[IGSREPORT-19036] Wk 1602 IGS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Oct 7 02:44:00 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1602 (Sep 19, 2010 - Sep 25, 2010)
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:
igs1602[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1602[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1602[0-6].cls IGS GPS clock combination summary report.
igs16027.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs16027.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 | ALL | 1
0 | COD | DGAR
0 | EMR | WTZR WTZR
0 | ESA | DUBO DUBO UNSA
0 | GFZ | 16 25 30 CRO1 KOUC MDVJ SFER
0 | GRG | 25 DGAR NRC1 RAMO
0 | JPL | 32
0 | MIT | 15 18 25 15 18 25
1 | ALL | 1 1
1 | COD | DGAR
1 | EMR | WTZR WTZR YAKT
1 | ESA | UNSA
1 | GFZ | 25 BAKO MDVJ SOFI YAKT
1 | GRG | 25 DGAR ONSA UNSA
1 | MIT | 11 23 25 11 23 25 HOB2 PTBB HOB2 PTBB
2 | ALL | 1
2 | COD | WROC DGAR WROC XMIS
2 | EMR | WTZR WTZR
2 | ESA | COCO UNSA
2 | GFZ | 1 25 CRO1 HYDE KOUC NRC1 SUTM SUWN
2 | GRG | 25 DGAR NRC1
2 | JPL | 32 SFER
2 | MIT | 25 1 25 FLIN
3 | ALL | 1
3 | EMR | 1 WTZR WTZR
3 | ESA | KERG SALU
3 | GFZ | 9 30 ALGO ARTU BAKO HYDE KIRU KOUC MAC1 MDVJ RABT
3 | GFZ | THTI UNBJ UNSA
3 | GRG | DGAR ONSA
3 | MIT | 25 25 DARW BRUS DARW
4 | ALL | 1 1
4 | COD | 25 25 DGAR
4 | EMR | TLSE WTZR TLSE WTZR
4 | ESA | BJFS SCH2 KERG SCH2 UNSA
4 | GFZ | 25 AREQ COCO IRKJ KOUC MDVJ SCH2 SFER WHIT
4 | GRG | DGAR ONSA
4 | JPL | 32
4 | MIT | GODE MDVJ GODE IRKJ MDVJ
5 | ALL | 1 1
5 | COD | 25 25 DAV1 DGAR
5 | EMR | 27 WTZR KERG WTZR
5 | ESA | NRIL SUTH
5 | GFZ | FAA1 GUAT MDVJ NRC1
5 | GRG | DGAR LPGS RAMO SPT0
5 | JPL | 27 32 HARB
5 | MIT | 27 27
6 | ALL | 1
6 | COD | 25 25
6 | EMR | 27 27 WTZR WTZR
6 | ESA | KERG SUTH UNSA
6 | GFZ | 25 30 BRUS CRO1 NYAL SFER
6 | GRG | DGAR ONSA
6 | JPL | 32 HARB
6 | MIT | 27 27 PIE1 USNO MDVJ NYA1 PIE1 USNO
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
----+------------+----------
G19 | 2010_09_21 | 2010126
G20 | 2010_09_23 | 2010127
6. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | GRG | 19
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 | .4 1.1 .9 -1 -5 -21 -.36
EMR | 3.1 7.7 -.8 25 -7 -13 .06
ESA | 3.6 5.6 9.2 96 14 -29 -.28
GFZ | .0 1.8 .3 24 -3 -47 -.14
GRG | 1.1 10.3 7.2 58 37 -80 .06
JPL | 4.8 9.9 -2.5 -1 -15 6 .07
MIT | 4.2 4.1 10.9 21 2 -33 -.29
NGS | 4.9 4.2 4.8 76 -79 10 -.23
SIO | 5.9 9.3 -6.4 137 -129 -31 -.22
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 1.1602.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1602.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 2.1602.[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 3.1602.[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 5.1602.0-6).
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 1602 summary. (Sep 19, 2010 - Sep 25, 2010)
Table 1.1602.a GPS week: 1602 MJD: 55458.000-55464.000
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 229| 0 0 0 82 -17 -37 -.25 8 7 | -535 291 14 60
| 0 0 0 11 10 15 .03 | 170 318
emr 90| 0 2 0 81 -12 19 .44 19 19 | -530 -393 14 83
| 1 2 2 22 22 15 .03 | 2107 1213
esa 131| 0 0 1 -85 -37 5 .24 7 7 | -1126 732 13 114
| 0 0 1 15 26 14 .05 | 705 946
gfz 193| 0 0 0 31 -42 -6 -.20 14 13 | -41 130 23 103
| 1 1 1 71 86 10 .04 | 367 469
grg 134| 1 1 2 -24 -101 1 .54 16 15 | 2857063 180 45 219
| 0 1 2 15 14 19 .02 | 4879553 284
igr n/a| 0 -1 0 89 -23 6 -.06 5 5 | 1966 -1003 16 56
| 0 0 0 16 18 17 .02 | 3639 1316
jpl 127| -1 0 -2 75 4 37 .50 19 19 | 3182 -678 17 111
| 1 0 1 19 15 37 .03 | 2789 1209
mit 260| 1 -2 0 42 -54 8 -.36 13 12 | -93 88 19 163
| 1 0 1 29 25 8 .02 | 415 655
ngs 214| 0 0 0 -49 141 18 -.24 11 8 | 53432 162192 2243 3773
| 0 0 0 18 44 11 .05 | 188032 753433
sio 255| 2 1 -2 -219 234 -1 -.14 23 22 | --- --- --- ---
| 0 2 1 27 33 7 .02 | --- ---
Table 1.1602.b GPS week : 1602 MJD: 55458.000-55464.000
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 | 12 16 14 13 23 19 23 |
2 | 4 5 5 5 5 6 5 |
3 | 4 4 3 4 4 4 4 |
4 | 3 4 4 4 4 5 5 |
5 | 4 5 4 5 5 5 5 |
6 | 4 4 3 4 4 4 4 |
7 | 4 5 5 5 5 5 5 |
8 | 3 4 4 4 5 4 5 |
9 | 4 5 5 5 5 6 6 |
10 | 3 3 4 4 4 4 4 |
11 | 4 4 4 4 5 4 4 |
12 | 5 5 5 6 6 5 5 |
13 | 4 4 4 5 5 5 5 |
14 | 4 4 4 5 5 5 4 |
15 | 5 6 6 6 5 5 5 |
16 | 6 5 5 7 6 6 6 |
17 | 4 5 5 5 5 4 5 |
18 | 5 4 4 5 5 5 5 |
19 | 4 4 0 5 5 5 5 |
20 | 4 4 4 4 21 5 4 |
21 | 5 4 5 5 5 5 7 |
22 | 4 4 4 4 4 4 4 |
23 | 4 5 4 5 5 5 5 |
24 | 4 4 4 4 5 4 5 |
25 | 11 11 10 9 13 10 11 |
26 | 4 4 4 4 4 4 4 |
27 | 4 5 5 6 6 5 5 |
28 | 4 5 5 5 5 5 5 |
29 | 4 5 5 5 5 5 5 |
30 | 4 4 5 5 5 4 5 |
31 | 5 4 4 5 5 4 4 |
32 | 4 4 4 4 5 5 5 |
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 2.1602.0 GPS week: 1602 Day: 0 MJD: 55458.000
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 229| 0 1 0 84 -18 -27 -.22 7 7 | -666 345 14 57
| -19 -1 |
emr 90| 0 0 -1 64 16 37 .48 19 19 | 1309 530 15 84
| -70 2 |
esa 131| 1 0 0 -79 -11 26 .28 7 7 | -940 749 13 110
| 18 -3 |
gfz 193| 0 1 1 8 -112 -19 -.18 14 13 | -143 426 23 97
| -75 13 |
grg 134| 2 2 3 -13 -105 10 .54 15 14 | -298 534 43 196
| -6 -26 |
igr n/a| -1 -1 0 97 -29 -6 -.04 5 5 | 6145 9 16 50
| -48 -5 |
jpl 127| -3 0 -3 65 2 -22 .53 19 19 | 6002 470 17 106
| 47 -163 |
mit 260| 0 -2 1 18 -62 -1 -.38 10 10 | -368 491 21 170
| 15 5 |
ngs 214| 0 0 0 -46 161 20 -.26 9 7 | -716 355 2135 3419
| -5 -3 |
sio 255| 1 -1 -2 -248 223 -4 -.15 22 23 | --- --- --- ---
| 109 -90 |
Table 2.1602.1 GPS week: 1602 Day: 1 MJD: 55459.000
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 229| 0 0 0 81 -21 -13 -.25 7 7 | -485 175 13 58
| 13 3 |
emr 90| 1 1 1 104 -7 11 .42 18 18 | 949 313 12 102
| -116 24 |
esa 131| 0 0 1 -85 1 4 .29 7 7 | -2158 2316 11 109
| 33 5 |
gfz 193| 1 0 -2 -23 -76 -3 -.17 13 12 | -367 367 23 102
| -47 14 |
grg 134| 2 1 -1 -33 -93 0 .55 15 13 | 9999999 -24 38 175
| 9 -56 |
igr n/a| -1 0 0 87 -15 -1 -.09 5 5 | 5286 -636 16 49
| -47 16 |
jpl 127| -2 -1 -3 83 -2 12 .46 19 19 | 5619 -56 17 122
| 16 -6 |
mit 260| 0 -2 1 47 -52 0 -.40 11 10 | -330 75 19 203
| 13 6 |
ngs 214| 0 0 0 -52 158 31 -.28 12 9 | -95237 1780889 2260 3454
| 4 40 |
sio 255| 2 0 -1 -210 228 -8 -.15 22 21 | --- --- --- ---
| 111 -88 |
Table 2.1602.2 GPS week: 1602 Day: 2 MJD: 55460.000
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 229| 0 0 -1 79 -13 -32 -.21 7 7 | -783 917 14 58
| 26 -2 |
emr 90| 3 1 2 108 -42 36 .46 19 19 | 1507 -1212 14 77
| -121 33 |
esa 131| 0 0 0 -73 -40 -11 .28 8 8 | -659 75 12 113
| 19 4 |
gfz 193| -1 0 0 -23 33 11 -.17 12 11 | -8 396 25 105
| -68 -6 |
grg 134| 2 2 0 -25 -90 -35 .55 16 17 | -8 99 46 227
| 4 -77 |
igr n/a| 0 -1 0 88 -16 14 -.05 4 4 | 4620 -2064 16 53
| -44 -21 |
jpl 127| -1 -1 -2 71 27 57 .53 19 19 | 5489 -1626 18 119
| 14 59 |
mit 260| 0 -2 0 22 -67 16 -.33 11 10 | -91 85 21 176
| 17 8 |
ngs 214| -1 0 0 -50 110 4 -.26 11 9 | 472282 -646955 1748 3534
| -116 77 |
sio 255| 1 0 -1 -227 211 13 -.11 22 22 | --- --- --- ---
| 113 -92 |
Table 2.1602.3 GPS week: 1602 Day: 3 MJD: 55461.000
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 229| 0 0 0 87 -33 -40 -.28 9 9 | -539 326 16 76
| -16 45 |
emr 90| 0 6 -1 89 -37 2 .46 18 18 | 493 -2019 14 81
| -96 1 |
esa 131| 1 -1 0 -90 -77 -13 .24 8 8 | -1374 1023 14 120
| 48 36 |
gfz 193| 0 0 1 63 115 -18 -.20 16 14 | 333 -409 24 111
| -67 13 |
grg 134| 1 2 5 -28 -104 -9 .50 17 17 | 8 161 47 207
| 4 -12 |
igr n/a| -1 -1 0 102 -54 -21 -.05 5 5 | 2613 -2524 18 67
| -47 10 |
jpl 127| 0 -1 -2 102 -4 95 .51 19 19 | 3983 -2066 20 121
| 13 79 |
mit 260| 1 -1 0 31 -19 2 -.34 12 11 | -146 473 18 155
| 5 4 |
ngs 214| -1 0 1 -36 60 22 -.30 10 8 | -679 476 2234 3742
| -23 159 |
sio 255| 3 1 -2 -229 294 -6 -.13 22 22 | --- --- --- ---
| 116 -115 |
Table 2.1602.4 GPS week: 1602 Day: 4 MJD: 55462.000
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 229| 0 1 0 63 0 -45 -.27 8 8 | -392 -125 16 65
| 54 -44 |
emr 90| 0 1 -1 46 -13 16 .42 21 21 | -1523 -1742 15 80
| -49 15 |
esa 131| 0 0 1 -115 -34 19 .23 8 8 | -1371 972 15 123
| 40 33 |
gfz 193| -1 0 -1 165 -92 -7 -.26 14 13 | 352 -360 26 108
| -61 9 |
grg 134| 1 1 3 -51 -96 25 .54 16 15 | 89 -255 45 271
| 79 -59 |
igr n/a| 0 0 1 70 1 13 -.08 5 5 | 131 -2471 16 60
| -46 4 |
jpl 127| -4 -1 -1 67 24 29 .49 21 21 | 1922 -2144 18 101
| 72 0 |
mit 260| 2 -2 0 89 -89 11 -.36 13 13 | 772 -1343 15 135
| 4 5 |
ngs 214| -1 0 0 -86 178 4 -.16 12 9 | -531 11 2366 3530
| 42 -19 |
sio 255| 3 2 -3 -171 199 -2 -.16 23 23 | --- --- --- ---
| 109 -97 |
Table 2.1602.5 GPS week: 1602 Day: 5 MJD: 55463.000
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 229| 0 0 -1 101 -9 -64 -.27 9 7 | -608 271 12 55
| -4 15 |
emr 90| -2 5 -1 91 14 33 .39 20 20 | -3666 711 16 83
| -75 -38 |
esa 131| 0 0 2 -70 -52 10 .17 7 7 | -1458 776 16 109
| 36 45 |
gfz 193| -2 0 0 -33 -115 -7 -.24 13 13 | -634 771 22 100
| -27 35 |
grg 134| 1 0 4 -4 -90 16 .56 16 14 | -345 219 46 237
| 4 -44 |
igr n/a| 0 0 0 112 -8 31 -.06 6 6 | -2571 130 17 67
| -31 12 |
jpl 127| 0 0 -1 92 0 35 .51 19 19 | -455 187 17 104
| 32 33 |
mit 260| 3 -2 -2 14 -64 14 -.36 15 14 | -478 411 22 138
| -1 4 |
ngs 214| 0 -1 0 -26 187 30 -.22 10 8 | -725 365 2473 4254
| -15 -14 |
sio 255| 2 2 -2 -249 222 -3 -.15 24 23 | --- --- --- ---
| 119 -99 |
Table 2.1602.6 GPS week: 1602 Day: 6 MJD: 55464.000
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 229| 0 0 0 77 -22 -38 -.28 9 7 | -275 132 13 56
| 59 26 |
emr 90| -1 0 -3 65 -15 0 .41 19 19 | -2780 668 15 80
| -56 12 |
esa 131| 0 -1 1 -83 -46 1 .20 7 7 | 73 -782 13 119
| 55 68 |
gfz 193| 0 2 1 61 -46 -2 -.19 13 13 | 174 -276 21 101
| -41 23 |
grg 134| 0 0 2 -15 -131 2 .52 17 16 | 9999999 528 50 220
| 10 -2 |
igr n/a| 0 0 0 67 -38 13 -.05 5 5 | -2458 535 17 50
| -18 19 |
jpl 127| 0 0 0 44 -14 51 .47 20 20 | -286 484 18 104
| 73 42 |
mit 260| 3 -1 -3 72 -22 19 -.35 15 13 | -13 428 22 170
| -4 3 |
ngs 214| 0 0 2 -45 133 17 -.21 9 8 | -368 205 2487 4483
| -34 59 |
sio 255| 1 4 -4 -200 263 4 -.13 24 20 | --- --- --- ---
| 123 -112 |
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 3.1602.0 GPS week: 1602 Day: 0 MJD: 55458.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 12 --- --- 24 --- 51 --- 18 --- --- 12 | 29 --- --- 40 --- 63 --- 35 --- --- 29
2 | 6 22 8 10 18 9 19 10 8 16 4 | 20 27 18 19 21 22 24 20 24 26 18
3 | 4 13 5 13 13 3 12 8 7 27 3 | 11 22 12 14 18 11 21 10 16 22 10
4 | 5 17 6 9 9 4 12 9 9 20 3 | 22 34 27 22 27 24 29 26 28 35 24
5 | 5 18 7 15 11 4 20 10 6 31 4 | 20 27 25 28 28 19 28 22 22 30 21
6 | 5 15 6 12 12 3 15 6 5 25 3 | 13 25 15 16 22 14 27 13 16 22 13
7 | 7 17 7 15 19 3 23 6 5 23 4 | 13 22 20 20 28 13 20 13 17 15 14
8 | 8 15 5 10 10 3 12 9 5 19 3 | 13 26 16 16 19 15 25 18 20 16 15
9 | 8 18 5 12 13 6 16 13 12 24 4 | 21 29 21 23 27 20 31 24 24 30 22
10 | 5 14 6 10 9 5 13 7 7 14 3 | 29 31 31 29 32 28 27 30 33 30 30
11E | 5 16 4 8 15 3 22 8 7 10 3 | 12 22 14 15 23 12 24 16 13 14 12
12 | 9 15 10 29 12 8 17 7 10 35 5 | 21 29 30 37 30 22 30 27 25 39 25
13 | 7 19 8 10 20 4 21 9 11 21 4 | 16 27 20 19 34 17 32 19 20 21 17
14 | 5 17 7 10 22 5 23 8 9 14 4 | 17 28 21 28 28 20 29 19 25 19 20
15 | 7 28 9 17 16 5 26 11 13 16 5 | 17 29 21 25 26 18 29 21 17 20 18
16 | 8 20 10 17 18 6 21 23 10 30 5 | 17 29 23 26 26 19 29 21 19 17 17
17 | 7 24 7 12 18 4 20 10 8 21 4 | 13 32 22 18 32 17 31 19 16 24 17
18 | 8 21 9 16 16 4 25 7 13 24 4 | 15 33 28 26 29 20 30 20 21 19 20
19 | 7 21 7 11 17 4 26 7 8 23 4 | 9 21 9 10 8 7 22 8 11 10 8
20 | 5 19 5 10 12 4 22 9 9 20 3 | 12 24 15 15 21 13 27 12 17 16 13
21 | 6 24 12 26 18 6 23 8 9 16 5 | 17 31 22 25 32 19 30 20 21 21 19
22 | 6 18 6 11 12 4 23 11 9 22 4 | 22 32 30 31 33 27 31 27 27 25 26
23 | 6 23 8 12 17 4 23 7 9 21 4 | 20 30 24 25 29 21 34 22 24 22 21
24 | 6 18 8 13 10 5 13 12 10 24 4 | 16 23 11 21 13 14 21 19 15 17 13
X25 | 34 --- 12 31 22 10 --- 18 14 --- 10 | 22 --- 31 30 38 23 --- 30 23 --- 22
26 | 6 13 8 10 10 4 14 12 9 13 3 | 14 21 18 15 17 14 20 18 15 18 15
27 | 8 18 5 12 10 7 17 15 12 20 4 | 40 52 44 45 51 44 53 46 45 45 44
28 | 5 17 6 13 10 7 21 12 8 30 4 | 22 32 28 31 33 24 34 30 23 28 25
X29 | 5 25 9 10 17 5 20 7 7 --- 4 | 16 30 17 15 24 18 29 15 19 --- 15
30 | 10 10 6 26 9 5 9 9 6 27 4 | 29 30 34 35 35 30 31 32 29 33 30
31 | 5 22 9 13 21 6 19 14 13 11 4 | 15 22 19 18 32 15 23 17 21 16 16
32 | 7 18 7 10 10 5 17 12 10 30 4 | 18 21 23 25 23 19 21 16 23 33 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 7 14 15 5 19 10 9 22 |T 18 28 22 23 27 20 28 21 21 23 19
WRMS | 7 19 7 13 14 5 19 10 7 23 |NE 17 26 21 23 26 20 27 20 20 22 18
MEDI | 6 18 7 12 13 5 20 9 9 21 |MD 17 28 21 23 28 19 29 20 21 22 18
Table 3.1602.1 GPS week: 1602 Day: 1 MJD: 55459.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 21 35 --- 23 --- 43 --- 37 41 --- 15 | 21 37 --- 33 --- 59 --- 47 39 --- 26
2 | 6 24 8 14 18 6 20 10 10 18 4 | 16 25 16 20 25 15 22 18 18 18 15
3 | 4 14 7 10 11 5 11 7 11 23 3 | 11 19 12 9 15 9 19 8 18 21 10
4 | 9 18 6 13 9 5 15 10 12 21 4 | 20 27 22 22 28 21 32 22 24 30 21
5 | 10 17 7 18 17 5 20 11 11 30 5 | 15 26 15 19 24 12 25 14 12 23 12
6 | 5 17 7 11 13 6 11 7 8 20 3 | 12 26 15 15 20 14 23 11 20 23 14
7 | 8 22 8 14 19 3 17 8 13 23 4 | 13 24 20 20 29 12 20 11 20 14 13
8 | 8 17 5 14 9 4 13 9 12 16 3 | 12 26 19 18 22 15 24 18 20 20 16
9 | 9 19 5 12 9 5 17 17 13 24 4 | 23 29 20 22 24 19 29 22 25 29 21
10 | 6 10 5 12 12 5 10 7 13 18 3 | 22 25 26 26 27 23 27 23 27 20 23
11E | 6 17 4 8 17 3 20 9 8 12 3 | 18 27 18 18 24 17 24 21 17 19 16
12 | 6 15 7 19 13 6 20 10 10 35 4 | 18 23 23 25 25 19 26 19 22 35 18
13 | 7 16 7 9 20 4 19 6 14 21 4 | 18 30 21 18 34 18 29 19 21 22 18
14 | 6 18 6 13 19 4 24 10 10 13 4 | 14 24 20 21 29 14 26 15 17 15 14
15 | 8 27 7 15 16 4 27 15 18 16 5 | 16 27 17 18 22 14 28 18 21 18 15
16 | 8 19 9 16 13 7 18 22 13 28 5 | 13 27 14 21 22 14 26 15 19 16 12
17 | 8 25 8 16 17 4 20 8 10 24 4 | 13 29 23 16 31 16 28 16 21 16 16
18 | 6 18 7 17 12 4 23 5 12 22 4 | 16 30 25 19 26 15 28 17 18 17 18
19 | 6 19 7 11 15 2 25 6 11 22 4 | 11 21 9 12 10 7 23 8 8 11 8
20 | 7 18 9 12 14 5 20 8 11 19 4 | 14 25 22 18 19 16 24 15 20 17 16
21 | 5 19 7 18 18 5 21 8 10 14 4 | 16 28 22 16 33 19 26 18 18 17 17
22 | 6 16 5 13 11 4 23 10 8 22 4 | 18 29 23 20 29 17 28 17 18 20 19
23 | 9 21 9 11 17 3 20 6 11 21 4 | 19 32 25 23 27 20 29 20 23 23 19
24 | 7 16 9 11 13 5 13 11 12 23 4 | 15 19 14 17 18 14 19 18 15 16 11
X25 | 35 --- 12 22 20 7 --- 22 15 --- 10 | 19 --- 23 22 33 17 --- 22 21 --- 16
26 | 7 14 7 11 11 3 14 13 13 13 3 | 11 16 15 12 16 9 17 15 17 14 11
27 | 7 17 6 12 14 7 18 17 16 20 4 | 32 41 35 38 38 35 45 37 41 37 36
28 | 7 19 10 11 13 7 21 10 10 31 4 | 20 31 30 28 31 21 33 23 17 21 23
X29 | 6 22 6 13 16 5 21 7 11 --- 4 | 16 25 16 18 23 16 26 15 17 --- 13
30 | 8 11 5 18 10 5 12 10 9 27 4 | 23 22 25 28 27 22 24 24 25 28 21
31 | 6 19 6 9 21 5 19 13 12 9 4 | 10 19 17 13 31 12 22 13 14 13 12
32 | 7 18 8 9 11 5 14 11 10 29 4 | 14 20 21 19 18 15 17 17 17 31 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 18 7 13 15 5 19 11 12 22 |T 16 26 20 20 25 17 25 18 20 20 16
WRMS | 7 18 7 12 13 5 19 10 9 21 |NE 15 25 19 19 24 16 24 17 19 19 15
MEDI | 7 18 7 13 14 5 19 10 11 21 |MD 16 26 20 19 25 16 26 18 19 20 16
Table 3.1602.2 GPS week: 1602 Day: 2 MJD: 55460.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 15 43 --- 40 --- 38 --- 22 29 --- 14 | 20 40 --- 51 --- 50 --- 35 28 --- 24
2 | 6 21 8 9 21 5 20 9 13 18 4 | 19 27 23 24 28 22 28 22 26 27 20
3 | 4 13 6 8 14 3 12 7 8 22 3 | 11 21 13 14 19 14 21 10 16 24 12
4 | 8 20 7 8 12 3 14 11 12 21 4 | 20 32 24 23 33 23 31 25 26 36 23
5 | 7 16 6 10 20 4 19 9 8 29 4 | 22 30 23 22 30 20 29 20 20 27 20
6 | 5 14 6 8 13 3 13 7 10 18 3 | 13 26 16 19 22 17 27 12 18 25 15
7 | 8 22 12 15 18 5 23 9 12 21 5 | 11 26 20 20 29 12 20 13 19 14 13
8 | 8 14 6 14 15 2 11 11 11 16 3 | 20 29 22 22 26 22 27 25 29 24 22
9 | 9 19 10 13 11 5 19 16 14 24 5 | 21 29 25 25 25 20 31 25 28 31 22
10 | 6 14 9 10 17 4 15 8 13 15 3 | 20 24 25 23 29 20 25 23 25 20 21
11E | 5 17 5 10 14 3 20 11 9 11 3 | 13 22 12 14 19 11 23 18 13 14 9
12 | 6 17 11 20 15 3 21 12 11 35 5 | 18 26 20 32 22 19 27 24 20 37 18
13 | 7 17 8 7 21 3 19 10 10 22 4 | 14 27 17 17 32 15 28 17 19 21 14
14 | 5 18 6 11 18 3 27 9 10 13 4 | 16 28 19 25 28 16 32 18 18 16 17
15 | 7 30 10 14 19 3 30 15 12 17 5 | 17 32 21 24 22 19 30 22 24 23 19
16 | 8 20 11 9 16 5 20 21 13 27 5 | 15 27 17 23 22 17 29 19 18 17 15
17 | 6 23 11 18 18 3 23 9 10 22 5 | 16 32 27 19 35 20 32 20 19 19 18
18 | 7 21 5 13 16 4 24 6 11 22 4 | 15 36 23 20 26 18 34 19 23 17 19
X19 | 6 --- --- --- --- 26 --- --- --- --- 0 | 19 --- --- --- --- 49 --- --- --- --- 19
20 | 7 19 5 8 13 3 21 10 10 18 4 | 13 25 16 20 20 15 28 15 17 19 15
21 | 7 18 9 16 23 3 20 8 8 14 4 | 21 27 24 17 38 20 32 20 19 19 19
22 | 6 16 5 12 12 5 25 9 11 22 4 | 19 33 24 27 32 25 32 24 24 24 23
23 | 6 20 8 9 18 3 22 7 10 20 4 | 14 28 18 18 24 16 30 16 23 21 15
24 | 6 17 10 8 12 5 14 12 12 22 4 | 13 21 13 17 17 15 20 16 14 18 11
X25 | 33 --- 12 15 21 8 --- 23 14 --- 10 | 20 --- 21 26 32 16 --- 26 19 --- 16
26 | 4 13 9 10 14 3 12 12 9 12 3 | 15 21 19 16 20 15 21 19 16 19 16
27 | 10 20 8 15 15 4 18 14 12 20 4 | 58 62 58 68 64 60 65 62 68 63 62
28 | 6 17 9 13 14 7 24 12 10 32 4 | 22 32 29 29 33 26 34 27 24 25 25
X29 | 7 28 8 13 17 4 26 7 11 --- 5 | 19 33 20 17 28 21 31 17 19 --- 16
30 | 9 11 9 16 11 4 12 13 10 30 4 | 26 24 23 27 30 24 26 30 22 35 23
31 | 4 22 6 7 21 5 16 11 15 9 4 | 14 24 16 20 33 16 27 17 25 18 17
32 | 7 18 7 8 13 4 17 10 11 29 4 | 14 22 18 21 22 16 24 17 22 33 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 19 8 12 16 4 19 11 11 22 |T 18 28 21 23 28 21 29 21 22 24 19
WRMS | 7 19 8 11 17 4 19 10 9 22 |NE 16 27 20 22 26 20 27 20 20 22 17
MEDI | 7 18 8 11 15 4 20 10 11 21 |MD 17 27 20 22 28 19 28 20 20 21 18
Table 3.1602.3 GPS week: 1602 Day: 3 MJD: 55461.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 16 31 --- 20 --- 35 --- 21 33 --- 12 | 30 32 --- 29 --- 32 --- 22 38 --- 21
2 | 7 16 7 11 27 6 17 10 11 19 4 | 20 25 23 21 30 22 24 22 22 25 19
3 | 8 13 5 12 14 6 13 10 8 23 3 | 10 22 15 12 20 15 18 12 13 22 12
4 | 9 16 9 13 12 4 12 11 13 20 4 | 21 34 28 27 31 26 30 25 24 35 25
5 | 9 18 9 17 20 6 19 9 9 29 5 | 22 30 26 34 32 22 29 23 21 29 22
6 | 9 15 5 10 12 5 14 10 7 19 3 | 12 26 17 15 23 17 24 14 15 23 15
7 | 8 19 7 14 19 3 20 9 7 18 4 | 16 27 18 19 30 16 21 16 15 16 16
8 | 9 14 8 11 10 3 12 13 8 16 3 | 26 32 26 27 25 27 30 26 23 29 24
9 | 11 21 8 15 13 5 16 17 11 24 5 | 24 35 27 27 30 27 33 27 27 35 27
10 | 7 12 7 14 19 4 10 8 8 17 3 | 26 33 29 36 36 30 30 27 26 27 27
11E | 8 16 8 11 13 5 22 11 8 12 4 | 15 24 19 20 25 18 22 20 15 20 17
12 | 9 15 9 24 16 6 18 12 14 35 5 | 26 36 31 37 32 31 33 33 31 42 29
13 | 7 16 5 12 23 3 18 11 7 22 4 | 21 31 24 23 36 23 29 22 20 26 20
14 | 8 18 8 14 20 5 25 10 14 12 4 | 18 30 22 25 32 19 29 20 21 19 20
15 | 9 25 11 13 22 5 27 14 8 18 5 | 22 33 28 27 29 23 32 25 24 28 24
16 | 11 22 10 38 17 7 23 23 12 30 7 | 17 30 23 39 26 21 27 22 20 20 19
17 | 7 22 6 12 17 4 22 9 7 22 4 | 19 33 26 20 34 23 32 20 22 24 21
18 | 8 19 8 17 15 9 23 10 12 22 4 | 19 34 27 29 33 25 33 25 24 20 23
X19 | 9 --- 7 11 393 7 --- 8 11 19 4 | 12 --- 13 15 75 14 --- 17 14 18 12
20 | 9 19 7 14 15 4 19 9 10 16 4 | 14 28 22 15 26 16 25 17 16 21 15
21 | 16 21 9 19 22 5 21 11 10 13 5 | 29 33 28 26 38 27 30 22 23 21 23
22 | 7 18 6 15 13 6 20 8 10 22 4 | 21 33 24 29 37 27 31 27 24 24 25
23 | 8 19 9 15 21 3 20 9 8 21 4 | 22 32 25 25 31 23 29 22 22 25 21
24 | 10 15 7 11 14 5 14 12 11 22 4 | 19 22 18 18 21 20 19 20 17 19 17
X25 | 31 --- 11 16 18 14 --- 21 16 --- 9 | 20 --- 32 29 36 23 --- 33 23 --- 24
26 | 5 11 6 8 16 5 12 13 9 15 3 | 19 22 24 20 27 20 25 23 20 23 21
27E | 20 26 8 15 18 7 20 18 13 20 6 | 40 59 51 47 58 51 56 52 46 51 48
28 | 8 19 9 20 12 6 23 11 8 31 5 | 26 37 34 37 35 28 35 30 23 27 29
X29 | 9 20 6 12 20 7 21 8 8 --- 4 | 25 35 30 24 34 28 34 24 24 --- 24
30 | 11 9 7 22 14 5 10 12 10 31 4 | 29 36 35 37 35 34 31 38 35 42 33
31 | 7 19 8 11 19 7 19 13 12 11 4 | 17 31 22 18 34 22 25 21 21 20 19
32 | 8 16 9 9 13 4 13 10 8 29 4 | 18 22 24 19 29 22 20 20 21 34 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 8 16 17 5 19 12 10 22 |T 21 31 25 25 32 24 28 23 22 26 22
WRMS | 9 18 8 14 17 5 19 11 8 22 |NE 20 30 24 25 32 23 27 23 22 25 21
MEDI | 9 18 8 14 17 5 19 11 10 20 |MD 20 32 25 25 32 23 29 22 22 24 21
Table 3.1602.4 GPS week: 1602 Day: 4 MJD: 55462.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 32 40 --- 67 --- 33 --- 28 62 --- 23 | 22 41 --- 80 --- 39 --- 27 54 --- 24
2 | 9 25 8 13 15 5 21 11 12 16 4 | 35 43 40 41 49 37 41 38 39 42 38
3 | 6 17 5 13 12 6 16 12 10 23 4 | 15 24 19 16 21 17 25 15 22 28 19
4 | 7 19 7 11 12 4 14 15 12 23 4 | 19 34 23 24 27 21 29 22 21 34 21
5 | 7 23 9 15 14 6 24 12 11 30 5 | 26 38 33 32 36 28 33 26 29 29 28
6 | 12 17 5 12 13 5 20 12 8 18 4 | 20 24 19 17 21 18 27 15 19 27 19
7 | 7 26 9 17 19 5 23 11 13 19 5 | 19 31 25 27 31 22 27 20 26 22 22
8 | 10 14 7 14 12 7 18 15 15 24 4 | 60 66 61 65 61 62 69 65 69 67 62
9 | 7 21 9 20 17 6 17 18 17 22 5 | 31 39 30 28 32 31 38 32 37 38 32
10 | 7 16 8 12 12 5 15 11 11 15 3 | 25 29 31 27 34 25 27 26 26 24 27
11E | 5 17 8 11 16 5 24 16 10 11 4 | 15 24 15 16 21 15 24 19 18 16 17
12 | 8 18 11 15 14 5 20 13 13 37 5 | 24 33 27 31 32 26 31 29 28 38 27
13 | 6 21 6 14 19 4 22 12 14 22 5 | 19 32 23 28 35 22 33 22 26 25 22
14 | 7 22 7 11 18 4 25 10 13 14 4 | 18 32 26 24 31 21 33 21 24 24 23
15 | 8 29 7 15 17 3 27 15 13 19 5 | 22 35 24 26 27 23 32 25 29 29 25
16 | 8 22 9 15 15 7 25 24 14 29 5 | 19 33 24 26 27 21 31 23 21 22 21
17 | 7 20 7 18 17 4 22 10 8 19 4 | 19 33 27 27 34 22 33 21 21 19 24
18 | 7 21 8 15 11 6 25 9 9 23 4 | 22 36 26 25 30 25 35 25 31 25 26
19 | 6 23 9 12 17 4 28 11 7 19 4 | 16 23 11 16 67 18 24 16 21 21 18
X20 | 9 --- --- 35 --- 19 --- --- --- --- 21 | 6 --- --- 40 --- 14 --- --- --- --- 11
21 | 14 27 9 17 16 5 22 12 13 14 5 | 26 36 26 22 36 24 33 26 26 27 26
22 | 6 20 6 11 11 8 20 10 12 24 4 | 22 33 27 26 33 26 33 24 28 26 26
23 | 7 24 7 14 18 4 22 12 15 22 5 | 19 33 22 26 28 21 32 23 24 26 21
24 | 5 20 11 10 14 6 18 16 17 22 5 | 15 22 16 18 18 16 22 20 20 19 15
X25 | 41 --- 15 35 20 10 --- 27 14 --- 12 | 27 --- 41 49 43 33 --- 44 30 --- 33
26 | 8 16 5 13 11 5 14 14 10 13 3 | 21 27 23 21 23 20 23 22 23 21 22
27E | 15 24 10 18 24 7 23 15 16 26 6 | 72 80 74 80 79 74 83 75 71 74 74
28 | 9 18 7 18 14 6 24 12 8 32 5 | 23 34 29 39 34 28 34 26 29 23 27
X29 | 7 19 7 14 16 5 26 10 12 --- 4 | 24 30 21 23 26 22 37 20 24 --- 21
30 | 7 13 6 12 14 6 11 14 12 32 4 | 30 30 33 30 33 30 31 33 29 36 30
31 | 7 21 8 8 21 4 20 14 12 10 4 | 18 27 19 21 35 20 28 19 18 18 20
32 | 7 16 8 8 16 5 16 12 11 29 4 | 20 23 21 20 27 21 21 19 26 33 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 21 8 14 16 5 21 13 12 23 |T 24 34 27 30 34 26 33 27 29 29 26
WRMS | 8 21 8 13 15 5 21 13 9 23 |NE 21 32 26 30 32 24 31 25 27 27 24
MEDI | 7 20 8 14 15 5 22 12 12 22 |MD 21 33 25 26 32 22 32 23 26 26 23
Table 3.1602.5 GPS week: 1602 Day: 5 MJD: 55463.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 23 43 --- 49 --- 20 --- 34 41 --- 18 | 21 36 --- 45 --- 38 --- 34 47 --- 25
2E | 11 24 6 15 14 7 17 21 12 33 5 | 17 30 23 28 29 20 24 26 22 34 22
3 | 5 15 9 14 13 5 11 14 8 23 4 | 11 16 13 10 15 10 18 12 14 22 8
4 | 11 19 8 12 17 6 17 16 12 30 5 | 31 41 35 30 43 32 44 36 33 44 32
5 | 7 19 5 12 16 6 19 14 11 30 4 | 23 31 23 26 33 20 28 23 23 28 21
6 | 6 17 6 16 13 5 16 14 8 18 4 | 13 20 15 15 19 12 23 13 15 24 11
7 | 11 24 8 17 18 5 21 12 11 20 5 | 16 24 17 17 28 11 21 12 18 18 13
8 | 9 16 7 12 11 6 11 16 10 23 4 | 36 43 38 39 41 38 40 42 38 44 39
9 | 19 21 6 14 21 6 18 22 12 22 5 | 35 46 41 36 49 37 48 38 34 45 36
10 | 5 17 5 11 20 6 10 12 8 15 3 | 20 24 19 21 28 17 22 19 19 17 17
11E | 8 21 8 8 15 8 20 16 10 11 4 | 15 26 16 21 24 18 23 21 20 19 15
12 | 10 18 8 11 16 5 20 14 9 40 5 | 22 31 23 28 26 22 29 23 25 41 23
13 | 7 17 4 9 21 6 18 17 8 23 4 | 20 28 23 19 35 21 29 23 19 25 18
14 | 6 21 7 13 17 3 23 13 11 15 4 | 15 27 18 20 27 15 26 16 16 16 14
15 | 6 24 6 14 16 6 25 14 12 20 5 | 21 32 21 24 27 20 31 21 25 27 21
16 | 8 23 7 14 15 6 22 27 12 29 5 | 15 26 14 16 20 14 25 18 18 16 12
17 | 5 22 5 13 15 4 20 9 10 20 4 | 13 26 18 15 29 13 28 13 16 15 15
18 | 7 21 7 16 13 3 25 11 12 26 4 | 17 31 25 25 26 21 30 23 21 24 20
19 | 7 23 9 14 19 5 26 14 6 18 5 | 14 23 13 17 49 14 26 13 14 16 12
X20 | 7 21 6 --- 14 7 19 13 15 18 4 | 8 20 10 --- 12 10 22 12 10 14 8
21 | 14 23 11 15 17 5 22 12 11 13 5 | 26 32 26 23 32 24 32 23 25 24 23
22 | 6 20 6 12 11 6 22 7 9 25 4 | 18 28 23 21 28 19 30 20 18 20 19
23 | 9 20 7 8 18 5 19 18 9 22 4 | 20 28 25 20 29 22 31 24 24 25 20
24 | 5 20 7 9 13 4 15 15 11 25 4 | 16 21 13 17 14 15 19 19 18 18 11
X25 | 37 --- 17 11 17 10 --- 23 12 --- 10 | 21 --- 32 30 32 26 --- 29 22 --- 23
26 | 6 14 6 8 14 5 13 14 10 13 3 | 15 21 14 15 19 13 17 16 17 14 14
27E | 12 21 8 15 21 10 17 16 16 22 5 | 51 55 53 60 58 56 55 57 58 53 56
28 | 8 19 11 13 15 7 19 13 9 33 5 | 16 29 25 27 28 20 31 21 20 22 20
X29 | 11 22 8 11 16 4 21 12 8 --- 4 | 27 30 23 24 25 25 31 24 26 --- 22
30 | 8 13 8 10 12 6 10 15 8 36 4 | 22 27 26 22 26 23 24 25 23 35 22
31 | 7 20 6 9 19 5 19 14 10 12 4 | 18 25 18 15 31 16 25 17 19 15 15
32 | 5 19 7 10 13 6 15 11 10 33 4 | 14 15 18 18 24 15 19 13 16 31 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 20 7 13 16 6 19 15 10 24 |T 20 28 22 24 29 21 28 22 22 25 20
WRMS | 7 20 7 13 14 6 19 14 8 23 |NE 18 26 20 21 26 18 26 20 20 22 17
MEDI | 7 20 7 12 16 6 19 14 10 22 |MD 18 28 23 21 28 20 26 21 20 24 19
Table 3.1602.6 GPS week: 1602 Day: 6 MJD: 55464.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 15 --- --- 33 --- 139 --- --- --- --- 23 | 26 --- --- 49 --- 136 --- --- --- --- 26
2E | 11 22 7 13 17 5 17 16 9 31 5 | 26 28 26 28 29 25 26 34 28 43 23
3 | 7 15 4 11 13 5 14 12 6 22 3 | 11 17 11 12 14 8 16 15 14 22 10
4E | 9 18 6 10 21 4 14 17 14 22 4 | 28 43 33 33 40 31 41 32 33 40 32
5 | 4 19 5 14 17 4 21 12 12 31 4 | 25 32 30 35 38 25 29 28 24 32 25
6 | 7 16 6 10 14 5 15 12 7 18 3 | 11 20 14 14 18 10 20 15 14 23 12
7 | 8 24 8 15 18 4 23 11 9 19 4 | 21 29 21 23 29 18 21 17 24 22 20
8 | 9 18 7 16 12 5 14 15 10 25 4 | 42 48 41 47 46 42 49 43 40 50 39
9E | 19 23 8 13 20 10 18 18 11 32 6 | 49 50 44 44 46 43 52 45 49 43 47
10 | 6 14 7 12 20 5 10 12 9 13 3 | 28 32 34 27 41 30 32 31 26 27 29
11E | 5 18 6 10 13 3 23 14 10 14 4 | 15 19 14 17 18 14 22 21 15 16 13
12 | 9 15 6 12 11 5 21 12 8 42 4 | 30 35 30 38 33 32 33 35 36 49 33
13 | 5 20 7 11 23 2 20 17 8 22 4 | 21 30 21 22 35 21 31 23 23 28 22
14 | 5 20 7 12 17 3 24 10 8 14 4 | 21 31 24 28 31 21 31 21 23 19 22
15 | 6 24 9 14 19 7 25 14 9 21 5 | 26 32 26 25 29 24 32 27 30 31 26
16 | 8 19 6 13 17 5 20 27 9 32 5 | 22 30 24 24 27 22 30 23 20 22 20
17 | 4 23 8 11 16 5 22 13 13 19 4 | 16 34 23 15 30 19 32 17 20 21 19
18 | 7 22 7 18 15 5 24 10 8 27 4 | 22 34 29 36 34 25 32 25 29 23 25
19 | 9 23 6 12 19 4 31 14 6 17 5 | 17 23 13 16 50 16 25 14 16 17 16
20 | 6 19 5 11 14 3 19 11 9 22 4 | 10 21 10 3 13 12 19 10 13 15 12
21E | 18 19 11 19 19 5 21 33 10 15 6 | 47 41 39 43 39 39 42 42 38 37 36
22 | 5 22 6 12 14 4 24 6 8 25 4 | 26 32 32 38 40 29 32 30 32 25 30
23 | 8 27 8 11 18 4 22 20 5 21 5 | 21 35 22 24 29 23 31 25 25 26 22
24 | 7 19 10 7 16 4 15 17 11 24 4 | 15 21 15 18 17 14 18 20 18 21 15
X25 | 38 --- 11 36 17 9 --- 19 14 --- 11 | 20 --- 43 50 43 31 --- 48 37 --- 35
26 | 5 17 4 11 18 5 13 14 8 13 3 | 19 25 18 17 25 17 22 20 21 15 18
27E | 11 18 5 15 16 11 17 17 16 21 5 | 82 86 80 82 86 76 86 82 76 77 79
28 | 6 18 7 16 14 7 23 10 8 28 4 | 26 35 32 36 36 27 32 28 29 28 28
X29 | 10 22 7 12 17 5 23 10 8 --- 4 | 28 33 24 29 34 28 38 26 24 --- 23
30 | 9 11 6 26 12 5 13 13 9 31 5 | 35 35 37 45 40 36 32 42 37 43 37
31 | 6 20 7 11 21 5 19 12 9 11 4 | 18 26 19 19 34 18 24 21 21 19 20
32 | 7 17 8 10 14 3 13 11 10 34 4 | 21 23 24 25 31 23 21 19 29 35 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 7 13 17 5 20 15 9 24 |T 25 32 27 30 34 29 31 28 27 29 26
WRMS | 7 19 7 13 16 5 20 13 8 20 |NE 22 29 24 27 31 27 28 24 25 26 23
MEDI | 7 19 7 12 17 5 20 13 9 22 |MD 22 32 24 27 34 24 31 25 25 26 23
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 4.1602 GPS week: 1602 MJD: 55458.0-55464.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 |U 8 8 23 |U 7 10 27 |U 8 10 24 |
emr | emr 2896 |U 9 8 29 |U 8 10 33 | 10 11 25 |
esa | esa 2948 | 8 7 25 |U 8 9 28 | 7 10 24 |
gfz | gfz 3027 |U 7 7 24 |U 8 9 30 |U 7 10 21 |
grg | grg 2948 | 9 8 27 |U 8 9 29 | 9 11 28 |
igr | igr 2957 | 8 7 24 | 8 9 29 | 8 8 23 |
igs | igs 2905 | 8 7 24 | 8 9 29 | 7 9 22 |
jpl | jpl 2834 |U 9 9 28 | 9 10 35 |U 10 10 23 |
mit | mit 3030 |U 10 10 29 |U 12 12 33 |U 8 9 22 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1602.0 GPS week: 1602 Day: 0 MJD: 55458.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3049 | 6 6 19 | 11 11 28 | 7 6 21 |
emr | emr 2880 | 8 8 25 | 12 12 32 | 9 8 22 |
esa | esa 2976 | 7 7 26 | 12 11 26 | 9 8 22 |
gfz | gfz 3071 | 6 6 21 | 12 12 31 | 9 6 21 |
grg | grg 2976 | 10 14 32 | 12 11 25 | 12 13 67 |
igr | igr 3031 | 6 7 22 | 12 11 28 | 9 7 20 |
igs | igs 2924 | 7 7 25 | 12 11 28 | 9 6 22 |
jpl | jpl 2874 | 7 8 27 | 13 12 36 | 11 7 23 |
mit | mit 3072 | 19 14 53 | 28 22 47 | 11 8 28 |
Table 5.1602.1 GPS week: 1602 Day: 1 MJD: 55459.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 | 8 6 21 | 5 9 25 | 6 11 19 |
emr | emr 2972 | 8 7 25 | 7 8 27 | 8 10 20 |
esa | esa 2976 | 7 5 18 | 5 8 21 | 7 12 22 |
gfz | gfz 3072 | 6 4 18 | 6 9 20 | 7 11 21 |
grg | grg 2976 | 8 6 21 | 7 8 20 | 6 13 18 |
igr | igr 2976 | 7 5 18 | 6 8 24 | 6 10 19 |
igs | igs 2909 | 7 5 19 | 6 8 22 | 6 9 19 |
jpl | jpl 2880 | 8 7 25 | 6 8 26 | 7 10 16 |
mit | mit 3072 | 11 15 26 | 7 8 27 | 8 8 18 |
Table 5.1602.2 GPS week: 1602 Day: 2 MJD: 55460.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 7 5 20 | 6 10 25 | 6 7 21 |
emr | emr 2867 | 8 8 28 | 8 11 41 | 6 8 20 |
esa | esa 2880 | 8 6 21 | 8 11 33 | 6 8 21 |
gfz | gfz 2976 | 7 5 22 | 8 12 36 | 6 8 18 |
grg | grg 2880 | 7 7 23 | 7 10 33 | 6 9 23 |
igr | igr 2880 | 8 6 21 | 7 10 36 | 5 7 18 |
igs | igs 2824 | 7 5 21 | 8 12 35 | 5 7 18 |
jpl | jpl 2784 | 9 9 22 | 9 13 44 | 6 7 20 |
mit | mit 2976 | 6 5 24 | 8 15 34 | 6 8 18 |
Table 5.1602.3 GPS week: 1602 Day: 3 MJD: 55461.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 7 8 22 | 7 8 29 | 5 7 21 |
emr | emr 2864 | 8 9 31 | 8 8 31 | 6 8 28 |
esa | esa 2976 | 7 6 22 | 7 8 30 | 5 7 26 |
gfz | gfz 3070 | 6 6 22 | 7 7 31 | 5 6 21 |
grg | grg 2976 | 7 7 23 | 8 9 34 | 6 5 24 |
igr | igr 2976 | 7 7 25 | 7 7 30 | 5 5 24 |
igs | igs 2880 | 6 5 22 | 7 7 30 | 5 6 24 |
jpl | jpl 2784 | 8 8 28 | 7 8 33 | 5 6 24 |
mit | mit 3072 | 10 9 27 | 7 7 28 | 6 7 23 |
Table 5.1602.4 GPS week: 1602 Day: 4 MJD: 55462.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 9 10 28 | 7 9 28 | 8 10 22 |
emr | emr 2855 | 11 12 35 | 7 9 33 | 9 9 22 |
esa | esa 2880 | 10 10 33 | 7 7 28 | 7 10 21 |
gfz | gfz 2971 | 9 9 30 | 7 7 34 | 8 10 16 |
grg | grg 2880 | 10 10 34 | 7 8 32 | 7 12 21 |
igr | igr 2904 | 9 8 30 | 6 8 29 | 7 10 19 |
igs | igs 2880 | 10 9 31 | 7 7 29 | 7 9 19 |
jpl | jpl 2784 | 11 12 34 | 8 10 37 | 8 10 21 |
mit | mit 2976 | 8 9 25 | 7 6 30 | 7 7 19 |
Table 5.1602.5 GPS week: 1602 Day: 5 MJD: 55463.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 | 10 9 28 | ---- ---- ---- | 14 11 42 |
emr | emr 2960 | 12 8 30 | ---- ---- ---- | 19 19 36 |
esa | esa 2976 | 10 10 31 | ---- ---- ---- | 8 9 33 |
gfz | gfz 2972 | 11 11 36 | ---- ---- ---- | 7 13 33 |
grg | grg 2976 | 10 9 32 | ---- ---- ---- | 17 11 24 |
igr | igr 2976 | 10 11 33 | ---- ---- ---- | 16 7 44 |
igs | igs 2968 | 10 9 32 | ---- ---- ---- | 8 8 34 |
jpl | jpl 2875 | 11 11 34 | ---- ---- ---- | 21 14 35 |
mit | mit 3072 | 10 9 27 | ---- ---- ---- | 10 8 30 |
Table 5.1602.6 GPS week: 1602 Day: 6 MJD: 55464.0
CENT| CLK EPO | BRUS | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3051 | 8 9 21 | ---- ---- ---- | 9 16 21 |
emr | emr 2876 | 10 7 30 | ---- ---- ---- | 10 14 24 |
esa | esa 2976 | 9 7 21 | ---- ---- ---- | 9 15 21 |
gfz | gfz 3059 | 8 7 22 | ---- ---- ---- | 9 14 20 |
grg | grg 2976 | 9 7 23 | ---- ---- ---- | 10 13 20 |
igr | igr 2962 | 8 6 21 | ---- ---- ---- | 9 14 20 |
igs | igs 2954 | 8 6 21 | ---- ---- ---- | 9 15 21 |
jpl | jpl 2862 | 9 7 24 | ---- ---- ---- | 10 18 24 |
mit | mit 2976 | 8 6 21 | ---- ---- ---- | 10 18 24 |
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 6.1602 GPS week: 1602 MJD: 55458.500-55464.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 3 -11 87 32 -5 | 16 20
| 19 29 86 105 8 | 3
emr uuuuu | 2 88 56 227 -6 | 63 64
| 30 19 74 81 5 | 2
esa uuuuu | -18 -31 44 21 -4 | 23 26
| 20 13 79 97 10 | 2
gfz uuuuu | -5 60 -49 -110 -1 | 9 14
| 22 19 38 32 8 | 2
grg uuuux | 48 -10 -56 -41 -4 | 5 21
| 24 21 70 73 29 | 2
igr xxxxx | 4 45 22 19 -7 | 2 12
| 19 17 53 56 8 | 2
irf xxxxx | 9 5 -101 -53 -3 | 9 17
| 20 15 78 43 12 | 4
jpl uuuuu | 3 -33 47 158 -5 | 18 23
| 66 19 81 77 8 | 3
mit uuuuu | 4 -2 -219 -43 0 | 25 29
| 21 21 107 62 11 | 5
ngs uuuuu | -34 26 101 -88 2 | 6 13
| 49 36 74 153 10 | 2
sio uuuuu | 108 -109 117 26 -5 | 35 40
| 30 16 105 58 14 | 6
Table 7.1602.0 GPS week: 1602 Day: 0 MJD: 55458.500
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 | -17 21 65 -40 -1 | 13 18
emr uuuuu | -20 72 84 206 -2 | 63 64
esa uuuuu | -15 -16 -55 81 4 | 21 24
gfz uuuuu | -31 77 -96 -57 2 | 7 12
grg uuuux | 8 8 -62 -35 -44 | 7 21
igr xxxxx | -13 50 -46 45 -9 | 4 11
irf xxxxx | -18 2 3 -68 5 | 4 15
jpl uuuuu | 145 -45 16 195 2 | 18 23
mit uuuuu | -23 -13 -92 -78 7 | 19 24
ngs uuuuu | -15 7 132 -157 -11 | 9 16
sio uuuuu | 72 -107 275 26 6 | 27 34
Table 7.1602.1 GPS week: 1602 Day: 1 MJD: 55459.500
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 -8 105 47 -4 | 15 20
emr uuuuu | -23 121 22 231 -6 | 63 64
esa uuuuu | -4 -28 -67 70 9 | 22 25
gfz uuuuu | -13 52 -37 -103 3 | 8 13
grg uuuux | 57 -4 -9 28 20 | 2 21
igr xxxxx | -15 52 -1 31 -7 | 4 11
irf xxxxx | 1 5 -21 -28 2 | 5 17
jpl uuuuu | 7 -11 -36 87 -11 | 19 25
mit uuuuu | -5 -8 -107 -5 5 | 21 26
ngs uuuuu | -39 1 237 -289 -4 | 8 14
sio uuuuu | 89 -106 218 83 3 | 29 37
Table 7.1602.2 GPS week: 1602 Day: 2 MJD: 55460.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 11 -48 169 -3 1 | 16 20
emr uuuuu | -24 99 -81 91 -5 | 63 64
esa uuuuu | 5 -41 52 136 -3 | 24 27
gfz uuuuu | 15 46 -3 -146 3 | 9 14
grg uuuux | 86 -26 -86 16 -17 | 4 23
igr xxxxx | 30 22 46 -8 -22 | 5 11
irf xxxxx | 9 -22 -50 -46 10 | 7 17
jpl uuuuu | -50 -36 -44 61 -11 | 21 25
mit uuuuu | 1 -39 -142 -1 14 | 23 28
ngs uuuuu | -68 94 137 -159 -3 | 7 13
sio uuuuu | 101 -135 176 -5 10 | 33 39
Table 7.1602.3 GPS week: 1602 Day: 3 MJD: 55461.500
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 | -6 17 50 197 6 | 18 21
emr uuuuu | 38 97 45 186 -1 | 64 64
esa uuuuu | 3 -47 159 -23 4 | 23 27
gfz uuuuu | 26 68 -99 -117 8 | 10 14
grg uuuux | 51 -3 -156 9 -28 | 7 18
igr xxxxx | 29 48 106 -74 -4 | 2 13
irf xxxxx | 39 1 -120 29 5 | 11 17
jpl uuuuu | -40 -12 50 90 -11 | 21 25
mit uuuuu | 35 -4 -226 51 9 | 27 30
ngs uuuuu | -120 24 44 -133 -6 | 6 12
sio uuuuu | 154 -115 74 125 4 | 38 41
Table 7.1602.4 GPS week: 1602 Day: 4 MJD: 55462.500
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 | 41 -27 -77 -39 -18 | 21 22
emr uuuuu | -18 76 152 289 -14 | 64 65
esa uuuuu | -36 -13 78 -59 -15 | 25 28
gfz uuuuu | -12 88 -35 -144 -15 | 12 16
grg uuuux | 56 -52 60 -177 30 | 3 18
igr xxxxx | -7 73 8 13 -7 | 2 13
irf xxxxx | -3 27 -194 -71 -19 | 15 17
jpl uuuuu | -3 -45 134 220 -15 | 20 24
mit uuuuu | -8 23 -352 -43 -14 | 31 32
ngs uuuuu | 16 -15 35 132 16 | 5 11
sio uuuuu | 94 -82 12 -24 -21 | 42 43
Table 7.1602.5 GPS week: 1602 Day: 5 MJD: 55463.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -10 12 177 -85 -13 | 18 20
emr uuuuu | 43 83 64 348 -10 | 62 63
esa uuuuu | -40 -28 61 -137 -15 | 23 26
gfz uuuuu | -30 35 -12 -120 -6 | 10 15
grg uuuux | 49 4 -34 -34 27 | 6 22
igr xxxxx | -7 39 -21 113 -1 | 1 12
irf xxxxx | 5 8 -165 -96 -14 | 14 16
jpl uuuuu | -28 -24 39 261 2 | 17 20
mit uuuuu | 1 9 -316 -107 -10 | 31 32
ngs uuuuu | 19 23 84 108 12 | 5 13
sio uuuuu | 104 -111 34 6 -19 | 41 42
Table 7.1602.6 GPS week: 1602 Day: 6 MJD: 55464.500
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 | 5 -46 118 149 -3 | 14 21
emr uuuuu | 19 69 108 241 -5 | 59 61
esa uuuuu | -37 -42 77 82 -13 | 20 28
gfz uuuuu | 8 54 -60 -81 -3 | 8 17
grg uuuux | 33 3 -105 -95 -14 | 5 22
igr xxxxx | 12 31 65 15 4 | -2 16
irf xxxxx | 31 13 -159 -90 -14 | 10 19
jpl uuuuu | -11 -60 171 190 6 | 13 20
mit uuuuu | 28 17 -297 -118 -11 | 27 32
ngs uuuuu | -28 47 35 -120 7 | 3 14
sio uuuuu | 143 -110 31 -30 -20 | 37 41
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