Date: Fri, 02 Feb 2007 11:41:36 +0100 To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-14740] Wk 1410 IGS Final Orbits Message-ID: <45C31560.mailxBMV11F0PJ@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 02 Feb 02:41:48 PST 2007 Message Number 14740 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1410 (Jan 14, 2007 - Jan 20, 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: igs1410[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1410[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1410[0-6].cls IGS GPS clock combination summary report. igs14107.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14107.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 | RAMO SANT 0 | EMR | KOUR 0 | ESA | BILI LPGS SANT 0 | MIT | DAV1 LHAS SANT 1 | COD | BAKO 1 | EMR | KOUR ONSA 1 | ESA | YELL 1 | JPL | DARW KIT3 1 | MIT | 26 KIT3 KOUR 2 | COD | YELL 2 | EMR | KOUR ONSA 2 | JPL | KARR NISU 2 | MIT | 15 ARTU BAHR DAEJ GLPS JPLM KARR LHAS MATE 3 | EMR | GODE KOUR ONSA 3 | ESA | 11 NYAL 3 | MIT | 15 DAEJ IISC IRKT 4 | EMR | KOUR 4 | ESA | IRKT KOUR LPGS MATE ZAMB 4 | JPL | 26 4 | MIT | 15 BAHR DAEJ IRKT 5 | COD | BOR1 DAEJ 5 | EMR | ONSA WTZR 5 | ESA | LPGS POTS ZAMB 5 | GFZ | KERG 5 | JPL | 12 5 | MIT | BAHR DAEJ SUTM TIXI 6 | COD | DAEJ 6 | EMR | KOUR ONSA USUD 6 | ESA | MAW1 RBAY 6 | GFZ | 31 6 | MIT | BAHR DAEJ RBAY 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 ----+------------+---------- G17 | 2007_01_19 | 2007015 G17 | 2007_01_20 | 2007015 G25 | 2007_01_16 | 2007017 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 ----+--------+--------------- 3 | ESA | 11 5 | NGS | 16 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 G26 | | | | | 4 | | | 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 | .0 .4 .3 2 1 0 -.22 EMR | .6 -.6 -.9 -37 10 31 .01 ESA | 5.1 .0 2.8 0 4 -12 -.83 GFZ | .3 -.1 1.1 5 -8 5 -.50 JPL | 6.7 8.8 9.0 226 -69 264 .22 MIT | -1.7 .5 -16.0 -6 6 -9 .18 NGS | 6.5 2.4 -5.0 40 -111 13 -1.00 SIO | .2 3.8 1.0 45 -28 54 .02 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 1.1410.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1410.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 2.1410.[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 3.1410.[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 5.1410.0-6). 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 1410 summary. (Jan 14, 2007 - Jan 20, 2007) Table 1.1410.a GPS week: 1410 MJD: 54114.000-54120.000 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 176| 1 0 -1 5 -18 -30 -.30 13 12 | -121 99 46 85 | 1 0 1 6 3 12 .01 | 1210 1319 emr 49| 1 1 1 73 -37 -26 .25 15 15 | -115291 -873 54 91 | 1 1 1 11 17 14 .03 | 2957 1969 esa 65| 0 1 7 53 -23 -36 .17 24 22 | 8457 420 58 137 | 0 1 2 83 50 23 .04 | 843 2007 gfz 183| -3 -2 -3 2 9 -47 .03 15 15 | -47 -32 33 126 | 1 0 0 24 19 47 .02 | 333 685 igr n/a| 0 0 0 4 -42 -22 -.02 8 8 | -4128 -132 36 73 | 0 0 1 16 19 21 .03 | 1500 2124 jpl n/a| 0 -3 -8 -250 56 312 .07 38 38 | 5896 424 95 145 | 5 4 3 45 31 22 .03 | 984 2103 mit 171| 0 0 0 -10 -58 2 .08 23 21 | 429 151 72 139 | 1 0 0 57 42 23 .04 | 2105 1804 ngs 163| 0 3 0 -38 148 41 -.06 22 15 | 365 -1116 2541 4477 | 1 1 2 33 26 26 .06 | 2499 2670 sio 96| 1 -2 0 -123 -32 27 -.01 35 33 | --- --- --- --- | 1 1 1 46 27 29 .05 | --- --- Table 1.1410.b GPS week : 1410 MJD: 54114.000-54120.000 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: mm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------+------------------------------------+------------------------------------------ 1 | 7 7 7 7 7 7 7 | 2 | 10 9 9 9 9 10 9 | 3 | 7 6 6 7 7 9 9 | 4 | 7 7 7 8 7 6 6 | 5 | 7 7 7 7 7 7 7 | 6 | 5 6 5 6 7 7 6 | 7 | 5 5 5 5 5 7 6 | 8 | 8 7 7 7 7 7 7 | 9 | 6 7 6 6 6 6 6 | 10E | 9 8 11 9 8 8 9 | 11 | 8 7 8 8 8 8 7 | 12 | 9 9 9 10 10 11 10 | 13 | 9 8 9 8 9 9 9 | 14 | 8 8 8 8 8 8 8 | 15 | 13 11 11 10 11 10 11 | 16 | 8 8 9 8 9 10 8 | 17 | 9 9 10 10 9 0 18 | 18E | 7 7 7 7 6 6 6 | 19 | 8 8 8 9 8 10 8 | 20E | 9 9 7 8 7 8 8 | 21 | 9 9 8 9 9 9 8 | 22E | 6 7 6 8 8 9 8 | 23 | 9 8 9 9 9 9 9 | 24 | 5 5 5 5 5 5 5 | 25 | 6 7 0 8 7 8 8 | 26 | 6 6 6 5 10 8 6 | 27 | 8 7 7 7 7 8 6 | 28 | 9 8 9 9 9 9 8 | 29 | 6 7 6 6 8 6 6 | 30 | 6 7 7 7 6 7 7 | 31 | 8 8 9 11 8 9 8 | 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 2.1410.0 GPS week: 1410 Day: 0 MJD: 54114.000 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 176| 0 0 -1 5 -20 -36 -.28 13 13 | -1710 2369 42 74 | 35 -16 | emr 49| 0 2 2 72 -27 -44 .20 14 14 | -110375 -2929 55 90 | 35 -50 | esa 65| 0 0 6 44 -63 -52 .19 20 20 | 9574 -1512 53 122 | 33 44 | gfz 183| -2 -1 -4 18 20 22 .03 14 14 | -48 4 32 121 | -30 -20 | igr n/a| 0 0 0 7 -46 -46 -.03 8 8 | -1402 -2470 35 91 | -13 21 | jpl n/a| 6 -8 -9 -278 70 279 .08 39 39 | 6899 -2049 95 143 | 99 -53 | mit 171| 2 0 0 -8 -30 -10 .07 26 22 | -1183 2439 70 130 | -5 28 | ngs 163| -2 1 0 -50 122 5 -.10 19 16 | -518 -180 2141 3885 | -70 51 | sio 96| 1 -1 0 -155 -18 1 -.06 37 33 | --- --- --- --- | 157 87 | Table 2.1410.1 GPS week: 1410 Day: 1 MJD: 54115.000 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 176| 0 0 -1 5 -17 -14 -.31 12 12 | 1483 -2093 44 91 | 40 -23 | emr 49| 2 3 1 79 -13 -30 .28 16 16 | -112881 -1087 53 98 | 70 -35 | esa 65| 0 0 8 -71 -69 -44 .18 21 21 | 8176 901 59 137 | 29 -8 | gfz 183| -3 -3 -2 12 -4 -42 .04 14 14 | 8 -286 32 142 | -3 -23 | igr n/a| -1 0 1 13 -16 -30 .02 7 7 | -3628 239 32 67 | -9 -15 | jpl n/a| 2 -10 -9 -233 101 307 .07 39 39 | 5132 752 101 151 | 86 -30 | mit 171| 1 0 0 39 -93 8 .08 22 20 | 1838 -1739 71 162 | -6 62 | ngs 163| 0 4 -2 -35 155 15 -.07 17 13 | -658 -384 2521 4521 | -75 34 | sio 96| 1 0 1 -71 -60 9 -.01 34 34 | --- --- --- --- | 102 99 | Table 2.1410.2 GPS week: 1410 Day: 2 MJD: 54116.000 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 176| 0 1 -2 13 -23 -46 -.31 13 13 | 205 -156 47 82 | 27 -8 | emr 49| 0 2 2 54 -35 -24 .25 15 15 | -114659 -3593 56 96 | 44 -35 | esa 65| 1 2 8 45 -11 -41 .10 22 22 | 8364 -2908 53 159 | -25 -74 | gfz 183| -2 -3 -2 13 29 -43 .06 14 14 | 643 -1275 34 127 | -29 -29 | igr n/a| 0 0 0 9 -46 -32 -.03 8 8 | -3705 -3526 33 75 | -24 38 | jpl n/a| 1 0 -2 -252 81 319 .11 40 40 | 5595 -2739 95 145 | 51 -30 | mit 171| 1 0 -1 -14 -99 15 .03 22 21 | 1491 -1237 74 140 | 46 82 | ngs 163| 0 2 -3 18 157 55 -.08 19 15 | -164 -800 3470 4854 | -185 2 | sio 96| 1 -4 -1 -186 -33 12 -.02 32 30 | --- --- --- --- | 133 99 | Table 2.1410.3 GPS week: 1410 Day: 3 MJD: 54117.000 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 176| 1 0 -1 7 -17 -37 -.29 13 12 | -474 375 43 85 | 39 12 | emr 49| 3 2 2 74 -41 -38 .26 14 14 | -117258 762 55 110 | 55 -31 | esa 65| 0 1 9 178 -86 -28 .19 36 23 | 7109 2169 66 157 | -45 -79 | gfz 183| -6 -3 -4 -46 35 -7 .01 15 15 | -323 248 37 130 | 9 -22 | igr n/a| 0 0 2 -6 -49 -41 -.07 9 9 | -5750 1782 39 84 | 52 25 | jpl n/a| 2 -3 -11 -231 65 310 .09 40 40 | 4301 2724 102 147 | 78 -31 | mit 171| 1 0 0 -53 -30 0 .13 20 19 | -554 1032 71 161 | 62 41 | ngs 163| 2 2 -1 -52 125 31 -.07 20 17 | -141 -765 2656 5104 | 8 16 | sio 96| 1 -3 -1 -137 2 30 -.04 34 32 | --- --- --- --- | 101 63 | Table 2.1410.4 GPS week: 1410 Day: 4 MJD: 54118.000 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 176| 2 0 -1 -3 -16 -36 -.31 12 12 | 1056 -152 51 87 | 79 9 | emr 49| 3 0 0 66 -46 -27 .28 15 15 | -115432 -1549 56 91 | 17 28 | esa 65| 0 3 4 -22 27 10 .23 26 25 | 9369 13 61 143 | 14 -69 | gfz 183| -3 -2 -3 26 -16 -56 .03 14 15 | -241 844 33 126 | -23 22 | igr n/a| 0 0 0 30 -21 -16 .01 9 9 | -3772 -218 42 69 | -36 -7 | jpl n/a| -4 0 -5 -335 17 330 .06 38 38 | 7052 310 97 152 | 117 14 | mit 171| 0 0 0 72 -52 -40 .11 23 22 | 3081 -1436 75 115 | -60 -8 | ngs 163| 0 2 2 -66 174 81 -.10 18 15 | 5621 -6286 2719 4697 | -79 -52 | sio 96| 3 -1 0 -51 -40 3 .01 36 35 | --- --- --- --- | 68 74 | Table 2.1410.5 GPS week: 1410 Day: 5 MJD: 54119.000 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 176| 3 1 0 -1 -14 -14 -.30 13 13 | -1539 -190 49 95 | 57 -5 | emr 49| 0 0 -1 75 -31 2 .23 14 14 | -117489 713 51 80 | 89 36 | esa 65| 1 0 7 111 39 -35 .19 23 23 | 7961 2144 63 125 | 15 -74 | gfz 183| -1 -3 -4 3 14 -117 .03 15 15 | -323 517 33 129 | 3 12 | igr n/a| 1 -1 0 0 -40 12 .00 10 9 | -5458 1469 39 69 | 11 36 | jpl n/a| -7 2 -12 -224 36 345 .02 36 36 | 5893 1710 86 136 | 38 -7 | mit 171| -2 0 0 -9 -107 6 .12 23 22 | -3037 2428 73 129 | 17 19 | ngs 163| 0 4 3 -77 186 58 -.09 42 16 | 761 -1980 2057 3822 | -23 -53 | sio 96| 0 -2 2 -126 -73 74 .08 35 35 | --- --- --- --- | 110 67 | Table 2.1410.6 GPS week: 1410 Day: 6 MJD: 54120.000 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 176| 3 0 1 12 -20 -23 -.32 12 12 | 126 540 51 81 | 26 25 | emr 49| 1 0 1 90 -68 -24 .22 14 14 | -118948 1567 53 78 | 39 29 | esa 65| -1 0 4 88 0 -62 .14 22 22 | 8652 2138 57 121 | 19 -30 | gfz 183| 0 -1 -4 -6 -8 -90 .01 15 15 | -46 -279 35 113 | -19 -7 | igr n/a| 0 0 -1 -20 -77 0 -.01 7 7 | -5184 1799 34 62 | 46 17 | jpl n/a| -7 -3 -5 -195 20 292 .05 36 36 | 6403 2261 94 143 | 23 -21 | mit 171| 0 0 0 -101 3 36 .05 25 23 | 1370 -426 76 140 | 56 -14 | ngs 163| -1 3 0 -8 119 40 .08 16 14 | -2343 2582 2226 4458 | -146 60 | sio 96| 1 -1 -1 -136 -4 64 -.02 34 29 | --- --- --- --- | 124 52 | 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 3.1410.0 GPS week: 1410 Day: 0 MJD: 54114.000 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 8 20 11 11 18 36 17 43 7 | 82 82 86 77 78 84 68 74 88 77 2 | 20 15 17 17 9 54 52 26 44 10 | 30 47 46 43 37 59 46 32 42 35 3 | 9 15 19 11 7 11 26 20 46 6 | 32 41 34 39 35 40 34 39 42 34 4 | 8 9 17 9 9 14 34 15 55 7 | 29 31 33 31 31 40 38 31 58 30 5 | 12 13 24 11 9 12 22 17 46 6 | 21 25 40 25 21 30 30 19 39 21 6 | 8 7 17 8 4 13 14 19 30 5 | 35 36 36 36 32 40 33 29 36 33 7 | 7 8 14 9 8 14 15 16 16 4 | 33 35 32 34 34 40 29 33 35 31 8 | 13 13 22 16 6 16 27 19 49 7 | 21 33 36 29 25 30 29 23 26 23 9 | 11 10 25 14 6 14 20 15 24 6 | 20 28 34 27 22 31 28 22 27 21 10E | 18 15 25 30 8 20 27 28 24 8 | 34 36 44 46 33 38 33 45 38 33 11 | 14 15 29 17 8 52 22 15 31 8 | 28 41 41 32 25 29 30 23 29 26 X12 | 14 19 27 10 9 60 27 20 --- 9 | 31 44 50 35 34 48 30 31 --- 32 13 | 17 14 22 19 8 61 21 18 46 8 | 24 39 46 35 30 37 22 26 24 26 14 | 17 19 14 15 9 51 24 19 23 7 | 27 45 37 36 29 40 32 24 32 29 X15 | 12 --- --- --- 18 32 30 23 --- 12 | 27 --- --- --- 34 39 36 41 --- 31 16 | 16 16 17 16 8 65 24 20 28 8 | 34 50 52 43 38 60 31 32 32 38 X17 | 10 9 15 11 8 57 44 15 --- 8 | 23 32 25 29 28 30 50 29 --- 27 18E | 11 13 11 10 6 51 16 17 39 6 | 25 33 28 27 25 29 27 23 43 24 19 | 7 9 17 9 6 53 30 13 52 7 | 38 47 40 39 37 42 34 35 59 37 20E | 12 30 14 16 10 51 19 18 38 8 | 37 35 43 38 38 39 44 36 57 34 21 | 16 18 19 16 6 58 32 22 34 8 | 24 41 37 36 29 45 30 26 34 27 22E | 13 13 9 10 6 51 15 15 11 6 | 26 33 32 29 27 32 28 26 33 26 23 | 15 16 17 15 9 61 23 22 40 8 | 26 42 46 34 31 47 29 31 31 30 24 | 6 9 21 9 7 15 17 16 31 5 | 29 29 30 33 30 30 33 28 43 28 25 | 13 10 17 13 6 17 27 18 27 6 | 21 26 31 22 21 25 25 15 30 20 26 | 10 9 22 12 7 10 29 20 28 6 | 81 84 87 86 84 84 82 84 87 83 27 | 12 14 21 15 6 20 24 21 56 7 | 20 31 35 27 22 29 29 22 26 21 28 | 15 14 25 15 7 53 20 24 43 8 | 38 48 54 50 43 53 33 44 46 40 29 | 11 7 22 12 6 11 16 20 36 6 | 37 36 43 35 35 35 35 38 37 33 30 | 9 10 24 11 8 12 26 18 34 6 | 51 52 58 51 49 55 62 51 57 51 31 | 13 16 15 17 9 54 25 19 26 7 | 35 47 36 49 40 50 38 35 44 37 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 14 20 14 8 39 26 19 37 |T 32 40 42 38 34 42 36 33 41 33 WRMS | 13 14 20 14 8 39 22 16 33 |NE 33 42 43 38 35 43 36 33 41 34 MEDI | 12 13 19 12 8 32 24 19 34 |MD 29 36 37 35 32 40 33 31 37 31 Table 3.1410.1 GPS week: 1410 Day: 1 MJD: 54115.000 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 11 18 12 7 17 22 11 50 6 | 30 35 34 29 30 34 35 28 56 29 2 | 17 15 19 18 7 58 36 22 40 9 | 26 42 42 38 32 50 37 27 31 29 3 | 8 12 16 12 8 11 25 12 31 5 | 30 36 33 34 33 35 31 34 41 31 4 | 10 10 16 8 7 18 25 11 54 6 | 25 27 26 25 28 36 29 27 49 24 5 | 11 15 21 13 6 18 23 14 40 6 | 16 28 29 27 18 27 31 18 38 19 6 | 7 10 24 9 5 15 13 13 34 5 | 30 31 33 31 27 32 26 25 31 26 7 | 7 9 17 9 4 15 15 13 15 4 | 26 29 28 26 25 31 23 29 25 24 8 | 12 12 26 13 7 19 23 12 40 6 | 18 27 31 24 19 28 28 16 24 18 9 | 11 12 29 12 6 16 22 21 26 6 | 23 33 32 29 23 31 24 28 27 22 10E | 17 18 23 28 8 22 22 22 23 8 | 33 36 38 43 32 36 24 42 32 30 11 | 14 15 18 17 9 49 19 18 22 7 | 23 37 36 33 22 27 26 15 27 22 X12 | 15 16 27 10 10 60 28 15 --- 8 | 25 42 41 29 29 43 27 28 --- 27 13 | 16 19 21 17 8 54 19 17 38 8 | 18 36 37 33 27 35 18 21 19 21 14 | 14 16 17 16 5 52 20 22 22 7 | 19 37 31 30 22 33 24 22 31 22 X15 | 17 --- --- 17 10 26 37 24 26 10 | 23 --- --- 35 25 37 45 34 36 26 16 | 15 17 22 14 4 58 21 20 25 8 | 33 45 45 36 33 49 29 28 28 32 X17 | 7 10 24 13 9 63 42 12 --- 9 | 24 30 23 28 27 39 50 28 --- 27 18E | 8 16 22 10 6 50 16 12 32 6 | 18 30 32 24 21 25 27 20 37 20 19 | 8 11 14 10 7 49 29 17 52 7 | 33 41 35 35 33 39 32 28 40 31 20E | 15 37 17 14 8 55 23 14 33 9 | 32 45 35 32 29 38 35 30 41 30 21 | 16 18 20 16 5 58 27 18 28 8 | 20 41 34 32 26 42 23 28 27 24 22E | 11 13 14 12 6 48 16 26 17 6 | 19 31 23 27 22 26 26 24 26 20 23 | 14 17 21 14 10 59 20 18 35 8 | 22 37 33 34 30 41 24 26 35 25 24 | 6 8 18 10 5 16 16 13 23 4 | 21 23 21 25 22 24 24 28 29 20 25 | 13 13 25 13 7 17 24 15 30 6 | 17 21 27 19 17 21 24 16 24 16 26 | 10 12 22 12 6 13 20 22 28 6 | 61 67 68 66 64 65 62 66 79 63 27 | 12 15 21 13 7 19 22 14 33 6 | 17 25 26 23 17 24 26 12 22 14 28 | 13 17 27 16 7 54 19 17 42 8 | 37 45 56 43 41 49 38 36 44 39 29 | 10 17 23 15 13 22 18 21 44 7 | 78 81 77 82 77 87 88 79 54 78 30 | 10 15 25 12 9 19 25 13 35 6 | 65 72 64 68 70 72 81 70 86 69 31 | 13 16 32 17 7 55 22 16 27 8 | 26 38 40 37 30 38 29 31 40 28 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 16 21 14 7 39 22 17 34 |T 28 38 37 34 30 38 33 30 37 29 WRMS | 12 16 21 14 7 39 20 13 34 |NE 29 38 37 35 31 39 34 30 37 29 MEDI | 12 15 21 13 7 26 22 16 32 |MD 25 36 33 32 27 36 28 28 32 26 Table 3.1410.2 GPS week: 1410 Day: 2 MJD: 54116.000 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 19 13 7 18 21 13 46 6 | 28 33 39 25 27 30 36 24 54 27 2 | 16 15 21 17 8 60 24 24 34 8 | 28 43 48 42 33 57 38 23 30 33 3 | 8 16 13 13 8 15 24 13 34 6 | 31 42 34 36 32 38 33 37 37 33 4 | 10 8 21 11 9 25 20 19 45 6 | 30 33 39 29 33 48 37 30 61 32 5 | 12 13 30 12 7 20 24 19 39 7 | 22 27 26 27 22 29 34 24 42 22 6 | 7 8 18 9 6 15 14 17 28 5 | 34 33 39 35 30 35 35 30 34 32 7 | 8 10 12 8 6 17 15 16 16 4 | 30 31 34 33 30 32 31 37 35 30 8 | 14 16 29 13 8 19 23 13 40 7 | 21 29 32 24 20 27 28 21 31 21 9 | 10 12 28 11 6 17 19 22 15 6 | 21 30 35 28 23 30 26 30 25 24 10E | 18 38 30 27 14 25 27 23 26 10 | 35 47 50 42 35 40 37 38 30 31 11 | 15 16 24 16 11 45 17 25 25 7 | 26 42 38 30 23 31 27 21 29 25 X12 | 14 17 32 11 10 65 25 18 --- 9 | 28 39 39 33 28 42 31 22 --- 27 13 | 18 19 21 18 10 60 16 21 30 8 | 22 40 36 33 27 37 22 25 23 24 14 | 16 15 22 17 6 55 20 21 35 8 | 26 40 37 32 29 35 29 24 39 28 X15 | 22 24 --- 22 17 17 24 47 24 11 | 35 36 --- 31 26 32 40 56 35 30 16 | 15 17 22 14 5 65 21 19 32 8 | 35 49 52 44 40 58 34 38 41 39 X17 | 10 11 16 17 8 56 45 19 --- 9 | 23 26 23 25 22 26 37 26 --- 22 18E | 9 12 16 12 7 47 19 15 31 6 | 24 33 30 29 27 30 33 25 36 25 19 | 9 10 9 9 9 46 31 18 50 7 | 37 46 40 39 37 40 38 31 46 36 20E | 13 17 18 16 6 50 14 13 29 7 | 30 45 35 37 33 38 38 31 46 33 21 | 16 17 23 18 8 56 24 19 25 8 | 27 42 38 36 28 43 28 27 28 29 22E | 12 11 14 12 5 47 12 20 18 6 | 29 36 30 32 27 34 34 28 35 28 23 | 14 17 21 15 10 62 18 23 37 8 | 25 43 37 33 30 44 27 32 27 28 24 | 8 8 18 9 6 19 23 12 22 5 | 27 28 29 32 30 28 40 26 37 28 X25 | 6 --- --- --- 27 --- --- --- --- 0 | 30 --- --- --- 24 --- --- --- --- 32 26 | 11 9 21 11 4 13 17 20 20 5 | 69 75 74 72 70 74 66 64 76 69 27 | 13 13 27 13 7 21 25 13 38 7 | 23 33 37 26 23 29 29 21 28 23 28 | 13 16 32 16 10 53 33 23 36 9 | 27 34 43 31 31 41 31 35 35 26 29 | 10 9 24 12 11 11 23 14 36 6 | 73 77 76 74 67 77 76 65 60 71 30 | 11 13 23 10 10 19 24 19 29 6 | 36 40 40 40 43 42 46 44 50 37 31 | 16 17 27 19 7 55 21 22 29 8 | 32 38 40 40 33 41 35 31 43 31 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 15 22 14 8 40 22 19 32 |T 31 39 39 35 31 39 35 32 39 31 WRMS | 13 15 22 14 8 40 21 15 30 |NE 31 39 40 35 31 40 35 32 39 31 MEDI | 12 13 21 13 8 25 21 19 30 |MD 28 38 38 33 30 37 34 30 35 29 Table 3.1410.3 GPS week: 1410 Day: 3 MJD: 54117.000 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 13 21 14 6 18 15 18 45 6 | 32 38 44 29 35 35 36 42 60 33 2 | 17 15 18 17 11 60 23 23 33 8 | 27 42 44 37 34 50 36 30 35 30 3 | 10 16 21 14 10 13 22 16 39 6 | 29 39 37 31 31 35 29 35 36 29 4 | 8 10 23 17 10 22 22 20 65 8 | 34 39 39 33 38 50 33 43 76 35 5 | 10 14 21 12 10 20 18 19 36 6 | 22 29 41 24 21 34 31 25 34 22 6 | 7 8 13 9 7 18 19 17 40 5 | 36 37 37 33 33 42 32 36 30 32 7 | 8 7 15 10 8 17 15 15 25 4 | 31 36 38 30 33 40 28 40 36 30 8 | 12 14 26 13 7 18 17 13 48 7 | 24 31 44 29 26 32 25 25 17 24 9 | 10 13 27 10 12 15 15 24 23 6 | 24 33 47 29 25 33 26 32 25 26 10E | 18 17 18 25 8 26 29 20 29 8 | 34 41 42 40 33 36 24 38 30 29 11 | 13 16 143 16 7 52 17 20 18 8 | 32 40 123 38 30 33 33 29 32 30 X12 | 16 21 26 12 15 65 24 25 --- 9 | 27 41 47 27 23 44 26 26 --- 27 13 | 16 17 22 17 12 57 16 24 31 8 | 26 42 44 38 34 45 25 35 24 29 14 | 16 20 23 16 10 53 18 23 21 8 | 25 41 40 30 28 33 23 33 26 26 X15 | 18 27 --- 23 16 23 29 25 30 10 | 33 35 --- 41 38 55 47 43 35 38 16 | 14 16 24 11 10 60 22 21 27 8 | 39 51 52 42 36 54 32 35 40 39 X17 | 12 14 32 13 16 56 42 24 --- 10 | 23 33 33 29 31 35 48 32 --- 26 18E | 10 13 22 13 6 46 15 13 24 6 | 28 36 45 31 32 33 31 30 36 29 19 | 9 15 23 12 9 46 33 18 50 8 | 32 43 41 33 31 39 35 25 45 30 20E | 15 21 18 22 10 50 13 21 28 8 | 34 41 41 44 37 44 36 43 45 34 21 | 16 16 22 16 9 53 29 19 29 8 | 25 42 51 35 33 43 26 36 33 29 22E | 15 12 18 27 9 46 14 23 20 7 | 27 34 41 34 29 31 27 31 34 26 23 | 15 17 19 14 12 58 21 25 36 8 | 29 48 49 40 37 53 35 42 34 34 24 | 5 7 19 10 7 20 10 15 24 4 | 29 29 29 30 29 31 31 32 35 26 X25 | 14 14 --- 14 13 20 15 21 56 8 | 28 28 --- 22 21 25 25 30 33 28 26 | 9 11 21 9 9 11 18 16 12 5 | 71 75 81 72 73 76 73 73 83 72 27 | 13 13 20 13 9 22 23 17 38 6 | 24 29 43 31 28 33 25 29 19 23 28 | 13 17 28 16 11 58 19 18 39 8 | 44 48 48 51 48 56 44 47 44 44 29 | 9 12 22 10 13 12 21 21 25 6 | 49 48 56 49 51 50 54 50 60 48 30 | 11 13 22 12 11 23 22 19 26 6 | 47 54 53 47 46 57 63 54 51 49 31 | 15 15 52 21 10 61 24 20 38 10 | 35 47 50 46 39 50 35 46 54 37 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 14 36 15 9 40 20 19 34 |T 32 40 47 36 34 42 34 37 39 32 WRMS | 12 14 23 15 9 40 19 17 32 |NE 32 40 48 36 34 43 35 37 39 33 MEDI | 13 14 22 14 10 26 19 20 30 |MD 29 40 44 33 33 40 32 35 35 30 Table 3.1410.4 GPS week: 1410 Day: 4 MJD: 54118.000 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 8 35 11 9 19 18 13 49 7 | 34 35 39 31 32 30 38 30 66 32 2 | 17 16 17 18 9 55 27 22 33 8 | 25 41 37 37 31 45 38 29 32 28 3 | 11 16 26 12 7 11 24 19 39 7 | 29 34 30 31 26 28 30 34 29 27 4 | 7 11 19 9 6 18 16 24 45 6 | 25 27 35 27 28 33 25 29 42 25 5 | 12 13 34 11 8 17 30 14 33 7 | 23 29 34 26 21 28 36 25 32 22 6 | 12 10 25 8 8 14 24 16 41 6 | 37 40 48 37 34 37 32 35 36 35 7 | 10 9 21 10 7 15 19 16 19 5 | 30 32 35 31 28 33 25 34 26 28 8 | 13 16 20 12 7 16 21 22 35 6 | 24 25 35 32 27 27 27 31 26 25 9 | 11 12 24 11 7 14 25 14 26 6 | 26 32 40 29 26 32 39 26 24 27 10E | 17 20 27 23 9 20 25 16 33 8 | 30 30 32 33 25 29 23 29 28 23 11 | 12 16 26 17 12 49 20 17 19 7 | 27 38 48 34 29 30 30 26 35 26 X12 | 14 18 29 13 10 61 36 20 --- 9 | 31 37 40 31 30 36 40 32 --- 30 13 | 16 17 29 17 11 55 23 20 34 8 | 27 37 38 39 36 40 22 34 25 28 14 | 14 16 20 16 9 53 18 21 21 7 | 25 36 35 32 27 34 20 23 28 25 X15 | 21 29 --- 18 23 33 31 34 28 11 | 31 45 --- 43 41 52 37 53 33 39 16 | 15 16 29 14 10 59 24 22 31 8 | 36 46 49 42 39 56 33 43 32 39 X17 | 13 10 22 12 12 58 43 16 --- 9 | 19 28 26 25 29 35 47 27 --- 23 18E | 9 14 12 11 6 45 16 16 23 6 | 32 36 34 35 31 33 33 32 37 31 19 | 10 11 24 9 9 43 32 16 51 8 | 30 38 32 33 30 36 26 26 44 28 20E | 11 13 20 10 7 50 18 15 32 7 | 28 31 25 30 29 35 32 32 46 27 21 | 15 16 23 17 9 53 29 20 26 8 | 24 38 37 33 28 38 23 28 27 25 22E | 16 12 17 28 8 43 17 17 28 8 | 31 30 28 35 26 30 32 24 39 25 23 | 14 18 19 14 11 59 26 17 38 8 | 28 36 35 37 34 41 27 33 31 28 24 | 7 10 23 12 7 13 21 13 21 5 | 28 27 25 29 27 27 29 30 28 25 X25 | 12 12 --- 12 8 18 18 15 49 7 | 26 27 --- 24 21 23 28 21 43 24 26 | 12 25 55 12 13 20 35 23 32 9 | 183 180 206 183 185 187 183 186 150 184 27 | 10 13 20 13 8 17 21 23 31 6 | 29 31 38 35 29 35 28 34 25 28 28 | 15 22 33 14 8 57 22 24 42 9 | 40 48 51 44 41 53 44 44 45 41 29 | 9 15 33 13 12 22 17 16 69 8 | 87 92 90 92 85 89 90 82 53 86 30 | 11 12 21 13 7 17 21 13 29 6 | 34 40 42 32 31 36 47 36 40 34 31 | 13 16 19 16 9 54 22 16 37 8 | 29 38 35 38 33 42 30 26 52 29 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 15 26 14 9 38 23 18 36 |T 35 41 44 40 36 42 38 37 39 35 WRMS | 12 15 25 15 9 38 22 15 35 |NE 36 42 46 41 38 43 39 39 40 36 MEDI | 12 15 23 13 9 33 22 17 33 |MD 29 36 35 33 29 35 32 31 33 28 Table 3.1410.5 GPS week: 1410 Day: 5 MJD: 54119.000 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 11 28 15 6 19 18 11 48 7 | 34 39 46 30 33 37 37 33 58 32 2 | 17 15 21 19 7 59 37 26 40 10 | 31 47 44 40 39 50 53 36 44 36 3 | 11 13 23 16 7 18 33 47 40 9 | 33 43 38 38 33 41 31 59 39 32 4 | 8 13 22 11 12 16 18 22 36 6 | 28 40 35 30 32 33 29 34 45 29 5 | 13 13 26 13 7 13 20 21 31 6 | 25 32 32 27 25 28 32 23 35 23 6 | 11 7 22 11 10 11 23 40 36 7 | 34 42 39 39 37 40 40 43 44 34 7 | 12 8 20 11 10 11 22 44 23 7 | 33 38 34 34 36 36 31 51 35 30 8 | 14 13 22 10 7 23 20 16 43 6 | 29 36 40 30 28 34 28 30 34 27 9 | 10 10 24 11 5 15 20 19 30 6 | 25 35 36 29 27 33 28 31 25 25 10E | 19 14 21 21 9 21 24 22 36 8 | 32 40 45 41 32 40 26 36 34 31 11 | 12 16 24 18 11 38 17 27 24 7 | 31 43 56 37 34 39 32 34 37 31 X12 | 16 17 36 16 12 68 25 29 --- 11 | 28 37 43 29 28 35 21 28 --- 25 13 | 18 20 25 16 11 54 20 28 42 9 | 29 43 42 37 32 41 24 36 30 29 14 | 15 17 21 14 8 51 21 20 24 8 | 28 45 46 35 31 42 29 31 33 30 X15 | 20 22 --- 25 16 16 28 31 34 10 | 33 46 --- 37 44 39 32 50 33 34 16 | 13 15 30 13 18 52 29 165 31 9 | 65 76 70 71 61 76 62 150 68 65 X17 | 5 --- --- --- 26 --- --- --- --- 0 | 13 --- --- --- 36 --- --- --- --- 17 18E | 11 12 14 12 6 44 14 20 22 6 | 30 37 35 32 32 31 30 37 34 30 19 | 12 14 15 11 8 38 29 57 48 9 | 43 53 45 46 41 46 37 68 40 38 20E | 11 16 28 11 9 45 13 23 38 7 | 27 37 43 31 30 36 33 34 48 29 21 | 16 15 24 16 7 49 32 26 29 8 | 27 44 43 32 30 37 28 35 30 29 22E | 15 16 15 29 7 41 22 23 24 8 | 37 48 47 47 38 42 39 40 42 37 23 | 16 21 20 12 14 54 24 28 38 9 | 31 46 47 38 35 46 31 40 37 33 24 | 7 10 20 13 9 10 14 26 14 5 | 28 32 32 32 32 35 32 33 30 27 25 | 12 12 20 16 7 16 26 19 53 7 | 27 33 37 26 27 29 33 33 48 26 X26 | 13 12 43 11 16 12 15 26 --- 8 | 133 134 138 134 134 133 133 139 --- 133 27 | 14 12 22 14 10 36 21 21 37 7 | 29 37 42 26 26 37 26 31 31 25 28 | 16 17 29 14 10 46 24 22 38 8 | 53 63 59 59 56 69 54 59 57 56 29 | 10 10 20 10 12 16 19 23 27 5 | 49 53 56 49 47 52 47 47 43 47 30 | 11 12 25 12 7 13 22 19 32 6 | 38 46 45 40 38 43 51 36 41 38 31 | 14 16 20 17 11 54 23 20 38 8 | 32 43 42 38 36 45 37 33 48 33 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 14 23 15 10 36 23 42 35 |T 35 46 46 40 38 44 38 45 40 35 WRMS | 13 14 23 15 9 36 22 16 35 |NE 36 47 47 40 39 45 39 47 40 36 MEDI | 13 13 22 13 9 23 22 23 36 |MD 31 43 43 37 33 39 32 36 37 31 Table 3.1410.6 GPS week: 1410 Day: 6 MJD: 54120.000 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 11 19 16 8 17 17 13 44 6 | 36 43 43 32 38 37 39 37 59 36 2 | 16 14 14 17 7 57 37 16 33 8 | 33 46 45 42 39 57 45 28 41 35 3 | 11 15 25 17 7 12 38 12 62 8 | 48 55 54 49 47 53 52 53 51 48 4 | 8 10 28 8 7 16 18 13 36 6 | 36 40 46 38 41 45 34 36 58 37 5 | 12 12 38 15 7 13 20 14 32 7 | 37 42 47 36 36 41 38 35 40 35 6 | 9 8 19 10 6 12 32 11 28 6 | 45 51 53 47 47 52 40 46 38 44 7 | 11 11 17 10 7 15 33 16 22 6 | 35 42 40 40 39 45 44 40 41 37 8 | 13 13 18 10 5 18 23 16 45 6 | 33 37 44 36 35 39 31 28 39 32 9 | 10 12 26 11 5 16 18 15 26 6 | 35 44 54 37 37 44 34 37 37 36 10E | 19 20 24 23 9 18 27 21 33 8 | 42 49 52 48 44 51 40 46 42 42 11 | 14 14 19 17 10 44 19 17 31 7 | 38 48 51 41 37 38 38 35 46 37 X12 | 15 16 30 16 9 67 24 17 --- 9 | 47 52 55 42 46 49 41 46 --- 45 13 | 18 19 20 17 10 53 26 18 26 8 | 33 47 47 44 42 50 30 33 38 36 14 | 13 17 23 14 9 49 19 18 21 7 | 32 48 44 36 34 43 27 28 34 33 X15 | 21 35 --- 22 14 18 28 20 28 10 | 40 46 --- 53 47 53 43 56 38 46 16 | 12 16 14 13 9 57 26 15 29 7 | 47 55 57 54 50 68 42 50 42 48 X17 | 17 --- --- --- 25 --- 41 21 --- 17 | 16 --- --- --- 19 --- 12 10 --- 16 18E | 8 13 16 12 6 46 16 16 22 6 | 44 51 54 44 43 50 38 42 41 43 19 | 10 12 17 10 8 41 32 20 49 8 | 47 56 50 46 44 48 38 40 49 43 20E | 10 13 17 16 5 51 20 15 40 7 | 34 38 39 39 37 37 40 37 57 35 21 | 15 14 15 16 8 50 33 18 29 8 | 30 44 44 37 34 44 32 34 33 32 22E | 14 15 16 28 6 42 20 18 16 7 | 32 42 39 42 34 37 35 31 35 32 23 | 15 18 20 13 7 58 27 17 35 8 | 37 53 51 43 45 55 45 37 47 41 24 | 8 8 23 13 6 10 13 14 17 5 | 32 36 37 39 36 40 37 33 36 33 25 | 12 13 23 15 8 14 34 19 45 8 | 32 35 35 31 34 33 44 38 54 34 26 | 9 9 21 10 7 13 18 17 25 5 | 121 122 129 120 118 120 118 116 136 120 27 | 12 12 22 12 5 17 23 15 33 6 | 37 45 47 44 42 46 37 37 42 38 28 | 13 21 26 11 6 54 19 20 35 8 | 47 54 56 48 46 62 39 42 45 45 29 | 12 11 21 14 5 14 23 19 26 6 | 36 43 45 35 38 43 36 35 38 35 30 | 11 13 37 14 7 16 24 14 35 7 | 35 43 45 38 37 42 48 35 45 36 31 | 14 16 18 17 10 53 21 18 26 7 | 36 46 48 44 43 49 33 39 45 38 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 14 22 15 7 36 25 16 34 |T 39 48 50 44 42 49 40 40 46 40 WRMS | 12 14 22 15 7 36 23 14 29 |NE 40 48 50 44 42 49 40 40 46 40 MEDI | 12 13 20 14 7 18 23 17 31 |MD 36 46 47 42 39 45 38 37 42 37 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 4.1410 GPS week: 1410 MJD: 54114.0-54120.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2944 |U 22 24 45 |U 17 18 70 |U 21 30 57 | emr | emr 2894 |U 18 25 40 | 19 24 69 | 28 24 49 | esa | esa 2714 | 25 36 60 |U 17 25 72 | 30 28 61 | gfz | gfz 2903 |U 20 27 40 |U 17 21 64 |U 25 20 42 | igr | igr 2941 | 21 29 51 | 18 26 69 | 23 28 69 | igs | igs 2932 | 20 27 47 | 18 22 70 | 21 27 68 | jpl | jpl 2917 | 23 27 45 | 22 28 73 | 28 23 44 | mit | mit 2948 |U 18 27 46 |U 18 23 70 |U 18 27 62 | 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 5.1410.0 GPS week: 1410 Day: 0 MJD: 54114.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2958 | 11 15 32 | 15 13 67 | 12 19 47 | emr | emr 2876 | 12 16 34 | 15 15 56 | 18 20 48 | esa | esa 2784 | 14 22 39 | 14 13 63 | 15 18 50 | gfz | gfz 2864 | 18 16 30 | 15 14 63 | 13 16 38 | igr | igr 2953 | 12 21 36 | 15 20 76 | 19 22 58 | igs | igs 2880 | 13 15 32 | 14 14 61 | 15 19 50 | jpl | jpl 2962 | 19 22 41 | 19 21 66 | 15 16 43 | mit | mit 2976 | 12 19 37 | 15 16 72 | 11 13 38 | Table 5.1410.1 GPS week: 1410 Day: 1 MJD: 54115.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2968 | 37 38 41 | 12 15 63 | 12 15 33 | emr | emr 2876 | 15 23 36 | 13 18 61 | 18 16 37 | esa | esa 2784 | 29 37 57 | 12 16 53 | 17 18 42 | gfz | gfz 2961 | 18 26 33 | 12 16 52 | 12 9 27 | igr | igr 2974 | 24 36 56 | 17 24 70 | 16 15 38 | igs | igs 2976 | 23 32 41 | 13 18 55 | 14 13 34 | jpl | jpl 2968 | 16 16 37 | 18 19 63 | 13 13 35 | mit | mit 2976 | 21 34 56 | 14 18 60 | 13 11 30 | Table 5.1410.2 GPS week: 1410 Day: 2 MJD: 54116.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2867 | 18 26 54 | 18 24 86 | 11 15 25 | emr | emr 2872 | 20 22 44 | 22 31 89 | 14 15 30 | esa | esa 2688 | 25 34 65 | 17 24 93 | 16 14 28 | gfz | gfz 2864 | 22 23 44 | 17 24 82 | 13 7 31 | igr | igr 2878 | 17 29 48 | 19 31 79 | 16 11 40 | igs | igs 2880 | 17 27 49 | 19 22 90 | 17 10 36 | jpl | jpl 2876 | 22 17 44 | 21 28 90 | 19 19 32 | mit | mit 2880 | 21 33 51 | 20 24 90 | 11 15 27 | Table 5.1410.3 GPS week: 1410 Day: 3 MJD: 54117.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2955 | 25 38 47 | 18 17 77 | 14 17 24 | emr | emr 2961 | 23 29 40 | 22 25 75 | 14 18 29 | esa | esa 2688 | 34 51 64 | 21 26 92 | 17 19 36 | gfz | gfz 2962 | 23 29 47 | 20 25 70 | 11 10 28 | igr | igr 2969 | 28 38 57 | 20 23 67 | 19 15 31 | igs | igs 2974 | 25 37 54 | 20 24 74 | 14 14 29 | jpl | jpl 2959 | 25 29 40 | 25 29 79 | 19 22 34 | mit | mit 2976 | 26 37 55 | 21 23 76 | 14 19 28 | Table 5.1410.4 GPS week: 1410 Day: 4 MJD: 54118.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2937 | 33 30 50 | 17 16 57 | 15 22 35 | emr | emr 2946 | 23 26 21 | 19 19 65 | 15 24 42 | esa | esa 2679 | 28 57 61 | 19 36 65 | 18 22 47 | gfz | gfz 2942 | 24 28 23 | 17 21 58 | 14 18 33 | igr | igr 2965 | 29 39 46 | 19 24 68 | 14 23 38 | igs | igs 2963 | 29 37 41 | 19 20 67 | 14 21 40 | jpl | jpl 2953 | 30 27 28 | 24 31 71 | 18 18 30 | mit | mit 2976 | 24 33 31 | 16 25 66 | 13 25 40 | Table 5.1410.5 GPS week: 1410 Day: 5 MJD: 54119.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2955 | 15 14 46 | 20 18 62 | 14 14 32 | emr | emr 2870 | 16 20 53 | 25 32 70 | 13 22 52 | esa | esa 2688 | 27 13 78 | 20 30 70 | 17 20 46 | gfz | gfz 2864 | 19 28 53 | 20 22 60 | 14 20 42 | igr | igr 2878 | 22 24 66 | 20 33 62 | 16 18 54 | igs | igs 2880 | 20 23 60 | 21 30 75 | 16 18 50 | jpl | jpl 2856 | 26 31 59 | 24 35 64 | 17 15 31 | mit | mit 2880 | 13 22 49 | 20 30 70 | 13 21 43 | Table 5.1410.6 GPS week: 1410 Day: 6 MJD: 54120.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2968 | 12 10 41 | 19 27 76 | 67 107 201 | emr | emr 2861 | 14 39 52 | 19 29 66 | 103 56 103 | esa | esa 2688 | 15 35 54 | 18 33 66 | 112 87 175 | gfz | gfz 2864 | 14 39 51 | 19 24 61 | 98 59 95 | igr | igr 2976 | 14 15 47 | 19 24 58 | 59 95 227 | igs | igs 2975 | 14 14 52 | 18 26 68 | 60 96 239 | jpl | jpl 2847 | 21 48 68 | 24 37 78 | 95 58 99 | mit | mit 2976 | 11 14 45 | 17 24 59 | 54 86 229 | 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 6.1410 GPS week: 1410 MJD: 54114.500-54120.500 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 | 1 -27 19 18 8 | -9 24 | 14 20 45 32 5 | 3 emr uuuuu | 9 -33 -52 -2 -3 | 31 38 | 32 17 53 58 12 | 5 esa uuuuu | 42 11 36 8 -14 | 42 48 | 46 34 76 46 8 | 3 gfz uuuuu | 10 30 14 -15 -8 | 14 27 | 17 9 57 42 10 | 3 igr xxxxx | -16 13 90 -12 0 | 4 23 | 23 32 60 75 7 | 3 irf xxxxx | 0 16 26 18 -11 | 8 24 | 8 15 44 40 6 | 3 jpl uuxuu | 23 -54 -5 168 15 | -21 32 | 20 37 213 61 7 | 3 mit uuuuu | -30 1 -207 -112 4 | 13 26 | 42 46 55 134 10 | 4 ngs uuuxu | -8 98 150 14 -6 | -10 24 | 45 53 196 247 10 | 5 sio uuuuu | -77 -97 31 43 -7 | 20 32 | 24 35 73 123 9 | 3 Table 7.1410.0 GPS week: 1410 Day: 0 MJD: 54114.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 14 -20 19 57 5 | -13 24 emr uuuuu | 48 -20 -96 25 -20 | 37 42 esa uuuuu | -46 -18 29 12 -7 | 38 47 gfz uuuuu | 18 45 -58 -25 7 | 9 24 igr xxxxx | -23 28 177 -85 8 | 0 21 irf xxxxx | -2 15 -15 33 0 | 6 23 jpl uuxuu | 51 -84 177 64 10 | -22 30 mit uuuuu | -30 20 -306 -296 21 | 5 22 ngs uuuxu | -53 85 416 -97 -27 | -3 20 sio uuuuu | -89 -142 15 226 5 | 15 30 Table 7.1410.1 GPS week: 1410 Day: 1 MJD: 54115.500 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 -20 5 10 2 | -11 23 emr uuuuu | 34 -50 8 101 -12 | 35 41 esa uuuuu | 7 -9 84 71 -8 | 41 48 gfz uuuuu | 22 23 -49 -7 0 | 13 24 igr xxxxx | 14 29 23 7 7 | 2 20 irf xxxxx | -1 20 35 21 -7 | 9 22 jpl uuxuu | 29 -66 146 178 2 | -23 30 mit uuuuu | -63 26 -210 -277 12 | 9 23 ngs uuuxu | -35 95 151 62 -10 | -6 23 sio uuuuu | -100 -82 -18 -61 1 | 18 30 Table 7.1410.2 GPS week: 1410 Day: 2 MJD: 54116.500 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 | 1 -29 99 -24 3 | -10 22 emr uuuuu | 28 -46 31 -4 -12 | 32 39 esa uuuuu | 67 23 182 -3 -17 | 44 48 gfz uuuuu | 22 27 -13 66 -4 | 14 23 igr xxxxx | -45 22 21 -17 -1 | 4 19 irf xxxxx | -7 -2 113 -54 -13 | 10 22 jpl uuxuu | 23 -53 79 162 18 | -24 31 mit uuuuu | -89 -48 -225 -95 5 | 12 22 ngs uuuxu | -9 183 -215 -381 -3 | -7 24 sio uuuuu | -106 -135 167 -34 -8 | 20 30 Table 7.1410.3 GPS week: 1410 Day: 3 MJD: 54117.500 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 | -18 -7 37 14 7 | -5 24 emr uuuuu | 25 -23 -111 -61 -1 | 33 40 esa uuuuu | 73 77 4 57 -17 | 48 52 gfz uuuuu | 16 23 55 -68 -14 | 20 28 igr xxxxx | -31 -20 130 8 -1 | 9 23 irf xxxxx | -6 32 43 47 -14 | 13 25 jpl uuxuu | 25 -46 109 234 15 | -19 32 mit uuuuu | -47 -30 -186 10 2 | 17 29 ngs uuuxu | -22 24 189 86 -2 | -6 25 sio uuuuu | -69 -69 63 89 -2 | 24 34 Table 7.1410.4 GPS week: 1410 Day: 4 MJD: 54118.500 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 -70 4 36 7 | -9 25 emr uuuuu | -25 -8 -77 -32 4 | 27 35 esa uuuuu | 72 -5 12 -45 -8 | 43 49 gfz uuuuu | -19 32 40 -3 -13 | 15 28 igr xxxxx | 10 45 127 86 -12 | 6 24 irf xxxxx | 3 9 16 63 -13 | 8 25 jpl uuxuu | -11 -108 81 243 15 | -20 33 mit uuuuu | 11 69 -155 -137 2 | 15 28 ngs uuuxu | 55 88 158 -2 -2 | -13 24 sio uuuuu | -71 -59 -27 89 -8 | 21 33 Table 7.1410.5 GPS week: 1410 Day: 5 MJD: 54119.500 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 | 7 -18 19 -18 17 | -12 26 emr uuuuu | -34 -50 -75 20 11 | 23 32 esa uuuuu | 76 24 -9 17 -12 | 39 47 gfz uuuuu | -10 36 97 -44 -20 | 11 29 igr xxxxx | -34 28 46 50 1 | 1 26 irf xxxxx | 2 39 3 -16 -18 | 4 27 jpl uuxuu | 9 1 -299 155 25 | -23 35 mit uuuuu | -17 22 -140 45 -5 | 13 29 ngs uuuxu | 55 62 66 447 -5 | -17 28 sio uuuuu | -65 -71 60 -129 -16 | 18 33 Table 7.1410.6 GPS week: 1410 Day: 6 MJD: 54120.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -9 -24 -51 53 12 | -5 25 emr uuuuu | -13 -37 -45 -66 9 | 28 37 esa uuuuu | 46 -17 -52 -52 -29 | 41 49 gfz uuuuu | 23 21 28 -21 -15 | 14 29 igr xxxxx | -1 -44 103 -130 -3 | 7 25 irf xxxxx | 16 2 -12 35 -15 | 6 27 jpl uuxuu | 37 -21 -326 139 19 | -15 31 mit uuuuu | 30 -54 -231 -32 -7 | 18 29 ngs uuuxu | -44 148 282 -17 6 | -14 25 sio uuuuu | -36 -122 -42 121 -20 | 22 33