[IGSREPORT-27281] Wk 2105 IGLOS Final Orbits
acc
acc at igs.org
Thu May 28 23:36:27 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2105 (May 10, 2020 - May 16, 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 2.2105.
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:
igl2105[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2105 in the SP3 format.
igl21057.sum Combination Report for GPS Week 2105.
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 | 0.5 ns
1 | -1.2 ns
2 | -0.5 ns
3 | -0.9 ns
4 | -0.0 ns
5 | -1.0 ns
6 | -1.2 ns
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 1.2105, 1a.2105).
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 2.2105.0-6)
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 3.2105.0-6).
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 2105 summary. (May 10, 2020 - May 16, 2020)
Table 1.2105.a GPS week : 2105 MJD: 58979.0-58985.0
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 -2 21 -14 54 .14 20 15 | 19788 395 2902 8082
| 0 0 1 18 14 20 .04 | 696 1131
cof n/a| 0 -1 -3 16 10 57 .08 23 18 | 19782 390 2906 8090
| 1 1 2 25 22 30 .09 | 700 1127
emx n/a| 0 0 4 30 14 25 -.01 32 31 | -5658 531 2914 8311
| 1 1 3 21 32 25 .05 | 11082 645
esx n/a| 1 0 0 1 14 -48 .09 28 21 | -1751 1164 2905 10070
| 0 1 1 24 17 44 .10 | 10672 1423
gfz n/a| 0 0 0 -2 27 -23 .15 28 17 | 0 156 2928 7615
| 0 1 2 15 12 33 .07 | 0 1189
grg n/a| 0 0 0 -53 -12 -32 -.27 22 19 | -760 396 2897 7052
| 0 1 4 14 33 60 .07 | 388 1085
iac n/a| 0 0 0 10 -18 16 -.04 19 19 | 1122 -38 2900 8234
| 1 1 1 22 32 45 .07 | 996 609
Table 1.2105.b GPS week : 2105 MJD: 58979.0-58985.0
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 | 12 12 13 16 16 17 16 |
R02 | 6 5 6 7 6 7 6 |
R03 | 6 6 8 6 6 6 6 |
R04 | 13 9 8 9 7 8 9 |
R05 | 9 9 9 10 7 8 8 |
R07 | 6 6 7 7 6 7 5 |
R08 | 7 6 7 8 6 9 6 |
R09 | 8 8 10 7 7 8 8 |
R11 | 6 7 7 6 6 8 7 |
R12 | 9 9 8 9 9 10 10 |
R13 | 22 21 18 20 17 16 16 |
R14 | 8 8 8 6 6 6 7 |
R15 | 8 9 8 9 7 9 7 |
R16 | 15 11 12 13 13 11 13 |
R17 | 7 7 8 7 8 8 8 |
R18 | 6 6 6 7 6 7 8 |
R19 | 16 19 20 19 17 17 21 |
R20 | 23 23 20 22 22 24 21 |
R21 | 7 9 9 9 8 8 8 |
R22 | 9 9 8 8 8 9 9 |
R23 | 9 10 9 12 10 9 9 |
R24 | 7 9 9 7 9 8 8 |
R26 | 21 16 17 14 13 19 27 |
Table 1.2105.c GPS week : 2105 MJD: 58979.0-58985.0
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 2105 0 | -80 10 227 -1097 -1215 -817 82.1 1553 1553 | 501 0
brd 2105 1 | 58 116 190 -1033 1900 672 82.8 1614 1614 | -1250 0
brd 2105 2 | -19 49 230 -1048 2775 609 81.8 1648 1648 | -548 0
brd 2105 3 | 3 41 184 -623 -399 -998 81.9 1518 1518 | -907 0
brd 2105 4 | -56 8 254 0 148 330 83.4 1532 1532 | -46 0
brd 2105 5 | 19 13 270 1687 1100 185 82.0 1521 1521 | -978 0
brd 2105 6 | 33 33 276 -226 -417 279 82.3 1521 1521 | -1246 0
-------------+------------------------------------------------------------+----------------
brd 2105 mean| -6 39 233 -334 555 37 82.3 1558 1558 | -639 0
brd 2105 sdev| 49 37 36 989 1425 670 .6 52 52 | 656 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 2.2105.0 GPS week: 2105 Day: 0 MJD: 58979
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 3 -20 57 .10 18 13 | 20722 2051 2872 8258
cof n/a| 0 -3 -2 3 39 -3 .21 23 16 | 20713 2068 2879 8264
emx n/a| 0 -2 1 55 66 16 -.01 33 29 | 709 1447 2880 8531
esx n/a| 2 -1 0 -30 22 -138 .18 29 21 | -2605 2520 2876 10009
gfz n/a| 0 -1 -5 -6 31 -88 .18 28 19 | 0 1850 2921 8098
grg n/a| 0 1 0 -37 -1 -21 -.31 22 19 | -329 1867 2875 7439
iac n/a| 0 1 3 40 -81 77 -.08 21 21 | 2840 -565 2872 8376
Table 2.2105.1 GPS week: 2105 Day: 1 MJD: 58980
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 -1 -4 12 -10 24 .12 19 15 | 19509 -1175 2936 7643
cof n/a| 0 -1 -8 1 -11 87 .18 23 19 | 19507 -1172 2944 7654
emx n/a| 2 0 2 41 -32 31 -.05 36 33 | -7415 -64 2952 7979
esx n/a| 1 -1 -3 0 13 -53 .20 28 23 | 7156 258 2946 9961
gfz n/a| 0 -2 0 -25 44 -28 .19 32 20 | 0 -1276 2966 7273
grg n/a| 0 0 6 -54 -22 84 -.29 19 17 | -686 -1030 2936 6713
iac n/a| -3 1 -1 13 -6 -46 -.02 19 19 | -495 776 2935 7853
Table 2.2105.2 GPS week: 2105 Day: 2 MJD: 58981
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 -1 0 -27 88 .09 19 17 | 19255 1009 2798 7270
cof n/a| 0 -1 -1 -2 -17 76 .01 22 19 | 19264 976 2805 7271
emx n/a| 0 0 2 36 -7 76 -.10 34 34 | 3228 788 2810 7408
esx n/a| 1 0 0 -20 -8 -40 .11 25 21 | 5811 1332 2796 9282
gfz n/a| 0 1 -3 -19 20 -4 .14 26 17 | 0 563 2804 6627
grg n/a| -1 0 -1 -36 40 -84 -.33 23 22 | -755 617 2789 6425
iac n/a| 0 -1 0 28 -3 -25 -.02 20 20 | 1322 291 2797 7370
Table 2.2105.3 GPS week: 2105 Day: 3 MJD: 58982
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 13 -12 60 .10 19 14 | 19013 -812 2866 7884
cof n/a| 0 -1 -1 62 39 51 -.05 22 16 | 18987 -794 2867 7890
emx n/a| -2 0 4 37 8 -4 -.03 30 30 | 11514 -430 2880 8153
esx n/a| 0 0 0 4 2 -31 .15 28 22 | -7186 -1401 2870 9925
gfz n/a| 1 1 1 17 22 -41 .24 27 15 | 0 -1389 2885 7362
grg n/a| 0 1 -7 -62 -13 -77 -.29 27 21 | -379 -830 2863 6713
iac n/a| 0 0 3 -23 -8 55 -.16 20 20 | 751 -205 2874 8094
Table 2.2105.4 GPS week: 2105 Day: 4 MJD: 58983
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 1 -1 48 -31 56 .16 19 13 | 19238 1176 2823 7699
cof n/a| 0 -1 -2 6 0 50 .06 23 17 | 19228 1157 2825 7705
emx n/a| 0 0 5 27 9 9 .06 30 30 | -14143 1069 2836 7895
esx n/a| 0 0 0 -11 1 -56 .08 29 18 | 12519 2731 2827 9815
gfz n/a| 0 0 0 0 13 -4 .16 27 18 | 0 1120 2844 7013
grg n/a| 0 0 0 -78 -14 -50 -.31 21 16 | -626 1537 2831 6553
iac n/a| 0 0 0 13 24 42 -.04 17 17 | 1269 604 2821 7899
Table 2.2105.5 GPS week: 2105 Day: 5 MJD: 58984
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 -4 31 -11 55 .20 23 18 | 20235 269 3085 9340
cof n/a| -2 0 -6 40 13 56 .01 24 18 | 20228 260 3086 9356
emx n/a| -1 2 5 29 45 25 .02 31 31 | -15925 541 3104 9590
esx n/a| 2 0 0 33 37 6 -.05 30 23 | -11319 933 3095 11247
gfz n/a| 1 0 0 13 42 11 .04 26 16 | 0 -98 3102 9048
grg n/a| -2 -1 0 -55 -73 -79 -.20 20 19 | -1166 361 3070 8284
iac n/a| 0 1 0 -12 -21 20 .06 18 18 | 1396 -849 3076 9496
Table 2.2105.6 GPS week: 2105 Day: 6 MJD: 58985
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 41 12 36 .18 21 16 | 20545 253 2936 8483
cof n/a| 0 0 -4 1 10 80 .10 24 19 | 20552 235 2939 8493
emx n/a| -3 3 11 -14 12 22 .02 31 31 | -17575 368 2942 8621
esx n/a| 1 -2 0 32 36 -25 -.04 29 17 | -16633 1777 2928 10254
gfz n/a| 1 0 2 3 15 -12 .07 29 18 | 0 325 2976 7888
grg n/a| 0 0 -5 -50 -4 -1 -.15 20 18 | -1380 256 2921 7242
iac n/a| -1 0 0 13 -33 -5 -.02 17 17 | 772 -324 2928 8551
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 3.2105.0 GPS week: 2105 Day: 0 MJD: 58979
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1331 17 24 38 34 32 25 14 12 | 67 68 79 56 47 64 60 58
R02 | 1576 10 10 15 18 11 11 12 5 | 46 48 44 56 55 51 50 49
R03 | 588 8 9 12 14 11 19 16 6 | 56 57 61 65 63 65 56 60
XR04 | 734 15 21 28 38 --- 26 25 13 | 65 65 69 58 --- 74 59 63
R05 | 604 13 19 18 29 26 11 14 8 | 45 54 52 53 60 43 40 45
R07 | 895 8 11 14 15 16 14 12 5 | 54 55 54 60 58 61 61 57
R08 | 1415 9 11 14 18 10 17 18 6 | 49 51 53 59 53 51 60 52
R09 | 4204 13 11 12 12 13 27 22 8 | 81 83 88 87 87 85 88 85
R11 | 890 10 18 18 9 14 17 7 5 | 71 75 57 69 67 62 70 66
R12 | 1603 25 19 35 21 11 13 11 9 | 79 74 56 51 63 57 67 62
R13 | 824 24 28 70 75 35 50 41 22 | 100 104 58 49 96 93 99 79
R14 | 1012 11 19 29 17 13 14 14 7 | 83 83 64 70 72 73 82 74
R15 | 1879 17 18 23 19 18 15 17 8 | 72 71 47 49 70 54 68 60
R16 | 1774 33 30 31 43 40 34 20 15 | 69 69 58 76 64 73 78 67
R17E | 681 10 11 23 16 19 10 12 6 | 107 109 108 110 109 106 111 107
R18E | 711 9 12 18 12 14 14 12 5 | 29 30 31 33 29 27 29 27
R19E | 1256 27 38 54 39 44 30 25 16 | 33 40 38 45 66 34 37 30
R20E | 1270 31 63 75 50 74 32 48 23 | 111 108 104 114 112 121 112 106
R21E | 631 9 14 23 14 19 11 12 6 | 42 41 41 40 46 37 40 39
R22E | 2518 13 16 24 16 23 18 29 9 | 90 92 82 88 90 90 88 87
R23E | 1216 21 22 14 23 27 18 19 9 | 128 133 132 128 129 132 123 127
R24E | 1014 13 20 22 16 21 7 18 7 | 30 35 28 30 31 20 29 25
XR26E | ---- 22 36 --- --- --- --- 19 21 | 66 65 --- --- --- --- 85 72
------+----------------------------------------------+------------------------------------------
RMS | 1552 18 23 33 29 28 22 21 |T 68 70 63 65 69 66 69 65
WRMS | 1552 13 16 29 21 19 19 21 |NE 66 68 60 61 65 64 67 62
MEDI | 1014 13 19 23 18 19 17 17 |MD 67 68 57 58 64 62 67 62
Table 3.2105.1 GPS week: 2105 Day: 1 MJD: 58980
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 991 18 15 47 30 38 18 15 12 | 41 36 47 34 48 50 42 37
R02 | 1162 9 13 13 10 10 10 10 4 | 29 36 30 34 40 38 34 33
R03 | 602 7 13 15 9 13 17 10 5 | 33 37 36 39 33 43 30 35
XR04 | 859 18 15 20 25 --- 12 11 8 | 49 48 47 41 --- 51 51 47
R05 | 773 20 20 22 20 34 11 17 9 | 35 46 32 46 63 31 31 35
R07 | 1000 11 18 16 12 12 15 11 6 | 37 36 34 39 47 51 45 42
R08 | 1416 7 10 7 13 15 8 18 5 | 33 30 30 33 37 35 39 32
R09 | 4058 19 27 19 8 22 20 19 8 | 78 84 94 80 88 86 76 81
R11 | 990 13 14 18 14 26 11 11 6 | 50 51 42 41 32 47 48 42
R12 | 1421 18 19 29 22 29 13 18 9 | 59 62 35 44 67 48 50 48
R13 | 1767 21 42 66 72 46 38 32 20 | 67 78 39 34 83 65 80 58
R14 | 636 19 22 29 20 9 19 8 8 | 91 96 80 85 85 96 89 87
R15 | 2659 21 28 28 18 14 17 24 9 | 56 58 39 39 50 44 61 47
R16 | 1213 14 20 41 24 29 24 20 11 | 55 67 53 71 65 60 66 60
R17E | 825 10 15 24 24 18 12 10 7 | 122 123 121 130 133 112 124 123
R18E | 1460 9 13 19 16 20 11 10 6 | 31 29 32 35 26 25 34 28
R19E | 2046 37 35 66 41 66 27 21 18 | 32 31 50 45 74 43 29 32
R20E | 1581 40 40 79 53 73 26 47 22 | 111 122 141 134 144 111 120 119
R21E | 651 13 16 30 15 38 16 10 9 | 39 41 36 36 57 37 45 39
R22E | 2231 18 12 29 21 16 17 13 8 | 75 84 76 84 80 90 75 78
R23E | 1256 28 34 20 22 29 19 17 10 | 122 120 116 121 115 105 118 115
R24E | 592 13 19 41 22 16 14 19 9 | 24 22 36 37 30 21 24 24
XR26E | ---- 17 26 --- --- --- --- 14 15 | 45 58 --- --- --- --- 57 52
------+----------------------------------------------+------------------------------------------
RMS | 1613 19 23 36 28 32 19 19 |T 57 60 56 58 66 58 59 56
WRMS | 1613 15 19 33 23 20 17 19 |NE 50 54 45 47 56 53 53 48
MEDI | 1162 18 19 24 20 22 16 15 |MD 49 51 39 41 63 48 50 47
Table 3.2105.2 GPS week: 2105 Day: 2 MJD: 58981
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 571 26 21 39 22 27 36 23 12 | 55 49 56 43 42 26 49 42
R02 | 1333 15 15 7 13 13 18 12 6 | 42 40 37 44 36 38 35 38
R03 | 508 9 11 10 12 10 26 22 7 | 41 48 40 49 48 56 35 43
XR04 | 1137 11 12 16 10 --- 16 20 7 | 47 48 49 60 --- 45 42 46
R05 | 1107 20 14 20 19 24 15 12 8 | 33 30 39 43 43 33 38 34
R07 | 1368 13 18 11 11 14 21 19 7 | 38 42 39 41 48 44 54 42
R08 | 1038 14 13 16 16 19 12 15 7 | 39 41 37 37 37 40 36 35
R09 | 3860 25 27 20 13 14 32 16 9 | 93 93 101 104 105 106 104 100
R11 | 1041 11 11 24 9 9 16 20 7 | 93 99 87 96 94 105 101 96
R12 | 1010 15 18 30 12 16 18 17 8 | 57 58 40 42 54 47 43 46
R13 | 1458 26 46 56 59 33 41 16 17 | 80 97 39 37 84 88 64 63
R14 | 1142 19 30 20 20 11 17 14 7 | 70 81 59 82 72 61 62 67
R15 | 2317 15 20 27 23 10 16 19 8 | 52 58 33 35 47 48 59 46
R16 | 2508 16 18 36 17 34 33 22 11 | 66 72 58 77 75 76 83 70
R17E | 1963 11 12 21 18 17 25 14 8 | 68 63 63 55 59 84 65 64
R18E | 1214 9 12 15 12 10 15 11 5 | 23 23 19 25 26 29 27 22
R19E | 2140 30 35 68 42 65 22 40 20 | 32 41 39 30 85 36 40 31
R20E | 1432 30 40 68 54 48 31 35 19 | 82 81 84 76 95 90 80 78
R21E | 827 19 21 28 19 19 20 18 9 | 37 39 37 35 34 39 38 33
R22E | 1762 10 14 28 12 29 19 6 8 | 55 46 53 47 59 49 50 50
R23E | 1424 22 16 28 25 12 16 17 9 | 71 70 72 68 64 64 65 66
R24E | 755 12 13 38 12 25 16 19 9 | 21 24 23 18 35 19 31 20
XR26E | ---- 15 26 --- --- --- --- 18 16 | 40 39 --- --- --- --- 37 36
------+----------------------------------------------+------------------------------------------
RMS | 1647 19 22 34 25 26 23 20 |T 53 55 50 52 59 55 53 50
WRMS | 1647 17 19 34 21 17 22 20 |NE 57 61 51 56 60 58 57 54
MEDI | 1214 15 18 24 16 17 18 18 |MD 52 48 40 43 54 47 49 46
Table 3.2105.3 GPS week: 2105 Day: 3 MJD: 58982
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 802 30 43 37 25 35 58 21 15 | 64 77 61 54 59 38 53 48
R02 | 1517 11 15 12 12 20 9 19 6 | 45 49 41 47 53 42 45 44
R03 | 673 7 12 10 9 8 16 20 5 | 50 48 50 55 53 53 52 51
XR04 | 1725 7 12 28 20 --- 18 18 9 | 51 54 63 45 --- 51 43 49
R05 | 1270 12 14 23 26 28 30 13 10 | 38 39 51 42 43 51 45 40
R07 | 1061 12 15 17 10 18 19 18 7 | 53 47 43 42 47 46 53 46
R08 | 1059 13 16 16 16 16 18 19 7 | 44 41 46 42 52 45 42 43
R09 | 3552 11 14 27 17 17 15 12 7 | 46 46 35 39 48 43 46 42
R11 | 1133 9 16 24 14 15 8 13 6 | 91 91 88 94 92 91 98 92
R12 | 1210 13 20 26 18 18 12 25 8 | 65 72 49 55 53 62 65 57
R13 | 962 36 31 53 64 36 47 23 19 | 101 97 60 53 98 111 77 80
R14 | 1180 15 14 20 11 10 13 10 6 | 105 107 98 106 102 107 100 103
R15 | 783 15 9 24 22 18 14 21 8 | 60 54 40 47 57 62 48 52
R16 | 2841 15 18 28 20 42 45 17 12 | 81 80 70 77 88 82 74 77
R17E | 2363 16 15 20 16 11 14 10 6 | 157 154 153 167 160 165 164 161
R18E | 1133 12 13 25 15 15 14 16 7 | 24 26 24 30 34 28 36 27
R19E | 1237 25 32 42 52 54 47 34 19 | 29 38 32 34 54 59 40 30
R20E | 978 37 39 63 68 55 35 32 21 | 144 148 156 160 146 153 152 147
R21E | 612 12 13 32 17 18 17 20 8 | 36 37 36 36 39 34 37 33
R22E | 1395 13 15 30 14 16 17 13 7 | 62 64 70 67 69 66 68 65
R23E | 1671 28 35 21 24 21 25 32 11 | 94 97 97 104 97 93 103 96
R24E | 534 13 16 22 14 16 16 14 7 | 23 25 29 28 33 22 29 23
XR26E | ---- 12 30 --- --- --- --- 16 14 | 30 45 --- --- --- --- 35 30
------+----------------------------------------------+------------------------------------------
RMS | 1518 19 22 30 28 27 27 20 |T 64 66 63 64 70 68 65 62
WRMS | 1518 14 16 30 22 15 21 20 |NE 63 64 56 57 65 63 60 58
MEDI | 1133 13 15 24 17 18 17 18 |MD 53 54 50 47 54 53 52 49
Table 3.2105.4 GPS week: 2105 Day: 4 MJD: 58983
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1627 28 42 50 41 47 34 22 16 | 50 72 63 56 63 31 49 43
R02 | 1504 11 12 13 9 14 13 13 5 | 41 39 39 39 42 37 38 37
R03 | 730 11 12 14 9 14 18 11 6 | 41 41 47 48 39 55 46 44
XR04 | 2362 14 16 19 11 --- 11 16 7 | 45 40 46 42 --- 44 39 41
R05 | 1061 14 10 19 15 18 19 11 7 | 31 33 36 42 34 37 37 34
R07 | 964 13 12 12 15 15 12 14 6 | 42 44 39 52 40 48 40 42
R08 | 843 12 11 15 15 15 13 14 6 | 38 41 39 46 49 47 34 40
R09 | 2442 13 17 23 11 11 14 14 6 | 83 83 91 97 91 89 85 88
R11 | 942 7 9 19 9 23 12 9 6 | 83 82 75 85 83 80 92 83
R12 | 1607 10 14 32 18 17 14 22 8 | 74 76 56 58 82 66 78 69
R13 | 1575 34 52 47 58 37 36 20 17 | 76 90 59 54 81 54 64 60
R14 | 1144 7 12 20 8 12 15 11 5 | 55 59 57 51 59 43 60 53
R15 | 726 17 23 20 19 12 11 8 6 | 50 55 39 39 44 40 41 41
R16 | 1817 14 24 24 31 34 34 27 12 | 52 60 47 50 57 62 71 54
R17E | 2945 14 15 25 17 20 11 15 7 | 91 90 98 92 85 91 81 88
R18E | 743 12 13 14 17 10 14 11 6 | 18 19 18 21 19 23 21 17
R19E | 908 29 30 44 46 62 23 27 17 | 38 50 33 41 74 30 30 31
R20E | 793 43 45 55 70 55 40 29 21 | 109 115 109 150 138 89 90 107
R21E | 630 15 16 31 24 11 10 16 8 | 36 36 37 37 40 37 40 35
R22E | 3191 17 15 33 15 16 16 13 8 | 71 70 65 63 69 58 60 63
R23E | 1494 17 21 25 27 20 21 20 9 | 46 50 49 62 52 45 43 46
R24E | 700 21 22 30 16 24 12 14 8 | 28 24 24 22 37 23 26 21
XR26E | ---- 13 35 --- --- --- --- 11 12 | 42 52 --- --- --- --- 46 43
------+----------------------------------------------+------------------------------------------
RMS | 1531 19 23 30 29 27 21 17 |T 53 57 53 56 60 51 52 51
WRMS | 1531 13 17 30 18 18 16 17 |NE 54 58 52 54 58 52 55 52
MEDI | 1061 14 16 23 16 17 14 14 |MD 46 52 47 50 57 45 46 43
Table 3.2105.5 GPS week: 2105 Day: 5 MJD: 58984
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1367 31 31 44 53 47 22 21 16 | 36 54 51 58 57 40 28 34
R02 | 1543 13 20 12 20 16 20 13 7 | 26 28 31 31 32 35 25 26
R03 | 482 17 21 13 13 10 12 8 5 | 34 35 38 50 47 43 48 42
XR04 | 2201 13 20 21 23 --- 13 11 8 | 46 52 49 43 --- 41 43 43
R05 | 868 14 19 24 18 22 15 10 7 | 28 32 39 52 46 30 30 34
R07 | 1513 8 10 18 14 8 14 19 6 | 34 34 40 39 33 36 30 32
R08 | 1173 14 13 16 13 23 23 19 8 | 32 34 37 43 54 48 30 39
R09 | 1867 14 17 22 21 14 18 17 8 | 62 64 63 48 57 55 62 57
R11 | 1090 14 13 20 18 11 23 12 7 | 118 119 120 129 127 120 126 122
R12 | 1808 15 19 31 21 17 21 22 9 | 55 57 43 43 55 41 59 48
R13 | 1735 52 35 41 42 38 20 21 16 | 82 72 57 60 65 60 60 60
R14 | 1154 14 13 16 14 12 14 10 6 | 77 74 77 80 83 76 71 76
R15 | 824 27 22 23 12 14 17 20 8 | 50 47 39 41 39 43 35 38
R16 | 1098 26 21 27 24 26 26 19 11 | 62 71 70 70 80 69 71 68
R17E | 2174 18 12 27 12 16 22 12 8 | 156 158 158 163 164 164 155 159
R18E | 658 9 12 16 24 8 21 9 6 | 19 18 25 25 22 25 22 20
R19E | 612 35 40 49 44 40 26 31 16 | 30 35 26 38 50 36 40 27
R20E | 1686 43 56 73 78 65 33 35 24 | 143 148 154 149 134 138 146 137
R21E | 640 15 13 30 26 7 16 15 8 | 39 41 34 34 39 40 39 36
R22E | 3574 17 17 30 23 19 17 17 9 | 85 87 85 85 93 83 81 84
R23E | 1287 19 21 21 25 21 17 12 8 | 88 83 83 83 87 85 90 85
R24E | 1510 22 31 29 21 16 13 12 8 | 27 32 27 25 27 24 22 19
XR26E | ---- 24 37 --- --- --- --- 14 19 | 52 65 --- --- --- --- 54 52
------+----------------------------------------------+------------------------------------------
RMS | 1521 23 24 31 30 26 20 18 |T 60 62 61 63 66 60 59 58
WRMS | 1521 18 18 31 23 16 19 18 |NE 53 55 53 56 59 52 51 51
MEDI | 1287 17 20 23 21 16 18 15 |MD 50 54 43 48 55 43 48 43
Table 3.2105.6 GPS week: 2105 Day: 6 MJD: 58985
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 956 37 36 44 48 43 14 19 15 | 67 66 76 52 47 48 58 52
R02 | 1286 12 13 13 5 19 13 12 5 | 42 38 43 40 49 41 35 40
R03 | 520 11 16 11 17 15 18 9 6 | 53 52 54 64 65 62 55 57
XR04 | 1687 11 20 20 28 --- 15 11 8 | 65 64 70 55 --- 64 64 63
R05 | 919 15 14 23 20 31 11 11 8 | 41 42 49 65 64 50 47 49
R07 | 2506 6 10 14 8 14 8 9 4 | 51 51 55 58 63 54 52 54
R08 | 935 14 16 17 12 14 12 15 6 | 46 43 46 57 60 57 50 52
R09 | 2029 14 14 17 14 18 20 17 7 | 83 84 84 89 89 81 88 84
R11 | 821 12 18 17 12 11 19 17 7 | 122 125 121 125 125 120 126 123
R12 | 1250 17 27 27 22 13 27 20 9 | 87 97 63 80 88 69 93 80
R13 | 1958 35 47 36 56 35 24 25 16 | 97 109 72 95 92 71 87 80
R14 | 696 10 11 27 16 16 11 10 6 | 75 78 64 84 78 78 71 74
R15 | 720 17 19 21 16 11 10 14 6 | 69 67 49 51 56 54 57 55
R16 | 2730 16 25 42 18 37 35 21 13 | 72 69 74 66 70 78 77 70
R17E | 1799 17 10 23 9 27 11 12 7 | 135 133 135 134 134 133 137 134
R18E | 651 9 11 15 21 17 21 13 7 | 30 34 34 37 35 33 31 30
R19E | 543 37 36 56 45 76 31 30 20 | 37 46 35 34 93 35 36 34
R20E | 2345 38 42 64 70 42 32 31 20 | 118 118 123 117 125 129 107 115
R21E | 643 15 17 28 18 20 13 14 8 | 52 55 46 55 59 49 55 51
R22E | 2659 15 19 30 21 15 15 18 8 | 101 99 97 99 104 96 91 96
R23E | 1241 21 25 18 25 24 19 11 9 | 86 89 89 84 84 75 78 80
R24E | 776 15 20 32 18 17 16 15 8 | 29 32 33 26 34 27 25 24
XR26E | ---- 29 101 --- --- --- --- 24 26 | 68 106 --- --- --- --- 67 65
------+----------------------------------------------+------------------------------------------
RMS | 1521 21 24 31 29 29 20 17 |T 70 73 68 71 76 68 69 67
WRMS | 1521 16 19 31 17 18 18 17 |NE 69 70 65 70 72 66 68 66
MEDI | 956 15 19 23 18 18 15 15 |MD 68 67 63 64 70 62 64 63
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