[IGSREPORT-22748] Wk 1791 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri May 23 12:11:31 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1791 (May 04, 2014 - May 10, 2014)
Contacts: igs.acc 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 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:
igs1791[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1791[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1791[0-6].cls IGS GPS clock combination summary report.
igs17917.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17917.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 | GRAZ MAL2
0 | EMR | FAIR FAIR MCM4 YAKT
0 | ESA | DRAG WUHN
0 | GFZ | 1 2 1 IRKJ MAL2 IRKJ MAL2
0 | GRG | DRAG HYDE KELY NYA1 RBAY WUHN HYDE KELY NTUS NYA1
0 | GRG | RBAY WUHN
0 | MIT | ALRT IRKJ ALRT BRFT IRKJ MDVJ NTUS
1 | EMR | WUHN WUHN
1 | ESA | BRMU BOGT BRMU
1 | GFZ | 1 2 1 BOR1 BRMU WUHN BRMU WUHN
1 | GRG | ALRT GRAZ RBAY ZIMM ALRT GRAZ RBAY ZIMM
1 | MIT | MAW1 ONSA MAW1 ONSA
2 | COD | NTUS
2 | EMR | YAKT
2 | GFZ | 1 2 1 ISPA NTUS ISPA NTUS
2 | GRG | HOLB HYDE KELY MAL2 MOBS NTUS RBAY ALRT HYDE KELY
2 | GRG | MAL2 MOBS RBAY
2 | MIT | 23 23 TLSE BRFT HNPT MDVJ TLSE
3 | COD | BOR1 REUN BOR1 REUN
3 | EMR | YAKT
3 | ESA | UNSA
3 | GFZ | 1 2 1 DRAG DRAG
3 | GRG | KELY PIMO RBAY SHAO KELY PIMO RBAY SHAO
3 | JPL | 29 CHAN SHAO
3 | MIT | REUN MDVJ REUN
4 | EMR | MCM4 TSKB WUHN MCM4 SCH2 TSKB WUHN YAKT
4 | GFZ | 1 2 1 DAEJ WUHN WUHN
4 | GRG | DAEJ MAC1 MAW1 RBAY MAC1 MAW1 RBAY
4 | JPL | TIXI
4 | MIT | DAV1 DAV1 MAC1 MAW1 MDVJ
5 | EMR | YAKT
5 | ESA | IRKJ WUHN IRKJ WUHN
5 | GFZ | 1 2 1 QAQ1 QAQ1
5 | GRG | ALRT IRKJ MOBS ALRT BOR1 IRKJ MAL2 MOBS
5 | MIT | KOUR MDVJ PARC
6 | COD | KARR ONSA MAW1 ONSA
6 | EMR | MCM4 MCM4 WES2
6 | ESA | IRKJ NTUS IRKJ
6 | GFZ | 1 2 1 NTUS ONSA NTUS ONSA
6 | GRG | IRKJ KELY WUHN IRKJ KELY MAW1
6 | JPL | CAS1
6 | MIT | ONSA CONZ MDVJ XMIS
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
4 | EMR | ~20:33 | ~ 0.28 ns
6. 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.
7. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G23 | 2014_05_08 | 2014041
G23 | 2014_05_09 | 2014041
8. 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.
9. 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 | -.3 .1 -.6 -19 8 -22 .64
EMR | 0 | 2.0 -5.9 20.0 1 -6 -25 .62
ESA | 0 | .0 .7 -1.4 9 3 15 .51
GFZ | 0 | -.2 .1 -1.3 -3 -22 -5 .11
GRG | 0 | 2.0 -5.9 7.0 -8 6 -10 .63
JPL | 0 | 6.9 -9.3 21.5 -14 -10 84 -.14
MIT | 0 | -2.5 -2.5 17.9 43 12 11 .51
NGS | 0 | .9 -6.8 23.6 -53 1 -6 .54
SIO | 0 | -2.8 .5 -18.4 7 -29 20 .52
COD | 1 | -1.2 .4 -1.4 -26 12 -17 .51
EMR | 1 | 6.7 -12.3 16.4 3 8 -49 .53
ESA | 1 | .0 .3 -1.0 -11 0 2 .35
GFZ | 1 | .3 -.5 -1.8 -18 -28 -13 .11
GRG | 1 | 2.4 -7.4 13.1 -16 26 -12 .39
JPL | 1 | 1.3 -7.1 21.4 -54 -8 76 .04
MIT | 1 | -3.6 -4.9 13.7 10 10 -39 .49
NGS | 1 | -4.4 -13.9 18.7 -105 26 -28 .43
SIO | 1 | -1.8 1.1 -29.1 17 -1 -123 .40
COD | 2 | -.8 .2 -1.3 -34 20 -29 .51
EMR | 2 | 5.3 2.1 8.9 -6 -3 -29 .45
ESA | 2 | .3 1.0 -1.1 -8 -12 20 .42
GFZ | 2 | -.1 -.4 -1.9 -21 -21 -20 .28
GRG | 2 | 6.3 -.8 11.5 -12 9 -20 .67
JPL | 2 | 3.9 1.9 14.2 -15 6 49 .49
MIT | 2 | -.5 -4.9 14.4 -6 -4 -36 .59
NGS | 2 | .8 -12.4 11.2 -80 -5 -9 .75
SIO | 2 | 7.5 -2.1 -25.5 -24 -1 76 .44
COD | 3 | -.7 .7 -1.1 -32 19 -23 .67
EMR | 3 | 11.7 -1.5 7.2 0 -6 -33 .68
ESA | 3 | .5 1.0 -2.0 -11 -21 32 .57
GFZ | 3 | -.6 .3 -2.2 -15 -12 -12 .22
GRG | 3 | 17.3 -7.9 9.0 -8 -1 -18 .69
JPL | 3 | 12.9 -4.2 20.2 -26 -16 15 -.35
MIT | 3 | 3.8 -5.2 13.1 -2 -4 -34 .74
NGS | 3 | 5.3 -12.1 18.8 -81 -26 8 .70
SIO | 3 | 10.9 -3.9 -37.0 20 11 1951 .54
COD | 4 | -1.2 .3 -1.4 -18 39 -40 .58
EMR | 4 | 10.7 -1.7 7.7 14 5 -34 .39
ESA | 4 | .7 .3 -1.2 -10 -15 12 .33
GFZ | 4 | .2 .2 -1.2 -12 -31 -6 -.22
GRG | 4 | 14.3 -3.7 16.2 -13 17 -36 .68
JPL | 4 | 9.6 -8.7 16.8 -8 11 66 -.56
MIT | 4 | 5.9 -6.9 10.2 -3 16 -53 .57
NGS | 4 | .8 -.3 9.0 -12 -7 12 .41
SIO | 4 | 6.2 -1.1 -19.7 -6 -11 -71 .43
COD | 5 | -1.1 .1 -1.7 -25 16 -36 .59
EMR | 5 | 11.7 -2.7 7.6 -5 6 -31 .39
ESA | 5 | .5 .4 -1.3 -15 -29 21 .28
GFZ | 5 | .2 .4 -1.6 -20 -27 -13 -.07
GRG | 5 | 13.0 -6.6 10.8 -19 10 -21 .55
JPL | 5 | 3.4 -6.5 7.5 -47 48 7 -.09
MIT | 5 | 4.9 -7.2 17.3 3 -21 -46 .48
NGS | 5 | 8.8 -11.0 22.7 -101 -41 18 .49
SIO | 5 | 9.3 -1.8 -28.0 3 -1 95 .39
COD | 6 | -.1 .1 -.7 -18 21 -37 .61
EMR | 6 | 8.5 -6.5 3.8 6 12 -28 .58
ESA | 6 | .9 .5 -1.2 -14 -30 29 .51
GFZ | 6 | .9 .1 -1.8 4 -18 -13 .28
GRG | 6 | 3.2 -3.7 5.4 -1 21 -58 .63
JPL | 6 | 2.9 -4.6 23.0 -70 43 5 -.55
MIT | 6 | 6.5 -9.2 14.2 -14 22 -82 .60
NGS | 6 | 10.5 -2.3 17.4 -53 -52 32 .60
SIO | 6 | 7.9 -4.6 -37.8 45 -31 2991 .33
10. 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.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution 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 1.1791.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1791.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 2.1791.[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 3.1791.[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 5.1791.0-6). 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 1791 summary. (May 04, 2014 - May 10, 2014)
Table 1.1791.a GPS week: 1791 MJD: 56781.000-56787.000
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 252| 0 0 -3 22 31 -13 .02 9 9 | -1098 -31 16 108
| 0 0 1 14 18 10 .02 | 203 219
emr 80| 0 0 0 0 -35 44 .29 12 12 | 3507 1000 13 122
| 0 0 1 19 13 22 .02 | 1357 861
esa 150| 0 0 -4 2 5 -6 -.35 12 11 | -615 152 10 167
| 0 0 0 10 15 11 .02 | 1129 1186
gfz 199| 0 -1 0 -7 -1 -5 .08 11 11 | -157 459 10 119
| 0 1 0 12 22 7 .03 | 547 964
grg 181| 3 0 10 -33 -14 1 .24 15 15 | -132 205 15 156
| 0 0 2 15 16 12 .03 | 227 506
igr n/a| 0 0 -1 0 25 -14 -.18 5 5 | 10592 980 16 78
| 0 0 1 14 12 16 .01 | 1485 912
jpl 80| 0 2 -2 4 -6 20 .06 13 12 | 2495 1025 16 133
| 0 1 2 8 16 16 .03 | 1502 860
mit 299| 0 0 4 9 -2 2 -.20 13 11 | -121 54 22 198
| 1 0 1 22 31 16 .03 | 202 340
ngs 228| 0 0 0 -12 3 -24 -.06 12 10 | -1075 -62 1772 3476
| 1 0 2 37 12 22 .03 | 212 232
sio 488| 0 0 -7 -9 -40 702 -.74 22 21 | --- --- --- ---
| 0 0 2 26 70 1260 .09 | --- ---
Table 1.1791.b GPS week : 1791 MJD: 56781.000-56787.000
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 | 4 4 4 4 4 5 5 |
2 | 4 4 4 4 4 4 4 |
3 | 4 4 4 4 4 5 4 |
4 | 4 4 3 3 4 4 3 |
5 | 5 6 5 5 5 6 5 |
6 | 0 0 --- --- --- --- --- |
7 | 5 4 4 4 4 5 4 |
8 | 4 4 3 4 4 3 3 |
9 | 4 4 4 3 4 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 4 5 4 |
12 | 5 5 5 6 6 6 6 |
13 | 5 5 5 5 5 5 5 |
14 | 4 4 5 5 5 5 5 |
15 | 6 6 6 6 6 6 6 |
16 | 5 5 5 5 5 5 5 |
17 | 6 5 5 5 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 4 5 5 5 5 |
20 | 4 4 4 5 5 5 5 |
21 | 4 4 4 4 4 5 4 |
22 | 5 5 4 4 4 4 4 |
23 | 5 5 5 5 0 0 4 |
24 | 4 5 4 4 4 4 4 |
25 | 5 5 5 5 5 5 5 |
26 | 4 4 4 4 4 4 4 |
27 | 5 6 4 5 4 5 5 |
28 | 4 4 4 4 4 4 4 |
29 | 5 6 5 6 6 5 5 |
30 | 0 0 0 0 0 0 0 |
31 | 5 6 5 5 5 5 5 |
32 | 4 5 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
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 2.1791.0 GPS week: 1791 Day: 0 MJD: 56781.000
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 251| 0 0 -1 0 37 -25 .03 9 9 | -966 -249 16 104
emr 80| 0 -2 3 -10 -41 37 .28 12 12 | 1329 1070 15 140
esa 150| 0 0 -4 4 28 -10 -.34 12 11 | -302 554 11 160
gfz 199| 0 0 0 -3 18 -15 .05 12 12 | -354 5 10 119
grg 183| 3 0 4 -47 -37 7 .23 15 15 | -97 -351 16 193
igr n/a| 0 0 -2 -30 16 -33 -.17 5 5 | 8172 956 17 87
jpl 80| 0 1 -3 6 -9 31 .10 13 12 | 250 612 17 142
mit 299| 0 0 3 17 -37 18 -.19 14 13 | -136 -229 23 199
ngs 228| 0 0 2 23 10 -25 -.12 11 10 | -954 -274 1582 3155
sio 497| 0 1 -6 -26 -30 9 -.63 24 20 | --- --- --- ---
Table 2.1791.1 GPS week: 1791 Day: 1 MJD: 56782.000
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 256| 0 0 -4 38 46 -18 .06 10 10 | -855 -274 21 98
emr 80| 1 0 0 -11 -24 37 .29 13 13 | 2308 2333 16 121
esa 150| 0 0 -3 17 17 -30 -.37 11 11 | -686 452 10 160
gfz 202| 0 0 -1 -21 -12 -12 .07 12 12 | -938 2165 12 129
grg 187| 4 0 9 -26 -26 6 .26 15 14 | -349 847 16 138
igr n/a| 0 0 -2 6 12 -20 -.18 5 5 | 9205 2580 17 78
jpl 80| 0 1 -3 7 -20 40 .05 13 12 | 987 2514 19 151
mit 299| -1 0 3 48 4 -7 -.18 13 12 | -290 598 26 164
ngs 229| -2 -1 2 -44 -6 6 -.07 12 11 | -850 -275 1915 3882
sio 494| 0 1 -8 32 5 -122 -.64 22 20 | --- --- --- ---
Table 2.1791.2 GPS week: 1791 Day: 2 MJD: 56783.000
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 254| -1 0 -2 28 0 -9 -.00 7 7 | -1007 63 14 108
emr 80| 1 0 0 -11 -48 30 .31 13 13 | 3110 483 12 121
esa 150| 0 0 -4 -7 7 -3 -.36 11 11 | 741 -395 9 170
gfz 203| -1 0 0 -23 -4 1 .08 10 10 | 714 -680 10 118
grg 186| 3 0 10 -26 7 -1 .29 14 13 | 209 -605 15 138
igr n/a| 0 0 -2 9 7 -33 -.20 5 5 | 10197 644 17 67
jpl 80| 0 2 0 21 19 21 .02 13 13 | 1933 697 15 120
mit 300| -1 0 3 13 32 -6 -.17 13 11 | 187 -481 21 207
ngs 227| 0 0 -1 -1 -1 -17 -.03 10 9 | -932 -48 1479 3174
sio 496| 0 0 -6 10 -197 13 -.75 23 21 | --- --- --- ---
Table 2.1791.3 GPS week: 1791 Day: 3 MJD: 56784.000
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 252| -1 0 -4 15 53 -2 .01 8 8 | -1471 364 18 110
emr 80| 0 0 0 -15 -49 35 .28 12 12 | 3832 1550 12 112
esa 150| 1 0 -3 15 5 -3 -.32 11 11 | -171 -24 12 160
gfz 198| 0 0 0 0 -11 -9 .07 12 12 | 391 -361 11 114
grg 180| 3 0 12 -31 -10 9 .25 15 14 | -219 358 15 129
igr n/a| 0 0 -2 -3 37 -10 -.19 5 4 | 11130 1539 16 77
jpl 80| -1 5 -3 0 -28 20 .07 13 12 | 2875 1649 18 130
mit 300| -1 0 4 11 -3 0 -.19 12 11 | -198 121 20 194
ngs 230| 1 -1 1 -5 10 -27 -.08 10 9 | -1486 385 2000 3556
sio 481| 0 1 -7 6 -11 1962 -.76 22 21 | --- --- --- ---
Table 2.1791.4 GPS week: 1791 Day: 4 MJD: 56785.000
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 -2 15 31 -19 .04 7 8 | -1013 -115 14 106
emr 80| 0 0 0 -2 -14 24 .27 11 11 | 4830 26 15 125
esa 150| 0 0 -3 -11 -2 6 -.38 12 12 | -2891 1774 11 176
gfz 199| 0 -2 0 -6 6 -2 .08 11 11 | -423 482 10 121
grg 179| 4 0 11 -54 -18 -7 .20 16 17 | 21 359 15 195
igr n/a| -1 0 -1 -3 31 5 -.18 5 4 | 12149 -84 14 88
jpl 80| 0 4 0 1 -12 32 .06 13 12 | 4056 1 17 140
mit 300| -1 0 4 -5 -9 6 -.26 13 12 | 10 45 23 210
ngs 228| 0 -1 -2 38 -14 -2 -.04 13 11 | -1007 -116 1596 3422
sio 488| -1 0 -7 -36 -33 -50 -.79 22 23 | --- --- --- ---
Table 2.1791.5 GPS week: 1791 Day: 5 MJD: 56786.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 0 0 -3 42 35 -22 .00 11 11 | -1202 -76 15 121
emr 80| 0 0 -2 13 -27 52 .30 12 12 | 4023 1493 14 124
esa 150| 0 0 -3 0 2 -3 -.34 12 12 | -105 -2055 10 183
gfz 199| 0 -2 -1 11 29 0 .05 11 11 | -298 441 10 115
grg 179| 3 0 9 -37 -19 16 .20 16 14 | -456 296 14 159
igr n/a| 0 0 -2 12 38 -16 -.17 5 5 | 11227 1164 15 72
jpl 80| -1 2 -4 2 6 -2 .08 12 12 | 3180 1328 15 132
mit 300| 0 0 4 4 -42 25 -.21 12 10 | -414 121 22 225
ngs 228| 1 1 4 -69 2 -57 -.06 13 12 | -1126 -177 1832 3540
sio 481| 0 0 -11 -28 -10 88 -.70 22 20 | --- --- --- ---
Table 2.1791.6 GPS week: 1791 Day: 6 MJD: 56787.000
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 256| -1 2 -2 20 12 0 .02 8 8 | -1177 68 15 110
emr 80| 0 0 0 39 -42 91 .27 12 12 | 5118 46 13 114
esa 150| 0 0 -4 0 -20 0 -.34 12 12 | -896 759 11 160
gfz 196| 0 -1 -1 -10 -37 1 .14 11 11 | -193 1165 11 118
grg 179| 1 0 12 -7 6 -20 .23 15 14 | -36 532 14 145
igr n/a| 0 0 1 4 31 4 -.19 6 6 | 12070 61 17 82
jpl 80| 0 0 -5 -6 -1 0 .06 13 12 | 4187 375 16 119
mit 300| 1 -1 6 -24 39 -22 -.22 12 10 | -7 208 25 188
ngs 228| 0 0 0 -27 23 -46 -.02 11 10 | -1173 69 2000 3604
sio 483| 0 0 -4 -26 -8 3019 -.87 22 20 | --- --- --- ---
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 3.1791.0 GPS week: 1791 Day: 0 MJD: 56781.000
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 7 12 12 9 4 14 8 9 13 4 | 41 41 35 42 48 34 44 37 37 29 39
2 | 11 8 11 10 11 5 10 15 7 34 4 | 18 26 21 25 24 19 21 28 20 28 20
3 | 7 8 10 10 11 5 8 12 10 43 3 | 32 29 31 29 24 26 28 25 34 51 28
4 | 11 9 12 10 11 6 10 14 12 21 4 | 26 26 23 31 31 21 23 32 29 34 25
5 | 9 12 9 15 19 3 15 23 9 17 5 | 24 25 16 24 28 17 24 19 24 18 19
X6 | 3 --- --- --- --- 68 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
7 | 8 11 15 14 16 5 11 10 12 29 4 | 31 29 21 32 31 21 26 25 24 32 25
8 | 5 8 12 8 12 5 8 14 8 16 3 | 24 25 21 24 20 20 23 27 23 25 21
9 | 6 8 14 7 11 6 10 19 10 17 4 | 27 25 22 26 24 23 25 31 26 24 24
10 | 7 8 11 10 12 6 9 15 13 25 4 | 24 29 24 23 23 20 27 24 25 37 23
11 | 8 8 13 11 11 4 11 8 9 39 3 | 40 40 32 37 49 32 37 36 35 52 37
12E | 9 13 8 12 25 5 19 13 11 11 5 | 28 26 21 32 21 21 24 25 25 23 23
13 | 7 13 11 17 21 6 13 19 11 14 5 | 24 27 18 29 36 18 25 18 20 18 20
14 | 8 13 10 12 16 6 12 7 10 19 4 | 23 22 17 26 26 18 20 17 20 21 19
15 | 10 19 13 17 21 5 16 23 13 19 6 | 30 35 22 36 31 27 27 26 29 22 26
16E | 7 19 8 13 12 5 17 12 18 13 5 | 28 25 22 28 27 23 24 23 33 20 24
17 | 10 13 13 13 18 13 16 16 19 30 5 | 28 33 25 32 34 28 28 31 36 28 27
18 | 9 13 9 13 19 5 13 10 12 18 4 | 26 27 22 24 26 21 25 20 24 19 21
19 | 9 13 12 14 15 5 14 11 8 27 4 | 27 30 24 28 31 23 26 23 25 21 24
20 | 8 11 9 12 15 4 14 9 9 20 4 | 24 24 21 18 22 18 23 17 23 26 19
21 | 9 9 13 12 13 5 11 9 12 35 4 | 24 28 23 29 28 22 24 25 31 34 24
22 | 8 10 10 10 18 4 9 13 15 18 4 | 25 24 20 25 31 19 22 18 27 19 21
23 | 8 14 9 16 16 5 16 12 10 22 4 | 23 25 18 22 27 17 23 16 22 16 20
24 | 8 8 13 9 17 5 11 13 10 11 4 | 24 26 24 25 27 19 28 19 19 12 22
25E | 8 11 14 9 15 5 12 20 10 16 4 | 22 25 28 21 23 17 22 27 20 19 21
26 | 10 8 11 9 13 4 8 14 10 18 4 | 23 24 19 20 18 18 20 17 21 21 19
X27 | 13 9 12 14 --- 6 13 9 11 15 4 | 28 22 24 24 --- 20 26 21 23 15 21
28E | 7 11 11 10 12 4 13 14 12 26 4 | 28 25 23 26 24 22 26 33 31 37 25
29 | 9 15 13 16 15 6 17 12 11 28 5 | 32 36 34 35 28 29 33 27 31 34 30
X30 | 3 --- --- --- --- 13 --- --- --- --- 0 | 30 --- --- --- --- 22 --- --- --- --- 29
31 | 13 12 13 13 17 7 11 14 12 32 5 | 24 31 24 32 36 25 29 25 30 29 26
32 | 8 12 11 12 15 6 10 16 9 18 4 | 31 29 29 24 24 26 28 30 27 29 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 11 12 15 5 13 14 11 24 |T 27 27 23 27 28 22 26 24 26 26 24
WRMS | 9 12 11 12 15 5 12 13 10 20 |NE 27 28 23 27 29 22 26 24 26 26 24
MEDI | 8 11 11 12 15 5 12 13 10 19 |MD 26 26 22 26 27 21 25 25 25 24 24
Table 3.1791.1 GPS week: 1791 Day: 1 MJD: 56782.000
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 | 5 6 13 14 13 4 14 11 9 13 4 | 26 30 23 25 34 20 31 23 21 19 24
2 | 12 7 12 11 12 4 11 13 11 26 4 | 17 21 19 20 21 16 18 22 19 20 17
3 | 7 8 11 11 12 7 9 13 11 42 4 | 27 29 27 26 28 23 29 24 26 50 25
4 | 13 8 10 8 10 6 8 13 15 17 4 | 23 19 16 20 22 15 18 23 12 25 17
5 | 13 15 9 15 20 5 13 20 10 14 5 | 24 27 16 23 29 17 23 20 22 17 18
X6 | 4 --- --- --- --- 517 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
7 | 8 9 14 13 12 5 11 9 9 32 4 | 24 26 19 26 27 19 21 22 20 32 21
8 | 6 10 11 10 9 5 12 13 12 14 4 | 20 21 18 19 18 16 22 22 18 20 17
9 | 6 10 11 8 7 6 11 14 10 18 3 | 21 22 20 19 19 18 22 24 18 22 19
10 | 8 10 11 9 9 5 8 13 11 22 3 | 21 28 20 21 22 19 24 25 23 33 21
11 | 7 8 14 15 12 4 10 9 10 29 4 | 26 32 22 22 35 21 27 24 21 36 24
12E | 10 12 9 12 23 5 19 12 13 13 5 | 26 25 19 27 19 21 21 24 24 25 21
13 | 11 11 10 15 19 6 12 19 9 14 5 | 22 27 15 23 33 16 22 15 18 17 17
14 | 8 11 8 13 15 5 14 11 10 22 4 | 22 22 16 25 25 16 19 19 18 22 18
15 | 13 18 10 16 18 5 16 24 13 16 6 | 26 34 18 28 29 21 24 23 23 20 21
16E | 12 22 8 11 13 4 16 12 14 11 5 | 26 28 20 25 24 21 21 22 24 19 21
17 | 11 12 12 16 18 6 14 15 13 23 5 | 26 33 24 31 32 24 27 27 28 24 25
18 | 9 13 8 10 18 5 15 12 11 23 4 | 23 24 19 20 25 17 24 20 16 21 19
19 | 7 12 12 16 16 7 15 11 12 28 4 | 21 28 21 26 26 19 27 21 20 20 21
20 | 8 11 12 10 15 3 13 11 11 20 4 | 15 20 17 11 19 10 18 13 17 26 12
21 | 7 10 12 10 15 3 9 10 16 31 4 | 15 23 17 17 19 14 21 17 18 21 16
22 | 8 13 8 11 19 6 13 11 15 22 4 | 22 22 17 19 27 16 21 17 22 20 18
23 | 10 15 9 14 12 4 15 12 13 23 4 | 17 23 12 18 20 12 18 15 19 14 14
24 | 13 9 15 13 13 5 14 10 15 11 5 | 21 28 23 22 25 20 27 22 22 16 21
25E | 13 19 15 8 15 6 10 16 12 13 5 | 21 33 26 19 22 18 21 21 18 21 20
26 | 12 11 11 10 13 4 10 12 10 21 4 | 22 24 19 19 20 18 19 22 21 27 19
X27 | 11 22 14 14 --- 6 12 9 14 12 5 | 19 30 20 18 --- 16 23 17 20 11 18
28E | 10 12 8 11 15 6 12 14 8 16 4 | 26 23 20 23 22 20 23 29 24 26 22
29 | 12 18 13 14 14 5 15 13 14 23 5 | 24 32 21 26 23 19 24 21 21 25 20
X30 | 4 --- --- --- --- 18 --- --- --- --- 0 | 26 --- --- --- --- 24 --- --- --- --- 26
31 | 14 22 13 13 18 6 13 14 14 24 5 | 25 38 22 27 34 21 28 24 22 25 24
32 | 9 12 11 15 14 4 11 13 9 16 4 | 23 26 21 20 20 18 20 24 23 24 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 11 12 15 5 13 13 12 22 |T 22 26 19 22 24 18 22 21 20 23 19
WRMS | 10 13 11 12 14 5 12 12 11 20 |NE 22 26 19 21 25 17 22 21 20 23 19
MEDI | 9 11 11 12 14 5 12 12 11 20 |MD 23 26 19 22 24 18 22 22 21 21 20
Table 3.1791.2 GPS week: 1791 Day: 2 MJD: 56783.000
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 | 5 8 12 9 13 4 15 8 6 9 3 | 30 35 25 30 40 27 36 28 25 23 29
2 | 9 9 13 9 8 4 9 14 8 29 3 | 14 21 19 19 18 17 19 22 19 29 16
3 | 7 9 10 9 14 5 8 7 9 42 3 | 18 22 16 18 21 15 17 15 17 42 16
4 | 8 9 11 10 8 5 8 11 5 19 3 | 19 24 18 22 23 19 21 24 20 30 19
5 | 8 17 10 13 19 4 12 22 11 19 5 | 19 28 18 23 29 16 20 20 20 23 17
7 | 7 13 14 11 12 4 11 9 10 34 4 | 28 31 21 27 30 21 22 23 25 34 24
8 | 3 11 11 7 8 5 10 10 7 12 3 | 20 24 18 18 20 17 21 20 20 19 19
9 | 4 11 12 6 8 4 10 13 8 14 3 | 24 27 22 22 23 21 23 26 25 24 23
10 | 6 10 11 10 10 6 13 12 9 23 3 | 24 29 23 24 23 20 26 25 23 33 23
11 | 7 9 13 9 14 3 11 6 8 50 3 | 30 36 27 29 43 26 32 29 26 54 29
12E | 8 16 10 9 16 4 19 13 10 11 4 | 26 29 21 26 26 21 21 24 25 21 23
13 | 10 13 11 12 17 6 13 19 8 11 4 | 26 29 16 24 34 17 22 18 21 17 20
14 | 8 15 10 13 15 8 15 11 14 17 4 | 24 24 19 23 26 16 19 17 18 19 19
15 | 8 18 8 11 16 4 16 23 14 13 5 | 26 32 20 27 26 22 24 24 23 24 21
16E | 7 17 8 14 18 5 17 12 9 12 4 | 22 23 19 26 24 20 20 22 25 20 20
17 | 6 14 15 10 16 6 15 12 10 23 4 | 25 34 22 26 32 23 27 24 30 21 24
18 | 8 14 9 11 18 6 19 11 11 21 4 | 20 26 19 19 26 17 27 17 17 21 18
19 | 7 14 12 11 14 5 13 9 10 21 4 | 22 30 23 26 31 22 27 21 20 21 23
20 | 6 12 10 9 13 5 13 11 8 19 3 | 16 24 16 16 18 13 18 13 19 25 15
21 | 8 10 12 11 14 5 13 10 13 35 4 | 17 23 18 20 22 17 22 20 20 26 18
22 | 8 13 9 9 17 6 14 12 11 19 4 | 20 24 18 19 28 15 19 14 21 20 18
23 | 8 16 8 15 10 4 18 11 9 22 4 | 18 27 14 19 23 13 21 17 20 15 17
24 | 9 10 14 9 12 4 11 11 8 11 4 | 23 27 23 23 24 20 26 21 24 18 22
25E | 7 12 16 7 16 5 14 16 9 13 4 | 21 25 27 22 21 18 24 22 20 17 20
26 | 7 11 11 8 13 6 8 10 9 20 3 | 23 25 22 23 21 21 20 22 22 27 21
X27 | 8 10 13 12 --- 5 11 7 10 15 4 | 20 24 21 18 --- 18 24 19 23 18 19
28E | 8 11 9 7 14 4 11 14 9 13 4 | 30 26 23 23 24 22 23 29 23 26 24
29 | 8 18 14 13 14 4 17 15 10 24 5 | 27 34 29 27 29 25 30 25 28 26 26
X30 | 2 --- --- --- --- 24 --- --- --- --- 0 | 28 --- --- --- --- 23 --- --- --- --- 27
31 | 9 11 13 11 16 5 13 13 11 27 4 | 25 31 19 27 33 20 25 23 25 28 23
32 | 5 9 10 11 13 6 11 13 9 20 3 | 24 27 22 21 21 18 22 24 26 24 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 11 10 14 5 13 13 10 23 |T 22 27 20 22 26 19 23 21 22 24 21
WRMS | 7 13 11 10 13 5 13 11 9 21 |NE 22 27 20 22 26 19 23 21 22 25 21
MEDI | 8 11 11 10 14 5 13 11 9 19 |MD 23 27 20 23 24 20 22 22 22 23 21
Table 3.1791.3 GPS week: 1791 Day: 3 MJD: 56784.000
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 | 7 7 12 11 12 4 16 8 11 7 4 | 27 34 29 34 41 28 36 30 28 26 30
2 | 10 9 12 11 12 3 10 12 9 23 4 | 16 21 16 15 20 11 16 18 16 20 14
3 | 6 8 11 8 14 4 11 8 10 36 3 | 20 21 17 19 21 14 18 17 19 36 17
4 | 7 7 10 9 9 4 8 12 8 18 3 | 23 22 19 21 27 19 22 24 23 28 21
5 | 7 10 10 14 19 4 14 21 9 15 5 | 20 26 17 21 26 17 24 17 20 20 17
7 | 7 11 14 12 13 4 11 10 9 36 4 | 27 28 21 31 28 21 24 23 25 36 23
8 | 7 9 11 9 11 4 10 10 11 12 3 | 21 20 17 19 18 17 23 19 20 16 18
9 | 6 10 12 6 9 5 10 11 6 11 3 | 26 24 21 22 21 20 24 24 21 18 21
10 | 6 9 12 10 12 4 9 11 9 26 3 | 22 26 24 22 21 21 27 23 23 34 22
11 | 8 10 13 12 16 3 10 7 12 35 4 | 27 36 27 34 45 27 32 31 24 41 29
12E | 9 16 9 12 20 4 23 13 13 11 5 | 26 27 17 26 25 18 26 26 24 21 22
13 | 8 12 11 12 18 4 13 19 12 12 5 | 22 27 15 22 32 17 23 18 25 14 19
14 | 10 15 9 14 14 6 14 10 10 14 4 | 25 24 18 27 25 17 22 18 17 17 20
15 | 8 19 10 15 17 4 20 22 15 13 6 | 25 29 17 29 27 20 24 25 30 23 21
16E | 7 19 8 12 19 5 12 12 8 12 4 | 24 26 21 26 22 20 23 22 25 18 22
17 | 6 14 13 10 16 4 17 14 9 31 4 | 24 33 23 29 35 24 29 28 30 29 26
18 | 9 15 10 14 17 6 13 10 10 21 4 | 19 28 19 18 24 14 27 16 17 20 17
19 | 8 14 12 15 15 5 13 10 10 26 4 | 20 27 21 29 30 21 24 21 22 23 21
20 | 10 12 10 14 16 5 12 11 13 20 4 | 20 22 19 15 16 15 20 13 21 23 15
21 | 9 9 12 11 14 5 10 10 14 36 4 | 15 22 20 22 26 16 20 21 22 27 18
22 | 8 12 10 11 16 5 13 10 9 25 4 | 20 24 19 20 26 13 22 13 18 23 17
23 | 9 14 10 14 12 4 16 11 8 21 4 | 15 23 13 15 22 9 19 14 17 17 14
24 | 6 10 12 8 14 3 11 9 9 12 3 | 20 25 22 21 25 18 25 20 21 17 20
25E | 6 10 14 10 17 5 13 14 11 14 4 | 21 24 26 19 29 17 24 22 19 20 20
26 | 9 10 10 10 13 5 11 14 11 23 4 | 25 25 18 21 18 19 21 20 25 27 20
X27 | 14 10 15 9 --- 5 12 10 12 12 5 | 22 19 20 20 --- 16 23 16 18 15 17
28E | 8 11 7 8 17 4 11 14 9 16 4 | 26 23 21 23 21 20 25 26 27 24 22
29 | 8 18 14 15 16 6 18 15 11 24 5 | 22 28 23 21 24 18 24 20 25 21 20
X30 | 4 --- --- --- --- 16 --- --- --- --- 0 | 28 --- --- --- --- 24 --- --- --- --- 28
31 | 10 12 13 13 19 5 11 11 14 23 4 | 29 33 24 32 36 26 30 27 29 27 27
32 | 8 11 10 13 14 5 8 12 8 17 4 | 27 28 24 22 19 21 24 25 23 26 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 11 12 15 5 13 12 10 22 |T 22 25 20 23 25 18 24 21 22 23 20
WRMS | 8 12 11 12 14 4 12 11 9 21 |NE 22 25 20 23 26 18 23 20 22 24 20
MEDI | 8 11 11 11 15 4 12 11 10 18 |MD 22 25 20 22 25 18 24 21 22 23 20
Table 3.1791.4 GPS week: 1791 Day: 4 MJD: 56785.000
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 | 5 7 13 10 12 5 14 10 13 10 4 | 29 33 27 35 37 28 36 28 27 27 29
2 | 9 9 12 11 10 4 10 12 15 26 4 | 16 20 19 20 15 15 17 19 20 20 15
3 | 6 8 12 10 16 4 9 11 10 37 3 | 21 22 18 19 18 17 20 16 22 39 18
4 | 6 7 10 9 11 4 10 10 12 12 3 | 18 22 19 23 22 20 21 23 22 24 19
5 | 8 13 9 13 16 4 14 19 9 12 4 | 23 27 20 25 27 21 24 21 24 23 20
7 | 7 9 15 10 14 4 10 11 8 29 4 | 27 30 23 29 31 24 25 27 31 35 25
8 | 5 8 13 10 9 4 8 11 10 13 3 | 19 21 19 19 19 18 21 21 27 19 19
9 | 7 9 12 10 8 5 9 10 10 13 3 | 24 25 22 25 21 23 23 25 31 21 23
10 | 6 8 12 10 10 6 8 11 8 26 3 | 22 27 23 23 20 23 24 24 25 34 22
11 | 6 8 15 9 15 4 10 9 13 52 4 | 30 33 25 31 39 26 33 26 28 56 29
12E | 7 14 9 10 29 5 20 13 16 10 5 | 29 31 24 31 25 25 30 29 32 24 27
13 | 8 11 11 8 22 4 10 20 15 9 5 | 26 28 22 30 35 24 25 25 35 20 25
14 | 7 14 9 9 18 7 14 9 15 17 4 | 25 23 19 25 28 22 23 20 27 20 21
15 | 7 19 10 15 21 5 17 21 14 17 5 | 28 34 20 33 28 24 28 26 31 26 25
16E | 7 11 9 13 20 5 14 14 15 8 4 | 29 27 26 30 26 26 27 26 30 23 26
17 | 9 10 15 19 15 4 14 12 14 30 5 | 27 33 28 43 35 29 30 29 35 35 29
18 | 9 12 9 10 19 4 14 12 16 18 4 | 24 25 21 21 23 19 25 21 19 20 20
19 | 7 13 14 13 16 4 13 11 9 22 4 | 24 29 22 29 30 23 27 23 24 23 23
20 | 8 12 11 10 17 4 15 12 12 19 4 | 23 24 23 18 18 18 24 17 22 28 19
21 | 8 9 12 7 13 4 12 11 14 33 4 | 20 22 21 21 19 19 21 22 22 26 18
22 | 8 9 11 8 15 5 11 9 12 23 4 | 21 22 17 21 24 18 19 18 22 24 18
X23 | 3 --- --- --- --- 101 --- --- --- --- 0 | 38 --- --- --- --- 226 --- --- --- --- 38
24 | 6 7 13 9 14 3 12 10 13 10 4 | 22 26 23 25 25 21 29 21 23 16 22
25E | 7 9 14 11 16 4 12 15 18 15 4 | 24 28 28 25 22 23 31 28 29 22 24
26 | 9 9 8 15 11 5 10 13 8 14 4 | 23 25 22 28 21 21 20 23 22 22 22
X27 | 7 8 14 10 --- 3 12 11 10 13 4 | 20 21 21 21 --- 20 26 21 24 16 19
28E | 7 10 8 8 19 4 11 12 8 12 4 | 26 22 22 24 22 22 24 27 29 22 23
29 | 8 17 13 13 16 4 19 14 18 23 5 | 26 29 24 26 22 23 25 23 27 24 22
X30 | 3 --- --- --- --- 22 --- --- --- --- 0 | 31 --- --- --- --- 32 --- --- --- --- 30
31 | 11 15 13 11 19 5 13 16 13 25 5 | 24 32 23 28 34 23 30 27 29 26 25
32 | 8 9 11 12 16 4 8 11 11 23 4 | 27 26 23 22 18 21 21 24 26 29 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 11 12 11 16 5 13 13 13 22 |T 24 26 22 25 25 28 25 23 26 25 23
WRMS | 8 11 12 11 17 4 12 12 11 23 |NE 24 26 21 25 25 29 24 22 25 26 22
MEDI | 7 9 12 10 16 4 12 11 13 17 |MD 24 26 22 25 23 23 25 23 27 24 23
Table 3.1791.5 GPS week: 1791 Day: 5 MJD: 56786.000
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 | 14 8 15 14 14 6 15 6 15 11 5 | 23 29 20 29 33 20 33 22 18 19 23
2 | 10 7 12 11 8 3 8 10 18 27 4 | 16 18 16 15 13 13 17 15 24 17 13
3 | 7 9 12 13 16 5 9 9 20 33 4 | 19 21 17 19 20 14 18 15 23 35 16
4 | 6 8 10 9 7 2 6 8 15 16 3 | 21 21 19 20 22 18 23 19 26 22 19
5 | 10 15 9 16 18 4 13 19 13 12 5 | 19 24 13 20 27 13 22 14 21 16 14
7 | 9 10 14 12 16 6 11 10 11 30 4 | 27 28 19 26 29 20 23 21 22 29 21
8 | 6 8 10 10 10 4 9 7 9 13 3 | 20 21 18 19 19 17 23 18 22 19 18
9 | 8 9 10 8 9 4 9 9 10 15 3 | 24 23 20 20 17 18 22 20 19 21 19
10 | 8 7 12 9 11 5 7 11 13 22 3 | 23 25 21 19 22 17 24 23 22 30 20
11 | 12 10 17 9 14 5 10 6 15 49 4 | 24 30 22 25 34 21 28 23 26 53 23
12E | 11 13 9 13 25 6 22 12 14 10 5 | 24 27 18 26 18 17 27 23 23 17 20
13 | 11 12 9 9 23 4 12 18 11 11 5 | 27 27 19 21 34 16 22 16 23 14 19
14 | 16 12 9 14 19 6 12 11 13 17 5 | 26 21 15 25 26 17 22 20 24 16 18
15 | 11 19 12 14 17 4 18 21 15 16 6 | 23 32 17 29 26 19 26 18 21 17 19
16E | 12 15 10 10 20 3 12 14 11 8 5 | 23 25 20 24 20 20 21 23 25 16 21
17 | 9 12 12 10 17 3 14 11 16 25 4 | 24 30 23 27 31 22 28 24 34 19 24
18 | 16 13 12 12 16 5 15 12 8 25 5 | 24 25 20 20 25 16 28 17 19 23 18
19 | 10 12 13 14 20 6 11 9 17 25 5 | 17 25 18 20 27 15 21 16 21 14 17
20 | 11 13 11 10 18 6 12 10 11 17 4 | 19 21 17 17 18 13 20 11 14 18 12
21 | 14 8 14 7 13 3 11 10 12 34 4 | 17 20 19 15 17 13 20 18 17 26 14
22 | 11 11 12 10 17 5 10 9 13 24 4 | 17 23 16 22 26 15 24 17 20 22 16
X23 | 4 --- --- --- --- 15 --- --- --- --- 0 | 15 --- --- --- --- 27 --- --- --- --- 12
24 | 8 9 14 9 12 5 11 13 14 9 4 | 19 25 21 22 22 17 26 18 19 10 18
25E | 10 11 14 9 16 4 12 13 14 16 4 | 23 25 26 19 20 17 26 20 20 20 19
26 | 11 8 10 10 12 5 9 9 14 15 4 | 19 21 16 19 16 14 22 17 16 19 16
X27 | 9 8 15 11 --- 5 11 9 10 14 4 | 17 19 21 19 --- 15 24 16 18 13 16
28E | 9 13 6 9 12 5 10 11 13 10 4 | 26 23 21 25 21 20 24 25 28 17 22
29 | 13 16 13 13 16 5 16 12 12 25 5 | 26 26 21 23 21 19 25 19 22 18 19
X30 | 4 --- --- --- --- 17 --- --- --- --- 0 | 26 --- --- --- --- 21 --- --- --- --- 25
31 | 12 14 14 12 17 5 10 11 13 23 4 | 21 30 18 23 31 17 25 22 20 23 20
32 | 10 10 10 14 15 5 7 11 8 18 4 | 28 28 24 22 20 20 24 21 21 24 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 12 11 16 5 12 12 13 22 |T 21 24 19 21 23 17 23 19 21 20 18
WRMS | 11 11 12 11 14 5 12 10 12 20 |NE 21 24 18 21 24 17 23 18 21 21 18
MEDI | 10 11 12 10 16 5 11 11 13 17 |MD 23 25 19 21 22 17 24 19 21 19 19
Table 3.1791.6 GPS week: 1791 Day: 6 MJD: 56787.000
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 7 15 12 14 6 15 9 14 14 4 | 40 43 34 45 50 36 45 37 31 36 38
2 | 9 8 11 11 9 5 9 10 9 24 3 | 21 27 22 24 24 20 25 26 22 23 21
3 | 7 9 10 9 14 5 8 9 12 39 3 | 22 26 21 24 22 17 25 17 22 41 20
4 | 6 7 7 7 9 4 5 9 11 13 3 | 28 31 29 31 36 29 31 32 28 31 29
5 | 9 15 10 14 18 5 16 18 13 16 5 | 26 34 23 27 33 22 32 17 22 27 23
7 | 8 10 13 13 13 6 11 8 11 34 4 | 33 35 27 36 35 27 31 29 28 41 29
8 | 5 8 10 11 10 5 9 6 8 11 3 | 25 29 23 26 28 22 30 23 24 22 24
9 | 7 10 11 10 10 5 9 6 8 16 3 | 30 33 28 31 32 27 33 28 28 28 29
10 | 6 7 10 10 10 3 8 12 9 18 3 | 29 36 30 27 29 26 35 30 26 34 29
11 | 8 8 15 8 14 5 10 7 11 46 4 | 35 39 29 38 48 32 37 35 30 56 34
12E | 9 19 8 15 23 5 20 13 9 9 5 | 30 37 24 33 27 25 29 31 23 23 27
13 | 7 12 8 12 19 6 12 18 8 9 4 | 31 33 21 31 39 24 28 24 27 21 26
14 | 10 17 10 10 15 8 11 10 9 16 4 | 30 29 21 32 33 24 27 25 23 21 25
15 | 10 22 11 14 17 7 18 21 19 11 6 | 36 38 25 38 32 30 33 29 36 30 30
16E | 7 16 10 12 14 6 14 13 8 8 4 | 31 35 32 35 32 29 33 30 29 28 30
17 | 8 13 14 11 16 6 14 11 8 35 4 | 32 39 30 40 44 34 36 36 38 40 34
18 | 10 12 12 12 17 7 14 13 13 21 4 | 30 33 28 25 31 22 35 18 22 26 25
19 | 10 12 12 14 16 8 14 10 11 20 4 | 28 34 26 35 36 27 30 27 26 26 28
20 | 9 14 11 11 18 6 17 14 15 17 5 | 25 30 25 24 25 19 30 22 25 26 22
21 | 10 8 14 10 12 4 11 12 10 38 4 | 21 28 25 27 28 20 27 28 20 33 22
22 | 8 10 12 8 17 6 10 9 14 21 4 | 25 28 24 24 30 19 28 19 20 22 22
23 | 7 15 7 13 11 8 15 12 10 15 4 | 15 18 9 9 8 19 16 8 7 7 16
24 | 12 11 13 7 15 6 14 9 8 12 4 | 33 31 28 31 28 26 32 24 22 21 27
25E | 7 10 14 10 15 7 14 11 12 14 4 | 30 32 33 30 32 28 36 31 24 27 29
26 | 10 13 12 10 11 7 10 9 10 19 4 | 30 30 25 30 26 22 29 23 21 25 26
X27 | 13 10 17 10 --- 7 12 9 10 14 4 | 26 26 26 26 --- 21 31 23 23 20 24
28E | 7 11 8 10 18 6 12 11 9 6 4 | 28 26 24 27 28 23 27 26 27 20 25
29 | 9 17 15 13 14 11 17 12 13 23 5 | 25 33 24 27 30 24 30 25 22 26 24
X30 | 2 --- --- --- --- 20 --- --- --- --- 0 | 35 --- --- --- --- 26 --- --- --- --- 34
31 | 8 10 16 10 17 6 12 9 11 23 4 | 26 34 22 31 38 24 32 27 26 28 27
32 | 6 9 10 13 15 7 9 10 11 17 4 | 32 33 32 29 28 26 32 30 33 32 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 12 11 15 6 13 12 11 22 |T 28 32 25 29 31 24 30 26 25 28 26
WRMS | 8 12 12 11 14 6 12 10 10 20 |NE 28 31 25 29 31 24 30 25 25 28 26
MEDI | 8 10 11 11 15 6 12 10 10 16 |MD 30 33 25 30 31 24 31 26 24 26 27
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 4.1791 GPS week: 1791 MJD: 56781.0-56787.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
igs | igs 2852 | 7 6 18 | 9 11 27 | 7 9 17 |
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 5.1791.0 GPS week: 1791 Day: 0 MJD: 56781.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
igs | igs 2880 | 4 5 11 | 5 6 14 | 8 8 19 |
Table 5.1791.1 GPS week: 1791 Day: 1 MJD: 56782.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
igs | igs 2880 | 6 6 16 | 5 6 23 | 9 14 19 |
Table 5.1791.2 GPS week: 1791 Day: 2 MJD: 56783.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
igs | igs 2880 | 8 8 20 | 7 7 22 | 7 9 15 |
Table 5.1791.3 GPS week: 1791 Day: 3 MJD: 56784.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
igs | igs 2880 | 5 5 16 | 6 9 17 | 8 9 17 |
Table 5.1791.4 GPS week: 1791 Day: 4 MJD: 56785.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
igs | igs 2784 | 9 7 26 | 6 5 17 | 7 9 16 |
Table 5.1791.5 GPS week: 1791 Day: 5 MJD: 56786.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
igs | igs 2784 | 7 7 15 | 7 11 25 | 7 10 14 |
Table 5.1791.6 GPS week: 1791 Day: 6 MJD: 56787.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
igs | igs 2880 | 9 7 22 | 27 31 73 | 7 6 18 |
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 6.1791 GPS week: 1791 MJD: 56781.500-56787.500
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 | -69 -30 32 -187 3 | 16 21
| 19 16 70 89 5 | 1
emr uuuxu | 60 -4 -49 379 3 | 50 54
| 18 5 101 50 9 | 4
esa uuuuu | -10 -4 64 -11 1 | 19 22
| 12 10 45 74 3 | 1
gfz uuuuu | -10 6 -43 -97 3 | 22 24
| 21 17 72 97 4 | 1
grg uuxuu | 32 46 -329 108 -3 | 30 32
| 11 13 82 77 4 | 3
igr xxxxx | -12 24 -7 85 0 | 7 14
| 12 19 77 64 5 | 1
irf xxxxx | 18 2 -46 40 -1 | 2 13
| 16 7 31 17 1 | 1
jpl uuuuu | 33 -5 -18 251 8 | 33 38
| 20 10 73 56 10 | 5
mit uuuuu | 13 1 -60 1 -4 | 23 26
| 43 17 59 38 3 | 2
ngs uuuuu | 1 22 68 84 -4 | 9 16
| 54 43 137 102 5 | 2
sio xxxxx | 39 34 50 175 -1 | 46 49
| 27 17 83 45 8 | 1
Table 7.1791.0 GPS week: 1791 Day: 0 MJD: 56781.500
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 | -58 -18 40 -66 2 | 15 19
emr uuuxu | 48 -5 -32 331 14 | 44 49
esa uuuuu | -25 -2 10 42 0 | 20 22
gfz uuuuu | -17 18 -75 9 8 | 20 22
grg uuxuu | 27 51 -362 34 -8 | 33 34
igr xxxxx | 7 55 -77 58 3 | 6 12
irf xxxxx | -5 8 -91 35 -1 | 1 12
jpl uuuuu | 21 11 -19 180 24 | 25 32
mit uuuuu | -46 -21 -100 -27 -2 | 22 25
ngs uuuuu | 71 -9 120 -102 -11 | 10 16
sio xxxxx | 18 32 51 138 2 | 44 46
Table 7.1791.1 GPS week: 1791 Day: 1 MJD: 56782.500
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 | -79 -43 -3 -339 14 | 16 20
emr uuuxu | 44 -1 1 439 4 | 48 52
esa uuuuu | -19 -14 26 103 -3 | 20 23
gfz uuuuu | 20 26 -146 43 3 | 22 24
grg uuxuu | 40 38 -368 7 -2 | 33 34
igr xxxxx | -9 9 -56 175 10 | 8 13
irf xxxxx | 14 -4 -64 72 0 | 3 12
jpl uuuuu | 43 -5 -103 197 7 | 30 37
mit uuuuu | -12 -4 -39 14 0 | 24 26
ngs uuuuu | -2 22 237 87 -10 | 11 16
sio xxxxx | 5 15 183 191 13 | 46 48
Table 7.1791.2 GPS week: 1791 Day: 2 MJD: 56783.500
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 | -38 -30 71 -184 -1 | 18 22
emr uuuxu | 92 0 86 406 11 | 48 53
esa uuuuu | -17 2 54 37 2 | 20 22
gfz uuuuu | -6 16 7 -71 3 | 22 25
grg uuxuu | 26 54 -460 205 -6 | 32 33
igr xxxxx | -16 10 108 56 -3 | 8 14
irf xxxxx | 24 9 -35 28 -1 | 3 12
jpl uuuuu | 2 -3 -53 229 -8 | 32 38
mit uuuuu | 39 2 -38 -49 -3 | 24 27
ngs uuuuu | -38 -5 -152 49 1 | 11 16
sio xxxxx | 60 31 47 137 -3 | 48 50
Table 7.1791.3 GPS week: 1791 Day: 3 MJD: 56784.500
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 | -88 -21 -7 -159 1 | 17 22
emr uuuxu | 78 -1 -62 310 -5 | 51 55
esa uuuuu | -12 -18 132 -49 2 | 19 22
gfz uuuuu | -3 -16 84 -107 6 | 23 25
grg uuxuu | 33 45 -360 132 1 | 31 32
igr xxxxx | -33 19 31 35 -4 | 8 14
irf xxxxx | 20 9 -72 36 -1 | 4 12
jpl uuuuu | 66 4 31 281 12 | 33 38
mit uuuuu | 33 27 -170 -17 -4 | 24 27
ngs uuuuu | -25 7 -15 85 -5 | 10 16
sio xxxxx | 43 57 -99 131 0 | 47 49
Table 7.1791.4 GPS week: 1791 Day: 4 MJD: 56785.500
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 | -54 -14 -88 -110 2 | 14 22
emr uuuxu | 44 -13 23 437 3 | 50 54
esa uuuuu | -1 11 68 -42 0 | 17 21
gfz uuuuu | -15 3 -59 -173 -3 | 22 25
grg uuxuu | 12 69 -238 61 1 | 27 30
igr xxxxx | -10 41 16 93 -4 | 6 16
irf xxxxx | 7 3 -37 21 -3 | 1 14
jpl uuuuu | 36 -15 102 345 10 | 34 38
mit uuuuu | -28 4 -41 -10 -10 | 22 26
ngs uuuuu | 56 -7 91 95 2 | 6 17
sio xxxxx | 23 57 40 178 -2 | 46 48
Table 7.1791.5 GPS week: 1791 Day: 5 MJD: 56786.500
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 | -87 -59 110 -216 0 | 16 23
emr uuuxu | 57 1 -198 362 0 | 55 57
esa uuuuu | -8 -1 45 -111 3 | 18 22
gfz uuuuu | -49 -17 -60 -165 -1 | 23 26
grg uuxuu | 38 38 -275 191 0 | 29 31
igr xxxxx | -11 33 -110 9 -4 | 8 16
irf xxxxx | 15 -8 -12 35 0 | 2 14
jpl uuuuu | 26 -12 -95 253 2 | 38 41
mit uuuuu | 30 -16 17 34 -3 | 22 26
ngs uuuuu | 25 114 205 144 -1 | 8 18
sio xxxxx | 37 20 83 194 -2 | 47 50
Table 7.1791.6 GPS week: 1791 Day: 6 MJD: 56787.500
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 | -82 -26 101 -236 5 | 16 23
emr uuuxu | 55 -8 -162 370 -10 | 53 55
esa uuuuu | 11 -9 114 -58 5 | 17 22
gfz uuuuu | 1 11 -51 -217 4 | 22 25
grg uuxuu | 48 29 -239 124 -4 | 26 30
igr xxxxx | -11 4 42 167 -2 | 5 16
irf xxxxx | 49 0 -10 51 0 | 1 15
jpl uuuuu | 40 -16 11 276 6 | 39 42
mit uuuuu | 76 13 -47 62 -5 | 20 25
ngs uuuuu | -79 29 -12 234 -3 | 5 15
sio xxxxx | 85 24 47 258 -13 | 46 49
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