From IGS.ACC at noaa.gov Thu Aug 27 04:58:08 2009 From: IGS.ACC at noaa.gov (Jim Ray) Date: Thu, 27 Aug 2009 11:58:08 +0000 Subject: [IGSREPORT-17737] Wk 1544 IGLOS Final Orbits Message-ID: <4a9674d0.dM1MM+L7dPE5DysQ%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 27 Aug 04:58:30 PDT 2009 Message Number 17737 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 IGLOS Orbit Combination - Week 1544 (Aug 09, 2009 - Aug 15, 2009) Contact: J. Ray (jim.ray at noaa.gov), J. Griffiths (jake.griffiths at noaa.gov) 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 2.1544. 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: igl1544[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1544 in the SP3 format. igl15447.sum Combination Report for GPS Week 1544. 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 | 227.0 ns 1 | 222.7 ns 2 | 226.3 ns 3 | 226.0 ns 4 | 227.0 ns 5 | 223.7 ns 6 | 222.9 ns 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 1.1544, 1a.1544). 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 2.1544.0-6) 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 3.1544.0-6). 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 1544 summary. (Aug 09, 2009 - Aug 15, 2009) Table 1.1544.a GPS week : 1544 MJD: 55052.0-55058.0 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 109| 2 0 -9 -9 -11 43 -.12 31 26 | 0 -174 3499 3990 | 2 0 4 32 30 158 .05 | 0 475 cod 235| -3 0 -3 4 9 58 -.15 15 12 | --- --- --- --- | 2 1 2 14 29 27 .02 | --- --- esx 126| 0 0 0 24 8 31 .41 25 23 | 113487 1984 4903 10007 | 2 0 3 29 37 76 .06 | 5248 2015 iac n/a| 3 0 12 -37 -6 -149 -.05 26 26 | 225082 -705 4905 9949 | 1 0 5 24 31 81 .05 | 1547 1370 mcc n/a| -5 -1 44 -23 -26 207 .37 148 148 | --- --- --- --- | 9 7 7 99 70 230 .28 | --- --- Table 1.1544.b GPS week : 1544 MJD: 55052.0-55058.0 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 ------+------------------------------------+------------------------------------------ R02 | 17 11 12 11 11 9 12 | R03 | 10 9 14 13 12 10 11 | R07 | 10 11 12 9 14 9 10 | R08 | 8 7 12 9 11 12 9 | R10 | 10 12 16 12 12 14 10 | R11 | 10 12 17 15 10 7 12 | R13 | 11 9 9 13 10 10 10 | R14 | 14 13 10 7 14 12 12 | R15 | 9 15 14 14 11 14 14 | R17 | 22 14 16 14 17 14 13 | R18 | 15 11 11 16 16 11 11 | R19 | 9 12 11 16 9 7 9 | R20 | 12 14 21 13 12 15 17 | R21 | 18 13 19 15 10 12 11 | R22 | 15 10 17 16 10 11 14 | R23 | 16 17 16 18 18 18 14 | R24 | 25 11 17 14 18 33 30 | Table 1.1544.c GPS week : 1544 MJD: 55052.0-55058.0 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 1544 0 | -104 40 504 -1272 -2156 -13860 89.8 2735 2735 | 226959 0 brd 1544 1 |52950 ---- ---- -161300 -368800 376800 <<<< >>>>> >>>>> | 222716 0 brd 1544 2 | 55 -8 584 2027 238 -13460 88.0 46770 46770 | 226313 0 brd 1544 3 | 7 -59 542 566 463 -14170 87.4 2723 2723 | 226043 0 brd 1544 4 | 62 40 470 -764 511 -16470 88.0 2639 2639 | 227007 0 brd 1544 5 | -31 82 496 -2140 441 -13180 85.2 2909 2909 | 223684 0 brd 1544 6 | 110 -39 413 969 3022 -11610 91.0 3058 3058 | 222876 0 -------------+------------------------------------------------------------+---------------- brd 1544 mean| 7578 -7287 -3874 -23130 -52325 42007 <<<< >>>>> >>>>> | 225085 0 brd 1544 sdev|20007 19306 11577 60943 139560 147636 743.5 >>>>> >>>>> | 1918 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 2.1544.0 GPS week: 1544 Day: 0 MJD: 55052 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 109| 2 0 -4 -29 -5 158 -.03 33 26 | 0 384 3197 3626 cod 235| -4 -1 -6 11 -26 46 -.12 15 12 | --- --- --- --- esx 126| 0 0 -2 43 63 62 .45 29 24 | 108263 3964 4775 11586 iac n/a| 4 0 15 -26 6 -246 -.12 27 27 | 224763 527 4770 11410 mcc n/a| -3 -4 47 -168 19 592 .41 168 168 | --- --- --- --- Table 2.1544.1 GPS week: 1544 Day: 1 MJD: 55053 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 109| 5 0 -14 -30 12 163 -.13 26 24 | 0 -622 3758 4120 cod 235| -4 0 -2 -21 -28 63 -.13 13 12 | --- --- --- --- esx 126| 0 0 6 28 15 -92 .41 21 19 | 113875 -1231 4999 9539 iac n/a| 4 0 17 -30 10 -93 -.12 25 25 | 224805 -1208 4996 9621 mcc n/a| -9 -13 31 -120 -49 -78 .56 185 185 | --- --- --- --- Table 2.1544.2 GPS week: 1544 Day: 2 MJD: 55054 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 109| 0 0 -12 58 31 -201 -.14 32 28 | 0 31 3853 4604 cod 235| -7 0 -3 -3 -1 61 -.14 17 14 | --- --- --- --- esx 126| 2 0 -2 -22 -31 97 .39 27 28 | 114889 1224 5711 9909 iac n/a| 5 0 15 -10 32 -22 -.02 27 27 | 225094 -718 5697 10097 mcc n/a| 12 -6 41 105 27 51 .50 127 127 | --- --- --- --- Table 2.1544.3 GPS week: 1544 Day: 3 MJD: 55055 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 109| 0 1 -6 -4 -47 149 -.18 30 27 | 0 -552 2907 3294 cod 235| -1 0 -2 10 20 23 -.13 15 14 | --- --- --- --- esx 126| 0 0 -3 1 12 69 .38 24 23 | 111687 3306 4909 10240 iac n/a| 0 0 12 -31 -40 -222 -.04 27 27 | 226385 -365 4943 9622 mcc n/a| -20 9 47 83 -25 356 .20 122 122 | --- --- --- --- Table 2.1544.4 GPS week: 1544 Day: 4 MJD: 55056 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 109| -1 0 -3 -6 -50 165 -.07 26 25 | 0 247 2859 3233 cod 235| -1 1 0 22 48 30 -.16 13 11 | --- --- --- --- esx 126| 3 -1 1 17 -31 -7 .48 26 26 | 107018 1384 4728 9482 iac n/a| 2 -1 5 -72 4 -216 -.02 30 30 | 227449 -2416 4727 9354 mcc n/a| -8 3 43 -49 -122 331 -.17 122 122 | --- --- --- --- Table 2.1544.5 GPS week: 1544 Day: 5 MJD: 55057 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 109| 1 0 -8 -38 -23 -147 -.12 35 26 | 0 102 4427 5164 cod 235| 0 0 -1 14 27 82 -.16 15 12 | --- --- --- --- esx 126| -4 1 0 69 47 119 .47 28 25 | 115999 804 4285 9976 iac n/a| 1 -1 6 -70 -57 -120 -.05 23 23 | 224574 -2146 4295 10000 mcc n/a| -4 4 56 4 -104 121 .65 141 141 | --- --- --- --- Table 2.1544.6 GPS week: 1544 Day: 6 MJD: 55058 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 109| 5 1 -15 -13 5 18 -.17 34 24 | 0 -813 3495 3894 cod 235| -2 2 -6 -1 26 100 -.18 15 13 | --- --- --- --- esx 126| -2 0 5 36 -15 -31 .31 23 20 | 122678 4443 4915 9319 iac n/a| 4 0 17 -21 0 -126 -.00 25 25 | 222507 1386 4908 9539 mcc n/a| -2 0 45 -20 68 73 .48 169 169 | --- --- --- --- 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 3.1544.0 GPS week: 1544 Day: 0 MJD: 55052 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1520 23 15 53 23 --- 17 | 19 25 25 28 --- 18 R03 | 5666 19 12 24 17 --- 10 | 21 27 27 28 --- 21 R07 | 1320 19 15 19 18 --- 10 | 24 36 36 29 --- 29 R08 | 1193 17 7 11 21 55 8 | 29 22 23 22 65 20 R10 | 4136 16 13 25 17 --- 10 | 17 17 28 17 --- 13 R11 | 1572 11 12 27 13 154 9 | 25 30 47 26 73 28 R13 | 993 27 9 14 26 --- 11 | 26 26 37 29 --- 24 R14 | 2509 29 17 17 35 --- 14 | 21 27 38 34 --- 23 R15 | 5131 15 10 10 21 80 8 | 21 21 31 21 35 20 R17 | 1640 41 20 43 51 --- 21 | 49 49 62 64 --- 48 R18 | 1813 38 15 30 26 --- 15 | 88 96 96 81 --- 89 R19 | 1599 16 8 20 22 --- 9 | 79 91 96 94 --- 89 R20 | 3075 25 13 26 25 --- 12 | 59 62 62 76 --- 63 R21 | 571 59 15 31 20 --- 18 | 78 89 98 90 --- 85 R22 | 1107 47 16 19 19 --- 14 | 112 133 139 127 --- 128 R23 | 2321 30 17 29 38 283 16 | 41 65 72 89 110 65 R24 | 3373 69 25 48 39 --- 25 | 204 249 265 227 --- 237 ------+------------------------------------+-------------------------------- RMS | 2734 33 15 29 27 168 |T 53 62 69 63 70 58 WRMS | 2734 26 12 24 27 168 |NE 53 62 69 63 70 58 MEDI | 1640 25 15 25 22 80 |MD 29 36 47 34 65 29 Table 3.1544.1 GPS week: 1544 Day: 1 MJD: 55053 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 |>>>>> 19 16 16 26 --- 11 | 15 33 29 30 --- 22 R03 |>>>>> 21 11 13 17 --- 8 | 19 27 37 26 --- 22 R07 |>>>>> 21 10 22 22 --- 10 | 25 28 34 26 --- 22 R08 |>>>>> 13 8 8 19 114 7 | 19 18 16 22 53 15 R10 | ---- 10 17 30 18 --- 11 | 24 13 39 29 --- 17 R11 |>>>>> 20 15 28 20 187 12 | 13 29 51 25 70 26 R13 |>>>>> 20 11 10 22 --- 9 | 21 26 21 19 --- 19 R14 |63347 25 11 22 33 --- 12 | 22 26 40 32 --- 25 R15 |>>>>> 24 13 31 36 98 15 | 14 13 39 42 62 19 R17 |>>>>> 27 14 33 18 --- 13 | 28 36 35 60 --- 35 R18 |>>>>> 21 16 13 23 --- 10 | 102 120 111 93 --- 109 R19 |>>>>> 22 14 22 24 --- 11 | 101 113 125 129 --- 116 R20 |>>>>> 41 12 13 33 --- 14 | 43 63 61 65 --- 56 R21 |>>>>> 36 9 24 18 --- 12 | 146 171 184 184 --- 172 R22 |>>>>> 31 11 8 17 --- 10 | 171 172 166 182 --- 172 R23 |>>>>> 42 14 28 39 283 17 | 26 41 56 66 84 43 R24 |>>>>> 24 13 15 26 --- 10 | 244 280 271 277 --- 270 ------+------------------------------------+-------------------------------- RMS |>>>>> 26 13 21 25 185 |T 60 71 77 76 67 68 WRMS |>>>>> 24 12 19 25 185 |NE 60 71 77 76 67 68 MEDI |>>>>> 22 13 22 22 114 |MD 25 33 40 42 62 26 Table 3.1544.2 GPS week: 1544 Day: 2 MJD: 55054 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 825 12 13 26 25 --- 11 | 27 24 30 29 --- 17 R03 | 9814 16 10 38 24 --- 13 | 26 31 41 37 --- 25 R07 | 1683 21 16 26 16 --- 11 | 27 35 38 25 --- 26 R08 | 1154 33 11 21 20 83 12 | 25 33 46 37 33 30 R10 | 3117 34 22 35 19 --- 15 | 24 35 57 19 --- 26 R11 | 1693 35 21 37 25 198 16 | 25 29 62 43 36 32 R13 | 1610 19 8 19 19 --- 9 | 32 26 29 24 --- 23 R14 | 3178 20 10 18 20 --- 9 | 29 21 33 22 --- 20 R15 | 3165 21 22 27 21 68 13 | 24 23 30 29 29 17 R17 | 1057 35 16 31 28 --- 15 | 20 37 50 39 --- 32 R18 | 1146 22 14 15 26 --- 11 | 117 123 122 104 --- 116 R19 | 1006 32 12 11 20 --- 11 | 97 133 144 138 --- 130 R20 |>>>>> 31 19 43 52 --- 21 | 52 63 64 90 --- 63 R21 | 2090 53 29 22 23 --- 18 | 100 166 161 163 --- 150 R22 | 620 43 21 25 28 --- 16 | 123 162 155 161 --- 151 R23 | 1923 44 11 23 35 118 16 | 35 54 53 72 43 52 R24 | 2385 44 21 28 29 --- 17 | 137 156 169 156 --- 153 ------+------------------------------------+-------------------------------- RMS |46771 32 17 27 27 127 |T 54 67 75 69 35 62 WRMS |46771 28 14 28 27 127 |NE 54 67 75 69 35 62 MEDI | 1693 32 16 26 24 83 |MD 29 35 53 39 33 32 Table 3.1544.3 GPS week: 1544 Day: 3 MJD: 55055 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 926 21 9 21 26 --- 11 | 20 20 28 33 --- 16 R03 | 6011 24 13 29 23 --- 12 | 25 26 38 36 --- 23 R07 | 2098 18 10 18 18 --- 9 | 20 35 31 31 --- 27 R08 | 1943 24 10 12 18 93 9 | 22 35 41 36 27 30 R10 | 948 25 19 20 19 --- 12 | 15 34 27 32 --- 22 R11 | 733 32 17 32 24 188 14 | 18 23 42 18 28 18 R13 | 1844 36 10 29 18 --- 13 | 32 21 35 21 --- 14 R14 | 6769 15 10 14 11 --- 7 | 30 30 26 34 --- 28 R15 | 1408 30 14 26 29 82 14 | 17 29 42 27 31 22 R17 | 1124 24 19 25 30 --- 14 | 22 31 34 35 --- 26 R18 | 858 40 20 18 36 --- 16 | 91 119 117 98 --- 107 R19 | 670 36 18 30 31 --- 16 | 130 140 140 147 --- 137 R20 | 3925 30 15 19 29 --- 13 | 34 49 42 50 --- 42 R21 | 982 39 15 27 26 --- 15 | 181 195 204 179 --- 189 R22 | 672 41 19 27 24 --- 15 | 187 200 221 198 --- 200 R23 | 2027 35 17 31 41 91 17 | 46 52 76 85 42 61 R24 | 2204 25 18 18 32 --- 13 | 146 179 176 159 --- 168 ------+------------------------------------+-------------------------------- RMS | 2723 30 15 24 27 122 |T 60 71 77 71 32 66 WRMS | 2723 27 14 23 27 122 |NE 60 71 77 71 32 66 MEDI | 1408 30 15 25 26 91 |MD 30 35 42 36 28 28 Table 3.1544.4 GPS week: 1544 Day: 4 MJD: 55056 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1731 18 7 25 30 --- 11 | 16 28 35 31 --- 21 R03 | 5022 18 12 20 35 --- 12 | 18 16 30 23 --- 14 R07 | 2185 18 10 39 31 --- 14 | 18 20 38 22 --- 18 R08 | 2682 17 11 26 25 107 11 | 26 31 34 45 14 28 R10 | 1824 25 13 16 34 --- 12 | 17 19 29 28 --- 11 R11 | 828 15 11 22 19 165 9 | 12 29 53 29 14 28 R13 | 1983 15 14 21 20 --- 10 | 18 18 32 27 --- 18 R14 | 6847 35 12 32 21 --- 14 | 22 30 41 19 --- 20 R15 | 1795 20 9 10 36 106 11 | 10 21 17 25 13 13 R17 | 1034 42 10 40 31 --- 17 | 25 41 51 43 --- 36 R18 | 1115 36 15 31 35 --- 16 | 125 141 152 118 --- 135 R19 | 979 16 10 13 22 --- 8 | 89 101 101 108 --- 99 R20 | 3313 23 12 27 21 --- 11 | 42 48 63 75 --- 52 R21 | 727 25 10 15 19 --- 9 | 93 117 123 109 --- 111 R22 | 634 23 7 22 21 --- 10 | 96 116 132 123 --- 116 R23 | 1330 35 19 28 50 97 18 | 33 37 64 81 38 47 R24 | 1775 41 22 25 42 --- 18 | 266 284 299 322 --- 290 ------+------------------------------------+-------------------------------- RMS | 2638 26 13 26 30 122 |T 54 64 76 72 19 62 WRMS | 2638 25 11 26 30 122 |NE 54 64 76 72 19 62 MEDI | 1775 23 11 25 30 106 |MD 25 31 51 43 14 28 Table 3.1544.5 GPS week: 1544 Day: 5 MJD: 55057 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 6052 18 12 14 17 --- 8 | 17 25 22 24 --- 16 R03 | 6658 21 9 20 21 --- 10 | 16 24 31 18 --- 16 R07 | 2058 21 11 19 16 --- 9 | 35 26 27 25 --- 22 R08 | 2331 26 12 30 16 116 11 | 22 39 48 34 15 33 R10 | 1703 22 21 31 20 --- 13 | 25 24 41 17 --- 19 R11 | 1166 11 7 17 16 173 7 | 28 27 37 35 18 29 R13 | 1038 19 14 24 14 --- 10 | 22 21 26 13 --- 11 R14 | 4526 24 15 26 18 --- 11 | 28 23 45 29 --- 24 R15 | 3459 31 10 32 25 135 13 | 9 17 42 20 23 15 R17 | 1056 43 9 33 16 --- 14 | 35 46 62 47 --- 46 R18 | 888 26 13 19 21 --- 11 | 82 109 118 84 --- 99 R19 | 1794 12 9 11 17 --- 7 | 104 102 101 105 --- 103 R20 | 1821 22 15 44 24 --- 15 | 46 50 45 68 --- 49 R21 | 938 16 14 31 24 --- 12 | 164 157 158 173 --- 162 R22 | 1288 21 10 22 24 --- 10 | 166 150 158 160 --- 156 R23 | 886 36 22 26 42 132 18 | 37 44 45 70 34 45 R24 | 1912 108 35 47 36 --- 32 | 192 273 287 268 --- 257 ------+------------------------------------+-------------------------------- RMS | 2909 35 15 28 23 141 |T 60 68 76 70 22 64 WRMS | 2909 26 12 25 23 141 |NE 60 68 76 70 22 64 MEDI | 1794 22 12 26 20 132 |MD 35 39 45 35 18 33 Table 3.1544.6 GPS week: 1544 Day: 6 MJD: 55058 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 3741 25 12 21 25 --- 11 | 19 28 29 25 --- 20 R03 | 8947 28 8 17 21 --- 10 | 28 17 20 23 --- 13 R07 | 3247 14 17 12 20 --- 9 | 33 38 30 30 --- 31 R08 | 1365 11 14 18 17 140 9 | 36 41 32 24 24 32 R10 | 2414 21 9 15 26 --- 10 | 22 19 32 15 --- 17 R11 | 2744 20 11 26 28 186 12 | 26 30 33 21 24 24 R13 | 1474 20 11 18 18 --- 9 | 19 20 19 22 --- 13 R14 | 2953 30 12 23 20 --- 11 | 23 22 38 25 --- 21 R15 | 2439 24 17 30 28 186 14 | 12 21 38 25 23 18 R17 | 1931 20 17 25 27 --- 12 | 34 47 50 53 --- 45 R18 | 795 26 14 16 24 --- 11 | 89 102 99 95 --- 97 R19 | 1944 13 12 18 19 --- 9 | 93 95 98 96 --- 95 R20 | 1217 44 12 34 27 --- 16 | 44 59 63 70 --- 58 R21 | 1234 13 13 19 25 --- 10 | 155 155 157 168 --- 158 R22 | 1707 37 10 25 29 --- 14 | 137 132 133 145 --- 135 R23 | 1234 38 14 20 25 160 13 | 48 63 82 90 42 68 R24 | 2591 97 36 37 37 --- 30 | 176 284 289 243 --- 256 ------+------------------------------------+-------------------------------- RMS | 3058 34 15 23 25 169 |T 58 69 73 68 28 64 WRMS | 3058 24 13 20 25 169 |NE 58 69 73 68 28 64 MEDI | 1944 24 12 20 25 160 |MD 34 41 38 30 24 32