From igsacc at gfz-potsdam.de Fri Aug 26 01:19:24 2005 From: igsacc at gfz-potsdam.de (Gerd Gendt3) Date: Fri, 26 Aug 2005 10:19:24 +0200 Subject: [IGSREPORT-12893] Wk 1335 IGLOS Final Orbits Message-ID: <430ED08C.mailx2AF1XXBTJ@kg20> ****************************************************************************** IGS Electronic Report 26 Aug 01:19:48 PDT 2005 Message Number 12893 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam IGLOS Orbit Combination - Week 1335 (Aug 07, 2005 - Aug 13, 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 2.1335. 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: igl1335[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6 of GPS Week 1335 in the SP3 format. igl13357.sum Combination Report for GPS Week 1335. 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 | 245.5 ns 1 | 236.5 ns 2 | 218.6 ns 3 | 234.8 ns 4 | 230.9 ns 5 | 217.8 ns 6 | 227.7 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 ----+--------+--------------- 0 | ALL | R02 0 | ESX | R17 R06 1 | BKG | R06 1 | ESX | R17 2 | ESX | R17 3 | ESX | R17 4 | ESX | R17 5 | ESX | R17 6 | ESX | R17 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 1.1335, 1a.1335). 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 2.1335.0-6) 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 3.1335.0-6). 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 1335 summary. (Aug 07, 2005 - Aug 13, 2005) Table 1.1335.a GPS week : 1335 MJD: 53589.0-53595.0 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 44|-.00 .00 .00 -.09 -.01 .23 -.2 .10 .09 | .0 -.3 4.65 | .01 .00 .00 .11 .07 .35 .3 | .0 .4 cod 173| .00 -.00 .01 .00 -.03 -.13 -.1 .04 .03 | --- --- --- | .00 .00 .00 .06 .04 .11 .1 | --- --- esx 53|-.00 .00 -.02 .06 .02 .13 .3 .45 .06 | 887.1 7.9 14.87 | .01 .01 .01 .08 .11 .09 .2 | 35.3 10.8 mcc n/a|-.02 .01 -.02 -.42 -.07 1.87 .7 .23 .23 | --- --- --- | .01 .02 .03 .31 .20 1.12 .4 | --- --- Table 1.1335.b GPS week : 1335 MJD: 53589.0-53595.0 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 ------+-----------------------------+------------------------------------------ R01E | 3 4 2 4 5 4 5 | R02E | --- 5 2 2 4 4 5 | R03E | 3 3 6 5 4 5 8 | R04E | 3 3 3 2 2 3 7 | R06E | --- 6 9 9 10 8 7 | R07E | 3 5 8 5 5 6 7 | R08E | 2 4 4 3 10 10 9 | R17 | 10 7 4 5 3 5 5 | R18 | 3 2 4 3 5 3 3 | R21 | 4 3 3 3 5 3 3 | R22 | 3 2 4 5 4 3 3 | R23 | 2 3 2 2 4 3 3 | R24 | 3 2 4 3 3 4 4 | Table 1.1335.c GPS week : 1335 MJD: 53589.0-53595.0 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 1335 0 | -.11 -.13 .64 41.99 -19.50 -402.00 73.5 7.86 7.86 | 245.5 .0 .0 brd 1335 1 | .15 -.44 .24 40.72 -20.40 -389.20 76.4 7.35 7.35 | 236.6 .0 .0 brd 1335 2 | .12 .03 .29 34.31 -30.83 -366.00 92.2 6.03 6.03 | 218.6 .0 .0 brd 1335 3 | .11 .14 -.37 42.22 -23.11 -350.40 90.3 5.02 5.02 | 234.8 .0 .0 brd 1335 4 | -.12 -.29 -.14 41.19 -25.81 -344.40 88.6 4.13 4.13 | 230.9 .0 .0 brd 1335 5 | -.10 .18 -.17 32.83 -21.89 -351.30 90.4 4.38 4.38 | 217.8 .0 .0 brd 1335 6 | -.10 -.19 -.45 35.73 -22.43 -361.00 82.5 4.83 4.83 | 227.7 .0 .0 -------------+-------------------------------------------------------------+--------------------- brd 1335 mean| -.01 -.10 .01 38.43 -23.42 -366.33 84.8 5.66 5.66 | 230.3 .0 .0 brd 1335 sdev| .13 .23 .39 3.99 3.84 21.54 7.5 1.47 1.47 | 9.9 .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 2.1335.0 GPS week: 1335 Day: 0 MJD: 53589 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 44| .00 -.00 -.00 .05 .06 .00 .3 .05 .05 | .0 .0 3.07 cod 173|-.00 -.01 .01 -.04 -.05 .00 -.2 .04 .03 | --- --- --- esx 53| .00 .01 -.02 -.02 -.04 .11 .1 .46 .05 | 849.7 6.1 11.94 mcc n/a|-.01 .05 -.04 .10 .11 1.94 .7 .32 .32 | --- --- --- Table 2.1335.1 GPS week: 1335 Day: 1 MJD: 53590 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 44| .00 .01 .00 -.01 -.02 -.10 -.2 .11 .08 | .0 -.7 5.41 cod 173| .00 -.00 -.00 -.00 .00 .04 -.1 .04 .03 | --- --- --- esx 53|-.02 .01 -.02 .04 .07 .14 .4 .54 .07 | 846.3 17.6 13.76 mcc n/a|-.02 -.02 -.05 -.62 .03 2.55 .8 .20 .20 | --- --- --- Table 2.1335.2 GPS week: 1335 Day: 2 MJD: 53591 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 44|-.01 .01 .00 -.09 -.04 .06 .1 .08 .09 | -.0 .4 3.95 cod 173| .00 -.00 .00 .00 -.08 -.15 -.1 .04 .04 | --- --- --- esx 53|-.01 .00 -.01 .02 .18 .13 .3 .44 .07 | 860.6 17.4 12.24 mcc n/a|-.01 -.01 .00 -.41 -.12 2.90 1.3 .16 .16 | --- --- --- Table 2.1335.3 GPS week: 1335 Day: 3 MJD: 53592 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 44|-.02 .01 .01 -.22 -.03 .01 -.3 .09 .08 | .0 -.8 5.33 cod 173| .00 -.00 .01 .10 .02 -.17 -.2 .04 .04 | --- --- --- esx 53| .00 -.00 -.01 -.04 -.10 .27 .4 .94 .06 | 900.1 3.1 10.53 mcc n/a|-.01 .01 .03 -.92 .22 3.13 .5 .20 .20 | --- --- --- Table 2.1335.4 GPS week: 1335 Day: 4 MJD: 53593 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 44|-.00 -.00 .01 -.09 .05 .24 -.2 .09 .09 | .0 -.0 3.68 cod 173| .01 -.00 .01 -.09 .03 -.20 -.2 .05 .04 | --- --- --- esx 53|-.00 -.00 -.02 .15 -.04 .13 .5 .31 .07 | 895.7 20.3 11.88 mcc n/a|-.01 .02 -.03 -.34 -.16 .87 .1 .14 .14 | --- --- --- Table 2.1335.5 GPS week: 1335 Day: 5 MJD: 53594 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 44|-.01 -.00 -.01 -.24 -.15 .91 -.4 .13 .12 | .0 -.3 5.60 cod 173| .01 -.00 .01 .03 -.06 -.25 .0 .04 .03 | --- --- --- esx 53|-.00 .00 -.01 .10 .13 -.02 .1 .18 .05 | 931.6 -8.6 22.97 mcc n/a|-.03 .01 -.04 -.39 -.36 .03 .7 .21 .21 | --- --- --- Table 2.1335.6 GPS week: 1335 Day: 6 MJD: 53595 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------+------------------------------------------------+--------------------- bkg 44| .01 -.00 .00 -.04 .04 .45 -.5 .14 .12 | .0 -.5 5.53 cod 173|-.00 -.00 .01 .00 -.04 -.15 -.1 .04 .03 | --- --- --- esx 53|-.01 .01 -.03 .15 -.06 .14 .4 .28 .08 | 925.6 -.4 20.79 mcc n/a|-.03 .01 -.04 -.39 -.19 1.70 .5 .36 .36 | --- --- --- 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 3.1335.0 GPS week: 1335 Day: 0 MJD: 53589 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL ------+--------------------------+---------------------- R01E |1121 4 2 5 --- 3 | 12 10 12 --- 11 R03E | 473 4 3 6 11 3 | 5 6 7 2 6 R04E | 367 5 4 5 --- 3 | 5 4 6 --- 4 XR07E |1252 --- 3 4 --- 3 | --- 5 5 --- 5 R08E |1260 2 2 3 --- 2 | 8 6 7 --- 6 R17 | 245 11 9 145 --- 10 | 6 13 99 --- 7 R18 |1045 5 4 3 --- 3 | 29 30 29 --- 29 R21 | 794 6 3 7 --- 4 | 6 8 9 --- 6 R22 | 530 4 3 5 47 3 | 8 8 5 13 7 R23 | 924 3 3 4 --- 2 | 5 8 6 --- 5 R24 | 222 2 4 6 27 3 | 5 6 6 13 4 ------+--------------------------+---------------------- RMS | 785 5 4 46 32 |T 9 9 24 9 8 WRMS | 785 5 3 5 32 |NE 10 12 26 13 10 MEDI | 794 4 3 5 27 |MD 6 8 7 13 6 Table 3.1335.1 GPS week: 1335 Day: 1 MJD: 53590 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL ------+--------------------------+---------------------- R01E | 988 7 3 7 --- 4 | 6 8 13 --- 8 R02E | 721 6 6 8 --- 5 | 4 5 61 --- 4 R03E | 539 5 4 5 11 3 | 7 9 9 2 6 R04E | 456 3 2 6 --- 3 | 4 4 7 --- 4 R06E | 843 36 4 8 --- 6 | 12 6 35 --- 7 XR07E | 781 --- 4 8 --- 5 | --- 6 8 --- 6 R08E |1050 5 3 10 --- 4 | 6 8 6 --- 7 R17 | 261 9 6 187 --- 7 | 4 13 99 --- 7 R18 |1066 3 2 4 --- 2 | 23 24 23 --- 23 R21 | 607 3 3 8 --- 3 | 4 2 10 --- 4 R22 | 353 4 3 4 29 2 | 5 6 6 12 5 R23 | 954 4 3 7 --- 3 | 4 7 11 --- 6 R24 | 271 2 3 4 17 2 | 5 7 7 7 6 ------+--------------------------+---------------------- RMS | 735 11 4 54 20 |T 7 8 23 7 7 WRMS | 735 8 3 7 20 |NE 8 10 26 10 9 MEDI | 721 4 3 7 17 |MD 5 7 10 7 6 Table 3.1335.2 GPS week: 1335 Day: 2 MJD: 53591 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL ------+--------------------------+---------------------- R01E | 786 4 2 3 --- 2 | 9 7 8 --- 7 R02E | 567 4 2 3 --- 2 | 4 6 30 --- 5 R03E | 427 15 6 5 13 6 | 8 7 5 2 5 R04E | 699 4 3 5 --- 3 | 5 9 12 --- 8 R06E | 298 20 8 11 --- 9 | 8 6 14 --- 6 XR07E | 458 --- 6 10 --- 8 | --- 9 8 --- 7 R08E | 747 8 2 7 --- 4 | 7 7 8 --- 6 R17 | 266 5 3 152 --- 4 | 11 10 99 --- 10 R18 | 890 6 3 8 --- 4 | 24 23 23 --- 23 R21 | 410 5 3 3 --- 3 | 7 11 10 --- 9 R22 | 300 4 4 8 18 4 | 8 9 8 15 7 R23 | 871 2 2 4 --- 2 | 4 6 7 --- 5 R24 | 474 5 5 5 16 4 | 3 11 6 9 6 ------+--------------------------+---------------------- RMS | 603 8 4 44 16 |T 8 9 18 9 8 WRMS | 603 9 4 7 16 |NE 10 12 26 12 10 MEDI | 474 5 3 5 16 |MD 7 9 8 9 7 Table 3.1335.3 GPS week: 1335 Day: 3 MJD: 53592 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL ------+--------------------------+---------------------- R01E | 796 9 3 4 --- 4 | 7 9 10 --- 8 R02E | 526 5 2 3 --- 2 | 6 10 23 --- 8 R03E | 447 12 4 4 12 5 | 7 7 6 4 5 R04E | 723 2 2 3 --- 2 | 5 5 6 --- 5 R06E | 522 24 6 9 --- 9 | 11 5 13 --- 5 XR07E | 304 --- 4 6 --- 5 | --- 6 5 --- 5 R08E | 560 5 2 6 --- 3 | 8 8 9 --- 7 R17 | 177 7 4 324 --- 5 | 8 5 99 --- 5 R18 | 463 7 2 3 --- 3 | 24 24 24 --- 23 R21 | 344 5 4 5 --- 3 | 9 12 5 --- 9 R22 | 196 3 5 9 25 5 | 9 12 8 19 9 R23 | 623 3 2 5 --- 2 | 7 8 6 --- 6 R24 | 117 5 2 6 22 3 | 6 8 6 19 6 ------+--------------------------+---------------------- RMS | 502 9 4 94 20 |T 9 9 17 14 8 WRMS | 502 8 4 6 20 |NE 11 12 25 19 10 MEDI | 463 5 3 5 22 |MD 7 8 8 19 6 Table 3.1335.4 GPS week: 1335 Day: 4 MJD: 53593 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL ------+--------------------------+---------------------- R01E | 636 10 5 5 --- 5 | 8 12 13 --- 11 R02E | 399 7 5 3 --- 4 | 5 7 24 --- 6 R03E | 264 5 4 7 10 4 | 8 4 9 4 5 R04E | 674 4 1 3 --- 2 | 4 3 6 --- 3 R06E | 529 19 10 15 --- 10 | 5 10 14 --- 7 XR07E | 417 --- 3 7 --- 5 | --- 5 8 --- 5 R08E | 293 18 4 23 --- 10 | 6 6 11 --- 6 R17 | 169 3 2 102 --- 3 | 6 9 99 --- 8 R18 | 221 6 4 11 --- 5 | 24 24 25 --- 24 R21 | 558 9 3 8 --- 5 | 3 9 8 --- 6 R22 | 199 2 4 9 21 4 | 10 9 8 24 8 R23 | 336 5 5 7 --- 4 | 6 13 9 --- 10 R24 | 222 5 3 7 8 3 | 5 6 9 12 6 ------+--------------------------+---------------------- RMS | 413 9 5 31 14 |T 8 9 19 13 8 WRMS | 413 9 4 7 14 |NE 9 12 26 18 10 MEDI | 336 5 4 7 10 |MD 6 9 9 12 6 Table 3.1335.5 GPS week: 1335 Day: 5 MJD: 53594 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL ------+--------------------------+---------------------- R01E | 708 9 3 6 --- 4 | 10 6 8 --- 6 R02E | 196 10 5 3 --- 4 | 6 9 22 --- 7 R03E | 272 13 5 4 16 5 | 12 5 7 2 5 R04E | 859 8 2 3 --- 3 | 8 6 7 --- 4 R06E | 211 21 6 8 --- 8 | 6 6 9 --- 4 XR07E | 259 --- 5 7 --- 6 | --- 4 8 --- 5 R08E | 579 28 5 11 --- 10 | 9 13 21 --- 14 R17 | 158 8 3 61 --- 5 | 7 11 65 --- 10 R18 | 306 6 3 4 --- 3 | 26 23 23 --- 24 R21 | 519 9 3 4 --- 3 | 6 5 6 --- 4 R22 | 261 7 3 4 13 3 | 5 6 5 13 4 R23 | 304 5 4 4 --- 3 | 3 9 6 --- 6 R24 | 161 10 3 3 29 4 | 4 11 10 8 9 ------+--------------------------+---------------------- RMS | 438 13 4 18 21 |T 9 9 15 8 8 WRMS | 438 12 3 5 21 |NE 9 11 19 11 10 MEDI | 272 9 3 4 16 |MD 6 6 8 8 6 Table 3.1335.6 GPS week: 1335 Day: 6 MJD: 53595 Weighted Average Orbit Dynamics (7 days) PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL ------+--------------------------+---------------------- R01E | 827 15 2 8 --- 5 | 8 9 8 --- 8 R02E | 181 14 5 6 --- 5 | 6 8 31 --- 6 R03E | 154 18 4 15 11 8 | 10 4 10 2 5 R04E | 771 16 4 12 --- 7 | 9 3 11 --- 4 R06E | 240 21 4 10 --- 7 | 9 4 13 --- 4 XR07E | 154 --- 4 11 --- 7 | --- 9 5 --- 7 R08E | 552 21 6 17 --- 9 | 10 9 18 --- 9 R17 | 181 9 2 93 --- 5 | 5 12 86 --- 10 R18 | 269 5 3 7 --- 3 | 30 30 27 --- 29 R21 | 673 8 3 5 --- 3 | 5 10 11 --- 8 R22 | 480 4 3 6 32 3 | 5 6 7 15 5 R23 | 537 6 3 6 --- 3 | 5 10 7 --- 8 R24 | 172 10 2 5 54 4 | 4 10 10 12 9 ------+--------------------------+---------------------- RMS | 483 14 4 28 36 |T 9 10 19 10 9 WRMS | 483 12 3 8 36 |NE 9 13 25 14 12 MEDI | 269 10 3 8 32 |MD 6 9 11 12 8