[IGSREPORT-20073] Wk 1648 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 25 10:12:40 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1648 (Aug 07, 2011 - Aug 13, 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:
igs1648[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1648[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1648[0-6].cls IGS GPS clock combination summary report.
igs16487.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16487.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 | 3 6 3 6
0 | ESA | UNSA
0 | GFZ | 6 DAEJ
0 | GRG | NKLG
0 | JPL | 3 25 TIXI
0 | MIT | 3 6 13 3 6 13
1 | EMR | 6 3 6
1 | ESA | 21 21 IRKJ UNSA
1 | GFZ | 3 6 MDVJ
1 | GRG | IRKJ NKLG USN3
1 | JPL | 6 25 CAS1
1 | MIT | 1 3 6 12 1 3 6 12 CAS1 KOSG CAS1 KOSG
2 | EMR | 3 6 3 4 6
2 | ESA | 4 IRKJ MATE UNSA
2 | GFZ | 4 6 21 DUBO KARR KOSG
2 | GRG | IRKJ USN3
2 | JPL | 3 4 6 25 IRKJ
2 | MIT | 3 4 6 7 15 21 3 4 6 7 15
3 | COD | CHUR CHUR
3 | EMR | 19 21 3 21
3 | ESA | IRKJ UNSA
3 | GFZ | 3 6 17 29 MDVJ
3 | GRG | IRKJ USN3
3 | JPL | 3 25 IRKJ
3 | MIT | 19 29 31 3 19 29 31 KHAJ KHAJ
4 | COD | WILL
4 | EMR | 3 6 3 6
4 | ESA | IRKJ UNSA
4 | GFZ | 29 MDVJ WHIT
4 | GRG | IRKJ NRMD USN3
4 | JPL | 25 IRKJ
4 | MIT | 1 3 6 19 27 30 1 3 6 19 27 30
5 | COD | 19 19 SOFI WES2
5 | ESA | KOSG IRKJ MAW1 UNSA
5 | GFZ | 3 6 29 DAV1 MDVJ YAKT
5 | GRG | IRKJ SOFI USN3
5 | JPL | 3 15 25 IRKJ PALM
5 | MIT | 1 3 6 19 21 27 30 1 3 6 19 21 27 30
6 | ESA | IRKJ
6 | GFZ | 17 19 29 NKLG
6 | GRG | IRKJ USN3
6 | JPL | 25 IRKJ PALM
6 | MIT | 1 3 6 27 30 1 3 6 27 30 GRAZ
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
----+------------+----------
G17 | 2011_08_11 | 2011060
G17 | 2011_08_12 | 2011060
6. Velocity changes were estimated to alleviate the effects of modeling
problems, experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G01 | | | | | 4 | | |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
8. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .7 .3 .7 -18 -7 7 .01
EMR | 3.3 3.8 1.3 4 9 -5 .34
ESA | -.4 -1.1 16.5 -10 3 45 .17
GFZ | -1.3 .2 .1 -23 4 0 -.07
GRG | 2.2 -2.7 11.9 -8 -20 2 -.07
JPL | 3.2 2.1 -8.9 -15 8 50 -1.27
MIT | 4.4 -4.3 15.4 -15 5 -21 -.01
NGS | 6.2 1.0 12.1 -26 -22 20 .04
SIO | -3.4 -1.2 2.3 -35 41 13 -.10
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution does not yet use IGS08/igs08.atx, which causes their RMS
clock residuals to be higher than for the other centres; for the same
reason, the JPL solution is excluded from the weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1648.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1648.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 2.1648.[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 3.1648.[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 5.1648.0-6).
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 1648 summary. (Aug 07, 2011 - Aug 13, 2011)
Table 1.1648.a GPS week: 1648 MJD: 55780.000-55786.000
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 250| 0 0 -1 8 -3 14 -.21 7 7 | -471 -1 16 84
| 0 0 0 11 11 9 .03 | 545 910
emr 92| 0 2 -5 -66 -5 5 .41 18 18 | 3845 258 18 118
| 0 1 3 35 15 10 .02 | 1236 925
esa 130| 0 0 2 -37 45 -12 .28 8 8 | -418 -1267 19 161
| 0 0 1 23 17 12 .02 | 1474 1952
gfz 192| 0 0 0 9 -43 -5 -.22 11 10 | 168 -91 25 141
| 0 1 1 42 35 9 .03 | 254 500
grg 129| 1 0 6 -12 28 10 .76 15 14 | -3 -47 46 220
| 0 0 2 14 16 33 .09 | 395 769
igr n/a| 0 0 0 7 2 -27 -.06 5 5 | 6531 196 21 100
| 0 0 1 15 8 18 .01 | 1287 890
jpl 132| -1 0 -11 2 -29 -23 .56 20 19 | 1952 257 21 313
| 1 0 1 13 12 68 .03 | 1382 924
mit 258| 0 0 1 3 -26 -7 -.36 12 9 | -267 155 24 187
| 0 0 1 23 24 16 .01 | 416 1099
ngs 217| 0 0 2 35 38 1 -.20 9 7 | 222664 -313867 2120 3869
| 0 0 1 33 21 12 .04 | 518694 474298
sio 245| -2 0 0 47 -87 12 -.21 20 18 | --- --- --- ---
| 0 1 1 28 36 15 .02 | --- ---
Table 1.1648.b GPS week : 1648 MJD: 55780.000-55786.000
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 | 15 13 13 20 26 22 16 |
2 | 5 4 5 4 5 4 4 |
3 | 7 6 5 4 4 4 5 |
4 | 4 3 3 3 4 4 4 |
5 | 4 4 4 4 4 4 4 |
6 | 5 5 5 6 8 8 6 |
7 | 4 4 4 4 4 3 4 |
8 | 4 3 3 3 4 4 3 |
9 | 4 4 4 4 4 4 4 |
10 | 3 3 3 3 4 3 4 |
11 | 4 4 4 3 4 4 4 |
12 | 5 5 4 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 5 5 5 6 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 4 5 5 0 0 4 |
18 | 5 5 5 5 5 5 5 |
19 | 4 4 4 4 4 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 5 5 4 5 5 5 5 |
22 | 4 4 3 4 4 4 4 |
23 | 4 4 4 5 5 5 4 |
24 | 3 3 3 3 3 3 4 |
25 | 5 5 5 6 5 4 4 |
26 | 5 4 4 4 4 4 4 |
27 | 4 4 4 4 7 7 8 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 4 5 5 5 5 |
30 | 0 0 0 0 11 19 9 |
31 | 4 4 4 4 4 4 4 |
32 | 3 4 3 4 3 3 3 |
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 2.1648.0 GPS week: 1648 Day: 0 MJD: 55780.000
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 250| 0 0 -1 18 -14 0 -.21 7 6 | -188 -491 13 74
| 34 31 |
emr 92| 0 1 -7 -60 -7 3 .42 18 18 | 1734 803 16 127
| 36 -25 |
esa 130| 0 0 2 -42 50 -11 .29 9 9 | 711 -2693 18 176
| 24 9 |
gfz 192| 0 0 2 -23 -19 -7 -.20 10 9 | 325 -93 25 153
| 22 52 |
grg 129| 1 0 5 12 22 4 .68 15 14 | 31 -369 47 206
| -14 60 |
igr n/a| 0 0 2 27 -6 -31 -.06 5 5 | 4455 637 19 90
| 24 38 |
jpl 132| 0 -1 -10 -10 -43 -14 .57 19 19 | -346 787 20 315
| 77 -6 |
mit 258| 0 0 2 -13 -13 26 -.35 14 11 | -211 -447 29 246
| 12 23 |
ngs 217| 0 1 2 46 29 -5 -.15 10 7 | 133004 -999999 2313 4224
| -28 -18 |
sio 245| -3 1 -2 61 -50 34 -.18 22 19 | --- --- --- ---
| -51 23 |
Table 2.1648.1 GPS week: 1648 Day: 1 MJD: 55781.000
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 250| 0 0 -1 12 -21 26 -.21 7 6 | -318 343 14 78
| 44 5 |
emr 92| 0 3 -9 -80 -10 -9 .37 18 18 | 2706 978 16 106
| 60 -31 |
esa 130| 0 1 2 -68 52 -11 .26 8 7 | -998 -169 18 169
| 60 -8 |
gfz 192| -1 -1 0 27 21 3 -.17 10 10 | -58 198 26 140
| -19 59 |
grg 129| 1 0 7 -8 5 18 .70 13 12 | -17 111 50 196
| 12 62 |
igr n/a| 0 0 0 -7 0 -49 -.03 5 5 | 5227 979 21 90
| 28 27 |
jpl 132| -1 1 -11 10 -38 -79 .55 21 20 | 605 1167 21 319
| -9 43 |
mit 258| 0 -1 1 31 -25 -10 -.38 12 10 | -9 255 29 186
| -9 4 |
ngs 217| 0 0 3 20 16 -5 -.19 9 8 | -215 276 2136 3833
| -2 18 |
sio 245| -2 1 -2 79 -90 -4 -.21 20 18 | --- --- --- ---
| -57 20 |
Table 2.1648.2 GPS week: 1648 Day: 2 MJD: 55782.000
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 250| 0 0 0 17 0 20 -.18 7 6 | -294 108 16 77
| -12 13 |
emr 92| 0 0 -6 -110 -7 16 .42 19 19 | 3496 341 23 132
| 50 -53 |
esa 130| -1 0 0 -41 23 3 .28 8 8 | -452 -632 21 159
| 56 19 |
gfz 192| -1 0 -1 42 -58 0 -.22 11 10 | -40 494 26 136
| -18 77 |
grg 129| 2 0 8 -6 16 0 .74 14 13 | 104 -187 44 218
| 24 11 |
igr n/a| 0 0 0 -9 -4 -45 -.07 5 5 | 6125 666 23 105
| 19 7 |
jpl 132| -1 0 -12 0 -29 -69 .58 19 19 | 1593 773 23 332
| 0 -17 |
mit 258| 1 0 1 10 -3 -3 -.36 10 9 | 193 -311 22 190
| -17 5 |
ngs 217| 1 0 1 1 39 -10 -.22 8 7 | 34522 -198348 2281 4013
| 43 -18 |
sio 245| -1 1 -1 48 -68 29 -.19 19 16 | --- --- --- ---
| -49 27 |
Table 2.1648.3 GPS week: 1648 Day: 3 MJD: 55783.000
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 250| 0 0 -1 8 5 9 -.19 8 7 | 36 -1211 17 92
| 39 -24 |
emr 92| -1 2 -6 -106 26 0 .45 19 19 | 4669 -1304 19 130
| 53 -63 |
esa 130| 0 0 0 -38 63 -20 .30 8 8 | 1868 -5086 19 160
| 66 -5 |
gfz 192| 0 0 -1 36 -86 2 -.24 12 11 | 644 -1026 25 131
| -13 26 |
grg 129| 1 0 5 -13 56 39 .70 14 13 | 787 -1348 43 225
| 7 -42 |
igr n/a| 1 0 1 -3 19 -14 -.06 5 5 | 7666 -1179 21 97
| 25 16 |
jpl 132| 0 0 -12 -19 -16 -37 .59 20 19 | 3134 -1131 21 308
| -4 44 |
mit 258| 0 0 2 23 -74 -4 -.36 10 7 | -119 -1365 27 210
| -7 34 |
ngs 217| 1 0 4 13 84 -1 -.20 8 6 | 1393712 -999999 1833 3621
| -26 -20 |
sio 245| -2 0 1 63 -151 14 -.20 18 17 | --- --- --- ---
| -40 53 |
Table 2.1648.4 GPS week: 1648 Day: 4 MJD: 55784.000
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 250| 0 0 -1 10 11 15 -.21 7 6 | -1296 1061 22 78
| 8 17 |
emr 92| -1 2 -1 -59 -19 19 .42 18 18 | 4712 1410 16 110
| 13 10 |
esa 130| 0 0 1 8 33 -32 .31 8 8 | -334 -662 24 150
| 39 13 |
gfz 192| -1 2 0 -30 -63 3 -.25 12 11 | 1 297 26 146
| -15 71 |
grg 129| 1 -1 2 -23 39 63 .85 17 17 | -411 1216 55 230
| 31 -10 |
igr n/a| 0 0 0 12 -1 0 -.06 5 5 | 7694 1178 22 112
| 26 51 |
jpl 132| 0 0 -10 9 -30 -51 .58 19 19 | 3219 1136 21 297
| 9 91 |
mit 258| 1 -1 1 -9 -9 -21 -.36 11 8 | -1094 2163 23 167
| 4 10 |
ngs 217| 1 1 2 34 27 -3 -.17 10 7 | -1287 1031 2754 4472
| 30 39 |
sio 245| -2 -1 1 21 -61 17 -.20 20 19 | --- --- --- ---
| -39 35 |
Table 2.1648.5 GPS week: 1648 Day: 5 MJD: 55785.000
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 250| 0 0 -2 -16 -4 25 -.24 7 6 | -39 -908 17 90
| 55 10 |
emr 92| 0 4 -2 -19 -5 9 .39 17 17 | 4639 31 18 102
| -35 -5 |
esa 130| 1 0 1 -51 25 3 .26 7 7 | -2868 341 18 145
| 61 17 |
gfz 192| -1 1 0 62 -35 -19 -.23 11 10 | 237 -244 22 135
| -19 49 |
grg 129| 0 0 7 -32 30 -15 .90 15 13 | -215 -53 41 222
| 57 34 |
igr n/a| 0 0 0 6 1 -35 -.06 5 5 | 7387 -342 19 110
| -2 39 |
jpl 132| -3 0 -10 5 -39 -37 .52 20 20 | 2848 -381 20 312
| -33 81 |
mit 258| 1 0 0 17 -16 -24 -.36 12 9 | -157 79 20 132
| -2 4 |
ngs 217| 0 0 0 30 34 17 -.26 11 8 | -18 -907 1572 3340
| -47 56 |
sio 245| 0 0 0 62 -66 0 -.24 21 18 | --- --- --- ---
| -41 27 |
Table 2.1648.6 GPS week: 1648 Day: 6 MJD: 55786.000
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 250| 0 0 -1 11 1 7 -.25 8 7 | -1198 1090 19 100
| 4 -14 |
emr 92| 0 3 -4 -24 -18 0 .41 18 18 | 4960 -450 19 125
| 7 5 |
esa 130| 0 0 3 -26 68 -18 .28 8 7 | -856 32 16 171
| 34 17 |
gfz 192| 1 0 0 -48 -61 -17 -.22 10 9 | 68 -263 26 147
| -30 63 |
grg 129| 0 0 7 -11 29 -36 .76 14 13 | -305 296 42 249
| 12 25 |
igr n/a| 0 0 -1 26 8 -13 -.06 4 4 | 7163 -567 24 100
| -14 49 |
jpl 132| -2 0 -8 20 -9 122 .54 20 19 | 2616 -546 22 312
| 14 -57 |
mit 258| 0 -1 0 -33 -42 -14 -.34 12 10 | -474 715 22 179
| 10 -15 |
ngs 217| -1 0 0 105 38 22 -.21 10 7 | -1066 877 1955 3582
| -75 76 |
sio 245| -1 0 0 -1 -121 -2 -.23 21 17 | --- --- --- ---
| -13 38 |
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 3.1648.0 GPS week: 1648 Day: 0 MJD: 55780.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 20 --- 22 --- --- 19 --- 23 --- --- 15 | 63 --- 48 --- --- 56 --- 47 --- --- 51
2 | 5 19 10 6 12 4 26 11 6 28 4 | 25 36 26 22 33 23 40 24 23 27 24
3E | 15 17 10 13 15 7 20 35 17 36 6 | 82 93 89 82 89 84 96 87 81 80 84
4 | 6 15 9 8 13 4 14 11 8 12 3 | 33 35 38 38 39 33 35 36 38 37 36
5 | 5 14 11 8 13 5 18 16 8 23 4 | 30 30 34 34 34 31 29 29 32 29 30
6E | 10 17 10 12 15 6 19 20 13 31 5 | 105 96 100 105 98 99 92 102 102 104 101
7 | 4 21 7 14 14 5 18 10 12 18 4 | 27 34 28 30 33 28 34 25 33 24 27
8 | 7 15 8 10 10 3 9 13 14 15 3 | 22 26 21 23 22 23 23 25 26 23 21
9 | 7 15 10 5 11 4 11 12 8 29 4 | 21 27 17 20 21 20 21 21 21 30 19
10 | 4 11 8 5 14 5 9 6 11 23 3 | 34 36 37 36 40 33 32 34 37 30 35
11 | 8 11 5 8 17 3 16 6 9 14 3 | 22 33 28 26 43 25 34 24 27 25 25
12 | 6 21 9 13 19 4 23 11 6 22 4 | 20 30 20 22 29 18 32 23 20 23 19
13E | 5 20 10 8 13 4 15 10 9 17 3 | 47 44 46 48 53 47 46 43 47 43 46
14 | 5 12 8 8 17 7 22 12 10 16 4 | 20 24 23 22 28 19 22 21 21 17 19
15 | 5 23 9 8 14 5 21 8 9 18 4 | 22 26 24 24 29 20 25 22 23 22 21
16 | 6 21 12 11 17 6 23 8 9 26 4 | 20 29 25 23 26 20 32 19 18 18 19
17E | 5 23 9 9 17 5 23 14 11 13 4 | 28 30 21 25 26 25 24 23 23 24 27
18 | 6 19 9 12 11 5 21 24 10 32 5 | 23 27 29 31 31 24 26 29 23 29 23
19E | 6 20 7 12 13 4 22 11 7 17 4 | 26 36 31 30 35 28 31 28 26 28 27
20 | 5 17 9 10 11 4 16 14 7 24 4 | 24 27 29 29 28 27 24 25 27 21 25
21 | 6 23 8 6 15 3 28 13 9 24 4 | 27 41 29 25 34 26 42 23 25 25 26
22 | 6 18 9 7 9 4 21 13 9 21 4 | 27 27 30 30 31 28 28 33 30 22 27
23 | 6 24 9 8 17 4 18 10 8 17 4 | 19 27 24 19 30 19 26 18 22 18 19
24 | 6 11 6 7 13 4 13 9 8 12 3 | 29 32 34 31 33 30 31 30 31 32 30
25 | 6 13 8 24 13 5 23 12 11 15 5 | 24 30 27 34 33 25 44 24 26 24 26
26E | 11 16 12 9 19 5 15 13 12 34 5 | 48 57 54 52 59 52 56 49 56 47 52
27 | 8 16 9 7 13 5 11 13 9 26 4 | 25 32 25 25 17 26 14 23 12 24 23
28 | 6 18 9 7 17 5 20 10 12 20 4 | 19 28 24 22 27 19 29 23 26 19 20
29E | 7 18 11 7 23 6 26 14 10 14 4 | 45 47 52 47 49 47 48 48 46 45 46
X30 | 3 --- --- --- --- --- --- --- --- --- 0 | 129 --- --- --- --- --- --- --- --- --- 129
31 | 6 20 10 11 20 6 18 12 10 16 4 | 25 30 26 26 34 24 30 24 24 24 24
32 | 4 13 6 9 10 5 15 7 5 15 3 | 22 24 26 27 28 24 27 24 26 22 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 9 10 15 5 19 14 10 22 |T 35 36 34 33 37 32 35 32 32 31 35
WRMS | 6 18 9 9 13 5 19 11 7 19 |NE 30 30 28 26 30 25 29 26 25 24 29
MEDI | 6 17 9 8 14 5 18 12 9 18 |MD 25 30 28 27 33 26 31 25 26 24 26
Table 3.1648.1 GPS week: 1648 Day: 1 MJD: 55781.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 20 --- 25 --- --- 16 --- 18 --- 34 13 | 62 --- 61 --- --- 61 --- 71 --- 4 64
2 | 4 22 7 6 12 4 25 12 7 26 4 | 17 32 23 18 30 17 33 18 15 18 18
3E | 12 17 10 11 14 8 22 26 17 34 6 | 70 82 76 70 83 72 87 71 73 69 72
4 | 5 14 7 6 9 4 15 7 9 11 3 | 26 28 31 25 29 27 28 29 29 28 27
5 | 4 14 6 8 11 7 19 12 6 22 3 | 18 19 23 18 22 17 19 19 18 19 17
6E | 10 16 9 11 13 8 20 20 10 31 5 | 107 103 104 106 97 104 97 111 102 102 104
7 | 6 18 6 8 14 5 23 9 7 13 3 | 16 27 21 16 26 14 27 19 18 18 17
8 | 6 12 5 8 10 3 11 9 9 13 3 | 23 26 23 21 22 21 21 25 26 23 22
9 | 6 14 8 7 10 4 13 10 9 24 3 | 15 21 14 18 20 14 21 19 17 28 15
10 | 4 12 7 6 13 5 13 7 9 20 3 | 20 19 22 19 23 18 18 22 19 20 19
11 | 6 14 7 7 18 6 18 8 7 15 3 | 20 31 23 19 40 19 31 19 18 20 21
12 | 6 21 8 16 17 5 26 12 8 21 4 | 11 27 15 15 26 10 29 19 14 18 12
13 | 6 21 7 9 16 5 21 11 5 12 3 | 32 33 32 30 41 29 34 26 29 28 30
14 | 7 18 7 9 16 4 23 9 8 13 4 | 10 19 15 14 25 10 20 12 14 11 11
15 | 6 25 10 10 17 4 21 7 7 19 4 | 14 24 21 19 30 13 21 17 15 20 15
16 | 7 21 8 13 14 5 25 9 7 23 4 | 13 26 14 13 22 11 28 15 10 13 12
17E | 6 17 10 8 12 5 23 10 6 13 3 | 24 23 21 23 23 21 22 23 26 23 23
18 | 9 19 8 13 7 5 22 23 7 30 5 | 15 25 18 20 21 14 25 25 15 21 15
19E | 6 18 6 9 12 5 22 9 7 18 3 | 18 32 22 23 32 18 26 19 18 21 19
20 | 5 15 9 12 12 6 18 11 8 24 4 | 15 22 22 23 22 19 22 18 19 14 18
21 | 6 23 7 9 15 4 28 9 9 22 4 | 18 35 22 18 34 20 39 16 17 16 19
22 | 5 18 7 7 9 3 20 9 8 19 3 | 15 22 18 20 19 15 21 20 17 13 15
23 | 5 25 7 9 16 5 20 9 5 13 4 | 11 24 16 11 28 10 19 12 12 11 12
24 | 6 15 7 8 11 6 16 9 8 12 3 | 31 34 33 32 33 29 33 27 29 31 30
25 | 6 12 6 22 15 5 28 8 9 15 4 | 15 24 20 25 27 15 42 15 13 19 16
26 | 13 17 6 10 13 7 15 7 9 28 4 | 29 32 32 29 34 30 31 28 28 40 29
27 | 8 13 9 9 11 3 12 9 9 20 3 | 23 28 25 26 20 26 16 27 9 27 25
28 | 7 17 8 9 15 7 22 9 9 17 4 | 11 25 19 17 23 13 26 19 16 14 14
29E | 8 21 7 8 16 4 29 13 9 12 4 | 40 36 43 42 49 39 40 39 38 38 39
X30 | 4 --- --- --- --- --- --- --- --- --- 0 | 53 --- --- --- --- --- --- --- --- --- 54
31 | 8 17 8 12 16 5 15 14 13 15 4 | 15 26 16 19 27 14 22 16 19 16 15
32 | 6 12 7 13 12 7 16 8 9 14 3 | 12 16 17 19 21 12 19 15 13 13 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 8 10 13 5 21 12 9 20 |T 25 30 27 25 31 24 30 26 23 24 26
WRMS | 6 18 7 10 12 5 20 10 8 18 |NE 19 25 22 19 25 18 25 21 17 18 20
MEDI | 6 17 7 9 13 5 20 9 8 19 |MD 18 26 22 19 26 18 26 19 18 20 18
Table 3.1648.2 GPS week: 1648 Day: 2 MJD: 55782.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 19 --- 18 --- --- 29 --- 18 --- --- 13 | 62 --- 78 --- --- 68 --- 71 --- --- 67
2 | 6 21 12 10 15 4 26 13 7 22 4 | 18 31 22 17 28 17 35 15 18 20 17
3E | 12 19 8 11 12 6 21 18 10 27 5 | 74 86 81 74 85 78 90 74 78 69 77
4 | 5 16 9 10 11 3 16 8 6 13 3 | 21 25 24 26 23 23 23 25 26 25 23
5 | 5 13 8 10 11 6 20 12 8 22 3 | 20 21 20 24 25 21 22 19 25 21 19
6E | 12 18 9 11 15 5 19 18 10 31 5 | 98 92 93 100 85 95 87 103 96 89 95
7 | 4 21 7 8 12 2 18 8 7 12 3 | 18 27 24 18 29 18 27 19 24 18 19
8 | 6 19 8 9 11 3 9 6 5 13 3 | 24 32 23 26 24 25 27 27 27 30 24
9 | 9 16 7 9 10 5 16 10 6 21 3 | 18 26 21 24 22 19 24 25 21 33 20
10 | 3 16 6 8 13 4 10 6 8 18 3 | 23 26 25 26 29 23 23 26 28 23 24
11 | 8 14 6 8 18 4 17 8 5 14 3 | 15 30 22 17 38 17 26 17 18 18 18
12 | 7 22 8 15 15 5 22 9 7 18 4 | 15 30 18 19 26 14 26 17 12 17 14
13 | 5 24 6 9 21 3 15 6 8 9 3 | 22 29 26 23 44 22 27 22 22 21 23
14 | 6 15 6 8 17 4 19 8 7 12 3 | 13 22 19 18 30 14 20 14 12 16 14
15 | 7 28 8 12 17 5 23 15 10 17 4 | 15 25 18 19 28 13 23 18 17 20 15
16 | 6 24 7 14 14 6 25 7 7 23 4 | 12 28 16 16 21 12 28 14 15 18 13
17E | 8 22 11 10 19 7 22 11 11 23 4 | 24 25 21 21 29 23 21 23 23 30 24
18 | 6 18 7 16 8 6 19 14 8 30 4 | 16 27 22 24 25 18 26 20 15 22 17
19E | 5 19 8 8 14 4 22 9 5 14 3 | 20 32 27 24 32 23 29 22 23 24 23
20 | 6 15 10 14 12 4 16 12 8 25 4 | 18 25 27 28 25 21 24 21 24 17 21
21 | 6 23 8 11 12 5 27 7 7 22 4 | 21 37 31 25 36 22 38 19 20 24 23
22 | 5 15 6 8 8 4 15 8 7 19 3 | 18 23 19 21 24 18 22 22 18 18 17
23 | 5 26 6 11 17 4 20 10 9 12 4 | 14 28 18 15 30 13 23 15 15 13 14
24 | 5 15 7 7 10 2 16 8 5 11 3 | 22 28 27 23 27 22 23 22 25 25 23
25 | 6 15 7 23 15 4 25 7 7 13 4 | 17 29 25 30 32 19 42 19 19 20 20
26 | 6 17 6 11 12 6 12 9 7 24 3 | 24 29 24 28 30 23 29 22 23 31 23
27 | 10 16 8 11 12 5 16 9 6 12 3 | 28 34 31 33 23 29 22 31 14 23 29
28 | 5 20 7 10 14 4 18 8 8 18 3 | 12 28 16 15 23 12 26 17 14 15 13
29E | 8 20 7 11 12 5 31 13 7 12 4 | 40 45 48 45 46 43 44 44 40 43 42
X30 | 3 --- --- --- --- --- --- --- --- --- 0 | 45 --- --- --- --- --- --- --- --- --- 45
31 | 5 19 7 9 15 4 14 11 9 12 3 | 21 29 24 20 29 18 24 18 20 21 19
32 | 5 12 8 11 10 7 13 7 9 14 3 | 14 21 20 19 25 16 22 18 18 16 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 8 11 14 5 19 10 8 19 |T 25 32 29 27 32 25 30 27 25 26 26
WRMS | 6 19 8 10 13 5 19 9 7 16 |NE 20 27 24 21 27 20 25 22 19 20 21
MEDI | 6 18 7 10 12 4 18 9 7 17 |MD 20 28 24 23 28 21 26 21 20 21 20
Table 3.1648.3 GPS week: 1648 Day: 3 MJD: 55783.000
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 | 32 --- 28 --- --- 26 --- 21 --- --- 20 | 68 --- 73 --- --- 72 --- 80 --- --- 70
2 | 7 20 9 7 12 5 26 10 6 22 4 | 20 33 24 20 31 19 38 18 17 20 20
3E | 9 16 6 9 14 4 19 11 10 24 4 | 77 88 84 77 90 79 95 76 77 68 79
4 | 6 12 8 7 9 4 12 4 7 11 2 | 23 25 29 27 29 24 24 28 24 26 25
5 | 6 13 8 11 9 6 19 10 5 23 3 | 20 22 27 27 28 24 25 23 23 24 22
6E | 13 18 9 13 16 6 19 21 11 24 5 | 125 123 123 124 116 125 115 133 125 126 124
7 | 5 18 7 9 15 4 18 6 5 14 3 | 16 27 19 19 27 17 27 15 19 17 16
8 | 10 14 8 9 8 6 10 8 6 12 3 | 17 21 21 15 19 16 18 16 18 15 15
9 | 10 17 11 8 8 9 13 8 12 16 4 | 16 22 16 18 17 18 21 18 21 20 15
10 | 5 13 8 10 13 4 14 5 8 18 3 | 23 25 25 27 31 24 22 28 25 27 24
11 | 7 14 6 8 17 4 15 6 5 15 3 | 18 33 26 20 38 22 30 22 23 22 22
12 | 8 22 8 15 17 6 25 8 10 19 4 | 13 28 16 18 24 12 30 14 13 15 11
13 | 7 20 7 9 19 4 17 7 7 11 3 | 16 22 22 17 38 18 26 17 20 19 18
14 | 8 15 6 10 15 5 18 5 7 12 3 | 13 24 21 17 26 16 21 16 17 16 15
15 | 10 27 7 10 16 5 23 14 10 18 4 | 14 25 18 18 25 15 24 18 19 20 14
16 | 7 26 6 16 17 6 25 10 12 22 5 | 13 29 20 18 22 16 30 13 20 15 14
17E | 10 18 10 10 11 6 24 22 7 11 5 | 28 27 29 27 32 25 29 38 28 32 28
18 | 7 20 7 12 10 5 19 12 7 30 4 | 17 26 25 22 24 20 27 18 20 20 18
19E | 5 25 5 11 13 5 26 9 6 12 4 | 20 38 27 23 29 24 31 25 25 24 23
20 | 5 15 8 14 11 5 18 8 7 23 4 | 23 27 26 28 28 24 26 22 22 18 22
21 | 5 30 11 10 15 4 28 9 6 22 5 | 21 42 31 22 35 23 41 19 20 18 22
22 | 5 17 6 10 9 4 17 9 10 21 3 | 19 25 22 24 23 21 25 24 22 22 20
23 | 7 27 7 11 15 4 20 11 9 15 4 | 12 27 19 14 29 15 24 16 16 15 14
24 | 5 16 7 10 14 9 13 7 9 11 3 | 28 34 35 30 33 30 31 29 30 32 30
25 | 6 14 9 33 18 4 24 7 10 16 5 | 16 25 22 35 31 18 40 18 20 20 18
26 | 9 20 11 10 9 6 11 8 7 23 4 | 20 31 21 22 25 18 27 18 21 27 19
X27 | 11 19 9 9 7 8 --- 8 --- 13 4 | 16 24 19 16 19 18 --- 17 --- 18 15
28 | 8 21 8 11 15 5 20 8 6 20 4 | 12 27 16 15 24 12 27 14 12 18 11
29E | 12 18 6 10 17 5 29 9 8 18 4 | 62 63 69 65 67 65 65 64 62 64 64
X30 | 3 --- --- --- --- --- --- --- --- --- 0 | 21 --- --- --- --- --- --- --- --- --- 22
31 | 6 19 10 9 17 5 16 7 9 14 3 | 19 27 21 24 30 20 25 18 23 21 19
32 | 6 8 8 9 23 6 14 6 7 13 3 | 14 20 21 18 31 18 21 18 19 15 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 12 14 5 20 10 8 18 |T 26 33 31 28 34 28 33 28 27 27 27
WRMS | 7 19 8 11 13 5 19 7 6 17 |NE 19 26 24 21 27 21 27 21 20 19 20
MEDI | 7 18 8 10 14 5 19 8 7 16 |MD 19 27 22 22 29 20 27 18 21 20 19
Table 3.1648.4 GPS week: 1648 Day: 4 MJD: 55784.000
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 | 41 --- 41 --- --- 25 --- 21 --- --- 26 | 99 --- 95 --- --- 81 --- 90 --- --- 96
2 | 6 23 11 10 15 5 22 7 10 22 4 | 16 30 20 16 30 16 30 15 16 15 16
3E | 8 18 7 8 16 6 17 9 12 27 4 | 75 81 81 72 92 75 88 73 75 64 76
4 | 7 14 10 6 14 3 11 9 9 13 3 | 17 19 22 22 22 18 18 21 21 21 19
5 | 5 14 7 12 10 4 17 9 9 25 3 | 16 21 23 18 24 18 19 20 18 23 18
6E | 19 18 12 13 34 9 20 37 20 32 8 | 126 117 120 124 121 119 112 117 121 110 119
7 | 4 21 8 11 12 4 19 6 8 15 3 | 14 28 20 19 28 17 25 15 18 15 17
8 | 6 11 7 10 16 4 10 11 6 14 3 | 16 22 17 17 22 17 20 18 16 14 15
9 | 7 16 9 10 14 6 14 11 9 17 3 | 9 17 14 14 19 10 20 15 16 14 11
10 | 6 15 10 9 14 5 12 10 8 20 3 | 18 28 23 23 26 19 15 21 19 21 19
11 | 7 12 7 9 20 4 16 7 6 18 3 | 11 28 22 17 39 16 26 14 17 15 16
12 | 11 24 11 16 18 5 23 12 10 18 5 | 18 31 17 18 27 13 29 16 15 16 15
13 | 7 21 8 13 25 6 20 5 8 12 4 | 13 23 21 20 44 18 25 15 19 16 17
14 | 6 14 10 9 21 3 20 7 11 17 4 | 9 19 16 16 33 11 19 13 16 14 11
15 | 8 29 7 8 21 4 23 18 9 22 5 | 13 26 18 16 36 14 23 25 13 24 16
16 | 7 25 8 15 14 6 26 9 9 23 4 | 9 29 15 14 23 11 30 14 15 14 10
X17E | 3 --- --- --- --- 70 --- --- --- --- 0 | 12 --- --- --- --- 156 --- --- --- --- 13
18 | 6 16 7 16 10 5 18 11 8 30 4 | 17 25 20 25 26 18 26 20 18 20 18
19E | 4 19 7 12 15 5 25 12 8 15 4 | 19 29 24 20 30 22 29 24 21 24 21
20 | 5 12 6 10 12 4 18 8 7 23 3 | 17 24 27 22 25 22 24 16 22 13 19
21 | 6 21 8 12 16 4 28 9 7 20 4 | 16 34 22 20 35 18 35 15 16 11 17
22 | 6 14 6 12 10 4 15 9 9 25 3 | 19 22 20 26 24 21 24 22 21 20 19
23 | 6 26 8 12 19 5 22 11 8 15 4 | 15 29 21 13 34 16 27 15 19 13 16
24 | 4 14 7 9 14 4 15 6 7 16 3 | 18 26 26 23 26 21 22 18 22 22 20
25 | 5 16 5 20 16 5 23 6 13 18 4 | 16 27 23 29 30 17 38 17 15 18 18
26 | 6 16 8 7 12 4 10 10 12 23 3 | 16 27 20 18 29 15 25 21 15 26 18
X27 | 12 20 15 17 --- 12 --- 8 --- --- 7 | 9 22 19 23 --- 12 --- 17 --- --- 13
28 | 6 16 8 9 16 5 19 7 10 20 4 | 13 26 21 15 24 14 25 16 16 17 15
29E | 7 21 8 11 17 6 29 8 12 13 4 | 47 47 51 50 52 47 48 47 46 43 47
X30 | 11 --- 22 --- --- 27 --- 12 --- --- 11 | 25 --- 26 --- --- 19 --- 9 --- --- 24
31 | 4 23 7 11 14 4 17 7 15 13 4 | 15 28 18 17 30 15 25 14 18 15 15
32 | 5 10 6 10 11 4 16 7 9 15 3 | 11 20 19 15 25 14 20 15 15 12 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 8 12 17 5 19 11 10 20 |T 23 31 29 25 34 28 30 25 24 23 24
WRMS | 6 18 8 11 17 5 19 8 7 19 |NE 18 25 23 19 27 18 24 19 17 16 19
MEDI | 6 16 8 11 15 5 18 9 9 18 |MD 16 27 21 19 28 17 25 17 18 16 17
Table 3.1648.5 GPS week: 1648 Day: 5 MJD: 55785.000
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 | 26 --- 40 --- --- 17 --- 23 --- --- 22 | 63 --- 80 --- --- 70 --- 68 --- --- 67
2 | 5 20 7 8 14 6 24 6 7 24 4 | 14 27 17 15 30 14 28 15 13 18 15
3E | 6 16 4 13 10 4 18 7 10 34 4 | 71 79 79 72 87 74 88 73 73 63 74
4 | 7 15 7 7 13 5 13 13 11 12 3 | 20 21 21 21 25 19 21 24 22 20 20
5 | 7 15 7 10 10 5 20 12 10 27 4 | 16 23 21 23 26 18 26 18 19 23 18
6E | 16 17 9 18 15 7 22 36 22 38 7 | 121 116 118 120 110 116 108 131 116 122 118
7 | 3 18 7 5 12 5 17 5 6 15 3 | 14 26 19 16 28 15 26 15 15 17 16
8 | 7 15 7 7 19 5 13 12 9 13 3 | 18 22 17 17 22 14 20 23 18 19 17
9 | 10 15 10 13 18 3 17 10 8 17 4 | 16 22 20 24 23 17 24 21 20 18 17
10 | 4 14 6 10 13 4 13 7 7 20 3 | 16 22 20 23 26 18 21 21 19 20 19
11 | 7 13 6 8 20 4 15 8 10 18 3 | 13 28 20 16 41 16 30 17 15 16 17
12 | 6 23 8 16 10 5 28 10 12 20 4 | 10 30 16 18 26 11 30 14 15 12 12
13 | 6 19 6 10 25 6 19 6 10 11 4 | 13 23 19 18 47 16 27 14 16 16 17
14 | 7 13 8 8 21 4 21 7 12 15 4 | 10 18 13 11 34 12 21 16 20 16 12
15 | 7 26 9 9 20 5 28 20 12 18 5 | 16 26 19 16 35 14 27 22 17 20 16
16 | 7 22 8 15 11 7 24 12 11 22 4 | 10 28 16 14 22 11 28 13 13 15 11
X17E | 4 --- --- --- --- 24 --- --- --- --- 0 | 16 --- --- --- --- 21 --- --- --- --- 15
18 | 6 19 9 9 8 4 19 15 10 29 4 | 14 25 20 16 25 14 25 19 22 18 15
X19E | 7 20 6 9 20 10 --- 17 13 16 4 | 24 29 25 25 38 26 --- 29 27 23 25
20 | 6 11 6 12 10 3 14 11 6 23 3 | 16 23 21 22 24 17 24 14 15 12 17
21 | 7 24 9 9 18 4 27 11 7 18 4 | 16 33 22 17 41 18 37 18 19 11 19
22 | 7 13 7 9 9 4 16 7 12 24 3 | 15 21 18 21 22 16 23 20 23 21 16
23 | 6 20 8 11 20 4 22 14 14 16 4 | 12 24 17 12 37 12 25 16 17 14 13
24 | 4 12 6 7 14 4 11 8 9 18 3 | 21 27 24 21 27 19 24 19 18 23 21
25 | 6 12 6 13 10 5 23 7 14 16 4 | 13 24 20 24 29 15 40 16 21 15 17
26 | 6 16 6 9 14 4 13 10 10 21 3 | 23 31 24 24 33 22 31 26 22 29 24
X27 | 11 19 15 10 --- 5 --- 11 --- --- 6 | 19 26 24 23 --- 22 --- 22 --- --- 21
28 | 6 22 7 7 15 6 20 9 8 24 4 | 11 27 17 14 23 12 27 14 11 20 13
29E | 10 18 8 10 21 3 31 13 9 13 5 | 31 37 38 37 34 33 34 37 32 33 33
X30 | 26 --- 46 --- 20 27 --- 20 --- --- 18 | 26 --- 46 --- 16 14 --- 8 --- --- 39
31 | 6 20 8 9 13 6 18 6 11 12 3 | 17 30 21 21 30 17 25 18 22 20 18
32 | 7 12 5 12 9 4 11 8 10 16 3 | 14 18 18 16 24 13 21 15 12 14 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 17 7 11 15 5 20 12 11 21 |T 22 30 28 24 33 23 31 25 24 23 24
WRMS | 6 17 7 10 13 5 20 9 8 18 |NE 17 24 22 18 27 17 26 19 17 17 19
MEDI | 7 17 7 9 14 5 19 10 10 18 |MD 16 26 20 21 28 16 26 18 19 18 17
Table 3.1648.6 GPS week: 1648 Day: 6 MJD: 55786.000
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 | 26 --- 21 --- --- 24 --- 15 --- --- 15 | 69 --- 64 --- --- 65 --- 67 --- --- 65
2 | 6 20 8 6 14 5 24 7 7 26 4 | 25 36 31 25 36 26 38 26 28 25 26
3E | 8 15 6 8 13 4 16 10 8 42 4 | 90 98 96 89 102 92 102 90 91 84 92
4 | 8 12 7 7 8 3 15 16 11 11 3 | 27 26 32 28 31 28 30 36 30 29 28
5 | 7 14 9 10 8 4 20 9 9 29 4 | 29 31 39 34 37 32 33 32 32 35 32
6E | 13 18 10 11 16 6 18 30 16 28 6 | 102 95 98 103 89 101 91 109 102 95 99
7 | 6 17 8 6 17 4 18 8 7 11 3 | 21 31 24 22 33 23 27 22 24 20 22
8 | 7 15 7 8 14 4 11 8 7 15 3 | 21 24 22 17 23 19 21 20 20 19 19
9 | 8 17 7 9 15 4 13 10 9 20 4 | 18 27 22 23 23 18 27 25 21 19 20
10 | 6 12 6 7 15 4 16 9 9 21 3 | 28 32 36 34 42 30 28 34 31 31 31
11 | 9 12 5 11 19 4 18 7 10 16 4 | 21 33 27 24 42 25 32 23 31 22 24
12 | 8 24 9 15 11 4 26 14 10 22 5 | 22 34 22 25 30 19 37 19 18 23 20
13 | 6 16 7 6 22 4 20 9 9 9 3 | 22 27 28 23 47 24 30 22 26 22 25
14 | 7 17 7 9 17 4 16 10 11 18 4 | 17 26 23 21 34 20 25 21 21 21 19
15 | 8 26 8 7 14 5 25 14 12 18 4 | 20 30 24 23 33 20 30 23 23 25 21
16 | 9 23 10 12 14 6 23 11 9 26 5 | 18 31 19 18 26 17 33 20 19 21 17
17E | 7 20 7 7 15 5 26 10 9 13 4 | 12 19 10 7 14 17 19 8 7 9 12
18 | 7 22 8 20 8 4 18 15 10 31 5 | 24 33 31 34 34 25 31 27 28 27 26
19E | 8 19 7 8 15 3 30 20 7 13 4 | 31 36 35 32 45 31 32 36 28 34 31
20 | 7 12 8 9 11 3 14 10 6 22 3 | 26 29 35 30 33 29 28 24 28 21 27
21 | 6 25 9 10 15 4 27 8 11 18 4 | 25 41 31 26 46 26 41 27 25 21 27
22 | 5 16 6 9 9 4 20 10 7 23 3 | 27 31 30 31 32 28 31 31 30 28 28
23 | 6 21 8 9 17 4 21 10 7 15 4 | 20 27 25 20 35 21 29 21 22 19 20
24 | 7 13 4 9 15 3 17 8 10 15 3 | 31 36 36 35 36 34 35 32 39 33 33
25 | 7 14 5 11 8 7 24 7 10 19 3 | 24 28 27 28 36 24 45 22 22 22 24
26 | 8 17 11 7 12 5 13 9 11 23 4 | 28 36 29 29 35 26 36 30 28 32 28
X27 | 13 20 18 12 --- 13 --- 11 --- --- 7 | 17 29 27 22 --- 18 --- 25 --- --- 21
28 | 9 20 8 8 14 4 21 8 12 23 4 | 19 30 24 19 30 19 30 19 17 23 20
29E | 9 19 6 11 15 3 29 13 12 16 4 | 61 63 66 62 69 63 65 63 64 60 63
X30 | 17 --- 18 --- 13 10 --- 11 --- --- 9 | 33 --- 20 --- 13 15 --- 10 --- --- 34
31 | 6 27 7 9 14 6 17 8 11 12 4 | 23 36 24 25 32 22 29 22 24 24 23
32 | 9 11 6 7 10 3 13 9 5 17 3 | 19 25 27 24 30 23 24 22 23 20 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 10 14 4 20 12 10 21 |T 30 36 33 31 38 30 36 31 31 29 31
WRMS | 7 18 7 9 13 4 19 10 7 17 |NE 24 30 28 25 32 25 31 26 25 24 25
MEDI | 7 17 7 9 14 4 18 10 9 18 |MD 24 31 27 25 34 24 31 24 26 23 25
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 4.1648 GPS week: 1648 MJD: 55780.0-55786.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3044 |U 15 11 34 |U 7 8 27 |U 9 9 18 |
emr | emr 2844 |U 18 12 37 |U 8 8 30 | 12 11 24 |
esa | esa 2989 | 15 11 36 |U 6 7 25 | 10 13 18 |
gfz | gfz 2843 |U 17 14 38 |U 9 10 43 |U 11 11 23 |
grg | grg 2838 | 17 13 37 |U 7 8 27 | 9 14 18 |
igr | igr 2946 | 15 12 37 | 6 7 22 | 9 12 17 |
igs | igs 2925 | 15 11 35 | 6 7 25 | 10 11 20 |
jpl | jpl 2773 |U 16 11 38 |U 7 7 30 |U 10 9 22 |
mit | mit 2989 |U 13 10 34 |U 8 8 36 |U 23 22 72 |
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 5.1648.0 GPS week: 1648 Day: 0 MJD: 55780.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 9 7 24 | 11 10 50 | 7 5 17 |
emr | emr 2872 | 13 8 27 | 9 7 46 | 8 6 22 |
esa | esa 2976 | 7 7 21 | 9 8 36 | 8 7 17 |
gfz | gfz 2868 | 12 8 21 | 7 6 39 | 8 7 18 |
grg | grg 2880 | 12 8 24 | 11 12 52 | 9 7 20 |
igr | igr 2945 | 8 6 21 | 5 6 19 | 7 6 15 |
igs | igs 2896 | 8 7 23 | 5 6 23 | 7 6 18 |
jpl | jpl 2865 | 15 10 25 | 10 7 45 | 8 6 20 |
mit | mit 2976 | 7 6 20 | 12 11 55 | 12 9 25 |
Table 5.1648.1 GPS week: 1648 Day: 1 MJD: 55781.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 8 7 21 | 7 6 24 | ---- ---- ---- |
emr | emr 2872 | 15 10 35 | 6 6 26 | ---- ---- ---- |
esa | esa 2976 | 11 9 34 | 6 5 19 | 10 11 20 |
gfz | gfz 2871 | 13 9 33 | 8 6 35 | ---- ---- ---- |
grg | grg 2880 | 13 10 36 | 6 7 19 | 11 12 21 |
igr | igr 2923 | 15 10 40 | 6 5 19 | ---- ---- ---- |
igs | igs 2923 | 10 8 27 | 5 5 23 | ---- ---- ---- |
jpl | jpl 2870 | 13 10 41 | 7 6 28 | 11 8 25 |
mit | mit 2976 | 10 8 31 | 7 6 33 | 11 16 25 |
Table 5.1648.2 GPS week: 1648 Day: 2 MJD: 55782.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 8 8 23 | 4 7 19 | 10 10 16 |
emr | emr 2872 | 12 8 28 | 7 6 25 | 9 8 18 |
esa | esa 2976 | 9 7 19 | 3 5 17 | 10 8 15 |
gfz | gfz 2872 | 9 6 20 | 7 7 28 | 9 8 15 |
grg | grg 2880 | 10 6 20 | 4 6 16 | 11 9 15 |
igr | igr 2958 | 9 7 20 | 4 6 14 | 9 8 18 |
igs | igs 2872 | 9 7 23 | 4 6 17 | 10 8 16 |
jpl | jpl 2861 | 11 7 26 | 5 4 23 | 9 7 17 |
mit | mit 2976 | 10 9 22 | 5 7 20 | 68 49 305 |
Table 5.1648.3 GPS week: 1648 Day: 3 MJD: 55783.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 17 13 43 | 9 8 23 | 9 8 15 |
emr | emr 2872 | 19 14 36 | 11 9 32 | 13 8 21 |
esa | esa 2976 | 18 15 44 | 10 8 24 | 9 8 14 |
gfz | gfz 2872 | 25 22 70 | 15 13 55 | 12 9 19 |
grg | grg 2880 | 27 22 65 | 9 11 24 | 10 8 17 |
igr | igr 2970 | 14 12 32 | 10 7 24 | 9 7 13 |
igs | igs 2941 | 18 14 45 | 10 7 23 | 10 8 14 |
jpl | jpl 2775 | 19 10 38 | 11 14 32 | 9 7 17 |
mit | mit 2976 | 21 15 57 | 14 9 53 | 15 16 38 |
Table 5.1648.4 GPS week: 1648 Day: 4 MJD: 55784.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 17 11 47 | 6 7 26 | 11 12 19 |
emr | emr 2776 | 13 8 31 | 7 9 35 | 18 19 40 |
esa | esa 2976 | 18 11 48 | 5 7 28 | 14 15 24 |
gfz | gfz 2775 | 16 16 35 | 6 8 39 | 20 20 35 |
grg | grg 2688 | 12 10 29 | 6 8 25 | 16 18 35 |
igr | igr 2943 | 16 13 56 | 5 9 27 | 14 16 25 |
igs | igs 2924 | 18 11 46 | 6 10 33 | 15 16 35 |
jpl | jpl 2680 | 14 9 31 | 6 7 32 | 14 16 37 |
mit | mit 2976 | 17 10 41 | 6 11 33 | 23 16 26 |
Table 5.1648.5 GPS week: 1648 Day: 5 MJD: 55785.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 | 33 23 51 | 4 8 20 | 10 12 29 |
emr | emr 2776 | 38 27 65 | 7 10 20 | ---- ---- ---- |
esa | esa 2976 | 25 17 48 | 4 7 25 | 10 9 20 |
gfz | gfz 2776 | 29 21 46 | 7 7 34 | 6 9 23 |
grg | grg 2784 | 29 21 48 | 5 7 23 | 0 0 0 |
igr | igr 2921 | 29 20 47 | 4 7 22 | ---- ---- ---- |
igs | igs 2905 | 28 19 44 | 5 7 23 | ---- ---- ---- |
jpl | jpl 2584 | 27 18 57 | 6 7 22 | ---- ---- ---- |
mit | mit 2976 | 12 9 26 | 5 6 31 | ---- ---- ---- |
Table 5.1648.6 GPS week: 1648 Day: 6 MJD: 55786.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 12 11 32 | 5 7 28 | 6 8 15 |
emr | emr 2872 | 15 14 36 | 7 8 29 | 9 12 18 |
esa | esa 3072 | 14 13 38 | 6 7 25 | 8 32 15 |
gfz | gfz 2872 | 14 14 42 | 15 21 70 | 13 11 27 |
grg | grg 2880 | 14 13 38 | 7 7 27 | 9 46 19 |
igr | igr 2963 | 15 14 43 | 6 7 25 | 7 23 15 |
igs | igs 3017 | 13 12 36 | 6 9 30 | 8 19 15 |
jpl | jpl 2776 | 16 15 50 | 6 7 27 | 8 13 18 |
mit | mit 3072 | 13 14 39 | 6 7 28 | 7 25 15 |
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 6.1648 GPS week: 1648 MJD: 55780.500-55786.500
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 -17 -99 -49 4 | 6 20
| 19 28 104 56 5 | 1
emr uuuuu | 42 -19 202 0 1 | 39 46
| 18 30 82 51 8 | 2
esa uuuuu | 10 -41 56 18 -1 | 14 27
| 11 17 75 69 6 | 2
gfz uuuuu | -38 21 -43 -19 1 | 3 23
| 16 16 46 65 4 | 2
grg uuuux | -1 -11 -132 -140 37 | 43 62
| 35 24 96 70 61 | 12
igr xxxxx | -14 -8 -18 -16 -3 | 5 21
| 9 11 78 52 5 | 1
irf xxxxx | 19 8 -22 -14 0 | 4 21
| 11 8 28 44 3 | 3
jpl uuuuu | -7 0 -4 55 1 | 29 34
| 52 34 83 64 9 | 3
mit uuuuu | 9 9 -62 -113 -5 | 18 28
| 24 17 65 92 3 | 4
ngs uuuuu | 0 23 17 84 -2 | 9 20
| 31 34 35 132 5 | 3
sio uuuuu | -13 49 -20 147 15 | 36 40
| 18 21 74 90 13 | 2
Table 7.1648.0 GPS week: 1648 Day: 0 MJD: 55780.500
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 -24 -76 -11 6 | 7 17
emr uuuuu | 40 -26 198 11 -8 | 43 46
esa uuuuu | 6 -14 162 -27 -4 | 19 25
gfz uuuuu | -37 -12 -107 2 -6 | 7 18
grg uuuux | -45 24 -300 -265 10 | 52 71
igr xxxxx | -23 -14 25 -11 6 | 7 19
irf xxxxx | 15 10 31 -46 -3 | 9 17
jpl uuuuu | 21 -67 -115 113 16 | 33 35
mit uuuuu | -8 -2 -21 -192 -6 | 24 28
ngs uuuuu | 33 38 22 239 3 | 14 18
sio uuuuu | -8 61 131 77 22 | 35 38
Table 7.1648.1 GPS week: 1648 Day: 1 MJD: 55781.500
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 -34 -112 -14 12 | 4 20
emr uuuuu | 49 -50 113 -98 -11 | 39 46
esa uuuuu | 26 -50 163 161 -12 | 15 27
gfz uuuuu | -41 29 4 -79 1 | 3 23
grg uuuux | -44 -2 -114 -190 -12 | 42 63
igr xxxxx | -9 -18 104 -48 3 | 5 22
irf xxxxx | 18 10 -46 -38 1 | 5 22
jpl uuuuu | -25 19 48 -54 -2 | 31 35
mit uuuuu | 14 19 -178 -220 -10 | 21 29
ngs uuuuu | 0 12 -25 181 5 | 10 20
sio uuuuu | -2 67 -50 116 28 | 33 37
Table 7.1648.2 GPS week: 1648 Day: 2 MJD: 55782.500
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 30 -213 5 7 | 4 20
emr uuuuu | 62 -32 281 9 -1 | 37 46
esa uuuuu | -10 -38 42 42 1 | 13 28
gfz uuuuu | -68 36 -99 -121 0 | 2 24
grg uuuux | -2 -6 -116 -93 20 | 31 51
igr xxxxx | 2 -1 48 4 -3 | 5 22
irf xxxxx | 9 18 -53 -25 3 | 3 23
jpl uuuuu | 26 18 75 122 -5 | 28 34
mit uuuuu | 4 35 -113 -157 -6 | 18 30
ngs uuuuu | 27 -25 67 112 -4 | 9 21
sio uuuuu | -18 67 -78 127 27 | 33 37
Table 7.1648.3 GPS week: 1648 Day: 3 MJD: 55783.500
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 | 27 -32 -228 -108 6 | 6 21
emr uuuuu | 66 -46 277 -27 1 | 39 47
esa uuuuu | 8 -59 24 -27 -1 | 14 29
gfz uuuuu | -23 20 -55 11 0 | 3 24
grg uuuux | 45 0 -202 -94 -16 | 30 50
igr xxxxx | -13 -18 -110 36 -3 | 6 22
irf xxxxx | 3 7 -40 -14 4 | 4 23
jpl uuuuu | -41 11 86 24 4 | 29 35
mit uuuuu | -31 14 -17 -101 0 | 18 30
ngs uuuuu | 23 33 -2 97 -7 | 9 21
sio uuuuu | -50 47 -12 192 20 | 36 41
Table 7.1648.4 GPS week: 1648 Day: 4 MJD: 55784.500
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 6 31 -7 3 | 7 21
emr uuuuu | 20 1 292 54 7 | 38 46
esa uuuuu | 17 -25 -14 -29 2 | 14 29
gfz uuuuu | -41 29 -27 9 -1 | 2 24
grg uuuux | 40 -17 -106 -79 81 | 35 50
igr xxxxx | -21 -12 -54 -100 -6 | 6 21
irf xxxxx | 30 14 -13 77 -1 | 4 22
jpl uuuuu | -61 5 -97 55 -12 | 29 34
mit uuuuu | 20 10 14 60 -5 | 17 29
ngs uuuuu | -9 -16 -19 -171 3 | 8 20
sio uuuuu | -5 53 1 329 10 | 37 43
Table 7.1648.5 GPS week: 1648 Day: 5 MJD: 55785.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 20 -54 -123 -74 -2 | 5 20
emr uuuuu | 35 36 154 43 5 | 37 45
esa uuuuu | 13 -60 -5 -21 0 | 12 27
gfz uuuuu | -19 20 7 -30 8 | 0 23
grg uuuux | -4 -56 -85 -88 155 | 45 61
igr xxxxx | -9 3 -47 51 -7 | 4 21
irf xxxxx | 30 1 -21 1 0 | 1 21
jpl uuuuu | -51 34 27 22 -2 | 26 32
mit uuuuu | 26 3 -53 -72 -1 | 14 26
ngs uuuuu | -26 48 24 113 -6 | 6 19
sio uuuuu | 3 42 -39 124 6 | 37 42
Table 7.1648.6 GPS week: 1648 Day: 6 MJD: 55786.500
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 | 40 -11 31 -134 -1 | 6 21
emr uuuuu | 21 -14 100 8 10 | 39 47
esa uuuuu | 9 -41 21 24 6 | 12 27
gfz uuuuu | -37 23 -23 76 5 | 1 24
grg uuuux | 1 -19 3 -168 20 | 64 89
igr xxxxx | -23 7 -89 -45 -10 | 4 21
irf xxxxx | 26 -7 -10 -50 -5 | 1 21
jpl uuuuu | 83 -21 -49 104 7 | 26 32
mit uuuuu | 41 -17 -64 -107 -3 | 13 26
ngs uuuuu | -50 68 54 17 -7 | 6 19
sio uuuuu | -12 6 -92 66 -9 | 39 44
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