[IGSREPORT-15280] Wk 1433 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Jul 12 05:07:20 PDT 2007
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IGS Electronic Report 12 Jul 05:07:32 PDT 2007 Message Number 15280
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1433 (Jun 24, 2007 - Jun 30, 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 2.1433.
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:
igl1433[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1433 in the SP3 format.
igl14337.sum Combination Report for GPS Week 1433.
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 | 1076.0 ns
1 | 1086.7 ns
2 | 1100.9 ns
3 | 1114.9 ns
4 | 1095.1 ns
5 | 1103.8 ns
6 | 1085.3 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 | R23 R24
1 | COD | R15
1 | ESX | R23 R24
2 | COD | R15
2 | ESX | R23 R24
3 | COD | R15
3 | ESX | R19 R23 R24
4 | COD | R15
4 | ESX | R23 R24
5 | COD | R15
5 | ESX | R03 R04 R18 R19 R21 R23 R24
6 | COD | R15
6 | ESX | 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 1.1433, 1a.1433).
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 2.1433.0-6)
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 3.1433.0-6).
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 1433 summary. (Jun 24, 2007 - Jun 30, 2007)
Table 1.1433.a GPS week : 1433 MJD: 54275.0-54281.0
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 58| -2 2 -24 -37 40 155 .05 74 57 | 0 282 3842 4060
| 3 5 12 84 63 109 .23 | 0 712
cod 169| 2 -5 8 79 -40 0 .00 64 47 | --- --- --- ---
| 4 6 6 83 75 105 .15 | --- ---
esx 47| -3 2 6 -17 -6 70 -.16 4147 79 | -494864 -8287 294163 300096
| 10 9 9 151 186 297 .35 | 512819 17839
iac n/a| -1 2 10 -30 32 -163 .11 55 55 | 499595 -4703 295546 303288
| 5 5 18 61 60 131 .12 | 1024487 10099
Table 1.1433.b GPS week : 1433 MJD: 54275.0-54281.0
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
------+------------------------------------+------------------------------------------
R01E | 32 27 24 24 26 30 47 |
R02E | --- --- --- --- --- 0 --- |
R03E | 34 21 22 54 60 33 28 |
R04E | 36 28 23 25 44 30 22 |
R06E | 30 42 29 31 54 32 25 |
R07E | 18 20 29 19 21 19 31 |
R08E | 21 21 19 26 28 18 24 |
R10E | 25 27 27 21 34 30 25 |
R14E | 17 23 23 16 23 24 30 |
R19 | 0 0 0 305 64 71 31 |
R21 | 29 43 41 36 49 46 43 |
R22 | 0 0 0 0 0 0 0 |
R23 | 30 29 34 55 50 53 44 |
R24 | 25 21 21 28 30 37 31 |
Table 1.1433.c GPS week : 1433 MJD: 54275.0-54281.0
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 1433 0 | -129 84 -689 4878 482 -337800 101.2 7256 7256 | 1075995 0
brd 1433 1 | -364 -151 -589 -1880 -2676 -343700 96.0 7098 7098 | 1086669 0
brd 1433 2 | 846 -132 -790 -6662 -6555 -335300 93.8 8544 8544 | 1100897 0
brd 1433 3 | 55 -205 -453 1863 -2104 -348300 92.9 7307 7307 | 1114869 0
brd 1433 4 | -13 511 -672 -11120 -5127 -359400 72.0 11300 11300 | 1095144 0
brd 1433 5 | -274 -397 -458 -5193 -4180 -322500 90.1 8547 8547 | 1103800 0
brd 1433 6 | -93 18 -875 -2074 1649 -334700 90.1 7744 7744 | 1085281 0
-------------+------------------------------------------------------------+----------------
brd 1433 mean| 3 -38 -647 -2883 -2644 -340242 90.9 8256 8256 | 1094665 0
brd 1433 sdev| 398 288 159 5352 2952 11689 9.2 1468 1468 | 13110 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 2.1433.0 GPS week: 1433 Day: 0 MJD: 54275
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 58| -6 -2 -15 98 30 263 -.03 46 39 | 0 -41 3628 3774
cod 169| 1 -2 9 4 -50 -22 .10 47 42 | --- --- --- ---
esx 47| 2 8 8 -109 115 -333 -.75 217 89 | -537698 -5449 11910 19951
iac n/a| 0 5 0 15 -62 -69 .26 36 36 | 1076430 -2081 10704 19928
Table 2.1433.1 GPS week: 1433 Day: 1 MJD: 54276
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 58| 0 -1 -6 -25 50 305 .05 41 33 | 0 474 4724 4898
cod 169| 4 0 9 35 80 -19 -.03 46 32 | --- --- --- ---
esx 47| -6 5 -9 200 17 -190 .04 235 72 | 50320 -41359 9529 18734
iac n/a| 0 -1 -10 -83 -14 -153 .13 40 40 | 1098956 -15193 9578 18479
Table 2.1433.2 GPS week: 1433 Day: 2 MJD: 54277
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 58| 0 1 -20 -54 55 -11 .18 52 46 | 0 -379 4015 4266
cod 169| 0 -2 11 16 -60 160 -.12 42 42 | --- --- --- ---
esx 47| -4 3 15 -65 119 86 -.36 242 62 | 1086 -15472 11132 18373
iac n/a| 7 -4 -10 37 30 -255 .20 40 40 | 1097673 -3717 10928 18265
Table 2.1433.3 GPS week: 1433 Day: 3 MJD: 54278
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 58| -7 -5 -29 -115 -66 121 -.13 175 96 | 0 110 4366 4547
cod 169| 0 -3 3 75 -154 -24 .10 158 67 | --- --- --- ---
esx 47| 14 4 4 94 45 71 .21 >>>> 53 | 22236 17687 17892 28128
iac n/a| -10 0 18 -55 12 -78 -.06 103 103 | 1113451 14749 16485 29294
Table 2.1433.4 GPS week: 1433 Day: 4 MJD: 54279
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 58| -3 9 -26 -127 112 70 -.17 83 69 | 0 64 3012 3205
cod 169| 10 -4 3 90 21 83 .10 53 44 | --- --- --- ---
esx 47| -8 -18 20 -244 -393 598 -.40 254 95 | -999999 -320 8684 15491
iac n/a| -7 12 10 10 61 -327 .04 67 67 | 1110657 -14275 21132 37053
Table 2.1433.5 GPS week: 1433 Day: 5 MJD: 54280
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 58| 2 5 -27 -85 -9 194 -.09 48 48 | 0 -46 3027 3311
cod 169| 6 -18 20 251 -30 4 .12 68 61 | --- --- --- ---
esx 47| -20 10 1 89 133 47 -.07 509 111 | -999999 -8980 999999 999999
iac n/a| -2 2 39 -132 108 -285 .20 58 58 | -999999 -9334 999999 999999
Table 2.1433.6 GPS week: 1433 Day: 6 MJD: 54281
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 58| -4 8 -46 45 111 142 .50 72 71 | 0 1793 4125 4421
cod 169| -2 -9 0 85 -87 -181 -.27 36 40 | --- --- --- ---
esx 47| 1 2 4 -85 -83 213 .18 264 71 | -999999 -4117 999999 999999
iac n/a| 0 0 23 -1 90 28 -.00 43 43 | -999999 -3074 999999 999999
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 3.1433.0 GPS week: 1433 Day: 0 MJD: 54275
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 9929 21 79 54 52 32 | 84 77 86 66 69
R03 |10539 48 38 121 46 34 | 196 199 249 240 220
R04 | 6851 62 34 135 37 36 | 60 53 102 71 51
R06 | 7477 33 77 76 26 30 | 38 70 51 35 38
R07 | 4672 25 32 37 30 17 | 49 49 57 40 41
R08 | 5641 40 38 54 24 21 | 59 80 85 65 67
XR10E | 7267 33 38 --- 35 25 | 68 65 --- 82 70
XR14E | 7980 26 21 --- 22 16 | 38 54 --- 51 44
XR19 | ---- --- 7 --- --- 0 | --- 651 --- --- 632
R21 | 6452 68 25 84 26 28 | 241 291 354 267 270
XR22 | ---- --- 6 --- --- 0 | --- 272 --- --- 270
R23 | 4062 56 19 435 42 30 | 68 40 382 45 35
R24 | 7036 40 37 425 27 24 | 43 72 446 40 48
------+-------------------------------+---------------------------
RMS | 7255 46 47 217 36 |T 85 151 201 91 142
WRMS | 7255 39 42 89 36 |NE 93 168 201 96 158
MEDI | 7036 40 34 84 30 |MD 60 72 102 65 67
Table 3.1433.1 GPS week: 1433 Day: 1 MJD: 54276
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 7684 28 58 69 35 27 | 58 86 71 46 58
R03 |15131 26 27 57 43 21 | 183 208 225 205 203
R04 | 7764 52 33 47 59 28 | 85 89 96 58 78
R06 | 6016 30 77 143 41 41 | 41 67 88 38 35
R07 | 4257 34 15 54 40 20 | 45 44 79 62 51
R08 | 2822 40 34 37 30 20 | 45 77 82 56 60
XR10E | 5418 26 25 --- 57 27 | 36 40 --- 53 39
XR14E | 4898 31 35 --- 30 22 | 45 45 --- 59 47
XR19 | ---- --- 8 --- --- 0 | --- 385 --- --- 435
R21 | 2328 67 59 140 47 43 | 144 201 188 119 159
XR22 | ---- --- 7 --- --- 0 | --- 182 --- --- 182
R23 | 5339 51 39 465 28 29 | 80 47 187 42 48
R24 | 2995 20 33 478 33 21 | 39 44 268 46 35
------+-------------------------------+---------------------------
RMS | 7098 41 46 235 40 |T 72 116 142 71 110
WRMS | 7098 33 32 72 40 |NE 80 130 142 74 122
MEDI | 5339 31 33 69 40 |MD 45 77 96 56 58
Table 3.1433.2 GPS week: 1433 Day: 2 MJD: 54277
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 5996 46 50 37 28 23 | 66 94 100 75 79
R03E |19754 39 30 46 38 22 | 179 179 176 190 181
R04 | 7864 38 29 56 36 23 | 58 53 83 54 52
R06 | 9557 62 40 43 53 28 | 44 45 89 59 42
R07 | 4092 36 56 50 50 28 | 58 53 78 92 62
R08 | 2287 30 20 48 31 19 | 51 52 85 51 53
XR10E | 5237 32 33 --- 44 26 | 44 59 --- 67 54
XR14E | 9481 35 36 --- 25 22 | 47 54 --- 51 48
XR19 | ---- --- 11 --- --- 0 | --- 380 --- --- 318
R21 | 3594 102 52 85 43 40 | 167 257 284 177 216
XR22 | ---- --- 12 --- --- 0 | --- 271 --- --- 269
R23 | 5437 39 56 474 46 34 | 66 56 304 81 54
R24 | 3623 39 27 532 24 21 | 49 42 391 45 36
------+-------------------------------+---------------------------
RMS | 8543 52 42 242 40 |T 75 122 176 85 112
WRMS | 8543 46 42 62 40 |NE 69 130 176 79 118
MEDI | 5437 39 33 50 38 |MD 58 56 100 67 54
Table 3.1433.3 GPS week: 1433 Day: 3 MJD: 54278
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 6248 41 49 47 27 23 | 37 74 106 59 61
R03E |14855 64 115 113 81 54 | 274 224 259 292 253
R04 | 2808 32 47 57 39 25 | 81 86 96 39 65
R06 | 9377 46 41 51 66 30 | 37 47 63 56 44
R07 | 3249 27 26 51 19 18 | 35 54 78 56 47
R08 | 3331 40 47 60 34 26 | 87 97 108 78 85
XR10E | 7316 29 31 --- 27 20 | 71 84 --- 111 87
XR14E | 8756 23 21 --- 23 16 | 41 51 --- 56 50
R19 |10234 534 456 >>>> 290 304 | 169 448 9999 268 259
R21 | 3864 81 81 38 33 35 | 171 269 286 227 213
XR22 | ---- --- 11 --- --- 0 | --- 197 --- --- 196
R23 | 5300 47 113 590 69 55 | 52 109 426 94 61
R24 | 2988 53 26 512 34 28 | 52 65 441 95 62
------+-------------------------------+---------------------------
RMS | 7306 175 158 >>>> 103 |T 92 138 207 119 114
WRMS | 7306 96 67 53 103 |NE 80 144 200 108 109
MEDI | 5300 41 47 57 34 |MD 52 86 108 78 65
Table 3.1433.4 GPS week: 1433 Day: 4 MJD: 54279
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 7783 50 43 51 41 26 | 73 86 145 77 78
R03E |25098 149 79 93 96 60 | 94 204 198 265 151
R04 | 4003 60 43 170 56 43 | 51 89 316 58 71
R06 | 6195 64 41 210 86 54 | 53 66 200 72 60
R07E | 3262 29 32 55 37 21 | 55 83 99 69 68
XR08E | 6843 25 36 --- 49 27 | 76 86 --- 66 74
XR10E |10676 48 34 --- 60 33 | 75 101 --- 86 78
XR14E | 7447 43 17 --- 38 23 | 64 58 --- 72 60
XR19 | 3275 105 84 --- 85 63 | 111 262 --- 271 247
XR21 | 2743 106 27 --- 74 49 | 100 149 --- 194 148
XR22 | ---- --- 10 --- --- 0 | --- 181 --- --- 182
R23 | 3155 91 63 548 62 50 | 52 69 357 59 46
XR24 | 3221 61 34 --- 32 29 | 56 79 --- 65 64
------+-------------------------------+---------------------------
RMS |11295 83 53 254 67 |T 71 116 219 112 102
WRMS |11295 69 44 95 67 |NE 70 127 291 119 116
MEDI | 4003 60 36 93 56 |MD 64 86 198 72 74
Table 3.1433.5 GPS week: 1433 Day: 5 MJD: 54280
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 7616 28 38 123 32 30 | 64 64 125 63 60
XR02E | ---- --- --- 16 --- 0 | --- --- 11 --- 20
R03E |18855 37 61 266 44 33 | 181 219 230 229 214
R04E | 4014 34 51 860 47 30 | 103 70 625 67 79
R06E |12622 39 73 55 59 31 | 54 90 81 71 47
R07E | 4205 14 36 53 41 19 | 42 60 58 60 46
R08E | 3830 17 31 54 37 18 | 60 53 69 72 52
XR10E | 9905 32 52 --- 45 29 | 106 103 --- 77 89
XR14 | 7171 27 38 --- 41 24 | 57 68 --- 70 60
R19 | 3702 99 119 321 76 70 | 73 280 9999 156 173
R21 | 6517 44 52 983 97 45 | 96 109 759 161 108
XR22 | ---- --- 23 --- --- 0 | --- 64 --- --- 66
R23 | 5706 61 103 620 61 53 | 49 83 355 28 32
R24 | 4519 45 62 551 51 36 | 51 68 370 60 51
------+-------------------------------+---------------------------
RMS | 8547 48 68 509 58 |T 78 102 268 92 78
WRMS | 8547 48 61 111 58 |NE 65 112 494 95 81
MEDI | 5706 34 52 266 45 |MD 60 70 125 70 60
Table 3.1433.6 GPS week: 1433 Day: 6 MJD: 54281
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 8052 90 33 182 31 47 | 50 64 100 69 54
R03E | 5290 62 37 44 53 28 | 170 178 216 197 182
R04E | 4152 60 24 32 34 21 | 64 73 213 66 68
R06E |19674 31 35 43 55 24 | 37 50 61 48 36
R07E | 2772 28 47 107 30 30 | 61 91 77 72 71
R08E | 2360 53 30 63 35 24 | 88 94 79 83 82
XR10 | 7399 58 28 --- 25 25 | 74 74 --- 62 67
XR14 | 8344 47 36 --- 47 30 | 60 58 --- 62 56
R19 | 2689 87 30 71 41 31 | 73 290 9999 204 260
R21 | 5088 106 35 125 56 43 | 150 205 352 240 202
XR22 | ---- --- 13 --- --- 0 | --- 203 --- --- 197
R23 | 5739 100 41 578 55 44 | 66 58 462 56 34
R24 | 4811 58 45 538 31 31 | 42 64 479 55 52
------+-------------------------------+---------------------------
RMS | 7743 72 36 264 43 |T 77 115 226 101 104
WRMS | 7743 71 40 71 43 |NE 77 136 431 113 124
MEDI | 5088 58 35 71 35 |MD 64 74 213 66 68
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