From IGS.ACC at noaa.gov Thu Oct 16 04:48:05 2008 From: IGS.ACC at noaa.gov (Jim Ray) Date: Thu, 16 Oct 2008 11:48:05 +0000 Subject: [IGSREPORT-16724] Wk 1499 IGLOS Final Orbits Message-ID: <48f729f5.9+RnQygyzh7jk+dL%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 16 Oct 04:48:07 PDT 2008 Message Number 16724 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 IGLOS Orbit Combination - Week 1499 (Sep 28, 2008 - Oct 04, 2008) 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 2.1499. 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: igl1499[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1499 in the SP3 format. igl14997.sum Combination Report for GPS Week 1499. 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 | 663.8 ns 1 | 660.8 ns 2 | 654.7 ns 3 | 595.1 ns 4 | 595.2 ns 5 | 653.0 ns 6 | 635.9 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 ----+--------+--------------- 1 | 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 1.1499, 1a.1499). 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 2.1499.0-6) 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 3.1499.0-6). 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 1499 summary. (Sep 28, 2008 - Oct 04, 2008) Table 1.1499.a GPS week : 1499 MJD: 54737.0-54743.0 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 64| 0 0 -1 0 5 -14 -.07 33 30 | 0 -160 2396 2524 | 2 2 6 34 41 79 .10 | 0 92 cod 237| -2 0 0 8 -19 7 -.12 24 20 | --- --- --- --- | 2 3 2 12 35 41 .06 | --- --- esx 123| 1 1 5 33 33 -3 .42 39 29 | 143187 8646 6521 18915 | 3 3 7 39 38 38 .03 | 27062 8879 iac n/a| 3 0 -4 -24 -13 -14 -.10 35 35 | 638687 540 6171 13035 | 2 1 4 27 36 76 .05 | 27986 5787 mcc n/a| 2 -1 40 60 -20 463 -.28 348 348 | --- --- --- --- | 8 15 21 148 100 526 .75 | --- --- Table 1.1499.b GPS week : 1499 MJD: 54737.0-54743.0 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 | 27 29 19 37 28 41 31 | R04 | 15 17 10 16 35 18 22 | R06 | 33 31 14 23 25 25 29 | R07 | 18 12 9 12 12 15 14 | R09 | --- --- --- 0 0 0 --- | R10 | 15 15 13 12 18 13 14 | R11 | 16 16 15 11 15 15 23 | R13 | 17 13 25 22 18 14 16 | R14 | 8 12 16 11 12 14 12 | R15 | 14 12 14 13 12 14 14 | R17 | 22 16 17 14 14 12 12 | R19 | 17 20 12 18 15 12 13 | R20 | 16 19 19 12 13 14 11 | R23 | 35 36 26 22 19 24 15 | R24 | 23 18 15 14 14 20 14 | Table 1.1499.c GPS week : 1499 MJD: 54737.0-54743.0 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 1499 0 | -11 147 167 -493 -1970 -14350 93.4 2380 2380 | 663773 0 brd 1499 1 | 1463 1672 -1132 -12910 4259 48040 <<<< >>>>> >>>>> | 660757 0 brd 1499 2 | -229 -343 90 -1171 -5841 -12040 93.0 4439 4439 | 654677 0 brd 1499 3 | -127 -224 237 447 -3233 -6225 97.4 3331 3331 | 595090 0 brd 1499 4 | 268 -147 304 1434 4895 -9511 98.4 2850 2850 | 595219 0 brd 1499 5 | 5 -9 146 119 995 -7929 98.0 3218 3218 | 653032 0 brd 1499 6 | 30 -131 152 357 -1607 -1720 94.0 4333 4333 | 635940 0 -------------+------------------------------------------------------------+---------------- brd 1499 mean| 199 137 -4 -1745 -357 -533 <<<< >>>>> >>>>> | 636926 0 brd 1499 sdev| 577 694 501 4989 3941 21801 678.3 >>>>> >>>>> | 29871 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 2.1499.0 GPS week: 1499 Day: 0 MJD: 54737 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 64| 4 -1 -6 -7 12 143 -.26 36 32 | 0 -58 2130 2312 cod 237| -7 0 -2 -3 -37 10 -.08 42 27 | --- --- --- --- esx 123| -5 6 20 68 -1 42 .38 41 31 | 168989 -462 4770 18150 iac n/a| 5 -1 -2 5 -35 -161 -.09 25 25 | 664427 -106 4786 10414 mcc n/a| 3 -14 8 246 -182 221 .48 200 200 | --- --- --- --- Table 2.1499.1 GPS week: 1499 Day: 1 MJD: 54738 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 64| 0 4 -5 -59 -15 35 .02 42 38 | 0 -93 2254 2373 cod 237| 0 0 5 -2 -12 16 -.13 18 13 | --- --- --- --- esx 123| 4 3 7 96 54 -57 .43 37 28 | 149592 13359 6826 18675 iac n/a| 2 1 -12 -6 15 -45 -.10 84 84 | 657142 7855 7012 13885 mcc n/a| 12 -2 54 162 51 622 .36 272 272 | --- --- --- --- Table 2.1499.2 GPS week: 1499 Day: 2 MJD: 54739 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 64| 3 0 4 29 0 -46 -.04 33 29 | 0 -315 2212 2304 cod 237| -4 -1 0 13 -55 5 -.08 18 15 | --- --- --- --- esx 123| 2 0 1 -21 47 -44 .43 42 26 | 150877 14627 7060 21335 iac n/a| 5 0 -4 -15 36 63 -.04 27 27 | 657774 4956 7087 18312 mcc n/a| 0 -7 69 107 25 768 -.33 546 546 | --- --- --- --- Table 2.1499.3 GPS week: 1499 Day: 3 MJD: 54740 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 64| -1 0 -3 29 -5 -65 -.06 33 29 | 0 -181 2962 3033 cod 237| -1 6 -1 20 -13 59 -.18 20 20 | --- --- --- --- esx 123| 3 -1 0 11 39 -15 .43 28 23 | 113050 -3210 7242 17715 iac n/a| 0 -2 1 -28 -22 -37 -.09 29 29 | 603092 -8301 7259 15762 mcc n/a| -15 12 35 -230 101 1432 -.09 308 308 | --- --- --- --- Table 2.1499.4 GPS week: 1499 Day: 4 MJD: 54741 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 64| 0 -1 -6 -17 -21 -67 -.14 32 29 | 0 -227 2825 2968 cod 237| -2 0 0 9 24 10 -.04 18 18 | --- --- --- --- esx 123| 0 -2 8 20 24 10 .38 54 38 | 97601 4411 7734 21955 iac n/a| 5 0 -1 -11 -32 13 -.12 30 30 | 596237 -1698 6167 10796 mcc n/a| 3 -23 20 37 -124 80 .03 485 485 | --- --- --- --- Table 2.1499.5 GPS week: 1499 Day: 5 MJD: 54742 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 64| 0 1 9 -14 -29 -72 -.05 30 26 | 0 -74 2208 2334 cod 237| -1 -3 0 25 23 -78 -.17 29 27 | --- --- --- --- esx 123| -1 0 0 38 92 41 .42 30 20 | 160756 10054 5950 20979 iac n/a| 5 2 -6 -78 -69 49 -.21 26 26 | 654849 -4172 4915 10438 mcc n/a| 6 6 41 64 -26 248 -.69 346 346 | --- --- --- --- Table 2.1499.6 GPS week: 1499 Day: 6 MJD: 54743 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 64| -3 -1 -2 36 93 -27 .02 27 26 | 0 -175 2184 2348 cod 237| 0 0 3 -7 -63 27 -.18 25 21 | --- --- --- --- esx 123| 6 1 3 17 -25 1 .45 41 34 | 161447 21746 6065 13602 iac n/a| 0 1 -5 -33 11 14 -.07 26 26 | 637292 5249 5976 11642 mcc n/a| 5 21 55 37 12 -130 -1.71 282 282 | --- --- --- --- 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 3.1499.0 GPS week: 1499 Day: 0 MJD: 54737 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- XR01 | ---- --- 32 --- 23 --- 27 | --- 61 --- 75 --- 68 R04 | 1425 22 35 29 15 --- 14 | 45 62 58 44 --- 46 R06 | 4311 82 75 33 27 --- 33 | 92 147 120 86 --- 100 R07 | 1304 30 23 52 16 --- 18 | 28 42 40 31 --- 29 R10 | 1296 30 24 36 17 --- 15 | 33 49 47 42 --- 38 R11 | 746 30 25 36 18 130 15 | 49 42 36 32 62 32 R13 | 1105 33 27 39 21 --- 17 | 42 43 60 30 --- 34 R14 | 2065 10 14 17 13 --- 7 | 34 35 41 36 --- 35 R15 | 1196 23 13 40 14 134 13 | 47 37 38 41 50 36 R17E | 3016 21 65 26 29 --- 21 | 34 64 44 44 --- 40 R19E | 1006 37 35 20 24 --- 17 | 37 50 42 38 --- 35 R20E | 1231 25 27 32 23 --- 15 | 55 55 78 75 --- 64 R23E | 2062 29 74 94 42 --- 35 | 50 74 97 89 --- 63 R24E | 5125 39 47 32 40 292 23 | 73 82 89 108 361 89 ------+------------------------------------+-------------------------------- RMS | 2379 36 42 41 25 200 |T 47 60 60 55 157 50 WRMS | 2379 32 27 31 25 200 |NE 46 57 55 46 56 46 MEDI | 1304 30 27 33 21 134 |MD 45 50 47 42 62 38 Table 3.1499.1 GPS week: 1499 Day: 1 MJD: 54738 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- XR01 | ---- --- 19 --- 42 --- 29 | --- 46 --- 61 --- 45 R04 |>>>>> 40 25 32 16 --- 16 | 44 52 39 39 --- 39 R06 |>>>>> 71 32 59 65 --- 31 | 79 152 179 147 --- 137 R07 |>>>>> 24 10 28 26 --- 12 | 34 46 55 39 --- 41 R10 |>>>>> 19 15 32 39 --- 15 | 36 38 40 29 --- 35 R11 |>>>>> 18 16 41 31 123 15 | 28 25 49 36 42 25 R13 |>>>>> 37 7 23 26 --- 13 | 25 33 55 46 --- 34 R14 |>>>>> 25 7 21 32 --- 12 | 40 43 32 44 --- 36 R15 |>>>>> 19 14 17 30 88 11 | 31 24 35 36 35 26 R17E |>>>>> 42 18 27 25 --- 15 | 41 55 62 63 --- 53 R19E |>>>>> 46 20 25 48 --- 19 | 42 42 44 62 --- 42 R20E |>>>>> 48 15 33 41 --- 18 | 40 62 75 50 --- 55 R23E |>>>>> 60 23 77 276 --- 36 | 75 104 143 181 --- 100 R24E |>>>>> 55 13 25 33 447 17 | 37 50 58 52 291 46 ------+------------------------------------+-------------------------------- RMS |>>>>> 42 18 37 84 272 |T 42 55 66 63 122 51 WRMS |>>>>> 38 13 28 84 272 |NE 39 51 60 53 38 46 MEDI |>>>>> 40 15 28 32 123 |MD 40 46 55 46 42 41 Table 3.1499.2 GPS week: 1499 Day: 2 MJD: 54739 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- XR01 | ---- --- 14 --- 25 --- 19 | --- 68 --- 58 --- 62 R04 | 2066 25 14 21 12 --- 10 | 43 58 55 47 --- 49 R06 | 3198 31 15 41 12 --- 14 | 110 122 147 135 --- 123 R07 | 1961 19 14 11 15 --- 8 | 24 38 32 35 --- 31 R10 | 1616 19 11 27 33 --- 13 | 32 41 47 46 --- 39 R11 | 5335 20 19 39 25 144 14 | 36 38 64 34 59 38 R13 | 1276 26 25 82 39 --- 25 | 46 53 111 26 --- 46 R14 | 3157 39 10 33 33 --- 16 | 33 25 28 37 --- 22 R15 | 2967 18 17 31 33 59 14 | 30 37 37 56 52 37 R17 |12934 41 18 28 31 --- 16 | 31 73 74 63 --- 57 R19 | 909 21 12 25 25 --- 11 | 33 31 31 54 --- 27 R20E | 1483 34 20 54 25 --- 18 | 54 44 69 59 --- 49 R23E | 1938 64 33 60 27 --- 26 | 58 88 85 71 --- 71 R24E | 3502 36 14 33 26 933 15 | 41 49 59 52 487 45 ------+------------------------------------+-------------------------------- RMS | 4439 33 18 42 27 546 |T 43 54 64 55 199 49 WRMS | 4439 29 15 26 27 546 |NE 44 53 65 52 55 49 MEDI | 2066 26 14 33 25 144 |MD 36 44 59 52 59 45 Table 3.1499.3 GPS week: 1499 Day: 3 MJD: 54740 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- XR01 | ---- --- 29 --- 45 --- 36 | --- 75 --- 55 --- 62 R04 | 2248 50 16 18 17 --- 15 | 38 48 50 42 --- 38 R06 | 1444 69 40 14 16 --- 23 | 85 134 126 118 --- 110 R07 | 854 12 18 23 27 --- 12 | 37 30 50 30 --- 33 XR09 | 8340 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999 R10 | 2204 15 10 26 26 --- 11 | 43 38 49 41 --- 39 R11 | 5613 19 17 20 14 201 10 | 31 34 46 39 115 35 R13 | 1553 26 18 46 51 --- 21 | 37 32 58 44 --- 25 R14 | 3078 19 13 13 27 --- 10 | 33 56 52 41 --- 43 R15 | 2426 25 21 16 24 58 12 | 27 35 46 42 58 31 R17 | 3304 23 19 26 29 --- 14 | 54 50 64 70 --- 55 R19 | 1265 40 25 25 32 --- 17 | 51 36 44 34 --- 36 R20 | 1388 22 12 23 25 --- 11 | 51 41 52 38 --- 41 R23 | 1637 37 21 51 41 --- 22 | 81 97 96 94 --- 87 R24 | 8066 28 20 30 21 491 14 | 61 66 73 63 484 62 ------+------------------------------------+-------------------------------- RMS | 3330 33 20 28 29 308 |T 48 55 62 53 219 49 WRMS | 3330 29 20 23 29 308 |NE 41 53 59 50 86 46 MEDI | 2204 25 18 23 26 201 |MD 43 41 52 42 115 39 Table 3.1499.4 GPS week: 1499 Day: 4 MJD: 54741 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- XR01 | ---- --- 21 --- 36 --- 28 | --- 55 --- 73 --- 59 R04 | 2359 42 24 132 53 --- 35 | 40 63 138 32 --- 54 R06 | 1302 46 23 83 31 --- 25 | 157 173 207 180 --- 173 R07 | 1954 25 20 21 17 --- 12 | 16 34 23 22 --- 21 XR09 |12468 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999 R10 | 1220 26 21 30 43 --- 17 | 29 28 44 45 --- 28 R11 | 5237 20 8 56 18 129 14 | 30 25 54 29 118 24 R13 | 4767 26 26 34 36 --- 17 | 37 54 50 36 --- 37 R14 | 1083 21 14 36 19 --- 12 | 21 25 37 36 --- 22 R15 | 3515 26 16 23 19 55 11 | 39 29 33 31 71 27 R17 | 3492 31 20 26 23 --- 14 | 44 33 54 52 --- 39 R19 | 2068 36 13 27 26 --- 14 | 31 26 36 31 --- 24 R20 | 1013 21 14 40 19 --- 12 | 48 44 63 44 --- 44 R23 | 1477 45 18 44 34 --- 19 | 82 90 104 97 --- 88 R24 | 3104 33 14 35 23 828 14 | 53 66 80 65 536 63 ------+------------------------------------+-------------------------------- RMS | 2849 32 18 54 30 485 |T 48 53 71 55 241 50 WRMS | 2849 29 18 38 30 485 |NE 46 54 73 53 94 49 MEDI | 2068 26 18 34 23 129 |MD 39 34 54 36 118 37 Table 3.1499.5 GPS week: 1499 Day: 5 MJD: 54742 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- XR01 | ---- --- 41 --- 41 --- 41 | --- 81 --- 56 --- 60 R04 | 3719 24 48 20 29 --- 18 | 30 63 78 25 --- 35 R06 | 2714 57 27 53 28 --- 25 | 101 112 150 106 --- 110 R07 | 2133 36 21 14 23 --- 14 | 27 35 48 42 --- 35 XR09 |10429 --- --- 9 --- --- 0 | --- --- 9999 --- --- 9999 R10 | 732 16 23 24 23 --- 12 | 29 29 27 29 --- 19 R11 | 3028 16 24 33 24 102 14 | 27 25 59 28 52 31 R13 | 4434 20 25 24 23 --- 13 | 28 40 33 27 --- 27 R14 | 954 23 28 19 21 --- 13 | 29 42 45 44 --- 36 R15 | 1752 25 35 16 15 56 14 | 29 22 29 27 39 24 R17 | 4226 14 11 27 20 --- 11 | 27 28 45 33 --- 29 R19 | 5016 22 20 20 20 --- 12 | 46 36 51 47 --- 40 R20 | 1218 19 30 11 31 --- 14 | 42 35 38 52 --- 38 R23 | 1795 36 38 51 36 --- 23 | 76 101 90 87 --- 80 R24 | 5266 44 27 36 31 588 20 | 46 61 69 50 172 48 ------+------------------------------------+-------------------------------- RMS | 3217 30 29 30 26 346 |T 41 50 58 46 87 43 WRMS | 3217 26 27 20 26 346 |NE 37 49 58 42 45 41 MEDI | 2714 23 27 20 23 102 |MD 29 36 48 42 52 35 Table 3.1499.6 GPS week: 1499 Day: 6 MJD: 54743 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------------+-------------------------------- XR01 | ---- --- 29 --- 32 --- 30 | --- 57 --- 94 --- 72 R04 | 3364 24 32 59 39 --- 22 | 41 65 74 29 --- 47 R06 | 4719 45 60 50 42 --- 29 | 77 101 111 76 --- 85 R07 | 3980 33 23 23 18 --- 14 | 21 36 36 29 --- 25 R10 | 1412 25 18 35 19 --- 13 | 29 37 46 41 --- 31 R11 | 4865 28 14 78 35 108 23 | 28 26 71 34 50 26 R13 | 4124 34 12 49 16 --- 16 | 39 34 43 29 --- 28 R14 | 1762 15 21 23 23 --- 12 | 27 33 35 28 --- 25 R15 | 3765 25 18 34 21 71 14 | 37 40 59 45 46 40 R17 | 6748 26 15 15 20 --- 11 | 44 43 44 64 --- 47 R19 | 6859 22 22 26 20 --- 13 | 44 36 48 48 --- 40 R20 | 2023 20 11 28 15 --- 10 | 42 40 52 49 --- 42 R23 | 3720 20 24 28 28 --- 14 | 88 92 86 104 --- 90 R24 | 4916 24 20 32 21 471 13 | 64 66 69 72 229 65 ------+------------------------------------+-------------------------------- RMS | 4333 27 25 41 26 282 |T 44 50 59 53 108 47 WRMS | 4333 26 21 34 26 282 |NE 37 47 59 45 48 42 MEDI | 3980 25 20 32 21 108 |MD 41 40 52 45 50 40