From IGS.ACC at noaa.gov Thu Mar 18 05:30:27 2010 From: IGS.ACC at noaa.gov (Jim Ray) Date: Thu, 18 Mar 2010 12:30:27 +0000 Subject: [IGSREPORT-18395] Wk 1573 IGLOS Final Orbits Message-ID: <4ba21ce3.WfaCU0pNLrFkTAu7%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 18 Mar 05:30:40 PDT 2010 Message Number 18395 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 IGLOS Orbit Combination - Week 1573 (Feb 28, 2010 - Mar 06, 2010) 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 2.1573. 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: igl1573[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1573 in the SP3 format. igl15737.sum Combination Report for GPS Week 1573. 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 | 478.1 ns 1 | 479.3 ns 2 | 434.6 ns 3 | 480.5 ns 4 | 481.4 ns 5 | 486.9 ns 6 | 485.0 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 1.1573, 1a.1573). 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 2.1573.0-6) 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 3.1573.0-6). 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 1573 summary. (Feb 28, 2010 - Mar 06, 2010) Table 1.1573.a GPS week : 1573 MJD: 55255.0-55261.0 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 130| 2 0 6 -8 -16 -85 -.22 31 29 | 0 -13 1609 1669 | 1 1 3 21 32 103 .06 | 0 60 cod 243| -1 0 -8 5 8 27 -.21 17 15 | --- --- --- --- | 1 1 1 11 15 46 .07 | --- --- esx 128| 0 0 -10 4 -14 12 .33 29 24 | 129999 -1928 3791 7957 | 2 1 4 38 15 57 .04 | 16421 2517 iac n/a| 2 1 27 -21 18 27 .05 35 35 | 475011 -136 3756 8322 | 1 0 4 32 23 168 .05 | 18515 1662 mcc n/a| 11 5 44 -106 75 -687 .08 142 142 | --- --- --- --- | 10 12 11 80 61 566 .23 | --- --- Table 1.1573.b GPS week : 1573 MJD: 55255.0-55261.0 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 | 11 14 10 11 10 15 10 | R02 | 15 12 10 11 10 9 11 | R03 | 17 16 15 10 10 10 8 | R04 | 14 18 15 12 13 12 9 | R05 | 12 13 13 16 13 12 12 | R07 | 11 10 9 14 15 17 12 | R08 | 13 12 8 10 8 11 14 | R10 | 8 12 10 12 13 12 13 | R11 | 13 12 13 14 14 13 36 | R13 | 12 11 14 11 8 9 10 | R14 | 12 45 --- --- --- --- 227 | R15 | 17 12 15 10 10 11 11 | R17 | 17 27 22 17 18 18 13 | R18 | 20 19 19 22 28 21 19 | R19 | 20 18 13 18 18 18 16 | R20 | 21 22 21 23 19 19 21 | R21 | 23 21 25 19 14 17 19 | R23 | 28 22 23 18 17 18 19 | Table 1.1573.c GPS week : 1573 MJD: 55255.0-55261.0 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 1573 0 | 80 63 190 -947 1403 -6635 86.3 2151 2151 | 478099 0 brd 1573 1 | 40 4 147 422 52 -7903 87.5 2358 2358 | 479322 0 brd 1573 2 | -77 -50 143 1744 -2610 -13030 89.9 1937 1937 | 434574 0 brd 1573 3 | -165 -17 134 -365 -345 -13480 88.1 2004 2004 | 480487 0 brd 1573 4 | -87 -86 156 -1336 -707 -14560 87.5 2061 2061 | 481414 0 brd 1573 5 | 48 -30 148 -2191 968 -19450 87.5 2306 2306 | 486913 0 brd 1573 6 | 6 -15 89 -483 756 -19820 87.1 2058 2058 | 484987 0 -------------+------------------------------------------------------------+---------------- brd 1573 mean| -21 -18 144 -450 -68 -13554 87.7 2125 2125 | 475113 0 brd 1573 sdev| 89 46 29 1267 1346 5084 1.1 156 156 | 18144 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 2.1573.0 GPS week: 1573 Day: 0 MJD: 55255 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 130| 3 1 7 -50 -11 -110 -.29 37 33 | 0 -112 1865 1935 cod 243| 0 2 -5 0 -12 80 -.24 17 15 | --- --- --- --- esx 128| 0 -4 -17 53 7 -42 .35 28 26 | 142707 -5178 4753 7912 iac n/a| 1 0 34 -43 27 19 .07 39 39 | 477588 -781 4832 8311 mcc n/a| 18 7 59 -27 164 -199 -.23 146 146 | --- --- --- --- Table 2.1573.1 GPS week: 1573 Day: 1 MJD: 55256 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 130| 4 1 13 3 -28 -101 -.27 39 38 | 0 51 1556 1598 cod 243| -2 0 -9 10 7 69 -.33 21 18 | --- --- --- --- esx 128| 1 0 -8 15 1 -29 .36 22 20 | 129900 -574 3564 8819 iac n/a| 2 0 23 -49 6 -5 .03 35 35 | 478246 2335 3647 9705 mcc n/a| 6 21 43 -159 -31 -49 .26 189 189 | --- --- --- --- Table 2.1573.2 GPS week: 1573 Day: 2 MJD: 55257 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 130| 2 0 6 -11 -35 -58 -.18 32 28 | 0 -40 1711 1755 cod 243| -2 -1 -9 9 25 16 -.19 19 15 | --- --- --- --- esx 128| 3 0 -4 -28 -22 116 .29 27 21 | 94015 -21 4256 8642 iac n/a| 2 2 23 3 19 -65 -.00 33 33 | 433762 806 4339 9236 mcc n/a| 6 -9 33 -136 91 -1591 -.14 168 168 | --- --- --- --- Table 2.1573.3 GPS week: 1573 Day: 3 MJD: 55258 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 130| 2 0 6 3 -7 -161 -.28 28 26 | 0 42 1544 1599 cod 243| 0 -1 -10 6 6 49 -.22 17 13 | --- --- --- --- esx 128| 2 0 -10 -5 -23 64 .41 28 23 | 139090 -4836 3612 8323 iac n/a| 2 0 32 -62 1 -12 .03 35 35 | 482413 -3079 3603 8340 mcc n/a| 29 -9 55 -139 75 -648 .41 141 141 | --- --- --- --- Table 2.1573.4 GPS week: 1573 Day: 4 MJD: 55259 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 130| 1 2 3 13 50 -241 -.17 28 26 | 0 43 1423 1498 cod 243| -1 0 -6 -6 -12 -41 -.17 17 14 | --- --- --- --- esx 128| -2 0 -10 -31 -32 11 .31 27 23 | 132941 -2148 3392 6517 iac n/a| 3 0 23 29 43 400 .10 34 34 | 481132 456 2927 6757 mcc n/a| 1 18 35 -22 62 -734 .20 118 118 | --- --- --- --- Table 2.1573.5 GPS week: 1573 Day: 5 MJD: 55260 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 130| 1 -2 4 4 -42 8 -.18 27 25 | 0 -34 1483 1551 cod 243| 0 0 -10 -5 26 44 -.17 16 14 | --- --- --- --- esx 128| -3 1 -6 57 -4 -22 .30 30 25 | 137411 -2450 3604 7707 iac n/a| 0 0 25 -7 -16 -59 .12 34 34 | 487681 -534 3572 8273 mcc n/a| 18 -2 32 -29 43 -1264 .09 125 125 | --- --- --- --- Table 2.1573.6 GPS week: 1573 Day: 6 MJD: 55261 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 130| 0 0 3 -19 -37 68 -.18 28 26 | 0 -45 1684 1749 cod 243| 0 0 -7 27 15 -26 -.13 16 15 | --- --- --- --- esx 128| 0 0 -13 -32 -28 -9 .32 42 28 | 133929 1706 3362 7784 iac n/a| 4 2 29 -24 50 -86 .02 32 32 | 484260 -155 3372 7635 mcc n/a| 0 11 52 -227 120 -327 -.01 106 106 | --- --- --- --- 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 3.1573.0 GPS week: 1573 Day: 0 MJD: 55255 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 1680 27 15 10 21 --- 10 | 31 56 59 43 --- 49 R02 | 723 40 12 12 42 --- 15 | 31 53 61 75 --- 52 R03 | 1152 40 19 31 31 --- 16 | 31 55 77 59 --- 54 XR04 | 2288 32 8 19 --- --- 13 | 28 54 56 --- --- 46 R05 | 795 24 17 16 29 --- 12 | 32 64 63 53 --- 54 R07 | 4071 17 12 28 19 --- 11 | 68 63 80 54 --- 64 R08 | 1807 33 14 23 27 199 13 | 34 55 59 34 58 45 R10 | 2439 19 10 13 17 --- 8 | 19 18 20 20 --- 15 R11 | 1186 24 15 25 28 135 12 | 37 35 37 34 87 32 R13 | 1744 22 14 29 18 --- 12 | 22 24 29 23 --- 20 R14 | 4291 32 13 22 16 --- 11 | 130 124 4 8 --- 121 R15 | 2303 42 18 39 18 80 17 | 35 34 39 26 36 26 R17E | 1593 31 17 28 49 --- 17 | 53 67 72 88 --- 68 R18E | 1751 52 22 21 46 --- 19 | 148 144 148 146 --- 145 R19E | 425 34 22 30 57 --- 20 | 30 37 32 53 --- 31 R20E | 2347 37 20 44 51 --- 21 | 62 56 94 81 --- 65 R21E | 1882 41 23 28 68 --- 22 | 111 110 107 134 --- 110 R23E | 2137 74 19 50 58 --- 28 | 46 45 51 73 --- 47 ------+------------------------------------+-------------------------------- RMS | 2151 37 17 28 39 146 |T 52 60 60 59 60 58 WRMS | 2151 33 15 26 39 146 |NE 41 52 48 39 60 48 MEDI | 1751 32 15 25 29 135 |MD 34 55 59 53 58 49 Table 3.1573.1 GPS week: 1573 Day: 1 MJD: 55256 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 946 31 13 25 26 --- 13 | 16 36 50 17 --- 30 R02 | 836 26 20 13 21 --- 11 | 43 39 35 44 --- 37 R03 | 1699 36 23 13 37 --- 15 | 13 31 35 47 --- 29 XR04 | 1959 45 13 20 --- --- 18 | 29 46 60 --- --- 44 R05 | 763 36 13 14 25 --- 12 | 18 30 21 35 --- 21 R07 | 4324 13 14 19 17 --- 9 | 35 40 18 35 --- 29 R08 | 2451 24 16 15 27 258 11 | 38 47 47 36 128 42 R10 | 1226 21 21 12 26 --- 11 | 19 31 24 10 --- 20 R11 | 824 25 15 20 27 177 12 | 23 31 27 28 160 20 R13 | 1432 20 19 20 14 --- 10 | 23 34 38 39 --- 30 XR14 |15617 95 50 --- 44 --- 44 | 154 156 --- 6 --- 156 R15 | 2831 37 17 9 23 94 12 | 33 37 42 30 82 33 R17E | 2077 80 24 28 58 --- 26 | 48 91 86 101 --- 83 R18E | 1127 47 20 30 34 --- 18 | 127 144 152 151 --- 143 R19E | 937 43 22 27 38 --- 18 | 27 29 26 35 --- 19 R20E | 1855 37 31 34 50 --- 21 | 52 73 62 75 --- 61 R21E | 1342 59 24 22 47 --- 21 | 87 109 103 118 --- 102 R23E | 5934 42 33 33 51 --- 22 | 38 45 47 50 --- 38 ------+------------------------------------+-------------------------------- RMS | 2357 39 21 22 35 189 |T 45 58 51 50 123 52 WRMS | 2357 38 18 20 35 189 |NE 37 46 36 29 123 40 MEDI | 1432 36 20 20 27 177 |MD 33 39 42 36 128 33 Table 3.1573.2 GPS week: 1573 Day: 2 MJD: 55257 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 807 13 16 21 16 --- 10 | 33 47 39 44 --- 39 R02 | 789 18 12 18 20 --- 9 | 29 33 48 30 --- 33 R03 | 1853 23 23 24 32 --- 14 | 34 53 56 47 --- 46 XR04 | 1828 28 19 15 --- --- 14 | 22 47 37 --- --- 35 R05 | 888 33 10 29 15 --- 13 | 32 42 65 51 --- 47 R07 | 3554 12 14 19 10 --- 8 | 37 47 41 35 --- 39 R08 | 2731 20 12 12 13 91 8 | 46 40 32 29 125 34 R10 | 1087 22 10 16 21 --- 10 | 36 24 38 22 --- 25 R11 | 1009 28 17 27 19 261 13 | 21 37 48 35 123 30 R13 | 1454 28 15 26 26 --- 13 | 24 26 30 26 --- 21 R15 | 2872 38 16 22 25 92 14 | 35 34 41 34 89 30 R17E | 1571 43 23 36 48 --- 21 | 41 44 58 63 --- 45 R18E | 1223 47 29 15 40 --- 19 | 117 123 115 133 --- 120 R19E | 1689 22 18 20 32 --- 13 | 22 30 32 35 --- 26 R20E | 1246 45 18 41 43 --- 21 | 54 51 71 67 --- 56 R21E | 815 50 26 48 51 --- 24 | 126 140 160 147 --- 139 R23E | 3577 33 29 28 64 --- 22 | 34 35 53 63 --- 38 ------+------------------------------------+-------------------------------- RMS | 1936 32 19 27 33 168 |T 43 50 56 53 112 47 WRMS | 1936 28 15 21 33 168 |NE 31 39 43 35 112 34 MEDI | 1454 28 17 22 25 92 |MD 34 42 48 35 123 38 Table 3.1573.3 GPS week: 1573 Day: 3 MJD: 55258 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 865 21 13 23 21 --- 11 | 31 53 65 36 --- 46 R02 | 1393 21 7 21 23 --- 10 | 50 41 40 50 --- 43 R03 | 2357 11 8 19 28 --- 9 | 40 41 62 40 --- 44 XR04 | 1962 16 13 23 --- --- 12 | 39 47 47 --- --- 41 R05 | 1716 44 18 15 30 --- 16 | 32 55 54 61 --- 47 R07 | 4535 23 18 26 30 --- 13 | 31 51 53 30 --- 39 R08 | 2036 12 17 16 22 55 9 | 31 51 47 32 64 40 R10 | 887 27 13 21 26 --- 12 | 46 36 43 25 --- 34 R11 | 1196 29 23 18 20 210 13 | 25 59 50 38 70 41 R13 | 1441 20 15 17 22 --- 10 | 30 33 38 36 --- 31 R15 | 1477 16 13 19 22 114 10 | 27 30 28 28 50 23 R17E | 2139 27 16 25 53 --- 17 | 50 61 69 88 --- 63 R18E | 1566 44 18 38 54 --- 21 | 177 183 205 210 --- 190 R19E | 1955 28 22 38 38 --- 17 | 29 30 45 31 --- 23 R20E | 1346 42 15 54 45 --- 22 | 67 68 97 77 --- 72 R21E | 838 28 22 35 50 --- 19 | 106 83 99 110 --- 94 R23E | 2909 34 22 32 43 --- 18 | 54 53 64 69 --- 54 ------+------------------------------------+-------------------------------- RMS | 2003 28 17 28 35 141 |T 50 57 65 60 61 54 WRMS | 2003 26 13 23 35 141 |NE 34 45 47 37 61 39 MEDI | 1566 27 16 23 28 114 |MD 39 51 53 38 64 43 Table 3.1573.4 GPS week: 1573 Day: 4 MJD: 55259 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 707 19 8 21 19 --- 9 | 40 49 56 48 --- 45 R02 | 1310 16 12 24 19 --- 10 | 43 26 39 39 --- 32 R03 | 1468 22 9 13 23 --- 9 | 39 36 40 41 --- 36 XR04 | 1420 24 14 14 --- --- 12 | 26 42 51 --- --- 37 R05 | 1175 34 19 11 23 --- 13 | 24 60 47 65 --- 47 R07 | 3025 30 17 32 27 --- 15 | 26 40 57 40 --- 38 R08 | 800 10 9 18 19 109 8 | 36 35 40 29 30 31 R10 | 697 26 22 23 21 --- 13 | 14 27 22 27 --- 14 R11 | 2001 34 12 22 31 146 14 | 42 41 55 35 54 37 R13 | 1150 15 12 15 16 --- 8 | 23 32 37 40 --- 27 R15 | 4952 20 11 20 21 90 10 | 28 19 33 16 26 19 R17E | 1780 29 19 32 50 --- 18 | 43 49 71 77 --- 53 R18E | 1086 58 28 52 62 --- 28 | 108 144 156 116 --- 129 R19E | 538 27 18 27 54 --- 18 | 35 21 35 46 --- 20 R20E | 3628 29 21 39 44 --- 18 | 78 76 74 82 --- 72 R21E | 1290 17 15 28 34 --- 13 | 96 97 96 88 --- 93 R23E | 1612 27 23 25 41 --- 16 | 54 44 53 61 --- 48 ------+------------------------------------+-------------------------------- RMS | 2061 28 17 27 34 118 |T 44 49 56 53 36 45 WRMS | 2061 26 14 23 34 118 |NE 31 37 43 38 36 33 MEDI | 1310 26 15 23 23 109 |MD 39 41 51 41 30 37 Table 3.1573.5 GPS week: 1573 Day: 5 MJD: 55260 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 1410 31 15 33 28 --- 15 | 29 44 72 52 --- 46 R02 | 1361 16 14 14 18 --- 9 | 29 38 22 26 --- 28 R03 | 1748 14 11 27 13 --- 9 | 41 36 24 28 --- 30 XR04 | 1035 17 12 21 --- --- 11 | 37 40 54 --- --- 41 R05 | 745 27 18 18 17 --- 11 | 35 58 38 60 --- 47 R07 | 2058 41 10 35 32 --- 17 | 12 34 61 57 --- 36 R08 | 581 24 10 14 26 175 10 | 29 41 45 50 30 39 R10 | 1442 28 13 22 25 --- 12 | 24 29 31 19 --- 19 R11 | 2568 19 15 34 21 105 13 | 23 35 53 21 64 26 R13 | 3002 13 10 24 16 --- 9 | 19 28 32 17 --- 20 R15 | 3991 24 17 12 24 72 11 | 13 30 28 33 32 23 R17E | 895 24 20 48 36 --- 18 | 34 50 59 67 --- 46 R18E | 1466 51 14 23 55 --- 21 | 195 220 230 256 --- 223 R19E | 1449 22 18 27 54 --- 17 | 22 19 22 53 --- 17 R20E | 4876 21 19 37 56 --- 19 | 92 90 104 121 --- 97 R21E | 2900 23 17 43 34 --- 16 | 71 69 76 72 --- 68 R23E | 1466 26 21 34 43 --- 17 | 47 52 66 80 --- 55 ------+------------------------------------+-------------------------------- RMS | 2305 27 16 30 34 125 |T 44 53 59 63 42 50 WRMS | 2305 25 14 25 34 125 |NE 26 37 41 36 42 32 MEDI | 1466 24 15 27 26 105 |MD 29 40 53 52 32 39 Table 3.1573.6 GPS week: 1573 Day: 6 MJD: 55261 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R01 | 2101 21 5 20 26 --- 10 | 38 58 66 63 --- 54 R02 | 2500 24 11 23 22 --- 11 | 26 47 59 45 --- 42 R03 | 1149 17 6 17 14 --- 7 | 42 54 62 50 --- 51 XR04 | 792 11 9 19 --- --- 9 | 33 42 51 --- --- 39 R05 | 486 22 10 33 18 --- 11 | 49 69 80 70 --- 65 R07 | 2496 20 16 29 17 --- 11 | 35 49 62 46 --- 45 R08 | 861 38 8 11 31 121 13 | 24 46 43 56 68 39 R10 | 1529 18 19 31 22 --- 12 | 17 32 24 23 --- 20 R11 | 2064 44 32 125 26 69 35 | 41 38 87 33 104 36 R13 | 1987 17 9 20 25 --- 9 | 27 24 34 16 --- 23 XR14 |17862 322 159 --- --- --- 227 | 159 82 --- --- --- 89 R15 | 1706 24 12 19 21 121 10 | 25 22 27 29 48 21 R17E | 1438 14 14 13 44 --- 13 | 44 47 57 84 --- 52 R18E | 3023 35 16 44 40 --- 18 | 185 198 221 230 --- 204 R19E | 626 30 11 26 43 --- 15 | 29 17 29 46 --- 17 R20E | 2604 32 18 53 49 --- 21 | 123 128 127 153 --- 129 R21E | 3404 39 18 37 44 --- 19 | 98 91 105 101 --- 93 R23E | 2266 29 27 32 44 --- 18 | 68 67 78 80 --- 69 ------+------------------------------------+-------------------------------- RMS | 2058 28 16 42 32 106 |T 59 61 71 70 73 60 WRMS | 2058 26 15 28 32 106 |NE 43 46 54 43 73 43 MEDI | 1987 24 12 26 26 121 |MD 38 47 62 50 68 45