Date: Fri, 12 Oct 2007 11:05:27 +0200 To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-15560] Wk 1446 IGS Final Orbits User-Agent: Heirloom mailx 12.3 7/15/07 Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20071012090527.96FF250984@kg20.gfz-potsdam.de> From: igsacc@gfz-potsdam.de (Gerd Gendt3) Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 12 Oct 02:05:41 PDT 2007 Message Number 15560 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1446 (Sep 23, 2007 - Sep 29, 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: igs1446[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1446[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1446[0-6].cls IGS GPS clock combination summary report. igs14467.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14467.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Day | Centre | PRN/STA list ----+--------+--------------- 0 | COD | SANT 0 | EMR | SPT0 0 | ESA | 3 AMC2 SYOG ZAMB 0 | GFZ | 11 CHAT DAV1 0 | JPL | 10 SANT TIDB 0 | MIT | 6 7 19 29 31 KELY TIDB 1 | COD | 3 YELL 1 | EMR | 26 KERG ONSA SPT0 1 | ESA | 3 BILI HARB 1 | GFZ | 21 BAKO 1 | JPL | 26 KERG 1 | MIT | 7 28 29 BILI CHUR HRAO 2 | COD | 6 ARTU 2 | EMR | 26 2 | ESA | 3 6 26 ARTU BILI TSKB 2 | GFZ | DAV1 MALI TLSE 2 | MIT | 29 3 | COD | 6 26 BAKO 3 | ESA | 1 6 26 CRO1 3 | GFZ | NLIB 3 | MIT | 7 29 4 | COD | 6 26 FAIR 4 | EMR | ONSA 4 | ESA | 6 26 BILI TIXI 4 | GFZ | 17 26 4 | JPL | NRIL 4 | MIT | 1 7 NRIL 5 | COD | 6 26 5 | ESA | 6 26 TIDB 5 | JPL | 1 5 | MIT | 1 7 18 29 MATE 6 | COD | 1 26 6 | ESA | 1 3 6 7 26 KIRU SYOG 6 | GFZ | 1 16 6 | JPL | FAIR 6 | MIT | DAEJ FAIR 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 ----+------------+---------- G07 | 2007_09_25 | 2007110 6. The following orbit solutions were excluded from the combination because they were biasing the weighted average (generally indicated by long arc RMS). They were still used for statistics computation. Day | Centre | PRN list ----+--------+--------------- 0 | JPL | 10 7. 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 G03 | | | | 1 | | | 1 | PRN G29 | 2 | | 1 | | 2 | 1 | | 8. 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. 9. 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 | .1 .1 .4 2 -1 1 -.06 EMR | 4.3 -9.7 11.6 32 -11 54 -.17 ESA | 4.5 2.2 -6.7 -15 -25 0 -1.53 GFZ | .9 .1 1.7 -1 -22 5 -.66 JPL | 4.1 4.2 8.6 -6 -9 354 -.06 MIT | 10.5 -3.6 10.8 20 2 -17 -.17 NGS | 2.3 2.3 -.3 36 -39 -1 -.96 SIO | 1.9 4.1 -7.7 85 -86 37 .15 10. 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. 11. 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. 12. 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 1.1446.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1446.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 2.1446.[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 3.1446.[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 5.1446.0-6). 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 1446 summary. (Sep 23, 2007 - Sep 29, 2007) Table 1.1446.a GPS week: 1446 MJD: 54366.000-54372.000 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 172| 0 0 1 30 -24 -80 -.29 13 13 | -292 -427 46 92 | 0 0 1 10 14 30 .03 | 417 614 emr 61| 3 -1 0 -56 -29 -70 .38 17 17 | -105152 -297 64 115 | 1 1 1 21 35 22 .05 | 48872 2031 esa 64| -1 0 0 108 1 -48 .34 22 22 | 2549981 50964 53 164 | 2 1 1 54 86 60 .04 | 1125559 23514 gfz 179| -2 0 -1 48 1 -18 -.14 14 14 | -171 298 38 142 | 0 0 2 30 24 55 .05 | 397 1238 igr n/a| 0 0 -1 26 -23 -56 .05 7 7 | 1728 -681 34 84 | 0 0 1 15 13 26 .02 | 2979 2284 jpl 100| 1 0 0 19 -42 335 .57 18 18 | 3101 -192 38 87 | 1 1 1 24 22 18 .04 | 2002 2075 mit 276| -1 1 2 14 -1 -64 -.31 18 15 | -356 218 48 110 | 0 1 1 40 50 24 .04 | 322 764 ngs 193| 0 0 -2 -51 39 -33 -.31 15 11 | -230 -531 2691 4241 | 0 1 1 30 26 33 .06 | 397 679 sio 99| 0 -2 -2 -169 114 -42 .24 26 23 | --- --- --- --- | 1 1 1 19 36 20 .04 | --- --- Table 1.1446.b GPS week : 1446 MJD: 54366.000-54372.000 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: mm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------+------------------------------------+------------------------------------------ 1E | 7 8 8 8 10 8 8 | 2 | 7 8 7 7 7 7 7 | 3E | 8 7 7 9 8 7 7 | 4 | 6 5 5 5 5 5 6 | 5 | 6 5 6 5 5 5 5 | 6E | 8 8 7 7 8 8 10 | 7E | 15 14 0 12 8 10 7 | 8 | 6 5 5 4 5 5 5 | 9 | 7 6 6 5 5 6 5 | 10 | 7 6 5 5 5 6 6 | 11 | 7 7 7 7 7 7 6 | 12 | 7 7 7 7 7 6 7 | 13E | 6 6 6 5 5 5 5 | 14E | 5 6 6 5 6 6 6 | 16 | 7 7 7 8 8 7 8 | 17E | 5 6 6 6 6 6 6 | 18 | 7 7 7 7 7 7 7 | 19E | 6 6 7 6 6 6 7 | 20 | 7 7 7 7 6 7 7 | 21 | 8 8 8 8 7 7 8 | 22 | 6 7 7 6 7 6 7 | 23E | 6 6 6 6 6 7 6 | 24 | 6 7 7 6 7 7 7 | 25 | 5 5 5 5 5 5 5 | 26E | 9 8 7 7 8 7 8 | 27 | 6 5 6 5 5 6 5 | 28 | 7 8 7 7 7 7 7 | 29E | 15 9 11 10 27 12 27 | 30 | 5 5 6 4 5 4 5 | 31 | 8 8 8 8 8 8 9 | 32 | 15 23 23 13 18 23 20 | 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 2.1446.0 GPS week: 1446 Day: 0 MJD: 54366.000 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 172| -1 0 0 40 -36 -130 -.25 14 13 | -469 -228 51 88 | -1 8 | emr 61| 1 -2 1 -61 -45 -71 .45 19 19 | -120144 -1772 76 126 | 48 27 | esa 64| 0 -2 -1 120 83 -13 .36 23 23 | 7722 -2167 56 152 | -73 -8 | gfz 179| -1 0 -3 35 -20 15 -.20 14 14 | -106 -174 36 138 | -35 34 | igr n/a| 0 0 -1 39 -52 -96 .05 7 7 | 6766 -2797 36 76 | 0 15 | jpl 100| 0 1 0 8 -42 325 .60 32 32 | 6322 -1971 33 81 | 1 25 | mit 276| 0 2 4 6 21 -54 -.38 18 15 | -34 -241 79 162 | 3 -29 | ngs 193| 1 0 -2 -32 31 -90 -.34 16 14 | -380 -314 2131 3592 | 136 59 | sio 99| 0 -4 0 -171 79 -26 .24 25 21 | --- --- --- --- | 66 -60 | Table 2.1446.1 GPS week: 1446 Day: 1 MJD: 54367.000 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 172| 0 0 1 33 -8 -70 -.26 14 14 | -69 -1071 52 94 | 20 -20 | emr 61| 4 0 0 -86 -38 -96 .41 18 18 | 5619 -4159 64 103 | 31 -33 | esa 64| -5 -1 -2 153 -59 -48 .37 22 22 | 2828261 55693 54 162 | -63 -1 | gfz 179| -1 0 -2 40 23 56 -.18 15 15 | 256 -486 40 136 | -6 -7 | igr n/a| 0 0 0 30 -23 -68 .05 8 7 | 5235 -4832 33 87 | 3 -18 | jpl 100| 1 0 0 17 -84 347 .61 16 16 | 5481 -4006 37 78 | 12 8 | mit 276| -1 0 3 27 60 -104 -.34 17 15 | 34 -657 48 92 | 16 -33 | ngs 193| 0 -1 -3 -61 -5 -70 -.41 15 11 | 1 -1217 2598 4301 | 149 105 | sio 99| 1 -2 -1 -136 128 -42 .25 25 23 | --- --- --- --- | 50 -72 | Table 2.1446.2 GPS week: 1446 Day: 2 MJD: 54368.000 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 172| 0 0 0 24 -8 -102 -.28 13 12 | 94 -1227 50 114 | 39 -33 | emr 61| 2 -2 0 -81 -82 -90 .36 19 19 | -124549 290 67 122 | 10 85 | esa 64| -2 0 0 41 148 31 .38 24 24 | 2883603 60385 59 163 | 6 -23 | gfz 179| -1 0 -2 65 5 -93 -.15 15 15 | 168 -894 39 151 | -15 -8 | igr n/a| 0 -1 0 47 -10 -49 .05 8 7 | 571 -41 32 83 | -19 -5 | jpl 100| 1 1 -2 -6 -49 358 .56 16 16 | 1625 403 36 90 | 6 26 | mit 276| 0 1 2 49 -86 -65 -.32 17 14 | -708 71 36 104 | -56 73 | ngs 193| 0 0 1 -26 58 -8 -.28 15 12 | 172 -1434 2821 4136 | 100 63 | sio 99| -1 0 -3 -149 104 -36 .30 25 23 | --- --- --- --- | 82 -52 | Table 2.1446.3 GPS week: 1446 Day: 3 MJD: 54369.000 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 172| -1 0 2 39 -23 -75 -.31 13 12 | 61 98 42 81 | -1 -22 | emr 61| 3 0 0 -29 -59 -45 .41 16 16 | -125261 1992 61 111 | 53 22 | esa 64| -1 0 0 124 -5 -9 .36 22 21 | 2942428 60871 50 158 | 21 -32 | gfz 179| -2 2 0 12 41 -34 -.11 14 14 | -878 2671 35 138 | 11 -45 | igr n/a| 0 0 -1 29 -13 -21 .07 7 7 | -511 1588 35 84 | 30 -36 | jpl 100| 1 0 2 55 -51 353 .53 17 17 | 1014 2103 41 89 | 17 -17 | mit 276| 0 0 1 -33 0 -91 -.27 18 15 | -473 1129 45 100 | 64 -32 | ngs 193| 0 0 -3 -8 51 -16 -.35 14 10 | -2 209 2519 4427 | 97 39 | sio 99| 2 0 -3 -175 61 -47 .28 26 22 | --- --- --- --- | 83 -24 | Table 2.1446.4 GPS week: 1446 Day: 4 MJD: 54370.000 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 172| 0 0 2 12 -22 -91 -.31 12 12 | -813 -46 40 101 | 7 -22 | emr 61| 5 -3 1 -36 1 -81 .36 16 16 | -123859 317 59 122 | -45 -9 | esa 64| -4 0 0 47 -2 -134 .31 20 20 | 3003071 59360 51 157 | -30 28 | gfz 179| -3 1 -4 74 -12 37 -.06 14 14 | -298 562 36 132 | -61 15 | igr n/a| 0 -1 -3 5 -20 -80 .03 8 7 | 374 36 33 89 | -33 -23 | jpl 100| 4 -2 1 -1 -16 334 .57 16 16 | 2393 472 36 90 | -92 -43 | mit 276| -1 1 0 79 -40 -53 -.28 17 15 | -546 628 32 97 | -64 21 | ngs 193| -1 1 -2 -94 56 -8 -.31 16 11 | -752 -79 2735 4598 | 126 65 | sio 99| 0 -4 -1 -187 129 -73 .22 29 21 | --- --- --- --- | 58 -63 | Table 2.1446.5 GPS week: 1446 Day: 5 MJD: 54371.000 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 172| 0 0 2 27 -26 -55 -.32 13 12 | -864 329 40 83 | 26 -8 | emr 61| 2 -1 2 -41 10 -69 .35 16 16 | -123627 663 66 125 | 58 -29 | esa 64| 2 -1 1 190 -66 -43 .30 23 22 | 3062695 60565 56 180 | -63 0 | gfz 179| -1 0 0 15 -26 -52 -.13 13 13 | -425 990 40 141 | 12 24 | igr n/a| 0 0 -1 18 -24 -39 .03 8 7 | 138 496 35 83 | -5 -6 | jpl 100| 1 0 -1 53 -21 322 .52 15 15 | 2667 794 44 92 | 38 5 | mit 276| -2 1 1 -13 -13 -50 -.28 19 17 | -693 1163 50 108 | 50 4 | ngs 193| 0 0 -5 -61 68 -17 -.23 15 11 | -754 135 3110 4542 | 132 22 | sio 99| 0 -1 -1 -179 131 -12 .22 27 22 | --- --- --- --- | 76 -102 | Table 2.1446.6 GPS week: 1446 Day: 6 MJD: 54372.000 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 172| 0 0 0 38 -48 -40 -.30 14 14 | 11 -847 53 86 | -12 10 | emr 61| 5 -2 -1 -59 4 -35 .29 16 16 | -124245 588 55 98 | -24 -26 | esa 64| -1 -1 3 85 -86 -123 .29 22 21 | 3122088 62045 51 182 | 0 -5 | gfz 179| -3 0 0 93 2 -59 -.13 14 14 | 82 -577 42 159 | -47 11 | igr n/a| -1 0 -1 10 -22 -40 .08 8 7 | -475 781 35 88 | 16 -12 | jpl 100| 1 0 0 10 -31 305 .60 16 16 | 2206 858 44 94 | -27 -6 | mit 276| -2 2 2 -16 47 -34 -.31 19 15 | -74 -567 51 107 | -7 -26 | ngs 193| 0 2 -3 -78 15 -21 -.25 16 10 | 102 -1020 2929 4096 | 176 177 | sio 99| 3 -3 -3 -187 169 -57 .19 28 27 | --- --- --- --- | 67 -103 | 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 3.1446.0 GPS week: 1446 Day: 0 MJD: 54366.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- 1E | 17 19 27 17 9 15 23 18 21 7 | 62 64 72 68 67 66 72 67 70 66 2 | 14 20 24 17 5 15 22 14 26 7 | 14 31 30 27 19 25 19 20 20 17 3E | 17 29 23 11 14 15 21 22 21 7 | 113 105 100 110 109 102 111 116 101 107 4 | 9 17 29 9 5 13 15 14 22 6 | 26 39 28 26 31 33 32 33 32 28 5 | 6 17 27 12 7 13 9 14 22 5 | 18 27 42 22 24 28 23 26 37 24 6E | 17 20 25 12 5 19 29 21 27 8 | 101 99 93 98 95 93 99 99 103 96 X7E | 27 25 --- 20 15 26 65 41 38 14 | 12 22 --- 23 16 20 78 50 20 24 8 | 7 17 28 14 7 10 10 16 21 5 | 37 43 44 32 38 40 39 43 44 38 9 | 9 15 37 13 6 9 28 12 20 7 | 27 34 36 28 27 27 27 29 28 26 10 | 11 24 24 13 5 151 12 18 16 7 | 23 33 33 18 23 93 25 25 24 22 11 | 15 17 24 20 6 14 18 14 19 6 | 31 42 43 31 32 42 34 28 31 30 12 | 14 19 26 14 6 14 13 20 28 6 | 21 36 47 35 27 40 23 22 32 28 13E | 12 17 19 15 6 16 16 16 18 6 | 15 33 25 19 20 27 21 17 25 18 14E | 16 15 10 9 6 16 12 14 14 5 | 24 29 30 23 23 26 23 30 23 23 16 | 16 19 16 13 8 14 16 20 32 6 | 24 38 35 31 26 36 23 28 24 25 17E | 10 17 15 10 4 14 13 9 28 5 | 59 63 62 58 59 63 57 59 26 59 18 | 19 19 17 16 6 17 17 17 28 7 | 20 35 32 28 23 34 21 22 24 22 19E | 11 17 20 9 6 17 15 14 11 5 | 16 31 29 21 19 28 23 22 24 20 20 | 15 19 22 15 4 16 22 17 29 7 | 27 39 36 33 28 37 38 30 24 29 21 | 15 18 18 16 5 19 26 17 33 7 | 24 42 37 32 29 41 29 26 40 29 22 | 12 18 20 15 6 12 15 17 26 6 | 22 38 35 29 24 32 27 23 31 25 23E | 13 16 14 14 3 17 19 12 17 5 | 17 30 28 21 22 31 24 22 27 22 24 | 9 19 16 12 7 11 10 14 40 6 | 35 43 29 34 37 39 37 38 62 36 25 | 8 17 21 12 6 9 11 12 25 5 | 27 34 41 23 32 34 29 30 38 29 26E | 23 21 22 18 9 17 34 22 22 8 | 76 66 77 76 73 80 64 76 73 71 27 | 17 17 25 13 7 12 10 11 22 6 | 27 34 37 21 29 31 29 31 29 27 28 | 14 20 18 17 6 16 19 13 38 7 | 14 34 35 29 22 35 18 21 31 21 X29E | 23 34 --- 24 16 26 21 70 30 14 | 69 76 --- 75 64 64 69 87 20 68 30 | 8 14 18 13 4 10 8 15 18 4 | 27 35 41 27 33 35 30 35 31 30 31 | 17 18 30 18 7 14 17 19 28 7 | 33 45 41 33 33 39 34 29 31 32 X32 | 17 --- --- --- 27 --- 22 23 --- 14 | 18 --- --- --- 44 --- 23 45 --- 22 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 19 23 14 7 32 18 16 25 |T 34 44 43 37 37 44 38 39 37 35 WRMS | 13 19 23 14 7 32 15 14 21 |NE 24 36 36 28 29 37 28 29 32 27 MEDI | 14 18 22 14 6 15 17 16 22 |MD 26 36 36 29 29 35 29 30 31 28 Table 3.1446.1 GPS week: 1446 Day: 1 MJD: 54367.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- 1E | 19 19 28 22 10 14 26 22 23 8 | 55 63 77 65 62 63 65 63 63 60 2 | 13 18 35 18 8 17 20 14 29 7 | 16 35 37 29 21 29 21 18 16 20 3E | 17 18 26 12 12 15 19 15 24 6 | 89 86 88 86 89 84 89 89 82 85 4 | 7 11 27 9 6 10 10 12 20 5 | 20 25 28 16 23 26 25 23 23 19 5 | 6 11 17 12 5 13 8 13 26 5 | 19 22 30 22 20 26 20 19 32 19 6E | 16 26 22 15 5 22 27 18 24 8 | 106 97 102 101 105 104 119 106 111 103 X7E | 26 26 --- 20 11 26 60 32 31 13 | 13 19 --- 21 18 20 75 48 21 24 8 | 5 12 21 10 6 12 12 9 19 4 | 33 38 43 31 36 39 39 34 39 35 9 | 12 14 23 14 7 8 18 13 24 5 | 23 25 23 18 20 23 24 19 20 18 10 | 12 15 21 15 14 15 13 15 13 5 | 22 26 27 20 22 38 19 27 20 19 11 | 14 21 27 20 6 14 20 14 22 7 | 20 39 36 25 22 36 21 21 22 21 12 | 16 18 23 14 5 15 16 12 34 6 | 19 34 37 30 23 33 23 17 25 21 13E | 12 18 19 16 9 14 16 16 18 6 | 14 35 27 18 18 26 15 12 19 17 14E | 14 17 12 11 6 18 12 16 14 5 | 30 27 24 25 28 34 23 32 31 28 16 | 17 22 17 13 8 22 15 21 30 7 | 16 36 28 25 19 35 21 25 21 21 X17E | 13 16 15 8 5 15 15 11 --- 5 | 33 40 40 37 33 38 30 35 --- 36 18 | 19 25 19 19 9 17 18 14 26 7 | 19 35 31 25 20 35 20 17 21 20 19E | 12 21 22 13 7 15 17 20 13 6 | 12 27 29 18 15 26 20 19 18 17 20 | 16 18 24 16 7 18 20 16 21 7 | 15 34 29 25 20 33 20 19 18 18 21 | 17 22 19 16 5 19 26 14 39 8 | 21 41 36 31 26 39 28 24 40 26 22 | 13 20 18 16 5 16 18 13 25 6 | 20 33 35 25 23 34 21 17 29 22 23E | 13 18 17 13 6 18 16 13 18 6 | 13 30 26 17 18 31 15 16 21 16 24 | 9 18 22 14 5 15 15 6 37 6 | 37 36 37 36 37 40 39 35 57 36 25 | 9 13 17 10 5 10 8 10 20 4 | 19 32 33 18 24 31 21 21 38 25 26E | 24 18 28 17 15 18 16 16 23 7 | 42 44 39 42 42 44 34 43 49 41 27 | 19 13 17 10 5 11 10 11 18 5 | 20 29 33 19 23 30 24 19 31 23 28 | 15 22 23 17 5 19 21 14 37 7 | 16 32 35 26 22 35 20 20 31 19 X29E | 16 31 --- 17 10 20 15 21 --- 9 | 73 81 --- 80 73 71 78 82 --- 74 30 | 8 9 22 12 6 11 6 13 13 4 | 20 24 33 19 23 28 22 20 22 19 31 | 18 22 25 20 6 20 19 19 24 7 | 29 48 44 31 32 41 29 28 27 28 X32 | 22 --- --- --- 38 --- 31 41 --- 22 | 37 --- --- --- 58 --- 18 63 --- 34 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 18 22 15 8 16 17 15 25 |T 29 39 38 32 32 39 33 33 33 31 WRMS | 13 18 22 15 7 16 15 11 23 |NE 22 32 33 24 25 33 23 24 28 23 MEDI | 14 18 22 14 6 15 16 14 23 |MD 20 34 33 25 23 34 23 23 25 22 Table 3.1446.2 GPS week: 1446 Day: 2 MJD: 54368.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- 1E | 17 18 30 16 13 15 30 23 23 8 | 69 74 83 74 75 75 77 77 84 74 2 | 13 16 22 19 6 14 17 15 28 6 | 16 29 30 31 20 26 20 22 19 18 3E | 17 20 23 14 11 16 21 21 23 7 | 122 119 107 119 120 113 123 123 107 118 4 | 9 14 18 11 6 13 7 10 19 4 | 20 32 29 27 24 31 25 26 28 23 5 | 7 23 31 12 5 12 9 11 20 5 | 18 32 42 24 19 26 19 21 28 20 6E | 15 22 24 10 5 20 24 17 20 7 | 90 82 80 87 83 79 98 86 90 85 X7E | 7 --- --- --- 141 --- --- --- --- 0 | 95 --- --- --- 87 --- --- --- --- 96 8 | 7 11 19 12 7 8 8 14 23 4 | 26 31 39 26 30 34 29 30 28 28 9 | 12 18 23 15 6 11 13 15 17 5 | 25 31 34 25 23 27 26 27 25 23 10 | 10 11 21 12 7 14 13 8 17 5 | 19 26 28 23 21 26 19 23 25 19 11 | 16 20 27 22 6 12 19 15 27 7 | 24 37 38 31 22 34 23 26 22 24 12 | 12 19 23 17 6 15 13 19 28 6 | 18 32 39 33 22 31 19 21 24 20 13E | 11 15 20 15 7 14 15 14 15 5 | 17 32 33 27 20 29 23 19 23 21 14E | 11 22 14 12 7 18 13 13 13 5 | 25 34 35 27 28 31 27 32 23 25 16 | 14 21 17 14 6 19 15 17 31 6 | 25 40 38 31 27 38 24 28 30 28 X17E | 11 15 14 12 6 19 14 14 --- 5 | 40 43 39 40 39 45 41 37 --- 39 18 | 14 20 19 17 6 21 19 16 34 7 | 17 35 35 27 22 34 20 20 23 20 19E | 11 25 22 13 9 19 19 16 16 6 | 13 32 25 22 15 27 21 16 15 17 20 | 14 21 31 16 5 14 21 16 25 7 | 22 37 43 27 25 33 28 29 25 24 21 | 15 22 21 16 5 23 23 15 34 7 | 16 39 42 30 23 37 29 20 30 23 22 | 14 17 25 17 8 18 18 16 28 7 | 20 34 39 26 24 32 24 19 29 22 23E | 12 14 13 11 7 18 17 15 16 5 | 20 31 29 27 21 32 27 20 25 24 24 | 10 18 35 14 8 15 11 11 40 7 | 25 32 45 32 28 27 36 27 41 27 25 | 9 12 19 12 6 10 10 13 27 5 | 20 31 29 24 25 31 24 22 36 23 26E | 18 18 16 15 11 19 18 16 23 6 | 32 31 33 34 25 36 30 25 37 28 27 | 14 13 33 12 8 10 10 18 23 6 | 26 30 44 24 27 29 25 28 22 25 28 | 12 19 18 18 8 14 17 15 42 7 | 17 35 38 31 26 35 21 25 31 23 X29E | 20 39 --- 24 15 26 18 20 --- 11 | 146 141 --- 153 133 138 146 135 --- 140 30 | 7 34 23 11 5 12 11 12 18 6 | 21 48 38 24 22 29 24 24 28 24 31 | 16 19 43 18 11 19 19 14 26 7 | 30 46 43 36 35 41 34 35 34 32 X32 | 25 --- --- --- 44 --- 20 45 --- 22 | 15 --- --- --- 56 --- 19 63 --- 21 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 19 24 15 8 16 17 15 25 |T 35 44 42 39 37 41 36 36 34 36 WRMS | 12 19 24 15 7 16 14 12 23 |NE 21 34 37 28 26 31 24 26 27 23 MEDI | 12 19 22 14 7 15 17 15 23 |MD 22 34 38 27 25 32 25 26 28 24 Table 3.1446.3 GPS week: 1446 Day: 3 MJD: 54369.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- 1E | 17 28 26 13 11 17 21 19 25 7 | 51 66 61 57 55 69 61 53 78 56 2 | 13 18 22 17 9 16 19 13 27 6 | 15 32 31 28 23 29 25 23 19 20 3E | 17 21 29 15 11 23 34 24 27 8 | 140 138 127 138 139 135 140 144 134 137 4 | 10 13 18 10 9 16 12 8 18 4 | 24 31 30 27 28 35 27 27 32 26 5 | 8 13 21 14 6 11 8 11 25 5 | 16 25 27 20 19 22 21 25 26 18 6E | 14 23 18 10 8 17 30 18 21 7 | 75 74 65 76 74 72 85 81 73 74 X7E | 34 19 --- 15 22 28 47 23 32 12 | 116 107 --- 106 103 113 98 104 114 106 8 | 6 11 18 12 8 10 9 6 22 4 | 36 45 42 37 41 43 39 38 39 38 9 | 10 13 25 14 4 9 9 10 15 5 | 21 25 34 21 23 22 27 24 24 21 10 | 9 12 21 11 7 11 13 10 20 4 | 25 27 31 19 24 29 25 26 23 23 11 | 13 15 24 25 7 15 17 16 18 6 | 15 32 38 21 20 32 23 17 23 18 12 | 14 16 22 19 5 15 21 13 29 6 | 20 31 30 35 22 34 23 22 18 21 13E | 10 14 18 12 6 14 15 10 19 5 | 11 26 27 16 16 24 16 16 17 14 14E | 12 16 15 9 6 19 16 13 11 5 | 24 28 27 22 22 26 19 27 25 21 16 | 17 20 21 13 8 27 16 16 37 7 | 21 36 31 30 25 37 18 23 26 22 X17E | 14 18 17 10 8 16 15 11 --- 5 | 61 64 64 56 58 63 58 58 --- 58 18 | 16 17 18 17 6 21 18 15 33 7 | 19 34 30 26 20 32 21 17 22 20 19E | 9 18 27 12 9 21 18 15 15 6 | 15 29 19 19 15 26 21 18 18 17 20 | 16 18 19 16 5 15 17 15 27 6 | 18 34 34 30 22 32 28 23 22 22 21 | 16 18 17 16 5 21 28 14 33 7 | 17 34 35 30 23 35 31 19 32 23 22 | 13 16 18 14 6 17 18 14 28 6 | 21 34 33 26 21 32 28 22 28 23 23E | 13 15 18 9 8 21 18 12 18 5 | 17 29 26 23 20 32 25 21 22 20 24 | 9 12 22 11 8 14 17 8 42 6 | 38 36 40 37 37 41 39 44 56 38 25 | 7 11 21 11 6 12 10 10 27 4 | 25 30 34 21 26 32 28 26 39 26 26E | 15 17 21 13 9 24 18 19 27 7 | 23 24 35 24 22 37 23 23 38 23 27 | 12 11 17 12 6 11 11 11 24 5 | 24 31 30 22 27 31 24 26 34 25 28 | 13 17 19 17 6 14 20 15 42 7 | 15 34 38 28 23 33 12 24 34 20 X29E | 19 22 --- 14 18 30 15 26 --- 9 | 91 91 --- 100 74 73 84 82 --- 84 30 | 7 8 19 12 4 11 10 11 10 4 | 24 29 33 22 25 27 30 29 27 25 31 | 18 18 38 15 9 20 16 19 25 7 | 39 46 47 36 36 43 38 39 38 37 X32 | 12 --- --- --- 13 --- --- 13 --- 13 | 18 --- --- --- 25 --- --- 29 --- 18 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 16 22 14 7 17 18 14 26 |T 34 43 39 38 35 43 37 37 38 35 WRMS | 12 16 21 14 7 17 15 10 22 |NE 22 32 34 27 25 32 26 26 29 24 MEDI | 13 16 19 13 8 16 17 13 25 |MD 23 32 33 27 24 32 27 26 27 23 Table 3.1446.4 GPS week: 1446 Day: 4 MJD: 54370.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- X1E | 17 18 35 17 10 --- 23 20 --- 9 | 46 53 62 44 47 --- 47 48 --- 47 2 | 13 18 20 19 7 12 18 14 25 6 | 18 29 29 30 21 27 20 22 23 19 3E | 17 16 25 15 7 19 27 26 23 8 | 99 97 99 104 97 95 102 101 90 98 4 | 10 17 20 11 7 9 14 11 17 5 | 20 29 32 20 24 30 28 28 26 23 5 | 5 13 16 14 8 11 11 14 24 4 | 14 22 24 15 23 26 22 22 33 17 6E | 12 18 19 14 7 17 34 18 24 7 | 57 57 56 60 57 55 63 63 56 56 X7E | 16 21 --- 14 13 17 33 18 20 8 | 71 58 --- 61 81 61 71 66 58 71 8 | 9 18 24 14 7 7 7 12 26 5 | 35 45 48 36 39 43 37 41 46 38 9 | 8 17 22 12 12 8 13 13 20 5 | 20 26 32 18 28 25 26 28 20 20 10 | 9 16 21 14 6 12 10 11 28 5 | 22 33 34 21 27 30 30 28 39 25 11 | 14 16 20 21 6 15 14 17 24 6 | 18 34 36 26 22 32 17 21 23 19 12 | 13 17 19 15 6 16 16 13 35 6 | 16 30 37 29 22 34 18 20 35 21 13E | 12 14 11 11 7 16 13 13 20 5 | 9 28 24 18 19 27 17 22 19 16 14E | 10 15 13 12 6 20 17 15 12 5 | 32 39 32 35 33 39 38 37 37 34 16 | 15 17 24 12 6 23 17 23 38 7 | 25 37 32 32 24 43 18 27 33 26 X17E | 10 14 18 10 7 17 22 14 --- 6 | 62 69 64 67 65 72 71 66 --- 66 18 | 15 15 16 18 7 18 18 16 37 7 | 19 35 35 28 23 34 23 20 27 22 19E | 10 13 20 12 11 23 17 21 16 6 | 18 29 30 27 17 29 23 23 20 21 20 | 15 18 18 15 7 16 17 15 24 6 | 20 38 31 27 21 32 25 22 25 22 21 | 15 17 20 14 5 19 24 14 40 7 | 21 40 40 29 29 42 32 24 39 28 22 | 13 15 15 16 8 17 19 16 32 6 | 24 36 36 28 26 34 31 22 38 26 23E | 10 13 19 10 9 19 16 13 18 5 | 16 29 20 20 20 31 27 26 23 20 24 | 6 14 21 10 7 13 20 6 51 6 | 26 31 34 27 29 30 26 29 67 27 25 | 8 16 23 10 5 9 10 9 34 5 | 18 30 37 21 25 30 21 27 40 23 26E | 17 15 19 19 10 25 15 25 23 7 | 32 37 40 30 30 41 28 34 34 30 27 | 13 16 17 11 7 9 10 10 29 5 | 23 32 33 24 26 33 25 28 37 25 28 | 13 18 25 17 6 16 15 19 43 7 | 14 31 35 25 20 33 16 16 34 18 X29E | 28 43 --- 80 40 68 53 73 --- 26 | 117 112 --- 149 98 111 118 115 --- 113 30 | 5 16 22 13 7 10 14 10 13 4 | 21 27 33 19 27 29 28 23 25 21 31 | 17 18 34 16 14 20 17 16 27 7 | 51 59 47 46 53 55 49 48 53 48 X32 | 16 --- --- --- 38 --- 21 36 --- 17 | 19 --- --- --- 40 --- 26 45 --- 22 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 16 20 14 8 16 17 16 29 |T 32 41 39 37 35 41 36 36 37 34 WRMS | 12 16 20 14 7 16 15 11 21 |NE 22 33 35 26 27 33 25 27 34 24 MEDI | 13 16 20 14 7 16 17 15 24 |MD 21 34 34 28 27 33 27 28 34 25 Table 3.1446.5 GPS week: 1446 Day: 5 MJD: 54371.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- 1E | 17 18 38 13 10 18 27 20 26 8 | 34 41 64 35 36 45 40 41 46 38 2 | 15 17 22 16 7 12 19 13 26 6 | 18 33 30 30 21 29 25 25 22 24 3E | 14 18 26 16 7 14 21 25 20 7 | 112 105 107 110 110 102 112 117 98 109 4 | 9 12 20 9 7 8 17 9 18 4 | 21 27 31 25 24 26 29 27 29 25 5 | 6 13 18 7 6 8 10 8 27 4 | 17 24 22 21 21 21 22 24 37 22 6E | 20 22 23 13 13 16 37 22 21 8 | 83 74 81 78 78 72 93 82 78 77 X7E | 17 19 --- 14 10 19 43 22 24 9 | 69 58 --- 62 75 66 73 64 64 72 8 | 7 14 21 9 9 10 17 11 23 5 | 50 55 58 54 51 57 58 51 62 53 9 | 10 14 31 9 10 10 15 14 17 5 | 21 25 27 20 22 21 22 27 22 21 10 | 8 17 24 15 7 11 10 11 26 5 | 18 26 31 17 21 21 22 27 27 21 11 | 16 17 23 17 7 15 17 14 20 6 | 21 30 34 22 23 30 18 16 23 20 12 | 13 15 22 11 6 13 18 13 35 6 | 14 28 37 25 18 31 17 16 32 18 13E | 10 15 17 9 8 14 18 13 15 5 | 11 29 24 19 19 27 21 20 18 19 14E | 15 12 13 9 6 20 17 15 13 5 | 27 25 29 29 25 29 29 26 27 26 16 | 15 15 18 14 5 20 18 17 35 6 | 23 35 30 31 27 39 20 30 23 26 X17E | 10 13 23 10 6 14 19 11 --- 5 | 43 48 56 47 45 50 46 45 --- 45 18 | 14 15 13 13 4 19 18 14 37 6 | 18 34 30 26 21 35 21 21 29 22 19E | 11 15 21 12 5 19 18 17 17 6 | 16 26 22 19 15 25 20 16 19 17 20 | 16 17 23 13 8 25 22 18 24 7 | 20 36 35 29 23 32 27 26 20 24 21 | 17 16 16 13 6 20 27 16 37 7 | 17 36 36 31 27 40 29 23 39 27 22 | 17 13 14 13 6 16 18 13 31 6 | 20 32 28 26 22 30 23 19 29 21 23E | 13 13 20 13 7 20 22 18 22 6 | 18 27 24 19 17 31 26 27 27 19 24 | 8 21 22 10 7 10 19 8 51 6 | 29 29 36 30 29 31 36 32 55 29 25 | 5 11 25 11 7 12 14 12 26 5 | 25 29 36 24 28 32 28 31 34 28 26E | 15 18 23 15 10 19 18 15 25 6 | 21 27 37 24 23 33 26 22 31 24 27 | 11 13 27 12 9 10 15 12 24 5 | 20 26 33 20 23 27 22 23 27 21 28 | 12 20 22 15 6 14 14 16 41 7 | 16 32 39 30 24 36 22 25 31 24 X29E | 18 26 --- 23 13 23 35 31 --- 11 | 136 125 --- 146 116 119 132 125 --- 129 30 | 6 12 18 8 7 9 12 9 16 4 | 20 23 29 22 24 24 25 28 26 24 31 | 20 15 33 17 10 19 17 20 22 7 | 50 59 71 52 49 58 47 50 54 52 X32 | 25 --- --- --- 25 --- 15 46 --- 22 | 27 --- --- --- 35 --- 24 48 --- 20 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 16 23 13 8 15 19 15 27 |T 33 40 39 37 35 40 37 37 36 35 WRMS | 12 16 22 13 7 15 17 11 22 |NE 23 32 35 28 26 32 26 28 32 26 MEDI | 14 15 22 13 7 14 18 14 24 |MD 21 30 33 26 24 31 26 27 29 24 Table 3.1446.6 GPS week: 1446 Day: 6 MJD: 54372.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------+---------------------------------------------------+---------------------------------------------------- 1E | 16 23 24 16 8 21 27 19 21 7 | 41 51 52 41 42 47 54 40 53 43 2 | 15 16 14 17 8 18 18 14 24 6 | 19 29 29 26 20 29 24 20 21 20 3E | 12 14 24 14 10 20 21 23 27 7 | 121 128 121 122 122 124 126 125 114 123 4 | 9 12 26 10 7 12 19 12 16 5 | 28 36 41 30 33 37 29 35 34 31 5 | 7 13 24 12 5 10 10 11 30 5 | 25 36 42 27 29 32 31 30 32 29 6E | 23 24 28 13 14 19 47 30 23 10 | 139 129 133 132 124 121 152 136 126 132 7E | 16 16 24 15 6 17 21 12 28 6 | 93 81 17 80 100 90 77 75 89 94 8 | 10 14 19 16 8 9 10 7 18 4 | 36 46 42 38 41 42 39 44 42 40 9 | 9 13 19 11 7 12 9 15 29 5 | 27 36 36 24 29 32 28 30 24 27 10 | 12 16 27 11 6 12 14 9 34 6 | 26 34 32 22 27 33 29 27 28 26 11 | 16 16 22 18 7 13 12 13 20 6 | 21 31 33 25 20 28 23 19 24 19 12 | 13 17 27 13 5 15 17 17 36 7 | 26 30 43 32 28 37 24 23 24 25 13E | 14 11 11 12 6 18 15 13 18 5 | 15 26 21 22 18 27 19 20 22 17 14E | 13 15 12 13 6 20 15 13 15 5 | 35 37 38 32 33 34 31 36 41 33 16 | 17 19 22 17 8 19 16 15 41 7 | 28 45 31 41 30 44 30 30 40 32 17E | 12 13 18 11 6 19 15 14 30 6 | 61 62 64 57 58 63 60 59 38 59 18 | 19 18 17 18 5 15 20 14 38 7 | 21 39 34 27 24 37 26 19 35 24 19E | 11 21 18 12 7 22 22 21 16 7 | 30 41 35 36 33 47 39 35 33 34 20 | 18 17 22 16 7 18 19 18 23 7 | 22 36 36 26 23 31 26 21 19 22 21 | 15 15 17 16 6 18 23 18 40 7 | 19 34 33 26 24 36 30 24 36 22 22 | 14 18 17 17 7 15 16 19 28 6 | 28 41 36 30 27 35 30 29 34 28 23E | 17 14 24 10 6 21 15 11 25 6 | 29 37 32 29 27 35 33 34 35 29 24 | 8 15 21 15 7 10 11 14 47 6 | 25 33 30 23 25 29 30 29 52 26 25 | 7 14 21 13 6 10 12 9 23 5 | 33 37 41 27 31 36 32 31 44 32 26E | 20 19 27 13 11 22 18 19 26 7 | 25 31 41 28 27 41 30 22 32 26 27 | 17 11 19 15 9 9 13 8 19 5 | 26 32 31 22 28 32 26 28 35 26 28 | 16 16 18 19 8 14 15 19 41 7 | 17 34 40 32 27 35 21 24 32 24 X29E | 41 57 --- 70 41 72 54 87 64 26 | 150 166 --- 153 148 167 160 155 29 149 30 | 6 13 16 11 3 10 8 10 21 4 | 30 40 33 29 35 35 36 36 36 33 31 | 21 18 42 19 10 15 20 20 26 8 | 43 49 52 37 38 47 44 37 37 40 X32 | 18 --- --- --- 33 --- 25 36 --- 19 | 23 --- --- --- 50 --- 23 54 --- 29 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 16 22 14 8 16 19 16 28 |T 40 49 43 42 42 48 43 42 41 41 WRMS | 14 16 21 14 7 16 15 10 27 |NE 26 36 36 28 29 35 29 29 33 27 MEDI | 15 16 21 14 7 15 16 14 26 |MD 28 37 36 29 29 36 30 30 35 29 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 4.1446 GPS week: 1446 MJD: 54366.0-54372.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 |U 8 8 18 |U 7 9 28 |U 8 7 19 | emr | emr 2838 |U 7 8 20 |U 13 20 44 | 10 10 33 | esa | esa 2699 |U 9 10 27 |U 7 9 30 | 10 10 27 | gfz | gfz 2783 |U 11 12 29 |U 14 23 57 |U 12 10 30 | igr | igr 2849 | 10 9 21 | 10 18 43 | 11 15 34 | igs | igs 2900 | 7 8 21 | 11 17 46 | 11 10 28 | jpl | jpl 2828 |U 8 9 21 |U 12 22 42 | 9 8 26 | mit | mit 2948 |U 6 9 19 |U 15 27 48 |U 10 10 26 | 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 5.1446.0 GPS week: 1446 Day: 0 MJD: 54366.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 | 8 4 15 | 9 9 33 | 8 7 20 | emr | emr 2856 | 7 5 29 | 13 16 46 | 10 9 23 | esa | esa 2687 | 7 5 24 | 9 9 35 | 11 9 22 | gfz | gfz 2841 | 11 8 27 | 14 24 60 | 12 10 32 | igr | igr 2872 | 6 5 12 | 10 20 46 | 9 11 23 | igs | igs 2883 | 6 3 18 | 11 16 51 | 12 11 21 | jpl | jpl 2851 | 10 5 21 | 10 14 40 | 10 11 22 | mit | mit 2976 | 6 4 13 | 16 25 51 | 12 9 24 | Table 5.1446.1 GPS week: 1446 Day: 1 MJD: 54367.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2966 | 11 12 15 | 8 9 39 | 6 10 20 | emr | emr 2856 | 9 12 16 | 16 23 40 | 13 10 30 | esa | esa 2687 | 10 18 15 | 6 7 21 | 10 11 27 | gfz | gfz 2745 | 16 15 25 | 14 23 48 | 13 10 32 | igr | igr 2867 | 17 14 20 | 7 15 33 | 9 10 24 | igs | igs 2942 | 9 17 18 | 10 16 38 | 10 11 28 | jpl | jpl 2856 | 10 14 16 | 13 23 39 | 10 8 23 | mit | mit 2976 | 8 14 13 | 13 26 42 | 10 9 18 | Table 5.1446.2 GPS week: 1446 Day: 2 MJD: 54368.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2937 | 6 4 22 | 6 8 26 | 9 6 14 | emr | emr 2743 | 9 4 24 | 15 25 47 | 12 8 38 | esa | esa 2688 | 10 4 28 | 5 7 23 | 10 9 24 | gfz | gfz 2652 | 11 11 35 | 15 27 55 | 13 9 21 | igr | igr 2773 | 8 9 25 | 11 24 42 | 13 16 42 | igs | igs 2837 | 6 6 22 | 10 20 49 | 11 10 24 | jpl | jpl 2764 | 9 6 20 | 12 24 39 | 11 6 23 | mit | mit 2880 | 6 5 22 | 10 22 30 | 9 10 22 | Table 5.1446.3 GPS week: 1446 Day: 3 MJD: 54369.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2955 | 8 11 15 | 9 14 28 | 10 8 30 | emr | emr 2856 | 7 3 14 | 12 21 31 | 11 9 35 | esa | esa 2688 | 6 8 13 | 7 11 26 | 11 12 35 | gfz | gfz 2744 | 11 8 28 | 12 14 47 | 13 12 34 | igr | igr 2862 | 9 6 18 | 8 9 28 | 17 15 32 | igs | igs 2860 | 5 4 19 | 10 17 30 | 10 9 29 | jpl | jpl 2856 | 6 4 10 | 11 23 29 | 9 8 31 | mit | mit 2880 | 5 3 13 | 17 30 42 | 10 7 27 | Table 5.1446.4 GPS week: 1446 Day: 4 MJD: 54370.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2955 | 7 4 19 | 5 8 21 | 8 6 15 | emr | emr 2845 | 7 6 19 | 13 15 42 | 12 14 38 | esa | esa 2677 | 9 6 36 | 5 9 27 | 9 9 26 | gfz | gfz 2826 | 9 10 31 | 14 19 71 | 13 10 37 | igr | igr 2841 | 8 9 18 | 9 12 38 | 14 14 51 | igs | igs 2915 | 7 8 29 | 11 15 49 | 10 10 32 | jpl | jpl 2764 | 8 7 35 | 14 23 40 | 8 7 29 | mit | mit 2976 | 5 4 28 | 16 28 49 | 11 10 27 | Table 5.1446.5 GPS week: 1446 Day: 5 MJD: 54371.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 | 8 15 21 | 8 7 32 | 6 7 15 | emr | emr 2856 | 5 19 14 | 11 16 40 | 6 9 29 | esa | esa 2688 | 7 14 24 | 7 9 40 | 8 7 26 | gfz | gfz 2839 | 7 22 26 | 16 26 66 | 7 8 23 | igr | igr 2863 | 14 14 21 | 15 26 70 | 8 21 40 | igs | igs 2931 | 8 14 23 | 13 16 54 | 11 12 33 | jpl | jpl 2855 | 6 12 18 | 13 18 39 | 6 6 24 | mit | mit 2976 | 6 15 19 | 19 30 58 | 12 15 29 | Table 5.1446.6 GPS week: 1446 Day: 6 MJD: 54372.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2956 | 6 8 22 | 7 8 16 | 7 5 19 | emr | emr 2856 | 7 9 27 | 12 27 66 | 10 10 38 | esa | esa 2784 | 12 15 48 | 8 13 36 | 8 10 26 | gfz | gfz 2839 | 8 11 34 | 14 26 53 | 11 12 32 | igr | igr 2871 | 8 6 30 | 10 18 47 | 10 21 30 | igs | igs 2935 | 6 4 17 | 11 21 51 | 11 10 32 | jpl | jpl 2856 | 8 15 29 | 13 27 66 | 9 8 31 | mit | mit 2976 | 7 14 24 | 16 31 66 | 9 10 33 | 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 6.1446 GPS week: 1446 MJD: 54366.500-54372.500 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 | 17 9 -24 22 -3 | -3 16 | 17 24 92 75 8 | 2 emr uuuux | 0 1 112 -135 -8 | 52 54 | 39 24 165 75 21 | 2 esa uuuux | 11 49 -26 -8 11 | 101 103 | 22 44 117 113 18 | 6 gfz uuuuu | 1 40 -13 41 4 | 13 22 | 23 11 38 36 7 | 1 igr xxxxx | 17 21 -13 0 -2 | 1 17 | 11 17 78 62 10 | 2 irf xxxxx | 5 20 -18 13 -3 | -8 19 | 11 20 81 73 6 | 3 jpl uuuux | 5 27 -83 -196 -594 | 128 455 | 21 23 97 59 355 | 175 mit uuuuu | 8 19 17 34 -8 | 22 29 | 36 33 140 93 9 | 6 ngs uuuuu | -71 -111 54 206 4 | 9 18 | 47 37 132 116 11 | 3 sio uuuuu | 73 -49 -22 15 -2 | 64 67 | 33 19 108 100 14 | 1 Table 7.1446.0 GPS week: 1446 Day: 0 MJD: 54366.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 5 17 18 12 5 | -3 16 emr uuuux | -14 -32 265 -83 7 | 51 54 esa uuuux | 21 89 65 -14 42 | 91 93 gfz uuuuu | -21 51 34 3 -8 | 15 23 igr xxxxx | -2 16 -19 -16 6 | 1 16 irf xxxxx | 13 16 30 1 -5 | -3 18 jpl uuuux | -12 15 -254 -156 -396 | 293 380 mit uuuuu | 42 13 118 55 -15 | 31 39 ngs uuuuu | -46 -120 -115 188 1 | 12 18 sio uuuuu | 73 -50 -30 6 10 | 63 65 Table 7.1446.1 GPS week: 1446 Day: 1 MJD: 54367.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 19 10 -68 45 11 | -2 16 emr uuuux | 32 -1 265 -253 12 | 51 54 esa uuuux | 0 93 -187 94 7 | 97 99 gfz uuuuu | 6 36 -24 61 3 | 14 23 igr xxxxx | 17 27 102 32 5 | 2 16 irf xxxxx | -1 30 -161 88 -1 | -5 18 jpl uuuux | -9 18 -36 -131 -719 | 297 378 mit uuuuu | 32 14 175 11 -6 | 27 35 ngs uuuuu | -106 -119 -90 85 -17 | 13 19 sio uuuuu | 71 -20 -76 114 13 | 64 66 Table 7.1446.2 GPS week: 1446 Day: 2 MJD: 54368.500 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 | 52 -20 -181 -17 -8 | -2 16 emr uuuux | -66 9 306 -106 5 | 51 54 esa uuuux | 42 13 -44 -164 14 | 99 101 gfz uuuuu | 27 34 -70 82 8 | 12 22 igr xxxxx | 24 38 -125 91 2 | 1 16 irf xxxxx | 19 19 -91 -7 -2 | -8 18 jpl uuuux | -7 13 -10 -147 -925 | 256 402 mit uuuuu | -54 75 140 14 -9 | 23 30 ngs uuuuu | -44 -81 95 273 8 | 10 18 sio uuuuu | 71 -63 -219 -96 -1 | 64 67 Table 7.1446.3 GPS week: 1446 Day: 3 MJD: 54369.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 10 41 79 101 -6 | -1 15 emr uuuux | -34 -13 -62 -214 1 | 54 56 esa uuuux | 20 19 -18 135 25 | 105 107 gfz uuuuu | 33 29 -15 64 7 | 13 23 igr xxxxx | 24 10 -49 -104 6 | 2 17 irf xxxxx | -12 40 29 24 4 | -9 18 jpl uuuux | 5 23 -62 -275 -960 | 177 452 mit uuuuu | 20 -24 -11 -19 5 | 20 28 ngs uuuuu | -51 -57 1 120 2 | 10 18 sio uuuuu | 12 -43 105 110 3 | 66 68 Table 7.1446.4 GPS week: 1446 Day: 4 MJD: 54370.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 24 -25 -83 -8 -6 | -2 16 emr uuuux | 11 27 51 -158 -7 | 53 56 esa uuuux | -26 12 -106 78 1 | 107 108 gfz uuuuu | -13 43 -50 34 13 | 12 22 igr xxxxx | 25 15 -53 39 -14 | 2 17 irf xxxxx | 2 -18 -13 52 3 | -10 19 jpl uuuux | 45 74 30 -235 -767 | 70 508 mit uuuuu | -19 46 7 -16 0 | 19 26 ngs uuuuu | -63 -144 172 327 0 | 9 18 sio uuuuu | 65 -76 -14 19 2 | 66 68 Table 7.1446.5 GPS week: 1446 Day: 5 MJD: 54371.500 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 16 66 -101 -12 | -5 18 emr uuuux | 27 -16 51 -51 -33 | 51 55 esa uuuux | -2 105 173 -84 -14 | 106 108 gfz uuuuu | -26 30 9 -17 -3 | 12 22 igr xxxxx | 4 47 -20 -18 -18 | -1 19 irf xxxxx | -2 42 5 -132 -7 | -11 20 jpl uuuux | -7 4 -166 -258 -427 | -46 539 mit uuuuu | -6 -8 -220 233 -11 | 17 25 ngs uuuuu | -24 -90 70 365 15 | 5 16 sio uuuuu | 100 -34 85 -139 -16 | 65 67 Table 7.1446.6 GPS week: 1446 Day: 6 MJD: 54372.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 5 24 -1 120 -5 | -6 18 emr uuuux | 41 36 -91 -84 -43 | 48 51 esa uuuux | 20 12 -61 -100 0 | 106 107 gfz uuuuu | 4 59 24 61 6 | 11 20 igr xxxxx | 27 -4 77 -26 -3 | -3 18 irf xxxxx | 15 12 75 65 -14 | -13 20 jpl uuuux | 21 39 -80 -169 37 | -148 529 mit uuuuu | 41 19 -86 -38 -23 | 15 23 ngs uuuuu | -162 -164 245 85 16 | 6 18 sio uuuuu | 118 -55 -1 90 -25 | 63 65