 16 23 9 22 8 13 15 5 | 36 43 37 45 44 36 41 42 41 44 38
13 | 7 19 6 13 21 5 22 8 7 13 4 | 13 28 17 18 34 14 28 16 16 15 14
14 | 7 20 7 8 19 4 20 7 11 11 4 | 14 28 17 16 26 16 26 15 26 18 17
15 | 7 21 8 12 21 5 20 10 6 12 4 | 12 27 15 15 26 12 23 16 18 20 12
16 | 10 24 8 11 16 4 25 5 10 16 4 | 50 55 50 50 54 49 55 50 54 51 50
17 | 12 17 11 13 12 5 17 6 10 22 4 | 16 22 18 21 20 15 23 18 22 21 16
18E | 15 21 8 11 19 4 18 15 11 16 5 | 35 45 40 44 41 36 41 40 40 40 37
19 | 8 15 7 7 13 4 16 10 13 25 4 | 17 21 15 12 17 15 22 15 27 16 14
20 | 15 15 9 9 12 5 12 6 6 15 3 | 60 67 63 63 62 62 64 63 63 60 61
21 | 14 16 7 11 9 5 17 10 12 23 4 | 16 28 15 12 26 14 28 14 23 12 15
22E | 7 15 7 9 16 4 12 6 14 16 3 | 25 30 26 26 32 26 32 27 33 31 26
23 | 6 21 8 12 17 5 21 7 6 16 4 | 13 28 17 14 27 13 26 16 19 15 13
24 | 7 12 6 5 14 5 9 5 11 17 3 | 19 20 21 18 21 19 21 23 33 25 22
X25E | 96 --- 32 --- --- 34 --- 41 25 --- 24 | 89 --- 9999 --- --- 117 --- --- --- --- 108
26 | 5 16 5 10 12 6 14 10 6 12 3 | 14 21 14 11 20 12 20 17 18 20 12
X27 | 8 17 7 5 16 8 --- 9 11 12 3 | 22 27 22 21 26 21 --- 25 25 25 21
28 | 10 16 8 7 28 6 13 8 14 13 4 | 52 49 48 46 48 47 49 52 52 53 49
X29 | 10 17 10 9 16 6 19 12 8 --- 4 | 21 27 23 24 30 22 29 20 24 --- 21
30E | 13 23 12 11 17 5 18 17 20 17 5 | 42 47 40 51 41 42 43 49 51 41 43
31 | 8 16 8 8 24 6 17 9 9 16 4 | 15 24 16 15 32 17 29 15 24 17 15
32E | 12 22 8 16 19 7 14 12 22 15 5 | 28 28 24 32 27 25 27 28 34 28 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 8 11 17 5 17 10 12 17 |T 26 31 25 26 32 27 31 26 31 28 27
WRMS | 9 19 7 11 14 5 16 8 8 19 |NE 16 24 18 17 25 16 24 18 23 19 16
MEDI | 9 17 8 9 16 5 17 9 11 16 |MD 19 28 20 19 28 18 27 22 26 24 19
Table 3.1588.2 GPS week: 1588 Day: 2 MJD: 55362.000
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 | 14 36 19 --- --- 20 --- 13 25 --- 10 | 25 54 19 --- --- 40 --- 29 46 --- 28
2 | 7 16 6 8 11 3 19 9 6 32 4 | 17 22 17 18 17 14 24 19 17 27 15
3 | 11 13 5 9 15 4 10 7 11 18 3 | 16 17 17 18 22 15 14 17 26 16 16
4 | 5 12 6 8 13 4 10 8 11 9 3 | 19 18 17 18 23 18 19 22 18 23 17
5E | 12 19 7 14 19 5 15 20 11 22 5 | 33 37 33 38 39 33 33 36 33 38 32
6 | 10 11 5 8 15 4 10 5 11 18 3 | 16 17 19 20 23 17 17 18 23 19 17
7 | 15 19 6 12 23 4 19 12 9 17 5 | 21 29 21 17 35 18 28 22 18 20 18
8 | 8 18 7 8 21 4 14 12 9 16 4 | 15 22 19 12 33 15 23 17 15 20 15
9 | 8 16 6 9 12 5 13 18 18 12 4 | 17 22 13 16 19 17 21 25 23 21 15
10E | 27 20 11 10 21 10 15 16 13 16 6 | 87 90 87 91 96 86 94 90 86 92 88
11 | 8 14 4 11 7 4 14 7 8 19 3 | 20 31 24 25 35 22 33 21 23 15 21
12E | 13 22 9 10 21 4 23 13 10 14 5 | 28 35 30 30 39 28 35 32 32 36 30
13 | 7 19 8 12 24 5 21 9 8 12 4 | 15 27 20 17 34 16 27 15 17 15 15
14 | 8 18 10 8 18 2 19 8 13 11 4 | 10 24 18 14 26 13 23 13 22 15 13
15 | 7 16 7 9 19 4 16 9 8 12 4 | 18 24 18 18 26 15 23 15 18 24 14
16 | 17 21 8 13 19 7 20 6 13 21 5 | 98 101 99 104 102 95 102 100 89 104 98
17 | 11 18 8 15 14 5 18 7 11 20 4 | 19 25 19 23 21 18 26 19 22 21 17
18E | 12 26 9 12 21 6 21 8 8 20 5 | 21 33 28 28 33 26 31 23 29 30 25
19 | 8 15 7 9 14 5 17 13 11 25 4 | 19 22 16 16 22 15 22 18 17 18 15
20 | 9 14 7 8 11 3 13 5 9 13 3 | 24 31 29 24 36 26 26 23 25 22 24
21 | 12 15 5 10 12 4 18 8 11 23 4 | 16 25 16 9 26 13 29 14 16 11 14
22E | 9 16 5 8 19 6 12 7 11 12 3 | 22 32 30 26 30 26 30 26 30 26 25
23 | 7 23 8 15 19 4 23 7 9 17 4 | 13 27 19 15 27 15 26 14 17 16 13
24 | 7 10 4 7 12 4 9 5 11 17 3 | 19 19 19 20 24 19 18 18 27 22 19
X25E | 27 --- 21 --- --- 22 --- 30 23 --- 14 | 107 --- 9999 --- --- 127 --- --- --- --- 132
26 | 6 14 4 9 13 5 11 9 8 13 3 | 18 19 13 15 19 14 18 16 16 23 13
27 | 7 18 6 9 14 5 12 12 15 12 4 | 19 24 15 17 20 17 21 21 24 20 16
28 | 29 13 11 16 12 7 18 9 8 11 5 | 77 90 91 92 88 81 89 86 86 88 86
X29 | 12 18 6 9 14 4 20 12 9 --- 4 | 19 29 25 23 28 21 30 19 22 --- 21
30E | 14 22 13 12 18 8 19 22 18 14 6 | 30 35 29 33 28 28 32 33 35 26 27
31 | 9 14 7 11 24 6 18 8 10 14 4 | 14 24 17 16 34 17 28 13 18 13 14
32E | 12 21 8 9 17 6 15 12 23 17 5 | 26 25 26 28 29 28 29 31 40 31 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 7 11 17 5 16 11 12 17 |T 28 33 27 28 34 29 32 27 30 29 29
WRMS | 9 17 6 11 14 5 15 9 9 19 |NE 17 23 18 17 25 16 23 17 19 18 15
MEDI | 9 18 7 9 15 5 16 9 11 16 |MD 19 25 19 18 28 18 26 21 23 22 17
Table 3.1588.3 GPS week: 1588 Day: 3 MJD: 55363.000
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 --- 17 --- --- 16 --- 11 27 --- 10 | 31 --- 24 --- --- 32 --- 26 46 --- 30
2 | 7 17 7 8 11 4 19 12 8 34 4 | 20 25 21 18 24 20 29 24 19 30 19
3 | 8 13 7 10 14 4 13 5 9 16 3 | 26 25 24 24 28 23 27 23 27 24 23
4 | 6 13 6 6 12 5 11 9 12 13 3 | 22 20 23 19 30 20 17 24 24 25 20
5 | 7 23 8 10 20 4 20 10 14 12 4 | 38 40 38 39 52 35 38 38 32 42 36
6 | 8 15 4 10 13 4 11 5 8 17 3 | 18 22 21 23 27 19 20 20 25 21 20
7 | 12 19 7 9 20 4 20 9 7 16 4 | 19 30 25 18 34 21 32 23 21 25 20
8 | 10 15 8 8 16 3 14 13 9 17 4 | 13 23 18 14 29 15 22 20 18 23 15
9 | 9 17 9 10 9 3 14 11 10 12 3 | 15 24 22 18 21 17 25 18 19 16 16
10E | 17 26 9 10 21 8 13 13 12 17 5 | 116 122 118 121 120 119 121 123 111 123 118
11 | 6 15 4 5 12 3 18 5 5 18 3 | 20 32 28 24 36 24 32 23 24 18 23
12E | 12 26 9 8 19 6 24 15 9 14 5 | 34 42 41 36 44 37 41 41 36 43 37
13 | 8 21 8 12 21 3 26 8 8 12 4 | 13 28 20 18 33 16 28 14 22 15 15
14 | 7 21 7 7 17 4 18 8 11 9 4 | 14 29 18 16 26 16 22 14 23 16 15
15 | 8 20 8 10 16 4 18 9 8 11 4 | 12 23 16 13 26 10 22 15 15 20 10
16E | 7 22 8 14 20 4 24 7 14 14 4 | 53 61 54 51 60 55 61 54 64 53 54
17 | 11 19 11 17 13 5 24 12 10 21 5 | 23 32 25 28 29 24 35 25 28 25 23
18E | 15 18 8 12 23 4 19 10 10 17 4 | 25 32 31 35 36 29 27 29 36 33 29
19 | 7 17 5 9 14 6 19 14 11 24 4 | 19 25 22 15 23 17 25 22 23 19 18
20 | 10 18 6 9 14 5 15 6 5 13 3 | 32 34 34 30 41 32 37 31 34 29 31
21 | 9 16 7 9 14 3 18 8 10 24 4 | 15 25 20 13 24 15 30 16 21 15 15
22E | 19 16 6 7 20 7 15 6 10 11 4 | 53 54 51 49 54 49 57 49 55 49 50
23 | 7 25 6 13 18 4 28 7 11 16 4 | 13 29 19 17 26 15 29 14 20 17 14
24 | 7 11 6 9 13 3 9 7 7 18 3 | 22 22 24 25 30 22 17 20 27 24 22
X25E | 29 --- 28 --- --- 26 --- 50 33 --- 20 | 136 --- 9999 --- --- 137 --- --- --- --- 145
26 | 6 15 6 9 11 4 12 9 10 10 3 | 14 19 16 13 20 12 21 13 16 14 11
27 | 7 17 7 9 12 4 13 7 12 14 3 | 12 24 17 16 20 15 21 13 17 16 13
28E | 18 17 7 8 18 5 26 11 10 26 5 | 61 72 67 70 74 69 75 70 74 76 69
X29 | 11 19 7 9 14 5 19 15 9 --- 4 | 23 32 28 27 32 27 31 27 32 --- 26
30E | 14 23 12 13 17 5 21 25 20 16 6 | 38 46 36 41 39 40 38 45 51 36 38
31 | 7 19 4 9 18 5 19 7 11 13 4 | 14 27 18 14 32 15 28 14 22 14 15
32E | 13 21 8 13 20 7 19 14 23 18 5 | 30 28 31 34 34 31 32 35 40 36 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 7 10 16 5 19 10 11 17 |T 31 34 30 29 36 32 34 29 32 30 31
WRMS | 8 19 7 10 14 4 17 9 7 18 |NE 17 25 21 18 27 18 25 19 22 19 17
MEDI | 8 18 7 9 16 4 18 9 10 16 |MD 22 28 24 23 30 22 29 23 25 24 22
Table 3.1588.4 GPS week: 1588 Day: 4 MJD: 55364.000
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 35 --- --- --- 22 --- 12 16 --- 10 | 20 44 --- --- --- 36 --- 23 32 --- 22
2 | 7 18 5 6 13 4 21 12 13 36 4 | 14 20 19 16 14 16 22 22 24 31 16
3 | 6 14 8 8 14 5 12 8 8 17 3 | 14 18 12 15 17 14 14 15 15 18 12
4 | 9 13 5 4 15 6 11 9 11 16 3 | 18 20 20 20 22 19 19 24 24 26 19
5 | 6 21 7 7 20 5 19 10 13 13 4 | 25 32 31 27 41 25 29 25 24 30 26
6 | 6 14 6 6 11 4 11 7 6 18 3 | 13 19 13 18 20 14 15 16 15 17 13
7 | 9 16 7 8 21 4 17 7 6 16 4 | 13 27 20 17 34 15 25 13 15 15 15
8 | 6 16 7 8 15 4 15 12 8 15 3 | 17 23 19 13 25 16 25 21 17 23 16
9 | 11 16 5 7 14 4 14 10 10 14 3 | 14 21 13 14 16 11 20 14 17 14 11
10 | 25 20 14 12 16 10 15 12 10 17 5 | 82 90 83 88 86 80 89 80 86 86 83
11 | 8 16 6 8 11 5 17 9 8 21 3 | 17 35 25 25 33 23 33 21 22 15 21
12E | 13 27 9 8 19 4 28 14 11 18 5 | 26 33 25 28 34 25 34 32 29 38 26
13 | 7 20 10 10 22 3 21 11 7 14 4 | 12 26 21 16 34 14 26 14 17 14 15
14 | 7 22 9 6 19 5 18 9 8 11 4 | 10 27 18 12 23 10 21 12 16 14 11
15 | 8 19 9 11 16 4 20 10 9 15 4 | 10 24 15 15 24 10 21 14 13 23 10
16E | 7 21 8 10 16 5 23 8 7 15 4 | 32 38 33 31 38 33 43 31 30 32 32
17 | 6 21 8 15 14 5 21 10 12 23 4 | 17 26 19 24 22 18 28 19 26 21 18
18 | 10 21 6 9 16 3 22 8 9 20 4 | 32 44 40 42 46 38 40 37 39 37 37
19 | 8 17 11 8 18 4 18 14 8 24 4 | 15 22 21 15 19 15 24 15 18 15 15
20 | 6 20 9 7 19 5 14 9 6 18 4 | 26 29 28 24 41 23 30 25 28 24 25
21 | 9 14 4 8 11 5 17 6 8 28 3 | 12 25 18 14 21 14 27 13 13 18 14
22 | 24 17 4 8 12 5 18 8 9 12 4 | 62 74 73 73 75 72 74 72 73 70 70
23 | 8 25 11 11 17 4 26 11 8 15 5 | 12 31 22 16 27 15 29 14 15 14 14
24 | 7 14 5 5 11 4 9 8 11 20 3 | 15 18 19 19 22 17 14 16 19 18 16
X25E | 67 --- 27 --- --- 18 --- 48 38 --- 26 | 135 --- 9999 --- --- 125 --- --- --- --- 131
26 | 6 14 8 10 9 4 13 5 10 12 3 | 12 18 14 12 18 10 18 13 14 16 10
27 | 7 13 6 6 12 4 12 5 9 14 3 | 12 17 13 12 19 9 17 11 14 14 10
28E | 5 17 7 8 18 6 18 11 8 21 4 | 37 39 36 38 40 37 40 38 42 41 37
X29 | 10 19 8 8 14 5 19 12 6 --- 4 | 19 27 24 21 29 20 28 19 20 --- 20
30E | 16 24 14 11 15 5 20 28 26 21 7 | 34 42 32 36 39 33 39 45 44 39 34
31 | 7 20 9 7 25 6 19 9 10 12 4 | 11 24 15 11 33 11 25 13 16 12 12
32E | 16 23 9 14 18 8 15 15 21 24 5 | 25 27 24 27 28 25 27 27 35 30 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 8 9 16 5 18 11 11 19 |T 25 30 25 24 31 26 29 24 26 26 26
WRMS | 8 19 8 9 14 5 18 9 7 17 |NE 13 23 18 16 23 14 22 15 17 17 14
MEDI | 8 19 8 8 15 5 18 10 9 17 |MD 17 27 20 18 27 17 26 19 20 21 16
Table 3.1588.5 GPS week: 1588 Day: 5 MJD: 55365.000
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 | 17 32 --- --- --- 37 --- 18 28 --- 13 | 31 36 --- --- --- 39 --- 21 35 --- 22
2 | 10 15 9 10 9 5 17 11 10 41 5 | 13 20 16 16 14 16 24 20 22 38 15
3 | 8 16 8 8 17 4 11 11 9 21 4 | 24 25 26 26 26 25 26 30 36 30 26
4 | 8 13 11 7 9 7 9 10 12 20 3 | 19 19 21 19 25 18 23 23 24 25 19
5 | 8 22 10 11 20 6 14 8 8 16 4 | 22 27 26 25 37 21 27 22 26 26 22
6 | 8 14 8 8 13 4 10 10 8 19 3 | 20 21 23 19 24 22 22 26 32 23 22
7 | 14 19 8 10 20 4 17 13 11 18 5 | 17 28 18 20 34 17 29 16 18 17 16
8 | 8 18 9 9 16 3 12 12 11 10 4 | 15 27 18 19 28 17 25 19 20 18 16
9 | 8 15 8 8 11 4 11 9 11 13 3 | 14 21 19 18 19 16 22 16 19 19 15
10 | 15 17 11 11 11 8 13 13 9 18 4 | 41 52 48 49 48 49 53 50 47 50 46
11 | 6 15 6 7 9 5 14 10 8 21 3 | 15 31 25 21 31 21 35 19 21 16 20
12E | 12 25 11 10 17 6 24 13 8 17 5 | 24 28 25 28 25 20 29 28 28 32 23
13 | 7 18 9 10 19 6 18 15 14 16 4 | 11 27 18 13 33 14 28 16 20 17 14
14 | 8 21 7 9 16 4 17 9 12 14 4 | 12 27 17 15 24 16 26 14 23 16 14
15 | 8 20 7 12 17 5 20 10 8 16 4 | 10 24 16 17 24 15 24 15 20 20 13
16E | 8 22 14 13 22 6 21 9 12 32 5 | 23 34 27 22 34 25 33 23 33 32 25
17 | 8 21 9 19 18 6 21 11 11 26 5 | 20 31 23 27 26 23 33 23 27 26 22
18 | 8 24 8 9 17 3 19 8 8 19 4 | 23 32 28 26 36 24 28 22 27 26 24
19 | 8 17 8 9 13 4 16 11 13 24 4 | 14 23 16 11 21 14 26 14 25 12 14
20 | 7 17 8 8 16 4 14 10 11 18 4 | 28 33 34 26 41 29 37 29 32 28 29
21 | 10 17 11 9 9 7 14 8 13 28 4 | 18 29 26 14 27 20 31 15 24 20 19
22 | 7 16 9 8 15 3 13 9 8 13 3 | 24 29 29 25 37 24 28 24 24 20 24
23 | 7 23 10 10 16 5 21 14 12 17 5 | 10 28 19 12 26 14 28 15 20 14 13
24 | 8 13 8 8 13 3 7 9 13 22 3 | 16 16 24 17 22 17 20 15 21 18 18
X25E | 5 --- --- --- --- >>>> --- --- --- --- 0 | 47 --- --- --- --- 1 --- --- --- --- 49
26 | 7 14 7 9 11 5 12 7 10 13 3 | 13 18 18 17 15 14 21 12 16 15 13
X27 | 7 16 7 7 14 4 --- 7 11 14 3 | 13 20 17 18 20 15 --- 15 16 19 14
28E | 6 17 11 11 17 4 17 10 15 15 4 | 27 32 25 26 33 26 32 28 31 31 26
X29 | 11 19 8 10 11 7 20 8 9 --- 4 | 20 29 28 22 29 23 32 21 27 --- 23
30E | 14 23 12 13 26 8 21 26 22 20 7 | 42 47 42 43 41 41 46 50 51 42 41
31 | 7 17 7 12 18 5 18 7 11 14 4 | 15 26 19 15 30 17 29 14 24 15 15
32E | 13 27 9 8 22 7 18 16 26 29 6 | 38 44 42 38 43 38 39 40 49 45 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 9 10 16 5 16 12 12 21 |T 21 28 24 22 29 21 29 22 27 24 22
WRMS | 9 19 9 10 15 5 15 10 10 18 |NE 15 24 20 17 24 17 26 17 22 19 17
MEDI | 8 17 8 9 16 5 17 10 11 18 |MD 19 28 23 19 27 20 28 21 24 20 20
Table 3.1588.6 GPS week: 1588 Day: 6 MJD: 55366.000
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 | 18 63 --- --- --- 34 --- 27 22 --- 18 | 33 52 --- --- --- 35 --- 29 44 --- 30
2 | 11 15 9 10 11 6 18 12 10 45 5 | 17 24 23 18 20 19 29 24 26 41 19
3 | 11 22 10 10 12 2 12 8 8 17 4 | 18 26 19 25 23 20 16 24 29 25 21
4 | 10 10 13 5 12 4 11 11 11 17 4 | 24 22 32 23 30 23 21 25 33 26 24
5 | 9 19 9 12 18 7 17 8 9 18 4 | 29 35 35 35 46 31 34 31 34 33 31
6 | 8 21 7 9 10 3 13 7 10 17 3 | 19 28 23 29 30 24 18 26 29 26 23
7 | 19 21 9 10 19 5 21 19 14 17 5 | 22 32 22 20 35 19 33 23 25 20 19
8 | 4 16 6 8 10 5 16 10 10 13 3 | 15 26 18 22 26 16 28 15 24 23 18
9 | 10 15 7 9 11 5 13 10 14 13 4 | 16 22 16 21 19 15 23 17 21 19 15
10 | 12 19 10 11 11 8 13 16 10 20 4 | 73 81 73 78 79 74 79 76 76 78 75
11 | 7 13 6 8 12 7 16 13 7 25 4 | 23 36 31 33 41 28 35 26 30 25 28
12E | 12 30 10 12 28 4 22 10 10 15 5 | 33 46 35 38 41 34 41 38 40 41 35
13 | 7 25 10 14 18 5 24 19 11 18 5 | 12 27 20 21 33 16 29 23 25 21 17
14 | 8 19 8 10 15 5 15 10 11 13 4 | 16 28 23 18 27 18 26 22 29 23 20
15 | 10 18 7 12 15 6 21 12 10 21 4 | 11 23 18 18 25 14 23 18 25 23 14
16E | 10 18 11 14 20 5 21 8 10 15 4 | 40 46 40 39 42 40 48 39 44 42 39
17 | 9 20 12 28 20 6 26 13 11 27 6 | 23 32 29 35 35 24 34 23 31 31 24
18 | 10 25 9 8 13 4 20 10 10 18 4 | 32 41 38 34 46 34 34 35 39 33 35
19 | 9 21 9 7 13 5 19 14 11 24 4 | 20 29 23 19 24 21 27 21 27 20 20
20 | 8 17 6 12 17 6 17 8 8 19 4 | 27 31 30 33 38 27 34 26 34 25 28
21 | 12 15 10 9 12 6 16 8 14 29 4 | 20 25 21 12 28 18 31 16 30 22 20
22 | 9 19 9 6 15 5 13 8 7 13 3 | 36 42 43 38 50 40 39 37 43 35 39
23 | 9 24 14 15 16 4 27 13 11 17 5 | 12 28 20 19 26 15 30 17 23 16 15
24 | 8 14 8 5 13 4 9 9 11 21 3 | 23 24 28 26 31 25 20 25 33 30 26
X25E | 22 --- 24 --- --- 45 --- --- --- --- 23 | 31 --- 5 --- --- 1 --- --- --- --- 30
26 | 8 14 7 8 10 5 14 9 7 15 3 | 13 16 16 14 16 12 21 14 22 17 13
X27 | 7 15 7 8 11 5 --- 7 11 15 3 | 12 21 15 18 18 13 --- 13 19 19 13
28E | 7 16 8 12 16 4 21 10 9 14 4 | 39 43 40 44 45 40 45 40 41 40 40
X29 | 10 18 9 10 9 7 20 7 14 --- 4 | 25 33 32 28 35 28 35 28 31 --- 27
30E | 13 24 14 24 16 4 22 28 22 19 7 | 42 47 39 51 42 43 43 55 57 42 43
31 | 7 19 8 11 20 6 18 6 12 14 4 | 16 30 20 18 33 18 32 17 28 21 19
32E | 11 25 9 10 21 8 16 21 17 20 5 | 77 63 75 76 76 74 77 76 74 75 74
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 9 12 16 5 18 13 11 20 |T 26 34 29 30 35 26 33 29 34 30 27
WRMS | 10 20 9 12 14 5 17 10 9 18 |NE 17 26 22 21 27 19 26 20 27 23 19
MEDI | 9 19 9 10 13 5 17 10 11 17 |MD 23 30 23 25 33 23 32 25 30 25 24
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1588 GPS week: 1588 MJD: 55360.0-55366.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 |U 10 11 25 |U 7 10 22 |U 12 18 27 |
emr | emr 2933 | 13 11 30 |U 9 11 44 |U 11 15 25 |
esa | esa 2989 | 10 10 29 |U 6 9 23 | 10 12 22 |
gfz | gfz 2869 |U 10 9 28 |U 6 9 22 |U 11 14 22 |
grg | grg 2880 | 11 10 27 |U 9 9 25 | 11 16 27 |
igr | igr 2946 | 10 10 26 | 6 9 23 | 11 14 21 |
igs | igs 2943 | 10 10 24 | 6 9 23 | 11 14 21 |
jpl | jpl 2827 |U 11 11 29 | 9 12 40 |U 11 14 24 |
mit | mit 3030 |U 9 9 27 |U 8 10 34 |U 13 18 32 |
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 5.1588.0 GPS week: 1588 Day: 0 MJD: 55360.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 9 11 23 | ---- ---- ---- | 9 13 26 |
emr | emr 2871 | 12 11 32 | ---- ---- ---- | 17 16 28 |
esa | esa 2880 | 9 8 25 | ---- ---- ---- | 9 10 24 |
gfz | gfz 2868 | 9 8 33 | ---- ---- ---- | 10 9 25 |
grg | grg 2880 | 9 8 25 | ---- ---- ---- | 9 9 28 |
igr | igr 2911 | 9 8 26 | ---- ---- ---- | 10 10 24 |
igs | igs 2879 | 9 8 25 | ---- ---- ---- | 10 10 23 |
jpl | jpl 2868 | 11 10 43 | ---- ---- ---- | 10 10 22 |
mit | mit 2976 | 8 8 34 | ---- ---- ---- | 12 10 28 |
Table 5.1588.1 GPS week: 1588 Day: 1 MJD: 55361.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 7 6 28 | ---- ---- ---- | 9 22 34 |
emr | emr 2963 | 11 8 30 | ---- ---- ---- | 9 9 21 |
esa | esa 3072 | 7 7 29 | ---- ---- ---- | 8 6 21 |
gfz | gfz 2868 | 8 6 26 | ---- ---- ---- | 8 7 19 |
grg | grg 2880 | 14 7 31 | ---- ---- ---- | 10 11 27 |
igr | igr 2956 | 8 6 27 | ---- ---- ---- | 8 7 17 |
igs | igs 2950 | 7 6 29 | ---- ---- ---- | 7 7 18 |
jpl | jpl 2772 | 9 8 31 | ---- ---- ---- | 9 7 20 |
mit | mit 3072 | 8 6 34 | ---- ---- ---- | 14 26 67 |
Table 5.1588.2 GPS week: 1588 Day: 2 MJD: 55362.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 | 7 7 20 | 9 7 34 | 12 11 29 |
emr | emr 2963 | 11 10 29 | 13 11 57 | 8 6 20 |
esa | esa 3072 | 8 8 26 | 8 6 32 | 7 3 21 |
gfz | gfz 2869 | 8 8 24 | 8 7 36 | 7 4 19 |
grg | grg 2880 | 9 9 20 | 9 8 32 | 9 7 23 |
igr | igr 2991 | 8 8 19 | 8 7 37 | 7 5 20 |
igs | igs 2951 | 7 8 20 | 8 7 35 | 7 4 17 |
jpl | jpl 2868 | 9 8 23 | 11 12 64 | 7 5 22 |
mit | mit 3072 | 7 7 21 | 15 14 81 | 7 7 21 |
Table 5.1588.3 GPS week: 1588 Day: 3 MJD: 55363.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3049 | 6 4 21 | 6 7 19 | 29 54 30 |
emr | emr 2870 | 9 10 25 | 10 9 46 | 19 42 34 |
esa | esa 3072 | 7 5 42 | 5 5 18 | 23 45 28 |
gfz | gfz 2866 | 7 4 16 | 5 5 16 | 31 52 28 |
grg | grg 2880 | 7 5 16 | 8 6 19 | 22 49 34 |
igr | igr 2964 | 7 5 19 | 6 6 20 | 28 50 28 |
igs | igs 2995 | 6 4 16 | 5 5 19 | 26 49 31 |
jpl | jpl 2869 | 9 6 20 | 6 8 27 | 24 44 31 |
mit | mit 3072 | 7 6 14 | 5 5 23 | 31 53 34 |
Table 5.1588.4 GPS week: 1588 Day: 4 MJD: 55364.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3049 | 22 21 34 | 5 8 15 | 8 6 26 |
emr | emr 2959 | 24 18 42 | 8 9 53 | 8 9 23 |
esa | esa 2976 | 20 18 32 | 4 8 13 | 9 5 22 |
gfz | gfz 2868 | 22 16 39 | 3 8 12 | 8 5 25 |
grg | grg 2880 | 22 16 54 | 9 8 20 | 10 9 27 |
igr | igr 2967 | 20 17 34 | 4 7 11 | 8 8 23 |
igs | igs 2869 | 25 20 36 | 4 7 18 | 8 6 24 |
jpl | jpl 2868 | 23 18 38 | 7 11 21 | 8 8 21 |
mit | mit 3072 | 20 19 38 | 5 6 17 | 10 8 28 |
Table 5.1588.5 GPS week: 1588 Day: 5 MJD: 55365.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 | 10 15 26 | 4 10 16 | 10 8 18 |
emr | emr 2957 | 12 12 27 | 5 10 26 | 9 11 18 |
esa | esa 2880 | 11 15 33 | 4 10 19 | 11 9 21 |
gfz | gfz 2873 | 11 14 41 | 4 9 19 | 11 10 23 |
grg | grg 2880 | 11 14 25 | ---- ---- ---- | ---- ---- ---- |
igr | igr 2906 | 11 16 38 | 5 10 19 | 8 7 16 |
igs | igs 2948 | 10 14 26 | 4 10 18 | 9 8 17 |
jpl | jpl 2775 | 11 16 28 | 12 16 58 | 11 10 27 |
mit | mit 2976 | 9 12 26 | 5 9 18 | 10 9 18 |
Table 5.1588.6 GPS week: 1588 Day: 6 MJD: 55366.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 7 11 21 | 9 15 28 | 8 9 24 |
emr | emr 2951 | 9 10 25 | 11 17 40 | 8 14 29 |
esa | esa 2976 | 7 9 19 | 9 14 30 | 6 8 17 |
gfz | gfz 2872 | 7 7 17 | 9 15 29 | 6 8 17 |
grg | grg 2880 | 7 10 19 | 8 13 28 | 8 12 22 |
igr | igr 2932 | 7 9 19 | 8 13 28 | 6 10 20 |
igs | igs 3010 | 7 9 18 | 9 14 28 | 7 11 21 |
jpl | jpl 2774 | 8 9 19 | 12 15 32 | 7 13 24 |
mit | mit 2976 | 7 7 18 | 10 15 29 | 9 11 24 |
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 6.1588 GPS week: 1588 MJD: 55360.500-55366.500
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 | 36 -52 178 -16 -6 | 3 11
| 13 17 57 73 5 | 2
emr uuuxu | 48 35 -85 421 11 | 17 24
| 15 15 79 79 5 | 7
esa uuuuu | -30 -4 30 -125 2 | 8 17
| 13 15 114 50 6 | 4
gfz uuuuu | -15 47 43 -67 5 | -4 16
| 12 19 55 45 6 | 5
grg uuuux | -1 -119 242 -73 -11 | 1 18
| 30 29 184 95 17 | 3
igr xxxxx | -14 19 -16 2 -3 | 1 12
| 13 13 101 66 11 | 3
irf xxxxx | 2 -12 -13 2 -17 | 15 34
| 8 7 43 56 11 | 5
jpl uuuuu | 24 -28 81 98 -2 | 6 16
| 45 30 91 92 12 | 3
mit uuuuu | -25 -17 -79 -5 -3 | 3 16
| 14 7 63 67 14 | 5
ngs uuuuu | 22 -6 -37 204 0 | 0 11
| 45 35 97 121 10 | 3
sio uuuuu | 70 96 -169 58 -2 | 10 18
| 22 12 97 134 13 | 4
Table 7.1588.0 GPS week: 1588 Day: 0 MJD: 55360.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 49 -36 120 -102 -6 | 6 12
emr uuuxu | 35 12 -37 312 4 | 14 21
esa uuuuu | -28 14 -122 -70 -11 | 8 13
gfz uuuuu | -23 76 -37 -88 -3 | -4 15
grg uuuux | -23 -135 546 32 1 | 3 18
igr xxxxx | -29 33 -157 -9 -1 | 3 11
irf xxxxx | -7 -13 16 -17 -4 | 13 35
jpl uuuuu | 21 -45 -2 14 9 | 7 19
mit uuuuu | -43 -17 -1 -55 16 | 0 18
ngs uuuuu | 71 -35 45 166 -4 | 3 10
sio uuuuu | 35 81 -54 113 14 | 8 20
Table 7.1588.1 GPS week: 1588 Day: 1 MJD: 55361.500
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 | 36 -34 251 54 -9 | 3 13
emr uuuxu | 38 52 -205 436 13 | 11 18
esa uuuuu | -31 5 -34 -72 1 | 4 15
gfz uuuuu | -11 64 78 -9 -2 | -8 17
grg uuuux | -4 -80 232 -142 -11 | 0 18
igr xxxxx | -24 20 -95 -40 -21 | 0 12
irf xxxxx | -2 -14 39 83 -5 | 10 35
jpl uuuuu | 4 -20 -72 -31 3 | 4 17
mit uuuuu | -32 -21 2 111 15 | -2 17
ngs uuuuu | 66 -62 36 -35 -15 | -1 10
sio uuuuu | 46 82 -88 191 14 | 5 17
Table 7.1588.2 GPS week: 1588 Day: 2 MJD: 55362.500
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 | 46 -82 247 46 -15 | 0 10
emr uuuxu | 31 36 -158 370 17 | 10 18
esa uuuuu | -26 1 -59 -127 1 | 3 13
gfz uuuuu | -7 32 130 -58 7 | -10 15
grg uuuux | 26 -148 390 -224 -24 | -2 18
igr xxxxx | -12 15 63 -58 -12 | -3 11
irf xxxxx | 15 -16 13 49 -12 | 10 35
jpl uuuuu | 17 -3 61 67 -10 | 3 15
mit uuuuu | -3 -14 -72 42 3 | -2 17
ngs uuuuu | -22 -4 -40 211 -6 | -4 9
sio uuuuu | 68 94 -119 209 3 | 5 16
Table 7.1588.3 GPS week: 1588 Day: 3 MJD: 55363.500
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 | 51 -44 157 39 -9 | 2 10
emr uuuxu | 51 51 -93 450 14 | 16 23
esa uuuuu | -27 -19 112 -176 4 | 6 15
gfz uuuuu | -30 32 43 -91 10 | -6 15
grg uuuux | 25 -128 259 -62 -7 | -1 18
igr xxxxx | 2 15 117 73 -1 | -2 11
irf xxxxx | 1 -9 -22 17 -17 | 15 34
jpl uuuuu | 121 8 154 190 -19 | 5 15
mit uuuuu | -20 -12 -90 26 -2 | 3 16
ngs uuuuu | -38 1 -194 242 1 | -2 10
sio uuuuu | 76 101 -192 102 -3 | 9 18
Table 7.1588.4 GPS week: 1588 Day: 4 MJD: 55364.500
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 -63 143 23 -2 | 2 10
emr uuuxu | 70 22 -12 481 13 | 19 26
esa uuuuu | -20 -19 -2 -87 9 | 8 17
gfz uuuuu | -26 26 66 -6 13 | -4 15
grg uuuux | -39 -145 137 -116 4 | -1 18
igr xxxxx | 6 18 75 43 6 | -1 12
irf xxxxx | 10 -10 -44 12 -25 | 17 34
jpl uuuuu | 8 -21 164 74 -15 | 4 15
mit uuuuu | -13 -10 -118 -47 -15 | 5 16
ngs uuuuu | 21 36 19 206 6 | -1 10
sio uuuuu | 94 117 -267 10 -13 | 10 18
Table 7.1588.5 GPS week: 1588 Day: 5 MJD: 55365.500
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 | 22 -55 122 -107 -1 | 4 11
emr uuuxu | 46 44 -105 541 11 | 24 31
esa uuuuu | -20 -20 129 -193 5 | 12 20
gfz uuuuu | -14 60 -5 -124 10 | 1 16
grg uuuux | -29 -119 158 -37 2 | 4 16
igr xxxxx | -18 33 -52 87 10 | 3 13
irf xxxxx | -2 1 -90 -52 -28 | 21 34
jpl uuuuu | -21 -85 156 209 7 | 7 13
mit uuuuu | -40 -16 -173 -37 -18 | 9 14
ngs uuuuu | 59 34 29 332 7 | 2 13
sio uuuuu | 81 103 -321 -66 -17 | 14 18
Table 7.1588.6 GPS week: 1588 Day: 6 MJD: 55366.500
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 | 20 -50 209 -68 -1 | 6 12
emr uuuxu | 67 31 14 358 5 | 28 34
esa uuuuu | -58 10 189 -151 3 | 15 22
gfz uuuuu | 3 42 31 -94 4 | 5 18
grg uuuux | 34 -78 -24 40 -44 | 5 17
igr xxxxx | -23 -4 -59 -80 -2 | 6 16
irf xxxxx | 1 -21 -1 -78 -28 | 22 34
jpl uuuuu | 20 -27 108 165 9 | 11 15
mit uuuuu | -27 -32 -101 -77 -17 | 10 14
ngs uuuuu | -5 -15 -149 309 14 | 4 14
sio uuuuu | 88 96 -137 -153 -15 | 15 19
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