[IGSREPORT-18970] Wk 1599 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 16 05:24:10 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1599 (Aug 29, 2010 - Sep 04, 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:
igs1599[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1599[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1599[0-6].cls IGS GPS clock combination summary report.
igs15997.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15997.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 | DGAR
0 | EMR | 6 6 WTZR YELL WTZR YELL
0 | ESA | IRKJ MATE RAMO SUTH UNSA
0 | GFZ | 3
0 | GRG | DGAR IRKJ ONSA
0 | JPL | 6
0 | MIT | 6 6 TSKB
1 | ALL | 1 1
1 | COD | DGAR WILL
1 | EMR | WTZR WTZR
1 | ESA | IRKJ SUTH
1 | GFZ | CONZ MDVJ MIZU
1 | GRG | DGAR IRKJ ONSA SANT
1 | JPL | 32
1 | MIT | IENG IENG KOUC
2 | ALL | 1
2 | COD | DGAR
2 | EMR | WTZR WES2 WTZR
2 | ESA | SUTH
2 | GFZ | KERG MATE MDVJ STJO TIDB
2 | GRG | DGAR ONSA
2 | JPL | 32 HARB
2 | MIT | 6 6 COCO
3 | ALL | 1
3 | COD | DGAR
3 | EMR | 6 6 WTZR ONSA WTZR
3 | ESA | IRKJ RAMO SUTH
3 | GFZ | MATE
3 | GRG | DGAR IRKJ ONSA
3 | JPL | 6 32 PALM
3 | MIT | FLIN
4 | COD | DGAR
4 | EMR | WTZR WTZR
4 | ESA | IRKJ SUTH
4 | GFZ | KERG MDVJ WES2
4 | GRG | DGAR IRKJ ONSA
4 | JPL | 32 AREQ
4 | MIT | CONZ TLSE CONZ TLSE TWTF
5 | COD | 21 DGAR
5 | EMR | WTZR WTZR
5 | ESA | IRKJ SUTH
5 | GFZ | 1 21 CHUR MDVJ SCUB
5 | GRG | DGAR IRKJ ONSA
5 | JPL | 21 32 AREQ
5 | MIT | 1 1 USNO USNO WES2
6 | ALL | 1
6 | COD | DGAR
6 | EMR | WTZR WTZR
6 | ESA | MATE KERG MATE UNSA
6 | GRG | DGAR ONSA
6 | JPL | 32
6 | MIT | 19 26 28 19 25 26 BRMU BRMU SYOG
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 | EMR | 1
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 G06 | | | | 2 | | | |
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 | .6 1.5 .6 5 -15 -9 -.32
EMR | 2.4 6.3 -4.9 3 0 -16 .14
ESA | 3.9 4.0 6.7 54 -10 -36 -.16
GFZ | .4 2.1 .9 25 4 -47 .03
GRG | 5.1 14.1 -1.5 5 40 -28 -.12
JPL | .5 7.9 -9.3 15 21 42 -.06
MIT | 2.5 .2 6.6 24 18 -30 -.20
NGS | 3.0 4.7 9.7 82 -15 -4 -.14
SIO | -1.4 3.4 -4.6 47 5 -3 -.12
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 1.1599.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1599.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 2.1599.[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 3.1599.[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 5.1599.0-6).
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 1599 summary. (Aug 29, 2010 - Sep 04, 2010)
Table 1.1599.a GPS week: 1599 MJD: 55437.000-55443.000
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 230| 0 0 0 52 14 -32 -.18 7 7 | -361 -98 15 65
| 0 0 0 7 9 16 .02 | 319 487
emr 94| 0 2 -6 48 12 13 .50 19 19 | -2140 885 16 90
| 1 3 1 12 20 15 .05 | 2401 1166
esa 131| 0 -1 2 -37 10 -19 .32 8 8 | -1934 1196 13 105
| 0 1 1 16 29 19 .02 | 1089 733
gfz 194| 0 1 0 20 -6 14 -.13 11 11 | 313 -248 22 106
| 0 0 1 54 53 16 .05 | 398 669
grg 126| 0 0 1 45 -100 3 .68 18 17 | 0 -171 51 205
| 1 1 2 14 21 24 .13 | 402 724
igr n/a| 0 0 1 68 4 -7 .01 5 5 | -1399 1329 16 59
| 0 0 0 18 20 26 .02 | 3294 1239
jpl 130| 0 0 -7 28 -26 52 .53 19 19 | 1163 790 19 112
| 0 1 1 14 12 44 .04 | 2073 1332
mit 260| 0 0 -2 9 -30 19 -.32 9 9 | -36 -58 21 172
| 0 0 1 21 24 9 .02 | 414 755
ngs 216| 0 0 3 -84 33 6 -.18 9 7 | 484625 -228020 2206 3882
| 0 0 2 43 38 19 .02 | 1103111 406501
sio 259| -1 0 -1 -42 15 -6 -.41 19 18 | --- --- --- ---
| 0 0 1 23 33 15 .02 | --- ---
Table 1.1599.b GPS week : 1599 MJD: 55437.000-55443.000
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 18 13 15 13 18 19 |
2 | 5 5 5 5 5 5 5 |
3 | 6 5 4 4 4 4 4 |
4 | 3 3 3 3 3 3 3 |
5 | 4 5 4 4 4 4 4 |
6 | 5 5 5 7 5 4 4 |
7 | 5 5 5 5 5 4 5 |
8 | 3 4 3 3 3 3 4 |
9 | 4 4 4 4 4 4 4 |
10 | 4 5 4 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 4 4 4 4 5 |
13 | 4 4 4 4 4 4 5 |
14 | 5 4 4 4 4 4 4 |
15 | 5 5 5 4 5 5 5 |
16 | 6 6 6 6 6 6 6 |
17 | 5 4 4 4 4 4 4 |
18 | 5 5 5 5 4 4 4 |
19 | 5 5 5 4 4 5 5 |
20 | 4 4 3 4 4 4 4 |
21 | 5 6 4 5 5 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 4 5 5 4 5 5 5 |
24 | 4 4 3 3 3 3 3 |
25 | 9 10 9 10 10 10 8 |
26 | 5 4 4 4 4 4 4 |
27 | 4 4 4 4 4 3 4 |
28 | 4 4 4 4 4 4 5 |
29 | 5 5 5 4 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 4 4 4 4 5 4 4 |
32 | 4 3 3 4 4 4 4 |
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 2.1599.0 GPS week: 1599 Day: 0 MJD: 55437.000
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 230| 1 -1 1 54 18 -35 -.18 7 7 | -298 -455 15 66
| 12 19 |
emr 94| -1 4 -8 43 5 16 .48 19 19 | -5433 1455 15 78
| -17 0 |
esa 131| 0 -3 1 -9 -12 -5 .31 11 11 | -1526 2391 16 110
| 19 52 |
gfz 194| 0 1 1 -6 14 24 -.10 10 9 | -79 282 22 111
| -21 -35 |
grg 126| 1 1 0 43 -82 7 .62 16 15 | -195 -122 43 206
| 65 83 |
igr n/a| 0 0 1 65 0 26 .01 5 5 | -6226 2066 16 54
| -32 -16 |
jpl 130| 0 0 -8 49 -28 3 .50 19 18 | -1756 1355 20 114
| -11 -32 |
mit 260| 0 0 -2 -21 -52 25 -.29 10 10 | -175 45 20 182
| 4 10 |
ngs 216| 0 0 4 -97 42 -13 -.16 9 8 | -328 -348 2203 3781
| 38 44 |
sio 259| -2 1 -3 -60 -2 8 -.39 22 19 | --- --- --- ---
| -4 6 |
Table 2.1599.1 GPS week: 1599 Day: 1 MJD: 55438.000
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 230| 0 -1 0 39 10 -61 -.21 9 9 | 15 -569 18 68
| 35 13 |
emr 94| 0 7 -5 35 -12 13 .41 20 20 | -4063 1006 18 103
| -27 10 |
esa 131| 0 -1 2 -35 -13 10 .32 8 8 | -2298 1348 16 111
| -19 23 |
gfz 194| -1 0 0 90 33 2 -.12 11 10 | 344 -362 22 97
| -55 -8 |
grg 126| 3 0 2 39 -90 -10 .54 18 16 | -232 419 59 230
| 34 105 |
igr n/a| 0 -1 1 75 -11 -4 .00 5 5 | -4193 1672 17 59
| -34 -32 |
jpl 130| 0 2 -7 34 -28 59 .47 19 18 | -422 954 22 112
| 31 -108 |
mit 260| 2 0 -3 9 -18 18 -.32 10 9 | -289 362 21 178
| 9 2 |
ngs 216| 0 0 4 -103 15 29 -.17 10 8 | 2958934 -999999 2186 3605
| -5 46 |
sio 259| -1 1 -3 -52 23 -14 -.39 19 20 | --- --- --- ---
| 18 16 |
Table 2.1599.2 GPS week: 1599 Day: 2 MJD: 55439.000
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 230| 0 -1 1 49 32 -34 -.19 8 8 | -55 -568 14 68
| 19 -21 |
emr 94| 1 0 -4 45 35 26 .48 20 20 | -2190 -1181 17 115
| -29 -6 |
esa 131| 0 0 3 -44 23 -14 .34 7 7 | -753 281 13 111
| 5 31 |
gfz 194| 0 1 1 6 -102 2 -.15 10 10 | 659 -990 22 111
| -14 -24 |
grg 126| -1 0 2 59 -118 37 .62 18 17 | 637 -1065 59 208
| 20 100 |
igr n/a| 0 -1 1 82 44 18 -.02 5 5 | -1597 -873 17 70
| -23 -39 |
jpl 130| -1 0 -8 26 -20 8 .56 19 18 | 1532 -1653 20 118
| -9 22 |
mit 260| 0 0 -3 27 -54 28 -.32 9 8 | 509 -713 22 189
| 13 4 |
ngs 216| 1 0 0 -53 92 8 -.17 8 6 | -196 -375 2413 4336
| -91 -62 |
sio 259| -2 0 -2 -39 -30 -6 -.39 17 16 | --- --- --- ---
| 16 36 |
Table 2.1599.3 GPS week: 1599 Day: 3 MJD: 55440.000
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 230| 0 0 1 64 11 -42 -.17 7 7 | -181 -293 14 60
| -11 -5 |
emr 94| -1 3 -5 72 26 20 .48 20 20 | -2868 0 16 83
| -36 -20 |
esa 131| 0 -1 2 -24 57 -21 .32 7 7 | -3188 1411 13 108
| 32 4 |
gfz 194| 0 2 0 -68 -44 28 -.10 12 11 | 520 -560 22 104
| -38 -26 |
grg 126| 0 -1 4 62 -130 35 .82 18 18 | 411 -1238 46 205
| -16 102 |
igr n/a| 0 -1 2 85 3 -28 .01 5 5 | -1810 194 17 52
| -53 -17 |
jpl 130| 1 0 -9 27 -17 15 .52 20 20 | 591 -289 19 112
| 36 -74 |
mit 260| 0 0 -2 -16 -61 30 -.33 8 7 | 506 -1319 17 138
| 20 9 |
ngs 216| 0 0 2 -23 61 -6 -.18 9 6 | -195 -297 2246 4129
| -112 -9 |
sio 259| -1 0 -1 -80 -17 10 -.42 20 16 | --- --- --- ---
| 18 38 |
Table 2.1599.4 GPS week: 1599 Day: 4 MJD: 55441.000
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 230| 0 0 0 53 1 -16 -.17 7 7 | -827 338 14 61
| 15 33 |
emr 94| -1 -1 -7 53 -6 -7 .54 19 19 | -2331 2466 16 90
| -16 14 |
esa 131| 1 0 3 -63 28 -37 .35 9 8 | -3516 1684 11 104
| 29 25 |
gfz 194| 0 1 -1 5 56 10 -.09 12 11 | -237 811 22 135
| -60 1 |
grg 126| -1 0 3 47 -119 -25 .88 18 17 | -530 518 51 202
| -9 136 |
igr n/a| 0 0 1 78 -5 -36 .02 5 5 | -1247 2768 17 67
| -66 -11 |
jpl 130| 0 0 -6 4 -36 78 .54 19 19 | 677 2249 18 108
| 47 -54 |
mit 260| 0 0 -2 12 -6 8 -.32 9 8 | -532 492 18 156
| 20 -1 |
ngs 216| 0 0 3 -53 -24 31 -.15 8 6 | -882 423 2409 3871
| -32 65 |
sio 259| 0 1 -1 -36 55 -35 -.45 18 18 | --- --- --- ---
| 6 21 |
Table 2.1599.5 GPS week: 1599 Day: 5 MJD: 55442.000
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 230| 0 0 0 53 11 -26 -.18 7 7 | -501 238 15 63
| 14 -7 |
emr 94| 1 0 -6 43 37 -6 .57 20 20 | 503 1092 17 82
| 6 1 |
esa 131| -1 0 1 -40 -28 -22 .29 7 7 | -949 541 16 108
| 35 32 |
gfz 194| 0 1 -2 34 17 -7 -.08 12 12 | 860 -980 23 89
| -51 -2 |
grg 126| 1 -1 0 48 -73 -15 .74 19 17 | 62 -167 55 182
| 25 77 |
igr n/a| 0 0 2 32 12 7 .04 6 5 | 1865 1655 18 61
| -8 -23 |
jpl 130| 0 0 -7 39 -9 87 .57 18 18 | 3224 1177 18 107
| 31 -7 |
mit 260| 1 -1 0 29 -18 9 -.34 9 8 | 76 -168 23 159
| 6 8 |
ngs 216| 0 0 2 -103 41 10 -.21 8 6 | 435746 -596167 1813 3485
| 58 -19 |
sio 259| -2 0 0 -16 23 -3 -.42 18 17 | --- --- --- ---
| -3 36 |
Table 2.1599.6 GPS week: 1599 Day: 6 MJD: 55443.000
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 230| 0 0 0 53 14 -14 -.19 7 7 | -682 620 16 72
| 28 15 |
emr 94| 1 1 -5 41 2 34 .56 19 19 | 1398 1362 16 79
| -21 -2 |
esa 131| 0 0 0 -41 15 -46 .31 7 7 | -1314 721 12 89
| 32 -20 |
gfz 194| 0 0 -2 83 -22 37 -.23 11 12 | 128 58 21 95
| -36 -15 |
grg 126| 0 0 0 19 -90 -4 .56 20 20 | -151 453 47 206
| 101 54 |
igr n/a| 0 0 1 61 -14 -36 .01 5 5 | 3410 1821 15 55
| -10 -20 |
jpl 130| 0 -1 -6 19 -47 117 .57 19 19 | 4298 1740 17 116
| 56 113 |
mit 260| 1 0 0 28 -4 13 -.34 11 10 | -348 892 30 206
| 4 14 |
ngs 216| 0 0 7 -154 2 -15 -.19 10 8 | -698 622 2172 3971
| 96 93 |
sio 259| -1 0 0 -14 54 -5 -.39 20 17 | --- --- --- ---
| -5 40 |
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 3.1599.0 GPS week: 1599 Day: 0 MJD: 55437.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 12 --- --- 21 --- 143 --- --- --- --- 16 | 19 --- --- 28 --- 89 --- --- --- --- 18
2 | 6 26 20 8 15 4 25 8 9 23 5 | 26 41 31 28 42 28 42 25 25 27 28
3E | 10 21 10 15 22 9 19 17 11 50 6 | 75 86 80 85 91 79 86 77 79 79 80
4 | 5 16 8 6 9 5 12 9 8 19 3 | 15 20 16 15 16 13 18 13 16 12 13
5 | 4 17 12 9 13 4 16 11 11 30 4 | 26 26 30 29 30 26 25 22 23 24 22
6E | 9 19 9 10 17 5 15 8 12 27 4 | 23 33 27 29 33 24 32 30 28 34 27
7 | 15 21 10 10 24 7 23 12 12 14 5 | 24 31 22 21 32 20 28 22 20 21 19
8 | 5 15 7 7 12 4 12 7 11 16 3 | 17 22 19 17 20 15 19 18 18 17 15
9 | 5 21 11 9 9 3 15 11 6 12 3 | 15 29 20 20 19 18 20 24 19 27 19
10 | 5 16 14 9 9 6 11 8 12 21 3 | 38 34 42 35 39 36 30 38 39 30 36
11 | 7 13 8 8 21 6 20 8 10 12 4 | 14 25 19 15 36 14 25 17 15 17 14
12 | 8 18 13 10 23 5 24 9 12 28 5 | 21 29 25 20 31 21 31 23 23 19 20
13 | 6 18 8 5 20 6 19 9 8 22 4 | 16 21 20 18 34 15 23 17 17 25 15
14 | 5 20 8 13 19 4 25 10 8 15 4 | 18 23 19 18 33 15 23 16 12 17 13
15 | 8 26 13 11 16 4 25 14 7 12 5 | 12 25 20 20 26 12 23 16 13 20 14
16 | 7 25 11 11 17 8 21 15 9 40 5 | 22 33 22 20 32 20 33 20 19 30 19
17E | 8 21 9 13 18 5 23 8 10 11 4 | 21 33 25 27 21 22 27 26 26 29 23
18 | 7 19 9 14 11 6 22 19 7 21 4 | 17 23 22 26 21 17 20 21 17 19 17
19E | 6 25 7 13 18 4 27 10 7 19 4 | 15 29 21 20 24 16 24 17 14 18 14
20 | 5 13 7 9 18 4 14 6 11 17 3 | 23 25 29 27 31 25 22 22 27 20 24
21 | 6 25 8 11 14 6 27 11 11 18 4 | 21 36 19 13 27 17 34 20 20 20 18
22 | 7 16 9 10 13 6 21 7 7 19 3 | 20 24 26 27 29 23 25 25 22 25 22
23 | 7 22 9 8 17 6 20 9 7 25 4 | 11 24 18 17 27 13 22 15 15 22 13
24 | 4 11 8 9 17 5 13 9 7 19 3 | 18 20 23 21 25 20 22 19 19 18 19
X25 | 23 --- 18 11 --- 13 --- 19 12 --- 9 | 21 --- 19 14 --- 16 --- 24 15 --- 12
26 | 9 15 25 7 12 6 13 11 12 24 5 | 19 27 25 18 25 18 26 18 18 29 17
27 | 7 22 11 10 10 5 14 10 7 13 3 | 15 29 19 15 20 15 18 20 15 24 15
28 | 6 19 9 11 14 6 21 7 9 23 4 | 13 28 20 20 27 17 28 17 17 22 17
X29E | 7 16 9 14 19 4 20 10 8 --- 4 | 26 25 22 30 27 23 26 25 24 --- 23
30 | 5 11 12 13 14 4 12 9 9 19 3 | 26 27 27 29 29 26 25 32 28 23 27
31 | 6 17 11 8 22 5 17 7 6 15 4 | 24 29 23 22 37 21 27 19 22 22 21
32 | 6 12 8 6 16 5 18 8 10 13 3 | 22 24 26 24 29 23 24 23 28 20 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 11 10 16 5 19 10 9 22 |T 21 29 25 24 30 23 27 23 22 24 21
WRMS | 7 19 11 9 15 5 18 10 8 19 |NE 19 27 23 21 28 21 25 21 20 22 18
MEDI | 6 18 9 10 16 5 19 9 9 19 |MD 20 27 22 20 29 20 25 21 19 22 19
Table 3.1599.1 GPS week: 1599 Day: 1 MJD: 55438.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 25 79 --- 18 --- 42 --- 23 45 --- 17 | 15 52 --- 19 --- 66 --- 17 35 --- 17
2 | 5 26 7 11 18 7 27 9 9 22 4 | 23 39 26 26 37 25 41 23 25 26 26
3 | 12 17 7 11 20 3 16 10 10 19 4 | 54 64 63 57 60 60 68 58 59 52 57
4 | 6 17 6 9 11 3 11 8 9 15 3 | 11 17 13 13 14 11 20 10 13 10 10
5 | 9 21 10 13 13 6 19 10 13 26 4 | 15 25 23 24 22 17 26 14 18 16 17
6E | 12 19 7 11 19 4 18 9 13 21 4 | 17 25 16 18 22 15 23 21 16 20 16
7 | 16 23 9 9 26 8 24 12 10 15 5 | 16 26 20 17 31 14 27 15 16 16 13
8 | 8 15 5 7 16 5 12 11 7 11 3 | 22 18 18 17 21 19 21 19 17 19 16
9 | 7 22 12 6 13 4 12 10 10 16 4 | 16 28 20 18 20 17 24 19 21 22 17
10 | 17 16 8 11 11 8 11 10 16 19 4 | 31 34 32 35 30 31 35 30 33 27 30
11 | 6 15 7 9 23 5 21 7 8 14 4 | 13 25 20 14 33 15 27 15 15 16 15
12 | 6 17 9 11 21 5 21 9 10 24 4 | 16 28 18 17 26 15 28 17 14 16 15
13 | 7 19 6 11 25 7 16 11 7 20 4 | 14 23 18 15 34 15 23 13 15 18 13
14 | 5 20 6 11 19 5 23 7 9 14 4 | 12 22 17 13 24 13 24 16 19 18 15
15 | 8 26 8 14 21 5 22 10 10 13 4 | 10 24 19 23 26 13 27 15 16 20 14
16 | 11 24 12 15 18 7 24 18 12 35 6 | 15 29 23 14 25 16 32 14 20 30 16
17E | 7 17 9 16 18 3 21 8 8 9 4 | 18 25 19 27 21 19 24 20 23 23 18
18 | 8 22 9 14 13 5 23 20 10 23 5 | 15 27 25 25 23 17 26 20 22 18 18
19E | 9 23 10 14 25 4 26 9 7 21 5 | 14 32 25 20 22 17 27 13 17 21 18
20 | 6 14 8 11 16 4 16 6 9 17 3 | 16 24 27 21 25 21 26 17 19 14 19
21 | 14 26 9 13 18 4 29 12 12 17 5 | 21 29 14 15 23 13 29 16 17 15 13
22 | 5 19 5 9 11 4 23 8 6 19 3 | 15 25 21 23 22 18 25 23 20 21 19
23 | 8 22 9 10 21 5 21 10 9 23 4 | 13 24 20 14 28 16 25 13 14 22 13
24 | 7 12 6 7 17 5 16 7 7 17 3 | 18 23 28 20 26 21 27 17 23 18 21
X25 | 29 --- 9 11 --- 16 --- 19 17 --- 9 | 24 --- 22 19 --- 21 --- 22 16 --- 17
26 | 6 19 7 9 14 7 14 10 8 23 4 | 17 28 18 17 23 17 31 19 18 29 18
27 | 7 25 11 11 14 4 12 9 12 14 4 | 18 33 24 23 24 21 27 22 25 25 21
28 | 8 22 7 11 17 6 22 7 6 22 4 | 11 28 19 14 23 15 27 11 18 18 14
X29E | 8 18 9 16 14 6 23 11 12 --- 5 | 27 26 20 30 21 23 27 26 23 --- 22
30 | 5 14 6 11 12 7 10 9 9 20 3 | 18 22 20 23 20 20 22 23 22 16 19
31 | 9 17 6 13 22 4 17 10 9 16 4 | 16 25 21 17 28 16 30 14 18 17 16
32 | 5 12 7 8 15 4 13 7 6 14 3 | 23 26 30 25 29 28 31 26 23 23 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 8 11 18 5 19 10 10 19 |T 18 28 22 21 26 20 28 19 20 20 18
WRMS | 9 20 8 10 16 5 18 9 8 20 |NE 16 27 21 19 25 19 27 17 19 19 17
MEDI | 8 19 8 11 17 5 19 10 9 19 |MD 16 26 20 19 24 17 27 17 18 19 17
Table 3.1599.2 GPS week: 1599 Day: 2 MJD: 55439.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 11 --- --- 14 --- 151 --- --- --- --- 12 | 14 --- --- 29 --- 102 --- --- --- --- 14
2 | 6 30 8 9 15 7 23 8 9 22 4 | 22 39 25 20 32 25 36 21 24 28 23
3 | 8 20 5 8 21 5 14 8 6 18 3 | 33 40 34 33 40 35 41 35 40 34 34
4 | 4 16 7 9 12 6 12 7 7 13 3 | 14 17 13 14 17 11 16 13 15 13 12
5 | 5 19 9 13 14 4 20 8 11 24 4 | 20 28 27 25 28 20 27 19 23 20 21
6E | 13 21 6 15 19 4 18 9 13 20 4 | 24 37 30 38 36 29 36 34 32 37 29
7 | 17 24 10 10 24 7 22 7 7 13 5 | 23 30 27 23 32 19 28 20 20 21 20
8 | 6 14 7 4 16 7 14 6 6 12 3 | 16 18 20 17 17 16 19 17 19 16 16
9 | 8 21 7 8 13 5 13 8 9 13 3 | 14 28 22 17 20 16 21 17 21 20 17
10 | 7 16 9 10 21 6 15 11 12 17 4 | 61 61 66 57 61 62 59 62 63 62 61
11 | 9 12 9 9 23 4 19 9 8 11 4 | 12 25 21 18 35 15 27 15 17 17 17
12 | 7 20 7 10 19 7 24 7 7 20 4 | 15 29 17 15 27 15 29 12 17 14 14
13 | 8 21 4 6 24 6 21 10 10 16 4 | 14 22 19 18 36 14 26 17 18 20 15
14 | 6 19 7 10 20 6 20 6 7 13 3 | 18 25 21 20 26 17 23 18 19 21 18
15 | 11 26 8 10 20 6 22 9 8 10 4 | 9 24 22 17 26 14 24 17 19 21 16
16 | 12 24 7 16 18 8 27 20 12 33 6 | 14 30 19 16 25 14 34 16 22 31 15
17E | 7 22 8 9 19 5 19 6 8 9 3 | 24 31 22 25 26 21 26 26 30 30 23
18 | 6 18 6 15 14 6 22 15 7 20 4 | 14 24 20 28 26 16 23 20 21 17 17
19E | 6 25 8 14 15 5 25 9 8 17 4 | 15 29 18 20 25 15 26 16 18 18 14
20 | 6 15 6 8 13 4 15 6 9 16 3 | 18 25 24 23 27 20 24 16 18 15 18
21 | 8 22 6 10 14 4 25 10 10 15 4 | 18 31 19 14 28 16 31 20 23 20 17
22 | 8 12 7 11 13 4 21 8 7 18 3 | 17 26 23 27 27 20 25 25 24 24 21
23 | 9 25 10 7 19 5 20 10 8 23 4 | 12 26 22 16 30 14 25 17 18 22 14
24 | 6 12 7 9 17 3 14 7 6 13 3 | 13 22 20 16 25 14 20 15 15 16 15
X25 | 25 --- 9 11 --- 29 --- 20 15 --- 8 | 19 --- 22 19 --- 39 --- 24 22 --- 18
26 | 7 16 7 9 14 5 13 7 8 22 3 | 15 25 20 17 24 15 27 16 16 26 17
27 | 10 18 6 11 12 4 14 8 9 13 3 | 15 23 23 17 21 16 20 18 20 22 17
28 | 7 20 9 9 17 6 23 6 8 20 4 | 13 25 17 15 24 11 26 13 16 20 13
X29E | 8 22 9 13 19 5 21 9 10 --- 4 | 22 28 14 21 25 19 22 21 22 --- 18
30 | 5 12 6 8 22 6 10 9 8 16 3 | 22 24 22 22 28 22 20 26 27 19 22
31 | 6 18 6 9 21 5 17 10 6 13 3 | 22 27 22 20 28 19 26 18 22 21 19
32 | 5 12 6 7 17 4 16 7 4 11 3 | 16 23 24 19 25 19 25 17 18 15 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 7 10 18 5 19 9 8 17 |T 18 28 23 21 28 22 27 20 22 22 19
WRMS | 8 20 7 10 17 5 18 8 6 16 |NE 17 27 22 20 27 22 26 19 21 21 18
MEDI | 7 19 7 9 17 5 19 8 8 16 |MD 16 26 22 19 26 16 26 18 20 20 17
Table 3.1599.3 GPS week: 1599 Day: 3 MJD: 55440.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 10 --- --- 22 --- 167 --- --- --- --- 15 | 19 --- --- 28 --- 153 --- --- --- --- 19
2 | 7 27 8 9 17 7 25 9 9 21 4 | 24 42 26 26 36 27 41 22 25 25 25
3 | 6 22 7 11 23 4 16 8 6 19 4 | 29 38 35 31 33 33 40 30 35 28 31
4 | 5 17 6 11 12 5 11 6 8 13 3 | 14 18 12 19 16 11 16 14 17 9 11
5 | 8 14 7 13 18 4 19 5 9 24 4 | 20 25 22 25 31 21 24 18 20 21 19
6E | 11 22 11 19 26 7 18 19 15 51 7 | 64 71 68 69 72 69 67 66 71 81 67
7 | 15 26 9 11 21 4 23 5 12 14 5 | 23 32 22 22 34 19 27 18 18 19 18
8 | 6 14 5 8 18 5 12 6 11 12 3 | 16 18 13 18 19 13 16 16 19 14 14
9 | 7 20 6 8 17 5 15 8 10 17 3 | 14 26 15 16 18 13 20 17 17 23 13
10 | 5 15 5 9 13 6 13 5 9 14 3 | 39 37 39 37 42 39 39 38 36 39 37
11 | 8 17 7 10 24 4 18 8 12 11 4 | 17 28 22 19 38 18 27 18 17 19 17
12 | 7 18 6 14 17 5 22 5 9 21 4 | 14 27 15 19 27 12 26 14 11 11 12
13 | 6 19 8 12 24 5 20 7 5 13 4 | 15 24 21 18 38 16 25 17 11 16 15
14 | 5 21 7 14 20 6 22 6 7 13 4 | 13 23 17 19 28 12 22 13 14 17 12
15 | 10 25 7 11 20 5 25 7 8 9 4 | 11 23 17 18 28 12 25 15 15 17 13
16 | 11 25 8 15 16 8 25 20 12 35 6 | 16 31 21 15 27 19 31 15 22 31 15
17E | 6 23 7 10 13 5 24 5 4 11 3 | 21 32 18 21 19 21 26 24 24 25 20
18 | 6 21 8 15 10 5 22 11 9 20 4 | 17 27 25 27 22 19 22 21 22 19 18
19E | 7 26 8 12 14 5 25 8 8 17 4 | 13 29 23 20 27 16 25 15 16 19 15
20 | 5 15 5 11 19 4 18 6 8 17 3 | 25 28 28 27 33 26 26 23 25 20 24
21 | 12 23 9 12 15 6 25 8 9 18 4 | 23 34 22 15 28 20 33 20 19 19 19
22 | 6 19 6 12 10 5 22 6 6 18 3 | 18 25 24 28 28 21 24 23 23 22 20
23 | 6 22 9 9 18 4 19 7 7 23 4 | 13 27 19 16 32 16 26 16 13 23 14
24 | 4 12 6 10 15 4 14 5 6 14 3 | 19 23 24 21 26 21 26 18 21 16 19
X25 | 31 --- 15 14 --- 13 --- 17 10 --- 10 | 23 --- 22 20 --- 19 --- 20 14 --- 14
26 | 8 19 8 12 15 4 15 7 9 22 4 | 18 28 22 20 26 17 27 14 14 25 16
27 | 7 16 7 8 17 5 15 8 11 16 3 | 14 21 18 18 18 15 18 18 17 25 14
28 | 7 20 5 10 15 6 23 6 9 21 4 | 13 27 20 17 24 16 29 17 17 20 15
X29E | 7 16 8 15 19 4 20 10 9 --- 4 | 23 22 18 21 25 18 22 21 22 --- 17
30 | 6 12 4 13 24 4 10 4 6 19 3 | 24 24 20 25 31 23 23 26 25 17 22
31 | 5 20 8 11 21 5 20 10 8 14 4 | 18 27 22 18 31 17 27 17 18 19 17
32 | 7 15 9 11 20 5 15 7 9 13 3 | 26 31 31 32 36 29 30 29 27 25 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 20 7 12 18 5 20 8 9 20 |T 20 28 23 23 29 25 27 21 21 22 19
WRMS | 7 20 7 11 18 5 20 7 6 16 |NE 18 27 21 21 28 23 26 19 19 20 17
MEDI | 7 19 7 11 17 5 19 7 9 17 |MD 18 27 22 20 28 19 26 18 19 20 17
Table 3.1599.4 GPS week: 1599 Day: 4 MJD: 55441.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 21 --- --- 31 --- 25 --- 15 22 --- 12 | 20 --- --- 40 --- 41 --- 17 36 --- 24
2 | 6 25 9 10 16 5 24 13 8 19 4 | 21 35 25 23 36 20 34 23 21 21 22
3 | 5 19 7 10 20 4 14 7 6 20 3 | 26 34 30 26 33 26 33 27 27 32 27
4 | 5 18 9 9 11 7 13 5 6 12 3 | 12 19 12 14 13 10 19 13 15 9 11
5 | 5 16 8 15 18 7 19 5 11 24 4 | 15 21 20 22 29 19 24 14 15 16 15
X6 | 9 20 9 --- 19 8 16 8 6 22 4 | 47 51 41 --- 43 49 49 48 46 44 44
7 | 15 24 9 10 25 4 25 6 9 13 5 | 19 27 17 17 31 13 27 16 15 17 14
8 | 5 15 6 7 19 4 12 7 8 11 3 | 17 15 13 14 17 13 17 16 16 12 14
9 | 6 19 6 12 13 3 12 7 8 15 3 | 13 24 14 18 19 16 22 18 19 22 16
10 | 4 13 7 10 15 5 11 6 8 14 3 | 27 30 32 30 34 28 31 26 30 24 28
11 | 7 16 9 10 22 3 14 7 6 11 3 | 10 26 19 13 36 13 23 12 12 12 11
12 | 6 20 10 11 16 6 23 6 7 21 4 | 16 27 17 13 28 17 30 13 17 14 14
13 | 8 21 8 10 24 8 18 7 5 13 4 | 13 23 17 18 37 14 23 13 15 13 13
14 | 4 16 10 11 20 6 20 8 5 11 3 | 9 19 13 16 27 9 19 11 11 15 9
15 | 9 26 9 13 17 3 27 11 7 12 4 | 10 25 14 15 28 10 27 15 9 15 11
16 | 10 22 9 16 19 9 26 20 11 33 6 | 16 28 16 14 22 13 31 14 16 29 12
17E | 7 17 8 12 9 5 19 9 10 10 3 | 20 26 20 22 23 19 26 22 26 25 20
18 | 5 20 10 18 9 4 21 10 7 21 4 | 12 22 15 28 19 13 21 15 17 15 13
19E | 6 24 9 12 16 4 24 9 5 16 4 | 11 28 17 13 28 12 25 12 9 14 11
20 | 5 16 11 9 20 5 19 6 6 19 3 | 19 25 29 24 30 23 24 21 21 16 21
21 | 6 23 9 14 17 7 26 6 11 21 4 | 18 28 15 14 25 15 29 17 20 19 15
22 | 6 19 8 11 8 5 21 8 8 18 3 | 16 24 21 25 24 19 21 21 22 21 18
23 | 9 22 11 12 22 5 22 7 6 22 4 | 12 24 17 16 30 13 24 11 10 21 11
24 | 5 13 6 11 15 4 12 6 6 13 3 | 16 20 22 15 21 16 21 16 20 13 17
X25 | 27 --- 15 14 --- 10 --- 18 10 --- 9 | 21 --- 16 17 --- 14 --- 19 18 --- 12
26 | 7 14 6 8 17 3 11 7 9 23 3 | 12 21 14 15 26 12 22 13 13 24 13
X27 | 7 21 7 9 12 5 --- 7 5 14 3 | 11 24 14 16 18 14 --- 17 17 22 15
28 | 8 19 9 14 16 4 21 7 7 24 4 | 17 28 24 21 26 18 30 21 19 20 18
X29E | 6 17 9 20 18 5 23 7 7 --- 4 | 24 25 21 29 30 24 28 25 25 --- 22
30 | 5 17 7 8 23 5 10 7 7 17 3 | 20 25 19 24 28 22 23 25 25 16 21
31 | 6 21 7 15 22 5 19 16 6 16 4 | 14 25 15 17 28 13 25 14 12 16 12
32 | 6 16 11 7 21 3 15 6 8 15 3 | 16 22 27 22 28 20 22 19 20 15 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 9 12 18 5 19 9 8 18 |T 17 25 19 19 27 18 25 18 19 19 16
WRMS | 7 19 8 11 17 5 19 8 6 18 |NE 15 24 18 19 26 16 24 16 17 17 15
MEDI | 6 19 9 11 17 5 19 7 7 16 |MD 16 25 17 17 28 15 24 16 17 16 15
Table 3.1599.5 GPS week: 1599 Day: 5 MJD: 55442.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 20 54 --- 26 --- 40 --- 27 53 --- 18 | 26 47 --- 18 --- 63 --- 24 46 --- 26
2 | 8 25 9 15 19 8 21 18 8 20 5 | 21 32 23 20 33 21 30 21 19 21 20
3 | 7 18 6 11 27 4 16 7 8 22 4 | 22 33 28 27 35 26 34 25 26 29 25
4 | 5 15 6 10 12 5 12 5 6 10 2 | 11 20 11 14 12 12 13 13 13 9 11
5 | 6 19 8 12 17 5 17 8 9 25 4 | 10 25 17 17 26 15 24 13 11 14 14
6 | 7 20 6 10 22 4 16 7 8 25 4 | 32 40 30 31 39 32 39 36 36 32 32
7 | 7 21 8 10 24 6 21 9 7 13 4 | 14 28 18 16 30 15 25 15 16 15 14
8 | 7 18 5 9 16 5 11 7 5 13 3 | 17 23 16 20 16 16 17 19 17 17 17
9 | 8 18 5 9 12 6 12 7 11 14 3 | 16 26 19 24 18 17 21 18 20 22 18
10 | 5 15 6 9 15 6 12 5 8 15 3 | 27 29 29 28 32 28 28 26 29 28 28
11 | 7 16 7 12 23 4 12 7 6 10 3 | 16 29 22 20 38 15 27 15 12 16 16
12 | 7 18 9 13 20 7 19 5 7 24 4 | 19 28 19 23 29 16 27 14 19 16 17
13 | 6 20 5 14 27 9 19 6 8 11 4 | 13 22 17 16 37 16 22 14 17 16 14
14 | 5 16 6 9 23 4 22 6 10 12 3 | 13 21 16 17 27 15 22 16 16 20 14
15 | 9 29 7 14 19 7 24 10 6 13 4 | 8 26 17 18 26 13 22 16 13 19 13
16 | 10 22 8 16 19 7 25 20 11 32 5 | 11 29 17 15 25 13 30 15 12 28 12
17E | 8 18 7 14 17 6 21 8 6 11 3 | 26 30 26 26 29 27 29 30 29 33 26
18 | 7 19 7 17 11 5 19 8 6 21 4 | 13 25 17 27 20 17 23 19 17 19 17
19E | 7 27 5 13 23 7 23 11 7 14 4 | 9 30 18 21 24 14 23 14 11 13 12
20 | 5 14 7 13 17 3 17 6 7 19 3 | 17 24 24 25 24 18 21 17 16 14 18
21 | 5 30 9 17 15 9 25 8 12 20 5 | 15 35 17 20 27 16 31 18 17 20 15
22 | 8 16 5 10 12 5 19 12 6 19 3 | 13 22 15 20 20 15 22 23 17 24 15
23 | 8 22 8 13 24 5 21 5 10 23 4 | 13 27 17 18 33 14 24 14 15 22 13
24 | 5 13 6 9 16 4 12 6 8 12 3 | 13 21 18 15 17 16 20 13 15 16 14
X25 | 32 --- 9 16 --- 4 --- 17 11 --- 10 | 30 --- 20 23 --- 17 --- 20 18 --- 15
26 | 7 15 6 9 16 4 12 8 8 23 3 | 12 24 19 16 25 15 22 13 14 25 15
27 | 7 20 4 10 13 5 13 8 6 12 3 | 14 25 20 22 18 17 20 18 17 22 18
28 | 8 22 6 8 18 6 22 8 7 22 4 | 15 30 20 18 25 18 30 19 16 24 17
X29E | 6 21 9 24 15 5 22 6 11 --- 5 | 26 27 24 33 24 22 27 24 22 --- 22
30 | 6 13 7 13 30 3 9 10 9 18 4 | 20 24 21 27 33 19 21 26 20 17 21
31 | 4 21 5 12 20 5 18 14 9 12 4 | 14 25 16 15 28 13 23 16 13 18 13
32 | 7 13 8 11 18 5 16 6 8 13 3 | 30 36 35 37 34 30 35 32 30 30 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 20 7 12 19 6 18 9 8 18 |T 17 27 20 21 26 19 25 19 19 20 17
WRMS | 7 20 7 12 17 5 18 8 6 17 |NE 16 27 19 20 26 18 24 18 17 19 16
MEDI | 7 19 7 12 18 5 18 8 8 15 |MD 15 27 19 20 26 16 23 18 17 20 16
Table 3.1599.6 GPS week: 1599 Day: 6 MJD: 55443.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 14 --- --- 26 --- 150 --- --- --- --- 19 | 29 --- --- 42 --- 64 --- --- --- --- 29
2 | 7 24 10 13 23 6 24 18 10 21 5 | 24 39 27 26 34 25 39 24 24 30 24
3 | 7 16 7 12 23 2 15 7 9 23 4 | 26 36 30 29 33 29 38 26 29 31 28
4 | 4 14 8 10 15 3 10 9 8 11 3 | 15 18 15 15 20 13 18 14 18 13 14
5 | 6 14 6 8 20 6 19 12 9 27 4 | 20 25 22 24 32 22 26 22 22 21 21
6 | 8 21 7 9 17 3 15 7 11 25 4 | 29 35 29 24 32 29 35 32 33 34 30
7 | 6 19 9 12 26 4 22 11 12 15 4 | 18 29 23 21 33 17 29 16 17 17 17
8 | 6 15 6 8 16 4 15 7 8 18 3 | 15 23 14 17 18 13 20 15 16 18 13
9 | 7 21 4 8 18 5 16 12 9 14 3 | 15 27 13 14 18 14 21 14 15 17 13
10 | 4 12 8 12 16 5 13 5 9 17 3 | 33 29 32 33 38 32 34 34 34 36 32
11 | 8 15 6 9 26 6 19 9 7 12 4 | 17 32 25 16 41 20 32 20 19 20 21
12 | 7 19 9 11 22 5 22 8 10 25 4 | 17 31 19 16 28 14 33 18 14 13 16
13 | 9 18 6 13 27 7 24 6 11 15 4 | 18 27 19 22 37 20 29 16 14 15 16
14 | 5 16 6 8 24 4 22 8 7 14 3 | 13 22 17 16 25 14 24 18 19 23 15
15 | 9 27 6 10 21 4 21 14 8 14 4 | 10 27 17 15 25 13 25 20 16 18 14
16 | 10 23 9 19 18 8 23 22 15 35 6 | 18 30 19 22 24 18 32 23 21 36 19
17E | 5 24 6 10 14 4 22 9 7 10 3 | 30 38 28 33 30 31 38 33 35 39 31
18 | 6 20 6 14 17 4 19 7 9 21 4 | 16 25 22 27 24 18 23 21 19 23 19
19E | 7 24 8 14 24 4 25 13 10 17 5 | 11 26 18 16 17 11 23 15 13 14 11
20 | 3 17 7 15 20 5 17 7 12 20 4 | 25 30 33 32 37 30 27 28 28 24 28
21 | 8 27 9 13 22 4 26 8 11 25 5 | 18 36 19 13 29 17 36 22 24 26 20
22 | 8 17 6 9 14 4 18 13 9 21 4 | 19 24 24 27 27 23 25 30 22 32 23
23 | 9 24 9 13 23 4 22 6 11 23 4 | 15 29 20 21 32 17 28 14 16 22 15
24 | 5 12 7 7 17 3 13 8 9 12 3 | 15 19 15 17 21 14 21 15 17 19 14
X25 | 23 --- 10 12 --- 10 --- 13 14 --- 8 | 26 --- 20 19 --- 17 --- 23 16 --- 19
26 | 6 13 8 9 17 4 11 10 6 24 3 | 17 25 22 18 25 19 25 15 20 27 19
27 | 6 23 6 9 19 5 16 12 10 13 4 | 13 29 15 14 20 14 22 15 18 18 14
28 | 6 21 6 12 15 5 25 11 7 28 4 | 18 30 24 20 23 20 28 24 23 32 21
X29E | 6 16 8 17 23 3 21 9 10 --- 4 | 25 26 22 29 28 23 29 27 25 --- 23
30 | 8 14 6 14 21 5 11 8 10 18 3 | 25 28 26 31 32 24 24 30 27 23 26
31 | 6 20 6 12 23 3 17 14 10 11 4 | 18 27 20 20 28 19 26 18 23 21 19
32 | 6 15 7 10 21 5 15 7 9 13 3 | 27 31 35 30 38 31 33 31 30 24 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 11 20 5 19 11 10 20 |T 19 28 22 22 28 21 28 21 21 23 20
WRMS | 7 19 7 12 20 5 19 10 8 17 |NE 19 27 21 21 28 20 27 20 20 22 19
MEDI | 6 18 7 12 20 4 19 9 9 18 |MD 18 28 22 21 28 19 27 21 20 23 19
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 4.1599 GPS week: 1599 MJD: 55437.0-55443.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3050 |U 8 8 25 |U 6 8 22 |U 12 13 32 |
emr | emr 2900 |U 9 9 28 |U 7 9 26 | 12 12 29 |
esa | esa 2976 | 7 7 23 |U 6 8 23 | 11 11 30 |
gfz | gfz 3052 |U 7 7 20 |U 7 8 23 |U 11 11 29 |
grg | grg 2880 | 17 22 46 |U 9 9 29 | 12 12 34 |
igr | igr 2986 | 7 8 21 | 6 8 23 | 11 12 29 |
igs | igs 2973 | 7 7 22 | 6 8 22 | 11 11 30 |
jpl | jpl 2862 |U 8 7 24 | 7 8 27 |U 12 12 29 |
mit | mit 3017 |U 7 6 21 |U 7 8 25 |U 14 14 34 |
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 5.1599.0 GPS week: 1599 Day: 0 MJD: 55437.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 7 7 25 | 5 7 23 | 11 13 22 |
emr | emr 2876 | 10 10 34 | 6 8 26 | 11 10 19 |
esa | esa 2976 | 8 7 33 | 5 7 27 | 11 13 21 |
gfz | gfz 3064 | 7 7 24 | 5 7 33 | 12 13 20 |
grg | grg 2880 | 9 7 33 | ---- ---- ---- | ---- ---- ---- |
igr | igr 2999 | 7 8 25 | 5 7 26 | 12 12 21 |
igs | igs 2930 | 9 7 33 | 5 6 23 | 11 11 20 |
jpl | jpl 2873 | 9 7 38 | 5 7 24 | 11 11 20 |
mit | mit 2976 | 8 7 32 | 5 7 23 | 10 11 22 |
Table 5.1599.1 GPS week: 1599 Day: 1 MJD: 55438.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 19 20 60 | 4 6 16 | 15 23 70 |
emr | emr 2949 | 13 17 34 | 5 10 22 | 16 22 61 |
esa | esa 2976 | 10 12 23 | 4 5 17 | 11 16 58 |
gfz | gfz 3055 | 10 12 22 | 6 7 16 | 14 20 63 |
grg | grg 2880 | 24 87 170 | 8 6 34 | 11 21 74 |
igr | igr 3011 | 10 14 23 | 5 6 17 | 14 21 61 |
igs | igs 2967 | 11 13 23 | 4 6 17 | 11 20 62 |
jpl | jpl 2874 | 12 13 30 | 6 7 23 | 18 21 65 |
mit | mit 3072 | 10 11 21 | 5 6 22 | 8 22 61 |
Table 5.1599.2 GPS week: 1599 Day: 2 MJD: 55439.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3050 | 6 6 17 | ---- ---- ---- | 7 6 20 |
emr | emr 2876 | 8 10 25 | ---- ---- ---- | 7 9 21 |
esa | esa 2976 | 7 7 21 | ---- ---- ---- | 7 8 19 |
gfz | gfz 3068 | 6 6 20 | ---- ---- ---- | 8 9 20 |
grg | grg 2880 | 7 7 19 | ---- ---- ---- | 7 8 21 |
igr | igr 2974 | 6 8 20 | ---- ---- ---- | 7 9 17 |
igs | igs 2973 | 6 6 20 | ---- ---- ---- | 6 8 17 |
jpl | jpl 2876 | 7 7 21 | ---- ---- ---- | 8 9 20 |
mit | mit 2976 | 6 6 18 | ---- ---- ---- | 8 12 21 |
Table 5.1599.3 GPS week: 1599 Day: 3 MJD: 55440.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 6 6 17 | 4 6 19 | 11 10 21 |
emr | emr 2880 | 8 7 25 | 5 7 22 | 12 13 24 |
esa | esa 2976 | 6 6 20 | 3 7 18 | 10 11 20 |
gfz | gfz 3068 | 5 5 18 | 4 6 17 | 10 10 21 |
grg | grg 2880 | 31 24 29 | 5 7 23 | 12 12 22 |
igr | igr 2998 | 6 6 18 | 4 7 18 | 11 11 21 |
igs | igs 2974 | 6 5 20 | 4 6 18 | 10 10 20 |
jpl | jpl 2876 | 7 6 19 | 6 9 23 | 11 11 25 |
mit | mit 2976 | 6 5 20 | 4 6 20 | 10 10 22 |
Table 5.1599.4 GPS week: 1599 Day: 4 MJD: 55441.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 | 7 6 18 | 17 15 36 | 8 10 16 |
emr | emr 2880 | 8 7 22 | 14 14 40 | 8 6 18 |
esa | esa 2976 | 8 8 22 | 15 13 34 | 8 8 14 |
gfz | gfz 2973 | 8 6 20 | 16 13 37 | 7 7 14 |
grg | grg 2880 | 33 16 29 | 20 16 36 | 11 9 20 |
igr | igr 2976 | 7 7 19 | 15 12 34 | 8 10 14 |
igs | igs 2976 | 7 7 19 | 17 15 37 | 7 8 15 |
jpl | jpl 2784 | 8 6 20 | 13 13 41 | 8 8 17 |
mit | mit 3072 | 7 6 18 | 16 14 36 | 17 19 25 |
Table 5.1599.5 GPS week: 1599 Day: 5 MJD: 55442.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 7 6 19 | 5 8 21 | 8 12 20 |
emr | emr 2961 | 7 6 27 | 6 7 22 | 10 6 19 |
esa | esa 2976 | 6 6 21 | 5 7 21 | 8 9 18 |
gfz | gfz 3071 | 6 6 20 | 5 8 20 | 7 8 16 |
grg | grg 2880 | 7 8 23 | 6 7 29 | 9 9 20 |
igr | igr 2973 | 6 6 22 | 6 8 22 | 8 9 20 |
igs | igs 3019 | 6 6 20 | 5 7 21 | 7 8 19 |
jpl | jpl 2878 | 7 6 25 | 6 7 25 | 8 7 17 |
mit | mit 3072 | 5 6 19 | 6 8 24 | 10 10 23 |
Table 5.1599.6 GPS week: 1599 Day: 6 MJD: 55443.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3061 | 6 4 18 | 4 6 19 | 22 15 56 |
emr | emr 2880 | 7 8 26 | 7 7 22 | 22 15 44 |
esa | esa 2976 | 6 5 20 | 4 6 19 | 21 13 62 |
gfz | gfz 3065 | 6 5 20 | 4 8 18 | 22 12 50 |
grg | grg 2880 | 7 4 18 | 5 8 26 | 20 12 46 |
igr | igr 2976 | 6 6 20 | 4 7 18 | 20 12 52 |
igs | igs 2976 | 5 5 19 | 4 6 19 | 22 13 56 |
jpl | jpl 2878 | 7 6 18 | 5 6 23 | 20 18 40 |
mit | mit 2976 | 6 4 20 | 5 6 24 | 34 14 60 |
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 6.1599 GPS week: 1599 MJD: 55437.500-55443.500
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 | 7 -13 5 -111 3 | 4 22
| 11 19 126 103 2 | 2
emr uuuuu | 14 23 247 125 -2 | 59 63
| 8 13 71 41 12 | 3
esa uuuuu | -7 -16 15 153 -3 | 17 28
| 27 19 42 70 5 | 3
gfz uuuuu | 29 42 -95 -105 3 | 6 20
| 13 26 90 54 7 | 2
grg uuuux | -80 -29 8 -219 24 | 8 41
| 29 31 64 66 61 | 13
igr xxxxx | 36 35 5 131 5 | 0 20
| 10 18 69 34 8 | 3
irf xxxxx | 14 3 -60 -73 -3 | 3 22
| 10 17 46 35 5 | 3
jpl uuuuu | 34 -23 -22 130 -3 | 15 31
| 70 25 68 80 11 | 7
mit uuuuu | 7 -8 -126 -154 -4 | 17 28
| 11 23 93 47 5 | 3
ngs uuuuu | -9 10 83 109 0 | 5 19
| 45 61 110 64 4 | 2
sio uuuuu | -14 -4 28 -235 -2 | 28 36
| 19 27 86 66 7 | 4
Table 7.1599.0 GPS week: 1599 Day: 0 MJD: 55437.500
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 | -2 -2 155 -42 3 | 4 24
emr uuuuu | 17 27 256 72 -15 | 63 67
esa uuuuu | -35 -9 16 101 0 | 18 29
gfz uuuuu | 52 31 -56 -61 7 | 4 19
grg uuuux | -66 -55 63 -98 1 | 1 36
igr xxxxx | 33 42 -24 173 15 | -4 20
irf xxxxx | 17 10 -72 -97 -12 | 6 25
jpl uuuuu | 49 21 -150 150 -24 | 24 41
mit uuuuu | 7 6 -173 -184 -11 | 21 31
ngs uuuuu | -27 -28 131 207 6 | 2 19
sio uuuuu | 11 14 -7 -330 -15 | 34 43
Table 7.1599.1 GPS week: 1599 Day: 1 MJD: 55438.500
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 | 1 -42 -10 -11 6 | 2 22
emr uuuuu | 4 20 299 170 -15 | 60 64
esa uuuuu | -9 12 -9 81 2 | 16 28
gfz uuuuu | 22 48 12 -67 5 | 3 19
grg uuuux | -91 -41 -64 -241 -19 | 2 36
igr xxxxx | 46 27 128 141 13 | -4 20
irf xxxxx | 14 -7 -126 -77 -6 | 3 23
jpl uuuuu | 122 -38 10 203 -5 | 18 35
mit uuuuu | 12 -16 -253 -184 -5 | 17 28
ngs uuuuu | -32 -2 214 164 2 | 3 19
sio uuuuu | -2 -25 -130 -225 -8 | 30 38
Table 7.1599.2 GPS week: 1599 Day: 2 MJD: 55439.500
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 -36 -106 -254 0 | 5 23
emr uuuuu | 7 12 294 69 -5 | 61 64
esa uuuuu | -30 -22 -3 129 -3 | 20 30
gfz uuuuu | 25 -3 -63 -74 -1 | 6 20
grg uuuux | -99 -37 -16 -220 5 | 1 36
igr xxxxx | 40 6 -41 135 12 | 0 22
irf xxxxx | 1 -17 -116 -104 -1 | 4 23
jpl uuuuu | -21 -8 40 213 -1 | 18 35
mit uuuuu | -3 -30 -235 -194 1 | 18 29
ngs uuuuu | 63 74 157 141 2 | 5 20
sio uuuuu | -35 -33 -2 -253 2 | 29 37
Table 7.1599.3 GPS week: 1599 Day: 3 MJD: 55440.500
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 | 5 -1 184 -187 4 | 7 22
emr uuuuu | 20 24 161 157 -1 | 62 66
esa uuuuu | -4 -44 63 239 -9 | 22 30
gfz uuuuu | 26 26 -92 -98 1 | 9 19
grg uuuux | -102 4 70 -267 110 | -4 32
igr xxxxx | 17 41 -1 89 4 | 4 19
irf xxxxx | 0 -12 -22 -119 3 | 6 22
jpl uuuuu | 74 -48 -28 131 -9 | 19 36
mit uuuuu | -9 -32 -38 -185 2 | 20 29
ngs uuuuu | 9 100 -66 82 2 | 8 19
sio uuuuu | -38 -30 55 -302 7 | 30 38
Table 7.1599.4 GPS week: 1599 Day: 4 MJD: 55441.500
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 | -7 -17 23 11 0 | 5 23
emr uuuuu | 12 14 250 115 -1 | 58 62
esa uuuuu | 1 -31 72 263 -4 | 17 29
gfz uuuuu | 25 58 -30 -176 7 | 6 20
grg uuuux | -110 7 -40 -266 108 | 7 39
igr xxxxx | 37 64 57 174 1 | 1 20
irf xxxxx | 26 -2 -17 -42 0 | 2 23
jpl uuuuu | 80 -49 -7 34 2 | 11 30
mit uuuuu | 27 -22 -93 -65 -3 | 17 28
ngs uuuuu | -39 30 -52 23 -5 | 6 19
sio uuuuu | 5 -8 106 -210 2 | 26 35
Table 7.1599.5 GPS week: 1599 Day: 5 MJD: 55442.500
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 | 18 5 -63 -194 2 | 3 21
emr uuuuu | 10 13 328 158 9 | 56 60
esa uuuuu | -21 -16 14 112 -9 | 15 26
gfz uuuuu | 13 70 -231 -71 12 | 7 21
grg uuuux | -66 -6 -46 -162 14 | 21 57
igr xxxxx | 34 27 -4 107 -3 | 2 20
irf xxxxx | 11 19 -47 -41 0 | 0 20
jpl uuuuu | 18 -12 45 9 2 | 7 22
mit uuuuu | 3 13 -43 -132 -4 | 15 25
ngs uuuuu | 30 -39 39 81 -5 | 5 18
sio uuuuu | -25 22 43 -188 2 | 24 32
Table 7.1599.6 GPS week: 1599 Day: 6 MJD: 55443.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 11 1 -148 -100 2 | 3 21
emr uuuuu | 28 50 140 137 16 | 55 58
esa uuuuu | 46 -3 -47 149 2 | 13 25
gfz uuuuu | 41 65 -205 -188 -9 | 8 21
grg uuuux | -28 -72 89 -275 -48 | 30 53
igr xxxxx | 46 39 -81 100 -5 | 1 20
irf xxxxx | 26 29 -23 -30 -5 | -1 21
jpl uuuuu | -87 -27 -64 171 13 | 4 21
mit uuuuu | 12 25 -48 -132 -10 | 13 25
ngs uuuuu | -67 -67 159 67 0 | 5 18
sio uuuuu | -14 34 129 -137 0 | 24 31
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