[IGSREPORT-18902] Wk 1596 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 26 08:05:17 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1596 (Aug 08, 2010 - Aug 14, 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:
igs1596[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1596[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1596[0-6].cls IGS GPS clock combination summary report.
igs15967.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs15967.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 1
0 | COD | USNO USNO
0 | EMR | WTZR WTZR
0 | ESA | CEDU CEDU IRKJ SUTH UNSA
0 | GFZ | 3 6 26
0 | GRG | DGAR IRKJ ONSA
0 | JPL | 26 32
0 | MIT | 3 10 25 26 3 10 25 26 29 BRUS
1 | ALL | 1 1
1 | COD | DGAR NRIL
1 | EMR | 26 3 6 26 WES2 WTZR
1 | ESA | IRKJ SUTH UNSA
1 | GFZ | 3 6 26 HARB MDVJ NRC1
1 | GRG | DGAR IRKJ ONSA SANT
1 | JPL | 3 32
1 | MIT | 25 26 3 6 25 26 WES2 WES2
2 | ALL | 1
2 | EMR | 26 26 WTZR WES2 WTZR
2 | ESA | IRKJ SUTH
2 | GFZ | 1 HARB UNSA
2 | GRG | DGAR IRKJ ONSA
2 | JPL | 32
2 | MIT | 25 26 25 26 MDVJ TNML MDVJ TNML
3 | ALL | 1
3 | COD | USNO DGAR USNO
3 | EMR | 3 6 26 WTZR WTZR
3 | ESA | IRKJ SUTH UNSA
3 | GFZ | 3 6 26 KERG WES2
3 | GRG | DGAR IRKJ ONSA
3 | JPL | 32
3 | MIT | 25 26 3 6 25 26
4 | ALL | 1 1
4 | COD | DGAR
4 | EMR | 26 3 26 WTZR WTZR
4 | ESA | KERG SUTH UNSA
4 | GFZ | 6
4 | GRG | DGAR ONSA
4 | JPL | 6 26 32
4 | MIT | 25 26 3 6 25 26 USN3 PDEL USN3
5 | ALL | 1
5 | COD | USN3 RABT USN3
5 | EMR | 3 6 WTZR WTZR
5 | ESA | SUTH UNSA
5 | GFZ | 3 6 GRAZ
5 | GRG | DGAR ONSA
5 | JPL | 3
5 | MIT | 6 25 26 3 6 25 26 SANT
5 | NGS | 25
6 | ALL | 1
6 | COD | DGAR
6 | EMR | 26 26 WTZR WTZR
6 | ESA | IRKJ
6 | GFZ | 6 HARB MDVJ
6 | GRG | DGAR IRKJ ONSA
6 | JPL | 3 26 32
6 | MIT | 3 6 25 26 3 6 25 26 USNO USNO
6 | NGS | 25
5. 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.
6. 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 | .4 1.3 2.3 -5 16 -26 -.54
EMR | 3.0 1.3 .3 31 23 -10 -.01
ESA | 3.5 .4 2.2 37 -24 -15 -.42
GFZ | .2 2.2 1.1 28 0 -61 -.17
GRG | 3.3 6.5 10.3 5 31 -22 -.05
JPL | 2.0 6.6 -10.8 -3 -75 -69 -.24
MIT | 4.5 2.4 16.5 17 -7 -36 -.36
NGS | 4.5 .5 8.0 13 -48 5 -.41
SIO | .3 -.6 1.9 -25 12 4 -.18
7. 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.
8. 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.
9. 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 1.1596.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1596.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 2.1596.[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 3.1596.[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 5.1596.0-6).
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 1596 summary. (Aug 08, 2010 - Aug 14, 2010)
Table 1.1596.a GPS week: 1596 MJD: 55416.000-55422.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -2 41 -47 -3 -.24 7 7 | -23 412 14 57
| 0 0 0 9 9 27 .02 | 400 719
emr 89| 1 -1 -6 -27 -31 -5 .41 17 17 | -1878 -444 17 74
| 1 0 1 12 22 11 .03 | 2401 1815
esa 130| 1 0 2 -60 1 -7 .25 8 8 | -1206 398 14 101
| 0 1 1 25 16 17 .02 | 1728 1522
gfz 195| 0 0 1 -42 -2 -17 -.27 10 9 | -11 -32 21 97
| 1 0 0 36 57 14 .03 | 300 587
grg 124| 1 0 8 0 -69 -17 .59 18 16 | -224 139 51 204
| 1 1 3 40 18 16 .04 | 205 610
igr n/a| 0 0 0 32 12 -30 -.04 5 5 | -9946 -258 16 52
| 0 0 0 35 14 12 .04 | 1952 1855
jpl 120| 0 -1 -10 32 139 49 .57 18 17 | -439 -456 17 102
| 0 1 1 14 14 33 .04 | 2471 1977
mit 258| 0 0 0 -12 -13 12 -.27 11 10 | 769 673 22 159
| 0 0 2 35 19 9 .02 | 746 940
ngs 215| 0 0 0 45 86 0 -.16 12 9 | 181789 -144956 2200 5864
| 0 0 1 32 33 22 .03 | 463602 377087
sio 259| -2 0 2 71 -37 0 -.14 19 17 | --- --- --- ---
| 0 0 1 31 30 17 .03 | --- ---
Table 1.1596.b GPS week : 1596 MJD: 55416.000-55422.000
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 | 17 16 15 15 24 15 17 |
2 | 6 6 5 5 6 6 6 |
3 | 5 5 5 4 5 5 5 |
4 | 4 3 4 4 4 4 4 |
5 | 5 4 5 4 4 4 5 |
6 | 6 6 5 5 5 5 5 |
7 | 5 5 4 4 4 4 4 |
8 | 4 4 4 4 4 4 4 |
9 | 4 4 4 4 4 4 4 |
10 | 4 3 3 4 4 4 4 |
11 | 4 4 4 3 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 5 |
14 | 4 4 4 4 4 4 4 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 4 5 5 5 |
17 | 6 4 4 5 5 4 4 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 4 4 4 4 |
20 | 5 4 4 4 4 4 5 |
21 | 4 5 5 5 4 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 4 4 5 |
24 | 4 4 4 3 3 3 3 |
25 | 12 11 12 13 14 13 11 |
26 | 5 5 5 5 6 6 6 |
27 | 4 3 4 4 4 4 4 |
28 | 4 4 5 4 5 5 5 |
29 | 5 5 5 6 5 5 6 |
30 | 3 3 3 3 3 4 3 |
31 | 5 4 4 4 4 4 4 |
32 | 4 3 3 3 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 2.1596.0 GPS week: 1596 Day: 0 MJD: 55416.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 0 47 -48 -31 -.22 8 8 | -432 -86 16 61
| 35 8 |
emr 89| 0 -1 -9 -42 -35 0 .37 17 17 | -2201 -792 18 90
| -3 -10 |
esa 130| 2 0 4 -74 -11 8 .30 8 8 | -1732 1110 12 87
| 54 15 |
gfz 195| 0 0 2 -26 -7 -13 -.27 10 10 | 144 -75 19 96
| -15 -21 |
grg 124| 1 0 12 -47 -41 -1 .56 23 18 | -103 -475 60 202
| 143 -28 |
igr n/a| 0 0 0 -41 28 -11 .02 5 5 | -9878 -958 16 50
| -31 -3 |
jpl 120| 0 0 -12 27 139 48 .57 18 17 | 217 -756 18 112
| 42 -4 |
mit 259| 0 0 -3 40 0 -4 -.31 11 11 | -261 -256 19 164
| -6 9 |
ngs 215| -1 0 2 -23 82 33 -.20 11 9 | 44093 -16104 2154 3511
| 20 -2 |
sio 259| -3 1 1 115 -74 3 -.10 19 15 | --- --- --- ---
| -96 42 |
Table 2.1596.1 GPS week: 1596 Day: 1 MJD: 55417.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| -1 0 -1 40 -40 -11 -.23 7 7 | -111 -778 13 59
| 39 22 |
emr 89| 2 -1 -6 -47 -54 -12 .44 17 17 | -2070 1651 18 82
| -6 9 |
esa 130| 1 -1 4 -77 -16 -14 .26 8 7 | -1434 1588 12 103
| 27 35 |
gfz 195| 0 0 0 -50 32 2 -.30 10 9 | 481 -1176 19 93
| -34 -17 |
grg 124| 0 1 10 22 -67 9 .53 16 14 | -176 -601 42 183
| 19 0 |
igr n/a| 0 0 0 36 17 -43 -.04 5 5 | -9975 1314 17 51
| -53 4 |
jpl 120| 0 0 -10 30 150 78 .63 17 17 | 312 1300 16 103
| 33 -1 |
mit 259| 0 0 -2 3 8 8 -.28 10 10 | -50 -45 20 162
| 10 11 |
ngs 215| 0 0 1 43 66 -7 -.19 11 9 | -39 -747 2238 4934
| -75 19 |
sio 259| -3 0 0 93 -63 -10 -.13 18 16 | --- --- --- ---
| -84 39 |
Table 2.1596.2 GPS week: 1596 Day: 2 MJD: 55418.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -2 35 -55 31 -.25 8 7 | -235 65 21 55
| 19 32 |
emr 89| 3 -1 -4 -15 -26 -20 .41 17 17 | 752 -1146 20 64
| -53 -11 |
esa 130| 1 0 0 -98 -13 0 .24 9 8 | -1291 575 20 103
| 55 14 |
gfz 195| 0 0 2 -30 67 -33 -.28 9 9 | -327 280 25 96
| -44 2 |
grg 124| 0 -1 8 -23 -80 -29 .63 17 17 | 36 -455 61 187
| 70 55 |
igr n/a| 0 0 1 32 -11 -25 -.09 5 5 | -7857 -1321 20 53
| -34 13 |
jpl 120| 0 -1 -10 30 122 51 .58 19 18 | 2360 -1576 15 87
| 4 -21 |
mit 259| 0 0 0 6 -8 9 -.24 9 8 | 907 -554 33 154
| 10 9 |
ngs 215| 0 0 2 49 31 -25 -.10 11 9 | 1232455 -999999 2205 6112
| -31 35 |
sio 259| -2 0 3 91 -34 -27 -.10 19 17 | --- --- --- ---
| -90 21 |
Table 2.1596.3 GPS week: 1596 Day: 3 MJD: 55419.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -2 32 -54 -25 -.26 7 7 | -258 611 13 57
| 43 29 |
emr 89| 1 -2 -5 -20 -12 -18 .43 17 17 | 635 -659 15 71
| -51 -25 |
esa 130| 0 0 0 -67 23 11 .26 6 6 | -584 -481 14 105
| 9 5 |
gfz 195| 0 0 0 8 -24 -8 -.31 11 10 | -416 762 20 101
| -42 -41 |
grg 124| 2 2 9 -37 -63 -27 .62 17 15 | -322 691 52 207
| 69 -7 |
igr n/a| 0 0 1 67 21 -32 -.09 4 4 | -8192 -530 15 54
| -75 -14 |
jpl 120| 0 -3 -7 32 124 31 .53 18 18 | 1835 -723 18 101
| -17 -30 |
mit 259| 0 0 2 -5 -29 12 -.25 10 10 | 464 1289 18 148
| 19 12 |
ngs 215| 0 0 0 56 97 -7 -.16 11 7 | -137 556 2036 8049
| -63 -11 |
sio 259| -2 1 5 79 -37 14 -.16 19 17 | --- --- --- ---
| -75 25 |
Table 2.1596.4 GPS week: 1596 Day: 4 MJD: 55420.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -3 47 -31 1 -.26 7 7 | 20 797 13 57
| -9 -6 |
emr 89| 2 -2 -7 -24 3 6 .38 17 17 | -396 -3426 20 71
| -41 -42 |
esa 130| 0 2 3 -36 20 2 .24 7 7 | 62 -854 14 97
| 20 3 |
gfz 195| -1 0 1 -106 -112 -16 -.24 10 9 | 93 -144 21 100
| -28 -38 |
grg 124| 4 1 10 33 -54 -11 .57 17 15 | -53 629 48 211
| 1 -12 |
igr n/a| 0 -1 0 28 0 -18 -.04 4 4 | -8624 -2969 16 53
| -62 -13 |
jpl 120| 1 0 -8 46 162 3 .58 17 17 | -350 -3413 16 105
| -44 -70 |
mit 259| 0 0 2 -41 -48 23 -.26 12 10 | 1192 1171 23 166
| 27 22 |
ngs 215| 0 0 0 71 142 -19 -.16 11 8 | -5 748 2643 10562
| -154 -55 |
sio 259| -3 0 3 41 -58 23 -.16 20 18 | --- --- --- ---
| -83 21 |
Table 2.1596.5 GPS week: 1596 Day: 5 MJD: 55421.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -1 27 -42 36 -.24 7 7 | 55 1335 13 61
| 23 48 |
emr 89| 0 0 -7 -17 -37 -2 .40 18 18 | -4529 -701 17 76
| -68 -21 |
esa 130| 0 1 2 -37 7 -32 .25 8 8 | -4475 2620 14 116
| 1 9 |
gfz 195| -2 0 2 -26 -6 -37 -.24 10 10 | 6 42 24 104
| -86 -60 |
grg 124| 2 0 5 -10 -85 -31 .60 17 16 | -445 570 42 204
| 41 19 |
igr n/a| 0 0 0 54 13 -45 -.03 5 4 | -12318 -108 18 49
| -85 -20 |
jpl 120| 0 -1 -11 8 132 29 .52 18 17 | -4444 -751 18 114
| 6 -19 |
mit 259| 0 0 2 -19 -14 12 -.25 12 11 | 1412 1215 21 185
| 25 22 |
ngs 215| 1 0 0 44 100 3 -.14 13 10 | -1965 746 2052 3777
| -138 19 |
sio 259| -3 0 2 34 -6 0 -.14 19 18 | --- --- --- ---
| -78 13 |
Table 2.1596.6 GPS week: 1596 Day: 6 MJD: 55422.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 233| 0 0 -2 56 -58 -21 -.25 8 7 | 800 945 11 51
| -6 19 |
emr 89| -1 0 -5 -24 -58 5 .42 17 17 | -5342 1959 16 67
| -42 14 |
esa 130| 0 1 2 -33 -1 -24 .22 7 8 | 1011 -1766 14 102
| -8 33 |
gfz 195| -1 -1 2 -67 29 -18 -.24 9 8 | -59 84 19 91
| -53 -4 |
grg 124| 2 -1 2 62 -94 -27 .65 19 18 | -511 617 56 239
| -48 78 |
igr n/a| 0 0 0 47 20 -36 -.01 4 4 | -12784 2762 15 55
| -68 8 |
jpl 120| 0 0 -9 53 146 105 .61 19 19 | -3008 2727 18 92
| 3 33 |
mit 259| 0 0 3 -71 -6 25 -.27 11 10 | 1721 1897 24 138
| 26 19 |
ngs 215| 0 0 0 73 84 28 -.15 14 11 | -1878 102 2072 4108
| -75 39 |
sio 259| -2 1 1 42 10 -8 -.15 21 18 | --- --- --- ---
| -105 9 |
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 3.1596.0 GPS week: 1596 Day: 0 MJD: 55416.000
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 | 19 56 --- 27 --- 49 --- 22 --- --- 17 | 26 39 --- 18 --- 74 --- 16 --- --- 17
2 | 7 18 10 9 42 4 20 12 8 46 6 | 24 34 27 28 38 27 34 28 25 45 25
3E | 9 16 10 10 14 6 14 16 20 14 4 | 17 25 26 18 25 16 30 21 24 24 19
4 | 6 11 7 9 18 5 14 9 9 24 3 | 25 26 29 30 34 29 22 29 31 33 27
5 | 8 20 9 12 13 5 21 9 10 20 4 | 12 26 17 21 24 16 25 19 14 17 15
6E | 12 22 10 13 17 4 16 20 20 17 5 | 25 37 33 28 37 30 38 37 32 41 30
7 | 13 20 10 10 19 4 20 7 13 17 4 | 17 30 22 15 31 17 31 17 16 12 16
8 | 7 10 7 8 18 5 10 7 9 23 3 | 21 28 23 22 32 25 32 24 27 34 24
9 | 7 10 6 7 22 4 12 12 15 20 4 | 13 14 12 12 16 11 16 16 16 18 10
10 | 8 11 9 8 16 4 12 10 7 17 3 | 24 27 32 29 36 27 24 26 26 23 27
11 | 7 16 5 10 19 6 20 10 9 11 3 | 27 36 31 30 48 30 38 30 33 31 30
12 | 8 17 8 17 33 4 24 9 9 18 5 | 18 27 17 18 35 17 29 17 18 20 16
13E | 7 13 5 8 19 5 21 11 10 19 4 | 19 23 20 19 29 17 26 16 15 21 17
14E | 7 10 7 9 18 4 22 10 7 15 3 | 13 21 19 15 26 15 23 18 15 18 15
15E | 10 31 10 8 17 4 23 8 12 18 5 | 16 32 20 20 22 19 25 18 16 28 18
16 | 10 20 8 13 24 5 21 14 11 21 5 | 20 30 19 12 32 18 33 17 23 22 17
17E | 7 18 8 9 67 5 18 10 10 10 6 | 41 44 41 42 55 41 46 40 38 41 39
18 | 6 19 11 10 18 5 23 10 12 31 5 | 22 33 24 22 33 23 35 24 26 31 22
19 | 7 20 10 11 19 5 18 16 8 12 4 | 54 59 55 55 54 52 55 58 55 57 54
20 | 7 15 11 13 13 4 20 9 9 21 4 | 18 24 22 22 27 18 26 20 20 15 18
21 | 9 15 6 8 16 5 22 11 8 19 4 | 28 40 31 29 33 29 39 26 31 31 28
22 | 8 17 8 9 16 3 18 9 10 21 4 | 15 26 22 22 25 21 30 22 17 19 18
23E | 7 16 7 12 13 4 18 10 10 15 4 | 16 24 20 15 25 14 26 17 13 21 15
24 | 8 11 8 9 16 5 12 16 11 16 4 | 38 35 41 42 41 39 38 39 38 37 38
X25 | 29 --- 22 24 --- 26 --- 19 24 --- 12 | 58 --- 50 44 --- 44 --- 44 49 --- 46
26E | 13 13 11 10 24 6 16 10 19 12 4 | 19 22 23 20 32 17 30 16 24 19 17
27 | 7 10 8 8 21 4 12 10 15 16 4 | 13 14 14 10 15 11 19 15 17 15 11
28 | 7 19 7 5 26 5 18 9 9 19 4 | 19 29 21 14 34 17 31 14 18 19 17
X29E | 7 18 9 10 18 6 24 10 12 --- 4 | 28 32 27 29 32 26 36 33 28 --- 28
30 | 5 15 5 8 14 4 12 11 7 9 3 | 16 28 18 17 25 21 26 15 18 14 17
31 | 8 16 7 13 23 4 25 13 11 14 4 | 14 27 17 18 30 16 30 17 14 15 15
32 | 7 13 8 9 15 4 15 10 7 13 3 | 12 17 18 15 22 12 20 17 14 14 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 8 10 23 5 18 11 11 19 |T 22 29 25 23 31 24 30 23 24 25 22
WRMS | 8 17 8 10 18 5 17 11 9 15 |NE 20 27 23 21 29 25 27 21 22 23 19
MEDI | 7 16 8 9 18 5 18 10 10 17 |MD 19 28 22 20 32 19 30 19 23 21 18
Table 3.1596.1 GPS week: 1596 Day: 1 MJD: 55417.000
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 58 --- 17 --- 71 --- 22 --- --- 16 | 28 37 --- 32 --- 87 --- 15 --- --- 23
2 | 7 17 10 14 15 5 18 9 7 45 5 | 18 24 20 25 21 19 27 20 20 38 17
3E | 10 15 6 13 13 4 13 13 19 16 4 | 19 28 25 25 28 20 30 25 26 32 22
4 | 6 10 7 8 9 5 9 5 6 23 3 | 27 24 27 27 28 25 24 28 27 31 26
5 | 5 20 8 13 14 6 21 9 10 19 4 | 12 23 15 20 16 13 24 16 16 14 12
6E | 13 21 10 15 19 5 17 18 21 16 5 | 31 42 32 32 40 29 43 36 31 37 31
7 | 12 22 8 9 18 5 23 9 9 17 4 | 16 31 19 16 28 15 31 17 15 14 15
8 | 6 12 6 9 15 4 8 8 12 22 3 | 26 29 26 26 28 26 29 26 23 33 25
9 | 6 12 9 8 15 5 11 9 9 15 3 | 14 15 14 17 22 13 16 18 14 22 13
10 | 5 12 4 9 13 5 11 5 8 14 3 | 19 19 19 17 21 18 18 18 20 21 18
11 | 5 15 6 10 16 3 16 9 9 7 3 | 27 31 29 26 39 24 34 27 25 23 26
12M | 7 19 7 15 28 5 24 7 8 16 4 | 26 30 23 23 39 24 33 24 23 26 23
13E | 5 18 6 7 16 6 19 9 11 11 3 | 17 29 20 15 26 17 23 16 17 17 16
14E | 6 11 8 9 15 5 19 11 9 12 3 | 10 17 16 13 23 12 19 15 12 12 10
15E | 6 25 8 13 12 3 24 8 8 15 4 | 17 26 19 20 21 16 23 17 19 20 17
16 | 8 24 9 12 18 5 22 14 9 19 4 | 18 30 17 13 30 15 30 18 18 18 15
17E | 5 13 8 6 22 3 14 8 8 15 3 | 36 37 36 36 40 38 38 36 35 42 35
18 | 8 21 8 10 13 4 22 8 10 28 4 | 23 29 23 25 27 22 35 22 23 30 22
19E | 7 20 7 12 20 7 17 17 14 12 4 | 56 59 57 55 58 57 59 57 60 56 56
20 | 6 16 9 14 10 4 17 9 8 19 4 | 17 21 13 18 20 13 23 18 15 18 13
21M | 8 18 7 6 14 8 23 16 11 17 4 | 34 35 31 31 34 35 40 35 36 37 32
22 | 5 17 7 7 15 4 19 10 9 19 4 | 13 24 20 14 29 15 26 15 13 16 14
23E | 6 22 7 11 13 5 17 10 7 10 3 | 15 28 16 16 18 14 22 15 13 14 13
24 | 7 11 6 8 13 5 11 14 10 17 3 | 39 39 41 41 42 41 39 43 42 43 39
X25M | 23 --- 15 27 --- 17 --- 21 19 --- 10 | 65 --- 61 58 --- 59 --- 58 61 --- 60
26E | 9 14 8 12 14 6 14 8 24 13 4 | 19 23 22 26 24 21 25 21 30 27 20
27 | 7 11 9 9 12 4 11 9 9 12 3 | 14 17 15 19 18 15 19 20 15 22 14
28 | 7 20 6 8 21 4 17 9 10 20 4 | 17 29 23 14 31 17 30 15 16 21 17
X29E | 8 18 8 11 17 4 22 14 8 --- 4 | 19 25 20 20 29 21 26 23 23 --- 19
30M | 5 15 5 6 11 6 13 9 9 9 3 | 20 26 21 20 28 18 25 23 18 21 20
31 | 7 16 9 9 22 4 21 9 10 14 4 | 17 25 18 17 29 16 29 18 18 17 15
32 | 5 14 6 7 12 5 15 8 7 11 3 | 13 17 14 11 19 11 18 15 11 13 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 8 10 16 5 17 10 11 18 |T 23 28 24 24 28 24 28 24 23 25 22
WRMS | 7 17 7 9 14 5 17 10 9 16 |NE 20 25 20 22 25 25 25 21 20 24 18
MEDI | 7 17 8 9 15 5 17 9 9 16 |MD 19 28 20 20 28 18 26 20 20 22 18
Table 3.1596.2 GPS week: 1596 Day: 2 MJD: 55418.000
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 | 28 --- --- 21 --- 28 --- 13 38 --- 14 | 27 --- --- 23 --- 43 --- 9 3 --- 15
2 | 7 17 8 9 16 5 18 6 6 44 5 | 19 27 23 22 22 20 29 21 20 39 20
3E | 9 16 8 7 19 6 15 9 22 14 4 | 30 37 35 30 34 31 40 32 36 29 30
4 | 8 9 10 10 13 3 11 5 9 25 3 | 43 44 45 50 46 44 42 45 47 43 44
5 | 6 18 8 14 16 5 21 10 11 18 4 | 11 23 13 18 20 12 24 16 13 15 11
6E | 11 19 10 11 20 7 16 15 22 17 5 | 36 44 41 39 48 40 46 44 51 48 41
7 | 7 19 9 10 19 4 17 6 11 18 4 | 16 31 22 21 29 17 29 20 20 19 19
8M | 7 12 7 6 18 3 9 7 12 23 3 | 32 36 32 33 35 32 35 35 33 39 32
9 | 8 16 9 5 13 4 13 9 8 14 3 | 19 23 24 19 24 22 21 23 21 24 20
10 | 7 12 5 7 14 4 12 5 8 15 3 | 16 23 21 20 25 19 19 19 20 20 18
11M | 7 15 8 9 20 5 17 5 6 9 3 | 25 35 31 29 39 28 33 30 30 30 28
12 | 7 21 10 14 22 5 25 10 10 17 4 | 20 29 14 17 31 16 30 17 19 18 15
13E | 5 16 8 8 13 7 19 7 8 11 3 | 20 24 20 20 31 18 27 21 19 21 19
14E | 7 11 7 11 16 5 21 9 8 12 3 | 11 20 15 15 20 12 20 15 14 14 12
15E | 8 27 10 11 15 3 24 10 7 15 4 | 12 26 18 18 21 14 24 14 9 21 13
16 | 8 22 9 12 15 6 28 9 11 17 4 | 16 27 19 12 30 14 33 17 18 19 16
17E | 7 16 9 8 27 5 19 7 8 21 4 | 27 34 30 27 32 26 36 26 28 26 27
18M | 8 19 10 13 14 6 26 9 8 28 4 | 29 38 35 35 33 32 41 35 35 44 33
19E | 10 24 10 11 23 5 20 12 9 12 4 | 36 50 43 42 47 40 46 45 42 47 41
20M | 6 17 11 8 10 7 18 11 10 24 4 | 18 22 16 18 22 17 24 23 19 25 17
21 | 8 20 8 8 16 6 26 11 8 19 4 | 29 39 30 28 33 26 38 28 31 32 29
22M | 8 17 11 7 15 5 22 9 7 20 4 | 9 23 15 13 23 11 26 16 13 14 12
23E | 7 19 8 9 22 5 18 8 11 12 4 | 10 26 15 17 21 13 22 12 15 14 12
24 | 5 13 5 8 15 7 14 9 11 17 3 | 29 31 30 29 33 31 28 33 37 39 32
X25 | 26 --- 24 23 --- 13 --- 25 20 --- 12 | 65 --- 57 54 --- 57 --- 54 55 --- 54
26E | 12 12 12 10 16 5 15 10 23 15 4 | 20 23 25 26 27 21 27 19 27 25 20
27 | 7 14 9 7 13 5 14 9 10 13 3 | 25 28 30 26 31 27 27 29 28 27 26
28M | 9 19 7 9 21 5 17 8 11 23 4 | 20 31 25 16 31 17 30 20 19 20 18
X29E | 9 24 9 11 17 4 23 8 9 --- 4 | 21 30 22 26 29 21 30 26 23 --- 21
30 | 6 12 5 6 15 4 14 9 10 13 3 | 15 20 20 18 23 16 21 21 19 19 17
31 | 7 16 6 11 22 5 25 9 8 14 4 | 12 26 16 15 29 12 27 15 15 13 13
32M | 6 13 7 8 16 5 14 7 9 10 3 | 11 18 14 12 21 12 19 14 15 15 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 9 9 17 5 19 9 11 19 |T 22 29 25 24 29 23 29 24 24 26 23
WRMS | 7 17 8 9 17 5 18 8 9 17 |NE 21 28 24 23 28 23 27 22 22 25 21
MEDI | 7 16 9 9 16 5 18 9 9 17 |MD 20 27 23 21 29 20 28 21 20 24 19
Table 3.1596.3 GPS week: 1596 Day: 3 MJD: 55419.000
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 | 18 --- --- 29 --- 35 --- 17 --- --- 15 | 25 --- --- 24 --- 72 --- 13 --- --- 22
2 | 9 18 6 13 19 5 21 8 7 45 5 | 22 31 23 27 29 24 33 22 26 41 23
3E | 9 16 6 10 14 4 16 11 20 11 4 | 18 27 25 22 27 22 29 25 34 24 22
4 | 7 12 5 9 12 3 13 10 7 23 3 | 31 30 28 38 33 30 30 31 30 36 30
5 | 6 20 7 13 12 3 22 9 11 17 4 | 12 24 16 21 20 14 26 17 17 16 14
6E | 11 16 7 10 14 5 16 15 21 16 4 | 35 43 40 37 43 37 45 42 45 43 38
7 | 6 17 6 10 14 5 19 9 6 14 3 | 14 25 19 18 27 16 25 14 18 12 15
8 | 6 14 6 8 16 3 10 11 7 23 3 | 18 23 23 21 20 18 23 17 19 29 18
9 | 8 16 6 9 16 4 12 13 9 15 3 | 13 18 15 15 16 9 17 18 12 17 11
10 | 7 14 6 9 12 4 17 11 6 18 3 | 17 23 23 25 28 21 24 25 20 25 20
11 | 7 14 5 9 17 3 18 5 9 10 3 | 20 27 20 22 34 20 29 20 17 21 19
12 | 8 22 8 16 32 6 26 8 12 20 5 | 24 33 24 24 33 22 34 25 22 22 21
13E | 6 15 5 12 19 4 22 8 10 13 3 | 22 28 25 27 27 22 28 23 25 24 23
14E | 8 14 10 9 17 6 18 17 8 11 4 | 14 24 26 14 25 18 25 28 19 21 19
15E | 8 23 7 12 24 3 22 12 7 15 4 | 15 23 20 19 24 16 24 18 17 22 16
16 | 7 21 6 16 12 6 25 8 10 17 4 | 21 32 20 16 28 19 34 20 26 22 20
17E | 6 20 8 13 23 4 19 10 9 26 4 | 40 45 42 44 45 42 46 41 42 49 41
18 | 6 20 5 14 16 5 22 8 6 29 4 | 18 29 21 25 26 17 29 23 20 26 19
19E | 5 21 9 10 16 5 18 9 12 11 4 | 49 57 53 53 56 51 57 51 56 49 51
20 | 7 15 4 12 10 4 17 6 8 19 3 | 21 21 20 21 24 16 21 18 19 14 17
21 | 10 19 6 8 13 5 22 13 13 22 4 | 28 36 29 31 36 28 36 30 29 30 28
22 | 7 17 5 8 15 6 18 11 8 23 4 | 14 26 23 21 27 16 28 23 18 22 18
23E | 9 21 6 14 19 4 19 9 9 10 4 | 19 28 20 19 21 18 25 18 17 18 17
24 | 5 11 6 7 16 5 11 9 11 17 3 | 54 56 57 60 61 58 57 59 58 59 57
X25 | 34 --- 17 25 --- 13 --- 28 20 --- 13 | 64 --- 55 44 --- 46 --- 40 39 --- 48
26E | 12 15 8 10 22 4 17 12 18 17 4 | 18 23 21 24 33 18 27 20 24 23 18
27 | 8 12 6 10 15 3 12 13 7 14 3 | 18 20 23 18 23 17 23 21 19 21 18
28 | 6 20 6 8 18 3 19 10 5 23 4 | 15 30 21 21 32 16 31 18 16 21 17
X29E | 10 26 8 13 17 5 25 19 10 --- 5 | 30 39 30 32 37 31 37 38 35 --- 31
30 | 7 15 4 7 11 3 15 11 9 12 3 | 14 20 15 17 21 14 21 20 14 16 13
31 | 6 15 7 12 18 5 23 8 12 14 4 | 17 27 21 18 28 17 29 19 26 19 18
32 | 5 14 7 9 13 4 11 8 8 11 3 | 18 21 19 18 24 17 21 19 18 18 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 6 11 17 4 18 10 11 19 |T 23 29 26 26 30 25 30 25 25 26 23
WRMS | 7 17 6 10 15 4 18 10 7 17 |NE 22 28 24 25 29 27 29 23 25 26 22
MEDI | 7 16 6 10 16 4 18 10 9 17 |MD 18 27 23 22 27 18 28 21 20 22 19
Table 3.1596.4 GPS week: 1596 Day: 4 MJD: 55420.000
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 65 --- 28 --- 115 --- --- --- --- 24 | 19 36 --- 27 --- 63 --- --- --- --- 17
2 | 8 21 9 9 17 4 22 12 12 46 5 | 23 32 29 25 22 25 32 27 28 43 25
3E | 9 17 7 14 21 5 14 11 18 10 4 | 16 26 18 23 25 20 25 21 24 19 18
4 | 6 12 6 8 13 4 11 17 9 21 4 | 42 41 46 42 44 42 39 50 40 45 43
5 | 9 17 10 11 12 3 17 9 9 18 4 | 17 21 20 22 24 17 22 22 18 21 17
6E | 9 20 8 12 15 4 16 17 21 17 5 | 24 39 30 25 36 26 39 35 30 35 28
7 | 8 16 8 10 17 3 18 7 12 12 4 | 14 26 22 17 29 16 28 17 14 14 16
8 | 5 11 7 5 15 5 9 10 11 22 3 | 18 25 21 23 24 20 27 22 21 30 19
9 | 7 17 5 6 13 4 14 12 10 15 3 | 17 25 20 24 22 19 18 27 25 28 19
10 | 8 13 6 8 12 4 11 11 7 18 3 | 21 24 28 25 29 24 23 28 25 30 24
11 | 8 15 6 7 18 4 17 6 9 13 3 | 22 29 27 23 37 23 30 24 20 24 23
12 | 8 21 11 16 25 5 24 14 9 18 5 | 23 31 20 25 29 20 33 22 17 21 19
13E | 6 18 5 7 15 5 19 9 11 10 3 | 19 27 19 18 30 18 26 21 20 19 19
14E | 7 14 7 10 15 4 20 12 10 13 4 | 17 21 21 18 23 15 23 20 20 17 17
15E | 6 22 8 11 17 4 21 13 11 18 4 | 14 24 20 24 21 18 24 19 16 24 16
16 | 8 23 8 14 18 4 21 9 10 15 4 | 18 31 19 15 29 17 32 19 20 20 18
17E | 7 18 7 11 25 4 18 15 9 19 4 | 31 35 29 27 31 28 32 38 31 39 30
18 | 7 22 9 10 13 5 23 12 7 28 4 | 22 31 25 25 26 22 33 23 20 26 21
19E | 5 20 6 11 18 6 16 7 7 15 3 | 52 56 52 47 53 50 51 52 53 56 51
20 | 6 17 6 8 10 3 15 7 5 19 3 | 19 23 22 19 26 18 22 20 18 18 19
21 | 7 19 8 8 14 4 23 9 11 21 4 | 21 31 26 25 29 24 32 25 23 24 23
22 | 8 19 9 10 16 5 18 11 9 23 4 | 15 27 24 21 26 17 29 24 19 22 19
23E | 7 19 6 8 16 4 18 11 11 23 4 | 17 28 21 14 26 18 26 21 20 27 18
24 | 5 10 5 9 13 5 12 8 9 15 3 | 30 29 31 24 34 29 29 27 34 29 30
X25 | 36 --- 19 24 --- 16 --- 26 19 --- 13 | 61 --- 45 32 --- 39 --- 28 30 --- 40
26E | 10 17 8 11 23 6 14 21 22 22 5 | 14 25 20 22 31 18 26 28 29 26 18
27 | 7 17 6 8 13 5 14 14 10 15 3 | 26 32 26 32 27 27 26 36 32 37 27
28 | 7 19 8 7 22 4 17 11 8 25 4 | 19 29 23 21 34 18 31 22 17 27 19
X29E | 7 23 10 12 11 3 21 9 12 --- 4 | 29 36 33 27 33 29 37 29 33 --- 30
30 | 6 15 5 7 16 3 12 8 10 14 3 | 18 23 22 22 22 18 24 21 19 18 18
31 | 5 14 7 9 21 4 18 9 11 14 3 | 16 27 21 20 30 17 28 18 19 18 17
32 | 5 15 8 8 13 3 12 12 7 10 3 | 15 18 21 15 23 16 18 20 18 17 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 7 10 17 4 17 12 11 20 |T 22 29 25 24 29 24 28 26 24 26 22
WRMS | 7 17 7 9 15 4 17 10 8 18 |NE 22 29 26 24 29 26 27 27 25 28 23
MEDI | 7 17 7 9 15 4 17 11 10 18 |MD 19 28 22 23 29 20 28 23 20 24 19
Table 3.1596.5 GPS week: 1596 Day: 5 MJD: 55421.000
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 --- --- 18 --- 312 --- --- --- --- 15 | 17 --- --- 28 --- 175 --- --- --- --- 18
2 | 8 21 10 10 17 6 23 15 10 48 6 | 21 32 28 23 29 24 34 25 21 48 23
3E | 10 20 8 7 25 4 16 10 25 10 5 | 18 28 21 24 33 22 29 24 37 24 22
4 | 8 14 10 8 11 5 12 12 12 21 4 | 29 33 33 32 30 30 34 35 29 37 30
5 | 8 18 8 12 11 4 19 9 8 18 4 | 11 22 14 19 16 15 24 18 14 20 13
6E | 10 22 8 8 19 4 17 16 23 17 5 | 30 46 39 35 46 37 47 44 42 46 37
7 | 7 18 5 10 16 4 18 8 10 12 3 | 11 25 17 15 27 12 26 13 12 11 13
8 | 5 12 7 8 14 4 11 11 10 21 3 | 16 23 18 19 18 16 23 21 14 28 17
9 | 6 12 8 5 12 3 10 13 11 14 3 | 14 21 17 21 22 17 22 27 20 24 17
10 | 8 12 7 10 16 5 13 12 13 18 4 | 20 23 25 22 26 21 24 24 19 27 21
11 | 7 16 5 11 19 6 22 7 9 10 3 | 15 27 17 18 34 15 28 15 20 16 16
12 | 7 18 8 15 24 5 22 9 13 18 4 | 21 26 17 20 28 17 29 22 15 19 17
13E | 5 16 8 7 22 4 21 8 10 14 4 | 21 26 25 24 32 23 30 23 25 25 23
14E | 6 17 9 11 17 3 20 10 12 14 4 | 14 22 23 19 24 16 23 21 18 17 17
15E | 9 28 9 15 15 5 22 12 13 17 5 | 13 29 22 26 27 19 26 22 19 28 18
16 | 6 22 8 15 18 4 24 10 12 17 4 | 17 30 20 14 27 17 34 19 18 20 18
17E | 6 17 9 12 18 4 22 10 12 10 4 | 38 43 44 38 41 40 47 39 39 39 39
18 | 6 22 10 9 13 5 24 21 9 28 5 | 15 28 21 21 23 19 31 22 22 20 16
19E | 4 19 8 7 16 7 16 11 9 12 3 | 30 35 34 29 34 30 38 30 33 30 30
20 | 6 17 6 11 12 4 16 9 12 20 4 | 15 20 16 17 18 13 22 18 15 14 13
21 | 7 20 9 6 14 6 27 11 8 20 4 | 23 34 29 27 33 28 40 27 27 25 26
22 | 7 18 12 7 15 5 21 9 7 22 4 | 16 29 26 20 28 20 31 22 21 23 20
23E | 7 19 9 8 18 6 20 11 11 15 4 | 14 24 17 14 18 12 22 19 16 21 14
24 | 4 10 7 6 17 3 11 9 11 14 3 | 40 43 48 46 48 45 45 46 46 48 45
X25 | 25 --- 21 27 --- 23 --- 32 28 --- 13 | 49 --- 53 37 --- 41 --- 31 30 --- 39
26E | 11 19 8 10 20 5 14 19 23 19 5 | 13 26 19 22 26 17 26 23 26 25 17
27 | 7 13 9 9 16 4 10 15 12 12 4 | 22 30 25 31 33 25 28 35 27 31 26
28 | 6 20 9 9 23 5 17 9 8 27 4 | 12 29 22 16 31 15 28 15 15 22 15
X29E | 5 32 7 11 15 6 22 10 9 --- 5 | 16 33 19 19 27 18 29 19 15 --- 17
30 | 6 12 5 11 17 4 12 10 10 14 3 | 14 20 17 15 21 14 22 17 15 15 14
31 | 7 14 7 9 23 3 19 8 10 16 4 | 16 27 19 17 30 17 28 16 19 17 15
32 | 6 16 5 9 14 4 12 13 12 13 3 | 13 13 17 16 19 14 20 20 17 17 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 8 10 17 5 18 12 13 19 |T 19 28 24 23 28 26 29 24 22 25 21
WRMS | 7 18 8 10 16 4 17 11 10 18 |NE 19 28 24 24 28 36 29 25 22 28 21
MEDI | 7 18 8 9 16 4 18 10 11 17 |MD 16 27 21 21 27 18 28 22 20 24 17
Table 3.1596.6 GPS week: 1596 Day: 6 MJD: 55422.000
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 --- --- 20 --- 228 --- --- --- --- 17 | 24 --- --- 23 --- 174 --- --- --- --- 21
2 | 7 23 7 8 14 4 24 13 12 50 6 | 24 34 24 21 30 23 35 22 22 51 22
3E | 9 18 6 9 12 4 18 13 24 13 4 | 26 32 25 21 28 24 34 23 36 22 23
4 | 7 11 9 5 15 4 10 14 13 22 4 | 29 27 30 31 36 27 28 32 27 40 28
5 | 9 18 11 11 18 3 19 6 17 23 4 | 13 20 16 16 24 13 25 16 17 21 13
6E | 8 19 7 9 15 4 17 17 23 14 4 | 33 45 37 38 43 36 46 41 46 42 37
7 | 7 21 7 10 20 4 20 5 11 14 4 | 12 27 19 15 27 13 27 12 13 13 13
8 | 5 12 7 4 18 3 8 5 15 22 3 | 16 21 17 12 18 13 23 16 17 26 16
9 | 9 13 8 7 13 4 11 10 16 12 3 | 19 23 21 11 22 16 23 16 15 17 17
10 | 7 11 7 6 16 4 11 7 13 17 3 | 22 22 25 22 32 22 23 25 22 23 22
11 | 6 15 6 6 20 4 19 8 9 9 3 | 22 29 27 26 39 24 30 25 20 26 23
12 | 7 19 12 11 25 5 24 9 14 21 5 | 23 31 21 15 32 20 35 22 17 23 19
13E | 7 13 6 7 19 3 20 10 15 28 4 | 22 25 22 17 28 19 27 22 23 31 20
14E | 7 16 8 10 16 5 20 13 13 16 4 | 12 22 20 15 23 14 23 19 17 18 14
15E | 8 23 10 13 17 4 22 9 14 18 4 | 15 22 19 17 24 13 23 18 15 25 16
16 | 7 22 6 13 25 5 22 12 9 22 4 | 22 34 20 18 37 20 36 20 26 21 21
17E | 7 15 7 8 24 4 21 13 13 11 4 | 32 41 39 36 38 35 41 30 35 35 33
18 | 7 19 8 10 15 3 23 18 9 30 5 | 17 28 20 21 24 17 31 22 17 26 17
19E | 6 22 6 13 21 4 17 8 9 10 4 | 55 63 56 57 55 56 60 54 59 56 54
20 | 7 16 7 10 21 5 22 10 14 24 4 | 19 23 22 18 28 18 24 17 18 17 18
21 | 10 19 8 8 19 6 27 12 13 19 4 | 24 36 24 23 32 22 36 25 20 23 22
22 | 8 16 7 9 14 3 23 6 7 21 4 | 18 28 22 19 27 17 29 18 17 20 17
23E | 6 19 8 10 19 5 20 9 14 26 4 | 14 23 15 15 19 12 23 14 15 23 12
24 | 4 10 4 8 17 3 14 8 11 13 3 | 37 38 40 42 44 38 35 38 40 43 38
X25 | 25 --- 20 21 --- 16 --- 24 20 --- 11 | 64 --- 51 43 --- 41 --- 38 39 --- 46
26E | 13 14 8 9 18 6 15 22 24 18 5 | 16 22 19 24 21 17 26 26 28 27 18
27 | 8 14 7 8 13 5 10 13 16 13 3 | 22 27 25 15 25 20 27 20 19 20 21
28 | 7 21 7 10 21 5 19 8 13 27 4 | 18 28 20 17 31 16 31 18 18 26 17
X29E | 9 22 9 11 26 3 27 10 13 --- 5 | 25 31 25 21 35 25 38 24 29 --- 24
30 | 8 10 6 7 21 4 11 6 11 13 3 | 18 22 17 18 28 17 26 16 19 14 18
31 | 5 16 7 10 21 6 16 7 11 17 3 | 17 28 16 21 33 18 29 17 18 19 18
32 | 6 13 6 9 20 5 20 15 14 14 4 | 15 19 18 13 27 15 20 20 16 16 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 7 9 19 4 19 11 14 21 |T 23 29 24 22 30 26 30 23 23 26 22
WRMS | 7 17 8 8 18 4 19 10 11 18 |NE 21 28 23 21 31 34 28 21 21 26 21
MEDI | 7 16 7 9 18 4 19 10 13 18 |MD 22 27 22 19 28 19 28 22 19 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 4.1596 GPS week: 1596 MJD: 55416.0-55422.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 |U 8 8 23 |U 7 9 27 |U 9 8 18 |
emr | emr 2906 | 11 10 28 |U 10 15 38 | 10 9 21 |
esa | esa 2976 | 9 9 25 |U 7 9 26 | 9 8 18 |
gfz | gfz 3060 |U 8 8 23 |U 8 14 31 |U 8 7 17 |
grg | grg 2880 | 9 10 23 |U 6 10 27 | 10 7 20 |
igr | igr 2970 | 9 8 24 | 7 11 27 | 9 8 17 |
igs | igs 2951 | 9 8 23 | 7 9 26 | 9 8 18 |
jpl | jpl 2865 |U 9 9 25 | 9 15 37 | 8 8 20 |
mit | mit 3030 |U 8 8 22 |U 10 19 39 |U 15 16 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 5.1596.0 GPS week: 1596 Day: 0 MJD: 55416.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 11 11 27 | ---- ---- ---- | 10 8 28 |
emr | emr 2957 | 11 11 22 | ---- ---- ---- | 10 8 23 |
esa | esa 2976 | 9 9 18 | ---- ---- ---- | 9 7 20 |
gfz | gfz 3060 | 9 8 18 | ---- ---- ---- | 8 6 20 |
grg | grg 2880 | 10 10 17 | ---- ---- ---- | ---- ---- ---- |
igr | igr 2986 | 9 7 17 | ---- ---- ---- | 9 6 19 |
igs | igs 2958 | 9 8 17 | ---- ---- ---- | 9 7 21 |
jpl | jpl 2868 | 10 8 19 | ---- ---- ---- | 9 8 23 |
mit | mit 3072 | 8 8 18 | ---- ---- ---- | 11 12 40 |
Table 5.1596.1 GPS week: 1596 Day: 1 MJD: 55417.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 7 6 15 | 5 9 20 | 8 8 14 |
emr | emr 2957 | 8 8 24 | 9 12 28 | 11 8 17 |
esa | esa 2976 | 7 8 19 | 6 7 19 | 9 6 13 |
gfz | gfz 3060 | 7 7 20 | 5 11 21 | 8 6 12 |
grg | grg 2880 | 7 7 20 | 8 9 26 | 10 5 15 |
igr | igr 2933 | 8 7 21 | 5 10 23 | 8 5 15 |
igs | igs 2918 | 7 7 18 | 6 7 23 | 8 6 13 |
jpl | jpl 2866 | 7 7 18 | 7 15 24 | 9 7 16 |
mit | mit 3072 | 7 7 19 | 7 15 22 | 9 12 33 |
Table 5.1596.2 GPS week: 1596 Day: 2 MJD: 55418.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 6 6 18 | 17 17 54 | 10 11 18 |
emr | emr 2868 | 11 12 26 | 18 26 62 | 13 13 22 |
esa | esa 2976 | 7 6 19 | 17 18 55 | 10 9 21 |
gfz | gfz 3061 | 7 6 21 | 17 18 58 | 9 9 20 |
grg | grg 2880 | ---- ---- ---- | 9 15 34 | ---- ---- ---- |
igr | igr 3002 | 8 7 19 | 13 17 40 | 10 10 20 |
igs | igs 3003 | 7 6 18 | 16 18 55 | 11 9 20 |
jpl | jpl 2861 | 8 8 23 | 17 22 59 | 10 11 23 |
mit | mit 3072 | 7 7 19 | 19 26 66 | 46 53 79 |
Table 5.1596.3 GPS week: 1596 Day: 3 MJD: 55419.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 10 7 26 | 8 11 33 | 9 9 18 |
emr | emr 2867 | 15 12 41 | 11 19 50 | 11 13 24 |
esa | esa 2976 | 12 8 33 | 8 12 31 | 8 10 22 |
gfz | gfz 3060 | 11 7 26 | 9 21 40 | 8 10 20 |
grg | grg 2880 | 12 8 27 | 7 14 40 | 11 11 22 |
igr | igr 2969 | 12 8 34 | 8 12 32 | 8 10 20 |
igs | igs 2911 | 12 8 30 | 8 12 31 | 8 10 23 |
jpl | jpl 2867 | 11 9 32 | 10 15 50 | 9 11 22 |
mit | mit 3072 | 10 7 26 | 11 19 45 | 13 14 30 |
Table 5.1596.4 GPS week: 1596 Day: 4 MJD: 55420.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 9 9 31 | 5 5 18 | 11 9 18 |
emr | emr 2961 | 11 9 31 | 8 11 26 | 11 11 19 |
esa | esa 2976 | 9 10 33 | 5 5 16 | 11 9 16 |
gfz | gfz 3060 | 9 9 32 | 6 8 21 | 10 8 16 |
grg | grg 2880 | 9 9 27 | 5 7 17 | 13 9 19 |
igr | igr 2967 | 10 9 31 | 5 6 21 | 11 9 16 |
igs | igs 2967 | 9 8 31 | 4 4 16 | 10 9 17 |
jpl | jpl 2861 | 10 8 29 | 7 11 26 | 9 9 22 |
mit | mit 2976 | 9 8 31 | 9 19 31 | 9 8 18 |
Table 5.1596.5 GPS week: 1596 Day: 5 MJD: 55421.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 9 12 26 | 5 4 19 | 7 5 14 |
emr | emr 2868 | 11 12 31 | 7 7 26 | 7 5 21 |
esa | esa 2976 | 10 13 29 | 4 5 19 | 8 6 14 |
gfz | gfz 3060 | 8 11 27 | 7 16 27 | 7 6 14 |
grg | grg 2880 | 10 12 23 | 4 7 21 | 9 4 21 |
igr | igr 2957 | 9 12 28 | 4 6 18 | 7 5 13 |
igs | igs 2934 | 10 11 28 | 5 5 18 | 7 5 13 |
jpl | jpl 2865 | 10 13 33 | 6 10 22 | 7 6 19 |
mit | mit 2976 | 8 10 27 | 8 18 29 | 8 5 16 |
Table 5.1596.6 GPS week: 1596 Day: 6 MJD: 55422.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3050 | 7 9 16 | 4 5 17 | 9 9 18 |
emr | emr 2868 | 11 10 24 | 6 17 35 | 7 6 20 |
esa | esa 2976 | 8 9 25 | 4 5 16 | 8 8 18 |
gfz | gfz 3060 | 7 8 17 | 4 7 21 | 8 8 17 |
grg | grg 2880 | 8 13 22 | 5 7 22 | 9 7 23 |
igr | igr 2979 | 7 8 17 | 4 13 29 | 8 7 18 |
igs | igs 2971 | 8 9 21 | 4 5 15 | 8 8 19 |
jpl | jpl 2867 | 8 8 21 | 6 18 39 | 7 9 17 |
mit | mit 2976 | 7 7 16 | 7 16 39 | 8 11 22 |
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 6.1596 GPS week: 1596 MJD: 55416.500-55422.500
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 | -19 -36 39 -60 -7 | 6 13
| 19 18 102 87 6 | 2
emr uuuuu | 15 22 45 155 14 | 44 46
| 7 18 66 82 6 | 10
esa uuuuu | -13 -38 78 -1 3 | 14 20
| 7 14 62 53 6 | 5
gfz uuuuu | 29 27 -66 11 0 | 1 11
| 15 16 47 50 4 | 3
grg uuuux | -12 -58 110 -252 -26 | -1 32
| 30 48 180 134 41 | 4
igr xxxxx | 7 42 -2 38 2 | 1 12
| 8 11 40 36 7 | 5
irf xxxxx | 3 -16 -39 -55 -4 | -1 13
| 15 18 78 48 11 | 4
jpl uuuuu | 19 -20 25 -33 3 | 38 41
| 19 22 123 60 16 | 7
mit uuuuu | -12 -32 -56 -172 -3 | 11 18
| 17 30 95 66 12 | 4
ngs uuuuu | -3 58 -48 231 1 | 6 13
| 20 43 104 103 9 | 3
sio uuuuu | -21 71 -37 43 -9 | 32 34
| 20 23 142 97 12 | 3
Table 7.1596.0 GPS week: 1596 Day: 0 MJD: 55416.500
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 -20 -113 -223 -4 | 1 13
emr uuuuu | 11 18 -50 35 14 | 30 33
esa uuuuu | -14 -39 65 48 12 | 7 14
gfz uuuuu | 22 30 -124 105 -1 | -4 11
grg uuuux | 29 -128 360 -9 -110 | 8 20
igr xxxxx | 4 46 -41 67 3 | -7 14
irf xxxxx | 1 15 -6 -117 7 | -9 14
jpl uuuuu | 5 -27 -7 -115 23 | 25 32
mit uuuuu | -8 21 6 -308 5 | 5 12
ngs uuuuu | 3 -5 -48 219 -18 | 2 12
sio uuuuu | -41 111 5 -75 3 | 27 29
Table 7.1596.1 GPS week: 1596 Day: 1 MJD: 55417.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -8 -50 7 32 -4 | 5 13
emr uuuuu | 5 -5 46 150 22 | 35 38
esa uuuuu | -21 -38 81 -2 1 | 11 18
gfz uuuuu | 31 23 -129 5 -6 | -1 11
grg uuuux | 14 -30 25 -201 -26 | -1 33
igr xxxxx | 10 42 8 74 4 | -3 13
irf xxxxx | 14 -11 25 -11 5 | -5 14
jpl uuuuu | 15 -44 51 -9 21 | 32 38
mit uuuuu | 3 -21 75 -123 7 | 8 15
ngs uuuuu | -5 64 -152 125 0 | 4 11
sio uuuuu | -25 73 9 78 2 | 30 32
Table 7.1596.2 GPS week: 1596 Day: 2 MJD: 55418.500
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 -23 -27 4 -14 | 6 12
emr uuuuu | 23 49 -10 103 12 | 40 42
esa uuuuu | -2 -59 196 38 -4 | 13 19
gfz uuuuu | 10 40 -35 41 -3 | 0 9
grg uuuux | -43 -74 104 -434 8 | -5 34
igr xxxxx | -1 30 13 66 -5 | 0 10
irf xxxxx | 12 -4 -72 15 4 | -3 12
jpl uuuuu | 33 -8 -50 -45 -1 | 38 41
mit uuuuu | 3 -14 -77 -120 8 | 10 16
ngs uuuuu | -23 27 -61 165 1 | 5 11
sio uuuuu | -9 86 -147 157 0 | 31 33
Table 7.1596.3 GPS week: 1596 Day: 3 MJD: 55419.500
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 -58 -1 -125 -15 | 7 12
emr uuuuu | 18 36 33 135 19 | 44 46
esa uuuuu | -12 -24 6 39 1 | 14 20
gfz uuuuu | 34 27 -35 -31 -3 | 1 10
grg uuuux | 0 -84 205 -220 11 | -2 34
igr xxxxx | 7 60 17 -17 -7 | 2 10
irf xxxxx | -7 -15 -95 -40 -1 | -1 13
jpl uuuuu | 23 2 277 -108 -21 | 40 43
mit uuuuu | -19 -34 -124 -141 2 | 12 19
ngs uuuuu | 4 48 -24 131 4 | 6 12
sio uuuuu | -32 60 -130 133 -6 | 32 34
Table 7.1596.4 GPS week: 1596 Day: 4 MJD: 55420.500
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 | -13 -22 109 -26 -7 | 5 12
emr uuuuu | 23 10 72 274 5 | 48 50
esa uuuuu | -22 -51 98 -103 2 | 15 20
gfz uuuuu | 19 -3 -53 -40 1 | 1 10
grg uuuux | -7 -32 78 -252 -19 | -2 34
igr xxxxx | -6 31 -72 37 -2 | 2 10
irf xxxxx | -19 -31 -77 -53 -7 | 0 13
jpl uuuuu | 51 13 -81 46 -4 | 39 42
mit uuuuu | -41 -58 -127 -147 -7 | 13 19
ngs uuuuu | 36 123 39 263 2 | 7 13
sio uuuuu | -40 52 -76 95 -15 | 33 35
Table 7.1596.5 GPS week: 1596 Day: 5 MJD: 55421.500
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 -60 101 -46 1 | 7 13
emr uuuuu | 18 31 71 249 14 | 53 55
esa uuuuu | -12 -38 79 4 10 | 19 24
gfz uuuuu | 57 49 -80 -20 3 | 4 13
grg uuuux | -22 -78 211 -358 -9 | -2 34
igr xxxxx | 17 48 18 -3 12 | 5 12
irf xxxxx | -3 -37 -137 -97 -17 | 3 13
jpl uuuuu | 16 -43 45 11 -6 | 44 46
mit uuuuu | -25 -62 -181 -196 -18 | 16 21
ngs uuuuu | -22 101 105 308 6 | 10 16
sio uuuuu | -16 41 -162 -11 -25 | 35 37
Table 7.1596.6 GPS week: 1596 Day: 6 MJD: 55422.500
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 -22 194 -40 -3 | 7 14
emr uuuuu | 10 14 156 137 10 | 56 59
esa uuuuu | -9 -20 21 -33 2 | 21 26
gfz uuuuu | 28 25 -4 17 6 | 5 14
grg uuuux | -54 20 -213 -290 -38 | -3 33
igr xxxxx | 16 40 43 39 9 | 7 16
irf xxxxx | 24 -28 90 -85 -19 | 3 12
jpl uuuuu | -9 -31 -62 -12 11 | 46 48
mit uuuuu | 5 -54 33 -167 -21 | 15 20
ngs uuuuu | -15 47 -197 408 10 | 11 19
sio uuuuu | 15 77 245 -78 -24 | 34 35
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