[IGSREPORT-19773] Wk 1634 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu May 19 23:41:47 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1634 (May 01, 2011 - May 07, 2011)
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:
igs1634[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1634[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1634[0-6].cls IGS GPS clock combination summary report.
igs16347.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16347.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 of poorer consistency (GRG),
they 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 | EMR | 8 8 MCM4 MCM4 YELL
0 | ESA | UNSA
0 | GFZ | 8 13 DAV1 GUAM MCM4 MDVJ
0 | JPL | 8 15 25 TIXI
0 | MIT | DAV1 SOFI
1 | COD | NRMD
1 | EMR | 8 8 KERG
1 | ESA | MCM4 MCM4 UNSA
1 | GFZ | 8 MDVJ
1 | GRG | USN3
1 | JPL | 8 15 25 MAC1 TIXI
1 | MIT | DARW MAC1 TIXI DARW MAC1
2 | ALL | 1 1
2 | EMR | 8 8
2 | GFZ | 8 MAW1 MDVJ
2 | JPL | 8 15 25 MAW1
2 | MIT | CHUR MAW1 MAW1 SOFI
3 | COD | ALGO ALGO BRAZ
3 | EMR | 8 8
3 | ESA | UNSA
3 | GFZ | 8 MAW1
3 | JPL | 8 15 25
3 | MIT | MAW1 HARB MAW1 MDVJ
4 | COD | MAS1 MAS1
4 | EMR | 8 10 8 10
4 | ESA | DAV1 UNSA
4 | GFZ | 8 10 MAS1 MDVJ
4 | GRG | DAV1 MAS1 WTZR
4 | JPL | 8 10 25 CHPI MAS1 MAW1
4 | MIT | CAS1 HARB MAW1 CAS1 MAS1
5 | COD | ONSA WILL
5 | EMR | 10 10 ONSA
5 | ESA | 9 9 MCM4 MCM4 UNSA
5 | GFZ | 8 DAV1 POVE SCH2 YAKT
5 | JPL | 9 10 25
5 | MIT | 9 MAW1 SCH2 MAW1 SCH2 SFER
6 | ESA | KERG UNSA
6 | GFZ | 8 MDVJ
6 | JPL | 15 25 TIXI
6 | MIT | 8 8 MAW1
5. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G11 | 2011_05_03 | 2011037
G11 | 2011_05_04 | 2011037
G23 | 2011_05_05 | 2011038
6. 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
----+--------+---------------
6 | GFZ | 10
6 | GRG | 10
6 | MIT | 10
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) 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. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
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 | -1.0 .4 -.1 -29 -17 -1 .32
EMR | -1.1 3.0 11.5 4 13 25 .55
ESA | .9 -4.2 17.0 -22 14 66 .32
GFZ | -3.4 .3 -1.0 -14 39 12 .40
GRG | 4.3 -4.0 25.5 -10 23 -37 .29
JPL | -1.1 -2.0 11.1 23 -51 47 -.63
MIT | 3.5 -6.5 14.4 -11 3 -16 .40
NGS | 5.6 -9.1 7.4 -39 -15 16 .42
SIO | 1.1 1.3 6.8 11 -19 -34 .49
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 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution does not yet use IGS08/igs08.atx, which causes their RMS
clock residuals to be higher than for the other centres; for the same
reason, the JPL solution is excluded from the weekly SINEX combination.
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 1.1634.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1634.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 2.1634.[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 3.1634.[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 5.1634.0-6).
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 1634 summary. (May 01, 2011 - May 07, 2011)
Table 1.1634.a GPS week: 1634 MJD: 55682.000-55688.000
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 247| 1 0 0 28 32 14 -.27 9 8 | -607 98 18 82
| 0 0 1 16 11 19 .02 | 262 343
emr 107| 0 2 2 -10 -38 6 .36 18 18 | 130 71 14 99
| 0 2 1 14 22 11 .03 | 843 1416
esa 143| -1 0 -2 20 28 15 .29 9 9 | -1384 162 16 118
| 0 0 1 24 18 19 .02 | 1018 2159
gfz 193| 0 0 0 -40 -120 -2 -.18 10 10 | 30 91 22 138
| 1 0 1 31 29 9 .05 | 262 403
grg 134| 2 0 6 -19 -50 -18 .59 15 15 | -117 209 51 236
| 1 1 1 17 21 16 .04 | 333 728
igr n/a| 0 0 -3 -3 4 -27 -.03 5 5 | -1083 101 18 94
| 0 0 1 19 10 24 .03 | 873 1573
jpl 119| 0 2 0 -69 102 26 .46 21 19 | 555 -49 19 309
| 1 1 1 18 18 62 .05 | 976 1518
mit 262| 0 -2 0 -23 0 -25 -.31 11 10 | -361 486 20 144
| 0 0 1 30 33 21 .02 | 485 1124
ngs 225| 0 -1 -2 64 36 -7 -.20 10 9 | -632 103 2310 3871
| 0 0 0 22 31 8 .05 | 254 334
sio 251| -2 2 4 -58 34 -38 -.13 22 21 | --- --- --- ---
| 1 0 1 32 37 10 .03 | --- ---
Table 1.1634.b GPS week : 1634 MJD: 55682.000-55688.000
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 | 26 0 20 0 0 0 --- |
2 | 5 5 6 5 5 5 5 |
3 | 4 4 4 4 3 4 3 |
4 | 4 4 6 3 4 4 4 |
5 | 5 5 5 5 4 4 5 |
6 | 4 3 4 4 3 3 4 |
7 | 5 5 6 5 5 4 5 |
8 | 5 5 5 5 6 6 7 |
9 | 4 4 4 4 4 5 4 |
10 | 5 4 4 6 5 5 0 |
11 | 4 4 0 0 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 6 5 5 4 5 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 6 6 6 6 5 5 5 |
16 | 5 5 7 5 4 5 5 |
17 | 4 4 4 4 5 5 5 |
18 | 6 5 6 5 5 5 5 |
19 | 5 4 5 4 4 4 4 |
20 | 5 5 4 4 5 4 4 |
21 | 5 5 5 4 4 4 5 |
22 | 5 5 6 5 4 4 4 |
23 | 5 5 5 5 0 8 5 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 4 4 4 4 4 5 |
28 | 5 4 4 5 5 5 5 |
29 | 5 5 5 5 4 5 5 |
30 | 5 4 4 4 4 4 4 |
31 | 5 5 5 5 5 5 5 |
32 | 4 4 4 4 4 5 6 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1634.0 GPS week: 1634 Day: 0 MJD: 55682.000
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 247| 1 0 0 39 21 28 -.28 8 8 | -346 -276 18 83
| 10 43 |
emr 107| 0 1 0 -26 -75 1 .40 19 19 | -156 -233 12 93
| -10 28 |
esa 143| -1 0 -2 4 11 21 .28 9 9 | -1205 -2894 17 132
| 15 22 |
gfz 193| 0 0 0 -6 -94 -10 -.17 14 13 | 300 -511 24 147
| -6 89 |
grg 134| 2 0 6 -27 -85 -22 .67 18 17 | 225 -796 60 224
| 66 108 |
igr n/a| 0 0 -3 -33 -9 -55 -.01 6 6 | -858 -609 17 103
| 44 -4 |
jpl 119| -1 1 0 -65 81 -35 .55 22 20 | 894 -563 18 315
| 31 33 |
mit 275| 0 -2 0 -22 23 0 -.30 11 10 | 83 -633 19 175
| 13 -14 |
ngs 225| 0 0 -2 28 27 -23 -.10 10 8 | -416 -219 2407 4001
| 63 -22 |
sio 251| -3 4 1 -40 66 -30 -.13 23 22 | --- --- --- ---
| -55 -28 |
Table 2.1634.1 GPS week: 1634 Day: 1 MJD: 55683.000
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 247| 0 0 0 26 42 17 -.29 8 8 | -296 -340 17 75
| 40 -9 |
emr 107| 0 4 3 -13 -33 -4 .39 19 19 | 489 440 15 104
| -51 13 |
esa 143| 0 0 -1 24 57 15 .25 8 8 | 514 -1545 15 117
| 9 19 |
gfz 193| 1 0 -1 -59 -152 15 -.26 10 10 | 9 427 24 138
| -25 47 |
grg 134| 0 0 6 -15 -31 -21 .62 14 13 | 212 -133 49 220
| 15 -15 |
igr n/a| 0 0 -6 -1 -2 -35 -.06 6 5 | -644 51 19 96
| 4 22 |
jpl 119| 0 4 -2 -86 118 -23 .50 21 20 | 1114 41 22 308
| -18 -25 |
mit 275| 1 -3 0 -15 -40 -7 -.34 11 10 | 176 -394 17 138
| 11 -4 |
ngs 225| 0 0 -3 66 55 -2 -.20 10 10 | -328 -327 2213 3557
| 61 -9 |
sio 251| -3 2 2 -37 -14 -39 -.15 21 20 | --- --- --- ---
| -43 -12 |
Table 2.1634.2 GPS week: 1634 Day: 2 MJD: 55684.000
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 247| 1 0 -1 56 20 14 -.30 11 9 | -533 360 22 104
| -19 97 |
emr 107| 0 2 4 6 -60 0 .35 19 19 | 1567 -1838 15 102
| -31 51 |
esa 143| -2 0 -2 56 23 36 .26 8 8 | -2136 -918 14 117
| -9 36 |
gfz 193| 0 0 -1 -78 -77 -7 -.20 11 10 | 264 -80 22 147
| -26 78 |
grg 134| 1 -1 4 -18 -71 -43 .54 17 15 | -83 253 51 194
| 33 51 |
igr n/a| 0 0 -4 15 -3 -23 -.06 6 5 | 177 -1980 18 90
| -5 45 |
jpl 119| 1 2 1 -47 84 -6 .43 21 19 | 1962 -1938 20 325
| 18 39 |
mit 275| 1 -3 1 -70 43 -16 -.32 13 11 | -133 241 20 122
| 22 -18 |
ngs 225| 0 -1 -2 82 -13 -10 -.21 11 9 | -532 339 2502 3674
| -42 53 |
sio 251| 0 3 5 -112 83 -33 -.10 23 21 | --- --- --- ---
| -7 -3 |
Table 2.1634.3 GPS week: 1634 Day: 3 MJD: 55685.000
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 247| 2 0 -1 13 28 7 -.23 10 8 | -654 290 18 83
| 58 12 |
emr 107| -1 6 5 -23 -39 22 .37 19 19 | -948 2381 15 109
| -53 7 |
esa 143| -1 0 0 -1 51 38 .31 10 10 | -2690 3531 12 107
| 18 -7 |
gfz 193| 0 0 -1 -10 -103 -3 -.16 9 8 | -112 437 24 150
| 33 51 |
grg 134| 0 0 8 -41 -34 -1 .57 15 14 | -699 1498 48 228
| 75 -22 |
igr n/a| 0 0 -2 -14 20 -42 .02 5 5 | -2529 2622 17 83
| 15 39 |
jpl 119| 1 2 -2 -97 104 -21 .43 21 19 | -749 2552 19 314
| -2 8 |
mit 275| 0 -2 0 14 -12 -29 -.28 9 8 | -785 992 20 145
| -6 -11 |
ngs 225| 0 -2 -2 67 33 2 -.21 10 8 | -687 275 2614 3846
| 32 59 |
sio 251| -1 1 3 -30 40 -55 -.11 21 21 | --- --- --- ---
| -38 -9 |
Table 2.1634.4 GPS week: 1634 Day: 4 MJD: 55686.000
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 247| 0 1 0 33 26 13 -.28 8 8 | -1086 531 18 82
| -18 27 |
emr 107| 0 1 2 12 -18 -3 .31 18 18 | 173 201 14 99
| -70 2 |
esa 143| -1 0 -4 41 9 -5 .32 8 8 | -1847 1850 20 113
| 2 7 |
gfz 193| 0 -2 0 -65 -153 1 -.12 10 9 | -424 605 21 124
| 12 82 |
grg 134| 1 1 8 -3 -59 4 .56 15 16 | -254 581 54 284
| 24 1 |
igr n/a| 0 0 -2 -15 4 19 -.01 5 4 | -1197 341 20 99
| 10 61 |
jpl 119| 0 2 1 -69 85 66 .42 19 18 | 531 155 19 299
| -8 60 |
mit 275| 0 -2 2 -56 33 -30 -.31 10 9 | -1167 2731 22 131
| 4 -19 |
ngs 225| 1 -2 -2 98 60 0 -.25 11 9 | -1115 550 2121 4071
| 34 36 |
sio 251| -2 2 6 -96 57 -37 -.13 20 19 | --- --- --- ---
| -20 14 |
Table 2.1634.5 GPS week: 1634 Day: 5 MJD: 55687.000
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 247| 1 0 0 4 45 42 -.28 8 7 | -630 -140 18 76
| 50 -15 |
emr 107| -2 1 0 -13 -30 10 .37 17 17 | 491 -1373 16 97
| -48 -12 |
esa 143| 0 0 -3 32 24 -11 .28 9 9 | -1231 731 21 123
| 23 -5 |
gfz 193| -1 0 1 -4 -129 -13 -.22 10 9 | -77 -133 23 128
| 4 33 |
grg 134| 2 1 4 -35 -35 -15 .59 14 13 | 93 -275 54 253
| 61 -16 |
igr n/a| 0 0 -3 2 14 -36 -.02 5 4 | -729 -1200 19 98
| 12 15 |
jpl 119| 2 1 0 -65 113 115 .45 19 17 | 826 -1533 19 294
| 61 0 |
mit 275| 0 -2 1 -17 -36 -64 -.31 11 11 | -200 32 25 163
| -5 9 |
ngs 225| 0 -1 -2 51 80 -9 -.22 10 7 | -648 -160 2346 4287
| 28 -14 |
sio 251| -2 1 3 -58 -4 -48 -.12 22 20 | --- --- --- ---
| -23 7 |
Table 2.1634.6 GPS week: 1634 Day: 6 MJD: 55688.000
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 247| 1 0 1 25 44 -20 -.25 8 7 | -710 265 19 77
| 56 19 |
emr 107| 0 1 1 -18 -12 19 .34 18 18 | -706 921 15 92
| -2 -10 |
esa 143| -1 0 -2 -11 23 15 .30 8 8 | -1094 382 17 118
| 44 -10 |
gfz 193| 0 0 -1 -56 -135 -1 -.16 10 10 | 251 -104 22 133
| 31 70 |
grg 134| 5 0 5 7 -36 -28 .58 15 14 | -314 340 47 251
| 18 -6 |
igr n/a| 0 0 -3 21 7 -18 -.03 5 5 | -1802 1485 19 92
| 36 23 |
jpl 119| 0 3 0 -50 129 93 .49 21 19 | -688 943 20 314
| 30 -149 |
mit 275| 1 -2 1 2 -10 -35 -.32 12 10 | -507 437 20 139
| -13 -6 |
ngs 225| 0 -1 -3 53 13 -12 -.23 12 10 | -699 266 1971 3662
| -33 -17 |
sio 251| -2 2 5 -36 12 -24 -.20 23 23 | --- --- --- ---
| -20 1 |
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 3.1634.0 GPS week: 1634 Day: 0 MJD: 55682.000
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 --- --- --- --- 42 --- 33 --- --- 25 | 38 --- --- --- --- 44 --- 12 --- --- 25
2 | 8 22 11 14 19 6 25 9 11 26 5 | 27 34 27 24 30 29 34 25 26 34 24
3 | 9 16 11 12 16 5 16 10 9 23 4 | 31 41 38 40 43 36 35 36 40 34 36
4 | 7 11 9 13 20 5 12 11 11 13 4 | 23 26 30 30 27 25 26 30 29 39 27
5 | 8 22 9 11 24 5 23 13 13 26 5 | 20 25 21 21 31 20 22 21 24 21 19
6 | 8 15 10 13 16 6 15 11 9 23 4 | 20 29 30 29 33 26 26 23 26 25 24
7E | 7 15 12 16 21 4 16 17 12 15 5 | 27 30 31 29 37 28 29 37 25 36 28
8E | 10 19 10 8 16 7 17 16 10 22 4 | 60 62 61 62 63 58 60 67 60 64 61
9 | 8 20 9 13 15 4 20 10 10 15 4 | 22 33 24 27 27 23 29 23 25 24 22
10 | 9 17 9 12 19 9 14 13 9 20 4 | 49 40 34 37 43 51 37 35 37 34 47
11 | 4 18 9 8 17 6 20 7 6 17 3 | 9 22 12 7 7 9 18 10 10 12 9
12 | 8 23 12 9 21 5 27 14 11 22 5 | 17 32 20 19 26 18 32 24 20 21 17
13 | 8 25 9 33 21 8 24 11 12 23 6 | 22 34 26 30 34 23 32 28 23 22 22
14 | 9 25 9 18 13 7 27 10 10 20 5 | 25 33 35 37 34 34 29 30 36 28 29
15 | 5 23 12 17 17 5 28 10 15 35 5 | 18 28 26 21 30 23 29 19 27 29 19
16 | 7 21 10 14 18 5 26 12 8 19 4 | 22 32 26 24 30 24 34 25 24 21 22
17 | 4 10 8 11 14 6 17 10 9 21 3 | 27 28 29 33 29 28 26 30 28 27 27
18 | 9 24 8 19 17 8 31 13 12 24 5 | 44 48 45 48 45 45 49 47 44 49 43
19 | 8 19 8 12 13 6 19 9 8 30 4 | 26 29 30 30 31 28 31 29 30 30 27
20E | 10 23 8 10 21 8 19 9 10 21 4 | 15 25 23 19 25 20 23 18 23 22 18
21 | 7 23 8 14 18 5 25 11 10 21 4 | 32 35 26 29 26 29 34 31 32 35 28
22 | 7 22 10 12 20 3 32 14 10 20 5 | 58 61 60 61 60 58 61 64 55 57 57
23 | 6 19 10 12 20 8 23 13 9 34 5 | 12 25 13 18 21 14 26 16 12 27 13
24 | 5 13 10 9 16 5 13 9 8 15 3 | 16 23 23 16 18 18 22 17 22 23 17
25 | 8 18 8 11 17 5 23 12 9 14 4 | 15 30 21 17 29 18 40 14 17 18 17
26 | 7 15 10 12 11 5 15 8 14 19 4 | 15 17 22 17 22 16 20 14 22 22 15
27 | 8 22 9 13 15 6 22 8 11 18 4 | 23 29 26 25 25 22 24 22 23 26 22
28 | 9 22 11 14 17 6 23 10 9 15 4 | 17 26 20 21 27 18 27 19 19 18 16
29 | 9 15 7 12 19 5 19 10 11 38 5 | 26 26 26 28 27 25 30 27 25 28 24
30 | 8 16 7 13 13 4 16 10 8 33 4 | 19 29 23 23 28 21 26 20 21 31 20
31E | 9 24 7 13 19 5 26 11 7 16 4 | 34 34 31 32 37 31 33 32 30 29 30
32 | 8 15 7 10 19 6 19 7 9 17 4 | 22 26 28 23 10 25 30 25 27 30 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 9 14 18 6 22 11 10 23 |T 25 32 28 28 30 27 31 27 27 29 25
WRMS | 8 19 9 13 17 6 20 10 8 22 |NE 20 29 23 24 27 22 28 22 23 25 20
MEDI | 8 19 9 12 17 5 20 10 10 21 |MD 22 29 26 27 29 25 29 25 25 28 24
Table 3.1634.1 GPS week: 1634 Day: 1 MJD: 55683.000
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 | 5 --- --- --- --- 105 --- --- --- --- 0 | 27 --- --- --- --- 90 --- --- --- --- 23
2 | 9 24 9 13 15 6 24 9 10 24 4 | 21 33 21 21 29 22 30 21 22 30 19
3 | 7 12 7 8 14 5 11 9 9 23 3 | 33 35 35 29 33 31 33 35 33 34 32
4 | 10 13 6 10 11 5 10 10 11 12 3 | 20 24 18 23 22 18 22 21 17 24 18
5 | 14 26 8 11 13 6 26 9 9 19 5 | 19 34 23 26 26 23 31 23 28 34 22
6 | 5 11 7 9 13 4 9 8 6 20 3 | 16 22 18 14 22 15 19 15 15 17 15
7E | 6 16 9 14 15 5 23 19 12 15 5 | 44 45 44 50 52 41 44 45 41 42 43
8E | 11 19 10 9 18 6 20 16 13 20 5 | 45 46 46 49 47 48 43 51 53 47 45
9 | 8 20 8 10 12 6 20 9 7 12 4 | 22 30 30 26 29 22 31 23 26 26 25
10 | 9 17 6 12 9 6 14 12 11 18 4 | 51 41 39 42 42 52 44 34 40 43 51
11 | 5 15 8 7 19 4 20 6 7 15 3 | 9 19 9 8 8 10 20 10 9 10 9
12 | 10 24 10 8 16 9 30 13 13 20 5 | 18 32 27 20 27 19 31 21 25 22 20
13 | 8 19 8 9 15 5 22 12 12 24 4 | 15 27 15 16 29 14 29 16 19 20 13
14 | 10 21 9 12 9 5 26 12 9 20 4 | 16 29 25 27 25 22 28 24 23 23 20
15 | 7 27 7 14 19 8 27 11 9 35 5 | 18 30 22 17 30 20 31 17 22 31 18
16 | 7 20 8 10 14 6 26 10 11 18 4 | 26 36 33 32 37 29 39 31 28 32 29
17 | 8 12 9 10 9 7 19 10 13 21 4 | 16 22 20 26 15 18 21 19 21 23 16
18 | 14 25 9 12 17 6 27 14 8 22 5 | 31 43 31 36 34 33 39 33 31 40 31
19 | 7 15 6 9 10 5 20 8 11 29 4 | 17 26 23 21 22 20 27 20 19 17 18
20E | 8 15 9 8 17 5 20 13 11 22 4 | 14 25 21 22 30 16 24 19 15 19 17
21 | 6 25 7 10 15 3 25 10 10 22 4 | 21 30 22 24 17 21 27 22 22 27 18
22 | 10 24 11 10 17 5 26 15 10 19 5 | 55 61 55 62 58 58 62 56 55 58 55
23 | 6 18 5 11 13 4 24 11 8 32 4 | 9 23 14 16 19 10 26 14 10 25 9
24 | 6 14 7 8 11 4 13 9 10 13 3 | 14 24 21 18 22 18 22 20 18 21 17
25 | 8 16 8 10 12 6 25 11 9 18 4 | 12 23 22 18 27 13 38 10 14 21 14
26 | 6 15 7 8 9 6 15 9 9 18 3 | 12 18 13 12 16 11 20 11 16 19 10
27 | 7 19 8 9 12 6 19 9 6 15 3 | 18 25 27 20 25 18 23 19 21 22 20
28 | 8 19 7 11 14 7 26 9 11 15 4 | 14 25 17 14 25 13 28 11 17 11 11
29 | 7 14 7 10 14 5 18 11 11 36 4 | 16 20 19 20 15 15 22 18 17 25 15
30 | 5 12 6 9 9 5 16 14 9 29 4 | 15 23 17 14 22 14 24 16 19 29 15
31E | 10 20 8 12 11 6 20 12 11 12 4 | 28 34 35 35 34 29 30 31 35 30 30
32 | 9 16 7 9 13 4 19 7 11 16 4 | 19 28 23 22 12 23 32 21 27 24 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 10 14 6 21 11 10 21 |T 22 30 25 25 27 25 30 23 24 27 22
WRMS | 8 19 8 10 13 5 20 10 10 20 |NE 16 26 21 19 24 17 27 17 20 22 16
MEDI | 8 18 8 10 13 5 20 10 10 20 |MD 18 28 22 22 26 20 29 21 22 25 18
Table 3.1634.2 GPS week: 1634 Day: 2 MJD: 55684.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1M | 32 --- --- --- --- 28 --- 23 27 --- 20 | 46 --- --- --- --- 55 --- 18 6 --- 32
2M | 11 22 9 15 18 6 26 15 10 32 5 | 23 31 22 18 32 24 33 23 24 28 20
3M | 6 11 7 7 12 6 13 15 9 21 3 | 32 36 31 38 33 32 33 34 34 33 32
4M | 12 17 11 11 11 5 17 27 13 34 6 | 34 39 39 35 34 34 36 46 36 54 35
5E | 9 21 9 14 19 5 24 8 11 14 5 | 31 35 33 30 35 27 33 29 23 23 28
6M | 6 12 6 6 9 5 13 8 11 22 3 | 17 25 22 20 24 18 23 18 16 19 18
7E | 26 16 10 13 14 7 17 22 12 21 6 | 72 78 82 84 81 73 79 69 78 86 75
8E | 14 21 9 11 20 4 18 17 10 21 5 | 45 44 46 47 46 43 39 48 48 41 44
9 | 10 20 7 10 11 5 17 9 10 13 4 | 16 29 18 19 20 15 26 16 18 20 16
10 | 10 15 7 14 10 4 14 15 7 24 4 | 51 47 45 56 53 55 45 57 47 43 56
X11M | 6 --- --- --- --- 1055 --- --- --- --- 0 | 21 --- --- --- --- 9999 --- --- --- --- 23
12 | 9 23 12 10 19 4 26 13 12 19 5 | 14 29 19 18 29 14 27 17 16 16 16
13 | 8 20 10 11 18 7 25 12 8 21 4 | 17 30 25 20 34 19 30 22 18 19 20
14 | 11 23 9 12 14 6 26 14 16 20 5 | 24 30 31 30 31 28 28 26 32 21 26
15 | 6 26 7 14 17 6 27 9 11 32 5 | 18 29 21 19 30 17 29 16 18 25 17
16M | 9 21 9 12 48 7 26 18 11 31 7 | 36 44 39 36 64 38 45 40 37 39 37
17M | 9 13 8 12 10 4 14 11 12 23 4 | 18 25 22 26 19 20 22 25 20 25 20
18E | 18 25 7 14 17 7 29 16 9 19 5 | 74 79 81 74 77 73 78 78 76 76 75
19M | 10 15 7 10 15 5 17 7 12 27 4 | 21 27 26 25 25 24 28 24 26 23 23
20E | 9 17 8 9 14 6 18 10 7 9 4 | 16 29 29 22 26 22 26 20 19 23 22
21 | 7 24 7 10 15 4 22 9 10 19 4 | 26 32 23 23 19 24 29 25 28 28 23
22E | 16 21 6 8 20 8 29 18 9 18 5 | 127 128 134 124 125 125 127 129 122 126 126
23 | 6 20 9 8 16 6 24 9 8 33 4 | 15 28 21 17 23 20 27 19 14 24 19
24M | 8 16 5 7 11 5 11 8 11 17 3 | 20 30 24 18 23 21 24 23 27 29 23
25M | 9 15 6 10 13 3 20 9 13 15 4 | 15 24 18 17 30 16 35 11 15 15 16
26 | 8 19 8 6 11 4 13 7 8 21 3 | 15 25 18 12 21 16 18 15 17 32 17
X27 | 8 22 6 11 12 7 --- 8 11 16 4 | 17 29 19 19 22 16 --- 17 19 22 17
28 | 9 19 9 8 16 3 19 8 12 17 4 | 16 29 19 16 26 16 24 15 21 15 15
29M | 13 12 8 12 13 6 21 9 12 36 5 | 25 20 25 26 21 21 24 23 21 32 23
30M | 7 13 8 7 10 5 11 8 6 34 4 | 21 28 24 19 28 22 25 21 22 35 23
31E | 9 22 10 11 13 6 21 12 12 15 4 | 64 61 62 67 66 60 59 60 58 58 60
32 | 10 17 6 9 16 6 20 7 8 12 4 | 20 33 30 25 14 25 34 23 23 27 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 8 11 17 6 21 13 11 23 |T 31 38 34 33 37 32 37 32 31 35 31
WRMS | 9 19 8 10 15 5 19 11 9 21 |NE 17 29 21 19 25 18 26 18 20 22 18
MEDI | 9 19 8 10 14 6 20 10 11 21 |MD 21 30 25 23 29 24 29 23 23 27 23
Table 3.1634.3 GPS week: 1634 Day: 3 MJD: 55685.000
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 | 4 --- --- --- --- 105 --- --- --- --- 0 | 29 --- --- --- --- 111 --- --- --- --- 30
2 | 9 21 7 10 17 5 26 7 7 25 4 | 21 32 21 21 28 21 32 22 20 29 21
3 | 6 12 12 7 12 5 11 8 10 22 3 | 19 31 27 23 30 21 23 22 23 19 22
4 | 8 12 8 8 11 4 12 8 8 14 3 | 25 31 30 24 28 26 29 27 24 36 26
5E | 8 22 12 12 14 4 30 6 14 17 5 | 21 36 27 25 34 22 32 26 23 30 24
6 | 5 12 12 8 9 5 13 7 10 18 3 | 21 31 29 21 31 23 23 23 26 19 23
7 | 16 14 11 11 14 6 18 8 10 22 4 | 58 65 67 69 69 64 65 62 66 63 64
8E | 17 24 10 10 15 5 19 10 9 22 5 | 49 57 56 55 58 56 54 58 57 57 54
9 | 8 21 10 8 8 4 20 9 9 11 4 | 21 35 26 25 28 23 31 24 24 25 23
10E | 23 23 9 12 19 6 16 11 13 20 5 | 53 46 41 46 43 49 46 45 43 37 46
X11 | 4 --- --- --- --- 8 --- --- --- --- 0 | 10 --- --- --- --- 176 --- --- --- --- 10
12 | 12 24 12 7 17 4 28 9 10 19 5 | 20 35 25 24 31 21 33 22 21 23 22
13 | 5 18 12 8 21 6 22 7 8 17 4 | 23 33 29 22 36 22 31 27 24 20 24
14 | 10 22 11 13 12 5 25 9 10 19 4 | 22 31 31 33 30 26 28 28 33 21 26
15 | 6 27 13 14 17 6 28 8 12 30 5 | 21 36 27 24 32 23 36 24 23 29 22
16 | 7 20 9 9 15 5 27 9 10 21 4 | 21 30 25 18 31 22 32 21 25 20 21
17 | 9 13 9 8 11 6 17 13 5 25 4 | 26 31 28 28 28 27 28 30 25 29 26
18E | 8 24 8 12 19 5 26 8 10 17 4 | 44 56 49 48 50 47 54 48 49 53 47
19 | 7 12 12 7 12 6 16 9 9 28 4 | 24 31 32 27 32 28 28 27 31 25 27
20E | 7 17 10 8 14 6 19 10 8 9 3 | 22 30 28 26 29 25 29 28 26 28 25
21 | 7 23 10 9 15 4 23 6 5 20 4 | 25 31 21 26 23 22 30 24 22 27 22
22E | 8 21 9 6 17 4 25 9 12 15 4 | 64 76 66 66 69 68 74 68 69 72 67
23 | 7 19 11 9 17 5 23 8 10 32 4 | 15 27 18 17 22 13 28 18 14 28 15
24 | 9 14 11 6 12 4 12 9 8 14 3 | 17 25 22 20 24 18 22 21 21 24 19
25 | 9 17 9 6 13 3 22 7 8 14 3 | 17 32 24 19 32 20 39 19 21 25 21
26 | 6 14 11 6 12 5 15 8 12 21 4 | 19 23 22 18 23 18 24 16 24 26 18
27 | 9 20 9 8 9 4 19 7 11 13 4 | 19 33 24 23 28 22 22 22 22 25 21
28 | 8 21 12 11 16 4 25 8 7 16 4 | 17 30 19 20 27 16 28 17 19 18 16
29 | 8 12 7 6 14 4 23 8 6 36 4 | 20 24 24 24 24 21 27 23 25 27 21
30 | 7 12 6 7 12 5 13 12 11 29 4 | 25 31 25 24 31 24 30 25 24 34 24
31 | 9 25 9 10 23 6 19 10 12 17 5 | 44 44 42 43 49 40 41 43 42 38 41
X32 | 10 15 12 6 --- 7 18 6 11 16 4 | 23 32 28 25 --- 24 34 24 31 29 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 10 9 15 5 21 9 10 21 |T 26 36 31 29 34 35 34 29 29 31 27
WRMS | 8 19 10 8 14 5 19 8 8 21 |NE 20 31 24 23 28 20 29 22 22 24 20
MEDI | 8 19 10 8 14 5 19 8 10 19 |MD 21 31 27 24 31 23 30 24 24 27 23
Table 3.1634.4 GPS week: 1634 Day: 4 MJD: 55686.000
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 | 5 --- --- --- --- 47 --- --- --- --- 0 | 31 --- --- --- --- 37 --- --- --- --- 32
2 | 10 22 7 18 16 5 24 7 10 27 5 | 19 31 19 20 25 21 30 15 19 29 17
3 | 5 11 5 7 11 3 10 7 10 21 3 | 16 22 21 21 26 18 18 19 21 17 18
4 | 8 13 6 10 13 5 13 7 13 15 3 | 22 26 25 24 29 21 28 23 24 27 24
5E | 7 21 6 9 16 6 20 10 11 14 4 | 18 29 22 24 30 20 27 18 17 26 20
6 | 5 9 6 7 10 3 9 7 10 16 3 | 14 23 23 18 25 18 20 20 18 12 17
7 | 9 17 13 10 20 7 18 10 9 19 4 | 35 39 42 41 46 37 38 33 37 29 36
8E | 18 24 13 12 17 6 20 9 9 21 5 | 36 43 37 42 39 39 42 46 44 38 38
9 | 10 17 7 6 10 3 19 12 10 12 4 | 15 27 18 16 22 17 28 18 19 20 16
10E | 14 20 9 12 17 7 18 15 15 20 5 | 53 41 32 61 61 54 42 69 38 39 52
11 | 5 18 7 9 18 6 19 8 14 19 4 | 10 21 11 12 17 96 17 11 16 17 12
12 | 7 22 8 10 17 4 23 13 9 19 4 | 19 32 25 22 27 21 33 23 23 21 21
13 | 5 19 9 8 23 4 23 8 11 17 4 | 19 30 24 23 34 20 30 24 23 14 21
14 | 6 25 6 9 13 4 26 10 11 16 4 | 19 32 26 25 30 21 30 24 20 22 21
15 | 5 23 10 11 17 4 24 15 10 28 5 | 21 34 27 26 33 23 34 23 23 25 22
16 | 5 20 6 8 14 3 23 6 9 26 4 | 17 31 24 22 32 21 33 20 21 17 20
17 | 10 10 7 11 10 6 14 17 10 29 4 | 21 25 24 24 24 23 24 29 24 34 22
18E | 8 20 6 8 18 3 26 8 11 15 4 | 26 36 30 30 34 31 38 30 34 35 29
19 | 6 12 7 9 14 4 14 10 8 28 4 | 22 24 28 26 26 23 27 22 26 18 22
20E | 8 20 12 13 15 4 20 9 13 12 4 | 30 36 40 33 33 30 36 33 38 34 34
21 | 8 22 9 7 15 3 21 6 9 20 4 | 26 30 25 21 18 24 31 24 26 27 22
22E | 7 19 6 8 14 4 26 10 8 12 4 | 39 45 38 40 42 41 47 40 40 42 39
X23 | 5 --- --- --- --- 30 --- --- --- --- 0 | 13 --- --- --- --- 50 --- --- --- --- 14
24 | 7 14 9 9 11 4 11 6 14 16 3 | 14 19 19 18 16 15 18 18 20 19 15
25 | 9 19 6 8 13 4 23 9 12 14 4 | 15 31 21 21 29 19 40 16 19 23 18
26 | 6 10 7 7 14 5 11 9 11 20 3 | 12 15 19 16 20 17 20 16 21 24 16
27 | 10 16 7 6 12 3 16 11 9 14 3 | 15 25 21 17 24 19 22 17 22 23 17
28 | 8 18 12 10 19 5 21 8 11 16 4 | 14 24 20 18 27 18 28 17 18 19 15
29 | 8 11 8 8 14 5 16 9 8 36 4 | 15 18 19 17 20 18 20 17 21 23 14
30 | 7 12 6 10 8 2 10 8 9 28 3 | 17 26 19 17 24 16 24 20 17 30 18
31 | 8 25 7 13 22 5 20 18 11 11 5 | 39 46 44 42 48 41 45 46 45 43 41
X32 | 10 16 7 13 --- 4 17 6 10 17 4 | 23 32 30 31 --- 25 32 25 29 28 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 10 15 5 19 10 11 20 |T 22 29 25 25 29 27 30 25 25 25 23
WRMS | 8 18 8 9 16 4 18 9 9 19 |NE 17 27 22 20 26 23 28 20 21 21 18
MEDI | 7 18 7 9 14 4 19 9 10 17 |MD 19 30 24 22 27 21 30 22 22 24 21
Table 3.1634.5 GPS week: 1634 Day: 5 MJD: 55687.000
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 | 5 --- --- --- --- 92 --- --- --- --- 0 | 38 --- --- --- --- 48 --- --- --- --- 40
2 | 7 19 8 11 16 5 21 12 12 25 4 | 19 34 26 24 33 24 32 21 21 25 22
3 | 7 10 7 8 9 3 10 9 13 21 3 | 11 19 17 14 17 14 17 15 18 13 13
4 | 8 12 7 9 12 5 11 10 10 13 3 | 14 24 19 17 20 16 20 19 16 22 16
5E | 7 21 7 11 10 4 21 8 11 18 4 | 10 26 16 16 21 12 20 12 14 20 11
6 | 5 9 7 8 9 3 10 10 11 17 3 | 13 20 20 15 20 15 19 17 18 13 15
7 | 7 14 13 10 17 5 13 11 8 17 4 | 26 28 27 28 36 24 26 22 22 27 24
8E | 18 24 15 15 15 8 20 15 9 24 6 | 49 51 49 52 49 46 47 47 54 47 47
9 | 10 19 9 8 11 5 19 16 12 12 4 | 19 30 22 22 27 21 29 20 26 25 21
10E | 13 17 10 11 16 4 14 13 11 28 5 | 56 38 35 70 64 65 36 75 36 35 62
11 | 8 16 11 7 16 5 16 8 9 16 4 | 9 21 13 11 9 78 20 12 15 16 13
12 | 7 23 9 8 17 5 28 9 12 20 4 | 18 33 25 24 32 22 33 24 25 21 23
13 | 5 18 8 19 18 6 22 11 11 19 5 | 14 30 19 27 33 18 29 21 17 13 17
14 | 6 21 6 11 12 4 27 12 8 17 4 | 23 31 27 28 31 24 31 24 24 22 23
15 | 5 20 10 11 16 2 26 9 9 32 5 | 17 27 22 19 29 18 29 19 17 30 18
16 | 6 20 9 8 13 4 24 8 9 26 4 | 14 33 24 17 30 19 31 18 19 16 18
17 | 10 13 10 9 13 5 12 19 12 28 4 | 14 23 23 22 19 19 19 27 17 32 17
18E | 10 21 7 10 9 4 25 11 9 19 4 | 16 29 20 20 21 17 26 20 19 25 17
19 | 6 12 8 5 12 5 18 10 12 27 4 | 20 28 34 24 25 26 28 23 28 32 24
20E | 6 18 10 10 16 6 19 13 8 12 4 | 20 29 30 26 26 23 30 19 24 24 23
21 | 8 21 9 9 15 2 23 8 8 19 4 | 19 28 16 18 17 17 26 20 23 26 17
22E | 8 16 8 7 14 5 24 13 5 13 4 | 18 27 24 20 22 20 29 20 22 22 20
X23 | 6 --- 10 --- --- 7 --- 9 --- 33 7 | 13 --- 10 --- --- 13 --- 12 --- 13 14
24 | 6 12 11 7 11 4 7 9 9 15 3 | 9 18 19 16 14 14 17 17 16 20 13
25 | 8 16 8 5 12 3 20 10 12 20 4 | 9 28 20 12 26 13 34 12 11 20 13
26 | 6 11 9 9 11 2 14 11 8 23 3 | 9 17 17 17 17 13 16 15 16 26 12
X27 | 10 21 6 7 13 4 --- 12 9 17 4 | 16 27 20 19 25 17 --- 16 22 26 17
28 | 7 16 14 11 16 6 20 11 6 17 4 | 13 24 18 17 25 15 25 18 14 18 13
29 | 7 12 7 8 13 4 16 10 15 39 4 | 28 31 33 34 33 30 29 29 34 41 31
30 | 7 13 6 7 7 3 13 9 7 27 3 | 16 25 16 13 19 14 24 13 13 31 15
31 | 9 27 6 8 20 5 22 13 11 14 5 | 34 47 35 35 45 34 37 37 38 33 35
X32 | 16 19 7 12 --- 5 16 8 8 20 5 | 45 52 49 44 --- 45 48 47 44 50 45
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 9 10 14 5 19 11 10 22 |T 20 29 24 24 27 24 27 22 22 25 22
WRMS | 7 17 9 9 13 4 17 11 7 20 |NE 16 27 19 21 26 17 27 18 20 22 17
MEDI | 7 17 8 9 13 5 19 10 9 19 |MD 16 28 22 20 25 19 29 20 19 25 17
Table 3.1634.6 GPS week: 1634 Day: 6 MJD: 55688.000
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
------+--------------------------------------------------------+---------------------------------------------------------
2 | 7 20 6 12 16 4 27 11 8 26 4 | 22 34 25 20 34 23 38 21 24 25 22
3 | 5 12 4 7 11 4 9 9 7 24 3 | 18 24 21 20 27 19 22 20 18 20 19
4 | 9 11 8 10 13 5 14 7 10 12 3 | 24 29 28 30 30 25 34 31 28 35 27
5E | 6 17 8 14 13 5 23 9 14 21 4 | 17 26 19 26 23 18 27 21 22 39 19
6 | 6 10 6 9 10 5 10 16 8 17 3 | 23 27 27 26 31 23 27 26 22 19 23
7 | 6 14 11 10 19 5 17 15 12 16 4 | 38 43 42 45 50 41 43 40 35 38 40
8E | 21 26 12 14 16 5 20 22 15 26 6 | 60 65 67 69 67 67 64 75 74 68 65
9 | 8 18 7 9 11 4 20 16 13 16 4 | 21 29 24 24 28 23 32 23 24 28 22
X10E | 5 --- --- 148 114 35 --- 235 --- --- 0 | 147 --- --- 81 114 159 --- 62 --- --- 147
11 | 6 15 9 9 16 5 18 8 13 16 4 | 13 19 9 10 16 85 22 10 12 13 13
12 | 7 23 7 9 17 4 33 8 14 21 5 | 26 38 29 29 38 26 38 27 27 30 28
13 | 6 19 10 10 19 6 25 9 7 18 4 | 21 35 28 26 40 23 33 24 22 19 24
14 | 7 20 6 12 15 4 24 12 12 18 4 | 26 33 33 34 35 27 31 32 25 25 28
15 | 6 22 8 10 19 5 28 11 9 27 5 | 20 31 27 23 30 21 34 22 20 26 21
16 | 5 21 5 8 13 5 23 9 17 38 5 | 21 30 24 20 32 23 33 21 24 28 21
17 | 10 12 6 9 10 5 15 22 17 33 5 | 26 29 30 32 28 28 29 37 30 37 28
18E | 10 20 9 9 23 3 26 11 12 17 5 | 39 46 44 40 46 41 49 38 41 50 40
19 | 4 12 7 7 12 5 14 9 12 28 3 | 30 32 35 32 34 32 37 31 35 35 32
20E | 7 21 8 8 11 8 22 12 6 13 4 | 27 36 31 32 33 26 33 36 30 35 30
21 | 7 21 8 11 17 3 24 7 12 20 4 | 25 31 24 21 25 23 32 22 20 26 21
22E | 7 15 6 6 16 4 23 13 9 15 4 | 44 51 45 46 46 46 53 44 44 53 45
23 | 6 18 8 11 17 7 24 7 9 32 4 | 10 22 12 12 4 11 22 13 4 14 10
24 | 5 12 7 11 12 4 9 11 13 17 3 | 17 22 18 14 21 17 24 17 22 23 16
25 | 8 18 7 8 15 4 27 11 11 17 4 | 18 36 26 24 32 22 46 19 23 25 23
26 | 7 12 7 7 14 3 11 10 11 25 3 | 17 19 20 17 23 18 23 16 25 27 17
X27 | 9 20 6 7 13 5 --- 14 12 22 4 | 20 27 25 22 26 22 --- 23 22 31 22
28 | 6 18 8 9 18 5 20 18 11 18 4 | 16 26 21 19 28 18 27 24 18 21 17
29 | 6 13 8 12 16 7 20 9 12 37 4 | 22 27 27 31 27 26 26 27 27 35 25
30 | 6 13 5 8 10 3 13 7 12 32 3 | 24 27 23 21 27 23 27 19 22 35 22
31 | 8 24 10 12 20 5 24 7 12 22 5 | 44 44 43 45 53 43 44 46 42 45 43
X32E | 11 18 10 11 --- 11 18 19 10 36 5 | 47 55 53 53 --- 46 53 52 49 47 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 10 15 5 21 12 12 23 |T 29 33 29 30 34 33 34 29 27 31 30
WRMS | 7 18 8 10 14 5 19 10 10 23 |NE 20 29 24 22 27 21 30 22 20 24 21
MEDI | 7 18 7 9 15 5 20 11 12 21 |MD 23 30 27 26 30 23 33 24 24 28 23
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 4.1634 GPS week: 1634 MJD: 55682.0-55688.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3012 |U 9 9 21 |U 8 9 29 |U 14 9 19 |
emr | emr 2903 |U 10 8 25 |U 9 11 31 |U 16 10 19 |
esa | esa 2921 | 7 7 20 |U 7 9 26 | 13 9 19 |
gfz | gfz 2910 |U 7 8 20 |U 8 11 30 |U 14 9 17 |
grg | grg 2860 | 8 9 22 |U 8 9 32 | 15 10 21 |
igr | igr 2931 | 7 8 20 | 7 9 26 | 14 9 18 |
igs | igs 2922 | 7 8 20 | 7 9 25 | 13 9 18 |
jpl | jpl 2861 |U 8 8 26 |U 8 12 31 | 14 10 20 |
mit | mit 2962 |U 8 8 18 |U 8 10 27 |U 15 10 20 |
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 5.1634.0 GPS week: 1634 Day: 0 MJD: 55682.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 9 11 19 | 11 15 45 | 5 4 16 |
emr | emr 2972 | 9 6 21 | 12 13 44 | 8 5 18 |
esa | esa 2976 | 6 8 19 | 11 15 41 | 5 5 15 |
gfz | gfz 2972 | 6 7 16 | 12 16 41 | 5 6 16 |
grg | grg 2976 | 7 8 17 | 12 15 43 | 6 6 21 |
igr | igr 2965 | 7 8 18 | 12 16 44 | 5 5 14 |
igs | igs 2971 | 6 7 18 | 11 15 41 | 6 5 15 |
jpl | jpl 2969 | 7 7 24 | 10 17 43 | 7 6 17 |
mit | mit 3072 | 8 10 18 | 11 15 48 | 6 5 21 |
Table 5.1634.1 GPS week: 1634 Day: 1 MJD: 55683.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 9 6 21 | 9 9 40 | 7 9 21 |
emr | emr 2972 | 10 10 26 | 8 10 39 | 8 6 21 |
esa | esa 2976 | 8 7 20 | 8 9 38 | 7 8 20 |
gfz | gfz 2972 | 7 9 19 | 9 8 41 | 6 9 19 |
grg | grg 2976 | 9 9 22 | 9 11 44 | 9 8 26 |
igr | igr 2958 | 8 9 20 | 9 9 43 | 7 7 17 |
igs | igs 2975 | 8 8 20 | 8 8 36 | 7 7 19 |
jpl | jpl 2969 | 9 9 27 | 9 10 44 | 9 8 17 |
mit | mit 2976 | 7 7 17 | 9 7 38 | 7 7 18 |
Table 5.1634.2 GPS week: 1634 Day: 2 MJD: 55684.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 9 12 33 | 8 8 23 | 6 8 19 |
emr | emr 2876 | 10 9 30 | 7 6 22 | 9 8 19 |
esa | esa 2880 | 7 7 25 | 7 6 20 | 6 8 17 |
gfz | gfz 2876 | 6 7 24 | 7 7 23 | 6 6 14 |
grg | grg 2879 | 7 7 26 | 7 9 25 | 8 8 17 |
igr | igr 2938 | 7 8 25 | 8 8 23 | 6 7 20 |
igs | igs 2865 | 7 8 25 | 8 7 22 | 6 7 16 |
jpl | jpl 2780 | 9 8 31 | 7 9 24 | 7 7 15 |
mit | mit 2976 | 13 10 20 | 9 8 22 | 8 8 17 |
Table 5.1634.3 GPS week: 1634 Day: 3 MJD: 55685.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 7 8 17 | 7 8 21 | 7 11 19 |
emr | emr 2876 | 10 8 25 | 8 7 25 | 10 11 16 |
esa | esa 2880 | 7 8 19 | 6 6 20 | 7 10 19 |
gfz | gfz 2877 | 7 10 20 | 7 5 22 | 7 11 15 |
grg | grg 2783 | 8 12 23 | 7 6 21 | 7 10 18 |
igr | igr 2858 | 7 9 20 | 6 6 18 | 7 12 17 |
igs | igs 2859 | 7 9 19 | 6 5 20 | 8 13 18 |
jpl | jpl 2876 | 8 10 28 | 7 9 27 | 7 11 20 |
mit | mit 2880 | 7 8 18 | 9 7 21 | 12 14 18 |
Table 5.1634.4 GPS week: 1634 Day: 4 MJD: 55686.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 9 7 22 | 8 10 31 | ---- ---- ---- |
emr | emr 2872 | 10 8 25 | 12 20 31 | ---- ---- ---- |
esa | esa 2880 | 7 6 22 | 6 10 21 | 5 6 21 |
gfz | gfz 2872 | 7 7 22 | 10 20 29 | ---- ---- ---- |
grg | grg 2783 | 8 7 23 | 6 10 26 | ---- ---- ---- |
igr | igr 2946 | 7 6 23 | 4 8 19 | ---- ---- ---- |
igs | igs 2874 | 7 6 22 | 7 11 22 | 5 6 21 |
jpl | jpl 2872 | 8 8 28 | 9 20 27 | 6 7 18 |
mit | mit 2880 | 6 8 22 | 7 12 23 | ---- ---- ---- |
Table 5.1634.5 GPS week: 1634 Day: 5 MJD: 55687.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3008 | 8 11 21 | 5 7 21 | 52 19 26 |
emr | emr 2874 | 11 13 25 | 10 14 22 | 52 19 20 |
esa | esa 2976 | 8 9 20 | 5 6 20 | 51 17 24 |
gfz | gfz 2872 | 8 12 22 | 6 7 24 | 51 17 20 |
grg | grg 2784 | 9 12 23 | 7 7 35 | 51 21 23 |
igr | igr 2973 | 8 10 20 | 4 6 15 | 51 17 23 |
igs | igs 2975 | 8 10 20 | 5 6 17 | 51 18 23 |
jpl | jpl 2778 | 9 11 26 | 6 11 28 | 53 21 24 |
mit | mit 2976 | 7 10 18 | 6 8 18 | 52 18 26 |
Table 5.1634.6 GPS week: 1634 Day: 6 MJD: 55688.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2939 | 9 7 17 | 5 8 23 | 7 6 16 |
emr | emr 2880 | 12 7 20 | 8 7 30 | 11 8 19 |
esa | esa 2880 | 9 5 18 | 6 9 22 | 8 8 20 |
gfz | gfz 2933 | 8 6 18 | 9 10 31 | 7 6 17 |
grg | grg 2842 | 8 5 19 | 6 9 26 | 8 7 22 |
igr | igr 2880 | 8 5 17 | 5 8 23 | 7 7 18 |
igs | igs 2939 | 9 6 16 | 5 8 21 | 7 6 18 |
jpl | jpl 2784 | 8 7 20 | 6 8 26 | 10 9 24 |
mit | mit 2976 | 9 6 16 | 6 10 22 | 7 8 20 |
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 6.1634 GPS week: 1634 MJD: 55682.500-55688.500
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 -17 90 -88 -4 | -5 14
| 27 29 84 70 5 | 3
emr uuuuu | 3 46 63 -15 -10 | 44 47
| 12 24 145 54 6 | 6
esa uuuuu | 5 -6 -57 207 -1 | 3 15
| 11 13 36 83 7 | 4
gfz uuuuu | -50 5 86 -31 1 | 4 19
| 17 21 89 44 18 | 4
grg uuuux | 0 -33 142 -113 1 | -3 22
| 41 21 180 99 24 | 3
igr xxxxx | -15 -8 -22 -17 2 | -3 15
| 20 11 67 63 7 | 3
irf xxxxx | 14 8 -5 -36 3 | -4 14
| 15 9 47 44 4 | 3
jpl uuuuu | 19 -8 59 47 1 | 8 19
| 59 25 120 98 7 | 4
mit uuuuu | 23 5 -133 -71 2 | 6 15
| 23 19 65 78 7 | 3
ngs uuuuu | 2 -12 1 -37 -2 | 6 12
| 28 38 103 106 4 | 2
sio uuuuu | 18 38 -44 -174 6 | 24 29
| 21 24 120 104 7 | 3
Table 7.1634.0 GPS week: 1634 Day: 0 MJD: 55682.500
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 10 18 -8 -8 | -3 15
emr uuuuu | -7 30 333 -17 -15 | 52 57
esa uuuuu | -1 5 -75 201 -8 | 8 20
gfz uuuuu | -68 26 25 1 20 | 2 20
grg uuuux | -87 -46 526 -252 29 | -8 22
igr xxxxx | 25 -24 78 76 -3 | -1 18
irf xxxxx | 21 20 -77 -30 -1 | -3 15
jpl uuuuu | -12 -11 272 234 -4 | 12 25
mit uuuuu | 35 7 -258 -33 -4 | 8 18
ngs uuuuu | 43 -43 -104 -57 0 | 6 15
sio uuuuu | 49 75 -221 -260 -7 | 28 33
Table 7.1634.1 GPS week: 1634 Day: 1 MJD: 55683.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 16 -36 68 -224 -9 | -2 14
emr uuuuu | -6 55 116 -93 -19 | 52 56
esa uuuuu | -12 -5 -50 208 -6 | 8 20
gfz uuuuu | -40 29 -57 36 13 | 4 21
grg uuuux | 22 -11 23 -74 28 | -4 22
igr xxxxx | -15 0 -127 -78 2 | -1 18
irf xxxxx | 7 4 -27 -82 -2 | -2 15
jpl uuuuu | 32 22 132 59 0 | 12 25
mit uuuuu | 11 -7 -124 -108 -8 | 10 18
ngs uuuuu | 16 -57 138 -30 4 | 8 15
sio uuuuu | 19 47 -72 -325 -2 | 27 32
Table 7.1634.2 GPS week: 1634 Day: 2 MJD: 55684.500
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 | -59 11 210 -48 -10 | -5 15
emr uuuuu | -13 23 -2 -82 -4 | 46 51
esa uuuuu | 2 1 -8 221 -8 | 4 18
gfz uuuuu | -40 18 81 -15 12 | 2 20
grg uuuux | -13 -41 140 -241 -14 | 0 21
igr xxxxx | -7 -3 30 -95 9 | -4 17
irf xxxxx | 38 -8 22 30 5 | -5 14
jpl uuuuu | -1 -26 0 -69 -8 | 7 19
mit uuuuu | 56 -30 -112 42 -1 | 6 16
ngs uuuuu | -15 34 -49 -105 2 | 6 14
sio uuuuu | 41 -1 17 -35 9 | 22 27
Table 7.1634.3 GPS week: 1634 Day: 3 MJD: 55685.500
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 -44 9 -118 0 | -9 13
emr uuuuu | 7 67 116 0 -12 | 40 42
esa uuuuu | 21 -4 -68 376 -2 | -1 10
gfz uuuuu | -37 -19 82 -29 9 | 0 18
grg uuuux | 36 -61 159 -72 -26 | -2 21
igr xxxxx | -25 -1 -6 -5 10 | -7 12
irf xxxxx | 14 14 7 -48 7 | -8 12
jpl uuuuu | 6 16 30 -42 -3 | 3 13
mit uuuuu | 25 20 -144 -126 5 | 2 10
ngs uuuuu | -45 -18 -7 -61 -4 | 3 8
sio uuuuu | 23 52 -3 -186 12 | 19 22
Table 7.1634.4 GPS week: 1634 Day: 4 MJD: 55686.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -4 21 168 -52 -4 | -8 12
emr uuuuu | 21 73 -48 53 -11 | 38 40
esa uuuuu | 16 1 -92 124 7 | -1 10
gfz uuuuu | -59 -9 227 -46 -1 | 4 18
grg uuuux | 22 -21 101 -107 7 | -3 21
igr xxxxx | -38 -7 -43 -51 -3 | -6 12
irf xxxxx | 23 3 56 3 6 | -6 12
jpl uuuuu | -37 11 101 28 -1 | 5 13
mit uuuuu | 42 -1 -97 8 3 | 3 11
ngs uuuuu | -13 -31 -134 -75 -7 | 3 8
sio uuuuu | 9 23 98 -101 12 | 21 24
Table 7.1634.5 GPS week: 1634 Day: 5 MJD: 55687.500
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 | 17 -36 12 -72 -1 | -7 13
emr uuuuu | 14 62 -110 21 -6 | 38 39
esa uuuuu | 7 -9 -96 136 6 | 0 14
gfz uuuuu | -31 10 107 -94 -20 | 8 21
grg uuuux | 18 -47 40 -65 -28 | 1 24
igr xxxxx | -13 2 -75 -13 5 | -4 14
irf xxxxx | 2 14 31 -95 0 | -3 15
jpl uuuuu | 2 -47 -63 49 13 | 6 16
mit uuuuu | -7 19 -48 -171 3 | 5 15
ngs uuuuu | 16 -14 79 193 -7 | 5 11
sio uuuuu | -5 37 57 -219 7 | 24 29
Table 7.1634.6 GPS week: 1634 Day: 6 MJD: 55688.500
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 | -24 -45 148 -90 5 | -4 13
emr uuuuu | 5 13 33 12 -4 | 40 41
esa uuuuu | 5 -33 -11 185 5 | 4 16
gfz uuuuu | -75 -20 137 -72 -26 | 12 18
grg uuuux | 1 -7 2 21 9 | -2 23
igr xxxxx | -28 -25 -14 48 -9 | 0 16
irf xxxxx | -5 11 -45 -27 5 | 1 15
jpl uuuuu | 144 -19 -62 72 8 | 11 21
mit uuuuu | 1 24 -150 -111 12 | 9 18
ngs uuuuu | 12 44 82 -120 -1 | 7 13
sio uuuuu | -6 31 -181 -89 12 | 28 33
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