[IGSREPORT-20397] Wk 1664 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Dec 15 06:18:31 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1664 (Nov 27, 2011 - Dec 03, 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:
igs1664[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1664[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1664[0-6].cls IGS GPS clock combination summary report.
igs16647.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16647.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 | 30 27 30
0 | ESA | NICO KOUR NKLG UNSA
0 | GFZ | 27 30 DAV1 GUAT INVK MDVJ NTUS NYAL WILL
0 | GRG | KOUR USN3
0 | JPL | AREQ
0 | MIT | 10 16 23 27 29 30 10 16 23 27 29 30 NICO
1 | COD | WTZR
1 | EMR | 30 32 30 32
1 | ESA | DAV1 KOUR
1 | GFZ | 10 30 CHUR
1 | GRG | AMC2 KOUR LHAZ LPGS
1 | JPL | 30 AREQ REUN
1 | MIT | 1 10 29 30 32 1 10 29 30 32 CAS1 BAKO CAS1
2 | COD | HNPT YELL
2 | EMR | 30 32 30 32 YELL IRKT
2 | ESA | NTUS FLIN NTUS
2 | GFZ | 2 25 28 30 ABMF MDVJ
2 | GRG | AMC2
2 | JPL | BRMU
2 | MIT | 27 30 32 8 27 30 32 CAS1 MAW1 CAS1 MAW1
3 | COD | 32 PDEL PDEL YELL
3 | EMR | 30 32 30
3 | ESA | 32 TIXI UNSA WUHN YELL
3 | GFZ | 12 28 30 CAS1 MDVJ YELL
3 | GRG | USN3
3 | JPL | 30 AREQ
3 | MIT | 8 10 16 25 27 29 30 32 25 CAS1 YELL
4 | EMR | 30 30
4 | GFZ | 25 28 30 ALRT GRAS NURK POTS
4 | GRG | AMC2
4 | JPL | 27 30 AREQ
4 | MIT | 12 20 27 29 30 31 12 20 27 29 30 31 DAV1 DAV1 GRAZ
5 | COD | MOBS KARR MOBS
5 | EMR | 30 30
5 | GFZ | 11 25 30 32 DAV1 IRKJ MDVJ
5 | JPL | 30
5 | MIT | 1 6 8 10 19 27 29 30 31 1 6 8 10 19 27 29 30 31 SCOR
6 | COD | WROC WROC
6 | EMR | 30 30 YELL YELL
6 | ESA | KOUR POTS UNSA
6 | GFZ | 25 28 30 ALRT
6 | GRG | KOUR USN3
6 | JPL | AREQ YELL
6 | MIT | 10 27 30 10 27 30 DAV1
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
----+--------+--------+-------------
3 | MIT | ~05:59 | ~ -0.41 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
----+------------+----------
G05 | 2011_12_02 | 2011099
G20 | 2011_11_30 | 2011097
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 current IGS reference frame. These rotations were
estimated in the IGS SINEX combination process, performed by the IGS Reference
Frame Coordinator at the Institut Geographique National (IGN). 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 | .3 -.2 -.2 -49 -15 33 .12
EMR | 5.0 8.7 8.9 23 -63 -104 .28
ESA | 7.1 2.3 -8.8 103 -191 120 .25
GFZ | -.6 1.0 -.4 -32 -21 -6 .05
GRG | 3.7 4.2 1.4 -23 6 -4 -.01
JPL | 2.2 5.8 6.7 -20 56 52 .27
MIT | 6.7 2.9 -4.4 -16 9 -37 .25
NGS | 8.6 2.7 -5.8 47 -63 51 .38
SIO | 2.3 1.1 21.2 -41 33 1 .18
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting 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 did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 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 1.1664.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1664.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 2.1664.[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 3.1664.[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 5.1664.0-6).
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 1664 summary. (Nov 27, 2011 - Dec 03, 2011)
Table 1.1664.a GPS week: 1664 MJD: 55892.000-55898.000
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 251| 0 0 4 99 -45 -12 -.23 9 8 | -212 -429 18 97
| 0 0 1 11 23 10 .02 | 309 396
emr 94| 0 2 6 -54 67 -43 .39 19 19 | 1890 -386 16 101
| 1 1 1 32 41 20 .02 | 944 983
esa 126| 1 0 1 -111 188 33 .21 7 7 | -517 941 14 175
| 0 0 1 17 23 8 .02 | 1372 842
gfz 198| -1 0 -6 62 -17 -8 -.28 11 11 | -24 661 23 108
| 0 1 1 62 108 10 .05 | 637 1256
grg 127| 0 0 -3 35 -79 -15 .66 16 15 | 375 -329 46 225
| 1 1 2 12 22 14 .06 | 553 542
igr n/a| 0 0 0 0 -57 -41 -.07 5 5 | 161 -432 18 76
| 0 0 1 14 23 9 .02 | 1159 995
jpl 148| -1 0 1 38 -209 62 .52 15 14 | 1793 -358 18 90
| 1 1 1 9 26 46 .04 | 1088 985
mit 260| 0 0 -5 32 -99 -19 -.38 11 10 | -93 -262 25 187
| 0 0 1 20 15 14 .04 | 237 564
ngs 220| 0 0 -3 -87 55 -22 -.25 11 9 | 20411 -30522 1811 3625
| 1 0 2 36 52 15 .03 | 54564 79565
sio 250| -1 0 9 74 -147 -27 -.15 17 15 | --- --- --- ---
| 0 1 1 22 16 21 .04 | --- ---
Table 1.1664.b GPS week : 1664 MJD: 55892.000-55898.000
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 | 4 4 4 4 4 4 4 |
2 | 4 4 5 4 4 4 4 |
3 | 4 4 3 4 4 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 5 5 5 4 5 0 5 |
6 | 4 4 3 4 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 4 4 4 4 4 |
9 | 4 4 4 3 4 3 3 |
10 | 7 9 6 5 4 4 4 |
11 | 4 4 4 4 4 5 4 |
12 | 5 5 5 4 4 5 4 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 4 4 5 4 |
16 | 4 4 4 5 5 5 5 |
17 | 5 4 5 4 4 4 4 |
18 | 4 5 4 4 4 4 4 |
19 | 5 4 4 4 4 4 4 |
20 | 4 4 4 0 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 3 3 4 4 4 4 4 |
23 | 4 5 5 5 4 5 5 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 3 3 4 4 |
27 | 12 6 7 7 8 9 10 |
28 | 3 4 4 4 4 4 4 |
29 | 4 4 4 5 5 5 5 |
30 | 5 5 5 5 5 5 6 |
31 | 4 4 4 4 4 4 4 |
32 | 6 6 6 6 6 5 5 |
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 2.1664.0 GPS week: 1664 Day: 0 MJD: 55892.000
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 251| 0 0 5 97 -20 3 -.23 8 8 | -326 -784 22 104
| 6 -14 |
emr 94| 0 0 6 -87 89 -1 .39 18 18 | 2230 -656 22 92
| 2 -14 |
esa 126| 0 0 0 -102 215 31 .23 7 7 | 229 -160 16 174
| 4 29 |
gfz 198| -1 0 -5 148 -141 11 -.27 12 12 | -540 2166 27 122
| -34 -15 |
grg 127| 2 1 0 40 -72 -6 .62 15 14 | 250 -453 41 222
| 3 -31 |
igr n/a| 0 -1 -1 -7 -32 -34 -.04 6 6 | 718 -789 20 71
| -32 50 |
jpl 148| 0 -1 2 48 -193 16 .53 15 14 | 2326 -823 19 84
| -14 93 |
mit 260| 0 0 -4 12 -106 -15 -.32 10 9 | 167 -682 20 142
| 4 25 |
ngs 220| 2 1 -7 -122 105 -46 -.21 10 8 | -301 -824 1754 3329
| 65 -74 |
sio 250| -1 -3 9 55 -143 0 -.21 18 16 | --- --- --- ---
| -19 63 |
Table 2.1664.1 GPS week: 1664 Day: 1 MJD: 55893.000
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 251| 0 0 3 110 -12 -26 -.24 10 8 | -41 -177 17 94
| 23 -24 |
emr 94| 0 2 7 -30 125 -38 .36 19 19 | 2952 -1218 18 94
| -25 -56 |
esa 126| 0 0 3 -83 171 32 .22 7 6 | 1358 378 16 185
| 43 15 |
gfz 198| -1 0 -6 -27 -147 -1 -.33 13 13 | 117 292 24 111
| -22 -3 |
grg 127| 0 1 0 29 -69 -40 .56 16 14 | 407 114 49 243
| 10 -49 |
igr n/a| 0 0 0 19 -47 -47 -.07 6 5 | 1550 -1170 18 83
| -25 71 |
jpl 148| -1 0 2 47 -206 87 .47 14 14 | 2945 -1080 19 85
| 0 74 |
mit 260| 0 0 -7 17 -125 -8 -.36 12 9 | -23 267 28 176
| -2 41 |
ngs 220| 1 1 -4 -49 139 -19 -.23 10 9 | 70 -344 1692 3817
| -36 -139 |
sio 250| -1 -2 6 72 -151 -45 -.16 19 15 | --- --- --- ---
| -29 72 |
Table 2.1664.2 GPS week: 1664 Day: 2 MJD: 55894.000
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 251| 0 0 6 103 -59 -16 -.25 11 10 | -21 -599 20 90
| 15 18 |
emr 94| 0 2 7 -3 66 -56 .40 19 19 | 1732 -282 17 110
| -71 -37 |
esa 126| 1 1 1 -107 174 37 .18 6 6 | -289 662 14 175
| 30 -6 |
gfz 198| 0 -2 -5 -8 -28 -9 -.28 14 12 | 607 -486 24 109
| -14 39 |
grg 127| 0 -2 -3 24 -93 1 .63 16 15 | 895 -678 53 260
| 34 -17 |
igr n/a| 0 0 -1 17 -91 -40 -.06 5 5 | 365 -741 19 88
| 16 52 |
jpl 148| 0 -1 1 40 -218 1 .50 15 14 | 1811 -742 17 105
| 20 31 |
mit 260| 0 0 -5 55 -90 -1 -.36 9 9 | -437 -138 25 207
| -14 20 |
ngs 220| 1 0 -5 -29 52 -18 -.22 10 8 | 144150 -210957 1527 3409
| -13 -51 |
sio 250| -1 0 9 86 -130 -23 -.15 15 14 | --- --- --- ---
| -22 64 |
Table 2.1664.3 GPS week: 1664 Day: 3 MJD: 55895.000
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 251| 0 -1 4 84 -54 -9 -.20 8 7 | -343 176 18 95
| 7 -41 |
emr 94| 2 2 7 -52 20 -54 .40 20 19 | 1229 812 16 109
| -31 23 |
esa 126| 1 1 0 -113 177 39 .20 7 6 | -1008 1569 13 160
| 48 13 |
gfz 198| -1 0 -8 77 101 -6 -.30 12 12 | -115 342 22 106
| -38 2 |
grg 127| 0 0 -7 43 -90 -16 .69 16 18 | -182 634 50 235
| 29 -12 |
igr n/a| 0 -1 0 -8 -58 -54 -.06 5 5 | -660 645 20 73
| 2 17 |
jpl 148| 0 0 0 24 -206 129 .51 16 15 | 857 872 21 96
| 6 99 |
mit 260| 0 -1 -4 35 -104 -30 -.38 11 10 | -321 646 34 247
| -18 3 |
ngs 220| 1 0 -2 -88 34 -42 -.24 11 9 | -341 144 1632 3796
| -4 -5 |
sio 250| -3 0 10 64 -152 -58 -.08 16 14 | --- --- --- ---
| -33 66 |
Table 2.1664.4 GPS week: 1664 Day: 4 MJD: 55896.000
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 251| 0 0 3 87 -79 -2 -.24 9 8 | 108 -522 22 107
| 6 15 |
emr 94| -1 2 4 -54 5 -66 .40 19 18 | 2102 -545 15 109
| -33 -5 |
esa 126| 2 0 1 -115 165 21 .21 6 6 | 309 374 13 171
| 47 20 |
gfz 198| 0 -1 -5 98 138 -15 -.33 10 10 | 593 -673 25 106
| 1 -19 |
grg 127| 1 0 -1 21 -95 -9 .70 16 15 | 674 -545 39 202
| 48 7 |
igr n/a| 1 0 0 -21 -65 -49 -.11 6 6 | 95 -493 19 67
| -14 7 |
jpl 148| 0 1 0 34 -240 88 .57 15 14 | 1894 -437 20 90
| -22 142 |
mit 260| 0 0 -7 65 -93 -43 -.43 13 11 | 157 -357 22 198
| -26 -8 |
ngs 220| 0 0 -1 -126 -17 -8 -.30 10 9 | 153 -601 1897 3510
| -3 39 |
sio 250| -1 0 9 116 -136 -42 -.13 16 15 | --- --- --- ---
| -56 81 |
Table 2.1664.5 GPS week: 1664 Day: 5 MJD: 55897.000
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 251| 0 -1 3 96 -33 -14 -.22 8 8 | -805 -151 17 96
| -1 -7 |
emr 94| 0 4 6 -98 87 -44 .40 19 19 | 211 925 13 101
| 29 -15 |
esa 126| 1 0 2 -122 225 26 .21 8 8 | -2878 1605 14 167
| 27 -16 |
gfz 198| -1 -1 -7 97 -24 -17 -.21 11 10 | -1143 2608 23 107
| -14 26 |
grg 127| 1 0 -2 33 -99 -26 .74 15 15 | -462 -369 43 183
| 47 13 |
igr n/a| 0 0 0 -4 -28 -38 -.08 5 5 | -1938 1164 17 72
| 13 32 |
jpl 148| 0 0 0 26 -164 81 .50 14 13 | -94 1141 17 88
| 5 68 |
mit 260| 0 -1 -7 21 -102 -23 -.39 11 10 | -224 -959 27 170
| -13 -5 |
ngs 220| 0 0 -2 -96 53 -6 -.27 11 9 | -829 -131 2130 3736
| -30 -31 |
sio 250| -2 1 9 74 -181 -13 -.15 17 16 | --- --- --- ---
| -42 104 |
Table 2.1664.6 GPS week: 1664 Day: 6 MJD: 55898.000
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 251| 0 0 6 115 -55 -22 -.26 7 7 | -60 -952 16 93
| -14 19 |
emr 94| 0 3 6 -58 77 -40 .41 18 18 | 2775 -1744 14 96
| -2 -44 |
esa 126| 1 0 0 -138 189 47 .20 7 7 | -1344 2164 15 196
| 65 11 |
gfz 198| 0 0 -5 49 -15 -19 -.22 8 8 | 309 382 22 101
| -1 3 |
grg 127| 0 0 -6 56 -35 -7 .66 16 13 | 1046 -1006 52 232
| 26 1 |
igr n/a| 0 0 1 -2 -79 -27 -.07 4 4 | 997 -1643 18 82
| -5 64 |
jpl 148| -4 0 1 44 -239 32 .58 14 13 | 2817 -1443 19 88
| 11 61 |
mit 260| 1 -2 -5 22 -75 -14 -.43 13 12 | 30 -613 19 169
| -21 -20 |
ngs 220| 0 -1 -2 -102 24 -16 -.29 12 10 | -19 -945 2050 3779
| -45 53 |
sio 250| 0 0 11 50 -140 -10 -.17 18 16 | --- --- --- ---
| -41 85 |
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 3.1664.0 GPS week: 1664 Day: 0 MJD: 55892.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 5 11 12 6 17 9 10 12 3 | 53 65 59 52 66 56 72 57 54 49 57
2 | 6 18 6 12 11 7 18 9 10 22 4 | 27 37 33 31 29 29 34 28 29 32 30
3 | 9 16 5 12 15 6 8 11 12 13 3 | 31 31 28 33 31 29 29 35 33 32 30
4 | 6 14 8 12 12 6 13 11 9 30 4 | 25 31 28 35 34 29 29 31 27 37 28
5E | 9 19 7 12 11 6 20 8 14 18 4 | 42 43 41 48 30 45 44 44 43 41 42
6 | 5 21 5 13 13 6 7 7 9 12 3 | 26 29 27 33 32 29 27 33 28 27 28
7 | 6 19 9 12 15 5 15 8 8 10 3 | 20 33 24 19 26 21 28 22 20 19 20
8 | 10 17 8 12 16 6 14 12 11 14 4 | 16 24 15 16 17 14 23 20 18 18 14
9 | 8 15 5 15 12 4 11 7 8 12 3 | 20 24 17 29 21 17 23 20 14 20 17
10E | 15 25 11 13 19 11 26 22 10 30 6 | 78 82 81 78 84 83 85 84 79 91 81
11 | 7 14 6 12 13 7 13 10 8 18 3 | 33 41 35 36 42 37 40 38 37 31 35
12E | 8 23 7 12 18 5 20 8 12 15 4 | 37 44 38 41 44 32 41 34 32 34 36
13 | 6 17 9 9 21 8 11 7 11 9 3 | 14 28 21 16 36 17 26 13 15 14 16
14 | 6 21 6 9 15 6 13 11 6 14 3 | 27 38 33 23 32 29 30 26 27 25 28
15 | 6 24 5 11 18 5 18 5 7 11 3 | 18 30 23 23 28 20 26 19 20 20 19
16E | 7 22 8 9 21 7 12 7 11 17 4 | 20 27 23 16 26 21 23 20 16 24 20
17 | 8 14 8 21 12 4 18 12 9 20 4 | 24 32 32 37 29 26 31 29 22 23 27
18E | 8 16 5 10 17 7 10 9 11 12 3 | 24 34 31 29 35 30 28 27 32 25 28
19 | 8 18 6 10 9 6 12 14 9 33 4 | 26 34 32 25 30 29 31 28 31 28 28
20 | 8 14 8 10 22 7 15 9 8 20 4 | 14 19 16 17 9 12 17 14 14 14 11
21 | 6 19 5 10 8 5 13 8 7 22 3 | 34 49 40 29 43 38 44 31 36 33 36
22E | 8 12 6 10 11 5 9 9 9 14 3 | 28 34 35 29 35 32 33 29 28 24 30
23 | 10 22 9 10 19 9 15 11 8 12 4 | 19 32 25 14 28 20 28 20 21 20 20
25E | 8 14 6 10 17 4 20 15 9 15 4 | 18 23 24 18 28 20 29 17 18 20 18
26 | 7 13 5 15 11 4 12 9 9 16 3 | 15 21 14 23 14 12 20 18 14 17 12
X27 | 18 22 30 22 --- 16 --- 19 --- --- 11 | 18 23 38 33 --- 20 --- 15 --- --- 18
28E | 7 13 6 13 14 5 9 6 8 13 3 | 19 26 19 18 26 18 24 19 18 20 18
29 | 7 18 8 11 11 7 16 7 8 26 4 | 29 34 33 28 35 30 35 27 29 27 30
X30E | 13 16 7 10 13 6 --- 14 13 --- 5 | 24 24 26 27 17 27 --- 28 32 --- 25
31 | 8 22 4 11 17 4 16 11 13 17 4 | 24 35 29 19 33 25 31 26 24 26 26
X32E | 20 30 8 11 --- 10 17 10 15 17 6 | 96 103 92 91 --- 90 95 88 89 88 92
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 12 15 6 15 10 10 18 |T 29 36 32 31 32 30 35 30 30 30 29
WRMS | 8 18 7 12 14 6 14 9 8 16 |NE 24 32 28 27 30 25 31 26 25 25 25
MEDI | 8 18 6 11 14 6 14 9 9 15 |MD 24 32 29 29 30 29 29 27 27 25 28
Table 3.1664.1 GPS week: 1664 Day: 1 MJD: 55893.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 13 6 11 14 5 16 7 11 10 3 | 41 51 45 40 50 41 59 43 43 39 44
2 | 5 19 8 18 12 6 12 10 10 21 4 | 21 33 24 25 23 22 30 23 25 26 22
3 | 8 14 5 11 18 5 8 15 10 15 4 | 48 40 42 36 40 41 39 45 40 43 41
4 | 7 12 5 12 14 6 9 13 8 27 4 | 16 19 19 23 22 19 19 19 21 28 17
5 | 11 22 6 16 14 9 21 10 13 22 5 | 88 95 90 99 89 86 95 95 84 89 91
6 | 7 15 4 15 13 5 6 8 10 12 3 | 30 27 29 31 31 29 28 30 26 30 27
7 | 6 22 7 15 18 4 15 5 8 10 4 | 20 31 22 22 28 18 27 18 17 16 18
8 | 11 14 6 11 14 4 15 11 13 12 4 | 16 21 15 18 19 12 26 18 21 14 13
9 | 8 18 4 14 14 5 11 10 10 13 3 | 15 21 16 22 19 14 19 16 20 12 14
10E | 23 30 10 20 26 7 23 34 10 44 8 | 43 59 47 51 58 47 59 64 50 63 49
11 | 4 16 5 11 15 5 11 7 7 17 3 | 30 34 30 30 33 28 37 30 27 25 28
12E | 10 29 6 11 14 6 25 8 11 16 4 | 31 40 31 36 39 32 38 33 39 34 33
13 | 9 21 8 13 23 5 14 6 8 9 4 | 14 24 19 16 37 14 24 12 12 11 14
14 | 6 21 5 10 16 5 12 9 12 15 3 | 23 32 27 24 34 24 27 23 25 23 24
15 | 8 22 8 9 20 6 17 8 11 14 4 | 19 27 20 25 29 17 24 19 20 20 18
16E | 8 21 7 14 18 5 12 8 11 15 4 | 27 26 28 16 31 25 27 24 24 26 24
17 | 10 16 5 15 12 6 17 10 6 22 4 | 20 28 25 28 25 23 30 26 23 20 22
18E | 12 18 6 13 15 6 11 15 8 23 4 | 27 35 32 27 32 30 31 25 28 28 27
19 | 8 17 8 10 10 6 15 10 8 25 4 | 25 28 24 26 26 23 29 25 21 27 23
20 | 6 15 8 11 19 4 13 6 11 20 4 | 15 21 18 13 9 14 22 13 13 19 13
21 | 7 16 5 12 6 4 12 14 8 21 3 | 31 42 35 32 40 32 43 28 31 29 32
22E | 9 14 7 9 10 5 9 5 8 13 3 | 27 25 27 23 26 23 27 23 20 20 23
23 | 10 25 7 16 21 7 17 7 7 11 4 | 18 26 20 16 30 15 23 14 14 15 15
25E | 8 19 8 12 17 4 16 12 8 15 4 | 19 23 21 17 31 13 25 15 16 18 15
26 | 8 14 6 11 11 6 10 12 16 13 3 | 13 18 11 17 16 9 18 17 16 15 10
X27 | 11 16 9 19 --- 22 11 12 --- --- 5 | 16 20 25 13 --- 25 18 17 --- --- 15
28E | 8 13 5 10 17 5 9 6 11 12 3 | 22 26 27 16 26 21 27 21 22 25 21
29 | 7 17 6 12 12 6 17 6 14 27 4 | 29 36 35 36 34 31 39 34 31 34 32
30E | 15 13 7 15 17 4 16 9 8 16 4 | 23 22 22 26 16 21 22 26 23 16 19
31 | 8 23 6 10 19 4 13 12 9 17 4 | 23 32 26 25 35 24 29 26 25 26 24
32E | 17 28 8 12 20 7 15 14 16 23 5 | 77 81 76 75 35 77 83 75 80 78 76
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 7 13 16 6 14 12 10 19 |T 27 33 29 29 32 27 33 28 28 28 27
WRMS | 8 19 6 13 14 5 14 9 9 15 |NE 23 29 25 24 29 22 29 23 23 23 22
MEDI | 8 17 6 12 15 5 13 10 10 15 |MD 23 28 26 25 31 23 27 24 23 25 23
Table 3.1664.2 GPS week: 1664 Day: 2 MJD: 55894.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 11 4 8 12 6 16 8 11 11 3 | 36 41 40 37 48 41 51 40 43 30 38
2 | 12 15 6 33 12 5 12 8 6 20 5 | 28 28 23 39 23 26 31 27 26 26 23
3 | 9 16 4 9 14 6 8 8 10 13 3 | 23 24 22 27 29 23 26 26 24 25 23
4 | 9 16 5 20 13 5 8 10 8 27 4 | 21 25 24 36 28 24 27 21 27 31 23
5 | 18 21 7 11 17 6 18 7 11 14 4 | 47 49 48 46 41 50 50 45 51 38 47
6 | 7 15 5 12 12 5 7 7 9 10 3 | 23 22 20 26 25 22 24 26 21 22 22
7 | 7 21 7 12 18 4 15 5 9 9 3 | 23 33 23 23 38 24 31 24 26 22 22
8 | 10 14 5 10 15 4 15 9 14 13 4 | 18 22 18 19 23 18 26 21 26 18 17
9 | 7 17 5 10 15 7 10 11 10 10 3 | 19 23 17 18 21 18 27 21 20 20 16
10 | 25 21 5 15 22 7 22 11 10 19 5 | 91 101 95 100 100 92 101 97 97 92 95
11 | 4 18 5 12 14 5 14 8 12 16 3 | 27 30 24 29 32 26 33 29 28 18 24
12E | 11 31 7 13 18 7 23 7 8 17 5 | 35 43 33 40 40 32 44 34 35 33 33
13 | 11 19 6 13 24 4 14 7 9 10 4 | 17 27 16 15 39 16 27 17 17 16 15
14 | 8 21 5 14 18 4 11 9 11 13 4 | 17 30 25 16 35 18 26 22 21 22 20
15 | 7 23 6 9 21 5 20 8 11 13 4 | 23 39 27 22 39 25 37 30 28 30 25
16E | 7 19 6 15 17 6 13 13 11 15 4 | 21 26 19 21 24 18 23 15 16 18 16
17 | 11 16 8 15 10 6 17 11 7 21 4 | 24 27 24 27 25 21 30 25 25 22 22
18 | 15 19 5 13 19 5 12 13 10 12 4 | 23 31 28 31 35 27 31 27 28 22 25
19 | 8 19 5 9 11 6 13 9 9 20 3 | 20 25 18 20 22 19 26 21 18 21 17
X20 | 7 21 5 14 --- 5 11 8 9 --- 4 | 13 24 11 14 --- 12 18 15 9 --- 9
21 | 10 15 3 9 11 3 13 12 11 20 4 | 32 32 26 23 32 26 35 29 26 28 26
22 | 11 16 5 10 17 5 8 10 14 7 3 | 28 30 30 30 38 30 34 30 26 28 27
23 | 12 25 7 14 20 5 18 7 12 12 4 | 20 30 21 20 32 18 30 19 21 17 18
25E | 6 22 4 12 10 5 18 10 7 10 3 | 16 26 19 18 23 16 28 19 19 20 16
26 | 14 13 6 7 9 5 10 9 13 11 3 | 20 22 12 14 19 14 23 22 17 19 13
X27 | 16 20 9 22 --- 11 13 12 --- --- 6 | 22 24 18 19 --- 21 23 19 --- --- 15
28E | 8 15 8 10 23 5 8 7 9 13 3 | 19 27 21 18 24 18 25 17 18 20 17
29 | 9 19 5 10 9 4 18 9 8 26 4 | 27 35 27 32 30 30 38 29 30 29 27
30E | 16 17 6 15 19 5 19 11 8 16 4 | 24 25 24 29 23 22 23 27 25 15 22
31 | 6 24 4 13 20 4 11 10 7 14 4 | 22 28 22 20 36 19 29 26 24 25 21
X32E | 15 31 7 11 --- 6 16 13 10 25 5 | 65 65 61 59 --- 62 65 61 61 59 61
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 6 14 16 5 15 9 10 15 |T 27 32 26 28 33 26 33 28 28 27 25
WRMS | 10 19 6 12 15 5 14 9 8 14 |NE 22 28 21 23 30 21 29 24 23 23 20
MEDI | 9 19 5 12 15 5 13 9 10 13 |MD 23 28 23 23 30 22 29 26 25 22 22
Table 3.1664.3 GPS week: 1664 Day: 3 MJD: 55895.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 14 6 13 13 8 18 14 10 10 4 | 51 57 54 54 61 51 59 61 51 49 54
2 | 5 15 5 13 13 4 13 11 11 21 4 | 35 38 34 38 33 36 35 38 38 40 35
3 | 9 12 6 9 12 7 10 11 13 15 3 | 30 29 26 30 32 24 29 32 22 28 26
4 | 6 11 7 10 13 5 8 14 10 26 4 | 25 26 24 29 32 26 27 26 28 30 24
5 | 8 21 9 13 19 4 20 8 7 11 4 | 28 35 30 32 42 28 35 26 26 27 28
6 | 5 14 6 13 12 5 8 8 19 11 3 | 29 32 30 37 35 29 33 35 27 32 30
7 | 6 23 6 12 20 5 19 8 9 9 4 | 27 38 29 22 36 28 33 30 26 24 26
8 | 9 21 5 9 18 6 17 10 11 12 4 | 23 27 22 19 23 23 29 27 24 22 20
9 | 7 19 5 8 11 4 11 9 8 12 3 | 16 24 14 14 22 14 20 21 12 18 14
10 | 8 22 7 13 13 8 20 10 11 20 4 | 77 81 78 82 84 81 85 78 81 74 78
11 | 5 17 7 12 13 7 14 10 9 17 3 | 39 41 40 44 47 38 41 47 41 36 40
12E | 7 25 7 11 16 5 22 6 10 13 4 | 23 35 27 19 33 21 32 25 22 24 23
13 | 7 20 4 14 22 3 17 10 10 9 4 | 16 31 19 16 37 17 27 21 18 17 17
14 | 5 20 6 11 15 5 14 9 8 13 3 | 30 38 34 28 37 31 34 33 32 28 31
15 | 6 24 6 6 20 4 21 9 9 12 4 | 31 37 30 28 41 27 34 30 30 30 29
16E | 6 25 8 14 23 5 15 13 12 12 4 | 16 25 17 19 23 16 19 23 20 21 16
17 | 9 17 8 15 13 4 19 9 7 20 4 | 28 32 34 36 33 31 33 34 28 30 30
18 | 6 21 6 9 18 5 13 14 11 11 4 | 15 28 16 16 26 16 22 23 17 22 15
19 | 6 17 6 10 11 8 15 11 11 22 4 | 37 42 35 38 39 34 37 42 42 39 37
X20 | 7 --- --- --- --- 34 --- --- --- --- 0 | 21 --- --- --- --- 33 --- --- --- --- 16
21 | 7 15 6 9 10 5 13 11 13 21 3 | 36 46 40 37 41 37 41 39 37 41 38
22 | 7 14 8 10 18 3 10 9 13 10 3 | 22 29 26 29 31 24 24 28 30 27 24
23 | 9 24 4 20 20 5 19 9 13 13 4 | 23 37 26 19 33 21 32 24 27 22 24
25E | 8 22 6 9 14 5 19 11 11 14 4 | 20 27 22 18 28 20 28 25 22 24 19
26 | 9 14 6 8 10 5 14 11 8 10 3 | 17 20 12 17 16 16 19 24 18 22 14
X27 | 12 18 12 14 --- 12 15 19 --- --- 6 | 22 24 14 20 --- 25 20 25 --- --- 14
28E | 7 19 6 10 20 5 14 7 10 12 3 | 23 33 25 18 30 23 27 24 27 22 21
29 | 7 19 5 15 12 6 20 16 11 26 4 | 37 40 37 34 40 36 40 42 38 41 37
30E | 15 17 9 15 17 6 18 14 7 19 5 | 24 29 24 29 26 24 23 34 28 15 23
31 | 7 19 6 14 17 4 13 8 9 12 3 | 32 41 32 30 38 31 38 35 32 30 32
32E | 17 34 9 12 24 8 19 13 12 28 6 | 76 83 76 79 55 74 77 81 78 83 77
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 7 12 16 5 16 11 11 16 |T 29 36 30 31 36 30 34 34 31 31 29
WRMS | 7 19 6 12 18 5 15 10 9 14 |NE 28 35 29 29 35 28 33 33 30 30 28
MEDI | 7 19 6 12 15 5 15 10 10 13 |MD 27 33 27 29 33 27 32 30 28 28 26
Table 3.1664.4 GPS week: 1664 Day: 4 MJD: 55896.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 12 8 11 15 8 16 10 10 10 4 | 33 43 40 39 43 36 48 43 36 30 37
2 | 4 15 5 9 10 4 14 14 9 22 3 | 23 28 23 23 20 22 25 25 24 21 21
3 | 7 15 5 12 17 6 9 17 11 20 4 | 21 32 22 21 25 21 27 24 22 19 20
4 | 6 10 9 13 11 4 9 18 7 26 4 | 21 25 20 28 24 21 23 28 23 29 21
X5 | 7 20 10 9 --- 5 17 11 14 13 4 | 31 40 36 35 --- 32 40 35 34 32 31
6 | 7 12 5 11 17 5 8 11 12 15 3 | 24 33 25 26 29 25 29 28 24 26 24
7 | 7 24 6 8 15 4 16 8 6 11 3 | 16 33 20 16 27 20 26 20 23 17 18
8 | 10 17 5 11 13 5 14 10 9 7 3 | 11 23 16 13 19 17 22 21 17 15 13
9 | 7 17 7 7 9 6 10 12 11 13 3 | 18 27 17 14 20 18 23 22 22 20 16
10 | 10 20 7 7 15 5 16 15 11 15 4 | 48 58 53 51 54 51 57 48 48 51 51
11 | 8 15 6 11 13 7 11 11 10 14 3 | 28 33 27 34 31 29 32 36 29 25 27
12E | 7 22 6 8 13 5 24 11 11 14 4 | 22 31 22 19 24 22 28 23 27 25 20
13 | 8 17 4 9 25 4 15 11 10 10 4 | 13 26 16 12 39 15 23 18 16 12 13
14 | 6 21 7 11 15 6 14 10 10 10 3 | 12 26 16 20 26 14 21 13 17 16 14
15 | 6 22 6 9 16 7 22 9 10 11 4 | 14 27 15 15 25 15 25 19 16 17 14
16E | 6 21 7 11 20 7 16 17 15 18 4 | 20 34 24 18 31 23 28 24 26 21 21
17 | 7 13 5 17 13 4 17 9 9 18 4 | 19 24 20 27 25 21 25 24 24 19 19
18 | 7 21 7 8 16 6 10 20 11 12 4 | 13 35 21 16 27 18 24 22 19 22 17
19 | 7 16 6 10 13 5 14 12 9 22 4 | 17 24 18 21 18 19 23 24 19 18 16
X20 | 6 14 9 13 16 7 11 8 11 --- 4 | 12 19 11 12 13 16 15 13 17 --- 11
21 | 6 15 6 8 8 6 12 9 10 21 3 | 19 33 22 21 27 23 32 20 19 21 21
22 | 8 14 7 6 17 6 8 12 12 14 3 | 11 26 18 15 25 16 19 18 19 19 14
23 | 10 22 5 11 19 5 17 10 9 13 4 | 13 30 18 15 28 14 24 19 17 16 14
25E | 5 24 5 8 14 6 17 10 7 13 3 | 15 28 19 13 26 17 25 21 21 21 15
26 | 9 15 6 8 11 6 11 11 9 10 3 | 20 23 13 15 15 14 20 21 17 18 14
X27 | 12 21 16 20 --- 29 16 15 --- --- 7 | 18 27 21 18 --- 22 21 22 --- --- 15
28E | 8 17 7 13 21 6 8 10 13 9 4 | 18 30 20 18 27 21 23 20 25 17 18
29 | 6 18 4 8 12 8 17 21 11 26 4 | 19 27 21 23 27 19 25 30 26 22 20
30E | 16 19 6 13 15 6 19 15 9 21 5 | 27 34 26 33 24 27 27 42 35 26 27
31 | 9 21 6 11 18 5 16 14 11 11 4 | 20 34 21 21 29 21 28 22 27 23 20
32E | 19 31 7 15 22 9 16 12 13 26 6 | 93 93 87 83 75 88 87 88 94 90 88
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 6 10 16 6 15 13 10 16 |T 22 32 24 23 28 23 28 26 26 24 22
WRMS | 8 18 6 10 15 6 14 11 9 15 |NE 18 28 20 20 25 20 25 23 21 20 18
MEDI | 7 17 6 11 15 6 15 11 10 14 |MD 19 30 21 20 26 21 25 22 23 21 19
Table 3.1664.5 GPS week: 1664 Day: 5 MJD: 55897.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 13 8 9 11 5 17 12 10 15 4 | 31 40 37 39 41 32 45 39 31 29 35
2 | 6 16 8 13 10 4 14 13 12 22 4 | 20 25 19 19 19 21 24 27 27 24 20
3 | 8 15 5 6 14 5 7 9 12 19 3 | 22 24 20 22 28 21 26 25 23 28 22
4 | 5 11 8 10 10 4 10 15 11 26 4 | 17 20 16 21 21 18 20 24 21 28 18
X5 | 7 --- --- --- --- 17 --- --- --- --- 0 | 5 --- --- --- --- 13 --- --- --- --- 4
6 | 7 14 5 10 13 5 7 8 13 19 3 | 23 25 24 24 30 23 27 27 23 31 24
7 | 8 19 9 12 15 3 14 6 10 12 4 | 19 29 21 17 28 18 25 19 17 18 18
8 | 10 15 9 10 16 6 12 10 15 10 4 | 12 21 16 11 17 12 20 19 19 15 13
9 | 7 17 5 5 10 4 12 9 10 14 3 | 14 19 14 15 18 15 18 20 19 18 14
10 | 9 18 8 12 13 4 15 12 13 15 4 | 44 54 47 47 51 46 55 46 52 48 47
11 | 8 17 8 30 12 5 14 11 11 16 5 | 22 27 22 38 25 20 26 31 27 21 22
12E | 10 24 8 8 10 7 22 7 15 12 4 | 12 22 12 14 19 10 21 16 21 15 12
13 | 9 16 8 9 21 3 13 8 8 10 4 | 9 24 15 12 34 10 21 13 13 10 11
14 | 7 22 8 5 14 5 11 7 8 13 3 | 24 31 27 20 33 26 27 22 31 24 24
15 | 7 27 8 10 14 4 19 10 13 12 4 | 15 29 18 16 28 13 24 17 17 17 15
16E | 5 25 7 11 17 5 19 10 10 15 4 | 14 26 20 17 25 15 22 16 15 19 16
17 | 6 16 7 11 15 4 16 8 10 18 4 | 18 25 18 20 24 18 23 20 21 18 17
18 | 6 20 6 12 19 4 9 15 8 9 4 | 14 28 17 19 27 15 20 21 19 20 17
19 | 7 20 6 9 11 4 15 14 8 25 4 | 21 29 20 25 21 21 25 26 25 25 21
20 | 8 19 11 12 18 4 11 7 7 17 4 | 12 23 15 12 13 14 16 11 9 12 12
21 | 5 17 7 10 10 4 9 7 10 23 3 | 26 31 28 23 29 26 29 25 26 25 25
22 | 7 14 8 8 19 3 11 12 9 12 3 | 15 21 17 20 23 17 21 21 18 25 16
23 | 11 21 8 11 17 5 17 12 13 15 4 | 13 26 16 12 26 13 22 14 15 14 12
25E | 6 28 10 8 13 6 17 10 8 14 4 | 10 25 18 12 24 13 24 19 15 19 12
26 | 7 17 8 9 11 5 12 13 14 11 3 | 12 22 12 16 13 10 20 18 15 15 11
X27 | 16 27 28 15 --- 19 15 15 --- --- 9 | 14 20 24 16 --- 13 14 20 --- --- 13
28E | 8 16 6 9 21 4 8 10 9 8 3 | 10 24 16 11 20 11 19 14 18 14 12
29 | 7 27 7 10 13 7 17 20 11 26 5 | 23 33 24 23 25 24 28 29 28 29 23
X30E | 13 16 8 11 14 6 17 18 11 --- 5 | 23 26 20 27 19 22 23 36 29 --- 22
31 | 6 21 7 8 13 5 11 11 11 16 3 | 24 31 25 21 32 24 29 23 28 24 23
32E | 18 22 7 15 18 7 17 10 11 22 5 | 56 64 65 70 65 65 68 68 67 69 63
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 11 15 5 14 11 11 17 |T 19 28 22 21 26 19 26 24 23 23 19
WRMS | 8 19 8 10 15 5 13 10 9 16 |NE 18 26 20 20 25 18 24 22 21 21 18
MEDI | 7 17 8 10 14 5 14 10 11 15 |MD 17 25 19 19 25 18 23 21 21 20 17
Table 3.1664.6 GPS week: 1664 Day: 6 MJD: 55898.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 12 6 6 14 5 18 12 13 15 3 | 47 53 52 54 60 51 61 57 52 44 51
2 | 6 14 6 8 11 4 12 12 10 22 3 | 31 33 28 26 26 28 30 34 31 30 28
3 | 9 18 4 7 11 5 8 13 12 19 3 | 23 27 25 23 31 22 27 29 22 27 23
4 | 6 11 5 6 11 5 9 13 8 24 3 | 27 29 28 32 33 28 31 31 29 33 28
5 | 6 28 10 10 17 4 17 21 13 24 5 | 7 28 4 4 6 8 18 5 4 3 6
6 | 8 15 6 7 13 4 8 10 10 21 3 | 26 28 29 30 34 26 30 33 26 33 28
7 | 7 20 8 10 17 4 16 9 10 16 4 | 21 30 19 19 30 19 29 21 16 18 18
8 | 9 15 12 8 16 6 13 15 14 11 4 | 15 22 18 17 20 13 27 20 15 16 14
9 | 6 16 4 6 9 4 12 11 11 12 3 | 14 21 13 13 15 14 21 18 17 15 12
10 | 8 20 6 9 13 6 14 15 12 15 4 | 65 70 68 69 70 66 75 67 65 69 67
11 | 7 16 9 12 10 4 11 15 12 18 4 | 39 39 38 49 42 39 41 49 40 35 39
12E | 8 18 6 7 12 4 24 10 11 12 4 | 16 23 17 18 23 15 26 19 20 18 16
13 | 9 15 5 6 25 4 13 13 11 13 4 | 14 25 17 13 38 15 25 15 14 12 14
14 | 6 20 7 5 16 3 12 9 12 11 3 | 20 30 26 20 37 21 30 25 22 17 22
15 | 7 19 8 7 18 6 20 14 11 15 4 | 16 28 20 17 31 15 30 16 22 14 17
16E | 7 23 7 10 21 5 14 11 13 22 4 | 11 25 17 18 21 16 20 19 19 26 14
17 | 6 16 7 10 10 4 16 9 12 19 3 | 24 29 28 28 30 26 30 29 26 25 25
18 | 7 18 6 7 15 4 11 15 9 11 3 | 20 27 19 17 27 17 24 24 16 24 18
19 | 7 19 5 7 10 5 17 14 9 30 4 | 26 30 27 33 25 30 28 36 30 31 27
20 | 7 16 9 13 19 5 9 8 13 14 4 | 20 25 17 20 12 17 22 18 16 14 18
21 | 5 16 5 9 11 2 12 8 16 26 4 | 28 32 27 24 27 26 34 25 25 26 25
22 | 7 16 7 5 22 2 10 13 13 13 3 | 19 23 19 19 26 16 22 20 16 23 17
23 | 9 22 7 12 23 5 17 18 12 18 5 | 16 29 18 12 30 15 27 15 15 14 13
25E | 6 20 5 6 13 3 17 9 11 10 3 | 15 22 18 14 27 15 27 19 18 17 14
26 | 7 16 7 10 9 5 9 18 16 13 4 | 16 23 16 19 19 13 24 19 18 14 13
X27 | 20 21 28 17 --- 16 14 16 --- --- 9 | 17 25 40 26 --- 24 26 20 --- --- 20
28E | 10 12 7 8 23 4 10 12 13 12 4 | 12 23 20 18 24 15 25 15 17 17 15
29 | 6 17 6 9 11 4 16 22 13 25 4 | 26 29 29 30 28 27 32 31 33 31 27
X30E | 15 18 8 9 17 8 --- 26 18 --- 6 | 28 31 24 31 26 29 --- 46 39 --- 27
31 | 4 18 7 6 19 3 11 11 14 17 3 | 26 33 27 26 39 25 35 27 26 24 25
32 | 11 23 8 9 26 6 16 9 14 30 5 | 53 59 58 56 64 56 53 60 59 65 56
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 8 16 4 14 13 12 18 |T 23 30 26 25 30 24 31 27 25 25 23
WRMS | 7 18 7 8 13 4 13 12 10 16 |NE 23 29 25 25 30 23 30 27 24 23 23
MEDI | 7 18 7 8 14 4 13 13 12 16 |MD 20 28 24 20 27 21 27 24 22 24 20
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 4.1664 GPS week: 1664 MJD: 55892.0-55898.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2938 |U 8 9 25 |U 11 13 35 |U 9 9 20 |
emr | emr 2941 |U 12 12 29 |U 13 11 35 | 10 10 21 |
esa | esa 2948 | 9 10 26 |U 11 12 32 | 10 8 20 |
gfz | gfz 2939 |U 11 11 26 |U 14 15 43 |U 11 11 21 |
grg | grg 2796 | 16 17 48 |U 11 13 36 | 13 15 30 |
igr | igr 2932 | 9 10 25 | 11 12 33 | 9 9 19 |
igs | igs 2928 | 10 11 26 | 10 12 32 | 8 8 18 |
jpl | jpl 2897 |U 14 15 46 |U 11 13 37 |U 9 8 21 |
mit | mit 2948 |U 13 13 37 |U 13 13 34 |U 11 11 23 |
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 5.1664.0 GPS week: 1664 Day: 0 MJD: 55892.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2965 | 8 6 22 | 8 12 28 | 10 11 17 |
emr | emr 2961 | 14 13 28 | 11 7 27 | 9 12 28 |
esa | esa 2976 | 9 9 24 | 8 11 23 | 12 12 19 |
gfz | gfz 2964 | 15 15 28 | 10 11 32 | 11 15 22 |
grg | grg 2783 | 12 15 47 | 9 13 27 | 12 18 27 |
igr | igr 2959 | 10 9 23 | 8 11 26 | 12 12 19 |
igs | igs 2946 | 14 13 29 | 8 10 24 | 9 11 18 |
jpl | jpl 2774 | 15 14 33 | 8 11 27 | 9 8 27 |
mit | mit 2976 | 19 19 32 | 20 13 41 | 14 14 31 |
Table 5.1664.1 GPS week: 1664 Day: 1 MJD: 55893.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2969 | 6 6 16 | 8 13 40 | 9 9 18 |
emr | emr 2968 | 16 18 23 | 9 13 35 | 9 8 16 |
esa | esa 2976 | 8 10 18 | 7 12 31 | 9 8 16 |
gfz | gfz 2966 | 11 12 18 | 10 17 46 | 8 8 14 |
grg | grg 2879 | 10 14 43 | 9 13 43 | 0 0 0 |
igr | igr 2976 | 12 12 15 | 7 12 30 | 8 10 15 |
igs | igs 2950 | 9 12 17 | 7 12 29 | 9 11 18 |
jpl | jpl 2962 | 17 20 86 | 11 16 43 | 10 8 21 |
mit | mit 2976 | 12 18 20 | 8 13 31 | 13 8 20 |
Table 5.1664.2 GPS week: 1664 Day: 2 MJD: 55894.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 11 9 30 | 10 12 24 | 11 9 21 |
emr | emr 2968 | 11 8 30 | 13 13 36 | 9 8 22 |
esa | esa 2976 | 11 10 27 | 10 12 24 | 9 7 19 |
gfz | gfz 2964 | 14 14 27 | 10 12 25 | 10 9 21 |
grg | grg 2688 | 15 16 48 | 12 13 35 | 14 11 42 |
igr | igr 2976 | 11 9 28 | 11 12 25 | 10 9 21 |
igs | igs 2923 | 11 10 28 | 10 13 26 | 7 7 16 |
jpl | jpl 2964 | 12 12 32 | 10 12 28 | 8 5 15 |
mit | mit 2976 | 10 9 26 | 10 13 25 | 9 13 25 |
Table 5.1664.3 GPS week: 1664 Day: 3 MJD: 55895.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2867 | 7 8 18 | 24 19 59 | 10 10 27 |
emr | emr 2872 | 9 11 16 | 23 9 45 | 12 13 29 |
esa | esa 2880 | 8 9 17 | 23 18 58 | 10 8 28 |
gfz | gfz 2873 | 8 9 18 | 28 27 68 | 14 12 25 |
grg | grg 2782 | 12 10 39 | 17 10 55 | 18 26 48 |
igr | igr 2880 | 7 10 17 | 24 19 60 | 10 8 27 |
igs | igs 2874 | 7 9 17 | 19 13 54 | 11 8 26 |
jpl | jpl 2867 | 10 10 17 | 21 11 36 | 10 13 30 |
mit | mit 2880 | 7 10 17 | 24 19 49 | 14 13 26 |
Table 5.1664.4 GPS week: 1664 Day: 4 MJD: 55896.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 8 9 35 | 7 10 26 | 8 9 17 |
emr | emr 2970 | 10 10 37 | 9 10 34 | 8 9 19 |
esa | esa 2976 | 8 9 34 | 7 10 24 | 7 9 15 |
gfz | gfz 2967 | 8 8 35 | 14 10 40 | 12 10 25 |
grg | grg 2781 | 23 35 80 | 8 8 27 | 21 30 49 |
igr | igr 2975 | 8 9 35 | 6 9 25 | 7 10 16 |
igs | igs 2951 | 8 9 33 | 7 9 24 | 7 7 14 |
jpl | jpl 2970 | 10 10 39 | 8 12 30 | 8 7 18 |
mit | mit 2976 | 9 10 36 | 7 10 28 | 7 9 17 |
Table 5.1664.5 GPS week: 1664 Day: 5 MJD: 55897.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2871 | 7 13 26 | 12 16 31 | ---- ---- ---- |
emr | emr 2876 | 9 10 31 | 14 16 40 | 11 11 18 |
esa | esa 2880 | 7 12 30 | 12 15 30 | 12 7 30 |
gfz | gfz 2872 | 8 9 25 | 15 19 48 | ---- ---- ---- |
grg | grg 2784 | 27 17 45 | 12 18 33 | 13 12 25 |
igr | igr 2880 | 7 12 29 | 12 15 31 | ---- ---- ---- |
igs | igs 2878 | 7 12 26 | 12 15 33 | ---- ---- ---- |
jpl | jpl 2871 | 20 30 70 | 12 16 59 | ---- ---- ---- |
mit | mit 2880 | 26 20 103 | 12 15 34 | ---- ---- ---- |
Table 5.1664.6 GPS week: 1664 Day: 6 MJD: 55898.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2961 | 10 9 31 | 11 10 35 | 8 7 19 |
emr | emr 2972 | 14 13 37 | 9 11 30 | 8 5 16 |
esa | esa 2976 | 13 10 35 | 11 8 33 | 8 7 16 |
gfz | gfz 2970 | 12 9 33 | 13 12 44 | 8 10 17 |
grg | grg 2879 | 12 10 32 | 12 12 32 | 10 10 21 |
igr | igr 2880 | 10 9 28 | 10 9 31 | 8 7 18 |
igs | igs 2976 | 11 9 32 | 10 9 32 | 8 7 15 |
jpl | jpl 2876 | 16 12 45 | 9 11 36 | 8 8 17 |
mit | mit 2976 | 11 7 24 | 11 10 33 | 9 9 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 6.1664 GPS week: 1664 MJD: 55892.500-55898.500
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 -2 -30 7 1 | 3 10
| 23 14 83 82 6 | 2
emr uuuuu | 32 23 75 118 0 | 28 31
| 21 31 102 81 9 | 2
esa uuuuu | 2 -34 18 60 1 | -5 10
| 17 19 61 55 2 | 1
gfz uuuuu | 6 21 41 18 6 | -6 11
| 27 14 55 114 4 | 2
grg uuuux | 24 -24 106 -27 14 | -8 23
| 15 18 76 76 17 | 4
igr xxxxx | -31 10 39 37 3 | 2 9
| 33 19 99 79 6 | 2
irf xxxxx | 11 4 20 -4 1 | -2 9
| 11 3 39 24 2 | 1
jpl uuuuu | -70 3 -47 -146 -8 | 12 18
| 29 15 120 40 10 | 2
mit uuuuu | 3 17 -111 -65 1 | 7 13
| 31 12 86 40 5 | 1
ngs uuuuu | 41 13 -32 -12 -8 | 5 10
| 57 36 58 142 6 | 1
sio uuuuu | -65 38 14 6 9 | 12 16
| 16 14 59 39 8 | 3
Table 7.1664.0 GPS week: 1664 Day: 0 MJD: 55892.500
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 0 -163 18 0 | 1 9
emr uuuuu | 22 4 82 88 7 | 27 30
esa uuuuu | -21 2 8 -5 1 | -5 11
gfz uuuuu | 23 40 -15 171 2 | -8 13
grg uuuux | 39 3 18 59 9 | -14 25
igr xxxxx | -42 38 -35 107 -1 | 0 8
irf xxxxx | 8 6 -6 6 0 | -3 10
jpl uuuuu | -85 20 122 -150 -7 | 14 18
mit uuuuu | -17 2 -76 -29 6 | 6 13
ngs uuuuu | 82 -59 -10 -50 -2 | 5 10
sio uuuuu | -55 25 -55 -8 -8 | 13 18
Table 7.1664.1 GPS week: 1664 Day: 1 MJD: 55893.500
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 -22 39 64 6 | 2 9
emr uuuuu | 51 26 -30 248 7 | 26 29
esa uuuuu | -20 -42 19 -9 5 | -5 11
gfz uuuuu | -2 23 98 -77 9 | -7 12
grg uuuux | 44 -9 0 49 1 | -13 24
igr xxxxx | -76 26 -80 140 2 | 1 8
irf xxxxx | -5 1 57 -48 3 | -2 10
jpl uuuuu | -79 1 -158 -91 -10 | 14 18
mit uuuuu | -46 3 -9 -123 5 | 7 14
ngs uuuuu | 134 37 3 159 -12 | 5 10
sio uuuuu | -77 30 60 -56 6 | 11 16
Table 7.1664.2 GPS week: 1664 Day: 2 MJD: 55894.500
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 | -15 -13 -59 8 11 | 1 8
emr uuuuu | 40 73 -60 201 5 | 25 28
esa uuuuu | 9 -28 21 27 -1 | -7 9
gfz uuuuu | -36 16 119 -137 8 | -8 11
grg uuuux | 20 -32 111 1 8 | -10 22
igr xxxxx | -49 -14 -17 -75 7 | 0 7
irf xxxxx | 3 2 62 -10 2 | -4 8
jpl uuuuu | -28 -18 -142 -171 -14 | 12 17
mit uuuuu | -17 16 -58 -57 1 | 5 12
ngs uuuuu | 54 15 -44 135 -12 | 4 10
sio uuuuu | -61 24 96 8 12 | 9 11
Table 7.1664.3 GPS week: 1664 Day: 3 MJD: 55895.500
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 -4 27 90 -1 | 5 11
emr uuuuu | -5 34 93 68 4 | 29 31
esa uuuuu | 5 -45 78 79 0 | -5 9
gfz uuuuu | 16 41 40 -50 6 | -5 12
grg uuuux | 30 -26 83 -12 19 | -7 22
igr xxxxx | 1 1 88 43 9 | 3 10
irf xxxxx | 18 3 63 -10 -1 | -1 9
jpl uuuuu | -81 -3 -171 -194 -22 | 13 17
mit uuuuu | 15 21 -51 -89 -6 | 8 14
ngs uuuuu | 23 7 -137 77 0 | 5 10
sio uuuuu | -48 36 52 4 13 | 11 16
Table 7.1664.4 GPS week: 1664 Day: 4 MJD: 55896.500
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 -1 -96 -37 -6 | 4 11
emr uuuuu | 33 38 76 21 1 | 28 31
esa uuuuu | 8 -42 -41 99 -1 | -5 10
gfz uuuuu | 47 4 63 44 0 | -5 12
grg uuuux | 21 -43 173 -38 28 | -7 22
igr xxxxx | 21 19 222 56 8 | 3 10
irf xxxxx | 28 5 -15 24 0 | -2 10
jpl uuuuu | -114 27 47 -182 2 | 9 17
mit uuuuu | 36 31 -200 -73 -4 | 6 14
ngs uuuuu | -11 8 38 -44 -5 | 4 10
sio uuuuu | -53 61 -8 3 17 | 11 16
Table 7.1664.5 GPS week: 1664 Day: 5 MJD: 55897.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 18 2 -33 -151 -5 | 4 11
emr uuuuu | 26 -28 254 131 -12 | 30 32
esa uuuuu | 27 -26 -66 118 3 | -6 10
gfz uuuuu | -15 15 -19 145 12 | -4 10
grg uuuux | -2 -46 184 -156 43 | -5 23
igr xxxxx | -21 -12 58 -58 4 | 5 10
irf xxxxx | 11 1 -4 -11 1 | -2 9
jpl uuuuu | -57 -4 57 -98 -13 | 10 17
mit uuuuu | 16 14 -143 -86 -3 | 7 14
ngs uuuuu | 42 31 -4 -144 -11 | 5 10
sio uuuuu | -93 43 10 12 10 | 14 18
Table 7.1664.6 GPS week: 1664 Day: 6 MJD: 55898.500
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 24 75 59 -1 | 4 11
emr uuuuu | 60 12 108 67 -12 | 31 33
esa uuuuu | 5 -55 108 113 2 | -4 9
gfz uuuuu | 13 11 3 28 7 | -2 10
grg uuuux | 15 -16 173 -89 -6 | -2 26
igr xxxxx | -48 15 40 46 -9 | 6 11
irf xxxxx | 16 10 -18 21 3 | 0 8
jpl uuuuu | -45 -1 -84 -134 7 | 10 17
mit uuuuu | 36 31 -241 -1 5 | 9 14
ngs uuuuu | -37 55 -69 -218 -16 | 5 10
sio uuuuu | -69 51 -56 78 15 | 17 20
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