From igs.acc at noaa.gov Thu May 20 05:49:13 2010 From: igs.acc at noaa.gov (Jim Ray) Date: Thu, 20 May 2010 12:49:13 +0000 Subject: [IGSREPORT-18601] Wk 1582 IGLOS Final Orbits Message-ID: <4bf52fc9.qATHOmEaewJb8F6H%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 20 May 05:49:25 PDT 2010 Message Number 18601 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 IGLOS Orbit Combination - Week 1582 (May 02, 2010 - May 08, 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 2.1582. 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: igl1582[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1582 in the SP3 format. igl15827.sum Combination Report for GPS Week 1582. 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 | 373.7 ns 1 | 398.1 ns 2 | 469.1 ns 3 | 459.6 ns 4 | 466.0 ns 5 | 462.6 ns 6 | 464.1 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 ----+--------+--------------- 6 | BKG | R06 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 1.1582, 1a.1582). 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 2.1582.0-6) 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 3.1582.0-6). 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 1582 summary. (May 02, 2010 - May 08, 2010) Table 1.1582.a GPS week : 1582 MJD: 55318.0-55324.0 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 124| 0 0 -5 7 0 5 -.14 32 32 | 0 4 1742 1814 | 1 1 3 21 38 137 .04 | 0 125 cod 247| -1 0 8 49 -27 0 -.15 18 16 | --- --- --- --- | 1 1 3 18 25 35 .03 | --- --- esx 145| 0 0 7 -54 77 45 .43 28 26 | 101468 1826 3972 8230 | 1 1 7 27 23 72 .03 | 46780 5447 gfz 198| 0 -1 14 -55 -40 89 -.14 31 31 | 275745 -30 3969 8255 | 1 2 3 40 83 63 .07 | 39001 5363 iac n/a| 1 0 -18 -38 -18 -68 -.08 35 35 | 442130 -254 3989 8767 | 1 0 7 28 20 74 .04 | 39340 2281 mcc n/a| 7 0 23 -102 -68 70 .70 196 196 | --- --- --- --- | 10 13 36 203 106 472 .63 | --- --- Table 1.1582.b GPS week : 1582 MJD: 55318.0-55324.0 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 | 10 15 13 16 11 11 13 | R02 | 9 14 13 11 12 9 14 | R03 | 18 19 12 8 9 11 9 | R04 | 13 11 13 9 11 8 11 | R05 | 13 15 12 9 12 11 12 | R06 | 78 36 42 33 33 60 95 | R07 | 9 12 11 12 12 16 9 | R08 | 11 10 12 11 8 12 12 | R10 | 36 29 20 22 17 18 19 | R11 | 30 29 28 21 24 29 33 | R13 | 28 28 22 14 14 15 19 | R14 | 25 20 17 20 17 20 13 | R15 | 23 20 16 18 23 18 19 | R17 | 17 18 12 18 16 17 18 | R18 | 14 14 12 14 13 15 11 | R19 | 18 16 11 11 13 15 10 | R20 | 12 14 15 15 14 15 17 | R21 | 20 17 12 15 13 10 16 | R22 | 12 20 19 15 14 14 14 | R23 | 18 13 11 11 13 14 14 | R24 | 13 19 10 10 15 10 14 | Table 1.1582.c GPS week : 1582 MJD: 55318.0-55324.0 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 1582 0 | 147 105 72 -477 61 -7708 85.5 1997 1997 | 373735 0 brd 1582 1 | -135 -44 115 -785 -1621 -11780 84.9 2100 2100 | 398071 0 brd 1582 2 | -109 72 158 -1931 -2971 -10470 84.1 2107 2107 | 469102 0 brd 1582 3 | -34 -27 264 -587 -4729 -6464 88.9 2170 2170 | 459637 0 brd 1582 4 | -66 -24 244 -2096 -5018 -3460 87.2 1825 1825 | 465997 0 brd 1582 5 | -69 93 274 -2918 -2352 -5653 88.2 1958 1958 | 462645 0 brd 1582 6 | -105 -74 206 -2571 -4481 -9376 90.0 2148 2148 | 464095 0 -------------+------------------------------------------------------------+---------------- brd 1582 mean| -53 14 190 -1623 -3015 -7844 87.0 2043 2043 | 441897 0 brd 1582 sdev| 94 73 77 998 1868 2906 2.2 123 123 | 38999 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 2.1582.0 GPS week: 1582 Day: 0 MJD: 55318 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 124| -1 -1 -1 -12 -11 -64 -.16 40 36 | 0 -7 1741 1795 cod 247| -1 0 15 66 -29 6 -.13 20 17 | --- --- --- --- esx 145| 1 1 -2 -58 105 111 .44 32 30 | 21855 -612 3903 8272 gfz 198| -1 2 12 -75 -39 160 -.16 32 32 | 210716 -2091 3887 8369 iac n/a| 0 0 -24 -65 -14 -106 -.14 43 43 | 372853 233 3950 8810 mcc n/a| 6 -15 48 -180 -85 -137 1.55 78 78 | --- --- --- --- Table 2.1582.1 GPS week: 1582 Day: 1 MJD: 55319 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 124| -1 1 -4 14 10 -21 -.13 36 37 | 0 165 1690 1764 cod 247| -2 0 12 25 -43 31 -.11 21 17 | --- --- --- --- esx 145| 0 0 1 -55 103 90 .41 32 30 | 48038 6877 3715 8021 gfz 198| -1 -2 18 -98 42 178 -.06 35 35 | 228467 5666 3712 7595 iac n/a| 2 0 -15 -2 -51 -177 -.10 41 41 | 398580 518 3728 8252 mcc n/a| 25 3 50 -429 33 106 1.01 74 74 | --- --- --- --- Table 2.1582.2 GPS week: 1582 Day: 2 MJD: 55320 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 124| 0 3 -5 -8 -6 116 -.16 33 33 | 0 -9 1871 1947 cod 247| 0 0 5 61 -14 -44 -.09 16 13 | --- --- --- --- esx 145| -1 -2 11 -98 81 -37 .42 27 25 | 129067 6720 4355 6360 gfz 198| 1 -3 19 -37 -15 27 -.18 28 28 | 304873 77 4335 6623 iac n/a| 1 1 -20 6 -10 -10 -.06 33 33 | 469760 -3320 4374 7086 mcc n/a| 8 27 74 -280 -179 324 1.47 58 58 | --- --- --- --- Table 2.1582.3 GPS week: 1582 Day: 3 MJD: 55321 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 124| 1 0 -5 4 26 -216 -.18 31 29 | 0 156 2019 2086 cod 247| 0 0 7 65 -47 23 -.16 15 13 | --- --- --- --- esx 145| 0 0 15 -74 49 148 .47 26 24 | 127692 1451 3827 7041 gfz 198| 1 -1 18 -11 -51 83 -.17 30 30 | 293213 -684 3841 7346 iac n/a| 2 0 -25 -41 -22 -21 -.08 31 31 | 460644 1441 3840 7679 mcc n/a| -11 -5 -33 -50 79 -836 .28 650 650 | --- --- --- --- Table 2.1582.4 GPS week: 1582 Day: 4 MJD: 55322 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 124| -2 0 -3 40 48 127 -.19 26 26 | 0 -176 1550 1652 cod 247| -2 -1 9 29 -45 -36 -.19 20 16 | --- --- --- --- esx 145| 0 0 3 -19 49 35 .46 24 22 | 139428 -7829 3842 9421 gfz 198| 2 1 12 3 59 111 -.09 29 29 | 303260 -8647 3843 9642 iac n/a| 2 1 -15 -64 14 -87 -.04 29 29 | 464878 -2181 3847 9985 mcc n/a| 8 -5 7 115 -85 45 .26 215 215 | --- --- --- --- Table 2.1582.5 GPS week: 1582 Day: 5 MJD: 55323 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 124| -1 0 -10 28 0 166 -.13 32 32 | 0 10 1513 1583 cod 247| 0 0 4 31 -40 -28 -.16 17 18 | --- --- --- --- esx 145| 1 1 9 -51 87 -1 .45 27 25 | 112199 6702 4372 9284 gfz 198| -2 -4 10 -91 -92 13 -.08 31 31 | 291492 7525 4375 8516 iac n/a| 0 2 -5 -45 -14 -117 -.09 31 31 | 463276 3249 4343 9509 mcc n/a| 11 -2 8 110 -29 352 .21 162 162 | --- --- --- --- Table 2.1582.6 GPS week: 1582 Day: 6 MJD: 55324 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 124| 1 -1 -8 -14 -73 -69 -.06 29 30 | 0 -106 1816 1877 cod 247| -3 2 7 62 24 42 -.17 18 18 | --- --- --- --- esx 145| 1 0 17 -20 68 -25 .38 26 23 | 131999 -525 3794 9211 gfz 198| -2 -1 10 -78 -185 53 -.24 28 28 | 298196 -2058 3793 9696 iac n/a| 3 0 -25 -54 -33 40 -.02 36 36 | 464920 -1719 3845 10053 mcc n/a| 7 -9 11 -5 -215 640 .12 137 137 | --- --- --- --- 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 3.1582.0 GPS week: 1582 Day: 0 MJD: 55318 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL ------+-----------------------------------------+------------------------------------- R01 | 2663 23 15 14 13 15 --- 9 | 47 55 47 55 46 --- 47 R02 | 1244 16 11 19 17 20 --- 9 | 21 23 30 25 31 --- 21 R03 | 890 39 30 13 25 36 --- 17 | 32 26 25 35 36 --- 21 R04 | 954 30 17 19 15 23 --- 12 | 23 26 23 26 32 --- 21 R05 | 1046 29 13 29 20 18 --- 13 | 29 34 32 30 33 --- 29 XR06 | ---- 113 53 --- --- --- --- 78 | 66 67 --- --- --- --- 65 R07 | 2297 11 11 15 28 21 --- 8 | 24 19 26 35 33 --- 20 R08 | 1732 10 17 21 15 25 --- 11 | 25 19 34 19 33 --- 22 R10E | 2187 81 37 53 50 85 --- 35 | 58 17 34 25 48 --- 21 R11E | 1262 67 36 32 41 75 --- 29 | 27 35 40 36 67 --- 31 R13E | 4320 57 18 46 69 77 --- 27 | 45 45 37 54 74 --- 40 R14E | 1669 44 19 41 39 72 --- 25 | 33 26 41 35 53 --- 25 R15E | 1718 51 29 37 40 52 78 23 | 33 36 47 38 43 28 30 R17 | 3022 43 8 20 43 47 --- 17 | 95 70 74 58 38 --- 67 R18 | 1843 33 11 18 19 35 --- 13 | 51 41 50 41 52 --- 41 R19 | 1267 25 18 47 17 30 --- 17 | 35 45 65 56 40 --- 38 R20 | 2060 29 14 10 31 25 --- 11 | 35 39 38 51 49 --- 34 R21 | 910 40 16 56 31 19 --- 20 | 65 58 63 51 38 --- 46 R22 | 1981 29 9 24 34 18 --- 11 | 48 59 61 74 41 --- 52 R23 | 1891 33 23 38 23 35 --- 18 | 34 41 39 46 38 --- 33 R24 | 1593 35 12 27 21 18 --- 13 | 35 44 48 52 39 --- 38 ------+-----------------------------------------+------------------------------------- RMS | 1997 40 20 32 32 43 78 |T 41 39 42 42 43 28 35 WRMS | 1997 36 17 30 32 43 78 |NE 41 41 43 43 38 --- 37 MEDI | 1718 33 17 24 25 25 78 |MD 35 39 39 38 39 28 33 Table 3.1582.1 GPS week: 1582 Day: 1 MJD: 55319 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL ------+-----------------------------------------+------------------------------------- R01 | 1486 20 12 30 27 41 --- 15 | 52 57 57 50 67 --- 54 R02 | 1636 26 17 29 36 23 --- 13 | 15 28 45 38 32 --- 21 R03 | 1154 26 25 47 27 34 --- 19 | 22 26 47 36 38 --- 23 R04 | 1731 24 11 20 31 17 --- 10 | 22 14 33 30 23 --- 15 R05 | 1104 15 19 41 28 19 --- 14 | 29 29 43 26 35 --- 23 XR06 | ---- 45 29 --- --- --- --- 36 | 72 73 --- --- --- --- 73 R07 | 2711 21 11 26 32 22 --- 11 | 21 18 31 28 29 --- 15 R08 | 1077 13 11 23 17 20 --- 9 | 17 15 31 22 27 --- 14 R10E | 1473 48 39 45 44 74 --- 29 | 55 22 37 30 38 --- 25 R11E | 1175 65 43 25 59 66 --- 29 | 32 31 46 47 59 --- 32 R13E | 5071 71 24 32 31 67 --- 28 | 41 49 60 52 80 --- 46 R14E | 2687 40 21 23 32 56 --- 20 | 23 36 39 41 54 --- 28 R15E | 2124 25 19 38 42 53 74 19 | 32 34 60 52 43 30 34 R17 | 2052 28 18 34 28 47 --- 18 | 54 43 57 52 26 --- 37 R18 | 2629 29 21 24 39 20 --- 13 | 70 36 62 38 42 --- 48 R19 | 1992 36 11 33 50 32 --- 16 | 32 43 65 67 37 --- 39 R20 | 2467 27 17 32 36 20 --- 14 | 32 34 38 50 24 --- 23 R21 | 1012 39 17 21 33 42 --- 17 | 43 38 48 58 26 --- 32 R22 | 1234 39 24 38 32 35 --- 19 | 38 40 40 48 34 --- 28 R23 | 1877 27 10 15 27 38 --- 13 | 29 36 27 41 56 --- 30 R24 | 969 46 21 38 24 20 --- 18 | 27 37 35 36 25 --- 19 ------+-----------------------------------------+------------------------------------- RMS | 2099 36 21 32 35 41 74 |T 36 35 45 42 39 30 31 WRMS | 2099 37 17 30 35 41 74 |NE 35 35 43 41 34 --- 30 MEDI | 1636 28 19 30 32 34 74 |MD 32 36 43 41 35 30 28 Table 3.1582.2 GPS week: 1582 Day: 2 MJD: 55320 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL ------+-----------------------------------------+------------------------------------- R01 | 1029 17 20 15 19 37 --- 13 | 40 51 65 62 53 --- 48 R02 | 1195 22 17 34 33 17 --- 13 | 16 22 30 27 29 --- 18 R03 | 1385 27 10 29 28 13 --- 11 | 26 34 32 29 42 --- 26 R04 | 2676 19 17 25 20 28 --- 12 | 19 19 36 31 27 --- 17 R05 | 1252 19 12 32 15 17 --- 11 | 30 20 47 21 22 --- 20 XR06 | 4415 59 29 --- --- --- --- 41 | 70 80 --- --- --- --- 63 R07 | 2490 18 10 27 36 18 --- 10 | 27 21 42 35 29 --- 19 R08 | 1753 22 11 25 24 25 --- 11 | 20 20 31 30 27 --- 15 R10E | 1548 59 20 23 21 37 --- 20 | 35 20 30 16 51 --- 17 R11E | 1589 76 29 44 25 47 --- 27 | 26 31 54 44 46 --- 30 R13E | 2414 40 26 23 32 64 --- 22 | 39 60 65 64 70 --- 50 R14E | 3546 41 14 18 40 48 --- 17 | 21 21 24 35 55 --- 17 R15E | 2009 31 14 26 29 44 58 16 | 20 40 33 32 56 41 28 R17 | 1392 21 18 22 26 21 --- 11 | 35 51 40 35 46 --- 41 R18 | 2398 35 10 18 39 16 --- 11 | 54 38 50 35 46 --- 44 R19 | 2540 15 11 21 29 30 --- 11 | 43 33 50 57 42 --- 38 R20 | 4294 32 12 43 35 15 --- 15 | 27 41 76 73 35 --- 41 R21 | 1305 22 16 20 38 29 --- 12 | 50 52 43 53 35 --- 45 R22 | 740 34 20 24 17 51 --- 18 | 35 56 65 48 27 --- 44 R23 | 1164 10 8 29 22 26 --- 11 | 21 23 32 42 35 --- 20 R24 | 1677 16 8 15 18 30 --- 10 | 31 30 29 27 41 --- 29 ------+-----------------------------------------+------------------------------------- RMS | 2107 33 16 27 28 33 58 |T 32 36 43 39 40 41 31 WRMS | 2107 33 13 25 28 33 58 |NE 34 36 44 40 35 --- 33 MEDI | 1677 22 14 24 26 28 58 |MD 30 33 40 35 41 41 29 Table 3.1582.3 GPS week: 1582 Day: 3 MJD: 55321 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL ------+-----------------------------------------+------------------------------------- R01 | 1107 39 15 29 32 30 --- 16 | 60 88 106 101 94 --- 85 R02 | 1157 17 16 20 22 22 --- 10 | 20 30 27 24 26 --- 18 R03 | 1321 13 9 17 23 19 --- 8 | 19 21 24 17 26 --- 18 R04 | 3267 11 6 20 18 24 --- 9 | 22 21 30 21 28 --- 18 R05 | 3080 15 12 15 14 22 --- 9 | 23 24 34 29 26 --- 17 XR06 | 2551 61 43 --- --- 34 --- 33 | 81 145 --- --- 50 --- 114 R07 | 1201 18 11 27 19 28 --- 11 | 31 30 44 28 30 --- 26 R08 | 2253 20 14 20 22 24 192 11 | 28 26 28 21 25 171 20 R10E | 876 48 28 34 20 44 --- 21 | 37 19 34 33 40 --- 20 R11E | 2511 57 17 32 46 41 --- 21 | 39 28 39 53 48 --- 29 R13E | 1975 22 15 17 46 39 --- 13 | 45 43 43 43 42 --- 38 R14E | 3156 40 18 33 29 49 --- 19 | 29 38 56 32 58 --- 35 R15E | 2111 29 17 28 43 49 98 17 | 22 35 38 30 54 38 27 R17 | 1729 44 22 33 44 28 --- 18 | 46 55 81 81 51 --- 51 R18 | 1293 41 16 21 29 17 --- 14 | 31 46 41 35 34 --- 36 R19 | 2402 16 11 22 21 27 --- 10 | 36 60 68 65 43 --- 51 R20 | 3796 36 10 22 26 36 --- 15 | 33 30 46 39 44 --- 31 R21 | 1782 35 13 35 24 19 --- 14 | 49 52 69 56 46 --- 50 R22 | 1933 25 17 38 26 27 --- 15 | 63 68 63 63 65 --- 62 R23 | 842 14 10 27 43 24 1106 11 | 28 26 32 40 26 994 20 R24 | 2305 11 17 18 23 22 --- 10 | 40 38 38 52 20 --- 29 ------+-----------------------------------------+------------------------------------- RMS | 2170 31 15 26 30 31 650 |T 37 43 47 43 41 401 37 WRMS | 2170 29 13 24 30 31 650 |NE 38 47 48 44 39 582 40 MEDI | 1975 25 15 22 24 27 192 |MD 33 35 39 35 42 171 29 Table 3.1582.4 GPS week: 1582 Day: 4 MJD: 55322 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL ------+-----------------------------------------+------------------------------------- R01 | 1946 20 20 19 22 17 --- 11 | 43 55 36 42 52 --- 43 R02 | 1335 17 20 17 24 25 --- 11 | 31 33 32 26 31 --- 25 R03 | 1150 15 7 22 19 15 --- 9 | 20 18 30 29 21 --- 18 R04 | 1477 16 16 24 17 17 --- 10 | 23 21 37 21 24 --- 21 R05 | 2840 18 17 27 40 18 --- 11 | 19 27 26 35 20 --- 17 XR06 | 2202 39 42 --- --- 58 --- 33 | 72 125 --- --- 58 --- 97 R07 | 2020 20 15 25 21 18 --- 11 | 28 30 35 29 32 --- 25 R08 | 920 18 13 10 24 15 80 8 | 19 22 29 30 24 15 19 R10E | 2212 33 24 21 30 37 --- 16 | 27 27 22 27 42 --- 22 R11E | 2204 46 28 37 45 53 --- 23 | 42 34 43 46 53 --- 30 R13E | 1771 22 23 21 38 30 --- 14 | 42 30 35 32 35 --- 27 R14E | 1810 30 18 27 35 41 --- 17 | 22 33 45 38 47 --- 27 R15E | 1288 42 30 23 44 57 125 22 | 25 44 36 24 61 25 26 R17 | 2224 21 26 32 22 25 --- 15 | 35 48 44 47 34 --- 35 R18 | 741 15 14 26 34 28 --- 12 | 34 32 31 29 50 --- 29 R19 | 1467 31 14 12 18 26 --- 12 | 22 43 36 45 39 --- 30 R20 | 1837 26 13 25 34 29 --- 13 | 33 32 42 60 38 --- 33 R21 | 1482 28 22 21 16 17 --- 13 | 44 55 47 49 55 --- 47 R22 | 3064 20 14 37 18 19 --- 13 | 56 52 87 70 50 --- 58 R23 | 1356 20 18 12 15 33 341 12 | 35 30 26 33 45 103 29 R24 | 1504 29 29 26 28 19 --- 15 | 62 53 75 64 52 --- 56 ------+-----------------------------------------+------------------------------------- RMS | 1825 26 20 24 29 29 215 |T 34 40 39 38 41 47 34 WRMS | 1825 26 16 22 29 29 215 |NE 36 42 40 40 39 59 36 MEDI | 1771 21 18 23 24 25 125 |MD 33 33 36 33 42 25 29 Table 3.1582.5 GPS week: 1582 Day: 5 MJD: 55323 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL ------+-----------------------------------------+------------------------------------- R01 | 2717 29 16 15 18 14 --- 11 | 56 68 76 72 62 --- 65 R02 | 1656 19 12 17 30 16 --- 9 | 31 16 28 28 28 --- 20 R03 | 1809 18 15 17 21 24 --- 10 | 19 20 27 18 25 --- 14 R04 | 1228 12 8 20 12 16 --- 8 | 14 16 26 16 20 --- 12 R05 | 1247 17 16 21 33 21 --- 10 | 16 31 26 26 20 --- 18 XR06 | 2655 78 81 --- --- 93 --- 59 | 153 123 --- --- 90 --- 138 R07 | 2309 18 31 30 17 27 --- 16 | 15 23 29 30 26 --- 16 R08 | 1529 20 15 27 32 22 98 12 | 18 21 31 43 20 16 14 R10E | 2506 33 18 31 32 44 --- 18 | 33 25 32 26 48 --- 21 R11E | 1376 76 22 47 54 53 --- 28 | 42 18 45 47 56 --- 24 R13E | 3280 23 22 27 30 30 --- 14 | 46 49 40 36 45 --- 39 R14E | 1103 36 20 45 31 39 --- 20 | 18 28 64 25 37 --- 23 R15E | 2226 45 16 30 43 38 99 18 | 25 18 29 39 44 25 15 R17 | 1938 23 20 24 25 48 --- 17 | 20 33 43 36 23 --- 25 R18 | 1096 22 13 28 14 39 --- 15 | 22 35 37 48 61 --- 34 R19 | 1148 37 14 28 27 21 --- 14 | 27 53 58 65 54 --- 45 R20 | 1888 33 16 15 18 37 --- 15 | 26 27 37 31 50 --- 27 R21 | 1616 23 11 21 22 17 --- 10 | 48 48 53 43 48 --- 46 R22 | 2665 33 16 31 33 21 --- 14 | 29 44 62 41 45 --- 41 R23 | 2251 37 15 27 49 19 243 14 | 30 26 47 61 23 75 22 R24 | 1676 22 11 17 27 20 --- 10 | 43 43 29 48 49 --- 38 ------+-----------------------------------------+------------------------------------- RMS | 1958 32 17 27 30 31 162 |T 34 36 40 38 41 38 33 WRMS | 1958 32 18 25 30 31 162 |NE 35 39 40 40 40 45 35 MEDI | 1809 23 16 27 27 24 99 |MD 27 28 37 36 45 25 24 Table 3.1582.6 GPS week: 1582 Day: 6 MJD: 55324 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL ------+-----------------------------------------+------------------------------------- R01 | 1726 17 24 17 15 33 --- 13 | 77 81 85 76 94 --- 82 R02 | 1668 17 26 26 28 21 --- 13 | 27 21 31 41 26 --- 21 R03 | 3302 13 12 14 22 20 --- 8 | 21 16 21 24 23 --- 15 R04 | 1552 15 16 21 20 21 --- 10 | 26 24 38 32 29 --- 25 R05 | 1298 23 13 22 24 25 --- 12 | 26 24 29 25 27 --- 23 XR06 |11541 400 36 --- --- 158 --- 95 | 157 390 --- --- 84 --- 395 R07 | 1553 14 9 16 32 21 --- 8 | 25 23 26 29 25 --- 20 R08 | 2883 26 11 24 23 20 115 11 | 25 22 36 27 25 24 20 R10E | 2031 37 14 26 27 53 --- 18 | 34 33 54 42 51 --- 30 R11E | 1125 79 20 66 56 57 --- 33 | 35 32 46 58 54 --- 29 R13E | 4996 26 24 31 20 55 --- 19 | 52 51 46 39 46 --- 41 R14E | 1786 20 17 17 30 37 --- 12 | 30 39 37 41 32 --- 29 R15E | 2149 39 33 19 44 37 94 19 | 21 23 29 45 40 27 18 R17 | 1303 36 11 20 26 52 --- 17 | 64 66 66 59 37 --- 56 R18 | 1742 17 13 14 19 32 --- 11 | 46 52 58 49 56 --- 50 R19 | 1687 10 14 14 21 28 --- 9 | 45 60 63 64 50 --- 53 R20 | 2822 20 22 16 15 54 --- 16 | 39 40 63 51 67 --- 48 R21 | 844 30 18 31 18 34 --- 16 | 50 58 76 60 42 --- 53 R22 | 1069 32 20 20 17 23 --- 14 | 45 63 65 59 42 --- 52 R23 | 2087 20 14 31 35 29 184 13 | 28 33 50 47 36 102 31 R24 | 921 13 17 33 35 26 --- 13 | 43 51 77 73 42 --- 51 ------+-----------------------------------------+------------------------------------- RMS | 2147 29 18 26 28 36 137 |T 43 57 49 47 44 51 54 WRMS | 2147 30 18 23 28 36 137 |NE 46 64 52 47 44 63 62 MEDI | 1726 20 17 20 23 32 115 |MD 35 39 46 45 42 27 31