[IGSREPORT-24546] Wk 1900 IGS Final Orbits
IGS ACC
acc at igs.org
Sat Jun 25 18:47:36 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1900 (Jun 05, 2016 - Jun 11, 2016)
Contacts: acc at igs.org
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 at each SP3 epoch. 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 with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations 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 over each daily arc. 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 10 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:
igs1900[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1900[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1900[0-6].cls IGS GPS clock combination summary report.
igs19007.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19007.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
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 | NKLG NKLG TRO1
0 | EMR | SYOG
0 | ESA | MAL2 MAL2
0 | GFZ | 32 32 ALGO DRAG IRKJ MAL2 THU3 TONG ALGO DRAG IRKJ
0 | GFZ | MAC1 MAL2 THU3 TONG
0 | GRG | HARB MAC1 NRMD POTS CCJ2 HARB MAC1 NRMD POTS
0 | MIT | IRKJ MAC1 SYOG IRKJ MAC1 SYOG
1 | COD | 29 DUBO
1 | EMR | SCH2 TWTF
1 | ESA | DUBO DUBO MAW1
1 | GFZ | 32 32 ALGO BJNM FAA1 IRKJ MAW1 NKLG POHN THU3 TONG
1 | GFZ | TWTF ALGO BJNM IRKJ MAW1 NKLG POHN THU3 TONG TWTF
1 | GRG | HARB NLIB RABT
1 | JPL | MAC1 SCH2 TUVA
1 | MIT | MAC1 MAC1
2 | COD | DAV1 SYOG
2 | EMR | YAKT
2 | ESA | 21 22 29 ARTU FAA1 ARTU FAA1 TIXI
2 | GFZ | 21 32 21 32 ALGO ARTU FAA1 IRKJ ONSA POHN QAQ1 THU3
2 | GFZ | TONG FAA1 IRKJ ONSA POHN QAQ1 THU3 TONG
2 | GRG | MAW1 HARB MAW1 SYOG
2 | JPL | TUVA
2 | MIT | JPLM ONSA QAQ1 JPLM ONSA QAQ1
3 | COD | SYOG
3 | ESA | MAL2 MAL2
3 | GFZ | 32 32 BJNM BRFT DRAO FAA1 POHN TONG TWTF BJNM DRAO
3 | GFZ | FAA1 POHN TONG TWTF
3 | GRG | ARTU HARB ARTU HARB LPGS WIND
3 | JPL | BRFT TUVA
4 | ESA | MAL2 SFER MAL2 SFER
4 | GFZ | 32 25 32 ALGO IRKJ MAL2 NANO POHN TONG MAL2 NANO
4 | GFZ | POHN SANT TONG
4 | GRG | FAA1 HARB NANO FAA1 HARB NANO NNOR
5 | COD | FAA1 MAL2
5 | EMR | SFER
5 | GFZ | 32 32 ALGO BJNM FAA1 IRKJ POHN SYOG TONG ALGO BJNM
5 | GFZ | IRKJ NRMD POHN SYOG TONG
5 | GRG | HARB MAW1 SYOG ARTU MAW1 SYOG
6 | COD | BJNM BOGT
6 | EMR | BJNM THU3 THU3
6 | ESA | BJNM SYOG SYOG
6 | GFZ | 32 32 ALGO ARTU IRKJ MAL2 NLIB STHL SYOG TONG BOGT
6 | GFZ | IRKJ MAL2 SYOG TONG
6 | GRG | 13 13 COCO MAL2 COCO HRAO MAL2 SYOG
5. 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 AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
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.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
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 RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. 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 | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.8 -2.3 -.8 -75 -14 5 .80
EMR | 0 | -9.1 -7.9 12.6 71 -5 29 .64
ESA | 0 | -.5 -1.7 -.5 -2 -39 22 .47
GFZ | 0 | .2 -.7 -.8 -57 -79 -35 .61
GRG | 0 | -2.1 -5.5 4.5 -28 -84 62 .47
JPL | 0 | .8 -10.2 3.1 -22 -5 30 .47
MIT | 0 | -.7 -9.5 13.1 3 -9 -21 .85
NGS | 0 | .9 -10.5 22.0 -138 -18 -12 .67
SIO | 0 | -4.3 -10.1 19.7 -23 -7 -15 .40
COD | 1 | -.4 -2.3 -.9 -51 -10 -31 .86
EMR | 1 | 2.2 -4.0 .1 55 -45 34 .62
ESA | 1 | -1.0 -1.3 -1.0 0 -27 11 .44
GFZ | 1 | .2 -.7 -1.6 -44 -68 -27 .58
GRG | 1 | 3.8 -2.0 11.1 -16 -80 52 .17
JPL | 1 | -1.2 -5.2 6.2 -32 -4 33 .39
MIT | 1 | -.6 -7.2 11.3 0 -5 -32 .77
NGS | 1 | -1.8 -9.1 16.5 -118 -6 -53 .83
SIO | 1 | -1.3 -4.3 6.1 -4 -24 22 .52
COD | 2 | -.7 -2.4 -1.4 -56 9 -42 .75
EMR | 2 | -4.6 -2.1 14.7 71 -64 43 .48
ESA | 2 | -.9 -2.1 -.4 -9 -35 51 .35
GFZ | 2 | .1 -.8 -1.2 -43 -80 -8 .67
GRG | 2 | 2.1 -.0 2.6 -5 -54 68 .35
JPL | 2 | 3.9 -2.6 4.6 -43 18 -8 .54
MIT | 2 | -1.0 -7.8 8.9 -8 0 -67 .69
NGS | 2 | -1.7 -6.4 11.7 -71 -31 -16 .61
SIO | 2 | -2.7 -3.1 6.2 -21 -5 -10 .61
COD | 3 | -.1 -2.0 -.8 -57 -3 -41 .62
EMR | 3 | -3.4 -2.1 11.7 78 -51 43 .44
ESA | 3 | -.3 -1.8 -.8 -5 -12 33 .24
GFZ | 3 | .2 -.9 -1.4 -46 -66 -13 .73
GRG | 3 | 2.1 -3.0 2.3 -8 -61 77 .22
JPL | 3 | -4.1 -3.2 -.3 -12 1 -35 .28
MIT | 3 | -.8 -4.8 8.0 -5 -1 -61 .75
NGS | 3 | 1.4 -4.8 10.3 -63 -34 -2 .55
SIO | 3 | -.9 -5.8 4.3 -37 -21 12 .63
COD | 4 | -.6 -1.4 -.4 -44 -21 -54 .72
EMR | 4 | -2.5 1.4 4.3 38 -8 -6 .42
ESA | 4 | -1.0 -2.0 -.3 -13 -14 37 .47
GFZ | 4 | .0 -.6 -1.7 -36 -95 -6 .82
GRG | 4 | 1.7 -2.4 -1.3 -15 -39 72 .27
JPL | 4 | .1 -3.8 4.9 -10 4 -11 .51
MIT | 4 | -2.8 -2.1 11.8 26 -21 -23 .75
NGS | 4 | -3.2 -7.6 12.5 -55 -44 -34 .58
SIO | 4 | .3 -2.0 -1.0 -16 -33 -16 .89
COD | 5 | -.9 -2.0 -.7 -64 -15 -26 .67
EMR | 5 | -3.3 -3.6 5.3 82 -15 51 .57
ESA | 5 | -1.0 -1.2 -.6 3 -23 34 .54
GFZ | 5 | .8 -2.0 -1.1 -69 -102 -3 .57
GRG | 5 | 5.9 -3.3 .1 -25 -71 93 .45
JPL | 5 | -2.3 -3.6 6.8 -31 -4 11 .46
MIT | 5 | -1.0 -2.7 6.2 3 1 -34 .73
NGS | 5 | -8.0 -5.6 6.2 -35 11 -66 .75
SIO | 5 | -1.7 -2.8 -7.5 -46 -17 2 .48
COD | 6 | -.6 -1.5 -.9 -40 -16 -10 .77
EMR | 6 | -3.6 3.7 -3.8 67 -22 28 .34
ESA | 6 | -.7 -1.5 -.0 -11 -23 28 .47
GFZ | 6 | .3 -1.7 -2.1 -52 -83 -22 .59
GRG | 6 | 3.1 -4.6 -4.8 -15 -63 95 -.07
JPL | 6 | -4.1 -6.5 .6 -9 -19 59 .52
MIT | 6 | -.6 -1.9 5.8 23 3 -54 .72
NGS | 6 | -5.2 1.7 -.9 27 2 -38 .62
SIO | 6 | -1.6 -3.8 -7.8 -7 -13 -3 .47
8. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
9. 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; from GPS Week 1632 through 1648 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 seven 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 1.1900.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1900.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 2.1900.[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 3.1900.[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 part,
Table 5, is similar to Table 4 and contains daily precise navigation
statistics (Tables 5.1900.0-6). The sixth part, Table 6, is a weekly
summary of daily ERP combination statistics. The seventh part, Table 7,
contains the daily ERP statistics. But this is not the IGS official ERP
combination products (which come from the accompanying SINEX combination)
but provided to check combination consistency, etc.
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 1900 summary. (Jun 05, 2016 - Jun 11, 2016)
Table 1.1900.a GPS week: 1900 MJD: 57544.000-57550.000
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 244| 0 0 0 12 -2 1 .14 11 10 | -1265 140 13 157
| 0 0 2 20 18 10 .04 | 173 516
emr 80| -1 0 0 -1 -20 7 .28 10 10 | 2678 315 16 131
| 1 1 1 11 14 12 .03 | 750 483
esa 150| 0 0 -4 12 2 1 -.41 7 8 | -690 103 8 177
| 0 0 0 10 7 17 .03 | 470 1284
gfz 209| 0 0 2 -3 -4 -27 .13 11 10 | -210 45 10 137
| 0 0 0 15 13 20 .02 | 314 472
grg 114| 1 0 0 -31 67 33 -.25 15 13 | -30 142 12 184
| 0 1 4 11 29 17 .14 | 133 198
jpl 80| -1 0 0 5 -1 9 .30 9 9 | 1184 453 15 118
| 1 0 1 12 28 27 .03 | 892 576
mit 349| 2 0 5 -17 -17 -2 -.17 13 12 | -132 43 44 360
| 0 0 0 25 30 19 .03 | 230 268
ngs 226| 0 1 2 1 5 -4 .08 10 9 | -1252 131 795 1964
| 0 0 3 15 23 12 .08 | 311 616
sio 306| 0 0 -2 -6 -9 -5 -.03 14 14 | --- --- --- ---
| 0 1 1 16 45 22 .05 | --- ---
Table 1.1900.b GPS week : 1900 MJD: 57544.000-57550.000
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 | 3 3 3 3 3 3 3 |
2 | 4 4 4 4 4 4 4 |
3 | 3 3 3 3 3 3 3 |
4 | 0 0 0 0 0 0 0 |
5 | 3 4 3 4 4 4 3 |
6 | 3 3 3 3 3 3 3 |
7 | 4 4 4 4 5 4 4 |
8 | 6 5 4 4 4 4 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 4 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 5 4 4 4 5 4 |
15 | 4 4 4 4 4 4 4 |
16 | 5 5 6 5 5 5 5 |
17 | 4 4 4 3 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 5 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 5 5 5 5 5 5 5 |
22 | 3 3 3 3 3 3 3 |
23 | 5 5 5 4 5 5 5 |
24 | 3 4 4 4 4 4 3 |
25 | 3 4 3 3 5 3 3 |
26 | 3 3 3 3 3 4 3 |
27 | 5 4 4 4 4 4 3 |
28 | 4 4 4 4 4 4 4 |
29 | 4 4 5 4 5 4 4 |
30 | 3 3 3 4 4 4 4 |
31 | 4 3 4 3 4 4 4 |
32 | 3 3 3 3 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
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1900.0 GPS week: 1900 Day: 0 MJD: 57544.000
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 237| 0 0 -2 -5 16 2 .20 10 10 | -1410 148 12 157
emr 80| -1 -1 0 -2 -32 12 .30 9 9 | 2475 -497 18 147
esa 150| 0 0 -6 21 -3 -15 -.45 7 7 | 231 -2547 8 169
gfz 206| -1 0 3 -18 -25 -35 .10 10 9 | 155 -189 10 112
grg 116| 0 0 6 -22 53 42 -.41 17 14 | 47 -33 12 180
jpl 80| 0 -1 -1 -6 -41 48 .33 10 10 | 927 -437 16 110
mit 350| 1 -1 5 33 29 -6 -.14 13 12 | -1 -216 41 374
ngs 233| -1 1 7 -15 1 5 .16 10 9 | -1289 -62 893 1823
sio 310| 0 1 -3 13 52 -22 .04 15 14 | --- --- --- ---
Table 2.1900.1 GPS week: 1900 Day: 1 MJD: 57545.000
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 244| 0 0 -1 -14 14 0 .14 10 10 | -1533 609 13 157
emr 80| 2 0 -4 -18 8 -5 .26 11 11 | 1840 174 19 120
esa 150| 0 0 -4 15 8 -23 -.44 7 7 | -1038 496 9 176
gfz 208| -1 0 2 -5 2 -31 .14 11 10 | -135 -597 10 137
grg 117| 0 0 4 -47 9 45 -.08 16 15 | -234 250 12 166
jpl 80| -2 0 0 18 22 30 .34 10 10 | 302 179 16 125
mit 350| 1 -1 5 -6 -64 10 -.16 12 11 | -466 332 41 359
ngs 233| 0 1 4 3 40 2 .16 10 8 | -1497 593 1132 2076
sio 310| 0 1 -2 8 -77 13 -.03 14 14 | --- --- --- ---
Table 2.1900.2 GPS week: 1900 Day: 2 MJD: 57546.000
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 243| 0 0 0 33 -17 -13 .17 11 10 | -1202 344 13 152
emr 80| -2 0 1 3 -29 25 .22 10 10 | 2459 52 18 136
esa 150| 0 0 -4 16 -5 25 -.41 7 7 | -1123 393 10 226
gfz 211| 0 1 1 16 -14 -26 .17 11 10 | -150 -66 10 111
grg 115| 1 0 5 -29 73 19 -.23 13 13 | 109 80 12 164
jpl 80| -1 0 0 1 -2 -1 .30 8 8 | 730 28 16 122
mit 350| 2 0 4 -48 0 -23 -.13 13 11 | 195 -153 41 343
ngs 224| 0 1 1 7 -4 -2 .15 11 9 | -1470 616 529 1710
sio 306| 0 0 -4 -31 24 -22 .00 13 13 | --- --- --- ---
Table 2.1900.3 GPS week: 1900 Day: 3 MJD: 57547.000
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 244| 0 1 1 -1 2 -9 .12 10 10 | -1333 368 14 161
emr 80| -3 0 -1 -12 -21 12 .30 9 9 | 1991 428 18 131
esa 150| 1 -1 -5 8 15 -4 -.40 7 8 | -689 -111 8 173
gfz 210| 0 0 3 10 7 -65 .16 11 11 | -852 824 12 136
grg 113| 0 0 0 -20 83 59 -.34 14 12 | -104 145 12 205
jpl 80| 0 0 -2 18 33 -14 .32 9 9 | 396 669 16 128
mit 350| 2 0 3 -20 -28 -14 -.17 13 12 | -158 88 46 343
ngs 226| 0 2 3 2 -36 11 .06 9 7 | -1384 441 739 2096
sio 305| 1 0 -1 7 -46 35 -.02 13 15 | --- --- --- ---
Table 2.1900.4 GPS week: 1900 Day: 4 MJD: 57548.000
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 246| 0 0 0 14 -36 3 .14 11 11 | -1231 112 15 167
emr 80| -2 0 0 0 -25 -1 .32 10 10 | 2702 693 15 125
esa 150| 0 0 -4 -8 2 13 -.39 8 8 | -1068 1621 8 171
gfz 211| -1 0 1 0 3 -15 .11 13 10 | -95 18 10 165
grg 115| 1 0 -3 -46 96 32 -.41 15 13 | 127 -121 12 205
jpl 80| -1 0 1 16 7 -30 .29 8 8 | 1259 728 15 124
mit 350| 3 0 5 -26 -25 21 -.19 13 12 | -51 -219 43 379
ngs 224| -1 1 1 26 6 -6 .04 10 9 | -1503 577 682 1873
sio 304| 1 0 -1 -7 -10 -1 -.04 14 14 | --- --- --- ---
Table 2.1900.5 GPS week: 1900 Day: 5 MJD: 57549.000
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 248| 0 0 1 22 -2 12 .07 13 12 | -1027 -969 16 158
emr 80| -2 0 1 17 -13 19 .30 9 9 | 3287 1022 15 139
esa 150| 0 0 -6 21 -2 12 -.36 8 9 | -570 250 9 161
gfz 212| 0 0 2 -26 10 -13 .12 11 10 | -313 499 10 175
grg 111| 2 -1 -2 -30 65 29 -.18 14 13 | -127 193 13 214
jpl 80| -1 0 1 -10 5 5 .26 8 8 | 1874 1335 15 119
mit 349| 3 0 5 -25 -35 -21 -.21 14 13 | -397 16 44 352
ngs 222| 0 0 0 7 9 -18 .01 11 9 | -869 -1050 702 1958
sio 307| 1 0 -1 -16 -29 -20 -.09 14 14 | --- --- --- ---
Table 2.1900.6 GPS week: 1900 Day: 6 MJD: 57550.000
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 246| 0 0 3 40 7 17 .11 9 9 | -1121 374 12 148
emr 80| -2 2 0 4 -28 -7 .29 9 9 | 3998 334 13 120
esa 150| 0 0 -3 10 1 2 -.42 8 8 | -576 623 8 165
gfz 211| 0 0 1 -1 -13 -2 .15 10 9 | -84 -172 11 128
grg 116| 0 -2 -5 -26 92 8 -.11 16 14 | -29 486 13 154
jpl 80| -1 0 1 0 -37 24 .26 8 8 | 2806 672 13 100
mit 349| 2 -1 6 -26 1 20 -.20 13 13 | -52 458 58 371
ngs 223| -1 1 -3 -21 20 -20 -.02 11 9 | -756 -194 889 2213
sio 306| 0 -1 0 -17 22 -19 -.09 12 12 | --- --- --- ---
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 3.1900.0 GPS week: 1900 Day: 0 MJD: 57544.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jpl mit ngs sio IGS | cod emr esa gfz grg jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 9 9 6 6 11 10 7 6 10 3 | 23 24 18 19 17 27 19 22 22 18
2 | 11 10 8 12 14 7 13 12 17 4 | 30 30 26 30 32 30 28 26 22 27
3 | 6 8 4 8 11 10 8 8 13 3 | 40 41 34 37 41 40 37 41 39 37
X4 | 3 --- --- --- --- --- --- --- --- 0 | 49 --- --- --- --- --- --- --- --- 49
5 | 9 7 8 9 7 7 11 9 17 3 | 31 32 32 33 32 32 29 35 30 31
6 | 10 8 5 5 11 8 11 9 14 3 | 23 27 19 20 19 27 19 23 22 21
7 | 9 11 6 13 11 10 12 9 17 3 | 31 34 26 33 29 32 23 28 27 28
8E | 16 11 7 10 46 13 8 12 14 5 | 28 26 20 23 44 27 23 29 19 21
9 | 7 11 5 7 14 9 8 10 11 3 | 26 30 24 26 26 29 23 28 25 25
10 | 8 8 4 12 12 9 13 8 14 3 | 51 52 43 49 46 52 49 51 44 47
11 | 7 9 14 9 16 10 12 7 12 4 | 26 32 24 24 30 31 19 28 24 24
12 | 11 10 7 13 17 9 26 12 19 4 | 25 29 18 24 25 25 25 22 20 19
13 | 8 9 7 10 19 7 12 11 18 4 | 25 29 23 24 23 29 20 23 19 22
14 | 12 11 7 13 14 8 14 12 19 4 | 26 22 18 18 18 20 18 20 17 17
15 | 8 10 6 12 18 7 13 11 18 4 | 27 31 24 26 24 29 16 23 17 23
16 | 12 12 8 14 19 10 26 14 21 5 | 27 27 19 22 23 24 23 19 13 18
17E | 10 10 5 7 12 12 13 8 10 3 | 33 34 30 33 27 35 24 33 29 31
18 | 10 7 11 15 8 6 10 9 17 3 | 25 27 22 21 26 27 24 24 18 23
19E | 13 10 7 6 13 8 15 10 8 3 | 26 28 23 26 23 28 24 30 23 24
20 | 10 9 11 8 7 9 12 9 16 3 | 26 30 25 29 30 30 29 30 21 27
21 | 13 9 8 12 11 12 22 17 15 4 | 34 38 28 37 34 35 37 37 28 33
22 | 8 6 7 8 9 7 11 9 12 3 | 27 21 19 21 23 21 22 27 21 20
23 | 13 13 7 11 23 10 12 11 21 4 | 27 27 21 21 29 26 19 21 16 20
24 | 10 8 6 6 15 9 13 7 7 3 | 20 25 18 21 23 22 22 20 19 19
25 | 11 8 5 6 12 8 7 7 14 3 | 22 28 20 26 17 26 20 23 19 22
26 | 8 7 5 6 12 9 9 9 11 2 | 29 30 21 25 23 28 25 25 21 24
27E | 17 10 7 9 34 11 9 10 10 4 | 35 29 24 29 37 27 28 29 23 26
28 | 10 8 7 11 19 9 14 9 21 4 | 22 27 19 24 24 27 21 23 20 20
29E | 9 13 6 9 19 18 8 12 10 4 | 55 56 52 54 65 51 54 53 54 54
30 | 9 8 5 8 12 9 8 8 10 3 | 28 30 18 23 21 28 21 25 22 22
31 | 10 8 6 10 16 11 12 14 9 3 | 44 46 40 46 36 41 42 44 42 42
32 | 8 7 6 9 11 7 12 10 9 3 | 42 43 38 39 42 43 36 36 43 39
------+---------------------------------------------------+----------------------------------------------------
RMS | 10 9 7 10 17 10 13 10 15 |T 30 31 25 28 29 30 26 28 25 27
WRMS | 10 9 7 9 14 10 12 9 14 |NE 29 30 24 26 27 29 25 27 23 26
MEDI | 10 9 7 9 13 9 12 9 14 |MD 27 30 23 26 26 28 23 27 22 24
Table 3.1900.1 GPS week: 1900 Day: 1 MJD: 57545.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jpl mit ngs sio IGS | cod emr esa gfz grg jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 9 8 5 8 10 8 6 6 10 2 | 19 26 18 19 19 26 18 22 23 18
2 | 8 12 10 12 22 8 14 13 16 4 | 26 25 23 26 29 24 21 24 20 20
3 | 10 10 4 8 8 9 8 6 9 3 | 34 34 30 31 34 38 30 35 31 31
X4 | 2 --- --- --- --- --- --- --- --- 0 | 79 --- --- --- --- --- --- --- --- 79
5 | 8 11 8 10 9 9 10 9 13 3 | 20 20 22 23 22 21 16 20 18 18
6 | 8 10 6 5 11 9 12 8 12 3 | 19 22 15 19 20 24 16 21 23 16
7 | 8 13 5 9 13 13 10 10 12 3 | 23 27 20 27 24 28 20 25 22 21
8E | 18 13 6 10 25 10 9 8 17 4 | 28 27 18 24 27 25 21 26 22 21
9 | 8 9 6 6 17 11 7 9 7 3 | 21 26 20 23 24 28 20 27 21 20
10 | 9 10 4 9 11 11 12 11 11 3 | 31 34 26 27 29 35 30 33 32 29
11 | 9 11 13 9 15 10 12 11 15 4 | 20 25 20 21 26 24 16 25 20 18
12 | 12 12 8 13 18 11 25 13 20 5 | 24 26 19 22 27 24 26 23 23 18
13 | 13 10 7 12 17 6 12 8 17 4 | 22 23 17 22 22 24 16 18 19 16
14 | 13 12 7 14 18 11 13 13 21 4 | 26 27 22 22 25 21 18 21 21 18
15 | 9 14 8 13 14 7 12 9 13 3 | 24 27 18 20 22 22 16 19 17 17
16 | 11 15 7 15 22 11 23 10 18 5 | 24 26 21 24 30 26 23 21 14 18
17E | 8 12 7 7 22 10 11 7 8 3 | 29 29 24 28 32 31 17 30 26 25
18 | 9 9 9 17 10 8 10 11 17 4 | 19 23 20 21 22 19 20 19 21 17
19E | 10 14 8 9 16 11 15 8 10 4 | 28 29 25 30 30 30 27 31 27 26
20 | 13 13 10 10 9 11 11 11 11 4 | 23 22 21 24 26 21 19 19 21 19
21 | 9 12 10 14 13 13 21 13 16 4 | 27 27 20 24 29 28 22 23 18 20
22 | 11 7 8 9 9 6 9 7 10 3 | 25 20 21 22 24 22 18 28 18 20
23 | 13 12 7 12 23 9 13 10 19 4 | 24 26 21 19 29 24 16 22 15 17
24 | 11 10 8 10 14 10 10 7 15 3 | 16 23 20 18 21 22 18 17 22 16
25 | 13 11 5 7 13 9 8 10 14 3 | 17 25 16 22 28 22 19 23 25 18
26 | 8 12 5 6 13 8 11 6 10 3 | 27 29 20 27 31 28 19 25 24 23
27E | 8 8 4 12 23 8 8 9 9 3 | 27 27 20 29 31 26 26 24 25 23
28 | 9 8 7 11 15 8 11 9 19 3 | 24 25 20 26 26 26 22 22 18 20
29E | 8 15 7 12 18 15 9 12 9 4 | 39 34 36 39 36 37 35 41 34 34
30 | 13 11 5 8 14 10 8 7 9 3 | 24 26 16 24 24 29 19 24 24 21
31 | 7 7 5 8 18 9 10 9 9 3 | 38 40 33 36 37 36 31 35 30 33
32 | 9 8 5 9 15 8 10 11 8 3 | 33 36 30 30 34 32 29 32 30 29
------+---------------------------------------------------+----------------------------------------------------
RMS | 10 11 7 10 16 10 12 10 14 |T 26 26 21 24 27 26 21 25 22 23
WRMS | 10 11 7 10 15 10 11 8 14 |NE 26 26 20 23 26 25 20 23 21 22
MEDI | 9 11 7 10 15 9 11 9 12 |MD 24 26 20 24 27 26 20 24 22 20
Table 3.1900.2 GPS week: 1900 Day: 2 MJD: 57546.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jpl mit ngs sio IGS | cod emr esa gfz grg jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 9 9 6 9 10 6 5 8 12 2 | 26 28 19 20 19 29 20 22 25 21
2 | 10 10 8 13 15 7 15 10 18 4 | 26 26 22 22 26 27 23 22 17 21
3 | 10 10 3 8 8 8 6 11 10 3 | 41 39 32 35 34 40 32 36 33 34
X4 | 3 --- --- --- --- --- --- --- --- 0 | 63 --- --- --- --- --- --- --- --- 62
5 | 7 8 7 10 6 9 12 10 13 3 | 24 20 20 25 20 22 19 24 21 20
6 | 12 10 7 6 8 7 12 5 8 3 | 22 28 20 21 22 28 21 23 27 21
7 | 11 16 5 12 13 10 10 11 10 3 | 27 28 23 30 27 31 23 28 23 24
8E | 13 17 5 11 19 8 11 8 13 4 | 27 30 19 24 23 26 22 26 25 21
9 | 9 8 5 6 11 9 8 5 8 2 | 23 26 19 23 21 30 21 24 22 21
10 | 6 10 5 9 6 7 7 14 13 3 | 42 46 35 38 38 44 37 42 35 38
11 | 6 10 13 11 12 7 13 11 14 4 | 23 25 20 22 22 25 17 25 19 19
12 | 13 9 7 13 16 9 27 13 21 5 | 32 27 23 25 24 31 28 26 24 23
13 | 10 9 6 11 13 7 11 10 14 3 | 24 23 17 23 20 25 18 20 15 18
14 | 11 11 7 14 16 7 11 10 17 4 | 24 24 17 22 22 20 20 19 17 17
15 | 9 9 8 13 10 7 11 11 14 3 | 25 23 18 21 18 23 15 22 16 18
16 | 15 12 7 19 19 10 25 15 18 5 | 34 27 24 27 29 27 26 25 19 22
17E | 13 8 6 6 17 8 12 9 7 3 | 31 27 24 29 25 28 18 29 27 25
18 | 10 13 10 15 10 8 13 12 14 4 | 20 24 18 17 20 19 21 19 18 17
19E | 15 10 7 10 13 8 15 12 9 4 | 31 27 29 33 28 32 32 33 28 28
20 | 9 9 10 11 8 12 12 10 14 3 | 21 21 19 25 23 21 22 19 18 19
21 | 8 17 11 15 11 7 22 14 17 5 | 28 34 24 32 28 29 27 28 20 25
22 | 10 7 7 9 9 6 8 10 13 3 | 28 21 21 21 22 21 17 24 18 19
23 | 14 9 6 12 19 9 14 14 20 4 | 28 24 22 21 29 28 18 22 16 20
24E | 11 8 6 11 14 9 9 10 11 3 | 23 26 19 22 21 22 22 22 28 21
25 | 13 9 5 6 12 8 9 8 13 3 | 30 27 23 29 20 30 27 27 24 25
26 | 10 9 5 8 13 7 11 9 9 3 | 33 30 23 29 30 31 26 29 27 27
27E | 11 9 6 10 18 7 9 9 8 3 | 29 30 23 28 32 28 26 29 25 25
28 | 8 8 8 11 13 6 12 10 20 3 | 24 25 22 27 19 27 25 25 22 22
29E | 19 10 7 12 17 11 13 16 11 4 | 33 25 26 32 30 27 26 32 28 26
30 | 14 13 5 7 12 8 8 8 6 3 | 25 25 15 23 23 26 20 25 23 20
31 | 11 9 5 10 20 7 9 11 11 3 | 42 39 33 38 40 39 34 39 36 36
32 | 8 8 5 7 12 7 6 7 10 2 | 29 32 25 30 30 32 29 28 32 28
------+---------------------------------------------------+----------------------------------------------------
RMS | 11 10 7 11 13 8 13 11 13 |T 29 27 22 26 25 28 23 26 23 24
WRMS | 10 10 7 10 13 8 11 9 13 |NE 28 27 21 25 24 27 23 25 22 24
MEDI | 10 9 6 11 13 8 11 10 13 |MD 27 27 22 25 23 28 22 25 23 21
Table 3.1900.3 GPS week: 1900 Day: 3 MJD: 57547.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jpl mit ngs sio IGS | cod emr esa gfz grg jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 9 9 7 7 10 8 8 6 8 2 | 22 24 18 21 19 23 18 19 18 18
2 | 8 9 8 14 12 9 13 10 17 4 | 31 32 28 30 26 30 28 27 22 26
3 | 8 9 4 11 7 9 7 7 10 3 | 42 45 38 43 40 43 38 37 40 39
X4 | 2 --- --- --- --- --- --- --- --- 0 | 56 --- --- --- --- --- --- --- --- 56
5 | 8 9 7 13 8 10 12 9 13 3 | 29 26 25 31 23 28 24 29 24 25
6 | 11 6 7 6 9 7 12 5 12 3 | 27 28 24 24 23 28 24 24 28 23
7 | 9 13 6 12 20 14 13 10 13 4 | 27 29 21 29 31 30 25 27 24 24
8E | 9 12 6 9 20 9 12 8 12 3 | 24 25 17 22 23 21 22 24 18 19
9 | 9 8 5 10 11 8 11 5 8 3 | 23 29 22 26 22 28 25 26 22 23
10 | 8 8 5 9 7 7 7 9 15 3 | 43 43 39 44 39 43 43 42 37 40
11 | 9 12 13 8 11 9 14 8 14 4 | 29 32 27 29 26 30 26 29 26 26
12 | 12 8 8 14 16 9 25 11 18 4 | 37 36 31 34 30 35 35 34 27 31
13 | 10 7 7 10 13 7 12 8 17 3 | 23 27 21 24 20 25 21 22 15 20
14 | 10 10 7 14 11 9 11 9 16 3 | 23 27 20 22 19 22 19 20 16 18
15 | 11 8 8 13 14 8 12 11 15 3 | 28 30 26 27 23 30 20 25 19 24
16 | 13 13 6 18 17 12 24 12 18 5 | 32 29 24 26 25 27 29 26 21 23
17E | 11 7 6 7 12 10 12 8 8 3 | 26 26 24 26 23 26 19 27 23 23
18 | 8 10 12 14 5 8 17 7 15 4 | 27 27 26 28 25 26 25 25 19 24
19E | 11 8 8 10 31 10 14 10 10 4 | 34 39 34 38 44 37 34 40 34 35
20 | 9 9 12 12 7 11 9 8 11 3 | 23 23 22 26 24 22 24 23 18 21
21 | 8 10 9 14 12 10 23 12 18 4 | 33 35 28 37 28 32 32 32 25 29
22 | 9 7 9 9 9 6 9 6 11 3 | 27 26 24 30 24 22 22 24 24 23
23 | 13 8 7 13 16 9 14 11 17 4 | 25 26 20 25 22 25 24 22 16 20
24E | 17 7 7 8 13 11 10 7 10 3 | 25 27 23 21 23 25 22 23 21 21
25 | 12 8 5 10 12 7 8 9 12 3 | 31 32 24 30 24 29 29 30 25 27
26 | 9 9 5 9 12 8 8 5 8 2 | 27 30 21 25 21 27 26 26 24 24
27E | 11 7 7 9 22 9 10 7 10 3 | 25 24 18 23 27 23 24 27 21 21
28 | 8 6 9 9 13 7 12 8 19 3 | 30 31 29 30 25 30 32 32 30 28
29E | 11 11 7 13 16 13 11 11 9 4 | 32 31 32 37 33 32 32 34 31 31
30 | 14 10 5 8 14 10 10 5 8 3 | 30 28 21 28 23 26 25 27 25 24
31 | 10 9 5 9 14 7 8 8 12 3 | 40 46 35 40 34 40 36 38 36 38
32 | 6 9 7 9 7 8 6 5 11 2 | 40 45 38 37 39 42 37 38 38 38
------+---------------------------------------------------+----------------------------------------------------
RMS | 10 9 7 11 14 9 13 9 13 |T 30 30 25 29 26 29 27 28 24 26
WRMS | 10 9 8 11 12 9 12 7 15 |NE 30 30 25 29 25 29 27 27 24 27
MEDI | 9 9 7 10 12 9 12 8 12 |MD 28 29 24 28 24 28 25 27 24 24
Table 3.1900.4 GPS week: 1900 Day: 4 MJD: 57548.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jpl mit ngs sio IGS | cod emr esa gfz grg jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 10 8 6 7 11 7 9 5 9 2 | 26 29 21 23 25 28 19 24 26 23
2 | 12 9 8 11 17 7 15 11 16 4 | 34 28 27 28 31 29 27 29 30 27
3 | 7 7 5 9 10 8 11 9 10 3 | 40 41 38 38 34 42 35 39 38 37
X4 | 3 --- --- --- --- --- --- --- --- 0 | 36 --- --- --- --- --- --- --- --- 34
5 | 7 8 11 11 7 9 12 10 10 3 | 25 27 27 29 27 25 26 23 28 25
6 | 8 6 7 6 11 6 14 6 9 3 | 26 29 23 27 29 27 22 30 29 25
7 | 11 17 7 12 18 13 12 11 15 4 | 39 41 32 38 41 40 37 39 35 36
8E | 11 9 6 10 26 8 16 11 14 4 | 23 29 23 26 32 26 22 26 30 23
9 | 15 8 6 9 12 7 11 8 8 3 | 40 32 29 34 33 35 27 33 32 31
10 | 5 8 6 11 10 8 7 12 16 3 | 44 42 40 44 35 43 39 41 38 40
11 | 7 12 13 10 16 6 14 9 13 4 | 25 31 26 28 31 29 23 29 27 26
12 | 15 9 8 14 17 9 25 14 19 5 | 32 31 29 31 33 30 32 32 35 28
13 | 11 9 7 12 18 7 13 11 14 4 | 24 29 21 25 31 26 20 22 23 22
14 | 11 10 7 13 17 8 11 11 18 4 | 25 25 23 25 24 22 21 24 27 21
15 | 9 9 9 13 14 8 14 11 15 4 | 30 32 27 26 30 29 21 24 26 25
16 | 16 12 6 17 18 8 24 14 18 5 | 35 31 27 29 37 31 29 28 30 27
17E | 8 8 6 10 13 10 12 10 9 3 | 29 31 24 32 27 30 20 29 26 26
18 | 9 7 13 15 10 8 16 10 15 4 | 24 23 24 27 24 22 29 21 28 22
19E | 8 12 7 9 19 8 12 10 9 3 | 27 27 27 31 32 29 24 31 27 26
20 | 9 11 13 13 7 12 11 10 11 4 | 22 24 22 28 25 25 25 21 27 22
21 | 12 11 9 17 12 9 23 13 20 5 | 31 31 25 29 28 31 30 27 26 26
22 | 9 6 10 8 8 6 10 7 10 3 | 29 25 27 25 24 26 21 30 25 25
23 | 20 8 6 13 20 8 15 13 19 4 | 39 30 26 27 37 31 24 28 28 27
24E | 14 11 8 10 13 7 10 7 10 3 | 23 26 20 19 26 23 23 21 25 20
25 | 15 8 7 31 12 7 8 11 11 4 | 25 31 26 49 33 31 28 28 33 29
26 | 10 10 4 8 13 6 8 8 10 3 | 29 32 25 29 33 33 27 30 31 28
27E | 9 10 8 9 23 7 11 9 11 3 | 24 27 22 25 29 23 22 25 26 22
28 | 12 9 8 11 13 7 11 12 19 4 | 30 37 26 36 35 34 31 32 32 30
29E | 15 13 10 17 14 12 13 14 10 4 | 32 33 32 34 32 31 32 33 35 31
30 | 14 11 7 8 11 9 9 9 13 3 | 39 32 21 28 31 29 28 31 31 28
31 | 11 8 6 9 13 7 12 9 16 3 | 42 46 39 43 50 45 45 48 46 44
32 | 8 8 7 9 11 8 6 7 12 3 | 37 39 34 39 38 35 34 35 42 36
------+---------------------------------------------------+----------------------------------------------------
RMS | 11 10 8 12 15 8 13 10 14 |T 30 31 26 30 31 30 27 29 30 27
WRMS | 11 10 8 10 13 8 12 9 14 |NE 31 30 26 30 30 30 26 28 30 27
MEDI | 10 9 7 11 13 8 12 10 13 |MD 29 31 26 29 31 29 27 29 29 26
Table 3.1900.5 GPS week: 1900 Day: 5 MJD: 57549.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jpl mit ngs sio IGS | cod emr esa gfz grg jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 7 8 6 8 10 7 10 5 11 2 | 23 24 19 25 25 24 23 21 21 21
2 | 11 8 8 11 17 7 14 14 16 4 | 30 30 26 27 32 30 24 24 18 25
3 | 8 7 5 10 9 9 10 13 12 3 | 29 35 29 29 30 34 30 32 29 30
X4 | 2 --- --- --- --- --- --- --- --- 0 | 68 --- --- --- --- --- --- --- --- 67
5 | 12 8 9 9 8 9 13 11 12 3 | 28 28 27 28 27 29 25 27 25 26
6 | 8 6 7 7 10 8 11 8 11 3 | 24 27 23 22 28 29 22 25 26 24
7E | 14 11 9 13 14 11 14 10 12 4 | 35 32 30 33 34 32 28 32 28 30
8E | 11 12 5 8 17 7 13 9 11 3 | 21 26 18 24 24 22 25 25 20 20
9 | 8 10 6 6 13 8 11 5 7 3 | 24 28 22 22 31 27 25 26 22 24
10 | 9 6 4 10 12 8 8 11 13 3 | 37 39 31 39 31 38 33 34 32 34
11 | 7 11 14 11 16 7 13 9 14 4 | 23 27 22 25 29 26 23 23 22 21
12 | 13 9 6 14 17 9 26 13 20 5 | 35 37 31 33 34 35 35 34 31 31
13 | 10 9 10 11 14 7 15 14 16 4 | 29 34 28 29 30 31 26 30 22 27
14 | 12 11 7 13 20 9 13 12 21 4 | 30 29 27 27 31 27 23 28 24 25
15 | 12 6 8 14 14 8 13 12 15 4 | 28 32 29 34 28 31 25 28 25 28
16 | 13 10 7 16 19 8 24 13 17 4 | 31 31 25 28 32 29 30 26 22 25
17E | 12 10 5 9 23 11 12 12 9 4 | 26 28 23 26 24 27 22 28 24 23
18 | 9 7 11 12 12 6 15 11 20 4 | 24 25 26 29 24 26 23 28 21 24
19E | 21 10 8 9 19 9 13 11 12 4 | 34 32 32 33 36 32 33 36 32 31
20 | 13 9 13 9 10 9 11 11 11 4 | 26 28 26 31 25 29 27 29 22 25
21 | 9 9 10 15 13 8 24 13 22 4 | 32 31 30 32 31 30 30 31 25 28
22 | 8 8 11 8 8 6 10 9 12 3 | 24 24 23 22 22 23 23 26 22 22
23 | 15 9 6 12 19 9 16 13 19 4 | 27 29 24 21 34 27 27 26 20 23
24E | 10 11 7 10 11 7 12 8 10 3 | 22 29 25 26 23 24 23 24 21 23
25 | 11 8 6 9 11 6 8 9 12 3 | 28 32 24 35 29 29 25 29 24 27
26 | 18 7 5 9 14 8 10 9 13 3 | 27 31 22 24 27 30 26 26 26 25
27E | 17 7 6 9 20 6 10 8 11 3 | 24 27 19 24 29 23 25 26 23 22
28 | 14 7 9 11 11 8 12 11 21 4 | 28 31 26 30 27 31 26 28 27 26
29E | 15 14 8 14 8 10 14 12 11 4 | 36 31 29 34 33 30 34 35 28 30
30 | 20 10 7 8 12 10 12 7 9 3 | 35 32 28 30 31 30 29 28 27 28
31 | 20 6 6 12 15 9 14 9 12 4 | 75 75 73 77 68 77 74 73 72 73
32 | 7 8 7 9 14 7 7 8 13 3 | 32 34 32 39 40 35 31 36 35 34
------+---------------------------------------------------+----------------------------------------------------
RMS | 13 9 8 11 14 8 14 11 14 |T 31 31 27 30 30 30 28 29 26 28
WRMS | 12 9 9 10 13 8 13 9 14 |NE 30 30 26 28 29 29 26 28 24 27
MEDI | 11 9 7 10 14 8 13 11 12 |MD 28 31 26 29 30 29 26 28 24 25
Table 3.1900.6 GPS week: 1900 Day: 6 MJD: 57550.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jpl mit ngs sio IGS | cod emr esa gfz grg jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 8 8 7 7 12 6 5 8 11 2 | 30 34 25 28 31 34 29 31 31 29
2 | 10 10 7 11 20 8 13 13 16 4 | 37 37 33 35 40 38 34 33 29 34
3 | 7 9 5 9 9 9 9 13 8 3 | 49 56 46 50 47 56 49 49 48 49
X4 | 3 --- --- --- --- --- --- --- --- 0 | 43 --- --- --- --- --- --- --- --- 43
5 | 6 6 10 8 10 9 12 8 10 3 | 41 39 38 41 36 41 38 38 39 39
6 | 9 6 5 7 9 7 9 5 13 2 | 32 35 28 32 36 34 30 34 34 32
7E | 7 11 6 11 18 12 12 11 12 3 | 44 44 40 46 49 45 41 43 41 42
8E | 9 9 5 6 21 7 11 8 11 3 | 29 35 24 28 28 32 32 31 31 28
9 | 6 8 5 7 15 6 10 7 6 2 | 34 37 29 30 39 37 33 33 31 32
10 | 7 8 5 7 8 8 7 13 9 3 | 58 58 51 57 49 59 54 54 51 54
11 | 9 9 13 8 16 7 11 10 13 3 | 31 35 27 29 33 34 27 30 28 28
12 | 14 9 8 12 14 8 25 15 19 5 | 37 37 32 32 29 36 34 34 31 32
13 | 10 8 10 13 15 8 14 12 13 4 | 33 35 28 35 34 35 29 30 24 30
14 | 7 8 8 14 19 7 13 11 16 4 | 32 30 27 31 35 29 27 27 23 27
15 | 9 7 10 14 17 7 15 13 14 4 | 38 41 34 37 38 40 30 35 30 35
16 | 9 11 8 18 18 9 23 12 18 4 | 31 32 27 32 33 31 30 30 25 27
17E | 9 10 6 9 19 12 11 12 8 3 | 33 37 28 34 27 33 27 36 31 30
18 | 8 7 9 10 10 7 15 10 13 3 | 30 30 30 29 27 33 31 29 28 29
19E | 10 9 6 7 20 9 12 10 6 3 | 36 35 36 37 36 38 37 36 35 35
20 | 9 10 12 9 11 12 12 9 9 3 | 31 30 29 34 26 36 34 28 29 30
21 | 9 12 10 15 19 8 26 15 19 5 | 38 39 32 41 37 39 39 38 33 35
22 | 7 6 9 10 11 5 9 12 10 3 | 32 32 28 31 28 30 29 32 28 29
23 | 13 9 8 14 24 7 15 13 17 4 | 37 38 32 31 45 38 34 33 27 33
24E | 11 8 6 8 16 7 13 7 12 3 | 32 36 30 31 29 34 28 30 31 30
25 | 5 9 6 7 13 7 10 9 9 2 | 29 34 27 35 28 33 29 32 28 30
26 | 9 9 4 9 12 6 10 6 7 2 | 30 34 24 27 30 33 28 28 27 28
27E | 10 8 6 7 20 8 9 7 10 3 | 32 35 24 30 32 30 32 31 31 29
28 | 9 8 7 10 11 7 12 11 18 3 | 30 34 27 31 28 32 30 28 27 28
29E | 17 10 6 14 10 9 12 17 8 4 | 36 34 32 38 32 33 33 40 32 33
30 | 12 11 6 8 15 8 16 8 7 3 | 50 47 42 46 42 47 41 44 44 44
31E | 13 6 6 10 17 7 9 10 9 3 | 79 78 75 79 77 80 77 81 77 78
32 | 7 7 7 12 16 8 8 9 10 3 | 44 48 42 45 52 47 42 48 50 45
------+---------------------------------------------------+----------------------------------------------------
RMS | 9 9 8 10 16 8 13 11 12 |T 37 38 33 36 36 38 35 36 34 35
WRMS | 9 9 8 9 14 8 13 9 12 |NE 36 37 32 35 35 37 33 34 32 34
MEDI | 9 9 7 9 15 8 12 10 11 |MD 33 35 30 34 34 35 32 33 31 32
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 4.1900 GPS week: 1900 MJD: 57544.0-57550.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 |U 11 9 19 |U 4 6 16 |U 9 9 19 |
emr | emr 2976 | 9 12 21 |U 7 6 17 | 11 10 21 |
esa | esa 2976 | 10 9 19 |U 4 7 19 | 9 9 20 |
gfz | gfz 2975 |U 8 9 19 |U 5 6 19 |U 9 10 22 |
grg | grg 2975 |U 11 9 22 |U 5 7 26 | 10 10 23 |
igs | igs 2976 | 11 9 19 | 4 6 17 | 9 9 21 |
jpl | jpl 2976 | 9 10 21 |U 5 6 18 |U 10 10 22 |
mit | mit 2976 | 10 13 24 |U 6 7 25 |U 9 10 23 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1900.0 GPS week: 1900 Day: 0 MJD: 57544.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 39 20 39 | 4 6 18 | 8 7 14 |
emr | emr 2976 | 15 16 37 | 7 6 21 | 9 7 17 |
esa | esa 2976 | 28 17 35 | 5 6 21 | 8 8 16 |
gfz | gfz 2976 | 14 15 34 | 6 6 30 | 9 7 17 |
grg | grg 2976 | 34 20 37 | 6 6 24 | 9 7 22 |
igs | igs 2976 | 33 19 36 | 5 6 20 | 9 7 16 |
jpl | jpl 2976 | 16 15 37 | 5 6 21 | 9 5 16 |
mit | mit 2976 | 16 14 37 | 6 7 26 | 9 8 18 |
Table 5.1900.1 GPS week: 1900 Day: 1 MJD: 57545.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 11 19 | 5 7 14 | 8 8 17 |
emr | emr 2976 | 11 16 21 | 9 5 18 | 14 11 21 |
esa | esa 2976 | 10 13 21 | 5 8 20 | 10 9 21 |
gfz | gfz 2976 | 10 12 20 | 6 6 19 | 10 12 23 |
grg | grg 2976 | 10 12 23 | 5 8 24 | 11 12 24 |
igs | igs 2976 | 10 13 21 | 5 6 18 | 10 10 21 |
jpl | jpl 2976 | 11 15 21 | 6 7 19 | 12 11 23 |
mit | mit 2976 | 11 13 22 | 8 8 25 | 9 10 24 |
Table 5.1900.2 GPS week: 1900 Day: 2 MJD: 57546.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 11 29 | 4 5 16 | 9 7 24 |
emr | emr 2976 | 11 13 30 | 7 6 19 | 11 9 26 |
esa | esa 2976 | 11 11 29 | 4 7 21 | 9 7 24 |
gfz | gfz 2976 | 10 11 30 | 4 6 19 | 10 8 27 |
grg | grg 2975 | 10 12 30 | 5 8 30 | 10 8 25 |
igs | igs 2976 | 10 11 29 | 4 6 20 | 10 8 25 |
jpl | jpl 2976 | 11 12 30 | 5 7 20 | 11 9 28 |
mit | mit 2976 | 10 11 31 | 6 6 28 | 9 7 24 |
Table 5.1900.3 GPS week: 1900 Day: 3 MJD: 57547.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 14 | 4 6 14 | 7 10 19 |
emr | emr 2976 | 8 7 17 | 6 7 17 | 9 8 22 |
esa | esa 2976 | 7 5 16 | 4 7 18 | 8 9 23 |
gfz | gfz 2975 | 7 5 14 | 4 7 15 | 8 9 24 |
grg | grg 2975 | 7 6 15 | 5 6 22 | 13 11 22 |
igs | igs 2976 | 7 5 14 | 4 6 17 | 8 8 23 |
jpl | jpl 2976 | 7 7 19 | 4 6 18 | 8 8 25 |
mit | mit 2976 | 11 27 33 | 7 9 32 | 7 9 22 |
Table 5.1900.4 GPS week: 1900 Day: 4 MJD: 57548.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 4 11 | 5 5 15 | 8 13 22 |
emr | emr 2976 | 5 8 13 | 7 6 15 | 11 15 25 |
esa | esa 2976 | 4 5 9 | 6 10 18 | 10 13 24 |
gfz | gfz 2976 | 4 5 12 | 6 6 18 | 10 15 27 |
grg | grg 2975 | 5 5 15 | 6 9 25 | 10 15 30 |
igs | igs 2976 | 4 6 11 | 5 7 16 | 9 14 25 |
jpl | jpl 2976 | 5 7 13 | 6 6 18 | 10 15 24 |
mit | mit 2976 | 5 7 14 | 6 6 24 | 9 14 27 |
Table 5.1900.5 GPS week: 1900 Day: 5 MJD: 57549.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 13 | 4 5 16 | 9 9 17 |
emr | emr 2976 | 6 10 15 | 5 6 16 | 10 8 19 |
esa | esa 2976 | 5 4 11 | 3 6 17 | 9 8 18 |
gfz | gfz 2976 | 5 5 13 | 3 4 17 | 9 9 18 |
grg | grg 2976 | 6 4 14 | 5 6 33 | 9 7 16 |
igs | igs 2976 | 5 6 12 | 3 4 16 | 9 8 18 |
jpl | jpl 2976 | 6 7 14 | 3 5 16 | 10 8 20 |
mit | mit 2976 | 6 7 12 | 5 8 26 | 9 12 18 |
Table 5.1900.6 GPS week: 1900 Day: 6 MJD: 57550.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 8 13 | 4 6 18 | 11 9 18 |
emr | emr 2976 | 6 11 14 | 5 7 15 | 12 12 18 |
esa | esa 2976 | 5 8 13 | 4 5 15 | 13 10 16 |
gfz | gfz 2976 | 5 8 14 | 4 6 14 | 10 8 17 |
grg | grg 2976 | 6 6 17 | 6 6 24 | 11 8 24 |
igs | igs 2976 | 5 8 12 | 4 5 14 | 11 9 17 |
jpl | jpl 2976 | 5 9 14 | 5 6 16 | 11 12 17 |
mit | mit 2976 | 8 10 21 | 4 6 17 | 11 8 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 : 10-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 6.1900 GPS week: 1900 MJD: 57544.500-57550.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -2 -7 -67 27 -2 | 18 32
| 18 16 102 113 5 | 3
emr uuuuu | 24 5 76 47 4 | 20 38
| 27 16 70 117 17 | 5
esa uuuuu | 3 -3 -57 8 8 | 8 27
| 12 18 53 50 4 | 5
gfz uuuuu | -3 13 -15 -117 6 | 4 27
| 29 14 71 185 6 | 5
grg uuuuu | -70 27 63 -58 -9 | -3 24
| 29 13 22 92 5 | 4
irf xxxxx | 19 -17 -2 -19 -4 | 1 26
| 11 10 20 17 4 | 3
jpl uuuuu | -2 -8 79 28 13 | 4 34
| 20 17 75 71 11 | 4
mit uuuuu | 18 -4 -24 -36 -5 | 13 27
| 12 9 52 38 7 | 3
ngs uuuuu | -32 -8 28 -55 -5 | 6 26
| 25 21 130 89 5 | 3
sio uuuux | 44 3 -94 139 -6 | 50 55
| 24 11 55 48 10 | 3
Table 7.1900.0 GPS week: 1900 Day: 0 MJD: 57544.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -21 13 -193 199 7 | 13 22
emr uuuuu | 36 31 -4 61 5 | 19 31
esa uuuuu | -5 -27 -105 -28 3 | 1 18
gfz uuuuu | -2 9 83 -23 7 | -3 19
grg uuuuu | -57 22 65 -200 -14 | -3 16
irf xxxxx | 8 -6 26 -34 -3 | -4 20
jpl uuuuu | 19 8 192 -59 19 | -3 25
mit uuuuu | -1 -4 17 -110 -10 | 11 21
ngs uuuuu | -5 -20 37 -6 0 | 2 18
sio uuuux | 4 -6 -2 101 -14 | 49 52
Table 7.1900.1 GPS week: 1900 Day: 1 MJD: 57545.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -10 7 110 49 -1 | 21 31
emr uuuuu | -11 22 114 -105 -3 | 27 39
esa uuuuu | 18 -6 -83 73 2 | 9 24
gfz uuuuu | 23 -2 16 -37 11 | 5 23
grg uuuuu | -15 49 25 -20 -11 | 4 15
irf xxxxx | 17 -17 17 5 -8 | 4 21
jpl uuuuu | -6 -27 84 135 33 | 5 32
mit uuuuu | 4 -4 50 1 -5 | 17 25
ngs uuuuu | -46 -11 -130 -218 -1 | 9 23
sio uuuux | 35 5 -128 91 -3 | 55 58
Table 7.1900.2 GPS week: 1900 Day: 2 MJD: 57546.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 23 -24 -24 17 2 | 18 30
emr uuuuu | -17 3 198 -132 -30 | 23 37
esa uuuuu | 14 -6 -60 62 10 | 5 24
gfz uuuuu | 38 3 -8 173 12 | 3 23
grg uuuuu | -78 28 94 -165 -12 | 0 19
irf xxxxx | 26 -23 -2 -27 -1 | 1 24
jpl uuuuu | -23 8 -34 -58 7 | 4 31
mit uuuuu | 15 -3 -14 0 2 | 13 25
ngs uuuuu | -23 3 -15 -35 1 | 6 24
sio uuuux | 38 -1 -83 97 -14 | 51 55
Table 7.1900.3 GPS week: 1900 Day: 3 MJD: 57547.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -21 -3 -7 -67 -6 | 18 30
emr uuuuu | 54 6 34 123 21 | 15 32
esa uuuuu | 0 -1 -37 -10 9 | 6 24
gfz uuuuu | 1 7 -93 -93 13 | 4 23
grg uuuuu | -64 11 61 33 -12 | -3 21
irf xxxxx | 31 -12 -36 0 -8 | 0 24
jpl uuuuu | -24 -15 -1 82 15 | 3 31
mit uuuuu | 18 3 -94 -15 -13 | 12 25
ngs uuuuu | -6 -9 159 -133 -11 | 7 23
sio uuuux | 31 14 -107 133 -11 | 48 53
Table 7.1900.4 GPS week: 1900 Day: 4 MJD: 57548.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 20 -8 -122 -124 -3 | 20 33
emr uuuuu | 31 -5 96 157 15 | 18 38
esa uuuuu | 1 32 -58 -19 11 | 10 29
gfz uuuuu | -37 37 -123 -195 -3 | 8 28
grg uuuuu | -95 35 49 -65 -11 | -2 21
irf xxxxx | 17 -9 -5 -40 1 | 3 26
jpl uuuuu | 0 -32 104 20 10 | 6 35
mit uuuuu | 32 -23 -7 -46 8 | 14 27
ngs uuuuu | -35 -31 148 38 -8 | 9 26
sio uuuux | 63 4 -181 196 14 | 50 55
Table 7.1900.5 GPS week: 1900 Day: 5 MJD: 57549.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 2 -6 -146 136 -10 | 15 38
emr uuuuu | 40 -16 13 125 18 | 13 40
esa uuuuu | 10 -9 -104 37 13 | 6 34
gfz uuuuu | -43 27 -2 -407 1 | 2 36
grg uuuuu | -80 29 80 -28 -8 | -10 36
irf xxxxx | 33 -15 -4 -27 -4 | -3 34
jpl uuuuu | -10 -3 118 21 9 | 1 40
mit uuuuu | 23 7 -35 -43 -8 | 9 32
ngs uuuuu | -35 -20 141 -17 -9 | 2 35
sio uuuux | 72 17 -94 148 -4 | 45 54
Table 7.1900.6 GPS week: 1900 Day: 6 MJD: 57550.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -10 -31 -89 -20 -3 | 22 42
emr uuuuu | 37 -3 80 104 6 | 23 48
esa uuuuu | -15 -1 49 -59 6 | 16 39
gfz uuuuu | -2 7 24 -238 5 | 11 39
grg uuuuu | -101 14 68 37 1 | -4 36
irf xxxxx | 3 -36 -10 -8 -9 | 5 36
jpl uuuuu | 29 5 89 55 -2 | 11 42
mit uuuuu | 31 -3 -86 -38 -5 | 16 36
ngs uuuuu | -78 32 -146 -13 -6 | 9 37
sio uuuux | 67 -12 -66 211 -8 | 52 61
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