[IGSREPORT-15472] Wk 1442 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Sep 13 01:44:12 PDT 2007
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IGS Electronic Report 13 Sep 01:44:16 PDT 2007 Message Number 15472
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1442 (Aug 26, 2007 - Sep 01, 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 2.1442.
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:
igl1442[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1442 in the SP3 format.
igl14427.sum Combination Report for GPS Week 1442.
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 | 1152.8 ns
1 | 1181.0 ns
2 | 1184.8 ns
3 | 1132.8 ns
4 | 1087.8 ns
5 | 1105.8 ns
6 | 1151.3 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 | R15
0 | ESX | R10 R14 R23 R24
1 | COD | R15
1 | ESX | R10 R14 R23 R24
2 | COD | R15
2 | ESX | R10 R14 R23 R24
3 | COD | R15
3 | ESX | R10 R14 R23 R24
4 | COD | R15
4 | ESX | R10 R14 R23 R24
5 | COD | R15
5 | ESX | R10 R14 R23 R24
6 | COD | R15
6 | ESX | R10 R14 R23 R24
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 1.1442, 1a.1442).
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 2.1442.0-6)
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 3.1442.0-6).
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 1442 summary. (Aug 26, 2007 - Sep 01, 2007)
Table 1.1442.a GPS week : 1442 MJD: 54338.0-54344.0
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 -10 -14 30 -195 .00 41 36 | 0 286 4824 5116
| 5 3 6 32 45 125 .06 | 0 1386
cod 174| -1 -5 -8 28 9 175 -.06 47 41 | --- --- --- ---
| 5 6 8 40 85 149 .05 | --- ---
esx 40| 0 0 -10 44 -50 124 -.30 255 83 | -5834 0 14985 25052
| 8 10 13 166 97 298 .05 | 485861 22295
iac n/a| 0 6 21 -20 6 44 .12 36 36 | 1140165 -620 14339 24405
| 3 4 7 72 30 157 .10 | 35254 11365
mcc n/a| 0 0 84 91 48 1562 .31 157 157 | --- --- --- ---
| 17 7 16 192 65 564 .47 | --- ---
Table 1.1442.b GPS week : 1442 MJD: 54338.0-54344.0
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 | 35 31 24 33 21 20 19 |
R04 | 24 39 37 19 22 18 16 |
R06 | 24 20 21 31 34 29 30 |
R07 | 18 20 17 19 15 28 19 |
R08 | 28 16 23 18 19 38 25 |
R10 | 26 16 27 26 19 26 26 |
R14 | 17 18 27 29 21 19 31 |
R21 | 32 45 47 32 30 21 37 |
R23 | 34 30 39 37 34 38 48 |
R24 | 27 17 20 26 27 24 44 |
Table 1.1442.c GPS week : 1442 MJD: 54338.0-54344.0
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 1442 0 | 62 10 -835 1365 -3493 -349300 86.5 4778 4778 | 1152761 0
brd 1442 1 | -75 -268 -758 -1971 -2725 -344400 92.1 10250 10250 | 1181030 0
brd 1442 2 | -2 144 -271 -5155 -5773 -343100 81.3 13450 13450 | 1184800 0
brd 1442 3 | 327 727 -164 -510 -8759 -334200 106.1 9544 9544 | 1132754 0
brd 1442 4 | -146 183 -1423 -6321 -5447 -336000 95.5 8241 8241 | 1087771 0
brd 1442 5 | -196 103 -508 -5495 -3436 -326100 86.4 6061 6061 | 1105767 0
brd 1442 6 | 44 146 -509 -4862 -10640 -344000 74.3 5331 5331 | 1151349 0
-------------+------------------------------------------------------------+----------------
brd 1442 mean| 2 149 -638 -3278 -5753 -339585 88.9 8236 8236 | 1142318 0
brd 1442 sdev| 172 297 420 2919 2962 7885 10.3 3111 3111 | 36278 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 2.1442.0 GPS week: 1442 Day: 0 MJD: 54338
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 4 -7 -21 47 -278 .06 51 38 | 0 307 3440 3586
cod 174| -1 -10 -13 27 -52 131 -.04 40 37 | --- --- --- ---
esx 40| -7 7 -9 275 64 409 -.36 217 71 | 4126 -20729 15584 23186
iac n/a| 6 8 29 -145 -26 -77 .12 40 40 | 1157693 -11489 14666 21882
mcc n/a| -1 6 64 97 32 1585 .40 136 136 | --- --- --- ---
Table 2.1442.1 GPS week: 1442 Day: 1 MJD: 54339
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 0 -19 -42 63 -325 .07 50 42 | 0 749 4632 4921
cod 174| 0 -7 -6 14 34 15 .02 34 33 | --- --- --- ---
esx 40| -5 -12 -20 196 -190 298 -.35 259 84 | 12603 3670 14286 20301
iac n/a| -3 12 22 -42 -37 130 .21 40 40 | 1175775 10946 13531 19771
mcc n/a| 16 6 87 121 -75 2082 .22 203 203 | --- --- --- ---
Table 2.1442.2 GPS week: 1442 Day: 2 MJD: 54340
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| 3 1 -10 -20 63 -286 -.08 43 43 | 0 -815 5643 6025
cod 174| 8 -2 0 49 -89 52 -.14 45 49 | --- --- --- ---
esx 40| 5 0 -20 49 -93 561 -.22 264 70 | -999999 15734 14012 21375
iac n/a| -4 2 19 -25 21 182 .13 37 37 | 1177678 -796 13661 20420
mcc n/a| 8 3 80 127 13 2492 -.10 334 334 | --- --- --- ---
Table 2.1442.3 GPS week: 1442 Day: 3 MJD: 54341
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 -2 -4 22 0 -236 .01 27 26 | 0 754 5121 5420
cod 174| -2 4 -11 33 30 445 -.04 64 49 | --- --- --- ---
esx 40| 16 16 -22 57 38 -77 -.27 276 99 | 228374 38201 16772 25897
iac n/a| 3 3 23 36 43 199 -.06 40 40 | 1136751 4077 15746 24401
mcc n/a| 13 -6 89 -38 102 1256 -.03 163 163 | --- --- --- ---
Table 2.1442.4 GPS week: 1442 Day: 4 MJD: 54342
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 2 -13 -45 10 1 -.09 27 25 | 0 2873 5673 5870
cod 174| -7 -14 -19 -14 132 114 -.10 53 39 | --- --- --- ---
esx 40| 3 8 4 52 23 -207 -.26 247 93 | 586990 -24388 13616 30891
iac n/a| -1 9 28 11 0 48 .24 35 35 | 1095212 -14418 13846 29709
mcc n/a| -9 -2 82 17 115 785 .26 84 84 | --- --- --- ---
Table 2.1442.5 GPS week: 1442 Day: 5 MJD: 54343
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| -3 -3 -17 -29 78 -197 .02 41 38 | 0 -1264 4783 5128
cod 174| -2 0 -12 104 -80 168 -.06 50 41 | --- --- --- ---
esx 40| 0 -5 11 -114 -51 32 -.32 274 86 | -12787 2697 15968 29161
iac n/a| -1 4 16 77 16 69 .04 30 30 | 1091199 15371 14597 30945
mcc n/a| -33 -12 73 464 65 1320 1.32 143 143 | --- --- --- ---
Table 2.1442.6 GPS week: 1442 Day: 6 MJD: 54344
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| 3 3 -1 39 -48 -48 .01 46 39 | 0 -600 4478 4867
cod 174| -7 -7 3 -12 88 300 -.07 44 40 | --- --- --- ---
esx 40| -5 -7 -15 -207 -144 -142 -.33 244 75 | 139850 -15184 14660 24558
iac n/a| 0 2 8 -56 31 -242 .13 31 31 | 1146851 -8036 14332 23712
mcc n/a| 9 -1 116 -149 83 1419 .12 34 34 | --- --- --- ---
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 3.1442.0 GPS week: 1442 Day: 0 MJD: 54338
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4245 98 42 27 49 --- 34 | 120 50 71 40 --- 56
R04 | 3375 39 36 56 38 --- 24 | 29 46 50 58 --- 37
R06 | 4652 25 25 59 49 --- 23 | 23 31 39 51 --- 27
R07 | 3103 20 27 50 25 43 18 | 26 32 49 35 39 25
R08 | 6861 39 50 55 46 --- 27 | 33 33 57 37 --- 30
XR10 | 4172 34 35 --- 40 --- 26 | 22 54 --- 43 --- 30
XR14 | 3209 26 25 --- 22 --- 17 | 42 49 --- 51 --- 45
R21 | 2715 56 37 90 33 --- 31 | 56 65 53 50 --- 46
R23 | 4712 51 51 397 40 --- 33 | 43 69 132 74 --- 55
R24 | 6730 40 40 447 33 188 26 | 69 108 160 79 82 83
------+------------------------------------+--------------------------------
RMS | 4778 51 40 217 40 136 |T 46 53 76 51 60 43
WRMS | 4778 38 37 71 40 136 |NE 46 53 76 51 60 43
MEDI | 4172 39 36 56 38 43 |MD 33 49 53 50 39 37
Table 3.1442.1 GPS week: 1442 Day: 1 MJD: 54339
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4331 92 35 44 34 --- 30 | 68 65 54 54 --- 49
R04 | 3870 57 60 45 85 --- 39 | 23 30 51 81 --- 31
R06 |27056 22 32 49 36 --- 20 | 35 57 60 47 --- 37
R07 | 2396 29 20 72 24 46 20 | 19 45 59 34 41 28
R08 | 6881 32 24 33 25 --- 16 | 32 35 55 28 --- 25
R10 | 3997 25 21 431 22 --- 16 | 20 34 155 42 --- 30
XR14 | 3856 34 20 --- 21 --- 17 | 29 34 --- 30 --- 28
R21 | 3570 64 39 183 27 --- 44 | 34 49 77 37 --- 30
R23 | 7365 51 35 422 42 --- 30 | 26 55 112 63 --- 39
R24 | 6632 36 20 440 15 283 16 | 47 46 89 53 148 44
------+------------------------------------+--------------------------------
RMS |10251 50 34 259 40 203 |T 33 45 79 46 94 34
WRMS |10251 42 33 84 40 203 |NE 33 45 79 46 94 34
MEDI | 3997 34 24 72 25 46 |MD 29 45 60 42 41 30
Table 3.1442.2 GPS week: 1442 Day: 2 MJD: 54340
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6140 42 40 47 37 --- 23 | 41 63 57 48 --- 41
R04 | 3646 54 71 94 54 --- 37 | 27 59 72 71 --- 38
R06 |36423 30 44 51 27 --- 20 | 33 52 77 57 --- 43
R07 | 1962 31 28 40 24 49 17 | 21 42 32 35 72 28
R08 | 7336 34 50 40 36 --- 23 | 26 46 58 26 --- 21
R10 | 2942 38 39 413 37 --- 27 | 33 49 93 40 --- 20
XR14 | 3671 37 36 --- 38 --- 26 | 68 53 --- 89 --- 71
R21 | 4268 37 48 219 28 --- 47 | 64 69 136 78 --- 72
R23 | 9792 70 36 403 50 --- 39 | 39 68 145 81 --- 51
R24 | 8378 32 32 481 20 470 20 | 48 78 173 62 296 58
------+------------------------------------+--------------------------------
RMS |13450 43 45 264 37 334 |T 40 57 93 58 184 44
WRMS |13450 43 49 70 37 334 |NE 40 57 93 58 184 44
MEDI | 4268 37 39 94 36 49 |MD 33 53 77 57 72 41
Table 3.1442.3 GPS week: 1442 Day: 3 MJD: 54341
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8636 29 46 136 44 --- 32 | 43 41 107 28 --- 25
XR04 | 3742 22 40 --- 24 --- 19 | 22 54 --- 35 --- 23
R06 |19800 26 97 56 49 --- 30 | 47 119 108 57 --- 60
R07 | 2111 19 53 62 18 90 19 | 30 62 62 23 46 25
R08 | 8172 26 25 29 38 --- 17 | 39 32 48 31 --- 28
R10 | 4274 30 51 404 37 --- 26 | 31 41 152 40 --- 31
XR14 | 4141 36 26 --- 50 --- 28 | 31 55 --- 73 --- 43
R21 | 2880 18 83 130 22 --- 31 | 42 66 65 41 --- 33
R23 |10381 37 70 417 61 --- 37 | 76 67 139 74 --- 60
R24 | 7510 25 54 478 39 213 25 | 71 94 182 85 338 72
------+------------------------------------+--------------------------------
RMS | 9543 27 64 276 40 163 |T 43 63 107 48 192 40
WRMS | 9543 26 49 99 40 163 |NE 43 63 107 48 192 40
MEDI | 4274 26 51 130 38 90 |MD 39 55 107 40 46 31
Table 3.1442.4 GPS week: 1442 Day: 4 MJD: 54342
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7046 29 33 65 29 --- 21 | 33 47 57 47 --- 36
R04 | 3546 24 37 69 35 --- 22 | 35 34 46 38 --- 24
R06 |18067 29 101 84 43 --- 34 | 23 129 82 50 --- 37
R07 | 2211 16 39 36 22 84 15 | 18 48 41 31 41 20
R08 | 8282 23 48 40 32 --- 19 | 40 46 62 45 --- 29
R10 | 4878 22 32 411 29 --- 19 | 23 41 131 40 --- 29
R14 | 3988 18 41 407 33 --- 20 | 57 47 103 61 --- 53
R21 | 5460 22 71 103 30 --- 29 | 54 119 108 76 --- 74
R23 | 8918 44 36 432 55 --- 33 | 47 57 128 68 --- 42
XR24 | 8975 33 44 --- 41 174 27 | 35 76 --- 69 177 50
------+------------------------------------+--------------------------------
RMS | 8240 27 53 247 35 84 |T 36 64 84 52 109 39
WRMS | 8240 25 39 93 35 84 |NE 36 64 84 52 109 39
MEDI | 5460 23 39 84 32 84 |MD 35 47 82 47 41 36
Table 3.1442.5 GPS week: 1442 Day: 5 MJD: 54343
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5024 35 40 39 28 --- 20 | 44 36 59 20 --- 21
R04 | 1823 27 29 40 29 --- 17 | 20 43 57 32 --- 25
R06 | 8885 29 36 99 35 --- 28 | 43 40 102 35 --- 41
R07 | 2330 32 89 27 25 57 27 | 19 96 30 21 32 28
R08 | 7460 75 55 113 24 --- 38 | 57 54 110 41 --- 41
R10 | 4875 28 54 406 29 --- 26 | 28 38 112 40 --- 26
R14 | 4146 27 36 364 20 --- 19 | 37 62 57 48 --- 46
R21 | 7245 25 37 54 32 --- 20 | 25 44 102 42 --- 33
R23 | 5349 66 51 425 43 --- 38 | 47 47 120 61 --- 34
R24 | 8756 34 42 494 29 195 24 | 40 75 155 54 90 50
------+------------------------------------+--------------------------------
RMS | 6060 41 50 274 30 143 |T 36 53 90 39 61 34
WRMS | 6060 38 41 86 30 143 |NE 36 53 90 39 61 34
MEDI | 5024 29 40 99 29 57 |MD 37 44 102 40 32 33
Table 3.1442.6 GPS week: 1442 Day: 6 MJD: 54344
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2983 38 32 33 29 --- 19 | 40 49 48 33 --- 32
R04 | 4191 18 30 56 19 --- 16 | 20 32 57 39 --- 24
R06 |12081 40 24 144 26 --- 29 | 39 55 69 45 --- 36
R07 | 2343 32 32 47 31 34 19 | 57 69 30 35 32 44
R08 | 3815 40 53 66 26 --- 24 | 31 36 41 30 --- 20
R10 | 4007 31 37 407 39 --- 26 | 26 44 138 64 --- 44
R14 | 2702 42 54 368 33 --- 30 | 70 88 55 54 --- 64
R21 | 5637 55 31 181 24 --- 36 | 53 48 98 30 --- 39
R23 | 2857 84 76 415 47 --- 48 | 78 54 185 61 --- 41
XR24 | 5681 94 46 --- 46 289 43 | 47 56 --- 63 159 49
------+------------------------------------+--------------------------------
RMS | 5331 46 44 244 31 34 |T 46 53 80 45 95 39
WRMS | 5331 39 40 75 31 34 |NE 46 53 80 45 95 39
MEDI | 3815 40 32 144 29 34 |MD 40 49 57 39 32 39
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