From IGS.ACC at noaa.gov Thu Feb 12 06:19:48 2009 From: IGS.ACC at noaa.gov (Jim Ray) Date: Thu, 12 Feb 2009 14:19:48 +0000 Subject: [IGSREPORT-17112] Wk 1516 IGLOS Final Orbits Message-ID: <49943004.5SZ8oI5RagU8qINy%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 12 Feb 06:19:50 PST 2009 Message Number 17112 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 IGLOS Orbit Combination - Week 1516 (Jan 25, 2009 - Jan 31, 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 2.1516. 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: igl1516[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1516 in the SP3 format. igl15167.sum Combination Report for GPS Week 1516. 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 | 172.2 ns 1 | 277.0 ns 2 | 182.4 ns 3 | 263.2 ns 4 | 259.1 ns 5 | 196.9 ns 6 | 255.3 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 ----+--------+--------------- 0 | ESX | R03 1 | ESX | R03 2 | ESX | R03 3 | ESX | R03 4 | ESX | R03 5 | ESX | R03 6 | ESX | R03 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 1.1516, 1a.1516). 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 2.1516.0-6) 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 3.1516.0-6). 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 1516 summary. (Jan 25, 2009 - Jan 31, 2009) Table 1.1516.a GPS week : 1516 MJD: 54856.0-54862.0 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 91| 0 -1 7 -9 2 -92 -.09 27 24 | 0 158 2603 2763 | 1 1 3 22 43 113 .02 | 0 349 cod 238| -1 0 0 31 4 26 -.11 16 14 | --- --- --- --- | 1 2 2 15 20 39 .03 | --- --- esx 132| 2 -1 -2 -53 17 -16 .40 87 40 | 73392 1589 6047 11982 | 1 2 3 27 30 65 .05 | 47513 6162 iac n/a| 0 0 -6 -12 -17 39 -.08 28 28 | 236355 -1424 5187 10678 | 2 0 3 6 35 88 .05 | 45474 3411 mcc n/a| -51 -16 23 162 -23 1067 1.38 589 589 | --- --- --- --- | 72 93 53 380 755 2506 2.14 | --- --- Table 1.1516.b GPS week : 1516 MJD: 54856.0-54862.0 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 | 10 12 10 8 11 13 13 | R03 | 10 11 15 11 12 13 12 | R04 | 12 16 19 15 11 16 16 | R06 | 0 0 --- --- --- --- --- | R07 | 9 12 14 12 8 17 12 | R10 | 12 16 14 13 10 18 13 | R11 | 15 12 12 9 17 11 11 | R13 | 12 16 11 15 16 12 12 | R14 | 11 13 12 14 12 16 8 | R15 | 16 19 16 14 15 11 10 | R17 | 15 16 18 15 13 14 13 | R18 | 9 13 11 14 12 17 12 | R19 | 9 11 15 9 8 14 13 | R20 | 18 13 9 12 18 19 22 | R21 | 14 11 11 10 14 16 11 | R22 | 10 13 14 14 9 19 11 | R23 | 17 17 18 17 21 23 15 | R24 | 36 46 38 35 31 16 23 | Table 1.1516.c GPS week : 1516 MJD: 54856.0-54862.0 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 1516 0 | 47 8 253 -1699 -276 -14750 89.4 2801 2801 | 172236 0 brd 1516 1 | -65 245 15 -4850 -2927 -14580 88.8 2758 2758 | 276971 0 brd 1516 2 | -13 -22 179 1149 -2925 -14460 91.8 3328 3328 | 182423 0 brd 1516 3 | -85 -27 14 -930 -214 -11510 91.6 3360 3360 | 263175 0 brd 1516 4 | 80 60 -6 -615 -503 -7269 91.4 2851 2851 | 259108 0 brd 1516 5 | -57 -30 -47 -1058 -625 -8195 94.5 2762 2762 | 196904 0 brd 1516 6 | 15 -92 36 3388 1179 -11570 96.6 3139 3139 | 255314 0 -------------+------------------------------------------------------------+---------------- brd 1516 mean| -11 20 63 -659 -898 -11762 92.0 2999 2999 | 229447 0 brd 1516 sdev| 62 109 109 2534 1506 3086 2.7 268 268 | 43757 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 2.1516.0 GPS week: 1516 Day: 0 MJD: 54856 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 91| 2 0 7 -4 9 -53 -.12 26 26 | 0 46 2154 2229 cod 238| 1 -1 3 61 28 33 -.06 17 15 | --- --- --- --- esx 132| 0 -1 -1 -53 4 54 .41 91 36 | 10401 -6303 4566 8700 iac n/a| -1 0 -7 -5 -34 -11 -.07 18 18 | 174379 -2622 4561 8259 mcc n/a| -181 55 18 348 879 -1244 -.71 775 775 | --- --- --- --- Table 2.1516.1 GPS week: 1516 Day: 1 MJD: 54857 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 91| 0 -3 6 -8 34 124 -.10 26 26 | 0 931 5475 6191 cod 238| -3 4 2 36 -9 -16 -.12 18 17 | --- --- --- --- esx 132| 1 0 -1 -63 4 -146 .47 88 38 | 114691 737 4418 8764 iac n/a| 0 -1 -9 -6 20 -1 -.08 23 23 | 276403 216 4423 7805 mcc n/a| -20 -215 123 619 -1577 -3325 5.92 1040 1040 | --- --- --- --- Table 2.1516.2 GPS week: 1516 Day: 2 MJD: 54858 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 91| 0 0 10 -32 -75 -95 -.06 32 24 | 0 11 1909 1960 cod 238| -2 0 -3 28 33 17 -.13 16 15 | --- --- --- --- esx 132| 2 0 -3 -48 71 -13 .42 89 38 | 23445 3180 4264 10127 iac n/a| 3 -2 -1 -19 -74 24 -.12 36 36 | 182121 -1467 4250 9200 mcc n/a| 21 66 -21 -346 205 1912 .50 575 575 | --- --- --- --- Table 2.1516.3 GPS week: 1516 Day: 3 MJD: 54859 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 91| -3 0 9 2 -7 -168 -.10 28 23 | 0 110 1998 2055 cod 238| 0 1 -1 26 11 -16 -.12 18 12 | --- --- --- --- esx 132| 4 -1 0 -25 20 -44 .42 96 39 | 103261 9083 5049 13931 iac n/a| -1 0 -4 -13 -31 210 -.16 29 29 | 264292 3915 5085 11886 mcc n/a| -65 3 -5 638 231 3035 1.77 428 428 | --- --- --- --- Table 2.1516.4 GPS week: 1516 Day: 4 MJD: 54860 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 91| 0 -1 10 -47 -25 -64 -.08 27 22 | 0 -76 2230 2292 cod 238| -1 -1 0 30 -11 15 -.09 18 16 | --- --- --- --- esx 132| 4 2 -7 -14 44 7 .40 83 34 | 107211 -3343 7660 11569 iac n/a| 0 0 -8 -19 13 47 -.04 28 28 | 262687 -6425 7558 11312 mcc n/a| -108 -26 66 -150 195 3859 .84 431 431 | --- --- --- --- Table 2.1516.5 GPS week: 1516 Day: 5 MJD: 54861 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 91| 1 -2 6 8 23 -204 -.11 21 21 | 0 -52 2238 2333 cod 238| -1 1 -2 26 0 89 -.10 14 13 | --- --- --- --- esx 132| 5 -6 -7 -97 -7 16 .30 86 42 | 36693 9855 11133 14807 mcc n/a| -2 8 9 36 -170 1826 .33 592 592 | --- --- --- --- Table 2.1516.6 GPS week: 1516 Day: 6 MJD: 54862 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 91| 0 -1 0 13 56 -188 -.06 29 26 | 0 140 2217 2287 cod 238| 0 0 -1 10 -19 62 -.13 13 11 | --- --- --- --- esx 132| 0 0 1 -68 -15 12 .36 75 53 | 118047 -2082 5245 15980 iac n/a| 0 0 -4 -8 1 -31 -.03 31 31 | 258251 -2162 5249 15609 mcc n/a| -3 -7 -22 -3 71 1410 1.02 283 283 | --- --- --- --- 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 3.1516.0 GPS week: 1516 Day: 0 MJD: 54856 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 2183 18 13 18 20 --- 10 | 27 33 37 33 --- 29 R03 | 2144 14 12 347 14 --- 9 | 24 28 210 32 --- 27 R04 | 2219 26 18 25 16 --- 12 | 30 38 37 40 --- 32 XR06 | ---- --- 5 --- --- --- 0 | --- 71 --- --- --- 70 R07 | 4294 15 12 21 14 --- 8 | 27 30 39 29 --- 28 R10 | 5691 18 12 28 21 --- 11 | 21 34 43 20 --- 28 R11 | 4033 32 19 39 15 256 15 | 18 22 53 22 95 23 R13 | 1676 14 18 26 19 --- 11 | 24 39 41 28 --- 30 R14 | 1666 18 19 19 19 --- 11 | 35 35 39 28 --- 30 R15 | 2854 41 18 29 19 1066 15 | 33 56 70 47 629 49 R17 | 3595 34 27 16 22 --- 15 | 38 60 57 56 --- 49 R18 | 2144 20 12 21 10 --- 9 | 24 39 37 33 --- 32 R19 | 988 17 13 19 15 --- 9 | 25 37 51 34 --- 35 R20 | 2599 54 11 30 26 --- 18 | 26 20 36 27 --- 20 R21 | 1461 25 12 40 17 --- 13 | 46 37 51 41 --- 38 R22 | 856 16 15 24 17 --- 10 | 50 65 63 45 --- 54 R23 | 1490 25 26 43 24 --- 16 | 78 70 102 80 --- 78 XR24 |>>>>> --- 34 --- 38 696 36 | --- 217 --- 213 512 218 ------+------------------------------------+-------------------------------- RMS | 2800 26 17 91 18 775 |T 32 51 60 47 412 48 WRMS | 2800 26 15 36 18 775 |NE 32 51 60 47 412 48 MEDI | 2183 18 13 25 19 696 |MD 27 37 43 33 512 32 Table 3.1516.1 GPS week: 1516 Day: 1 MJD: 54857 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1404 12 17 23 25 --- 11 | 25 21 41 37 --- 26 R03 | 1236 19 11 331 14 --- 10 | 28 19 194 26 --- 21 R04 | 3560 26 26 33 28 --- 16 | 36 38 47 29 --- 29 XR06 | ---- --- 4 --- --- --- 0 | --- 86 --- --- --- 88 R07 | 5116 13 19 30 18 --- 11 | 34 31 47 20 --- 31 R10 | 4317 16 27 42 20 --- 15 | 21 33 49 25 --- 29 R11 | 4185 21 14 23 21 307 11 | 15 16 40 20 40 16 R13 | 3069 27 22 37 23 --- 15 | 24 46 56 25 --- 33 R14 | 1824 34 17 24 15 --- 13 | 34 28 39 25 --- 24 R15 | 1359 42 23 24 37 1438 18 | 28 44 42 29 807 30 R17 | 3440 35 24 30 21 --- 16 | 43 63 56 50 --- 49 R18 | 2348 16 13 41 15 --- 12 | 27 30 41 20 --- 24 R19 | 798 14 15 24 20 --- 10 | 30 29 28 25 --- 25 R20 | 1251 32 13 24 15 --- 12 | 21 23 42 15 --- 20 R21 | 711 25 13 24 14 --- 11 | 23 37 52 46 --- 36 R22 | 1040 32 16 25 19 --- 13 | 31 44 36 42 --- 32 R23 | 2728 32 14 33 37 --- 17 | 53 54 73 41 --- 51 XR24 |13344 --- 40 --- 52 1036 46 | --- 245 --- 220 372 237 ------+------------------------------------+-------------------------------- RMS | 2757 26 18 88 23 1039 |T 29 49 55 40 406 44 WRMS | 2757 26 17 38 23 1039 |NE 29 49 55 40 406 44 MEDI | 2348 25 16 25 20 1036 |MD 28 33 42 26 372 29 Table 3.1516.2 GPS week: 1516 Day: 2 MJD: 54858 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1046 21 10 24 17 --- 10 | 24 29 40 25 --- 26 R03 | 1718 26 14 346 26 --- 15 | 24 26 205 37 --- 24 R04 | 1593 22 18 52 38 --- 18 | 49 48 72 61 --- 47 R07 | 3333 19 15 22 41 --- 14 | 26 28 47 36 --- 28 R10 | 4099 18 18 38 16 --- 13 | 19 21 34 20 --- 21 R11 | 2289 18 17 34 15 154 12 | 20 26 55 28 54 24 R13 | 3461 15 11 27 26 --- 11 | 19 31 48 32 --- 27 R14 | 1295 29 11 23 22 --- 12 | 28 27 33 22 --- 22 R15 | 3048 19 21 28 44 891 16 | 45 61 50 51 418 52 R17 | 1119 34 8 48 30 --- 17 | 49 42 44 47 --- 39 R18 | 1321 20 17 17 22 --- 11 | 44 44 29 26 --- 33 R19 | 1035 21 13 43 27 --- 15 | 29 30 49 19 --- 25 R20 | 915 16 9 23 14 --- 8 | 23 25 27 23 --- 21 R21 | 1752 19 17 15 24 --- 11 | 35 38 50 45 --- 37 R22 | 811 15 12 23 42 --- 13 | 33 35 41 48 --- 32 R23 | 1750 42 16 33 38 --- 18 | 40 62 62 56 --- 51 R24 |10673 92 34 44 90 419 37 | 60 142 59 156 288 136 ------+------------------------------------+-------------------------------- RMS | 3328 32 16 89 36 575 |T 33 42 55 43 253 37 WRMS | 3328 24 15 38 36 575 |NE 33 42 55 43 253 37 MEDI | 1718 20 15 28 26 419 |MD 29 31 48 36 288 28 Table 3.1516.3 GPS week: 1516 Day: 3 MJD: 54859 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1384 16 8 17 14 --- 7 | 40 36 45 25 --- 35 R03 | 2100 20 10 379 16 --- 10 | 37 42 237 34 --- 38 R04 | 1591 21 15 38 27 --- 14 | 56 61 59 61 --- 56 R07 | 1942 16 13 31 20 --- 11 | 46 39 54 40 --- 41 R10 | 4500 34 4 22 24 --- 12 | 31 45 68 49 --- 47 R11 | 712 12 8 25 15 147 8 | 25 34 52 17 58 29 R13 | 3327 20 19 38 26 --- 14 | 27 33 47 33 --- 27 R14 | 894 31 16 30 17 --- 13 | 43 33 48 37 --- 33 R15 | 3793 21 17 25 36 685 14 | 30 40 48 25 476 33 R17 | 1076 20 11 46 22 --- 14 | 42 42 63 44 --- 42 R18 | 849 30 13 32 21 --- 13 | 26 33 41 33 --- 28 R19 | 705 18 10 23 13 --- 9 | 49 43 31 32 --- 39 R20 | 782 20 13 31 21 --- 12 | 36 36 30 22 --- 28 R21 | 2108 14 13 22 20 --- 10 | 34 45 37 37 --- 37 R22 | 1397 22 11 30 33 --- 13 | 34 35 28 36 --- 26 R23 | 1461 33 18 19 42 --- 16 | 59 65 73 77 --- 64 R24 |10985 68 54 39 73 243 34 | 106 133 102 134 238 105 ------+------------------------------------+-------------------------------- RMS | 3359 28 18 96 29 428 |T 42 46 62 43 257 41 WRMS | 3359 23 12 39 29 428 |NE 42 46 62 43 257 41 MEDI | 1461 20 13 30 21 243 |MD 37 40 48 36 238 37 Table 3.1516.4 GPS week: 1516 Day: 4 MJD: 54860 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 1468 11 13 26 22 --- 10 | 29 39 40 35 --- 35 R03 | 1694 15 12 317 23 --- 11 | 25 33 159 44 --- 29 R04 | 2021 13 16 27 15 --- 10 | 33 25 50 42 --- 31 R07 | 3723 16 10 17 15 --- 8 | 27 29 43 27 --- 27 R10 | 3924 15 11 19 25 --- 10 | 22 25 49 36 --- 26 R11 | 872 31 9 42 35 166 17 | 22 32 57 37 86 31 R13 | 1715 14 27 30 37 --- 16 | 20 35 55 28 --- 27 R14 | 2693 15 16 34 17 --- 12 | 24 26 47 41 --- 31 R15 | 3515 25 15 32 33 630 15 | 34 51 62 35 719 44 R17 | 857 27 15 22 27 --- 13 | 48 70 84 69 --- 63 R18 | 750 23 16 14 28 --- 12 | 40 37 39 32 --- 33 R19 | 723 16 8 14 17 --- 8 | 32 32 37 46 --- 31 R20 | 787 25 31 22 39 --- 17 | 26 36 44 35 --- 33 R21 | 1325 23 25 22 22 --- 13 | 31 45 29 34 --- 30 R22 | 2397 16 11 19 17 --- 9 | 24 28 39 25 --- 26 R23 | 633 19 24 44 54 --- 20 | 38 51 65 63 --- 45 R24 | 8131 76 27 71 24 365 30 | 47 128 135 169 644 133 ------+------------------------------------+-------------------------------- RMS | 2850 27 18 83 28 431 |T 30 42 60 46 483 39 WRMS | 2850 22 16 34 28 431 |NE 30 42 60 46 483 39 MEDI | 1694 16 15 26 24 365 |MD 29 35 49 36 644 31 Table 3.1516.5 GPS week: 1516 Day: 5 MJD: 54861 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL ------+-------------------------------+--------------------------- R02 | 2792 18 11 30 --- 13 | 28 33 39 --- 32 R03 | 1626 15 11 329 --- 13 | 24 25 123 --- 25 R04 | 1817 21 16 33 --- 15 | 37 39 45 --- 36 R07 | 4104 24 16 37 --- 17 | 33 41 46 --- 36 R10 | 2482 21 10 46 --- 17 | 35 32 57 --- 36 R11 | 783 14 6 27 184 10 | 22 21 29 79 22 R13 | 2035 13 13 24 --- 11 | 14 21 31 --- 12 R14 | 6594 15 16 36 --- 15 | 24 33 48 --- 28 R15 | 3207 19 8 20 151 10 | 23 31 46 433 30 R17 | 1136 21 18 22 --- 14 | 74 76 92 --- 81 R18 | 1531 31 14 30 --- 17 | 28 40 56 --- 32 R19 | 1237 16 10 34 --- 13 | 39 42 47 --- 38 R20 | 828 17 24 42 --- 19 | 34 51 32 --- 43 R21 | 1728 27 18 25 --- 16 | 30 28 33 --- 22 R22 | 3224 25 17 41 --- 18 | 21 25 42 --- 16 R23 | 1045 24 17 58 --- 22 | 33 42 91 --- 40 R24 | 3756 31 11 24 998 15 | 77 144 80 546 144 ------+-------------------------------+--------------------------- RMS | 2762 21 14 86 592 |T 33 42 55 352 39 WRMS | 2762 21 13 42 592 |NE 33 42 55 352 39 MEDI | 1817 21 14 33 184 |MD 30 33 46 433 32 Table 3.1516.6 GPS week: 1516 Day: 6 MJD: 54862 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- R02 | 2860 29 7 32 23 --- 12 | 38 39 52 44 --- 40 R03 | 3928 19 10 290 23 --- 11 | 34 41 189 33 --- 36 R04 | 1223 38 23 29 20 --- 16 | 38 38 47 33 --- 36 R07 | 2811 22 9 26 32 --- 12 | 37 37 40 39 --- 34 R10 | 2311 26 8 31 26 --- 12 | 34 34 46 24 --- 32 R11 | 1351 22 11 24 20 173 10 | 31 33 47 27 51 30 R13 | 1393 21 12 33 17 --- 12 | 31 34 47 35 --- 34 R14 | 4949 15 10 15 13 --- 7 | 41 33 41 36 --- 35 R15 | 5138 24 9 19 19 69 9 | 29 37 42 29 503 33 R17 | 1814 32 9 20 32 --- 12 | 72 80 72 85 --- 74 R18 | 1981 25 14 22 28 --- 12 | 40 46 47 48 --- 41 R19 | 2322 20 11 27 34 --- 12 | 48 48 55 45 --- 47 R20 | 2016 37 15 45 59 --- 21 | 44 50 84 31 --- 50 R21 | 1490 19 13 13 30 --- 10 | 37 42 41 33 --- 37 R22 | 3676 20 12 27 19 --- 11 | 33 37 39 34 --- 32 R23 | 828 29 11 19 47 --- 15 | 59 62 66 77 --- 62 R24 | 6429 61 23 37 46 453 23 | 64 201 82 192 209 195 ------+------------------------------------+-------------------------------- RMS | 3138 29 13 75 31 283 |T 41 52 61 49 254 49 WRMS | 3138 26 11 53 31 283 |NE 41 52 61 49 254 49 MEDI | 2311 24 11 27 26 173 |MD 38 39 47 35 209 36