Date: Thu, 01 Mar 2007 13:40:14 +0100 To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-14834] Wk 1414 IGS Final Orbits Message-ID: <45E6C9AE.mailxGC811FTRX@kg20> User-Agent: nail 10.6 11/15/03 Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: 7bit From: igsacc@gfz-potsdam.de (Gerd Gendt3) Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 01 Mar 04:40:24 PST 2007 Message Number 14834 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1414 (Feb 11, 2007 - Feb 17, 2007) Contacts: G. Gendt (gendt@gfz-potsdam.de), Th. Nischan ( nisn@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: igs1414[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1414[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1414[0-6].cls IGS GPS clock combination summary report. igs14147.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14147.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 | ESA | ZAMB 0 | GFZ | QAQ1 0 | MIT | BAHR 1 | COD | QAQ1 1 | GFZ | GRAZ 1 | JPL | 18 20 23 NISU 1 | MIT | 15 BAHR BOR1 2 | ESA | RBAY 2 | GFZ | BILI KERG 2 | JPL | NISU 2 | MIT | BOR1 SANT VILL 3 | COD | YELL 3 | ESA | MAW1 3 | MIT | 15 20 ARTU BAHR MAW1 4 | COD | BRFT 4 | ESA | IRKT 4 | JPL | DARW KERG 4 | MIT | 15 BAHR 5 | ESA | POL2 UNSA 5 | JPL | 20 NISU 5 | MIT | 15 BAHR KOUR MAS1 6 | COD | MCM4 6 | ESA | 28 LPGS 6 | MIT | 28 BAHR KOUR 5. 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 G28 | | | | | | | 4 | PRN G29 | | | 4 | | | | | 6. 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. 7. 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 | .0 .1 .4 6 -5 -2 -.09 EMR | -8.4 -11.2 1.3 -5 5 31 .11 ESA | -5.2 3.6 -9.4 -7 -29 -10 -.92 GFZ | .4 -.1 .9 -9 -4 2 -.40 JPL | -7.0 3.8 12.9 173 -63 245 .36 MIT | -7.0 1.9 .6 -12 4 -9 .25 NGS | 5.1 3.7 -3.9 53 -85 0 -.93 8. 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. 9. 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. 10. 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 1.1414.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1414.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 2.1414.[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 3.1414.[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 5.1414.0-6). 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 1414 summary. (Feb 11, 2007 - Feb 17, 2007) Table 1.1414.a GPS week: 1414 MJD: 54142.000-54148.000 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 173| 1 0 -2 -11 0 -51 -.35 15 14 | -358 -397 51 92 | 0 1 0 23 17 21 .02 | 532 961 emr 52| 0 0 1 -9 -31 -59 .24 15 15 | -158952 -2797 54 92 | 1 1 1 19 15 21 .03 | 6608 1649 esa 65| 1 2 2 65 2 -52 .17 24 22 | 7940 -732 56 136 | 1 2 2 82 32 71 .04 | 2517 1450 gfz 187| 0 -1 2 55 -22 33 .01 15 14 | -99 143 30 119 | 1 0 1 12 26 56 .03 | 314 505 igr n/a| 1 0 0 10 -49 -6 -.01 8 7 | -14065 -407 34 72 | 0 0 0 18 23 17 .03 | 2261 1502 jpl n/a| -5 -4 -8 -182 -10 272 .01 41 41 | 5969 -625 93 146 | 4 5 5 30 51 31 .02 | 2298 1404 mit 159| 0 1 -3 36 -57 -7 .03 25 22 | -456 344 72 142 | 1 1 1 53 39 31 .02 | 797 693 ngs 169| 0 1 0 -66 106 59 -.07 18 13 | -272 -219 2371 4242 | 1 1 3 25 32 20 .03 | 361 845 Table 1.1414.b GPS week : 1414 MJD: 54142.000-54148.000 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 | 7 6 6 7 9 6 7 | 2 | 9 9 8 8 9 7 9 | 3 | 7 5 6 6 8 7 6 | 4 | 6 5 5 6 6 6 6 | 5E | 9 8 8 8 8 8 8 | 6 | 5 6 6 6 8 7 7 | 7 | 5 6 6 6 7 7 7 | 8 | 6 7 6 6 6 6 7 | 9 | 5 6 6 5 7 6 8 | 10 | 8 7 7 7 8 8 7 | 11 | 8 7 7 9 9 8 9 | 12E | 10 7 8 8 9 8 9 | 13 | 10 8 9 9 9 9 9 | 14 | 9 9 15 9 10 9 8 | 15 | 13 15 10 11 11 14 16 | 16E | 8 7 7 7 8 7 9 | 17 | 10 9 10 10 10 10 11 | 18 | 8 8 8 8 12 8 10 | 19 | 10 9 9 9 9 9 9 | 20 | 8 8 8 9 9 9 11 | 21 | 10 8 7 8 9 8 8 | 22 | 7 7 8 8 9 8 11 | 23 | 9 8 9 10 9 9 9 | 24 | 5 5 5 5 6 6 6 | 25 | 6 6 5 5 6 6 6 | 26 | 6 6 8 6 8 7 10 | 27 | 7 6 7 6 6 7 6 | 28E | 9 10 8 8 8 8 37 | 29 | 6 6 8 7 10 7 12 | 30E | 9 8 9 9 8 8 8 | 31 | 10 9 9 9 9 9 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 2.1414.0 GPS week: 1414 Day: 0 MJD: 54142.000 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 173| 1 -1 -3 -38 25 -76 -.33 15 15 | -1077 -707 61 116 | 88 -24 | emr 52| 2 0 2 -9 -55 -102 .20 15 15 | -151867 -2126 62 123 | 126 -5 | esa 65| 1 4 2 87 15 -38 .17 20 20 | 8542 -81 52 123 | 23 -8 | gfz 187| -1 -1 1 66 -20 105 .02 15 15 | -237 -15 30 111 | -15 6 | igr n/a| 1 0 -1 11 -11 -33 .03 8 8 | -13892 306 36 69 | 79 4 | jpl n/a| -7 -9 -3 -229 64 229 -.01 41 41 | 6325 32 93 163 | 92 -38 | mit 159| 0 0 -3 91 -41 3 .06 25 23 | -2076 408 73 171 | -24 8 | ngs 169| 0 2 0 -84 77 48 -.08 15 13 | -289 323 2463 3882 | -39 63 | Table 2.1414.1 GPS week: 1414 Day: 1 MJD: 54143.000 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 173| 1 0 -3 15 5 -81 -.35 12 12 | 352 -1180 44 84 | 51 -23 | emr 52| 0 0 0 -25 -28 -58 .23 13 13 | -152751 -316 50 83 | 113 0 | esa 65| 3 0 5 -6 22 5 .25 22 22 | 9843 1441 56 137 | -13 16 | gfz 187| -1 -2 3 59 -65 68 .04 16 16 | 107 296 27 110 | 26 35 | igr n/a| 2 0 0 36 -34 -24 .01 6 6 | -12302 1762 32 74 | 12 11 | jpl n/a| -9 -2 -2 -183 32 257 -.01 38 38 | 7654 1466 77 134 | 67 -21 | mit 159| 1 0 -5 81 -70 -57 .01 22 21 | -530 946 61 153 | -23 0 | ngs 169| 0 2 1 -43 134 53 -.07 15 12 | 270 -1101 2732 5219 | -121 -11 | Table 2.1414.2 GPS week: 1414 Day: 2 MJD: 54144.000 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 173| 2 0 -1 3 -19 -24 -.32 13 13 | -830 1349 52 82 | 34 8 | emr 52| -1 0 1 -38 -31 -67 .21 18 18 | -155574 -1722 51 76 | 110 -19 | esa 65| 0 4 5 210 -44 -125 .17 27 24 | 9713 21 57 134 | -39 70 | gfz 187| 0 -2 3 56 -10 64 .04 14 14 | -549 656 40 160 | 2 14 | igr n/a| 1 -1 0 12 -63 -13 .03 7 6 | -12561 265 37 74 | 10 37 | jpl n/a| -4 -9 0 -173 -2 245 .02 40 40 | 7316 111 98 139 | 59 -7 | mit 159| 3 0 -4 -41 -27 -34 .01 21 20 | -223 1071 74 122 | 62 -20 | ngs 169| 0 2 -5 -46 98 27 -.01 15 12 | -821 769 2389 4358 | -141 52 | Table 2.1414.3 GPS week: 1414 Day: 3 MJD: 54145.000 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 173| 1 1 -2 18 -11 -28 -.34 14 13 | -663 -866 42 77 | 54 2 | emr 52| 0 0 -1 -15 -16 -57 .27 14 14 | -156970 -3199 58 98 | 26 -30 | esa 65| 1 4 0 1 2 -147 .14 21 21 | 9790 -769 60 144 | 11 -5 | gfz 187| -1 0 3 51 -11 57 .01 13 13 | -357 424 29 115 | -7 5 | igr n/a| 1 0 0 25 -54 4 -.01 8 7 | -12300 -646 33 76 | -9 -23 | jpl n/a| 2 -12 -15 -177 -5 284 .00 41 41 | 7859 -1036 103 159 | 5 -22 | mit 159| 0 2 -4 54 -114 28 .02 25 23 | -670 -699 73 137 | 0 53 | ngs 169| 0 0 3 -72 121 49 -.12 18 14 | -581 671 2312 4004 | -8 -16 | Table 2.1414.4 GPS week: 1414 Day: 4 MJD: 54146.000 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 173| 2 0 -2 -19 18 -55 -.34 17 15 | -233 -193 60 110 | 61 -19 | emr 52| 0 1 0 8 -8 -39 .25 15 15 | -160114 -5603 55 91 | 63 -26 | esa 65| 1 0 3 79 -10 -93 .18 23 23 | 8956 -3197 59 133 | -18 -90 | gfz 187| -1 0 3 29 -47 7 .00 14 14 | 37 205 31 116 | 7 27 | igr n/a| 1 0 1 13 -61 11 -.06 8 8 | -12917 -3126 37 68 | 12 31 | jpl n/a| -9 -1 -15 -160 -21 319 .01 39 39 | 7149 -3059 100 144 | 19 13 | mit 159| 0 1 -4 -33 -99 18 .03 26 24 | 295 125 80 146 | 38 26 | ngs 169| 1 1 2 -40 151 85 -.09 21 16 | -312 -86 2306 4102 | -123 -19 | Table 2.1414.5 GPS week: 1414 Day: 5 MJD: 54147.000 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 173| 1 -1 -3 -32 -1 -43 -.38 16 16 | 228 -1443 43 81 | 81 -13 | emr 52| 0 2 4 21 -32 -47 .24 14 14 | -166323 -3369 57 93 | 71 -33 | esa 65| 2 0 0 -23 56 48 .15 21 21 | 5067 -1623 53 135 | -21 -51 | gfz 187| 0 -1 2 62 -17 -61 .01 13 13 | 395 -905 30 113 | 0 13 | igr n/a| 1 0 0 -5 -82 0 -.03 7 7 | -16659 -1065 33 68 | 48 39 | jpl n/a| -9 0 -8 -140 -42 273 .05 40 40 | 3494 -1250 87 139 | 29 -20 | mit 159| 0 1 -2 44 -36 11 .03 24 22 | -215 -369 69 125 | 7 -5 | ngs 169| 1 0 -4 -70 59 73 -.09 17 11 | 20 -1192 2466 4248 | -130 134 | Table 2.1414.6 GPS week: 1414 Day: 6 MJD: 54148.000 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 173| 1 1 -3 -26 -16 -52 -.37 20 15 | -289 259 57 94 | 67 -6 | emr 52| -1 1 2 -9 -45 -46 .28 17 17 | -169071 -3249 49 84 | 61 -5 | esa 65| 0 5 1 112 -24 -16 .16 34 23 | 3675 -916 58 150 | -40 13 | gfz 187| 1 -1 0 62 17 -5 -.05 21 14 | -92 342 29 110 | 22 14 | igr n/a| 1 0 0 -18 -38 7 -.04 12 8 | -17824 -345 35 77 | 52 2 | jpl n/a| -3 0 -9 -211 -95 299 .02 45 45 | 1991 -643 95 147 | 58 61 | mit 159| -1 2 -1 55 -9 -19 .04 36 24 | 227 931 80 146 | 5 -13 | ngs 169| 2 0 2 -109 102 80 -.05 28 15 | -195 -917 1929 3885 | -54 81 | 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 3.1414.0 GPS week: 1414 Day: 0 MJD: 54142.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs IGS | cod emr esa gfz igr jpl mit ngs IGS ------+----------------------------------------------+----------------------------------------------- 1 | 11 11 28 12 6 30 23 10 6 | 29 38 43 28 31 40 28 27 27 2 | 12 16 24 13 10 62 35 16 9 | 35 52 47 43 41 63 37 39 39 3 | 12 14 22 12 10 13 25 18 6 | 23 29 28 29 26 30 35 25 24 4 | 9 12 12 11 8 14 29 14 6 | 36 43 33 39 39 41 29 38 34 5E | 16 22 23 22 10 18 23 21 8 | 39 46 51 53 46 45 43 45 41 6 | 10 11 18 8 6 14 21 11 5 | 28 30 37 32 31 35 31 26 27 7 | 10 11 19 8 7 11 20 13 5 | 37 39 45 38 42 46 39 42 38 8 | 11 10 20 9 10 14 20 13 5 | 24 33 34 35 34 30 38 25 27 9 | 13 8 20 12 6 12 16 10 5 | 21 34 41 32 29 27 24 27 26 10 | 20 16 21 12 8 19 31 12 7 | 22 30 31 25 24 37 39 20 22 11 | 16 14 16 17 10 53 17 12 7 | 43 60 54 49 47 42 46 45 46 12E | 17 16 20 36 11 55 19 18 10 | 26 32 33 60 37 36 30 31 30 13 | 19 26 20 16 7 59 23 16 9 | 26 36 41 29 27 39 20 16 23 14 | 18 16 20 16 8 54 21 15 8 | 25 43 40 36 30 41 24 24 27 X15 | 22 33 --- 16 18 18 46 28 12 | 33 57 --- 22 40 51 33 38 38 16E | 18 16 14 18 9 51 17 17 8 | 22 29 28 34 28 32 25 20 22 17 | 22 17 22 17 6 63 26 19 9 | 27 45 40 35 30 55 36 24 29 18 | 13 16 15 8 6 55 19 15 7 | 25 43 35 30 30 46 25 27 27 19 | 16 16 19 14 12 49 43 24 9 | 26 45 41 38 36 45 43 28 31 20 | 17 17 17 11 7 59 24 14 8 | 30 49 40 39 37 50 42 32 35 21 | 20 12 24 14 8 55 40 16 9 | 32 45 37 37 33 41 39 31 33 22 | 13 14 15 8 6 50 17 13 6 | 27 37 36 32 31 42 28 28 28 23 | 13 15 23 14 8 62 21 15 8 | 30 40 43 31 32 47 33 21 28 24 | 9 13 16 11 6 10 14 13 5 | 32 41 30 40 36 38 32 33 33 25 | 11 13 18 10 7 21 25 14 6 | 31 39 43 35 33 36 36 29 31 26 | 14 10 17 14 8 11 21 11 5 | 27 31 35 26 29 26 32 18 23 27 | 16 12 23 10 9 14 25 13 6 | 28 34 40 32 33 33 34 25 27 28E | 16 15 12 22 7 55 18 17 8 | 19 32 27 36 28 32 28 18 21 29 | 14 12 22 13 9 11 21 14 6 | 38 41 49 40 41 37 51 37 38 30E | 22 19 24 20 12 17 27 17 8 | 65 67 67 74 70 69 68 68 66 31 | 14 19 27 19 6 54 30 19 9 | 25 44 42 42 30 51 29 23 29 ------+----------------------------------------------+----------------------------------------------- RMS | 15 15 20 15 8 41 25 15 |T 30 40 39 37 34 41 34 30 31 WRMS | 15 15 20 15 8 41 23 13 |NE 29 40 39 34 33 41 33 28 30 MEDI | 14 15 20 13 8 30 23 15 |MD 28 40 40 35 33 41 33 27 29 Table 3.1414.1 GPS week: 1414 Day: 1 MJD: 54143.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs IGS | cod emr esa gfz igr jpl mit ngs IGS ------+----------------------------------------------+----------------------------------------------- 1 | 9 10 32 11 4 14 18 12 6 | 27 33 42 34 31 39 29 28 28 2 | 12 13 21 14 7 60 32 16 8 | 30 46 42 38 36 57 32 35 35 3 | 9 9 21 14 8 9 17 11 5 | 26 28 31 29 26 28 32 22 24 4 | 9 11 13 10 8 13 26 8 5 | 33 39 36 38 36 37 36 33 32 5E | 14 15 32 23 8 12 20 18 8 | 37 45 46 47 40 45 44 39 39 6 | 10 9 21 11 7 8 24 14 5 | 25 26 26 28 27 25 29 22 22 7 | 9 8 23 13 7 7 24 12 5 | 39 37 41 39 38 38 33 35 34 8 | 11 10 28 14 6 16 24 13 6 | 22 26 35 30 25 29 31 24 22 9 | 10 10 28 14 5 13 15 16 6 | 27 32 36 30 29 29 29 26 25 10 | 14 12 23 14 5 11 28 16 7 | 27 35 32 29 27 35 41 21 26 11 | 12 14 15 17 6 45 20 13 7 | 34 49 41 41 39 39 36 35 37 12E | 14 13 16 14 6 50 15 14 7 | 25 33 28 27 25 30 29 22 24 13 | 12 15 19 15 5 54 20 18 8 | 24 37 39 29 26 37 22 19 23 14 | 16 14 29 17 5 56 16 18 8 | 25 37 50 36 31 38 26 26 27 X15 | 22 38 --- --- 20 30 41 20 15 | 34 46 --- --- 39 44 37 33 32 16E | 14 14 11 17 6 46 17 14 7 | 26 32 26 33 25 32 30 22 24 17 | 17 13 32 18 7 54 25 15 9 | 24 35 39 37 29 38 29 21 25 18 | 13 16 17 12 4 56 20 16 7 | 26 42 34 32 29 44 23 24 27 19 | 15 15 22 19 8 50 40 19 9 | 28 40 39 38 33 42 39 23 29 20 | 14 13 20 12 5 57 24 15 8 | 29 38 39 37 30 48 33 20 29 21 | 11 12 16 14 5 52 24 16 7 | 29 36 35 32 31 33 28 27 28 22 | 12 14 19 10 6 51 15 15 7 | 29 40 41 34 32 40 31 27 29 23 | 13 15 25 14 5 59 18 16 8 | 29 37 39 35 29 45 30 23 28 24 | 7 9 12 13 6 7 14 13 4 | 25 32 24 28 26 31 24 24 24 25 | 8 9 22 13 8 13 21 10 5 | 31 35 34 34 32 34 35 28 29 26 | 10 6 23 15 4 9 20 15 5 | 28 30 32 30 27 30 35 23 25 27 | 8 11 23 14 5 16 26 12 6 | 23 25 34 29 24 31 35 20 22 28E | 15 17 18 35 8 54 18 22 10 | 22 32 31 46 26 33 28 23 23 29 | 11 9 20 15 3 8 20 17 6 | 44 47 44 44 45 45 51 42 42 30E | 21 16 23 23 7 13 19 16 8 | 42 53 43 56 48 49 49 45 45 31 | 15 16 19 22 8 52 26 20 9 | 26 40 43 43 32 44 30 25 29 ------+----------------------------------------------+----------------------------------------------- RMS | 12 13 22 16 6 38 22 15 |T 28 36 36 35 31 37 32 27 28 WRMS | 12 13 22 16 6 38 21 12 |NE 28 36 37 34 31 37 32 26 28 MEDI | 12 13 21 14 6 30 20 15 |MD 27 37 36 34 30 38 31 24 28 Table 3.1414.2 GPS week: 1414 Day: 2 MJD: 54144.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs IGS | cod emr esa gfz igr jpl mit ngs IGS ------+----------------------------------------------+----------------------------------------------- 1 | 8 15 26 12 6 22 16 15 6 | 34 39 54 35 33 42 32 31 33 2 | 14 13 22 12 6 50 24 16 7 | 33 44 43 38 35 44 36 30 34 3 | 11 14 22 14 5 11 14 14 6 | 29 35 39 33 30 31 33 26 28 4 | 10 9 18 9 9 17 21 10 5 | 36 41 45 39 39 45 37 33 35 5E | 12 18 35 20 7 18 21 18 8 | 43 49 66 51 44 51 51 41 44 6 | 9 10 21 7 5 9 25 15 5 | 33 33 39 34 34 36 37 32 30 7 | 10 10 24 7 5 9 26 9 5 | 40 42 45 41 41 45 38 38 38 8 | 11 13 26 12 6 17 18 10 6 | 30 33 40 35 33 35 32 30 30 9 | 10 10 31 13 6 9 13 12 5 | 33 36 42 35 33 38 30 29 32 10 | 16 14 25 11 6 11 27 12 6 | 32 40 43 34 33 43 44 27 32 11 | 11 14 13 16 5 49 22 11 7 | 42 53 52 46 43 41 43 41 42 12E | 16 17 17 11 6 56 15 10 7 | 39 45 44 40 39 46 42 40 38 13 | 15 18 28 13 7 62 19 15 8 | 32 42 41 34 31 44 26 26 28 14 | 21 65 16 18 20 59 21 29 14 | 31 64 40 38 32 45 27 29 26 X15 | 19 19 --- 22 11 17 27 28 10 | 39 61 --- 25 37 45 37 47 40 16E | 11 14 14 12 6 48 16 17 7 | 33 36 40 36 30 36 36 27 30 17 | 20 14 44 17 6 58 22 16 10 | 30 41 55 40 33 43 30 29 30 18 | 12 15 25 11 4 51 18 14 7 | 33 43 48 36 34 50 27 24 32 19 | 13 17 17 16 5 54 34 18 9 | 29 44 44 37 33 46 38 23 31 20 | 15 15 13 11 7 59 18 13 7 | 30 45 47 40 33 50 37 26 34 21 | 11 14 17 12 5 50 21 14 7 | 34 41 42 37 34 40 36 30 33 22 | 11 16 34 12 5 52 15 18 8 | 36 45 50 41 36 49 33 30 34 23 | 14 19 25 12 6 60 24 18 8 | 33 43 39 34 33 47 28 32 31 24 | 9 11 18 10 4 8 14 11 4 | 34 38 41 39 36 40 32 36 34 25 | 7 15 18 9 6 15 20 10 5 | 33 40 41 35 31 36 36 26 32 26 | 15 10 44 13 9 10 20 11 7 | 35 37 53 32 33 37 37 29 32 27 | 11 14 34 10 5 18 23 11 6 | 30 36 58 35 33 38 35 29 31 28E | 12 11 26 12 5 54 17 16 7 | 26 34 42 29 28 34 31 25 25 29 | 16 8 53 15 9 9 22 10 8 | 66 63 83 61 62 67 64 60 63 30E | 20 17 32 23 7 17 24 17 8 | 57 63 66 66 58 63 59 53 58 31 | 16 20 19 20 9 50 24 17 9 | 33 43 48 46 36 50 34 29 34 ------+----------------------------------------------+----------------------------------------------- RMS | 13 18 27 14 7 40 21 15 |T 35 43 47 38 36 43 36 32 34 WRMS | 13 18 24 14 6 40 20 12 |NE 34 43 46 37 35 43 35 31 33 MEDI | 12 14 24 12 6 22 21 14 |MD 33 42 44 37 33 44 36 30 32 Table 3.1414.3 GPS week: 1414 Day: 3 MJD: 54145.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs IGS | cod emr esa gfz igr jpl mit ngs IGS ------+----------------------------------------------+----------------------------------------------- 1 | 10 16 25 10 7 31 21 15 6 | 32 36 42 31 32 45 33 36 32 2 | 13 13 20 13 9 54 23 21 8 | 30 43 41 35 35 43 31 39 34 3 | 11 11 20 12 7 14 18 14 5 | 32 31 33 34 30 32 34 33 29 4 | 12 15 14 10 7 19 19 15 5 | 31 44 37 40 37 48 32 39 35 5E | 14 16 27 21 5 18 27 17 8 | 41 48 63 49 43 48 46 44 45 6 | 8 8 22 7 9 13 30 12 5 | 29 25 34 29 31 33 29 27 25 7 | 8 9 24 7 6 12 29 10 5 | 38 33 39 36 38 44 34 36 34 8 | 13 11 17 12 8 17 24 10 5 | 29 36 34 40 34 35 38 36 33 9 | 11 9 17 10 8 12 20 15 5 | 29 32 42 38 35 32 24 41 33 10 | 15 13 23 13 7 14 28 19 7 | 25 30 39 28 27 29 40 29 25 11 | 15 17 24 18 10 51 20 19 8 | 39 51 44 44 41 40 39 39 40 12E | 17 13 14 13 9 52 21 15 7 | 38 42 44 40 41 43 47 38 37 13 | 16 17 24 12 6 57 24 16 8 | 34 39 42 34 31 41 26 29 30 14 | 17 17 20 14 6 58 20 17 8 | 28 44 41 35 26 40 28 29 30 X15 | 19 16 --- --- 13 23 30 25 10 | 41 52 --- --- 35 57 37 40 39 16E | 12 11 12 13 4 47 21 17 6 | 26 28 26 32 24 32 26 28 25 17 | 18 17 36 14 11 58 34 21 10 | 28 36 43 40 32 50 32 28 30 18 | 14 15 18 9 5 57 21 19 7 | 36 37 37 34 32 44 30 35 31 19 | 16 15 16 13 16 54 32 20 8 | 28 38 36 37 33 42 33 29 30 20 | 16 15 18 11 8 64 27 26 9 | 33 41 34 39 34 46 38 36 33 21 | 14 13 18 13 6 52 25 22 8 | 31 42 40 38 32 35 29 33 33 22 | 12 14 21 9 6 57 20 20 7 | 34 38 39 35 33 44 31 38 32 23 | 14 20 25 11 7 62 33 21 9 | 39 45 48 39 40 50 36 41 36 24 | 10 6 13 10 5 8 14 15 4 | 32 34 36 34 33 38 29 35 31 25 | 8 12 14 9 6 15 21 13 5 | 34 36 34 35 34 32 34 37 32 26 | 15 10 23 13 9 12 23 14 6 | 30 29 38 29 30 30 34 30 28 27 | 11 10 19 11 7 14 23 19 6 | 33 33 31 38 33 37 35 40 32 28E | 14 11 21 11 9 54 19 26 8 | 23 28 36 27 26 28 29 31 23 29 | 14 9 29 11 8 13 25 14 6 | 46 43 50 40 41 45 50 41 41 30E | 19 15 22 23 8 19 32 20 8 | 58 59 62 68 59 58 54 58 57 31 | 14 18 20 18 11 55 28 21 9 | 29 41 42 41 35 46 24 31 31 ------+----------------------------------------------+----------------------------------------------- RMS | 14 14 21 13 8 41 25 18 |T 33 38 40 37 34 40 34 35 33 WRMS | 13 14 21 13 7 41 23 14 |NE 32 38 39 36 33 40 33 34 32 MEDI | 14 13 20 12 7 31 23 17 |MD 32 38 39 36 33 42 33 36 32 Table 3.1414.4 GPS week: 1414 Day: 4 MJD: 54146.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs IGS | cod emr esa gfz igr jpl mit ngs IGS ------+----------------------------------------------+----------------------------------------------- 1 | 12 27 34 13 9 27 23 20 9 | 33 47 37 30 30 41 33 28 31 2 | 12 17 23 15 7 50 22 24 8 | 25 44 32 32 28 47 27 30 29 3 | 14 17 35 14 5 15 18 16 7 | 25 28 39 28 26 28 29 27 25 4 | 12 14 24 12 9 15 14 14 6 | 30 42 28 35 30 44 28 25 30 5E | 14 16 22 23 8 19 26 21 8 | 46 49 52 51 45 52 49 49 46 6 | 12 9 28 12 6 13 30 24 7 | 34 33 42 33 34 40 33 38 31 7 | 13 11 25 10 6 11 28 14 6 | 42 39 44 40 42 47 33 44 39 8 | 13 10 16 13 6 16 19 14 5 | 29 35 37 37 34 37 30 28 30 9 | 13 10 20 15 9 14 22 19 6 | 31 41 50 38 37 38 34 42 36 10 | 18 14 29 13 9 14 28 22 8 | 22 34 37 26 23 30 39 22 24 11 | 15 15 20 15 6 47 30 20 8 | 39 51 44 43 38 42 43 35 39 12E | 16 12 18 15 9 51 26 25 8 | 36 40 43 38 38 46 39 42 37 13 | 17 13 24 15 8 59 21 21 9 | 34 44 42 36 33 46 30 32 33 14 | 18 24 22 16 11 55 19 24 9 | 31 39 38 37 31 43 29 28 29 X15 | 16 20 --- --- 10 22 30 21 10 | 33 51 --- --- 40 46 31 46 37 16E | 17 13 17 16 7 46 14 23 8 | 30 32 34 32 27 35 28 24 27 17 | 21 15 34 16 14 55 32 23 10 | 30 41 53 40 32 52 32 34 34 18 | 43 18 21 14 14 53 26 22 11 | 62 42 41 34 31 45 28 28 35 19 | 17 17 17 16 8 50 30 28 9 | 29 40 38 38 30 45 29 32 31 20 | 17 15 20 13 7 62 26 23 9 | 44 49 44 50 40 54 47 36 42 21 | 15 16 24 12 7 50 28 22 8 | 34 44 45 36 35 33 25 37 33 22 | 13 17 24 9 6 54 21 22 8 | 32 39 44 34 29 41 30 25 29 23 | 16 13 20 11 9 64 27 24 9 | 40 51 42 42 38 55 33 38 39 24 | 10 10 14 11 5 10 20 19 5 | 29 35 27 33 30 40 29 32 29 25 | 9 9 19 11 6 22 18 14 5 | 34 38 40 35 32 33 36 31 32 26 | 15 11 29 13 7 9 28 20 7 | 31 37 41 30 32 34 31 35 31 27 | 14 10 19 15 7 16 20 17 6 | 35 35 38 38 35 37 34 30 32 28E | 15 12 13 10 8 51 17 21 7 | 25 31 33 27 24 31 29 26 24 29 | 16 14 22 14 11 14 54 23 9 | 80 81 75 74 74 75 82 75 75 30E | 16 17 22 19 9 19 28 24 8 | 54 60 58 59 56 61 58 59 56 31 | 18 15 23 18 8 45 28 23 9 | 28 41 35 40 29 40 28 31 29 ------+----------------------------------------------+----------------------------------------------- RMS | 17 15 23 14 8 39 26 21 |T 35 42 41 38 34 43 35 35 34 WRMS | 15 15 23 14 8 39 24 16 |NE 35 42 41 37 34 42 33 34 34 MEDI | 15 14 22 14 8 27 26 22 |MD 33 41 41 36 32 42 31 32 32 Table 3.1414.5 GPS week: 1414 Day: 5 MJD: 54147.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs IGS | cod emr esa gfz igr jpl mit ngs IGS ------+----------------------------------------------+----------------------------------------------- 1 | 9 12 19 11 9 29 19 15 6 | 34 40 34 33 34 38 36 28 31 2 | 15 13 16 10 5 49 20 15 7 | 28 41 34 34 32 45 31 29 31 3 | 14 13 25 15 7 13 20 14 6 | 41 45 39 45 39 41 43 37 40 4 | 13 13 18 8 7 29 14 15 6 | 33 38 34 36 35 59 31 36 32 5E | 15 17 21 17 8 17 22 19 7 | 43 52 51 52 45 52 47 46 45 6 | 12 11 24 11 4 13 33 9 6 | 29 28 27 29 28 35 40 25 25 7 | 12 14 21 9 5 11 33 8 6 | 37 35 38 36 34 40 37 32 33 8 | 13 9 19 11 7 14 24 20 6 | 29 30 21 32 32 33 32 33 27 9 | 13 11 21 13 7 14 19 12 6 | 23 35 35 29 28 30 27 23 25 10 | 20 15 25 12 7 12 29 20 7 | 25 37 36 31 31 38 38 27 27 11 | 15 16 19 16 9 49 26 15 8 | 34 49 40 43 39 43 36 32 36 12E | 18 14 15 14 6 55 20 20 8 | 38 43 33 37 37 48 38 40 35 13 | 20 15 22 14 8 58 23 21 9 | 35 43 38 32 33 44 28 25 30 14 | 20 16 22 13 8 56 23 19 8 | 28 37 31 36 32 40 27 29 27 X15 | 22 26 --- --- 23 17 39 30 14 | 31 50 --- --- 33 40 34 39 34 16E | 17 12 18 12 8 48 19 14 7 | 35 38 32 35 31 41 40 21 31 17 | 21 18 33 14 9 61 31 18 10 | 29 44 45 40 35 54 27 26 32 18 | 17 15 18 9 7 59 21 20 8 | 28 41 31 33 32 48 33 26 28 19 | 18 18 22 17 7 47 30 23 9 | 32 47 37 41 36 43 29 27 33 20 | 16 15 19 10 5 62 27 19 8 | 51 58 51 56 53 60 56 45 50 21 | 18 17 20 10 6 51 28 16 8 | 30 42 35 34 32 35 30 27 30 22 | 15 13 17 11 5 51 19 19 7 | 31 45 39 37 35 44 31 25 32 23 | 19 15 22 12 9 63 25 23 9 | 39 45 40 36 36 48 33 35 34 24 | 10 10 22 12 6 10 16 14 5 | 29 33 27 31 31 40 24 31 27 25 | 10 11 24 11 6 20 19 13 6 | 31 38 34 32 31 30 33 29 30 26 | 17 11 23 13 7 9 24 15 6 | 29 36 33 31 31 37 38 27 28 27 | 17 10 21 12 7 15 25 16 6 | 31 34 31 33 33 33 36 29 29 28E | 17 14 17 11 6 51 17 18 7 | 30 33 36 30 30 32 27 27 25 29 | 23 11 21 14 7 11 21 17 7 | 60 65 68 61 61 65 58 61 60 30E | 18 15 18 19 9 21 24 17 7 | 62 69 64 71 66 72 64 62 64 31 | 16 16 23 16 7 53 27 21 9 | 29 43 43 42 37 51 29 28 32 ------+----------------------------------------------+----------------------------------------------- RMS | 16 14 21 13 7 40 24 17 |T 34 42 37 38 36 43 35 32 33 WRMS | 16 14 21 13 7 40 22 11 |NE 32 41 36 36 35 42 34 31 32 MEDI | 17 14 21 12 7 29 23 17 |MD 31 41 35 35 33 41 33 29 31 Table 3.1414.6 GPS week: 1414 Day: 6 MJD: 54148.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs IGS | cod emr esa gfz igr jpl mit ngs IGS ------+----------------------------------------------+----------------------------------------------- 1 | 11 11 20 10 7 47 20 15 7 | 34 38 42 33 34 59 35 29 32 2 | 12 17 19 10 9 59 24 18 8 | 29 41 36 35 30 44 33 27 30 3 | 12 10 19 14 7 21 25 16 6 | 24 29 35 32 26 28 30 24 25 4 | 12 12 19 12 8 17 20 15 6 | 31 42 37 35 34 44 35 32 33 5E | 17 15 24 16 8 20 24 19 7 | 52 58 65 61 55 62 58 59 56 6 | 12 9 24 10 6 13 32 12 6 | 29 28 34 30 30 38 37 26 27 7 | 11 10 23 11 8 16 33 14 6 | 35 32 33 36 36 43 31 36 32 8 | 11 15 20 11 8 24 25 17 6 | 24 35 32 31 28 32 29 19 25 9 | 13 10 39 14 9 19 16 25 8 | 23 29 45 30 29 25 21 39 26 10 | 20 11 25 11 6 17 31 15 7 | 20 29 34 26 22 25 35 16 21 11 | 17 14 24 18 11 52 28 15 8 | 42 52 48 48 44 38 38 42 42 12E | 17 12 22 13 8 60 23 19 8 | 34 39 50 33 35 49 36 32 34 13 | 19 17 20 15 10 57 26 19 9 | 28 39 40 32 28 41 35 21 28 14 | 15 14 19 14 6 55 23 17 8 | 22 36 36 32 27 42 23 24 26 X15 | 21 29 --- --- 17 41 49 31 16 | 32 57 --- --- 37 58 32 33 37 16E | 18 13 21 15 9 50 28 26 9 | 24 31 28 30 26 35 29 28 24 17 | 22 16 30 18 6 58 37 22 10 | 26 39 49 37 29 52 31 28 29 18 | 29 15 26 14 8 56 27 23 10 | 37 36 27 31 27 48 25 29 26 19 | 18 14 18 16 10 51 32 16 8 | 30 43 45 42 37 52 30 30 34 20 | 21 17 23 14 10 64 33 35 11 | 91 91 89 89 84 81 87 93 88 21 | 18 14 14 12 8 51 28 16 8 | 31 41 33 35 31 32 28 30 31 22 | 16 17 23 13 7 54 21 51 11 | 22 35 31 34 30 42 32 62 28 23 | 17 15 22 14 9 59 22 19 8 | 37 45 42 40 38 51 40 41 38 24 | 10 9 16 12 5 15 17 18 5 | 29 36 26 40 33 41 28 33 31 25 | 8 10 20 9 7 29 18 14 5 | 27 36 34 32 32 36 34 25 28 26 | 16 13 25 15 7 17 33 44 9 | 27 28 27 28 25 27 40 47 23 27 | 12 11 20 13 8 23 24 10 6 | 29 39 42 37 34 40 38 26 32 28E | 53 57 142 87 54 95 136 88 36 | 55 31 57 66 42 34 98 37 35 29 | 34 15 31 20 9 16 28 43 11 | 63 60 65 64 60 55 68 72 58 30E | 20 16 21 17 6 21 30 19 8 | 63 74 79 76 69 70 64 71 68 31 | 18 11 22 18 8 50 32 18 8 | 21 37 40 36 26 38 28 17 25 ------+----------------------------------------------+----------------------------------------------- RMS | 20 17 34 21 12 45 36 28 |T 34 41 42 40 36 43 38 36 34 WRMS | 15 17 23 14 8 45 24 15 |NE 32 40 40 37 34 42 35 34 32 MEDI | 17 14 22 14 8 47 27 18 |MD 29 38 37 35 32 42 34 30 31 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 4.1414 GPS week: 1414 MJD: 54142.0-54148.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2952 |U 17 10 33 |U 17 18 44 |U 11 13 29 | emr | emr 2960 |U 30 19 68 | 16 20 47 | 13 15 32 | esa | esa 2784 | 19 12 43 |U 17 17 46 | 14 17 37 | gfz | gfz 2877 |U 19 12 41 |U 18 18 44 |U 14 16 35 | igr | igr 2964 | 20 15 41 | 18 21 50 | 13 15 34 | igs | igs 2969 | 17 12 36 | 18 19 47 | 13 14 32 | jpl | jpl 2950 | 25 17 46 | 17 20 45 | 19 19 42 | mit | mit 2976 |U 23 14 63 |U 21 22 45 |U 12 13 28 | 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 5.1414.0 GPS week: 1414 Day: 0 MJD: 54142.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 | 15 12 32 | 16 17 54 | 12 12 26 | emr | emr 2968 | 30 16 79 | 14 18 64 | 16 17 28 | esa | esa 2784 | 15 11 34 | 12 15 45 | 15 12 35 | gfz | gfz 2959 | 17 11 36 | 14 15 45 | 14 13 35 | igr | igr 2970 | 19 17 41 | 14 18 59 | 16 15 44 | igs | igs 2976 | 15 12 40 | 17 14 54 | 15 13 37 | jpl | jpl 2938 | 18 17 35 | 15 17 42 | 25 19 45 | mit | mit 2976 | 25 15 70 | 19 23 37 | 13 12 27 | Table 5.1414.1 GPS week: 1414 Day: 1 MJD: 54143.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2959 | 19 12 34 | 16 19 40 | 10 12 24 | emr | emr 2966 | 49 30 87 | 16 24 42 | 13 16 28 | esa | esa 2784 | 19 12 34 | 18 18 48 | 15 15 31 | gfz | gfz 2860 | 16 10 32 | 17 18 42 | 12 11 26 | igr | igr 2971 | 21 10 45 | 17 21 47 | 10 12 27 | igs | igs 2964 | 18 15 32 | 18 21 45 | 12 13 27 | jpl | jpl 2956 | 34 18 56 | 17 16 48 | 17 16 31 | mit | mit 2976 | 24 16 67 | 21 24 52 | 11 12 24 | Table 5.1414.2 GPS week: 1414 Day: 2 MJD: 54144.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2956 | 19 9 33 | 18 23 49 | 12 9 30 | emr | emr 2937 | 33 19 76 | 14 26 49 | 14 11 30 | esa | esa 2784 | 24 12 44 | 17 21 52 | 14 11 36 | gfz | gfz 2883 | 24 10 45 | 20 23 52 | 21 20 51 | igr | igr 2975 | 26 28 52 | 19 24 56 | 16 10 32 | igs | igs 2976 | 18 11 36 | 16 25 47 | 18 13 37 | jpl | jpl 2957 | 25 15 33 | 16 23 41 | 20 18 41 | mit | mit 2976 | 27 12 73 | 21 36 51 | 11 11 27 | Table 5.1414.3 GPS week: 1414 Day: 3 MJD: 54145.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2955 | 17 12 39 | 24 23 53 | 10 15 29 | emr | emr 2966 | 28 26 75 | 24 21 56 | 12 16 33 | esa | esa 2784 | 22 14 47 | 23 24 57 | 14 21 42 | gfz | gfz 2860 | 18 16 43 | 23 20 58 | 13 16 36 | igr | igr 2967 | 16 11 40 | 26 32 60 | 14 19 34 | igs | igs 2970 | 16 11 40 | 23 25 61 | 11 17 36 | jpl | jpl 2958 | 23 24 40 | 25 22 64 | 18 19 41 | mit | mit 2976 | 23 14 74 | 31 29 53 | 18 16 30 | Table 5.1414.4 GPS week: 1414 Day: 4 MJD: 54146.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2952 | 14 10 33 | 19 16 38 | 9 10 25 | emr | emr 2966 | 30 18 64 | 17 18 39 | 12 13 33 | esa | esa 2784 | 18 14 39 | 20 16 40 | 12 16 34 | gfz | gfz 2862 | 15 14 34 | 17 17 39 | 13 15 28 | igr | igr 2972 | 17 14 34 | 20 18 44 | 12 13 29 | igs | igs 2963 | 19 14 34 | 19 17 39 | 9 10 30 | jpl | jpl 2946 | 27 17 45 | 20 25 38 | 18 22 45 | mit | mit 2976 | 24 18 55 | 21 16 44 | 11 13 25 | Table 5.1414.5 GPS week: 1414 Day: 5 MJD: 54147.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2941 | 15 7 27 | 16 13 40 | 10 16 32 | emr | emr 2961 | 21 10 47 | 14 12 38 | 13 17 34 | esa | esa 2784 | 18 10 58 | 14 15 44 | 15 19 37 | gfz | gfz 2860 | 24 9 43 | 16 14 38 | 13 16 36 | igr | igr 2967 | 20 11 28 | 15 15 51 | 14 15 38 | igs | igs 2963 | 14 9 30 | 15 13 39 | 12 14 30 | jpl | jpl 2936 | 25 13 53 | 15 18 44 | 20 21 47 | mit | mit 2976 | 22 12 62 | 18 15 40 | 12 15 31 | Table 5.1414.6 GPS week: 1414 Day: 6 MJD: 54148.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2950 | 18 11 36 | 13 15 37 | 15 18 37 | emr | emr 2962 | 20 12 48 | 14 20 40 | 11 17 38 | esa | esa 2784 | 15 9 42 | 16 12 38 | 14 22 41 | gfz | gfz 2860 | 21 12 57 | 17 16 38 | 13 19 37 | igr | igr 2928 | 19 15 48 | 13 20 33 | 11 21 34 | igs | igs 2971 | 20 13 41 | 18 18 46 | 12 17 28 | jpl | jpl 2960 | 26 14 60 | 13 17 39 | 16 20 43 | mit | mit 2976 | 19 13 42 | 16 14 38 | 11 14 34 | 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 6.1414 GPS week: 1414 MJD: 54142.500-54148.500 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 | 14 -44 -37 51 2 | -5 17 | 12 16 70 70 7 | 3 emr uuuuu | 20 -63 109 43 -1 | 38 41 | 14 33 75 59 9 | 3 esa uuuux | 11 32 -48 66 19 | 79 87 | 45 20 100 64 44 | 11 gfz uuuuu | -13 13 -113 -43 -5 | 23 29 | 17 19 50 91 13 | 3 igr xxxxx | -11 -11 10 -39 -10 | 1 20 | 23 26 65 68 18 | 4 irf xxxxx | 3 18 -75 -73 -7 | 3 16 | 10 10 37 39 9 | 3 jpl uuuuu | 8 -29 -125 -49 -4 | -8 25 | 32 25 96 156 15 | 8 mit uuuuu | -4 9 -52 -220 -2 | 9 19 | 34 39 104 36 9 | 2 ngs uuuuu | -37 106 146 34 2 | -9 16 | 51 48 200 91 9 | 2 Table 7.1414.0 GPS week: 1414 Day: 0 MJD: 54142.500 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 -52 -46 85 -6 | -4 15 emr uuuuu | 10 -90 135 -30 -4 | 40 43 esa uuuux | 13 13 -97 90 82 | 61 65 gfz uuuuu | -1 51 -72 -64 19 | 20 25 igr xxxxx | 1 -43 94 45 5 | -1 16 irf xxxxx | 5 36 -20 -82 8 | 1 14 jpl uuuuu | 43 -56 -99 100 -26 | 4 27 mit uuuuu | -3 60 34 -251 11 | 7 16 ngs uuuuu | -58 75 44 65 -1 | -8 16 Table 7.1414.1 GPS week: 1414 Day: 1 MJD: 54143.500 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 -29 -46 6 -2 | -4 15 emr uuuuu | 0 -91 67 139 -11 | 41 43 esa uuuux | -16 35 -42 0 73 | 69 76 gfz uuuuu | -35 -4 -147 -221 1 | 23 27 igr xxxxx | -11 10 -3 -27 6 | 0 16 irf xxxxx | 0 22 -104 -129 -1 | 3 13 jpl uuuuu | 21 -45 -152 60 -6 | -2 26 mit uuuuu | 0 45 -29 -235 9 | 8 16 ngs uuuuu | 11 143 194 136 -2 | -7 15 Table 7.1414.2 GPS week: 1414 Day: 2 MJD: 54144.500 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 -26 -35 -10 1 | -4 15 emr uuuuu | 33 -102 197 83 -7 | 40 42 esa uuuux | -56 47 -84 13 17 | 80 89 gfz uuuuu | 0 6 -97 41 -6 | 25 29 igr xxxxx | -23 -2 -26 -93 14 | 2 16 irf xxxxx | 14 8 -42 -38 -12 | 4 13 jpl uuuuu | 21 -51 -59 15 6 | -7 22 mit uuuuu | 34 -54 43 -149 -3 | 10 18 ngs uuuuu | -38 149 -19 -43 1 | -8 15 Table 7.1414.3 GPS week: 1414 Day: 3 MJD: 54145.500 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 -39 -114 82 -2 | 0 15 emr uuuuu | 26 -11 166 64 -1 | 43 45 esa uuuux | 1 4 71 -1 3 | 89 96 gfz uuuuu | -9 22 -91 -71 -5 | 29 32 igr xxxxx | 19 24 40 55 -16 | 8 18 irf xxxxx | -4 15 -70 -89 -11 | 7 13 jpl uuuuu | 18 10 -21 -8 -9 | -3 23 mit uuuuu | -57 15 -52 -237 -5 | 14 19 ngs uuuuu | 12 23 28 43 9 | -9 14 Table 7.1414.4 GPS week: 1414 Day: 4 MJD: 54146.500 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 -47 56 -16 5 | -7 18 emr uuuuu | 13 -49 111 -8 2 | 37 40 esa uuuux | 77 32 -1 140 5 | 86 94 gfz uuuuu | -40 7 -112 -8 -18 | 25 30 igr xxxxx | -44 2 -111 -42 -21 | 2 22 irf xxxxx | -13 14 -64 -88 -15 | 3 18 jpl uuuuu | -26 -5 -277 -83 -16 | -13 23 mit uuuuu | -39 -24 31 -229 -9 | 11 21 ngs uuuuu | 6 137 -4 134 16 | -12 18 Table 7.1414.5 GPS week: 1414 Day: 5 MJD: 54147.500 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 | 20 -73 49 181 3 | -8 19 emr uuuuu | 40 -63 -33 46 0 | 34 38 esa uuuux | 58 29 41 72 -8 | 85 93 gfz uuuuu | -6 8 -64 -25 -20 | 21 30 igr xxxxx | -32 -40 32 -109 -31 | -2 26 irf xxxxx | 7 8 -105 -74 -17 | 0 21 jpl uuuuu | 27 -21 -222 -54 21 | -18 29 mit uuuuu | 12 1 -192 -245 -15 | 9 22 ngs uuuuu | -127 138 237 -116 7 | -12 18 Table 7.1414.6 GPS week: 1414 Day: 6 MJD: 54148.500 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 | 21 -43 -120 29 16 | -7 19 emr uuuuu | 20 -37 122 4 16 | 35 39 esa uuuux | 2 64 -225 149 -41 | 87 95 gfz uuuuu | 1 2 -207 49 -10 | 20 29 igr xxxxx | 13 -28 44 -104 -26 | -5 27 irf xxxxx | 15 24 -122 -10 -3 | -1 22 jpl uuuuu | -46 -34 -45 -373 1 | -15 28 mit uuuuu | 28 19 -198 -197 -1 | 9 22 ngs uuuuu | -66 78 540 22 -12 | -10 17