From igsacc at gfz-potsdam.de Thu Oct 18 03:54:57 2007 From: igsacc at gfz-potsdam.de (Gerd Gendt3) Date: Thu, 18 Oct 2007 12:54:57 +0200 Subject: [IGSREPORT-15578] Wk 1447 IGLOS Final Orbits Message-ID: <20071018105457.47F1550984@kg20.gfz-potsdam.de> ****************************************************************************** IGS Electronic Report 18 Oct 03:55:07 PDT 2007 Message Number 15578 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 IGLOS Orbit Combination - Week 1447 (Sep 30, 2007 - Oct 06, 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 2.1447. 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: igl1447[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1447 in the SP3 format. igl14477.sum Combination Report for GPS Week 1447. 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 | 1266.5 ns 1 | 1252.8 ns 2 | 1228.2 ns 3 | 1260.8 ns 4 | 1256.3 ns 5 | 1257.0 ns 6 | 1236.4 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 | R02 R03 R18 R19 R21 R24 1 | COD | R15 1 | ESX | R02 R03 R18 R19 R24 2 | COD | R15 2 | ESX | R02 R03 R18 R19 R23 R24 3 | COD | R15 3 | ESX | R02 R03 R18 R19 R23 R24 4 | COD | R15 4 | ESX | R02 R03 R18 R19 R23 R24 5 | COD | R15 5 | ESX | R02 R03 R18 R19 R24 6 | COD | R15 6 | ESX | R02 R03 R18 R19 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 1.1447, 1a.1447). 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 2.1447.0-6) 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 3.1447.0-6). 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 1447 summary. (Sep 30, 2007 - Oct 06, 2007) Table 1.1447.a GPS week : 1447 MJD: 54373.0-54379.0 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 56| 1 0 0 17 17 -59 .05 48 37 | 0 1001 4329 4801 | 4 5 10 86 21 111 .13 | 0 1928 cod 171| -1 -2 -9 -51 -56 -1 -.11 43 32 | --- --- --- --- | 6 6 6 81 44 83 .07 | --- --- esx 40| 7 9 56 -125 29 -24 -.33 401 127 | 3029035 108224 154316 169489 | 27 18 35 298 195 448 .54 | 4423644 220068 iac n/a| 0 0 -6 24 19 36 .09 44 44 | 1247855 -1553 12688 31786 | 3 4 9 42 25 106 .08 | 14829 13908 mcc n/a| 3 5 15 54 116 -377 .81 111 111 | --- --- --- --- | 35 7 12 81 251 601 .77 | --- --- Table 1.1447.b GPS week : 1447 MJD: 54373.0-54379.0 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 49 29 26 22 19 18 | R04 | 23 124 26 22 20 21 16 | R06 | 27 25 27 30 24 35 22 | R07 | 26 41 25 22 15 22 23 | R08 | 34 46 28 29 26 22 26 | R10 | 49 71 48 61 60 60 52 | R14 | 49 94 59 55 53 55 53 | R21E | 66 191 35 55 27 24 29 | R23E | 85 105 130 100 44 38 84 | R24E | 0 592 1191 480 330 --- --- | Table 1.1447.c GPS week : 1447 MJD: 54373.0-54379.0 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 1447 0 | -209 52 428 2847 2525 11330 93.8 3694 3694 | 1266501 0 brd 1447 1 | 233 115 281 -2339 1405 11640 97.7 3693 3693 | 1252763 0 brd 1447 2 | 67 47 349 2442 7664 6156 98.8 4310 4310 | 1228226 0 brd 1447 3 | 26 -194 96 6033 -3352 6856 96.7 4987 4987 | 1260776 0 brd 1447 4 | -181 2 272 -5783 686 7841 91.1 5574 5574 | 1256263 0 brd 1447 5 | -318 294 144 -2241 -3320 -6911 98.3 7631 7631 | 1257044 0 brd 1447 6 | 121 -148 220 -3883 2553 -6328 99.9 7833 7833 | 1236412 0 -------------+------------------------------------------------------------+---------------- brd 1447 mean| -37 24 256 -417 1165 4369 96.6 5388 5388 | 1251140 0 brd 1447 sdev| 201 163 114 4247 3803 7793 3.1 1737 1737 | 13750 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 2.1447.0 GPS week: 1447 Day: 0 MJD: 54373 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 56| 2 -5 11 103 23 42 -.08 48 34 | 0 685 3206 3392 cod 171| 3 1 0 -157 -49 103 -.07 56 34 | --- --- --- --- esx 40| -35 5 5 278 -89 -266 -.45 997 114 | -999999 36863 16005 38246 iac n/a| 1 0 -17 94 45 -20 .01 40 40 | 1267457 -19884 14920 35985 mcc n/a| -27 4 37 63 370 -862 1.52 136 136 | --- --- --- --- Table 2.1447.1 GPS week: 1447 Day: 1 MJD: 54374 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 56| 2 3 -11 -46 -1 -113 .24 72 33 | 0 487 5224 6001 cod 171| -12 -5 -11 -92 -117 14 -.10 49 40 | --- --- --- --- esx 40| 50 50 110 -664 -153 -904 -1.25 783 335 | 9999999 78945 22778 42901 iac n/a| 4 0 4 39 16 112 .08 62 62 | 1236373 19040 21125 45942 mcc n/a| -35 8 16 51 43 -710 1.87 142 142 | --- --- --- --- Table 2.1447.2 GPS week: 1447 Day: 2 MJD: 54375 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 56| -9 8 -15 34 -14 -221 .04 45 42 | 0 866 3586 3940 cod 171| 7 -8 -10 -19 -30 -36 -.05 34 27 | --- --- --- --- esx 40| 28 0 64 -292 419 69 .10 206 106 | 3294041 42810 14317 34482 iac n/a| -3 5 4 17 22 181 .05 43 43 | 1231024 -14389 14689 35392 mcc n/a| -25 0 0 109 -91 -818 -.08 128 128 | --- --- --- --- Table 2.1447.3 GPS week: 1447 Day: 3 MJD: 54376 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 56| 2 3 2 -123 40 -82 .20 52 41 | 0 5185 8106 9422 cod 171| 0 5 -19 89 -4 95 -.19 51 27 | --- --- --- --- esx 40| -5 -3 87 -50 133 -31 -.00 186 97 | 7489441 594737 999999 999999 iac n/a| 0 -1 -9 -45 0 -109 .13 50 50 | 1258503 -10212 10664 34760 mcc n/a| 6 4 25 1 -131 -760 -.09 110 110 | --- --- --- --- Table 2.1447.4 GPS week: 1447 Day: 4 MJD: 54377 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 56| 4 -5 9 -21 38 -11 -.05 32 31 | 0 534 3119 3278 cod 171| -5 6 -3 -9 -15 1 -.07 33 31 | --- --- --- --- esx 40| 16 -2 49 -103 -77 303 -.42 205 89 | 3419763 70430 8343 20199 iac n/a| 1 -7 -17 38 -24 -40 .04 35 35 | 1253194 8903 8267 19406 mcc n/a| 59 19 2 -96 415 -450 1.23 117 117 | --- --- --- --- Table 2.1447.5 GPS week: 1447 Day: 5 MJD: 54378 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 56| 3 -5 0 118 34 -135 .09 44 44 | 0 90 2576 2763 cod 171| -4 -5 -10 -58 -71 -59 -.07 30 30 | --- --- --- --- esx 40| -9 3 34 87 29 391 -.64 184 80 | -999999 664 9401 21377 iac n/a| -4 4 0 16 40 132 .24 45 45 | 1257480 287 8778 21272 mcc n/a| 35 -4 10 147 345 435 .80 74 74 | --- --- --- --- Table 2.1447.6 GPS week: 1447 Day: 6 MJD: 54379 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 56| 3 2 4 54 3 104 -.06 39 35 | 0 -836 4487 4817 cod 171| 5 -8 -10 -114 -110 -128 -.22 46 37 | --- --- --- --- esx 40| 4 12 39 -130 -58 267 .37 246 70 | -999999 -66878 9374 29220 iac n/a| -3 1 -10 7 38 -1 .07 36 36 | 1230956 5383 10375 29750 mcc n/a| 13 5 18 102 -134 525 .43 70 70 | --- --- --- --- 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 3.1447.0 GPS week: 1447 Day: 0 MJD: 54373 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 4390 27 40 60 43 --- 22 | 44 49 94 43 --- 39 R04 | 5346 38 29 114 27 --- 23 | 54 29 260 33 --- 31 R06 | 1954 33 25 161 38 --- 27 | 17 34 162 54 --- 34 R07 | 1078 25 45 143 28 136 26 | 21 66 175 41 30 33 R08 | 4023 47 43 184 45 --- 34 | 52 38 171 50 --- 23 R10 | 2015 32 23 377 20 --- 49 | 28 30 254 40 --- 31 R14 | 2913 36 31 363 24 --- 48 | 44 36 305 33 --- 33 R21E | 4593 96 123 2864 46 --- 65 | 317 333 9999 325 --- 324 R23E | 4488 55 68 618 65 --- 85 | 71 85 939 70 --- 70 XR24E | ---- --- 11 998 --- --- 0 | --- 592 9999 --- --- 9999 ------+------------------------------------+-------------------------------- RMS | 3694 48 56 997 40 136 |T 72 129 295 76 30 68 WRMS | 3694 34 34 114 40 136 |NE 37 40 203 42 30 32 MEDI | 4023 36 31 184 38 136 |MD 44 38 175 43 30 33 Table 3.1447.1 GPS week: 1447 Day: 1 MJD: 54374 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 5886 23 39 391 40 --- 49 | 33 36 330 48 --- 32 R04 | 4825 37 50 1046 64 --- 123 | 25 32 773 44 --- 34 R06 | 2161 39 30 152 21 --- 24 | 26 34 99 47 --- 23 R07 | 1067 26 44 313 22 142 40 | 18 26 273 42 23 28 R08 | 4785 26 35 347 56 --- 46 | 42 65 333 36 --- 42 R10 | 1307 26 39 594 41 --- 71 | 21 29 350 39 --- 22 R14 | 2230 36 36 797 42 --- 94 | 43 24 629 24 --- 43 R21E | 3771 177 78 1549 98 --- 190 | 209 290 9999 220 --- 230 R23E | 3901 95 65 798 108 --- 104 | 174 84 9999 70 --- 99 XR24E |62491 653 536 1074 --- --- 592 | 727 876 9999 --- --- 9999 ------+------------------------------------+-------------------------------- RMS | 3693 72 49 783 62 142 |T 131 149 398 63 23 61 WRMS | 3693 33 40 335 62 142 |NE 29 35 398 40 23 32 MEDI | 3771 36 39 594 42 142 |MD 33 34 333 44 23 34 Table 3.1447.2 GPS week: 1447 Day: 2 MJD: 54375 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 7525 54 24 78 62 --- 28 | 31 30 73 87 --- 29 R04 | 5529 35 34 126 37 --- 26 | 35 33 315 36 --- 26 R06 | 2883 28 36 119 46 --- 26 | 55 73 133 35 --- 49 R07 | 4546 31 16 146 33 128 25 | 16 26 136 53 21 25 R08 | 2940 29 17 179 23 --- 28 | 28 39 224 30 --- 27 R10 | 1062 45 36 300 51 --- 48 | 39 61 142 43 --- 42 R14 | 3065 53 33 394 36 --- 59 | 34 28 147 24 --- 15 R21E | 3638 71 59 70 43 --- 34 | 335 335 623 336 --- 319 XR23E | 7490 145 116 3781 --- --- 129 | 163 126 9999 --- --- 89 XR24E |>>>>> 1374 1032 1516 --- --- 1191 | 880 9999 9999 --- --- 9999 ------+------------------------------------+-------------------------------- RMS | 4309 45 34 206 43 128 |T 161 83 224 80 21 69 WRMS | 4309 42 27 106 43 128 |NE 34 41 167 44 21 30 MEDI | 3638 45 34 146 37 128 |MD 35 39 142 36 21 29 Table 3.1447.3 GPS week: 1447 Day: 3 MJD: 54376 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 3741 40 57 48 32 --- 26 | 25 38 73 55 --- 25 R04 |11572 29 31 75 38 --- 21 | 46 48 136 41 --- 32 R06 | 2316 30 62 65 51 --- 29 | 22 69 72 29 --- 28 R07 | 2275 34 20 105 26 109 22 | 34 30 117 27 29 21 R08 | 2456 27 32 149 33 --- 28 | 66 37 120 30 --- 37 R10 | 1173 52 43 327 82 --- 60 | 23 50 84 80 --- 30 R14 | 3890 53 31 325 33 --- 54 | 36 23 151 33 --- 21 R21E | 4235 104 93 131 71 --- 54 | 201 303 536 274 --- 245 XR23E | 5739 104 94 3914 --- --- 99 | 196 243 9999 --- --- 199 XR24E |>>>>> 496 464 1740 --- --- 479 | 580 9999 9999 --- --- 9999 ------+------------------------------------+-------------------------------- RMS | 4986 52 51 185 50 109 |T 122 93 161 71 29 70 WRMS | 4986 41 27 97 50 109 |NE 36 42 107 42 29 27 MEDI | 3741 40 43 131 33 109 |MD 36 48 117 33 29 30 Table 3.1447.4 GPS week: 1447 Day: 4 MJD: 54377 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 3625 26 23 124 24 --- 22 | 44 24 95 31 --- 26 R04 | 8121 39 29 38 32 --- 19 | 27 47 98 33 --- 27 R06 | 2360 32 51 55 31 --- 23 | 17 90 82 38 --- 39 R07 | 5088 18 20 68 21 117 14 | 26 20 61 31 16 20 R08 | 3857 25 13 168 18 --- 26 | 35 34 96 45 --- 30 R10 | 1486 41 40 391 50 --- 60 | 22 39 100 65 --- 37 R14 | 3273 29 37 358 21 --- 53 | 29 25 222 32 --- 22 R21E |10496 42 32 59 59 --- 27 | 320 326 438 331 --- 321 XR23E | 5913 43 45 1831 --- --- 44 | 166 123 9999 --- --- 138 XR24E |25380 326 334 3518 --- --- 330 | 870 9999 9999 --- --- 9999 ------+------------------------------------+-------------------------------- RMS | 5573 32 33 205 35 117 |T 155 80 149 75 16 73 WRMS | 5573 31 31 89 35 117 |NE 28 39 107 39 16 28 MEDI | 3857 32 32 124 24 117 |MD 29 39 96 33 16 30 Table 3.1447.5 GPS week: 1447 Day: 5 MJD: 54378 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 4692 39 24 57 29 --- 19 | 38 30 66 29 --- 19 R04 | 7425 18 18 88 43 --- 20 | 19 45 93 48 --- 29 R06 | 1831 69 38 57 73 --- 34 | 43 41 39 72 --- 20 R07 | 6755 20 23 93 43 74 22 | 25 32 55 48 16 28 R08 | 4706 44 17 95 26 --- 22 | 49 37 118 29 --- 31 R10 | 1648 57 32 356 50 --- 60 | 30 33 58 60 --- 31 R14 | 2193 34 43 334 35 --- 55 | 12 33 75 25 --- 19 R21E |17607 46 34 48 45 --- 24 | 225 231 379 219 --- 221 XR23E | 4233 39 54 --- 63 --- 37 | 81 72 --- 53 --- 62 ------+------------------------------------+-------------------------------- RMS | 7630 44 30 184 45 74 |T 58 61 110 64 16 51 WRMS | 7630 44 30 80 45 74 |NE 30 35 72 44 16 25 MEDI | 4692 39 32 88 43 74 |MD 38 37 66 48 16 29 Table 3.1447.6 GPS week: 1447 Day: 6 MJD: 54379 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 5758 22 42 58 20 --- 18 | 30 49 60 45 --- 33 R04 | 6958 25 21 81 12 --- 15 | 25 47 74 39 --- 27 R06 | 1717 36 25 106 24 --- 22 | 38 41 85 40 --- 33 R07 | 6659 41 37 56 37 70 23 | 43 37 90 34 16 28 R08 | 6931 55 46 40 37 --- 26 | 69 41 104 33 --- 40 R10 | 2502 40 23 340 34 --- 52 | 42 38 55 52 --- 36 R14 | 3140 31 43 345 35 --- 53 | 30 24 109 20 --- 22 R21E |18328 47 47 59 53 --- 29 | 316 310 688 313 --- 316 R23E | 4821 42 90 528 52 --- 83 | 45 75 842 78 --- 57 ------+------------------------------------+-------------------------------- RMS | 7833 39 46 245 36 70 |T 70 73 234 72 16 65 WRMS | 7833 35 37 70 36 70 |NE 39 39 82 37 16 31 MEDI | 5758 40 42 81 35 70 |MD 42 41 90 40 16 33