From IGS.ACC at noaa.gov Thu Jan 7 05:57:55 2010 From: IGS.ACC at noaa.gov (Jim Ray) Date: Thu, 07 Jan 2010 13:57:55 +0000 Subject: [IGSREPORT-18165] Wk 1563 IGLOS Final Orbits Message-ID: <4b45e863.nA9UKqE9+MbRn0Se%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 07 Jan 05:57:58 PST 2010 Message Number 18165 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 IGLOS Orbit Combination - Week 1563 (Dec 20, 2009 - Dec 26, 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 2.1563. 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: igl1563[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1563 in the SP3 format. igl15637.sum Combination Report for GPS Week 1563. 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 | 518.5 ns 1 | 430.9 ns 2 | 497.9 ns 3 | 500.3 ns 4 | 410.1 ns 5 | 426.0 ns 6 | 508.3 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 ----+--------+--------------- 3 | BKG | R11 3 | IAC | R11 4 | BKG | R11 4 | IAC | R11 5 | BKG | R11 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 1.1563, 1a.1563). 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 2.1563.0-6) 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 3.1563.0-6). 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 1563 summary. (Dec 20, 2009 - Dec 26, 2009) Table 1.1563.a GPS week : 1563 MJD: 55185.0-55191.0 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 126| 1 0 9 27 -19 1 -.17 84 31 | 0 -22 2562 2782 | 2 1 3 22 25 55 .06 | 0 1395 cod 239| -2 1 -4 38 14 50 -.14 20 16 | --- --- --- --- | 1 1 1 16 9 36 .02 | --- --- esx 126| -1 -2 2 -73 16 41 .33 32 25 | 98515 1310 4491 10151 | 1 2 5 29 37 91 .04 | 45603 2575 iac n/a| 3 0 -2 -25 -38 -115 -.09 68 68 | 470529 -484 4506 8827 | 1 2 7 32 23 75 .06 | 46004 1418 mcc n/a| 10 -4 21 -283 -31 3506 .70 245 245 | --- --- --- --- | 26 30 34 172 228 3625 .77 | --- --- Table 1.1563.b GPS week : 1563 MJD: 55185.0-55191.0 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 21 22 20 22 18 14 | R03 | 18 19 23 21 21 22 16 | R07 | 17 16 17 15 13 15 12 | R08 | 18 23 26 22 20 20 17 | R10 | 9 8 10 13 11 9 15 | R11 | 15 14 14 17 143 17 16 | R13 | 12 12 11 12 10 8 11 | R14 | 9 10 9 7 8 9 10 | R15 | 16 10 12 9 9 11 14 | R17 | 10 16 17 13 24 25 19 | R18 | 12 15 13 10 15 12 10 | R19 | 14 10 12 11 10 12 10 | R20 | 16 15 16 25 19 17 14 | R21 | 8 12 16 14 18 13 12 | R23 | 30 24 20 14 15 11 44 | Table 1.1563.c GPS week : 1563 MJD: 55185.0-55191.0 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 1563 0 | 83 70 204 -1391 -2420 -21450 86.6 2193 2193 | 518492 0 brd 1563 1 | 157 71 177 263 78 -17580 85.9 1975 1975 | 430866 0 brd 1563 2 | -4 16 62 -2013 278 -9565 90.1 2101 2101 | 497904 0 brd 1563 3 | 13 67 3 -1051 311 -4742 89.8 1894 1894 | 500261 0 brd 1563 4 | 71 -13 67 622 1535 -2375 88.7 2341 2341 | 410097 0 brd 1563 5 | 31 10 96 906 211 -4259 88.3 3685 3685 | 425986 0 brd 1563 6 | 105 67 119 -533 -2760 -5985 90.3 4774 4774 | 508291 0 -------------+------------------------------------------------------------+---------------- brd 1563 mean| 65 41 104 -456 -394 -9422 88.5 2709 2709 | 470271 0 brd 1563 sdev| 56 35 69 1095 1579 7317 1.7 1094 1094 | 45768 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 2.1563.0 GPS week: 1563 Day: 0 MJD: 55185 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 126| 2 -1 13 21 -42 75 -.27 31 32 | 0 159 1857 2051 cod 239| -4 0 -3 32 8 68 -.17 18 17 | --- --- --- --- esx 126| 0 -2 0 -40 28 -45 .36 24 23 | 141991 3151 4825 10183 iac n/a| 4 2 0 20 -43 -155 -.14 40 40 | 518334 415 4812 8916 mcc n/a| 4 21 35 -81 -128 289 .14 182 182 | --- --- --- --- Table 2.1563.1 GPS week: 1563 Day: 1 MJD: 55186 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 126| 0 0 14 38 -37 27 -.21 29 29 | 0 446 2258 2413 cod 239| -1 0 -5 48 18 20 -.13 17 14 | --- --- --- --- esx 126| -1 1 -5 -118 57 154 .32 28 27 | 43653 5073 4457 11132 iac n/a| 0 2 4 -13 -55 -243 -.03 40 40 | 430124 684 4426 10358 mcc n/a| -18 16 52 -141 215 416 .67 120 120 | --- --- --- --- Table 2.1563.2 GPS week: 1563 Day: 2 MJD: 55187 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 126| 0 -2 6 30 -55 -12 -.15 34 33 | 0 1484 3327 3733 cod 239| -1 1 -6 25 15 89 -.13 19 17 | --- --- --- --- esx 126| 0 0 3 -68 49 -20 .41 27 25 | 124323 2777 5081 10062 iac n/a| 1 -2 5 -5 -32 -24 -.12 36 36 | 498363 -1460 5087 9161 mcc n/a| -10 9 15 -288 102 870 .23 129 129 | --- --- --- --- Table 2.1563.3 GPS week: 1563 Day: 3 MJD: 55188 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 126| 2 0 8 -15 5 55 -.14 154 32 | 0 -1444 2441 2596 cod 239| -2 2 -3 58 11 -5 -.15 21 19 | --- --- --- --- esx 126| -1 -1 2 -56 1 52 .31 22 21 | 132736 1257 4191 11084 iac n/a| 2 -3 -1 -26 11 -50 -.15 77 77 | 501302 -2360 4224 9592 mcc n/a| 7 -20 -27 -357 -30 1110 .18 151 151 | --- --- --- --- Table 2.1563.4 GPS week: 1563 Day: 4 MJD: 55189 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 126| 3 0 9 22 13 -1 -.16 230 33 | 0 1774 3040 3319 cod 239| -2 3 -4 58 7 93 -.14 34 16 | --- --- --- --- esx 126| 0 -7 -1 -69 -35 -80 .33 52 25 | 47027 -2342 4439 9712 iac n/a| 5 0 0 -64 -44 -62 -.00 215 215 | 410738 -1622 4454 8138 mcc n/a| -2 -61 71 -496 -35 5950 2.33 376 376 | --- --- --- --- Table 2.1563.5 GPS week: 1563 Day: 5 MJD: 55190 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 126| 1 1 7 34 -16 -67 -.07 80 28 | 0 -689 2277 2412 cod 239| -2 1 -3 16 34 34 -.14 16 14 | --- --- --- --- esx 126| -4 -1 7 -47 -27 127 .28 29 27 | 60659 -1117 3650 9187 iac n/a| 5 -1 -8 -16 -54 -152 -.07 36 36 | 425802 1545 3666 7866 mcc n/a| 50 -17 -7 -128 -476 7340 .88 373 373 | --- --- --- --- Table 2.1563.6 GPS week: 1563 Day: 6 MJD: 55191 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 126| -3 -2 6 56 -6 -67 -.16 30 30 | 0 -1887 2734 2952 cod 239| -1 1 -3 29 5 52 -.09 18 14 | --- --- --- --- esx 126| 0 -3 8 -108 42 104 .31 41 25 | 139217 373 4794 9703 iac n/a| 2 0 -14 -70 -48 -116 -.08 33 33 | 509045 -592 4876 7760 mcc n/a| 43 21 10 -488 133 8566 .44 385 385 | --- --- --- --- 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 3.1563.0 GPS week: 1563 Day: 0 MJD: 55185 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02E | 2142 26 17 31 46 --- 16 | 29 31 51 53 --- 34 R03E | 2599 33 15 22 57 --- 17 | 28 35 35 53 --- 28 R07E | 4945 29 16 33 46 --- 17 | 18 19 33 42 --- 20 R08E | 1146 34 23 27 45 124 17 | 32 27 33 48 58 26 R10 | 1046 19 11 14 23 --- 9 | 19 22 27 30 --- 20 R11 | 1258 23 16 36 20 280 14 | 310 340 351 358 260 341 R13 | 3356 27 15 13 29 --- 11 | 27 31 32 19 --- 26 R14 | 1066 19 12 14 20 --- 9 | 28 30 38 23 --- 28 R15 | 1353 27 24 20 41 75 15 | 35 37 36 27 118 31 R17 | 1839 25 15 15 13 --- 10 | 48 74 78 64 --- 67 R18 | 1124 30 12 19 23 --- 11 | 52 73 83 74 --- 70 R19 | 1531 36 10 26 27 --- 14 | 38 64 81 75 --- 64 R20 | 2442 40 12 22 43 --- 16 | 24 38 56 63 --- 42 R21 | 1139 16 10 11 20 --- 8 | 50 67 62 62 --- 59 R23 | 1964 59 36 38 84 --- 29 | 36 29 49 69 --- 26 ------+------------------------------------+-------------------------------- RMS | 2193 31 18 24 40 182 |T 51 61 69 70 145 58 WRMS | 2193 32 17 23 40 182 |NE 60 73 81 78 189 70 MEDI | 1531 27 15 22 29 124 |MD 32 35 49 53 118 31 Table 3.1563.1 GPS week: 1563 Day: 1 MJD: 55186 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02E | 2470 48 21 24 52 --- 20 | 35 27 25 44 --- 18 R03E | 2134 41 10 31 55 --- 19 | 48 30 51 53 --- 33 R07E | 2108 22 17 24 48 --- 15 | 16 21 30 47 --- 18 R08E | 1029 32 28 36 65 144 22 | 29 37 43 60 39 32 R10 | 762 20 7 12 19 --- 8 | 16 25 32 25 --- 21 R11 | 1169 24 11 33 31 109 14 | 407 436 447 487 25 439 R13 | 2061 22 11 31 18 --- 12 | 17 21 52 21 --- 24 R14 | 1458 20 14 19 16 --- 9 | 26 30 38 18 --- 25 R15 | 2390 16 14 21 16 102 9 | 18 24 29 28 75 19 R17 | 1003 33 15 33 30 --- 15 | 34 54 79 38 --- 51 R18 | 1746 29 17 35 23 --- 15 | 37 59 83 44 --- 55 R19 | 1197 15 18 18 18 --- 10 | 39 58 43 44 --- 46 R20 | 3495 32 11 30 33 --- 14 | 18 29 55 40 --- 32 R21 | 1344 32 13 12 18 --- 11 | 20 49 50 42 --- 40 R23 | 2959 23 27 38 78 --- 24 | 12 36 60 42 --- 23 ------+------------------------------------+-------------------------------- RMS | 1974 29 17 28 40 120 |T 51 62 74 68 46 58 WRMS | 1974 29 14 27 40 120 |NE 58 74 88 75 50 70 MEDI | 1746 24 14 30 30 109 |MD 26 30 50 42 39 32 Table 3.1563.2 GPS week: 1563 Day: 2 MJD: 55187 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02E | 2001 48 17 41 44 --- 21 | 35 33 32 44 --- 25 R03E | 903 53 22 27 56 --- 22 | 47 28 30 57 --- 27 R07E | 1784 35 17 28 41 --- 17 | 27 24 38 47 --- 24 R08E | 933 58 31 38 59 140 26 | 32 30 47 51 56 26 R10 | 975 22 13 17 13 --- 9 | 16 29 40 24 --- 25 R11 | 1210 36 17 24 15 150 13 | 623 650 679 588 24 661 R13 | 1486 21 13 25 20 --- 11 | 22 22 44 32 --- 26 R14 | 2101 14 12 16 15 --- 8 | 26 24 30 23 --- 23 R15 | 3822 16 20 23 22 87 11 | 24 28 42 32 110 27 R17 | 963 43 26 22 18 --- 16 | 24 63 51 44 --- 46 R18 | 1700 16 14 30 27 --- 12 | 40 52 68 44 --- 50 R19 | 634 14 15 22 30 --- 12 | 42 59 64 34 --- 50 R20 | 4818 20 17 18 51 --- 16 | 25 30 22 40 --- 25 R21 | 521 35 11 37 21 --- 15 | 41 65 93 50 --- 63 R23 | 2443 24 31 27 53 --- 20 | 21 39 46 42 --- 32 ------+------------------------------------+-------------------------------- RMS | 2100 34 19 27 36 128 |T 69 78 88 76 63 75 WRMS | 2100 33 17 25 36 128 |NE 82 96 107 86 67 93 MEDI | 1486 24 17 25 27 140 |MD 27 30 44 44 56 27 Table 3.1563.3 GPS week: 1563 Day: 3 MJD: 55188 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02E | 1258 50 24 20 42 --- 19 | 33 29 29 46 --- 24 R03E | 1289 57 22 30 39 --- 21 | 46 25 39 41 --- 27 R07E | 1914 25 17 25 37 --- 15 | 21 20 33 45 --- 21 R08E | 569 59 24 26 46 176 22 | 48 36 44 58 143 37 R10 | 772 32 18 21 22 --- 13 | 27 28 34 25 --- 22 R11 | 2310 582 15 18 278 184 17 | 9999 829 824 9999 26 826 R13 | 1458 32 17 21 12 --- 12 | 23 28 34 21 --- 23 R14 | 1705 13 9 15 13 --- 7 | 24 27 38 24 --- 27 R15 | 3222 18 10 13 19 57 8 | 23 27 30 25 293 22 R17 | 750 33 18 21 19 --- 13 | 31 59 51 54 --- 48 R18 | 2964 13 18 16 19 --- 10 | 43 46 43 30 --- 38 R19 | 792 12 24 14 23 --- 11 | 39 57 40 41 --- 42 R20 | 2643 46 36 41 47 --- 24 | 28 40 85 54 --- 51 R21 | 763 42 15 19 23 --- 14 | 34 70 70 68 --- 61 R23 | 2772 17 28 13 32 --- 14 | 36 34 37 25 --- 30 ------+------------------------------------+-------------------------------- RMS | 1894 154 21 22 77 151 |T 32 90 95 39 154 86 WRMS | 1894 32 19 21 77 151 |NE 30 113 116 36 159 108 MEDI | 1458 32 18 20 23 176 |MD 31 34 39 41 143 30 Table 3.1563.4 GPS week: 1563 Day: 4 MJD: 55189 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02E | 1929 57 18 33 45 --- 22 | 38 33 38 51 --- 29 R03E | 972 40 26 34 50 --- 21 | 52 33 30 44 --- 24 R07E | 2850 19 13 19 37 --- 12 | 26 20 33 40 --- 18 R08E | 646 43 23 24 49 289 19 | 42 29 30 44 149 24 R10 | 1063 25 14 18 17 --- 10 | 25 21 32 23 --- 21 R11 | 6256 883 115 176 823 --- 142 | 9999 9999 9999 9999 --- 9999 R13 | 627 17 10 23 18 --- 10 | 22 26 35 17 --- 20 R14 | 1080 16 12 15 13 --- 8 | 21 21 27 19 --- 20 R15 | 1815 11 12 14 25 446 9 | 25 22 29 33 184 22 R17 | 849 36 21 37 71 --- 23 | 26 58 88 26 --- 48 R18 | 2812 19 25 28 29 --- 14 | 31 40 55 30 --- 34 R19 | 1187 22 11 13 23 --- 9 | 33 46 40 54 --- 40 R20 | 3183 39 19 29 46 --- 18 | 22 33 37 34 --- 24 R21 | 759 43 20 35 30 --- 18 | 31 62 82 39 --- 53 R23 | 1772 28 18 27 35 --- 15 | 21 29 61 26 --- 30 ------+------------------------------------+-------------------------------- RMS | 2341 230 34 52 215 376 |T 29 33 44 34 166 29 WRMS | 2341 33 16 25 215 376 |NE 25 35 48 30 184 31 MEDI | 1187 28 18 27 35 289 |MD 26 29 35 33 149 24 Table 3.1563.5 GPS week: 1563 Day: 5 MJD: 55190 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02E | 1420 44 18 29 35 --- 17 | 23 37 26 47 --- 25 R03E | 1182 37 27 35 55 --- 21 | 36 20 44 44 --- 20 R07E | 3362 16 14 30 46 --- 15 | 20 22 39 37 --- 20 R08E | 825 37 12 46 46 294 20 | 32 24 53 50 77 23 R10 | 1157 20 10 18 14 --- 9 | 21 27 30 19 --- 19 R11 |12645 295 19 29 28 --- 17 | 9999 9999 9999 9999 --- 9999 R13 | 1134 12 8 22 14 --- 8 | 16 20 36 23 --- 19 R14 | 847 12 7 20 23 --- 8 | 17 23 28 26 --- 19 R15 | 1820 15 14 18 31 438 11 | 19 21 19 28 89 17 R17 | 1068 46 27 34 68 --- 24 | 20 38 30 23 --- 22 R18 | 2232 19 16 22 31 --- 12 | 28 37 33 24 --- 27 R19 | 955 21 9 33 18 --- 12 | 14 24 44 21 --- 22 R20 | 2725 35 12 39 35 --- 17 | 22 37 26 37 --- 25 R21 | 1431 23 19 26 21 --- 12 | 29 47 42 44 --- 38 R23 | 2287 14 15 24 24 --- 11 | 28 20 63 30 --- 25 ------+------------------------------------+-------------------------------- RMS | 3685 80 16 29 36 373 |T 23 28 36 32 83 22 WRMS | 3685 28 14 27 36 373 |NE 21 29 35 27 89 23 MEDI | 1420 21 14 29 31 294 |MD 21 24 33 28 77 22 Table 3.1563.6 GPS week: 1563 Day: 6 MJD: 55191 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02E | 1062 31 16 20 33 --- 14 | 29 26 30 45 --- 23 R03E | 2253 29 17 29 41 --- 16 | 32 21 32 43 --- 23 R07E | 5962 15 10 25 31 --- 11 | 22 18 31 34 --- 19 R08E | 1565 31 17 25 46 364 16 | 34 29 44 59 74 31 R10 | 957 22 11 36 34 --- 14 | 23 31 40 23 --- 26 R11 |15264 37 13 34 31 --- 16 | 9999 9999 9999 9999 --- 9999 R13 | 1130 20 12 18 28 --- 11 | 25 24 36 27 --- 24 R14 | 1162 21 15 13 16 --- 9 | 25 30 29 24 --- 26 R15 | 766 11 14 23 44 405 14 | 18 24 21 22 54 18 R17 | 1595 49 19 26 42 --- 19 | 37 69 59 36 --- 51 R18 | 1010 17 13 11 28 --- 10 | 42 54 55 44 --- 47 R19 | 589 11 14 17 24 --- 9 | 44 58 59 54 --- 53 R20 | 2887 31 11 31 27 --- 14 | 25 35 42 60 --- 36 R21 | 1437 32 17 12 18 --- 12 | 39 70 60 64 --- 58 R23 | 6794 56 47 132 39 --- 43 | 37 30 144 38 --- 48 ------+------------------------------------+-------------------------------- RMS | 4773 30 18 41 33 385 |T 30 37 48 40 64 34 WRMS | 4773 30 14 25 33 385 |NE 31 42 54 39 54 38 MEDI | 1437 29 14 25 31 364 |MD 29 30 40 38 54 26