[IGSREPORT-27334] Wk 2109 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 26 00:24:22 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2109 (Jun 07, 2020 - Jun 13, 2020)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.2109.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed
to the values of the final IGS (GPS) combination.
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.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl2109[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2109 in the SP3 format.
igl21097.sum Combination Report for GPS Week 2109.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -4.0 ns
1 | -1.5 ns
2 | -2.6 ns
3 | -0.3 ns
4 | -3.2 ns
5 | 1.1 ns
6 | -0.6 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
1 | BKG | R22
1 | COD | R22
1 | COF | R22
1 | EMX | R22
1 | ESX | R22
1 | GFZ | R22
1 | GRG | R22
1 | IAC | R22
1 | MCC | R22
3 | ESX | R20
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
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 (Tables 1.2109, 1a.2109).
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 2.2109.0-6)
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 3.2109.0-6).
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.
Table 1: Week 2109 summary. (Jun 07, 2020 - Jun 13, 2020)
Table 1.2109.a GPS week : 2109 MJD: 59007.0-59013.0
Mean and standard deviations of transformation parameters to the
combined IGL 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 n/a| 0 0 0 -10 -1 17 -.00 23 20 | 1133956 -1522 5201 149924
| 1 0 1 15 7 30 .04 | 2943965 2730
cof n/a| 0 0 -1 -13 20 26 -.03 25 21 | 1133947 -1526 5195 149924
| 1 0 1 30 14 18 .05 | 2943961 2719
emx n/a| -1 0 4 33 -17 -21 -.09 35 35 | -8792 -673 2937 8643
| 2 0 1 22 8 27 .02 | 10748 1680
esx n/a| 1 0 1 36 -2 -5 -.01 33 27 | -895 -147 2929 10461
| 1 0 1 13 17 30 .03 | 14444 2930
gfz n/a| 0 0 -1 -30 12 -12 .07 28 18 | 0 -1117 2957 7879
| 1 1 1 12 9 26 .05 | 0 2623
iac n/a| 0 0 -4 -16 13 31 -.05 27 27 | 388176 -679 2940 150012
| 1 1 1 20 19 80 .05 | 1025120 1923
Table 1.2109.b GPS week : 2109 MJD: 59007.0-59013.0
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
------+------------------------------------+------------------------------------------
R01 | 14 16 20 14 12 22 19 |
R02 | 8 6 8 5 8 7 6 |
R03 | 9 5 6 6 7 6 9 |
R04 | 9 8 14 8 10 16 15 |
R05 | 8 8 11 10 8 8 11 |
R07 | 6 9 5 8 8 7 7 |
R08 | 9 6 7 6 7 14 6 |
R09 | 10 8 8 8 9 9 8 |
R11 | 8 8 7 7 7 7 7 |
R12 | 9 9 9 7 10 11 12 |
R13 | 18 17 20 20 18 21 24 |
R14 | 8 9 9 8 9 10 10 |
R15 | 11 10 9 10 8 10 9 |
R16 | 11 10 12 13 17 12 18 |
R17 | 12 13 11 10 13 11 14 |
R18 | 7 8 9 7 7 9 15 |
R19 | 26 27 28 29 32 38 37 |
R20 | 32 36 40 19 42 43 47 |
R21 | 13 15 13 11 11 14 13 |
R22 | 20 --- 0 0 0 --- --- |
R23 | 12 9 10 12 10 15 15 |
R24 | 16 14 16 16 17 19 15 |
R26 | 17 17 16 30 30 0 0 |
Table 1.2109.c GPS week : 2109 MJD: 59007.0-59013.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 2109 0 | -54 13 241 -1756 -241 6109 82.5 1811 1811 | -4004 0
brd 2109 1 | 46 -62 179 185 2086 3912 82.4 1652 1652 | -1457 0
brd 2109 2 | 48 68 219 356 2245 1995 82.2 1518 1518 | -2637 0
brd 2109 3 | 54 28 312 772 -281 162 82.5 1413 1413 | -303 0
brd 2109 4 | 19 55 318 607 1097 429 83.3 1716 1716 | -3185 0
brd 2109 5 | 2 80 257 -681 -1324 3372 82.7 1778 1778 | 1060 0
brd 2109 6 | 0 -33 280 -442 41 4260 84.0 1686 1686 | -580 0
-------------+------------------------------------------------------------+----------------
brd 2109 mean| 16 21 258 -136 517 2891 82.8 1653 1653 | -1586 0
brd 2109 sdev| 38 53 49 888 1329 2152 .6 142 142 | 1788 0
Table 2: Daily transformation of each centre to the combined IGL 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 2.2109.0 GPS week: 2109 Day: 0 MJD: 59007
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 n/a| 0 0 0 1 -4 13 -.02 21 17 | 7810242 -4375 18985 999999
cof n/a| 0 1 -1 19 24 26 -.06 24 18 | 7810223 -4358 18984 999999
emx n/a| 0 0 6 45 -9 -4 -.07 32 32 | -18925 -2242 3144 10013
esx n/a| 0 0 5 23 17 -5 .00 37 31 | 6876 -2789 3140 12104
gfz n/a| 1 3 -1 -16 27 -7 .11 28 24 | 0 -3814 3165 9392
iac n/a| -2 -1 -6 -26 -19 5 .01 22 22 | 2712931 -2690 3162 999999
Table 2.2109.1 GPS week: 2109 Day: 1 MJD: 59008
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 n/a| 0 0 -2 -8 9 -22 -.02 21 17 | 23026 -307 2807 9288
cof n/a| 0 -1 0 3 22 -2 -.03 22 19 | 23011 -299 2810 9289
emx n/a| -1 0 2 17 -21 3 -.06 35 36 | 315 -369 2800 9432
esx n/a| 0 0 1 26 -33 -45 -.01 37 26 | -16983 1344 2793 10848
gfz n/a| -1 1 -2 -19 19 -22 -.02 25 15 | 0 -191 2849 8589
iac n/a| 1 0 -2 -12 8 95 .00 24 24 | -283 227 2812 9493
Table 2.2109.2 GPS week: 2109 Day: 2 MJD: 59009
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 n/a| 0 0 0 10 -7 22 -.01 25 23 | 21570 -2687 2686 7371
cof n/a| 0 1 1 27 8 31 -.11 27 23 | 21568 -2714 2671 7366
emx n/a| 0 0 2 49 -3 11 -.11 41 42 | -19541 -1770 2681 7477
esx n/a| 2 1 1 38 0 1 -.01 36 27 | -4647 -2297 2674 9781
gfz n/a| 1 -1 0 -29 -1 -62 .11 25 17 | 0 -3221 2686 6732
iac n/a| -1 0 -5 -25 28 56 -.07 26 26 | -174 -1532 2688 7478
Table 2.2109.3 GPS week: 2109 Day: 3 MJD: 59010
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 n/a| -2 1 0 -6 -11 24 -.03 18 16 | 21154 1051 2995 9011
cof n/a| -2 0 -2 -20 0 8 .05 21 17 | 21156 1043 2987 9015
emx n/a| -6 -1 3 39 -23 -62 -.12 25 25 | -1580 1395 3049 9560
esx n/a| 2 0 0 41 -3 -14 .01 23 21 | -134 3151 2989 11168
gfz n/a| 2 -1 1 -43 11 -5 .11 20 14 | 0 1435 2989 8667
iac n/a| 0 0 -5 -16 19 23 -.09 21 21 | 1099 1087 2998 9147
Table 2.2109.4 GPS week: 2109 Day: 4 MJD: 59011
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 n/a| 0 0 0 -17 4 18 -.01 20 15 | 21177 -5612 3152 8068
cof n/a| 2 0 0 -35 43 50 -.00 25 19 | 21159 -5596 3143 8067
emx n/a| -2 0 6 2 -22 -22 -.07 45 45 | -17233 -2870 3133 8144
esx n/a| 2 0 2 42 -19 26 -.05 40 29 | 14795 -4250 3143 9765
gfz n/a| 1 0 -2 -25 10 -16 .11 30 19 | 0 -4303 3196 7664
iac n/a| -2 0 -4 27 -1 -41 -.00 26 26 | 291 -2507 3151 8220
Table 2.2109.5 GPS week: 2109 Day: 5 MJD: 59012
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 n/a| 0 0 -2 -16 4 -8 .08 26 22 | 19791 1377 2993 8133
cof n/a| 0 0 -4 -37 16 26 -.03 27 22 | 19791 1348 2990 8134
emx n/a| 0 0 4 15 -22 -21 -.11 33 33 | 7307 1275 2977 8240
esx n/a| 0 1 2 59 8 36 -.00 31 29 | -21284 2788 2988 9690
gfz n/a| 1 0 -2 -30 8 0 .03 32 15 | 0 2118 3019 7315
iac n/a| 0 -3 -5 -34 35 -78 -.09 37 37 | 1044 2344 2986 8150
Table 2.2109.6 GPS week: 2109 Day: 6 MJD: 59013
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 n/a| 0 0 0 -37 -5 74 .01 29 28 | 20732 -101 2792 7599
cof n/a| 2 0 0 -49 31 44 -.02 30 28 | 20722 -108 2786 7599
emx n/a| -1 -2 4 65 -21 -50 -.11 30 30 | -11891 -135 2775 7637
esx n/a| 0 0 0 22 9 -35 .03 29 29 | 15108 1024 2782 9877
gfz n/a| 0 0 -3 -50 10 23 .03 39 23 | 0 156 2800 6797
iac n/a| 0 1 -3 -24 26 158 -.12 35 35 | 2328 -1684 2783 7602
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 IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL 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 IGL 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 3.2109.0 GPS week: 2109 Day: 0 MJD: 59007
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac IGL | cod cof emx esx gfz iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1059 28 22 20 43 31 17 14 | 79 80 78 56 67 70 68
R02 | 2199 10 11 19 11 16 19 7 | 49 48 48 55 55 55 51
R03 | 2060 16 15 10 25 22 17 9 | 52 58 53 73 71 57 58
XR04 | 1042 13 15 19 22 --- 10 9 | 64 63 61 51 --- 55 57
R05 | 824 15 20 14 19 20 11 8 | 44 38 50 48 50 48 45
R07 | 1948 8 12 12 12 11 12 5 | 66 63 63 69 70 73 68
R08 | 711 14 15 14 24 22 15 9 | 57 57 59 76 70 62 63
R09E | 5733 15 13 21 17 20 22 9 | 62 66 66 69 67 67 65
R11E | 662 11 19 15 12 19 20 8 | 44 48 51 49 49 53 46
R12E | 1167 10 12 27 17 20 15 9 | 40 43 37 45 52 35 39
R13E | 1615 19 30 43 29 46 40 18 | 44 50 50 45 62 50 41
R14E | 786 12 11 18 17 15 17 8 | 45 47 45 50 45 44 44
R15E | 781 10 13 28 26 27 12 10 | 33 34 34 43 47 35 34
R16E | 970 12 16 15 29 29 21 10 | 46 50 49 56 64 46 48
R17 | 1456 18 17 32 32 14 18 11 | 63 63 30 32 60 69 52
R18 | 918 11 11 18 22 10 10 7 | 48 47 30 46 47 51 43
R19 | 1800 52 67 60 72 52 22 26 | 94 111 39 49 96 83 66
R20 | 1745 42 46 80 102 50 45 32 | 127 133 40 55 145 136 99
R21 | 721 13 13 33 35 17 31 13 | 83 84 57 57 83 93 74
XR22 | 4559 18 58 --- --- --- 21 19 | 18 68 --- --- --- 496 555
R23 | 703 22 19 15 38 25 18 12 | 38 47 34 65 34 43 39
R24 | 837 19 20 49 31 34 21 15 | 74 78 50 60 85 82 67
XR26 | ---- 16 42 --- --- --- 16 16 | 35 57 --- --- --- 48 40
------+-----------------------------------------+-------------------------------------
RMS | 1811 21 24 32 37 28 22 |T 56 62 48 54 65 80 76
WRMS | 1811 17 18 32 31 24 22 |NE 61 68 49 56 71 95 90
MEDI | 1042 15 16 19 25 20 18 |MD 49 57 50 55 62 55 52
Table 3.2109.1 GPS week: 2109 Day: 1 MJD: 59008
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac IGL | cod cof emx esx gfz iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1595 40 39 20 39 33 17 16 | 47 52 46 44 44 36 40
R02 | 735 8 12 11 11 10 19 6 | 38 39 39 39 40 46 39
R03 | 817 11 12 8 13 8 11 5 | 40 42 42 47 44 41 42
XR04 | 1016 8 15 15 12 --- 18 7 | 51 55 54 56 --- 43 50
R05 | 1090 17 14 16 17 12 15 7 | 35 35 42 46 41 40 37
R07 | 1071 12 8 19 21 13 22 8 | 47 53 48 63 60 63 55
R08 | 658 11 11 14 17 11 9 6 | 43 44 46 54 56 52 49
R09E | 5662 10 11 18 11 18 21 8 | 43 39 42 39 37 40 39
R11E | 1061 9 10 22 12 16 22 8 | 58 59 61 58 57 57 56
R12E | 1290 19 20 22 13 17 15 9 | 34 34 38 36 42 36 34
R13E | 1645 18 26 42 25 44 36 16 | 36 47 45 37 56 35 34
R14E | 1016 15 9 21 14 16 20 8 | 39 39 33 47 45 32 37
R15E | 915 12 10 27 21 25 15 10 | 23 27 27 35 32 29 26
R16E | 1877 17 24 21 16 22 21 9 | 43 46 42 38 46 41 39
R17 | 894 9 19 40 33 24 25 13 | 38 44 23 24 51 50 38
R18 | 601 9 15 26 14 12 12 7 | 29 33 21 34 28 31 27
R19 | 1073 54 40 63 71 45 24 26 | 42 43 36 46 50 39 36
R20 | 1008 37 41 93 114 57 58 36 | 61 60 45 36 71 78 51
R21 | 728 14 18 37 41 22 30 14 | 54 59 45 40 52 66 51
R23 | 808 16 22 14 35 12 10 9 | 25 23 28 40 28 31 27
R24 | 777 17 23 46 28 13 32 14 | 45 49 37 37 41 51 42
XR26 | ---- 15 67 --- --- --- 19 17 | 30 56 --- --- --- 23 20
------+-----------------------------------------+-------------------------------------
RMS | 1652 21 22 35 37 25 24 |T 40 47 40 42 46 59 39
WRMS | 1652 17 19 36 26 15 24 |NE 40 49 39 43 46 68 40
MEDI | 1016 14 15 21 17 16 19 |MD 40 44 42 40 44 41 39
Table 3.2109.2 GPS week: 2109 Day: 2 MJD: 59009
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac IGL | cod cof emx esx gfz iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1154 52 44 20 54 32 17 19 | 53 53 49 58 45 35 40
R02 | 674 17 16 14 15 18 11 7 | 37 41 45 48 58 41 45
R03 | 784 8 10 11 13 9 15 5 | 39 41 41 43 46 46 42
XR04 | 686 19 18 22 36 --- 13 13 | 50 50 50 35 --- 40 41
R05 | 886 27 20 19 22 23 17 11 | 33 40 55 67 63 43 49
R07 | 713 10 13 10 11 10 7 5 | 52 48 50 53 59 57 54
R08 | 783 8 11 11 14 9 19 6 | 52 49 48 53 49 51 50
R09E | 4838 13 16 19 8 17 19 8 | 46 47 49 49 53 50 49
R11E | 1057 11 10 19 11 11 16 6 | 55 56 56 50 49 57 52
R12E | 1204 14 13 29 13 10 20 8 | 37 40 43 48 52 34 41
R13E | 1596 40 48 45 29 46 33 19 | 43 53 45 58 81 46 49
R14E | 1853 15 13 22 14 19 18 9 | 45 44 39 37 45 38 39
R15E | 1247 15 13 27 15 21 12 9 | 35 33 37 42 52 38 39
R16E | 1325 16 32 31 15 29 20 11 | 49 65 32 48 65 62 51
R17 | 1274 9 11 26 27 9 34 11 | 45 44 34 29 37 62 41
R18 | 647 12 12 29 17 18 17 9 | 41 46 39 41 53 42 42
R19 | 644 52 55 87 70 33 37 28 | 68 80 49 46 66 62 50
R20 | 1070 53 50 117 106 61 66 40 | 91 100 97 71 110 111 80
R21 | 1351 11 10 33 33 22 26 12 | 64 61 51 51 71 74 62
XR22 |>>>>> --- --- --- --- --- 4 0 | --- --- --- --- --- 9999 9999
R23 | 721 16 21 27 28 13 16 10 | 36 33 43 45 38 41 38
R24 | 745 17 31 47 38 13 40 16 | 55 63 35 30 48 69 46
XR26 | ---- 14 67 --- --- --- 18 16 | 29 52 --- --- --- 41 35
------+-----------------------------------------+-------------------------------------
RMS | 1518 25 27 41 36 25 26 |T 47 51 47 47 57 51 47
WRMS | 1518 23 23 42 27 16 26 |NE 49 53 49 47 57 54 47
MEDI | 1057 15 16 26 17 18 18 |MD 45 48 45 48 52 46 45
Table 3.2109.3 GPS week: 2109 Day: 3 MJD: 59010
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac IGL | cod cof emx esx gfz iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1531 31 32 20 42 23 15 14 | 65 66 56 41 57 57 51
R02 | 754 10 11 10 10 8 10 5 | 41 35 38 44 47 36 40
R03 | 554 11 15 11 17 12 10 6 | 42 45 46 51 46 52 46
XR04 | 784 12 23 15 15 --- 11 7 | 49 55 40 35 --- 38 40
R05 | 549 23 25 17 18 16 19 9 | 35 34 48 52 54 46 44
R07 | 687 13 14 14 16 17 16 7 | 53 54 57 70 73 53 60
R08 | 1078 8 12 16 12 10 12 6 | 48 56 59 58 47 45 50
R09E | 3253 14 24 21 11 14 20 8 | 24 24 23 24 28 29 23
R11E | 631 8 10 25 6 12 15 6 | 65 64 68 67 65 69 66
R12E | 1131 11 16 25 11 9 16 7 | 36 39 35 34 37 36 34
R13E | 2953 32 42 39 34 52 36 19 | 40 48 38 44 73 30 40
R14E | 1460 12 12 20 18 13 16 8 | 30 32 27 36 32 31 28
R15E | 1256 13 14 27 22 17 22 10 | 28 30 28 45 38 32 31
R16E | 1146 21 30 31 16 32 20 12 | 42 49 33 52 63 57 48
R17 | 551 15 15 24 23 11 26 10 | 51 54 36 36 51 61 47
R18 | 685 9 9 14 12 15 19 7 | 34 35 32 40 29 42 32
XR19 | 1017 42 52 --- 82 32 28 28 | 79 91 --- 35 75 81 67
XR20 | 934 29 53 --- 185 25 26 19 | 127 149 --- 51 139 119 135
R21 | 1250 17 17 28 30 18 15 11 | 57 58 33 36 57 53 47
XR22 |>>>>> --- --- --- --- --- 3 0 | --- --- --- --- --- 333 455
R23 | 756 19 12 33 32 15 16 11 | 24 39 31 56 46 38 35
R24 | 1354 22 27 46 37 9 40 16 | 63 68 34 32 52 76 51
XR26 | ---- 26 46 --- --- --- 35 30 | 23 43 --- --- --- 48 30
------+-----------------------------------------+-------------------------------------
RMS | 1412 18 21 25 23 20 21 |T 48 53 40 44 55 63 65
WRMS | 1412 16 17 25 21 14 21 |NE 52 58 42 45 59 73 76
MEDI | 1017 14 16 21 18 15 16 |MD 42 48 36 44 51 48 46
Table 3.2109.4 GPS week: 2109 Day: 4 MJD: 59011
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac IGL | cod cof emx esx gfz iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1940 19 30 39 30 23 13 12 | 61 69 62 56 55 48 54
R02 | 1813 9 14 15 18 16 17 7 | 41 48 36 49 43 48 42
R03 | 696 11 11 12 17 9 20 7 | 42 39 37 45 46 47 42
XR04 | 791 14 22 17 20 --- 20 10 | 55 60 48 44 --- 43 46
R05 | 670 11 7 22 17 15 12 7 | 32 36 41 40 42 30 33
R07 | 572 7 11 10 20 19 16 7 | 49 49 57 63 45 47 50
R08 | 842 8 15 16 20 10 15 7 | 52 46 51 58 59 61 55
R09E | 4383 11 18 20 15 22 16 8 | 40 43 36 38 49 42 39
R11E | 677 9 13 16 7 19 14 6 | 57 55 51 54 51 56 54
R12E | 791 12 16 32 17 20 19 9 | 33 35 32 34 43 35 32
R13E | 3577 24 32 46 32 52 32 18 | 35 51 40 47 67 32 37
R14E | 1118 14 16 25 20 18 16 9 | 41 39 31 43 44 37 37
R15E | 1191 9 11 23 18 20 14 8 | 34 35 31 46 44 38 36
R16E | 2449 27 23 32 24 55 22 16 | 27 34 32 41 64 37 33
R17 | 495 13 13 35 36 24 21 12 | 50 50 32 31 60 54 47
R18 | 1178 8 12 20 9 13 17 6 | 31 31 28 32 30 34 29
R19 | 1013 56 57 112 71 35 48 32 | 75 75 64 41 75 91 64
R20 | 1049 36 51 118 133 75 66 42 | 108 117 59 45 135 119 90
R21 | 1390 18 23 32 26 22 14 11 | 55 55 41 42 57 54 49
XR22 | 4755 --- --- --- --- --- 4 0 | --- --- --- --- --- 494 553
R23 | 656 13 17 23 35 11 14 10 | 31 32 25 59 39 45 37
R24 | 1400 18 28 56 39 24 32 16 | 61 67 27 44 67 61 53
XR26 | ---- 25 55 --- --- --- 36 30 | 33 77 --- --- --- 66 46
------+-----------------------------------------+-------------------------------------
RMS | 1715 20 25 45 40 30 26 |T 47 51 41 45 55 70 67
WRMS | 1715 15 19 45 29 19 26 |NE 51 56 43 46 57 83 80
MEDI | 1049 13 16 23 20 20 17 |MD 41 48 37 44 49 47 46
Table 3.2109.5 GPS week: 2109 Day: 5 MJD: 59012
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac IGL | cod cof emx esx gfz iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1886 34 26 36 49 33 25 22 | 59 58 54 38 58 42 48
R02 | 514 10 6 11 12 14 28 6 | 38 42 46 43 51 48 42
R03 | 539 7 7 9 13 8 17 5 | 41 44 41 53 44 44 43
XR04 | 887 13 13 24 29 --- 17 16 | 39 37 45 35 --- 42 36
R05 | 616 16 13 12 12 12 26 8 | 33 32 33 36 37 34 32
R07 | 592 8 13 12 15 7 19 6 | 50 50 49 56 53 53 51
R08 | 1287 19 18 24 32 17 23 13 | 46 58 46 75 69 51 57
R09E | 4442 14 13 16 13 17 28 9 | 59 62 60 68 66 57 62
R11E | 517 7 11 17 10 14 18 7 | 43 43 46 42 48 51 44
R12E | 821 17 18 27 10 19 27 11 | 43 46 41 44 41 36 41
R13E | 3192 27 31 38 34 48 51 21 | 29 37 30 49 62 34 34
R14E | 1161 15 13 21 15 13 19 9 | 52 55 52 57 62 49 52
R15E | 2125 13 11 22 18 13 19 9 | 46 47 42 56 52 45 47
R16E | 2831 19 18 16 22 26 26 12 | 57 57 55 56 63 48 56
R17 | 773 17 21 23 19 19 23 11 | 46 48 40 45 44 43 40
R18 | 1143 11 12 20 10 17 28 8 | 37 40 44 41 38 43 37
R19 | 1520 71 71 82 52 51 74 38 | 65 74 57 41 65 84 48
R20 | 1916 57 61 73 81 89 93 43 | 77 80 38 43 100 92 51
R21 | 763 18 23 23 27 28 24 14 | 58 60 53 57 65 60 55
R23 | 733 14 15 12 34 33 25 14 | 35 35 46 47 31 39 36
R24 | 1721 21 27 42 26 42 39 19 | 56 55 45 47 71 52 50
XR26 | ---- 2 57 --- --- --- 38 0 | 40 58 --- --- --- 36 43
------+-----------------------------------------+-------------------------------------
RMS | 1778 26 27 33 31 32 37 |T 47 50 45 49 56 63 45
WRMS | 1778 22 22 33 29 15 37 |NE 48 51 45 46 55 71 44
MEDI | 1143 15 15 22 19 17 25 |MD 46 48 46 47 53 48 44
Table 3.2109.6 GPS week: 2109 Day: 6 MJD: 59013
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac IGL | cod cof emx esx gfz iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 978 35 38 19 35 38 21 19 | 79 83 65 39 67 58 58
R02 | 865 10 11 7 11 14 11 6 | 52 50 58 53 59 55 55
R03 | 636 15 16 13 15 20 15 9 | 59 58 59 66 73 63 63
XR04 | 471 13 17 21 26 --- 17 15 | 59 60 60 40 --- 48 51
R05 | 610 18 17 17 21 21 20 11 | 46 43 49 49 46 42 43
R07 | 541 9 12 16 11 14 22 7 | 67 68 65 68 66 71 65
R08 | 945 9 10 8 12 9 19 5 | 70 72 69 81 74 79 73
R09E | 4651 8 13 18 9 19 20 8 | 52 53 52 55 57 60 53
R11E | 1432 9 8 18 8 13 12 7 | 67 68 73 69 70 67 69
R12E | 828 15 20 23 13 28 16 11 | 41 40 44 43 56 46 43
R13E | 1575 40 41 29 30 63 62 23 | 61 64 54 72 89 62 57
R14E | 791 15 13 22 17 11 19 10 | 46 46 38 51 49 44 44
R15E | 2032 14 13 21 13 15 24 9 | 37 38 32 43 49 39 38
R16E | 2450 25 20 25 16 54 35 18 | 44 55 45 47 80 51 49
R17 | 1092 23 27 26 23 27 25 14 | 72 74 52 44 73 73 61
R18 | 858 14 11 23 17 44 25 14 | 50 53 42 48 72 57 49
R19 | 1263 69 65 77 45 62 52 37 | 101 105 39 35 102 96 64
R20 | 3006 72 78 66 89 99 94 47 | 136 142 44 31 158 148 96
R21 | 819 18 23 19 23 28 42 12 | 74 78 56 59 82 87 67
R23 | 702 17 20 19 29 34 28 14 | 36 40 52 70 32 48 46
R24 | 1356 25 24 32 21 21 31 14 | 81 84 44 57 82 86 66
XR26 | ---- 4 44 --- --- --- 32 0 | 52 64 --- --- --- 51 53
------+-----------------------------------------+-------------------------------------
RMS | 1686 29 30 30 29 39 35 |T 62 65 52 53 71 80 57
WRMS | 1686 28 28 30 29 23 35 |NE 68 71 53 52 75 93 60
MEDI | 945 15 17 21 17 21 22 |MD 59 60 52 51 70 60 55
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