[IGSREPORT-20048] Wk 1647 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 18 07:17:24 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1647 (Jul 31, 2011 - Aug 06, 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:
igs1647[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1647[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1647[0-6].cls IGS GPS clock combination summary report.
igs16477.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16477.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 | ESA | 30
0 | GFZ | MDVJ
0 | GRG | OHI3 SANT
0 | JPL | 25
0 | MIT | 1 6 11 26 30 1 3 6 11 26 30 CAS1 CAS1
1 | COD | CHUR
1 | ESA | REUN
1 | GFZ | SALU
1 | JPL | 25 26
1 | MIT | 30 26 30
2 | EMR | 3 6 3 6 KHAJ KHAJ
2 | ESA | NKLG
2 | GFZ | MDVJ
2 | JPL | 3 6 25 26 ASPA MDO1
2 | MIT | 3 19 30 3 19 30 BRUS NTUS
3 | EMR | 6 6
3 | ESA | IRKJ
3 | GFZ | 7 RAMO
3 | GRG | IRKJ
3 | JPL | 25 26 IRKJ
3 | MIT | 1 6 30 1 6 19 30
4 | COD | DAV1
4 | EMR | 3 6 3 6
4 | ESA | IRKJ
4 | GFZ | 3 7 MDVJ RAMO
4 | GRG | IRKJ NKLG
4 | JPL | 3 25 IRKJ
4 | MIT | 1 3 6 9 22 1 3 6 9 22 DAV1 DAV1
5 | EMR | 3 6 3 6
5 | ESA | DRAG UNSA
5 | GFZ | 3 7 HARB MDVJ OPMT
5 | JPL | 18 25 RAMO
5 | MIT | 1 3 6 17 21 1 3 6 21 DAV1
6 | COD | WROC
6 | EMR | 3 6 3 6 WHIT MATE WHIT
6 | ESA | CHUR CHUR HOFN MAW1 UNSA
6 | GFZ | 3 6 7 MDVJ NYAL YELL
6 | JPL | 3 25
6 | MIT | 1 3 5 6 9 13 19 21 26 3 5 6 9 13 19 21 26 KOSG MDVJ
6 | MIT | MIZU YELL BOR1 HARB HNPT KOSG
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
----+------------+----------
G24 | 2011_08_03 | 2011054
6. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | GRG | 3
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 | .5 .4 .0 -14 -6 20 .10
EMR | -2.2 -2.3 2.1 11 1 2 .37
ESA | -1.2 -7.1 17.4 -44 40 90 .14
GFZ | -1.2 .2 -.4 -20 5 6 .05
GRG | 2.9 -.3 9.6 -5 -5 13 .02
JPL | .3 2.3 -11.2 36 37 105 -1.17
MIT | 2.5 -9.4 27.9 -9 -4 -8 -.01
NGS | 2.2 -.6 13.7 -47 5 10 -.01
SIO | .5 -7.1 2.9 -134 -17 30 -.03
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 1.1647.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1647.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 2.1647.[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 3.1647.[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 5.1647.0-6).
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 1647 summary. (Jul 31, 2011 - Aug 06, 2011)
Table 1.1647.a GPS week: 1647 MJD: 55773.000-55779.000
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 -3 -19 -4 5 -.26 8 7 | -282 -114 19 88
| 0 0 1 8 8 20 .01 | 646 716
emr 91| -1 -1 -6 -62 27 -11 .34 18 18 | 1353 -687 21 126
| 1 1 1 43 23 10 .03 | 1434 935
esa 137| 0 0 2 -21 9 27 .24 8 7 | -1139 201 19 175
| 1 0 2 32 23 12 .02 | 1690 1396
gfz 196| -1 0 4 -11 -29 -31 -.28 12 12 | 17 -62 27 142
| 1 0 0 63 77 6 .03 | 241 309
grg 130| 0 1 7 -48 12 -11 .63 16 14 | 762 -806 41 233
| 0 0 2 16 26 20 .06 | 1190 844
igr n/a| 0 0 0 0 2 -54 -.11 6 5 | 5490 -883 21 102
| 0 0 1 18 9 8 .01 | 1136 728
jpl 128| 0 0 -13 -129 -87 3 .51 19 19 | 351 -826 22 302
| 1 1 1 13 8 61 .03 | 1131 849
mit 286| 0 -1 5 -21 16 -24 -.33 16 13 | 534 -536 29 202
| 1 1 0 11 20 19 .07 | 1146 1289
ngs 219| 0 0 1 84 4 -7 -.23 11 9 | 18833 -142970 2171 3911
| 1 1 0 51 46 25 .03 | 50279 377914
sio 251| -1 0 -2 205 43 11 -.24 18 16 | --- --- --- ---
| 1 0 2 13 23 25 .05 | --- ---
Table 1.1647.b GPS week : 1647 MJD: 55773.000-55779.000
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 | 22 19 25 23 19 10 17 |
2 | 5 6 5 5 5 6 5 |
3 | 6 7 7 7 7 6 7 |
4 | 3 4 4 4 4 4 3 |
5 | 4 5 5 5 5 4 5 |
6 | 5 6 5 6 6 6 6 |
7 | 4 4 4 5 5 4 5 |
8 | 4 4 4 4 4 4 3 |
9 | 4 4 4 4 4 4 4 |
10 | 4 4 4 4 4 3 4 |
11 | 4 4 4 4 4 4 3 |
12 | 6 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 5 7 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 4 5 4 4 4 |
18 | 5 5 5 5 5 5 5 |
19 | 4 4 4 5 4 4 4 |
20 | 4 4 4 5 4 4 4 |
21 | 5 5 5 5 5 5 4 |
22 | 4 5 5 5 4 4 4 |
23 | 4 5 5 5 5 5 5 |
24 | 4 4 4 0 4 4 3 |
25 | 4 5 5 5 5 5 4 |
26 | 6 7 6 6 7 6 5 |
27 | 4 4 4 4 5 4 4 |
28 | 5 5 5 5 5 5 4 |
29 | 5 5 5 5 5 5 6 |
30 | 7 8 9 8 0 --- 0 |
31 | 4 5 4 4 4 4 5 |
32 | 3 4 4 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 2.1647.0 GPS week: 1647 Day: 0 MJD: 55773.000
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 0 0 -.29 8 7 | -1093 966 26 83
| 30 -3 |
emr 91| -2 -1 -5 -34 -2 -12 .35 18 18 | 3507 -1432 33 134
| -11 3 |
esa 137| 2 0 -1 19 1 33 .21 7 7 | 1206 -1323 25 176
| 24 -5 |
gfz 196| 0 0 3 -105 50 -24 -.31 13 11 | -18 5 32 139
| 30 22 |
grg 130| 1 2 6 -83 58 -23 .59 14 14 | 2346 -1179 49 231
| 122 -42 |
igr n/a| 0 0 0 -14 5 -47 -.11 5 5 | 7053 -1006 26 92
| 7 31 |
jpl 128| -2 0 -14 -141 -89 -7 .53 19 18 | 1862 -1193 26 269
| 4 56 |
mit 300| 0 -2 6 -15 2 -45 -.32 15 12 | -375 646 37 214
| -7 -7 |
ngs 219| 0 -2 2 124 -63 -10 -.23 11 9 | -1108 952 2341 4146
| -95 105 |
sio 251| -4 1 1 194 14 34 -.19 19 18 | --- --- --- ---
| -115 -19 |
Table 2.1647.1 GPS week: 1647 Day: 1 MJD: 55774.000
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 1 -3 -11 -8 32 -.25 9 8 | 773 -1284 22 102
| 47 3 |
emr 91| -1 -1 -6 -12 3 -25 .35 17 17 | 2334 -263 34 131
| -36 -3 |
esa 137| 0 0 2 -56 5 25 .22 8 8 | -490 196 29 199
| 41 29 |
gfz 196| 0 1 4 -70 46 -23 -.29 14 14 | 294 -172 29 155
| 23 65 |
grg 130| 0 2 7 -49 19 3 .60 16 15 | 1590 62 58 264
| 44 -7 |
igr n/a| 0 0 0 -1 17 -56 -.10 6 5 | 6544 -45 24 94
| 16 35 |
jpl 128| 0 1 -11 -128 -97 -70 .53 19 19 | 1231 7 24 317
| -35 45 |
mit 300| 1 -2 4 -24 24 -35 -.29 15 12 | 1962 -2175 32 262
| -4 -15 |
ngs 219| 0 0 0 151 -28 -27 -.22 11 9 | 752 -1282 2093 4116
| -103 17 |
sio 251| -2 0 -1 223 37 41 -.22 18 17 | --- --- --- ---
| -126 -23 |
Table 2.1647.2 GPS week: 1647 Day: 2 MJD: 55775.000
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 1 -3 -34 2 -19 -.25 8 7 | -736 89 13 80
| 83 4 |
emr 91| -2 -1 -6 -29 30 -18 .38 17 17 | 1298 -937 17 135
| -29 -28 |
esa 137| 1 0 1 -64 13 14 .24 8 8 | -3827 2342 15 164
| 43 -15 |
gfz 196| 0 0 4 36 -39 -27 -.28 11 10 | -87 -466 25 130
| 33 82 |
grg 130| 0 1 7 -50 15 -28 .60 16 14 | 1381 -670 37 226
| 43 -6 |
igr n/a| 0 0 1 -25 4 -61 -.13 5 5 | 5901 -744 19 95
| 23 36 |
jpl 128| 0 0 -12 -133 -81 110 .53 17 17 | 772 -719 22 316
| 90 -116 |
mit 300| 1 -3 4 -24 15 -36 -.24 17 14 | -704 1111 28 162
| -11 -10 |
ngs 219| 0 0 1 113 4 2 -.17 11 9 | -763 105 2605 3853
| -75 -19 |
sio 251| -1 0 -1 210 27 37 -.20 18 16 | --- --- --- ---
| -111 -9 |
Table 2.1647.3 GPS week: 1647 Day: 3 MJD: 55776.000
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 -3 -27 -1 23 -.27 8 8 | -90 427 16 86
| 21 -8 |
emr 91| -1 0 -10 -35 16 -1 .28 18 18 | 596 -1923 13 102
| -27 -46 |
esa 137| 1 0 4 -9 -15 27 .28 7 7 | -2656 1300 16 190
| 38 21 |
gfz 196| 0 1 3 -55 11 -37 -.24 13 12 | -429 548 26 150
| 65 53 |
grg 130| 1 1 11 -30 10 -16 .57 24 22 | 636 -2134 36 217
| 9 14 |
igr n/a| 0 0 0 -3 -8 -45 -.12 5 5 | 5326 -2043 21 129
| 9 10 |
jpl 128| 0 1 -15 -104 -72 -50 .52 20 20 | 188 -2163 20 302
| 54 74 |
mit 300| 0 -3 5 -41 5 -40 -.29 16 14 | 2301 -2193 24 186
| -26 -5 |
ngs 219| 0 0 1 107 -8 20 -.24 13 12 | 231 208 2045 3540
| -52 19 |
sio 251| -1 0 -4 183 33 -7 -.30 16 15 | --- --- --- ---
| -116 -21 |
Table 2.1647.4 GPS week: 1647 Day: 4 MJD: 55777.000
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 -4 -11 -20 9 -.27 8 8 | 295 -526 18 91
| 40 42 |
emr 91| 1 2 -7 -94 33 4 .36 18 18 | -588 -482 18 135
| 11 -45 |
esa 137| 0 0 4 -41 -9 14 .23 8 7 | -1622 852 21 169
| 60 27 |
gfz 196| -2 0 5 59 -11 -39 -.32 14 13 | 7 -196 28 142
| 10 63 |
grg 130| 0 1 7 -45 -29 18 .70 15 13 | -964 -844 36 206
| 27 82 |
igr n/a| 0 0 1 5 -11 -44 -.12 5 5 | 3964 -1014 19 91
| -8 20 |
jpl 128| 0 -1 -13 -135 -84 -14 .47 20 19 | -1292 -845 22 295
| 17 63 |
mit 300| 1 0 4 -8 58 -18 -.31 18 14 | 163 -875 26 177
| -24 0 |
ngs 219| 0 0 1 39 4 2 -.22 11 8 | 426 -650 2293 4043
| -38 -61 |
sio 251| -1 1 -4 211 86 -3 -.30 17 16 | --- --- --- ---
| -138 -29 |
Table 2.1647.5 GPS week: 1647 Day: 5 MJD: 55778.000
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 -4 -12 -8 -22 -.27 10 7 | -585 -156 20 83
| 16 9 |
emr 91| 1 -3 -4 -116 46 -7 .33 20 20 | 86 1008 20 135
| 40 -34 |
esa 137| 1 0 3 3 55 51 .24 8 8 | -425 -1416 17 165
| 29 -3 |
gfz 196| -1 0 3 18 -109 -31 -.24 11 11 | 108 -38 26 139
| 1 34 |
grg 130| 0 1 3 -38 10 -36 .69 13 12 | -614 376 38 229
| 47 15 |
igr n/a| 0 0 0 17 9 -62 -.12 6 5 | 4200 37 21 107
| -12 26 |
jpl 128| 0 2 -14 -117 -94 3 .47 19 18 | -931 400 23 312
| 26 83 |
mit 300| 0 -1 5 -23 1 4 -.40 17 13 | 161 -136 29 215
| -12 17 |
ngs 219| 0 1 2 19 48 13 -.28 11 9 | -552 -125 1854 3591
| -61 -32 |
sio 251| -2 0 -4 198 41 -1 -.25 17 16 | --- --- --- ---
| -145 -22 |
Table 2.1647.6 GPS week: 1647 Day: 6 MJD: 55779.000
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 -4 -19 4 17 -.26 8 6 | -538 -315 18 93
| 57 11 |
emr 91| -2 -1 -7 -112 61 -17 .36 20 20 | 2243 -782 13 114
| 28 -68 |
esa 137| 0 0 4 -4 16 26 .25 6 6 | -164 -543 15 162
| 28 22 |
gfz 196| -2 0 3 33 -155 -36 -.26 12 12 | 248 -121 25 142
| -18 66 |
grg 130| -1 1 6 -43 0 3 .69 13 12 | 965 -1258 39 261
| 42 -15 |
igr n/a| 0 0 1 27 2 -62 -.09 6 5 | 5445 -1367 20 108
| 13 58 |
jpl 128| 0 0 -13 -142 -93 50 .50 20 20 | 630 -1270 23 305
| 71 41 |
mit 300| 2 0 4 -10 6 -2 -.44 15 12 | 231 -135 30 200
| -7 15 |
ngs 219| 2 0 0 37 75 -53 -.23 11 8 | 132847 -999999 1972 4088
| 18 -73 |
sio 251| 0 1 -4 216 59 -19 -.24 19 16 | --- --- --- ---
| -137 -16 |
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 3.1647.0 GPS week: 1647 Day: 0 MJD: 55773.000
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 | 37 --- 27 --- --- 27 --- 24 --- --- 22 | 115 --- 129 --- --- 138 --- 129 --- --- 122
2 | 7 18 6 11 12 4 21 13 9 37 5 | 39 48 39 41 43 41 51 41 39 54 40
3E | 13 18 11 12 15 7 20 30 23 11 6 | 57 59 56 61 58 58 59 65 67 58 57
4 | 6 9 7 6 12 3 14 10 12 12 3 | 25 26 32 27 33 26 28 33 24 30 27
5 | 6 15 7 12 10 6 20 14 11 21 4 | 37 41 37 40 39 39 43 36 40 34 36
6E | 12 20 8 13 14 7 19 23 16 14 5 | 26 40 35 34 41 29 44 39 33 36 32
7 | 7 16 8 9 17 6 20 8 9 16 4 | 17 30 24 22 29 22 31 18 22 17 20
8 | 8 11 5 11 14 4 12 10 9 20 3 | 17 25 23 19 21 19 26 19 19 22 19
9 | 9 16 8 12 12 5 16 14 10 17 4 | 17 21 18 15 20 14 22 23 15 28 17
10 | 5 9 4 13 12 5 9 13 11 21 3 | 26 30 29 32 36 26 28 34 28 25 28
11 | 7 18 5 12 16 3 17 11 11 10 4 | 23 33 23 24 34 22 29 23 22 22 22
12 | 7 22 7 23 17 6 30 18 11 20 5 | 18 29 19 28 27 16 31 23 16 23 17
13E | 8 18 7 10 12 6 17 14 8 17 4 | 16 30 24 18 30 19 27 20 17 21 19
14E | 6 19 6 12 17 5 21 12 8 15 4 | 19 25 23 19 26 19 30 20 21 18 19
15 | 12 26 7 12 12 7 21 11 11 13 4 | 32 32 33 31 37 30 34 25 29 25 28
16 | 9 23 7 13 16 6 23 12 10 17 4 | 19 33 20 17 31 20 32 18 20 18 19
17E | 8 13 7 10 22 6 22 12 9 16 4 | 30 37 34 27 33 30 37 33 31 34 31
18 | 8 21 7 18 13 7 22 12 8 32 5 | 19 30 21 21 26 17 33 22 17 22 19
19E | 6 24 7 11 13 6 19 13 7 9 4 | 26 37 31 21 31 23 34 31 24 25 27
20 | 6 13 5 14 9 4 15 9 7 22 3 | 19 23 22 26 21 20 20 20 19 19 19
21 | 7 20 7 11 12 6 24 22 7 20 4 | 31 45 33 28 40 29 44 26 28 29 31
22 | 7 16 6 12 11 6 18 15 8 19 4 | 26 30 27 30 31 27 35 36 26 28 26
23E | 6 20 6 14 12 6 19 14 9 17 4 | 44 46 50 51 51 47 45 48 48 46 46
24 | 6 12 6 9 13 5 13 13 10 19 3 | 21 17 17 14 14 18 11 21 14 16 18
25 | 6 15 5 7 18 6 25 16 8 15 4 | 14 23 19 18 34 16 39 15 16 17 15
26E | 15 14 9 13 17 5 14 23 16 26 5 | 59 63 57 60 59 57 59 73 65 64 60
27 | 9 15 7 12 12 4 16 14 9 15 4 | 13 20 16 14 20 12 22 22 16 24 15
28 | 10 18 6 12 19 5 17 9 6 25 4 | 21 32 23 20 33 20 30 20 21 19 21
29E | 9 23 8 11 17 6 25 14 8 9 4 | 17 29 19 15 21 16 30 18 19 19 16
X30 | 11 16 7 --- --- 13 --- 18 --- --- 7 | 32 25 23 --- --- 33 --- 18 --- --- 34
31 | 5 18 6 16 17 6 20 9 10 16 4 | 19 29 22 19 34 19 27 22 21 23 20
32 | 5 15 6 12 10 3 11 12 6 10 3 | 17 16 19 23 22 16 18 19 17 19 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 12 14 5 19 15 11 19 |T 28 32 31 27 32 29 33 31 26 27 29
WRMS | 7 18 7 11 14 5 18 12 9 17 |NE 26 29 29 24 29 27 30 28 22 24 27
MEDI | 7 18 7 12 13 6 19 13 9 17 |MD 21 30 23 23 31 22 31 23 21 23 21
Table 3.1647.1 GPS week: 1647 Day: 1 MJD: 55774.000
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 | 25 --- 27 --- --- 42 --- 26 --- --- 18 | 81 --- 91 --- --- 108 --- 94 --- --- 86
2 | 7 17 9 12 14 5 26 13 10 35 5 | 36 43 39 40 41 35 51 38 36 46 38
3E | 14 17 10 11 22 8 18 35 21 14 6 | 57 55 58 56 63 56 51 71 67 57 58
4 | 9 10 7 11 12 5 13 14 10 11 3 | 19 22 23 22 24 19 25 25 20 24 20
5 | 7 13 10 11 11 7 23 11 16 21 4 | 44 44 44 44 46 44 49 45 46 44 44
6E | 11 15 10 13 21 7 15 27 17 17 5 | 20 33 26 27 40 22 36 35 29 27 25
7 | 7 18 8 12 19 6 18 10 8 15 4 | 20 29 19 23 28 19 27 22 22 18 20
8 | 7 12 7 10 16 3 9 12 8 16 3 | 24 28 29 29 24 24 28 31 27 32 27
9 | 9 14 7 11 14 6 12 15 8 16 4 | 14 19 17 15 14 14 23 24 21 25 16
10 | 8 9 8 12 14 5 10 16 11 17 4 | 19 23 22 26 26 21 23 29 24 22 21
11 | 7 17 5 14 15 5 19 12 12 15 4 | 16 30 19 22 29 16 29 22 20 20 18
12 | 8 21 6 19 19 5 26 15 9 19 5 | 31 37 24 31 31 26 36 32 27 29 28
13E | 8 16 7 10 22 6 15 11 8 12 4 | 17 25 24 18 28 20 26 19 23 17 20
14E | 6 13 8 13 15 5 16 13 8 15 4 | 18 24 23 21 26 18 31 23 22 21 20
15 | 7 25 10 13 21 8 21 14 8 20 5 | 16 27 20 15 30 15 27 17 20 14 17
16 | 7 21 7 12 13 4 22 12 13 17 4 | 15 27 16 12 25 15 29 16 20 19 15
17E | 8 15 8 13 15 5 17 12 13 16 4 | 20 31 25 24 28 21 31 21 24 24 23
18 | 7 20 8 21 12 6 25 10 9 28 5 | 14 27 17 26 21 15 30 20 20 15 16
19E | 8 21 10 11 12 3 17 12 11 12 4 | 27 39 31 32 29 29 38 32 28 31 29
20 | 6 13 7 14 10 5 15 7 10 21 3 | 18 21 15 19 19 17 22 18 19 18 17
21 | 7 21 5 13 17 6 24 14 6 18 4 | 22 33 24 18 31 20 36 22 21 19 22
22 | 7 17 9 12 11 4 21 18 8 18 4 | 32 38 36 33 38 32 41 38 34 36 34
23E | 9 21 10 17 17 5 17 12 9 20 5 | 26 32 27 33 26 26 27 29 29 22 25
24 | 5 13 5 9 13 6 14 12 10 20 3 | 11 17 9 12 13 13 16 18 8 15 14
25 | 8 15 6 24 23 6 26 15 7 15 5 | 21 31 23 30 30 23 38 29 24 30 23
26E | 18 14 9 15 18 7 15 31 18 25 6 | 53 57 52 54 52 53 60 66 60 59 54
27 | 9 13 7 9 15 6 12 14 9 14 3 | 15 21 16 14 18 16 24 24 22 25 17
28 | 8 19 10 12 20 8 19 9 11 22 4 | 22 31 25 21 31 22 30 23 24 20 23
29E | 8 19 7 14 15 5 22 14 8 16 4 | 20 27 20 21 22 19 28 21 20 20 19
X30 | 11 15 13 --- --- 8 --- 14 --- --- 7 | 31 22 19 --- --- 28 --- 16 --- --- 32
31 | 7 19 9 18 17 5 18 9 11 12 4 | 14 28 19 22 28 16 28 18 17 20 17
32 | 7 15 8 12 12 5 15 10 11 11 3 | 22 22 21 22 25 21 23 23 24 21 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 8 14 16 6 19 15 11 18 |T 25 30 27 26 29 26 32 30 26 26 26
WRMS | 8 17 8 14 15 5 19 12 9 17 |NE 24 28 25 23 27 25 30 28 23 24 25
MEDI | 8 16 8 12 15 5 17 13 10 16 |MD 20 28 23 22 28 21 29 23 23 22 22
Table 3.1647.2 GPS week: 1647 Day: 2 MJD: 55775.000
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 --- 40 --- --- 18 --- 33 --- --- 25 | 119 --- 148 --- --- 137 --- 127 --- --- 130
2 | 9 16 9 12 13 5 21 17 9 35 5 | 37 45 38 38 44 35 51 37 37 52 38
3E | 14 19 9 11 34 6 20 39 20 12 7 | 33 31 32 35 53 35 37 56 41 34 34
4 | 6 12 7 7 13 4 12 14 13 13 3 | 17 22 21 21 25 19 27 24 19 24 18
5 | 8 14 10 10 13 5 16 18 10 21 4 | 26 30 28 30 35 27 38 27 27 27 27
6E | 9 20 8 10 15 5 17 29 17 13 5 | 21 35 32 26 37 25 41 38 30 30 27
7 | 6 17 7 11 17 5 15 12 10 13 4 | 13 22 15 16 24 11 28 17 14 14 13
8 | 7 13 8 9 12 3 10 14 9 10 3 | 14 24 19 15 18 13 29 26 14 20 16
9 | 11 14 7 8 13 5 13 17 11 14 4 | 12 18 17 16 15 13 28 26 19 25 15
10 | 6 14 9 9 13 7 9 15 11 16 3 | 18 23 21 24 30 19 24 29 21 21 20
11 | 6 14 5 11 18 4 15 12 10 14 3 | 13 27 17 15 31 13 31 14 15 15 14
12 | 7 19 10 16 17 6 19 19 9 24 5 | 19 27 14 26 20 15 27 22 14 18 14
13E | 7 12 7 8 17 6 17 13 10 10 3 | 19 28 22 23 31 20 35 21 22 20 21
14E | 7 15 11 10 14 8 18 13 10 13 4 | 15 21 21 15 24 15 31 19 16 16 15
15 | 6 26 9 11 19 6 20 16 11 17 5 | 13 25 17 17 24 13 24 18 17 16 14
16 | 6 18 11 11 15 5 22 12 13 17 4 | 15 26 16 12 23 11 27 14 15 11 12
17E | 6 20 10 9 12 4 18 16 8 14 4 | 19 33 24 22 28 21 35 19 24 19 22
18 | 7 20 9 16 12 7 19 12 8 27 5 | 12 26 17 22 17 14 29 17 11 15 11
19E | 5 18 7 9 16 5 19 19 10 11 4 | 20 35 28 20 28 24 38 23 22 26 23
20 | 6 13 10 12 9 5 15 9 10 22 4 | 16 18 18 21 17 15 22 12 16 14 14
21 | 7 22 7 12 12 5 22 12 7 18 4 | 21 33 25 19 30 20 37 22 21 21 21
22 | 8 14 7 11 13 7 19 23 11 25 4 | 22 32 29 23 34 26 38 32 28 28 25
23 | 7 19 9 12 20 7 17 13 11 18 4 | 46 51 50 54 53 51 52 53 53 47 49
24 | 5 11 4 9 13 4 12 12 11 19 3 | 12 12 13 15 10 11 15 16 15 11 12
25 | 7 13 7 15 17 4 28 15 7 15 4 | 10 21 14 20 25 8 40 18 14 14 11
26E | 15 19 8 11 20 6 15 30 18 24 6 | 39 44 41 44 41 39 47 51 41 50 40
27 | 9 16 4 8 16 4 12 17 12 12 4 | 12 23 16 13 16 13 26 26 18 23 14
28 | 6 18 10 9 19 6 18 13 10 23 4 | 12 26 17 14 27 11 32 18 14 14 13
29E | 8 24 9 13 18 5 22 14 12 10 5 | 16 28 17 15 19 13 29 14 20 15 15
X30 | 11 19 15 --- --- 15 --- 16 --- --- 8 | 39 23 25 --- --- 37 --- 23 --- --- 42
31 | 6 18 9 9 19 5 16 10 10 12 4 | 14 27 19 14 28 13 28 18 15 18 15
32 | 6 14 9 9 10 5 12 12 7 11 3 | 15 17 18 20 21 13 23 16 16 14 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 8 11 16 5 17 17 11 18 |T 22 27 26 22 27 23 32 27 21 22 24
WRMS | 7 17 8 10 14 5 17 14 9 16 |NE 21 24 25 19 24 22 29 26 18 19 22
MEDI | 7 17 9 10 15 5 17 14 10 14 |MD 16 26 19 20 25 15 29 22 18 19 15
Table 3.1647.3 GPS week: 1647 Day: 3 MJD: 55776.000
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 --- 35 --- --- 48 --- 25 --- --- 23 | 91 --- 112 --- --- 105 --- 105 --- --- 100
2 | 6 21 8 10 11 4 22 13 10 31 5 | 36 49 41 35 39 38 48 38 35 48 38
3E | 11 23 8 14 104 7 24 34 20 14 6 | 80 81 81 82 111 81 84 97 88 79 82
4 | 7 12 8 14 14 4 14 15 12 13 4 | 15 19 22 13 28 18 19 27 16 23 18
5 | 8 13 6 13 14 4 21 15 11 20 4 | 31 36 37 38 39 34 35 37 32 31 33
6E | 9 16 8 16 18 7 16 31 22 13 5 | 21 34 31 29 40 26 40 43 32 31 28
7 | 9 17 8 19 19 6 20 14 13 12 4 | 16 26 20 24 29 18 27 20 21 19 18
8 | 7 12 5 12 11 4 10 13 13 8 3 | 21 23 21 24 23 22 25 27 26 23 21
9 | 9 16 7 13 11 6 14 18 10 12 4 | 16 19 20 18 19 15 21 27 17 19 16
10 | 5 14 7 10 17 6 12 12 12 13 3 | 24 27 29 33 39 25 25 34 23 25 26
11 | 7 18 9 11 18 5 18 12 10 13 4 | 14 29 20 20 33 17 28 16 17 14 17
12 | 6 18 7 20 16 6 23 14 12 17 5 | 19 29 20 24 26 17 31 23 16 21 19
13E | 7 17 7 9 17 6 21 15 11 6 4 | 28 33 32 32 37 30 36 34 31 31 30
14E | 8 14 9 13 13 5 22 11 16 10 4 | 22 30 26 20 29 22 32 23 26 21 23
15 | 7 22 10 13 14 6 21 16 12 17 4 | 14 26 22 19 27 16 20 23 16 18 16
16 | 7 20 7 13 14 7 23 13 15 15 4 | 10 24 17 10 24 12 27 15 17 10 12
17E | 6 24 8 10 16 5 23 15 12 13 4 | 26 38 32 28 33 27 32 28 29 26 28
18 | 7 20 9 11 9 5 21 16 13 24 5 | 15 27 24 20 25 16 30 24 16 19 17
19E | 7 24 8 10 14 4 20 14 14 11 4 | 28 41 31 28 34 27 37 30 27 28 28
20 | 6 17 7 12 10 4 17 11 16 21 4 | 16 20 21 23 19 19 18 18 21 16 17
21 | 7 23 7 12 16 4 25 11 9 17 4 | 25 39 28 25 32 25 44 26 26 23 26
22 | 8 17 8 12 9 4 21 17 12 19 4 | 23 33 31 28 32 26 34 35 29 28 27
23 | 6 21 6 9 17 6 21 14 12 12 4 | 45 48 48 50 59 50 48 49 50 44 47
X24 | 5 --- --- --- --- 93 --- --- --- --- 0 | 9 --- --- --- --- 83 --- --- --- --- 9
25 | 10 15 5 18 13 4 27 14 9 14 4 | 19 32 26 23 32 21 44 24 21 22 22
26E | 18 18 7 15 17 5 16 27 20 24 6 | 65 66 61 62 66 63 64 70 63 69 63
27 | 9 19 6 14 13 6 14 17 10 11 4 | 16 25 19 18 19 16 22 26 18 20 17
28 | 8 17 6 14 16 6 21 11 10 21 4 | 14 28 20 18 28 16 29 22 16 16 17
29E | 9 19 8 11 23 4 26 10 10 11 4 | 21 34 26 24 31 23 35 22 22 25 24
X30 | 12 19 11 --- --- 9 --- 14 --- --- 7 | 43 47 40 --- --- 46 --- 31 --- --- 47
31 | 7 15 6 10 18 6 17 10 9 10 3 | 18 30 26 22 33 19 28 24 22 22 21
32 | 7 14 6 7 10 4 18 13 10 9 3 | 19 20 24 24 27 21 23 23 22 20 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 7 13 24 5 20 16 13 16 |T 26 33 32 28 34 31 34 33 27 27 29
WRMS | 8 18 7 12 22 5 20 14 12 15 |NE 22 28 29 22 28 28 28 29 21 21 25
MEDI | 7 17 7 12 14 5 21 14 12 13 |MD 21 30 26 24 32 22 31 27 22 23 22
Table 3.1647.4 GPS week: 1647 Day: 4 MJD: 55777.000
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 --- 25 --- --- 46 --- 40 --- --- 18 | 75 --- 88 --- --- 98 --- 89 --- --- 80
2 | 8 18 6 10 12 5 23 14 12 31 5 | 27 38 32 28 36 28 40 30 29 42 30
3E | 11 21 8 10 19 6 23 42 19 19 6 | 46 43 46 44 47 45 46 59 53 47 44
4 | 7 14 7 10 9 5 14 13 11 10 3 | 13 20 20 18 24 15 18 21 15 20 15
5 | 9 15 8 14 12 5 20 16 8 19 4 | 17 24 24 26 28 19 28 29 18 24 20
6E | 7 17 6 12 16 6 17 39 19 15 5 | 17 29 26 22 34 21 35 46 28 29 23
7 | 7 22 8 25 12 5 17 11 10 11 4 | 15 28 17 28 25 14 25 18 17 18 16
8 | 8 14 8 14 13 4 10 11 10 8 3 | 13 21 17 17 16 12 19 19 12 17 14
9 | 10 16 11 6 15 7 16 17 10 13 4 | 14 18 22 18 17 14 22 28 23 19 18
10 | 6 14 6 11 12 5 10 12 9 14 3 | 20 24 25 28 30 22 22 25 25 22 22
11 | 5 12 7 12 19 4 20 12 8 11 4 | 11 23 18 13 31 11 26 16 15 13 13
12 | 6 20 6 17 15 4 23 15 11 14 4 | 12 26 14 19 18 9 25 16 12 13 11
13E | 9 16 6 13 11 4 17 15 12 9 4 | 26 34 31 35 38 30 35 24 26 26 28
14E | 9 15 17 10 16 6 21 14 9 11 4 | 24 36 29 27 33 30 37 35 32 31 28
15 | 9 26 8 12 19 7 22 18 14 17 5 | 12 24 17 19 29 15 24 22 19 20 14
16 | 6 23 7 22 15 5 24 15 11 16 5 | 10 28 20 15 23 10 29 15 13 13 12
17E | 6 21 7 11 14 5 20 15 11 10 4 | 17 28 22 18 27 17 29 21 18 17 19
18 | 7 18 7 18 11 3 21 18 7 24 5 | 14 25 18 25 25 16 29 22 23 16 16
19E | 6 14 6 8 15 4 21 12 8 13 3 | 18 27 24 19 27 18 32 20 19 20 20
20 | 7 15 8 12 10 5 17 11 9 22 4 | 13 19 20 18 19 14 18 15 15 14 14
21 | 9 21 8 9 15 6 28 13 8 17 4 | 21 36 25 20 31 20 40 22 21 20 22
22 | 8 15 7 6 11 5 17 15 6 19 4 | 17 29 26 22 33 20 31 31 22 26 22
23 | 10 21 7 12 21 4 19 14 8 14 4 | 32 39 38 39 43 34 36 31 32 30 33
X24 | 4 --- 6 9 --- 7 14 14 10 17 4 | 7 --- 10 7 --- 30 10 17 11 10 7
25 | 8 15 6 20 11 4 25 14 12 14 4 | 9 20 14 16 23 8 36 13 15 11 11
26E | 20 20 11 14 18 5 15 33 20 30 7 | 70 73 73 73 73 71 72 87 73 73 71
X27 | 11 18 7 8 15 6 --- 18 9 11 4 | 15 23 21 19 17 19 --- 32 25 24 19
28 | 5 19 5 25 15 6 20 11 12 22 5 | 11 26 19 34 27 13 27 15 16 16 16
29E | 7 23 7 11 20 6 27 12 12 12 5 | 15 29 18 17 22 13 26 15 15 17 15
X30 | 5 --- --- --- --- 18 --- --- --- --- 0 | 33 --- --- --- --- 34 --- --- --- --- 37
31 | 7 17 6 12 13 6 16 13 12 10 4 | 15 28 21 20 29 16 25 17 16 16 18
32 | 7 14 4 10 10 5 16 13 6 10 3 | 15 20 22 21 23 18 24 21 22 18 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 18 8 14 15 5 20 18 11 17 |T 21 28 26 24 29 23 29 28 22 22 23
WRMS | 8 18 7 13 13 5 19 14 8 16 |NE 17 25 23 20 25 20 25 24 18 18 20
MEDI | 7 17 7 12 15 5 20 14 10 14 |MD 15 27 22 20 27 18 28 22 19 19 19
Table 3.1647.5 GPS week: 1647 Day: 5 MJD: 55778.000
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 | 14 --- 11 --- --- 23 --- 20 --- 25 9 | 89 --- 99 --- --- 85 --- 93 --- 3 94
2 | 7 26 9 7 12 5 24 10 9 36 5 | 36 47 40 35 47 36 45 33 33 53 37
3E | 11 17 12 6 17 6 21 39 19 18 6 | 80 78 78 79 76 82 77 90 85 78 78
4 | 7 17 6 7 10 4 15 12 8 11 3 | 12 18 21 14 22 13 18 20 14 19 14
5 | 7 18 7 11 11 6 18 12 10 20 4 | 29 37 36 32 40 33 36 31 31 32 31
6E | 12 20 8 11 17 6 19 34 18 15 6 | 18 32 27 24 37 22 37 44 25 27 24
7 | 6 23 7 18 10 5 18 12 8 12 4 | 14 28 21 23 26 19 24 18 19 16 16
8 | 8 16 4 12 13 4 11 12 9 6 3 | 16 24 21 18 19 17 22 21 22 18 17
9 | 7 17 8 9 14 4 13 15 11 12 4 | 11 19 20 18 17 12 17 21 16 14 12
10 | 5 13 5 9 9 5 10 10 6 17 3 | 17 22 26 24 23 20 19 19 23 22 20
11 | 7 12 6 10 17 6 18 15 11 14 4 | 14 27 21 14 35 15 25 24 20 20 17
12 | 6 22 7 12 11 5 23 14 12 16 4 | 19 30 18 23 22 17 28 22 20 21 17
13E | 8 21 7 8 12 5 22 14 10 10 4 | 27 38 35 31 38 28 35 34 32 32 31
14E | 31 16 12 12 12 14 17 13 15 13 6 | 83 76 82 79 82 70 77 73 76 70 77
15 | 8 32 7 13 17 6 21 19 12 16 5 | 13 26 22 21 32 17 21 26 17 24 16
16 | 8 24 10 16 14 6 25 21 9 17 5 | 10 27 19 12 22 14 27 20 14 11 12
17E | 7 21 9 7 13 6 23 11 8 14 4 | 28 37 32 29 36 28 34 28 28 26 29
18 | 7 23 10 13 9 5 21 20 11 25 5 | 17 29 24 24 22 17 30 26 20 19 19
19E | 8 25 9 8 12 5 20 11 10 10 4 | 21 40 29 21 35 22 31 24 24 23 24
20 | 7 17 6 14 9 5 17 12 10 23 4 | 10 20 17 20 14 12 17 16 12 15 12
21 | 9 20 8 10 12 4 24 13 10 19 4 | 19 33 27 21 33 20 36 20 19 19 21
22 | 6 17 7 9 6 4 18 14 8 18 3 | 19 31 26 21 28 22 32 23 16 20 21
23 | 8 22 8 11 17 5 23 13 8 22 4 | 29 37 36 35 41 32 34 33 30 31 32
24 | 6 13 6 9 11 6 14 16 9 16 3 | 10 9 16 11 5 15 12 22 13 18 12
25 | 8 16 7 18 12 5 21 13 11 13 4 | 16 25 21 22 26 19 36 20 18 19 17
26E | 20 21 8 14 18 13 14 23 17 26 6 | 90 95 91 94 92 95 92 102 95 93 91
27 | 7 17 8 11 15 5 13 17 10 10 4 | 12 17 19 20 17 14 18 25 19 14 13
28 | 7 23 7 11 10 5 19 12 11 20 4 | 10 28 16 14 26 12 25 15 15 16 12
29E | 10 18 8 9 21 5 25 15 15 13 5 | 18 26 24 18 27 18 28 19 17 20 17
31 | 6 18 8 10 14 6 17 17 11 15 4 | 23 30 28 27 35 22 32 28 21 25 24
32 | 6 15 7 10 8 6 12 11 8 12 3 | 13 18 20 19 18 15 18 20 15 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 8 11 13 6 19 17 11 17 |T 26 33 32 28 33 27 32 32 26 26 28
WRMS | 7 20 8 11 12 5 18 13 9 16 |NE 19 25 26 20 25 21 25 25 18 19 21
MEDI | 7 18 8 10 12 5 18 14 10 16 |MD 18 28 24 21 27 19 28 24 20 20 19
Table 3.1647.6 GPS week: 1647 Day: 6 MJD: 55779.000
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 --- 23 --- --- 22 --- 34 --- --- 17 | 112 --- 130 --- --- 125 --- 128 --- --- 122
2 | 6 22 5 12 13 7 25 10 9 36 5 | 35 46 41 32 48 36 50 32 34 60 38
3E | 12 19 8 9 16 10 20 40 23 24 6 | 98 96 92 96 93 95 96 116 100 87 96
4 | 5 17 4 9 9 6 13 8 11 10 3 | 20 26 28 23 34 21 27 24 21 27 23
5 | 6 15 9 15 12 5 23 8 11 25 4 | 30 35 40 37 43 34 39 29 33 29 33
6E | 12 21 7 7 14 5 23 23 13 29 5 | 25 35 36 30 43 29 41 39 34 44 31
7 | 6 20 6 26 13 4 23 15 8 14 4 | 16 27 17 36 24 17 26 16 22 20 18
8 | 6 13 5 12 12 4 12 11 11 8 3 | 13 22 18 24 19 14 21 20 18 20 16
9 | 7 17 7 9 13 3 13 12 9 14 3 | 13 17 17 14 15 14 18 16 15 15 12
10 | 5 13 6 14 13 3 12 10 8 20 3 | 29 33 34 38 41 31 32 30 34 29 31
11 | 6 15 4 9 17 4 17 6 8 10 3 | 17 33 24 21 41 20 27 20 19 24 21
12 | 7 20 7 12 13 5 20 16 12 22 4 | 17 27 17 22 21 14 27 20 13 17 15
13E | 8 21 6 16 11 4 20 11 9 12 4 | 18 26 25 28 32 22 27 15 22 19 21
14 | 21 20 6 8 15 14 20 11 16 16 5 | 84 94 88 91 91 82 95 94 93 86 89
15 | 6 28 6 15 15 3 25 15 12 15 4 | 14 23 20 24 29 16 24 22 16 21 16
16 | 6 24 5 14 12 6 26 18 10 19 4 | 12 30 17 8 22 14 31 19 14 13 12
17E | 4 21 6 13 14 6 23 9 7 16 4 | 27 37 33 27 40 29 38 29 28 34 30
18 | 5 22 6 16 9 4 23 22 10 24 5 | 16 26 23 27 22 18 28 26 18 20 17
19E | 4 24 6 8 12 4 20 8 9 10 3 | 21 41 28 22 30 24 34 20 24 27 24
20 | 6 18 6 14 8 5 16 6 10 24 3 | 18 23 22 29 21 21 20 19 18 19 19
21 | 7 20 8 6 12 4 29 11 8 18 4 | 25 36 29 20 34 23 45 21 24 23 25
22 | 5 18 4 9 8 3 22 13 15 20 4 | 21 32 27 26 34 25 31 28 25 21 24
23 | 6 24 5 13 17 4 22 9 8 21 4 | 39 45 44 44 48 42 40 40 42 41 41
24 | 5 17 7 10 11 5 13 9 5 16 3 | 9 15 13 10 7 17 12 14 11 13 9
25 | 5 12 6 10 12 6 24 16 13 12 4 | 15 24 17 24 25 15 37 18 12 13 15
26E | 12 21 8 11 19 12 13 13 14 27 5 | 120 127 122 119 123 115 122 119 119 125 120
27 | 8 17 6 9 14 4 13 9 14 11 3 | 16 19 19 17 19 17 20 15 20 18 15
28 | 6 21 6 13 12 4 21 8 10 22 4 | 10 30 17 17 26 13 26 12 17 18 12
29E | 8 24 12 11 21 5 28 17 11 18 5 | 20 29 28 24 27 19 31 21 22 21 21
X30 | 5 --- --- --- --- --- --- --- --- --- 0 | 8 --- --- --- --- --- --- --- --- --- 9
31 | 6 20 5 10 14 5 17 19 17 15 4 | 18 29 20 21 28 18 28 17 21 18 17
32 | 5 14 5 9 8 4 14 8 7 12 3 | 24 30 31 34 33 28 29 30 28 28 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 6 12 13 6 20 15 11 19 |T 30 37 36 32 37 32 37 34 30 31 31
WRMS | 6 20 6 12 12 5 20 12 8 16 |NE 22 27 28 24 27 25 28 26 20 22 23
MEDI | 6 20 6 11 13 5 20 11 10 16 |MD 18 30 27 24 30 21 29 21 22 21 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 4.1647 GPS week: 1647 MJD: 55773.0-55779.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 |U 11 10 28 |U 5 7 25 |U 10 10 20 |
emr | emr 2896 |U 13 11 33 |U 7 8 31 | 10 9 22 |
esa | esa 3017 | 10 11 27 |U 6 7 25 | 9 8 19 |
gfz | gfz 2852 |U 13 11 33 |U 6 7 31 |U 10 11 22 |
grg | grg 2852 | 14 12 35 |U 6 7 26 | 10 12 22 |
igr | igr 2963 | 11 11 28 | 6 7 25 | 9 9 19 |
igs | igs 2981 | 11 11 30 | 5 7 25 | 9 8 18 |
jpl | jpl 2838 |U 13 11 35 |U 7 12 35 | 9 10 25 |
mit | mit 3017 |U 18 17 83 |U 8 11 34 |U 12 11 22 |
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 5.1647.0 GPS week: 1647 Day: 0 MJD: 55773.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 7 5 18 | 4 6 22 | 12 8 24 |
emr | emr 2964 | 12 9 28 | 7 8 27 | 13 10 27 |
esa | esa 3072 | 8 6 17 | 5 6 22 | 10 8 25 |
gfz | gfz 2868 | 13 7 23 | 4 6 22 | 12 18 33 |
grg | grg 2880 | 13 8 23 | 5 7 25 | 13 25 36 |
igr | igr 3013 | 8 5 17 | 4 5 21 | 12 8 24 |
igs | igs 3070 | 8 5 18 | 4 8 25 | 11 8 23 |
jpl | jpl 2866 | 13 9 27 | 6 18 44 | 13 15 26 |
mit | mit 3072 | 56 54 396 | 9 20 45 | 25 18 30 |
Table 5.1647.1 GPS week: 1647 Day: 1 MJD: 55774.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 7 8 24 | 6 8 27 | 10 12 21 |
emr | emr 2964 | 8 9 28 | 8 11 31 | 9 8 18 |
esa | esa 3072 | 6 8 22 | 6 7 25 | 7 8 17 |
gfz | gfz 2868 | 8 9 27 | 6 7 27 | 8 9 19 |
grg | grg 2880 | 9 10 29 | 5 6 28 | 10 9 18 |
igr | igr 3020 | 6 9 24 | 5 7 26 | 7 9 18 |
igs | igs 3065 | 6 8 22 | 5 8 25 | 8 9 16 |
jpl | jpl 2868 | 10 8 29 | 8 20 37 | 7 8 20 |
mit | mit 3072 | 5 7 21 | 9 19 38 | 9 10 22 |
Table 5.1647.2 GPS week: 1647 Day: 2 MJD: 55775.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3061 | 8 11 25 | 8 7 25 | 8 7 19 |
emr | emr 2964 | 10 13 26 | 8 7 27 | 10 8 24 |
esa | esa 3072 | 8 13 24 | 7 6 22 | 8 6 20 |
gfz | gfz 2863 | 11 13 33 | 8 7 24 | 8 7 19 |
grg | grg 2880 | 11 11 38 | 8 7 24 | 8 8 19 |
igr | igr 3058 | 8 11 22 | 8 6 24 | 8 7 19 |
igs | igs 3068 | 8 12 22 | 7 7 23 | 7 6 19 |
jpl | jpl 2861 | 11 12 35 | 9 13 40 | 7 7 20 |
mit | mit 3072 | 18 12 36 | 10 8 30 | 9 9 18 |
Table 5.1647.3 GPS week: 1647 Day: 3 MJD: 55776.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2970 | 9 10 30 | 5 6 19 | 9 11 19 |
emr | emr 2868 | 11 10 35 | 6 8 23 | 10 9 22 |
esa | esa 2976 | 10 11 33 | 5 5 24 | 8 9 19 |
gfz | gfz 2767 | 12 10 34 | 6 6 34 | 8 10 23 |
grg | grg 2784 | 14 12 41 | 6 6 26 | 10 12 26 |
igr | igr 2939 | 10 11 32 | 5 5 23 | 9 11 20 |
igs | igs 2833 | 14 14 47 | 5 6 19 | 8 9 19 |
jpl | jpl 2772 | 12 10 43 | 6 13 29 | 9 9 26 |
mit | mit 2976 | 9 10 29 | 5 5 27 | 9 11 19 |
Table 5.1647.4 GPS week: 1647 Day: 4 MJD: 55777.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2688 | 17 10 35 | 8 7 31 | 10 12 20 |
emr | emr 2772 | 14 11 30 | 8 8 46 | 11 11 25 |
esa | esa 2976 | 13 12 25 | 8 7 34 | 9 9 18 |
gfz | gfz 2869 | 12 10 27 | 10 6 44 | 9 8 20 |
grg | grg 2784 | 14 10 30 | 8 9 34 | 11 13 22 |
igr | igr 2947 | 12 11 26 | 8 7 32 | 10 8 19 |
igs | igs 2940 | 12 11 26 | 8 7 33 | 10 8 17 |
jpl | jpl 2769 | 14 12 27 | 7 7 40 | 10 11 25 |
mit | mit 2976 | 11 12 28 | 8 9 46 | 13 12 21 |
Table 5.1647.5 GPS week: 1647 Day: 5 MJD: 55778.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2964 | 10 11 24 | 5 9 27 | 11 11 15 |
emr | emr 2868 | 12 13 29 | 8 10 30 | 11 9 18 |
esa | esa 2976 | 10 10 26 | 5 9 25 | 12 9 14 |
gfz | gfz 2868 | 14 12 32 | 5 10 29 | 12 11 15 |
grg | grg 2880 | 13 13 28 | 5 9 22 | 11 10 17 |
igr | igr 2913 | 10 11 26 | 6 9 24 | 11 9 13 |
igs | igs 2926 | 10 11 25 | 6 8 26 | 11 9 14 |
jpl | jpl 2867 | 13 12 29 | 6 8 26 | 9 12 38 |
mit | mit 2976 | 10 11 24 | 8 9 28 | 10 8 16 |
Table 5.1647.6 GPS week: 1647 Day: 6 MJD: 55779.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3013 | 16 14 42 | 4 5 24 | 9 13 20 |
emr | emr 2872 | 20 15 52 | 5 7 30 | 10 9 23 |
esa | esa 2976 | 16 15 45 | 4 6 25 | 10 11 21 |
gfz | gfz 2862 | 21 18 53 | 4 7 34 | 11 14 23 |
grg | grg 2880 | 22 18 53 | 5 7 26 | 9 9 20 |
igr | igr 2853 | 20 16 50 | 4 6 27 | 10 11 18 |
igs | igs 2970 | 16 15 47 | 4 5 25 | 10 11 19 |
jpl | jpl 2863 | 20 15 53 | 5 5 27 | 9 9 22 |
mit | mit 2976 | 16 15 50 | 4 5 28 | 12 12 26 |
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 6.1647 GPS week: 1647 MJD: 55773.500-55779.500
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 -45 29 -54 -1 | 3 15
| 19 22 66 61 6 | 2
emr uuxuu | 40 1 99 77 7 | 33 36
| 23 27 217 102 6 | 4
esa uuuuu | -3 -40 67 -76 3 | 12 19
| 15 15 59 61 4 | 4
gfz uuuuu | -47 -23 44 -51 5 | -2 16
| 27 30 131 124 4 | 5
grg uuuux | 2 -51 45 -127 -15 | 36 57
| 39 37 155 107 49 | 7
igr xxxxx | -23 -10 26 -54 7 | -2 17
| 21 15 79 34 5 | 4
irf xxxxx | 8 -3 -49 -11 -1 | 4 15
| 9 8 31 64 5 | 3
jpl uuuuu | -27 -35 123 -12 -1 | 27 31
| 62 36 63 70 7 | 3
mit uuuuu | 9 10 -200 -55 0 | 19 23
| 17 13 58 119 4 | 4
ngs uuuuu | 14 55 -55 243 -5 | 11 14
| 56 34 163 151 3 | 2
sio uuuuu | 28 124 -56 3 -9 | 35 37
| 14 16 55 146 12 | 2
Table 7.1647.0 GPS week: 1647 Day: 0 MJD: 55773.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 19 -33 68 -81 -1 | 0 15
emr uuxuu | 13 8 -65 -45 4 | 27 29
esa uuuuu | 21 -27 4 -78 0 | 7 14
gfz uuuuu | -6 -33 41 155 10 | -10 15
grg uuuux | 58 -125 333 -24 -79 | 33 54
igr xxxxx | -15 -10 110 -88 2 | -7 15
irf xxxxx | 16 -3 -81 53 8 | -2 11
jpl uuuuu | -40 -7 169 -70 1 | 24 28
mit uuuuu | 23 4 -235 43 2 | 14 18
ngs uuuuu | -89 92 -124 -1 -8 | 8 11
sio uuuuu | 35 112 -63 137 4 | 30 33
Table 7.1647.1 GPS week: 1647 Day: 1 MJD: 55774.500
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 -65 42 31 -3 | 1 16
emr uuxuu | 19 18 -82 34 4 | 29 33
esa uuuuu | -13 -59 93 -128 5 | 8 16
gfz uuuuu | -49 -41 180 16 7 | -7 17
grg uuuux | 23 -62 119 -229 -37 | 32 54
igr xxxxx | -19 -34 -11 -86 2 | -5 16
irf xxxxx | 16 -18 -59 95 4 | 1 14
jpl uuuuu | -29 17 63 -120 -4 | 26 30
mit uuuuu | 31 -14 -235 146 3 | 15 20
ngs uuuuu | -1 85 -140 146 -7 | 9 12
sio uuuuu | 39 108 -88 171 -4 | 33 37
Table 7.1647.2 GPS week: 1647 Day: 2 MJD: 55775.500
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 | -12 -82 19 -102 -8 | 2 16
emr uuxuu | 20 30 -152 45 -4 | 30 34
esa uuuuu | 7 -42 153 -130 0 | 9 18
gfz uuuuu | -90 -32 196 10 2 | -5 17
grg uuuux | -2 -42 101 -198 -18 | 32 54
igr xxxxx | -44 -22 53 -87 4 | -5 17
irf xxxxx | -8 1 -76 -10 -2 | 3 16
jpl uuuuu | 108 -89 73 10 1 | 25 30
mit uuuuu | 2 12 -283 -63 4 | 17 22
ngs uuuuu | 11 76 -259 214 0 | 11 14
sio uuuuu | 1 112 -125 106 -15 | 36 39
Table 7.1647.3 GPS week: 1647 Day: 3 MJD: 55776.500
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 | 23 -23 138 -14 -5 | 2 16
emr uuxuu | 61 25 100 98 11 | 31 35
esa uuuuu | -6 -40 106 -85 10 | 10 19
gfz uuuuu | -38 -67 116 -174 6 | -3 16
grg uuuux | 1 -11 -34 -172 -36 | 32 54
igr xxxxx | 5 -11 60 -22 10 | -4 16
irf xxxxx | 15 -2 -14 -36 -6 | 4 16
jpl uuuuu | -59 -56 141 15 -7 | 26 30
mit uuuuu | 20 24 -164 -81 -1 | 18 23
ngs uuuuu | -4 50 -188 445 -7 | 11 14
sio uuuuu | 36 114 -47 -27 -28 | 37 39
Table 7.1647.4 GPS week: 1647 Day: 4 MJD: 55777.500
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 | -31 -40 -76 -66 -1 | 6 16
emr uuxuu | 56 -11 136 239 14 | 36 39
esa uuuuu | -16 -60 -11 -126 4 | 15 22
gfz uuuuu | -52 -10 -12 -212 0 | 2 15
grg uuuux | -71 -27 -13 -239 39 | 33 55
igr xxxxx | -9 8 103 -57 14 | 1 17
irf xxxxx | 11 0 -71 -34 -5 | 7 16
jpl uuuuu | -52 -17 180 89 -6 | 31 33
mit uuuuu | 11 24 -209 -86 1 | 22 26
ngs uuuuu | 72 38 116 394 0 | 13 16
sio uuuuu | 40 138 -68 -3 -16 | 38 40
Table 7.1647.5 GPS week: 1647 Day: 5 MJD: 55778.500
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 -22 -5 -142 3 | 3 14
emr uuxuu | 39 -46 327 176 11 | 36 40
esa uuuuu | 8 -35 88 10 4 | 15 21
gfz uuuuu | -29 -7 -51 -70 6 | 2 15
grg uuuux | -10 -53 -137 -56 63 | 40 59
igr xxxxx | -21 6 -19 -13 6 | 2 17
irf xxxxx | 5 -6 -35 -95 -4 | 6 15
jpl uuuuu | -78 -32 195 -38 -7 | 30 32
mit uuuuu | -12 6 -162 -229 -3 | 22 25
ngs uuuuu | 37 55 51 290 -6 | 13 15
sio uuuuu | 27 139 -56 -213 -10 | 34 37
Table 7.1647.6 GPS week: 1647 Day: 6 MJD: 55779.500
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 | -10 -48 18 -5 10 | 4 15
emr uuxuu | 69 -19 427 -9 8 | 39 44
esa uuuuu | -21 -19 35 5 1 | 16 24
gfz uuuuu | -65 27 -165 -85 1 | 4 17
grg uuuux | 16 -33 -51 25 -35 | 52 71
igr xxxxx | -57 -4 -112 -25 10 | 4 19
irf xxxxx | 1 9 -5 -48 -3 | 7 16
jpl uuuuu | -40 -62 40 31 12 | 30 32
mit uuuuu | -14 16 -109 -115 -7 | 23 27
ngs uuuuu | 74 -9 161 210 -4 | 13 16
sio uuuuu | 17 146 53 -149 4 | 34 36
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