From igsacc at gfz-potsdam.de Wed May 9 22:38:19 2007 From: igsacc at gfz-potsdam.de (Gerd Gendt3) Date: Thu, 10 May 2007 07:38:19 +0200 Subject: [IGSREPORT-15082] Wk 1424 IGS Final Orbits Message-ID: <4642AFCB.mailxHL611RIAY@kg20> ****************************************************************************** IGS Electronic Report 09 May 22:40:01 PDT 2007 Message Number 15082 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1424 (Apr 22, 2007 - Apr 28, 2007) Contacts: G. Gendt (gendt at gfz-potsdam.de), Th. Nischan ( nisn at gfz-potsdam.de) 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: igs1424[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1424[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1424[0-6].cls IGS GPS clock combination summary report. igs14247.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14247.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 | COD | 32 NRIL 0 | EMR | 9 0 | ESA | BILI 0 | GFZ | BAN2 0 | JPL | 2 0 | MIT | BAHR KOUR NRIL 1 | COD | CHUR 1 | EMR | WTZR 1 | ESA | SCUB SYOG 1 | GFZ | BAKO BAN2 BOR1 NKLG 1 | JPL | DWH1 1 | MIT | 25 BAHR CHUR KOUR 2 | ESA | BILI KOUR 2 | GFZ | BAN2 DAV1 NISU NLIB 2 | MIT | 25 32 BAHR KOUR LPGS 3 | EMR | USUD 3 | JPL | 2 3 | MIT | 25 32 BAHR KOUR 4 | ESA | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 16 17 18 19 20 21 4 | ESA | 22 23 24 25 26 27 28 30 31 AREQ DGAR KIRU POTS TOW2 4 | GFZ | BOR1 UNSA 4 | JPL | 2 NISU QAQ1 4 | MIT | BAHR 5 | COD | NRIL YELL 5 | GFZ | BAKO DAV1 5 | MIT | GUAM KIT3 6 | COD | MAC1 6 | ESA | LPGS YELL 6 | GFZ | ARTU BAN2 6 | JPL | DAEJ DWH1 6 | MIT | JAMA MAC1 5. The following orbit solutions were excluded from the combination because they were biasing the weighted average (generally indicated by long arc RMS). They were still used for statistics computation. Day | Centre | PRN list ----+--------+--------------- 5 | NGS | 32 6. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G29 | | | | | 4 | | | 7. 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. 8. 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 | .3 .0 .5 -9 0 1 -.19 EMR | -.9 -2.7 13.3 -17 35 -15 -.06 ESA | -1.9 -2.4 7.5 -30 3 -6 -.88 GFZ | .9 .0 .7 -3 -35 2 -.42 JPL | 5.3 -5.0 15.1 154 -72 208 .05 MIT | 3.9 .4 20.7 -7 4 -13 .04 NGS | 7.4 -4.0 3.7 -50 -89 38 -1.04 SIO | -.6 -3.9 4.7 -55 -19 46 .21 9. 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. 10. 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. 11. 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 1.1424.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1424.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 2.1424.[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 3.1424.[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 5.1424.0-6). 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 1424 summary. (Apr 22, 2007 - Apr 28, 2007) Table 1.1424.a GPS week: 1424 MJD: 54212.000-54218.000 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 167| 0 -1 -1 -40 -43 -51 -.27 14 14 | -894 -19 57 102 | 0 0 0 10 26 15 .02 | 799 1072 emr 61| 0 2 3 15 -89 -22 .35 17 17 | 5159 -589 57 107 | 1 1 1 16 28 15 .06 | 2494 1185 esa 62| 0 0 6 24 -66 20 .18 21 21 | -125460 -14120 55 128 | 2 1 3 61 55 58 .03 | 345789 36574 gfz 184| 0 1 2 -17 57 31 .02 15 15 | 99 -86 29 103 | 1 1 1 13 14 34 .04 | 346 478 igr n/a| 0 0 1 -51 -51 -25 .00 8 7 | -20527 -1027 29 68 | 0 0 1 12 14 15 .03 | 3418 1355 jpl n/a| -4 -2 -16 -179 17 219 -.04 41 41 | 4671 -341 96 139 | 3 3 4 16 22 30 .07 | 2289 1500 mit 162| 0 0 -4 -44 -45 -27 -.08 22 21 | -806 737 77 133 | 1 1 0 29 26 12 .07 | 1783 3771 ngs 167| -1 0 0 75 115 2 -.01 14 11 | -80 -1088 2481 4190 | 0 0 1 24 17 17 .04 | 1246 3701 sio 93| 4 -2 -3 28 5 7 -.08 27 24 | --- --- --- --- | 1 1 1 27 46 24 .04 | --- --- Table 1.1424.b GPS week : 1424 MJD: 54212.000-54218.000 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 ------+------------------------------------+------------------------------------------ 1E | 6 6 6 6 7 7 6 | 2 | 8 9 8 8 8 8 8 | 3 | 8 7 7 7 6 6 6 | 4 | 7 6 7 6 6 6 6 | 5 | 7 6 6 6 6 6 6 | 6 | 7 6 7 7 6 6 6 | 7 | 7 7 7 6 6 6 6 | 8 | 6 6 6 5 5 5 5 | 9 | 8 6 6 6 6 6 7 | 10 | 6 6 6 6 6 6 6 | 11E | 8 9 8 10 8 7 6 | 12 | 8 7 8 8 7 7 7 | 13E | 7 7 8 7 7 6 7 | 14E | 7 7 7 7 7 7 7 | 16 | 8 8 8 8 8 8 8 | 17 | 8 8 8 8 8 8 8 | 18 | 9 9 9 9 9 9 9 | 19 | 8 9 9 8 8 8 8 | 20 | 8 8 9 8 9 9 8 | 21 | 9 10 9 10 8 8 8 | 22 | 8 8 9 9 8 9 9 | 23E | 7 8 8 9 7 7 8 | 24 | 6 6 6 6 6 6 6 | 25 | 7 8 8 9 6 5 5 | 26E | 8 6 8 7 7 6 7 | 27 | 6 7 6 6 6 5 5 | 28 | 9 10 9 9 8 8 7 | 29E | 7 6 9 7 13 8 9 | 30 | 7 8 7 7 7 7 7 | 31 | 8 8 8 8 9 8 8 | 32 | 29 23 37 28 27 18 19 | 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 2.1424.0 GPS week: 1424 Day: 0 MJD: 54212.000 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 167| 0 0 0 -23 7 -42 -.27 14 14 | -645 -2178 50 82 | 42 -51 | emr 61| 0 1 7 13 -135 -38 .42 19 18 | 6271 619 68 106 | -118 -79 | esa 62| 0 0 0 -24 -1 -38 .20 22 22 | 6219 929 57 131 | -8 -124 | gfz 184| 0 1 5 -7 52 73 -.03 14 14 | -145 159 26 105 | 43 -47 | igr n/a| 0 2 0 -32 -54 -28 -.01 9 9 | -17683 149 29 67 | 34 -9 | jpl n/a| -3 -1 -26 -144 42 242 .09 39 39 | 6068 739 99 145 | -33 -19 | mit 162| -1 0 -4 -23 -96 -44 -.15 24 21 | 765 -5233 77 127 | 82 51 | ngs 167| -1 0 -1 62 96 5 .00 13 11 | -1361 2919 2861 4806 | -62 57 | sio 93| 3 -3 -1 38 -72 -35 -.06 30 26 | --- --- --- --- | -6 19 | Table 2.1424.1 GPS week: 1424 Day: 1 MJD: 54213.000 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 167| 0 0 -1 -50 -30 -29 -.30 14 15 | -2650 1202 65 117 | 72 -15 | emr 61| 0 1 3 18 -98 -32 .34 16 16 | 7138 -1029 45 84 | -12 -29 | esa 62| 3 0 6 78 19 -72 .18 20 20 | 7195 -956 51 100 | 2 -34 | gfz 184| -1 2 2 4 69 80 .00 16 16 | -237 380 35 119 | 36 -32 | igr n/a| 0 0 1 -47 -26 -40 .03 8 7 | -17525 -1520 28 68 | 55 -24 | jpl n/a| 0 -5 -14 -180 33 236 -.00 41 41 | 6819 -1128 97 136 | -20 -32 | mit 162| 1 -1 -5 -39 -59 -6 -.15 21 21 | -4605 4505 79 137 | 59 38 | ngs 167| -2 1 0 44 111 -25 .02 16 13 | 1070 -2501 2475 3997 | -169 61 | sio 93| 3 -2 -5 49 -30 27 -.12 27 26 | --- --- --- --- | -29 -21 | Table 2.1424.2 GPS week: 1424 Day: 2 MJD: 54214.000 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 167| 0 -1 -1 -42 -60 -66 -.24 15 15 | -933 712 61 103 | 75 33 | emr 61| -1 2 3 39 -54 7 .43 18 18 | 7366 -202 59 107 | -12 -35 | esa 62| -1 -1 8 66 -120 24 .19 21 21 | 7273 53 55 114 | -19 4 | gfz 184| 0 2 2 -39 64 -2 .03 16 16 | 233 -108 28 97 | 29 2 | igr n/a| 0 0 3 -63 -69 -30 -.05 8 8 | -18027 -608 34 65 | 60 41 | jpl n/a| 0 -3 -13 -189 39 254 -.08 43 43 | 6483 -124 95 135 | -2 25 | mit 162| 1 -1 -5 -27 -22 -16 -.13 21 21 | -214 473 73 136 | 24 -11 | ngs 167| -1 0 0 55 102 9 -.09 14 13 | -694 415 2264 4041 | -1 38 | sio 93| 3 -3 -1 16 42 15 -.10 25 22 | --- --- --- --- | -33 -47 | Table 2.1424.3 GPS week: 1424 Day: 3 MJD: 54215.000 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 167| 0 -1 0 -30 -72 -43 -.27 15 15 | -285 -149 55 107 | 59 53 | emr 61| 1 5 4 7 -63 -30 .36 19 19 | 6873 -1794 56 110 | -31 -66 | esa 62| -2 -1 5 -17 -90 63 .22 21 21 | 6802 -1606 53 99 | 14 42 | gfz 184| 0 2 2 -12 65 14 .09 16 16 | 715 -966 33 115 | 25 -27 | igr n/a| 0 0 1 -38 -56 -27 .02 7 7 | -18931 -2299 29 65 | 28 -3 | jpl n/a| -7 -2 -16 -193 -1 240 -.12 42 42 | 5986 -1612 91 127 | 27 24 | mit 162| 0 -2 -4 -22 -23 -31 -.10 21 21 | -1267 6353 71 128 | 21 -2 | ngs 167| 0 0 0 66 100 -17 .01 13 10 | 2198 -8688 2483 4222 | 28 11 | sio 93| 5 -2 -1 50 63 17 -.06 26 21 | --- --- --- --- | -33 -90 | Table 2.1424.4 GPS week: 1424 Day: 4 MJD: 54216.000 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 167| 1 0 0 -36 -55 -76 -.28 14 14 | -714 376 57 115 | 65 18 | emr 61| 0 1 2 27 -82 -24 .34 15 15 | 4781 -1752 53 116 | -27 -8 | esa 62| 0 1 8 -75 -64 79 .17 22 22 | -909617 -97029 54 181 | 40 34 | gfz 184| 1 2 1 -21 28 34 .06 15 15 | 161 111 30 103 | 7 1 | igr n/a| 0 1 1 -59 -44 -39 -.01 7 7 | -21483 -2392 29 73 | 10 7 | jpl n/a| -6 -3 -12 -177 12 190 -.06 42 42 | 4089 -1700 93 147 | 12 49 | mit 162| 0 0 -4 -29 -40 -26 -.01 21 22 | -49 -732 78 132 | 67 -3 | ngs 167| -2 -1 1 85 143 12 -.06 13 10 | -645 208 2109 3945 | -91 51 | sio 93| 2 0 -4 52 19 37 -.08 27 24 | --- --- --- --- | -9 -40 | Table 2.1424.5 GPS week: 1424 Day: 5 MJD: 54217.000 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 167| 2 -1 0 -49 -43 -58 -.28 14 14 | -530 98 57 95 | 46 6 | emr 61| 0 4 2 18 -78 -13 .30 15 15 | 2897 -1228 60 126 | -23 -70 | esa 62| -2 0 9 67 -114 14 .16 21 21 | 3071 -1355 58 145 | -1 24 | gfz 184| 0 0 1 -24 51 24 .00 14 13 | 231 -469 28 98 | -14 -18 | igr n/a| 0 0 1 -62 -47 -3 .03 7 7 | -23812 -1772 29 65 | 27 -27 | jpl n/a| -8 -5 -15 -179 10 196 -.06 40 40 | 2334 -1008 95 143 | -8 -21 | mit 162| 2 0 -3 -99 -45 -25 .02 22 21 | 142 -503 76 136 | 99 -6 | ngs 167| -1 0 0 109 131 14 .01 13 11 | -597 174 2494 4130 | -80 11 | sio 93| 8 0 -1 -19 -8 -5 -.14 28 23 | --- --- --- --- | 15 -26 | Table 2.1424.6 GPS week: 1424 Day: 6 MJD: 54218.000 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 167| 0 -1 -1 -49 -50 -46 -.29 15 14 | -507 -198 59 95 | 89 23 | emr 61| 1 1 2 -11 -111 -22 .27 15 15 | 787 1258 64 103 | 24 12 | esa 62| -2 -1 5 72 -95 73 .13 21 20 | 837 1121 62 128 | 16 22 | gfz 184| 0 0 2 -18 69 -3 -.00 12 12 | -262 286 28 85 | -7 -15 | igr n/a| 0 0 0 -58 -64 -3 .03 7 7 | -26229 1250 27 76 | 39 41 | jpl n/a| -6 5 -19 -194 -16 178 -.05 41 41 | 921 2445 103 141 | 42 58 | mit 162| 0 -1 -3 -72 -27 -38 -.07 24 24 | -419 296 89 141 | 49 -45 | ngs 167| -1 -1 2 104 120 21 .02 13 12 | -537 -148 2686 4194 | -55 74 | sio 93| 4 -1 -4 10 27 -2 -.03 28 25 | --- --- --- --- | -9 -30 | 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 3.1424.0 GPS week: 1424 Day: 0 MJD: 54212.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1E | 10 13 26 15 5 26 18 15 18 6 | 34 43 45 38 35 36 37 34 32 34 2 | 13 20 28 10 8 58 27 14 20 8 | 34 40 39 36 34 54 38 31 33 33 3 | 13 19 27 15 9 22 24 16 35 7 | 30 40 33 36 30 34 39 33 34 31 4 | 16 15 23 11 10 15 36 12 21 7 | 28 30 36 32 29 34 38 25 34 28 5 | 12 22 24 9 11 18 27 13 27 6 | 24 30 39 33 33 27 34 31 32 28 6 | 15 19 33 14 7 15 17 13 21 6 | 29 29 43 32 30 31 29 33 33 30 7 | 15 20 24 14 7 17 17 13 28 6 | 29 27 33 33 29 30 30 30 42 28 8 | 10 17 21 7 10 20 13 7 30 5 | 29 39 35 34 35 28 35 31 27 31 9 | 8 35 21 11 10 20 32 11 18 7 | 32 41 36 39 36 32 43 36 30 33 10 | 12 17 18 10 6 12 21 9 22 5 | 26 34 35 34 30 34 29 30 32 28 11 | 14 20 23 17 13 54 19 15 24 7 | 66 77 71 70 75 81 70 73 79 70 12 | 14 16 17 9 9 51 34 13 34 7 | 27 31 33 33 29 50 36 30 37 28 13E | 15 18 19 19 7 49 12 9 18 7 | 26 39 35 38 31 38 32 25 35 28 14E | 17 14 16 13 7 55 13 12 19 6 | 32 36 37 33 32 40 30 31 28 31 16 | 13 20 16 13 9 42 25 17 36 7 | 38 49 36 45 40 61 43 40 41 40 17 | 15 19 24 15 10 57 20 11 32 8 | 40 50 55 53 46 57 42 45 44 45 18 | 16 20 16 19 8 46 27 19 38 8 | 25 40 36 40 31 41 29 28 32 27 19 | 14 17 18 15 6 55 21 16 36 8 | 36 45 36 44 37 59 34 37 33 36 20 | 17 19 20 16 6 52 23 13 28 7 | 32 45 35 34 32 44 30 32 26 30 21 | 18 24 21 17 8 57 33 17 24 9 | 28 40 38 42 36 46 39 34 34 32 22 | 18 19 23 21 9 43 22 15 29 8 | 31 44 40 43 34 42 30 30 31 31 23E | 12 18 17 10 8 49 17 11 23 6 | 32 44 42 39 35 50 32 29 29 34 24 | 11 14 23 11 5 12 24 11 24 6 | 28 36 37 32 31 36 35 29 36 29 X25 | 11 18 25 10 9 18 26 12 --- 6 | 36 40 43 38 38 40 45 33 --- 36 26E | 12 18 27 15 10 21 30 13 34 7 | 60 71 71 70 64 72 71 64 75 65 27 | 10 14 24 8 10 17 12 10 30 5 | 31 40 40 37 37 33 37 31 26 32 28 | 13 26 19 14 9 50 26 11 52 9 | 33 37 37 33 32 42 39 28 60 29 29E | 10 17 21 13 11 17 23 16 36 6 | 57 57 61 56 56 55 55 52 44 54 30 | 9 18 11 10 8 17 22 12 43 6 | 33 38 35 42 41 34 33 40 49 35 31 | 16 16 27 15 8 47 27 15 24 8 | 30 46 44 39 38 46 27 33 31 31 X32 | 35 --- --- --- 70 73 37 61 --- 29 | 31 --- --- --- 119 36 36 112 --- 47 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 19 22 14 9 39 24 13 30 |T 33 41 41 40 39 43 37 37 37 35 WRMS | 14 18 22 14 9 39 21 11 26 |NE 32 40 39 38 39 42 36 37 37 33 MEDI | 13 18 21 13 9 42 23 13 28 |MD 31 40 37 38 35 40 36 32 33 31 Table 3.1424.1 GPS week: 1424 Day: 1 MJD: 54213.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1E | 13 12 19 15 5 24 20 16 18 6 | 34 39 42 40 34 32 35 28 37 34 2 | 14 18 24 14 6 62 24 22 24 8 | 26 40 35 30 29 47 28 31 27 28 3 | 14 14 18 15 6 21 27 19 32 7 | 28 32 34 31 29 27 35 30 36 28 4 | 10 11 21 13 6 14 19 16 25 6 | 25 31 31 29 28 31 33 28 32 26 5 | 11 10 13 12 8 9 23 15 22 5 | 27 32 33 32 31 27 36 30 23 29 6 | 12 13 20 13 6 10 19 12 21 5 | 28 36 34 32 29 28 26 24 28 28 7 | 14 13 24 15 7 11 21 14 27 6 | 29 34 35 33 29 30 25 23 38 28 8 | 12 15 21 9 10 18 12 11 30 5 | 29 30 29 29 30 26 24 22 34 25 9 | 12 10 19 11 7 14 19 16 16 5 | 28 34 32 31 32 29 36 30 25 29 10 | 11 11 18 13 7 13 18 12 20 5 | 24 30 35 31 29 32 28 26 27 27 11E | 18 19 20 25 11 51 20 19 20 8 | 44 64 57 61 57 47 46 49 55 51 12 | 16 13 12 13 8 49 27 16 19 7 | 28 28 32 28 24 28 31 19 26 24 13E | 12 19 12 20 8 54 12 12 24 7 | 35 39 41 42 36 38 35 25 46 34 14E | 14 13 20 10 6 51 16 12 20 6 | 28 37 39 30 29 35 31 23 29 28 16 | 13 14 18 15 8 52 23 15 34 7 | 30 34 30 33 29 41 34 28 33 30 17 | 15 20 17 16 6 60 17 16 18 7 | 40 53 53 49 44 54 43 42 48 44 18 | 17 22 17 18 6 55 27 19 33 9 | 27 41 36 37 29 36 29 20 35 27 19 | 17 17 20 16 7 77 16 19 18 8 | 34 39 43 41 35 55 31 32 30 34 20 | 17 16 18 16 5 50 25 21 23 8 | 29 42 39 34 31 37 28 31 23 29 21 | 22 24 22 21 13 58 33 18 28 9 | 27 43 34 36 30 39 38 25 37 28 22 | 17 18 18 22 5 48 20 18 31 8 | 31 41 37 40 31 36 32 24 40 30 23E | 13 19 16 27 8 55 18 12 18 8 | 34 43 43 44 36 46 34 24 26 32 24 | 9 12 25 12 8 10 23 11 23 6 | 31 38 42 36 34 35 34 33 40 33 X25 | 16 14 23 13 6 19 23 21 --- 7 | 34 33 38 34 30 27 39 31 --- 31 26E | 12 14 22 12 8 15 19 18 23 6 | 67 70 71 76 67 70 76 66 79 70 27 | 20 14 20 11 6 21 14 10 31 6 | 32 35 35 32 32 29 27 25 28 29 28 | 15 20 15 16 6 54 27 12 60 9 | 29 37 34 31 28 33 32 29 65 29 29E | 10 10 21 12 11 12 19 16 24 6 | 70 73 65 70 74 70 73 70 57 69 30 | 11 8 30 12 6 13 20 15 43 7 | 33 34 43 39 37 30 28 35 44 32 31 | 16 16 25 14 6 54 25 18 21 8 | 29 42 48 37 33 42 34 26 24 32 X32 | 26 --- --- --- 48 36 39 52 --- 23 | 36 --- --- --- 54 26 39 53 --- 29 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 16 20 16 8 41 21 16 27 |T 33 40 40 38 35 37 35 31 36 33 WRMS | 15 16 20 16 7 41 21 13 26 |NE 29 36 36 34 31 34 32 29 33 29 MEDI | 14 14 20 14 7 36 20 16 23 |MD 29 37 36 34 31 35 34 28 34 29 Table 3.1424.2 GPS week: 1424 Day: 2 MJD: 54214.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1E | 16 16 20 13 13 25 20 12 17 6 | 30 39 41 36 31 31 35 32 31 32 2 | 13 19 21 8 9 64 23 14 23 7 | 25 38 34 29 25 47 29 23 28 25 3 | 14 20 21 12 9 19 19 11 30 6 | 23 34 35 29 25 27 36 29 33 27 4 | 12 17 25 14 7 16 19 17 29 7 | 21 28 31 24 21 27 23 24 32 21 5 | 12 14 17 10 8 12 21 13 18 5 | 24 30 31 28 30 27 30 27 23 25 6 | 17 15 24 13 6 11 24 17 21 6 | 25 32 39 26 22 26 23 27 25 24 7 | 17 17 23 13 6 8 20 11 23 6 | 28 35 39 28 25 25 25 27 31 27 8 | 9 13 26 12 7 15 14 11 30 6 | 26 30 42 27 29 24 28 29 37 26 9 | 9 22 21 13 7 14 18 13 16 6 | 28 35 36 30 28 28 33 29 28 28 10 | 14 11 21 13 8 11 14 17 21 6 | 21 24 33 26 23 27 21 26 27 22 11E | 17 22 17 22 7 56 17 12 19 8 | 40 55 47 45 45 54 38 48 45 42 12 | 17 18 19 12 9 51 28 13 18 7 | 31 31 32 27 27 37 30 23 25 25 13E | 16 18 15 29 7 58 12 11 19 8 | 30 40 41 44 31 37 35 28 36 31 14E | 17 17 22 11 6 55 9 12 13 6 | 25 32 32 23 24 36 22 26 20 23 16 | 18 18 15 14 8 51 22 15 31 7 | 27 40 31 36 31 41 37 34 35 32 17 | 15 20 20 19 8 57 16 17 18 7 | 40 51 48 41 35 51 39 31 34 38 18 | 16 23 21 18 6 57 27 16 32 9 | 23 43 35 35 25 37 28 28 32 25 19 | 17 24 19 16 8 72 17 14 18 8 | 31 41 38 37 30 54 28 32 26 32 20 | 19 19 30 18 6 52 28 14 22 8 | 31 43 37 32 27 37 27 25 24 26 21 | 17 19 22 16 9 63 29 16 24 8 | 26 35 32 31 25 40 31 26 27 24 22 | 17 25 22 21 10 50 22 15 31 8 | 25 45 40 39 28 36 25 29 29 27 23E | 14 14 19 19 9 55 18 17 21 7 | 26 36 32 32 26 35 28 27 28 24 24 | 12 13 27 13 6 10 20 11 22 6 | 30 36 41 30 30 31 28 35 34 31 X25 | 13 21 20 17 11 28 23 18 --- 7 | 38 41 48 40 35 30 34 39 --- 35 26E | 10 19 22 25 7 17 25 15 25 7 | 48 58 51 56 48 54 53 46 61 50 27 | 16 14 16 13 8 18 14 12 29 6 | 29 34 40 30 30 25 28 31 34 27 28 | 13 20 17 15 7 54 26 15 49 9 | 27 28 30 24 26 31 29 30 62 25 X29E | 20 23 32 16 11 25 25 20 --- 9 | 103 107 103 102 95 107 105 94 --- 100 30 | 13 14 19 11 8 13 25 10 32 6 | 33 35 41 33 35 32 29 34 32 31 31 | 14 19 24 18 13 53 28 17 16 8 | 27 38 39 30 30 39 36 28 28 27 X32 | 40 --- --- --- 116 57 60 84 --- 37 | 28 --- --- --- 152 31 31 129 --- 53 ------+---------------------------------------------------+---------------------------------------------------- RMS | 15 18 21 16 8 43 21 14 25 |T 31 39 39 35 35 37 33 35 32 31 WRMS | 15 18 21 16 8 43 21 13 22 |NE 27 35 37 30 33 33 29 33 31 28 MEDI | 16 18 21 14 8 50 21 14 22 |MD 28 36 38 30 29 35 29 29 31 27 Table 3.1424.3 GPS week: 1424 Day: 3 MJD: 54215.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1E | 15 16 20 15 10 21 18 14 16 6 | 25 36 33 35 32 35 37 37 32 30 2 | 13 22 14 12 5 60 24 11 25 7 | 27 34 31 29 29 48 30 29 30 26 3 | 16 17 25 12 7 20 20 15 29 7 | 22 28 28 25 24 24 31 32 37 24 4 | 13 18 20 13 7 17 20 11 27 6 | 21 28 29 24 21 34 28 23 35 22 5 | 15 13 15 12 7 10 23 8 26 5 | 20 30 29 31 26 24 27 24 30 24 6 | 14 14 22 13 6 11 30 10 18 6 | 24 24 33 25 22 23 25 24 29 21 7 | 15 15 24 12 6 11 21 7 23 6 | 26 26 31 26 23 25 22 23 34 22 8 | 9 15 18 12 6 15 8 9 27 5 | 23 32 31 25 25 25 22 26 34 23 9 | 12 15 21 12 5 14 20 13 16 5 | 26 30 30 34 29 28 32 27 28 27 10 | 13 24 22 11 4 12 20 12 17 6 | 21 36 23 25 25 25 26 27 22 21 11E | 13 24 20 33 9 55 18 14 35 9 | 32 46 43 50 37 48 33 37 42 34 12 | 16 20 19 13 7 51 27 11 21 7 | 24 30 23 27 23 39 25 27 26 22 13E | 12 16 15 18 8 55 15 11 14 6 | 26 34 35 28 26 31 26 27 30 25 14E | 18 17 19 12 5 51 10 12 18 6 | 29 37 37 32 27 37 25 30 26 28 16 | 15 17 13 13 7 56 25 15 36 8 | 30 37 30 35 31 50 34 33 39 31 17 | 14 14 24 16 7 54 20 17 17 7 | 47 51 61 54 51 62 40 53 44 49 18 | 16 26 21 18 8 55 27 15 28 8 | 20 44 30 32 25 35 28 23 26 22 19 | 19 20 20 13 6 64 17 12 16 7 | 31 38 41 34 30 54 27 33 34 32 20 | 17 17 19 16 6 52 29 19 21 8 | 26 40 32 32 28 35 30 30 21 25 21 | 15 36 24 13 10 64 26 18 28 9 | 23 58 31 32 26 35 25 33 39 27 22 | 16 25 20 20 7 53 19 14 32 8 | 25 39 34 35 28 36 27 29 36 24 23E | 16 22 19 25 7 56 25 15 17 8 | 30 36 37 42 31 44 35 29 32 29 24 | 13 12 29 13 7 10 20 11 17 6 | 29 34 36 31 27 31 30 30 37 28 X25 | 17 21 27 22 7 25 16 28 --- 9 | 26 32 45 38 27 25 33 39 --- 28 26E | 13 19 22 17 7 18 17 13 22 6 | 67 76 74 77 67 71 75 68 73 70 27 | 17 14 22 16 8 18 13 10 22 6 | 28 33 26 30 26 25 24 24 29 23 28 | 13 16 16 14 5 57 22 13 46 8 | 31 33 33 29 32 44 28 36 55 30 29E | 17 15 26 17 13 16 19 13 25 7 | 57 66 68 71 60 58 64 62 57 63 30 | 11 12 15 12 7 12 21 9 49 7 | 29 35 38 36 33 30 24 32 50 32 31 | 15 19 22 15 10 58 29 16 20 8 | 26 40 42 33 28 43 30 26 31 28 X32 | 37 --- --- --- 74 50 46 57 --- 28 | 36 --- --- --- 135 26 31 110 --- 48 ------+---------------------------------------------------+---------------------------------------------------- RMS | 15 19 20 16 7 42 21 13 26 |T 29 38 36 35 34 37 31 34 35 30 WRMS | 15 19 20 16 7 42 21 10 21 |NE 26 35 33 31 32 34 28 33 33 27 MEDI | 15 17 20 13 7 50 20 13 22 |MD 26 35 33 32 28 35 28 30 34 27 Table 3.1424.4 GPS week: 1424 Day: 4 MJD: 54216.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1E | 13 16 22 28 9 23 17 11 18 7 | 27 34 33 40 29 32 37 32 35 30 2 | 13 18 21 10 6 63 23 10 22 7 | 28 35 35 28 26 46 33 22 27 27 3 | 14 12 23 13 5 18 16 11 32 6 | 23 29 27 30 22 22 35 27 34 25 4 | 13 15 28 14 6 13 17 9 26 6 | 24 28 29 27 20 28 27 18 32 23 5 | 13 10 17 9 6 11 23 10 25 5 | 22 30 26 30 26 32 32 27 26 26 6 | 16 12 24 10 6 10 16 12 20 5 | 27 26 31 26 21 26 31 26 30 26 7 | 16 11 26 12 7 11 17 12 30 6 | 30 26 32 27 21 27 28 25 43 27 8 | 8 12 21 11 7 13 9 9 30 5 | 25 27 26 26 24 24 24 22 32 23 9 | 10 10 25 12 6 12 20 13 26 6 | 26 31 32 29 26 28 36 28 29 28 10 | 14 10 25 14 6 12 14 9 25 5 | 27 30 39 32 26 34 27 29 39 30 11E | 18 19 22 25 8 55 18 13 19 8 | 25 40 40 41 30 45 30 28 33 30 12 | 13 12 25 10 6 60 27 12 18 7 | 28 26 30 26 25 47 27 25 24 25 13E | 12 13 19 19 8 57 15 14 19 7 | 23 34 29 35 25 32 29 22 32 25 X14E | 18 15 20 14 6 53 11 11 --- 7 | 33 38 31 40 31 44 32 33 --- 33 16 | 12 13 18 11 7 57 27 17 35 7 | 27 34 30 31 29 40 36 27 37 29 17 | 17 15 15 17 8 55 21 15 26 7 | 39 46 47 47 39 55 39 42 48 42 18 | 15 22 19 16 10 57 28 17 29 8 | 21 38 30 34 25 36 29 28 25 25 19 | 16 16 19 15 6 62 18 16 15 7 | 29 38 32 40 30 51 33 31 35 32 20 | 19 18 26 18 7 56 31 14 29 8 | 26 39 34 37 28 34 31 26 35 28 21 | 17 20 14 13 6 62 21 13 25 7 | 29 35 29 29 26 34 30 29 29 27 22 | 16 18 18 19 7 50 23 16 31 8 | 23 39 33 40 30 36 27 33 29 29 23E | 12 15 15 14 5 59 19 11 17 6 | 27 40 28 36 28 41 31 27 30 30 24 | 16 15 25 13 7 13 15 9 29 6 | 22 28 28 24 19 23 23 21 31 21 25 | 9 9 27 12 6 16 16 9 24 5 | 25 29 34 26 23 26 35 23 27 26 26E | 11 16 21 17 10 18 22 17 21 6 | 57 63 66 64 55 59 73 57 64 60 27 | 12 13 20 11 4 14 18 12 21 5 | 27 29 29 24 23 24 25 26 27 24 28 | 11 15 16 11 7 52 21 11 47 7 | 35 31 30 32 31 36 32 34 61 32 X29E | 27 31 59 26 14 29 29 18 --- 12 | 94 71 75 88 88 73 84 94 --- 82 30 | 10 9 19 10 6 10 21 10 45 6 | 28 33 38 33 31 30 33 32 47 31 31 | 17 16 29 15 8 57 33 17 20 8 | 26 35 37 32 28 38 30 28 25 26 X32 | 38 --- --- --- 72 57 42 51 --- 26 | 44 --- --- --- 133 24 33 120 --- 42 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 15 22 15 7 42 21 13 27 |T 30 35 34 35 32 36 33 33 34 31 WRMS | 14 15 22 15 7 42 22 10 24 |NE 27 32 32 30 30 33 30 31 33 28 MEDI | 14 15 21 13 7 50 20 12 25 |MD 27 34 31 32 26 34 31 28 32 28 Table 3.1424.5 GPS week: 1424 Day: 5 MJD: 54217.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1E | 13 20 20 19 8 23 19 15 17 6 | 30 36 42 41 34 34 39 36 37 35 2 | 14 16 20 10 7 60 33 12 28 8 | 35 38 43 36 37 49 45 39 35 37 3 | 15 11 20 10 8 18 20 12 32 6 | 24 31 33 32 27 28 41 30 33 29 4 | 12 14 20 13 6 14 19 13 29 6 | 26 32 29 25 27 29 30 28 34 27 5 | 14 10 19 12 8 10 23 10 17 5 | 23 31 30 26 28 29 32 29 24 26 6 | 16 11 23 11 7 8 14 12 24 5 | 27 27 31 27 25 29 28 31 27 27 7 | 16 11 20 13 6 10 17 9 23 5 | 27 27 35 26 26 30 29 27 31 26 8 | 9 9 24 9 6 16 7 7 28 5 | 26 28 42 27 28 26 27 28 31 27 9 | 9 12 26 10 7 11 22 9 21 5 | 28 33 40 29 30 29 41 30 29 31 10 | 12 20 22 14 7 10 14 12 14 5 | 28 32 36 30 28 31 29 34 30 29 11E | 12 17 13 16 8 55 17 11 23 7 | 30 48 42 38 37 40 36 35 38 35 12 | 17 14 20 10 7 48 30 13 21 7 | 31 32 40 29 28 40 30 32 24 29 13E | 15 12 12 13 9 53 15 10 20 6 | 28 36 37 33 29 35 32 27 31 29 14E | 16 13 15 11 6 56 14 13 22 6 | 32 38 36 33 30 43 34 32 30 33 16 | 15 20 19 10 8 52 29 15 38 8 | 26 42 35 28 28 37 32 30 36 30 17 | 15 15 19 16 9 53 29 16 20 7 | 51 63 67 57 57 66 49 55 63 56 18 | 16 20 19 15 8 51 29 17 37 8 | 25 40 33 34 30 33 33 32 40 28 19 | 20 18 21 16 6 62 16 15 19 8 | 28 40 41 37 30 52 32 28 31 32 20 | 16 18 23 18 7 54 31 14 26 8 | 30 47 41 38 32 41 36 32 32 33 21 | 17 16 21 11 6 56 20 16 42 8 | 27 32 37 31 31 34 28 34 42 29 22 | 18 18 20 19 8 51 25 19 47 9 | 28 41 35 37 33 36 35 33 51 31 23E | 15 18 14 16 8 53 17 13 26 7 | 37 47 44 42 37 49 37 38 31 39 24 | 15 14 26 11 6 12 18 11 28 6 | 30 38 39 33 32 34 32 34 40 32 25 | 8 9 23 10 4 14 16 11 18 5 | 28 33 37 27 28 27 36 28 36 30 26E | 10 9 24 14 9 16 23 16 23 6 | 70 72 78 70 70 75 84 66 78 71 27 | 16 10 20 11 4 13 13 9 19 5 | 36 32 37 30 31 28 31 31 32 31 28 | 12 14 20 12 6 54 22 12 35 7 | 35 37 34 31 33 37 29 37 44 33 29E | 12 12 30 19 8 18 22 20 28 7 | 49 53 68 49 48 49 55 45 68 49 30 | 11 9 11 12 7 11 24 11 55 7 | 26 31 34 28 29 28 27 29 58 27 31 | 14 16 22 13 7 55 31 17 20 8 | 27 37 39 31 30 37 32 29 25 29 X32 | 11 --- --- --- 515 35 --- 474 --- 18 | 36 --- --- --- 444 26 --- 412 --- 29 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 15 21 14 7 40 22 13 28 |T 31 38 40 34 46 37 36 46 38 33 WRMS | 14 15 21 13 7 40 21 11 23 |NE 29 35 37 31 48 34 33 48 36 30 MEDI | 15 14 20 12 7 35 20 13 23 |MD 28 36 37 31 30 34 32 32 33 30 Table 3.1424.6 GPS week: 1424 Day: 6 MJD: 54218.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1E | 16 12 14 16 7 20 22 12 18 6 | 29 38 40 34 31 31 36 35 38 32 2 | 12 14 23 9 7 63 27 12 26 7 | 26 33 33 29 27 46 35 25 33 27 3 | 12 10 20 11 7 16 23 13 37 6 | 25 31 34 28 25 29 37 31 32 27 4 | 15 14 23 11 6 15 18 11 30 6 | 22 29 29 24 23 30 27 24 36 23 5 | 16 12 20 10 7 9 26 14 20 6 | 26 35 37 34 36 30 34 35 24 30 6 | 15 15 20 9 5 9 19 11 18 5 | 31 30 35 27 26 30 25 31 33 28 7 | 16 15 18 10 5 9 20 13 20 5 | 35 32 38 29 29 31 29 31 37 30 8 | 12 11 20 8 7 14 14 11 30 5 | 24 29 36 26 26 23 24 28 27 24 9 | 11 11 26 9 9 13 33 13 28 6 | 29 31 37 32 32 28 40 36 33 30 10 | 17 11 23 12 7 12 17 11 18 5 | 26 28 31 29 27 30 25 31 28 27 11E | 12 15 15 15 8 50 15 14 12 6 | 46 58 58 52 51 51 49 46 48 50 12 | 15 13 21 8 7 49 33 14 23 7 | 34 31 35 32 33 57 32 34 26 30 13E | 16 14 15 16 10 51 14 12 25 6 | 32 41 44 39 35 41 35 35 30 34 14E | 18 16 17 11 7 58 16 10 21 7 | 37 44 41 33 34 46 29 37 27 35 16 | 11 13 14 9 9 55 30 16 40 7 | 34 39 35 35 34 56 39 35 47 35 17 | 16 16 21 14 7 55 29 17 18 7 | 57 65 74 68 64 76 50 65 60 63 18 | 15 19 18 15 7 57 33 15 35 8 | 25 38 36 35 29 39 28 30 30 27 19 | 19 19 21 12 5 66 22 15 16 8 | 35 48 49 43 36 64 32 35 36 38 20 | 15 16 21 15 8 52 31 12 37 8 | 34 45 40 35 34 41 37 33 36 33 21 | 19 23 19 11 9 57 22 16 28 8 | 30 38 32 27 27 36 23 30 25 25 22 | 19 22 21 17 8 52 27 14 36 8 | 30 42 38 36 32 38 27 32 38 28 23E | 16 18 15 16 8 59 17 13 27 7 | 36 46 47 42 38 48 32 39 38 38 24 | 15 15 26 12 8 12 22 12 24 6 | 33 35 45 31 30 35 36 35 40 33 25 | 9 12 25 9 6 17 16 11 20 5 | 26 31 35 30 29 29 31 31 25 28 26E | 11 14 26 12 8 16 26 17 19 6 | 68 74 77 69 70 73 74 68 74 70 27 | 11 10 21 10 8 14 16 9 23 5 | 25 29 31 23 23 25 27 23 26 23 28 | 12 15 19 9 7 54 24 11 34 7 | 39 35 40 34 36 49 29 37 36 33 29E | 23 25 40 13 9 22 28 20 32 9 | 81 100 106 88 89 97 94 93 72 90 30 | 11 12 20 10 8 10 25 12 52 7 | 34 40 48 41 42 36 33 42 55 38 31 | 16 16 18 13 9 56 29 16 26 7 | 28 37 41 29 28 47 31 31 33 29 X32 | 20 --- --- --- 19 60 --- 21 --- 19 | 33 --- --- --- 125 25 --- 122 --- 31 ------+---------------------------------------------------+---------------------------------------------------- RMS | 15 15 21 12 7 41 24 13 28 |T 34 41 43 37 38 42 36 40 37 35 WRMS | 14 15 20 12 7 41 24 12 25 |NE 30 36 38 32 35 38 31 36 34 30 MEDI | 15 14 20 11 7 49 22 13 25 |MD 32 37 38 33 32 38 32 35 33 30 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 4.1424 GPS week: 1424 MJD: 54212.0-54218.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2941 |U 19 24 39 |U 14 23 41 |U 15 10 25 | emr | emr 2879 |U 20 22 38 |U 13 15 51 | 20 9 31 | esa | esa 2778 | 20 15 45 |U 16 27 46 | 19 9 30 | gfz | gfz 2851 |U 19 21 41 |U 15 19 48 |U 19 9 28 | igr | igr 2930 | 23 24 49 | 15 20 45 | 22 11 34 | igs | igs 2946 | 22 26 45 | 14 18 42 | 21 11 35 | jpl | jpl 2948 | 27 28 49 | 16 15 48 | 18 15 31 | mit | mit 2948 |U 19 24 38 |U 14 16 53 |U 13 9 23 | 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 5.1424.0 GPS week: 1424 Day: 0 MJD: 54212.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2954 | 10 11 23 | 14 25 41 | 16 12 25 | emr | emr 2876 | 14 8 33 | 13 13 53 | 20 11 29 | esa | esa 2780 | 12 12 35 | 17 28 49 | 21 11 34 | gfz | gfz 2852 | 9 8 31 | 15 13 52 | 20 12 30 | igr | igr 2926 | 23 18 49 | 14 14 48 | 21 16 37 | igs | igs 2931 | 20 15 37 | 13 14 46 | 27 17 48 | jpl | jpl 2950 | 15 6 29 | 16 13 51 | 19 15 27 | mit | mit 2976 | 9 8 24 | 15 12 51 | 16 10 25 | Table 5.1424.1 GPS week: 1424 Day: 1 MJD: 54213.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2924 | 14 12 31 | 14 23 50 | 15 11 27 | emr | emr 2880 | 15 7 31 | 12 16 56 | 20 11 30 | esa | esa 2784 | 20 10 48 | 15 27 56 | 24 10 33 | gfz | gfz 2857 | 19 10 44 | 14 14 61 | 21 11 30 | igr | igr 2927 | 16 18 36 | 13 18 51 | 23 11 33 | igs | igs 2959 | 20 21 37 | 12 18 49 | 22 13 33 | jpl | jpl 2957 | 30 16 53 | 16 16 49 | 20 17 27 | mit | mit 2976 | 16 9 34 | 15 18 56 | 17 14 36 | Table 5.1424.2 GPS week: 1424 Day: 2 MJD: 54214.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2945 | 32 53 70 | 12 22 37 | 13 16 24 | emr | emr 2880 | 29 56 57 | 12 12 56 | 18 8 31 | esa | esa 2781 | 37 29 91 | 14 29 41 | 16 7 29 | gfz | gfz 2852 | 38 62 73 | 14 16 51 | 16 7 27 | igr | igr 2937 | 39 22 87 | 15 21 40 | 20 11 33 | igs | igs 2954 | 32 19 76 | 13 17 43 | 16 9 34 | jpl | jpl 2956 | 32 84 80 | 15 14 42 | 14 17 28 | mit | mit 2976 | 34 75 71 | 13 15 56 | 13 9 25 | Table 5.1424.3 GPS week: 1424 Day: 3 MJD: 54215.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2937 | 16 11 40 | 14 21 41 | 15 8 24 | emr | emr 2880 | 15 11 36 | 14 13 58 | 23 9 35 | esa | esa 2784 | 18 9 41 | 17 26 51 | 20 7 31 | gfz | gfz 2851 | 16 11 35 | 19 23 43 | 22 9 28 | igr | igr 2917 | 17 11 45 | 17 24 50 | 24 11 37 | igs | igs 2946 | 17 13 39 | 16 17 39 | 23 10 33 | jpl | jpl 2954 | 25 10 49 | 16 13 56 | 17 16 31 | mit | mit 2976 | 16 9 36 | 15 14 57 | 19 10 33 | Table 5.1424.4 GPS week: 1424 Day: 4 MJD: 54216.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2945 | 15 10 46 | 17 24 44 | 16 6 24 | emr | emr 2880 | 19 13 50 | 14 15 44 | 22 7 30 | esa | esa 2755 | 19 11 47 | 18 27 42 | 19 7 31 | gfz | gfz 2844 | 16 13 47 | 14 16 48 | 20 6 28 | igr | igr 2919 | 20 19 52 | 17 21 48 | 28 8 42 | igs | igs 2952 | 15 14 43 | 13 20 42 | 21 6 34 | jpl | jpl 2948 | 25 16 53 | 17 21 48 | 19 14 35 | mit | mit 2976 | 16 11 46 | 14 18 57 | 0 0 0 | Table 5.1424.5 GPS week: 1424 Day: 5 MJD: 54217.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2942 | 37 63 45 | 14 23 38 | 16 9 29 | emr | emr 2880 | 36 45 40 | 11 22 50 | 21 8 32 | esa | esa 2784 | 23 19 35 | 15 26 42 | 20 9 30 | gfz | gfz 2852 | 27 39 37 | 15 26 43 | 21 8 28 | igr | igr 2942 | 36 57 46 | 15 23 45 | 21 11 31 | igs | igs 2942 | 38 79 58 | 14 21 41 | 23 8 32 | jpl | jpl 2958 | 44 56 53 | 15 16 48 | 20 14 43 | mit | mit 2880 | 27 40 37 | 14 17 59 | 15 8 27 | Table 5.1424.6 GPS week: 1424 Day: 6 MJD: 54218.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2946 | 10 10 21 | 15 25 34 | 12 10 25 | emr | emr 2880 | 11 16 22 | 13 16 42 | 18 13 28 | esa | esa 2784 | 10 12 21 | 16 28 44 | 15 10 22 | gfz | gfz 2853 | 11 8 20 | 16 23 40 | 14 10 25 | igr | igr 2946 | 13 22 27 | 15 22 35 | 18 10 25 | igs | igs 2944 | 13 21 26 | 16 21 36 | 18 10 32 | jpl | jpl 2916 | 17 9 27 | 15 14 42 | 15 15 30 | mit | mit 2880 | 12 14 19 | 14 16 37 | 13 9 20 | 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 6.1424 GPS week: 1424 MJD: 54212.500-54218.500 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 | -12 -59 62 -84 4 | -7 14 | 27 14 38 63 5 | 2 emr uuuuu | 37 33 -78 274 -15 | 79 81 | 22 40 100 167 13 | 3 esa uuuux | 2 -2 41 -80 5 | 1 28 | 49 21 58 69 25 | 8 gfz uuuuu | 17 -12 -44 -36 -11 | 24 29 | 11 25 44 62 5 | 2 igr xxxxx | -6 -32 -18 -36 -7 | 4 16 | 21 18 68 32 5 | 2 irf xxxxx | -2 5 74 -58 -12 | 1 19 | 14 10 38 76 7 | 3 jpl uuxux | -14 2 -46 39 -52 | -5 44 | 25 20 283 127 32 | 10 mit uuuuu | -5 -53 89 -51 -23 | 49 54 | 44 38 53 95 9 | 4 ngs uuuuu | -46 66 -45 -38 3 | 12 16 | 24 56 134 93 7 | 2 sio uuuuu | 31 19 82 -51 -15 | 48 52 | 42 24 115 101 9 | 3 Table 7.1424.0 GPS week: 1424 Day: 0 MJD: 54212.500 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 | 26 -47 82 17 8 | -10 15 emr uuuuu | 54 113 -1 16 4 | 78 79 esa uuuux | 99 3 -71 -18 47 | -12 31 gfz uuuuu | 22 -48 -6 -79 -5 | 23 28 igr xxxxx | -16 -39 -147 -37 2 | 2 15 irf xxxxx | -25 -5 80 80 2 | -2 20 jpl uuxux | -6 28 -612 -146 -17 | 5 33 mit uuuuu | -76 -87 9 56 -10 | 48 54 ngs uuuuu | -82 57 -103 27 -4 | 8 13 sio uuuuu | -44 1 182 126 -1 | 47 51 Table 7.1424.1 GPS week: 1424 Day: 1 MJD: 54213.500 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 | 9 -77 -6 -67 -1 | -8 15 emr uuuuu | 23 7 -216 287 -8 | 80 82 esa uuuux | 28 -7 38 9 13 | -6 33 gfz uuuuu | 26 -41 -123 -24 -10 | 24 29 igr xxxxx | 18 -60 -28 -39 -5 | 4 15 irf xxxxx | -6 -5 41 -64 -9 | 1 20 jpl uuxux | 26 15 -172 16 -22 | 4 33 mit uuuuu | -44 -64 137 7 -19 | 50 55 ngs uuuuu | -67 164 253 -201 5 | 10 14 sio uuuuu | 15 24 17 -62 -10 | 48 52 Table 7.1424.2 GPS week: 1424 Day: 2 MJD: 54214.500 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 | -29 -61 89 -93 4 | -5 13 emr uuuuu | 39 26 -185 421 -3 | 82 84 esa uuuux | 0 33 67 -122 2 | 0 32 gfz uuuuu | 2 -15 -38 7 -14 | 27 31 igr xxxxx | -37 -46 -33 -90 -13 | 7 15 irf xxxxx | 4 14 124 -105 -11 | 5 16 jpl uuxux | -21 16 -81 121 -57 | 4 33 mit uuuuu | 15 -10 127 -106 -16 | 53 56 ngs uuuuu | -34 15 -113 -97 0 | 14 17 sio uuuuu | 51 47 200 -100 -12 | 51 54 Table 7.1424.3 GPS week: 1424 Day: 3 MJD: 54215.500 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 | -57 -42 40 -100 12 | -8 14 emr uuuuu | 62 48 -26 520 -27 | 80 82 esa uuuux | -46 3 26 -168 18 | -1 32 gfz uuuuu | 23 -8 -15 -140 -13 | 24 29 igr xxxxx | -1 -11 50 -32 -7 | 4 16 irf xxxxx | -4 17 51 -140 -19 | 2 18 jpl uuxux | -28 -10 119 173 -102 | -3 40 mit uuuuu | -2 -4 30 -132 -30 | 51 55 ngs uuuuu | -15 -11 -57 40 -7 | 12 17 sio uuuuu | 86 50 60 -143 -17 | 48 52 Table 7.1424.4 GPS week: 1424 Day: 4 MJD: 54216.500 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 | -4 -65 102 -148 -2 | -4 12 emr uuuuu | 22 27 -6 281 -23 | 81 82 esa uuuux | -20 -40 64 -121 -4 | 8 23 gfz uuuuu | 13 -7 -88 41 -2 | 26 29 igr xxxxx | 7 -10 59 22 -7 | 6 15 irf xxxxx | 14 0 49 -73 -16 | 4 17 jpl uuxux | -35 -12 187 79 -83 | -8 48 mit uuuuu | 17 -67 70 -174 -31 | 51 55 ngs uuuuu | -37 91 -57 21 10 | 14 17 sio uuuuu | 54 9 -61 -119 -25 | 50 53 Table 7.1424.5 GPS week: 1424 Day: 5 MJD: 54217.500 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 | -19 -49 83 -31 5 | -6 14 emr uuuuu | 57 20 -141 252 -19 | 78 80 esa uuuux | -37 -2 116 -15 -10 | 9 22 gfz uuuuu | 5 11 -13 -64 -17 | 24 29 igr xxxxx | 14 -30 1 -43 -6 | 3 16 irf xxxxx | -13 -3 128 -110 -19 | 1 19 jpl uuxux | 8 5 58 147 -52 | -15 58 mit uuuuu | -7 -102 114 -74 -31 | 47 54 ngs uuuuu | -24 77 -125 -87 4 | 13 16 sio uuuuu | 13 -18 212 -111 -26 | 47 52 Table 7.1424.6 GPS week: 1424 Day: 6 MJD: 54218.500 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 | -8 -76 44 -162 -1 | -7 14 emr uuuuu | 3 -11 30 143 -31 | 74 77 esa uuuux | -7 -3 50 -123 -33 | 8 22 gfz uuuuu | 30 20 -28 8 -14 | 20 26 igr xxxxx | -26 -26 -29 -33 -13 | 1 16 irf xxxxx | 15 13 43 4 -14 | -2 21 jpl uuxux | -43 -29 176 -117 -31 | -22 63 mit uuuuu | 60 -36 134 68 -26 | 42 51 ngs uuuuu | -59 68 -110 35 12 | 12 16 sio uuuuu | 45 22 -34 53 -13 | 43 50