[IGSREPORT-15083] Wk 1424 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu May 10 00:05:17 PDT 2007
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IGS Electronic Report 10 May 00:05:23 PDT 2007 Message Number 15083
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1424 (Apr 22, 2007 - Apr 28, 2007)
Contact: Gerd Gendt (gendt at gfz-potsdam.de)
Thomas Nischan ( nisn at gfz-potsdam.de)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the centers
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 2.1424.
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:
igl1424[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1424 in the SP3 format.
igl14247.sum Combination Report for GPS Week 1424.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
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.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
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.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 843.9 ns
1 | 804.9 ns
2 | 829.5 ns
3 | 867.7 ns
4 | 870.2 ns
5 | 891.5 ns
6 | 885.7 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
----+--------+---------------
0 | COD | R21
0 | ESX | R23
0 | IAC | R21
1 | ESX | R23 R24
2 | ESX | R23
3 | COD | R21
3 | ESX | R23
3 | IAC | R21
4 | ESX | R23
5 | ESX | R23
6 | ESX | R23
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 1.1424, 1a.1424).
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 2.1424.0-6)
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 3.1424.0-6).
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 1424 summary. (Apr 22, 2007 - Apr 28, 2007)
Table 1.1424.a GPS week : 1424 MJD: 54212.0-54218.0
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]
--------+----------------------------------------------------+------------------------------
bkg 57| 0 0 -1 174 -41 -148 -.10 59 49 | 0 1433 4499 4884
| 2 3 7 54 51 152 .08 | 0 2213
cod 167| -3 -1 6 170 -97 157 -.13 57 47 | --- --- --- ---
| 6 3 9 80 89 139 .17 | --- ---
esx 45| 3 1 -14 101 -48 -35 -.25 172 65 | 672475 -3982 16440 25796
| 7 5 10 126 173 240 .10 | 1701738 22754
iac n/a| 0 3 -1 -250 94 3 .22 38 38 | 860009 -3927 15446 25020
| 2 4 7 54 42 61 .05 | 28128 12215
Table 1.1424.b GPS week : 1424 MJD: 54212.0-54218.0
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 | --- 0 178 159 68 27 25 |
R03 | 25 24 28 29 29 20 30 |
R04 | 20 27 19 25 30 18 18 |
R06 | 22 29 20 44 42 51 37 |
R07 | 19 14 19 21 18 21 34 |
R08 | 26 36 27 38 26 14 28 |
R10 | 24 24 22 20 24 18 27 |
R14 | 18 19 16 17 17 17 16 |
R18 | 64 49 38 36 33 43 40 |
R19 | 19 20 19 20 20 21 17 |
R21 | --- 0 0 --- 21 21 27 |
R22 | 37 29 25 35 44 34 40 |
R23 | 24 27 32 36 25 26 38 |
R24 | 96 30 113 --- --- --- --- |
Table 1.1424.c GPS week : 1424 MJD: 54212.0-54218.0
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 1424 0 | 241 322 -739 -6055 2885 -339100 107.5 9989 9989 | 843890 0
brd 1424 1 | 860 473 -597 -2045 3183 -349200 104.9 10620 10620 | 804924 0
brd 1424 2 | -470 652 -1140 10090 -3059 -365200 97.2 15480 15480 | 829461 0
brd 1424 3 | -377 88 -373 3379 2657 -367500 79.6 17390 17390 | 867677 0
brd 1424 4 | -507 -188 -322 1170 8198 -349400 92.1 18460 18460 | 870194 0
brd 1424 5 | -264 -352 -298 -1505 2927 -345600 80.8 10340 10340 | 891485 0
brd 1424 6 | 429 -92 246 6208 10240 -348300 80.8 7942 7942 | 885729 0
-------------+------------------------------------------------------------+----------------
brd 1424 mean| -12 129 -460 1606 3861 -352042 91.9 12888 12888 | 856194 0
brd 1424 sdev| 528 368 430 5449 4303 10409 11.8 4133 4133 | 31465 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 2.1424.0 GPS week: 1424 Day: 0 MJD: 54212
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]
--------+----------------------------------------------------+------------------------------
bkg 57| -6 3 -9 218 -50 -385 -.03 62 50 | 0 1291 3373 3865
cod 167| 6 -6 21 71 -200 443 -.22 65 50 | --- --- --- ---
esx 45| 7 -10 -13 265 206 0 -.13 196 61 | 89281 -33132 31087 43347
iac n/a| -1 0 4 -213 74 59 .23 43 43 | 866683 -21612 28040 40900
Table 2.1424.1 GPS week: 1424 Day: 1 MJD: 54213
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]
--------+----------------------------------------------------+------------------------------
bkg 57| 0 2 -5 200 -17 -60 -.04 45 43 | 0 -45 4257 4759
cod 167| -5 -2 11 207 -212 168 -.26 47 40 | --- --- --- ---
esx 45| 14 3 -37 4 -234 -178 -.13 236 83 | -36576 -15962 14248 23992
iac n/a| 0 6 1 -236 174 -7 .15 27 27 | 808987 -8794 13520 23109
Table 2.1424.2 GPS week: 1424 Day: 2 MJD: 54214
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]
--------+----------------------------------------------------+------------------------------
bkg 57| 0 -2 -1 86 20 -87 -.13 31 25 | 0 5920 5024 5498
cod 167| -5 0 12 94 -52 145 .11 35 32 | --- --- --- ---
esx 45| 7 4 -15 -26 93 -318 -.37 179 63 | 10265 -10552 11210 16972
iac n/a| -5 10 -16 -353 72 92 .25 55 55 | 836675 -5945 10477 16655
Table 2.1424.3 GPS week: 1424 Day: 3 MJD: 54215
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]
--------+----------------------------------------------------+------------------------------
bkg 57| 2 -1 5 142 -39 -42 .00 65 62 | 0 -211 3938 4317
cod 167| -13 0 -3 182 -60 99 .07 65 60 | --- --- --- ---
esx 45| 1 0 -2 145 -87 -175 -.22 150 52 | 4530704 33743 10110 16481
iac n/a| -2 5 -1 -272 122 13 .16 47 47 | 865354 1478 10583 17878
Table 2.1424.4 GPS week: 1424 Day: 4 MJD: 54216
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]
--------+----------------------------------------------------+------------------------------
bkg 57| -1 -5 -8 161 -142 -275 -.13 82 77 | 0 1953 3980 4270
cod 167| -4 2 0 314 -26 65 -.26 64 50 | --- --- --- ---
esx 45| 0 2 -11 152 25 257 -.30 155 74 | 41095 -2707 13275 21054
iac n/a| 2 2 -1 -243 51 -51 .28 34 34 | 868713 9707 12680 21612
Table 2.1424.5 GPS week: 1424 Day: 5 MJD: 54217
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]
--------+----------------------------------------------------+------------------------------
bkg 57| 0 0 -3 251 -9 -232 -.19 71 47 | 0 1698 5176 5448
cod 167| -1 3 -2 174 15 9 -.04 56 44 | --- --- --- ---
esx 45| -7 1 -14 -54 -281 319 -.35 142 54 | 32281 -17065 16426 30290
iac n/a| 0 -3 6 -181 100 1 .25 28 28 | 889294 -13897 15176 28322
Table 2.1424.6 GPS week: 1424 Day: 6 MJD: 54218
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]
--------+----------------------------------------------------+------------------------------
bkg 57| 1 -1 9 165 -49 44 -.21 56 43 | 0 -573 5749 6031
cod 167| 0 -5 8 146 -148 173 -.30 67 54 | --- --- --- ---
esx 45| 1 5 -9 220 -59 -156 -.26 148 69 | 40277 17795 18727 28441
iac n/a| 2 0 0 -254 64 -86 .21 32 32 | 884360 11574 17647 26667
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 3.1424.0 GPS week: 1424 Day: 0 MJD: 54212
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R03 |20997 46 46 71 22 25 | 51 40 46 46 31
R04 | 8959 31 52 42 18 19 | 45 46 60 34 38
R06 | 4197 43 46 54 17 22 | 45 45 72 28 26
R07 | 2102 27 47 44 21 19 | 30 42 50 34 29
XR08 | 5446 --- 37 47 32 26 | --- 41 53 40 34
XR10 | 6602 37 40 --- 27 24 | 30 38 --- 30 24
XR14 | 1577 22 34 --- 21 17 | 35 32 --- 39 29
XR18 |16148 100 84 76 --- 63 | 212 218 226 --- 211
R19 | 9916 34 38 29 31 19 | 68 65 85 67 64
R22 |10975 82 80 57 34 36 | 47 43 92 83 54
R23 | 4027 34 46 415 24 23 | 58 43 191 78 58
R24 | 4476 126 122 346 103 96 | 110 120 57 71 102
------+-------------------------------+---------------------------
RMS | 9989 62 65 196 43 |T 66 70 93 50 58
WRMS | 9989 50 50 61 43 |NE 66 70 93 50 58
MEDI | 5446 37 46 54 24 |MD 47 43 60 40 34
Table 3.1424.1 GPS week: 1424 Day: 1 MJD: 54213
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
XR01 |22963 --- 21 --- --- 0 | --- 243 --- --- 217
R03 |14953 17 54 84 19 23 | 32 41 41 31 28
R04 | 8979 49 73 48 22 27 | 41 82 66 28 26
R06 | 5565 52 58 81 30 28 | 42 38 89 41 29
R07 | 3092 16 26 43 19 14 | 29 44 33 27 23
XR08 | 5664 --- 38 100 34 35 | --- 39 95 36 34
XR10 | 6759 39 36 --- 30 24 | 37 40 --- 37 31
XR14 | 2387 20 33 --- 26 19 | 34 28 --- 28 25
XR18 |15906 41 58 118 --- 49 | 128 155 115 --- 125
R19 | 6818 39 24 73 18 20 | 51 57 82 45 47
XR21 |11057 --- 21 --- --- 0 | --- 280 --- --- 245
R22 |21446 64 37 82 34 28 | 34 35 72 56 30
R23 | 5473 35 51 488 31 27 | 45 54 170 62 47
R24 | 4654 60 32 421 37 30 | 66 73 44 60 70
------+-------------------------------+---------------------------
RMS |10623 45 47 236 27 |T 49 86 80 41 69
WRMS |10623 43 40 83 27 |NE 49 86 80 41 69
MEDI | 6759 39 36 82 30 |MD 41 44 72 37 31
Table 3.1424.2 GPS week: 1424 Day: 2 MJD: 54214
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
XR01 |14599 --- 127 --- 249 178 | --- 144 --- 216 121
R03 |35265 18 35 96 42 27 | 38 52 97 32 34
R04 | 6679 30 17 59 23 18 | 31 47 67 39 39
R06 | 8447 17 32 40 53 20 | 81 50 63 45 49
R07 | 6262 20 18 44 53 18 | 49 52 64 37 41
XR08 | 6976 --- 29 55 36 27 | --- 41 71 28 42
XR10 | 9550 19 18 --- 58 22 | 32 31 --- 27 25
XR14 | 4078 18 20 --- 33 16 | 30 30 --- 32 25
R18 |16650 60 63 70 73 37 | 151 163 220 116 163
R19 | 5045 30 23 54 30 19 | 71 89 98 48 70
XR21 |12274 --- 13 --- --- 0 | --- 344 --- --- 296
R22 |13493 31 27 55 67 24 | 53 63 108 83 61
R23 | 5795 24 43 479 72 32 | 77 43 179 98 59
XR24 |15832 180 175 --- 52 113 | 82 192 --- 65 107
------+-------------------------------+---------------------------
RMS |15480 31 35 179 55 |T 63 95 107 66 80
WRMS |15480 25 32 63 55 |NE 63 95 107 66 80
MEDI | 8447 24 27 55 53 |MD 53 52 97 45 49
Table 3.1424.3 GPS week: 1424 Day: 3 MJD: 54215
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
XR01 |14318 --- 194 --- 130 158 | --- 283 --- 134 153
R03 |47332 27 76 48 42 29 | 52 36 67 49 44
R04 | 7998 27 67 46 25 25 | 45 89 84 34 45
R06 |11682 118 87 37 60 44 | 141 119 38 21 55
R07 | 5932 43 19 50 22 21 | 34 52 38 41 26
R08 | 6243 100 79 35 48 38 | 34 40 92 68 58
XR10 |12202 18 32 --- 30 20 | 31 36 --- 30 23
XR14 | 5432 21 27 --- 22 16 | 32 29 --- 36 27
R18 |10200 57 60 67 62 36 | 129 122 127 117 113
R19 | 6351 56 34 22 22 19 | 68 56 72 49 53
R22 | 4523 61 66 53 61 34 | 41 55 60 58 34
R23 | 6509 23 64 432 52 35 | 76 50 152 97 69
------+-------------------------------+---------------------------
RMS |17391 65 65 150 47 |T 62 80 81 120 58
WRMS |17391 62 60 52 47 |NE 62 80 81 120 58
MEDI | 6509 43 64 48 42 |MD 45 55 72 49 45
Table 3.1424.4 GPS week: 1424 Day: 4 MJD: 54216
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 8107 137 102 192 78 67 | 71 108 113 84 54
R03 |55626 91 60 49 11 28 | 50 44 70 49 41
R04 | 5880 19 74 74 34 29 | 57 72 65 45 37
R06 |14394 137 75 65 29 41 | 99 101 70 36 42
R07 | 3541 20 32 60 15 17 | 32 50 60 27 30
R08 | 8122 76 45 61 20 26 | 22 47 87 39 36
XR10 | 2159 32 47 --- 25 23 | 32 31 --- 30 27
XR14 | 6752 23 28 --- 22 17 | 42 38 --- 30 31
R18 |11526 66 71 91 26 33 | 161 129 155 60 134
R19 | 4918 43 49 29 23 19 | 67 91 81 48 57
R21 | 8457 30 55 49 19 21 | 32 81 41 381 141
R22 | 2391 103 73 116 44 43 | 51 112 119 71 70
R23 | 5895 54 40 427 24 25 | 92 41 156 61 60
------+-------------------------------+---------------------------
RMS |18462 82 64 155 34 |T 62 72 92 73 58
WRMS |18462 77 50 74 34 |NE 62 72 92 73 58
MEDI | 6752 54 55 65 24 |MD 51 72 81 48 42
Table 3.1424.5 GPS week: 1424 Day: 5 MJD: 54217
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 8746 65 42 61 24 26 | 40 95 85 33 55
R03 |18308 44 38 45 20 20 | 33 45 72 29 31
R04 | 4400 24 53 35 10 18 | 50 48 53 52 44
R06 |15151 137 113 63 52 51 | 147 100 72 45 56
R07 | 4048 38 32 52 25 20 | 40 46 76 37 28
R08 |13644 34 16 34 13 13 | 41 53 62 36 41
XR10 | 4384 28 35 --- 16 17 | 29 32 --- 21 20
XR14 | 5226 32 24 --- 18 16 | 36 35 --- 31 26
R18 |14530 133 71 65 37 42 | 166 194 184 128 188
R19 | 6564 36 43 45 25 20 | 58 72 102 61 65
R21 | 6402 20 53 46 23 21 | 30 83 47 325 72
R22 | 1491 71 47 83 40 33 | 51 55 74 66 41
R23 | 3930 54 47 439 17 26 | 53 76 150 59 56
------+-------------------------------+---------------------------
RMS |10340 71 56 142 28 |T 59 71 88 71 55
WRMS |10340 47 44 54 28 |NE 59 71 88 71 55
MEDI | 6402 38 43 52 23 |MD 41 55 74 45 44
Table 3.1424.6 GPS week: 1424 Day: 6 MJD: 54218
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 7535 51 38 64 23 25 | 54 88 68 54 72
R03 | 4118 38 37 102 20 30 | 32 49 132 48 53
R04 | 5405 33 30 36 29 18 | 46 68 78 48 47
R06 | 1285 54 84 81 46 37 | 83 75 103 44 55
R07 | 4675 16 96 65 45 33 | 33 58 55 30 29
R08 |14688 19 31 94 28 27 | 42 61 51 51 44
XR10 | 3246 50 41 --- 24 26 | 41 50 --- 25 29
XR14 | 5092 24 22 --- 20 15 | 39 44 --- 47 39
R18 |13341 103 76 38 48 39 | 208 219 228 135 225
R19 |10806 31 38 31 22 17 | 70 88 104 69 74
R21 | 5259 62 58 46 24 26 | 30 71 56 353 94
R22 | 4541 79 115 49 33 40 | 61 56 92 63 55
R23 | 2926 66 73 446 25 37 | 46 64 208 54 45
------+-------------------------------+---------------------------
RMS | 7942 56 67 148 32 |T 60 76 106 78 66
WRMS | 7942 43 54 69 32 |NE 60 76 106 78 66
MEDI | 5092 50 41 64 25 |MD 46 64 92 51 53
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