[IGSREPORT-20362] Wk 1662 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Dec 1 12:07:17 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1662 (Nov 13, 2011 - Nov 19, 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:
igs1662[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1662[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1662[0-6].cls IGS GPS clock combination summary report.
igs16627.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16627.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 | DARW DARW KOSG TLSE
0 | ESA | KOUR UNSA
0 | GFZ | 20 KOSG MDVJ NICO
0 | GRG | AMC2 KOUR
0 | JPL | 32
0 | MIT | 3 6 7 27 30 32 3 6 7 27 30 32 NICO HYDE
1 | COD | 18 DARW DARW
1 | ESA | NICO NICO UNSA
1 | GFZ | 5 18 20 22 CAS1 MDVJ TIXI
1 | GRG | AMC2 GUAT SANT
1 | JPL | 32 CAS1
1 | MIT | 3 18 27 32 4 18 27 32 CAS1 CAS1 DAV1 HYDE
2 | COD | MAW1 MAW1
2 | EMR | 32 10 32
2 | ESA | NKLG UNSA
2 | GFZ | 5 10 18 20 22 MATE MDVJ
2 | GRG | AMC2
2 | JPL | 10 32 KARR YELL
2 | MIT | 1 10 21 27 1 10 21 27 32 BRMU HARB NICO BRMU HARB
2 | MIT | NICO
3 | COD | STHL
3 | EMR | 32 10 32
3 | ESA | 10 ABMF KOUR UNSA
3 | GFZ | 5 10 18 20 22 PRDS
3 | GRG | KOUR USN3
3 | JPL | 3 32
3 | MIT | 10 21 27 32 10 21 27 32 DAV1 DAV1 PRDS
4 | COD | NKLG TLSE
4 | EMR | 10 32 10 32
4 | ESA | UNSA
4 | GFZ | 5 10 18 20 22 IISC MDVJ
4 | GRG | AMC2
4 | JPL | 10 32 AREQ
4 | MIT | 8 10 27 32 8 10 27 32
5 | COD | STHL
5 | ESA | KOSG CEDU KOSG KOUR UNSA
5 | GFZ | 5 10 18 20 22 ALRT GUAT KOSG MDVJ OPMT STJO
5 | GRG | AMC2 CEDU KOUR
5 | JPL | 27
5 | MIT | 1 8 11 21 22 27 28 1 8 10 11 21 22 27 28 CEDU
6 | COD | NICO
6 | EMR | 10 10 HARB HARB
6 | ESA | CEDU CEDU UNSA
6 | GFZ | 5 10 18 20 22 30 32 KOSG KOUR MDVJ
6 | JPL | 32 AREQ
6 | MIT | 10 27 30 32 10 27 30 32 CAS1 KOSG MIZU BRUS CAS1
6 | MIT | KOSG MIZU
5. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G32 | 2011_11_18 | 2011092
6. 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.
7. 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 .1 -.5 -55 4 9 .09
EMR | 6.6 2.1 12.5 5 9 -6 .41
ESA | 5.9 2.0 -9.9 103 -191 107 .20
GFZ | -.6 .5 -.5 -48 -8 -2 .14
GRG | 8.6 1.2 3.8 -22 31 5 .07
JPL | 1.3 6.0 9.3 18 -19 -29 .25
MIT | 7.1 -.2 3.0 -29 18 -41 .14
NGS | 8.7 .6 3.2 -11 -46 42 .49
SIO | 4.4 2.9 11.2 11 -62 6 .20
8. 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.
9. 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.
10. 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 1.1662.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1662.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 2.1662.[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 3.1662.[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 5.1662.0-6).
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 1662 summary. (Nov 13, 2011 - Nov 19, 2011)
Table 1.1662.a GPS week: 1662 MJD: 55878.000-55884.000
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 257| 0 0 1 83 -71 -1 -.26 7 7 | -471 284 22 105
| 0 0 0 10 8 12 .02 | 564 696
emr 93| 0 0 10 -54 -80 -3 .37 19 18 | 2347 247 20 151
| 1 2 2 23 16 18 .04 | 757 1096
esa 125| 1 1 0 -122 168 28 .19 7 7 | -989 1322 15 178
| 0 0 1 13 15 8 .02 | 1687 1609
gfz 200| 0 0 -2 100 -33 -9 -.24 11 11 | 3 266 23 97
| 1 1 0 44 20 7 .02 | 401 608
grg 131| 2 2 -5 26 -130 -6 .61 15 14 | 19 422 49 225
| 1 1 0 6 9 15 .04 | 548 737
igr n/a| 0 0 -1 -31 -38 -31 -.11 5 5 | -512 328 20 77
| 0 0 1 11 10 15 .03 | 577 890
jpl 147| -1 0 3 -48 -6 19 .52 14 13 | 2489 177 20 98
| 1 1 1 17 5 42 .02 | 604 859
mit 259| 0 -1 -3 59 -101 -35 -.39 13 12 | -376 737 25 240
| 0 1 0 27 16 18 .01 | 224 383
ngs 218| 0 0 0 -13 65 0 -.26 13 10 | -463 323 1721 3712
| 0 0 2 26 11 20 .03 | 523 638
sio 253| -2 0 2 -19 67 -41 -.12 18 16 | --- --- --- ---
| 1 2 0 35 22 17 .04 | --- ---
Table 1.1662.b GPS week : 1662 MJD: 55878.000-55884.000
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 | 5 4 4 4 5 5 4 |
2 | 4 4 4 4 4 5 4 |
3 | 4 4 4 4 4 5 4 |
4 | 4 4 4 4 4 4 4 |
5 | 4 5 4 4 4 4 4 |
6 | 4 4 4 4 4 4 3 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 5 4 4 5 4 |
9 | 4 4 4 4 4 4 4 |
10 | 6 6 5 5 5 5 5 |
11 | 4 4 4 4 5 5 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 5 4 4 5 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 4 4 4 5 |
16 | 4 4 4 4 4 5 4 |
17 | 5 4 4 4 5 4 4 |
18 | 4 5 4 4 4 5 4 |
19 | 5 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 5 4 5 4 |
22 | 5 5 4 4 4 4 3 |
23 | 5 5 5 5 5 5 5 |
25 | 5 4 4 4 4 4 4 |
26 | 3 3 3 3 4 4 4 |
27 | 10 9 13 8 15 11 9 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 6 5 |
30 | 5 6 5 5 7 6 6 |
31 | 5 5 4 4 4 5 5 |
32 | 5 6 5 6 6 0 6 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1662.0 GPS week: 1662 Day: 0 MJD: 55878.000
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 257| 0 0 0 78 -79 1 -.27 8 8 | 17 -90 21 112
| 60 -3 |
emr 93| 0 0 12 -44 -91 20 .33 18 18 | 2682 -498 20 147
| 23 -10 |
esa 125| 1 1 0 -127 137 28 .18 7 7 | 2695 -2097 12 179
| 50 24 |
gfz 200| -2 0 -3 159 -12 -11 -.25 12 11 | 183 176 25 114
| -20 36 |
grg 131| 3 3 -4 27 -130 0 .61 15 14 | 79 586 44 223
| 58 -9 |
igr n/a| 0 0 -2 -37 -26 -34 -.13 6 6 | -281 -439 21 76
| 49 3 |
jpl 147| -3 0 3 -51 -10 -39 .56 13 12 | 3423 -689 20 103
| 103 -59 |
mit 259| 0 -3 -4 71 -81 -20 -.40 12 11 | -201 733 27 329
| -7 -14 |
ngs 218| 1 0 0 -34 62 2 -.26 15 11 | 87 -217 1917 4113
| -103 -23 |
sio 253| 0 -3 3 -4 112 -21 -.18 17 17 | --- --- --- ---
| 16 -71 |
Table 2.1662.1 GPS week: 1662 Day: 1 MJD: 55879.000
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 257| -1 0 1 85 -68 6 -.29 7 6 | 493 -686 23 91
| 52 -17 |
emr 93| 1 3 8 -49 -85 10 .35 18 18 | 1858 1140 27 160
| 38 -31 |
esa 125| 2 1 -1 -126 183 23 .16 7 6 | -1711 2762 20 182
| 84 14 |
gfz 200| -1 -1 -2 112 -40 -11 -.24 13 13 | 713 -737 23 90
| 3 10 |
grg 131| 0 0 -5 25 -116 13 .57 14 12 | 671 -17 49 225
| 49 -34 |
igr n/a| 0 0 -2 -10 -35 -15 -.13 5 5 | -950 1157 23 81
| 3 -12 |
jpl 147| -1 1 5 -30 -11 -6 .50 14 13 | 2456 801 22 98
| 63 -50 |
mit 259| 0 -1 -4 63 -128 -24 -.37 14 12 | -131 724 32 283
| -12 -10 |
ngs 218| 0 1 1 -12 63 11 -.25 13 10 | 413 -603 1850 3544
| -95 -51 |
sio 253| -2 -3 1 4 43 -42 -.15 18 16 | --- --- --- ---
| -7 -56 |
Table 2.1662.2 GPS week: 1662 Day: 2 MJD: 55880.000
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 257| -1 0 2 73 -75 -9 -.27 7 6 | -258 -61 20 101
| 40 -14 |
emr 93| -2 0 9 -83 -98 5 .41 20 20 | 1060 1770 17 160
| 71 -21 |
esa 125| 1 1 -1 -97 171 26 .18 7 7 | -1944 2495 15 166
| 56 19 |
gfz 200| -1 -2 -3 89 -46 -5 -.23 11 11 | -162 792 22 90
| -4 38 |
grg 131| 1 4 -4 23 -136 3 .60 14 14 | -410 999 44 212
| 35 -10 |
igr n/a| 0 0 0 -34 -35 -12 -.12 5 5 | -1478 1474 18 75
| 30 35 |
jpl 147| 0 0 4 -48 -5 -12 .52 14 13 | 1502 1418 20 97
| 91 -45 |
mit 259| 0 -1 -3 51 -95 -11 -.40 13 13 | -565 813 21 204
| -22 -18 |
ngs 218| 0 1 2 -4 77 -5 -.26 14 9 | -470 322 1432 3492
| -77 -78 |
sio 253| 0 0 2 -50 70 -32 -.15 17 16 | --- --- --- ---
| 36 -70 |
Table 2.1662.3 GPS week: 1662 Day: 3 MJD: 55881.000
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 257| -1 0 0 72 -82 8 -.26 7 7 | -893 902 31 110
| 52 3 |
emr 93| -1 -4 7 -65 -88 -27 .42 18 18 | 2458 831 15 124
| 46 -44 |
esa 125| 0 0 0 -135 174 14 .20 7 7 | -1550 1109 13 173
| 38 0 |
gfz 200| 0 1 -2 154 -1 -14 -.22 11 12 | 41 8 23 96
| 0 15 |
grg 131| 3 1 -5 40 -147 -10 .65 14 14 | 382 -197 52 202
| 55 14 |
igr n/a| 0 0 0 -47 -51 -37 -.12 5 5 | -580 637 19 75
| 34 40 |
jpl 147| 0 0 3 -75 -5 45 .52 14 14 | 2402 432 19 92
| 69 -44 |
mit 259| 0 -1 -3 82 -102 -31 -.40 12 11 | -538 570 25 233
| -16 -16 |
ngs 218| 1 1 0 -59 47 25 -.27 12 10 | -841 764 1593 3343
| 57 -15 |
sio 253| -2 0 1 0 63 -72 -.11 17 14 | --- --- --- ---
| 25 -65 |
Table 2.1662.4 GPS week: 1662 Day: 4 MJD: 55882.000
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 257| 0 0 0 92 -70 -2 -.23 7 7 | -927 -101 21 116
| 27 -17 |
emr 93| 0 0 7 -16 -53 4 .36 19 18 | 3286 329 17 160
| 0 -50 |
esa 125| 1 0 0 -127 176 32 .23 8 8 | -1843 1725 14 172
| 37 -3 |
gfz 200| 0 0 -3 79 -38 3 -.21 11 11 | 79 -101 23 94
| -28 35 |
grg 131| 1 1 -5 24 -128 -22 .63 15 14 | 566 -708 64 225
| 42 1 |
igr n/a| 0 0 0 -25 -54 -38 -.08 5 5 | 50 582 19 80
| 28 35 |
jpl 147| -2 0 2 -32 1 35 .52 14 14 | 2753 375 18 94
| 20 -39 |
mit 259| 0 0 -2 22 -103 -48 -.39 11 11 | -89 141 19 207
| 18 -10 |
ngs 218| 1 0 1 -5 63 6 -.22 11 9 | -889 145 1557 3467
| -52 -29 |
sio 253| -3 0 3 -66 68 -50 -.08 17 18 | --- --- --- ---
| 46 -63 |
Table 2.1662.5 GPS week: 1662 Day: 5 MJD: 55883.000
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 257| 0 0 1 101 -61 7 -.23 8 8 | -861 1253 25 101
| 20 -18 |
emr 93| -1 4 12 -42 -60 -16 .41 19 19 | 3026 -437 28 168
| 33 -43 |
esa 125| 2 0 2 -113 159 29 .22 8 8 | -1943 1692 19 178
| 44 14 |
gfz 200| 0 0 -1 36 -31 -16 -.27 11 11 | -564 957 25 106
| -43 10 |
grg 131| 2 0 -6 24 -126 -29 .54 15 16 | -412 1147 44 247
| 34 -8 |
igr n/a| 0 -1 -1 -28 -28 -57 -.06 5 5 | 198 -86 21 84
| 38 42 |
jpl 147| -1 -1 2 -35 -14 85 .50 14 13 | 2808 -5 24 109
| 18 -46 |
mit 259| 0 0 -4 25 -83 -63 -.39 14 12 | -596 1440 27 231
| 3 -20 |
ngs 218| 0 0 -4 23 80 -39 -.33 13 11 | -944 1340 2007 4337
| -2 -13 |
sio 253| -3 1 2 -49 67 -48 -.09 18 17 | --- --- --- ---
| 33 -67 |
Table 2.1662.6 GPS week: 1662 Day: 6 MJD: 55884.000
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 257| 0 0 2 84 -62 -25 -.26 7 7 | -872 776 19 107
| 52 -10 |
emr 93| -2 1 10 -78 -83 -23 .33 19 18 | 2059 -1405 16 144
| 72 -27 |
esa 125| 3 1 1 -132 179 41 .19 7 7 | -631 1571 16 197
| 76 -26 |
gfz 200| -1 0 -3 72 -62 -9 -.24 8 8 | -268 768 21 95
| -15 12 |
grg 131| 3 3 -5 18 -130 0 .65 14 11 | -738 1144 52 243
| 64 -2 |
igr n/a| 0 -1 -1 -33 -35 -26 -.11 4 4 | -549 -1028 19 72
| 20 23 |
jpl 147| 0 -2 2 -68 -3 30 .53 14 14 | 2082 -1093 18 94
| 69 -42 |
mit 259| 0 0 -4 95 -116 -49 -.38 15 13 | -517 743 24 198
| -29 -4 |
ngs 218| 1 0 -3 -2 64 -7 -.25 11 8 | -603 510 1695 3693
| 2 -35 |
sio 253| -3 2 2 29 47 -23 -.10 19 16 | --- --- --- ---
| 8 -49 |
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 3.1662.0 GPS week: 1662 Day: 0 MJD: 55878.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 10 18 7 8 --- 5 16 16 12 13 4 | 41 59 48 44 --- 45 65 47 44 49 48
2 | 8 20 6 16 9 4 16 11 9 20 4 | 17 28 16 18 17 18 27 21 24 19 16
3 | 10 10 5 11 11 5 8 12 16 19 4 | 22 23 22 23 29 21 25 25 25 24 22
4 | 10 13 4 10 11 5 8 12 11 28 4 | 33 31 32 32 35 33 30 34 32 38 31
5E | 6 17 6 10 12 4 12 12 12 10 3 | 51 55 50 50 53 52 54 57 56 55 52
6 | 5 8 5 15 12 6 8 12 14 19 3 | 23 26 26 31 33 25 27 33 24 29 26
7 | 6 18 10 12 19 5 15 7 13 11 4 | 14 29 22 15 27 15 26 20 26 13 18
8 | 11 21 7 14 13 5 11 11 14 14 4 | 13 29 17 14 19 13 24 23 25 21 17
9 | 7 21 7 14 11 8 9 7 13 20 4 | 20 33 21 19 29 16 29 20 24 22 19
10E | 17 21 8 14 20 6 19 21 25 12 6 | 41 46 39 42 50 39 49 45 49 44 41
11 | 8 17 6 8 14 8 10 10 12 19 3 | 30 40 34 36 49 35 40 38 37 37 35
12 | 6 27 10 13 15 7 19 9 16 18 4 | 18 35 24 17 31 17 26 20 24 19 19
13 | 6 19 9 8 22 5 13 10 16 12 4 | 20 34 24 19 39 21 31 21 22 18 21
14 | 9 19 6 12 17 8 12 13 13 15 4 | 18 29 20 23 29 20 25 22 27 19 20
15 | 6 18 7 8 21 5 13 9 9 14 3 | 20 31 24 20 39 22 28 23 25 19 21
16 | 4 24 6 10 18 4 13 8 15 12 4 | 15 32 15 15 25 14 22 15 21 18 15
17 | 9 14 6 20 15 4 15 8 15 20 4 | 26 26 33 37 32 29 30 31 34 24 29
18E | 8 18 6 12 17 6 12 12 14 12 4 | 30 34 35 30 46 30 33 39 38 34 33
19 | 8 17 7 10 9 5 11 18 14 25 4 | 22 26 28 27 25 28 27 31 31 31 26
20E | 4 11 7 8 13 6 14 11 15 14 3 | 25 33 28 25 34 28 29 22 30 27 25
21 | 9 21 5 10 12 6 15 10 15 22 4 | 22 40 27 21 39 23 38 21 29 16 25
22E | 5 18 10 12 14 6 13 18 12 15 4 | 22 27 26 23 30 20 25 36 30 25 23
23 | 8 23 9 10 17 6 13 17 15 15 4 | 23 38 24 19 34 22 31 24 21 22 21
25 | 8 15 9 16 14 7 16 11 15 17 4 | 28 35 30 27 36 26 32 28 35 28 28
26 | 9 13 5 8 9 4 11 11 12 9 3 | 20 20 15 14 20 15 19 19 24 14 15
X27 | 23 24 28 21 --- 19 15 12 --- --- 10 | 22 28 28 18 --- 29 21 16 --- --- 13
28 | 10 21 5 12 16 3 10 8 11 9 3 | 19 34 20 19 32 20 27 23 29 20 20
29 | 7 18 9 22 15 7 15 8 18 29 5 | 21 29 26 26 26 24 26 25 28 29 23
X30 | 9 16 5 16 17 8 --- 18 14 14 5 | 41 49 43 45 47 42 --- 43 47 25 43
31 | 6 18 5 12 20 5 14 16 14 12 4 | 15 28 16 18 27 14 26 18 24 17 16
32E | 11 24 5 10 17 7 15 9 23 14 4 | 20 30 24 22 16 21 29 22 29 18 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 12 15 6 13 12 15 17 |T 24 33 27 25 32 25 30 27 30 25 25
WRMS | 8 18 7 11 14 6 12 11 11 17 |NE 21 31 24 23 30 22 29 24 27 23 22
MEDI | 8 18 6 12 15 6 13 11 14 14 |MD 22 31 26 23 32 22 27 23 28 22 22
Table 3.1662.1 GPS week: 1662 Day: 1 MJD: 55879.000
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 | 6 13 5 10 --- 4 13 16 8 11 3 | 36 50 45 33 --- 37 57 36 40 45 42
2 | 4 20 7 17 10 6 16 10 12 22 4 | 11 23 10 13 12 11 21 16 21 17 11
3 | 7 9 5 15 12 6 8 12 11 23 3 | 15 18 19 17 22 16 18 18 20 21 16
4 | 5 11 4 8 9 5 9 11 13 27 3 | 22 26 24 23 29 24 25 25 28 32 23
5E | 6 21 6 12 16 6 14 22 12 32 5 | 26 30 27 24 34 25 27 25 29 26 23
6 | 6 10 5 14 10 7 7 16 13 22 4 | 17 21 20 21 21 18 17 23 22 22 18
7 | 5 21 6 13 15 4 16 8 9 11 3 | 12 32 17 16 28 16 25 17 22 14 15
8 | 10 18 7 14 13 5 14 11 8 13 4 | 11 22 11 15 14 11 21 18 18 16 10
9 | 6 15 5 14 8 6 11 10 10 17 3 | 17 24 15 12 20 15 21 16 23 19 16
10E | 12 25 7 13 19 6 18 20 25 16 5 | 27 42 34 33 43 32 40 38 43 36 33
11 | 7 14 4 10 12 4 12 10 13 18 3 | 22 35 27 21 35 23 34 26 27 29 25
12 | 6 27 8 14 15 5 22 8 11 17 4 | 18 32 21 16 30 18 28 21 22 20 19
13 | 6 20 7 12 17 3 14 11 12 12 4 | 15 33 21 18 36 16 28 17 20 14 18
14 | 8 19 7 15 13 7 13 15 12 16 4 | 14 27 20 18 27 16 24 19 22 15 17
15 | 4 21 7 9 14 3 12 7 16 13 3 | 15 26 17 16 27 16 21 17 23 15 15
16 | 5 21 6 11 16 6 12 14 9 15 4 | 13 25 13 11 25 10 18 14 18 16 12
17 | 6 13 5 17 11 4 15 8 13 19 4 | 17 21 18 25 23 20 25 21 28 16 19
18E | 8 14 10 12 12 6 13 22 14 14 4 | 20 26 27 23 23 20 26 20 22 17 21
19 | 7 13 4 11 8 5 11 12 16 25 4 | 17 23 21 18 21 19 23 22 21 23 18
20E | 5 11 8 10 10 3 12 11 15 13 3 | 17 23 21 18 24 16 24 16 21 19 17
21 | 6 20 6 12 14 4 15 10 9 21 4 | 21 39 27 20 39 23 33 19 26 13 25
22E | 7 22 7 13 15 5 12 19 15 16 4 | 24 31 29 26 27 26 28 29 28 26 26
23 | 10 24 9 15 16 4 14 18 8 14 4 | 19 35 24 20 29 18 27 22 19 18 19
25 | 7 16 6 15 17 4 13 11 12 16 4 | 24 30 24 20 36 22 31 22 30 23 24
26 | 5 14 4 9 6 5 9 8 10 8 2 | 13 18 10 12 15 11 16 16 18 14 11
X27 | 21 20 22 24 --- 38 17 15 --- --- 9 | 24 22 29 23 --- 30 21 18 --- --- 18
28 | 7 19 6 11 18 3 12 11 9 9 3 | 15 30 17 16 32 16 24 19 19 16 16
29 | 5 19 11 14 12 7 16 11 16 31 5 | 10 23 22 14 17 14 20 17 23 21 15
X30 | 8 21 7 16 14 7 --- 25 16 --- 6 | 34 50 40 36 39 35 --- 39 40 --- 38
31 | 5 16 6 14 17 5 15 19 15 11 4 | 10 23 15 15 25 11 23 16 17 11 12
X32E | 11 27 7 14 --- 5 15 12 23 14 5 | 19 35 23 19 --- 19 26 19 28 19 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 13 14 5 14 14 13 18 |T 18 28 22 19 26 19 25 21 24 20 19
WRMS | 6 18 6 13 12 5 13 12 10 16 |NE 17 27 20 18 25 17 25 19 22 19 18
MEDI | 6 19 6 13 13 5 13 11 12 16 |MD 17 26 21 18 27 18 24 19 22 19 18
Table 3.1662.2 GPS week: 1662 Day: 2 MJD: 55880.000
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 | 7 15 6 9 --- 6 12 15 15 13 4 | 35 51 44 37 --- 38 52 40 39 42 40
2 | 5 21 6 11 10 4 17 9 8 20 4 | 15 25 11 12 16 11 22 17 17 16 11
3 | 5 14 5 10 12 5 8 11 10 19 3 | 16 19 17 20 20 15 18 19 16 19 16
4 | 4 16 5 14 9 4 8 7 12 29 4 | 25 26 25 26 29 23 25 24 24 34 23
5E | 9 19 5 10 12 3 14 16 10 14 4 | 21 27 22 23 30 19 25 24 23 22 20
6 | 5 13 4 13 11 4 7 14 11 17 3 | 18 20 23 25 24 19 22 26 18 22 20
7 | 4 24 8 13 16 5 16 11 8 10 4 | 12 31 17 15 27 12 24 16 16 12 13
8 | 10 19 6 12 15 5 15 16 17 14 4 | 10 23 14 10 17 8 22 21 20 17 10
9 | 6 20 6 9 11 5 11 9 14 17 3 | 16 24 15 13 22 11 19 17 20 14 13
10E | 11 18 11 10 20 7 18 16 24 10 5 | 29 40 33 34 44 32 42 38 40 35 33
11 | 6 20 6 10 13 7 13 11 22 18 4 | 24 36 29 31 41 26 33 31 31 29 27
12 | 6 31 7 10 15 6 20 12 16 17 4 | 16 34 16 15 28 15 23 18 16 16 15
13 | 4 24 9 11 22 5 14 13 10 13 4 | 17 34 20 18 37 17 28 17 18 14 17
14 | 8 22 8 12 15 5 14 7 15 16 4 | 16 28 21 19 30 17 25 17 24 15 17
15 | 4 23 7 8 17 4 14 10 6 15 3 | 15 27 15 14 30 13 19 17 16 14 13
16 | 5 25 6 10 15 4 15 13 10 14 4 | 17 29 14 12 25 13 21 14 13 16 13
17 | 7 14 8 15 11 6 16 7 16 20 4 | 20 23 30 29 26 22 26 25 28 19 23
18E | 8 14 8 10 18 4 10 17 12 12 4 | 20 25 25 19 23 19 24 24 21 19 20
19 | 6 20 5 10 9 5 11 12 16 25 4 | 19 22 20 23 19 19 21 26 22 23 18
20E | 6 11 7 10 12 4 12 16 16 12 3 | 15 23 21 18 24 16 23 22 19 19 16
21 | 7 19 4 10 12 4 16 12 16 22 4 | 22 39 26 22 37 23 35 19 26 15 24
22E | 5 19 7 11 14 5 12 11 12 14 3 | 18 26 24 17 26 17 25 21 21 21 19
23 | 8 27 7 15 18 6 15 19 9 16 5 | 16 33 20 15 26 14 26 21 16 16 15
25 | 8 15 7 9 15 3 17 11 13 16 4 | 23 31 25 23 33 22 30 20 25 24 22
26 | 5 12 5 7 10 4 7 10 11 9 2 | 17 20 12 16 19 13 17 20 20 14 13
X27 | 23 22 45 19 --- 24 19 18 --- --- 13 | 17 26 52 13 --- 18 22 17 --- --- 19
28 | 7 15 8 10 16 4 11 11 13 10 3 | 12 26 20 14 30 12 21 15 15 15 13
29 | 6 17 11 10 12 5 16 14 13 32 5 | 16 24 25 21 19 18 22 19 23 19 17
30 | 9 19 8 14 17 4 16 25 12 17 5 | 33 48 38 39 36 36 20 36 38 29 36
31 | 5 17 5 10 19 3 15 14 12 11 4 | 15 25 16 15 27 10 25 17 14 14 13
32E | 12 23 5 13 16 4 14 14 20 16 4 | 22 29 25 23 16 21 31 23 26 22 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 20 7 11 14 5 14 13 14 17 |T 18 28 23 20 26 18 25 21 22 20 19
WRMS | 6 20 7 11 14 5 13 13 9 16 |NE 17 28 21 19 26 17 24 20 20 19 17
MEDI | 6 19 7 10 15 5 14 12 12 16 |MD 17 26 21 19 26 17 24 20 20 19 17
Table 3.1662.3 GPS week: 1662 Day: 3 MJD: 55881.000
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 | 9 12 8 8 --- 6 15 12 11 11 4 | 40 51 43 39 --- 40 57 45 35 45 42
2 | 5 19 7 12 8 5 16 8 12 20 4 | 14 26 11 12 13 15 22 18 22 17 13
3 | 10 10 7 10 14 6 10 14 15 21 4 | 20 24 20 21 24 18 22 23 21 22 19
4 | 6 12 7 7 10 4 9 9 12 27 3 | 28 29 31 28 34 31 29 30 32 35 28
5E | 7 19 5 11 11 5 16 13 10 13 4 | 15 24 19 18 24 17 24 19 19 22 16
6 | 5 11 8 11 13 4 7 13 16 17 3 | 21 26 22 29 27 24 24 30 26 25 23
7 | 6 21 6 12 19 3 16 7 8 10 4 | 14 29 19 14 28 14 25 18 16 14 15
8 | 9 16 6 8 12 5 14 12 11 10 3 | 13 24 16 12 17 12 21 22 17 16 13
9 | 7 16 6 9 15 5 12 12 15 15 4 | 19 30 19 16 27 18 25 23 19 18 18
10E | 14 19 7 12 17 7 19 14 15 11 5 | 35 45 37 36 49 35 48 41 36 42 37
11 | 9 18 10 13 15 5 13 11 10 15 4 | 34 40 28 39 44 33 38 37 30 32 32
12 | 7 25 8 12 16 3 19 16 10 16 4 | 19 34 23 20 31 21 28 23 22 21 20
13 | 6 19 6 11 18 5 13 10 7 11 3 | 17 34 22 20 39 19 27 20 19 17 20
14 | 5 17 8 12 14 5 13 9 15 15 4 | 15 27 20 19 29 18 23 17 27 17 18
15 | 4 23 6 8 15 5 15 10 11 13 4 | 20 33 25 20 33 22 26 26 24 22 21
16 | 4 23 6 12 17 4 13 13 14 16 4 | 16 31 19 16 25 16 20 13 20 17 16
17 | 8 15 6 19 12 5 17 8 10 18 4 | 25 29 27 32 31 26 31 29 30 22 26
18E | 6 16 7 11 13 6 10 17 14 9 4 | 17 26 23 22 27 19 26 24 19 18 20
19 | 5 12 4 9 10 5 13 11 11 26 3 | 24 27 26 28 25 26 27 30 28 28 25
20E | 6 11 6 12 15 3 12 16 10 10 3 | 22 29 21 23 29 21 26 24 20 23 21
21 | 8 21 4 11 11 4 16 10 12 24 4 | 21 38 25 21 36 22 35 18 21 15 23
22E | 5 18 7 10 15 5 10 9 13 12 3 | 20 27 25 21 27 20 28 21 25 25 22
23 | 9 23 7 13 17 5 15 15 10 15 4 | 23 41 26 26 35 24 32 26 21 24 24
25 | 8 12 7 13 16 5 17 12 11 14 4 | 25 33 32 29 37 29 34 25 31 27 28
26 | 10 13 5 8 10 4 10 10 9 9 3 | 24 21 15 13 21 16 18 23 20 18 16
X27 | 17 20 16 14 --- 25 --- 14 --- --- 8 | 24 24 21 18 --- 28 --- 22 --- --- 15
28 | 7 19 8 10 16 4 12 9 6 9 3 | 21 33 22 19 34 19 26 22 24 19 21
29 | 6 14 7 10 13 7 18 17 14 29 4 | 20 27 21 19 23 21 31 27 25 24 21
X30 | 7 22 8 14 15 5 --- 17 12 --- 5 | 40 55 43 44 46 42 --- 41 40 --- 42
31 | 7 19 9 13 17 5 15 11 8 16 4 | 13 26 20 18 28 14 24 15 19 14 15
X32E | 12 28 8 15 --- 6 13 11 14 19 5 | 21 36 24 22 --- 22 29 20 25 20 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 11 14 5 14 12 12 17 |T 21 31 24 23 30 22 28 24 24 22 22
WRMS | 7 18 7 12 14 5 14 11 10 14 |NE 21 30 23 22 29 21 28 24 23 22 21
MEDI | 7 18 7 11 15 5 13 12 11 15 |MD 21 29 22 21 28 21 26 23 22 22 21
Table 3.1662.4 GPS week: 1662 Day: 4 MJD: 55882.000
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 | 7 22 6 12 --- 5 17 13 13 15 4 | 35 57 44 36 --- 38 57 42 38 46 42
2 | 7 19 9 10 11 4 15 10 9 20 4 | 17 23 11 10 13 12 19 17 18 13 10
3 | 10 12 10 13 15 7 9 13 12 20 4 | 18 21 15 23 24 16 20 20 22 20 17
4 | 4 15 7 11 12 4 13 11 14 26 4 | 25 25 27 32 30 24 26 26 25 33 25
5E | 8 19 6 10 17 5 16 12 14 15 4 | 19 24 14 18 20 14 22 16 21 19 15
6 | 5 11 10 12 13 4 10 11 13 17 3 | 22 24 18 26 27 19 22 25 24 23 21
7 | 5 23 9 12 20 5 17 6 9 12 4 | 15 30 19 16 27 15 24 16 16 12 14
8 | 9 19 8 11 12 3 13 15 12 11 4 | 12 21 16 14 14 11 18 23 20 16 11
9 | 5 19 7 11 12 4 12 10 9 16 3 | 18 25 17 17 20 13 21 19 17 17 14
10E | 12 19 10 11 20 5 19 13 19 10 5 | 33 43 36 35 46 34 44 39 33 39 35
11 | 7 22 7 12 18 5 16 12 13 17 4 | 25 38 32 29 41 25 35 33 25 29 28
12 | 8 24 9 10 14 4 21 14 11 16 4 | 16 28 19 18 29 14 26 19 20 15 15
13 | 6 21 7 7 21 4 14 9 10 12 4 | 17 33 21 19 39 17 28 17 18 16 18
14 | 5 20 5 12 14 4 13 9 11 17 3 | 15 27 18 18 26 17 23 16 22 19 17
15 | 5 22 8 11 16 5 15 10 9 15 4 | 19 31 21 21 31 16 24 23 24 21 19
16 | 4 25 7 10 17 4 14 12 15 16 4 | 13 29 14 14 23 12 20 11 20 17 12
17 | 8 13 11 17 13 3 18 10 9 19 4 | 22 23 28 30 24 21 25 25 25 20 22
18E | 6 15 10 12 17 4 11 14 10 7 4 | 15 23 23 18 21 17 22 20 20 19 17
19 | 5 13 6 11 10 4 12 10 13 25 4 | 22 22 22 28 25 21 22 26 24 22 22
20E | 5 19 7 9 17 3 10 16 12 15 4 | 18 27 21 20 23 20 23 23 25 22 19
21 | 6 18 8 8 13 7 14 9 12 26 4 | 22 35 28 21 37 22 36 18 22 13 22
22E | 5 17 6 10 15 4 10 8 9 16 3 | 20 27 20 18 21 17 24 18 21 26 19
23 | 9 37 7 10 19 5 14 11 12 16 5 | 18 44 20 19 32 16 26 17 18 16 17
25 | 5 13 10 9 15 6 18 11 8 14 4 | 21 26 27 23 34 23 30 21 23 25 22
26 | 11 13 5 10 8 5 10 10 8 11 3 | 22 21 16 17 21 15 19 22 19 20 16
X27 | 27 20 46 16 --- 11 --- 19 --- --- 15 | 23 23 41 18 --- 14 --- 21 --- --- 12
28 | 6 18 6 12 18 3 13 9 9 10 3 | 16 27 18 16 33 15 24 18 19 18 15
29 | 7 16 11 7 12 8 17 17 10 29 4 | 22 27 30 24 22 19 27 24 24 24 21
X30E | 16 20 11 13 22 7 --- 18 12 --- 6 | 57 66 60 62 67 57 --- 62 58 --- 59
31 | 7 15 7 11 18 3 14 10 8 18 4 | 13 23 15 16 26 12 21 15 18 18 13
X32E | 13 31 6 13 --- 7 14 12 17 --- 6 | 21 34 24 23 --- 24 31 25 22 --- 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 8 11 15 5 14 11 11 17 |T 21 29 23 22 28 19 26 23 23 21 20
WRMS | 7 18 8 11 14 5 14 11 9 18 |NE 19 28 22 21 27 17 25 21 21 20 18
MEDI | 7 19 7 11 15 4 14 11 11 16 |MD 19 27 21 19 26 17 24 21 22 19 18
Table 3.1662.5 GPS week: 1662 Day: 5 MJD: 55883.000
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 | 7 15 11 --- --- 7 14 15 12 15 5 | 34 50 40 --- --- 37 54 37 33 40 39
2 | 7 23 10 18 9 7 15 13 9 21 4 | 14 26 9 15 14 9 21 15 12 14 8
3 | 12 11 7 11 15 6 10 14 13 21 4 | 20 21 18 24 24 20 25 16 23 19 18
4 | 4 13 7 6 12 5 9 19 12 27 4 | 23 22 23 21 29 22 24 30 25 35 22
5E | 8 21 7 10 11 4 18 13 11 10 4 | 16 24 19 19 20 17 23 18 17 19 15
6 | 6 11 6 11 12 5 9 8 9 18 3 | 20 26 18 30 25 23 25 21 23 22 21
7 | 5 17 10 8 20 4 13 9 14 13 4 | 14 29 19 19 28 17 24 16 14 15 15
8 | 10 21 9 10 12 7 13 19 13 11 4 | 12 25 18 18 18 13 19 27 15 17 13
9 | 7 17 8 8 11 6 10 12 13 18 3 | 14 25 14 15 20 15 20 17 20 17 14
10E | 13 20 5 6 12 5 17 13 12 14 4 | 34 42 40 37 49 39 48 42 39 45 39
11 | 6 17 9 11 16 5 14 14 14 18 4 | 24 34 24 28 36 26 35 30 25 26 25
12 | 10 24 9 9 16 6 21 17 16 14 5 | 14 27 19 15 28 15 26 19 15 15 15
13 | 8 19 8 6 25 5 12 12 11 18 4 | 14 32 21 18 39 19 27 14 18 12 17
14 | 6 19 8 10 16 5 12 11 11 14 4 | 17 27 20 21 29 18 22 19 22 20 19
15 | 5 19 10 6 20 4 15 11 12 14 4 | 13 26 16 12 30 13 21 18 15 17 13
16 | 6 28 8 13 17 6 13 11 12 16 4 | 13 34 17 22 22 14 19 13 14 20 14
17 | 5 14 8 11 11 5 13 11 13 20 4 | 21 22 25 22 24 21 24 25 26 18 20
18E | 6 18 11 13 15 4 9 18 14 16 4 | 16 25 25 20 20 20 22 19 19 22 19
19 | 6 15 6 8 9 8 11 9 15 28 4 | 21 25 20 25 22 26 26 23 27 21 21
20E | 7 13 7 9 12 5 9 13 11 17 3 | 22 27 25 25 29 24 27 28 26 28 23
21 | 9 21 7 11 11 6 13 12 12 25 4 | 22 38 29 25 37 25 35 19 24 15 25
22E | 6 17 9 9 12 3 11 10 12 14 3 | 20 25 26 22 24 23 25 19 25 31 22
23 | 11 22 7 10 21 5 14 14 14 18 4 | 19 32 24 20 31 21 29 19 23 17 19
25 | 7 15 10 11 14 5 15 14 16 11 4 | 18 29 24 23 30 19 29 17 20 21 19
26 | 9 13 9 11 9 6 9 14 12 8 3 | 18 17 16 15 18 15 16 20 18 15 14
X27 | 30 18 33 18 --- 14 16 17 --- --- 11 | 24 18 34 20 --- 19 23 21 --- --- 15
28 | 6 22 7 7 17 3 7 10 11 10 3 | 19 33 25 20 36 19 25 23 21 22 21
29 | 6 18 7 8 12 5 17 26 17 29 5 | 18 25 22 19 21 19 25 27 20 19 18
30E | 19 23 9 17 24 7 22 15 11 24 6 | 46 56 43 47 52 43 28 44 42 23 45
31 | 7 18 6 13 22 5 15 11 14 17 4 | 18 28 18 25 32 18 25 22 20 22 18
X32E | 8 --- --- --- --- 54 --- --- --- --- 0 | 16 --- --- --- --- 19 --- --- --- --- 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 11 15 5 14 14 13 18 |T 19 29 23 22 28 20 26 22 22 21 20
WRMS | 8 19 8 11 16 5 13 12 11 17 |NE 18 27 21 20 26 19 25 21 20 19 18
MEDI | 7 18 8 10 12 5 13 13 12 17 |MD 18 26 21 21 28 19 25 19 21 20 19
Table 3.1662.6 GPS week: 1662 Day: 6 MJD: 55884.000
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 | 8 12 6 6 --- 4 15 14 13 12 3 | 45 55 49 48 --- 47 63 51 48 47 48
2 | 7 20 7 9 7 3 14 17 9 24 4 | 16 26 13 14 15 13 21 22 19 19 13
3 | 10 11 7 9 12 4 10 13 12 19 3 | 18 21 21 26 28 22 24 23 23 23 21
4 | 6 11 4 5 12 5 9 18 14 27 4 | 33 31 32 36 40 34 34 37 35 42 33
5E | 4 16 6 9 13 4 20 11 8 12 3 | 15 25 17 20 20 15 25 13 13 19 15
6 | 7 11 6 9 9 3 8 10 10 19 3 | 25 25 26 33 32 26 27 30 24 27 27
7 | 6 20 9 12 15 3 14 9 14 17 4 | 15 26 16 20 28 14 24 14 16 13 14
8 | 9 21 7 9 10 6 15 19 12 15 4 | 11 24 13 16 17 12 22 23 13 15 11
9 | 7 17 8 5 10 3 10 13 9 20 3 | 16 24 19 15 17 16 20 20 15 19 15
10E | 15 21 7 9 19 7 21 18 13 16 5 | 43 54 48 47 62 45 63 49 45 54 49
11 | 6 16 5 9 13 4 14 15 16 14 4 | 36 40 37 43 49 37 40 44 38 35 37
12 | 7 25 8 5 16 5 22 18 12 16 4 | 18 34 24 20 30 20 29 25 17 22 21
13 | 6 19 10 4 20 4 13 13 10 18 4 | 17 32 22 19 37 18 28 16 16 17 19
14 | 7 19 9 7 13 4 13 13 12 16 4 | 21 32 26 21 33 22 29 21 26 24 23
15 | 6 23 9 8 16 5 16 15 12 20 4 | 16 27 21 17 31 16 22 22 17 20 17
16 | 5 27 6 8 17 3 13 14 10 22 4 | 14 31 17 13 25 12 20 14 21 21 14
17 | 8 14 6 9 12 6 16 12 14 21 4 | 29 30 34 35 36 33 34 36 35 26 32
18E | 7 14 7 8 19 3 11 17 8 10 3 | 16 25 22 17 21 17 25 19 17 20 18
19 | 5 14 3 8 9 4 11 12 14 28 3 | 28 27 30 38 32 35 29 35 35 33 30
20E | 7 14 4 9 19 5 11 14 11 14 3 | 22 29 24 29 26 25 26 28 25 29 22
21 | 8 21 7 8 11 4 14 12 10 28 4 | 23 39 29 25 38 24 37 21 22 16 26
22E | 7 17 6 5 13 3 10 11 6 15 3 | 18 26 24 17 26 18 27 17 20 28 21
23 | 9 34 10 8 16 5 16 14 11 19 5 | 17 41 22 18 27 18 28 19 21 19 18
25 | 5 15 7 6 16 3 17 15 12 15 4 | 23 33 29 26 35 26 32 26 24 28 26
26 | 11 14 8 8 8 4 9 12 13 11 3 | 28 28 21 23 25 20 24 23 22 24 21
X27 | 21 23 20 21 --- 9 16 18 --- --- 9 | 18 22 30 17 --- 14 17 24 --- --- 15
28 | 5 16 7 8 17 2 12 12 8 12 3 | 19 30 20 19 35 18 26 21 17 17 18
29 | 4 17 6 7 13 4 18 27 12 36 5 | 22 25 25 24 27 24 27 31 25 31 23
X30E | 15 23 8 10 16 6 --- 17 10 --- 5 | 55 60 54 56 56 52 --- 55 54 --- 54
31 | 6 26 8 10 17 4 14 18 10 20 4 | 17 31 19 20 30 15 25 23 17 18 16
X32E | 14 --- 6 7 20 9 16 18 14 --- 5 | 12 --- 6 7 9 12 12 7 6 --- 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 8 14 4 14 15 11 19 |T 22 31 25 25 30 23 28 26 24 25 23
WRMS | 7 18 7 8 11 4 14 13 8 16 |NE 21 30 24 24 30 22 28 25 23 24 22
MEDI | 7 17 7 8 13 4 14 14 12 17 |MD 18 29 24 20 30 20 26 23 21 22 21
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 4.1662 GPS week: 1662 MJD: 55878.0-55884.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2955 |U 7 6 19 |U 9 11 33 |U 12 13 27 |
emr | emr 2941 |U 15 13 27 |U 11 11 38 | 14 14 29 |
esa | esa 2962 | 8 6 20 |U 8 11 32 | 12 14 30 |
gfz | gfz 2937 |U 14 13 22 |U 19 23 71 |U 14 17 31 |
grg | grg 2728 | 21 19 34 |U 10 11 45 | 12 14 30 |
igr | igr 2959 | 7 6 21 | 9 10 34 | 12 13 27 |
igs | igs 2947 | 7 6 19 | 9 10 33 | 13 14 26 |
jpl | jpl 2853 |U 12 11 28 | 9 12 36 | 11 14 23 |
mit | mit 2962 |U 25 21 28 |U 10 13 37 |U 29 30 63 |
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 5.1662.0 GPS week: 1662 Day: 0 MJD: 55878.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 7 6 23 | 6 9 27 | 42 50 69 |
emr | emr 2968 | 11 7 32 | 11 12 31 | 45 42 77 |
esa | esa 2976 | 9 5 21 | 6 11 25 | 41 51 81 |
gfz | gfz 2968 | 8 6 20 | 11 10 72 | 39 47 66 |
grg | grg 2784 | 13 16 29 | 10 8 33 | 20 11 38 |
igr | igr 2976 | 9 7 25 | 7 10 27 | 41 47 71 |
igs | igs 2975 | 8 4 22 | 7 10 26 | 44 48 69 |
jpl | jpl 2860 | 10 7 37 | 6 11 23 | 23 36 35 |
mit | mit 2976 | 25 10 39 | 7 10 25 | 97 113 177 |
Table 5.1662.1 GPS week: 1662 Day: 1 MJD: 55879.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2967 | 6 5 16 | 8 10 31 | ---- ---- ---- |
emr | emr 2968 | 10 8 24 | 11 9 37 | ---- ---- ---- |
esa | esa 2976 | 10 6 18 | 8 10 30 | ---- ---- ---- |
gfz | gfz 2961 | 13 11 23 | 13 17 88 | ---- ---- ---- |
grg | grg 2688 | 11 13 33 | 10 11 40 | 10 14 28 |
igr | igr 2976 | 7 5 19 | 9 8 35 | ---- ---- ---- |
igs | igs 2976 | 7 5 18 | 8 9 32 | ---- ---- ---- |
jpl | jpl 2862 | 9 5 24 | 9 10 31 | 13 15 26 |
mit | mit 2976 | 13 14 25 | 14 10 36 | ---- ---- ---- |
Table 5.1662.2 GPS week: 1662 Day: 2 MJD: 55880.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 6 5 22 | 8 9 29 | 6 7 19 |
emr | emr 2968 | 21 8 29 | 11 9 30 | 9 8 17 |
esa | esa 2976 | 7 6 22 | 9 9 27 | 7 7 23 |
gfz | gfz 2968 | 12 10 17 | 20 22 51 | 10 10 28 |
grg | grg 2784 | 31 16 46 | 10 9 36 | 10 10 19 |
igr | igr 2976 | 7 5 22 | 10 10 28 | 6 6 21 |
igs | igs 2973 | 6 4 22 | 9 9 28 | 7 7 20 |
jpl | jpl 2966 | 17 9 28 | 11 10 28 | 8 8 21 |
mit | mit 2976 | 25 17 23 | 10 9 29 | 11 11 19 |
Table 5.1662.3 GPS week: 1662 Day: 3 MJD: 55881.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 17 | 10 14 28 | 7 5 19 |
emr | emr 2968 | 16 15 28 | 9 15 34 | 7 6 21 |
esa | esa 2976 | 7 6 18 | 9 14 30 | 5 6 18 |
gfz | gfz 2967 | 18 14 21 | 24 32 73 | 7 8 20 |
grg | grg 2688 | 19 14 29 | 10 16 44 | 10 20 32 |
igr | igr 2975 | 8 6 19 | 9 14 31 | 4 5 16 |
igs | igs 2932 | 8 7 18 | 9 13 31 | 5 5 14 |
jpl | jpl 2776 | 12 11 33 | 12 16 41 | 9 11 23 |
mit | mit 2976 | 21 21 24 | 10 19 32 | 9 12 22 |
Table 5.1662.4 GPS week: 1662 Day: 4 MJD: 55882.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 9 10 20 | 10 11 24 | 8 6 19 |
emr | emr 2968 | 15 20 29 | 10 13 32 | 11 11 26 |
esa | esa 2976 | 8 8 23 | 8 12 28 | 6 6 23 |
gfz | gfz 2959 | 20 21 27 | 18 28 53 | 8 11 20 |
grg | grg 2687 | 32 30 49 | 11 12 51 | 10 11 30 |
igr | igr 2959 | 8 7 24 | 9 11 27 | 6 7 21 |
igs | igs 2973 | 8 7 22 | 9 11 29 | 7 7 20 |
jpl | jpl 2776 | 16 23 33 | 10 13 31 | 10 11 22 |
mit | mit 2976 | 28 34 35 | 9 12 28 | 8 11 20 |
Table 5.1662.5 GPS week: 1662 Day: 5 MJD: 55883.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2873 | 6 5 17 | 12 13 58 | 6 4 15 |
emr | emr 2876 | 17 21 24 | 14 12 63 | 8 9 16 |
esa | esa 2880 | 7 6 19 | 12 11 56 | 5 7 14 |
gfz | gfz 2776 | 18 20 20 | 25 32 87 | 12 12 28 |
grg | grg 2688 | 20 23 19 | 14 14 69 | 9 14 20 |
igr | igr 2880 | 7 4 20 | 12 12 59 | 5 6 14 |
igs | igs 2880 | 7 5 19 | 12 11 57 | 5 9 13 |
jpl | jpl 2870 | 15 17 21 | 12 13 58 | 7 12 17 |
mit | mit 2880 | 40 31 27 | 12 20 72 | 38 21 118 |
Table 5.1662.6 GPS week: 1662 Day: 6 MJD: 55884.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2968 | 6 5 15 | 7 9 33 | 7 8 18 |
emr | emr 2872 | 14 13 25 | 9 7 40 | 8 10 19 |
esa | esa 2976 | 7 4 17 | 6 9 28 | 8 10 22 |
gfz | gfz 2963 | 11 11 24 | 20 21 71 | 9 13 25 |
grg | grg 2783 | 22 20 35 | 8 10 43 | 16 22 42 |
igr | igr 2975 | 7 4 18 | 6 9 30 | 7 11 22 |
igs | igs 2920 | 7 7 16 | 7 9 31 | 9 11 20 |
jpl | jpl 2867 | 8 8 23 | 8 10 39 | 7 10 19 |
mit | mit 2976 | 21 23 20 | 7 9 39 | 9 15 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 6.1662 GPS week: 1662 MJD: 55878.500-55884.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -4 -21 -37 90 0 | 1 17
| 7 10 50 84 4 | 3
emr uuuuu | 18 -18 14 -42 3 | 41 44
| 13 20 84 96 17 | 4
esa uuuuu | -20 -32 47 -116 4 | -7 19
| 15 16 47 51 4 | 2
gfz uuuuu | -37 38 -41 -93 -6 | 2 17
| 11 11 52 69 4 | 2
grg uuuux | -8 -26 40 -29 4 | -16 37
| 14 9 36 66 27 | 18
igr xxxxx | -38 -6 57 37 -1 | -3 18
| 21 19 40 75 4 | 1
irf xxxxx | -14 23 -6 -6 2 | -2 16
| 3 9 35 24 3 | 2
jpl uuuuu | 32 -39 -5 17 -11 | 29 32
| 9 28 67 86 11 | 2
mit uuuuu | -1 32 -135 95 5 | 6 18
| 8 24 55 52 3 | 3
ngs uuuuu | 20 61 76 140 -2 | 2 14
| 22 57 92 110 4 | 1
sio uuuuu | 49 0 -8 182 4 | 18 24
| 11 24 99 49 7 | 3
Table 7.1662.0 GPS week: 1662 Day: 0 MJD: 55878.500
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 -39 -58 167 4 | -2 17
emr uuuuu | 2 -2 13 154 3 | 36 40
esa uuuuu | -32 -29 -7 -150 1 | -8 20
gfz uuuuu | -44 41 -33 -131 -6 | 5 18
grg uuuux | 1 -37 94 52 42 | -50 94
igr xxxxx | -11 -28 105 156 -8 | -2 18
irf xxxxx | -8 21 12 4 0 | -3 17
jpl uuuuu | 51 -82 -75 110 9 | 30 32
mit uuuuu | 6 28 -104 -13 6 | 4 17
ngs uuuuu | 15 124 193 145 -1 | 1 14
sio uuuuu | 63 5 53 192 -7 | 17 23
Table 7.1662.1 GPS week: 1662 Day: 1 MJD: 55879.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -1 -26 35 37 5 | -1 18
emr uuuuu | 13 -12 -146 -88 14 | 36 40
esa uuuuu | -32 -58 109 -54 3 | -8 20
gfz uuuuu | -28 23 5 -99 -6 | 4 18
grg uuuux | 16 -23 79 -11 21 | -28 60
igr xxxxx | -6 23 91 18 3 | -3 18
irf xxxxx | -18 26 22 -38 2 | -3 17
jpl uuuuu | 32 -37 -95 58 -7 | 32 34
mit uuuuu | -8 38 -132 81 7 | 4 17
ngs uuuuu | 33 121 -38 69 -4 | 2 14
sio uuuuu | 38 33 86 91 3 | 15 22
Table 7.1662.2 GPS week: 1662 Day: 2 MJD: 55880.500
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 -15 -22 161 -1 | 0 17
emr uuuuu | 7 -46 25 -41 24 | 37 41
esa uuuuu | -33 -31 23 -66 1 | -8 20
gfz uuuuu | -52 29 1 -190 -4 | 3 17
grg uuuux | -4 -10 9 31 7 | -17 48
igr xxxxx | -49 -5 -5 68 -2 | -3 18
irf xxxxx | -14 25 28 12 3 | -3 17
jpl uuuuu | 31 -66 -28 57 -10 | 31 33
mit uuuuu | 4 47 -68 120 6 | 5 17
ngs uuuuu | 64 102 -49 5 -5 | 1 14
sio uuuuu | 56 -11 109 243 4 | 16 22
Table 7.1662.3 GPS week: 1662 Day: 3 MJD: 55881.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -17 -19 2 53 -1 | 2 17
emr uuuuu | 30 -13 56 -19 17 | 40 45
esa uuuuu | -14 -5 -2 -129 2 | -8 20
gfz uuuuu | -29 33 18 -102 -8 | 3 17
grg uuuux | -28 -22 49 -112 0 | -2 13
igr xxxxx | -54 -1 56 51 -1 | -3 18
irf xxxxx | -14 33 -1 -28 4 | -3 17
jpl uuuuu | 30 -36 41 6 -21 | 31 33
mit uuuuu | 2 49 -134 94 7 | 5 18
ngs uuuuu | 1 -24 60 224 -1 | 2 14
sio uuuuu | 51 8 -57 151 10 | 17 23
Table 7.1662.4 GPS week: 1662 Day: 4 MJD: 55882.500
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 -18 -91 -62 0 | 2 17
emr uuuuu | 36 9 -32 -59 1 | 43 47
esa uuuuu | -11 -28 48 -173 5 | -7 20
gfz uuuuu | -49 37 -105 -67 -11 | 1 18
grg uuuux | -15 -33 -5 -31 -4 | -3 14
igr xxxxx | -49 -19 42 12 1 | -3 18
irf xxxxx | -14 9 -16 -25 4 | -2 16
jpl uuuuu | 25 -11 40 90 -22 | 28 32
mit uuuuu | -4 -9 -106 118 3 | 7 18
ngs uuuuu | 15 61 152 75 3 | 2 14
sio uuuuu | 49 -37 -34 185 11 | 18 24
Table 7.1662.5 GPS week: 1662 Day: 5 MJD: 55883.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 4 -7 -104 132 0 | 1 17
emr uuuuu | 29 -20 82 -102 -12 | 43 47
esa uuuuu | -28 -31 108 -167 12 | -9 19
gfz uuuuu | -24 56 -105 -96 1 | -2 17
grg uuuux | -6 -21 23 -11 -46 | -5 13
igr xxxxx | -56 -25 87 -93 1 | -4 18
irf xxxxx | -14 13 -11 6 6 | -3 16
jpl uuuuu | 32 -5 -8 -93 -19 | 26 30
mit uuuuu | 6 10 -166 128 5 | 6 18
ngs uuuuu | -1 15 89 333 -7 | 1 13
sio uuuuu | 53 -20 -40 214 9 | 18 24
Table 7.1662.6 GPS week: 1662 Day: 6 MJD: 55884.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -8 -20 -23 139 -9 | 6 15
emr uuuuu | 9 -40 103 -142 -24 | 47 49
esa uuuuu | 8 -44 51 -70 4 | -3 18
gfz uuuuu | -30 47 -68 37 -6 | 3 16
grg uuuux | -16 -32 33 -121 4 | -8 17
igr xxxxx | -41 12 24 45 1 | 0 16
irf xxxxx | -18 32 -75 27 -2 | 2 14
jpl uuuuu | 24 -37 90 -106 -7 | 26 31
mit uuuuu | -14 61 -238 140 -2 | 12 18
ngs uuuuu | 17 30 127 126 5 | 4 12
sio uuuuu | 31 24 -175 201 -2 | 23 27
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