[IGSREPORT-20514] Wk 1670 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jan 27 05:53:58 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1670 (Jan 08, 2012 - Jan 14, 2012)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi 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:
igs1670[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1670[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1670[0-6].cls IGS GPS clock combination summary report.
igs16707.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16707.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because of poorer consistency (GRG),
they provide broadcast clocks (NGS), or clock corrections are not provided
(SIO). The clock information not used is still compared to combination for
completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
0 | COD | 21 22 23 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7 8
0 | COD | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 25 26
0 | COD | 27 28 29 30 31 32 ALGO ALIC AUCK BREW BRMU BRUS CAS1
0 | COD | CHUR DARW FAIR FLIN GLSV GODE HOB2 HRAO IENG KIRU
0 | COD | KOKB MAC1 MAS1 MATE MAW1 MDVJ MIZU MOBS NICO NTUS
0 | COD | PDEL PRDS PTBB QAQ1 SCH2 STJO SYOG TOW2 TSKB TWTF
0 | COD | USN3 USNO WHIT WSRT WTZR YELL ZECK ALBH ALGO ALIC
0 | COD | ALRT AMC2 AREQ ARTU AUCK BAKO BJFS BOGT BREW BRFT
0 | COD | BRMU BRUS CAS1 CHAT CHUR COCO DARW DAV1 DGAR DRAO
0 | COD | DUBO FAIR FLIN GLSV GODE GOLD GOPE GRAS GRAZ HARB
0 | COD | HNPT HOB2 HOLB HRAO IENG KIRU KOKB LAMA MAC1 MAG0
0 | COD | MAS1 MATE MAW1 MDVJ METS MIZU MOBS NANO NICO NKLG
0 | COD | NRIL NTUS ONSA OPMT PDEL POTS PRDS PTBB QAQ1 RESO
0 | COD | REUN SCH2 SCUB SOFI STHL STJO SUTM SYOG THU3 TIXI
0 | COD | TLSE TOW2 TSKB TWTF ULAB USN3 USNO WAB2 WHIT WILL
0 | COD | WSRT WTZR YAKT YAR2 YELL YSSK ZECK
0 | ESA | KOUR UNSA
0 | GFZ | 14 15 23 26 BRFT COCO HRAO
0 | GRG | KOUR USN3
0 | JPL | 26 AREQ NKLG
0 | MIT | 26 CAS1 MAW1 NYAL
1 | COD | ULAB
1 | EMR | 26 26
1 | ESA | UNSA
1 | GFZ | 13 14 15 23 26 BRFT CEDU DAV1 GMSD HOLB NKLG SCOR
1 | GFZ | STHL WHIT XMIS
1 | GRG | USN3
1 | JPL | 26
1 | MIT | 1 2 3 6 7 19 26 1 2 3 6 7 19 26 WSRT WSRT
2 | EMR | 26 26
2 | ESA | KOUR NKLG
2 | GFZ | 13 14 15 23 26 ALBH BRFT COCO DGAR GODE HOLB KERG
2 | GFZ | KIRU NKLG NRC1 POTS THU3 XMIS
2 | GRG | KOUR USN3
2 | JPL | AREQ
2 | MIT | 1 3 5 10 11 26 1 5 10 11 26 28 NYAL
3 | COD | HNPT
3 | EMR | 3 26 26 MATE
3 | ESA | SCOR UNSA
3 | GFZ | 3 13 14 15 23 26 30 BRFT DGAR HOLB HRAO KERG OHI2
3 | GFZ | WILL
3 | GRG | MATE USN3
3 | JPL | 26 AREQ
3 | MIT | 3 5 8 26 3 5 8 26 CAS1 CAS1 HYDE
4 | EMR | 3 26 3 26
4 | ESA | KOUR NNOR UNSA
4 | GFZ | 3 5 13 14 15 26 AUCK BRFT CEDU DAV1 DGAR OHI2 PDEL
4 | GFZ | WSRT
4 | GRG | AMC2 KOUR USNO
4 | JPL | 3 26 AREQ
4 | MIT | 3 8 26 30 3 5 8 26 30 AUCK CAS1 AUCK CAS1
5 | COD | USNO DAV1 USNO ZECK
5 | EMR | 3 26 3 26 NYAL
5 | ESA | NYAL UNSA
5 | GFZ | 3 5 13 14 23 26 BRFT DGAR HNPT KOUR MATE NYAL OHI2
5 | GFZ | PDEL THTI TIDB WSRT
5 | GRG | AMC2
5 | JPL | 3 AREQ
5 | MIT | 1 3 6 10 11 19 26 30 1 3 6 10 11 19 26 30 CAS1 SYDN
5 | MIT | CAS1 NYAL SYDN
6 | COD | MOBS MOBS WTZR
6 | EMR | 3 6 26 3 6 26
6 | ESA | KOUR WHIT
6 | GFZ | 3 13 14 23 26 30 BRFT PDEL
6 | GRG | AMC2 KOUR
6 | JPL | 3 6 26 AREQ
6 | MIT | 3 6 26 28 1 3 6 26 28 CAS1 CAS1
5. 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 G03 | | | | 1 | | | |
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for the homogeneously reprocessed IGS products from GPS
Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
7. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the current IGS reference frame. These rotations were
estimated in the IGS SINEX combination process, performed by the IGS Reference
Frame Coordinator at the Institut Geographique National (IGN). The estimated 7
transformations, from which only the 3 rotations are applied to the orbit and
ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | -.9 .3 -1.6 -38 -11 11 .14
EMR | 3.5 .7 15.4 7 11 4 .33
ESA | 5.6 6.6 3.9 160 -219 199 .07
GFZ | -1.8 .6 -1.4 -48 35 -3 .12
GRG | 3.4 -4.1 -.9 -12 29 -35 .01
JPL | .0 5.1 9.1 -10 -86 45 .26
MIT | 6.6 .3 1.8 -29 24 -52 .19
NGS | 3.9 2.9 -2.9 24 -39 29 .28
SIO | 3.3 4.9 10.5 58 -50 2 .06
8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN). For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1670.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1670.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 2.1670.[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 3.1670.[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 5.1670.0-6).
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 1670 summary. (Jan 08, 2012 - Jan 14, 2012)
Table 1.1670.a GPS week: 1670 MJD: 55934.000-55940.000
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 6 87 -58 -38 -.36 10 9 | -606 -255 16 68
| 0 0 0 16 16 14 .03 | 543 871
emr 92| 0 0 13 -29 -98 -46 .34 18 18 | 1378 317 14 95
| 1 1 1 26 28 25 .06 | 1114 996
esa 135| 0 1 0 -153 187 104 .08 7 7 | -636 522 13 123
| 0 0 1 6 20 43 .01 | 1447 1704
gfz 190| -1 -1 -4 151 -131 -36 .47 13 13 | 226 -765 34 105
| 0 1 1 85 47 15 .03 | 386 2094
grg 123| 1 0 -6 52 -134 -32 .58 15 14 | -14 -224 51 226
| 0 1 2 13 12 12 .02 | 330 958
igr n/a| 0 0 0 14 -78 -21 -.12 5 5 | -2803 120 20 81
| 0 0 0 15 24 16 .03 | 910 812
jpl 164| 0 -2 1 30 101 22 .44 15 15 | 2353 274 17 83
| 0 1 1 26 19 45 .04 | 1294 827
mit 257| 0 0 -4 102 -124 -35 -.45 13 11 | -164 -144 22 182
| 1 1 0 24 21 23 .01 | 214 795
ngs 213| 0 0 -3 -46 0 -42 -.31 11 9 | -543 -297 2139 3883
| 0 0 1 55 32 15 .07 | 439 732
sio 237| 0 0 2 -90 34 11 -.21 17 16 | --- --- --- ---
| 0 1 0 29 20 15 .03 | --- ---
Table 1.1670.b GPS week : 1670 MJD: 55934.000-55940.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 5 5 4 4 4 5 4 |
2 | 5 5 5 5 5 5 4 |
3 | 5 6 7 6 6 5 5 |
4 | 4 4 5 3 4 3 3 |
5 | 4 4 4 4 5 5 4 |
6 | 4 5 5 4 5 6 6 |
7 | 4 5 4 4 4 4 4 |
8 | 4 4 3 4 4 4 3 |
9 | 4 4 4 4 4 4 4 |
10 | 4 5 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 4 4 4 4 4 3 |
14 | 5 5 4 4 4 4 4 |
15 | 4 5 4 5 5 4 5 |
16 | 5 5 5 4 4 5 5 |
17 | 4 4 4 4 4 4 5 |
18 | 4 5 4 4 4 5 4 |
19 | 4 4 4 4 4 4 4 |
20 | 5 5 5 5 5 5 4 |
21 | 4 5 4 5 5 5 5 |
22 | 5 5 4 5 4 4 5 |
23 | 4 5 5 5 5 5 4 |
25 | 4 4 4 4 4 4 4 |
26 | 7 5 5 5 6 6 6 |
27 | 4 4 4 4 4 4 4 |
28 | 4 5 4 4 4 4 4 |
29 | 5 5 5 5 5 6 5 |
30 | 5 4 4 4 4 4 4 |
31 | 5 5 4 4 4 5 4 |
32 | 4 4 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1670.0 GPS week: 1670 Day: 0 MJD: 55934.000
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| -1 0 6 78 -41 -36 -.31 10 9 | -164 -690 0 0
| 55 -20 |
emr 92| 1 1 14 -45 -107 -34 .36 18 18 | -238 2098 18 103
| 27 15 |
esa 135| 1 0 -1 -149 221 101 .06 7 7 | 168 416 17 122
| 62 -8 |
gfz 190| -1 -2 -4 124 -180 -43 .47 13 13 | -512 826 36 98
| -4 32 |
grg 123| 0 1 -2 57 -143 -21 .59 15 14 | -545 1009 48 214
| 19 -22 |
igr n/a| -1 0 0 11 -40 -6 -.16 5 5 | -3984 1579 24 94
| -31 -6 |
jpl 164| 0 0 0 -6 137 93 .50 18 17 | 824 1599 20 81
| 29 -89 |
mit 257| 1 -2 -4 116 -146 -42 -.45 13 11 | -456 639 22 158
| -30 20 |
ngs 213| -1 0 -2 -20 -4 -63 -.27 9 7 | -304 -525 1771 3358
| -72 -36 |
sio 237| 0 -1 2 -56 23 19 -.26 18 15 | --- --- --- ---
| 70 -26 |
Table 2.1670.1 GPS week: 1670 Day: 1 MJD: 55935.000
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 5 97 -47 -55 -.35 9 9 | -671 -222 20 72
| -1 -22 |
emr 92| 0 2 12 -2 -119 -21 .38 18 18 | 1588 34 15 89
| 10 8 |
esa 135| 0 0 -2 -148 187 127 .09 8 8 | -1633 2858 15 133
| 62 13 |
gfz 190| -1 -3 -2 10 -155 -30 .48 16 15 | 296 191 34 112
| 9 41 |
grg 123| 0 0 -5 67 -121 -34 .58 14 13 | -134 573 57 214
| 1 -39 |
igr n/a| -1 0 0 1 -73 -14 -.11 5 5 | -2620 11 20 78
| 11 35 |
jpl 164| 0 -2 0 23 101 -39 .44 14 14 | 2341 -191 16 80
| 58 -83 |
mit 257| 2 -1 -2 90 -135 -13 -.44 14 12 | -173 388 21 208
| -37 -5 |
ngs 213| -1 1 -2 18 16 -40 -.27 11 9 | -785 -30 2442 3953
| -49 8 |
sio 237| 0 0 3 -107 14 18 -.24 16 15 | --- --- --- ---
| 79 -34 |
Table 2.1670.2 GPS week: 1670 Day: 2 MJD: 55936.000
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| -1 1 5 109 -87 -12 -.35 11 10 | -235 -1274 19 76
| 33 0 |
emr 92| 0 1 14 -9 -122 -13 .42 19 19 | 713 -539 15 90
| 17 -42 |
esa 135| 0 0 1 -164 208 11 .09 7 7 | 1017 -2497 14 121
| 7 14 |
gfz 190| -2 -2 -4 77 -58 -13 .44 13 14 | 244 -4711 38 111
| -25 68 |
grg 123| 1 2 -7 57 -155 -17 .58 16 15 | -70 -771 64 243
| 19 8 |
igr n/a| 0 0 0 32 -116 0 -.09 6 5 | -3385 -498 21 81
| 0 29 |
jpl 164| 0 0 1 34 84 46 .45 14 14 | 1445 -514 18 83
| 45 -115 |
mit 257| 1 -1 -4 104 -122 0 -.43 11 10 | -235 -796 30 225
| -1 -12 |
ngs 213| -1 0 -2 20 -35 -12 -.24 10 9 | -206 -1311 2168 3987
| -38 -9 |
sio 237| 1 0 1 -96 42 38 -.20 16 15 | --- --- --- ---
| 94 -52 |
Table 2.1670.3 GPS week: 1670 Day: 3 MJD: 55937.000
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| -1 1 6 75 -65 -28 -.36 9 8 | 49 -881 17 76
| 21 4 |
emr 92| 2 1 15 -62 -98 -44 .38 19 19 | 709 -471 15 93
| 49 -35 |
esa 135| 0 1 0 -158 178 121 .10 7 7 | -1952 680 14 125
| 12 34 |
gfz 190| 0 0 -6 238 -80 -47 .44 12 11 | 443 -627 35 112
| -50 63 |
grg 123| 1 0 -9 33 -129 -26 .60 15 14 | 492 -1560 50 213
| 30 0 |
igr n/a| 0 1 -1 5 -99 -24 -.11 5 5 | -3378 -647 18 69
| -1 27 |
jpl 164| 1 -3 3 4 90 -12 .48 15 15 | 1425 -349 17 82
| 41 -101 |
mit 257| 0 -1 -3 121 -87 -29 -.45 11 10 | 145 -1145 21 160
| -21 -25 |
ngs 213| -1 0 -3 -89 -31 -36 -.28 10 9 | 2 -660 2299 3819
| 51 39 |
sio 237| 0 0 1 -97 74 -8 -.17 16 15 | --- --- --- ---
| 90 -47 |
Table 2.1670.4 GPS week: 1670 Day: 4 MJD: 55938.000
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 6 98 -60 -42 -.36 10 9 | -1033 -210 19 78
| 6 -16 |
emr 92| 0 0 11 -60 -72 -56 .33 17 17 | 1888 -533 15 93
| 53 -53 |
esa 135| 0 1 0 -152 161 138 .09 7 7 | -1909 829 12 107
| 39 38 |
gfz 190| 0 -1 -4 224 -121 -59 .50 15 16 | 749 -2250 34 106
| -27 17 |
grg 123| 1 0 -6 53 -135 -54 .57 15 15 | 274 -1186 49 245
| 18 -2 |
igr n/a| 0 0 0 33 -88 -47 -.08 5 5 | -2630 -596 19 73
| -19 55 |
jpl 164| 2 -1 2 53 112 -3 .46 15 14 | 2693 -305 17 81
| 14 -111 |
mit 257| 0 -1 -4 105 -121 -42 -.43 12 10 | 76 -1008 23 142
| -20 -12 |
ngs 213| 0 0 -5 -74 -6 -49 -.30 11 8 | -840 -426 2104 3704
| 26 6 |
sio 237| 0 1 2 -84 27 1 -.18 15 14 | --- --- --- ---
| 75 -30 |
Table 2.1670.5 GPS week: 1670 Day: 5 MJD: 55939.000
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| 1 0 6 60 -43 -50 -.41 10 9 | -1511 1430 21 83
| 52 -3 |
emr 92| -1 0 11 -25 -47 -75 .27 18 18 | 1733 1078 12 96
| 1 -73 |
esa 135| 0 1 0 -145 178 131 .07 7 7 | -1522 1844 13 128
| 32 34 |
gfz 190| 0 0 -4 217 -182 -41 .49 13 14 | 294 1423 32 94
| -38 20 |
grg 123| 1 0 -4 34 -133 -40 .55 15 13 | -136 81 45 233
| 35 -16 |
igr n/a| 0 0 0 -7 -69 -28 -.17 5 5 | -2481 660 21 99
| -2 35 |
jpl 164| 0 -3 0 33 103 19 .42 15 14 | 3068 1110 15 73
| 19 -70 |
mit 257| 1 0 -4 123 -150 -51 -.47 13 11 | -347 545 21 177
| -31 8 |
ngs 213| 0 0 -4 -124 62 -47 -.40 12 9 | -1268 1085 2101 4186
| 79 -68 |
sio 237| 0 1 2 -52 17 12 -.23 18 18 | --- --- --- ---
| 73 -24 |
Table 2.1670.6 GPS week: 1670 Day: 6 MJD: 55940.000
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 6 94 -67 -43 -.38 10 8 | -679 56 20 92
| -34 29 |
emr 92| -1 -3 15 0 -118 -81 .28 18 18 | 3255 552 12 104
| -5 -5 |
esa 135| 0 1 3 -153 178 101 .08 6 6 | 1379 -474 12 131
| 3 21 |
gfz 190| -1 0 -6 166 -139 -23 .43 10 10 | 73 -213 29 104
| -88 37 |
grg 123| 1 0 -7 65 -121 -31 .57 15 13 | 16 280 46 226
| 17 -17 |
igr n/a| 0 0 -2 23 -63 -33 -.11 4 4 | -1146 331 19 78
| -15 34 |
jpl 164| 0 -2 1 67 82 55 .38 15 14 | 4676 574 17 101
| -3 -72 |
mit 257| 0 1 -5 53 -111 -70 -.46 13 12 | -163 363 21 206
| 3 2 |
ngs 213| 0 0 -5 -59 3 -47 -.41 11 9 | -403 -213 2093 4178
| 14 20 |
sio 237| 0 3 0 -137 44 -1 -.19 20 18 | --- --- --- ---
| 105 -31 |
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 3.1670.0 GPS week: 1670 Day: 0 MJD: 55934.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 13 5 15 10 6 18 14 8 28 4 | 64 60 71 68 72 67 68 73 67 65 68
2 | 10 16 4 17 13 4 19 10 7 27 4 | 20 25 22 32 22 21 24 26 24 23 21
3 | 9 18 8 14 14 6 14 20 8 14 4 | 41 46 47 45 42 46 47 47 49 43 46
4 | 12 10 7 14 12 7 12 11 6 13 3 | 24 26 32 40 37 28 33 35 30 34 31
5 | 10 13 6 15 11 4 17 8 7 19 4 | 17 25 20 26 27 19 29 18 21 22 20
6 | 9 17 7 14 12 6 15 18 9 13 4 | 25 32 30 31 31 27 34 27 31 30 29
7 | 7 18 7 9 19 4 16 11 8 13 4 | 20 33 25 29 35 22 27 23 24 19 23
8 | 9 12 7 8 13 5 12 9 8 11 3 | 12 22 20 19 20 18 25 17 21 21 20
9 | 8 11 6 13 13 4 13 10 10 15 3 | 19 22 19 23 24 18 26 19 22 16 19
10 | 12 12 6 12 15 6 10 11 8 26 4 | 20 27 30 40 40 30 32 34 29 40 30
11 | 7 19 5 13 14 6 15 17 8 10 4 | 37 40 44 41 52 40 48 46 40 41 42
12 | 10 22 6 14 18 5 20 7 11 14 4 | 16 28 19 27 25 18 31 17 22 19 18
13E | 8 20 6 11 21 5 13 11 11 16 4 | 34 47 37 43 39 38 44 40 37 36 37
14E | 10 17 9 14 14 6 12 29 10 14 5 | 21 27 25 26 29 22 28 22 24 22 23
15E | 8 13 6 16 14 5 21 12 9 16 4 | 33 37 32 40 30 35 41 29 36 30 33
16 | 7 26 10 11 17 5 20 16 11 13 5 | 18 31 21 18 19 17 27 20 24 21 21
17 | 8 21 8 12 16 6 15 9 9 8 4 | 25 38 24 29 36 23 30 21 23 24 24
18 | 8 21 8 17 10 5 15 8 9 20 4 | 22 38 27 41 33 28 40 24 31 26 30
19 | 7 22 10 13 18 4 13 12 10 8 4 | 22 32 23 19 29 22 26 22 25 20 22
20 | 10 20 8 11 10 5 17 15 6 31 4 | 21 32 29 25 30 23 35 23 22 28 26
21 | 7 16 8 12 8 5 12 7 6 31 4 | 19 26 26 26 27 23 28 21 23 22 24
22 | 14 19 9 15 13 6 12 16 5 21 4 | 17 35 28 31 37 24 36 26 25 29 26
23E | 7 22 7 10 13 4 17 9 11 15 4 | 29 39 32 37 37 31 33 35 33 28 32
25 | 12 15 8 9 15 5 20 9 12 11 4 | 18 22 25 26 28 22 32 16 26 20 21
26E | 19 23 9 13 11 6 51 12 11 20 7 | 23 28 26 23 25 27 42 33 34 38 26
X27 | 9 11 7 12 12 7 12 10 9 --- 3 | 13 17 14 17 19 15 19 18 20 --- 15
28 | 7 15 7 14 21 5 16 10 8 13 4 | 13 25 14 20 29 15 26 19 20 16 16
29 | 11 29 8 15 17 6 19 9 11 16 5 | 28 42 26 32 35 25 31 23 26 22 26
X30 | 11 16 9 9 20 6 --- 14 14 --- 5 | 17 25 18 20 21 19 --- 20 24 --- 20
31 | 9 19 7 10 21 4 11 19 8 15 4 | 22 33 23 28 37 23 28 23 23 24 24
32 | 9 16 6 11 13 4 13 6 10 16 3 | 19 24 26 26 32 22 28 27 24 29 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 7 13 15 5 18 13 9 18 |T 23 31 27 30 32 26 33 27 28 27 27
WRMS | 9 18 7 13 14 5 17 11 7 15 |NE 21 30 26 29 31 24 31 25 26 26 25
MEDI | 9 17 7 13 14 5 15 11 9 15 |MD 21 31 26 28 30 23 31 23 24 24 24
Table 3.1670.1 GPS week: 1670 Day: 1 MJD: 55935.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 13 12 20 10 7 19 13 10 21 5 | 46 41 53 48 45 50 46 52 47 39 45
2 | 8 19 7 24 13 4 16 12 7 25 4 | 18 24 19 30 14 17 20 22 16 21 16
3 | 13 17 10 17 18 5 13 27 14 17 5 | 54 55 57 60 54 55 56 56 60 54 56
4 | 9 13 4 17 13 4 9 13 9 14 3 | 32 31 31 34 33 29 35 35 35 35 31
5 | 10 18 8 14 14 6 16 12 9 16 4 | 13 25 15 22 25 14 23 14 15 17 14
6 | 8 18 8 18 10 4 11 22 15 12 4 | 19 32 27 30 29 21 30 25 20 25 23
7 | 6 21 8 15 18 5 14 15 11 12 4 | 18 31 27 27 33 20 29 23 21 22 21
8 | 9 14 5 16 12 5 11 10 10 16 3 | 16 21 17 26 21 16 26 16 15 16 14
9 | 7 14 4 16 12 3 11 12 12 12 3 | 22 26 23 21 26 19 21 20 19 15 20
10 | 13 14 6 13 12 5 9 13 11 24 4 | 21 26 24 29 29 24 28 26 24 34 24
11 | 8 18 8 13 12 7 13 13 11 9 4 | 28 34 36 30 39 32 35 35 31 31 31
12 | 11 22 6 12 21 6 23 14 8 16 5 | 16 28 20 25 28 15 28 16 16 18 17
13E | 7 20 6 14 11 4 12 11 11 13 4 | 20 32 25 27 34 21 26 22 19 23 21
14E | 7 18 11 15 15 6 12 22 11 11 4 | 14 25 23 25 20 18 20 22 22 17 17
15E | 7 20 6 22 17 5 21 11 13 9 4 | 27 30 27 28 26 25 29 28 26 26 24
16 | 6 25 10 12 19 5 18 18 10 14 5 | 14 28 20 17 24 11 24 19 14 15 15
17 | 8 21 8 13 16 3 17 9 11 6 4 | 20 33 23 26 36 20 32 18 19 22 21
18 | 8 20 8 18 11 4 13 9 13 19 4 | 16 34 25 36 29 20 27 19 24 20 22
19 | 7 21 10 14 15 5 12 14 11 7 4 | 19 29 22 18 26 16 23 21 20 19 19
20 | 7 20 6 17 10 6 15 18 10 25 5 | 19 30 28 23 26 22 29 28 23 25 23
21 | 8 17 6 17 7 4 11 10 13 30 4 | 12 26 22 23 22 16 22 17 22 17 17
22 | 12 17 9 20 12 7 11 12 9 19 4 | 16 31 25 28 30 21 29 22 23 20 21
23E | 7 20 12 17 11 4 11 11 15 16 4 | 25 32 30 30 31 26 26 31 29 33 25
25 | 10 16 8 12 15 4 14 11 4 9 3 | 17 25 23 24 29 17 28 19 17 23 19
26E | 16 18 9 19 14 5 21 14 10 12 5 | 20 21 18 17 17 18 25 26 20 25 15
X27 | 7 14 7 18 9 4 11 11 13 --- 4 | 14 22 16 20 19 14 21 17 19 --- 14
28 | 7 18 9 19 21 4 14 9 12 11 4 | 17 27 17 22 34 15 25 18 17 14 15
29 | 10 25 10 17 15 4 18 10 11 16 5 | 26 36 25 31 34 25 27 22 24 21 24
30 | 9 14 7 13 15 5 10 15 11 18 4 | 11 22 19 17 18 10 19 18 15 22 13
31 | 6 17 8 13 19 5 13 14 12 14 4 | 16 27 21 24 33 17 24 18 19 18 18
32 | 8 17 6 15 12 5 15 9 11 14 4 | 15 22 23 20 23 19 23 25 21 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 8 16 14 5 14 14 11 16 |T 20 29 25 27 28 21 27 24 22 23 21
WRMS | 9 18 8 15 13 5 14 12 9 15 |NE 19 28 23 25 28 19 26 22 21 22 20
MEDI | 8 18 8 16 13 5 13 12 11 14 |MD 18 28 23 26 29 19 26 22 20 22 20
Table 3.1670.2 GPS week: 1670 Day: 2 MJD: 55936.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 13 5 14 14 5 18 11 9 16 4 | 55 49 54 56 56 54 52 60 54 50 52
2 | 9 17 7 20 13 5 14 8 10 28 4 | 16 23 17 29 19 17 19 19 20 16 13
3E | 28 22 9 17 18 8 16 25 11 14 6 | 68 82 78 79 79 75 80 80 73 77 75
4 | 9 25 6 24 17 17 8 8 7 14 4 | 24 31 28 32 32 24 30 26 24 27 25
5 | 8 16 7 17 12 7 14 9 12 16 4 | 15 28 18 26 27 17 28 16 20 20 15
6 | 8 17 6 14 13 5 13 21 14 11 4 | 22 34 25 31 27 22 32 24 27 25 23
7 | 6 21 8 10 18 4 14 8 10 11 4 | 19 32 23 23 33 20 25 20 18 17 18
8 | 7 15 4 10 13 4 12 8 9 12 3 | 20 31 21 24 27 21 31 23 23 20 19
9 | 11 16 9 11 12 4 10 10 12 12 4 | 19 27 24 21 21 18 23 23 19 17 17
10 | 14 14 7 8 12 4 9 10 8 23 4 | 24 25 27 32 33 26 28 28 26 36 25
11 | 8 17 6 14 15 5 14 9 13 8 4 | 30 34 32 34 42 32 37 37 32 32 31
12 | 12 21 6 9 23 4 20 11 8 15 4 | 14 28 19 18 26 14 26 17 16 15 12
13E | 7 18 6 11 16 3 11 11 11 11 3 | 23 33 23 29 37 23 31 26 24 24 22
14E | 8 13 8 12 17 4 10 11 15 11 4 | 19 26 25 27 32 20 22 20 20 20 20
15E | 8 20 5 19 15 5 20 10 7 10 4 | 21 26 19 25 22 19 26 23 23 19 16
16 | 9 27 7 10 17 5 16 15 11 15 4 | 17 30 17 16 25 13 25 22 16 15 13
17 | 8 20 6 10 17 4 18 7 7 9 3 | 24 35 23 25 35 23 29 21 18 24 21
18 | 8 20 6 11 13 4 14 7 9 20 4 | 20 34 23 24 32 21 31 21 23 22 20
19 | 7 23 9 12 18 6 10 11 9 7 4 | 21 32 23 19 24 17 21 18 18 18 17
20 | 8 21 6 13 13 5 15 13 9 24 4 | 25 31 22 18 24 20 30 26 19 23 18
21 | 7 16 4 11 11 5 12 9 7 31 4 | 17 26 17 21 23 18 24 20 20 21 16
22 | 15 19 7 13 13 5 13 7 11 16 4 | 17 32 25 29 35 22 30 22 23 24 22
23E | 7 21 7 13 19 4 16 13 11 12 4 | 21 29 22 26 28 20 23 28 24 23 19
25 | 14 13 8 9 21 4 14 10 9 11 4 | 15 23 21 22 27 15 27 19 18 18 15
26E | 15 19 7 15 17 6 19 12 13 11 5 | 19 24 18 18 20 17 25 24 23 20 15
X27 | 8 16 5 12 14 4 11 8 11 --- 3 | 17 26 22 19 21 19 24 18 21 --- 16
28 | 6 20 7 15 21 5 15 10 11 13 4 | 18 32 17 21 32 18 27 19 19 15 15
29 | 11 25 7 14 14 6 17 8 9 16 4 | 23 37 23 29 28 20 27 20 20 20 20
30 | 10 15 6 12 16 4 10 10 10 16 4 | 15 25 17 17 24 16 20 19 18 18 13
31 | 8 18 8 9 18 5 13 9 10 13 4 | 19 29 22 26 39 21 27 22 19 19 19
32 | 7 16 5 10 12 5 10 11 11 14 3 | 20 21 19 19 27 17 24 25 19 24 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 7 13 16 6 14 11 10 16 |T 22 31 24 26 30 22 29 25 23 23 21
WRMS | 10 19 7 14 15 5 14 10 9 15 |NE 21 30 23 25 29 20 27 23 21 22 19
MEDI | 8 18 7 12 15 5 14 10 10 13 |MD 20 30 22 25 27 20 27 22 20 20 18
Table 3.1670.3 GPS week: 1670 Day: 3 MJD: 55937.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 13 5 16 10 5 16 8 10 8 3 | 55 50 54 61 60 56 56 61 51 53 54
2 | 7 17 5 21 11 5 18 9 8 26 4 | 18 25 20 37 21 21 25 22 19 18 18
3E | 16 19 10 13 21 6 20 23 9 24 6 | 130 133 126 132 127 130 133 137 129 131 129
4 | 8 11 5 11 12 5 10 8 9 14 3 | 39 43 43 48 48 45 42 44 45 43 42
5 | 8 18 7 11 10 6 17 8 10 17 4 | 18 29 17 26 27 19 28 17 21 20 18
6 | 8 17 9 10 15 5 13 17 11 10 4 | 21 34 27 29 27 24 31 23 27 23 24
7 | 6 21 7 8 16 3 15 6 12 12 4 | 21 37 26 26 34 21 30 22 19 19 22
8 | 9 12 7 10 13 5 11 7 11 12 3 | 20 30 24 25 24 22 30 23 21 22 21
9 | 9 15 5 11 10 3 12 10 11 14 3 | 17 26 19 18 23 20 22 24 23 18 17
10 | 11 13 6 11 14 6 9 11 9 23 4 | 23 29 27 39 38 32 31 33 30 41 30
11 | 6 19 7 16 13 6 13 8 9 8 3 | 32 37 41 40 46 36 40 40 34 37 36
12 | 10 24 8 14 16 5 23 10 9 14 4 | 17 32 20 25 28 21 31 19 19 20 18
13E | 6 17 7 11 17 5 11 12 13 10 4 | 21 33 24 30 36 25 33 30 26 28 25
14E | 8 18 8 10 12 3 11 9 11 21 4 | 15 25 22 24 24 20 20 19 22 20 18
15E | 8 16 8 12 14 4 19 19 11 14 4 | 35 41 34 37 35 37 41 44 38 39 36
16 | 7 22 7 8 17 5 15 14 8 15 4 | 16 27 17 21 23 15 23 18 14 14 15
17 | 7 23 8 14 16 4 21 7 9 9 4 | 21 41 24 27 35 23 31 21 23 23 22
18 | 8 18 7 14 12 4 18 7 10 21 4 | 20 34 28 37 32 25 33 24 27 26 26
19 | 6 25 8 11 19 5 14 9 8 8 4 | 23 34 19 19 27 19 28 18 22 18 19
20 | 10 20 8 13 11 6 15 12 11 22 4 | 26 34 29 28 33 27 34 30 23 30 26
21 | 7 15 6 10 7 7 17 7 18 34 4 | 16 26 20 23 26 22 24 18 29 18 19
22 | 15 17 7 11 15 5 11 10 11 19 4 | 17 33 29 30 37 26 33 27 25 27 26
23E | 6 20 8 13 12 4 14 16 14 14 4 | 22 33 24 30 30 23 28 32 23 24 24
25 | 9 14 7 8 19 5 13 8 9 8 3 | 16 24 22 20 27 20 28 21 22 21 18
26E | 18 26 9 10 15 6 20 13 12 9 5 | 22 31 18 17 21 21 25 26 28 21 18
X27 | 8 15 6 13 13 5 13 9 12 --- 4 | 17 27 20 21 23 22 28 23 27 --- 20
28 | 7 21 8 15 18 4 15 10 8 13 4 | 14 31 18 23 33 17 27 18 14 14 15
29 | 8 28 10 14 14 10 19 8 8 17 4 | 27 42 25 27 32 23 29 22 24 22 23
30 | 10 15 6 12 16 4 13 10 11 12 4 | 14 24 15 19 23 15 18 18 21 19 15
31 | 5 16 6 10 18 5 12 10 8 13 3 | 20 29 22 25 36 18 25 19 19 19 20
32 | 9 16 6 11 17 6 10 9 10 13 3 | 19 24 26 27 36 23 25 30 23 28 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 7 12 15 5 15 11 10 16 |T 25 35 28 31 34 28 33 29 28 28 27
WRMS | 8 19 7 11 14 5 15 10 9 15 |NE 21 32 25 28 32 24 30 25 24 24 23
MEDI | 8 17 7 11 14 5 14 9 10 14 |MD 20 32 24 27 32 22 29 23 23 22 22
Table 3.1670.4 GPS week: 1670 Day: 4 MJD: 55938.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 13 7 18 13 4 15 12 8 10 4 | 48 46 54 49 52 48 49 56 50 50 50
2 | 8 19 6 20 11 4 15 9 12 25 4 | 15 24 15 26 14 13 17 19 19 17 13
3E | 22 18 10 15 19 7 19 26 15 15 6 | 85 92 90 91 95 92 92 83 95 90 90
4 | 10 10 6 17 13 6 10 7 8 12 3 | 25 29 28 41 32 30 30 31 33 28 28
5 | 8 14 6 26 15 6 17 9 9 17 4 | 13 22 16 29 24 17 26 17 21 16 15
6 | 9 16 8 11 16 5 20 18 12 10 4 | 29 37 32 35 34 30 41 25 37 30 31
7 | 6 20 8 13 14 4 12 8 11 12 4 | 14 31 20 23 28 17 23 16 15 14 17
8 | 10 14 5 9 15 4 9 7 11 10 3 | 13 21 16 22 19 14 21 17 12 17 15
9 | 6 14 6 14 10 4 11 14 9 11 3 | 13 18 15 18 17 12 18 22 12 15 12
10 | 13 14 6 13 11 6 9 9 7 24 4 | 21 24 28 35 32 26 27 28 26 36 25
11 | 7 17 7 13 14 6 12 9 10 8 3 | 28 34 33 31 39 29 36 34 32 31 31
12 | 9 21 6 14 15 3 21 13 11 14 4 | 11 27 11 25 25 13 25 18 15 15 12
13E | 6 14 8 16 13 5 9 15 8 23 4 | 22 30 28 30 30 27 30 26 25 25 26
14E | 7 15 6 14 14 5 8 11 11 14 3 | 11 21 16 23 22 16 19 15 16 20 16
15E | 9 20 7 16 19 5 21 7 12 9 4 | 19 28 20 27 24 18 26 23 25 23 21
16 | 6 21 6 10 18 4 15 12 7 13 4 | 16 26 15 17 19 14 24 15 16 13 15
17 | 6 20 7 13 17 4 20 7 8 6 4 | 21 33 20 26 35 18 30 18 16 20 19
18 | 7 17 6 16 14 3 14 8 8 20 4 | 15 30 21 37 29 21 29 20 21 19 22
19 | 6 22 6 11 22 5 11 7 12 8 4 | 20 29 15 19 29 17 21 14 22 16 16
20 | 9 17 9 15 10 4 13 12 12 21 4 | 16 23 22 17 24 17 26 19 17 20 18
21 | 5 15 7 12 9 5 13 12 8 32 4 | 14 22 17 24 23 14 22 15 18 16 15
22 | 16 16 7 13 14 4 11 7 10 20 4 | 16 31 27 34 35 23 31 23 22 25 24
23E | 6 21 8 17 17 5 15 13 13 9 4 | 10 23 15 21 17 11 17 20 14 13 12
25 | 10 14 4 11 17 4 14 11 16 7 4 | 10 20 15 22 26 14 25 19 17 16 13
26E | 18 21 10 14 19 8 21 21 17 8 6 | 18 23 14 18 15 14 22 27 25 17 15
X27 | 6 15 4 13 11 5 11 12 9 --- 3 | 10 19 12 17 16 13 20 18 12 --- 12
28 | 7 20 8 15 18 4 13 10 9 13 4 | 12 29 16 24 30 14 24 14 10 13 13
29 | 8 21 6 12 18 6 21 13 12 16 4 | 21 35 22 27 34 19 30 18 22 17 21
30 | 8 16 6 12 16 3 12 8 11 11 3 | 13 23 14 16 19 14 19 14 15 17 15
31 | 6 17 6 12 19 7 13 12 8 16 4 | 14 26 17 24 34 17 24 15 16 19 17
32 | 9 15 6 13 13 3 13 8 15 12 3 | 16 22 24 21 27 20 24 24 20 26 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 7 15 15 5 15 12 11 15 |T 19 28 22 28 29 21 28 23 23 23 21
WRMS | 9 17 7 16 15 5 14 10 8 14 |NE 17 26 20 26 27 18 25 21 19 20 19
MEDI | 8 17 6 13 15 5 13 11 11 12 |MD 16 26 17 24 27 17 25 19 19 17 17
Table 3.1670.5 GPS week: 1670 Day: 5 MJD: 55939.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 11 5 15 13 5 18 13 12 16 4 | 40 34 41 38 40 38 35 46 39 36 38
2 | 8 15 5 20 9 4 13 9 9 25 4 | 14 18 16 31 15 14 18 19 22 12 14
3E | 14 13 8 12 20 10 14 20 14 14 5 | 90 95 88 94 94 91 93 90 90 91 91
4 | 8 10 3 11 12 5 9 9 9 12 3 | 30 33 34 39 38 32 36 33 39 34 34
5 | 8 18 8 24 12 5 18 12 9 22 5 | 12 24 18 30 23 14 27 16 20 17 16
6 | 28 19 9 11 19 7 17 21 12 16 6 | 26 48 43 48 46 35 50 43 32 35 36
7 | 6 20 6 11 16 3 14 8 10 12 4 | 13 25 20 24 29 16 23 19 16 14 17
8 | 10 12 7 9 16 5 12 10 11 11 3 | 14 19 21 24 21 16 25 20 19 16 18
9 | 7 12 5 11 11 5 10 16 10 13 3 | 12 17 12 18 16 12 17 21 14 14 13
10 | 12 13 6 11 10 3 9 12 6 30 4 | 18 25 26 34 29 23 26 28 24 40 25
11 | 7 17 5 11 14 7 12 10 13 13 3 | 23 30 27 25 32 24 30 30 25 27 26
12 | 9 27 8 16 16 6 25 13 12 14 5 | 12 33 17 27 23 13 29 18 18 15 15
13E | 7 18 7 12 15 3 8 13 12 14 4 | 15 25 18 25 22 17 22 24 18 22 18
14E | 7 16 7 10 12 3 11 12 10 14 3 | 10 23 20 23 17 17 16 17 17 15 17
15E | 8 20 5 12 10 5 20 9 13 11 4 | 28 29 26 32 28 26 31 27 26 26 26
16 | 9 19 9 10 17 4 15 12 15 15 4 | 13 24 17 19 19 13 22 17 15 13 15
17 | 7 16 6 13 16 5 19 8 14 8 4 | 18 28 18 27 33 15 30 17 16 19 18
18 | 9 19 7 15 12 4 15 10 12 20 4 | 16 32 23 40 28 22 29 24 21 21 24
19 | 6 20 8 10 18 4 10 7 14 13 4 | 17 27 18 19 25 16 22 15 20 16 16
20 | 10 16 6 12 11 6 11 15 9 27 4 | 18 24 20 20 22 18 24 22 15 23 18
21 | 7 16 6 14 8 5 14 12 16 33 5 | 13 24 18 27 23 16 21 17 24 17 18
22 | 12 16 7 7 13 4 11 8 12 23 4 | 15 31 25 31 31 20 30 21 20 27 24
23E | 7 21 7 14 15 5 12 17 11 10 4 | 13 23 14 21 19 12 16 24 15 16 14
25 | 9 16 8 8 17 3 11 11 13 13 4 | 16 27 22 22 24 16 25 19 22 14 17
26E | 17 19 8 10 17 7 19 22 16 12 5 | 17 21 17 16 13 17 21 27 21 15 15
X27 | 7 15 4 10 11 7 --- 11 9 --- 3 | 10 21 14 19 17 14 --- 20 19 --- 15
28 | 6 18 7 12 18 5 16 11 8 16 4 | 11 29 16 24 30 14 24 16 14 12 15
29 | 8 27 11 9 15 5 21 16 17 17 5 | 18 32 24 27 30 19 24 21 16 17 18
X30 | 9 16 6 11 13 4 --- 10 13 14 4 | 12 24 16 19 18 12 --- 15 12 15 14
31 | 7 19 8 12 21 6 13 14 12 19 4 | 16 29 21 26 37 16 25 18 17 19 20
32 | 8 13 7 9 14 6 14 11 13 17 4 | 13 17 16 17 20 14 17 22 12 23 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 7 13 15 5 15 13 12 18 |T 19 28 23 28 27 20 27 24 22 22 21
WRMS | 9 18 7 14 13 5 14 11 9 18 |NE 16 26 20 26 25 17 25 21 19 20 19
MEDI | 8 16 7 11 14 5 14 12 12 14 |MD 15 25 20 25 24 16 25 21 19 17 18
Table 3.1670.6 GPS week: 1670 Day: 6 MJD: 55940.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 13 4 12 9 2 19 11 9 27 4 | 66 60 67 70 67 67 66 75 66 70 66
2 | 9 18 5 16 11 5 13 8 10 26 4 | 20 26 21 34 23 21 24 24 25 20 21
3E | 13 14 7 11 21 5 18 12 15 10 4 | 87 92 91 92 93 89 94 91 84 92 89
4 | 8 10 3 9 12 5 8 9 11 14 3 | 33 35 38 43 46 37 41 40 38 34 38
5 | 6 17 6 9 9 5 15 12 10 23 3 | 16 24 21 28 27 21 29 21 21 22 20
6E | 23 25 9 13 24 8 19 14 13 30 6 | 67 81 68 71 74 68 76 70 74 70 70
7 | 8 20 6 8 11 4 14 9 9 12 3 | 17 28 21 23 27 18 23 17 21 17 19
8 | 8 12 7 8 13 4 9 13 7 9 3 | 14 22 18 23 22 15 23 20 14 16 16
9 | 8 15 5 9 11 4 10 13 8 13 3 | 16 22 14 20 20 14 18 21 17 14 14
10 | 8 15 4 8 11 6 7 13 12 28 4 | 29 32 33 41 40 35 35 39 34 46 34
11 | 11 18 5 8 14 6 14 10 9 12 3 | 37 36 38 43 46 38 43 44 38 40 38
12 | 10 25 6 12 14 4 27 13 9 12 4 | 13 30 13 20 23 12 29 15 15 14 12
13E | 6 14 4 10 11 3 9 13 10 11 3 | 21 26 23 25 30 22 26 27 24 25 22
14E | 9 21 6 9 13 3 9 16 10 15 4 | 11 21 18 24 22 14 18 16 17 19 16
15E | 8 25 5 13 12 4 23 8 11 13 4 | 23 26 18 26 24 20 27 22 21 21 19
16 | 5 24 6 12 16 4 15 14 14 15 4 | 14 26 17 17 20 12 23 21 18 19 14
17 | 6 17 8 9 16 4 21 16 12 12 4 | 23 33 24 26 38 21 33 24 18 25 23
18 | 8 17 5 16 15 4 12 10 9 23 4 | 21 30 24 40 32 24 30 22 21 22 23
19 | 9 21 7 10 19 3 12 8 12 15 4 | 24 31 22 22 29 19 22 19 23 21 19
20 | 8 18 4 9 10 4 12 11 11 31 4 | 25 31 27 27 29 25 31 30 22 35 25
21 | 9 17 6 10 8 4 15 13 12 33 4 | 15 23 19 23 25 15 23 17 19 19 16
22 | 11 18 7 11 11 4 13 9 10 36 4 | 21 33 30 37 38 26 34 27 24 37 27
23E | 7 22 7 10 19 3 13 15 8 12 4 | 20 27 21 25 20 20 25 26 21 22 19
25 | 8 13 5 7 17 4 15 11 10 16 3 | 15 21 17 19 24 16 26 15 18 17 16
26E | 17 19 7 11 20 4 18 24 15 22 5 | 16 21 16 12 13 14 19 28 22 19 12
X27 | 8 14 6 10 12 5 10 11 9 --- 3 | 12 22 15 22 19 14 23 21 16 --- 14
28 | 9 20 5 10 17 3 13 17 10 13 4 | 13 29 15 24 30 14 24 20 12 14 15
29 | 9 24 8 7 13 6 22 17 9 18 4 | 25 37 24 27 31 23 29 24 17 24 22
30 | 6 13 5 9 14 3 8 11 13 16 3 | 14 23 17 16 21 14 18 19 14 21 13
31 | 7 19 7 7 17 6 12 16 10 18 4 | 20 28 25 27 37 20 24 22 18 21 21
32 | 8 17 5 6 14 5 16 13 11 21 4 | 24 26 28 29 36 27 30 32 23 36 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 10 15 4 15 13 11 20 |T 24 32 27 31 33 25 31 29 26 29 25
WRMS | 8 18 6 10 13 4 14 12 9 18 |NE 21 29 24 29 31 22 29 26 23 26 23
MEDI | 8 18 6 10 13 4 13 13 10 15 |MD 20 28 21 26 29 20 26 22 21 21 20
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1670 GPS week: 1670 MJD: 55934.0-55940.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 |U 10 7 22 |U 10 11 36 |U 10 12 28 |
emr | emr 2970 | 10 8 29 |U 11 12 45 | 15 17 29 |
esa | esa 2976 | 9 7 23 |U 10 11 40 | 9 13 28 |
gfz | gfz 2968 |U 12 9 26 |U 11 20 79 |U 10 14 28 |
grg | grg 2976 | 9 9 34 |U 10 11 42 | 13 18 34 |
igr | igr 2975 | 9 7 23 | 9 10 40 | 9 13 28 |
igs | igs 2915 | 8 7 24 | 10 11 43 | 10 13 26 |
jpl | jpl 2926 |U 9 7 27 |U 10 12 42 | 10 27 34 |
mit | mit 2976 |U 9 8 30 |U 10 11 44 |U 15 20 36 |
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 5.1670.0 GPS week: 1670 Day: 0 MJD: 55934.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 7 17 | 6 8 24 | 25 28 86 |
emr | emr 2972 | 11 9 25 | 8 10 28 | 44 39 81 |
esa | esa 2976 | 9 7 16 | 7 9 28 | 15 31 86 |
gfz | gfz 2971 | 17 14 28 | 10 12 40 | 18 32 91 |
grg | grg 2976 | 9 7 32 | 6 9 30 | 18 29 96 |
igr | igr 2975 | 8 6 20 | 6 7 26 | 21 30 93 |
igs | igs 2941 | 8 7 21 | 7 8 31 | 27 31 80 |
jpl | jpl 2871 | 14 7 32 | 8 9 29 | 16 101 106 |
mit | mit 2976 | 10 6 33 | 7 12 34 | 27 29 72 |
Table 5.1670.1 GPS week: 1670 Day: 1 MJD: 55935.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 8 28 | 8 7 28 | 9 14 19 |
emr | emr 2972 | 13 8 41 | 11 9 76 | 13 17 23 |
esa | esa 2976 | 9 8 26 | 8 8 55 | 10 14 18 |
gfz | gfz 2971 | 9 9 30 | 6 23 38 | 10 15 21 |
grg | grg 2976 | 11 8 40 | 8 9 57 | 17 21 30 |
igr | igr 2976 | 9 8 28 | 7 8 58 | 10 14 18 |
igs | igs 2929 | 8 6 27 | 8 8 76 | 11 15 20 |
jpl | jpl 2969 | 9 6 33 | 7 8 54 | 15 18 27 |
mit | mit 2976 | 9 7 35 | 7 9 70 | 13 17 20 |
Table 5.1670.2 GPS week: 1670 Day: 2 MJD: 55936.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 6 23 | 10 12 24 | 7 9 26 |
emr | emr 2972 | 10 8 25 | 10 12 33 | 11 13 22 |
esa | esa 2976 | 9 9 28 | 9 9 24 | 7 9 27 |
gfz | gfz 2971 | 9 9 30 | 10 19 88 | 7 11 24 |
grg | grg 2976 | 10 14 40 | 8 8 26 | 9 17 29 |
igr | igr 2976 | 9 8 27 | 9 9 24 | 7 8 27 |
igs | igs 2927 | 8 8 25 | 9 10 25 | 7 9 24 |
jpl | jpl 2972 | 8 7 22 | 9 11 30 | 8 14 24 |
mit | mit 2976 | 12 14 35 | 12 14 33 | 18 22 46 |
Table 5.1670.3 GPS week: 1670 Day: 3 MJD: 55937.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 24 12 18 | 12 11 48 | 8 9 17 |
emr | emr 2970 | 9 7 20 | 12 12 45 | 10 13 18 |
esa | esa 2976 | 9 5 17 | 11 11 47 | 7 8 17 |
gfz | gfz 2967 | 8 5 16 | 12 21 94 | 10 10 21 |
grg | grg 2976 | 7 4 18 | 13 13 53 | 8 16 19 |
igr | igr 2976 | 8 6 15 | 11 11 46 | 6 8 13 |
igs | igs 2908 | 9 6 17 | 12 12 44 | 7 6 16 |
jpl | jpl 2964 | 10 5 17 | 13 11 49 | 8 15 18 |
mit | mit 2976 | 7 6 17 | 11 11 48 | 8 15 21 |
Table 5.1670.4 GPS week: 1670 Day: 4 MJD: 55938.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 28 | 10 13 47 | 6 9 18 |
emr | emr 2968 | 9 6 33 | 10 13 48 | 10 9 18 |
esa | esa 2976 | 10 8 29 | 10 11 48 | 8 9 20 |
gfz | gfz 2968 | 13 7 26 | 12 24 107 | 7 8 18 |
grg | grg 2976 | 11 13 38 | 11 11 46 | 15 17 20 |
igr | igr 2976 | 9 8 30 | 10 11 49 | 7 9 18 |
igs | igs 2877 | 10 9 27 | 10 13 45 | 6 8 16 |
jpl | jpl 2963 | 8 6 28 | 14 15 54 | 9 17 24 |
mit | mit 2976 | 9 9 31 | 10 11 42 | 8 14 19 |
Table 5.1670.5 GPS week: 1670 Day: 5 MJD: 55939.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 22 | 9 12 34 | 6 9 13 |
emr | emr 2968 | 9 7 25 | 9 11 41 | 8 16 24 |
esa | esa 2976 | 9 7 19 | 9 10 34 | 6 10 14 |
gfz | gfz 2967 | 9 6 20 | 11 19 105 | 7 10 14 |
grg | grg 2976 | 10 9 35 | 9 12 31 | 11 17 23 |
igr | igr 2976 | 8 7 18 | 9 10 34 | 6 11 14 |
igs | igs 2921 | 7 7 21 | 8 10 33 | 7 11 13 |
jpl | jpl 2776 | 8 7 31 | 9 11 34 | 7 15 19 |
mit | mit 2976 | 10 6 25 | 8 9 30 | 17 28 45 |
Table 5.1670.6 GPS week: 1670 Day: 6 MJD: 55940.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 5 20 | 14 17 47 | 6 8 14 |
emr | emr 2968 | 11 8 36 | 15 21 46 | 7 10 18 |
esa | esa 2976 | 10 6 25 | 13 17 47 | 7 9 15 |
gfz | gfz 2962 | 17 11 30 | 15 25 82 | 7 10 10 |
grg | grg 2976 | 9 7 32 | 13 16 48 | 11 12 23 |
igr | igr 2976 | 9 6 26 | 13 17 44 | 6 10 15 |
igs | igs 2905 | 8 6 28 | 14 16 46 | 7 8 12 |
jpl | jpl 2967 | 9 8 26 | 14 18 44 | 8 11 17 |
mit | mit 2976 | 9 7 38 | 15 15 49 | 13 17 31 |
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 6.1670 GPS week: 1670 MJD: 55934.500-55940.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -3 -5 23 74 -2 | 10 22
| 13 29 77 50 2 | 2
emr uuuuu | 19 -8 45 9 2 | 34 41
| 33 19 66 68 5 | 2
esa uuuuu | -28 -17 93 -17 -3 | -7 20
| 15 23 54 44 2 | 2
gfz uuuuu | -47 45 -3 -68 -4 | 13 22
| 19 28 131 50 3 | 3
grg uuuux | 6 -6 -21 -26 -5 | 21 38
| 16 13 29 88 24 | 10
igr xxxxx | -37 22 91 35 -3 | 1 19
| 18 14 37 53 7 | 2
irf xxxxx | -7 14 -11 -20 -2 | 2 19
| 7 9 28 29 5 | 2
jpl uuuuu | 85 -15 -37 -67 3 | 9 24
| 19 19 110 95 5 | 2
mit uuuuu | -4 33 -164 -74 2 | 7 20
| 19 23 37 108 2 | 1
ngs uuuuu | -1 12 -2 115 -2 | 3 17
| 31 53 173 119 8 | 1
sio uuuuu | 28 -70 64 164 3 | 27 34
| 14 20 47 79 17 | 3
Table 7.1670.0 GPS week: 1670 Day: 0 MJD: 55934.500
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 | 7 -46 -51 48 -3 | 11 20
emr uuuuu | -28 -18 34 100 1 | 34 40
esa uuuuu | -5 -53 73 68 -3 | -5 17
gfz uuuuu | -45 13 152 -13 -5 | 15 21
grg uuuux | 9 -10 -33 77 -38 | 40 59
igr xxxxx | -7 40 51 90 -5 | 4 15
irf xxxxx | -13 9 -8 -20 -9 | 4 17
jpl uuuuu | 76 -20 69 45 7 | 12 24
mit uuuuu | -33 39 -133 -155 -1 | 7 18
ngs uuuuu | 23 81 -139 -91 4 | 2 12
sio uuuuu | 13 -61 70 62 -21 | 32 36
Table 7.1670.1 GPS week: 1670 Day: 1 MJD: 55935.500
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 20 143 70 -1 | 10 20
emr uuuuu | -17 9 147 12 4 | 34 40
esa uuuuu | -22 -43 187 -53 -3 | -6 18
gfz uuuuu | -50 10 124 -88 -5 | 15 21
grg uuuux | 30 18 -14 96 -30 | 31 53
igr xxxxx | -44 8 76 65 -15 | 3 16
irf xxxxx | -9 19 15 -71 -4 | 3 17
jpl uuuuu | 74 -39 -98 24 -5 | 10 23
mit uuuuu | -4 56 -223 -279 4 | 7 18
ngs uuuuu | -17 68 -217 233 4 | 2 12
sio uuuuu | 25 -60 97 74 -13 | 30 35
Table 7.1670.2 GPS week: 1670 Day: 2 MJD: 55936.500
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 | -11 -25 30 176 0 | 10 20
emr uuuuu | 31 -9 23 98 9 | 35 40
esa uuuuu | -25 1 60 -47 -7 | -7 19
gfz uuuuu | -79 33 107 -153 -4 | 13 21
grg uuuux | -19 -11 12 -163 -17 | 18 42
igr xxxxx | -40 8 151 -42 -5 | 0 19
irf xxxxx | -11 8 11 -40 -6 | 2 19
jpl uuuuu | 104 -37 -49 -182 -3 | 9 24
mit uuuuu | 1 9 -152 -41 -1 | 7 18
ngs uuuuu | -2 46 -35 275 6 | 1 13
sio uuuuu | 41 -86 57 208 -7 | 27 35
Table 7.1670.3 GPS week: 1670 Day: 3 MJD: 55937.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -3 -2 20 94 -2 | 13 25
emr uuuuu | 36 -30 77 -48 6 | 39 47
esa uuuuu | -33 7 16 11 -4 | -5 21
gfz uuuuu | -62 69 -11 -65 -10 | 15 25
grg uuuux | 1 -11 14 -53 19 | 11 28
igr xxxxx | -26 20 129 12 -3 | 2 22
irf xxxxx | 1 19 9 13 -4 | 4 21
jpl uuuuu | 102 -22 87 -195 7 | 10 26
mit uuuuu | 26 40 -112 -1 0 | 10 23
ngs uuuuu | -38 -32 -39 83 5 | 5 20
sio uuuuu | 48 -71 85 244 2 | 29 37
Table 7.1670.4 GPS week: 1670 Day: 4 MJD: 55938.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 8 16 -63 59 -4 | 9 22
emr uuuuu | 45 -31 67 -73 -2 | 34 40
esa uuuuu | -46 -17 101 -10 0 | -9 21
gfz uuuuu | -25 49 -108 -97 -1 | 11 22
grg uuuux | -6 4 -29 -57 6 | 13 29
igr xxxxx | -63 41 95 81 6 | -1 21
irf xxxxx | -8 22 -29 -21 1 | -1 19
jpl uuuuu | 103 8 29 -71 7 | 7 23
mit uuuuu | 4 42 -173 30 2 | 6 20
ngs uuuuu | -14 -4 -34 80 -11 | 3 19
sio uuuuu | 22 -53 92 139 13 | 24 31
Table 7.1670.5 GPS week: 1670 Day: 5 MJD: 55939.500
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 -31 -19 39 -5 | 9 22
emr uuuuu | 60 20 38 6 -5 | 34 40
esa uuuuu | -47 -11 87 -46 -2 | -9 21
gfz uuuuu | -33 59 -164 -42 -4 | 11 22
grg uuuux | 3 -14 -72 -34 22 | 16 29
igr xxxxx | -48 23 60 64 4 | -1 21
irf xxxxx | -13 21 -64 -6 5 | 0 19
jpl uuuuu | 57 2 -62 -11 3 | 9 23
mit uuuuu | -21 52 -192 -60 3 | 7 20
ngs uuuuu | 55 -58 283 129 -8 | 3 19
sio uuuuu | 11 -52 -38 159 22 | 24 31
Table 7.1670.6 GPS week: 1670 Day: 6 MJD: 55940.500
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 | -25 32 100 30 2 | 7 22
emr uuuuu | 9 3 -71 -30 -1 | 32 39
esa uuuuu | -17 -5 129 -43 -3 | -10 22
gfz uuuuu | -33 86 -117 -15 0 | 9 22
grg uuuux | 21 -19 -25 -48 4 | 18 30
igr xxxxx | -30 13 76 -25 -4 | -2 21
irf xxxxx | 4 -2 -7 9 5 | -1 19
jpl uuuuu | 76 1 -230 -75 4 | 8 23
mit uuuuu | 2 -5 -162 -8 4 | 7 20
ngs uuuuu | -16 -16 169 95 -13 | 2 20
sio uuuuu | 35 -107 85 262 24 | 25 32
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