Date: Fri, 03 Aug 2007 10:50:20 +0200 To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-15342] Wk 1436 IGS Final Orbits Message-ID: <46B2EC4C.mailx3I81D0LWC@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 03 Aug 01:50:32 PDT 2007 Message Number 15342 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1436 (Jul 15, 2007 - Jul 21, 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: igs1436[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1436[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1436[0-6].cls IGS GPS clock combination summary report. igs14367.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14367.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 | SCUB 0 | GFZ | HARB 0 | JPL | 12 13 23 31 SCOR WAB2 0 | MIT | SYDN USN3 1 | ESA | YELL 1 | JPL | 12 31 MDVJ NISU SCOR WAB2 1 | MIT | 32 2 | JPL | 12 13 14 16 20 23 31 SCOR WAB2 3 | ESA | BILI KIT3 3 | GFZ | BOGT DAV1 YAKT 3 | JPL | 13 16 20 23 31 3 | MIT | 32 YAKT 4 | JPL | NISU SCOR 5 | ESA | BILI KERG MAC1 MATE YELL 5 | JPL | SCOR 5 | MIT | 32 FAIR 6 | COD | MCM4 6 | ESA | LPGS YELL 6 | GFZ | DAV1 6 | JPL | 12 16 20 23 31 NISU SCOR 6 | MIT | NISU 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 G29 | 2 | | 2 | | | | 1 | 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 | .5 .1 1.1 -4 -5 9 -.42 EMR | -.2 -1.1 4.0 -10 27 9 -.27 ESA | 3.1 -2.2 -11.4 -23 2 -20 -1.46 GFZ | 1.2 .2 1.5 -7 -30 1 -.78 JPL | 3.9 2.2 15.8 206 -62 172 -.26 MIT | -5.5 2.9 4.5 -11 -8 -1 -.40 NGS | 4.7 .7 3.8 3 -42 21 -1.39 SIO | -4.1 3.0 -12.8 69 9 24 -.20 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 1.1436.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1436.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 2.1436.[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 3.1436.[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 5.1436.0-6). 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 1436 summary. (Jul 15, 2007 - Jul 21, 2007) Table 1.1436.a GPS week: 1436 MJD: 54296.000-54302.000 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 170| 1 -1 2 0 -12 -45 -.12 12 12 | -66 -676 37 99 | 0 0 0 12 14 26 .03 | 558 790 emr 62| 2 0 3 23 -27 -10 .38 17 17 | 5292 -1353 52 115 | 0 2 0 18 18 14 .04 | 2512 1042 esa 64| 0 0 5 105 -64 -10 .28 21 21 | 5402 -1293 51 130 | 1 1 2 37 46 41 .04 | 2514 1020 gfz 184| 0 2 -5 8 16 35 -.12 12 12 | 173 -291 33 129 | 0 1 1 25 21 17 .04 | 323 564 igr n/a| 0 1 2 -4 -2 -5 -.02 7 7 | -12222 -2512 29 76 | 0 0 1 8 9 16 .02 | 5377 1258 jpl n/a| -3 -6 -11 -226 38 163 .18 39 39 | 4637 -1404 80 238 | 6 4 3 17 5 14 .07 | 2796 960 mit 267| -2 0 0 32 -5 -29 -.08 17 17 | 93 -339 60 130 | 1 0 0 37 24 22 .04 | 352 524 ngs 204| 0 0 1 1 75 13 -.24 15 12 | -95 -643 2591 4135 | 0 0 1 19 25 19 .05 | 525 765 sio 101| 1 0 1 -145 -76 21 .08 22 22 | --- --- --- --- | 1 1 1 29 33 31 .06 | --- --- Table 1.1436.b GPS week : 1436 MJD: 54296.000-54302.000 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 | 5 5 6 5 6 6 6 | 2 | 8 8 8 8 7 8 8 | 3 | 6 5 6 5 6 5 9 | 4 | 5 5 6 5 5 6 6 | 5E | 6 6 6 6 7 6 7 | 6 | 5 5 5 5 6 5 5 | 7 | 6 5 5 5 5 5 5 | 8 | 7 6 7 6 6 6 6 | 9 | 6 6 6 6 6 6 6 | 10E | 8 8 9 8 8 9 8 | 11 | 7 7 7 7 8 7 7 | 12 | 7 7 8 7 8 7 8 | 13 | 7 7 7 7 7 7 7 | 14 | 7 7 8 7 7 7 7 | 16 | 7 7 7 7 8 8 7 | 17 | 8 7 7 6 7 7 8 | 18E | 7 6 6 6 6 6 6 | 19 | 8 6 7 7 7 7 7 | 20E | 6 6 6 6 7 6 6 | 21 | 8 7 8 7 8 8 8 | 22E | 6 6 6 6 6 6 6 | 23 | 7 7 7 7 7 7 7 | 24 | 5 5 5 6 6 5 6 | 25 | 6 6 6 12 6 6 5 | 26 | 5 5 6 5 6 5 5 | 27 | 6 5 6 6 6 6 5 | 28 | 7 7 8 7 7 8 7 | 29 | 5 6 28 6 6 6 13 | 30 | 6 6 6 6 7 6 6 | 31 | 7 7 8 8 8 9 8 | 32E | 18 18 18 18 19 22 24 | 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 2.1436.0 GPS week: 1436 Day: 0 MJD: 54296.000 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 170| 0 0 0 0 8 -27 -.15 12 12 | 3 -444 35 96 | 73 -39 | emr 62| 1 -3 3 39 -44 -12 .38 14 14 | 9719 -1679 49 110 | 4 -25 | esa 64| 0 2 6 74 -50 -35 .23 20 20 | 9802 -1555 52 129 | -49 -13 | gfz 184| 0 2 -6 -5 26 40 -.16 12 12 | 480 -505 33 127 | 62 -1 | igr n/a| 0 1 0 -11 8 11 -.04 7 7 | -3699 -2838 30 75 | 18 -41 | jpl n/a| -6 -5 -9 -251 45 181 .19 40 40 | 9382 -1788 75 154 | 23 -28 | mit 272| -1 0 0 69 -13 -40 -.06 17 17 | 215 -283 64 137 | -30 31 | ngs 204| 0 0 0 -28 60 2 -.26 15 11 | -180 -200 2484 3958 | 59 -35 | sio 101| 0 1 3 -105 -54 61 .14 23 26 | --- --- --- --- | 4 -24 | Table 2.1436.1 GPS week: 1436 Day: 1 MJD: 54297.000 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 170| 1 -1 2 -17 6 -23 -.14 11 11 | -850 490 38 103 | 80 -52 | emr 62| 1 -2 4 19 -48 -14 .37 15 15 | 7822 -2949 48 119 | 34 -39 | esa 64| -1 2 4 70 -41 25 .28 22 21 | 7969 -2895 49 116 | -23 33 | gfz 184| 0 1 -5 3 42 2 -.10 12 12 | 158 52 33 114 | 57 -19 | igr n/a| 0 0 1 -6 5 -35 -.03 6 6 | -6784 -4173 25 69 | 49 -71 | jpl n/a| 1 -10 -5 -232 42 158 .12 41 41 | 7711 -3028 83 240 | 24 -24 | mit 272| -2 0 0 59 -12 -3 -.03 16 17 | -473 541 58 114 | -22 25 | ngs 204| -1 0 0 15 33 16 -.26 15 11 | -813 436 2939 3807 | 18 -8 | sio 101| 0 0 1 -113 -71 44 .13 22 23 | --- --- --- --- | 5 -4 | Table 2.1436.2 GPS week: 1436 Day: 2 MJD: 54298.000 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 170| 1 -1 1 -6 -8 -51 -.14 13 13 | 283 -948 38 105 | 78 -45 | emr 62| 2 -3 3 55 -27 -5 .34 15 15 | 5132 -2225 54 136 | -40 -21 | esa 64| 1 0 6 88 -3 -55 .24 21 21 | 5288 -2208 54 145 | 20 78 | gfz 184| 0 4 -5 -39 37 47 -.08 14 14 | -59 110 32 134 | 80 -34 | igr n/a| 0 0 3 -2 0 -15 -.02 7 7 | -10809 -3749 28 85 | 21 -28 | jpl n/a| -8 0 -15 -211 33 153 .15 40 40 | 4195 -538 79 479 | -21 13 | mit 272| -4 0 0 63 -36 1 -.14 17 17 | 281 -631 57 131 | -35 26 | ngs 204| -1 0 1 7 67 4 -.33 15 12 | 180 -820 2424 3904 | -50 -20 | sio 101| 1 -1 1 -137 -124 22 .10 21 20 | --- --- --- --- | 32 23 | Table 2.1436.3 GPS week: 1436 Day: 3 MJD: 54299.000 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 170| 1 -1 1 -8 -20 -19 -.10 12 12 | -420 -488 35 100 | 66 -13 | emr 62| 2 1 4 7 -18 3 .40 21 21 | 3836 -965 56 109 | 8 -59 | esa 64| 1 0 9 122 -41 -42 .27 20 19 | 3956 -931 48 122 | 47 85 | gfz 184| -1 2 -6 25 -17 41 -.07 11 11 | -123 82 38 146 | 33 -7 | igr n/a| 0 1 2 -11 0 0 -.00 7 7 | -13849 -2429 27 85 | -12 -32 | jpl n/a| -4 -9 -14 -220 31 184 .16 39 39 | 3644 -2166 71 178 | -17 -22 | mit 272| -2 0 0 49 -16 -54 -.10 17 17 | -341 132 55 127 | -22 -18 | ngs 204| 0 0 2 -2 110 -9 -.24 14 11 | -393 -529 2621 4302 | -54 -22 | sio 101| 3 0 1 -164 -101 20 .01 23 23 | --- --- --- --- | 42 10 | Table 2.1436.4 GPS week: 1436 Day: 4 MJD: 54300.000 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 170| 1 -1 2 0 -24 -79 -.11 12 12 | 920 -1990 41 102 | 39 -5 | emr 62| 2 0 2 5 5 2 .34 17 17 | 3829 -1347 54 100 | 49 -76 | esa 64| -3 -1 1 136 -149 -33 .31 21 21 | 3846 -1144 52 144 | -51 146 | gfz 184| -1 1 -3 8 12 22 -.10 12 12 | 723 -1283 33 135 | 6 31 | igr n/a| 0 0 2 6 -13 -3 -.02 7 7 | -15308 -2452 35 65 | 12 -11 | jpl n/a| 3 -7 -12 -207 42 166 .12 38 38 | 2861 -1038 91 311 | -11 -37 | mit 272| -2 0 1 18 -14 -37 -.12 18 18 | 454 -915 66 135 | 2 -30 | ngs 204| -1 1 1 30 99 50 -.22 15 12 | 883 -1949 2338 4062 | -1 -65 | sio 101| 2 -1 0 -182 -91 45 .00 23 21 | --- --- --- --- | 75 -17 | Table 2.1436.5 GPS week: 1436 Day: 5 MJD: 54301.000 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 170| 1 -1 3 12 -23 -30 -.09 12 12 | -200 -1176 44 105 | 27 29 | emr 62| 3 0 2 18 -25 -38 .36 16 16 | 3180 -350 52 101 | -5 -44 | esa 64| 1 -2 1 170 -91 11 .30 24 23 | 3316 -317 52 112 | -74 180 | gfz 184| 0 2 -4 34 0 55 -.13 12 12 | 155 -730 36 113 | -24 36 | igr n/a| 1 1 2 -11 -18 -4 -.02 7 7 | -17207 -1403 34 82 | -46 -13 | jpl n/a| -13 -9 -16 -211 33 151 .29 38 38 | 2356 -860 98 189 | -41 -18 | mit 272| -2 0 1 -7 37 -49 -.10 17 17 | 231 -820 66 149 | 13 -52 | ngs 204| 0 -1 2 -13 80 7 -.23 16 13 | -198 -1162 2654 4675 | 12 -56 | sio 101| 2 0 0 -174 -21 -19 .04 22 21 | --- --- --- --- | 70 -27 | Table 2.1436.6 GPS week: 1436 Day: 6 MJD: 54302.000 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 170| 1 -3 2 19 -25 -82 -.07 11 11 | -198 -178 32 85 | 17 12 | emr 62| 2 0 3 15 -34 -11 .44 22 19 | 3527 44 57 130 | 68 -4 | esa 64| 0 0 6 79 -74 54 .33 20 20 | 3639 -1 53 147 | 2 53 | gfz 184| 0 0 -5 31 11 37 -.19 11 11 | -123 231 29 135 | 25 13 | igr n/a| 0 0 0 6 0 10 .00 7 7 | -17903 -544 27 74 | -21 -42 | jpl n/a| 1 -2 -9 -246 41 149 .26 39 39 | 2310 -411 67 117 | 11 -13 | mit 272| -1 2 1 -24 15 -19 -.05 19 19 | 287 -399 60 122 | 24 1 | ngs 204| -1 0 1 4 77 20 -.16 14 11 | -148 -278 2677 4238 | 8 -53 | sio 101| 1 2 0 -139 -72 -20 .12 24 22 | --- --- --- --- | 21 -13 | 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 3.1436.0 GPS week: 1436 Day: 0 MJD: 54296.000 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 | 8 10 18 12 7 21 13 11 18 4 | 17 22 24 21 17 24 15 16 21 16 2 | 14 16 20 14 7 53 24 17 26 7 | 17 29 34 26 21 42 23 23 28 21 3 | 10 12 12 15 11 16 17 16 17 5 | 37 44 46 41 39 42 37 35 41 37 4 | 8 15 23 11 7 16 11 12 10 5 | 24 34 21 20 26 30 29 27 23 24 5 | 10 12 21 13 6 11 19 18 22 6 | 24 34 36 31 25 30 34 23 39 27 6 | 7 12 15 12 6 9 13 12 31 5 | 27 33 28 22 29 30 29 31 34 27 7 | 6 13 13 13 8 9 13 9 37 5 | 21 29 21 18 23 20 23 23 36 21 8 | 12 17 23 12 6 15 14 17 33 6 | 16 30 28 24 18 22 25 24 32 20 9 | 14 16 23 13 6 18 15 16 23 6 | 11 25 24 23 16 23 20 15 20 16 10E | 18 16 22 16 12 16 23 23 22 7 | 81 80 78 87 89 85 81 89 89 82 11 | 11 17 21 16 9 51 20 14 21 7 | 27 44 42 29 29 34 23 27 29 27 12 | 13 15 19 10 6 57 19 15 24 7 | 34 41 45 40 34 58 27 32 36 35 13 | 13 16 26 12 7 52 18 16 18 7 | 22 39 42 28 26 47 24 26 24 25 14 | 17 15 18 12 5 60 16 13 18 7 | 19 29 26 23 18 35 18 17 24 18 16 | 12 16 17 14 5 55 16 19 18 7 | 21 39 32 35 26 53 28 27 29 28 17 | 14 14 19 11 11 53 27 16 24 7 | 34 37 40 37 35 47 35 35 34 33 18E | 9 13 24 9 6 57 14 11 21 6 | 23 25 22 22 22 26 22 21 26 20 19 | 10 16 30 14 8 52 24 15 20 7 | 27 31 38 30 31 42 29 30 33 28 20E | 8 13 14 9 7 51 14 11 22 5 | 18 27 30 21 20 33 16 20 18 19 21 | 17 16 21 15 9 50 23 15 28 7 | 19 32 33 28 23 43 18 20 25 22 22E | 10 12 22 9 6 57 16 10 17 6 | 22 23 18 20 19 25 21 22 25 19 23 | 12 16 25 11 8 49 21 17 27 7 | 22 36 36 26 24 44 22 21 30 23 24 | 7 12 12 11 6 13 15 10 26 5 | 26 27 35 21 28 27 27 30 41 27 25 | 11 12 25 11 6 15 16 14 15 5 | 20 31 29 23 19 27 30 25 31 22 26 | 8 11 20 12 4 20 10 12 18 5 | 16 23 27 20 18 21 17 19 18 18 27 | 16 15 21 10 8 14 12 17 17 5 | 19 30 32 23 18 25 26 24 31 22 28 | 13 15 19 15 5 57 13 12 29 7 | 21 34 34 35 26 44 27 23 39 26 29 | 8 11 20 12 5 20 8 11 14 4 | 28 36 31 31 30 37 32 30 13 30 30 | 10 14 21 13 7 14 22 17 22 6 | 17 24 27 25 19 26 27 21 32 20 31 | 12 19 17 10 7 61 18 14 20 7 | 13 34 30 23 23 45 23 19 17 20 X32E | 22 --- --- --- 26 52 32 31 --- 17 | 56 --- --- --- 46 65 55 58 --- 57 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 14 20 12 7 40 17 15 23 |T 25 33 32 28 27 37 27 27 30 26 WRMS | 12 14 20 12 7 40 17 11 25 |NE 22 32 32 27 24 35 25 24 29 24 MEDI | 11 15 20 12 7 49 16 15 21 |MD 22 31 31 24 24 34 26 24 29 23 Table 3.1436.1 GPS week: 1436 Day: 1 MJD: 54297.000 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 | 10 13 22 10 5 19 13 9 25 5 | 11 20 29 17 12 19 14 13 22 15 2 | 12 18 17 14 6 55 25 14 28 7 | 14 28 29 24 17 34 19 16 23 17 3 | 11 12 16 11 6 13 14 13 19 5 | 34 42 37 35 36 37 37 39 41 36 4 | 6 18 14 12 5 16 14 10 20 5 | 16 22 23 17 17 20 23 19 23 17 5 | 9 11 22 12 5 12 19 15 26 5 | 27 32 34 31 29 32 35 28 43 30 6 | 9 10 18 11 6 10 13 15 12 4 | 19 27 27 22 23 25 28 28 26 23 7 | 7 14 23 13 6 10 12 13 19 5 | 19 29 30 21 22 23 25 26 35 23 8 | 12 13 20 11 6 13 15 13 27 5 | 15 26 26 20 17 21 23 19 31 18 9 | 12 16 27 13 7 19 14 16 22 6 | 13 26 24 22 15 22 19 18 20 17 10E | 12 19 28 11 7 17 16 32 18 7 | 43 48 50 46 46 45 46 56 45 44 11 | 10 17 22 15 10 54 21 14 18 7 | 17 38 37 24 24 33 16 21 18 20 12 | 13 15 27 9 5 58 19 15 28 7 | 24 33 38 27 24 48 19 22 29 24 13 | 10 15 23 13 7 51 16 15 15 6 | 14 33 36 24 21 40 20 17 22 20 14 | 16 15 27 13 6 58 14 12 20 7 | 12 28 32 24 17 31 18 15 24 18 16 | 13 17 16 12 7 57 15 19 19 6 | 14 31 26 25 19 41 21 25 25 21 X17 | 12 14 16 11 7 51 25 15 --- 7 | 21 26 25 24 20 28 26 24 --- 21 18E | 9 12 20 7 6 57 14 10 23 6 | 15 20 22 14 14 23 23 13 23 15 19 | 9 14 13 10 7 53 23 11 23 6 | 17 26 30 19 21 29 21 23 29 20 20E | 8 14 21 9 5 51 12 12 24 6 | 12 24 30 18 14 28 11 14 25 15 21 | 16 16 17 14 9 49 21 13 24 7 | 12 31 30 22 17 33 13 14 18 16 22E | 11 11 20 9 7 57 13 9 18 5 | 12 18 18 13 12 22 19 13 18 13 23 | 12 16 26 11 8 53 20 17 28 7 | 13 33 36 22 19 40 17 17 20 18 24 | 7 12 16 12 5 12 15 10 14 4 | 19 25 26 17 18 24 19 23 30 20 25 | 11 11 24 12 6 15 15 12 22 5 | 16 31 28 22 18 25 28 20 27 20 26 | 6 10 23 10 4 18 9 18 17 5 | 13 19 20 16 14 19 15 20 16 14 27 | 15 11 27 10 5 12 11 12 18 5 | 14 26 34 21 18 22 24 20 27 19 28 | 12 15 21 15 6 58 13 15 20 6 | 12 27 30 26 18 32 20 21 19 17 X29 | 8 16 23 11 6 18 8 19 --- 5 | 24 29 29 26 26 30 28 32 --- 25 30 | 11 13 24 12 6 15 22 13 28 6 | 11 19 26 17 13 22 26 15 36 16 31 | 13 21 19 10 8 64 16 13 26 7 | 13 27 27 20 17 37 19 16 23 16 X32E | 19 --- --- --- 28 38 38 34 --- 17 | 48 --- --- --- 62 45 53 51 --- 48 ------+---------------------------------------------------+---------------------------------------------------- RMS | 11 15 22 12 6 41 16 15 22 |T 18 28 29 22 21 30 23 22 26 21 WRMS | 11 15 21 12 6 41 17 11 23 |NE 16 28 29 22 19 29 22 21 26 20 MEDI | 11 14 21 11 6 38 15 13 20 |MD 15 27 29 22 18 29 21 20 24 19 Table 3.1436.2 GPS week: 1436 Day: 2 MJD: 54298.000 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 | 9 14 25 12 5 36 13 11 20 6 | 12 22 28 16 13 34 16 15 24 14 2 | 14 13 19 17 8 51 21 16 30 7 | 13 27 29 27 20 39 20 26 21 20 3 | 9 11 17 16 7 12 17 15 19 5 | 34 40 47 32 35 31 28 38 35 34 4 | 10 17 20 16 10 13 11 11 18 5 | 18 32 23 20 29 27 28 30 19 23 5 | 12 10 26 14 8 13 21 18 20 6 | 31 38 37 36 34 38 39 32 41 33 6 | 10 10 18 13 7 10 16 15 17 5 | 21 28 32 23 26 26 24 29 21 23 7 | 12 11 14 13 7 10 16 12 22 5 | 31 39 27 29 31 32 37 33 44 33 8 | 14 12 23 16 4 14 17 11 30 6 | 14 24 28 27 17 20 24 17 42 21 9 | 11 13 20 13 7 15 17 13 19 5 | 12 25 28 26 18 25 22 22 26 19 10E | 23 27 25 21 11 20 19 31 24 9 | 31 43 49 43 41 43 39 55 39 37 11 | 11 16 27 14 9 50 20 14 21 7 | 23 41 43 24 28 34 20 26 22 24 12 | 15 16 23 10 8 56 21 16 24 7 | 28 37 41 38 29 52 32 30 31 31 13 | 12 18 25 13 8 50 17 13 19 7 | 17 36 37 28 22 41 21 19 27 23 14 | 16 18 21 15 8 57 15 15 20 7 | 14 32 31 23 20 35 19 19 23 20 16 | 13 17 14 12 5 56 14 18 22 7 | 19 36 32 28 25 49 25 26 25 25 17 | 12 13 16 14 7 50 23 12 21 6 | 23 31 34 28 25 40 29 31 28 27 18E | 10 14 20 10 6 54 12 13 18 6 | 18 25 26 24 22 25 23 22 31 22 19 | 11 11 17 13 7 50 22 13 18 6 | 19 29 32 27 23 35 24 22 26 23 20E | 9 14 18 9 7 52 10 12 18 6 | 17 26 26 18 19 32 14 21 21 18 21 | 16 25 20 16 7 47 21 15 30 8 | 17 42 37 30 25 41 18 21 28 25 22E | 11 14 17 11 7 54 10 14 14 6 | 18 26 25 20 21 27 21 22 24 20 23 | 12 18 17 10 7 55 18 16 22 7 | 16 37 31 25 22 41 19 20 24 21 24 | 11 10 18 12 6 10 16 12 22 5 | 24 28 32 26 27 28 21 29 31 25 25 | 13 11 20 15 4 10 19 11 15 5 | 14 30 26 26 18 24 28 22 28 21 26 | 12 13 32 14 9 17 11 19 14 6 | 15 20 31 23 25 31 26 33 23 21 27 | 19 11 25 14 5 12 17 11 13 6 | 12 29 34 28 19 22 24 21 29 22 28 | 14 15 22 18 7 54 18 11 23 7 | 21 34 34 31 25 42 25 22 27 24 X29 | 75 66 80 40 32 77 63 84 --- 28 | 88 33 47 74 70 33 66 123 --- 57 30 | 12 13 18 15 7 15 21 16 17 6 | 15 24 28 22 17 27 27 19 28 20 31 | 13 19 17 11 9 60 16 16 24 7 | 14 30 28 21 19 40 20 17 21 17 X32E | 24 --- --- --- 36 56 30 28 --- 17 | 72 --- --- --- 72 74 62 73 --- 70 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 15 21 14 7 40 17 15 21 |T 23 31 32 28 27 35 27 30 27 26 WRMS | 13 15 21 14 7 40 17 12 20 |NE 21 31 32 28 25 34 26 28 27 24 MEDI | 12 14 20 14 7 50 17 14 20 |MD 18 30 31 26 25 34 24 22 27 23 Table 3.1436.3 GPS week: 1436 Day: 3 MJD: 54299.000 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 | 9 12 21 12 5 21 14 12 22 5 | 17 23 33 21 19 29 21 25 26 19 2 | 14 18 18 14 6 50 23 17 31 7 | 17 28 25 26 19 39 19 19 27 19 3 | 9 14 19 11 6 20 15 10 18 5 | 46 50 60 51 49 49 46 51 49 49 4 | 8 16 14 12 8 14 16 15 20 5 | 17 27 22 16 24 25 24 26 21 19 5 | 12 13 23 13 6 15 18 16 27 6 | 34 44 51 42 38 42 40 39 39 37 6 | 10 13 14 11 6 13 14 11 15 4 | 26 33 36 25 29 29 29 32 24 27 7 | 8 15 16 12 7 17 13 12 23 5 | 28 38 38 28 32 29 29 35 38 32 8 | 12 17 20 11 5 16 17 11 26 5 | 16 30 28 18 20 24 26 25 35 20 9 | 14 18 23 10 8 18 13 14 19 5 | 17 28 30 22 19 26 18 22 22 19 10E | 16 19 27 13 9 18 17 31 25 8 | 44 43 48 38 40 42 41 52 41 41 11 | 9 17 22 12 10 47 21 13 28 7 | 21 39 39 25 26 33 24 25 28 23 12 | 15 19 19 8 6 52 19 14 26 7 | 25 36 35 28 24 41 21 24 32 26 13 | 11 17 20 12 8 50 17 12 20 6 | 19 37 37 26 25 39 22 21 30 22 14 | 16 17 17 11 6 53 14 10 22 6 | 21 32 33 27 22 36 23 22 26 23 16 | 12 16 27 10 7 58 13 16 22 7 | 21 34 38 32 26 50 26 31 24 26 17 | 13 13 15 10 6 52 21 11 21 6 | 29 36 38 34 32 44 31 34 34 31 18E | 9 17 17 7 6 54 12 9 24 6 | 16 25 27 19 17 27 21 16 30 18 19 | 9 16 20 10 10 50 21 11 21 6 | 24 28 36 28 28 39 24 27 31 25 20E | 8 15 16 9 7 51 9 11 19 5 | 13 28 27 18 19 31 15 21 20 17 21 | 17 17 13 15 8 47 20 14 23 7 | 17 30 29 26 22 40 13 18 22 19 22E | 9 18 16 9 7 52 11 9 13 5 | 15 24 26 21 19 27 19 19 26 18 23 | 11 18 18 12 8 50 18 15 24 6 | 18 37 32 25 24 40 21 23 32 22 24 | 10 12 19 14 5 15 15 11 24 5 | 22 25 38 20 23 25 16 25 28 21 25 | 12 74 27 15 5 23 21 12 25 11 | 18 82 31 24 23 26 30 21 31 25 26 | 10 19 18 8 5 14 13 15 17 5 | 21 27 23 23 26 26 27 33 25 23 27 | 16 17 25 11 5 16 13 12 20 6 | 15 33 32 22 20 26 24 23 31 20 28 | 12 17 19 12 5 54 13 12 21 6 | 20 30 37 31 23 43 27 21 30 24 X29 | 10 20 18 8 6 11 10 16 --- 5 | 23 31 28 25 29 31 27 37 --- 26 30 | 12 15 19 12 7 18 22 15 28 6 | 18 29 27 24 20 26 29 22 36 21 31 | 10 23 17 11 9 60 18 15 31 7 | 20 30 30 22 21 39 20 22 30 20 X32E | 26 --- --- --- 64 42 31 31 --- 17 | 38 --- --- --- 62 57 44 49 --- 38 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 21 20 11 7 39 17 14 23 |T 22 33 33 26 26 34 25 27 29 24 WRMS | 12 21 19 11 7 39 17 11 23 |NE 21 34 34 26 25 34 25 27 30 24 MEDI | 11 17 19 11 6 42 16 12 22 |MD 20 30 32 25 24 33 24 25 30 23 Table 3.1436.4 GPS week: 1436 Day: 4 MJD: 54300.000 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 | 11 18 21 11 7 17 15 14 28 6 | 16 28 33 21 16 22 19 23 24 18 2 | 13 16 18 13 6 50 24 13 30 7 | 14 27 28 24 17 34 18 14 28 18 3 | 12 15 28 11 7 17 17 19 19 6 | 25 23 44 26 31 30 22 37 18 25 4 | 7 11 19 12 7 15 16 8 17 4 | 16 20 17 20 19 22 19 16 16 16 5 | 17 10 20 14 7 14 22 15 24 6 | 74 80 77 80 75 78 77 74 75 75 6 | 9 16 24 10 8 12 18 12 20 5 | 21 28 35 21 24 26 24 26 26 22 7 | 10 15 19 11 8 14 14 10 25 5 | 20 28 25 21 23 23 23 24 29 21 8 | 12 14 21 12 5 16 18 13 19 5 | 13 15 18 16 13 16 18 14 25 13 9 | 13 15 22 11 4 14 15 12 19 5 | 15 26 27 23 16 24 18 14 20 18 10E | 14 20 24 12 8 21 17 33 31 8 | 26 26 29 25 25 30 28 42 28 25 11 | 10 26 29 13 8 48 23 17 24 8 | 18 45 42 24 25 34 22 31 22 23 12 | 16 18 24 8 5 53 19 13 30 7 | 20 32 37 26 22 37 16 20 30 22 13 | 12 21 23 14 7 51 18 16 19 7 | 18 32 35 29 24 40 16 22 21 22 14 | 18 16 20 12 7 52 14 13 16 7 | 20 31 31 28 23 33 23 24 23 23 16 | 17 18 22 13 7 56 17 17 20 7 | 18 33 32 31 20 42 20 25 19 23 17 | 11 13 15 11 9 48 23 10 21 6 | 18 25 29 25 23 31 22 21 25 20 18E | 11 15 19 9 6 52 13 12 18 6 | 17 27 23 20 19 27 22 19 32 20 19 | 8 16 14 11 9 52 23 16 22 6 | 18 24 28 23 25 32 18 28 26 21 20E | 10 14 22 11 6 52 13 13 20 6 | 13 27 28 23 18 29 18 20 21 18 21 | 18 17 15 16 9 48 21 15 31 7 | 19 32 31 25 20 39 11 20 23 20 22E | 9 15 15 10 5 49 12 9 20 5 | 15 26 21 21 19 27 18 21 25 19 23 | 12 17 21 12 8 54 20 14 26 7 | 17 33 33 27 22 40 14 21 25 21 24 | 11 13 18 13 5 11 16 16 21 5 | 20 23 30 22 20 22 19 26 26 21 25 | 11 14 21 12 5 17 17 12 21 5 | 15 26 30 21 17 19 24 14 27 17 26 | 11 18 21 7 5 13 16 17 18 5 | 16 24 28 18 18 21 14 26 17 18 27 | 13 15 24 10 4 17 15 12 21 5 | 11 23 32 20 14 19 17 14 26 15 28 | 12 15 17 13 6 54 16 12 18 6 | 13 25 27 22 18 36 21 17 22 17 29 | 11 16 22 8 9 13 13 19 24 5 | 26 32 36 28 27 33 24 31 19 27 30 | 13 15 22 12 7 17 26 13 24 6 | 16 23 26 21 15 23 21 18 26 17 31 | 13 24 23 11 10 59 17 18 27 8 | 21 33 29 26 22 39 23 24 22 23 X32E | 22 --- --- --- 45 52 37 34 --- 19 | 40 --- --- --- 74 36 36 62 --- 41 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 17 21 12 7 38 18 15 23 |T 20 29 31 25 24 31 22 25 25 22 WRMS | 12 17 21 12 7 38 18 12 21 |NE 19 29 32 25 22 31 21 24 25 22 MEDI | 12 15 21 11 7 48 17 13 21 |MD 18 27 29 23 20 30 20 22 25 21 Table 3.1436.5 GPS week: 1436 Day: 5 MJD: 54301.000 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 | 11 15 21 13 5 14 13 12 18 5 | 13 24 27 19 12 22 15 17 18 14 2 | 14 17 21 13 6 50 23 19 28 7 | 16 26 29 22 20 35 17 25 20 18 3 | 10 12 20 11 8 17 19 14 17 5 | 46 47 43 42 44 45 41 43 44 43 4 | 9 16 17 12 8 14 17 12 24 5 | 15 22 21 17 19 23 21 23 19 16 5E | 13 13 20 12 4 17 18 17 20 5 | 33 36 40 34 32 39 40 34 39 34 6 | 11 11 24 10 6 12 15 14 18 5 | 17 19 23 18 19 20 19 19 16 16 7 | 8 14 20 10 7 15 15 12 18 5 | 14 22 20 16 19 20 21 19 25 17 8 | 11 16 25 12 6 19 14 14 23 6 | 13 19 17 19 17 20 20 22 31 16 9 | 12 14 25 11 5 17 13 11 20 5 | 16 24 25 20 16 27 17 17 25 17 10E | 18 21 24 13 9 20 16 35 28 8 | 35 39 40 38 37 45 36 53 36 37 11 | 12 18 25 13 10 43 24 15 25 7 | 20 40 40 28 24 32 18 19 22 21 12 | 13 17 20 10 7 54 19 13 23 7 | 25 34 39 29 23 42 19 22 27 25 13 | 12 14 22 16 9 50 18 16 16 6 | 14 32 34 25 24 38 14 17 18 18 14 | 17 21 18 12 6 46 16 13 19 6 | 17 29 30 21 19 34 19 19 19 18 16 | 14 19 26 10 6 56 16 23 15 7 | 18 31 37 23 18 39 18 21 21 19 17 | 12 10 23 12 6 49 22 15 29 7 | 14 24 28 23 19 32 24 24 32 19 18E | 7 14 13 8 8 53 14 12 26 6 | 15 22 22 19 19 26 20 16 25 17 19 | 9 11 19 13 5 49 22 17 24 6 | 14 23 27 19 18 28 18 19 22 16 20E | 11 13 25 10 4 51 13 11 19 6 | 14 26 28 19 19 32 16 19 20 17 21 | 15 16 21 16 8 46 22 16 27 7 | 17 30 32 27 19 37 12 10 26 17 22E | 9 15 11 9 7 50 11 12 19 5 | 15 22 21 16 16 26 18 17 20 15 23 | 13 17 24 12 7 54 21 15 21 7 | 15 34 31 24 20 40 12 17 20 17 24 | 9 14 13 12 7 12 16 13 15 5 | 22 28 26 23 27 28 18 26 31 23 25 | 10 10 24 13 5 16 15 12 20 5 | 17 29 26 22 21 23 25 20 28 19 26 | 11 17 19 8 5 16 16 12 19 5 | 16 22 24 19 19 26 17 17 17 17 27 | 15 12 28 12 6 18 12 12 21 5 | 16 23 29 22 19 22 19 18 29 17 28 | 11 20 43 11 7 56 14 12 17 7 | 20 31 52 26 23 39 21 25 22 23 29 | 11 15 34 10 6 21 13 14 22 6 | 30 35 41 33 31 40 31 33 19 30 30 | 12 14 21 13 7 17 22 17 22 6 | 13 21 24 20 15 23 21 18 27 16 31 | 13 29 40 9 8 57 16 19 26 8 | 19 39 40 24 22 38 24 26 25 22 X32E | 32 --- --- --- 24 50 48 30 --- 21 | 53 --- --- --- 55 34 40 56 --- 38 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 16 24 12 7 38 17 16 22 |T 20 28 30 23 22 31 21 23 24 21 WRMS | 12 16 23 12 7 38 17 13 21 |NE 18 28 30 23 21 30 20 21 24 19 MEDI | 12 15 21 12 7 43 16 14 20 |MD 16 26 28 22 19 32 19 19 22 18 Table 3.1436.6 GPS week: 1436 Day: 6 MJD: 54302.000 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 | 10 20 28 14 6 12 16 8 20 6 | 15 31 26 21 16 25 17 19 22 15 2 | 13 20 23 13 7 47 25 16 29 7 | 19 33 35 28 21 43 21 22 27 22 3 | 10 59 14 13 8 17 25 13 21 9 | 41 61 44 41 41 40 43 39 43 41 4 | 8 19 21 14 6 16 21 11 16 5 | 20 30 19 19 22 25 26 23 22 19 5E | 15 30 23 13 6 19 20 14 24 7 | 32 49 42 40 35 38 40 35 39 36 6 | 8 14 18 9 7 12 16 12 24 5 | 27 33 26 22 29 29 27 32 25 25 7 | 9 14 16 9 7 13 15 14 22 5 | 25 35 25 22 28 26 26 31 34 25 8 | 10 16 23 11 5 16 15 13 21 5 | 20 22 24 22 19 22 22 19 37 20 9 | 14 20 23 10 4 16 17 13 19 6 | 18 30 24 22 19 24 19 16 26 17 10E | 15 21 21 14 7 21 16 29 36 8 | 44 46 46 42 44 45 38 54 57 43 11 | 10 25 21 11 9 46 25 13 23 7 | 26 47 38 29 30 31 27 27 27 26 12 | 13 24 25 11 4 55 19 14 22 7 | 25 35 35 28 23 42 18 22 25 23 13 | 11 19 20 12 9 51 18 14 17 6 | 19 35 34 26 24 39 22 18 25 20 14 | 14 23 21 13 4 49 14 13 20 7 | 21 32 24 24 20 31 22 25 25 21 16 | 11 26 22 8 6 56 13 17 21 7 | 17 31 21 21 17 40 18 19 21 17 17 | 14 13 20 12 8 47 26 13 33 7 | 28 31 37 34 29 42 31 26 41 28 18E | 7 14 17 10 5 53 12 12 19 6 | 17 27 22 19 16 28 21 17 30 18 19 | 8 12 20 13 6 51 28 11 21 7 | 26 31 31 29 29 40 29 28 33 26 20E | 12 19 15 9 5 53 13 8 17 6 | 18 32 28 24 19 34 18 18 22 20 21 | 14 18 15 15 11 47 24 13 45 8 | 21 33 32 26 21 45 14 20 31 21 22E | 7 18 17 9 8 47 10 11 17 5 | 18 32 26 21 17 28 19 21 24 20 23 | 12 19 17 10 8 57 21 15 26 7 | 18 36 35 24 23 43 19 19 24 20 24 | 9 14 16 12 6 10 19 11 26 5 | 25 30 29 21 25 26 19 29 29 23 25 | 13 13 23 10 5 16 15 10 16 5 | 19 31 29 27 21 26 30 20 32 24 26 | 9 15 26 8 11 12 17 12 18 5 | 21 28 30 25 24 26 19 24 16 22 27 | 12 13 19 9 4 16 11 11 14 4 | 17 26 32 25 19 24 24 18 29 21 28 | 11 21 22 10 4 57 17 12 19 6 | 24 36 29 31 27 42 24 24 23 26 X29 | 16 16 91 14 11 14 18 14 --- 13 | 45 47 94 47 46 50 44 43 --- 48 30 | 11 16 17 12 6 18 22 13 29 6 | 16 23 26 20 18 23 24 20 33 17 31 | 11 23 20 13 10 56 20 13 29 7 | 25 33 38 32 27 48 29 27 26 28 X32E | 31 --- --- --- 35 41 --- 33 --- 23 | 52 --- --- --- 38 28 --- 43 --- 42 ------+---------------------------------------------------+---------------------------------------------------- RMS | 11 22 20 11 7 39 19 14 24 |T 24 34 32 27 25 33 25 25 29 24 WRMS | 11 19 20 11 7 39 19 11 22 |NE 23 33 32 26 24 34 24 24 28 23 MEDI | 11 19 20 11 6 41 17 13 21 |MD 21 32 29 25 23 31 22 23 27 22 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 4.1436 GPS week: 1436 MJD: 54296.0-54302.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2958 |U 20 15 57 |U 13 17 53 |U 14 17 41 | emr | emr 2878 |U 19 15 48 |U 12 19 55 | 14 22 44 | esa | esa 2784 |U 20 13 51 |U 13 15 57 | 13 19 42 | gfz | gfz 2863 |U 19 14 50 |U 10 15 46 |U 13 18 44 | igr | igr 2880 | 19 17 55 | 10 14 48 | 14 21 40 | igs | igs 2956 | 18 15 59 | 12 14 47 | 15 18 44 | jpl | jpl 2961 | 22 13 51 | 12 14 51 | 21 24 58 | mit | mit 2962 |U 18 14 55 |U 12 15 53 |U 13 17 40 | 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 5.1436.0 GPS week: 1436 Day: 0 MJD: 54296.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2966 | 15 11 41 | 14 20 45 | 14 25 38 | emr | emr 2880 | 14 13 32 | 11 19 48 | 17 26 46 | esa | esa 2784 | 17 12 36 | 12 14 52 | 15 23 39 | gfz | gfz 2864 | 18 13 38 | 9 17 44 | 14 20 47 | igr | igr 2880 | 15 16 44 | 10 13 41 | 16 28 39 | igs | igs 2969 | 18 17 51 | 11 16 42 | 15 26 43 | jpl | jpl 2967 | 21 11 39 | 12 16 48 | 23 26 67 | mit | mit 2976 | 15 16 45 | 11 15 45 | 14 21 40 | Table 5.1436.1 GPS week: 1436 Day: 1 MJD: 54297.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 | 14 19 43 | 12 18 50 | 11 16 33 | emr | emr 2880 | 17 17 39 | 13 18 50 | 11 21 34 | esa | esa 2784 | 18 14 39 | 12 15 54 | 10 18 32 | gfz | gfz 2864 | 17 20 42 | 9 13 43 | 11 17 38 | igr | igr 2880 | 17 21 40 | 9 13 45 | 10 18 29 | igs | igs 2950 | 16 20 42 | 11 16 43 | 10 15 31 | jpl | jpl 2963 | 22 16 42 | 11 15 49 | 18 23 46 | mit | mit 2976 | 15 18 38 | 12 13 50 | 11 15 35 | Table 5.1436.2 GPS week: 1436 Day: 2 MJD: 54298.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2956 | 50 32 88 | 12 18 48 | 14 17 50 | emr | emr 2879 | 42 24 69 | 12 21 51 | 18 19 55 | esa | esa 2784 | 44 24 70 | 13 16 55 | 13 16 49 | gfz | gfz 2864 | 25 14 59 | 9 15 43 | 15 15 52 | igr | igr 2880 | 38 24 71 | 10 18 39 | 15 23 47 | igs | igs 2967 | 32 19 71 | 10 19 44 | 13 18 45 | jpl | jpl 2961 | 29 10 61 | 11 15 46 | 19 23 64 | mit | mit 2976 | 30 19 65 | 12 17 47 | 11 18 40 | Table 5.1436.3 GPS week: 1436 Day: 3 MJD: 54299.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2959 | 14 8 62 | 14 16 45 | 16 14 44 | emr | emr 2880 | 15 8 47 | 12 22 44 | 15 19 46 | esa | esa 2784 | 12 8 65 | 14 17 48 | 14 17 44 | gfz | gfz 2866 | 13 11 61 | 13 16 41 | 13 17 41 | igr | igr 2880 | 14 14 65 | 11 14 47 | 16 17 42 | igs | igs 2947 | 14 10 70 | 15 10 39 | 19 13 56 | jpl | jpl 2962 | 19 12 63 | 11 13 46 | 25 22 55 | mit | mit 2976 | 13 8 59 | 11 16 48 | 13 16 38 | Table 5.1436.4 GPS week: 1436 Day: 4 MJD: 54300.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2959 | 16 9 61 | 13 17 62 | 11 19 38 | emr | emr 2880 | 15 14 56 | 13 16 60 | 13 27 45 | esa | esa 2784 | 11 9 49 | 15 15 65 | 14 22 46 | gfz | gfz 2864 | 16 7 56 | 11 15 49 | 11 22 45 | igr | igr 2880 | 15 12 58 | 13 13 55 | 13 25 46 | igs | igs 2960 | 14 12 67 | 13 13 56 | 13 21 43 | jpl | jpl 2962 | 20 16 59 | 14 15 52 | 18 27 49 | mit | mit 2976 | 16 10 72 | 12 12 55 | 11 22 40 | Table 5.1436.5 GPS week: 1436 Day: 5 MJD: 54301.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2959 | 18 15 55 | 12 14 61 | 15 17 46 | emr | emr 2880 | 19 14 45 | 12 15 67 | 12 23 43 | esa | esa 2784 | 22 14 51 | 13 13 66 | 13 18 41 | gfz | gfz 2860 | 19 14 41 | 10 13 51 | 12 19 43 | igr | igr 2880 | 19 17 49 | 10 11 58 | 12 18 38 | igs | igs 2950 | 18 16 47 | 11 11 57 | 13 17 36 | jpl | jpl 2956 | 26 17 49 | 11 13 61 | 21 25 61 | mit | mit 2976 | 19 14 53 | 12 14 62 | 13 15 41 | Table 5.1436.6 GPS week: 1436 Day: 6 MJD: 54302.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2956 | 13 13 53 | 12 16 62 | 15 15 41 | emr | emr 2869 | 15 15 48 | 13 21 66 | 15 21 43 | esa | esa 2784 | 16 12 45 | 13 14 59 | 14 18 44 | gfz | gfz 2859 | 21 18 51 | 9 14 48 | 14 16 44 | igr | igr 2880 | 15 14 57 | 10 15 51 | 16 19 42 | igs | igs 2951 | 16 14 62 | 10 14 52 | 18 20 56 | jpl | jpl 2958 | 18 11 46 | 12 14 57 | 24 25 66 | mit | mit 2880 | 15 12 52 | 12 15 62 | 16 14 48 | 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 6.1436 GPS week: 1436 MJD: 54296.500-54302.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 8 -36 13 -83 -4 | -4 14 | 24 23 67 64 5 | 2 emr uuuuu | 30 2 51 271 6 | 15 25 | 25 33 89 107 12 | 5 esa uuuuu | -88 37 22 -103 -3 | -12 25 | 61 43 72 79 15 | 3 gfz uuuuu | -11 -16 7 -75 3 | -25 31 | 22 30 88 61 9 | 2 igr xxxxx | 26 15 1 30 1 | -3 18 | 17 25 57 51 5 | 2 irf xxxxx | -8 18 14 -85 3 | -9 18 | 7 10 56 73 5 | 3 jpl uuxuu | 10 23 -200 56 8 | -5 24 | 16 15 261 167 14 | 6 mit uuuuu | -6 28 -93 43 -8 | 12 21 | 38 28 68 60 6 | 3 ngs uuuuu | 29 20 -7 14 2 | 0 14 | 27 36 92 132 11 | 1 sio uuuuu | -1 -17 8 -78 -3 | 22 29 | 21 38 74 96 5 | 2 Table 7.1436.0 GPS week: 1436 Day: 0 MJD: 54296.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 22 -45 0 -83 -9 | -2 16 emr uuuuu | 8 24 71 165 17 | 11 23 esa uuuuu | -4 77 24 -104 23 | -8 27 gfz uuuuu | -16 -34 34 -25 -7 | -22 30 igr xxxxx | 24 10 -44 3 -9 | -1 21 irf xxxxx | -17 28 3 -5 7 | -11 21 jpl uuxuu | 11 5 143 -165 31 | -12 26 mit uuuuu | -48 58 -82 -11 -5 | 17 29 ngs uuuuu | 18 -31 -60 35 -16 | 2 16 sio uuuuu | 7 24 -15 68 -1 | 26 35 Table 7.1436.1 GPS week: 1436 Day: 1 MJD: 54297.500 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 | 35 -48 100 32 -10 | -4 16 emr uuuuu | 22 -2 -14 152 13 | 11 23 esa uuuuu | -50 55 -42 13 8 | -9 26 gfz uuuuu | 2 -25 -24 -4 -3 | -27 31 igr xxxxx | 54 -17 16 89 3 | -5 19 irf xxxxx | -17 32 63 -21 6 | -13 20 jpl uuxuu | 7 8 133 -124 20 | -10 26 mit uuuuu | -42 54 -4 -21 -6 | 12 23 ngs uuuuu | -9 14 -84 -109 -2 | 0 16 sio uuuuu | -13 27 40 -98 -3 | 21 29 Table 7.1436.2 GPS week: 1436 Day: 2 MJD: 54298.500 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 | 37 -65 -32 -50 -6 | -4 16 emr uuuuu | 13 53 -82 243 13 | 12 23 esa uuuuu | -86 -7 34 -121 2 | -10 26 gfz uuuuu | 26 -67 185 -34 14 | -27 32 igr xxxxx | 20 -8 68 11 7 | -6 19 irf xxxxx | -8 13 47 2 7 | -12 19 jpl uuxuu | -21 34 -68 -69 6 | -7 25 mit uuuuu | -34 48 -59 6 -4 | 11 22 ngs uuuuu | 12 63 -77 -96 -5 | 0 16 sio uuuuu | -31 -19 17 25 3 | 20 28 Table 7.1436.3 GPS week: 1436 Day: 3 MJD: 54299.500 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 -50 55 -83 -5 | -5 16 emr uuuuu | 50 8 25 457 17 | 14 26 esa uuuuu | -94 -31 42 -88 -12 | -13 24 gfz uuuuu | -2 -17 -38 -66 13 | -27 32 igr xxxxx | 23 28 28 -23 3 | -5 20 irf xxxxx | -9 16 72 -149 5 | -10 20 jpl uuxuu | 13 33 -430 171 -8 | -4 26 mit uuuuu | 9 38 -150 94 -6 | 9 19 ngs uuuuu | 13 70 -1 -107 5 | -1 14 sio uuuuu | -19 -26 128 -194 3 | 20 28 Table 7.1436.4 GPS week: 1436 Day: 4 MJD: 54300.500 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 -23 39 -172 0 | -6 14 emr uuuuu | 67 -33 37 361 1 | 16 28 esa uuuuu | -155 67 -54 -27 -20 | -14 24 gfz uuuuu | -40 10 -49 -113 5 | -27 32 igr xxxxx | 2 4 -16 102 0 | -5 20 irf xxxxx | -9 16 37 -143 3 | -9 20 jpl uuxuu | 28 27 -380 211 -8 | -4 26 mit uuuuu | 21 14 -123 123 -4 | 8 19 ngs uuuuu | 56 17 89 -4 13 | -1 14 sio uuuuu | 8 -59 36 -164 -7 | 20 28 Table 7.1436.5 GPS week: 1436 Day: 5 MJD: 54301.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -26 -26 -105 -93 4 | -4 10 emr uuuuu | 47 6 133 256 -6 | 20 27 esa uuuuu | -177 75 -13 -214 -8 | -14 24 gfz uuuuu | -33 25 25 -177 8 | -25 30 igr xxxxx | 16 47 -97 -22 2 | -2 13 irf xxxxx | 3 1 -61 -152 -1 | -6 14 jpl uuxuu | 21 42 -423 164 12 | 0 19 mit uuuuu | 55 -12 -198 99 -11 | 11 17 ngs uuuuu | 59 -11 149 184 -1 | 1 13 sio uuuuu | 30 -69 -42 -119 -4 | 22 27 Table 7.1436.6 GPS week: 1436 Day: 6 MJD: 54302.500 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 5 33 -128 -1 | -2 11 emr uuuuu | 3 -46 185 267 -12 | 23 28 esa uuuuu | -54 20 161 -180 -17 | -14 24 gfz uuuuu | -14 -3 -81 -106 -5 | -22 27 igr xxxxx | 41 43 50 48 0 | 0 14 irf xxxxx | -1 22 -61 -127 -7 | -3 12 jpl uuxuu | 12 11 -371 202 6 | 4 20 mit uuuuu | -2 -2 -37 13 -20 | 12 17 ngs uuuuu | 52 14 -64 195 17 | 0 12 sio uuuuu | 12 1 -108 -64 -11 | 24 29