[IGSREPORT-27309] Wk 2106 IGLOS Final Orbits
acc
acc at igs.org
Sun Jun 14 17:17:09 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2106 (May 17, 2020 - May 23, 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 2.2106.
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:
igl2106[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2106 in the SP3 format.
igl21067.sum Combination Report for GPS Week 2106.
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 | -1.7 ns
1 | -0.7 ns
2 | -2.9 ns
3 | -1.3 ns
4 | -3.8 ns
5 | -3.0 ns
6 | -1.9 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 1.2106, 1a.2106).
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 2.2106.0-6)
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 3.2106.0-6).
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 2106 summary. (May 17, 2020 - May 23, 2020)
Table 1.2106.a GPS week : 2106 MJD: 58986.0-58992.0
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 2 -17 28 .21 24 19 | 21792 374 3094 7816
| 1 1 2 16 23 22 .07 | 816 1596
cof n/a| 0 0 -2 0 4 22 .19 27 20 | 21781 378 3094 7824
| 1 0 1 24 15 26 .11 | 821 1599
emx n/a| 0 0 9 -2 -6 10 .04 34 31 | -1853 445 3095 8015
| 1 1 2 26 18 39 .11 | 6811 1106
esx n/a| 1 0 1 19 10 -28 .10 29 20 | 1477 1326 3089 10048
| 1 1 1 16 19 31 .06 | 9478 1984
gfz n/a| 1 0 -1 0 10 -39 .03 28 17 | 0 412 3123 7318
| 1 1 2 24 24 20 .06 | 0 1698
grg n/a| 0 0 -3 -72 -32 -12 -.39 25 20 | -2290 357 3088 6805
| 1 1 4 20 27 69 .10 | 567 1774
iac n/a| -1 0 -1 60 37 47 .02 26 26 | -464 -44 3093 7939
| 1 2 1 126 84 38 .11 | 914 1413
Table 1.2106.b GPS week : 2106 MJD: 58986.0-58992.0
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 | 20 12 12 14 17 16 14 |
R02 | 8 6 6 8 6 7 7 |
R03 | 5 7 6 6 6 7 8 |
R04 | 8 8 7 7 8 12 8 |
R05 | 11 8 8 12 12 10 10 |
R07 | 8 7 6 5 9 7 6 |
R08 | 7 8 7 11 7 7 7 |
R09 | 9 7 7 8 9 8 8 |
R11 | 7 7 7 7 8 9 8 |
R12 | 10 10 8 8 8 11 10 |
R13 | 22 20 16 17 20 18 14 |
R14 | 9 8 8 7 8 12 6 |
R15 | 9 7 7 9 9 12 7 |
R16 | 14 14 13 18 17 11 12 |
R17 | 9 8 8 8 8 9 9 |
R18 | 8 9 7 7 8 8 7 |
R19 | 19 21 21 23 23 34 30 |
R20 | 22 23 25 21 26 26 31 |
R21 | 10 10 9 9 9 9 10 |
R22 | 10 11 10 11 9 10 10 |
R23 | 11 13 14 10 10 10 9 |
R24 | 9 8 8 10 8 10 11 |
R26 | 21 35 22 18 15 40 56 |
Table 1.2106.c GPS week : 2106 MJD: 58986.0-58992.0
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 2106 0 | -72 -10 203 -495 1403 1662 81.6 1718 1718 | -1713 0
brd 2106 1 | 5 4 192 1063 647 2639 82.1 1503 1503 | -727 0
brd 2106 2 | -22 -2 190 622 -8 2842 81.9 1431 1431 | -2941 0
brd 2106 3 | 3 -27 251 -1404 300 4086 83.4 1676 1676 | -1264 0
brd 2106 4 | -13 65 237 -71 629 4046 82.0 1761 1761 | -3753 0
brd 2106 5 | 78 48 336 -473 1510 2590 82.4 1813 1813 | -2961 0
brd 2106 6 | -35 -3 231 -386 3088 6302 82.8 1684 1684 | -1900 0
-------------+------------------------------------------------------------+----------------
brd 2106 mean| -8 10 234 -163 1081 3452 82.3 1655 1655 | -2179 0
brd 2106 sdev| 46 33 50 808 1041 1519 .6 138 138 | 1073 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 2.2106.0 GPS week: 2106 Day: 0 MJD: 58986
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 2 -4 -17 -53 47 .24 26 22 | 20758 -524 2751 7014
cof n/a| 0 1 -5 -24 -26 1 .21 30 23 | 20736 -495 2751 7018
emx n/a| -1 1 4 -46 -15 20 -.14 30 30 | 2967 -83 2746 7130
esx n/a| 3 0 0 -2 -5 -77 .05 28 17 | 12968 433 2742 9603
gfz n/a| 0 -1 0 -45 -23 -62 .06 24 18 | 0 -95 2781 6480
grg n/a| 0 1 2 -95 -86 86 -.29 25 18 | -1296 -641 2744 5949
iac n/a| 0 -3 -1 344 225 14 .15 32 32 | 360 -807 2738 7090
Table 2.2106.1 GPS week: 2106 Day: 1 MJD: 58987
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 -24 27 44 .25 26 16 | 20527 2649 3303 8354
cof n/a| -2 -1 -3 -19 19 36 .36 33 18 | 20515 2675 3306 8356
emx n/a| -1 0 7 -17 -27 -9 .09 34 31 | -11887 2200 3311 8537
esx n/a| 3 -1 0 33 -7 -39 .11 29 21 | 4455 4599 3311 10433
gfz n/a| 1 0 2 6 -8 -11 .08 27 20 | 0 2427 3336 7972
grg n/a| 1 1 -4 -42 -37 -72 -.35 22 19 | -1981 2727 3316 7348
iac n/a| 0 1 0 32 27 74 -.08 21 21 | 144 1515 3314 8404
Table 2.2106.2 GPS week: 2106 Day: 2 MJD: 58988
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| 1 -1 -1 11 -19 28 .16 26 17 | 22256 -1106 3078 8031
cof n/a| 3 0 -2 -23 -3 37 .15 27 17 | 22255 -1121 3074 8032
emx n/a| 3 -2 10 16 13 -37 .04 35 27 | -5523 -838 3073 8249
esx n/a| 1 -3 2 4 -8 -14 .15 27 20 | 5703 -20 3057 10183
gfz n/a| 1 -2 0 32 3 -23 .05 25 15 | 0 -1105 3110 7782
grg n/a| 0 -2 -5 -83 -12 61 -.46 27 22 | -2177 -1322 3070 7150
iac n/a| -3 3 -1 17 15 -16 .00 15 15 | 580 -2449 3067 8165
Table 2.2106.3 GPS week: 2106 Day: 3 MJD: 58989
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 7 -22 18 .10 21 16 | 22389 2535 3209 7399
cof n/a| 0 0 -3 -9 -1 19 .25 25 19 | 22392 2533 3213 7421
emx n/a| 0 1 13 -9 -31 15 -.00 38 36 | 2507 1644 3223 7517
esx n/a| 2 2 0 6 11 -26 .18 29 22 | -8109 3675 3218 9525
gfz n/a| 2 0 -4 8 29 -32 .07 27 15 | 0 2696 3244 6873
grg n/a| 1 0 -11 -72 -21 -9 -.40 28 22 | -2664 2788 3198 6394
iac n/a| -2 -3 -1 29 16 47 -.09 20 20 | -647 1280 3210 7456
Table 2.2106.4 GPS week: 2106 Day: 4 MJD: 58990
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 0 12 -19 -4 .26 25 21 | 22301 -1110 2970 7700
cof n/a| 1 -1 0 29 10 -26 .18 26 21 | 22277 -1096 2963 7701
emx n/a| 1 0 9 3 -1 -25 .06 33 33 | -7521 -402 2961 7892
esx n/a| 1 1 0 27 11 -52 .14 29 19 | -2368 -4 2953 10116
gfz n/a| 3 0 -2 -12 48 -67 .05 32 19 | 0 -1808 2978 7109
grg n/a| 0 0 0 -74 -41 0 -.37 25 21 | -2955 -1445 2957 6762
iac n/a| -1 -1 -2 27 -17 98 -.06 23 23 | -2039 -524 2965 7872
Table 2.2106.5 GPS week: 2106 Day: 5 MJD: 58991
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 -2 9 -20 54 .31 24 20 | 21813 -108 3015 7546
cof n/a| 0 0 -1 34 14 51 .16 23 19 | 21801 -118 3021 7557
emx n/a| 0 3 8 38 3 81 .23 37 29 | -1116 33 3021 7828
esx n/a| 0 0 3 37 29 2 -.00 29 20 | 10245 986 3015 9898
gfz n/a| 0 1 -3 13 18 -45 -.04 33 17 | 0 -130 3041 6828
grg n/a| -2 -3 1 -88 0 -102 -.56 24 20 | -2779 -160 3000 6527
iac n/a| -1 0 -4 -8 -17 68 .18 35 35 | -1060 -340 3010 7793
Table 2.2106.6 GPS week: 2106 Day: 6 MJD: 58992
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 20 -16 7 .16 24 19 | 22500 288 3336 8671
cof n/a| 0 0 -3 7 14 36 .01 25 20 | 22496 269 3332 8683
emx n/a| -1 0 10 -1 12 25 .01 32 29 | 7596 565 3331 8956
esx n/a| 0 0 2 28 41 10 .06 31 20 | -12550 -381 3329 10578
gfz n/a| 1 0 -5 0 3 -31 -.08 28 19 | 0 905 3377 8187
grg n/a| 2 0 -3 -46 -26 -52 -.29 23 20 | -2183 553 3336 7508
iac n/a| -1 0 -1 -21 12 43 .04 34 34 | -586 1012 3351 8794
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 3.2106.0 GPS week: 2106 Day: 0 MJD: 58986
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01M | 1047 47 49 35 60 30 43 47 20 | 25 32 51 74 53 35 49 37
R02M | 2335 13 12 12 10 16 16 30 7 | 23 23 34 35 31 29 52 28
R03M | 683 5 8 13 7 8 11 22 5 | 26 25 35 30 29 37 49 29
XR04M | 1140 15 22 15 10 --- 15 24 7 | 24 27 25 25 --- 22 43 22
R05 | 514 23 24 12 35 19 23 32 11 | 20 20 19 58 38 30 50 29
R07 | 2852 10 15 20 10 17 16 25 7 | 26 30 24 33 39 28 48 28
R08 | 1172 16 13 12 19 15 11 16 6 | 23 25 33 39 29 31 48 29
R09E | 2368 15 17 19 15 26 12 25 8 | 37 39 37 37 50 37 56 38
R11E | 571 12 10 17 10 15 14 27 7 | 113 113 109 115 108 120 112 112
R12E | 824 22 16 31 20 16 18 29 10 | 108 110 93 99 105 107 111 102
R13E | 2787 33 36 60 52 54 45 42 21 | 106 114 81 77 128 95 110 94
R14E | 815 15 17 31 19 8 14 31 9 | 83 83 64 77 80 80 86 76
R15E | 1084 21 24 25 16 16 15 28 9 | 68 69 54 53 59 55 68 57
R16E | 2267 22 25 26 33 35 37 27 14 | 68 72 68 79 62 78 78 68
R17E | 1759 23 28 27 10 16 17 28 9 | 78 81 63 65 68 65 80 67
R18E | 906 17 16 14 12 14 20 29 8 | 75 82 78 84 83 77 83 77
R19E | 1391 50 57 42 41 38 35 41 18 | 80 79 65 65 70 78 74 60
R20E | 2460 51 72 58 51 38 50 42 22 | 64 80 88 88 73 68 50 63
R21E | 608 15 19 31 17 21 11 41 10 | 112 112 99 100 113 104 125 107
R22E | 2405 22 19 31 13 17 14 29 9 | 137 146 122 138 145 140 142 137
R23E | 2238 20 26 14 30 19 27 34 11 | 191 185 183 171 179 173 185 178
R24E | 843 23 26 26 11 13 13 27 8 | 52 54 46 54 52 53 61 49
XR26E | ---- 21 42 --- --- --- --- 20 21 | 33 35 --- --- --- --- 75 46
------+----------------------------------------------+------------------------------------------
RMS | 1717 26 30 30 28 24 25 32 |T 68 71 66 72 75 70 79 66
WRMS | 1717 22 23 30 17 18 18 32 |NE 23 25 25 43 35 29 48 28
MEDI | 1140 21 22 25 16 17 16 29 |MD 68 72 63 65 68 65 74 60
Table 3.2106.1 GPS week: 2106 Day: 1 MJD: 58987
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01M | 736 19 25 37 34 23 27 15 11 | 20 31 51 41 33 17 22 21
R02M | 2078 8 11 16 22 10 12 14 6 | 15 20 20 23 21 21 27 17
R03M | 876 13 11 5 16 16 21 17 7 | 16 16 20 32 24 22 28 20
XR04M | 507 15 15 25 13 --- 11 15 8 | 16 17 23 14 --- 15 22 14
R05 | 684 18 16 21 18 24 11 14 8 | 20 30 15 31 41 31 25 23
R07 | 1843 10 14 11 18 16 12 17 6 | 17 20 14 28 23 15 21 15
R08 | 995 9 15 20 17 19 18 15 7 | 18 26 24 26 30 16 21 15
R09E | 2912 13 15 13 8 20 15 19 7 | 25 29 28 27 34 22 32 25
R11E | 515 12 16 17 11 14 24 15 7 | 88 91 91 87 81 89 85 86
R12E | 682 18 20 33 22 19 17 17 9 | 81 83 67 73 77 79 74 74
R13E | 1289 39 45 53 53 43 44 37 20 | 79 83 69 64 82 55 75 64
R14E | 1853 14 16 30 18 14 15 19 8 | 68 70 54 63 60 61 68 62
R15E | 1529 18 16 24 17 10 12 13 7 | 52 49 39 37 45 48 48 43
R16E | 802 36 30 20 37 47 17 21 14 | 43 43 38 50 48 53 42 37
R17E | 1562 18 20 27 20 12 15 16 8 | 50 49 40 31 41 42 46 39
R18E | 1143 21 16 23 12 23 21 17 8 | 104 110 107 114 120 109 114 110
R19E | 703 42 65 81 47 40 37 32 21 | 100 121 98 84 108 94 98 91
R20E | 2926 55 94 61 67 61 37 31 23 | 89 98 73 71 96 85 79 71
R21E | 1275 25 24 26 22 18 21 25 10 | 131 126 121 124 122 121 120 121
R22E | 1758 30 21 34 22 33 15 15 11 | 115 127 112 116 132 126 120 119
R23E | 1240 38 39 28 29 27 22 25 12 | 177 175 171 174 180 172 181 174
R24E | 747 14 23 27 18 18 14 18 8 | 48 53 42 50 53 48 41 45
XR26E | ---- 40 60 --- --- --- --- 29 34 | 24 81 --- --- --- --- 66 43
------+----------------------------------------------+------------------------------------------
RMS | 1502 26 33 34 29 27 22 21 |T 60 67 59 61 69 60 63 57
WRMS | 1502 16 18 31 21 20 19 21 |NE 18 25 17 28 31 20 22 17
MEDI | 1143 18 20 25 18 19 17 17 |MD 50 53 42 50 53 48 48 43
Table 3.2106.2 GPS week: 2106 Day: 2 MJD: 58988
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01M | 1366 33 24 24 33 31 20 11 11 | 22 23 20 31 42 25 26 23
R02M | 1921 9 10 13 16 14 16 12 6 | 20 24 27 30 28 26 27 23
R03M | 957 9 13 15 7 15 25 10 6 | 23 21 27 22 22 27 25 21
XR04M | 509 16 12 15 15 --- 15 12 7 | 15 15 20 23 --- 23 13 13
R05 | 662 21 11 15 27 17 16 11 8 | 11 31 26 49 39 28 21 25
R07 | 586 9 12 17 11 9 17 11 5 | 20 23 16 28 24 30 32 23
R08 | 888 8 9 10 10 21 17 14 6 | 18 23 21 24 35 24 17 19
R09E | 2446 17 18 12 13 17 12 17 7 | 27 31 27 30 36 26 33 27
R11E | 594 11 12 23 15 12 18 11 6 | 114 112 108 111 107 113 110 110
R12E | 1013 14 14 32 15 16 13 12 7 | 107 106 97 100 107 103 106 103
R13E | 1260 31 47 57 47 32 20 23 15 | 85 96 57 47 74 72 73 66
R14E | 1824 15 18 31 15 11 19 11 7 | 67 71 50 58 64 66 58 60
R15E | 1731 16 17 26 18 9 19 11 7 | 52 54 38 40 45 53 45 44
R16E | 811 11 18 23 22 41 50 15 12 | 65 75 59 72 68 98 70 69
R17E | 1070 16 17 33 18 12 24 9 8 | 48 51 32 38 49 57 47 43
R18E | 1131 12 12 27 10 11 21 14 7 | 60 58 55 62 57 61 54 56
R19E | 1234 48 56 82 45 40 56 26 21 | 100 113 85 109 123 142 121 108
R20E | 3089 72 69 74 63 60 34 33 25 | 115 146 143 144 159 130 130 131
R21E | 1226 18 24 31 19 7 29 10 8 | 83 80 61 65 74 87 78 73
R22E | 1340 15 12 37 23 25 18 10 9 | 80 80 66 75 92 85 73 77
R23E | 1344 36 32 24 36 34 40 10 13 | 101 115 117 118 118 105 114 111
R24E | 644 18 15 24 14 17 21 18 8 | 52 54 51 46 52 46 59 49
XR26E | ---- 29 38 --- --- --- --- 16 22 | 26 36 --- --- --- --- 37 31
------+----------------------------------------------+------------------------------------------
RMS | 1431 26 27 35 27 25 27 15 |T 57 62 54 60 67 64 59 56
WRMS | 1431 17 17 27 20 15 22 15 |NE 16 25 21 33 32 27 23 22
MEDI | 1131 16 17 24 16 17 19 12 |MD 52 54 50 47 57 57 54 49
Table 3.2106.3 GPS week: 2106 Day: 3 MJD: 58989
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01M | 2213 33 29 24 28 49 32 10 14 | 20 32 21 50 62 23 25 27
R02M | 2295 10 15 11 15 14 11 28 7 | 15 23 16 22 17 19 27 12
R03M | 1347 4 11 16 19 7 16 15 6 | 16 23 22 24 18 28 21 18
XR04M | 565 11 14 13 19 --- 17 12 7 | 15 18 21 21 --- 16 16 12
R05 | 568 31 18 32 32 32 14 14 12 | 13 25 18 60 60 37 34 32
R07 | 565 10 9 13 8 10 10 14 5 | 18 18 14 20 19 21 21 15
R08 | 2232 17 13 21 27 31 22 21 10 | 18 31 20 42 48 24 23 24
R09E | 2701 19 21 19 9 21 17 16 7 | 23 28 15 27 30 31 24 21
R11E | 600 8 10 17 10 14 15 21 6 | 79 86 77 85 79 79 81 79
R12E | 1233 13 13 32 11 13 18 14 7 | 88 89 75 78 77 85 83 81
R13E | 3744 29 38 58 55 40 31 14 17 | 103 110 71 62 114 112 80 89
R14E | 800 12 16 30 15 9 17 13 7 | 79 83 61 75 73 82 71 73
R15E | 1225 12 18 31 17 15 18 21 8 | 57 62 40 46 60 50 54 51
R16E | 1421 31 41 38 17 50 67 30 18 | 76 87 87 96 102 130 105 93
R17E | 1165 15 20 30 17 15 12 12 7 | 55 56 34 39 52 48 55 47
R18E | 711 6 8 25 14 14 22 9 6 | 64 68 56 75 69 66 69 66
R19E | 830 34 25 95 49 46 54 28 22 | 98 88 90 75 109 121 103 93
R20E | 2601 38 60 65 65 39 48 35 21 | 102 113 89 84 108 126 109 98
R21E | 923 15 19 31 22 10 15 18 8 | 94 97 84 83 93 81 97 89
R22E | 971 8 15 43 30 26 16 21 11 | 66 73 44 45 76 68 72 62
R23E | 1361 21 33 18 32 23 20 12 9 | 55 58 55 67 62 55 62 58
R24E | 1030 15 15 33 21 10 23 28 10 | 52 64 61 64 60 58 67 57
XR26E | ---- 17 51 --- --- --- --- 17 17 | 26 52 --- --- --- --- 34 27
------+----------------------------------------------+------------------------------------------
RMS | 1676 21 25 38 29 27 28 20 |T 53 60 48 56 66 61 57 53
WRMS | 1676 16 19 36 22 15 22 20 |NE 16 24 17 40 42 27 26 23
MEDI | 1165 15 18 30 19 15 17 16 |MD 55 62 44 60 62 55 62 57
Table 3.2106.4 GPS week: 2106 Day: 4 MJD: 58990
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01M | 2397 38 32 39 33 49 34 36 17 | 19 38 43 46 64 16 47 30
R02M | 1432 11 16 14 9 13 14 14 5 | 15 23 18 21 14 29 22 16
R03M | 1186 5 20 11 12 9 17 15 5 | 21 31 23 25 18 24 21 19
XR04M | 512 13 15 23 7 --- 17 18 8 | 14 17 14 15 --- 15 16 10
R05 | 724 27 25 28 27 38 16 16 11 | 11 12 14 45 55 28 33 24
R07 | 1113 17 18 19 20 19 14 26 8 | 17 19 19 33 29 22 34 20
R08 | 1972 14 21 16 16 20 8 19 7 | 15 18 16 32 35 22 16 19
R09E | 3110 15 17 23 13 16 17 25 8 | 24 34 36 34 39 29 32 28
R11E | 520 15 11 23 9 14 22 23 8 | 144 140 135 132 129 144 142 137
R12E | 973 10 23 26 9 14 24 20 8 | 123 129 113 118 123 130 119 121
R13E | 4625 41 52 51 54 37 44 31 19 | 115 121 93 93 106 118 103 100
R14E | 1153 22 15 24 14 11 19 14 8 | 101 106 93 104 102 108 97 100
R15E | 594 21 15 26 15 17 26 16 9 | 59 57 49 51 47 63 54 52
R16E | 1663 26 26 39 21 53 40 38 16 | 63 70 60 68 90 88 87 71
R17E | 2007 18 13 26 15 17 16 13 8 | 51 47 32 46 57 34 52 44
R18E | 707 11 12 19 15 16 21 18 7 | 56 55 49 56 55 55 45 51
R19E | 552 48 46 71 46 81 23 29 23 | 74 77 47 50 93 57 67 54
R20E | 1442 46 48 62 81 57 53 42 26 | 71 71 60 64 83 80 64 58
R21E | 777 20 20 26 15 22 22 15 9 | 76 73 58 66 80 55 73 66
R22E | 1083 21 20 30 20 15 17 19 9 | 50 50 33 36 41 41 49 38
R23E | 1562 23 18 17 33 24 14 14 9 | 106 107 109 113 111 95 108 105
R24E | 1548 16 18 32 14 15 17 12 8 | 54 51 42 51 56 56 52 50
XR26E | ---- 15 39 --- --- --- --- 14 15 | 37 57 --- --- --- --- 44 38
------+----------------------------------------------+------------------------------------------
RMS | 1761 25 26 33 29 32 25 23 |T 57 61 52 59 67 59 59 54
WRMS | 1761 20 21 33 18 19 21 23 |NE 14 16 16 36 39 24 27 21
MEDI | 1153 18 20 26 15 17 17 18 |MD 54 55 43 50 57 55 52 50
Table 3.2106.5 GPS week: 2106 Day: 5 MJD: 58991
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01M | 1870 32 36 45 35 33 39 26 16 | 17 57 36 59 58 39 20 29
R02M | 983 14 15 14 18 20 9 16 7 | 21 22 19 24 14 18 19 14
R03M | 927 13 13 16 10 13 18 17 6 | 19 19 26 24 21 25 25 20
XR04M | 512 21 16 29 21 --- 28 14 11 | 18 18 19 36 --- 28 21 20
R05 | 1104 19 13 28 17 24 22 22 10 | 14 14 18 29 34 28 27 16
R07 | 898 17 15 11 15 15 11 20 6 | 22 22 21 32 29 25 27 22
R08 | 675 12 14 14 14 15 17 13 6 | 18 20 17 28 31 24 27 21
R09E | 3055 16 18 24 12 19 14 22 8 | 33 37 39 41 48 42 45 39
R11E | 1000 18 14 29 14 14 22 16 8 | 165 173 165 178 176 171 166 170
R12E | 1740 13 11 35 18 11 23 41 11 | 119 122 107 118 115 105 132 115
R13E | 4351 31 34 54 44 37 25 47 17 | 112 116 88 97 101 117 104 100
R14E | 990 29 27 29 12 14 30 32 11 | 160 168 159 158 159 167 159 158
R15E | 882 18 29 25 15 24 35 30 11 | 85 90 81 81 80 87 82 79
R16E | 1230 14 20 29 26 30 27 24 11 | 73 77 65 78 81 81 78 74
R17E | 2275 19 23 26 17 23 16 14 8 | 46 49 30 33 53 35 43 39
R18E | 1298 13 12 14 28 16 13 15 8 | 55 57 51 59 54 54 53 52
R19E | 1317 36 33 82 61 119 34 101 33 | 62 67 58 55 131 65 57 56
R20E | 1278 54 44 82 70 32 46 64 26 | 51 50 73 69 70 55 51 45
R21E | 1808 19 21 33 24 15 13 16 9 | 93 95 76 80 90 79 93 84
R22E | 1749 14 19 34 20 10 24 27 10 | 53 58 40 45 52 63 56 50
R23E | 2216 25 21 15 33 23 14 16 10 | 90 90 84 79 73 77 90 81
R24E | 2037 20 23 36 15 22 17 14 9 | 39 39 39 40 45 41 37 36
XR26E | ---- 35 37 --- --- --- --- 46 40 | 41 52 --- --- --- --- 79 49
------+----------------------------------------------+------------------------------------------
RMS | 1812 24 23 37 29 33 24 35 |T 61 65 59 65 72 64 64 59
WRMS | 1812 20 19 29 20 17 20 35 |NE 18 18 18 29 31 25 27 19
MEDI | 1278 19 20 29 18 20 22 22 |MD 51 57 40 55 58 54 53 49
Table 3.2106.6 GPS week: 2106 Day: 6 MJD: 58992
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01M | 1022 39 23 28 34 35 25 17 14 | 16 43 36 55 52 35 38 34
R02M | 730 13 12 10 21 14 18 14 7 | 21 24 23 35 27 30 21 23
R03M | 1304 17 17 12 10 11 28 18 8 | 20 20 24 21 19 32 31 22
XR04M | 615 12 21 15 11 --- 13 27 8 | 14 19 19 16 --- 22 19 13
R05 | 1292 14 11 22 25 18 29 16 9 | 15 32 28 47 45 36 24 28
R07 | 624 11 10 15 9 10 20 11 6 | 18 20 20 25 22 31 26 20
R08 | 1497 7 8 7 17 21 14 17 6 | 17 15 22 22 26 21 21 18
R09E | 3219 16 12 20 11 18 17 21 7 | 44 42 46 46 56 43 46 44
R11E | 1878 11 12 22 10 15 19 19 7 | 140 143 133 141 134 148 137 139
R12E | 1955 16 17 38 17 21 15 19 9 | 171 169 155 171 172 163 171 167
R13E | 2461 39 35 41 29 33 24 20 14 | 134 134 119 122 130 128 127 125
R14E | 954 11 12 22 9 12 11 13 6 | 113 118 107 116 114 118 118 114
R15E | 989 15 15 23 14 15 12 20 7 | 72 68 71 58 58 65 67 63
R16E | 1631 18 21 26 25 23 33 27 11 | 57 63 61 61 74 56 60 56
R17E | 2131 20 21 28 19 27 18 9 9 | 66 67 42 46 73 46 60 55
R18E | 1377 8 13 15 22 13 19 16 7 | 49 52 43 55 51 43 53 47
R19E | 1751 50 62 59 67 87 39 88 29 | 111 118 90 92 132 93 97 92
R20E | 846 53 63 75 86 46 50 101 31 | 133 132 111 108 135 117 152 117
R21E | 887 19 22 34 24 18 12 28 10 | 86 85 62 65 84 71 89 75
R22E | 2054 16 14 36 27 14 11 19 9 | 81 79 48 53 77 70 80 68
R23E | 2524 19 22 19 29 19 15 21 9 | 107 108 111 107 102 104 108 105
R24E | 1419 19 18 40 24 15 16 31 11 | 63 61 58 64 66 57 68 59
XR26E | ---- 48 84 --- --- --- --- 64 55 | 51 67 --- --- --- --- 68 56
------+----------------------------------------------+------------------------------------------
RMS | 1683 24 25 32 31 28 23 34 |T 69 73 64 69 78 69 73 66
WRMS | 1683 19 20 29 20 19 20 34 |NE 16 22 23 31 31 29 23 22
MEDI | 1377 16 17 22 21 18 18 19 |MD 63 67 48 55 73 56 67 56
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