Date: Fri, 08 Feb 2008 22:20:08 +0100 To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-15927] Wk 1463 IGS Final Orbits [Resubmission_with_MIT] User-Agent: Heirloom mailx 12.3 7/15/07 Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20080208212008.E804350984@kg20.gfz-potsdam.de> From: igsacc@gfz-potsdam.de (Gerd Gendt3) Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 08 Feb 13:20:19 PST 2008 Message Number 15927 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1463 (Jan 20, 2008 - Jan 26, 2008) 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: igs1463[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1463[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1463[0-6].cls IGS GPS clock combination summary report. igs14637.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14637.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 | EMR | 10 ONSA SPT0 0 | ESA | 10 19 29 32 0 | GFZ | 16 19 29 1 | EMR | ONSA 1 | ESA | 29 32 KHAJ 1 | GFZ | 29 1 | JPL | IRKJ 1 | MIT | 32 USNO 2 | COD | MCM4 2 | EMR | GODE MAR6 ONSA 2 | ESA | 29 30 AREQ 2 | GFZ | 2 29 KERG 2 | JPL | AREQ 2 | MIT | 32 3 | COD | 30 3 | EMR | 32 KHAJ 3 | ESA | 5 29 30 32 3 | GFZ | CEDU 3 | MIT | 5 16 18 31 4 | EMR | MAR6 ONSA 4 | ESA | 29 MAS1 4 | GFZ | MAS1 NISU 4 | MIT | 5 14 28 32 MATE 5 | EMR | 18 ONSA 5 | ESA | 10 17 29 30 BRAZ CHUR HOLM SYOG 5 | GFZ | 5 29 5 | MIT | 5 26 30 THTI USN3 6 | EMR | HARB ONSA SPT0 WTZR 6 | ESA | 29 30 6 | GFZ | 29 NISU 6 | JPL | 5 12 HARB 6 | MIT | 5 30 5. 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. 6. 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 .5 .0 -16 9 -7 .17 EMR | 1.8 9.6 .1 -21 50 4 .27 ESA | 6.5 9.3 -5.6 31 -62 62 .82 GFZ | .7 .0 -.2 -6 -22 10 .06 JPL | -1.4 6.2 14.3 17 9 -18 .43 MIT | .6 6.6 -8.7 -13 12 -2 .03 NGS | 4.0 -2.3 -3.3 -45 -77 27 -.69 SIO | -1.1 9.8 12.7 115 -1 0 .66 7. 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. 8. 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. 9. 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 1.1463.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1463.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 2.1463.[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 3.1463.[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 5.1463.0-6). 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 1463 summary. (Jan 20, 2008 - Jan 26, 2008) Table 1.1463.a GPS week: 1463 MJD: 54485.000-54491.000 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 169| 1 0 -1 13 -26 -12 -.26 10 9 | -323 -312 31 80 | 0 0 1 20 14 35 .02 | 521 825 emr 66| 1 2 2 36 -129 -8 .40 16 16 | 4984 -286 59 124 | 2 1 1 14 40 12 .03 | 1858 2219 esa 106| 2 0 -2 -8 80 9 .20 13 13 | -7768 -288 33 168 | 1 1 2 38 85 20 .03 | 2213 2145 gfz 164| -1 1 2 -4 29 -12 -.08 14 14 | 29 129 33 117 | 0 0 1 25 23 32 .08 | 309 579 igr n/a| 0 -1 -1 -17 -15 -9 .03 7 7 | 12712 26 32 89 | 0 0 1 15 24 20 .03 | 2561 2584 jpl 116| 0 -3 9 -50 -33 -9 .51 14 14 | 7593 -147 37 81 | 1 1 0 27 27 17 .04 | 2068 2386 mit 310| -1 0 -8 28 -41 -2 -.33 14 13 | 121 -41 39 132 | 0 0 1 52 36 21 .03 | 895 717 ngs 184| -2 0 1 62 122 9 -.27 14 11 | -275 -370 2472 4228 | 1 0 1 36 50 27 .05 | 456 687 sio 86| 0 0 -1 -259 -39 12 .13 26 24 | --- --- --- --- | 2 1 1 39 29 35 .04 | --- --- Table 1.1463.b GPS week : 1463 MJD: 54485.000-54491.000 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: mm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------+------------------------------------+------------------------------------------ 1 | 5 5 5 5 6 5 6 | 2 | 6 6 6 6 6 6 5 | 3 | 5 5 4 5 5 5 5 | 4 | 5 5 5 5 5 5 4 | 5E | 6 6 6 7 7 7 7 | 6 | 4 5 5 4 5 4 4 | 8 | 6 5 5 4 4 5 4 | 9 | 5 5 4 4 4 4 4 | 10E | 8 8 7 6 7 7 6 | 11 | 6 6 5 5 5 5 5 | 12E | 6 6 6 7 6 5 6 | 13 | 6 5 6 6 5 5 5 | 14 | 6 6 6 6 6 5 5 | 15 | 5 6 6 6 6 6 6 | 16E | 6 6 7 6 6 6 6 | 17 | 6 5 6 6 6 6 5 | 18E | 6 5 7 5 5 5 5 | 19 | 8 7 6 6 6 6 6 | 20 | 6 5 5 5 5 5 5 | 21 | 6 5 6 5 6 5 6 | 22E | 6 5 6 5 5 5 5 | 23 | 6 6 6 6 5 5 5 | 24 | 4 4 4 4 5 4 5 | 25 | 5 5 4 4 4 4 4 | 26 | 5 5 5 5 6 6 6 | 27 | 6 5 5 4 4 4 4 | 28E | 6 6 6 6 6 6 6 | 29 | 7 7 7 7 7 7 7 | 30E | 7 6 6 6 7 7 8 | 31 | 6 5 6 6 6 6 6 | 32E | 13 13 15 15 12 12 14 | 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 2.1463.0 GPS week: 1463 Day: 0 MJD: 54485.000 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 169| 1 0 -3 1 -27 37 -.25 10 10 | 487 -2052 30 84 | 22 27 | emr 66| -1 1 3 35 -147 -24 .40 16 16 | 2919 1119 59 146 | 2 28 | esa 106| 4 4 0 -17 68 -14 .20 15 15 | -3122 -3797 35 190 | 77 9 | gfz 164| -1 1 0 24 59 -15 -.22 15 15 | 434 -481 35 131 | -11 -23 | igr n/a| 1 -2 -1 -8 12 -25 .00 8 8 | 8904 1787 40 121 | -15 -66 | jpl 116| 0 -3 9 -60 -37 -13 .56 14 14 | 5153 1310 38 86 | 40 -27 | mit 310| -2 0 -7 46 -15 -2 -.38 16 14 | 1960 -1058 38 150 | 13 -17 | ngs 184| -1 0 0 48 100 -8 -.24 14 13 | 411 -1859 2546 4706 | 45 84 | sio 86| -3 -1 -2 -205 -27 -60 .10 29 25 | --- --- --- --- | 125 46 | Table 2.1463.1 GPS week: 1463 Day: 1 MJD: 54486.000 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 169| 2 0 -3 20 -9 -58 -.29 10 9 | -844 544 35 92 | -7 18 | emr 66| 1 1 2 50 -75 -9 .35 16 16 | 3903 1753 62 125 | -23 -26 | esa 106| 1 1 1 -1 -36 40 .15 11 11 | -9074 212 33 175 | -28 -9 | gfz 164| -2 1 0 -1 37 23 -.13 14 14 | 200 -476 37 111 | -22 -30 | igr n/a| 0 -1 -2 -4 20 -23 -.02 8 7 | 10676 2504 33 80 | -28 -10 | jpl 116| 0 -2 8 -48 23 10 .52 13 13 | 6118 2013 37 87 | 6 -67 | mit 310| -1 0 -7 11 -80 -1 -.35 16 15 | -167 -282 38 139 | -6 8 | ngs 184| -2 0 0 68 195 -24 -.23 14 12 | -532 66 2547 4203 | 57 -7 | sio 86| 1 0 -1 -307 -37 9 .17 27 25 | --- --- --- --- | 152 40 | Table 2.1463.2 GPS week: 1463 Day: 2 MJD: 54487.000 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 169| 2 0 -1 44 -39 10 -.28 12 10 | -1060 -34 38 80 | -65 11 | emr 66| -1 2 2 54 -94 0 .41 16 16 | 5476 1675 65 115 | 23 -38 | esa 106| 3 1 -2 -49 33 -5 .17 13 12 | -9044 755 33 166 | -16 -65 | gfz 164| 0 1 0 -5 44 -49 -.11 14 14 | -207 14 35 116 | -12 -44 | igr n/a| 0 -2 -2 0 -17 4 .04 7 7 | 13003 2236 33 74 | 34 -18 | jpl 116| 0 -3 8 2 -32 -9 .52 14 14 | 7859 1844 41 89 | 20 -1 | mit 310| 0 0 -8 -76 -77 3 -.34 13 12 | -937 1125 44 105 | 44 24 | ngs 184| -2 0 1 129 166 30 -.31 13 10 | -1050 26 2549 3934 | -32 44 | sio 86| -2 -1 0 -276 -42 19 .18 25 23 | --- --- --- --- | 118 5 | Table 2.1463.3 GPS week: 1463 Day: 3 MJD: 54488.000 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 169| 1 0 0 -17 -29 -15 -.26 10 10 | -275 -409 32 93 | 23 9 | emr 66| 1 0 0 41 -109 -20 .39 16 16 | 6508 1137 55 124 | -32 3 | esa 106| 3 0 -3 47 71 5 .20 13 13 | -6766 -2255 36 156 | -2 -13 | gfz 164| 0 0 3 22 27 22 -.03 13 13 | -66 -64 29 117 | 9 -28 | igr n/a| 0 -1 -2 -43 -18 -35 .05 8 8 | 14585 1532 28 72 | 7 3 | jpl 116| 0 -4 9 -87 -29 -15 .54 16 16 | 9104 1562 37 77 | 26 8 | mit 310| -1 0 -8 47 -54 -2 -.32 13 12 | -253 222 36 127 | -55 6 | ngs 184| -1 0 2 19 152 -13 -.21 14 11 | -256 -438 2390 4503 | 70 32 | sio 86| -1 1 0 -272 -9 12 .16 25 24 | --- --- --- --- | 157 -8 | Table 2.1463.4 GPS week: 1463 Day: 4 MJD: 54489.000 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 169| 1 0 -1 32 -49 -30 -.26 10 9 | -212 143 34 77 | -2 6 | emr 66| 4 5 3 30 -131 1 .41 17 17 | 6888 -1971 61 125 | 38 6 | esa 106| 2 -1 -2 -64 244 5 .24 13 13 | -9234 2588 37 171 | 6 5 | gfz 164| 0 1 4 -51 -15 -16 .01 14 14 | -15 1146 35 138 | 61 -30 | igr n/a| 0 -1 0 -14 -48 -2 .03 8 8 | 15343 -1742 36 101 | 40 -1 | jpl 116| 0 -3 9 -39 -50 0 .47 14 14 | 9830 -1724 39 72 | 45 -8 | mit 310| -1 0 -10 44 -64 5 -.32 13 12 | 296 -301 45 156 | -24 -18 | ngs 184| -4 0 1 81 115 31 -.32 14 11 | -217 118 2289 4213 | -9 76 | sio 86| -1 0 -2 -212 -97 41 .11 27 25 | --- --- --- --- | 107 22 | Table 2.1463.5 GPS week: 1463 Day: 5 MJD: 54490.000 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 169| 1 0 0 11 -12 16 -.24 10 9 | -407 -177 25 63 | 8 1 | emr 66| 3 1 2 32 -156 -12 .38 16 16 | 6696 -3718 56 119 | -12 46 | esa 106| 0 0 -1 18 76 36 .23 11 12 | -8696 1040 31 147 | -34 -26 | gfz 164| -1 1 2 -18 32 8 -.03 13 13 | 315 565 30 105 | 11 -24 | igr n/a| 1 -1 0 -29 -28 23 .05 7 6 | 15434 -3917 28 75 | -21 -1 | jpl 116| 2 -1 9 -55 -55 -41 .45 15 15 | 9801 -3888 38 81 | 7 -37 | mit 310| -2 0 -8 36 0 -46 -.28 14 13 | 51 501 37 112 | -51 -13 | ngs 184| -2 0 0 58 62 1 -.32 13 11 | -335 -281 2685 4286 | -83 132 | sio 86| 2 0 -1 -294 -10 16 .09 24 23 | --- --- --- --- | 190 41 | Table 2.1463.6 GPS week: 1463 Day: 6 MJD: 54491.000 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 169| 1 0 -1 2 -21 -49 -.23 10 9 | 50 -204 26 74 | 31 -22 | emr 66| 2 2 4 11 -194 10 .47 18 18 | 2498 -2000 59 120 | 35 55 | esa 106| 1 -1 -6 4 105 0 .20 11 11 | -8444 -565 31 173 | 36 -38 | gfz 164| -1 1 3 -4 21 -58 -.05 13 13 | -454 200 31 105 | 35 -50 | igr n/a| 0 -1 -1 -23 -27 -2 .08 7 7 | 11041 -2213 31 100 | 0 -51 | jpl 116| 0 -1 9 -63 -54 6 .49 14 14 | 5290 -2152 33 79 | 49 -16 | mit 310| -2 0 -8 91 2 25 -.33 14 12 | -99 -495 38 137 | -40 -22 | ngs 184| 0 0 0 32 65 51 -.28 13 10 | 52 -228 2301 3757 | -78 84 | sio 86| 3 1 -1 -249 -47 47 .09 25 25 | --- --- --- --- | 187 63 | 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 3.1463.0 GPS week: 1463 Day: 0 MJD: 54485.000 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 | 7 12 17 14 9 10 8 11 29 4 | 26 34 24 32 28 35 26 26 42 28 2 | 10 12 11 16 6 10 15 12 45 5 | 43 46 46 48 41 45 44 46 43 43 3 | 10 11 11 9 12 8 13 14 34 5 | 25 29 29 26 28 24 31 25 34 24 4 | 8 13 12 12 9 8 15 12 32 4 | 39 41 40 37 42 36 36 40 43 37 5E | 12 17 11 15 8 14 23 14 29 6 | 40 40 36 42 41 36 31 44 46 37 6 | 6 10 9 13 5 10 11 12 24 4 | 33 36 35 33 38 32 41 39 39 35 8 | 8 12 14 13 6 11 22 18 29 5 | 24 27 21 30 26 27 31 25 28 24 9 | 9 14 14 13 6 10 15 13 19 4 | 24 30 25 28 24 27 27 20 28 23 10E | 20 19 22 21 8 16 16 17 55 8 | 79 82 74 78 81 81 75 83 86 77 11 | 8 16 15 11 10 18 14 19 29 6 | 46 54 44 47 44 48 48 41 44 44 12E | 12 18 14 10 5 16 11 11 25 5 | 36 42 30 39 36 42 36 36 33 35 13 | 9 17 13 17 7 12 15 15 24 5 | 19 34 21 28 25 29 20 22 23 21 14 | 12 22 18 15 9 14 11 14 13 5 | 20 34 22 25 23 27 21 23 22 20 15 | 9 19 14 14 6 13 14 12 19 5 | 20 33 24 29 23 26 22 22 22 22 16E | 10 15 16 17 7 18 18 14 31 6 | 17 31 22 27 20 31 21 21 25 20 17 | 11 18 12 14 9 17 8 14 23 5 | 28 32 25 35 27 34 27 29 28 26 18E | 10 17 11 19 6 19 11 13 20 5 | 31 37 30 38 31 36 33 31 31 30 19 | 13 17 34 13 11 16 30 17 27 8 | 24 32 43 30 25 34 31 26 22 24 20 | 10 20 14 9 10 15 14 15 24 5 | 19 33 18 23 24 28 25 21 30 20 21 | 10 15 13 14 5 15 11 11 32 5 | 36 44 38 41 37 43 35 37 39 37 22E | 12 14 16 28 9 15 12 11 17 6 | 23 29 25 38 28 27 25 26 24 22 23 | 11 21 13 12 6 14 17 15 26 5 | 21 39 22 30 27 33 22 21 32 24 24 | 6 11 11 12 7 10 12 14 21 4 | 33 38 34 34 35 30 35 36 32 33 X25 | 7 11 12 12 9 9 18 15 --- 5 | 23 26 22 29 27 28 26 23 --- 24 26 | 8 10 12 12 8 9 11 15 32 4 | 20 28 25 26 22 29 20 17 42 22 27 | 8 12 11 14 6 11 23 15 37 6 | 24 26 22 32 27 28 32 24 26 25 28E | 11 16 17 12 9 15 17 16 27 6 | 27 35 31 32 29 36 28 29 40 28 X29 | 16 18 17 13 8 21 18 16 --- 7 | 43 54 45 47 50 55 46 46 --- 46 30E | 12 17 14 15 8 16 22 19 28 6 | 52 55 48 55 53 46 54 57 55 50 31 | 11 17 15 16 8 17 12 11 36 6 | 19 35 21 29 25 33 24 23 41 23 X32E | 17 32 29 --- 45 --- 16 33 --- 12 | 71 79 70 --- 72 --- 78 76 --- 73 ------+---------------------------------------------------+---------------------------------------------------- RMS | 10 16 15 15 8 14 16 14 29 |T 31 39 32 35 34 35 33 33 35 32 WRMS | 10 16 15 15 8 14 14 13 25 |NE 27 35 29 32 30 33 30 28 33 28 MEDI | 10 16 14 13 8 14 15 14 27 |MD 26 35 29 32 28 33 31 26 32 26 Table 3.1463.1 GPS week: 1463 Day: 1 MJD: 54486.000 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 | 6 11 13 14 5 8 9 12 24 4 | 27 31 35 36 30 33 26 30 42 29 2 | 10 12 11 15 6 10 13 11 44 5 | 36 44 40 40 39 43 38 36 45 38 3 | 7 12 9 9 5 9 13 13 33 4 | 17 22 21 21 18 20 28 22 33 18 4 | 7 11 10 14 7 10 13 12 37 5 | 23 29 25 24 27 26 23 27 34 24 5E | 12 18 11 13 10 15 18 16 32 6 | 24 27 22 26 24 21 20 30 32 21 6 | 7 11 9 11 7 12 13 10 29 4 | 21 23 21 23 24 22 27 30 32 22 8 | 8 12 9 14 6 11 19 14 19 5 | 13 18 17 21 17 22 19 20 25 14 9 | 11 14 12 11 4 11 12 12 25 4 | 18 22 19 22 19 22 21 18 27 17 10E | 19 37 17 19 9 16 16 18 34 8 | 46 67 50 56 51 57 41 52 72 50 11 | 9 18 14 11 15 15 14 14 33 5 | 29 46 30 35 31 41 30 27 33 30 X12E | 12 15 --- 10 4 18 15 13 25 6 | 48 53 --- 52 49 55 49 53 46 50 13 | 8 18 13 18 7 10 15 12 22 5 | 14 32 24 27 23 28 14 21 22 19 14 | 13 19 12 17 7 14 12 19 12 5 | 17 29 21 27 22 24 21 27 24 19 15 | 10 19 14 17 6 15 14 20 25 6 | 14 29 24 24 20 24 17 19 23 17 16E | 9 14 11 9 7 18 18 13 28 5 | 22 33 24 27 26 34 29 32 33 26 17 | 12 15 10 16 11 16 9 15 20 5 | 15 24 13 24 20 24 17 24 21 14 18E | 13 17 12 11 8 18 12 13 19 5 | 42 54 55 54 50 53 55 51 51 49 19 | 10 17 12 14 10 17 37 14 33 7 | 17 33 26 30 24 34 42 27 32 23 20 | 9 18 9 12 7 12 9 13 25 4 | 13 27 13 17 15 21 12 17 24 12 21 | 10 14 11 14 5 15 10 10 29 5 | 26 36 31 33 30 35 28 31 36 29 22E | 11 15 11 12 10 13 11 16 16 5 | 23 31 26 32 21 25 23 29 25 24 23 | 10 19 11 13 6 15 17 16 20 5 | 15 35 22 26 23 31 18 23 24 20 24 | 6 9 7 15 5 10 9 12 22 4 | 23 23 22 22 24 21 23 29 31 22 25 | 6 10 11 12 6 9 20 13 15 4 | 14 21 22 24 18 23 18 20 23 17 26 | 7 13 9 14 5 11 13 18 31 5 | 17 28 25 25 19 26 16 19 41 20 27 | 6 10 10 13 6 10 22 15 24 5 | 14 20 22 21 17 23 21 20 29 16 28E | 13 18 13 16 5 18 15 18 27 6 | 20 34 30 24 21 35 21 29 39 23 X29 | 15 20 13 15 10 22 15 18 --- 7 | 54 63 56 58 56 65 60 56 --- 56 30E | 13 17 13 14 8 17 15 13 27 5 | 44 44 40 44 42 36 48 47 50 41 31 | 10 19 10 19 9 11 14 11 24 5 | 18 33 21 28 23 28 20 25 26 20 X32E | 11 38 29 --- 23 --- 18 30 --- 12 | 44 68 53 --- 59 --- 52 57 --- 50 ------+---------------------------------------------------+---------------------------------------------------- RMS | 10 16 11 14 8 13 16 14 27 |T 24 34 28 30 28 31 28 30 33 26 WRMS | 9 16 11 14 7 13 15 12 25 |NE 20 30 25 27 24 28 24 25 29 22 MEDI | 10 15 11 14 7 13 14 13 25 |MD 21 31 24 26 24 26 23 27 32 22 Table 3.1463.2 GPS week: 1463 Day: 2 MJD: 54487.000 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 15 12 15 6 10 8 13 24 4 | 24 33 21 27 23 29 19 33 35 24 2 | 8 15 14 12 5 12 12 12 40 5 | 35 36 37 38 34 36 33 33 49 33 3 | 8 14 10 11 7 9 6 8 26 4 | 21 31 23 21 21 23 23 25 27 21 4 | 9 12 13 11 6 8 10 12 23 4 | 26 31 34 25 30 28 27 31 32 26 5E | 12 17 12 12 8 16 18 18 26 6 | 25 26 20 24 24 22 19 34 29 20 6 | 6 12 12 12 9 10 12 11 29 4 | 20 27 24 24 26 25 32 29 35 24 8 | 10 13 9 13 7 10 9 13 25 4 | 11 18 12 19 13 19 16 15 25 11 9 | 8 14 10 11 4 11 10 9 20 4 | 16 21 16 19 16 22 13 20 11 14 10 | 19 17 15 23 9 15 18 16 26 7 | 90 97 92 97 96 102 94 101 98 94 11 | 7 15 10 10 10 16 12 10 22 4 | 33 42 29 32 33 38 33 32 32 31 X12E | 13 17 --- 10 8 17 14 11 27 6 | 31 31 --- 32 32 35 29 33 44 30 13 | 12 18 12 21 7 14 15 13 20 5 | 12 32 16 22 20 28 12 19 19 15 14 | 13 20 12 17 7 12 10 15 18 5 | 18 31 21 25 21 26 19 27 19 19 15 | 12 21 13 15 8 15 15 13 22 5 | 12 29 15 20 15 22 16 18 19 12 16E | 9 15 17 15 9 20 22 18 18 6 | 15 30 20 25 20 29 21 30 23 18 17 | 12 18 17 16 7 18 11 12 23 6 | 17 27 21 26 19 27 20 23 23 16 18E | 25 18 13 13 9 16 10 16 19 6 | 106 119 112 123 108 114 119 118 120 115 19 | 11 16 13 15 10 16 19 12 27 6 | 16 30 25 26 19 29 27 19 20 19 20 | 11 19 12 11 7 13 12 14 27 5 | 10 30 14 17 17 24 14 22 24 14 21 | 11 17 14 14 6 16 12 11 27 5 | 34 39 33 36 34 38 38 32 41 33 22E | 12 16 13 13 8 12 12 15 25 5 | 28 33 26 32 27 30 26 31 29 27 23 | 12 20 11 13 8 15 16 17 18 5 | 14 36 18 22 20 27 16 22 24 17 24 | 7 12 11 15 7 10 9 11 10 4 | 25 31 26 31 29 25 31 34 26 28 25 | 7 10 8 13 7 9 11 9 17 4 | 14 20 16 22 16 23 16 18 20 15 26 | 10 15 9 12 7 11 11 13 33 5 | 17 24 16 21 18 25 14 17 45 17 27 | 8 10 10 14 7 9 13 11 24 4 | 11 19 15 21 15 22 18 18 29 13 28E | 13 21 13 15 7 18 14 14 28 6 | 28 34 31 26 27 31 27 28 41 26 X29 | 13 20 15 16 14 21 15 18 --- 7 | 77 86 80 81 80 86 84 82 --- 80 30E | 15 17 17 13 9 19 15 12 25 6 | 44 44 40 45 40 35 46 49 45 41 31 | 11 17 13 18 7 16 12 11 32 5 | 15 30 14 24 19 27 16 26 30 17 X32E | 20 33 29 --- 37 --- 18 44 --- 14 | 68 72 79 --- 81 --- 73 81 --- 73 ------+---------------------------------------------------+---------------------------------------------------- RMS | 12 16 13 14 7 14 13 13 25 |T 29 38 31 33 32 34 31 35 34 30 WRMS | 10 16 12 14 7 14 12 10 23 |NE 24 34 26 30 27 32 27 30 31 25 MEDI | 11 17 12 13 7 14 12 13 25 |MD 21 31 21 25 23 27 23 29 29 21 Table 3.1463.3 GPS week: 1463 Day: 3 MJD: 54488.000 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 | 7 15 13 15 5 10 16 11 26 5 | 32 41 36 40 36 41 34 37 40 34 2 | 13 14 13 13 9 14 10 18 39 6 | 43 45 39 42 44 44 42 42 40 40 3 | 8 17 12 8 7 13 8 14 39 5 | 18 25 30 21 25 20 24 28 34 21 4 | 11 12 13 14 10 11 13 17 26 5 | 30 30 27 27 32 26 28 38 34 28 5E | 13 20 10 11 8 18 18 23 26 6 | 29 34 27 32 31 29 29 42 39 29 6 | 7 9 12 9 4 12 12 8 27 4 | 23 30 31 25 27 25 34 28 34 26 8 | 7 10 11 12 8 12 9 15 16 4 | 15 19 17 19 18 22 13 19 24 14 9 | 7 14 10 10 4 11 9 11 24 4 | 19 26 17 22 19 24 16 21 19 18 10 | 13 22 12 15 5 17 14 13 23 6 | 58 61 58 62 60 66 58 59 65 58 11 | 8 15 13 12 13 20 13 15 19 5 | 36 47 44 37 39 42 39 37 38 38 X12E | 17 16 --- 8 8 21 13 13 27 6 | 52 57 --- 52 54 58 52 57 47 52 13 | 10 18 16 16 10 14 10 12 22 5 | 16 34 25 25 26 30 18 23 21 20 14 | 10 20 13 13 8 18 15 15 29 6 | 20 31 20 26 25 30 22 25 29 21 15 | 11 19 14 14 6 15 10 12 21 5 | 19 31 21 25 21 25 19 21 20 18 16E | 8 17 25 10 6 18 13 14 24 6 | 18 28 32 23 22 30 20 28 26 20 17 | 15 18 18 17 9 22 13 12 21 6 | 18 28 20 26 19 29 17 21 16 17 18 | 9 15 12 9 11 20 11 14 20 5 | 64 66 63 64 63 61 65 66 58 63 19 | 10 13 16 14 8 18 21 14 30 6 | 16 25 21 24 19 26 19 22 19 16 20 | 10 18 11 12 7 14 8 15 23 5 | 12 27 13 19 17 24 11 15 26 13 21 | 7 14 12 14 7 15 15 12 24 5 | 33 40 31 33 33 38 30 35 29 31 22 | 17 17 12 11 6 15 8 12 14 5 | 27 38 36 35 33 33 32 35 31 31 23 | 13 20 11 11 9 18 10 14 29 5 | 16 37 25 26 25 33 20 21 37 21 24 | 8 12 9 11 6 12 9 10 16 4 | 28 33 34 29 33 30 36 34 39 30 25 | 7 7 12 11 6 12 9 11 21 4 | 13 22 19 19 17 24 17 18 22 15 26 | 10 12 8 13 6 10 14 15 33 5 | 21 27 24 28 24 27 25 22 45 22 27 | 6 9 12 11 6 11 10 12 21 4 | 15 21 17 20 18 24 17 19 27 16 28E | 10 16 14 11 10 21 15 16 23 5 | 40 48 42 36 41 45 39 38 57 39 X29 | 13 19 14 14 12 23 12 17 --- 6 | 120 129 127 123 124 128 131 122 --- 124 30E | 15 16 13 13 9 19 14 10 31 6 | 44 43 39 48 41 36 50 49 56 43 31 | 9 17 14 18 10 18 19 17 18 6 | 18 32 19 27 24 32 24 27 25 20 X32E | 29 44 18 --- 33 --- 19 38 --- 15 | 48 78 68 --- 65 --- 67 70 --- 60 ------+---------------------------------------------------+---------------------------------------------------- RMS | 10 16 13 13 8 16 13 14 25 |T 31 39 34 34 34 36 33 36 34 32 WRMS | 10 16 13 13 8 16 12 11 24 |NE 29 37 32 33 32 36 31 33 32 30 MEDI | 10 16 12 12 8 15 13 14 24 |MD 23 33 27 27 27 30 28 28 34 26 Table 3.1463.4 GPS week: 1463 Day: 4 MJD: 54489.000 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 23 11 16 7 12 13 13 24 5 | 18 35 29 28 23 31 21 27 31 23 2 | 10 15 13 14 10 12 15 15 37 5 | 29 31 39 32 32 32 28 37 26 29 3 | 9 14 10 8 6 12 9 10 40 5 | 17 23 21 16 20 18 22 22 30 18 4 | 8 10 14 12 9 9 15 15 22 4 | 27 27 38 24 29 27 29 33 33 27 5E | 15 19 14 13 8 16 13 29 24 6 | 23 27 26 25 25 24 23 43 33 22 6 | 5 12 15 11 5 11 14 12 26 4 | 29 30 35 29 30 30 39 34 43 31 8 | 5 12 13 12 6 11 9 11 18 4 | 12 19 21 18 17 20 13 19 21 13 9 | 7 14 9 11 7 9 11 12 24 4 | 16 22 25 22 18 21 14 24 20 16 10 | 11 27 13 16 8 16 19 15 32 6 | 35 55 45 41 35 43 37 41 55 38 11 | 7 14 11 13 11 17 11 12 28 5 | 35 44 41 37 34 39 33 35 33 34 12E | 12 17 14 10 8 20 13 16 21 5 | 19 32 31 21 22 31 21 30 21 21 13 | 9 17 12 17 8 12 10 10 24 5 | 14 32 29 22 21 28 15 17 21 17 14 | 11 20 15 17 8 14 12 16 20 5 | 16 29 27 24 20 24 18 24 22 18 15 | 14 20 14 16 8 16 14 17 24 6 | 15 31 26 25 21 25 18 29 19 18 16E | 9 18 16 12 8 20 16 18 25 6 | 13 23 25 22 18 25 22 29 24 17 17 | 11 19 17 17 9 17 13 12 21 5 | 18 26 29 26 18 27 18 24 22 18 18 | 9 16 12 11 9 13 11 14 17 4 | 37 42 46 38 37 39 38 36 37 37 19 | 10 14 16 15 9 16 17 13 27 5 | 14 25 25 23 17 25 17 20 18 16 20 | 9 17 12 12 7 16 9 15 22 5 | 9 25 26 17 14 24 12 22 20 12 21 | 9 15 11 13 7 16 16 10 33 5 | 24 35 34 30 27 33 27 31 30 27 22 | 12 15 9 11 7 14 7 10 15 4 | 26 31 32 28 24 27 27 28 25 25 23 | 10 18 11 12 6 14 9 12 34 5 | 13 32 29 22 20 28 14 21 37 18 24 | 9 12 9 14 5 10 9 9 32 4 | 24 29 33 28 27 23 32 33 34 27 25 | 6 10 12 12 5 10 8 9 17 3 | 14 22 27 19 17 21 17 21 24 17 26 | 10 14 9 12 7 14 17 15 38 5 | 15 25 26 21 16 24 16 21 48 17 27 | 5 12 13 12 6 10 7 12 26 4 | 14 21 24 20 16 20 17 21 25 16 28E | 9 13 15 12 8 17 14 12 30 5 | 16 27 25 21 21 28 19 23 35 18 X29 | 11 20 18 14 14 22 14 15 --- 6 | 95 99 95 98 100 101 100 98 --- 97 30E | 18 19 14 17 9 18 19 15 27 6 | 46 42 44 42 43 35 55 52 54 43 31 | 9 19 14 18 14 16 15 18 26 6 | 14 29 25 23 19 26 19 26 25 16 X32E | 22 32 16 --- 23 --- 16 32 --- 12 | 86 94 88 --- 94 --- 97 97 --- 89 ------+---------------------------------------------------+---------------------------------------------------- RMS | 10 17 13 14 8 14 13 14 27 |T 25 34 34 28 28 29 28 32 29 26 WRMS | 9 17 13 14 8 14 12 11 25 |NE 23 32 33 28 26 30 25 29 29 25 MEDI | 9 16 13 12 8 14 13 13 25 |MD 18 29 29 24 21 27 21 28 26 18 Table 3.1463.5 GPS week: 1463 Day: 5 MJD: 54490.000 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 20 9 14 6 13 14 11 22 5 | 25 36 28 30 27 30 20 29 33 25 2 | 10 13 12 15 7 17 17 12 24 5 | 28 31 28 31 28 33 31 31 25 26 3 | 8 14 9 9 7 11 16 12 31 5 | 19 23 22 17 19 23 24 25 29 19 4 | 7 13 10 14 8 10 18 13 15 4 | 23 25 24 21 22 24 29 25 28 22 5E | 12 19 15 12 7 18 13 25 21 6 | 24 29 24 24 24 25 30 42 35 24 6 | 6 13 9 7 7 12 14 10 16 4 | 36 38 35 36 38 42 38 43 41 37 8 | 8 13 10 12 6 12 11 14 21 4 | 15 24 16 20 19 24 15 23 30 16 9 | 7 11 9 10 5 12 11 11 25 4 | 14 22 19 20 17 20 14 20 20 15 10 | 13 20 12 15 7 19 15 12 43 6 | 33 43 32 41 36 44 35 37 54 35 11 | 6 15 8 11 8 16 11 10 35 5 | 28 42 32 32 32 40 30 29 25 30 12E | 12 17 12 11 8 18 11 12 19 5 | 24 31 20 27 26 33 27 23 28 25 13 | 10 16 9 19 6 15 12 11 18 5 | 13 33 19 25 21 30 18 18 19 17 14 | 11 18 11 13 7 11 12 12 22 5 | 13 26 17 23 18 23 13 24 23 15 15 | 14 22 16 13 7 17 10 12 30 6 | 11 30 21 21 18 24 17 27 22 15 16E | 11 16 16 12 6 21 19 14 18 6 | 14 27 27 23 19 29 24 23 20 18 17 | 10 21 14 17 9 19 10 12 22 5 | 14 29 11 22 15 25 15 19 14 11 18 | 9 21 11 11 8 17 9 10 18 5 | 25 36 29 28 27 31 30 31 33 27 19 | 9 16 12 16 7 18 11 16 29 5 | 10 28 16 22 16 27 14 19 19 14 20 | 9 17 9 11 6 17 9 10 21 4 | 7 26 13 17 15 26 13 14 18 11 21 | 8 13 12 14 6 15 13 12 29 5 | 22 28 23 25 22 28 24 22 32 21 22 | 11 17 9 11 6 14 8 14 20 4 | 15 26 21 19 18 23 21 21 22 17 23 | 11 19 10 12 5 14 14 11 18 5 | 16 35 22 24 22 30 15 21 24 19 24 | 7 12 8 14 4 9 9 11 20 4 | 21 26 26 25 23 27 30 29 27 24 25 | 7 11 8 11 4 10 11 10 21 4 | 16 22 20 19 20 26 18 19 28 17 26 | 11 13 12 12 7 14 18 13 36 5 | 16 24 24 26 20 25 21 22 45 20 27 | 6 13 10 11 4 11 8 10 23 4 | 15 24 20 21 20 26 17 18 35 18 28E | 9 17 14 14 7 15 16 14 24 5 | 27 44 30 32 31 37 30 32 46 30 X29 | 14 22 13 15 13 23 15 16 --- 6 | 115 129 119 119 124 132 119 125 --- 121 30E | 16 18 14 13 8 20 26 15 22 6 | 45 45 37 44 41 37 57 51 49 43 31 | 11 18 12 18 10 16 14 13 21 5 | 13 29 15 24 19 27 13 21 19 14 X32E | 19 26 23 --- 28 --- 22 25 --- 11 | 71 76 74 --- 91 --- 82 91 --- 76 ------+---------------------------------------------------+---------------------------------------------------- RMS | 10 16 11 13 7 15 14 13 24 |T 24 35 27 28 28 32 28 31 29 26 WRMS | 9 16 12 13 6 15 13 11 23 |NE 22 33 26 28 26 32 25 28 27 24 MEDI | 10 17 11 12 7 15 13 12 22 |MD 19 29 23 24 22 27 24 24 28 20 Table 3.1463.6 GPS week: 1463 Day: 6 MJD: 54491.000 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 26 12 15 7 10 14 15 23 5 | 17 31 25 26 21 27 17 29 30 21 2 | 12 16 11 11 7 16 15 10 23 5 | 36 39 38 39 36 39 41 36 38 36 3 | 8 18 10 6 7 10 13 11 29 4 | 21 29 26 23 26 24 27 28 23 23 4 | 9 13 9 13 6 8 15 10 13 4 | 36 36 39 33 39 35 38 42 39 36 5E | 16 24 14 15 9 19 15 26 22 7 | 36 38 34 37 33 32 45 51 42 35 6 | 7 13 11 8 6 12 12 10 16 4 | 30 34 33 30 34 32 35 35 26 31 8 | 8 12 7 12 5 10 8 8 29 4 | 20 22 20 22 22 22 14 24 29 18 9 | 8 14 7 11 6 8 14 9 14 4 | 19 22 19 22 20 21 15 21 12 17 10 | 12 19 10 16 6 14 19 10 38 6 | 55 63 55 61 57 60 56 55 67 56 11 | 7 15 12 11 10 18 10 12 26 5 | 46 57 49 48 47 48 48 45 38 46 12E | 12 17 12 11 8 24 14 17 20 6 | 29 33 25 32 32 37 29 43 22 30 13 | 8 19 13 15 5 11 11 9 16 4 | 17 34 22 23 23 28 15 19 21 18 14 | 9 23 13 15 9 12 10 10 22 5 | 17 30 21 26 22 24 16 24 23 19 15 | 14 21 13 16 7 14 10 13 23 5 | 15 31 19 25 20 23 18 24 18 16 16E | 10 17 12 10 5 21 19 13 21 5 | 19 29 23 24 23 33 23 24 17 21 17 | 10 18 12 17 7 16 10 11 22 5 | 19 30 22 28 21 27 18 18 21 17 18 | 9 18 10 12 6 15 13 13 24 5 | 37 46 41 37 39 40 43 37 45 38 19 | 9 17 13 16 8 13 13 13 28 5 | 16 31 22 29 22 30 21 21 16 19 20 | 8 18 15 12 6 17 10 14 20 5 | 12 27 17 21 19 27 13 17 19 14 21 | 9 16 10 13 5 16 18 10 29 5 | 31 39 32 33 33 36 35 32 37 31 22 | 9 18 10 13 6 12 10 9 26 4 | 22 31 22 23 22 25 30 24 32 22 23 | 8 18 13 12 5 13 11 13 26 5 | 15 32 21 23 20 26 13 19 22 17 24 | 8 16 9 13 5 11 11 10 28 4 | 35 39 40 36 37 34 46 38 48 38 25 | 6 14 8 12 5 9 9 6 20 3 | 19 22 22 22 23 22 14 22 24 19 26 | 10 18 9 13 7 13 15 14 35 5 | 18 28 21 21 19 24 13 21 43 18 27 | 7 13 5 12 5 10 6 12 30 4 | 21 24 23 24 25 23 17 25 33 20 28E | 10 19 15 11 10 15 12 17 23 5 | 39 44 36 38 37 40 35 38 43 37 X29 | 14 23 16 17 14 24 13 14 --- 7 | 112 122 122 109 113 121 116 111 --- 115 30E | 16 24 17 18 11 18 37 17 29 8 | 45 43 38 42 41 37 66 53 56 44 31 | 12 24 13 16 9 17 14 15 17 5 | 16 31 16 24 20 27 16 20 20 16 X32 | 28 24 24 --- 36 --- 17 39 --- 14 | 81 86 80 --- 67 --- 82 73 --- 77 ------+---------------------------------------------------+---------------------------------------------------- RMS | 10 18 11 13 7 14 14 13 25 |T 30 38 33 32 32 34 32 34 31 31 WRMS | 9 18 11 13 7 14 12 10 24 |NE 30 39 33 32 32 33 31 33 30 30 MEDI | 9 18 12 13 7 13 13 12 23 |MD 21 32 25 26 25 28 27 28 29 22 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1463 GPS week: 1463 MJD: 54485.0-54491.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2968 |U 8 8 17 |U 12 13 47 |U 7 7 16 | emr | emr 2960 |U 13 10 35 |U 15 17 48 | 9 7 19 | esa | esa 2934 | 12 11 22 |U 12 14 43 |U 9 9 18 | gfz | gfz 2851 |U 12 10 36 |U 15 19 55 |U 11 11 24 | igr | igr 2964 | 10 10 30 | 14 19 53 | 8 9 18 | igs | igs 2963 | 11 10 31 | 13 16 50 | 8 10 19 | jpl | jpl 2857 |U 12 10 31 |U 12 17 45 | 8 6 16 | mit | mit 2976 |U 11 12 32 |U 16 17 55 |U 7 8 19 | 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 5.1463.0 GPS week: 1463 Day: 0 MJD: 54485.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2967 | 8 7 20 | 16 25 78 | 6 7 18 | emr | emr 2960 | 15 10 36 | 15 31 67 | 10 8 23 | esa | esa 2976 | 12 12 24 | 13 21 72 | 8 8 21 | gfz | gfz 2820 | 18 12 53 | 23 42 91 | 13 20 34 | igr | igr 2967 | 10 10 33 | 17 37 87 | 9 10 24 | igs | igs 2974 | 12 10 30 | 19 30 88 | 10 19 23 | jpl | jpl 2868 | 14 10 37 | 20 40 82 | 7 6 15 | mit | mit 2976 | 11 8 34 | 19 26 79 | 6 7 20 | Table 5.1463.1 GPS week: 1463 Day: 1 MJD: 54486.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2969 | 6 7 18 | 18 19 55 | 9 10 19 | emr | emr 2953 | 14 11 44 | 21 19 59 | 10 9 20 | esa | esa 2880 | 12 17 30 | 16 22 54 | 10 10 21 | gfz | gfz 2846 | 11 10 45 | 21 16 61 | 11 13 22 | igr | igr 2965 | 11 9 41 | 19 14 62 | 10 11 20 | igs | igs 2954 | 8 9 32 | 20 19 64 | 9 10 20 | jpl | jpl 2872 | 14 10 46 | 20 16 58 | 9 8 17 | mit | mit 2976 | 8 9 31 | 20 17 62 | 9 11 22 | Table 5.1463.2 GPS week: 1463 Day: 2 MJD: 54487.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2962 | 9 10 16 | 10 8 34 | 6 8 17 | emr | emr 2958 | 15 13 37 | 21 14 48 | 8 7 20 | esa | esa 2880 | 15 15 21 | 12 12 32 | 8 11 21 | gfz | gfz 2849 | 15 11 38 | 13 12 39 | 9 9 17 | igr | igr 2962 | 11 12 25 | 13 16 55 | 7 6 17 | igs | igs 2960 | 11 9 31 | 10 7 33 | 6 7 18 | jpl | jpl 2872 | 14 11 35 | 10 9 37 | 6 5 12 | mit | mit 2976 | 11 10 25 | 13 10 37 | 7 7 14 | Table 5.1463.3 GPS week: 1463 Day: 3 MJD: 54488.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2972 | 7 5 16 | 10 13 48 | 7 7 14 | emr | emr 2957 | 12 9 36 | 13 16 47 | 9 6 18 | esa | esa 2880 | 11 10 18 | 13 13 40 | 10 8 13 | gfz | gfz 2858 | 10 9 29 | 12 17 53 | 11 8 25 | igr | igr 2960 | 8 7 23 | 15 22 48 | 8 8 15 | igs | igs 2948 | 10 7 24 | 14 19 51 | 7 8 21 | jpl | jpl 2868 | 9 6 21 | 10 16 40 | 8 5 17 | mit | mit 2976 | 12 7 30 | 14 15 51 | 7 8 17 | Table 5.1463.4 GPS week: 1463 Day: 4 MJD: 54489.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2968 | 12 11 19 | 9 8 39 | 7 7 12 | emr | emr 2964 | 13 13 31 | 11 11 34 | 9 6 17 | esa | esa 2976 | 15 12 27 | 11 7 33 | 9 6 16 | gfz | gfz 2861 | 14 13 34 | 13 17 54 | 11 10 24 | igr | igr 2963 | 12 14 27 | 10 17 35 | 7 6 15 | igs | igs 2970 | 13 11 24 | 10 10 41 | 9 8 16 | jpl | jpl 2872 | 13 13 24 | 9 14 30 | 7 6 13 | mit | mit 2976 | 13 12 21 | 18 18 63 | 9 7 33 | Table 5.1463.5 GPS week: 1463 Day: 5 MJD: 54490.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2969 | 6 7 15 | 11 9 47 | 6 7 19 | emr | emr 2964 | 12 9 32 | 15 16 55 | 8 6 19 | esa | esa 2976 | 8 9 19 | 10 11 42 | 8 9 18 | gfz | gfz 2863 | 10 9 32 | 14 16 40 | 11 10 23 | igr | igr 2966 | 7 11 31 | 14 17 48 | 7 9 20 | igs | igs 2969 | 14 10 31 | 11 12 42 | 7 7 16 | jpl | jpl 2782 | 9 9 25 | 11 12 41 | 8 6 19 | mit | mit 2976 | 12 8 23 | 15 19 55 | 7 8 13 | Table 5.1463.6 GPS week: 1463 Day: 6 MJD: 54491.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2971 | 7 8 17 | 10 12 27 | 7 6 17 | emr | emr 2967 | 12 7 30 | 8 11 30 | 10 8 17 | esa | esa 2976 | 9 6 18 | 10 9 26 | 8 8 17 | gfz | gfz 2860 | 9 10 24 | 11 14 51 | 11 9 20 | igr | igr 2969 | 11 9 28 | 11 14 40 | 8 10 17 | igs | igs 2972 | 13 14 44 | 9 12 34 | 8 10 21 | jpl | jpl 2868 | 9 8 30 | 6 11 29 | 9 8 17 | mit | mit 2976 | 12 33 62 | 15 16 37 | 7 8 14 | 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 6.1463 GPS week: 1463 MJD: 54485.500-54491.500 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 8 7 -30 3 | -3 19 | 17 28 67 69 7 | 3 emr uuuuu | -9 5 54 -148 -8 | 53 57 | 30 28 145 120 13 | 4 esa uuuux | 21 4 -50 -12 -30 | 27 45 | 23 27 111 61 16 | 12 gfz uuuuu | 34 -1 57 -4 8 | 0 19 | 9 29 27 71 13 | 3 igr xxxxx | 22 7 88 -11 5 | 1 18 | 30 28 62 76 8 | 2 irf xxxxx | 1 10 3 9 -3 | 3 19 | 9 14 43 29 10 | 3 jpl uuuuu | 23 -18 13 69 -10 | 21 30 | 26 10 127 85 12 | 2 mit uuuuu | 6 27 -122 102 -12 | 2 20 | 24 38 65 176 9 | 4 ngs uuuuu | -62 14 80 25 5 | -4 12 | 38 59 109 69 11 | 2 sio uuuuu | -28 -138 -8 -34 1 | 2 17 | 25 41 68 110 7 | 3 Table 7.1463.0 GPS week: 1463 Day: 0 MJD: 54485.500 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 9 -31 -27 -7 | 0 16 emr uuuuu | -15 29 -162 -223 -19 | 60 61 esa uuuux | 4 -46 132 -16 -47 | 46 52 gfz uuuuu | 36 42 28 47 -14 | 1 16 igr xxxxx | 79 46 -43 23 -1 | 4 18 irf xxxxx | 13 31 -22 39 -15 | 9 16 jpl uuuuu | 40 -9 100 -90 8 | 24 32 mit uuuuu | 30 18 -135 335 -16 | 8 16 ngs uuuuu | -71 -14 69 13 23 | -4 13 sio uuuuu | -33 -94 -31 -122 4 | 6 18 Table 7.1463.1 GPS week: 1463 Day: 1 MJD: 54486.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -29 9 -18 -109 -5 | -3 21 emr uuuuu | 15 25 -17 -51 -24 | 57 60 esa uuuux | -2 30 -40 -9 -54 | 39 52 gfz uuuuu | 19 24 72 -125 -1 | -1 20 igr xxxxx | -1 30 108 68 -9 | 2 19 irf xxxxx | -11 2 -28 55 -11 | 5 20 jpl uuuuu | 56 -4 99 44 -1 | 22 32 mit uuuuu | -19 8 -217 306 -16 | 5 20 ngs uuuuu | -4 -55 104 36 16 | -6 14 sio uuuuu | -51 -150 85 -68 -8 | 4 19 Table 7.1463.2 GPS week: 1463 Day: 2 MJD: 54487.500 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 64 55 -40 12 | -7 20 emr uuuuu | 31 -24 -32 -84 -17 | 53 58 esa uuuux | 58 15 -12 -92 -37 | 32 50 gfz uuuuu | 37 11 10 -50 5 | -3 20 igr xxxxx | 11 -35 117 -155 10 | -1 19 irf xxxxx | -7 -1 -55 -25 -10 | 3 20 jpl uuuuu | -6 -21 -56 49 -2 | 20 30 mit uuuuu | -31 -45 -131 184 -22 | 3 21 ngs uuuuu | -51 31 144 35 4 | -6 14 sio uuuuu | -12 -119 45 -92 -1 | 1 18 Table 7.1463.3 GPS week: 1463 Day: 3 MJD: 54488.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -8 -11 -107 -32 4 | -6 20 emr uuuuu | -2 44 84 -44 -11 | 51 56 esa uuuux | 14 14 -186 -4 -26 | 26 46 gfz uuuuu | 29 3 79 -45 14 | -3 20 igr xxxxx | -2 5 97 63 3 | -1 19 irf xxxxx | 1 12 52 3 -7 | 1 19 jpl uuuuu | -7 -14 216 141 -14 | 20 30 mit uuuuu | -5 67 -168 -49 -17 | 1 21 ngs uuuuu | -31 -58 252 63 8 | -5 14 sio uuuuu | 9 -145 -79 76 -7 | 0 16 Table 7.1463.4 GPS week: 1463 Day: 4 MJD: 54489.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -2 19 103 -104 9 | -5 19 emr uuuuu | -2 -21 97 -53 -3 | 49 54 esa uuuux | -1 11 -177 106 -13 | 20 42 gfz uuuuu | 34 -44 62 40 24 | -3 20 igr xxxxx | 5 -23 148 -3 2 | 0 18 irf xxxxx | 4 17 -15 -7 2 | 0 19 jpl uuuuu | 12 -28 -48 137 -24 | 20 30 mit uuuuu | 22 41 -124 -119 -8 | -1 22 ngs uuuuu | -72 26 88 134 -7 | -3 12 sio uuuuu | -18 -90 -13 -166 1 | -1 17 Table 7.1463.5 GPS week: 1463 Day: 5 MJD: 54490.500 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 -20 21 93 9 | 0 17 emr uuuuu | -35 0 108 -228 7 | 51 56 esa uuuux | 37 22 8 -10 -15 | 18 42 gfz uuuuu | 35 -23 78 34 18 | 3 21 igr xxxxx | 12 9 75 -35 14 | 3 17 irf xxxxx | 11 -12 41 12 5 | 2 19 jpl uuuuu | 48 -19 -117 50 -22 | 23 29 mit uuuuu | 24 39 -24 55 -5 | 0 22 ngs uuuuu | -121 71 -93 -88 -5 | -1 8 sio uuuuu | -30 -202 37 -1 6 | 3 15 Table 7.1463.6 GPS week: 1463 Day: 6 MJD: 54491.500 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 -14 23 12 -1 | -1 16 emr uuuuu | -58 -18 301 -351 10 | 49 53 esa uuuux | 35 -19 -77 -58 -16 | 10 32 gfz uuuuu | 47 -18 71 74 12 | 4 21 igr xxxxx | 48 17 115 -39 13 | 3 16 irf xxxxx | -3 17 46 -14 11 | 1 17 jpl uuuuu | 13 -32 -107 153 -15 | 19 26 mit uuuuu | 19 57 -54 5 4 | -3 20 ngs uuuuu | -87 95 -2 -19 -4 | -3 7 sio uuuuu | -66 -170 -103 138 11 | 2 14