[IGSREPORT-19726] Wk 1632 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Fri May 6 08:29:10 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1632 (Apr 17, 2011 - Apr 23, 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:
igs1632[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1632[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1632[0-6].cls IGS GPS clock combination summary report.
igs16327.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16327.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 | COD | MDVJ
0 | EMR | 8 9 27 8 9
0 | ESA | MAL2 UNSA
0 | GFZ | 7 8 9 27 DRAO MDVJ WES2 YELL
0 | GRG | NRC1
0 | JPL | 8 9 15 25 PRDS
0 | MIT | 11 22 11 22 CAS1 HYDE MAW1 CAS1 MAW1
1 | ALL | 1 1
1 | COD | WROC YELL DAV1 NRIL WROC YELL ZIMM
1 | EMR | 8 8 WILL
1 | GFZ | 7 8 9 27 31 FAA1 MDVJ
1 | JPL | 8 9 15 25 27 MDO1 PRDS
1 | MIT | 9 22 9 22 25 CAS1 MAW1 CAS1 MAW1 MDVJ
2 | ALL | 1 1
2 | COD | DAV1
2 | EMR | 8 8
2 | ESA | WHIT UNSA WHIT
2 | GFZ | 7 8 9 27 BAN2 MAW1 MDVJ
2 | JPL | 8 9 25 27 GUAT MAW1 WHIT
2 | MIT | 11 11 MAW1
3 | ALL | 1 1
3 | COD | CAS1
3 | EMR | 8 9 27 8 9 27
3 | ESA | UNSA
3 | GFZ | 7 8 9 27 DAV1 HARB MDVJ
3 | GRG | ALIC AMC2
3 | JPL | 8 9 15 25
3 | MIT | MAW1
4 | COD | WES2
4 | EMR | 8 9 8
4 | ESA | UNSA
4 | GFZ | 7 8 9 10 CAS1 DAV1 MDVJ
4 | GRG | USN3
4 | JPL | 8 15 25 GUAT MDO1
4 | MIT | 27 31 27 CAS1 CAS1 TLSE
5 | EMR | 8 9 27 8 9 27
5 | ESA | UNSA
5 | GFZ | 3 8 9 27 FAA1 MDVJ SFER
5 | GRG | GUAT
5 | JPL | 8 9 15 25 27 MDO1 TIDB
5 | MIT | CAS1 DAV1 CAS1 DAV1 IRKT MAW1
6 | ALL | 1 1
6 | COD | WES2 WILL
6 | EMR | 8 9 8
6 | ESA | UNSA
6 | GFZ | 8 27 MDVJ
6 | GRG | ALIC FAA1
6 | JPL | 8 15 25 MDO1 PRDS
6 | MIT | 9 ALGO AMC2 BRMU BRUS CAS1 CHUR CRO1 DAEJ DAV1 GODE
6 | MIT | HOB2 HOLM HRAO HYDE IENG KOUR MAS1 MATE MAW1 MDVJ
6 | MIT | MIZU NICO NNOR NRC1 ONSA PDEL PERT PIE1 PTBB SYDN
6 | MIT | TIXI TOW2 TSKB TWTF USN3 USNO WROC WSRT YELL DAV1
6 | MIT | IRKT MDVJ
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
6 | MIT | ~00:00 | ~ -0.37 ns
6. 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
----+------------+----------
G29 | 2011_04_21 | 2011033
7. 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 | NGS | 1
8. 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.
9. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | -.6 .1 -.4 -38 -1 -2 .21
EMR | -3.6 .8 3.9 -4 13 -17 .63
ESA | -1.1 -5.2 11.8 -54 29 59 .22
GFZ | -2.8 .1 -.6 -30 32 28 .45
GRG | -.1 2.4 15.1 -23 34 -18 .29
JPL | -2.2 5.6 7.1 6 -31 48 -.82
MIT | 2.4 -4.4 9.6 -12 8 -17 .31
NGS | 2.5 -5.9 7.4 -33 12 15 .48
SIO | .5 .1 -4.4 -6 -73 15 .06
10. 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.
11. 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.
12. 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 1.1632.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1632.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 2.1632.[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 3.1632.[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 5.1632.0-6).
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 1632 summary. (Apr 17, 2011 - Apr 23, 2011)
Table 1.1632.a GPS week: 1632 MJD: 55668.000-55674.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 1 0 1 19 16 3 -.25 8 7 | -398 -249 17 78
| 0 0 1 16 10 22 .02 | 345 478
emr 101| -2 1 0 -21 -1 33 .48 20 20 | 88876 -269 18 107
| 1 1 2 19 32 20 .02 | 236464 1045
esa 138| 0 0 -2 42 -14 9 .29 8 8 | -703 -150 19 117
| 1 0 1 21 15 16 .03 | 1474 1689
gfz 189| -1 0 -3 -13 -55 1 -.15 11 10 | 151 52 22 133
| 1 1 1 31 44 7 .03 | 416 834
grg 131| 2 1 2 -22 -51 -14 .66 16 15 | -26 -81 46 210
| 0 2 1 20 28 16 .06 | 181 479
igr n/a| 0 0 -3 -22 30 -13 -.00 5 5 | 3419 -522 19 105
| 0 0 0 11 28 13 .02 | 754 1106
jpl 127| 1 1 1 -55 70 5 .52 23 22 | 1168 -259 21 326
| 1 1 1 14 18 61 .04 | 855 1056
mit 260| 0 -2 0 -50 4 -31 -.36 12 11 | -162 -7 21 155
| 0 0 2 28 19 33 .02 | 254 517
ngs 211| 0 -1 -1 33 -5 0 -.21 11 9 | 14243 -56651 2149 3842
| 1 0 1 20 26 14 .02 | 38586 148820
sio 249| -2 1 6 -39 131 -4 -.27 21 21 | --- --- --- ---
| 1 0 2 29 26 8 .04 | --- ---
Table 1.1632.b GPS week : 1632 MJD: 55668.000-55674.000
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 | 0 18 18 27 0 0 41 |
2 | 6 5 5 5 5 5 5 |
3 | 4 4 4 4 4 3 4 |
4 | 5 5 4 4 4 4 5 |
5 | 5 5 4 5 5 5 5 |
6 | 4 4 3 4 4 3 4 |
7 | 5 5 4 4 4 4 5 |
8 | 7 5 5 5 5 5 5 |
9 | 6 6 5 5 5 5 5 |
10 | 4 4 3 3 3 3 4 |
11 | 4 5 4 4 4 4 4 |
12 | 5 5 5 5 5 5 6 |
13 | 5 5 5 5 5 5 5 |
14 | 6 6 5 6 5 5 5 |
15 | 6 6 6 6 6 5 6 |
16 | 5 5 5 5 5 5 5 |
17 | 6 4 5 4 4 4 5 |
18 | 5 6 5 5 5 5 5 |
19 | 5 5 5 5 5 5 5 |
20 | 6 5 5 4 5 4 5 |
21 | 4 5 4 4 5 4 5 |
22 | 5 5 5 5 5 5 5 |
23 | 5 4 5 5 4 5 5 |
24 | 5 5 4 5 5 4 5 |
25 | 5 4 5 5 5 5 5 |
26 | 4 4 4 3 3 3 4 |
27 | 5 5 4 5 5 5 5 |
28 | 5 5 5 5 4 5 5 |
29 | 5 5 5 5 0 5 5 |
30 | 4 4 4 4 4 3 4 |
31 | 5 6 5 5 6 5 5 |
32 | 4 4 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1632.0 GPS week: 1632 Day: 0 MJD: 55668.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 0 0 0 38 10 -5 -.22 7 6 | -554 375 17 74
| -1 31 |
emr 101| 0 2 0 -36 42 57 .47 20 20 | -1005 1204 17 102
| -53 -54 |
esa 138| 0 0 -1 67 -38 -12 .31 10 9 | 671 -2379 24 123
| 50 66 |
gfz 189| -1 1 -1 -55 -35 -1 -.12 10 9 | 81 -391 21 134
| -68 37 |
grg 131| 1 0 2 -36 -98 -15 .68 18 17 | -85 0 49 215
| 33 110 |
igr n/a| 0 0 -3 -21 41 -7 .05 6 6 | 3170 1303 18 162
| 17 14 |
jpl 127| 3 0 0 -56 85 -72 .55 23 23 | 576 1373 19 328
| -8 -14 |
mit 272| 0 0 2 -72 7 21 -.34 14 12 | 86 -249 21 165
| 18 -4 |
ngs 211| 0 -1 -2 51 -4 20 -.23 13 10 | 101747 -394145 2097 3632
| -20 75 |
sio 249| 0 1 8 -71 147 -9 -.25 22 21 | --- --- --- ---
| -35 -61 |
Table 2.1632.1 GPS week: 1632 Day: 1 MJD: 55669.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 1 0 0 37 16 -19 -.27 8 7 | -177 -388 17 72
| 28 31 |
emr 101| -2 1 1 -30 -17 -7 .47 20 20 | 454 -1426 24 108
| -52 11 |
esa 138| 1 0 -1 25 -20 25 .24 9 9 | 550 -1019 20 114
| 49 50 |
gfz 189| -2 0 -4 -22 -65 2 -.15 11 10 | 60 215 23 121
| -55 70 |
grg 131| 3 0 2 3 -13 -35 .68 15 14 | 59 255 49 190
| 23 -45 |
igr n/a| 0 0 -3 -38 15 -23 -.02 5 5 | 4851 -1510 21 104
| -19 71 |
jpl 127| 0 0 0 -83 64 81 .52 24 23 | 2233 -1401 21 324
| 113 136 |
mit 272| 1 -1 1 -23 9 -10 -.38 13 11 | 62 -4 24 129
| 12 -3 |
ngs 211| -1 -1 -1 23 -31 6 -.23 13 11 | -54 -569 1992 3792
| -4 47 |
sio 249| -1 1 4 -25 164 -15 -.27 21 22 | --- --- --- ---
| -17 -72 |
Table 2.1632.2 GPS week: 1632 Day: 2 MJD: 55670.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 3 0 1 20 26 9 -.26 8 7 | -121 -444 17 70
| 7 32 |
emr 101| -5 0 2 -33 -32 32 .49 20 20 | -1268 -987 17 118
| -20 -8 |
esa 138| -1 0 -4 9 -15 20 .26 8 8 | -2025 2698 21 127
| 48 64 |
gfz 189| 0 0 -4 31 -19 8 -.18 12 11 | -250 1423 24 133
| -29 25 |
grg 131| 1 0 0 -37 -63 3 .69 15 14 | 205 -505 56 228
| 82 -9 |
igr n/a| -1 0 -3 -28 1 -27 -.01 5 5 | 3076 -1154 20 105
| -8 42 |
jpl 127| -1 3 2 -46 47 -33 .52 22 22 | 460 -919 24 335
| -72 -4 |
mit 272| 0 -2 3 -9 9 -14 -.33 11 10 | 71 -434 18 157
| -4 -5 |
ngs 211| 0 -2 0 6 -12 -19 -.21 11 7 | -196 -380 1740 3904
| -58 5 |
sio 249| -1 1 7 4 128 -6 -.25 20 21 | --- --- --- ---
| -41 -43 |
Table 2.1632.3 GPS week: 1632 Day: 3 MJD: 55671.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 2 0 1 20 24 -5 -.27 7 7 | -582 -560 18 76
| 15 -14 |
emr 101| -3 0 -1 6 -10 44 .44 19 19 | -1136 -898 16 109
| -71 -24 |
esa 138| -2 0 -2 51 -20 -6 .29 8 8 | -2832 -952 20 131
| 1 53 |
gfz 189| 0 2 -1 -50 -64 9 -.10 12 11 | -53 173 20 128
| 15 20 |
grg 131| 2 3 2 -19 -30 -31 .71 14 14 | -275 -469 41 199
| 49 -21 |
igr n/a| 0 0 -3 -18 47 -5 -.00 5 5 | 2789 -1154 19 91
| 0 41 |
jpl 127| 3 1 0 -60 69 92 .45 22 22 | 300 -915 21 345
| 58 46 |
mit 272| 0 -1 1 -44 -15 -28 -.38 10 10 | -306 -376 21 139
| 4 -1 |
ngs 211| 1 -3 -3 39 19 0 -.18 12 10 | -665 -459 2365 4084
| 26 2 |
sio 249| -3 1 5 -41 112 0 -.30 20 20 | --- --- --- ---
| -24 -29 |
Table 2.1632.4 GPS week: 1632 Day: 4 MJD: 55672.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 2 0 2 20 0 25 -.24 7 7 | -251 -484 24 83
| 13 66 |
emr 101| -2 0 4 -3 -33 33 .49 19 19 | 625124 -206 23 98
| -57 -25 |
esa 138| -1 0 -3 53 -5 -2 .29 9 9 | -549 -997 20 108
| -14 25 |
gfz 189| 0 -1 -6 -7 11 -5 -.16 10 10 | 689 -946 26 139
| -49 45 |
grg 131| 1 2 1 -41 -62 -16 .70 15 16 | 176 -458 51 207
| 62 -29 |
igr n/a| 0 0 -3 -4 -9 -6 -.01 5 5 | 3347 -475 22 100
| -28 24 |
jpl 127| 1 1 3 -46 46 10 .52 23 22 | 1264 -212 24 326
| -38 62 |
mit 272| 0 -1 0 -91 7 -56 -.36 12 11 | -208 -89 25 159
| 28 6 |
ngs 211| 0 0 0 65 -40 -6 -.20 10 9 | -292 -484 2533 3763
| -60 57 |
sio 249| -3 2 7 -76 147 6 -.26 20 20 | --- --- --- ---
| -6 -27 |
Table 2.1632.5 GPS week: 1632 Day: 5 MJD: 55673.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 2 1 1 1 26 -21 -.25 7 6 | -71 -734 14 72
| 36 16 |
emr 101| -1 1 1 -11 -1 33 .51 19 19 | -1045 1125 16 101
| -44 11 |
esa 138| 0 0 -1 30 -13 28 .31 7 7 | -1607 1058 15 111
| 31 17 |
gfz 189| -1 0 -4 1 -98 5 -.18 10 11 | 770 -773 24 124
| 10 52 |
grg 131| 3 2 3 -32 -30 -14 .59 17 16 | -64 -194 43 198
| 37 -73 |
igr n/a| 0 0 -2 -30 69 4 -.01 5 5 | 2728 706 17 93
| 8 16 |
jpl 127| 3 2 1 -54 87 -17 .56 21 21 | 922 1011 19 328
| -55 37 |
mit 272| 0 -2 -1 -43 -23 -60 -.35 12 10 | -243 2 19 133
| -4 -8 |
ngs 211| -1 -1 0 33 36 12 -.19 10 7 | -79 -730 2260 3814
| 42 15 |
sio 249| -2 1 5 -13 83 3 -.22 21 22 | --- --- --- ---
| -43 -10 |
Table 2.1632.6 GPS week: 1632 Day: 6 MJD: 55674.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 0 0 2 -4 6 37 -.26 8 8 | -1035 487 17 100
| 16 43 |
emr 101| 0 0 -3 -45 44 42 .48 20 20 | 1013 -701 14 119
| -33 -51 |
esa 138| 0 0 0 62 11 9 .34 9 9 | 870 540 15 106
| 8 39 |
gfz 189| -2 0 -3 7 -114 -11 -.19 10 10 | -238 669 22 153
| -15 68 |
grg 131| 3 4 5 7 -64 9 .57 17 16 | -199 798 38 237
| -25 -25 |
igr n/a| 0 0 -3 -12 49 -31 .00 5 5 | 3976 -1375 17 85
| 0 29 |
jpl 127| 2 1 0 -36 89 -23 .50 23 22 | 2424 -752 20 302
| -28 -10 |
mit 272| 0 -3 -2 -69 36 -71 -.38 13 13 | -602 1100 19 207
| 4 -19 |
ngs 211| 0 -1 0 14 -1 -12 -.22 11 10 | -759 205 2060 3906
| 2 -42 |
sio 249| -3 0 2 -53 137 -11 -.33 22 21 | --- --- --- ---
| -11 -44 |
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 3.1632.0 GPS week: 1632 Day: 0 MJD: 55668.000
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 --- --- --- --- 205 --- --- --- --- 0 | 32 --- --- --- --- 120 --- --- --- --- 30
2 | 8 30 9 10 19 7 32 18 13 16 5 | 16 29 19 16 29 20 33 19 19 19 17
3 | 6 13 5 10 12 7 15 9 9 21 3 | 19 25 27 27 29 23 24 22 23 19 23
4 | 10 23 12 12 16 4 19 15 9 18 5 | 11 23 20 19 18 12 21 16 12 21 13
5 | 5 25 7 10 22 5 27 12 12 15 4 | 19 34 23 16 34 22 36 23 24 27 21
6 | 4 12 7 9 14 6 17 8 10 19 3 | 24 29 33 31 36 28 27 28 28 24 28
7E | 6 13 12 8 21 7 22 18 10 26 4 | 37 36 40 33 42 38 38 31 40 27 35
8E | 15 20 15 9 20 7 24 27 23 16 6 | 26 36 39 33 38 33 37 48 46 35 33
9E | 12 21 9 12 26 5 20 23 16 24 6 | 65 74 68 68 79 66 76 57 67 68 66
10 | 5 16 8 7 14 5 17 10 8 21 3 | 13 15 17 17 16 12 16 16 16 27 15
11 | 5 14 9 8 23 7 19 11 14 17 4 | 17 25 23 20 36 16 26 15 20 17 18
12 | 8 27 5 7 15 4 29 16 16 23 5 | 17 33 24 23 27 20 31 26 20 23 19
13 | 9 22 10 8 22 6 26 16 13 16 5 | 22 28 29 27 33 22 29 28 25 18 22
14 | 9 25 10 14 17 6 27 16 13 24 5 | 25 34 36 40 39 30 29 32 30 31 29
15 | 5 24 10 14 18 4 30 11 10 44 6 | 17 30 29 30 33 22 28 21 20 40 21
16 | 6 24 10 13 15 6 28 9 12 24 5 | 18 31 25 26 27 19 31 19 19 21 20
17 | 8 18 23 11 17 4 19 10 13 26 5 | 20 21 26 28 20 20 26 23 25 26 21
18 | 6 26 8 12 18 6 31 12 11 19 5 | 20 34 27 20 25 21 37 23 22 31 21
19 | 6 21 11 10 14 7 20 14 11 36 5 | 19 27 26 23 27 21 29 15 19 19 18
20 | 7 25 10 8 22 7 25 21 15 20 5 | 20 35 26 24 25 21 33 27 27 24 22
21 | 5 22 6 9 14 5 20 8 11 19 4 | 18 25 19 18 15 19 23 21 25 29 17
22 | 6 21 8 9 20 6 30 12 10 16 4 | 16 28 22 21 27 19 32 21 20 24 18
23 | 6 20 7 10 21 6 27 12 13 18 4 | 21 28 27 28 32 21 30 24 23 17 22
24 | 6 19 12 8 25 5 15 11 13 21 4 | 16 31 23 20 30 19 32 19 20 31 19
X25 | 7 18 9 9 13 7 26 13 9 --- 4 | 21 29 26 22 34 22 43 29 17 --- 22
26 | 3 12 6 9 17 5 18 11 14 15 3 | 48 45 50 49 50 48 45 44 55 41 46
X27E | 10 21 7 9 24 6 --- 15 11 22 5 | 64 72 71 74 76 66 --- 60 67 73 67
28 | 6 21 10 10 17 5 25 11 10 19 4 | 20 31 26 25 32 20 29 23 22 21 21
29 | 7 16 9 10 12 5 20 10 10 31 4 | 9 19 16 12 12 12 20 9 11 17 10
30 | 5 12 7 6 9 5 14 7 13 19 3 | 23 25 25 25 27 21 25 23 20 23 23
31E | 10 17 9 11 17 6 28 15 17 16 5 | 22 26 29 25 34 21 28 24 30 21 24
32 | 4 19 6 8 16 5 17 11 12 14 3 | 12 19 19 17 19 14 23 18 19 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 20 10 10 18 6 23 14 13 22 |T 23 31 29 27 32 27 31 25 26 27 24
WRMS | 6 20 9 9 17 6 23 12 10 21 |NE 19 28 25 24 28 24 29 22 22 24 21
MEDI | 6 21 9 9 17 6 22 12 12 19 |MD 20 29 26 25 30 21 29 23 22 24 21
Table 3.1632.1 GPS week: 1632 Day: 1 MJD: 55669.000
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 | 16 --- --- --- --- 49 --- 30 34 --- 18 | 30 --- --- --- --- 70 --- 21 55 --- 27
2 | 9 25 9 8 16 6 27 17 10 16 5 | 13 27 22 16 27 16 29 21 20 21 17
3 | 5 14 7 10 15 5 11 9 13 19 3 | 12 20 19 18 23 15 23 15 20 13 15
4 | 10 19 11 13 11 7 17 10 11 17 4 | 11 26 20 20 16 11 20 15 15 22 14
5 | 6 19 9 12 17 4 26 12 13 16 4 | 15 27 19 21 33 16 31 20 18 22 17
6 | 4 14 6 12 12 5 13 8 14 15 3 | 16 22 20 23 24 19 26 20 22 17 19
7E | 6 18 11 12 15 5 25 17 10 18 4 | 18 26 16 19 25 15 24 25 17 22 17
8E | 13 18 7 10 14 5 20 19 21 17 5 | 17 27 20 22 26 19 30 28 31 22 19
9E | 13 20 9 10 24 4 23 18 16 21 5 | 41 56 48 43 62 44 60 38 44 47 45
10 | 6 13 6 8 14 4 15 10 10 16 3 | 13 15 14 16 16 9 17 14 13 20 12
11 | 5 15 11 9 23 4 17 14 11 15 4 | 11 27 18 14 36 11 27 13 13 17 14
12 | 7 27 8 8 14 3 29 16 14 21 5 | 14 31 18 16 27 14 32 19 15 18 16
13 | 7 22 9 13 15 5 24 15 9 16 4 | 15 32 20 21 31 15 32 20 16 13 17
14 | 10 23 9 17 13 7 36 14 10 23 5 | 17 29 26 30 29 24 29 26 22 24 22
15 | 7 26 7 12 13 5 30 13 13 41 6 | 13 29 18 21 29 17 29 18 19 38 15
16 | 6 24 8 9 13 6 26 9 14 21 4 | 16 29 21 18 25 17 34 16 19 15 17
17 | 5 15 10 9 11 5 19 10 14 23 4 | 15 17 16 24 13 18 18 21 24 24 16
18 | 6 21 15 12 17 7 33 11 17 20 5 | 18 29 22 16 23 18 34 21 18 28 17
19 | 7 21 10 12 10 7 24 13 12 32 5 | 17 29 22 22 24 18 33 20 19 16 19
20 | 8 21 11 12 17 5 25 16 13 15 5 | 15 30 24 22 27 17 28 23 21 20 19
21 | 7 21 12 9 14 5 24 9 14 18 4 | 17 24 17 17 19 15 25 19 19 28 15
22 | 8 21 12 7 20 6 33 11 12 15 5 | 16 27 21 18 27 18 30 21 19 23 16
23 | 5 18 8 11 10 4 28 11 9 17 4 | 16 27 21 18 26 14 30 20 15 14 17
24 | 6 19 11 9 15 4 14 11 14 25 4 | 14 26 24 17 26 18 30 16 23 30 18
X25 | 6 16 6 9 10 5 22 15 13 --- 4 | 18 26 20 15 32 17 40 24 18 --- 19
26 | 9 19 6 10 10 4 16 11 12 16 4 | 42 45 43 49 41 42 43 48 45 49 45
27E | 10 16 9 10 24 4 21 14 10 21 5 | 48 59 54 51 68 51 48 50 53 55 53
28 | 8 24 6 12 14 5 25 11 13 21 4 | 15 30 17 17 26 14 27 17 19 16 15
29 | 8 16 10 10 12 6 25 10 14 30 4 | 9 16 14 9 12 10 26 12 14 16 10
30 | 5 12 6 4 10 4 12 10 15 16 3 | 21 24 22 19 24 22 29 23 25 22 22
31E | 13 27 7 10 13 4 29 13 19 20 5 | 14 35 23 25 27 21 27 26 26 29 21
32 | 7 20 6 12 11 3 20 10 9 14 4 | 13 29 20 17 19 13 26 15 17 19 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 9 11 15 5 24 13 13 21 |T 18 28 22 21 27 20 30 22 22 24 20
WRMS | 7 20 9 10 14 5 23 11 11 22 |NE 16 26 20 19 25 18 28 19 20 21 18
MEDI | 7 19 9 10 14 5 24 11 13 18 |MD 15 27 20 19 26 17 29 20 19 22 17
Table 3.1632.2 GPS week: 1632 Day: 2 MJD: 55670.000
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 | 22 --- --- --- --- 43 --- 24 32 --- 18 | 26 --- --- --- --- 63 --- 20 45 --- 25
2 | 7 25 8 9 18 4 27 12 7 16 4 | 14 30 16 16 26 16 30 18 19 22 15
3 | 4 15 5 9 14 6 14 7 11 18 3 | 14 23 17 18 25 16 23 18 16 16 16
4 | 8 17 7 11 12 3 14 9 10 17 3 | 12 28 17 19 19 16 26 15 19 20 15
5 | 7 21 8 12 17 5 25 7 6 14 4 | 18 34 22 15 32 19 38 20 19 24 20
6 | 3 12 6 8 11 4 13 7 9 14 3 | 19 22 20 20 23 18 20 21 17 19 18
7E | 5 16 10 9 13 4 23 13 9 15 4 | 11 24 13 16 26 13 21 17 13 16 13
8E | 14 20 9 9 12 5 19 16 19 18 5 | 18 30 23 27 30 23 34 30 33 27 23
9E | 12 20 7 13 18 6 21 16 13 20 5 | 51 63 53 54 67 50 65 46 49 55 52
10 | 7 13 6 8 16 4 14 8 8 13 3 | 14 25 17 19 20 17 27 17 23 23 18
11 | 5 15 8 9 22 5 18 12 5 14 4 | 13 27 17 17 36 13 24 16 18 20 15
12 | 8 22 7 9 14 5 26 13 14 22 4 | 15 30 19 16 26 16 32 22 19 19 16
13 | 8 22 8 10 17 4 26 10 9 15 4 | 19 32 24 22 33 19 29 23 20 16 20
14 | 10 23 7 23 15 5 27 12 10 22 5 | 23 34 33 41 37 29 32 27 31 23 29
15 | 8 22 8 21 13 4 28 10 14 40 6 | 14 29 22 23 30 17 29 18 21 38 16
16 | 6 24 5 12 14 5 26 9 7 19 4 | 14 31 18 19 25 16 31 17 19 15 16
17 | 6 24 7 10 10 5 22 10 16 26 4 | 20 31 21 28 15 23 30 26 31 28 22
18 | 6 23 7 11 15 4 28 11 7 19 4 | 17 32 20 18 23 19 32 22 23 28 18
19 | 6 19 8 9 10 5 21 11 11 32 4 | 29 35 36 29 35 29 33 28 31 25 29
20 | 8 26 12 12 18 4 25 11 13 13 5 | 14 31 23 22 25 19 29 20 25 20 18
21 | 6 24 7 11 17 5 19 7 6 17 4 | 18 29 15 19 18 17 23 18 19 28 15
22 | 7 17 8 12 16 5 26 12 12 16 4 | 17 27 21 19 27 19 28 20 20 23 17
23 | 7 22 10 10 10 3 25 9 9 20 4 | 19 33 29 23 29 20 29 21 21 18 22
24 | 7 18 10 8 12 7 14 10 10 23 4 | 16 33 27 21 28 19 29 20 23 33 21
X25 | 7 15 6 14 12 7 24 12 13 --- 4 | 17 26 18 20 29 15 38 21 17 --- 16
26 | 10 13 6 16 20 4 16 8 9 13 4 | 60 58 62 68 55 60 63 62 65 59 59
27E | 9 13 6 12 18 5 16 12 8 20 4 | 37 48 42 43 55 40 41 35 37 45 40
28 | 8 22 11 13 14 6 28 10 11 19 4 | 20 33 24 23 32 20 30 20 21 17 20
29 | 7 16 9 20 13 6 24 8 12 32 5 | 9 19 14 18 14 11 23 10 11 17 10
30 | 5 11 5 10 10 5 12 13 10 16 3 | 18 21 18 18 20 16 20 20 22 17 16
31E | 10 21 6 7 17 5 27 16 12 16 4 | 18 29 22 19 30 19 21 24 20 19 19
32 | 8 21 8 9 15 4 23 8 10 18 4 | 15 27 25 21 24 19 28 20 25 23 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 8 12 15 5 22 11 11 20 |T 19 31 24 24 29 22 30 22 24 25 21
WRMS | 7 20 8 11 14 5 22 10 7 21 |NE 18 30 22 22 27 21 29 21 23 23 20
MEDI | 7 20 7 10 14 5 23 10 10 18 |MD 17 30 21 20 27 19 29 20 21 22 18
Table 3.1632.3 GPS week: 1632 Day: 3 MJD: 55671.000
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 | 40 --- --- --- --- 57 --- 36 36 --- 27 | 41 --- --- --- --- 47 --- 14 46 --- 24
2 | 9 24 7 11 18 6 23 9 12 15 4 | 14 27 17 16 26 17 25 15 17 17 14
3 | 6 15 6 10 15 4 20 8 9 18 3 | 19 24 24 26 27 19 26 20 20 19 20
4 | 10 18 7 14 11 5 12 9 10 17 4 | 14 24 16 20 19 13 18 15 15 20 13
5 | 5 25 9 13 19 4 22 10 11 13 4 | 20 31 23 20 34 20 32 22 22 26 20
6 | 6 12 7 10 12 4 19 8 9 15 3 | 24 25 29 31 29 22 27 26 23 24 25
7E | 8 13 6 12 11 4 16 10 9 15 3 | 19 24 19 24 25 18 24 20 21 19 19
8E | 12 19 9 13 13 4 17 18 19 14 5 | 22 35 27 24 33 26 35 33 37 30 26
9E | 10 21 7 10 14 4 21 13 8 19 4 | 56 67 58 53 68 57 72 51 56 58 57
10 | 7 12 3 10 15 4 12 7 10 11 3 | 12 17 12 16 15 10 18 12 12 17 10
11 | 8 15 8 8 19 6 20 10 12 18 4 | 14 25 15 15 34 16 26 16 18 25 15
12 | 9 23 6 11 14 5 25 12 11 22 4 | 15 31 22 20 27 19 29 24 21 18 18
13 | 6 19 8 8 18 5 28 10 11 18 4 | 22 33 25 22 31 22 32 24 23 20 21
14 | 9 24 9 26 14 4 30 11 11 22 5 | 21 32 29 40 33 26 28 25 31 21 25
15 | 6 23 10 16 15 5 26 10 10 40 5 | 15 31 25 27 30 19 29 18 22 38 18
16 | 6 21 9 7 13 4 32 11 11 19 4 | 18 30 24 21 26 20 33 19 23 18 19
17 | 8 15 7 9 10 4 17 10 11 22 4 | 18 23 20 18 16 17 20 23 20 27 17
18 | 5 24 8 13 13 3 31 10 12 19 4 | 20 29 19 18 25 20 37 23 25 28 19
19 | 6 18 6 10 12 7 24 11 14 31 4 | 19 27 24 21 24 23 33 20 25 18 20
20 | 7 19 8 11 17 6 22 9 11 12 4 | 20 31 26 25 27 22 31 26 25 29 23
21 | 5 22 8 11 13 3 17 5 14 16 4 | 15 27 19 17 15 16 23 18 24 24 15
22 | 6 20 10 10 17 4 31 11 8 16 4 | 19 27 21 18 27 19 32 22 18 23 17
23 | 4 21 8 10 15 4 27 10 11 23 4 | 22 36 25 23 27 20 30 25 20 24 22
24 | 7 16 11 9 12 4 13 12 16 28 4 | 15 30 22 17 21 18 30 19 20 34 18
X25 | 8 16 7 15 11 5 26 11 13 --- 4 | 18 26 25 22 30 19 37 24 21 --- 20
26 | 6 12 5 8 13 6 10 9 10 12 3 | 24 27 28 27 29 26 30 27 27 25 25
X27E | 9 18 8 12 15 5 --- 12 9 23 4 | 58 64 62 60 68 59 --- 56 56 60 59
28 | 7 21 7 16 15 7 25 10 12 16 4 | 17 28 21 24 30 19 29 20 25 18 18
29 | 6 16 6 12 11 5 21 6 11 32 4 | 10 18 14 10 12 10 23 9 13 16 11
30 | 6 13 5 7 11 4 17 10 13 14 3 | 25 30 28 27 29 24 27 27 26 26 25
31E | 10 26 6 9 13 5 31 17 13 16 5 | 21 33 23 21 24 21 27 23 24 22 20
32 | 6 19 7 12 15 5 18 9 11 15 4 | 13 22 20 17 17 13 23 17 16 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 8 12 14 5 22 10 12 20 |T 21 30 24 23 28 22 29 22 24 25 21
WRMS | 7 19 8 11 14 5 22 10 10 20 |NE 18 27 22 21 25 19 28 20 22 22 18
MEDI | 7 19 7 11 14 4 21 10 11 17 |MD 19 28 23 21 27 19 29 22 22 23 19
Table 3.1632.4 GPS week: 1632 Day: 4 MJD: 55672.000
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 --- --- --- --- 70 --- --- --- --- 0 | 35 --- --- --- --- 70 --- --- --- --- 39
2 | 7 22 9 18 21 4 25 9 11 15 5 | 15 24 17 24 27 16 26 14 18 19 15
3 | 5 14 9 8 12 3 15 8 13 20 3 | 14 23 19 15 24 17 19 18 18 16 17
4 | 7 18 7 11 16 4 11 9 9 18 4 | 16 28 18 15 24 16 21 17 19 21 16
5 | 9 23 7 10 16 5 25 14 8 16 4 | 21 35 24 21 35 23 35 22 20 22 22
6 | 5 12 11 10 10 4 18 12 11 15 3 | 18 25 22 19 26 21 21 25 18 20 21
7E | 6 15 12 9 13 5 19 9 8 15 3 | 19 25 17 20 25 19 20 21 18 20 20
8E | 12 17 11 10 14 5 19 20 15 16 5 | 19 30 24 24 34 24 31 33 32 24 24
9E | 10 17 8 11 21 6 18 12 10 20 4 | 48 55 50 51 59 47 60 43 47 51 48
10 | 7 13 6 8 14 4 15 6 8 11 3 | 13 24 18 16 17 15 22 14 19 16 15
11 | 5 16 8 9 19 5 20 10 10 18 4 | 16 29 19 19 36 17 29 15 14 22 17
12 | 11 21 9 8 14 8 25 12 15 21 5 | 16 29 21 22 27 18 28 21 24 21 18
13 | 6 20 6 9 20 4 27 14 7 20 4 | 20 32 22 25 34 24 31 25 24 22 23
14 | 8 25 12 13 13 6 34 11 12 21 5 | 25 35 35 34 33 29 31 27 32 19 27
15 | 6 22 10 11 15 5 30 12 8 40 5 | 21 32 25 24 33 23 32 23 24 39 22
16 | 6 22 11 11 14 3 25 13 10 20 4 | 19 29 20 20 28 18 31 20 20 17 19
17 | 6 15 10 10 7 7 22 9 9 21 4 | 21 23 21 20 19 21 23 22 21 27 19
18 | 7 25 9 12 15 4 35 11 12 19 5 | 18 33 15 20 27 19 36 22 22 25 19
19 | 5 18 9 10 10 5 21 11 11 32 4 | 18 30 25 22 28 21 30 22 22 16 22
20 | 8 19 10 10 21 5 26 10 10 12 4 | 20 31 28 24 28 24 32 24 26 26 23
21 | 6 19 11 11 19 4 25 6 11 19 4 | 23 30 24 25 17 21 28 21 25 29 22
22 | 6 21 11 7 16 5 31 14 10 15 4 | 20 33 23 23 34 21 37 27 23 25 23
23 | 5 21 5 7 18 5 27 9 8 21 4 | 23 34 28 26 31 25 29 25 26 25 25
24 | 8 18 8 9 11 7 15 15 11 26 4 | 17 33 24 20 24 21 31 23 20 34 21
X25 | 8 17 7 7 17 7 25 8 17 --- 4 | 16 26 20 15 31 16 36 18 18 --- 16
26 | 6 14 6 6 14 7 14 10 8 11 3 | 23 28 24 25 26 23 22 27 20 26 24
27E | 10 15 9 9 19 5 17 12 10 25 4 | 36 44 40 40 46 37 40 39 39 49 38
28 | 6 19 10 10 13 4 29 9 7 17 4 | 19 29 18 16 29 17 28 18 19 16 16
X29 | 4 --- --- --- --- 28 --- --- --- --- 0 | 11 --- --- --- --- 20 --- --- --- --- 13
30 | 6 11 8 9 8 3 15 11 8 16 3 | 21 29 24 23 31 24 30 27 23 23 24
31E | 11 29 9 10 18 5 28 17 13 16 5 | 21 40 29 31 29 24 30 31 27 21 25
32 | 7 21 8 9 15 5 20 7 9 14 4 | 16 25 19 17 22 17 25 18 20 19 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 9 10 15 5 23 11 10 20 |T 20 30 23 23 29 23 29 23 23 24 22
WRMS | 7 19 9 10 16 5 22 11 9 20 |NE 19 29 22 21 27 22 28 21 21 22 20
MEDI | 6 18 9 10 15 5 22 11 10 18 |MD 19 29 22 22 28 21 30 22 21 22 21
Table 3.1632.5 GPS week: 1632 Day: 5 MJD: 55673.000
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 --- --- --- --- 196 --- --- --- --- 0 | 35 --- --- --- --- 116 --- --- --- --- 37
X2 | 7 24 8 --- 17 6 23 8 10 17 4 | 14 30 15 --- 19 19 27 18 18 23 14
3 | 5 14 6 7 15 7 15 9 8 19 3 | 17 23 23 16 21 20 21 18 19 19 17
4 | 8 17 5 11 16 4 13 10 10 16 3 | 15 26 18 19 16 18 23 22 20 21 16
5 | 4 21 6 11 24 6 24 16 9 14 4 | 21 31 24 26 35 24 34 24 23 28 22
6 | 4 11 7 8 12 5 16 10 5 14 3 | 21 24 26 22 26 23 20 24 22 26 21
7E | 7 13 10 7 15 4 19 9 10 19 3 | 26 30 25 26 29 26 29 25 26 28 24
8E | 11 19 8 11 15 5 17 19 17 16 5 | 21 31 27 27 32 26 32 34 31 26 25
9E | 10 19 7 9 18 4 19 11 12 19 4 | 47 59 54 50 64 52 61 47 50 56 51
10 | 6 12 4 9 13 5 12 7 9 13 3 | 11 18 18 19 18 16 22 18 16 19 14
11 | 6 14 5 9 21 5 18 9 8 19 3 | 16 25 22 21 33 17 27 17 20 26 18
12 | 7 26 8 18 13 5 28 15 11 23 5 | 16 34 23 23 26 22 31 25 19 21 19
13 | 8 19 8 8 22 5 24 19 11 21 5 | 17 29 23 20 35 20 32 24 22 18 18
14 | 10 19 10 17 17 6 28 8 9 21 5 | 21 34 31 35 30 29 33 26 29 23 25
15 | 5 22 9 7 20 5 26 10 11 41 5 | 21 35 27 24 33 27 35 26 31 43 23
16 | 6 23 5 11 15 4 28 13 6 23 4 | 17 32 22 22 25 22 33 18 21 19 19
17 | 6 13 6 11 10 5 16 12 12 26 4 | 18 21 17 21 11 20 22 29 26 36 18
18 | 7 24 7 10 19 4 28 11 11 20 4 | 19 32 20 16 24 19 31 21 26 26 18
19 | 6 16 7 10 10 7 21 15 10 32 4 | 15 28 26 20 21 21 29 21 20 16 19
20 | 6 19 5 14 20 4 24 11 10 16 4 | 14 22 17 19 25 15 26 18 16 21 14
21 | 6 20 8 11 15 4 22 8 5 22 4 | 18 27 16 21 13 19 26 23 18 35 16
22 | 6 19 6 11 22 6 27 13 8 14 4 | 25 31 26 31 33 30 33 30 30 30 26
23 | 6 21 7 8 18 4 24 10 11 26 4 | 18 32 26 21 30 21 30 19 22 19 20
24 | 7 18 8 9 15 7 14 15 10 23 4 | 15 31 23 17 19 18 30 23 20 32 19
X25 | 7 17 6 10 13 3 24 10 14 --- 4 | 17 26 20 18 28 19 38 21 19 --- 17
26 | 5 15 6 6 10 3 14 10 6 9 3 | 17 22 18 18 19 19 21 19 21 18 16
27E | 9 17 7 9 21 5 18 10 12 24 4 | 56 63 62 60 69 62 38 59 62 65 60
28 | 7 23 5 9 14 6 24 13 10 21 4 | 19 30 21 20 27 21 29 23 23 21 18
X29 | 5 15 8 --- 15 9 21 8 10 31 4 | 11 17 9 --- 7 17 22 10 10 8 10
30 | 4 12 5 11 11 5 14 9 6 15 3 | 21 25 20 26 24 22 25 19 21 19 20
31E | 10 20 6 13 25 6 26 12 12 16 5 | 23 30 29 28 29 25 31 27 25 25 24
32 | 8 21 4 7 17 6 20 7 9 16 3 | 12 21 20 17 18 14 24 17 19 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 10 17 5 21 12 10 21 |T 20 29 24 24 27 26 29 24 24 26 21
WRMS | 6 19 7 11 16 5 21 10 7 22 |NE 17 27 21 21 23 24 27 21 21 23 18
MEDI | 6 19 7 10 15 5 21 10 10 19 |MD 18 30 23 21 26 21 29 23 21 23 19
Table 3.1632.6 GPS week: 1632 Day: 6 MJD: 55674.000
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 | 29 --- --- --- --- 144 --- 54 142 --- 40 | 38 --- --- --- --- 127 --- 32 90 --- 38
2 | 9 25 8 10 17 6 25 12 12 16 4 | 17 31 23 18 32 22 30 22 24 24 21
3 | 5 13 7 11 15 4 12 15 12 18 4 | 20 27 24 24 31 22 25 25 20 20 22
4 | 9 19 12 13 16 3 13 14 11 18 4 | 22 28 25 27 23 23 25 27 24 29 22
5 | 8 22 6 13 22 4 22 17 11 19 5 | 22 37 27 27 35 25 36 26 27 29 24
6 | 5 12 8 12 13 4 15 14 11 14 3 | 24 26 26 25 32 23 26 28 24 24 24
7E | 8 15 12 12 14 5 19 12 10 20 4 | 18 26 23 26 29 21 27 26 21 26 21
8E | 12 19 9 11 12 4 18 18 14 21 5 | 27 38 30 32 35 30 40 35 30 30 29
9E | 8 23 10 10 15 5 20 13 12 20 4 | 56 69 58 55 67 57 69 49 53 61 57
10 | 8 17 6 10 18 3 15 9 12 18 4 | 16 24 20 23 21 18 22 21 22 20 18
11 | 9 19 9 7 19 5 19 9 8 14 4 | 21 31 28 22 38 23 32 21 20 22 23
12 | 9 27 9 9 18 6 29 12 14 24 5 | 22 34 25 25 33 23 34 27 26 26 23
13 | 6 17 9 10 21 4 28 17 11 21 5 | 22 32 26 29 41 25 34 26 24 18 24
14 | 9 22 9 14 17 4 29 10 9 19 5 | 26 30 30 37 38 30 29 29 30 26 27
15 | 6 23 10 11 19 7 26 10 15 40 5 | 22 35 26 28 32 26 33 25 29 41 23
16 | 9 21 10 11 15 4 27 14 8 26 5 | 21 33 27 25 29 24 36 22 25 25 23
17 | 11 18 9 9 12 5 21 14 14 24 4 | 20 24 20 22 21 19 25 26 24 33 19
18 | 8 28 9 9 18 6 28 15 8 18 5 | 20 41 23 19 29 23 39 23 23 28 22
19 | 5 19 11 10 10 6 20 18 10 33 5 | 20 28 27 22 25 23 32 24 20 17 21
20 | 6 22 8 15 18 5 22 13 11 13 4 | 20 28 24 24 30 22 31 20 21 22 21
21 | 8 26 7 9 20 4 22 9 7 18 4 | 20 35 24 25 25 23 28 24 23 29 21
22 | 9 24 8 7 20 5 30 18 8 12 5 | 20 34 22 21 30 21 37 26 22 25 20
23 | 5 19 9 10 17 4 29 10 8 22 4 | 22 32 29 30 34 25 34 26 24 22 24
24 | 9 16 13 12 14 4 14 14 11 22 4 | 22 33 35 24 27 26 36 26 27 36 27
X25 | 8 16 8 8 17 5 29 8 11 --- 4 | 22 27 23 21 34 21 42 26 18 --- 20
26 | 5 11 6 5 15 7 15 12 10 15 3 | 19 23 22 21 23 23 26 21 19 25 19
X27E | 7 21 9 10 19 5 --- 11 13 23 4 | 52 59 57 53 63 54 --- 48 50 58 54
28 | 9 22 9 9 16 6 26 16 10 23 5 | 24 32 28 28 32 23 30 26 25 25 23
29 | 7 15 9 10 18 4 26 11 10 28 4 | 8 15 11 5 7 10 22 12 11 11 9
30 | 5 14 8 10 15 3 12 13 9 16 3 | 21 30 23 25 28 21 26 23 18 21 21
31E | 8 20 10 9 20 4 28 12 8 28 5 | 24 27 26 28 31 24 29 28 27 37 25
32 | 6 17 10 9 17 6 19 9 10 24 4 | 17 24 25 21 22 20 27 20 22 25 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 9 10 17 5 23 13 11 22 |T 23 32 27 26 31 28 32 26 26 27 24
WRMS | 8 20 9 10 16 5 22 13 10 21 |NE 21 29 24 23 28 26 30 24 25 24 22
MEDI | 8 19 9 10 17 5 22 13 11 20 |MD 21 31 25 25 31 23 30 26 24 25 22
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 4.1632 GPS week: 1632 MJD: 55668.0-55674.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 |U 9 11 26 |U 7 9 24 |U 0 0 0 |
emr | emr 2950 |U 10 8 25 |U 8 9 26 |U 0 0 0 |
esa | esa 2962 | 9 8 22 |U 6 9 22 | 0 0 0 |
gfz | gfz 2921 |U 14 16 31 |U 6 9 26 |U 0 0 0 |
grg | grg 2961 | 9 8 23 |U 7 8 27 | 0 0 0 |
igr | igr 2917 | 9 8 22 | 6 8 23 | 0 0 0 |
igs | igs 2940 | 9 8 21 | 6 8 22 | 0 0 0 |
jpl | jpl 2907 |U 10 9 25 |U 7 10 27 | 0 0 0 |
mit | mit 3017 |U 14 12 31 |U 8 10 33 |U 0 0 0 |
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 5.1632.0 GPS week: 1632 Day: 0 MJD: 55668.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 9 10 29 | 7 9 27 | ---- ---- ---- |
emr | emr 2964 | 10 10 32 | 7 10 33 | ---- ---- ---- |
esa | esa 2976 | 8 9 26 | 7 7 29 | ---- ---- ---- |
gfz | gfz 2964 | 17 28 51 | 7 9 34 | ---- ---- ---- |
grg | grg 2976 | 10 9 27 | 7 8 43 | ---- ---- ---- |
igr | igr 2936 | 9 8 27 | 7 7 33 | ---- ---- ---- |
igs | igs 2966 | 9 9 27 | 7 7 29 | ---- ---- ---- |
jpl | jpl 2870 | 10 10 32 | 8 10 39 | ---- ---- ---- |
mit | mit 2976 | 41 30 93 | 9 8 27 | ---- ---- ---- |
Table 5.1632.1 GPS week: 1632 Day: 1 MJD: 55669.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3006 | 8 6 15 | 6 9 23 | ---- ---- ---- |
emr | emr 2964 | 7 7 17 | 7 12 21 | ---- ---- ---- |
esa | esa 2976 | 6 7 17 | 6 10 19 | ---- ---- ---- |
gfz | gfz 2964 | 15 25 38 | 6 9 26 | ---- ---- ---- |
grg | grg 2975 | 6 6 15 | 6 8 22 | ---- ---- ---- |
igr | igr 2932 | 6 6 16 | 6 9 19 | ---- ---- ---- |
igs | igs 2937 | 6 6 14 | 6 10 19 | ---- ---- ---- |
jpl | jpl 2961 | 7 6 16 | 7 11 23 | ---- ---- ---- |
mit | mit 3072 | 5 6 13 | 11 21 86 | ---- ---- ---- |
Table 5.1632.2 GPS week: 1632 Day: 2 MJD: 55670.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 8 7 18 | 6 8 21 | ---- ---- ---- |
emr | emr 2964 | 10 5 26 | 6 11 22 | ---- ---- ---- |
esa | esa 2976 | 7 6 21 | 6 8 20 | ---- ---- ---- |
gfz | gfz 2964 | 9 11 26 | 6 9 21 | ---- ---- ---- |
grg | grg 2976 | 8 7 22 | 6 7 23 | ---- ---- ---- |
igr | igr 2939 | 7 6 21 | 7 7 22 | ---- ---- ---- |
igs | igs 2975 | 7 6 22 | 6 9 19 | ---- ---- ---- |
jpl | jpl 2959 | 8 6 26 | 7 10 23 | ---- ---- ---- |
mit | mit 3072 | 8 7 17 | 7 9 21 | ---- ---- ---- |
Table 5.1632.3 GPS week: 1632 Day: 3 MJD: 55671.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3015 | 11 8 30 | 6 6 18 | ---- ---- ---- |
emr | emr 2964 | 12 7 30 | 8 8 23 | ---- ---- ---- |
esa | esa 2976 | 8 6 21 | 5 5 17 | ---- ---- ---- |
gfz | gfz 2964 | 8 6 24 | 6 6 17 | ---- ---- ---- |
grg | grg 2976 | 8 6 21 | 5 5 23 | ---- ---- ---- |
igr | igr 2941 | 8 6 22 | 5 5 18 | ---- ---- ---- |
igs | igs 2973 | 9 6 23 | 6 5 16 | ---- ---- ---- |
jpl | jpl 2872 | 9 7 29 | 5 7 20 | ---- ---- ---- |
mit | mit 3072 | 9 6 25 | 7 5 20 | ---- ---- ---- |
Table 5.1632.4 GPS week: 1632 Day: 4 MJD: 55672.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3011 | 10 27 40 | 6 7 23 | ---- ---- ---- |
emr | emr 2867 | 10 9 21 | 8 6 33 | ---- ---- ---- |
esa | esa 2880 | 12 14 27 | 5 8 21 | ---- ---- ---- |
gfz | gfz 2867 | 13 15 26 | 6 9 31 | ---- ---- ---- |
grg | grg 2879 | 13 15 25 | 7 7 21 | ---- ---- ---- |
igr | igr 2866 | 12 16 27 | 5 6 21 | ---- ---- ---- |
igs | igs 2879 | 11 12 23 | 5 6 20 | ---- ---- ---- |
jpl | jpl 2860 | 13 16 33 | 6 8 26 | ---- ---- ---- |
mit | mit 2880 | 13 16 27 | 6 7 21 | ---- ---- ---- |
Table 5.1632.5 GPS week: 1632 Day: 5 MJD: 55673.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 11 8 25 | 9 12 27 | ---- ---- ---- |
emr | emr 2964 | 12 9 25 | 11 8 26 | ---- ---- ---- |
esa | esa 2976 | 11 7 22 | 8 12 27 | ---- ---- ---- |
gfz | gfz 2760 | 29 20 27 | 9 14 32 | ---- ---- ---- |
grg | grg 2976 | 11 8 26 | 8 9 30 | ---- ---- ---- |
igr | igr 2849 | 12 10 26 | 8 13 26 | ---- ---- ---- |
igs | igs 2970 | 11 8 22 | 9 11 27 | ---- ---- ---- |
jpl | jpl 2958 | 12 8 21 | 8 12 26 | ---- ---- ---- |
mit | mit 2976 | 11 9 19 | 9 11 31 | ---- ---- ---- |
Table 5.1632.6 GPS week: 1632 Day: 6 MJD: 55674.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 9 8 26 | 6 12 27 | ---- ---- ---- |
emr | emr 2963 | 10 7 24 | 8 7 27 | ---- ---- ---- |
esa | esa 2976 | 9 7 20 | 6 9 21 | ---- ---- ---- |
gfz | gfz 2964 | 8 7 24 | 6 10 22 | ---- ---- ---- |
grg | grg 2975 | 9 7 22 | 6 9 24 | ---- ---- ---- |
igr | igr 2956 | 8 6 18 | 6 10 21 | ---- ---- ---- |
igs | igs 2880 | 8 7 19 | 6 11 21 | ---- ---- ---- |
jpl | jpl 2871 | 9 9 20 | 7 11 28 | ---- ---- ---- |
mit | mit 3072 | 9 8 21 | 6 9 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 6.1632 GPS week: 1632 MJD: 55668.500-55674.500
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 -18 61 -18 -11 | 3 11
| 25 10 92 117 4 | 3
emr uuuuu | 36 45 7 162 -7 | 62 64
| 28 21 39 75 10 | 7
esa uuuuu | -28 -27 -69 107 -3 | 11 14
| 18 25 99 138 8 | 3
gfz uuuux | -29 25 98 31 14 | 7 26
| 23 28 54 61 28 | 9
grg uuuux | 30 -39 105 -52 -8 | 6 15
| 53 36 123 123 31 | 3
igr xxxxx | -17 2 26 -16 10 | -7 13
| 21 16 43 53 6 | 3
irf xxxxx | 16 -2 28 -28 7 | -8 15
| 11 10 23 44 8 | 4
jpl uuuuu | -20 2 8 56 6 | 9 26
| 50 62 79 98 12 | 5
mit uuuuu | 21 -10 24 -161 1 | 6 12
| 8 20 32 91 2 | 2
ngs uuuuu | -6 8 -58 -41 0 | -1 6
| 30 31 148 146 2 | 1
sio uuuuu | 57 23 -96 -135 -3 | 48 49
| 29 21 57 60 13 | 2
Table 7.1632.0 GPS week: 1632 Day: 0 MJD: 55668.500
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 | 0 -6 49 37 -4 | 8 13
emr uuuuu | 85 46 -36 258 -24 | 73 76
esa uuuuu | -35 -57 -136 -37 8 | 16 20
gfz uuuux | -6 61 62 41 42 | -2 22
grg uuuux | -79 -40 346 -261 34 | 2 9
igr xxxxx | 17 -24 70 5 19 | -10 14
irf xxxxx | 31 -7 37 -2 13 | -10 17
jpl uuuuu | 45 1 21 133 -9 | 19 38
mit uuuuu | 35 -25 25 -83 3 | 9 18
ngs uuuuu | -44 13 -52 99 -1 | 1 8
sio uuuuu | 92 28 -86 -160 -3 | 49 51
Table 7.1632.1 GPS week: 1632 Day: 1 MJD: 55669.500
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 | -3 -21 -8 52 -13 | 6 12
emr uuuuu | 17 59 58 213 -9 | 68 70
esa uuuuu | -22 -42 -25 -11 -9 | 14 18
gfz uuuux | -42 62 61 59 47 | -1 23
grg uuuux | 73 -16 41 -2 1 | 4 14
igr xxxxx | -43 26 -12 16 17 | -9 14
irf xxxxx | 28 7 43 29 15 | -11 16
jpl uuuuu | -108 -106 120 -52 11 | 13 32
mit uuuuu | 31 -5 29 -37 2 | 7 14
ngs uuuuu | -19 11 -150 -113 0 | -1 6
sio uuuuu | 100 24 -87 -26 6 | 46 48
Table 7.1632.2 GPS week: 1632 Day: 2 MJD: 55670.500
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 -11 30 -33 -15 | 3 11
emr uuuuu | 21 16 33 16 -14 | 63 65
esa uuuuu | -51 -52 27 188 -16 | 10 13
gfz uuuux | -12 25 45 80 30 | 1 25
grg uuuux | 22 -86 10 -82 13 | 4 14
igr xxxxx | -29 4 72 -54 7 | -10 14
irf xxxxx | 13 -4 -16 15 13 | -12 16
jpl uuuuu | 17 68 -66 -113 2 | 9 26
mit uuuuu | 18 0 -14 -125 1 | 3 9
ngs uuuuu | 8 54 12 -72 2 | -2 5
sio uuuuu | 56 37 -167 -98 11 | 45 46
Table 7.1632.3 GPS week: 1632 Day: 3 MJD: 55671.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 26 -7 19 -243 -16 | 3 10
emr uuuuu | 36 79 35 165 -10 | 61 63
esa uuuuu | -41 7 88 13 -6 | 9 12
gfz uuuux | -8 -7 79 32 21 | 6 28
grg uuuux | 33 -41 89 -97 7 | 6 16
igr xxxxx | -29 8 34 -5 8 | -9 13
irf xxxxx | 12 8 31 -47 11 | -10 15
jpl uuuuu | -34 -50 -29 107 1 | 6 22
mit uuuuu | 13 4 43 -187 0 | 4 10
ngs uuuuu | 10 -18 -277 155 1 | -2 5
sio uuuuu | 41 32 -110 -119 6 | 47 48
Table 7.1632.4 GPS week: 1632 Day: 4 MJD: 55672.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -46 -31 22 94 -14 | 2 10
emr uuuuu | 45 39 -29 165 -4 | 58 60
esa uuuuu | -5 -4 -144 165 2 | 9 12
gfz uuuux | -25 31 161 -38 0 | 12 29
grg uuuux | 49 -80 141 -31 -21 | 10 16
igr xxxxx | -4 10 24 -110 7 | -7 13
irf xxxxx | 20 -18 55 -53 4 | -7 14
jpl uuuuu | -42 20 14 101 13 | 4 20
mit uuuuu | 14 -46 80 -172 -2 | 5 11
ngs uuuuu | -37 42 -140 -25 -1 | -2 6
sio uuuuu | 47 -12 3 -152 -3 | 49 50
Table 7.1632.5 GPS week: 1632 Day: 5 MJD: 55673.500
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 -27 48 -89 -8 | -1 11
emr uuuuu | 0 53 -33 140 2 | 55 56
esa uuuuu | -6 -22 -154 76 2 | 8 11
gfz uuuux | -41 -1 185 107 -16 | 15 28
grg uuuux | 84 -28 136 -39 -58 | 7 17
igr xxxxx | -5 1 42 -19 6 | -6 13
irf xxxxx | 11 9 15 -46 2 | -6 14
jpl uuuuu | -26 64 93 76 26 | 4 20
mit uuuuu | 19 13 -9 -204 4 | 4 11
ngs uuuuu | -4 -33 19 -35 -5 | -2 7
sio uuuuu | 21 52 -69 -194 -10 | 48 49
Table 7.1632.6 GPS week: 1632 Day: 6 MJD: 55674.500
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 | -42 -23 265 56 -8 | 1 12
emr uuuuu | 52 26 21 181 7 | 56 58
esa uuuuu | -38 -15 -140 353 0 | 11 15
gfz uuuux | -67 8 96 -61 -25 | 21 26
grg uuuux | 26 18 -28 151 -29 | 4 19
igr xxxxx | -28 -7 -47 54 3 | -1 13
irf xxxxx | 1 -7 31 -94 -8 | -2 12
jpl uuuuu | 11 21 -97 139 -4 | 9 26
mit uuuuu | 20 -11 13 -318 -3 | 7 14
ngs uuuuu | 43 -9 181 -294 2 | 0 8
sio uuuuu | 45 4 -156 -197 -28 | 50 51
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