[IGSREPORT-15303] Wk 1434 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Jul 19 23:07:49 PDT 2007
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IGS Electronic Report 19 Jul 23:07:55 PDT 2007 Message Number 15303
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1434 (Jul 01, 2007 - Jul 07, 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 2.1434.
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:
igl1434[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1434 in the SP3 format.
igl14347.sum Combination Report for GPS Week 1434.
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 | 1119.5 ns
1 | 1057.7 ns
2 | 1121.0 ns
3 | 1122.3 ns
4 | 1115.1 ns
5 | 1102.7 ns
6 | 1092.6 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
----+--------+---------------
5 | BKG | 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 1.1434, 1a.1434).
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 2.1434.0-6)
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 3.1434.0-6).
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 1434 summary. (Jul 01, 2007 - Jul 07, 2007)
Table 1.1434.a GPS week : 1434 MJD: 54282.0-54288.0
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| -2 3 -22 -30 48 117 .09 57 48 | 0 183 3746 3945
| 3 5 5 39 17 221 .23 | 0 523
cod 168| 4 -1 4 26 -39 88 -.03 74 41 | --- --- --- ---
| 8 4 9 63 56 138 .11 | --- ---
esx 43| -5 -1 26 96 5 -116 -.27 196 71 | 14620 1829 10220 18925
| 5 7 26 113 154 231 .24 | 33570 13630
iac n/a| -1 0 12 -87 -52 -221 .02 75 75 | 1104931 -317 10173 19625
| 3 5 10 48 48 115 .18 | 21669 6453
Table 1.1434.b GPS week : 1434 MJD: 54282.0-54288.0
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 | 23 28 35 43 23 20 33 |
R03E | 62 65 59 26 26 22 29 |
R04E | 26 25 17 17 25 17 22 |
R06E | 26 21 24 23 30 28 24 |
R07E | 21 22 27 35 22 22 29 |
R08E | 26 24 18 18 31 27 28 |
R10 | 28 21 24 14 36 32 35 |
R14 | 31 18 25 20 17 19 18 |
R15 | 0 0 0 0 0 0 0 |
R19 | 172 194 55 62 2695 --- --- |
R21 | 46 31 39 39 36 44 30 |
R22 | 0 0 0 0 0 0 0 |
R23 | 85 89 75 74 89 83 77 |
R24 | 89 96 71 42 25 46 0 |
Table 1.1434.c GPS week : 1434 MJD: 54282.0-54288.0
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 1434 0 | 568 -328 -862 -4486 3171 -345400 87.9 5483 5483 | 1119538 0
brd 1434 1 | -165 427 -452 -3121 1039 -357900 95.8 6970 6970 | 1057736 0
brd 1434 2 | -34 84 -43 -10150 -2356 -359600 109.7 5338 5338 | 1120968 0
brd 1434 3 | 532 156 -680 -6470 13040 -355300 97.1 7632 7632 | 1122256 0
brd 1434 4 | 46 -58 -154 3204 6830 -352600 90.9 7118 7118 | 1115054 0
brd 1434 5 | 54 -103 -361 479 5002 -348100 99.9 5771 5771 | 1102743 0
brd 1434 6 | -716 611 -488 -3565 5423 -345400 99.9 6051 6051 | 1092583 0
-------------+------------------------------------------------------------+----------------
brd 1434 mean| 40 112 -434 -3444 4592 -352042 97.3 6337 6337 | 1104411 0
brd 1434 sdev| 436 321 283 4376 4833 5861 7.1 896 896 | 23294 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 2.1434.0 GPS week: 1434 Day: 0 MJD: 54282
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 3 -29 -83 37 329 .46 82 53 | 0 162 3541 3743
cod 168| 7 -5 -13 -22 7 -22 -.19 148 46 | --- --- --- ---
esx 43| 3 -6 54 318 -64 -155 .04 205 83 | 84528 26067 10420 18381
iac n/a| 0 11 18 -150 -76 -193 -.34 96 96 | 1115526 11846 9875 18001
Table 2.1434.1 GPS week: 1434 Day: 1 MJD: 54283
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| -4 0 -23 -2 74 193 .17 85 64 | 0 135 4475 4709
cod 168| 13 6 3 -74 -139 -31 .11 171 45 | --- --- --- ---
esx 43| -13 -7 34 19 159 -29 -.18 197 78 | -2500 -19417 10432 17132
iac n/a| -7 -1 14 -124 -41 -230 -.05 115 115 | 1063574 -5794 10152 19561
Table 2.1434.2 GPS week: 1434 Day: 2 MJD: 54284
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 -30 -15 20 315 .34 65 54 | 0 192 4642 4982
cod 168| -1 0 12 28 22 -11 -.14 37 38 | --- --- --- ---
esx 43| -4 8 61 47 155 -506 -.67 233 81 | 18708 -3181 14261 25855
iac n/a| 2 -5 -7 -10 -48 -292 .15 75 75 | 1118993 -907 14056 26297
Table 2.1434.3 GPS week: 1434 Day: 3 MJD: 54285
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 3 -14 8 61 -230 -.07 43 47 | 0 1281 5020 5182
cod 168| 5 3 1 19 -16 237 -.07 39 36 | --- --- --- ---
esx 43| -11 -8 34 136 -287 -16 -.30 222 69 | -5647 5550 11632 22971
iac n/a| 2 -2 3 -83 -35 -24 .09 59 59 | 1129502 -7586 13059 25288
Table 2.1434.4 GPS week: 1434 Day: 4 MJD: 54286
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 -3 -19 -29 52 286 -.03 36 34 | 0 -365 3409 3603
cod 168| -12 -1 11 41 -90 26 -.03 51 41 | --- --- --- ---
esx 43| -1 8 -8 -14 9 -290 -.39 159 54 | -19176 129 7654 16498
iac n/a| -3 5 19 -113 -123 -392 .15 67 67 | 1110186 1854 7463 15934
Table 2.1434.5 GPS week: 1434 Day: 5 MJD: 54287
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 7 -20 -88 41 32 -.10 44 39 | 0 39 2844 3004
cod 168| 11 -4 11 125 -28 103 .08 37 39 | --- --- --- ---
esx 43| -7 -6 5 33 83 219 -.37 176 48 | 11203 5957 7872 12517
iac n/a| -2 -3 18 -87 35 -266 .01 57 57 | 1104673 1783 7726 14081
Table 2.1434.6 GPS week: 1434 Day: 6 MJD: 54288
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 13 -17 -2 50 -101 -.11 47 42 | 0 -159 2291 2395
cod 168| 6 -4 3 64 -31 314 .00 36 38 | --- --- --- ---
esx 43| -5 2 2 135 -19 -35 -.01 181 81 | 15229 -2302 9275 19123
iac n/a| -2 0 17 -43 -75 -153 .16 54 54 | 1092067 -3417 8886 18214
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 3.1434.0 GPS week: 1434 Day: 0 MJD: 54282
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 6141 45 23 50 38 22 | 41 46 76 53 39
R03E | 6794 136 111 85 66 61 | 132 42 105 50 59
R04E | 4147 26 26 82 51 25 | 74 93 121 75 81
R06E | 6788 39 30 62 55 26 | 57 45 70 77 55
R07E | 2863 34 25 57 36 20 | 23 36 56 37 26
R08E | 3501 43 39 80 27 25 | 127 128 116 113 121
XR10 | 7571 41 30 --- 45 27 | 29 35 --- 55 35
XR14 | 7518 40 30 --- 55 30 | 28 31 --- 37 28
XR15 | ---- --- 10 --- --- 0 | --- 9999 --- --- 9999
R19 | 7703 156 440 294 228 172 | 175 500 9999 89 9999
R21 | 4665 99 77 90 44 45 | 162 127 108 106 111
XR22 | ---- --- 10 --- --- 0 | --- 209 --- --- 209
R23 | 5892 63 33 356 136 85 | 41 71 369 77 48
R24 | 4140 52 51 414 78 88 | 39 9999 94 26 9999
------+-------------------------------+---------------------------
RMS | 5482 82 148 205 96 |T 77 113 123 66 73
WRMS | 5482 53 46 83 96 |NE 79 162 190 65 86
MEDI | 5892 43 30 82 51 |MD 41 46 105 55 55
Table 3.1434.1 GPS week: 1434 Day: 1 MJD: 54283
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 6701 42 54 65 38 28 | 54 44 78 35 35
R03E | 7705 133 92 115 91 64 | 104 41 102 70 60
R04E | 4752 38 34 47 54 24 | 33 45 64 46 36
R06E | 5150 28 23 53 45 20 | 37 44 31 50 34
R07E | 4313 25 28 56 49 21 | 27 52 38 49 34
R08E | 4118 39 49 56 24 24 | 59 89 67 79 67
XR10 | 8064 22 29 --- 39 20 | 30 37 --- 51 33
XR14 | 8950 20 21 --- 33 17 | 44 44 --- 33 37
XR15 | ---- --- 13 --- --- 0 | --- 9999 --- --- 9999
R19 |16422 202 522 186 274 194 | 68 598 9999 61 9999
R21 | 2520 45 46 86 54 31 | 67 65 82 76 51
XR22 | ---- --- 13 --- --- 0 | --- 117 --- --- 113
R23 | 3529 50 30 368 157 88 | 34 37 177 92 30
R24 | 2884 55 54 428 110 96 | 22 9999 98 39 9999
------+-------------------------------+---------------------------
RMS | 6969 85 171 197 115 |T 48 101 81 56 48
WRMS | 6969 64 45 78 115 |NE 44 149 119 58 52
MEDI | 4752 39 30 65 49 |MD 37 44 78 50 36
Table 3.1434.2 GPS week: 1434 Day: 2 MJD: 54284
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 4986 32 40 190 35 34 | 62 55 114 53 57
R03E | 8891 141 54 89 115 59 | 78 58 113 103 65
R04E | 5245 29 18 59 37 17 | 59 52 86 41 50
R06E | 3572 30 23 92 56 23 | 56 39 58 39 40
R07E | 5871 45 34 61 61 26 | 21 52 94 41 34
R08E | 6357 36 25 38 30 18 | 53 69 52 69 60
XR10 | 6438 19 26 --- 57 23 | 40 37 --- 41 33
XR14 | 8543 27 24 --- 57 24 | 39 40 --- 35 34
XR15 | ---- --- 8 --- --- 0 | --- 9999 --- --- 9999
R19 | 6125 96 48 202 112 54 | 127 193 9999 57 9999
R21 | 1742 52 61 180 22 39 | 65 92 126 67 66
XR22 | ---- --- 8 --- --- 0 | --- 189 --- --- 187
R23 | 4284 64 22 465 80 74 | 47 57 337 38 41
R24 | 2645 32 10 439 113 71 | 38 9999 115 52 9999
------+-------------------------------+---------------------------
RMS | 5338 65 37 233 75 |T 57 77 121 53 60
WRMS | 5338 54 38 81 75 |NE 59 101 192 48 72
MEDI | 5245 32 24 92 57 |MD 53 55 113 41 50
Table 3.1434.3 GPS week: 1434 Day: 3 MJD: 54285
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 5943 22 41 260 35 43 | 73 66 146 64 65
R03E |16372 43 39 62 51 26 | 105 78 82 62 55
R04E | 3865 20 26 32 40 16 | 37 43 41 52 37
R06E | 5227 25 29 62 60 23 | 21 36 96 44 29
R07E | 3342 66 57 72 52 34 | 22 58 78 50 32
R08E | 6270 35 27 41 26 17 | 112 81 84 77 89
XR10 | 6637 11 20 --- 26 13 | 45 33 --- 46 30
XR14 | 5831 23 28 --- 34 20 | 24 49 --- 55 38
XR15 | ---- --- 13 --- --- 0 | --- 9999 --- --- 9999
R19 | 9935 58 40 330 105 62 | 103 112 9999 48 9999
R21 | 3568 31 55 195 55 39 | 105 130 171 68 101
XR22 | ---- --- 13 --- --- 0 | --- 301 --- --- 297
R23 | 4072 60 21 460 69 74 | 53 53 379 57 49
XR24 | 3223 36 71 --- 65 41 | 65 9999 --- 44 9999
------+-------------------------------+---------------------------
RMS | 7631 43 39 222 59 |T 63 86 134 55 74
WRMS | 7631 47 36 69 59 |NE 65 113 275 53 103
MEDI | 5227 31 28 72 51 |MD 53 58 84 52 49
Table 3.1434.4 GPS week: 1434 Day: 4 MJD: 54286
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 6454 32 47 42 36 22 | 40 45 98 35 27
R03E |13641 34 55 49 44 26 | 52 86 75 47 46
R04E | 6618 32 38 35 61 24 | 45 46 49 80 42
R06E | 8045 35 65 54 59 30 | 37 81 74 58 44
R07E | 3539 28 30 38 57 21 | 25 40 49 60 27
R08E | 4292 58 41 57 54 30 | 81 68 69 69 64
XR10 | 9318 45 29 --- 75 35 | 30 28 --- 45 24
XR14 | 5874 19 23 --- 30 16 | 32 35 --- 39 33
XR15 | ---- --- 11 --- --- 0 | --- 9999 --- --- 9999
XR19 | ---- --- --- 2677 2702 2694 | --- --- 9999 92 9999
R21 | 5812 22 78 129 24 35 | 67 104 106 67 65
XR22 | ---- --- 12 --- --- 0 | --- 435 --- --- 434
R23 | 2072 38 35 415 139 88 | 56 44 314 61 59
XR24 | 3379 23 38 --- 48 24 | 85 9999 --- 70 9999
------+-------------------------------+---------------------------
RMS | 7117 36 51 159 67 |T 50 92 104 60 78
WRMS | 7117 34 41 54 67 |NE 54 129 210 62 123
MEDI | 5874 32 38 54 54 |MD 45 46 74 60 44
Table 3.1434.5 GPS week: 1434 Day: 5 MJD: 54287
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E | 8161 23 36 33 45 20 | 38 52 61 39 38
R03E | 5797 42 35 46 35 22 | 45 48 53 54 30
R04E | 5930 31 25 29 35 17 | 44 64 57 55 48
R06E | 8596 41 36 81 58 28 | 28 61 55 53 39
R07E | 3529 26 26 33 59 21 | 33 23 41 56 25
R08E | 4205 50 43 53 44 27 | 61 89 79 67 69
XR10 | 8360 52 16 --- 61 31 | 26 31 --- 47 31
XR14 | 6517 23 24 --- 33 18 | 31 40 --- 41 34
XR15 | ---- --- 13 --- --- 0 | --- 9999 --- --- 9999
R21 | 4885 21 48 233 32 44 | 68 76 157 63 53
XR22 | ---- --- 14 --- --- 0 | --- 909 --- --- 911
R23 | 1762 83 38 422 110 82 | 43 62 250 33 33
XR24 | 7583 2324 19 --- 70 46 | 69 9999 --- 56 9999
------+-------------------------------+---------------------------
RMS | 5770 44 37 176 57 |T 44 132 94 51 119
WRMS | 5770 39 39 48 57 |NE 47 223 203 48 212
MEDI | 5930 41 26 46 45 |MD 43 61 57 54 38
Table 3.1434.6 GPS week: 1434 Day: 6 MJD: 54288
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01E |10656 19 28 185 34 32 | 38 47 73 47 40
R03E | 7441 27 27 146 44 29 | 68 24 68 42 27
R04E | 6486 48 30 62 24 22 | 49 64 92 77 60
R06E | 3879 42 37 52 44 24 | 38 58 71 61 42
R07E | 4154 42 20 72 74 28 | 34 38 61 55 33
R08E | 5890 55 41 51 47 27 | 71 108 96 112 92
XR10 | 7682 61 36 --- 52 35 | 25 45 --- 61 40
XR14 | 6769 24 22 --- 30 18 | 36 37 --- 44 35
XR15 | ---- --- 18 --- --- 0 | --- 9999 --- --- 9999
R21 | 2236 34 36 139 41 30 | 98 87 134 79 77
XR22 | ---- --- 18 --- --- 0 | --- 9999 --- --- 9999
R23 | 3150 81 56 416 90 77 | 29 94 399 60 60
XR24 | ---- --- 18 --- --- 0 | --- 9999 --- --- 9999
------+-------------------------------+---------------------------
RMS | 6051 47 36 181 54 |T 48 60 124 63 50
WRMS | 6051 42 38 81 54 |NE 47 65 266 61 53
MEDI | 5890 42 28 72 44 |MD 38 47 73 60 40
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