[IGSREPORT-15601] Wk 1448 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Oct 26 02:32:28 PDT 2007
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IGS Electronic Report 26 Oct 02:32:40 PDT 2007 Message Number 15601
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1448 (Oct 07, 2007 - Oct 13, 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 2.1448.
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:
igl1448[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1448 in the SP3 format.
igl14487.sum Combination Report for GPS Week 1448.
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 | 1284.9 ns
1 | 1263.4 ns
2 | 1244.7 ns
3 | 1288.9 ns
4 | 1301.7 ns
5 | 1299.4 ns
6 | 1282.9 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 R24
0 | ESX | R23 R24
1 | COD | R15 R23 R24
1 | ESX | R23 R24
2 | COD | R15 R23 R24
2 | ESX | R23 R24
3 | COD | R15 R23 R24
3 | ESX | R23 R24
4 | COD | R15 R24
4 | ESX | R23 R24
5 | COD | R24
5 | ESX | R23 R24
6 | COD | R24
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 1.1448, 1a.1448).
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 2.1448.0-6)
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 3.1448.0-6).
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 1448 summary. (Oct 07, 2007 - Oct 13, 2007)
Table 1.1448.a GPS week : 1448 MJD: 54380.0-54386.0
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| 0 -1 7 37 20 -49 -.07 40 36 | 0 24 3442 3701
| 4 2 7 28 43 93 .10 | 0 435
cod 174| 0 -2 -10 -73 -37 12 -.07 44 37 | --- --- --- ---
| 5 2 2 63 50 148 .11 | --- ---
esx 41| 1 4 49 -37 50 252 -.27 181 81 | 3318 -919 8831 20327
| 6 5 10 208 116 116 .26 | 12950 4239
iac n/a| -3 1 -16 -6 -8 0 .19 46 46 | 1280240 526 8724 20791
| 4 3 11 22 56 62 .09 | 17934 4339
mcc n/a| -5 4 -38 50 45 1813 .37 146 146 | --- --- --- ---
| 32 14 75 339 158 1854 1.15 | --- ---
Table 1.1448.b GPS week : 1448 MJD: 54380.0-54386.0
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 | 33 37 24 29 32 23 21 |
R04 | 20 25 14 25 22 27 15 |
R06 | 30 28 22 32 23 25 27 |
R07 | 21 27 20 21 29 19 19 |
R08 | 26 25 37 38 25 23 17 |
R10 | 58 50 51 53 58 60 54 |
R14 | 66 58 56 52 58 48 63 |
R15 | --- --- --- --- --- 307 258 |
R21E | 45 33 44 45 38 30 28 |
R23E | 0 --- --- --- 0 40 36 |
Table 1.1448.c GPS week : 1448 MJD: 54380.0-54386.0
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 1448 0 | -333 111 578 -9397 10540 -5038 95.1 8090 8090 | 1284872 0
brd 1448 1 | 222 -401 1051 -278 -108 -11690 85.5 7095 7095 | 1263370 0
brd 1448 2 | -91 62 1301 -2612 -1020 -650 96.7 6067 6067 | 1244678 0
brd 1448 3 | 90 -247 900 1834 3697 1461 107.1 6283 6283 | 1288933 0
brd 1448 4 | -158 -92 618 -6390 1828 2738 104.8 5592 5592 | 1301694 0
brd 1448 5 | -126 -95 847 -5838 -3597 1975 93.6 5627 5627 | 1299395 0
brd 1448 6 | -145 383 268 -9382 -206 3959 93.4 4464 4464 | 1282878 0
-------------+------------------------------------------------------------+----------------
brd 1448 mean| -77 -39 795 -4580 1590 -1035 96.6 6174 6174 | 1280831 0
brd 1448 sdev| 181 255 339 4371 4554 5540 7.3 1162 1162 | 20322 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 2.1448.0 GPS week: 1448 Day: 0 MJD: 54380
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 0 8 79 27 61 .03 36 35 | 0 477 2627 2820
cod 174| 1 -3 -11 -133 -23 -75 -.19 44 37 | --- --- --- ---
esx 41| 4 3 52 361 62 348 -.09 174 81 | 18958 2980 8268 16732
iac n/a| -5 0 -40 -4 -1 -93 .32 71 71 | 1282854 5095 7962 17345
mcc n/a| 3 5 35 160 -92 1394 -.12 59 59 | --- --- --- ---
Table 2.1448.1 GPS week: 1448 Day: 1 MJD: 54381
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| -1 -2 12 21 70 -99 -.07 35 32 | 0 -436 2818 2977
cod 174| 0 -7 -11 -30 -140 33 .00 39 23 | --- --- --- ---
esx 41| 9 3 35 -24 43 318 -.46 184 80 | 4281 -907 6684 17435
iac n/a| 0 6 -17 -20 39 31 .23 57 57 | 1267045 -46 7047 17836
mcc n/a| 10 18 -104 499 -72 2187 .45 163 163 | --- --- --- ---
Table 2.1448.2 GPS week: 1448 Day: 2 MJD: 54382
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 -4 20 22 21 -175 -.16 47 38 | 0 -548 3771 4168
cod 174| 3 1 -9 -44 -3 263 -.25 51 45 | --- --- --- ---
esx 41| -8 12 39 -30 149 63 -.48 180 76 | -15496 -1233 7164 17058
iac n/a| 0 0 -14 0 4 -77 .13 32 32 | 1246031 -751 6827 18416
mcc n/a| -42 -22 -71 333 380 3603 -1.52 260 260 | --- --- --- ---
Table 2.1448.3 GPS week: 1448 Day: 3 MJD: 54383
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| -8 -5 4 72 -65 75 .09 49 43 | 0 159 2910 3048
cod 174| 9 -2 -13 -147 -5 -65 .00 52 49 | --- --- --- ---
esx 41| 0 -4 63 23 -128 362 -.47 192 94 | 11968 -1020 10470 17111
iac n/a| -7 -3 -6 11 26 33 .13 40 40 | 1291290 -1203 9804 17553
mcc n/a| -58 8 -163 -554 19 4853 2.18 382 382 | --- --- --- ---
Table 2.1448.4 GPS week: 1448 Day: 4 MJD: 54384
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 3 10 43 -98 -.12 39 36 | 0 615 4467 4854
cod 174| 3 -2 -7 -95 -43 163 .01 44 37 | --- --- --- ---
esx 41| -3 0 58 -104 190 143 -.36 177 76 | 15473 -4797 9190 28580
iac n/a| -12 2 -18 -40 -130 -9 .30 54 54 | 1296428 -3050 9221 28624
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1448.5 GPS week: 1448 Day: 5 MJD: 54385
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 -2 4 12 41 -15 -.17 34 30 | 0 -131 3519 3653
cod 174| -3 0 -9 -95 -53 -121 -.01 45 38 | --- --- --- ---
esx 41| 7 9 52 -307 110 327 -.23 186 101 | -3585 5493 12818 24268
iac n/a| 0 2 -14 27 9 37 .13 35 35 | 1293515 7779 12774 23825
mcc n/a| 36 18 14 -116 82 13 1.18 114 114 | --- --- --- ---
Table 2.1448.6 GPS week: 1448 Day: 6 MJD: 54386
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| 1 0 -4 42 7 -97 -.09 43 38 | 0 32 3985 4389
cod 174| -7 -2 -6 31 5 -109 -.05 37 32 | --- --- --- ---
esx 41| 3 6 42 -177 -73 202 .21 174 62 | -8367 -6950 7224 21105
iac n/a| 0 0 -6 -17 -9 71 .11 36 36 | 1284517 -4140 7438 21944
mcc n/a| 10 0 22 26 -1 647 .41 44 44 | --- --- --- ---
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 3.1448.0 GPS week: 1448 Day: 0 MJD: 54380
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7329 24 49 44 98 --- 32 | 27 60 62 87 --- 40
R04 | 5908 29 39 55 21 --- 20 | 37 44 41 37 --- 29
R06 | 3111 31 36 117 56 --- 30 | 25 40 78 34 --- 25
R07 | 6830 34 20 47 51 59 20 | 40 22 66 30 139 22
R08 | 9443 35 32 54 69 --- 26 | 41 34 71 80 --- 45
R10 | 3622 35 25 308 55 --- 57 | 23 36 81 49 --- 35
R14 | 5386 50 46 347 46 --- 66 | 37 26 104 29 --- 24
R21E |15730 45 77 59 123 --- 45 | 91 145 89 136 --- 111
XR23E |37816 --- 12 1528 --- --- 0 | --- 9999 9999 --- --- 434
------+------------------------------------+--------------------------------
RMS | 8091 36 44 174 71 59 |T 40 76 74 60 503 85
WRMS | 8091 35 37 81 71 59 |NE 32 68 71 49 503 31
MEDI | 6830 34 36 59 55 59 |MD 37 40 71 37 139 35
Table 3.1448.1 GPS week: 1448 Day: 1 MJD: 54381
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7922 27 53 50 104 --- 36 | 41 62 41 47 --- 36
R04 | 2378 32 10 138 24 --- 25 | 20 31 111 49 --- 27
R06 | 6251 25 50 111 45 --- 28 | 30 47 79 40 --- 27
R07 | 7940 25 12 116 60 163 26 | 29 22 96 34 87 23
R08 | 8740 30 31 95 52 --- 25 | 18 31 60 60 --- 23
R10 | 2131 29 22 300 52 --- 49 | 28 39 112 30 --- 27
R14 | 5016 44 32 349 38 --- 57 | 28 35 58 30 --- 26
R21E |11227 54 66 48 44 --- 32 | 46 63 75 69 --- 49
------+------------------------------------+--------------------------------
RMS | 7095 34 39 184 57 163 |T 30 56 79 44 321 29
WRMS | 7095 32 23 80 57 163 |NE 27 55 79 41 321 27
MEDI | 6251 29 31 111 45 163 |MD 28 39 75 40 87 27
Table 3.1448.2 GPS week: 1448 Day: 2 MJD: 54382
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8902 24 41 71 45 --- 24 | 41 57 78 33 --- 33
R04 | 3502 28 20 44 19 --- 14 | 27 31 80 36 --- 30
R06 | 6887 24 51 79 21 --- 22 | 32 65 33 40 --- 38
R07 | 8260 20 21 103 24 260 20 | 31 32 79 72 106 41
R08 | 7983 28 71 171 35 --- 36 | 39 83 116 47 --- 36
R10 | 2509 35 35 308 30 --- 50 | 40 38 46 34 --- 31
R14 | 1445 60 36 334 30 --- 56 | 40 32 75 40 --- 33
R21E | 3893 99 92 37 40 --- 43 | 95 93 115 90 --- 83
------+------------------------------------+--------------------------------
RMS | 6066 47 51 180 32 260 |T 43 78 77 49 492 40
WRMS | 6066 38 45 76 32 260 |NE 35 76 72 43 492 34
MEDI | 3893 28 36 79 30 260 |MD 39 57 78 40 106 33
Table 3.1448.3 GPS week: 1448 Day: 3 MJD: 54383
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8116 32 73 66 30 --- 28 | 27 85 89 38 --- 42
R04 | 5355 51 21 105 27 --- 24 | 38 41 48 34 --- 24
R06 | 6554 30 67 48 61 --- 32 | 22 63 39 70 --- 41
R07 | 6523 33 24 101 24 382 21 | 49 40 81 59 252 44
R08 | 7268 45 78 92 59 --- 37 | 24 96 72 81 --- 48
R10 | 2057 38 50 327 27 --- 52 | 41 50 108 49 --- 44
R14 | 2227 40 23 330 38 --- 52 | 52 46 81 50 --- 47
R21E | 8585 93 38 206 38 --- 44 | 83 125 149 72 --- 77
------+------------------------------------+--------------------------------
RMS | 6282 49 52 192 40 382 |T 42 104 83 56 553 45
WRMS | 6282 43 49 94 40 382 |NE 36 102 74 54 553 41
MEDI | 6523 38 38 101 30 382 |MD 38 63 81 50 252 44
Table 3.1448.4 GPS week: 1448 Day: 4 MJD: 54384
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7476 34 70 70 51 --- 31 | 41 80 69 54 --- 45
R04 | 4835 24 34 80 36 --- 21 | 35 48 51 28 --- 27
R06 | 5567 21 36 42 56 --- 22 | 44 34 89 62 --- 43
R07 | 7928 32 21 151 33 --- 29 | 35 22 114 37 --- 19
R08 | 6754 23 44 52 56 --- 25 | 32 50 36 64 --- 33
R10 | 1460 61 47 315 38 --- 57 | 27 46 109 70 --- 40
R14 | 1461 38 44 331 45 --- 58 | 34 37 92 58 --- 30
R21E | 5204 55 40 64 92 --- 37 | 161 107 59 72 --- 97
XR23E | ---- --- 12 292 --- --- 0 | --- 9999 9999 --- --- 547
------+------------------------------------+--------------------------------
RMS | 5591 39 44 177 54 0 |T 51 89 77 55 --- 97
WRMS | 5591 36 37 76 54 0 |NE 35 87 80 53 --- 33
MEDI | 5204 32 40 80 45 0 |MD 35 48 69 58 --- 40
Table 3.1448.5 GPS week: 1448 Day: 5 MJD: 54385
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6775 24 45 87 33 --- 23 | 52 64 93 56 --- 55
R04 | 3026 20 43 128 38 --- 27 | 18 38 63 47 --- 18
R06 | 3903 40 40 62 45 --- 25 | 41 38 90 85 --- 46
R07 | 6012 23 21 101 22 114 19 | 20 29 91 27 209 22
R08 | 8724 31 35 69 40 --- 22 | 25 39 60 58 --- 33
R10 | 2022 46 54 362 41 --- 59 | 52 55 94 66 --- 57
R14 | 2191 25 35 312 19 --- 48 | 20 27 83 40 --- 30
XR15 |>>>>> --- 357 --- 264 1461 306 | --- 307 --- 102 9999 69
R21E | 7865 47 68 71 31 --- 29 | 57 65 53 54 --- 39
XR23 | ---- --- 48 350 32 --- 39 | --- 461 507 49 --- 346
------+------------------------------------+--------------------------------
RMS | 5627 34 45 186 35 114 |T 35 112 126 58 209 71
WRMS | 5627 30 38 101 35 114 |NE 32 117 135 58 209 75
MEDI | 6012 25 43 101 33 114 |MD 25 39 90 54 209 39
Table 3.1448.6 GPS week: 1448 Day: 6 MJD: 54386
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7322 40 19 46 40 --- 20 | 34 62 66 57 --- 42
R04 | 2957 9 26 57 22 --- 14 | 29 40 46 35 --- 28
R06 | 1633 59 24 65 44 --- 26 | 48 65 57 89 --- 56
R07 | 3669 23 35 64 22 44 18 | 18 22 67 33 101 22
R08 | 7776 37 20 40 26 --- 17 | 36 50 80 50 --- 39
R10 | 1928 58 51 296 38 --- 53 | 45 46 97 44 --- 43
R14 | 1577 53 36 367 50 --- 63 | 37 30 85 32 --- 29
XR15 |10500 --- 265 --- 251 253 258 | --- 355 --- 91 9999 46
R21 | 3771 40 61 73 33 --- 28 | 122 104 110 119 --- 109
XR23 | ---- --- 36 438 34 --- 35 | --- 853 960 44 --- 481
------+------------------------------------+--------------------------------
RMS | 4463 43 37 174 36 44 |T 46 162 174 59 101 89
WRMS | 4463 38 32 62 36 44 |NE 46 162 174 59 101 89
MEDI | 3669 40 35 65 34 44 |MD 36 50 80 44 101 42
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