From IGS.ACC at noaa.gov Thu Dec 10 05:59:09 2009 From: IGS.ACC at noaa.gov (Jim Ray) Date: Thu, 10 Dec 2009 13:59:09 +0000 Subject: [IGSREPORT-18074] Wk 1559 IGLOS Final Orbits Message-ID: <4b20fead.CwcNCKlkjIKyU/sM%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 10 Dec 05:59:32 PST 2009 Message Number 18074 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 IGLOS Orbit Combination - Week 1559 (Nov 22, 2009 - Nov 28, 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 2.1559. 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: igl1559[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1559 in the SP3 format. igl15597.sum Combination Report for GPS Week 1559. 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 | 503.5 ns 1 | 502.4 ns 2 | 509.8 ns 3 | 520.1 ns 4 | 508.9 ns 5 | 511.2 ns 6 | 502.8 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 ----+--------+--------------- 4 | IAC | R23 5 | IAC | R23 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 1.1559, 1a.1559). 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 2.1559.0-6) 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 3.1559.0-6). 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 1559 summary. (Nov 22, 2009 - Nov 28, 2009) Table 1.1559.a GPS week : 1559 MJD: 55157.0-55163.0 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 110| 2 0 12 17 -25 -8 -.08 31 29 | 0 -355 3859 4467 | 0 2 6 40 31 122 .15 | 0 1047 cod 235| -2 0 -5 26 25 67 -.09 16 15 | --- --- --- --- | 1 2 1 26 29 34 .04 | --- --- esx 126| 0 0 -8 -32 -6 -71 .29 24 22 | 134448 -773 4637 9570 | 2 2 5 40 18 13 .14 | 7221 3435 iac n/a| 2 1 12 -41 -9 -47 -.12 30 30 | 508728 -735 4638 8818 | 1 2 8 30 25 78 .11 | 6013 1069 mcc n/a| -8 9 29 -58 -97 1048 .50 239 239 | --- --- --- --- | 20 13 22 105 213 760 .79 | --- --- Table 1.1559.b GPS week : 1559 MJD: 55157.0-55163.0 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 | 13 9 11 17 15 9 9 | R03 | 17 13 16 12 11 12 10 | R07 | 13 11 14 12 12 13 13 | R08 | 10 11 9 10 13 13 9 | R10 | 14 18 15 12 16 11 14 | R11 | 14 17 18 17 29 26 18 | R13 | 16 17 16 12 16 12 11 | R14 | 22 18 14 10 11 10 11 | R15 | 14 15 15 13 11 12 10 | R17 | 14 17 16 15 14 13 13 | R18 | 9 11 11 15 14 16 15 | R19 | 13 10 13 11 11 10 10 | R20 | 12 17 16 17 12 16 18 | R21 | 14 14 14 13 13 13 12 | R23 | 18 14 14 24 55 44 20 | Table 1.1559.c GPS week : 1559 MJD: 55157.0-55163.0 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 1559 0 | -25 80 106 -1312 -701 -16910 91.8 4205 4205 | 503458 0 brd 1559 1 | -206 -82 89 628 -2593 -17400 90.5 3910 3910 | 502395 0 brd 1559 2 | 111 -40 76 -2297 -719 -22000 93.3 2541 2541 | 509789 0 brd 1559 3 | 138 177 132 -2415 -3080 -20690 90.4 9648 9648 | 520119 0 brd 1559 4 | -98 -46 335 -814 1133 -11800 87.2 2563 2563 | 508926 0 brd 1559 5 | -201 -75 217 -2776 -634 -11940 86.9 2639 2639 | 511185 0 brd 1559 6 | 206 123 303 -1726 4644 -11190 87.0 2269 2269 | 502822 0 -------------+------------------------------------------------------------+---------------- brd 1559 mean| -10 19 180 -1530 -278 -15989 89.6 3967 3967 | 508384 0 brd 1559 sdev| 166 105 105 1167 2579 4435 2.6 2613 2613 | 6309 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 2.1559.0 GPS week: 1559 Day: 0 MJD: 55157 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 110| 2 2 9 9 -9 222 -.12 33 34 | 0 -531 3644 4047 cod 235| -1 0 -4 61 5 20 -.10 17 15 | --- --- --- --- esx 126| -2 -2 -13 -58 -9 -77 .24 23 22 | 132432 -2867 5554 11602 iac n/a| 2 1 21 -49 -10 -146 -.16 32 32 | 505919 -2034 5544 11651 mcc n/a| -46 -8 24 -91 -311 -80 1.07 457 457 | --- --- --- --- Table 2.1559.1 GPS week: 1559 Day: 1 MJD: 55158 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 110| 0 -2 13 -4 -41 -55 -.13 32 34 | 0 -1707 11196 14092 cod 235| -2 1 -7 28 54 88 -.06 18 15 | --- --- --- --- esx 126| 1 0 -1 18 -12 -82 .12 22 19 | 130713 -4477 5331 8328 iac n/a| 3 -1 8 -78 -45 51 .03 32 32 | 502282 -1192 5337 7672 mcc n/a| -7 0 40 -3 -258 738 -.05 119 119 | --- --- --- --- Table 2.1559.2 GPS week: 1559 Day: 2 MJD: 55159 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 110| 2 1 5 36 -44 -124 .00 30 29 | 0 302 2472 2742 cod 235| -3 1 -6 18 30 59 -.10 17 13 | --- --- --- --- esx 126| 3 0 -10 -10 -3 -88 .22 26 24 | 133622 -1765 4020 9614 iac n/a| 5 0 20 -45 -8 29 -.07 29 29 | 508990 -526 4014 8224 mcc n/a| 14 8 6 -40 161 989 -.23 146 146 | --- --- --- --- Table 2.1559.3 GPS week: 1559 Day: 3 MJD: 55160 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 110| 2 2 6 55 -58 3 -.04 28 24 | 0 -1310 2487 2674 cod 235| -3 -2 -6 30 49 61 -.05 18 16 | --- --- --- --- esx 126| -1 -3 -16 -80 0 -60 .22 28 24 | 148045 3145 4088 9043 iac n/a| 3 1 19 -19 -33 -7 -.06 26 26 | 520068 602 4079 7697 mcc n/a| -4 25 7 -229 62 428 -.17 162 162 | --- --- --- --- Table 2.1559.4 GPS week: 1559 Day: 4 MJD: 55161 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 110| 2 2 10 -45 -52 -66 .08 32 27 | 0 -676 2006 2104 cod 235| 0 -4 -4 53 57 97 -.15 15 13 | --- --- --- --- esx 126| 0 3 -5 -44 -21 -48 .36 26 24 | 139849 -2798 3789 9529 iac n/a| 0 5 6 -61 -13 -115 -.11 33 33 | 509561 -915 3803 9154 mcc n/a| 12 28 65 120 -17 1586 1.17 279 279 | --- --- --- --- Table 2.1559.5 GPS week: 1559 Day: 5 MJD: 55162 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 110| 2 -2 22 -2 5 -110 .04 34 30 | 0 1418 2639 2835 cod 235| -2 -2 -4 -14 0 114 -.06 16 16 | --- --- --- --- esx 126| 1 1 -5 16 -29 -77 .29 23 19 | 129477 -1511 4421 8308 iac n/a| 2 3 1 -46 14 -24 -.17 27 27 | 511209 -1773 4417 7292 mcc n/a| -13 0 47 -91 -377 2130 1.72 249 249 | --- --- --- --- Table 2.1559.6 GPS week: 1559 Day: 6 MJD: 55163 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 110| 1 0 21 75 23 74 -.37 31 27 | 0 18 2575 2781 cod 235| 0 0 -5 8 -16 33 -.12 13 13 | --- --- --- --- esx 126| -2 -2 -8 -70 29 -66 .56 22 20 | 127000 4859 5257 10569 iac n/a| 0 0 7 15 28 -117 -.32 31 31 | 503067 690 5273 10037 mcc n/a| -12 12 16 -76 57 1547 .01 260 260 | --- --- --- --- 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 3.1559.0 GPS week: 1559 Day: 0 MJD: 55157 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1927 33 16 17 28 --- 13 | 66 74 71 75 --- 70 R03 | 748 44 23 14 39 --- 17 | 47 72 76 71 --- 67 R07 | 2279 27 15 22 31 --- 13 | 26 26 31 49 --- 28 R08 |14954 24 12 10 24 770 10 | 78 77 81 85 680 78 R10E | 1139 29 15 22 31 --- 13 | 47 42 52 48 --- 43 R11E | 1391 19 15 24 38 150 14 | 88 99 120 113 101 103 R13E | 1938 41 13 26 38 --- 16 | 32 23 35 48 --- 23 R14E | 1649 52 23 37 48 --- 22 | 37 37 58 60 --- 37 R15E | 1727 31 13 14 38 104 13 | 33 24 34 33 65 26 R17 | 1566 36 12 23 28 --- 13 | 28 60 70 47 --- 52 R18 | 1390 24 11 14 17 --- 9 | 31 55 56 56 --- 49 R19 | 872 23 20 23 23 --- 12 | 46 62 79 70 --- 64 R20 | 2902 30 13 18 22 --- 11 | 52 54 70 69 --- 59 R21 | 1196 25 19 27 22 --- 13 | 63 82 95 81 --- 80 R23 | 2114 38 22 32 35 --- 17 | 170 164 141 141 --- 170 ------+------------------------------------+-------------------------------- RMS | 4205 33 17 23 32 456 |T 56 63 71 69 282 63 WRMS | 4205 34 15 22 32 456 |NE 60 72 77 74 680 71 MEDI | 1649 30 15 22 31 150 |MD 47 60 70 69 101 59 Table 3.1559.1 GPS week: 1559 Day: 1 MJD: 55158 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 2002 22 8 10 21 --- 8 | 111 96 95 87 --- 96 R03 | 996 27 14 15 35 --- 12 | 90 98 106 104 --- 98 R07 | 3034 23 12 18 23 --- 10 | 23 20 28 32 --- 22 R08 |12721 25 16 14 20 141 10 | 39 46 32 45 50 37 R10E | 1396 49 21 20 39 --- 18 | 33 46 52 64 --- 42 R11E | 1758 26 19 30 44 105 17 | 68 68 85 78 53 72 R13E | 3649 37 18 32 36 --- 17 | 43 43 51 60 --- 42 R14E | 1356 48 18 24 35 --- 17 | 27 60 62 63 --- 49 R15E | 1098 30 14 23 38 106 14 | 24 24 36 29 53 20 R17 | 2687 34 25 24 39 --- 17 | 17 45 27 29 --- 26 R18 | 1107 24 14 20 18 --- 10 | 24 38 40 35 --- 33 R19 | 659 28 9 12 20 --- 9 | 42 48 59 66 --- 52 R20 | 4270 40 19 19 44 --- 16 | 21 47 37 57 --- 39 R21 | 1154 19 24 28 23 --- 14 | 55 54 64 57 --- 55 R23 | 1848 24 22 24 27 --- 13 | 133 134 126 113 --- 134 ------+------------------------------------+-------------------------------- RMS | 3910 32 18 22 32 119 |T 50 57 60 61 52 54 WRMS | 3910 34 15 19 32 119 |NE 55 62 61 62 50 59 MEDI | 1758 27 18 20 35 106 |MD 39 47 52 60 53 42 Table 3.1559.2 GPS week: 1559 Day: 2 MJD: 55159 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1661 33 7 19 18 --- 11 | 59 75 81 82 --- 74 R03 | 1133 33 15 32 30 --- 15 | 43 64 88 62 --- 62 R07 | 4311 20 17 31 26 --- 13 | 24 20 43 32 --- 23 R08 | 5134 16 10 17 22 211 9 | 43 34 32 39 43 31 R10E | 1902 29 22 26 32 --- 15 | 29 45 54 46 --- 39 R11E | 2035 28 28 39 32 108 18 | 50 53 92 65 75 59 R13E | 2915 25 17 37 32 --- 16 | 41 36 67 56 --- 43 R14E | 1201 32 13 28 28 --- 14 | 23 45 63 48 --- 41 R15E | 1611 29 14 14 45 89 15 | 25 18 33 24 68 17 R17 | 3122 38 16 28 30 --- 15 | 65 64 53 50 --- 56 R18 | 1724 25 12 15 22 --- 10 | 56 41 48 48 --- 44 R19 | 1106 32 8 29 18 --- 12 | 55 60 77 54 --- 59 R20 | 843 36 21 21 33 --- 15 | 21 37 32 33 --- 29 R21 | 1830 37 20 20 17 --- 13 | 63 71 63 65 --- 63 R23 | 3089 31 16 24 31 --- 14 | 149 172 119 136 --- 169 ------+------------------------------------+-------------------------------- RMS | 2541 30 17 26 29 146 |T 49 55 63 56 62 53 WRMS | 2541 29 13 24 29 146 |NE 57 63 63 60 43 61 MEDI | 1830 31 16 26 30 108 |MD 43 45 63 50 68 44 Table 3.1559.3 GPS week: 1559 Day: 3 MJD: 55160 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1511 45 18 25 28 --- 17 | 144 161 164 160 --- 156 R03 | 1433 28 18 17 20 --- 12 | 64 93 88 88 --- 84 R07 | 5628 11 12 23 32 --- 12 | 23 18 37 35 --- 22 R08 | 3542 21 9 13 23 244 9 | 30 32 36 45 104 33 R10E | 3665 19 15 14 31 --- 12 | 42 45 47 55 --- 42 R11E | 2640 40 21 29 24 130 16 | 81 106 113 99 117 98 R13E | 2007 16 13 25 28 --- 12 | 20 23 43 34 --- 21 R14E | 1302 13 15 17 21 --- 10 | 42 50 50 46 --- 43 R15E | 2916 20 20 28 23 56 13 | 24 25 41 28 170 24 R17 | 2973 28 21 24 30 --- 15 | 42 68 75 31 --- 52 R18 | 1308 31 17 22 31 --- 14 | 43 42 55 62 --- 44 R19 | 808 16 13 25 19 --- 10 | 36 39 57 47 --- 40 R20 | 1098 36 19 35 31 --- 17 | 33 29 67 49 --- 37 R21 | 2803 32 15 31 9 --- 13 | 37 60 65 58 --- 53 R23 |35956 36 32 59 33 --- 23 | 152 147 189 150 --- 149 ------+------------------------------------+-------------------------------- RMS | 9648 28 18 28 26 162 |T 54 62 75 65 130 59 WRMS | 9648 24 16 24 26 162 |NE 60 68 83 72 104 67 MEDI | 2640 28 17 25 28 130 |MD 42 45 57 49 117 43 Table 3.1559.4 GPS week: 1559 Day: 4 MJD: 55161 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 730 36 20 21 30 --- 15 | 89 129 116 98 --- 112 R03 | 1533 19 14 19 24 --- 10 | 42 64 55 60 --- 54 R07 | 2471 18 15 17 33 --- 11 | 20 21 32 27 --- 22 R08 | 5884 31 9 23 29 116 13 | 29 23 42 30 97 25 R10E | 2764 35 13 26 38 --- 15 | 32 53 66 56 --- 49 R11E | 2050 80 22 55 44 396 28 | 57 93 125 78 103 86 R13E | 1365 31 23 29 31 --- 16 | 33 49 51 46 --- 39 R14E | 1913 18 14 20 24 --- 10 | 43 55 55 41 --- 47 R15E | 2499 22 11 25 17 251 10 | 25 22 33 31 105 23 R17 | 1618 28 13 23 39 --- 14 | 25 44 45 52 --- 38 R18 | 2310 16 12 23 47 --- 14 | 38 40 30 59 --- 36 R19 | 1102 7 12 26 29 --- 11 | 51 53 48 57 --- 49 R20 | 3168 14 12 24 32 --- 11 | 39 37 45 49 --- 37 R21 | 2350 27 10 16 36 --- 12 | 61 60 70 92 --- 65 XR23 | ---- 77 38 --- 251 --- 54 | 180 252 --- 146 --- 232 ------+------------------------------------+-------------------------------- RMS | 2563 32 15 26 33 279 |T 50 66 58 61 101 60 WRMS | 2563 27 13 24 33 279 |NE 57 72 53 67 97 67 MEDI | 2050 27 13 23 32 251 |MD 39 53 48 56 103 47 Table 3.1559.5 GPS week: 1559 Day: 5 MJD: 55162 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 672 19 10 13 20 --- 9 | 154 164 163 153 --- 160 R03 | 1010 28 14 20 21 --- 11 | 37 47 55 48 --- 45 R07 | 4529 28 13 12 37 --- 13 | 19 22 28 31 --- 21 R08 | 3781 30 17 18 27 137 13 | 18 31 36 39 66 28 R10E | 3588 25 11 13 25 --- 10 | 31 37 39 51 --- 35 R11E | 1389 77 18 48 38 --- 25 | 57 63 97 77 --- 71 R13E | 1044 34 16 17 22 --- 12 | 19 38 38 37 --- 31 R14E | 2815 20 14 17 17 --- 9 | 39 41 47 39 --- 38 R15E | 2892 28 14 25 20 325 12 | 30 27 37 23 94 26 R17 | 924 28 20 17 28 --- 13 | 20 37 35 35 --- 27 R18 | 3496 34 16 33 27 --- 15 | 17 44 73 53 --- 47 R19 | 1052 22 16 15 18 --- 10 | 50 64 55 64 --- 57 R20 | 3620 27 21 22 43 --- 16 | 30 30 41 56 --- 34 R21 | 1320 31 17 23 21 --- 13 | 54 69 80 84 --- 71 XR23 | 7618 69 26 --- 279 --- 43 | 141 143 --- 123 --- 139 ------+------------------------------------+-------------------------------- RMS | 2639 34 16 23 27 249 |T 47 57 58 60 80 55 WRMS | 2639 30 16 19 27 249 |NE 54 65 62 68 66 62 MEDI | 2815 28 16 17 25 137 |MD 31 41 41 51 66 38 Table 3.1559.6 GPS week: 1559 Day: 6 MJD: 55163 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 968 17 13 11 24 --- 9 | 112 133 130 122 --- 126 R03 | 912 17 13 19 22 --- 9 | 50 47 56 57 --- 50 R07 | 1720 34 13 17 29 --- 12 | 30 35 31 37 --- 30 R08 | 2846 15 7 15 25 116 8 | 27 25 33 46 69 29 R10E | 3953 44 9 23 26 --- 14 | 56 70 81 70 --- 69 R11E | 1154 57 10 25 37 --- 18 | 67 91 109 93 --- 90 R13E | 1298 33 9 15 24 --- 11 | 49 46 53 48 --- 46 R14E | 1967 31 11 17 20 --- 11 | 55 54 54 53 --- 52 R15E | 2321 19 13 15 22 349 9 | 43 48 39 35 101 40 R17 | 724 21 12 26 32 --- 12 | 39 55 66 48 --- 50 R18 | 3484 34 13 15 46 --- 15 | 50 53 62 84 --- 57 R19 | 1403 14 15 22 19 --- 10 | 88 81 93 91 --- 85 R20 | 2723 23 21 21 56 --- 17 | 35 48 70 79 --- 54 R21 | 1201 20 14 28 24 --- 12 | 76 89 102 91 --- 89 R23 | 3605 44 20 43 40 --- 20 | 138 165 177 184 --- 164 ------+------------------------------------+-------------------------------- RMS | 2269 31 13 22 31 260 |T 61 69 77 75 85 68 WRMS | 2269 27 13 20 31 260 |NE 64 73 82 83 69 73 MEDI | 1720 23 13 19 25 116 |MD 50 54 66 70 69 54