Date: Thu, 24 May 2007 10:14:22 +0200 To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-15114] Wk 1426 IGS Final Orbits Message-ID: <4655495E.mailxCQU1WGA3P@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 24 May 01:14:35 PDT 2007 Message Number 15114 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1426 (May 06, 2007 - May 12, 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: igs1426[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1426[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1426[0-6].cls IGS GPS clock combination summary report. igs14267.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14267.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 | BILI YELL 0 | MIT | DAEJ IRKT 1 | EMR | IRKT KOUR YELL 1 | ESA | BILI LPGS PERT YELL 1 | GFZ | BAN2 NISU PERT 1 | JPL | YELL 1 | MIT | BOR1 DAEJ KOUR NRIL 2 | COD | DAEJ GRAZ NRIL 2 | ESA | IRKT PERT 2 | GFZ | BAN2 PERT 2 | JPL | BJFS 2 | MIT | CHUR DAEJ IRKT KOUR MAW1 VILL 3 | COD | NRIL 3 | ESA | BILI KERG LPGS 3 | GFZ | KERG NKLG 3 | MIT | 27 BOR1 4 | COD | ARTU 4 | ESA | UNSA 4 | GFZ | BAN2 BOR1 DAV1 4 | JPL | KERG NISU 4 | MIT | UNSA 5 | ESA | 4 ARTU 5 | GFZ | BAN2 5 | JPL | 21 5 | MIT | ARTU GUAM SUTM 6 | EMR | ALGO PRDS SCH2 YELL 6 | ESA | 4 ALGO YELL 6 | GFZ | ALGO BAN2 YELL 6 | MIT | GLPS SANT 5. The following table lists all maneuvered satellites for this week. The solutions from COD and ESA, which modeled the maneuver, are used that day for combination. An associated accuracy code of 0 (unknown) is given if only one AC is left (no redundancy). For the long arc evaluation the arc is split into two parts at the given maneuver epoch. PRN | Date | Ref. NANU ----+------------+---------- G20 | 2007_05_10 | 2007065 G20 | 2007_05_11 | 2007065 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 | | | | | 1 | | | 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 | .0 .0 .2 -3 4 0 -.18 EMR | 1.3 -2.1 12.4 -39 30 -38 -.04 ESA | 3.3 .5 2.8 -45 6 -22 -1.08 GFZ | .3 -.2 .9 -23 -6 -15 -.38 JPL | 5.1 -4.4 9.1 150 -53 174 .20 MIT | -1.3 -1.0 10.2 -20 6 -3 -.15 NGS | 2.5 1.5 -2.5 26 -47 7 -1.05 SIO | -3.2 -3.0 1.2 -38 28 32 .15 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 1.1426.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1426.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 2.1426.[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 3.1426.[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 5.1426.0-6). 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 1426 summary. (May 06, 2007 - May 12, 2007) Table 1.1426.a GPS week: 1426 MJD: 54226.000-54232.000 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 168| 1 -1 -2 -35 0 21 -.18 14 14 | -431 130 60 100 | 0 0 1 6 8 36 .04 | 229 449 emr 66| 1 1 8 72 -43 30 .33 17 17 | 6952 -1007 52 92 | 1 1 1 7 23 39 .03 | 1706 1262 esa 61| 0 0 7 67 -36 71 .17 21 21 | 6930 -880 55 128 | 1 0 1 37 57 22 .02 | 1619 1324 gfz 183| -1 1 1 41 5 -191 -.21 14 14 | -49 153 30 106 | 1 1 1 26 29 105 .03 | 315 634 igr n/a| 0 0 0 -28 -7 53 .01 8 8 | -21925 -801 30 73 | 1 0 1 15 12 42 .02 | 1422 1381 jpl n/a| -3 -3 -13 -175 66 233 .02 39 39 | 7093 -657 90 128 | 2 5 5 16 15 47 .04 | 1166 1544 mit 188| -1 -1 -5 11 -29 21 -.00 22 21 | -108 199 77 123 | 1 1 1 23 41 39 .06 | 361 743 ngs 164| -2 0 -1 -72 81 70 .02 14 12 | 63762 -571259 2327 4070 | 0 1 1 32 20 46 .05 | 281352 534731 sio 93| 4 -2 -1 10 -66 67 -.03 27 23 | --- --- --- --- | 0 1 3 24 27 32 .06 | --- --- Table 1.1426.b GPS week : 1426 MJD: 54226.000-54232.000 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 | 6 6 6 6 6 6 6 | 2E | 8 8 7 7 6 6 6 | 3 | 6 6 6 6 6 6 7 | 4E | 8 9 7 8 7 8 9 | 5 | 5 5 5 6 6 7 6 | 6 | 6 5 5 6 5 5 5 | 7 | 6 5 6 6 5 5 5 | 8 | 7 7 6 7 6 6 6 | 9 | 6 6 6 6 6 6 6 | 10 | 6 6 6 5 6 6 6 | 11E | 8 8 8 8 8 8 8 | 12 | 7 7 7 7 7 8 7 | 13 | 7 7 7 7 7 7 7 | 14 | 8 8 8 8 8 8 8 | 16 | 8 8 8 8 8 9 8 | 17 | 8 8 8 8 8 8 9 | 18 | 8 9 9 9 9 9 8 | 19 | 9 9 9 9 8 9 9 | 20 | 8 8 8 8 0 0 9 | 21E | 9 9 9 8 7 8 7 | 22 | 9 9 9 9 8 9 9 | 23 | 7 7 8 7 7 8 7 | 24E | 10 9 6 7 7 7 7 | 25 | 6 6 7 6 6 5 6 | 26 | 7 6 6 6 7 5 7 | 27 | 6 6 6 6 6 6 6 | 28 | 8 9 9 8 8 8 9 | 29 | 8 6 6 7 15 6 11 | 30 | 5 6 6 5 5 6 6 | 31 | 8 8 9 8 9 9 9 | 32 | 15 20 16 15 17 18 23 | 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 2.1426.0 GPS week: 1426 Day: 0 MJD: 54226.000 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 168| 1 0 -2 -40 5 -43 -.21 14 14 | -492 233 59 90 | 60 -20 | emr 66| 2 2 10 74 -68 -6 .32 15 15 | 7526 414 57 93 | -20 -9 | esa 61| -1 -1 6 107 15 77 .18 22 22 | 7367 778 61 130 | -61 -44 | gfz 183| -1 0 0 48 -11 -13 -.27 15 15 | 243 -520 31 105 | 4 -2 | igr n/a| 0 0 0 -47 -29 12 .04 8 8 | -21875 767 30 70 | 21 1 | jpl n/a| -6 7 -11 -158 75 173 .09 39 39 | 6436 1080 95 121 | -42 -59 | mit 189| -2 -3 -7 16 -78 -26 -.09 25 23 | 82 -33 81 121 | -21 84 | ngs 164| -2 0 -2 -96 102 7 .08 13 11 | -492 166 2231 3808 | 9 -104 | sio 93| 6 -4 -3 8 -47 32 -.10 29 25 | --- --- --- --- | 45 32 | Table 2.1426.1 GPS week: 1426 Day: 1 MJD: 54227.000 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 168| 1 -1 -4 -25 5 9 -.25 15 14 | -500 207 63 102 | 42 -8 | emr 66| 1 3 9 75 -48 -15 .28 16 16 | 8759 -441 57 89 | -25 -25 | esa 61| -2 0 9 5 -22 42 .16 20 20 | 8546 -15 57 131 | -5 -19 | gfz 183| -2 1 2 62 31 -108 -.17 14 14 | -138 551 32 121 | 3 -47 | igr n/a| -1 0 2 -32 -8 5 .02 9 9 | -20520 112 32 72 | 31 -66 | jpl n/a| -3 -5 -19 -167 57 183 .03 41 41 | 8088 329 91 122 | -39 -68 | mit 189| 0 -2 -6 56 -79 -7 -.04 21 21 | -196 780 79 125 | 20 82 | ngs 164| 0 1 -2 -111 83 51 .08 14 11 | -503 244 1980 3943 | 24 -70 | sio 93| 4 -4 1 41 -75 14 -.08 29 26 | --- --- --- --- | 47 22 | Table 2.1426.2 GPS week: 1426 Day: 2 MJD: 54228.000 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 168| 0 -1 -5 -29 -16 2 -.20 14 14 | -491 673 62 96 | 57 3 | emr 66| 3 2 7 74 -58 0 .32 17 17 | 8539 -1422 53 76 | -29 51 | esa 61| -1 0 8 39 12 73 .16 21 21 | 8392 -1145 60 133 | 24 1 | gfz 183| -1 1 3 65 -33 -145 -.20 15 15 | 15 348 29 112 | -19 19 | igr n/a| 0 0 0 -5 -8 36 .02 8 8 | -20430 -1407 35 69 | -10 44 | jpl n/a| -4 -7 -11 -185 47 199 -.00 38 38 | 8375 -1317 89 120 | -15 42 | mit 189| -3 -1 -6 -23 -35 -17 -.04 21 21 | -32 308 73 114 | 16 33 | ngs 164| -1 0 0 -35 105 33 -.00 12 10 | -554 768 2466 3922 | -59 -54 | sio 93| 3 -3 1 -1 -61 73 -.03 27 25 | --- --- --- --- | 69 36 | Table 2.1426.3 GPS week: 1426 Day: 3 MJD: 54229.000 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 168| 1 -1 -1 -31 2 20 -.18 14 14 | -108 -434 56 100 | 46 8 | emr 66| 2 1 9 56 -31 55 .33 18 18 | 7173 -1408 44 90 | 31 -85 | esa 61| 0 0 8 110 -135 53 .18 20 20 | 7315 -1403 51 106 | 9 8 | gfz 183| -2 1 0 36 53 -252 -.23 14 14 | 289 -647 32 111 | 14 -38 | igr n/a| -1 0 -1 -49 2 50 .01 7 7 | -21743 -1195 27 77 | 69 -94 | jpl n/a| -5 -3 -13 -192 58 247 .00 39 39 | 7180 -986 88 129 | 17 -71 | mit 189| -1 0 -3 7 -12 51 .01 20 20 | 88 -444 75 114 | 16 0 | ngs 164| -3 0 -2 -85 61 94 .03 14 11 | -118007 -999999 2332 4170 | -40 -48 | sio 93| 5 -1 1 19 -68 75 -.06 26 22 | --- --- --- --- | 48 72 | Table 2.1426.4 GPS week: 1426 Day: 4 MJD: 54230.000 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 168| 2 0 -1 -39 5 41 -.18 14 14 | -793 391 59 101 | 39 -26 | emr 66| 1 3 7 69 -69 56 .37 18 18 | 6262 587 56 108 | -21 38 | esa 61| -1 0 4 83 12 51 .14 20 20 | 6391 417 52 141 | 18 -40 | gfz 183| 0 0 3 64 -5 -309 -.17 12 12 | -669 1151 36 109 | -5 19 | igr n/a| -1 0 0 -16 12 103 -.02 7 7 | -22415 769 31 65 | -22 -36 | jpl n/a| -5 -7 -5 -198 86 296 .03 40 40 | 6796 1056 88 135 | -43 17 | mit 189| 0 0 -5 4 -26 71 .01 21 21 | -883 1449 78 111 | 18 9 | ngs 164| -1 -1 -1 -96 90 146 -.04 13 13 | 1407 -999999 2422 4166 | -53 -13 | sio 93| 5 -1 -4 -27 -114 102 -.02 26 21 | --- --- --- --- | 24 101 | Table 2.1426.5 GPS week: 1426 Day: 5 MJD: 54231.000 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 168| 0 -1 -1 -42 5 53 -.13 14 14 | -170 -540 64 111 | 54 -2 | emr 66| 0 0 7 76 -24 89 .35 19 19 | 6743 -1876 51 98 | -7 -83 | esa 61| 0 -1 7 61 -69 102 .19 19 19 | 6784 -1945 53 123 | 43 -12 | gfz 183| 0 3 1 -3 10 -264 -.21 12 12 | -48 345 28 98 | 10 -10 | igr n/a| 0 0 0 -26 -12 117 .02 7 7 | -21805 -1818 29 62 | 8 -21 | jpl n/a| 1 -6 -21 -160 84 264 .03 38 38 | 7806 -1713 89 137 | 0 -35 | mit 189| -3 -1 -4 8 -15 61 .07 22 22 | 182 100 77 156 | 25 -5 | ngs 164| -2 1 0 -29 77 97 .01 15 14 | -124059 -999999 2581 4486 | -27 -10 | sio 93| 4 0 -3 -2 -73 79 .07 27 22 | --- --- --- --- | -2 29 | Table 2.1426.6 GPS week: 1426 Day: 6 MJD: 54232.000 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 168| 1 0 -1 -40 -1 65 -.14 15 14 | -468 386 63 106 | 53 24 | emr 66| 1 -1 8 79 -6 35 .35 16 16 | 3666 -2904 51 96 | -8 -45 | esa 61| 0 -1 7 65 -69 96 .15 23 21 | 3715 -2848 51 134 | 5 -8 | gfz 183| 0 0 0 19 -10 -247 -.20 13 13 | -40 -152 26 92 | 12 37 | igr n/a| 0 0 1 -22 -11 49 -.02 7 7 | -24690 -2837 28 98 | -11 15 | jpl n/a| -2 0 -12 -167 55 267 -.03 37 37 | 4972 -3051 90 135 | -17 25 | mit 189| -1 -1 -5 9 39 18 .05 25 23 | 0 -765 82 124 | 39 -40 | ngs 164| -3 2 0 -53 51 61 -.04 15 12 | 688547 -999999 2281 4001 | -76 90 | sio 93| 3 -1 -6 38 -23 93 .03 28 22 | --- --- --- --- | 7 14 | 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 3.1426.0 GPS week: 1426 Day: 0 MJD: 54226.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1 | 14 11 20 13 6 21 16 10 19 5 | 24 36 33 34 27 29 22 27 28 27 2E | 12 15 14 18 6 59 20 14 23 7 | 23 31 26 31 25 36 21 22 27 23 3 | 11 14 17 12 7 18 24 12 33 6 | 28 43 37 35 34 32 37 42 33 35 4E | 14 17 25 15 13 16 28 11 51 8 | 74 74 69 74 71 68 66 68 77 70 5 | 12 12 15 11 7 11 20 13 14 5 | 27 38 40 31 32 31 36 33 37 33 6 | 9 13 25 9 8 8 16 12 27 5 | 23 30 34 27 27 24 26 24 31 25 7 | 10 14 25 11 7 8 15 10 29 5 | 27 30 31 28 26 23 26 23 27 24 8 | 13 12 28 14 9 14 15 9 38 6 | 21 26 38 29 24 21 22 18 39 21 9 | 15 13 26 14 6 14 16 11 23 6 | 21 32 36 29 25 26 24 24 31 25 10 | 12 10 20 12 6 9 19 15 21 5 | 19 24 30 29 23 25 23 25 24 22 11E | 11 20 19 18 9 49 21 12 31 7 | 22 41 29 24 25 36 23 23 29 23 12 | 12 14 19 11 7 47 19 11 34 7 | 25 33 32 25 28 36 30 26 48 27 13 | 12 12 24 15 7 55 12 11 21 7 | 29 35 38 34 29 39 25 25 28 28 14 | 20 16 19 15 7 55 15 13 22 7 | 26 36 33 30 24 38 24 23 29 26 16 | 14 13 17 14 11 47 31 14 29 7 | 31 37 28 32 28 33 31 30 37 30 17 | 17 17 21 20 11 58 27 14 20 8 | 37 37 44 47 36 51 32 37 40 36 18 | 16 21 16 16 8 55 24 16 30 8 | 27 42 35 31 31 41 26 30 37 27 19 | 16 16 23 16 7 60 26 16 39 8 | 28 41 49 40 32 57 26 28 29 32 20 | 16 15 31 16 6 51 24 16 21 8 | 25 30 30 28 23 31 23 20 22 23 21E | 21 20 13 17 12 54 31 18 32 9 | 25 33 30 31 26 40 33 24 34 26 22 | 18 19 17 21 10 48 36 16 26 8 | 30 44 39 30 32 38 34 33 30 29 23 | 15 16 17 11 7 52 16 11 26 7 | 26 40 41 34 29 42 23 27 22 28 24E | 21 21 28 16 8 19 61 14 33 10 | 136 129 135 135 134 133 159 138 148 137 25 | 10 15 29 11 8 16 14 13 22 6 | 23 33 41 31 25 27 24 26 32 27 26 | 13 13 25 16 9 15 21 16 23 6 | 20 28 34 32 22 23 33 28 33 25 27 | 18 13 21 13 6 15 16 11 20 6 | 34 33 40 36 31 29 31 30 34 31 28 | 12 11 18 13 8 56 28 12 45 8 | 31 39 38 36 30 30 36 29 49 31 29 | 11 15 36 19 13 21 26 15 34 8 | 64 70 77 67 70 68 74 72 63 68 30 | 10 9 18 11 9 10 17 12 27 5 | 35 45 47 40 40 39 38 38 51 39 31 | 15 16 24 14 9 53 32 13 20 8 | 25 37 37 30 27 42 33 20 35 25 X32 | 17 --- --- --- 23 38 --- 18 --- 14 | 38 --- --- --- 46 27 --- 43 --- 39 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 15 22 15 8 39 25 13 29 |T 33 40 41 38 34 39 35 34 39 34 WRMS | 14 15 22 15 8 39 23 11 25 |NE 28 36 38 33 30 34 30 30 34 30 MEDI | 14 14 20 14 8 38 20 13 26 |MD 27 36 37 31 28 36 26 27 33 27 Table 3.1426.1 GPS week: 1426 Day: 1 MJD: 54227.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1 | 15 13 19 12 9 28 16 12 22 6 | 22 33 28 28 25 29 26 26 30 24 2E | 13 16 19 21 13 60 13 16 17 7 | 18 29 21 31 20 33 24 23 23 19 3 | 11 17 19 10 5 18 15 10 38 6 | 29 40 30 35 32 34 35 32 35 31 4E | 16 17 25 22 12 20 21 21 52 8 | 71 67 66 74 72 70 61 73 53 65 5 | 11 9 16 13 9 13 18 14 20 5 | 23 30 31 29 30 27 34 33 36 28 6 | 10 11 23 9 7 12 12 10 24 5 | 28 31 26 31 27 28 31 26 26 27 7 | 10 13 18 8 8 11 13 8 29 5 | 31 34 32 33 29 31 31 24 29 29 8 | 15 12 34 11 8 13 15 8 30 6 | 17 22 35 23 21 18 22 18 31 18 9 | 14 15 25 12 9 10 17 15 19 6 | 19 27 34 25 24 20 27 27 37 22 10 | 12 12 19 10 7 11 13 14 26 5 | 25 30 29 33 27 29 30 29 39 27 11E | 11 27 16 18 9 55 14 11 27 7 | 19 43 24 22 25 41 22 23 33 20 12 | 12 12 13 10 7 52 20 13 33 6 | 20 27 26 24 25 27 31 23 48 23 13 | 11 14 17 12 8 58 14 16 25 7 | 20 33 35 28 25 35 24 21 30 22 14 | 19 18 20 14 7 52 19 14 19 7 | 27 40 34 31 28 35 26 28 32 27 16 | 12 19 20 15 7 43 30 12 31 7 | 24 32 29 32 24 25 29 24 33 26 17 | 19 15 21 19 11 61 27 13 19 8 | 31 32 31 37 28 43 25 28 33 27 18 | 18 22 17 19 9 53 23 17 35 8 | 27 42 37 33 31 40 27 29 42 29 19 | 18 20 18 18 5 58 23 13 37 8 | 28 45 38 38 32 51 32 27 30 31 20 | 13 15 16 17 8 51 24 17 29 7 | 26 32 33 35 27 33 30 21 23 25 21E | 22 23 23 14 5 69 23 15 18 9 | 33 34 37 32 29 59 36 27 42 30 22 | 20 19 19 18 10 52 29 15 33 8 | 25 42 36 31 30 37 29 25 36 26 23 | 13 19 15 10 7 53 17 15 30 7 | 22 36 36 26 26 35 24 22 24 23 24E | 19 19 24 21 12 16 45 18 23 9 | 127 131 123 128 125 123 134 132 129 128 25 | 12 18 20 10 7 18 15 12 25 5 | 20 35 30 26 25 24 25 21 41 23 26 | 13 13 19 11 7 16 19 15 26 6 | 18 25 30 28 22 22 33 25 35 23 27 | 16 13 22 10 6 13 18 12 20 5 | 24 30 33 30 28 26 30 27 35 27 28 | 12 14 17 14 10 56 30 12 50 8 | 21 26 26 25 21 26 30 18 45 20 29 | 14 11 23 11 8 15 19 17 21 6 | 31 34 39 37 33 32 38 31 44 33 30 | 9 11 17 11 9 11 16 11 35 5 | 29 35 35 30 34 32 32 35 43 31 31 | 15 18 20 15 14 52 29 16 24 8 | 19 35 36 27 25 35 30 22 27 22 X32 | 24 --- --- --- 21 54 --- 23 --- 19 | 42 --- --- --- 33 37 --- 49 --- 38 ------+---------------------------------------------------+---------------------------------------------------- RMS | 15 16 20 14 9 41 21 14 29 |T 29 37 36 34 31 36 33 31 38 30 WRMS | 14 16 20 14 9 41 20 11 26 |NE 24 33 32 30 27 31 29 26 34 26 MEDI | 13 15 19 12 8 43 18 14 26 |MD 25 33 33 31 27 33 30 26 35 27 Table 3.1426.2 GPS week: 1426 Day: 2 MJD: 54228.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1 | 12 20 17 14 5 27 15 11 17 6 | 30 34 34 34 28 33 26 29 34 29 2E | 11 16 19 12 8 57 20 11 14 7 | 24 33 26 29 23 35 25 19 29 24 3 | 11 13 22 10 7 21 16 9 27 5 | 29 36 33 31 33 31 36 34 44 32 4E | 16 12 18 16 11 16 23 14 40 7 | 74 71 75 76 72 66 64 70 53 69 5 | 11 13 13 12 5 11 18 11 17 5 | 32 39 41 39 36 35 38 34 38 35 6 | 12 14 19 9 9 10 15 9 26 5 | 27 31 39 32 29 30 32 26 33 29 7 | 11 14 24 10 9 9 14 7 31 5 | 29 33 36 32 29 28 32 25 40 29 8 | 14 17 24 10 9 13 15 8 34 6 | 23 30 38 29 21 23 31 18 34 24 9 | 15 14 19 15 5 16 15 11 18 5 | 25 33 35 31 26 31 28 24 41 28 10 | 15 12 23 12 6 9 16 13 15 5 | 25 30 35 34 25 29 30 28 35 29 11E | 13 22 22 15 9 46 13 17 21 7 | 30 45 35 32 29 34 26 34 33 31 12 | 11 16 15 11 5 45 19 9 28 6 | 29 33 36 32 30 30 32 25 51 30 13 | 12 14 22 15 8 50 14 14 20 7 | 25 33 40 29 25 35 25 19 29 25 14 | 17 15 17 23 7 53 14 12 16 7 | 25 37 28 33 25 35 23 23 27 25 16 | 13 13 15 14 9 48 29 12 34 7 | 34 37 37 34 33 34 32 35 33 34 17 | 16 18 23 16 6 50 25 13 25 8 | 35 37 38 37 32 46 29 28 31 31 18 | 15 22 20 18 9 56 35 18 31 9 | 25 42 35 33 29 38 29 28 30 27 19 | 19 16 21 21 7 59 27 13 32 8 | 31 40 45 41 34 49 32 32 33 34 20 | 13 17 23 19 9 52 28 12 26 8 | 33 31 30 36 31 34 36 21 25 31 21E | 18 25 22 20 11 55 17 19 23 8 | 35 40 31 36 34 36 32 35 29 32 22 | 16 19 17 22 9 51 29 15 32 8 | 28 43 35 33 30 38 31 30 35 28 23 | 14 19 25 13 7 53 17 9 34 7 | 29 42 48 34 28 41 27 25 28 30 24E | 13 15 23 16 11 14 21 10 25 6 | 75 79 74 73 77 73 81 77 78 75 25 | 12 22 26 14 11 19 15 15 26 6 | 27 40 45 34 26 33 32 29 36 32 26 | 12 11 21 16 7 13 21 10 21 5 | 25 33 36 37 28 31 35 31 37 30 27 | 15 18 26 12 6 12 15 9 21 6 | 26 29 29 28 22 23 28 20 31 23 28 | 11 19 25 13 9 47 29 11 48 8 | 27 32 37 31 24 29 36 30 43 28 29 | 11 11 23 18 8 13 17 9 27 6 | 67 71 72 68 69 70 76 72 73 69 30 | 10 12 23 13 7 9 17 11 21 5 | 33 40 37 35 37 36 32 34 38 34 31 | 16 23 26 15 10 52 30 11 24 8 | 30 40 38 29 27 37 33 23 32 27 X32 | 19 --- --- --- 30 52 --- 13 --- 16 | 56 --- --- --- 62 25 --- 49 --- 48 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 17 21 15 8 38 21 12 27 |T 33 39 39 37 34 37 34 32 37 33 WRMS | 14 17 21 15 8 38 21 10 25 |NE 30 37 38 34 31 34 32 29 36 31 MEDI | 13 16 22 14 8 45 17 11 25 |MD 29 37 36 33 29 34 32 29 34 30 Table 3.1426.3 GPS week: 1426 Day: 3 MJD: 54229.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1 | 13 17 19 13 6 19 17 15 16 6 | 25 39 42 29 29 28 30 26 28 27 2E | 10 15 21 10 7 59 16 12 19 6 | 23 34 28 26 25 35 29 22 29 23 3 | 10 21 17 11 6 16 12 13 26 5 | 30 43 37 34 36 34 39 36 43 34 4E | 12 18 30 12 12 17 17 15 49 8 | 67 67 74 65 68 64 59 64 63 63 5 | 11 16 18 14 8 12 17 10 19 5 | 23 36 36 26 30 29 35 28 32 27 6 | 10 11 20 11 7 10 14 16 24 5 | 27 35 39 32 31 28 31 29 28 28 7 | 11 13 19 8 7 8 11 14 28 5 | 31 33 35 32 32 28 31 30 36 29 8 | 15 12 37 12 6 12 13 11 35 7 | 24 39 47 31 32 28 25 26 43 27 9 | 17 14 28 13 5 15 12 10 21 6 | 22 33 44 30 25 27 26 19 38 25 10 | 9 11 19 12 11 11 19 14 17 5 | 23 32 30 28 28 29 28 29 28 25 11E | 13 30 17 14 7 46 13 13 29 7 | 27 54 38 30 33 42 31 28 39 29 12 | 10 16 16 10 6 45 20 10 34 6 | 24 33 32 26 28 33 34 20 47 25 13 | 13 20 20 13 8 54 12 14 21 7 | 29 45 50 35 37 41 36 32 34 32 14 | 17 22 16 15 5 55 16 15 19 7 | 28 40 40 29 26 41 29 22 30 26 16 | 12 16 14 14 8 47 30 13 31 7 | 25 32 31 26 26 29 30 24 30 25 17 | 16 16 19 18 7 55 26 13 21 8 | 35 38 45 41 33 48 35 29 35 32 18 | 16 25 19 22 6 51 26 18 30 9 | 31 44 37 31 34 36 28 35 46 30 19 | 19 30 19 16 5 57 21 17 29 9 | 28 50 40 36 34 50 31 31 33 32 20 | 14 20 19 14 6 55 25 13 20 7 | 32 36 37 31 35 37 34 22 27 31 21E | 16 20 17 16 7 53 15 17 19 7 | 39 45 37 40 41 45 41 37 45 38 22 | 18 20 19 23 7 48 27 16 27 8 | 33 48 40 30 32 39 29 32 40 29 23 | 14 23 15 9 6 53 16 12 17 6 | 29 43 44 33 35 40 30 28 26 29 24E | 14 16 20 17 13 16 29 13 23 7 | 109 113 117 110 111 111 113 114 124 111 25 | 12 17 21 10 5 19 16 11 19 5 | 26 43 45 30 31 30 25 25 31 28 26 | 11 10 18 15 5 13 21 12 21 5 | 20 29 34 30 25 25 28 22 31 23 27 | 19 16 20 13 6 15 14 10 21 6 | 30 48 47 38 37 36 36 35 33 34 28 | 15 15 14 12 8 53 27 11 44 8 | 36 49 47 41 35 34 39 33 49 37 X29 | 12 9 23 18 9 14 19 12 --- 6 | 117 117 112 113 115 115 120 117 --- 114 30 | 9 13 10 13 6 11 15 9 22 4 | 32 46 47 32 36 39 36 31 39 34 31 | 13 17 25 17 11 54 30 16 20 8 | 25 35 35 31 28 42 34 20 31 25 X32 | 19 --- --- --- 20 29 --- 20 --- 14 | 44 --- --- --- 45 42 --- 38 --- 38 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 18 20 14 7 39 20 14 26 |T 35 45 45 38 38 41 38 34 39 35 WRMS | 14 18 20 14 7 39 20 11 22 |NE 31 42 42 35 35 38 35 31 34 32 MEDI | 13 16 19 13 7 29 17 13 21 |MD 29 40 40 31 33 36 31 29 34 29 Table 3.1426.4 GPS week: 1426 Day: 4 MJD: 54230.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1 | 13 15 19 15 3 18 19 12 20 6 | 24 35 39 29 25 30 26 23 24 26 2E | 11 15 12 11 6 57 18 11 17 6 | 23 28 27 24 22 29 28 15 23 21 3 | 14 13 16 11 7 18 13 15 33 6 | 29 36 34 32 32 34 34 34 37 32 4E | 15 16 23 12 10 16 13 11 37 6 | 72 71 78 71 71 70 65 72 65 69 5 | 12 16 14 11 7 14 18 15 17 5 | 26 36 33 34 30 35 34 26 29 29 6 | 11 18 16 11 7 8 11 13 20 5 | 31 39 32 33 30 32 33 28 31 30 7 | 11 17 15 10 6 9 11 13 24 5 | 32 35 34 32 31 32 32 30 31 30 8 | 13 16 27 11 7 14 12 11 31 6 | 23 27 40 26 20 22 26 19 30 23 9 | 16 19 21 11 5 15 19 13 16 6 | 21 29 33 29 21 26 27 19 28 24 10 | 12 17 18 9 6 10 26 10 19 5 | 20 27 33 25 21 23 41 16 25 23 11E | 13 20 25 15 8 49 13 15 35 7 | 26 39 29 28 24 26 28 29 38 26 12 | 10 17 16 10 5 46 19 13 30 6 | 22 32 30 29 24 27 31 20 44 25 13 | 15 18 20 13 5 56 15 11 25 7 | 23 31 38 29 24 33 29 20 26 24 14 | 19 20 18 12 6 54 18 14 19 7 | 27 37 32 27 23 36 24 19 21 24 16 | 12 15 18 11 9 52 31 13 36 8 | 26 34 33 26 25 27 28 29 26 26 17 | 15 19 29 11 8 52 25 14 20 7 | 34 35 46 35 30 39 31 33 31 32 18 | 15 24 17 14 7 58 26 22 31 8 | 25 42 34 32 27 35 25 30 35 27 19 | 19 18 15 15 6 60 24 14 33 8 | 26 39 37 34 27 40 29 22 33 28 X20 | 4 --- --- --- 43 --- --- --- --- 0 | 27 --- --- --- 250 --- --- --- --- 21 21E | 20 18 18 12 7 57 15 16 12 7 | 28 33 31 30 29 34 28 29 30 27 22 | 17 20 19 16 8 52 22 17 28 8 | 27 41 37 31 28 36 31 28 27 28 23 | 16 20 16 12 7 55 16 14 23 7 | 26 37 38 31 27 35 26 21 20 26 24E | 12 21 21 13 8 15 29 11 26 6 | 75 88 87 83 79 79 85 81 87 82 25 | 10 19 21 12 5 17 15 10 20 5 | 23 33 34 24 23 28 26 23 30 24 26 | 15 16 20 11 6 16 38 13 21 7 | 20 30 34 30 22 29 46 23 25 25 27 | 20 14 26 9 5 15 14 10 16 6 | 30 28 43 29 24 25 27 22 26 27 28 | 11 14 16 11 7 53 25 10 44 7 | 27 34 30 32 27 26 31 26 32 27 X29 | 23 31 36 17 15 29 84 17 --- 15 | 127 124 98 118 112 130 128 120 --- 116 30 | 9 15 13 11 7 12 15 14 18 5 | 34 41 38 38 35 39 33 31 35 34 31 | 17 17 25 13 11 55 31 16 28 8 | 26 37 40 31 28 39 35 20 34 26 X32 | 19 --- --- --- 18 34 --- 25 --- 17 | 48 --- --- --- 50 21 --- 57 --- 47 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 18 20 12 7 40 21 13 26 |T 33 40 40 36 40 37 36 32 32 33 WRMS | 14 18 20 12 7 40 21 13 21 |NE 30 38 38 34 39 35 34 29 29 30 MEDI | 14 17 18 11 7 29 18 13 23 |MD 26 35 34 31 27 32 31 26 30 27 Table 3.1426.5 GPS week: 1426 Day: 5 MJD: 54231.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1 | 12 15 17 12 5 25 16 15 20 5 | 29 38 38 32 29 39 30 31 30 31 2E | 9 14 15 7 6 54 14 14 18 6 | 33 38 34 31 32 38 37 32 31 32 3 | 11 21 14 10 6 18 13 10 31 5 | 33 43 34 30 32 34 40 31 41 33 4E | 16 17 24 20 11 20 18 15 38 7 | 69 68 69 74 67 66 62 66 63 66 5 | 13 18 21 12 9 15 32 16 19 7 | 30 35 38 36 34 32 41 31 35 32 6 | 8 15 20 9 6 11 15 14 22 5 | 32 33 37 32 31 34 39 30 33 31 7 | 9 17 17 6 5 11 16 13 18 5 | 33 34 35 28 30 32 37 29 33 30 8 | 14 21 23 10 6 11 11 10 28 6 | 27 37 36 29 28 28 30 29 33 28 9 | 14 22 20 9 5 16 12 13 19 5 | 28 40 36 35 32 32 35 29 39 32 10 | 11 19 21 8 4 8 10 12 25 5 | 29 34 34 29 29 31 33 31 36 29 11E | 15 20 28 13 8 46 20 13 20 7 | 31 39 40 28 28 31 39 28 42 29 12 | 11 23 16 16 7 47 28 17 33 8 | 28 37 35 36 30 32 37 25 51 30 13 | 17 18 24 12 6 47 17 15 22 7 | 34 43 47 35 33 39 36 35 29 34 14 | 19 26 17 11 5 54 22 19 18 8 | 36 47 39 31 31 43 32 28 31 31 16 | 14 14 16 14 10 47 39 15 35 8 | 27 34 27 26 25 32 27 26 31 25 17 | 17 16 23 11 8 54 28 18 23 8 | 37 39 44 39 33 42 38 32 36 35 18 | 15 28 18 13 5 54 26 18 32 8 | 34 47 40 36 35 43 33 31 42 34 19 | 18 19 18 17 5 61 21 15 37 8 | 33 42 45 37 31 50 33 28 39 33 X20 | 4 --- --- --- 25 --- --- --- --- 0 | 24 --- --- --- 28 --- --- --- --- 24 21E | 15 20 16 11 8 66 11 18 20 7 | 39 44 40 41 41 75 36 39 43 38 22 | 17 31 20 17 7 49 27 18 34 9 | 33 50 41 33 31 41 32 30 38 31 23 | 18 19 18 10 6 48 22 16 25 7 | 37 45 43 35 34 41 31 37 28 34 24E | 11 18 20 10 8 16 28 13 29 6 | 95 97 100 95 93 90 93 98 101 96 25 | 11 13 20 12 6 16 15 11 21 5 | 31 38 43 30 31 33 32 31 33 31 26 | 11 13 18 8 5 14 17 15 22 5 | 27 34 37 29 27 28 31 31 30 28 27 | 18 19 21 9 5 14 14 14 25 6 | 39 46 41 35 35 35 36 37 35 36 28 | 11 19 13 12 8 52 26 10 43 8 | 31 44 41 35 33 33 34 35 47 33 29 | 11 12 16 10 12 13 17 15 30 5 | 82 83 74 80 85 84 70 81 68 78 30 | 10 15 20 10 6 13 22 16 18 5 | 33 37 37 34 33 31 35 31 31 32 31 | 14 18 22 11 11 59 34 20 25 8 | 28 39 39 28 29 46 38 28 32 29 X32 | 22 --- --- --- 49 40 --- 24 --- 18 | 50 --- --- --- 68 41 --- 49 --- 45 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 19 19 12 7 38 22 15 27 |T 37 44 42 37 37 41 38 36 40 36 WRMS | 14 19 19 12 7 38 22 14 22 |NE 34 41 40 34 34 38 35 33 36 33 MEDI | 14 18 20 11 6 25 18 15 25 |MD 33 39 39 34 32 35 36 31 35 32 Table 3.1426.6 GPS week: 1426 Day: 6 MJD: 54232.000 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 ------+---------------------------------------------------+---------------------------------------------------- 1 | 13 13 17 15 7 19 21 17 23 6 | 30 34 33 34 27 30 28 23 30 29 2E | 11 13 16 8 6 51 13 11 18 6 | 30 36 31 29 29 36 33 25 34 29 3 | 12 15 17 18 9 18 27 14 25 6 | 27 41 38 27 33 33 38 32 36 31 4E | 16 18 24 24 13 19 20 14 50 8 | 78 74 80 81 75 70 74 72 73 74 5 | 13 16 15 10 6 12 25 12 19 5 | 34 46 41 35 41 39 50 42 40 38 6 | 10 13 23 7 8 11 15 12 16 5 | 42 50 50 43 45 42 51 43 47 45 7 | 9 15 21 7 7 11 16 13 19 5 | 40 47 46 41 45 39 46 43 50 43 8 | 14 15 26 12 4 13 14 11 24 6 | 24 33 37 25 23 25 29 20 36 25 9 | 13 17 26 10 5 15 15 18 15 6 | 27 32 38 29 27 28 31 23 32 28 10 | 14 15 23 10 6 10 16 17 19 6 | 24 29 34 26 24 27 33 21 32 25 11E | 12 20 25 16 10 46 24 11 31 7 | 34 47 49 38 33 35 43 28 34 36 12 | 12 19 20 9 5 43 27 13 31 7 | 30 43 32 33 33 38 47 30 54 34 13 | 14 14 19 10 7 52 18 13 20 6 | 26 38 42 29 28 36 35 23 28 29 14 | 19 17 16 10 9 55 23 15 25 7 | 30 40 35 29 29 40 28 27 28 28 16 | 15 13 17 16 9 48 34 13 35 8 | 30 37 32 26 30 35 32 30 33 30 17 | 17 16 27 11 5 56 36 16 33 8 | 37 39 46 39 34 47 42 33 42 35 18 | 16 22 16 11 8 53 27 19 28 8 | 36 49 41 40 41 38 38 43 37 38 19 | 19 16 20 17 4 58 40 17 30 9 | 29 46 48 39 34 57 31 32 34 34 X20 | 16 16 --- 12 7 54 21 16 --- 8 | 26 22 --- 18 26 26 9 8 --- 27 21E | 21 15 16 9 11 51 22 15 20 7 | 65 65 69 58 57 61 63 56 64 61 22 | 18 23 19 15 8 49 29 16 36 8 | 37 49 44 36 37 41 42 38 35 35 23 | 16 17 21 9 4 53 20 15 17 7 | 29 42 41 31 30 39 31 23 26 30 24E | 13 17 17 16 8 14 22 21 25 6 | 85 89 92 83 86 87 87 87 91 86 25 | 11 16 22 10 5 16 22 10 20 5 | 26 42 34 29 29 30 34 25 33 29 26 | 14 13 23 12 4 11 22 21 23 6 | 23 33 42 32 27 24 34 28 38 28 27 | 19 16 20 12 5 12 17 12 22 6 | 29 37 37 28 29 29 33 28 36 29 28 | 9 19 25 14 8 53 26 12 52 9 | 35 47 52 37 34 35 43 31 60 37 29 | 17 14 64 12 11 16 36 24 29 10 | 54 58 68 59 57 56 68 58 46 57 30 | 11 14 11 10 5 10 26 11 24 5 | 41 54 47 41 46 46 49 45 34 43 31 | 16 17 25 15 10 53 40 17 31 9 | 29 42 41 34 32 49 40 26 32 30 X32 | 18 --- --- --- 40 76 --- 23 --- 23 | 49 --- --- --- 63 45 --- 61 --- 45 ------+---------------------------------------------------+---------------------------------------------------- RMS | 15 16 23 13 7 37 25 15 28 |T 36 44 45 37 38 40 41 35 41 37 WRMS | 14 16 21 13 7 37 23 12 22 |NE 32 41 41 33 34 37 37 32 37 33 MEDI | 14 16 20 11 7 43 22 15 24 |MD 30 42 41 34 33 38 38 30 36 34 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 4.1426 GPS week: 1426 MJD: 54226.0-54232.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2948 |U 21 23 48 |U 19 26 59 |U 13 20 27 | emr | emr 2852 |U 32 28 59 |U 18 29 57 | 18 17 36 | esa | esa 2742 | 31 31 59 |U 20 28 62 | 18 19 41 | gfz | gfz 2832 |U 28 30 56 |U 19 26 56 |U 16 17 34 | igr | igr 2875 | 26 32 57 | 19 28 61 | 20 18 42 | igs | igs 2908 | 23 32 57 | 22 31 64 | 20 17 41 | jpl | jpl 2928 | 31 26 54 | 20 25 68 | 18 24 37 | mit | mit 2852 |U 22 24 49 |U 19 30 60 |U 16 19 34 | 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 5.1426.0 GPS week: 1426 Day: 0 MJD: 54226.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 | 37 52 70 | 16 36 60 | 15 18 20 | emr | emr 2880 | 39 51 75 | 15 46 62 | 20 15 22 | esa | esa 2784 | 39 45 72 | 14 33 51 | 19 14 24 | gfz | gfz 2860 | 38 51 72 | 17 42 55 | 17 14 19 | igr | igr 2918 | 42 71 73 | 15 34 54 | 24 10 28 | igs | igs 2949 | 42 72 79 | 17 39 64 | 19 15 30 | jpl | jpl 2959 | 44 40 78 | 17 35 61 | 20 25 31 | mit | mit 2880 | 39 49 69 | 16 42 65 | 15 17 21 | Table 5.1426.1 GPS week: 1426 Day: 1 MJD: 54227.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2946 | 10 10 32 | 22 33 80 | 14 15 23 | emr | emr 2880 | 39 22 52 | 17 34 65 | 16 14 23 | esa | esa 2784 | 34 30 57 | 23 38 80 | 15 11 29 | gfz | gfz 2860 | 42 43 76 | 18 28 63 | 14 13 23 | igr | igr 2927 | 27 21 54 | 24 37 81 | 22 12 38 | igs | igs 2928 | 13 11 34 | 25 37 79 | 19 13 34 | jpl | jpl 2965 | 23 14 45 | 23 32 82 | 18 19 26 | mit | mit 2880 | 16 11 40 | 21 32 67 | 14 15 23 | Table 5.1426.2 GPS week: 1426 Day: 2 MJD: 54228.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2948 | 31 17 44 | 15 20 50 | 12 19 29 | emr | emr 2880 | 62 34 84 | 19 28 56 | 15 12 33 | esa | esa 2784 | 61 34 83 | 18 23 55 | 14 15 34 | gfz | gfz 2861 | 41 22 55 | 17 22 44 | 15 15 34 | igr | igr 2880 | 29 17 43 | 15 19 52 | 17 15 34 | igs | igs 2933 | 24 14 41 | 21 25 52 | 19 12 41 | jpl | jpl 2963 | 41 24 56 | 17 21 64 | 15 23 37 | mit | mit 2880 | 29 15 40 | 17 33 60 | 13 15 30 | Table 5.1426.3 GPS week: 1426 Day: 3 MJD: 54229.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2949 | 17 21 53 | 18 25 50 | 13 18 30 | emr | emr 2880 | 19 22 56 | 16 23 47 | 17 17 41 | esa | esa 2784 | 16 22 55 | 17 25 51 | 16 15 38 | gfz | gfz 2861 | 15 21 54 | 16 23 47 | 15 13 35 | igr | igr 2921 | 20 28 66 | 16 27 42 | 19 17 41 | igs | igs 2928 | 22 36 71 | 20 29 58 | 20 15 44 | jpl | jpl 2932 | 23 19 53 | 18 22 60 | 17 23 36 | mit | mit 2880 | 16 22 57 | 17 25 56 | 14 16 33 | Table 5.1426.4 GPS week: 1426 Day: 4 MJD: 54230.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2941 | 20 22 53 | 23 24 56 | 13 31 30 | emr | emr 2784 | 25 25 58 | 18 24 61 | 21 23 49 | esa | esa 2688 | 25 25 52 | 20 25 66 | 21 27 55 | gfz | gfz 2765 | 22 26 53 | 18 21 47 | 20 24 47 | igr | igr 2834 | 23 33 62 | 22 28 69 | 19 28 49 | igs | igs 2834 | 23 32 63 | 22 28 66 | 21 22 50 | jpl | jpl 2866 | 30 31 61 | 21 19 79 | 21 31 50 | mit | mit 2784 | 20 25 50 | 19 25 63 | 20 28 47 | Table 5.1426.5 GPS week: 1426 Day: 5 MJD: 54231.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2951 | 19 22 43 | 19 22 51 | 12 19 29 | emr | emr 2784 | 23 28 50 | 22 23 52 | 20 24 49 | esa | esa 2688 | 23 32 41 | 24 25 53 | 22 31 60 | gfz | gfz 2760 | 21 29 44 | 24 25 60 | 19 26 52 | igr | igr 2782 | 23 29 53 | 23 24 55 | 21 32 58 | igs | igs 2849 | 22 33 57 | 27 31 61 | 21 25 55 | jpl | jpl 2866 | 31 35 45 | 25 22 63 | 20 28 49 | mit | mit 2784 | 20 29 46 | 24 25 54 | 20 29 54 | Table 5.1426.6 GPS week: 1426 Day: 6 MJD: 54232.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2950 | 16 20 42 | 21 24 64 | 13 19 28 | emr | emr 2880 | 17 16 37 | 20 24 61 | 17 17 38 | esa | esa 2688 | 18 28 51 | 23 25 79 | 20 22 50 | gfz | gfz 2860 | 15 21 37 | 20 21 73 | 15 15 31 | igr | igr 2869 | 17 25 47 | 22 25 74 | 20 15 44 | igs | igs 2941 | 17 27 52 | 22 28 70 | 20 15 36 | jpl | jpl 2946 | 24 21 39 | 20 23 64 | 15 21 32 | mit | mit 2880 | 15 20 42 | 20 26 59 | 16 16 30 | 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 6.1426 GPS week: 1426 MJD: 54226.500-54232.500 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 -44 52 -34 7 | -6 12 | 20 11 29 81 5 | 5 emr uuuxu | 16 17 -89 390 5 | 56 57 | 48 17 103 116 8 | 6 esa uuuuu | 9 1 47 -49 7 | -3 25 | 25 33 85 103 16 | 8 gfz uuuuu | -4 3 -53 1 -1 | -1 9 | 18 9 50 38 2 | 2 igr xxxxx | 16 -7 42 54 5 | -2 14 | 39 26 108 73 6 | 5 irf xxxxx | -7 6 59 -25 -2 | -8 16 | 17 7 54 53 4 | 5 jpl uuuuu | 14 26 -63 111 -13 | 2 29 | 32 20 130 42 16 | 9 mit uuuuu | -30 -10 76 -35 5 | 34 37 | 58 19 72 94 8 | 7 ngs uuuuu | 23 37 -18 60 -7 | 12 16 | 51 34 141 83 10 | 1 sio uuuuu | -51 -28 60 -26 -5 | 35 38 | 35 28 117 38 8 | 4 Table 7.1426.0 GPS week: 1426 Day: 0 MJD: 54226.500 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 | -2 -57 16 -66 5 | -12 16 emr uuuxu | -13 23 -84 211 9 | 48 49 esa uuuuu | 22 64 -71 -183 23 | -13 28 gfz uuuuu | -20 -1 -77 -19 -5 | -2 9 igr xxxxx | -23 -18 42 96 6 | -10 16 irf xxxxx | -22 3 94 -32 0 | -15 21 jpl uuuuu | 37 45 12 143 17 | -16 51 mit uuuuu | -106 24 62 -78 5 | 23 29 ngs uuuuu | 82 -6 77 180 -1 | 10 14 sio uuuuu | -54 -42 155 -25 4 | 28 33 Table 7.1426.1 GPS week: 1426 Day: 1 MJD: 54227.500 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 | -13 -31 43 12 1 | -9 14 emr uuuxu | 4 36 -113 298 2 | 51 53 esa uuuuu | -2 16 103 -20 -1 | -8 29 gfz uuuuu | 26 8 -107 18 0 | -2 9 igr xxxxx | 45 -20 205 72 12 | -7 15 irf xxxxx | -21 11 -14 -69 -5 | -12 19 jpl uuuuu | 47 50 69 96 -12 | -4 38 mit uuuuu | -103 -9 22 -106 4 | 27 32 ngs uuuuu | 49 -13 94 53 0 | 12 16 sio uuuuu | -43 -36 -55 -80 -11 | 32 36 Table 7.1426.2 GPS week: 1426 Day: 2 MJD: 54228.500 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 -59 75 -142 4 | -8 13 emr uuuxu | -44 27 -210 340 15 | 52 54 esa uuuuu | 6 -26 -1 -138 -6 | -8 28 gfz uuuuu | -12 17 -86 30 -1 | -2 9 igr xxxxx | -37 8 -138 -31 11 | -5 15 irf xxxxx | 7 -2 139 -13 1 | -10 18 jpl uuuuu | -35 13 -206 120 -5 | 3 30 mit uuuuu | -26 -18 202 32 13 | 30 34 ngs uuuuu | 61 57 38 132 -3 | 13 17 sio uuuuu | -29 -71 152 -46 -1 | 34 37 Table 7.1426.3 GPS week: 1426 Day: 3 MJD: 54229.500 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 | -30 -32 88 109 6 | -7 13 emr uuuxu | 63 -17 -221 376 9 | 55 57 esa uuuuu | -30 5 161 111 30 | -6 27 gfz uuuuu | 16 0 -96 -49 -2 | -2 9 igr xxxxx | 72 -55 80 -23 -3 | -2 15 irf xxxxx | -22 14 11 -49 1 | -9 17 jpl uuuuu | 49 -3 -69 31 -21 | 9 24 mit uuuuu | -22 -2 13 -94 12 | 34 37 ngs uuuuu | 26 54 114 -79 -7 | 12 16 sio uuuuu | -94 -34 -75 27 -4 | 35 38 Table 7.1426.4 GPS week: 1426 Day: 4 MJD: 54230.500 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 | 33 -42 16 -91 12 | -5 10 emr uuuxu | -31 18 32 500 6 | 59 60 esa uuuuu | 47 -21 -31 -124 7 | 1 24 gfz uuuuu | -12 2 -23 37 -2 | -1 8 igr xxxxx | 43 19 43 182 -1 | 0 12 irf xxxxx | 7 -3 38 43 -1 | -6 13 jpl uuuuu | -10 40 88 164 -12 | 10 22 mit uuuuu | -2 -21 19 83 7 | 38 39 ngs uuuuu | 20 50 -48 20 -19 | 14 16 sio uuuuu | -94 -27 68 14 -1 | 36 39 Table 7.1426.5 GPS week: 1426 Day: 5 MJD: 54231.500 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 -40 78 -14 15 | -2 10 emr uuuxu | 67 21 -59 515 1 | 61 62 esa uuuuu | -4 -29 118 -1 -16 | 5 23 gfz uuuuu | -6 4 8 33 3 | 0 8 igr xxxxx | 5 6 -35 32 6 | 1 12 irf xxxxx | -16 14 98 -94 2 | -5 12 jpl uuuuu | 19 14 -251 111 -30 | 8 20 mit uuuuu | -11 -11 147 -150 7 | 40 41 ngs uuuuu | -6 41 -271 47 -23 | 13 15 sio uuuuu | -45 16 212 -15 -3 | 37 39 Table 7.1426.6 GPS week: 1426 Day: 6 MJD: 54232.500 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 -52 51 -49 7 | 2 11 emr uuuxu | 63 9 35 487 -9 | 64 65 esa uuuuu | 26 -4 53 11 8 | 10 17 gfz uuuuu | -19 -11 12 -46 1 | 3 8 igr xxxxx | 3 12 99 50 4 | 6 12 irf xxxxx | 18 1 49 41 -8 | -1 9 jpl uuuuu | -7 18 -80 113 -25 | 3 17 mit uuuuu | 58 -38 68 67 -11 | 45 46 ngs uuuuu | -72 77 -128 65 3 | 12 15 sio uuuuu | 4 -6 -36 -56 -18 | 41 42