Date: Thu, 24 Apr 2008 12:07:55 +0000 From: Jim Ray Subject: [IGSREPORT-16170] Wk 1474 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4810781b.3vPsPhQJUS4ZBFZl%igs.acc@noaa.gov> Content-type: text/plain; charset=us-ascii Content-transfer-encoding: 7bit User-Agent: nail 11.25 7/29/05 Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 24 Apr 05:08:05 PDT 2008 Message Number 16170 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1474 (Apr 06, 2008 - Apr 12, 2008) Contacts: J. Ray (jim.ray@noaa.gov), J. Griffiths (jake.griffiths@noaa.gov) COMBINATION STRATEGY: --------------------- Starting with GPS week 860, the IGS Final orbit combination is done directly in the ITRF without any alignment to the Bulletin B EOP series. Each centre satellite clock corrections are first transformed to a common reference. One of the following two methods can be used (the REMARKS section of this report gives which method is used): [1] For each centre, a clock offset and a drift are estimated with respect to the broadcast clock corrections using only non-SA satellites; [2] A chosen reference centre is aligned to the broadcast clock corrections using all satellites. All other centres are then aligned to that reference centre. The offsets and drifts are used to align each centre satellite clock corrections to GPS time. Ephemerides and clock corrections are then combined as weighted averages computed over all centres. Each centre is given a position weight and a clock weight. The position weights are computed from each centre's absolute deviation to the unweighted average orbit after the estimation of a 7-parameter Helmert transformation. The clock weights are either computed from [1] the absolute deviation of the initial alignment to broadcast clock for the non-SA satellites, or [2] from the absolute deviation of centre's aligned clock corrections with respect to the unweighted mean. Finally, a 7-parameter Helmert transformation and clock offset and drift are estimated for each centre with respect to the combined solutions and parameters and RMS of fit reported. All the above estimations are performed using the L1-norm robust scheme. Each centre ephemerides are also evaluated individually and independently from the orbit combination by using week long arcs. The Earth Orientation Parameters (EOP) used in this evaluation are those submitted by the respective centres. The IGS combined orbits/clocks and all centres providing both orbit and clock solutions are further evaluated by an independent point positioning (navigation) program that uses both phase and pseudorange data. This is primarily intended for testing clock solution precision as well as the orbit/clock consistency. Like the clock solutions broadcast in the navigation message, the combined satellite clocks are corrected for the periodical relativistic correction (see e.g. GPS interface Control document ICD-GPS-200, p.73): -2*(X.V)/c [distance unit], where X and V are the inertial sv state and velocity vectors and c is the speed of light. Also for compatibility, no satellite L1/L2 delay calibration should be applied. 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. PRODUCTS GENERATED: ------------------- The resulting average ephemeris and clocks are output to daily files in SP3 format. The satellite accuracy codes displayed in the header are based on the weighted RMS for each satellite. Note that each file contains all the satellites that appear in any of the centre ephemeris files. If a satellite or centre was excluded from combination, a note in the REMARKS section of this report will identify the exclusion and the reason. The resulting x and y earth rotation parameters (ERP) associated with the IGS ephemeris files and their rates (xrt, yrt) are computed using a weighted average of all available centres (weights are those from the orbit combination). Pole rate combination uses only centres providing estimated pole rates. Starting with GPS wk 0894, IGS LOD combinations were implemented in the Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to the last non-predicted day of Bulletin A. AC LOD biases are removed and the new AC bias-free LODs are used to compute a weighted IGS LOD which in turn is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC values are printed in the IGS Final erp file. The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are: igs1474[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1474[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1474[0-6].cls IGS GPS clock combination summary report. igs14747.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14747.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Day | Centre | PRN/STA list ----+--------+--------------- 0 | ALL | 7 0 | COD | 26 0 | EMR | SFER YELL 0 | ESA | 1 26 KELY 0 | GFZ | 26 29 0 | JPL | 32 0 | MIT | 1 CAS1 MAW1 1 | COD | 26 SYOG 1 | EMR | DAEJ NYAL SFER 1 | ESA | 1 DAEJ KOUR NRIL SYOG 1 | GFZ | 7 29 BJFS KOUR NRIL 1 | JPL | 26 32 1 | MIT | 1 7 DAEJ DARW 2 | ALL | 7 2 | COD | 26 2 | EMR | WTZR 2 | ESA | 26 ONSA 2 | GFZ | 13 29 COCO NKLG YELL 2 | JPL | 32 SANT 2 | MIT | 32 DARW MAR6 3 | COD | 26 YELL 3 | EMR | SFER USUD 3 | ESA | 26 3 | GFZ | 1 7 29 3 | JPL | 32 3 | MIT | 7 YELL 4 | ALL | 1 4 | EMR | HARB NLIB 4 | ESA | NRC1 4 | GFZ | 7 26 29 CEDU NKLG NRC1 4 | JPL | 26 32 CEDU HARB 4 | MIT | 7 11 19 26 IENG NRC1 5 | COD | DRAO 5 | EMR | SFER TWTF 5 | GFZ | 7 10 26 29 LHAZ NLIB 5 | JPL | 32 5 | MIT | 1 7 15 19 26 6 | EMR | 17 SFER YELL 6 | ESA | RAMO 6 | GFZ | 7 29 6 | JPL | 32 6 | MIT | 1 3 7 YELL 5. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGs05). For more information see IGSMAIL #5447. 6. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .2 .3 .2 -5 -1 -7 -.06 EMR | 3.4 -6.1 -.8 33 15 -24 .21 ESA | .5 -.5 6.0 20 16 14 .09 GFZ | .6 .3 .6 14 -12 1 -.15 JPL | 6.7 -2.8 1.5 -7 4 -11 .20 MIT | 7.2 -10.9 2.8 1 13 5 .05 NGS | 7.1 -2.8 1.2 -30 -101 22 -.93 SIO | 4.0 -4.5 11.7 -89 -139 35 .43 7. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 8. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 9. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five parts. The first, 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 (table 1.1474.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1474.b). The second part, 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 2.1474.[0-6]). The third part, 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 3.1474.[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. The fourth part, Table 4, is a weekly summary of the daily precise navigation summaries for centres providing both orbit and clock solutions. It contains weekly station RMS w.r.t. the initial coordinates for the Latitude, Longitude and Height components for up to three IGS stations (table 4.1307). The fifth and final part, Table 5, is similar to Table 4 and contains daily precise navigation statistics (tables 5.1474.0-6). In tables 1-3, the most important statistic which is meaningful for intra centre/satellite analysis is labeled WRMS. It is a weighted RMS where normalized weights are based on accuracy codes given in the SP3 files, and should not be affected by downweighted/problem satellites when acknowledged by individual centres in their SP3 file. Table 1: Week 1474 summary. (Apr 06, 2008 - Apr 12, 2008) Table 1.1474.a GPS week: 1474 MJD: 54562.000-54568.000 Mean and standard deviations of transformation parameters to the combined IGS 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] --------+----------------------------------------------------+------------------------------ cod 178| 0 -1 0 0 -12 4 -.21 10 9 | -185 -584 16 76 | 0 0 0 17 18 16 .04 | 351 464 emr 71| 0 0 3 -84 -98 -19 .47 18 18 | 731175 -1157 23 98 | 0 2 0 42 31 20 .02 | 1928198 1325 esa 111| 0 0 0 -55 -84 -7 .27 13 12 | -8894 -135 20 104 | 3 1 3 56 70 26 .09 | 821 1195 gfz 184| 0 0 0 -13 -4 -32 -.19 15 15 | 305 -386 23 123 | 0 0 1 14 21 53 .05 | 288 527 igr n/a| 0 0 -1 2 -37 -2 -.02 6 6 | 30231 -339 22 66 | 0 1 0 11 10 19 .07 | 1387 1381 jpl 118| 0 1 3 -17 -9 23 .52 19 19 | 3350 -724 17 80 | 1 1 1 35 17 11 .03 | 847 1365 mit 308| 0 -1 -4 6 -58 -8 -.25 14 12 | 210 -263 25 143 | 0 1 0 29 33 20 .03 | 166 590 ngs 220| -1 1 -1 65 141 20 -.30 13 12 | -231 -773 2447 4329 | 0 1 0 49 47 30 .02 | 377 456 sio 113| 0 0 0 177 218 24 .12 21 21 | --- --- --- --- | 1 1 1 13 29 25 .03 | --- --- Table 1.1474.b GPS week : 1474 MJD: 54562.000-54568.000 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 ------+------------------------------------+------------------------------------------ 1 | 8 10 9 8 11 11 10 | 2 | 6 6 5 5 6 6 6 | 3 | 5 5 5 5 5 5 5 | 4 | 5 5 5 5 4 5 4 | 5 | 4 5 5 4 4 5 4 | 6 | 5 5 5 5 5 5 5 | 7 | 8 8 8 8 7 7 7 | 8 | 5 4 4 4 4 4 4 | 9 | 5 5 4 5 4 5 5 | 10 | 4 5 4 4 4 4 4 | 11 | 6 7 9 8 6 6 7 | 12 | 5 5 5 5 5 5 5 | 13 | 5 5 6 6 5 5 6 | 14 | 5 6 6 5 6 6 6 | 15 | 7 6 7 7 6 6 6 | 16 | 5 6 6 6 6 6 6 | 17 | 6 6 5 5 5 6 6 | 18 | 6 6 7 6 7 7 6 | 19 | 6 6 6 6 6 6 6 | 20 | 6 7 7 7 7 7 7 | 21 | 6 6 6 6 5 6 5 | 22 | 6 6 6 6 6 6 6 | 23 | 6 6 7 7 7 6 6 | 24 | 5 5 5 5 5 5 5 | 25 | 5 5 5 5 5 5 5 | 26 | 6 5 6 6 6 7 6 | 27 | 5 4 4 4 4 4 4 | 28 | 6 6 6 6 5 5 6 | 29 | 5 6 6 6 6 5 6 | 30 | 4 4 5 4 4 4 4 | 31 | 6 6 7 6 6 6 6 | 32 | 9 9 10 10 9 10 9 | Table 2: Daily transformation of each centre to the combined IGS 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 2.1474.0 GPS week: 1474 Day: 0 MJD: 54562.000 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] --------+----------------------------------------------------+------------------------------ cod 178| 1 0 1 30 -41 1 -.22 9 9 | -408 -653 15 68 | 10 12 | emr 71| 0 2 2 -103 -38 -25 .49 20 20 | 3132 -3199 17 85 | 22 -23 | esa 111| -4 -1 -6 -56 -173 18 .42 13 13 | -9598 1277 19 98 | 39 50 | gfz 184| 1 0 2 -23 -45 -135 -.20 15 15 | 190 -539 25 126 | -2 45 | igr n/a| -1 0 -1 -3 -25 8 .07 6 6 | 29303 -2412 20 61 | -16 3 | jpl 118| 1 -1 4 -29 -4 19 .49 20 20 | 3657 -2807 17 74 | 83 -23 | mit 308| 0 0 -3 12 -65 3 -.21 14 12 | 489 -1297 26 188 | -1 18 | ngs 220| -1 0 0 38 200 70 -.30 12 11 | -527 -552 2672 4322 | 24 40 | sio 113| 0 -1 1 185 275 58 .11 20 19 | --- --- --- --- | -124 -191 | Table 2.1474.1 GPS week: 1474 Day: 1 MJD: 54563.000 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] --------+----------------------------------------------------+------------------------------ cod 178| 0 0 0 5 -20 -7 -.25 9 9 | -159 -502 15 79 | 39 16 | emr 71| -1 -1 4 -145 -90 -24 .47 19 19 | 1829 -56 21 111 | 30 15 | esa 111| -1 -1 -3 60 -155 30 .36 13 13 | -7903 -447 20 116 | 1 13 | gfz 184| 1 0 0 4 2 -79 -.20 16 16 | -46 430 23 127 | -32 21 | igr n/a| -1 1 -1 -15 -31 23 .04 6 6 | 28840 557 20 67 | -2 -41 | jpl 118| 1 0 4 -79 5 40 .52 19 19 | 2745 0 15 75 | 108 -54 | mit 308| 0 0 -2 52 -4 -37 -.25 15 12 | 8 400 21 153 | 1 -24 | ngs 220| -1 0 -2 -17 163 49 -.29 13 12 | -140 -571 2259 4115 | 24 -1 | sio 113| 0 0 0 160 198 54 .15 21 21 | --- --- --- --- | -63 -121 | Table 2.1474.2 GPS week: 1474 Day: 2 MJD: 54564.000 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] --------+----------------------------------------------------+------------------------------ cod 178| 0 -1 0 -2 20 25 -.26 11 10 | 27 -599 15 61 | 51 -32 | emr 71| -1 -3 3 -129 -111 -29 .47 18 18 | 1488 -236 18 74 | 25 81 | esa 111| 0 1 0 -28 -130 -1 .21 14 13 | -10083 1677 18 100 | 26 -1 | gfz 184| 1 0 1 9 -3 0 -.17 16 16 | 625 -1079 21 123 | -36 -11 | igr n/a| 0 1 0 -5 -32 -5 .02 7 7 | 29036 -54 23 64 | -43 45 | jpl 118| 0 1 4 -38 12 29 .52 19 19 | 2387 -570 16 71 | 71 -33 | mit 308| 1 -1 -4 41 -106 -29 -.25 14 13 | 348 -368 24 104 | -6 43 | ngs 220| -1 3 -1 31 203 -7 -.27 14 12 | -180 -1072 2440 3947 | -17 -28 | sio 113| 0 0 -1 169 195 -8 .16 21 22 | --- --- --- --- | -40 -136 | Table 2.1474.3 GPS week: 1474 Day: 3 MJD: 54565.000 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] --------+----------------------------------------------------+------------------------------ cod 178| 0 -1 0 0 -5 2 -.21 11 9 | -160 -195 17 91 | 73 -6 | emr 71| -1 -2 4 -55 -132 -17 .49 17 17 | 1928 514 18 111 | -37 49 | esa 111| 1 2 0 -96 -6 -35 .25 13 13 | -8881 -1365 19 105 | 21 -17 | gfz 184| 0 0 0 -18 21 1 -.27 16 16 | 437 -783 23 120 | -23 -32 | igr n/a| 0 1 0 8 -55 5 -.02 6 6 | 29529 960 23 72 | 4 29 | jpl 118| 0 1 3 -13 -30 5 .58 20 20 | 2477 458 17 82 | 42 -7 | mit 308| 0 0 -4 -18 -37 17 -.26 12 11 | 209 -451 24 144 | 19 -29 | ngs 220| -2 0 -1 111 109 19 -.32 15 14 | -178 -252 2154 3942 | -74 117 | sio 113| 0 1 0 174 191 -3 .12 20 20 | --- --- --- --- | -58 -108 | Table 2.1474.4 GPS week: 1474 Day: 4 MJD: 54566.000 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] --------+----------------------------------------------------+------------------------------ cod 178| 0 -1 0 -13 -11 29 -.16 10 9 | -686 -200 12 78 | 19 -2 | emr 71| 0 0 3 -32 -124 0 .48 17 17 | 3405 -2095 21 99 | -96 66 | esa 111| 3 1 2 -90 -27 -38 .22 13 13 | -8351 -1112 21 103 | 36 13 | gfz 184| 0 0 1 -23 -2 1 -.22 15 15 | 49 -125 22 120 | -32 16 | igr n/a| 0 0 -2 1 -48 1 -.00 6 6 | 31354 -1224 22 73 | -27 21 | jpl 118| 1 2 2 -4 -35 15 .55 20 20 | 3969 -1603 18 87 | -7 -1 | mit 308| 0 -1 -4 -22 -40 -7 -.25 13 12 | 145 -328 22 153 | 27 -42 | ngs 220| -2 0 -1 75 90 -13 -.29 12 10 | -759 -823 2061 4338 | -31 79 | sio 113| -1 2 -2 179 214 27 .13 20 21 | --- --- --- --- | -68 -107 | Table 2.1474.5 GPS week: 1474 Day: 5 MJD: 54567.000 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] --------+----------------------------------------------------+------------------------------ cod 178| 0 -1 0 -24 -14 -10 -.18 11 10 | 425 -1555 17 80 | 50 -37 | emr 71| 0 -1 3 -66 -100 -53 .44 19 19 | 5103919 -1080 19 90 | -38 43 | esa 111| 3 0 0 -94 -88 0 .22 11 11 | -9359 0 23 105 | 41 21 | gfz 184| 0 0 0 -25 9 -11 -.10 14 14 | 177 58 24 122 | -2 9 | igr n/a| 0 0 0 17 -33 -38 -.10 5 5 | 31160 1256 24 67 | -27 2 | jpl 118| 0 4 4 21 -4 25 .50 18 18 | 3548 1091 17 83 | 18 -40 | mit 308| 0 -3 -4 -12 -69 8 -.29 14 13 | 51 465 26 107 | 25 -28 | ngs 220| 0 1 -1 110 120 4 -.33 13 11 | 455 -1629 2435 4323 | -79 -1 | sio 113| -1 0 -1 200 229 18 .10 22 23 | --- --- --- --- | -72 -126 | Table 2.1474.6 GPS week: 1474 Day: 6 MJD: 54568.000 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] --------+----------------------------------------------------+------------------------------ cod 178| 0 -1 0 5 -14 -7 -.18 10 9 | -338 -385 23 80 | 48 -14 | emr 71| 0 1 2 -59 -87 11 .46 17 17 | 2529 -1948 47 121 | -41 13 | esa 111| 4 0 0 -83 -13 -24 .21 10 10 | -8088 -977 21 102 | 9 -21 | gfz 184| 0 0 0 -17 -16 -4 -.16 15 15 | 708 -668 26 124 | -14 32 | igr n/a| 0 -1 -2 11 -34 -13 -.13 6 6 | 32400 -1461 23 63 | -51 -6 | jpl 118| -1 3 2 19 -9 31 .48 19 19 | 4667 -1642 20 91 | 15 -3 | mit 308| 0 -2 -3 -3 -86 -16 -.28 14 12 | 221 -264 36 155 | 9 -24 | ngs 220| -1 1 -2 109 101 19 -.29 14 12 | -292 -518 3108 5317 | -45 58 | sio 113| -2 1 -1 169 227 24 .06 23 22 | --- --- --- --- | -39 -121 | 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 IGS column gives resulting satellite accuracy measures found in SP3 header. The last IGS column gives the RMS fit of the IGS 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 IGS 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 3.1474.0 GPS week: 1474 Day: 0 MJD: 54562.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- X1E | 13 23 18 24 8 --- 14 19 --- 8 | 59 58 62 61 61 --- 61 70 --- 61 2 | 10 19 12 16 5 22 12 12 23 5 | 16 33 20 29 23 31 19 21 24 19 3 | 9 14 12 14 4 13 13 11 25 5 | 17 28 25 24 20 29 18 17 42 20 4 | 10 17 12 14 6 12 10 12 25 5 | 16 21 18 27 17 19 19 23 23 16 5M | 9 16 12 9 5 12 8 12 18 4 | 14 24 22 20 18 20 17 28 13 17 6M | 9 18 12 13 5 15 17 10 21 5 | 17 28 22 24 21 32 16 22 40 20 7 | 8 21 12 21 7 21 32 20 26 7 | 36 37 29 42 35 36 32 45 37 32 8 | 6 18 13 8 5 12 10 14 14 4 | 19 29 25 23 21 27 17 24 26 21 9 | 7 16 10 10 7 13 13 12 16 4 | 19 28 18 26 23 25 21 31 26 21 10 | 5 17 9 7 4 15 10 12 13 4 | 14 29 23 21 19 19 19 23 15 18 11 | 14 19 14 22 8 14 15 13 16 6 | 19 28 20 23 19 20 26 21 25 17 12M | 7 15 11 14 6 16 10 11 27 5 | 25 30 25 31 25 31 24 30 25 25 13E | 7 19 13 17 4 17 13 9 12 5 | 34 43 38 37 36 44 35 39 39 36 14E | 9 18 14 13 6 19 14 12 13 5 | 33 43 36 39 36 42 37 38 38 36 15E | 11 34 13 12 5 22 15 12 22 6 | 35 51 40 37 36 37 46 38 40 37 16M | 8 16 13 16 5 18 10 12 21 5 | 23 32 29 31 25 34 25 24 30 25 17 | 9 24 14 16 6 19 14 11 15 5 | 21 32 22 29 24 30 23 29 20 22 18 | 10 23 13 17 6 20 18 10 28 6 | 17 37 28 27 22 29 31 21 28 21 19 | 12 23 16 18 7 19 14 11 15 6 | 21 35 20 24 23 29 24 24 23 21 20 | 10 20 15 23 6 18 15 11 28 6 | 20 32 30 24 21 27 28 24 27 19 21 | 8 22 16 18 6 17 14 9 23 5 | 14 30 19 24 18 25 17 24 26 17 22 | 9 20 14 21 6 19 15 9 19 5 | 27 40 37 28 30 34 37 29 31 29 23E | 6 22 17 11 5 24 11 12 17 5 | 26 39 29 33 29 39 28 37 33 29 24M | 9 17 11 14 6 11 8 10 23 4 | 15 27 20 27 20 21 20 28 27 20 25 | 6 18 10 12 4 14 14 11 14 4 | 16 24 16 24 18 25 19 26 17 17 26E | 9 22 12 16 6 15 12 16 22 5 | 50 61 52 55 55 55 58 56 64 53 27 | 6 19 11 9 5 15 9 13 15 4 | 14 26 16 22 17 24 15 25 16 16 28 | 9 20 12 16 7 17 14 18 26 6 | 23 33 29 27 25 30 24 25 25 23 29M | 9 21 11 13 7 15 15 15 16 5 | 43 48 39 48 42 45 42 48 45 44 30M | 10 14 11 10 3 10 11 11 18 4 | 24 33 32 30 28 27 29 33 22 26 31 | 9 18 15 22 9 17 12 14 15 5 | 16 33 24 26 21 28 21 22 19 19 32 | 8 19 20 11 7 65 15 11 20 9 | 15 24 28 21 14 49 20 16 27 15 ------+---------------------------------------------------+---------------------------------------------------- RMS | 9 20 13 15 6 20 14 12 20 |T 23 34 27 30 26 31 27 30 28 25 WRMS | 9 20 13 15 6 20 12 11 19 |NE 18 30 23 26 21 28 22 24 25 20 MEDI | 9 19 12 14 6 17 13 12 19 |MD 19 32 25 27 23 29 24 25 26 21 Table 3.1474.1 GPS week: 1474 Day: 1 MJD: 54563.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- X1E | 17 20 25 26 9 --- 21 17 --- 9 | 41 36 52 44 34 --- 38 43 --- 39 2 | 11 20 13 15 5 19 11 10 23 5 | 18 35 20 26 22 30 18 22 22 19 3 | 9 12 11 14 6 11 12 13 24 4 | 15 31 27 26 22 31 16 25 42 23 4 | 8 18 10 14 6 14 14 9 20 5 | 21 28 20 31 23 21 19 26 25 21 5 | 8 16 10 10 4 11 10 10 23 4 | 13 19 15 17 15 14 17 21 18 13 6 | 9 18 11 15 7 11 13 9 24 5 | 17 31 23 27 20 30 16 22 41 22 7 | 9 22 11 24 8 19 37 20 21 8 | 36 40 32 46 36 36 38 42 36 34 8 | 4 15 11 9 3 10 10 12 12 4 | 19 29 21 24 22 27 20 24 29 22 9 | 7 19 10 11 6 13 11 13 15 4 | 12 25 13 17 12 17 14 18 22 12 10 | 5 15 12 11 6 12 8 15 17 4 | 11 24 21 19 18 18 16 25 14 16 11 | 25 18 16 22 7 16 12 11 18 7 | 20 28 14 19 14 20 16 14 18 12 12 | 7 13 11 14 4 14 12 12 32 5 | 19 27 19 26 20 24 20 25 24 19 13E | 8 16 13 15 6 21 11 10 14 5 | 38 47 44 46 43 46 42 41 42 40 14E | 10 21 15 19 7 20 11 17 14 6 | 20 33 23 26 23 25 23 28 24 21 15E | 9 24 11 18 6 20 18 10 24 6 | 30 37 35 31 30 33 35 31 37 30 16 | 10 16 12 18 8 17 12 16 24 5 | 15 27 23 25 19 29 16 19 23 17 17 | 9 25 14 16 6 20 12 15 16 5 | 13 33 18 23 17 28 16 22 17 16 18 | 11 23 12 17 6 20 16 13 28 6 | 15 36 22 28 24 32 28 20 31 21 19 | 11 21 16 16 7 18 14 14 13 5 | 14 28 20 22 17 26 24 17 22 18 20 | 10 25 13 20 7 17 18 12 30 6 | 12 30 22 23 17 26 19 15 22 13 21 | 7 18 16 22 8 15 12 14 24 6 | 15 29 19 28 20 25 21 17 27 18 22 | 9 20 15 22 7 17 14 13 23 6 | 20 39 30 28 26 33 28 23 30 24 23E | 9 24 14 14 6 24 13 12 16 5 | 30 45 34 35 34 42 37 36 37 33 24 | 8 17 13 15 7 10 11 13 21 5 | 15 25 18 25 18 21 21 22 26 18 25 | 8 16 9 11 4 12 12 13 16 4 | 12 22 15 20 14 24 16 18 15 13 26E | 9 18 13 15 5 17 12 11 24 5 | 36 39 39 42 37 38 43 41 36 37 27 | 6 17 10 10 4 11 11 15 11 4 | 12 25 12 20 15 22 14 23 14 14 28 | 9 19 13 14 7 20 16 17 24 6 | 18 32 22 27 20 30 18 28 21 20 29 | 8 21 12 15 7 17 14 15 17 5 | 38 44 32 43 35 41 38 41 37 37 30 | 6 13 11 13 5 9 10 10 18 4 | 18 21 20 22 19 18 18 22 17 16 31 | 9 19 15 25 7 13 13 18 16 6 | 14 31 20 27 19 27 20 23 15 18 32 | 9 16 20 11 6 60 21 15 20 9 | 13 25 25 18 15 34 18 16 31 15 ------+---------------------------------------------------+---------------------------------------------------- RMS | 9 19 13 16 6 19 15 13 21 |T 20 31 24 27 22 28 23 25 26 21 WRMS | 9 19 13 16 6 19 12 12 21 |NE 16 30 21 25 19 27 20 22 24 18 MEDI | 9 18 12 15 6 17 12 13 20 |MD 17 30 21 26 20 27 19 23 24 19 Table 3.1474.2 GPS week: 1474 Day: 2 MJD: 54564.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- X1E | 18 15 16 30 15 --- 19 18 --- 9 | 51 57 44 57 49 --- 53 53 --- 49 2 | 10 18 13 15 6 15 11 11 23 5 | 15 32 18 24 21 28 18 21 20 18 3 | 8 13 11 15 11 13 12 12 25 5 | 19 31 25 28 26 32 19 24 43 24 4 | 9 16 12 14 7 11 11 9 18 4 | 31 34 31 38 33 29 35 38 32 31 5 | 9 12 12 10 4 8 10 17 18 4 | 15 20 19 19 16 18 15 25 12 15 6 | 8 17 9 13 6 11 12 13 24 5 | 13 31 18 21 20 26 15 23 37 19 7 | 9 21 14 26 7 19 36 18 24 8 | 22 34 18 37 24 29 32 31 24 21 8 | 6 15 8 9 6 10 10 10 12 3 | 15 25 18 20 21 23 18 25 21 18 9 | 8 12 10 13 5 9 10 12 15 4 | 14 24 15 23 17 23 16 21 23 16 10 | 6 12 9 9 7 9 10 16 20 4 | 15 24 21 20 20 22 20 26 20 18 11 | 32 24 19 22 10 16 12 19 19 8 | 25 34 19 21 17 20 22 21 22 16 12 | 8 12 11 13 5 11 13 16 29 5 | 16 27 20 24 18 26 19 26 20 18 13E | 8 19 15 26 6 19 11 11 26 6 | 52 57 53 64 55 58 54 59 53 54 14E | 13 17 15 21 6 18 13 16 14 6 | 29 37 29 37 29 32 29 28 30 28 15E | 16 23 18 13 5 21 13 14 24 6 | 47 56 52 51 49 48 51 52 55 49 16 | 8 17 18 13 7 16 11 13 28 5 | 20 31 27 25 24 28 19 26 23 21 17 | 10 20 14 15 7 16 13 11 13 5 | 20 33 18 28 25 30 22 24 19 21 18 | 12 21 15 18 6 19 17 15 27 6 | 14 39 23 31 26 33 24 25 24 21 19 | 11 20 19 17 6 15 9 13 13 5 | 15 26 18 21 18 23 20 22 23 17 20 | 11 19 12 21 7 18 15 12 32 6 | 19 31 19 25 22 29 25 21 25 18 21 | 10 19 14 19 8 15 14 16 22 6 | 16 33 20 30 25 27 18 26 25 20 22 | 10 18 14 21 8 16 17 16 20 6 | 19 38 26 30 26 33 28 23 27 22 23E | 10 26 16 22 8 26 10 10 17 6 | 49 57 49 54 50 59 49 52 44 49 24 | 8 17 11 15 6 11 9 14 18 4 | 14 26 15 24 19 21 20 21 26 17 25 | 7 16 9 12 5 14 12 12 18 4 | 16 23 17 24 18 24 22 26 23 18 26E | 8 18 17 12 7 18 12 15 25 5 | 57 62 57 62 62 58 65 65 62 59 27 | 6 15 10 11 6 12 10 13 12 4 | 13 27 17 22 19 23 17 24 17 16 28 | 10 19 13 14 6 17 16 15 26 6 | 22 31 23 27 25 29 22 26 17 21 29 | 11 24 12 13 3 22 15 12 21 6 | 33 44 26 39 33 42 36 41 38 35 30 | 7 10 12 11 5 8 11 16 21 4 | 21 27 28 24 24 23 22 33 21 21 31 | 12 22 15 20 6 18 14 19 17 6 | 18 40 21 29 23 34 24 21 16 21 32 | 7 14 23 12 6 67 20 15 22 10 | 17 25 24 20 18 48 23 21 29 17 ------+---------------------------------------------------+---------------------------------------------------- RMS | 11 18 14 16 7 19 14 14 21 |T 23 34 25 31 27 31 27 30 28 25 WRMS | 10 18 13 16 7 19 13 12 22 |NE 17 30 20 26 22 28 22 24 23 19 MEDI | 9 17 13 14 6 16 12 14 21 |MD 19 31 21 25 24 29 22 25 24 21 Table 3.1474.3 GPS week: 1474 Day: 3 MJD: 54565.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- X1E | 18 --- 13 23 9 --- 17 19 16 8 | 43 --- 47 44 46 --- 43 50 8 43 2 | 10 16 13 12 6 17 10 12 21 5 | 16 31 23 23 22 27 21 23 21 19 3 | 11 12 12 12 4 12 11 17 24 5 | 16 28 23 24 20 31 17 19 39 20 4 | 8 12 12 16 5 13 9 12 15 4 | 30 29 26 35 28 32 28 26 27 26 5 | 7 14 9 9 3 10 8 15 17 4 | 13 23 15 14 15 15 15 22 14 13 6 | 9 15 12 13 5 12 10 12 28 5 | 17 31 17 22 17 29 17 18 40 19 7 | 9 19 15 26 6 17 29 16 22 7 | 48 55 46 56 48 51 52 54 51 48 8 | 7 14 9 8 5 10 12 14 10 4 | 16 25 22 22 19 24 17 21 25 18 X9 | 8 16 10 11 4 --- 8 13 18 4 | 16 25 17 22 19 --- 17 18 27 16 10 | 6 10 9 15 8 12 10 17 13 4 | 13 18 20 25 19 19 15 22 15 15 11 | 31 20 12 23 10 17 11 18 16 7 | 31 37 21 25 21 26 30 21 29 23 12 | 6 13 10 13 4 10 8 14 29 5 | 22 25 21 26 21 26 21 23 22 20 13E | 8 16 13 21 3 20 14 13 12 5 | 33 43 32 42 36 43 34 37 35 34 14E | 10 15 11 16 8 18 10 17 11 5 | 40 43 40 43 41 44 41 38 41 39 15 | 24 23 14 17 9 21 11 16 25 7 | 73 79 89 80 80 78 86 82 83 79 16 | 7 15 14 15 6 16 10 21 26 5 | 22 30 24 26 20 29 20 23 24 21 17 | 9 19 17 15 7 18 9 15 10 5 | 20 32 17 28 23 30 20 23 23 20 18 | 11 19 14 19 6 22 12 12 26 6 | 18 35 24 28 23 31 25 22 24 20 19 | 10 17 16 16 5 18 10 21 13 5 | 16 27 14 22 17 27 19 17 20 16 20 | 11 21 16 21 8 19 13 16 31 6 | 22 36 26 29 23 32 29 18 30 22 21 | 10 16 15 21 6 14 9 15 22 5 | 14 27 19 29 18 23 15 20 24 16 22 | 9 16 14 23 7 17 13 15 20 6 | 26 36 29 28 26 31 29 28 25 25 23E | 18 22 19 13 7 24 13 13 21 6 | 69 80 80 73 72 77 69 76 77 73 24 | 9 15 13 13 5 12 9 13 18 4 | 12 23 17 24 13 20 15 21 22 13 25 | 9 14 10 12 4 14 10 14 18 4 | 13 22 16 23 16 23 18 20 23 14 26E | 10 20 15 16 4 20 12 14 18 5 | 57 64 55 63 58 59 57 62 59 57 27 | 8 15 9 10 5 11 10 13 11 4 | 16 29 18 24 19 24 18 21 22 17 28 | 8 18 11 14 8 14 12 16 23 5 | 22 32 25 27 23 31 22 23 20 21 29 | 9 21 12 11 4 20 11 20 21 5 | 39 46 32 40 34 43 37 43 41 37 30 | 4 9 9 10 5 10 7 13 19 3 | 21 28 23 23 24 22 24 30 22 21 31 | 9 17 14 21 7 16 11 17 17 5 | 16 33 16 25 18 29 15 15 17 16 32 | 10 14 20 8 9 65 21 17 20 9 | 18 27 22 22 15 46 29 14 29 18 ------+---------------------------------------------------+---------------------------------------------------- RMS | 11 17 13 16 6 20 12 15 20 |T 26 35 28 32 27 34 28 29 30 26 WRMS | 9 17 13 16 6 20 11 14 20 |NE 19 30 22 27 22 30 22 22 25 20 MEDI | 9 16 13 15 6 16 10 15 18 |MD 20 31 23 26 21 29 21 22 24 20 Table 3.1474.4 GPS week: 1474 Day: 4 MJD: 54566.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- X1E | 16 --- 15 29 10 --- 24 20 --- 10 | 43 --- 44 41 40 --- 44 47 --- 40 2 | 11 19 15 13 8 17 10 9 23 5 | 18 35 22 26 21 28 18 19 20 19 3 | 9 13 9 15 5 12 20 10 24 5 | 15 28 21 26 20 27 24 17 39 20 4 | 8 11 12 13 9 13 9 7 14 4 | 86 89 87 90 83 84 87 87 80 85 5 | 6 12 9 10 3 11 9 10 16 4 | 10 21 21 20 14 15 15 23 16 15 6 | 10 13 11 14 4 13 11 9 27 5 | 13 30 19 24 19 29 21 18 40 19 7 | 9 20 14 22 5 18 30 15 22 7 | 29 33 27 40 28 30 31 34 36 28 8 | 8 15 9 11 5 9 14 10 11 4 | 21 31 26 23 20 28 26 21 25 21 9 | 7 12 11 12 4 10 8 11 17 4 | 13 23 15 22 14 22 14 16 21 14 10 | 5 11 10 8 7 10 10 10 12 3 | 10 19 18 15 16 20 16 17 15 13 11E | 16 18 10 19 6 16 15 15 23 6 | 26 37 29 32 27 29 28 28 23 26 12 | 7 14 10 12 6 13 8 11 28 4 | 14 23 19 22 18 21 17 22 19 16 13E | 10 16 15 15 5 19 13 11 12 5 | 44 51 42 53 48 50 46 46 45 45 14E | 17 20 12 15 8 22 10 10 15 5 | 39 49 46 45 44 50 44 45 44 43 15 | 10 19 17 12 7 19 8 14 27 6 | 29 37 36 30 32 31 34 31 35 30 16 | 7 17 13 14 5 17 14 14 29 5 | 16 34 20 25 20 29 20 23 26 20 17 | 8 20 17 14 7 19 10 12 13 5 | 14 31 12 21 19 29 19 19 19 15 18 | 11 20 17 20 5 21 15 12 28 6 | 16 33 22 26 20 30 21 19 20 17 19 | 10 17 14 17 4 16 17 14 13 5 | 14 28 14 25 17 27 21 15 21 16 X20 | 10 --- 11 22 11 22 20 12 30 7 | 19 --- 22 27 24 29 31 17 29 19 21 | 11 17 12 16 5 16 12 8 23 5 | 14 29 19 27 18 27 16 17 25 16 22 | 11 18 14 22 8 21 15 13 22 6 | 20 34 24 28 23 31 28 22 21 20 23 | 23 20 15 13 6 25 16 11 19 7 | 60 69 67 64 64 66 69 63 68 63 24 | 8 14 11 14 6 11 11 11 19 4 | 9 22 14 22 13 19 14 16 21 11 25 | 8 14 10 11 6 15 14 12 16 4 | 11 21 12 19 11 20 15 15 18 11 26E | 12 18 18 16 5 19 12 12 25 6 | 86 95 89 90 90 90 90 92 89 88 27 | 7 14 10 10 3 13 11 11 13 4 | 12 23 14 18 13 21 15 17 18 13 28 | 9 19 13 13 6 15 12 9 24 5 | 20 35 23 23 22 30 20 18 19 19 29 | 9 21 11 13 6 17 15 11 19 5 | 33 41 28 35 33 36 31 36 33 32 30 | 4 10 9 9 5 9 11 8 15 3 | 18 26 25 24 22 21 20 26 20 20 31 | 12 17 15 17 8 15 11 15 17 5 | 14 33 18 24 20 29 15 20 15 16 32 | 7 19 17 11 5 65 15 13 23 9 | 18 26 26 18 18 35 26 20 27 18 ------+---------------------------------------------------+---------------------------------------------------- RMS | 10 17 13 15 6 20 13 12 20 |T 25 36 28 32 27 33 29 28 30 26 WRMS | 9 17 13 15 6 20 12 10 21 |NE 20 32 23 27 22 30 24 22 26 21 MEDI | 9 17 12 14 6 16 12 11 19 |MD 18 31 22 25 20 29 21 20 23 19 Table 3.1474.5 GPS week: 1474 Day: 5 MJD: 54567.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- X1E | 20 27 17 36 10 --- 24 13 --- 10 | 41 47 38 49 40 --- 42 42 --- 38 2 | 11 22 12 10 4 17 12 13 23 5 | 15 31 18 23 17 27 18 16 21 16 3 | 11 14 8 11 3 9 16 11 28 5 | 17 29 19 25 17 26 17 17 44 20 4 | 8 13 10 14 5 14 10 13 16 4 | 59 67 62 64 65 62 62 64 61 61 5 | 8 13 9 12 4 8 13 12 21 4 | 13 21 15 20 17 17 18 22 20 15 6 | 9 14 9 11 5 11 15 11 28 5 | 15 27 17 22 16 25 22 16 41 18 7 | 8 21 12 18 5 18 26 15 19 6 | 43 54 42 49 44 49 43 44 48 43 8 | 7 11 6 11 6 9 9 10 13 3 | 21 24 23 21 21 25 25 21 25 21 9 | 8 16 9 12 5 12 11 15 22 4 | 15 27 17 24 17 25 16 18 23 16 10 | 8 14 8 10 8 12 9 10 12 3 | 10 19 18 19 16 18 14 16 17 13 11E | 14 23 10 17 7 16 13 18 26 6 | 24 32 23 24 22 23 22 26 24 20 12 | 9 14 13 11 4 10 9 13 29 5 | 17 28 17 22 20 23 19 22 20 17 13E | 10 20 14 11 4 18 14 11 9 5 | 45 53 43 50 48 51 48 47 47 45 14E | 17 20 15 14 5 18 16 11 15 6 | 68 69 71 69 65 72 69 66 67 68 15 | 11 21 16 13 5 18 9 15 28 6 | 22 32 34 24 26 29 28 25 34 25 16 | 9 15 10 15 4 14 15 11 30 5 | 16 27 18 24 16 24 16 18 24 17 17 | 9 20 13 14 5 17 12 16 15 5 | 16 29 14 26 17 27 20 19 24 16 18 | 11 22 15 17 4 20 16 12 28 6 | 13 33 15 26 15 30 17 14 20 15 19 | 10 20 13 16 4 15 21 17 17 6 | 14 27 11 23 14 22 21 19 21 14 20 | 11 23 12 22 4 19 21 16 34 7 | 17 32 17 24 18 26 23 18 22 15 21 | 11 20 11 14 5 13 15 10 26 5 | 14 31 19 25 16 23 18 20 28 17 22 | 11 21 14 21 4 16 15 11 21 6 | 19 31 21 26 19 29 22 17 18 19 23 | 9 26 12 10 7 21 17 12 18 5 | 24 37 23 26 27 30 31 26 27 22 24 | 10 16 10 16 5 11 13 9 20 4 | 8 23 11 23 12 19 15 17 23 13 25 | 7 17 7 11 6 13 17 14 14 4 | 13 22 13 21 14 21 20 16 22 14 26E | 23 20 12 17 6 15 13 11 22 6 | 102 107 102 107 105 105 105 106 108 103 27 | 7 13 10 10 5 10 9 12 12 4 | 10 21 14 19 14 18 14 15 17 12 28 | 8 18 11 12 4 15 12 15 27 5 | 14 28 16 21 15 24 17 16 20 14 29 | 10 23 11 12 5 14 15 12 17 5 | 30 39 26 36 29 32 32 36 34 31 30 | 7 11 9 9 4 8 8 9 19 3 | 20 25 20 21 21 22 19 24 17 19 31 | 13 20 11 19 7 15 10 13 19 5 | 13 32 16 24 17 28 13 17 15 15 32 | 14 25 15 10 9 62 15 17 27 9 | 14 23 18 14 12 35 19 12 25 12 ------+---------------------------------------------------+---------------------------------------------------- RMS | 11 19 11 14 5 18 14 13 22 |T 24 35 25 30 26 31 27 27 30 25 WRMS | 10 19 11 14 5 18 13 11 23 |NE 18 31 20 26 20 28 22 21 26 19 MEDI | 10 20 11 12 5 15 13 12 21 |MD 16 29 18 24 17 26 20 19 24 17 Table 3.1474.6 GPS week: 1474 Day: 6 MJD: 54568.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- X1E | 18 23 16 31 13 --- 22 20 --- 9 | 56 51 60 71 62 --- 57 67 --- 59 2 | 9 20 13 11 4 17 13 14 23 5 | 19 35 20 24 20 30 21 20 23 20 3 | 10 11 8 12 5 12 10 15 27 4 | 15 27 20 25 18 25 20 24 44 20 4 | 8 17 10 12 5 12 9 12 13 4 | 52 52 52 53 49 55 51 53 54 51 5 | 8 12 7 9 4 9 11 10 22 4 | 14 26 20 22 21 20 24 26 22 19 6 | 9 12 8 11 3 12 17 12 27 5 | 13 25 14 20 14 22 21 19 38 16 7 | 9 21 12 22 8 20 30 15 25 7 | 31 40 29 38 31 36 46 31 28 30 8 | 6 12 8 9 5 10 10 12 16 3 | 32 35 32 34 33 37 33 36 37 32 9 | 6 17 6 11 3 12 14 15 23 4 | 15 29 17 23 16 24 17 15 26 16 10 | 5 9 7 8 5 11 11 12 13 3 | 13 19 22 20 19 20 21 23 20 17 11E | 22 18 9 25 8 17 14 19 25 7 | 34 36 29 38 31 30 29 33 31 29 12 | 8 14 9 11 4 13 8 14 31 4 | 21 27 22 26 23 28 22 22 23 21 13 | 15 19 11 14 4 17 13 10 17 5 | 90 100 91 95 94 94 92 89 89 91 14 | 9 19 11 15 6 21 10 13 21 5 | 36 39 35 32 32 37 35 30 37 32 15 | 11 24 12 11 9 19 15 14 29 6 | 34 44 39 37 37 37 40 38 44 35 16 | 8 14 12 14 4 17 14 15 29 5 | 23 31 24 29 22 31 23 30 31 24 17 | 9 22 14 15 6 19 10 15 17 5 | 17 31 15 29 19 30 20 22 26 18 18 | 10 20 13 16 5 22 14 14 28 6 | 19 32 23 27 20 30 25 22 24 20 19 | 10 17 11 17 6 17 15 20 14 5 | 16 27 11 23 13 27 24 20 24 16 20 | 10 19 13 23 3 20 19 16 39 7 | 20 32 24 24 22 26 28 22 35 19 21 | 9 19 12 15 5 14 12 10 25 5 | 16 32 22 28 20 25 18 20 30 19 22 | 10 20 12 20 5 19 12 13 23 6 | 27 37 30 28 25 30 34 26 29 26 23 | 10 20 12 12 4 21 15 17 17 5 | 27 35 33 29 29 29 29 29 28 26 24 | 8 12 10 16 6 10 12 10 24 4 | 10 19 12 24 15 19 14 18 28 12 25 | 8 14 9 12 3 13 23 15 18 5 | 13 22 12 19 14 21 18 15 19 12 26 | 17 14 11 16 12 13 12 14 21 5 | 74 86 81 82 77 82 81 79 79 80 27 | 6 12 9 10 3 13 11 9 16 4 | 15 22 13 21 15 20 16 16 18 14 28 | 7 16 8 15 4 13 13 17 32 5 | 23 30 26 26 23 29 24 27 27 22 29 | 10 22 11 13 6 18 18 11 19 5 | 40 44 32 43 36 43 35 40 41 37 30 | 6 12 6 8 6 9 10 9 20 3 | 26 34 30 31 31 28 31 32 26 28 31 | 9 18 10 21 5 16 12 13 17 5 | 17 32 18 27 20 27 17 18 18 18 32 | 8 17 10 11 11 64 11 18 25 8 | 16 20 20 18 16 43 20 17 25 14 ------+---------------------------------------------------+---------------------------------------------------- RMS | 10 17 10 15 6 19 14 14 23 |T 27 35 29 33 28 33 30 30 33 27 WRMS | 9 17 10 15 6 19 12 12 22 |NE 20 30 22 27 21 29 25 23 28 21 MEDI | 9 17 10 13 5 16 12 14 23 |MD 20 32 23 27 22 29 24 24 28 20 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1474 GPS week: 1474 MJD: 54562.0-54568.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3066 |U 7 6 17 |U 6 8 25 |U 6 6 15 | emr | emr 3023 | 9 9 21 |U 8 8 32 | 8 7 20 | esa | esa 3072 | 8 8 22 |U 8 11 24 |U 12 7 16 | gfz | gfz 3049 |U 7 7 18 |U 7 8 29 |U 6 6 17 | igr | igr 3056 | 7 7 18 | 6 7 24 | 6 5 15 | igs | igs 3009 | 7 7 19 | 6 7 25 | 7 6 15 | jpl | jpl 2960 | 8 9 21 |U 6 6 29 |U 7 5 17 | mit | mit 3072 |U 7 6 19 |U 7 10 29 |U 17 11 49 | Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit positions and satellite clock corrections at 15 min intervals. Each line gives the daily station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. CLK - Satellite clocks used. EPO - Number of satellite clock epochs available for that day. Units: mm. Table 5.1474.0 GPS week: 1474 Day: 0 MJD: 54562.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3067 | 7 7 14 | 6 9 31 | 5 7 17 | emr | emr 3059 | 9 9 21 | 7 6 30 | 8 8 21 | esa | esa 3072 | 9 7 20 | 7 10 27 | 13 9 17 | gfz | gfz 3044 | 6 9 17 | 7 10 36 | 5 5 18 | igr | igr 3029 | 8 8 19 | 6 6 25 | 6 6 16 | igs | igs 2956 | 8 7 18 | 5 8 30 | 7 8 19 | jpl | jpl 2972 | 7 10 21 | 5 6 32 | 7 6 18 | mit | mit 3072 | 14 6 23 | 6 11 29 | 74 24 103 | Table 5.1474.1 GPS week: 1474 Day: 1 MJD: 54563.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3069 | 6 7 16 | 7 10 23 | 7 6 14 | emr | emr 3061 | 8 9 24 | 8 10 38 | 7 8 17 | esa | esa 3072 | 8 10 25 | 8 13 26 | 14 7 15 | gfz | gfz 3048 | 6 6 15 | 9 9 29 | 6 6 15 | igr | igr 3063 | 7 8 20 | 8 11 24 | 7 6 15 | igs | igs 3060 | 6 8 20 | 8 9 30 | 8 6 14 | jpl | jpl 2972 | 7 8 20 | 8 7 30 | 6 5 17 | mit | mit 3072 | 6 7 21 | 8 11 29 | 10 14 150 | Table 5.1474.2 GPS week: 1474 Day: 2 MJD: 54564.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3068 | 7 6 16 | 6 7 18 | 6 5 12 | emr | emr 3061 | 9 10 18 | 8 8 30 | 7 6 19 | esa | esa 3072 | 9 9 21 | 8 12 19 | 16 6 16 | gfz | gfz 3048 | 7 9 16 | 7 10 23 | 8 7 17 | igr | igr 3071 | 7 8 16 | 6 7 23 | 8 5 13 | igs | igs 2878 | 7 8 18 | 6 8 24 | 7 5 16 | jpl | jpl 2972 | 7 10 19 | 6 6 29 | 7 5 17 | mit | mit 3072 | 7 7 16 | 7 11 27 | 8 7 17 | Table 5.1474.3 GPS week: 1474 Day: 3 MJD: 54565.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3064 | 8 6 15 | 6 8 27 | 6 6 16 | emr | emr 2972 | 9 8 20 | 10 10 35 | 8 8 20 | esa | esa 3072 | 10 11 24 | 9 14 25 | 12 7 20 | gfz | gfz 3047 | 8 8 19 | 7 9 32 | 7 7 19 | igr | igr 3068 | 7 6 16 | 6 9 28 | 7 6 19 | igs | igs 3054 | 7 7 16 | 7 9 26 | 7 7 17 | jpl | jpl 2876 | 10 13 26 | 6 8 34 | 7 8 23 | mit | mit 3072 | 6 7 14 | 8 11 32 | 8 10 18 | Table 5.1474.4 GPS week: 1474 Day: 4 MJD: 54566.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3064 | 7 5 20 | 6 8 21 | 6 5 12 | emr | emr 2880 | 9 9 19 | 10 9 35 | 9 5 20 | esa | esa 3072 | 8 6 24 | 7 14 22 | 11 6 14 | gfz | gfz 3052 | 6 7 20 | 6 6 26 | 7 6 15 | igr | igr 3069 | 6 5 20 | 6 10 17 | 6 5 11 | igs | igs 2976 | 6 5 20 | 5 9 17 | 6 6 12 | jpl | jpl 2976 | 7 7 20 | 5 7 25 | 7 5 15 | mit | mit 3072 | 6 4 19 | 7 12 23 | 8 10 17 | Table 5.1474.5 GPS week: 1474 Day: 5 MJD: 54567.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3065 | 6 7 21 | 5 6 29 | 6 6 10 | emr | emr 3065 | 9 9 21 | 9 5 27 | 8 7 18 | esa | esa 3072 | 8 7 19 | 7 7 24 | 10 5 12 | gfz | gfz 3050 | 7 7 19 | 5 6 31 | 6 5 14 | igr | igr 3036 | 6 6 17 | 6 5 23 | 7 4 12 | igs | igs 3067 | 7 6 20 | 5 5 26 | 8 5 9 | jpl | jpl 2976 | 7 8 20 | 5 6 24 | 6 4 12 | mit | mit 3072 | 7 6 17 | 6 7 24 | 7 9 11 | Table 5.1474.6 GPS week: 1474 Day: 6 MJD: 54568.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3069 | 6 5 18 | 6 6 24 | 8 6 22 | emr | emr 3068 | 7 10 24 | 8 6 28 | 8 8 23 | esa | esa 3072 | 7 8 20 | 6 6 25 | 8 6 16 | gfz | gfz 3057 | 7 6 18 | 7 5 26 | 6 5 21 | igr | igr 3060 | 6 6 20 | 7 4 26 | 6 4 17 | igs | igs 3072 | 6 5 19 | 6 4 23 | 6 4 16 | jpl | jpl 2976 | 7 6 24 | 6 5 29 | 6 4 19 | mit | mit 3072 | 7 6 19 | 10 6 35 | 8 6 25 | Table 6: Earth Orientation Parameters weekly summary. Weekly mean and standard deviation of Centre ERP, ERP rates and LOD differences with respect to IGS combined values. See Table 7 for the daily summaries. Xpole,Xrt: x pole and x pole rate Ypole,Yrt: y pole and y pole rate LOD : Length Of Day AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A AC LOD BIAS RMS: RMS of AC LOD BIAS FLAG: "u" (used), "x" (excluded), "-" (no submission) for Xpole, Ypole, Xrt, Yrt and LOD Table 6.1474 GPS week: 1474 MJD: 54562.500-54568.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 5 -36 19 29 -4 | -3 10 | 17 22 54 68 6 | 2 emr uuxuu | -38 25 143 111 10 | 65 67 | 38 37 367 135 14 | 6 esa uuuuu | -12 -19 20 -13 -10 | 16 23 | 23 21 59 65 18 | 5 gfz uuuuu | -15 25 -72 19 4 | 1 12 | 25 18 37 23 4 | 5 igr xxxxx | -11 28 -50 -15 4 | -3 13 | 28 20 53 80 6 | 4 irf xxxxx | -4 5 -2 46 5 | 2 14 | 8 10 74 41 12 | 6 jpl uuuxx | 19 -42 107 128 10 | 10 30 | 16 32 124 229 27 | 20 mit uuuuu | 9 -5 10 115 13 | 18 24 | 33 22 198 98 15 | 7 ngs uuuuu | -41 34 -84 -258 -3 | 0 11 | 46 37 155 113 5 | 2 sio uuuuu | 126 72 4 20 19 | 40 44 | 32 31 72 94 12 | 8 Table 7.1474.0 GPS week: 1474 Day: 0 MJD: 54562.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -6 1 26 -76 -10 | -3 9 emr uuxuu | 29 -11 470 339 -2 | 61 62 esa uuuuu | -44 -28 21 -27 26 | 9 20 gfz uuuuu | -39 13 -55 0 8 | -4 11 igr xxxxx | 3 27 8 15 0 | -6 12 irf xxxxx | 6 11 16 110 10 | -5 11 jpl uuuxx | 29 -72 -55 520 -23 | 0 0 mit uuuuu | -12 12 92 -22 9 | 12 15 ngs uuuuu | -34 -13 -48 -24 -8 | 1 12 sio uuuuu | 197 135 -29 -8 10 | 34 37 Table 7.1474.1 GPS week: 1474 Day: 1 MJD: 54563.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -24 -21 -88 53 -10 | -4 9 emr uuxuu | -23 -12 585 249 11 | 59 59 esa uuuuu | -21 17 38 -129 2 | 12 23 gfz uuuuu | -29 50 -68 4 6 | -3 11 igr xxxxx | 33 20 -3 133 0 | -7 11 irf xxxxx | -8 18 108 84 12 | -5 11 jpl uuuxx | 46 -90 163 323 26 | -21 21 mit uuuuu | 16 17 185 154 14 | 11 14 ngs uuuuu | -7 -6 -100 -243 -2 | -2 9 sio uuuuu | 113 81 -102 -99 25 | 33 35 Table 7.1474.2 GPS week: 1474 Day: 2 MJD: 54564.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 22 -37 -1 -31 -8 | -6 11 emr uuxuu | -91 -11 456 -6 18 | 58 59 esa uuuuu | -9 -12 -98 50 -23 | 15 23 gfz uuuuu | 1 50 -64 70 3 | -3 11 igr xxxxx | -55 57 -91 -24 4 | -7 12 irf xxxxx | -10 14 50 41 9 | -3 11 jpl uuuxx | 23 -57 236 -64 40 | -8 15 mit uuuuu | -53 20 253 119 21 | 12 15 ngs uuuuu | 18 31 -309 -266 -3 | -3 9 sio uuuuu | 126 54 -35 131 24 | 33 36 Table 7.1474.3 GPS week: 1474 Day: 3 MJD: 54565.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 3 -68 45 51 -2 | -4 12 emr uuxuu | -52 42 157 49 32 | 63 65 esa uuuuu | 14 -16 -2 44 -10 | 18 24 gfz uuuuu | 29 28 -105 17 7 | 0 14 igr xxxxx | -32 1 -121 -52 14 | -4 15 irf xxxxx | -3 5 -2 -5 18 | 2 16 jpl uuuxx | 4 -37 250 -108 40 | 15 38 mit uuuuu | 26 -14 45 106 32 | 17 25 ngs uuuuu | -120 79 -261 -378 -12 | 0 12 sio uuuuu | 105 63 13 18 35 | 38 43 Table 7.1474.4 GPS week: 1474 Day: 4 MJD: 54566.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 11 -31 12 125 1 | -2 11 emr uuxuu | -57 84 -157 -8 16 | 68 71 esa uuuuu | -4 -48 57 -42 -24 | 21 24 gfz uuuuu | -7 20 -124 11 -3 | 3 14 igr xxxxx | -12 15 -2 -8 10 | -1 15 irf xxxxx | 9 -12 1 33 7 | 6 17 jpl uuuxx | 10 -5 154 0 12 | 27 46 mit uuuuu | 51 -39 -6 206 21 | 22 31 ngs uuuuu | -70 19 -47 -341 2 | 0 12 sio uuuuu | 116 56 9 70 25 | 44 50 Table 7.1474.5 GPS week: 1474 Day: 5 MJD: 54567.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 23 -48 73 4 -1 | -2 11 emr uuxuu | -57 40 -272 29 8 | 71 73 esa uuuuu | -35 -39 87 -33 -19 | 20 24 gfz uuuuu | -23 4 -78 15 5 | 5 13 igr xxxxx | -16 29 -94 -129 -3 | 2 14 irf xxxxx | -14 2 -104 55 -3 | 8 17 jpl uuuxx | 26 -16 11 26 -3 | 29 44 mit uuuuu | 14 -23 -261 239 6 | 25 33 ngs uuuuu | -13 81 103 -286 0 | 1 12 sio uuuuu | 112 74 49 121 14 | 47 53 Table 7.1474.6 GPS week: 1474 Day: 6 MJD: 54568.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 10 -48 64 77 4 | -1 11 emr uuxuu | -17 41 -236 122 -13 | 74 77 esa uuuuu | 17 -9 35 43 -21 | 20 25 gfz uuuuu | -36 14 -8 13 -1 | 8 13 igr xxxxx | 2 51 -47 -41 6 | 4 13 irf xxxxx | -4 0 -86 4 -17 | 11 17 jpl uuuxx | -1 -15 -11 196 -24 | 30 43 mit uuuuu | 20 -9 -241 0 -14 | 29 35 ngs uuuuu | -62 45 73 -268 3 | 3 12 sio uuuuu | 117 39 126 -93 -2 | 52 57