From igsacc at gfz-potsdam.de Thu Apr 20 21:42:40 2006 From: igsacc at gfz-potsdam.de (Gerd Gendt3) Date: Fri, 21 Apr 2006 06:42:40 +0200 Subject: [IGSREPORT-13736] Wk 1369 IGLOS Final Orbits Message-ID: <444862C0.mailx6EI11R89N@kg20> ****************************************************************************** IGS Electronic Report 20 Apr 21:42:48 PDT 2006 Message Number 13736 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam IGLOS Orbit Combination - Week 1369 (Apr 02, 2006 - Apr 08, 2006) Contact: Gerd Gendt (gendt at gfz-potsdam.de) Thomas Nischan ( nisn at gfz-potsdam.de) 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 2.1369. 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: igl1369[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1369 in the SP3 format. igl13697.sum Combination Report for GPS Week 1369. 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 | 317.6 ns 1 | 319.5 ns 2 | 317.2 ns 3 | 308.4 ns 4 | 313.6 ns 5 | 318.8 ns 6 | 316.5 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 ----+--------+--------------- 2 | ESX | R20 3 | ESX | R20 R24 6 | IAC | R05 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 1.1369, 1a.1369). 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 2.1369.0-6) 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 3.1369.0-6). 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 1369 summary. (Apr 02, 2006 - Apr 08, 2006) Table 1.1369.a GPS week : 1369 MJD: 53827.0-53833.0 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. Units: mas, ppb, meters, nano-sec, nano-sec/day. CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 40|-.00 -.00 .01 .03 .02 -.09 -.2 .05 .05 | .0 .2 3.36 | .00 .00 .00 .08 .05 .18 .1 | .0 .3 cod 176| .00 .00 .02 .07 -.09 .18 .0 .06 .06 | --- --- --- | .00 .00 .01 .08 .04 .11 .1 | --- --- esx 47| .00 .00 -.00 .01 .04 -.04 -.0 .06 .06 | 165.8 385.8 10.34 | .00 .00 .01 .13 .06 .11 .1 | 105.4 176.6 iac n/a|-.00 -.00 -.08 -.33 -.03 -.00 .5 .09 .09 | 164.1 4.4 118.65 | .01 .00 .01 .10 .10 .17 .1 | 384.2 11.4 mcc n/a|-.00 -.01 -.08 -.17 .03 .36 .4 .15 .15 | --- --- --- | .02 .02 .03 .13 .14 1.07 .5 | --- --- Table 1.1369.b GPS week : 1369 MJD: 53827.0-53833.0 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: cm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------+-----------------------------+------------------------------------------ R01 | 4 3 3 3 3 3 3 | R02 | 4 3 3 3 3 3 3 | R03 | 4 4 3 3 4 2 3 | R04 | 3 3 4 3 3 3 3 | R05 | --- --- --- --- 9 7 36 | R06 | 5 4 5 5 5 4 3 | R07 | 4 3 3 3 3 3 4 | R08 | 3 4 3 4 2 3 4 | R17E | 4 2 3 4 3 5 3 | R19E | 3 3 3 3 3 3 5 | R20E | --- --- --- --- 14 3 3 | R21E | 3 4 3 3 3 3 4 | R22E | 3 3 5 3 2 2 3 | R23E | --- --- --- --- 7 4 4 | R24E | --- --- --- --- 11 8 6 | Table 1.1369.c GPS week : 1369 MJD: 53827.0-53833.0 Daily transformation of broadcast orbits (brd) to the combined IGL orbit. Mean and standard deviations of the transformation parameters for the whole gpsweek. Units: mas, ppb, meters, nano-sec, nano-sec/day CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS -------------+-------------------------------------------------------------+--------------------- brd 1369 0 | .24 -.11 -.80 -31.01 -33.05 -415.80 96.3 6.06 6.06 | 317.6 .0 .0 brd 1369 1 | .19 -.90 -1.15 -18.04 -33.87 -440.70 97.2 7.69 7.69 | 319.5 .0 .0 brd 1369 2 | .03 .39 -1.48 -32.28 -32.90 -436.00 94.1 6.77 6.77 | 317.2 .0 .0 brd 1369 3 | -.11 -.30 -.61 -21.59 -24.90 -450.50 77.3 7.29 7.29 | 308.4 .0 .0 brd 1369 4 | -.38 -.13 -.21 -28.07 -21.73 -412.80 85.9 7.63 7.63 | 313.6 .0 .0 brd 1369 5 | -.46 .03 .07 -25.27 -24.96 -398.40 82.8 7.19 7.19 | 318.9 .0 .0 brd 1369 6 | .17 .23 -.44 -25.90 -30.03 -394.90 95.2 5.82 5.82 | 316.5 .0 .0 -------------+-------------------------------------------------------------+--------------------- brd 1369 mean| -.04 -.11 -.66 -26.02 -28.78 -421.30 89.8 6.92 6.92 | 316.0 .0 .0 brd 1369 sdev| .28 .42 .53 5.04 4.87 21.48 7.8 .74 .74 | 3.8 .0 .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. Units: mas, ppb, meters, nano-sec, nano-sec/day. Table 2.1369.0 GPS week: 1369 Day: 0 MJD: 53827 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 40|-.00 -.00 .02 .05 -.05 .04 -.2 .04 .04 | .0 -.1 3.17 cod 176| .01 .01 .03 -.03 -.15 .24 .1 .08 .08 | --- --- --- esx 47|-.00 .00 .01 .11 .08 -.19 .1 .06 .06 | 281.6 499.3 11.55 iac n/a| .00 -.00 -.08 -.36 -.11 -.15 .7 .09 .09 | 313.9 -2.5 11.65 mcc n/a| .01 -.02 -.10 -.25 -.00 .83 .7 .18 .18 | --- --- --- Table 2.1369.1 GPS week: 1369 Day: 1 MJD: 53828 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 40|-.00 -.00 .01 -.04 .01 -.20 -.0 .03 .03 | .0 -.3 3.67 cod 176| .00 -.00 .03 .12 -.09 .25 -.0 .06 .06 | --- --- --- esx 47|-.00 .00 -.01 .16 .03 .08 -.0 .06 .06 | 231.8 493.2 11.41 iac n/a|-.01 -.00 -.09 -.45 .09 .04 .6 .09 .09 | 313.8 2.7 11.33 mcc n/a| .03 -.01 -.06 -.26 -.06 1.89 .1 .15 .15 | --- --- --- Table 2.1369.2 GPS week: 1369 Day: 2 MJD: 53829 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 40|-.00 -.00 .01 -.03 .05 -.06 -.1 .04 .04 | .0 .5 3.46 cod 176|-.00 .00 .03 .09 -.05 .27 -.0 .07 .07 | --- --- --- esx 47| .00 .00 -.01 .06 -.05 -.13 .1 .05 .04 | 99.4 95.6 15.38 iac n/a| .00 .00 -.08 -.35 -.05 .03 .4 .09 .09 | 307.4 -3.6 14.61 mcc n/a| .01 .00 -.08 -.04 .08 -1.30 .6 .21 .21 | --- --- --- Table 2.1369.3 GPS week: 1369 Day: 3 MJD: 53830 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 40|-.00 -.00 .02 -.02 .08 -.02 .1 .05 .05 | -.0 .4 3.75 cod 176|-.00 .00 .02 .01 -.06 .08 .0 .05 .05 | --- --- --- esx 47| .01 .00 -.00 .06 .03 .10 -.0 .07 .07 | -8.1 184.0 8.39 iac n/a| .00 -.00 -.09 -.23 .09 -.22 .5 .09 .09 | 306.2 -2.5 8.49 mcc n/a|-.03 .00 -.09 -.08 .15 -.72 1.1 .14 .14 | --- --- --- Table 2.1369.4 GPS week: 1369 Day: 4 MJD: 53831 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 40|-.00 -.01 .02 .17 .03 -.19 -.2 .04 .04 | .0 .2 3.54 cod 176|-.00 .00 .02 -.00 -.09 .28 -.1 .05 .05 | --- --- --- esx 47| .00 .00 -.00 -.14 .01 -.01 .0 .05 .06 | 190.3 386.4 7.82 iac n/a|-.01 -.00 -.08 -.17 .01 -.05 .5 .09 .09 | 304.6 7.7 7.96 mcc n/a|-.02 -.03 -.07 -.06 .19 .35 -.1 .11 .11 | --- --- --- Table 2.1369.5 GPS week: 1369 Day: 5 MJD: 53832 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 40|-.01 -.01 .01 -.03 -.03 -.38 -.3 .09 .09 | .0 .2 3.12 cod 176| .00 .00 .01 .20 -.06 .17 .1 .04 .04 | --- --- --- esx 47| .00 .00 -.00 -.18 .12 -.03 -.2 .06 .06 | 263.6 544.9 9.28 iac n/a|-.01 -.01 -.06 -.42 -.14 .32 .4 .10 .10 | 310.0 .4 10.06 mcc n/a|-.00 .01 -.04 -.37 -.22 .96 .3 .10 .10 | --- --- --- Table 2.1369.6 GPS week: 1369 Day: 6 MJD: 53833 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 40|-.01 .00 .01 .13 .03 .16 -.2 .07 .07 | .0 .4 2.83 cod 176| .00 .00 .01 .08 -.14 .01 .1 .05 .05 | --- --- --- esx 47| .01 -.00 .01 -.00 .10 -.08 -.3 .05 .05 | 102.1 497.0 8.53 iac n/a|-.02 .00 -.07 -.36 -.11 .02 .7 .11 .11 | -707.2 28.7 766.46 mcc n/a|-.01 .01 -.13 -.09 .06 .49 -.3 .18 .18 | --- --- --- 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: cm. Table 3.1369.0 GPS week: 1369 Day: 0 MJD: 53827 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 823 3 11 5 11 --- 4 | 7 12 9 5 --- 7 R02 | 582 7 9 6 6 --- 4 | 4 8 9 4 --- 5 R03 | 601 3 10 7 7 13 4 | 6 7 7 4 2 5 R04 | 400 2 9 5 8 --- 3 | 4 8 5 5 --- 4 R06 | 369 7 7 10 8 --- 5 | 8 5 10 6 --- 5 R07 | 613 2 8 7 11 13 4 | 5 7 6 6 5 5 R08 | 390 2 7 4 11 --- 3 | 6 8 5 6 --- 5 R17E | 358 4 4 7 11 --- 4 | 8 6 6 8 --- 6 R19E | 930 4 5 5 10 --- 3 | 8 7 9 6 --- 7 R21E | 506 5 6 7 8 --- 3 | 10 14 12 13 --- 11 R22E | 771 3 6 3 7 24 3 | 10 11 9 9 13 9 ------+------------------------------+-------------------------- RMS | 606 4 8 6 9 18 |T 7 8 8 7 7 6 WRMS | 606 4 8 6 9 18 |NE 6 8 7 5 4 5 MEDI | 582 3 7 6 8 13 |MD 7 8 9 6 5 5 Table 3.1369.1 GPS week: 1369 Day: 1 MJD: 53828 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 743 3 6 6 10 --- 3 | 7 9 8 4 --- 6 R02 | 643 3 5 3 10 --- 3 | 5 8 7 6 --- 5 R03 | 859 4 10 7 8 12 4 | 9 11 12 5 3 8 R04 | 876 3 9 4 5 --- 3 | 3 5 6 3 --- 3 R06 | 737 4 8 10 8 --- 4 | 8 9 8 5 --- 5 R07 | 410 4 6 6 9 9 3 | 6 6 8 5 7 5 R08 | 690 3 6 9 11 --- 4 | 5 6 8 8 --- 5 R17E | 514 3 3 4 8 --- 2 | 3 3 6 5 --- 3 R19E |1273 3 3 4 9 --- 3 | 5 3 4 4 --- 3 R21E | 516 4 6 8 10 --- 4 | 9 12 10 9 --- 9 R22E | 836 3 4 5 9 21 3 | 6 6 6 11 13 6 ------+------------------------------+-------------------------- RMS | 769 3 6 6 9 15 |T 6 7 8 6 8 5 WRMS | 769 3 6 6 9 15 |NE 6 8 8 5 5 5 MEDI | 737 3 6 6 9 12 |MD 6 6 8 5 7 5 Table 3.1369.2 GPS week: 1369 Day: 2 MJD: 53829 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 629 2 7 4 9 --- 3 | 4 6 4 6 --- 4 R02 | 823 5 6 3 8 --- 3 | 6 10 7 5 --- 6 R03 | 913 3 9 5 9 11 3 | 6 9 8 4 4 5 R04 | 811 4 11 4 8 --- 4 | 5 9 5 3 --- 4 R06 | 309 6 13 6 13 --- 5 | 6 14 7 9 --- 5 R07 | 375 3 5 4 11 15 3 | 4 5 6 6 7 4 R08 | 622 3 6 5 8 --- 3 | 4 6 8 6 --- 4 R17E | 367 3 4 5 7 --- 3 | 5 4 6 4 --- 4 R19E | 926 4 3 4 8 --- 3 | 3 6 8 4 --- 4 R21E | 625 4 4 6 9 --- 3 | 5 8 8 10 --- 6 R22E | 687 7 6 8 11 30 5 | 6 8 9 8 10 6 ------+------------------------------+-------------------------- RMS | 677 4 7 5 9 21 |T 5 8 15 6 7 5 WRMS | 677 4 7 4 9 21 |NE 5 8 6 6 6 5 MEDI | 629 4 6 5 9 15 |MD 5 8 7 6 7 4 Table 3.1369.3 GPS week: 1369 Day: 3 MJD: 53830 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 251 2 6 8 7 --- 3 | 3 5 8 5 --- 4 R02 | 628 4 6 6 8 --- 3 | 4 8 4 4 --- 4 R03 | 981 5 5 6 8 10 3 | 8 9 6 4 2 6 R04 |1057 2 4 3 10 --- 3 | 6 6 6 4 --- 4 R06 | 723 8 5 10 11 --- 5 | 5 9 12 8 --- 5 R07 | 512 4 3 6 10 13 3 | 5 5 9 6 6 4 R08 | 259 5 6 4 10 --- 4 | 6 9 9 10 --- 7 R17E | 348 8 3 10 7 --- 4 | 4 6 9 4 --- 5 R19E |1076 4 4 5 7 --- 3 | 5 5 8 5 --- 5 R21E |1034 3 4 5 8 --- 3 | 9 11 12 10 --- 10 R22E | 342 5 3 5 8 18 3 | 7 8 8 6 10 7 ------+------------------------------+-------------------------- RMS | 729 5 5 7 9 14 |T 6 7 22 6 6 6 WRMS | 729 5 5 7 9 14 |NE 5 7 8 6 4 5 MEDI | 628 4 4 6 8 13 |MD 5 8 9 5 6 5 Table 3.1369.4 GPS week: 1369 Day: 4 MJD: 53831 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 265 2 6 4 11 --- 3 | 3 5 6 5 --- 3 R02 | 415 5 3 5 7 --- 3 | 4 4 4 3 --- 2 R03 | 605 4 7 8 8 6 4 | 3 7 7 7 4 4 R04 |1262 3 5 3 9 --- 3 | 4 8 6 4 --- 5 XR05 | 930 12 10 --- 16 --- 9 | 12 11 --- 13 --- 10 R06 |1388 6 5 9 14 --- 5 | 6 6 10 7 --- 4 R07 | 624 4 4 6 10 12 3 | 4 5 9 4 4 5 R08 | 393 2 4 3 9 --- 2 | 4 4 4 6 --- 3 R17E | 275 5 4 6 9 --- 3 | 11 8 10 7 --- 8 R19E | 760 4 5 3 8 --- 3 | 6 5 7 5 --- 5 XR20E | 894 12 16 --- --- --- 14 | 3 8 --- --- --- 5 R21E | 975 4 4 3 7 --- 3 | 9 10 11 11 --- 10 R22E | 360 4 4 4 6 14 2 | 7 7 8 8 10 7 XR23E | 358 10 5 14 --- --- 7 | 5 5 6 --- --- 4 XR24E | 854 20 12 13 --- --- 11 | 5 2 99 --- --- 4 ------+------------------------------+-------------------------- RMS | 763 4 5 5 9 11 |T 6 6 14 7 6 5 WRMS | 763 4 5 6 9 11 |NE 5 6 7 6 4 5 MEDI | 624 4 5 5 9 12 |MD 5 6 7 6 4 5 Table 3.1369.5 GPS week: 1369 Day: 5 MJD: 53832 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 388 3 4 5 9 --- 3 | 3 4 8 4 --- 3 R02 | 489 5 4 6 10 --- 3 | 4 4 5 3 --- 3 R03 | 250 3 2 5 7 4 2 | 7 6 6 4 8 4 R04 | 981 4 3 5 7 --- 3 | 6 5 7 5 --- 5 XR05 | 919 10 7 --- 17 --- 7 | 19 21 --- 18 --- 17 R06 |1618 7 3 6 12 --- 4 | 8 6 9 6 --- 4 R07 | 578 5 4 5 10 10 3 | 7 9 8 4 5 7 R08 | 471 5 5 7 7 --- 3 | 5 6 9 5 --- 5 R17E | 233 11 4 9 11 --- 5 | 9 7 4 4 --- 5 R19E | 717 6 2 7 9 --- 3 | 6 6 8 5 --- 5 R20E | 538 4 4 7 11 --- 3 | 4 5 99 5 --- 3 R21E | 767 8 4 4 10 --- 3 | 12 14 13 10 --- 12 R22E | 525 4 2 3 8 14 2 | 6 7 7 7 11 6 R23E | 632 8 3 6 12 --- 4 | 4 4 7 3 --- 4 R24E | 725 25 6 8 16 --- 8 | 5 3 99 3 --- 4 ------+------------------------------+-------------------------- RMS | 719 9 4 6 10 10 |T 7 7 21 6 8 6 WRMS | 719 9 4 6 10 10 |NE 7 8 7 6 7 6 MEDI | 578 5 4 6 10 10 |MD 6 6 8 5 8 5 Table 3.1369.6 GPS week: 1369 Day: 6 MJD: 53833 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 599 3 5 4 7 --- 3 | 5 4 7 4 --- 4 R02 | 510 4 4 5 11 --- 3 | 5 5 7 5 --- 4 R03 | 481 3 3 4 10 19 3 | 5 3 4 6 10 3 R04 | 310 5 4 5 6 --- 3 | 6 6 6 6 --- 5 XR05 | 687 44 30 --- 90 --- 36 | 17 20 --- 21 --- 16 R06 | 951 5 3 3 14 --- 3 | 8 5 10 7 --- 6 R07 | 423 5 4 6 15 12 4 | 8 9 13 5 8 8 R08 | 681 6 7 4 7 --- 4 | 7 9 5 5 --- 5 R17E | 187 6 3 3 12 --- 3 | 8 9 10 7 --- 8 R19E | 865 14 6 5 11 --- 5 | 9 9 8 8 --- 8 R20E | 423 3 3 6 11 --- 3 | 3 5 99 3 --- 3 R21E | 414 8 6 6 9 --- 4 | 13 15 19 14 --- 15 R22E | 602 6 4 3 8 20 3 | 7 5 6 6 15 6 R23E | 719 6 5 8 12 --- 4 | 4 4 6 7 --- 4 R24E | 490 17 9 4 14 --- 6 | 4 3 99 4 --- 4 ------+------------------------------+-------------------------- RMS | 582 7 5 5 11 18 |T 7 7 21 7 11 7 WRMS | 582 7 5 5 11 18 |NE 8 8 7 7 9 6 MEDI | 510 6 4 4 11 19 |MD 7 5 7 6 10 5