[IGSREPORT-15512] Wk 1444 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Sep 27 05:32:58 PDT 2007
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IGS Electronic Report 27 Sep 05:33:06 PDT 2007 Message Number 15512
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1444 (Sep 09, 2007 - Sep 15, 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 2.1444.
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:
igl1444[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1444 in the SP3 format.
igl14447.sum Combination Report for GPS Week 1444.
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 | 1203.4 ns
1 | 1190.5 ns
2 | 1174.1 ns
3 | 1241.9 ns
4 | 1225.2 ns
5 | 1224.5 ns
6 | 1251.9 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 R21
0 | ESX | R02 R03 R10 R14 R18 R19 R21 R23 R24
1 | COD | R15 R21 R21
1 | ESX | R10 R14 R23 R24
2 | COD | R15 R21
2 | ESX | R10 R14 R23 R24
3 | COD | R15 R21
3 | ESX | R10 R14 R23 R24
4 | COD | R15 R21
4 | ESX | R10 R14 R23 R24
5 | COD | R15 R21
5 | ESX | R10 R14 R23 R24
6 | COD | R15
6 | ESX | R02 R03 R04 R08 R10 R14 R18 R19 R21 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 1.1444, 1a.1444).
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 2.1444.0-6)
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 3.1444.0-6).
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 1444 summary. (Sep 09, 2007 - Sep 15, 2007)
Table 1.1444.a GPS week : 1444 MJD: 54352.0-54358.0
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 55| 0 2 3 -5 14 -181 -.08 38 38 | 0 207 3477 3752
| 5 4 5 39 72 213 .14 | 0 556
cod 173| -1 -5 0 -7 -37 83 -.02 42 35 | --- --- --- ---
| 6 6 5 82 63 226 .08 | --- ---
esx 41| 5 1 -4 -8 -18 359 -.21 328 181 | 600166 18154 8835 21165
| 7 10 30 134 71 247 .17 | 1054845 28875
iac n/a| 0 4 -1 45 -6 -18 .18 63 63 | 1212775 4908 9032 21613
| 4 6 11 74 66 238 .12 | 25385 8033
mcc n/a| -3 -6 61 154 82 457 .46 108 108 | --- --- --- ---
| 12 10 33 194 179 791 .76 | --- ---
Table 1.1444.b GPS week : 1444 MJD: 54352.0-54358.0
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 | 19 20 25 19 24 22 32 |
R04 | 21 24 23 22 48 19 33 |
R06 | 35 28 34 29 25 20 27 |
R07 | 25 18 19 18 24 20 25 |
R08 | 18 29 30 20 24 32 47 |
R10 | 24 41 21 20 19 16 22 |
R14 | 15 33 23 33 16 21 22 |
R23E | 55 62 148 92 --- --- 0 |
R24E | --- 0 0 0 0 353 122 |
Table 1.1444.c GPS week : 1444 MJD: 54352.0-54358.0
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 1444 0 | 74 114 -769 -11280 7769 -329700 99.4 5524 5524 | 1203431 0
brd 1444 1 | 118 135 -158 -9323 -4761 -341600 99.8 5011 5011 | 1190517 0
brd 1444 2 | 23 164 -260 1705 -2533 -333100 89.8 5848 5848 | 1174052 0
brd 1444 3 | -58 -39 -370 683 -3913 -320200 104.4 5340 5340 | 1241897 0
brd 1444 4 | 148 581 -380 1462 -7094 -324700 100.0 4765 4765 | 1225199 0
brd 1444 5 | 589 964 -486 -1424 2905 -332200 90.2 5117 5117 | 1224532 0
brd 1444 6 | 26 349 -874 2003 -648 -357300 97.8 4859 4859 | 1251938 0
-------------+------------------------------------------------------------+----------------
brd 1444 mean| 131 324 -471 -2310 -1182 -334114 97.3 5209 5209 | 1215938 0
brd 1444 sdev| 213 344 261 5602 5068 12247 5.4 385 385 | 27948 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 2.1444.0 GPS week: 1444 Day: 0 MJD: 54352
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 55| 2 7 5 -29 -34 -195 -.07 40 41 | 0 -248 4851 5219
cod 173| -1 -10 0 35 -29 210 .01 44 37 | --- --- --- ---
esx 41| 6 5 -38 26 27 -132 -.07 278 105 | -6888 18684 11859 23335
iac n/a| -1 5 13 -11 -114 -81 .26 43 43 | 1186984 16089 11931 24220
mcc n/a| -11 -10 78 -15 -116 1248 .19 132 132 | --- --- --- ---
Table 2.1444.1 GPS week: 1444 Day: 1 MJD: 54353
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 55| -4 -1 0 -67 -21 -453 -.18 53 53 | 0 11 3763 4211
cod 173| 9 -11 -8 97 32 -168 -.11 56 47 | --- --- --- ---
esx 41| -2 1 -38 -41 61 231 -.24 268 90 | -27346 -5713 9533 16076
iac n/a| 3 2 14 4 -14 322 .19 43 43 | 1197454 -9951 8964 16150
mcc n/a| -8 1 25 -4 0 263 .04 73 73 | --- --- --- ---
Table 2.1444.2 GPS week: 1444 Day: 2 MJD: 54354
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 55| 4 5 10 -4 4 -7 -.28 47 50 | 0 900 3274 3401
cod 173| -1 0 -2 -31 -21 -89 .02 48 26 | --- --- --- ---
esx 41| 3 20 -8 120 -61 569 -.06 285 126 | -75378 -4749 6885 16353
iac n/a| -3 -4 -9 -71 69 14 .27 155 155 | 1177688 1784 7115 16905
mcc n/a| 0 -6 12 80 197 -363 -.49 120 120 | --- --- --- ---
Table 2.1444.3 GPS week: 1444 Day: 3 MJD: 54355
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 55| 5 -3 0 19 132 26 .05 34 33 | 0 500 3238 3391
cod 173| -12 5 5 4 -63 8 .09 28 28 | --- --- --- ---
esx 41| 15 -5 -6 -186 66 450 -.55 190 57 | 12496 -7333 7882 23382
iac n/a| -2 6 -11 127 -15 -389 .23 45 45 | 1237671 3563 8411 24866
mcc n/a| 4 -7 49 263 75 -393 -.04 117 117 | --- --- --- ---
Table 2.1444.4 GPS week: 1444 Day: 4 MJD: 54356
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 55| 4 2 6 -8 -9 -294 -.14 35 37 | 0 907 2842 3028
cod 173| -5 -6 -1 -30 -43 414 .05 33 30 | --- --- --- ---
esx 41| 14 7 16 -110 -125 439 -.13 213 65 | 2137289 54307 7258 21024
iac n/a| -3 4 -8 120 -12 -230 .27 46 46 | 1224180 5796 7771 21549
mcc n/a| 14 0 77 187 -104 -105 .59 82 82 | --- --- --- ---
Table 2.1444.5 GPS week: 1444 Day: 5 MJD: 54357
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 55| -2 5 7 60 -67 -409 .11 24 25 | 0 -190 2242 2499
cod 173| -3 -4 -5 -164 21 305 -.14 46 37 | --- --- --- ---
esx 41| -2 -3 -4 -66 -55 375 -.31 216 59 | 2150079 61623 7652 21835
iac n/a| 8 0 -1 89 -41 128 .06 39 39 | 1222992 7376 8258 20781
mcc n/a| -1 3 104 38 131 1408 1.51 116 116 | --- --- --- ---
Table 2.1444.6 GPS week: 1444 Day: 6 MJD: 54358
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 55| -7 3 -6 -5 94 64 -.02 31 26 | 0 -427 4130 4517
cod 173| 1 -10 4 38 -158 -98 -.02 38 37 | --- --- --- ---
esx 41| 1 -12 50 201 -46 580 -.14 842 763 | 10911 10264 10776 26156
iac n/a| 3 17 -9 58 83 106 -.05 66 66 | 1242461 9700 10777 26821
mcc n/a| -25 -27 86 529 393 1146 1.44 114 114 | --- --- --- ---
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 3.1444.0 GPS week: 1444 Day: 0 MJD: 54352
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2892 21 37 51 30 --- 19 | 28 43 64 39 --- 34
R04 | 4935 20 42 54 31 --- 20 | 46 29 237 46 --- 45
R06 | 9527 56 65 82 50 --- 35 | 48 76 95 49 --- 36
R07 | 2629 32 33 78 38 132 25 | 60 34 92 30 94 37
R08 | 5113 24 27 41 31 --- 17 | 22 41 127 41 --- 27
R10 | 3322 18 33 469 45 --- 23 | 41 36 323 60 --- 43
R14 | 4810 13 26 431 23 --- 15 | 30 23 203 55 --- 30
R23 | 7304 84 70 441 76 --- 55 | 43 167 9999 91 --- 178
------+------------------------------------+--------------------------------
RMS | 5523 40 44 278 43 132 |T 39 56 163 51 94 53
WRMS | 5523 41 37 105 43 132 |NE 39 56 163 51 94 53
MEDI | 4810 21 33 78 31 132 |MD 41 36 127 46 94 36
Table 3.1444.1 GPS week: 1444 Day: 1 MJD: 54353
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2486 27 42 60 20 --- 19 | 18 48 68 41 --- 28
R04 | 7124 25 57 70 29 --- 24 | 24 35 210 44 --- 22
R06 | 4012 61 44 64 28 --- 27 | 40 72 116 29 --- 39
R07 | 3632 17 45 50 20 73 17 | 40 34 71 40 47 28
R08 | 6750 53 42 83 38 --- 29 | 37 39 127 57 --- 50
R10 | 2719 39 78 387 57 --- 40 | 24 53 120 55 --- 27
R14 | 6287 35 49 362 50 --- 32 | 30 14 212 74 --- 41
R23 | 4702 107 77 521 73 --- 61 | 31 144 9999 103 --- 152
XR24 | ---- --- 14 559 --- --- 0 | --- 431 9999 --- --- 454
------+------------------------------------+--------------------------------
RMS | 5010 53 56 268 43 73 |T 30 96 132 55 47 93
WRMS | 5010 53 47 90 43 73 |NE 30 96 132 55 47 93
MEDI | 4012 35 45 83 29 73 |MD 30 48 120 44 47 39
Table 3.1444.2 GPS week: 1444 Day: 2 MJD: 54354
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2177 41 21 100 40 --- 24 | 53 37 76 49 --- 30
R04 | 2673 21 23 65 67 --- 22 | 22 32 173 78 --- 17
R06 | 2891 40 28 154 61 --- 33 | 54 37 92 48 --- 28
R07 | 2989 18 16 80 43 120 19 | 32 33 68 41 52 27
R08 | 9810 56 13 107 63 --- 29 | 18 40 96 74 --- 34
R10 | 4089 28 23 377 44 --- 21 | 46 67 180 41 --- 49
R14 | 7328 16 22 383 63 --- 23 | 27 34 251 76 --- 34
R23 | 8815 97 123 551 415 --- 147 | 35 159 9999 387 --- 126
XR24 | ---- --- 5 446 --- --- 0 | --- 642 9999 --- --- 660
------+------------------------------------+--------------------------------
RMS | 5847 47 48 285 155 120 |T 35 120 133 99 52 111
WRMS | 5847 50 26 126 155 120 |NE 35 120 133 99 52 111
MEDI | 2989 28 22 154 61 120 |MD 32 37 96 49 52 34
Table 3.1444.3 GPS week: 1444 Day: 3 MJD: 54355
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1705 44 22 35 26 --- 19 | 47 57 50 58 --- 44
R04 | 5294 21 25 65 46 --- 21 | 30 27 178 52 --- 26
R06 | 3921 36 31 94 52 --- 29 | 50 56 80 46 --- 45
R07 | 3508 19 24 43 42 117 17 | 43 39 63 30 53 32
R08 | 8653 30 30 39 44 --- 20 | 47 64 174 87 --- 55
R10 | 4870 21 27 343 38 --- 20 | 41 48 160 37 --- 40
R14 | 6509 51 31 344 59 --- 33 | 47 41 148 58 --- 23
XR23 |13321 --- 34 743 148 --- 91 | --- 633 9999 158 --- 630
XR24 | ---- --- 9 327 --- --- 0 | --- 930 9999 --- --- 931
------+------------------------------------+--------------------------------
RMS | 5339 34 28 190 45 117 |T 43 210 121 65 53 202
WRMS | 5339 33 28 57 45 117 |NE 43 210 121 65 53 202
MEDI | 4870 30 27 94 44 117 |MD 47 56 148 52 53 44
Table 3.1444.4 GPS week: 1444 Day: 4 MJD: 54356
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2494 25 35 64 53 --- 23 | 51 54 68 62 --- 45
R04 | 7192 59 32 204 45 --- 48 | 17 55 383 20 --- 38
R06 | 3253 36 41 41 56 --- 24 | 29 50 41 51 --- 28
R07 | 4112 40 38 61 36 82 24 | 38 55 67 44 61 38
R08 | 5728 22 30 50 68 --- 23 | 43 34 139 54 --- 31
R10 | 3367 24 30 373 25 --- 19 | 32 47 146 42 --- 34
R14 | 5418 22 23 354 21 --- 16 | 43 51 109 61 --- 48
XR24E |19058 --- 23 518 --- --- 0 | --- 649 9999 --- --- 624
------+------------------------------------+--------------------------------
RMS | 4765 35 33 213 46 82 |T 36 124 136 47 61 110
WRMS | 4765 37 30 65 46 82 |NE 36 49 136 47 61 37
MEDI | 4112 25 30 64 45 82 |MD 38 51 109 51 61 38
Table 3.1444.5 GPS week: 1444 Day: 5 MJD: 54357
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4630 23 60 37 34 --- 22 | 49 78 59 64 --- 52
R04 | 7461 25 35 43 34 --- 19 | 32 34 282 19 --- 25
R06 | 2329 25 33 47 38 --- 20 | 47 59 89 58 --- 53
R07 | 3579 21 28 50 44 116 20 | 48 52 75 39 65 43
R08 | 5405 34 74 67 57 --- 32 | 26 77 391 43 --- 26
R10 | 3881 19 29 438 19 --- 15 | 32 55 222 26 --- 31
R14 | 6607 16 42 352 33 --- 20 | 61 40 85 36 --- 39
XR24E | 8111 --- 359 381 345 --- 352 | --- 652 9999 199 --- 468
------+------------------------------------+--------------------------------
RMS | 5117 24 46 216 39 116 |T 42 130 171 60 65 92
WRMS | 5117 25 37 59 39 116 |NE 42 56 171 40 65 38
MEDI | 4630 23 35 50 34 116 |MD 47 55 89 39 65 39
Table 3.1444.6 GPS week: 1444 Day: 6 MJD: 54358
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4913 43 39 123 48 --- 31 | 54 79 95 78 --- 65
R04 | 8463 33 31 1748 80 --- 33 | 29 37 9999 39 --- 26
R06 | 1565 18 56 64 56 --- 26 | 41 74 83 51 --- 43
R07 | 2314 20 32 114 32 114 24 | 37 57 109 43 45 39
R08 | 4038 48 32 1260 120 --- 47 | 61 54 615 90 --- 39
R10 | 4311 22 34 412 42 --- 22 | 27 48 228 33 --- 29
R14 | 5174 20 34 351 43 --- 22 | 32 42 168 50 --- 35
XR23E | ---- --- 13 >>>> --- --- 0 | --- 423 9999 --- --- 424
XR24E | 7789 --- 97 607 153 --- 121 | --- 370 9999 235 --- 345
------+------------------------------------+--------------------------------
RMS | 4858 31 38 842 66 114 |T 40 131 216 77 45 116
WRMS | 4858 26 37 763 66 114 |NE 40 55 216 54 45 39
MEDI | 4311 22 34 412 48 114 |MD 37 57 109 50 45 39
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