[IGSREPORT-15579] Wk 1446 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Oct 18 04:21:46 PDT 2007
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IGS Electronic Report 18 Oct 04:21:53 PDT 2007 Message Number 15579
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1446 (Sep 23, 2007 - Sep 29, 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 2.1446.
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:
igl1446[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1446 in the SP3 format.
igl14467.sum Combination Report for GPS Week 1446.
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 | 1268.4 ns
1 | 1265.6 ns
2 | 1286.4 ns
3 | 1276.1 ns
4 | 1267.1 ns
5 | 1215.2 ns
6 | 1250.5 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
----+--------+---------------
1 | COD | R15
2 | COD | R15
3 | COD | R15
4 | COD | R15
5 | COD | R15
6 | COD | R15
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 1.1446, 1a.1446).
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 2.1446.0-6)
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 3.1446.0-6).
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 1446 summary. (Sep 23, 2007 - Sep 29, 2007)
Table 1.1446.a GPS week : 1446 MJD: 54366.0-54372.0
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 53| 1 1 -2 36 22 -140 .02 60 44 | 0 511 4791 5288
| 3 3 9 52 54 265 .17 | 0 2498
cod 172| -5 0 -3 -70 -113 19 -.16 63 45 | --- --- --- ---
| 3 5 6 83 59 168 .13 | --- ---
esx 41| 1 7 49 8 153 207 -.41 229 118 | 2725857 52629 66694 170639
| 16 8 18 200 158 303 .23 | 1269557 35086
iac n/a| -1 4 -1 8 17 -17 .14 58 58 | 1420159 -3169 113045 171256
| 3 4 10 41 74 168 .19 | 433839 9061
mcc n/a| 18 2 9 40 86 43 .81 128 128 | --- --- --- ---
| 27 7 26 172 208 469 1.28 | --- ---
Table 1.1446.b GPS week : 1446 MJD: 54366.0-54372.0
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 | 23 19 26 24 20 24 29 |
R04 | 23 30 41 34 24 32 24 |
R06 | 31 31 59 25 46 27 25 |
R07 | 28 49 40 19 20 34 29 |
R08 | 62 51 59 28 22 46 39 |
R10 | 56 53 55 67 65 65 70 |
R14 | 56 58 65 48 49 57 51 |
R21E | 72 56 73 57 46 73 60 |
R23E | 62 61 63 75 77 77 65 |
R24E | 0 --- --- 0 0 0 0 |
Table 1.1446.c GPS week : 1446 MJD: 54366.0-54372.0
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 1446 0 | -393 49 566 -4585 3491 -3621 89.5 4230 4230 | 1268350 0
brd 1446 1 | 243 -142 355 1630 8787 -4736 90.1 3425 3425 | 1265629 0
brd 1446 2 | -39 -140 125 3385 5115 -2984 95.6 4529 4529 | 1286412 0
brd 1446 3 | -158 102 167 -4190 5728 2765 93.1 4935 4935 | 1276137 0
brd 1446 4 | 53 148 189 3914 3944 -864 104.5 5312 5312 | 1267096 0
brd 1446 5 | -88 240 345 -3632 3231 -4372 98.8 4866 4866 | 1215155 0
brd 1446 6 | -129 180 352 1818 12880 -4223 94.5 4773 4773 | 1250484 0
-------------+------------------------------------------------------------+----------------
brd 1446 mean| -73 62 300 -237 6168 -2576 95.2 4581 4581 | 1261323 0
brd 1446 sdev| 196 151 152 3744 3510 2686 5.2 611 611 | 23090 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 2.1446.0 GPS week: 1446 Day: 0 MJD: 54366
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 53| -2 -2 2 14 34 -399 -.04 59 42 | 0 -818 3537 3821
cod 172| -2 0 -4 -11 -96 305 -.06 62 42 | --- --- --- ---
esx 41| 7 6 26 -41 168 237 -.19 231 126 | 10119 -21937 9531 19903
iac n/a| -5 9 -7 -46 -88 -53 .16 63 63 | 1267162 -7843 9704 20868
mcc n/a| -1 6 32 58 23 828 -.12 51 51 | --- --- --- ---
Table 2.1446.1 GPS week: 1446 Day: 1 MJD: 54367
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 53| 0 0 -5 71 27 193 -.18 58 51 | 0 -61 2118 2334
cod 172| -8 5 5 -159 -165 -236 -.32 68 45 | --- --- --- ---
esx 41| 1 5 38 205 298 401 -.46 204 114 | 4108588 50786 383346 999999
iac n/a| 2 2 -6 40 24 -156 .44 56 56 | 2402355 -18568 704834 999999
mcc n/a| 10 12 18 -170 -72 244 .44 94 94 | --- --- --- ---
Table 2.1446.2 GPS week: 1446 Day: 2 MJD: 54368
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 53| 7 7 -4 -29 16 -315 .30 72 54 | 0 6077 6556 7668
cod 172| -11 -8 -6 59 -124 -106 -.04 86 58 | --- --- --- ---
esx 41| -5 20 52 -303 -53 531 -.31 251 174 | 2913512 51268 11695 22855
iac n/a| 1 4 6 16 100 111 -.06 55 55 | 1290153 -6446 12004 23396
mcc n/a| -5 2 48 45 -1 345 -.62 109 109 | --- --- --- ---
Table 2.1446.3 GPS week: 1446 Day: 3 MJD: 54369
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 53| 1 1 -3 28 32 -485 -.17 66 41 | 0 449 4859 5108
cod 172| -2 -3 5 -72 -118 37 -.24 65 51 | --- --- --- ---
esx 41| 19 14 62 -35 87 555 -.54 231 102 | 2926632 69785 11368 26631
iac n/a| 0 0 -5 26 60 270 .03 37 37 | 1270668 8798 11950 27058
mcc n/a| 45 -3 -11 30 335 -480 2.67 176 176 | --- --- --- ---
Table 2.1446.4 GPS week: 1446 Day: 4 MJD: 54370
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 53| 0 -2 -12 79 -76 132 .13 41 33 | 0 -780 5321 6027
cod 172| -3 7 -8 -129 9 -5 -.06 48 27 | --- --- --- ---
esx 41| -30 6 72 295 -30 -204 -.59 243 108 | 2984743 84982 14100 33783
iac n/a| 0 0 10 66 57 -237 -.07 68 68 | 1260543 -1209 14010 34269
mcc n/a| 61 10 -24 -58 429 -426 2.51 183 183 | --- --- --- ---
Table 2.1446.5 GPS week: 1446 Day: 5 MJD: 54371
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 53| 1 4 -10 -18 109 -107 .04 66 44 | 0 -486 4878 5193
cod 172| -5 0 -9 -21 -164 86 -.32 62 49 | --- --- --- ---
esx 41| 11 -8 64 -121 249 -7 -.71 215 89 | 3014645 73102 14692 48334
iac n/a| 0 9 8 -41 56 -9 .27 73 73 | 1211430 -2428 16804 50972
mcc n/a| 25 -3 -12 -11 -9 -238 .58 158 158 | --- --- --- ---
Table 2.1446.6 GPS week: 1446 Day: 6 MJD: 54372
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 53| 5 4 15 110 12 2 .05 60 43 | 0 -800 6272 6867
cod 172| -1 -6 -7 -158 -134 55 -.10 48 40 | --- --- --- ---
esx 41| 2 8 31 59 352 -63 -.08 231 115 | 3122761 60423 22126 42969
iac n/a| -7 4 -17 -3 -85 -51 .23 55 55 | 1238806 5509 22012 42233
mcc n/a| -8 -4 17 388 -103 27 .20 129 129 | --- --- --- ---
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 3.1446.0 GPS week: 1446 Day: 0 MJD: 54366
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4607 32 32 84 38 --- 23 | 22 44 88 45 --- 30
R04 | 5491 33 32 100 23 --- 22 | 25 56 100 43 --- 35
R06 | 2286 41 42 93 65 --- 31 | 25 42 63 61 --- 27
R07 | 3500 41 27 91 59 51 28 | 31 45 75 69 28 36
R08 | 2855 56 29 313 107 --- 61 | 33 42 306 62 --- 33
R10 | 2395 32 44 338 35 --- 55 | 37 40 230 66 --- 56
R14 | 1619 49 47 325 45 --- 56 | 48 39 103 38 --- 38
R21E | 2124 136 150 82 74 --- 71 | 117 170 116 106 --- 107
R23E | 8432 24 53 349 78 --- 61 | 55 39 92 78 --- 39
XR24E | ---- --- 18 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 4229 59 62 231 63 51 |T 43 57 130 63 28 44
WRMS | 4229 42 42 126 63 51 |NE 31 44 137 54 28 36
MEDI | 2855 41 32 100 59 51 |MD 33 42 100 62 28 36
Table 3.1446.1 GPS week: 1446 Day: 1 MJD: 54367
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5626 23 22 75 29 --- 18 | 39 38 38 32 --- 23
R04 | 6008 25 35 148 31 --- 29 | 24 40 106 35 --- 22
R06 | 1856 25 66 52 65 --- 31 | 59 72 50 81 --- 42
R07 | 1951 86 104 104 54 94 49 | 45 102 112 60 42 54
R08 | 2936 43 54 273 36 --- 51 | 39 47 140 57 --- 23
R10 | 2170 30 35 301 39 --- 53 | 63 50 131 72 --- 63
R14 | 1257 65 45 310 28 --- 57 | 44 26 118 73 --- 48
R21E | 1995 115 99 71 76 --- 56 | 150 210 180 187 --- 158
R23E | 3414 31 93 255 100 --- 60 | 44 31 121 98 --- 41
------+------------------------------------+--------------------------------
RMS | 3425 58 68 204 56 94 |T 56 68 110 77 42 52
WRMS | 3425 51 45 114 56 94 |NE 44 53 99 58 42 39
MEDI | 2170 31 54 148 39 94 |MD 44 47 118 72 42 42
Table 3.1446.2 GPS week: 1446 Day: 2 MJD: 54368
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7010 44 23 98 41 --- 26 | 28 27 86 70 --- 31
R04 | 4648 44 26 235 26 --- 40 | 29 35 184 27 --- 22
R06 | 3134 49 160 102 75 --- 58 | 46 159 114 49 --- 45
R07 | 3239 59 86 136 33 108 39 | 61 46 119 43 54 24
R08 | 3968 63 55 336 39 --- 59 | 44 44 163 44 --- 28
R10 | 1098 40 59 309 47 --- 54 | 41 53 171 90 --- 59
R14 | 1118 50 37 387 53 --- 65 | 66 39 246 38 --- 49
R21E | 4750 145 146 152 83 --- 72 | 170 268 165 167 --- 148
R23E | 7261 92 63 304 71 --- 63 | 58 43 167 76 --- 37
------+------------------------------------+--------------------------------
RMS | 4528 72 86 251 55 108 |T 60 79 157 67 54 49
WRMS | 4528 54 58 174 55 108 |NE 45 57 154 51 54 36
MEDI | 3968 50 59 235 47 108 |MD 46 44 165 49 54 37
Table 3.1446.3 GPS week: 1446 Day: 3 MJD: 54369
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6802 32 30 106 33 --- 23 | 34 57 108 65 --- 42
R04 | 3998 21 34 203 24 --- 33 | 36 70 120 66 --- 46
R06 | 3307 44 45 74 32 --- 24 | 52 127 56 38 --- 67
R07 | 5185 31 29 80 18 176 18 | 56 71 64 46 80 48
R08 | 5618 64 40 86 26 --- 28 | 66 45 126 52 --- 27
R10 | 1762 58 51 421 30 --- 67 | 78 78 223 71 --- 62
R14 | 1468 30 38 295 36 --- 47 | 55 57 155 48 --- 55
R21E | 8391 119 121 110 51 --- 57 | 187 157 163 129 --- 133
R23E | 3438 110 114 364 62 --- 75 | 117 40 208 73 --- 60
XR24E | ---- --- 10 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 4934 66 65 231 37 176 |T 75 78 135 65 80 60
WRMS | 4934 41 51 102 37 176 |NE 53 72 121 55 80 49
MEDI | 3998 44 38 110 32 176 |MD 56 70 126 65 80 55
Table 3.1446.4 GPS week: 1446 Day: 4 MJD: 54370
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6921 29 24 77 40 --- 20 | 35 38 95 52 --- 33
R04 | 3243 28 27 104 45 --- 23 | 21 51 61 74 --- 33
R06 | 2222 40 78 102 113 --- 45 | 63 99 57 33 --- 52
R07 | 3435 31 18 98 27 183 20 | 23 59 93 35 47 26
R08 | 6268 38 16 99 29 --- 21 | 54 48 102 45 --- 27
R10 | 1578 37 38 426 32 --- 64 | 47 68 131 53 --- 56
R14 | 1866 33 33 312 30 --- 48 | 26 40 88 50 --- 33
R21E |11095 59 68 97 112 --- 46 | 162 240 187 189 --- 184
R23E | 3221 60 74 444 94 --- 76 | 64 65 234 93 --- 52
XR24E | ---- --- 10 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 5311 41 48 243 68 183 |T 55 78 116 69 47 55
WRMS | 5311 33 27 108 68 183 |NE 38 57 89 48 47 37
MEDI | 3243 37 27 102 40 183 |MD 47 59 95 52 47 33
Table 3.1446.5 GPS week: 1446 Day: 5 MJD: 54371
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5596 45 25 87 32 --- 24 | 23 51 91 60 --- 38
R04 | 4222 46 52 100 46 --- 31 | 19 81 127 41 --- 35
R06 | 1713 30 39 101 41 --- 26 | 15 45 72 68 --- 22
R07 | 1130 40 50 56 82 158 34 | 65 69 42 44 40 43
R08 | 4886 49 70 53 116 --- 46 | 54 70 49 100 --- 40
R10 | 1754 49 50 335 78 --- 65 | 40 62 108 101 --- 49
R14 | 2310 41 43 296 58 --- 56 | 41 58 72 68 --- 45
R21E |10987 152 114 180 77 --- 73 | 202 206 185 204 --- 181
R23E | 2595 52 74 388 89 --- 76 | 42 52 224 76 --- 37
XR24E | ---- --- 13 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 4866 66 62 215 73 158 |T 55 77 107 84 40 54
WRMS | 4866 44 49 89 73 158 |NE 36 62 80 68 40 38
MEDI | 2595 46 50 101 77 158 |MD 41 62 91 68 40 40
Table 3.1446.6 GPS week: 1446 Day: 6 MJD: 54372
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5581 51 33 96 50 --- 29 | 29 67 127 46 --- 49
R04 | 5093 46 29 74 40 --- 24 | 18 38 84 37 --- 23
R06 | 1928 34 21 96 49 --- 25 | 25 31 57 47 --- 15
R07 | 1280 26 47 61 63 129 28 | 61 80 60 39 55 45
R08 | 5316 47 75 63 76 --- 39 | 61 67 68 53 --- 32
R10 | 2129 52 28 422 50 --- 69 | 43 71 211 46 --- 58
R14 | 3410 30 40 309 23 --- 51 | 36 49 102 36 --- 38
R21E | 8424 137 81 166 60 --- 59 | 297 157 147 168 --- 193
R23E | 5210 36 40 383 66 --- 65 | 42 41 160 76 --- 35
XR24E | ---- --- 13 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 4772 60 48 231 55 129 |T 68 66 112 60 55 54
WRMS | 4772 43 40 115 55 129 |NE 39 57 101 43 55 37
MEDI | 5093 46 33 96 50 129 |MD 42 67 102 46 55 38
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