From igsacc at gfz-potsdam.de Wed Oct 12 05:20:40 2005 From: igsacc at gfz-potsdam.de (Gerd Gendt3) Date: Wed, 12 Oct 2005 14:20:40 +0200 Subject: [IGSREPORT-13047] Wk 1342 IGLOS Final Orbits Message-ID: <434CFF98.mailxGTH110F2K@kg20> ****************************************************************************** IGS Electronic Report 12 Oct 05:20:50 PDT 2005 Message Number 13047 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam IGLOS Orbit Combination - Week 1342 (Sep 25, 2005 - Oct 01, 2005) 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 2.1342. 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: igl1342[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1342 in the SP3 format. igl13427.sum Combination Report for GPS Week 1342. 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 | 255.2 ns 1 | 286.7 ns 2 | 249.5 ns 3 | 230.2 ns 4 | 248.8 ns 5 | 249.3 ns 6 | 253.7 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 | ESX | R22 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 1.1342, 1a.1342). 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 2.1342.0-6) 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 3.1342.0-6). 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 1342 summary. (Sep 25, 2005 - Oct 01, 2005) Table 1.1342.a GPS week : 1342 MJD: 53638.0-53644.0 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 45|-.00 -.00 .01 .03 -.03 -.04 -.2 .08 .06 | .0 1.3 1.78 | .01 .00 .01 .03 .08 .09 .1 | .0 11.4 cod 176| .01 .00 .02 .06 .05 -.05 -.2 .06 .06 | --- --- --- | .00 .00 .01 .06 .05 .07 .1 | --- --- esx 52|-.00 .00 .01 .04 -.04 .17 .2 .08 .05 | 135.7 21.1 1.12 | .00 .00 .01 .08 .08 .07 .1 | 34.8 13.8 iac n/a|-.00 -.00 -.10 -.33 .08 -.17 .7 .11 .11 | 250.4 -2.1 .88 | .00 .01 .01 .06 .09 .23 .2 | 19.3 12.3 mcc n/a| .01 -.01 .00 -.40 -.09 1.36 .2 .15 .15 | --- --- --- | .02 .03 .03 .13 .12 .68 .6 | --- --- Table 1.1342.b GPS week : 1342 MJD: 53638.0-53644.0 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 | 3 3 3 2 3 2 3 | R02 | 3 3 3 2 3 3 3 | R03 | 4 4 3 3 4 3 3 | R04 | 3 3 3 3 3 3 2 | R05 | 3 3 4 3 3 4 3 | R06 | 8 8 8 8 10 9 8 | R07 | 6 4 4 5 10 6 3 | R08 | 3 3 2 3 3 4 3 | R17 | 4 3 3 3 3 5 7 | R18 | 4 4 3 4 5 4 4 | R21 | 4 5 4 3 3 3 3 | R22 | 3 3 3 3 11 19 6 | R23 | 3 4 3 3 4 4 3 | R24 | 5 6 3 3 5 5 3 | Table 1.1342.c GPS week : 1342 MJD: 53638.0-53644.0 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 1342 0 | .49 -.33 .08 44.80 8.43 -338.30 82.0 6.62 6.62 | 264.4 -13.1 .85 brd 1342 1 | .06 -.08 .00 42.37 5.18 -315.30 84.8 5.87 5.87 | 272.9 22.9 1.11 brd 1342 2 | -.11 .14 -.32 41.42 7.11 -294.30 93.2 4.95 4.95 | 258.1 .8 .85 brd 1342 3 | -.09 -.08 -.85 46.00 10.09 -287.80 91.5 4.58 4.58 | 242.7 -9.3 .83 brd 1342 4 | .02 -.14 -.54 39.95 9.21 -284.60 89.0 4.69 4.69 | 243.5 9.9 1.00 brd 1342 5 | .00 .12 -.36 43.64 11.02 -284.50 81.4 5.75 5.75 | 252.4 -2.1 .72 brd 1342 6 | -.07 -.07 -.54 42.46 19.11 -285.10 87.6 6.78 6.78 | 249.0 4.8 .78 -------------+-------------------------------------------------------------+--------------------- brd 1342 mean| .04 -.06 -.36 42.95 10.02 -298.56 87.1 5.61 5.61 | 254.7 2.0 .88 brd 1342 sdev| .21 .16 .32 2.05 4.45 20.68 4.6 .89 .89 | 11.1 12.1 .13 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 2.1342.0 GPS week: 1342 Day: 0 MJD: 53638 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 45| .00 -.01 .01 -.01 .05 -.14 -.3 .08 .08 | .0 -15.0 1.46 cod 176| .00 .00 .02 -.03 -.03 -.05 -.1 .05 .05 | --- --- --- esx 52| .00 .01 -.00 .10 -.02 .10 .1 .05 .04 | 91.0 .5 .91 iac n/a| .00 -.01 -.10 -.34 .24 -.16 .7 .13 .13 | 272.9 -23.8 .85 mcc n/a| .01 -.04 -.01 -.42 -.17 1.64 .5 .16 .16 | --- --- --- Table 2.1342.1 GPS week: 1342 Day: 1 MJD: 53639 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 45| .01 -.00 -.00 -.00 .05 -.02 -.3 .08 .07 | .0 20.7 1.86 cod 176| .01 .00 .02 -.03 .08 -.06 -.2 .06 .06 | --- --- --- esx 52|-.00 .01 .01 .11 -.16 .22 .2 .06 .06 | 127.8 11.9 1.25 iac n/a|-.00 .01 -.10 -.32 .13 -.67 .8 .12 .12 | 281.1 -11.9 1.11 mcc n/a| .04 .03 -.04 -.39 .12 1.41 -.8 .13 .13 | --- --- --- Table 2.1342.2 GPS week: 1342 Day: 2 MJD: 53640 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 45|-.01 -.01 .01 .04 .00 -.12 -.2 .07 .07 | -.0 1.6 1.32 cod 176| .01 .00 .03 .09 .03 .00 -.1 .05 .05 | --- --- --- esx 52|-.00 -.00 .01 .02 -.06 .18 .2 .06 .05 | 102.4 41.1 1.07 iac n/a| .00 .00 -.08 -.31 .07 -.12 .7 .09 .09 | 238.9 10.9 .85 mcc n/a|-.00 -.02 .02 -.64 -.26 1.63 .2 .14 .14 | --- --- --- Table 2.1342.3 GPS week: 1342 Day: 3 MJD: 53641 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 45|-.01 .01 .02 .02 -.17 -.12 -.2 .08 .06 | .0 -8.3 1.74 cod 176| .00 -.00 .02 .06 .08 .04 -.2 .04 .04 | --- --- --- esx 52| .00 -.01 -.00 .13 .07 .10 .3 .05 .05 | 121.6 15.4 1.12 iac n/a|-.00 .01 -.08 -.42 -.06 -.08 .9 .09 .09 | 227.6 -3.3 .83 mcc n/a| .01 .03 .04 -.38 -.04 .07 -.4 .17 .17 | --- --- --- Table 2.1342.4 GPS week: 1342 Day: 4 MJD: 53642 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 45|-.01 -.00 .01 .04 -.10 .08 -.2 .08 .06 | .0 7.1 2.25 cod 176| .00 -.00 .02 .09 .07 -.18 -.3 .09 .08 | --- --- --- esx 52| .00 .00 .02 -.04 -.01 .16 .1 .22 .07 | 149.3 29.1 1.73 iac n/a|-.01 -.01 -.09 -.37 .08 -.10 .8 .10 .10 | 245.3 4.7 1.00 mcc n/a|-.01 .01 .02 -.19 -.05 1.00 .3 .17 .17 | --- --- --- Table 2.1342.5 GPS week: 1342 Day: 5 MJD: 53643 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 45|-.00 -.00 .01 .08 .01 -.01 -.2 .08 .06 | .0 -.9 1.56 cod 176| .01 .01 .00 .13 .10 -.08 -.2 .06 .05 | --- --- --- esx 52|-.00 .00 .03 -.07 -.13 .30 .1 .08 .06 | 177.5 17.5 .59 iac n/a|-.01 -.01 -.12 -.24 .03 .07 .4 .11 .11 | 241.5 -.3 .72 mcc n/a|-.02 -.02 -.00 -.40 -.08 1.52 .4 .13 .13 | --- --- --- Table 2.1342.6 GPS week: 1342 Day: 6 MJD: 53644 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 45|-.01 -.00 .02 .07 -.07 .04 -.1 .08 .06 | .0 3.9 2.26 cod 176| .01 -.00 .03 .10 .01 -.04 -.2 .06 .05 | --- --- --- esx 52|-.00 -.00 .01 .02 .01 .13 .1 .07 .04 | 180.3 32.3 1.17 iac n/a|-.00 .00 -.10 -.33 .04 -.15 .6 .09 .09 | 245.3 8.8 .78 mcc n/a| .01 -.04 -.00 -.41 -.17 2.26 1.0 .17 .17 | --- --- --- 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 3.1342.0 GPS week: 1342 Day: 0 MJD: 53638 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 |1096 4 5 3 12 --- 3 | 3 3 4 5 --- 3 R02 | 651 4 4 3 13 --- 3 | 3 4 5 6 --- 3 R03 | 355 6 6 4 13 18 4 | 4 5 6 6 6 4 R04 | 483 3 5 5 10 --- 3 | 4 7 3 4 --- 3 R05 | 255 4 4 4 13 --- 3 | 9 7 7 12 --- 7 R06 | 509 22 10 6 16 --- 8 | 8 6 7 8 --- 4 XR07 | 315 --- 7 7 18 15 6 | --- 6 8 6 9 5 R08 |1174 4 4 3 11 --- 3 | 4 6 5 4 --- 4 R17 | 280 6 4 5 16 --- 4 | 7 9 11 7 --- 7 R18 | 693 4 5 4 15 --- 4 | 12 13 11 12 --- 11 R21 | 668 6 4 6 14 --- 4 | 29 31 33 29 --- 31 R22 | 407 3 3 2 12 13 3 | 9 12 19 5 15 10 R23 | 710 3 4 3 14 --- 3 | 7 9 7 8 --- 7 R24 | 580 10 4 8 9 --- 5 | 7 7 9 6 --- 7 ------+------------------------------+-------------------------- RMS | 662 8 5 5 13 16 |T 8 9 10 8 10 8 WRMS | 662 8 5 4 13 16 |NE 8 9 10 8 10 8 MEDI | 509 4 4 4 13 15 |MD 7 7 7 6 9 5 Table 3.1342.1 GPS week: 1342 Day: 1 MJD: 53639 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 |1021 4 6 2 11 --- 3 | 4 4 5 4 --- 3 R02 | 656 4 4 4 12 --- 3 | 4 4 4 8 --- 2 R03 | 195 5 4 8 15 11 4 | 5 4 9 7 4 4 R04 | 476 6 4 4 12 --- 3 | 4 5 6 7 --- 3 R05 | 209 6 4 4 10 --- 3 | 6 7 8 6 --- 6 R06 | 412 19 12 9 12 --- 8 | 7 9 10 7 --- 4 XR07 | 190 --- 4 3 13 18 4 | --- 6 7 5 8 5 R08 | 768 5 4 5 11 --- 3 | 6 6 8 4 --- 5 R17 | 600 5 4 3 13 --- 3 | 7 7 8 6 --- 6 R18 | 314 5 3 5 13 --- 4 | 10 10 9 8 --- 9 R21 | 297 10 8 5 13 --- 5 | 21 27 25 22 --- 24 R22 | 260 3 4 4 11 14 3 | 7 10 18 3 11 8 R23 | 982 3 3 6 14 --- 4 | 5 7 6 5 --- 5 R24 | 602 8 7 12 13 --- 6 | 7 9 8 5 --- 7 ------+------------------------------+-------------------------- RMS | 587 8 6 6 12 13 |T 7 8 9 7 8 7 WRMS | 587 7 6 6 12 13 |NE 7 8 9 7 8 7 MEDI | 412 5 4 4 12 14 |MD 6 7 8 6 8 5 Table 3.1342.2 GPS week: 1342 Day: 2 MJD: 53640 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 800 3 5 3 10 --- 3 | 3 6 6 4 --- 4 R02 | 530 6 4 5 10 --- 3 | 5 6 7 5 --- 4 R03 | 215 4 6 6 8 9 3 | 4 6 8 7 6 3 R04 | 438 3 6 5 8 --- 3 | 3 5 5 6 --- 3 R05 | 230 6 6 3 12 --- 4 | 6 10 7 7 --- 5 R06 | 652 19 9 12 8 --- 8 | 8 6 7 8 --- 5 XR07 | 98 --- 4 4 10 24 4 | --- 8 6 7 16 5 R08 | 398 3 2 2 9 --- 2 | 3 5 5 5 --- 3 R17 | 737 3 4 5 10 --- 3 | 7 8 9 7 --- 7 R18 | 251 5 5 5 8 --- 3 | 10 10 8 8 --- 8 R21 | 304 7 6 6 8 --- 4 | 23 28 27 25 --- 26 R22 | 265 4 5 4 9 17 3 | 8 11 18 4 20 9 R23 | 690 3 3 5 9 --- 3 | 7 9 9 9 --- 8 R24 | 388 3 4 4 10 --- 3 | 4 7 8 6 --- 5 ------+------------------------------+-------------------------- RMS | 495 7 5 6 9 14 |T 7 9 9 8 14 7 WRMS | 495 7 5 5 9 14 |NE 7 9 9 8 14 7 MEDI | 388 4 5 5 9 17 |MD 6 7 7 7 16 5 Table 3.1342.3 GPS week: 1342 Day: 3 MJD: 53641 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 353 3 2 4 7 --- 2 | 3 4 5 6 --- 4 R02 | 272 3 2 4 9 --- 2 | 4 6 7 4 --- 5 R03 | 264 6 3 5 9 6 3 | 5 6 8 5 8 4 R04 | 580 4 3 4 8 --- 3 | 5 3 4 6 --- 3 R05 | 419 4 4 4 11 --- 3 | 6 9 7 8 --- 6 R06 | 902 23 8 12 12 --- 8 | 10 10 6 10 --- 5 XR07 | 160 --- 6 4 15 11 5 | --- 10 8 5 4 7 R08 | 303 6 2 5 7 --- 3 | 6 4 7 6 --- 4 R17 | 685 4 3 4 9 --- 3 | 11 10 10 13 --- 10 R18 | 302 5 5 6 11 --- 4 | 11 9 9 7 --- 8 R21 | 369 6 5 3 10 --- 3 | 19 14 17 14 --- 15 R22 | 269 4 3 2 10 23 3 | 10 16 33 4 15 12 R23 | 424 4 3 5 9 --- 3 | 9 12 9 10 --- 9 R24 | 297 5 3 5 9 --- 3 | 10 14 11 10 --- 11 ------+------------------------------+-------------------------- RMS | 458 8 4 5 9 17 |T 8 9 10 8 9 7 WRMS | 458 6 4 5 9 17 |NE 8 9 10 8 9 7 MEDI | 303 4 3 4 9 11 |MD 9 9 8 6 8 6 Table 3.1342.4 GPS week: 1342 Day: 4 MJD: 53642 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 231 4 6 5 7 --- 3 | 3 5 6 6 --- 4 R02 | 176 2 2 3 10 --- 3 | 5 4 7 7 --- 4 R03 | 253 3 8 7 10 7 4 | 5 7 8 6 3 3 R04 | 617 3 6 4 9 --- 3 | 3 5 6 6 --- 3 R05 | 673 4 5 2 8 --- 3 | 4 8 6 5 --- 5 R06 | 310 16 15 20 16 --- 10 | 8 22 7 6 --- 7 XR07 | 217 --- 16 9 18 11 10 | --- 18 8 11 4 8 R08 | 365 5 3 5 9 --- 3 | 5 6 6 5 --- 4 R17 | 523 5 3 3 8 --- 3 | 7 10 11 8 --- 8 R18 | 433 8 10 4 14 --- 5 | 11 11 9 9 --- 8 R21 | 582 3 4 4 10 --- 3 | 16 18 20 16 --- 18 R22 | 719 15 18 75 10 24 11 | 10 27 65 4 14 15 R23 | 553 6 8 3 10 --- 4 | 7 12 9 14 --- 9 R24 | 173 7 11 7 10 --- 5 | 8 15 12 8 --- 10 ------+------------------------------+-------------------------- RMS | 469 8 9 22 10 17 |T 7 12 13 8 7 8 WRMS | 469 6 8 7 10 17 |NE 7 12 13 8 7 8 MEDI | 365 5 6 4 10 11 |MD 7 10 8 6 4 7 Table 3.1342.5 GPS week: 1342 Day: 5 MJD: 53643 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 278 3 2 4 8 --- 2 | 3 4 5 4 --- 4 R02 | 390 3 4 7 8 --- 3 | 5 4 5 6 --- 3 R03 | 462 5 4 4 8 13 3 | 4 8 6 4 5 5 R04 | 445 4 3 4 10 --- 3 | 5 5 6 5 --- 3 R05 | 777 4 4 7 13 --- 4 | 7 8 9 9 --- 7 R06 | 291 20 9 15 19 --- 9 | 8 10 9 13 --- 4 XR07 | 205 --- 7 7 13 10 6 | --- 10 6 8 3 5 R08 | 651 4 4 6 13 --- 4 | 6 5 8 5 --- 4 R17 | 686 7 6 13 8 --- 5 | 13 12 14 12 --- 12 R18 | 378 9 6 7 11 --- 4 | 10 9 9 8 --- 7 R21 | 793 4 3 5 9 --- 3 | 24 22 26 23 --- 24 XR22 |---- 22 17 --- --- 25 19 | 13 29 --- --- 9 20 R23 | 963 4 8 4 12 --- 4 | 10 13 10 8 --- 11 R24 | 207 5 9 6 12 --- 5 | 14 14 11 8 --- 12 ------+------------------------------+-------------------------- RMS | 575 8 6 8 11 13 |T 9 11 10 9 6 9 WRMS | 575 6 5 6 11 13 |NE 9 11 10 9 6 9 MEDI | 445 4 4 6 11 13 |MD 8 9 9 8 5 5 Table 3.1342.6 GPS week: 1342 Day: 6 MJD: 53644 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL ------+------------------------------+-------------------------- R01 | 605 3 4 3 9 --- 3 | 3 5 5 5 --- 3 R02 | 244 3 3 3 11 --- 3 | 5 6 7 10 --- 5 R03 | 769 5 4 5 7 17 3 | 4 5 8 5 5 4 R04 | 288 3 3 3 6 --- 2 | 5 5 7 5 --- 5 R05 | 682 4 3 5 6 --- 3 | 7 8 7 5 --- 6 R06 | 410 23 8 12 10 --- 8 | 11 8 8 6 --- 4 XR07 | 207 --- 4 3 8 7 3 | --- 7 6 5 3 5 R08 | 753 4 5 3 12 --- 3 | 4 5 3 5 --- 3 R17 | 832 10 10 17 12 --- 7 | 16 14 16 14 --- 13 R18 | 351 8 8 5 7 --- 4 | 12 12 10 8 --- 9 R21 | 843 7 3 2 10 --- 3 | 27 27 30 28 --- 28 XR22 |1390 7 9 9 --- 18 6 | 12 14 24 --- 14 13 R23 |1251 3 5 3 8 --- 3 | 10 10 8 9 --- 9 R24 | 347 3 5 3 11 --- 3 | 12 12 13 9 --- 11 ------+------------------------------+-------------------------- RMS | 678 8 6 7 9 17 |T 10 10 11 9 7 8 WRMS | 678 6 5 4 9 17 |NE 10 10 11 9 7 8 MEDI | 605 4 4 3 9 17 |MD 10 8 8 6 5 5