[IGSREPORT-19357] Wk 1616 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jan 13 05:38:58 PST 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1616 (Dec 26, 2010 - Jan 01, 2011)
Contacts: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1616[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1616[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1616[0-6].cls IGS GPS clock combination summary report.
igs16167.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16167.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because they either provide broadcast
clocks (NGS) or clock corrections are not provided (SIO). The clock
information not used is still compared to combination for completeness.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 28 28 HARB DGAR HARB XMIS
0 | EMR | 30 30 WTZR WTZR
0 | ESA | CAS1 SUTH
0 | GFZ | 22 DGAR HARB MAW1 RAMO
0 | GRG | DGAR
0 | JPL | 30 ALRT MCM4
0 | MIT | 30 30
1 | EMR | 30 30 WTZR WTZR
1 | GFZ | 22 DAV1 ISPA KERG MDVJ THU3
1 | JPL | 30 DGAR
1 | MIT | 30 30 DAV1 DAV1
2 | COD | USNO
2 | EMR | 30 30 WTZR WTZR
2 | ESA | TIXI SUTH
2 | GFZ | 4 22 AUCK DAV1 MAW1 MDVJ
2 | GRG | AMC2 DGAR GUAT
2 | JPL | 22 30 MAC1 POTS UNSA
2 | MIT | 3 10 11 15 19 23 30 32 3 10 11 15 19 23 24 30 32
2 | MIT | DAV1 KOUR MAS1 MAW1 DAV1 FLIN MAW1
3 | COD | MCM4 DGAR MCM4
3 | EMR | 30 30 HARB WTZR HARB WTZR
3 | ESA | KERG SUTH UNSA
3 | GFZ | 22 ASPA BOR1 BRFT KIRU MDVJ
3 | GRG | DGAR GUAT SANT
3 | JPL | 30 HARB
3 | MIT | 30 30 FLIN
4 | ALL | 1
4 | COD | DGAR HARB INVK XMIS
4 | EMR | 30 30 WTZR KERG WTZR
4 | ESA | SUTH UNSA
4 | GFZ | 2 ALGO CAS1 DGAR NICO
4 | GRG | DGAR USN3
4 | JPL | 30 POTS
4 | MIT | 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
4 | MIT | 21 22 23 24 25 26 27 28 29 30 31 32 2 3 4 5 6 7 8
4 | MIT | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
4 | MIT | 26 27 28 29 30 31 32
5 | COD | DAV1 DGAR SUTH XMIS
5 | EMR | 30 WTZR WTZR
5 | ESA | DAV1 UNSA
5 | GFZ | DGAR IRKT KOUC MDVJ
5 | GRG | DGAR
5 | JPL | 22 30 MCM4
5 | MIT | 7 11 23 24 26 30 32 3 7 8 11 23 24 26 30 31 32 DAV1
5 | MIT | SANT
6 | COD | DAV1
6 | EMR | WTZR WTZR
6 | ESA | MAW1 KERG MAW1 UNSA
6 | GFZ | DARW HARB MDVJ ZWE2
6 | GRG | ALRT DGAR SANT
6 | JPL | HARB
6 | MIT | 3 4 6 11 14 19 22 24 30 3 4 6 11 14 19 24 30 DAV1
6 | MIT | WROC WTZR DAV1 GRAZ SANT WROC WTZR
5. The following table lists all maneuvered satellites for this week.
The solutions from COD and ESA, which modeled the maneuver, are used
that day for combination. An associated accuracy code of 0 (unknown)
is given if only one AC is left (no redundancy). For the long arc
evaluation the arc is split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G24 | 2010_12_28 | 2010157
G24 | 2010_12_29 | 2010157
6. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | MIT | 30
2 | MIT | 30
4 | COD | 1
7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) 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.
8. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the IGS05 frame. These rotations were estimated in the IGS
SINEX combination process, performed by the IGS Reference Frame Coordinator
at the Institut Geographique National (IGN), and are based on the common
stations between the individual AC SINEX solutions and the IGS05.snx SINEX
frame. The estimated 7 transformations, from which only the 3 rotations are
applied to the orbit and ERP values, are:
| DX DY DZ RX RY RZ SCL
Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+---------------------------------------------------
COD | .0 1.3 .5 -26 10 -27 .23
EMR | 1.0 3.9 2.3 25 -37 -11 .35
ESA | 5.6 8.3 1.8 104 -37 -12 .22
GFZ | -.4 1.5 .5 9 7 -33 .19
GRG | 4.2 14.5 -14.4 59 60 -98 .32
JPL | 4.3 7.6 4.6 77 -75 32 -.05
MIT | -2.0 7.4 4.5 35 -34 -33 .28
NGS | -1.0 3.8 .8 62 24 -8 .17
SIO | 1.1 8.7 -5.5 146 -44 -7 .43
9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and
ERPs as generated by IGN. For more information see IGSMAIL #2750.
Because of this change in alignment Table 2 has been enhanced with one
additional line per AC. This additional line shows the X- and Y-rotations
which were applied to each of the AC orbits prior to the orbit combination.
These rotations are based on the difference between the individual AC ERP
estimates and the IGS reference frame ERP product. The total rotation of
the individual AC orbits w.r.t. the IGS combined orbit is the sum of the
values in the two lines of Table 2 plus the reference frame rotation.
11. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna
model is introduced (IGSMAIL #5272). The antenna phase center offsets and
phase center variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (table 1.1616.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1616.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 2.1616.[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 3.1616.[0-6]). The first type of satellite RMS is
based on orbit combination and the second RMS type is a result of the 7-day
arc evaluation of each centre ephemerides. The fourth part, Table 4, is a
weekly summary of the daily precise navigation summaries for centres
providing both orbit and clock solutions. It contains weekly station RMS
w.r.t. the initial coordinates for the Latitude, Longitude and Height
components for up to three IGS stations (table 4.1307). The fifth and final
part, Table 5, is similar to Table 4 and contains daily precise navigation
statistics (tables 5.1616.0-6).
In tables 1-3, the most important statistic which is meaningful for intra
centre/satellite analysis is labeled WRMS. It is a weighted RMS where
normalized weights are based on accuracy codes given in the SP3 files, and
should not be affected by downweighted/problem satellites when acknowledged
by individual centres in their SP3 file.
Table 1: Week 1616 summary. (Dec 26, 2010 - Jan 01, 2011)
Table 1.1616.a GPS week: 1616 MJD: 55556.000-55562.000
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 232| 0 0 3 126 -22 -22 -.21 9 7 | -448 -77 15 75
| 1 0 1 6 16 29 .03 | 546 889
emr 99| 0 0 6 9 80 7 .40 19 19 | -885 284 15 95
| 1 1 1 31 37 16 .03 | 1401 1327
esa 133| 0 0 -2 -61 38 9 .21 8 7 | -520 -28 15 109
| 0 0 1 13 13 28 .02 | 1272 1996
gfz 190| -1 0 -3 52 -46 2 -.22 11 10 | -95 227 21 97
| 0 0 1 36 83 16 .05 | 179 359
grg 135| 1 0 -14 -37 -138 -34 .66 17 16 | 20 28 52 233
| 0 1 1 15 17 19 .05 | 373 660
igr n/a| 0 0 1 61 10 20 -.04 5 5 | -2243 80 16 84
| 0 0 1 20 16 29 .03 | 1227 1214
jpl 125| 0 0 4 -81 148 16 .46 18 16 | 1687 354 17 113
| 1 0 2 22 17 65 .04 | 1246 1216
mit 280| 0 1 0 22 2 15 -.41 18 13 | -107 178 39 182
| 0 1 0 25 28 11 .04 | 327 691
ngs 215| 0 0 1 -46 -45 5 -.20 12 9 | -547 90 2064 3769
| 0 0 1 13 48 16 .04 | 450 722
sio 253| 0 1 2 -214 57 -40 -.06 22 21 | --- --- --- ---
| 1 0 0 28 31 11 .05 | --- ---
Table 1.1616.b GPS week : 1616 MJD: 55556.000-55562.000
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 | 0 0 0 0 34 0 0 |
2 | 5 4 4 4 6 4 6 |
3 | 4 3 4 4 4 4 4 |
4 | 5 4 6 4 4 4 4 |
5 | 5 4 5 5 5 4 5 |
6 | 4 3 4 4 3 3 4 |
7 | 5 5 5 5 5 5 5 |
8 | 4 4 4 4 4 4 4 |
9 | 4 4 4 4 4 4 4 |
10 | 5 4 4 4 4 4 4 |
11 | 4 4 4 5 5 5 5 |
12 | 5 5 4 5 5 5 6 |
13 | 4 4 5 5 4 4 5 |
14 | 5 4 4 4 4 4 7 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 6 |
17 | 5 5 5 5 5 5 5 |
18 | 4 4 4 4 4 4 5 |
19 | 5 5 5 5 5 5 5 |
20 | 5 4 4 4 4 5 5 |
21 | 4 3 4 4 4 4 4 |
22 | 4 5 4 4 4 4 4 |
23 | 4 4 5 5 5 5 5 |
24 | 5 4 4 0 3 4 4 |
25 | 6 6 7 6 5 5 5 |
26 | 5 4 4 5 5 5 5 |
27 | 4 4 4 4 5 4 4 |
28 | 5 5 4 4 4 4 4 |
29 | 6 5 6 6 5 6 5 |
30 | 9 12 9 10 10 9 8 |
31 | 5 5 5 5 5 5 5 |
32 | 5 4 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1616.0 GPS week: 1616 Day: 0 MJD: 55556.000
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 232| -1 0 2 128 -26 -56 -.20 9 8 | -939 613 19 62
| 21 13 |
emr 99| 0 -2 6 60 41 13 .41 18 18 | -824 1125 17 96
| -37 11 |
esa 133| 1 -1 -3 -49 39 44 .19 8 8 | 227 -1687 14 98
| -58 -15 |
gfz 190| -1 0 -5 -12 -108 30 -.20 12 12 | -160 204 22 98
| -94 0 |
grg 135| 1 0 -17 -26 -126 -3 .74 17 17 | -474 1169 51 266
| -53 -86 |
igr n/a| -1 0 0 89 -7 5 -.03 5 5 | -1577 1009 16 91
| -83 46 |
jpl 125| 1 0 8 -36 113 -58 .50 17 16 | 1550 1305 18 107
| -76 -20 |
mit 280| 0 0 0 -27 31 18 -.34 21 11 | -537 994 21 151
| 10 34 |
ngs 215| 0 1 2 -22 -10 4 -.20 14 10 | -949 600 2031 4154
| -25 -21 |
sio 253| -2 1 1 -258 72 -31 .01 24 22 | --- --- --- ---
| 56 62 |
Table 2.1616.1 GPS week: 1616 Day: 1 MJD: 55557.000
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 232| 0 0 4 124 2 -20 -.18 9 7 | -1040 868 15 80
| 40 -15 |
emr 99| 0 -1 5 25 135 -5 .35 19 19 | -762 -669 16 76
| -16 -64 |
esa 133| 1 0 0 -59 57 18 .18 6 6 | -1156 1945 16 113
| -43 -22 |
gfz 190| -1 0 -4 62 -161 12 -.19 10 8 | -298 399 20 95
| -55 -14 |
grg 135| 2 0 -15 -52 -140 -35 .59 18 16 | -278 177 58 287
| 17 -60 |
igr n/a| 0 -1 1 71 19 12 -.05 4 4 | -1531 -730 15 78
| -29 -7 |
jpl 125| 2 -2 7 -90 167 -43 .50 18 17 | 1808 -394 17 107
| -43 -38 |
mit 280| 0 1 -1 22 -6 -4 -.39 18 10 | -217 270 25 164
| -12 36 |
ngs 215| 0 0 2 -54 8 18 -.25 13 10 | -1053 865 2463 3752
| 22 12 |
sio 253| 0 2 0 -222 15 -56 -.06 23 20 | --- --- --- ---
| 55 78 |
Table 2.1616.2 GPS week: 1616 Day: 2 MJD: 55558.000
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 232| 0 0 2 114 -13 -28 -.19 8 7 | 336 -1004 13 66
| 20 -22 |
emr 99| 2 0 6 -29 124 12 .38 20 20 | -893 -956 14 92
| 59 -76 |
esa 133| 0 0 0 -60 51 12 .21 7 7 | 1758 -1137 14 108
| -2 -18 |
gfz 190| 0 0 -4 69 -97 7 -.18 11 12 | 101 -262 20 106
| -38 -33 |
grg 135| 1 0 -14 -44 -130 -24 .62 17 18 | 637 -516 56 219
| 25 -22 |
igr n/a| 0 0 2 61 37 23 -.06 5 5 | -1687 -1469 17 84
| -35 -3 |
jpl 125| -1 0 2 -102 153 11 .42 19 18 | 1976 -1082 18 116
| 3 -29 |
mit 280| 1 0 0 32 -49 10 -.42 22 15 | 438 -552 26 158
| -22 43 |
ngs 215| -1 0 0 -58 9 14 -.25 13 9 | -76 -354 1859 3276
| -70 -64 |
sio 253| 0 0 2 -199 16 -27 .01 22 20 | --- --- --- ---
| 37 57 |
Table 2.1616.3 GPS week: 1616 Day: 3 MJD: 55559.000
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 232| 0 0 5 133 -31 -15 -.21 8 8 | -282 -735 14 64
| 19 -7 |
emr 99| 2 0 4 -6 75 20 .39 19 19 | -3049 936 15 119
| 52 -53 |
esa 133| 1 0 -1 -64 41 11 .24 8 8 | -443 -644 18 120
| 8 -34 |
gfz 190| -2 -1 0 52 27 3 -.17 9 9 | -63 129 22 105
| -53 6 |
grg 135| 1 2 -14 -10 -163 -24 .63 17 18 | 150 -938 50 214
| 20 66 |
igr n/a| 0 0 0 53 -10 1 -.03 5 5 | -4299 588 17 79
| -45 24 |
jpl 125| -1 0 0 -88 151 -26 .44 18 17 | -263 887 19 135
| 17 -60 |
mit 280| 0 1 -1 34 7 21 -.44 20 15 | 108 -841 25 130
| -20 29 |
ngs 215| 0 0 0 -48 -95 -11 -.20 11 8 | -557 -51 1792 3337
| -52 31 |
sio 253| 0 3 1 -201 59 -35 -.09 21 21 | --- --- --- ---
| 50 55 |
Table 2.1616.4 GPS week: 1616 Day: 4 MJD: 55560.000
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 232| 1 0 5 132 -51 -24 -.24 9 8 | -981 869 15 84
| 44 10 |
emr 99| 2 0 8 -20 54 30 .38 19 19 | -2002 1970 14 98
| 32 -25 |
esa 133| 0 0 -3 -56 20 7 .21 8 8 | -2171 3001 20 101
| 3 1 |
gfz 190| 0 0 -2 98 79 -14 -.26 11 10 | -349 774 20 92
| -63 -22 |
grg 135| 2 0 -11 -54 -162 -40 .70 16 14 | -217 229 50 198
| 50 38 |
igr n/a| 0 -1 0 57 4 2 -.08 5 5 | -3576 1539 16 71
| -39 -7 |
jpl 125| -1 0 6 -92 141 30 .43 18 17 | 676 1885 16 98
| 30 -23 |
mit 280| 0 0 0 32 26 22 -.44 17 14 | -256 638 124 345
| -29 22 |
ngs 215| 0 0 0 -57 -105 -4 -.19 11 8 | -960 787 1904 3541
| 4 65 |
sio 253| 1 2 1 -202 87 -33 -.10 21 21 | --- --- --- ---
| 44 46 |
Table 2.1616.5 GPS week: 1616 Day: 5 MJD: 55561.000
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 232| 0 0 2 127 -18 -45 -.21 9 8 | -285 8 16 84
| 18 -6 |
emr 99| 0 -2 6 5 47 -9 .46 19 19 | -50 1148 15 99
| 10 -8 |
esa 133| 0 0 -3 -51 31 21 .21 8 8 | -433 771 15 127
| -2 32 |
gfz 190| -1 -1 -2 77 -23 -13 -.27 9 9 | 37 485 23 90
| -70 3 |
grg 135| 3 2 -15 -37 -122 -60 .67 19 17 | 100 150 57 234
| 24 29 |
igr n/a| 0 -1 2 74 7 11 .03 5 5 | -2114 910 18 97
| -53 -24 |
jpl 125| -1 0 3 -95 151 80 .51 17 16 | 2415 1030 19 113
| -10 -10 |
mit 280| 1 2 0 7 22 8 -.42 16 13 | -342 779 31 168
| -33 13 |
ngs 215| 0 0 3 -49 -74 30 -.12 10 7 | -255 -62 2204 3863
| -61 27 |
sio 253| 2 2 2 -240 92 -54 -.11 22 19 | --- --- --- ---
| 61 45 |
Table 2.1616.6 GPS week: 1616 Day: 6 MJD: 55562.000
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 232| 1 0 2 127 -18 35 -.26 10 7 | 50 -1164 19 89
| 39 -40 |
emr 99| -2 0 8 31 81 -12 .41 19 19 | 1381 -1563 18 89
| -16 -44 |
esa 133| 1 0 -1 -89 25 -47 .21 8 8 | -1427 -2446 14 102
| 12 18 |
gfz 190| 0 -1 -2 22 -44 -10 -.28 12 12 | 67 -136 23 99
| 11 21 |
grg 135| 0 2 -14 -33 -123 -53 .65 16 14 | 225 -70 45 218
| 60 -4 |
igr n/a| 0 0 2 23 22 86 -.03 7 5 | -919 -1284 19 89
| 1 -29 |
jpl 125| 0 0 4 -68 162 119 .42 17 16 | 3651 -1151 18 120
| 40 -7 |
mit 280| 0 2 -1 53 -11 29 -.44 16 14 | 55 -42 26 159
| -49 26 |
ngs 215| -1 0 1 -32 -52 -14 -.21 12 10 | 20 -1154 2197 4462
| 102 -25 |
sio 253| 1 1 3 -175 56 -43 -.08 23 21 | --- --- --- ---
| 28 48 |
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 3.1616.0 GPS week: 1616 Day: 0 MJD: 55556.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 9 --- --- --- --- 162 --- --- --- --- 0 | 44 --- --- --- --- 170 --- --- --- --- 40
2 | 6 12 7 20 15 5 15 12 11 35 4 | 41 44 46 51 46 42 42 41 42 45 42
3 | 8 14 6 10 18 7 11 13 9 18 3 | 14 24 16 20 30 13 24 17 16 25 15
4 | 6 11 7 18 13 3 11 17 9 39 5 | 42 45 47 50 53 43 44 41 41 34 42
5 | 6 23 8 10 20 5 19 10 13 16 4 | 19 30 15 15 33 15 26 17 18 20 15
6 | 7 13 9 10 15 6 11 10 8 18 3 | 14 24 21 20 30 15 23 16 14 27 16
7 | 16 22 9 7 18 8 19 11 10 23 5 | 18 33 25 24 31 19 27 20 17 25 19
8 | 6 13 6 6 12 5 13 14 8 19 3 | 28 29 29 30 33 22 29 25 24 31 26
9 | 7 13 8 13 16 5 13 9 11 18 3 | 17 19 19 21 21 18 17 18 18 23 16
10 | 8 15 8 11 15 4 12 16 11 27 4 | 17 25 23 27 27 19 27 19 20 34 19
11 | 7 14 7 9 15 4 12 11 12 36 4 | 42 48 43 44 58 42 44 45 44 57 43
12E | 9 21 9 15 19 5 27 15 12 17 5 | 18 24 25 30 23 23 26 22 24 23 20
13 | 5 17 9 5 22 4 17 8 13 14 4 | 25 33 28 27 46 23 32 27 22 26 25
14 | 9 23 9 12 17 6 17 9 11 19 4 | 25 35 27 25 31 25 33 28 23 27 24
15 | 15 26 9 13 14 6 19 13 13 14 5 | 102 100 102 97 102 99 102 100 97 100 99
16E | 8 20 10 8 26 8 26 12 12 16 5 | 17 27 24 25 38 21 30 21 22 20 20
17 | 8 20 9 20 17 3 19 12 14 28 5 | 24 36 27 30 32 25 34 26 24 24 24
18 | 7 21 6 7 19 3 21 11 10 15 4 | 23 34 19 19 28 22 34 21 20 25 19
19 | 6 20 10 10 14 6 22 12 9 36 5 | 25 35 25 26 33 22 37 21 24 29 23
20 | 6 20 9 14 23 4 20 10 14 24 5 | 20 28 17 15 25 15 27 16 20 19 15
21 | 8 12 5 9 9 5 12 8 10 28 3 | 36 42 40 41 44 39 41 40 40 38 38
22 | 7 15 7 8 18 6 17 11 8 16 4 | 20 26 18 19 32 19 29 19 16 20 16
23 | 5 21 7 7 22 6 17 9 8 16 4 | 18 27 17 16 26 13 21 16 16 21 14
24 | 8 11 8 13 17 4 8 11 11 37 4 | 17 15 12 14 13 11 9 13 9 10 11
X25E | 9 25 12 10 18 5 --- 22 13 --- 6 | 16 29 20 20 24 17 --- 22 17 --- 15
26 | 10 16 8 15 11 4 12 11 14 23 4 | 19 26 23 27 24 19 24 23 21 30 20
27 | 7 15 8 11 14 3 10 8 11 27 4 | 16 23 22 20 19 19 15 19 17 34 16
28E | 7 16 6 12 18 6 23 13 12 20 4 | 20 25 21 25 27 20 29 22 22 26 20
X29 | 13 25 12 11 15 5 21 17 11 --- 5 | 25 33 24 24 24 22 32 26 21 --- 21
30E | 18 24 12 15 15 7 20 97 47 22 9 | 28 36 30 35 38 29 35 96 62 36 29
31 | 7 20 10 10 19 6 19 11 11 22 4 | 15 28 23 18 33 18 29 21 20 21 18
32 | 11 19 8 13 20 6 18 14 13 16 5 | 17 24 19 19 21 15 25 21 18 15 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 8 12 17 5 17 21 14 24 |T 25 32 27 28 33 29 31 28 26 29 24
WRMS | 8 18 8 12 16 5 16 11 10 22 |NE 23 30 25 26 31 22 29 24 22 27 22
MEDI | 7 19 8 11 17 5 17 11 11 20 |MD 20 29 23 25 31 20 29 21 21 26 20
Table 3.1616.1 GPS week: 1616 Day: 1 MJD: 55557.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 8 --- --- --- --- 359 --- --- --- --- 0 | 64 --- --- --- --- 364 --- --- --- --- 59
2 | 7 15 4 10 13 4 15 10 9 33 4 | 21 24 25 29 27 23 27 18 23 30 23
3 | 5 17 5 6 16 4 9 9 8 15 3 | 17 23 17 18 21 17 24 17 19 23 17
4 | 8 13 7 13 14 5 9 15 8 34 4 | 31 30 33 36 42 33 34 26 33 23 30
5 | 6 22 6 9 19 4 21 10 8 18 4 | 14 30 17 17 30 14 29 15 17 18 15
6 | 5 18 3 4 14 4 9 9 9 17 3 | 17 27 18 18 25 17 24 15 20 27 17
7 | 13 22 7 7 22 4 21 10 11 23 4 | 18 30 20 23 30 18 29 18 19 30 17
8 | 6 14 5 7 18 5 13 11 8 18 3 | 19 23 20 19 27 18 25 22 18 30 19
9 | 8 15 4 8 11 4 12 11 12 17 3 | 12 17 17 19 21 15 20 16 19 24 14
10 | 6 15 5 6 14 3 12 13 9 27 3 | 15 22 19 20 21 17 24 16 18 35 17
11 | 6 16 6 7 13 4 13 10 9 38 4 | 24 34 24 28 38 25 31 28 27 46 25
12E | 8 24 8 10 18 5 30 17 11 15 5 | 17 25 20 23 24 17 26 20 22 19 18
13 | 5 21 5 4 29 4 21 8 10 16 4 | 17 27 17 19 39 17 27 19 21 19 18
14 | 6 25 5 12 21 4 18 9 10 16 4 | 22 31 25 22 35 22 33 23 24 25 23
15E | 9 21 8 11 19 3 19 13 12 30 5 | 51 58 57 53 58 53 57 54 54 52 53
16E | 8 22 6 8 18 2 27 12 12 15 4 | 16 25 18 20 22 19 28 23 25 22 18
17 | 10 19 10 11 13 4 21 12 8 28 4 | 19 24 19 20 29 16 30 19 16 23 16
18 | 6 20 6 5 17 4 22 10 13 14 4 | 19 29 19 17 26 18 31 19 18 20 18
19 | 6 21 6 8 13 3 23 10 8 32 4 | 20 31 19 17 25 18 33 17 18 21 17
20 | 7 19 6 9 20 7 18 8 15 21 4 | 16 25 13 15 23 15 25 14 17 16 13
21 | 5 13 5 8 10 3 14 8 10 24 3 | 19 25 23 23 24 21 26 21 21 21 20
22 | 7 19 5 22 22 7 21 13 13 15 5 | 20 28 22 31 32 20 31 22 19 20 21
23 | 6 25 5 8 24 3 20 8 12 15 4 | 15 28 14 15 25 13 23 15 14 18 13
24 | 6 9 4 11 14 3 9 8 9 35 3 | 9 9 7 13 7 8 10 11 9 15 7
X25E | 14 26 10 8 14 7 --- 18 18 --- 6 | 20 26 17 16 20 15 --- 17 23 --- 15
26 | 10 17 7 8 12 3 12 10 11 23 4 | 16 27 25 27 28 20 28 22 21 32 21
X27 | 9 16 5 8 13 4 --- 13 15 --- 4 | 13 21 19 22 24 16 --- 20 19 --- 16
28E | 11 18 5 7 16 6 24 13 11 20 4 | 15 22 15 19 17 14 26 14 15 24 14
X29 | 7 24 8 9 13 5 25 18 14 --- 5 | 19 30 19 19 20 19 29 23 20 --- 18
30E | 24 26 14 14 23 8 22 76 44 29 11 | 23 33 24 31 36 30 33 83 64 31 30
31 | 6 21 6 8 23 4 22 14 13 19 4 | 22 29 22 22 34 21 34 27 22 24 22
32 | 11 25 7 7 17 5 14 10 12 15 4 | 13 29 17 15 16 14 24 18 17 15 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 6 10 18 4 18 18 13 23 |T 20 27 20 22 27 30 28 22 22 25 20
WRMS | 7 19 6 8 16 4 17 10 10 20 |NE 18 26 19 21 26 18 27 19 19 24 18
MEDI | 7 19 6 8 16 4 19 10 11 19 |MD 18 27 19 20 25 18 28 19 19 23 18
Table 3.1616.2 GPS week: 1616 Day: 2 MJD: 55558.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 8 --- --- --- --- 539 --- --- --- --- 0 | 56 --- --- --- --- 373 --- --- --- --- 56
2 | 6 15 6 11 13 5 15 16 9 29 4 | 27 31 30 26 31 27 31 28 29 33 27
3 | 7 19 8 10 17 4 13 16 12 13 4 | 18 28 23 19 26 21 28 22 18 30 19
4 | 8 15 8 32 12 10 15 18 9 30 6 | 31 35 33 42 39 30 37 30 30 22 29
5 | 5 24 5 9 18 5 19 18 8 23 4 | 12 28 17 14 28 13 26 15 19 16 13
6 | 6 16 5 8 12 4 11 16 9 15 3 | 18 24 21 17 25 20 28 20 19 30 19
7 | 6 21 9 10 21 4 19 14 13 28 4 | 10 28 16 16 25 16 27 17 20 32 14
8 | 7 15 7 8 14 4 12 16 11 18 3 | 13 18 17 19 19 17 20 21 22 27 16
9 | 8 15 6 7 13 4 12 14 8 17 3 | 14 18 19 19 21 14 20 18 19 26 15
10 | 5 14 6 9 11 4 13 19 8 27 4 | 12 18 16 16 20 14 23 16 18 32 14
11 | 7 15 4 8 11 4 14 13 12 36 4 | 33 40 33 36 45 33 41 37 36 51 34
12E | 6 17 6 9 22 3 24 19 6 13 4 | 14 21 15 21 20 17 24 20 20 18 14
13 | 7 24 7 8 25 5 22 14 9 16 4 | 16 28 16 15 35 15 27 17 18 17 14
14 | 5 22 5 9 18 5 22 14 12 14 4 | 18 26 22 18 35 20 32 20 18 21 20
15E | 7 27 7 13 15 4 26 11 11 20 4 | 43 50 50 45 55 46 53 47 48 48 47
16E | 5 23 10 8 18 4 25 18 11 18 4 | 14 23 20 17 22 18 28 25 24 23 17
17 | 8 21 7 10 15 5 21 11 8 37 4 | 16 26 17 16 27 15 27 16 15 33 14
18 | 6 22 6 6 17 5 20 16 12 14 4 | 16 28 16 11 23 15 27 15 15 18 13
19 | 7 26 10 7 11 4 24 17 12 29 5 | 18 31 21 16 24 19 33 19 21 24 17
20 | 6 20 7 9 20 5 19 13 10 15 4 | 12 25 12 15 22 13 22 14 15 14 12
21 | 6 12 7 8 9 3 13 14 9 22 3 | 20 29 25 27 29 25 28 25 28 28 24
22 | 5 19 4 7 18 5 18 15 11 16 4 | 15 27 15 11 28 14 24 16 12 18 12
23 | 9 22 5 13 22 7 22 12 9 13 4 | 18 28 17 23 26 19 27 21 17 24 17
X24 | 5 --- 3 9 --- 5 --- 11 --- --- 4 | 9 --- 8 18 --- 10 --- 11 --- --- 10
X25E | 17 27 9 10 19 7 --- 26 14 --- 6 | 20 28 13 17 24 10 --- 20 14 --- 10
26 | 9 19 6 7 12 4 16 13 10 20 4 | 13 24 20 22 24 16 27 20 22 31 17
27 | 8 16 8 7 14 3 10 15 11 29 4 | 15 19 21 20 22 15 18 21 18 38 16
28E | 8 20 5 9 17 3 24 16 7 16 4 | 14 20 12 13 17 12 24 17 19 22 13
X29 | 8 25 10 8 13 3 27 25 12 --- 5 | 22 30 22 16 19 19 30 27 20 --- 17
30E | 17 26 11 13 20 6 17 84 44 23 8 | 19 33 21 26 31 21 33 85 59 32 22
31 | 7 18 10 9 24 5 21 16 13 18 4 | 20 26 25 17 33 20 29 24 19 24 20
32 | 10 20 4 6 18 6 18 12 11 13 4 | 8 20 11 11 18 12 23 12 14 13 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 7 11 17 5 19 22 13 22 |T 18 27 20 19 27 29 28 23 22 26 19
WRMS | 7 20 7 12 18 5 18 15 9 20 |NE 16 26 19 19 26 18 27 20 20 26 17
MEDI | 7 20 7 9 17 4 19 16 11 18 |MD 16 27 19 17 25 17 27 20 19 24 16
Table 3.1616.3 GPS week: 1616 Day: 3 MJD: 55559.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 9 --- --- --- --- 469 --- --- --- --- 0 | 41 --- --- --- --- 258 --- --- --- --- 56
2 | 7 14 5 13 14 3 12 15 9 27 4 | 37 38 38 41 38 37 37 36 41 40 37
3 | 7 15 7 8 16 4 12 15 12 17 4 | 22 28 23 28 27 26 33 29 30 29 26
4 | 7 10 7 12 11 5 9 15 9 28 4 | 38 41 41 38 45 40 42 38 43 31 38
5 | 6 23 10 8 16 3 19 16 9 19 4 | 22 32 22 22 33 20 29 20 26 21 21
6 | 6 15 7 6 14 3 9 12 8 17 3 | 22 29 23 26 30 25 32 24 25 31 25
7 | 8 19 9 6 22 6 21 14 9 24 4 | 21 31 25 25 31 22 33 23 24 30 22
8 | 5 16 9 7 16 5 10 17 7 18 3 | 28 30 28 32 33 28 31 30 30 34 29
9 | 7 13 6 10 12 6 11 15 8 20 3 | 18 22 21 22 18 21 20 19 24 25 18
10 | 6 15 10 7 11 4 12 20 9 26 4 | 23 27 26 23 29 23 28 22 26 36 23
11 | 7 17 6 10 10 6 11 16 7 37 4 | 35 46 39 40 49 39 44 41 39 52 38
12E | 8 21 8 9 13 5 23 19 8 14 4 | 24 28 21 24 30 21 26 24 25 24 21
13 | 5 22 7 6 27 4 20 11 7 16 4 | 27 34 28 27 42 29 37 29 31 29 27
14 | 6 18 6 8 18 6 21 15 8 13 4 | 23 30 27 26 35 24 36 25 24 24 25
15E | 7 21 6 10 19 2 23 12 7 21 4 | 50 52 49 50 55 49 55 50 48 53 49
16E | 7 21 7 11 17 3 24 19 11 18 5 | 23 29 22 26 30 24 30 28 25 24 22
17 | 9 19 8 6 15 5 21 12 5 39 4 | 27 32 29 23 33 27 36 26 30 41 26
18 | 9 21 5 9 16 3 23 16 7 13 4 | 25 32 25 26 28 25 36 25 25 25 23
19 | 5 26 7 6 12 4 22 18 9 21 4 | 25 34 24 25 29 26 38 28 27 25 25
20 | 6 21 8 9 16 6 21 14 10 15 4 | 22 32 24 22 26 22 31 23 27 22 22
21 | 8 12 6 6 9 4 10 13 9 23 3 | 34 38 36 37 40 37 37 35 39 35 35
22 | 7 19 7 7 20 5 21 14 9 16 4 | 25 33 25 26 34 25 34 23 21 24 23
23E | 10 25 6 11 18 4 18 17 10 18 4 | 31 38 30 37 39 29 35 24 31 25 30
X24 | 9 --- --- --- --- 17 --- --- --- --- 0 | 17 --- --- --- --- 15 --- --- --- --- 16
X25E | 12 25 8 9 19 6 --- 24 12 --- 6 | 23 32 22 23 27 22 --- 22 26 --- 22
26 | 11 21 10 11 13 2 15 13 9 20 4 | 20 29 21 26 26 20 29 24 20 31 20
X27 | 8 15 6 7 14 5 --- 18 8 --- 4 | 18 22 22 21 18 21 --- 22 22 --- 18
28E | 6 17 9 6 17 5 20 16 10 16 4 | 24 30 25 21 26 23 31 24 28 24 23
X29 | 13 24 13 13 13 5 26 24 10 --- 6 | 28 37 32 31 27 30 37 30 28 --- 27
30E | 19 26 15 14 23 5 19 65 37 29 10 | 33 35 31 31 40 33 37 80 59 34 33
31 | 11 21 7 9 22 6 21 16 10 19 5 | 20 30 25 23 36 21 32 23 21 25 21
32 | 12 19 7 7 16 6 17 15 10 13 4 | 18 25 22 21 23 19 28 19 22 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 19 8 9 17 5 18 20 11 21 |T 26 32 27 28 32 33 34 28 29 30 26
WRMS | 8 19 8 9 18 5 17 15 8 21 |NE 24 31 27 27 31 25 33 26 28 29 25
MEDI | 7 19 7 8 16 5 19 15 9 19 |MD 24 32 25 26 30 25 33 24 26 29 23
Table 3.1616.4 GPS week: 1616 Day: 4 MJD: 55560.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 111 --- --- 40 --- 83 --- 45 55 --- 33 | 56 --- --- 10 --- 145 --- 6 19 --- 60
2 | 7 17 7 31 14 6 15 14 7 28 5 | 34 35 39 48 36 38 34 33 38 38 36
3 | 9 17 11 6 13 5 10 13 7 18 3 | 33 36 32 32 36 32 34 28 32 34 31
4 | 6 13 14 11 9 4 8 13 7 29 4 | 34 37 48 40 43 38 39 35 36 27 37
5 | 6 25 9 8 16 5 21 13 11 14 4 | 22 36 24 23 34 23 34 21 27 22 24
6 | 7 14 7 6 14 5 9 11 7 17 3 | 26 29 26 26 32 26 29 19 25 29 25
7 | 7 19 9 7 19 4 21 14 8 24 4 | 25 29 28 21 36 22 28 20 26 26 23
8 | 8 14 6 8 14 4 9 15 7 18 3 | 29 29 29 24 31 26 30 26 31 32 28
9 | 8 15 5 9 13 4 12 12 10 19 3 | 18 19 16 18 20 16 21 18 14 25 15
10 | 8 14 5 9 14 3 11 14 7 25 3 | 23 27 28 27 27 25 29 22 27 38 26
11 | 5 15 7 12 7 5 14 17 7 38 4 | 30 36 34 37 40 34 37 34 32 50 32
12E | 11 23 8 15 18 3 23 18 10 16 5 | 21 26 22 23 22 20 23 23 20 25 20
13 | 6 19 6 8 23 4 17 11 10 14 4 | 25 32 27 22 43 25 30 26 30 30 26
14 | 6 20 8 10 16 5 17 14 11 12 4 | 22 27 27 24 35 23 29 23 24 21 23
15E | 7 24 7 13 16 3 19 10 9 15 4 | 29 35 30 34 34 30 35 29 29 33 29
16E | 7 24 8 8 15 4 26 20 7 20 5 | 22 32 24 23 27 24 31 23 25 26 23
17 | 7 18 8 9 13 5 20 13 6 34 4 | 23 30 26 24 30 22 33 21 23 34 23
18 | 7 22 5 8 17 5 22 14 8 13 4 | 26 37 25 24 30 27 38 24 25 26 25
19 | 7 22 10 8 13 5 23 19 7 22 4 | 26 34 26 25 32 25 36 23 25 22 25
20 | 7 19 5 9 14 5 20 15 8 17 4 | 24 30 19 22 29 21 31 20 23 21 21
21 | 11 13 10 9 10 6 12 12 8 23 4 | 31 33 38 33 32 30 34 30 30 30 31
22 | 7 20 7 9 19 5 18 11 13 15 4 | 24 33 28 23 35 26 32 22 26 24 24
23E | 10 23 6 10 19 6 19 16 10 16 4 | 29 36 23 28 32 26 32 26 24 27 24
X24 | 5 10 3 12 9 5 10 13 9 --- 3 | 15 12 9 8 8 15 10 12 10 --- 14
X25E | 13 23 6 10 15 5 --- 19 10 --- 5 | 21 29 23 20 34 22 --- 22 24 --- 21
26 | 10 23 6 13 12 3 12 11 13 20 4 | 19 28 24 26 30 23 29 23 25 30 22
X27 | 9 18 6 8 12 4 --- 13 8 31 4 | 17 19 14 17 21 15 --- 19 14 36 14
28E | 7 14 8 10 17 3 20 12 9 14 4 | 21 27 22 21 25 21 27 21 23 20 21
X29 | 11 24 9 6 11 5 26 20 10 --- 5 | 24 31 24 24 27 23 34 25 26 --- 23
30E | 26 24 12 14 27 4 22 55 37 25 9 | 32 36 29 31 42 31 35 66 50 32 30
31 | 6 25 9 5 18 5 21 19 9 18 4 | 20 28 20 19 33 17 27 20 20 25 19
32 | 10 17 8 9 14 6 15 13 10 15 4 | 22 25 19 24 25 21 25 21 23 20 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 8 11 16 5 18 17 11 21 |T 25 30 25 25 31 28 30 24 25 28 25
WRMS | 8 19 8 10 14 5 17 14 8 21 |NE 24 29 26 25 31 24 30 23 25 29 24
MEDI | 7 19 7 9 14 5 18 14 9 18 |MD 24 30 26 24 32 24 31 23 25 27 24
Table 3.1616.5 GPS week: 1616 Day: 5 MJD: 55561.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 9 --- --- --- --- 258 --- --- --- --- 0 | 61 --- --- --- --- 239 --- --- --- --- 62
2 | 8 11 6 11 15 5 13 12 6 30 4 | 20 24 24 28 24 21 25 23 29 31 23
3 | 5 16 6 10 17 5 10 12 10 21 3 | 16 23 20 19 20 19 23 19 22 27 17
4 | 8 11 4 7 14 7 9 14 9 29 3 | 25 33 31 32 36 29 33 30 34 27 29
5 | 6 23 8 9 17 4 19 11 7 14 4 | 9 28 16 14 26 11 26 9 13 12 12
6 | 4 14 7 8 15 6 10 12 7 18 3 | 15 21 18 17 21 17 22 16 17 25 15
7 | 7 24 8 8 24 5 18 12 8 22 4 | 18 31 21 25 28 19 27 20 22 25 20
8 | 9 11 8 6 16 4 9 14 9 16 3 | 28 28 26 28 31 26 30 29 30 31 27
9 | 8 13 6 6 17 3 10 12 10 19 3 | 13 15 15 13 16 11 17 15 14 22 11
10 | 7 14 6 9 13 4 10 14 5 26 3 | 17 23 20 23 21 16 23 18 21 32 18
11 | 7 14 7 9 14 6 13 14 9 39 4 | 22 31 25 31 35 23 31 25 27 43 25
12E | 8 21 10 10 22 4 25 19 9 21 5 | 16 26 17 22 19 17 28 21 20 29 18
13 | 6 21 6 6 29 4 19 10 6 11 4 | 22 30 24 23 41 22 32 23 23 24 22
14 | 11 19 7 8 23 4 19 14 6 13 4 | 28 31 29 27 43 24 34 26 25 27 27
15E | 9 21 8 14 20 5 21 12 8 12 4 | 27 31 30 28 36 26 32 29 30 31 27
16E | 5 27 8 12 22 5 26 21 10 14 5 | 11 25 15 16 24 11 26 17 14 17 10
17 | 7 18 10 8 16 5 20 13 7 29 4 | 22 30 28 25 26 23 32 23 23 35 23
18 | 8 21 8 7 18 6 20 14 8 17 4 | 20 32 21 19 25 19 32 23 21 26 19
19 | 7 23 7 7 14 6 23 16 9 23 4 | 16 30 19 19 19 16 31 21 21 20 17
20 | 7 19 10 11 17 6 21 13 9 17 4 | 14 25 16 15 19 12 24 13 16 15 11
21 | 5 14 10 11 11 6 11 13 11 24 4 | 23 26 26 26 26 20 25 24 24 28 22
22 | 6 17 7 7 21 6 18 10 7 15 3 | 19 29 22 19 30 18 30 20 19 22 18
23E | 8 25 7 12 22 6 22 13 6 15 4 | 15 28 16 16 25 14 25 18 13 20 13
24 | 9 11 5 10 12 4 9 11 6 36 4 | 12 15 11 14 10 13 13 9 16 9 14
X25E | 9 24 9 6 22 5 --- 20 7 --- 5 | 16 28 17 19 22 16 --- 18 22 --- 18
26 | 11 21 10 11 15 5 12 14 10 20 4 | 13 28 16 25 24 16 23 20 22 26 16
X27 | 9 17 6 7 15 4 --- 12 7 28 4 | 12 18 13 12 16 11 --- 15 15 30 10
28E | 7 15 8 6 19 3 19 13 9 11 4 | 14 21 13 15 21 14 23 16 19 14 14
X29 | 9 26 11 8 13 5 25 23 11 --- 5 | 15 29 19 21 18 18 28 22 21 --- 17
30E | 25 24 14 13 22 6 21 47 35 23 9 | 23 35 29 35 34 29 38 60 48 29 29
31 | 7 20 8 6 23 3 20 17 8 21 4 | 14 23 18 14 31 14 27 17 18 22 15
32 | 10 18 8 10 16 4 16 9 8 15 4 | 12 21 15 18 15 12 21 14 14 14 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 8 9 19 5 17 16 10 22 |T 19 26 20 21 25 24 26 21 21 24 19
WRMS | 8 19 8 9 16 5 16 13 7 19 |NE 17 26 20 21 25 17 26 19 21 24 18
MEDI | 8 19 8 8 17 5 19 13 8 20 |MD 16 28 19 19 24 17 27 20 21 26 18
Table 3.1616.6 GPS week: 1616 Day: 6 MJD: 55562.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 9 --- --- --- --- 144 --- --- --- --- 0 | 57 --- --- --- --- 174 --- --- --- --- 54
2 | 9 9 9 27 14 6 13 16 16 30 5 | 43 45 46 50 46 43 43 45 47 47 44
3 | 7 16 10 7 16 7 11 16 7 18 4 | 22 29 22 25 28 25 25 23 20 25 23
4 | 7 13 6 11 12 6 7 15 9 30 4 | 38 41 44 43 51 42 42 43 40 34 40
5 | 6 20 8 11 18 6 20 11 14 14 4 | 19 32 19 21 31 22 30 20 22 22 20
6 | 5 14 8 7 14 6 11 19 10 17 3 | 19 28 20 22 29 23 25 20 17 27 21
7 | 8 20 11 11 18 5 21 12 8 22 4 | 19 28 22 22 26 23 29 23 19 25 20
8 | 10 13 7 8 14 5 10 14 8 17 3 | 26 28 25 27 26 26 28 25 26 28 26
9 | 7 13 5 9 14 5 10 10 16 16 3 | 15 19 16 16 16 17 20 19 14 23 15
10 | 7 13 7 11 12 6 12 10 11 25 4 | 20 22 22 23 26 21 26 21 19 34 20
11 | 7 14 7 7 11 4 12 14 8 38 4 | 40 47 46 46 54 43 44 44 39 56 43
12E | 9 21 10 20 30 5 21 17 11 25 6 | 22 30 22 34 32 22 26 26 24 27 22
13 | 5 19 8 10 24 4 24 10 8 13 4 | 26 31 25 27 36 27 37 26 28 27 25
14 | 30 22 12 15 17 20 16 19 21 17 7 | 65 84 85 85 84 67 86 84 67 80 80
15E | 6 21 8 10 17 6 17 14 13 13 4 | 52 55 49 53 56 53 57 54 50 57 52
16E | 7 25 9 17 17 6 26 25 9 16 5 | 21 31 21 27 29 23 29 25 23 23 20
17 | 8 20 6 9 18 7 19 13 10 21 4 | 26 30 23 26 29 25 31 26 28 35 25
18 | 7 24 10 11 16 6 22 16 11 20 5 | 26 35 25 21 25 26 36 27 24 27 22
19 | 6 21 7 11 16 10 21 13 9 30 4 | 27 35 25 29 29 27 36 24 25 33 25
20 | 8 22 9 11 16 4 21 16 8 20 4 | 22 28 19 19 24 19 29 20 19 23 18
21 | 4 12 10 11 11 4 12 14 10 25 4 | 37 39 37 40 43 38 40 40 41 40 38
22 | 6 19 7 12 15 5 20 11 10 16 4 | 25 32 21 23 30 24 33 22 24 26 20
23E | 8 22 8 15 19 6 24 15 14 13 5 | 27 37 24 27 32 25 35 28 24 30 25
24 | 7 10 4 9 9 4 9 11 9 40 4 | 12 12 11 14 9 12 10 9 14 11 12
X25E | 8 23 9 9 18 6 --- 16 12 --- 5 | 22 31 21 20 27 20 --- 22 24 --- 20
26 | 11 22 7 12 13 6 14 15 18 20 4 | 18 26 18 25 25 19 27 23 19 29 18
27 | 6 18 5 8 16 5 9 12 15 26 4 | 14 22 13 16 16 16 15 20 13 33 14
28E | 6 16 7 8 16 5 19 13 10 11 4 | 22 25 20 21 18 21 25 22 26 20 22
29 | 9 24 8 9 15 5 23 17 14 17 5 | 29 37 26 30 27 32 37 31 25 8 28
30E | 21 25 9 15 18 11 19 33 27 42 8 | 69 76 70 67 82 66 73 79 82 77 68
31 | 7 23 8 8 17 5 20 20 9 23 5 | 20 32 21 22 34 22 30 25 21 25 21
32 | 9 17 8 8 13 5 15 13 10 16 4 | 19 22 25 20 24 21 25 20 22 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 8 12 16 7 17 16 12 23 |T 28 34 28 30 33 33 34 30 28 32 28
WRMS | 7 19 8 12 14 5 16 14 10 21 |NE 26 32 27 28 32 27 32 28 26 30 26
MEDI | 7 20 8 11 16 6 17 14 10 20 |MD 22 31 22 25 29 24 30 25 24 27 22
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 4.1616 GPS week: 1616 MJD: 55556.0-55562.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2993 |U 8 10 23 |U 10 13 37 |U 19 11 41 |
emr | emr 2944 |U 15 13 28 |U 12 13 40 | 22 19 56 |
esa | esa 2948 | 10 11 23 |U 10 13 37 | 18 13 40 |
gfz | gfz 2956 |U 10 11 24 |U 11 13 42 |U 21 15 47 |
grg | grg 2948 | 11 13 25 |U 10 14 42 | 19 14 44 |
igr | igr 2951 | 9 10 23 | 10 13 38 | 18 12 40 |
igs | igs 2947 | 10 10 23 | 10 13 37 | 19 12 41 |
jpl | jpl 2791 |U 20 24 55 | 12 14 45 |U 21 16 53 |
mit | mit 2962 |U 14 13 34 |U 11 16 48 |U 25 19 58 |
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 5.1616.0 GPS week: 1616 Day: 0 MJD: 55556.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 8 8 18 | 9 12 37 | 6 6 15 |
emr | emr 2972 | 14 11 25 | 11 11 41 | 18 20 46 |
esa | esa 2976 | 8 9 22 | 10 13 40 | 8 7 17 |
gfz | gfz 2972 | 8 9 24 | 18 11 67 | 10 11 21 |
grg | grg 2976 | 11 12 23 | 10 13 42 | 7 7 19 |
igr | igr 2976 | 8 8 20 | 10 12 40 | 9 8 17 |
igs | igs 2976 | 8 9 21 | 10 12 40 | 8 7 16 |
jpl | jpl 2876 | 13 13 27 | 10 13 41 | 9 14 30 |
mit | mit 2976 | 9 8 22 | 10 14 43 | 12 12 27 |
Table 5.1616.1 GPS week: 1616 Day: 1 MJD: 55557.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 7 6 17 | 8 12 41 | 93 42 200 |
emr | emr 2972 | 16 10 23 | 9 13 45 | 92 56 199 |
esa | esa 2976 | 8 5 19 | 8 12 41 | 86 49 180 |
gfz | gfz 2972 | 9 5 18 | 8 13 44 | 98 47 212 |
grg | grg 2976 | 8 9 21 | 8 12 40 | 87 44 191 |
igr | igr 2976 | 9 5 19 | 8 13 42 | 84 42 186 |
igs | igs 2976 | 9 5 17 | 7 12 41 | 91 46 195 |
jpl | jpl 2779 | 19 22 48 | 9 14 39 | 101 52 234 |
mit | mit 2976 | 8 5 20 | 8 13 44 | 96 53 202 |
Table 5.1616.2 GPS week: 1616 Day: 2 MJD: 55558.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2923 | 6 8 21 | 8 10 27 | 6 5 11 |
emr | emr 2876 | 16 14 30 | 8 9 36 | 7 11 23 |
esa | esa 2880 | 9 10 18 | 7 9 33 | 7 7 12 |
gfz | gfz 2877 | 10 10 18 | 7 10 30 | 8 10 21 |
grg | grg 2880 | 8 12 20 | 8 11 37 | 9 9 15 |
igr | igr 2880 | 9 10 23 | 8 9 30 | 6 5 13 |
igs | igs 2879 | 10 10 19 | 8 9 30 | 7 6 12 |
jpl | jpl 2773 | 21 25 55 | 9 9 43 | 8 8 14 |
mit | mit 2880 | 9 9 18 | 7 8 39 | 10 15 36 |
Table 5.1616.3 GPS week: 1616 Day: 3 MJD: 55559.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2928 | 5 8 17 | 11 12 35 | 6 5 12 |
emr | emr 2876 | 13 8 24 | 12 11 34 | 11 15 40 |
esa | esa 2880 | 7 5 14 | 10 11 32 | 6 5 15 |
gfz | gfz 2876 | 8 5 17 | 10 14 33 | 6 8 15 |
grg | grg 2880 | 7 7 15 | 10 13 40 | 7 8 17 |
igr | igr 2880 | 6 5 16 | 11 11 32 | 6 6 14 |
igs | igs 2879 | 7 6 16 | 11 11 33 | 6 6 14 |
jpl | jpl 2683 | 15 14 41 | 11 13 35 | 8 11 29 |
mit | mit 2880 | 10 7 20 | 11 11 33 | 7 10 31 |
Table 5.1616.4 GPS week: 1616 Day: 4 MJD: 55560.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3027 | 15 24 44 | 16 19 51 | 8 7 18 |
emr | emr 2972 | 21 25 44 | 16 21 46 | 8 16 33 |
esa | esa 2976 | 17 25 46 | 15 19 48 | 8 8 18 |
gfz | gfz 3053 | 17 24 44 | 15 21 50 | 8 9 20 |
grg | grg 2976 | 17 25 46 | 16 22 56 | 10 11 20 |
igr | igr 3005 | 16 23 44 | 15 21 46 | 8 9 18 |
igs | igs 2976 | 17 24 44 | 15 21 46 | 8 8 18 |
jpl | jpl 2778 | 31 37 79 | 17 24 49 | 10 15 24 |
mit | mit 3072 | 30 33 41 | 21 34 82 | 29 25 48 |
Table 5.1616.5 GPS week: 1616 Day: 5 MJD: 55561.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 8 8 20 | 8 10 29 | 5 8 17 |
emr | emr 2972 | 15 12 27 | 11 11 31 | 8 7 29 |
esa | esa 2976 | 10 11 21 | 8 9 26 | 6 7 18 |
gfz | gfz 2972 | 11 13 22 | 9 10 28 | 7 9 18 |
grg | grg 2976 | 21 16 24 | 10 11 33 | 8 10 23 |
igr | igr 2969 | 10 8 19 | 9 11 30 | 6 8 19 |
igs | igs 2971 | 10 9 21 | 9 9 28 | 6 8 17 |
jpl | jpl 2780 | 33 44 108 | 11 12 41 | 7 8 28 |
mit | mit 2976 | 18 20 82 | 10 13 42 | 9 9 28 |
Table 5.1616.6 GPS week: 1616 Day: 6 MJD: 55562.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3015 | 8 7 22 | 13 15 41 | 6 8 16 |
emr | emr 2971 | 13 9 24 | 15 16 47 | 10 9 24 |
esa | esa 2976 | 8 11 20 | 13 15 42 | 7 8 18 |
gfz | gfz 2970 | 9 11 25 | 12 14 43 | 9 10 22 |
grg | grg 2975 | 8 9 28 | 11 14 44 | 8 8 25 |
igr | igr 2975 | 8 9 20 | 13 16 47 | 8 8 17 |
igs | igs 2975 | 8 9 21 | 13 15 43 | 8 8 19 |
jpl | jpl 2871 | 10 10 30 | 15 17 67 | 8 7 16 |
mit | mit 2976 | 13 12 36 | 13 18 52 | 11 12 34 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1616 GPS week: 1616 MJD: 55556.500-55562.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 9 -41 -8 72 1 | -2 24
| 20 17 99 66 3 | 3
emr uuuuu | 37 -24 123 203 -4 | 12 26
| 25 38 153 62 9 | 3
esa uuuuu | 5 -1 61 -4 3 | -12 25
| 18 18 59 65 4 | 3
gfz uuuuu | 5 39 -74 51 3 | -5 21
| 16 17 59 26 7 | 4
grg uuuux | 5 -33 6 27 -6 | -1 38
| 48 21 151 80 19 | 3
igr xxxxx | 0 28 8 -74 -1 | -2 19
| 33 12 74 73 6 | 4
irf xxxxx | 0 -12 -142 17 2 | -7 23
| 14 21 64 30 9 | 4
jpl uuuuu | 26 -7 -113 103 -12 | -7 25
| 18 25 103 78 9 | 6
mit uuxuu | -29 10 -385 -68 1 | 5 24
| 24 38 102 102 13 | 4
ngs uuuuu | -4 -1 -11 -202 1 | -8 19
| 34 49 128 128 13 | 3
sio uuuuu | -56 -60 33 33 1 | 8 24
| 23 31 126 56 10 | 4
Table 7.1616.0 GPS week: 1616 Day: 0 MJD: 55556.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -18 -62 1 49 -1 | -1 19
emr uuuuu | -16 -4 -102 161 -8 | 15 23
esa uuuuu | 10 17 69 -89 -3 | -8 18
gfz uuuuu | -5 53 -71 70 7 | -6 15
grg uuuux | 81 12 -277 39 26 | 4 38
igr xxxxx | -51 42 20 -190 4 | 2 15
irf xxxxx | -5 -41 -58 53 6 | -7 17
jpl uuuuu | 15 35 -70 106 -12 | 1 20
mit uuxuu | -39 -51 -237 95 7 | 6 18
ngs uuuuu | 16 -16 139 -250 -1 | -4 12
sio uuuuu | -67 -97 214 62 3 | 8 17
Table 7.1616.1 GPS week: 1616 Day: 1 MJD: 55557.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 4 -62 -170 151 -2 | -4 23
emr uuuuu | 53 -6 100 256 -15 | 11 25
esa uuuuu | 11 21 -8 35 1 | -13 24
gfz uuuuu | 3 33 -82 63 9 | -9 20
grg uuuux | 49 -39 -35 162 -27 | 2 38
igr xxxxx | -4 7 -67 -41 -6 | -3 19
irf xxxxx | -11 -22 -80 54 11 | -10 21
jpl uuuuu | 27 21 -104 -39 -11 | -4 26
mit uuxuu | -47 -10 -254 41 13 | 2 19
ngs uuuuu | -23 -44 100 -435 -17 | -8 19
sio uuuuu | -89 -77 174 45 11 | 4 20
Table 7.1616.2 GPS week: 1616 Day: 2 MJD: 55558.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -1 -33 124 -33 3 | -4 23
emr uuuuu | 53 -72 287 134 -12 | 11 25
esa uuuuu | -5 -11 68 45 0 | -13 24
gfz uuuuu | 10 25 -119 73 8 | -8 19
grg uuuux | -1 -38 -12 104 -17 | -2 38
igr xxxxx | -20 22 -103 -61 -10 | -3 19
irf xxxxx | -23 -13 -181 -17 11 | -9 21
jpl uuuuu | 6 -16 -244 176 -30 | -5 26
mit uuxuu | -66 9 -454 -134 14 | 3 20
ngs uuuuu | 41 57 28 -237 -11 | -9 20
sio uuuuu | -80 -50 -5 -81 12 | 5 20
Table 7.1616.3 GPS week: 1616 Day: 3 MJD: 55559.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 8 -29 86 131 5 | -2 24
emr uuuuu | 54 -62 281 157 -8 | 11 26
esa uuuuu | 35 -18 53 71 9 | -12 25
gfz uuuuu | -5 43 -66 11 8 | -4 22
grg uuuux | -65 -30 11 -3 -16 | 0 38
igr xxxxx | -23 35 97 -72 -6 | -3 20
irf xxxxx | 1 -10 -215 19 5 | -6 24
jpl uuuuu | 61 -27 -231 67 -15 | -7 26
mit uuxuu | -28 10 -489 -55 6 | 6 24
ngs uuuuu | -30 42 39 -188 -6 | -8 20
sio uuuuu | -54 -60 -125 60 4 | 9 25
Table 7.1616.4 GPS week: 1616 Day: 4 MJD: 55560.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 2 -44 -88 28 -3 | 4 26
emr uuuuu | 37 -32 225 203 -3 | 16 27
esa uuuuu | 11 -3 50 14 3 | -7 25
gfz uuuuu | 34 63 -167 30 4 | 1 23
grg uuuux | -26 -50 207 -16 12 | -1 38
igr xxxxx | 19 39 56 -130 2 | 1 19
irf xxxxx | 12 0 -212 25 -4 | 0 23
jpl uuuuu | 35 -30 15 128 -12 | -3 24
mit uuxuu | -10 29 -459 -96 -4 | 11 27
ngs uuuuu | -53 -4 -70 -171 11 | -6 20
sio uuuuu | -34 -44 -93 97 -6 | 14 28
Table 7.1616.5 GPS week: 1616 Day: 5 MJD: 55561.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 23 -42 7 54 3 | -1 27
emr uuuuu | 25 -34 105 199 6 | 13 27
esa uuuuu | -15 -22 17 -7 3 | -11 28
gfz uuuuu | 14 46 -15 77 -9 | -2 24
grg uuuux | -12 -48 27 -28 -16 | -2 38
igr xxxxx | 41 29 69 -66 1 | -2 21
irf xxxxx | 17 -24 -103 -15 -7 | -4 26
jpl uuuuu | 27 -14 -3 86 -4 | -10 27
mit uuxuu | 4 9 -378 -167 -11 | 7 28
ngs uuuuu | -10 37 -71 -101 15 | -9 22
sio uuuuu | -28 -85 48 23 -7 | 10 29
Table 7.1616.6 GPS week: 1616 Day: 6 MJD: 55562.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 45 -14 -20 125 1 | -7 27
emr uuuuu | 49 41 -39 310 11 | 8 24
esa uuuuu | -13 13 178 -96 8 | -17 30
gfz uuuuu | -16 14 4 35 -7 | -8 27
grg uuuux | 9 -35 122 -67 -9 | -6 41
igr xxxxx | 34 24 -19 43 5 | -9 21
irf xxxxx | 5 25 -145 -4 -9 | -11 29
jpl uuuuu | 12 -15 -157 196 -2 | -19 28
mit uuxuu | -21 74 -428 -160 -19 | 0 28
ngs uuuuu | 30 -77 -240 -31 13 | -14 22
sio uuuuu | -43 -3 19 23 -14 | 4 28
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