Date: Thu, 03 Jan 2008 08:57:58 +0100 To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-15814] Wk 1458 IGS Final Orbits [Resubmission] User-Agent: Heirloom mailx 12.3 7/15/07 Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20080103075758.B40CD50984@kg20.gfz-potsdam.de> From: igsacc@gfz-potsdam.de (Gerd Gendt3) Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 02 Jan 23:58:02 PST 2008 Message Number 15814 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1458 (Dec 16, 2007 - Dec 22, 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: igs1458[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1458[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1458[0-6].cls IGS GPS clock combination summary report. igs14587.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14587.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 | SCH2 0 | MIT | 30 31 32 IRKT 0 | NGS | 7 1 | ALL | 7 1 | EMR | FAIR YAR2 1 | ESA | 11 15 LPGS SUTM TIDB TIXI URUM YAR2 1 | GFZ | 21 1 | MIT | 1 2 3 4 5 6 8 9 10 11 12 13 14 15 16 17 18 19 20 1 | MIT | 21 22 23 24 25 26 27 28 30 31 32 NRIL 2 | COD | AMC2 2 | ESA | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 2 | ESA | 21 22 23 24 25 26 27 28 30 31 DRAO FAIR HARB IISC 2 | ESA | KOUR MKEA OHI2 SCUB SUTH SUTM TIXI 2 | MIT | 32 FAIR GRAZ MCM4 NRIL TLSE 3 | EMR | FAIR 3 | ESA | SUTM VILL 3 | JPL | 9 3 | MIT | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 3 | MIT | 21 22 23 24 25 26 27 28 30 31 32 4 | COD | 32 MCM4 4 | ESA | BILI SUTM TIXI VILL YELL 4 | MIT | 7 11 12 13 30 TIXI 5 | ESA | MATE 5 | GFZ | WTZR 5 | MIT | 7 12 27 CHUR 6 | EMR | 32 YELL 6 | ESA | YELL 6 | MIT | 3 7 16 18 23 ALBH 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 | .1 .0 .3 -7 -4 3 -.08 EMR | 1.4 -1.9 .1 3 -13 29 .25 ESA | 2.4 4.4 -3.3 -7 -9 -12 -.60 GFZ | .5 -.1 .9 -11 -10 5 -.25 JPL | .2 3.4 2.7 -8 -17 2 .15 MIT | -1.3 2.2 2.3 7 1 0 -.24 NGS | 3.7 -.2 -3.9 -10 -82 15 -.83 SIO | -3.3 8.0 7.6 96 25 12 .35 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 1.1458.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1458.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 2.1458.[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 3.1458.[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 5.1458.0-6). 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 1458 summary. (Dec 16, 2007 - Dec 22, 2007) Table 1.1458.a GPS week: 1458 MJD: 54450.000-54456.000 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 177| 0 1 -2 0 -5 -19 -.20 14 13 | -349 -125 45 82 | 1 0 1 9 11 29 .02 | 494 1027 emr 69| 2 -1 2 14 -19 -8 .41 16 16 | 1694 363 59 91 | 1 1 0 49 14 27 .03 | 661 1298 esa 64| 0 0 -1 36 -57 -28 .28 26 25 | 1683 469 55 155 | 2 2 2 44 22 51 .04 | 624 1337 gfz 174| -1 0 2 24 10 -6 -.12 12 12 | 5155 213 29 94 | 0 0 1 17 15 95 .03 | 14036 669 igr n/a| 0 0 0 -16 -15 -30 .02 7 7 | -4218 261 30 65 | 0 0 1 11 17 30 .03 | 651 1331 jpl 119| 0 0 2 17 43 33 .49 13 13 | 4773 323 32 69 | 1 0 1 23 20 23 .04 | 680 1262 mit 267| -1 -2 -3 -27 -101 -1 -.51 19 17 | -1995 -1114 60 153 | 1 1 1 45 30 33 .03 | 4109 3413 ngs 191| 1 0 0 22 112 2 -.34 17 13 | 1494 753 2396 3995 | 1 1 1 30 15 20 .05 | 4568 3137 sio 94| 0 0 -4 -213 -89 4 -.03 27 26 | --- --- --- --- | 3 1 1 18 13 45 .09 | --- --- Table 1.1458.b GPS week : 1458 MJD: 54450.000-54456.000 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: mm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------+------------------------------------+------------------------------------------ 1 | 6 6 6 6 6 7 6 | 2 | 9 7 7 8 8 7 7 | 3 | 7 7 8 6 6 8 8 | 4 | 6 5 6 6 7 6 7 | 5 | 5 5 5 5 6 5 5 | 6 | 5 4 5 4 6 5 5 | 7 | 7 10 8 10 7 7 8 | 8E | 8 7 8 8 7 8 8 | 9E | 7 7 8 8 8 8 9 | 10E | 7 7 6 6 6 8 8 | 11 | 7 8 6 7 7 8 8 | 12 | 7 7 7 7 6 7 7 | 13 | 7 7 7 7 7 7 7 | 14 | 7 6 6 6 6 6 7 | 15 | 8 8 8 7 8 9 8 | 16 | 7 7 7 7 7 8 8 | 17 | 6 6 6 6 6 7 6 | 18E | 7 6 6 6 6 6 5 | 19 | 5 5 5 5 5 6 7 | 20E | 6 6 5 5 6 7 6 | 21 | 6 6 6 6 6 7 6 | 22E | 6 5 6 6 6 6 5 | 23 | 7 7 6 6 7 7 7 | 24 | 6 5 5 5 6 6 5 | 25E | 9 8 8 8 8 8 7 | 26 | 7 6 7 6 6 7 6 | 27E | 9 8 9 8 9 8 8 | 28 | 8 8 7 7 7 7 7 | 30 | 5 4 4 5 5 5 5 | 31E | 6 6 6 5 6 7 7 | 32E | 21 11 12 13 16 15 16 | 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 2.1458.0 GPS week: 1458 Day: 0 MJD: 54450.000 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 177| 1 1 -2 2 -8 -32 -.19 15 13 | -73 -557 41 80 | 42 -23 | emr 69| 2 0 2 -23 -19 -19 .38 14 14 | 2171 -2081 61 93 | 2 -16 | esa 64| 0 2 0 16 -98 -26 .23 23 23 | 2144 -2034 52 148 | 10 94 | gfz 174| 0 0 1 37 20 40 -.12 12 12 | 252 -667 26 86 | -13 -57 | igr n/a| 0 -1 -1 -12 -14 -59 .03 7 7 | -3154 -2317 27 67 | -7 -27 | jpl 119| -1 0 2 -16 38 16 .43 14 14 | 5394 -2186 31 73 | 52 -78 | mit 267| -3 0 -3 37 -122 -18 -.53 22 20 | -4912 -7543 52 132 | -44 60 | ngs 191| 0 -1 0 6 125 -12 -.34 16 11 | 5070 5259 2402 4109 | 58 46 | sio 94| -1 0 -7 -208 -69 5 -.02 28 29 | --- --- --- --- | 106 5 | Table 2.1458.1 GPS week: 1458 Day: 1 MJD: 54451.000 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 177| 1 0 -2 7 -3 -47 -.17 15 14 | 94 -1567 54 85 | 7 -26 | emr 69| 1 0 3 -36 -27 -59 .43 15 15 | 272 -193 45 71 | 35 -8 | esa 64| 0 0 0 32 -57 -30 .27 26 25 | 353 -139 60 146 | 57 24 | gfz 174| 0 0 3 27 -1 152 -.07 12 12 | 71 -660 25 78 | 12 -37 | igr n/a| 0 0 0 0 -6 -74 .00 6 6 | -5273 -258 29 67 | 40 -27 | jpl 119| -1 2 0 27 33 10 .54 13 13 | 3378 164 37 78 | 32 -59 | mit 267| -2 -1 -3 -53 -86 -58 -.52 20 17 | -9742 1747 52 132 | 19 38 | ngs 191| 2 0 -1 61 100 -28 -.44 15 12 | 10265 -4829 2202 4108 | -30 91 | sio 94| -4 -2 -4 -216 -83 -46 .01 29 26 | --- --- --- --- | 73 19 | Table 2.1458.2 GPS week: 1458 Day: 2 MJD: 54452.000 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 177| 1 0 -1 3 -7 -48 -.18 13 12 | -154 -904 33 69 | 35 -51 | emr 69| 1 -2 2 -30 -35 -17 .46 16 16 | 1780 1230 68 104 | 8 -15 | esa 64| 1 4 -2 77 -38 41 .29 25 23 | 1735 1376 49 121 | 77 40 | gfz 174| -1 0 1 34 23 62 -.13 13 13 | 36980 755 31 109 | 5 -48 | igr n/a| 0 0 0 -26 -12 -30 .03 7 6 | -4177 1125 31 67 | 18 -13 | jpl 119| 0 1 2 -17 31 8 .55 14 14 | 4767 1236 33 75 | 27 -96 | mit 267| 0 -1 -4 19 -99 -10 -.53 19 16 | 2900 -3961 55 131 | -18 54 | ngs 191| 0 -2 0 24 105 -4 -.29 16 12 | -2797 3040 2579 4178 | -46 84 | sio 94| 1 -1 -3 -248 -99 -63 -.14 29 27 | --- --- --- --- | 108 68 | Table 2.1458.3 GPS week: 1458 Day: 3 MJD: 54453.000 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 177| 0 1 -1 3 3 -30 -.21 15 14 | -919 1097 46 75 | 7 -25 | emr 69| 3 0 2 1 -28 0 .41 16 16 | 1629 573 52 74 | 1 -3 | esa 64| 0 -1 -1 49 -50 33 .31 23 23 | 1595 791 53 133 | 6 68 | gfz 174| -2 0 2 21 11 -50 -.16 12 12 | -512 938 26 77 | -24 -41 | igr n/a| 0 0 1 -34 -36 -23 .02 6 6 | -4610 713 28 58 | 63 -13 | jpl 119| -1 0 1 25 18 28 .51 12 12 | 4627 634 25 53 | 1 -59 | mit 267| 0 -1 -5 -16 -48 0 -.53 18 16 | -236 -169 37 163 | 17 60 | ngs 191| 1 3 1 -13 86 0 -.30 18 13 | -1066 1337 2569 4094 | 68 46 | sio 94| 1 0 -4 -206 -76 46 -.11 28 28 | --- --- --- --- | 107 34 | Table 2.1458.4 GPS week: 1458 Day: 4 MJD: 54454.000 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 177| 0 1 -4 -7 10 -12 -.20 14 14 | -313 159 46 83 | 23 -21 | emr 69| 0 -3 2 54 -4 7 .40 16 16 | 1850 2077 68 98 | -54 -14 | esa 64| -1 -1 -5 -33 -42 -56 .26 26 26 | 1828 2234 60 183 | 10 1 | gfz 174| -1 0 5 45 6 -44 -.11 12 12 | -44 -25 38 103 | -10 -21 | igr n/a| 0 0 -2 -13 -23 -29 .01 7 7 | -4250 1889 33 60 | 24 -33 | jpl 119| 0 1 3 28 39 53 .50 12 12 | 5018 1810 33 68 | 30 -68 | mit 267| 0 -1 -5 -36 -96 0 -.50 18 17 | -967 1203 62 149 | 1 93 | ngs 191| 0 0 0 -15 116 20 -.30 17 15 | -122 -224 1843 3032 | 56 -28 | sio 94| 1 1 -4 -190 -102 -2 -.08 26 24 | --- --- --- --- | 77 29 | Table 2.1458.5 GPS week: 1458 Day: 5 MJD: 54455.000 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 177| -1 1 -2 -19 -5 -2 -.20 16 14 | 74 -337 52 91 | 44 -27 | emr 69| 2 -1 3 50 -25 30 .39 17 17 | 2230 662 66 101 | -71 -23 | esa 64| 0 0 0 101 -37 -57 .35 28 27 | 2202 690 62 170 | 20 20 | gfz 174| -2 0 1 0 27 -120 -.09 12 12 | -240 497 31 111 | -5 -26 | igr n/a| 0 1 -1 -22 14 20 .05 8 8 | -3833 576 35 75 | 22 -61 | jpl 119| 0 0 2 38 68 64 .45 14 14 | 5372 522 31 69 | 3 -118 | mit 267| -1 -3 -2 -48 -143 41 -.47 20 17 | -150 -262 78 176 | 24 64 | ngs 191| 2 0 -3 52 129 31 -.37 21 16 | 15 -263 2875 4617 | -23 21 | sio 94| 4 0 -1 -223 -100 41 .03 26 25 | --- --- --- --- | 69 45 | Table 2.1458.6 GPS week: 1458 Day: 6 MJD: 54456.000 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 177| 0 1 -1 2 -27 35 -.24 14 13 | -1157 1232 45 93 | 12 -3 | emr 69| 3 -2 1 88 3 -3 .39 16 16 | 1931 275 58 97 | -83 -44 | esa 64| -4 1 0 11 -75 -102 .29 27 25 | 1930 366 55 189 | 72 -3 | gfz 174| -2 0 2 3 -18 -82 -.14 12 12 | -422 653 27 94 | -16 -19 | igr n/a| 0 0 -1 -8 -30 -18 -.03 8 8 | -4234 99 31 67 | 13 -9 | jpl 119| 0 0 2 33 74 50 .46 13 13 | 4859 84 34 67 | 3 -89 | mit 267| -2 -4 -2 -97 -116 31 -.48 19 16 | -860 1187 88 188 | 38 47 | ngs 191| 2 2 -1 39 126 13 -.35 17 13 | -904 955 2302 3829 | 31 53 | sio 94| 3 0 -5 -198 -98 48 .11 25 23 | --- --- --- --- | 35 48 | 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 3.1458.0 GPS week: 1458 Day: 0 MJD: 54450.000 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 10 24 11 6 14 18 10 41 6 | 15 25 28 20 19 21 21 21 39 18 X2 | 16 --- 50 17 9 16 19 14 31 9 | 25 --- 51 41 33 36 28 29 34 31 3 | 5 11 13 20 7 9 11 14 51 6 | 24 28 25 25 23 17 31 24 51 22 4 | 11 13 26 9 6 10 19 14 24 5 | 13 19 28 17 17 17 16 26 20 15 5 | 7 14 22 9 5 11 16 11 13 4 | 23 27 37 21 23 24 25 28 24 23 6 | 7 9 21 6 4 10 14 9 24 4 | 33 36 34 31 32 35 35 38 42 34 X7 | 11 13 28 15 8 --- 13 15 --- 7 | 37 43 27 37 32 --- 36 38 --- 36 8E | 19 14 21 12 8 16 22 27 34 7 | 20 27 28 22 20 28 33 35 26 20 9E | 19 15 29 12 8 13 28 18 32 7 | 37 36 34 34 35 37 48 38 40 34 10 | 16 14 32 12 10 12 24 15 20 6 | 106 107 102 108 102 103 114 107 109 106 11 | 13 19 27 15 11 14 19 18 19 6 | 28 39 38 32 31 32 24 25 26 28 12 | 18 14 23 15 5 15 22 15 27 6 | 24 31 28 29 24 28 25 26 24 23 13 | 15 18 18 11 8 13 22 16 28 6 | 27 43 39 33 36 38 33 30 27 30 14 | 14 14 18 15 6 15 26 16 25 6 | 20 34 29 26 25 29 29 29 31 23 15 | 22 17 24 12 8 18 26 17 29 7 | 29 38 32 32 32 32 29 32 30 29 16 | 17 18 15 13 6 13 25 19 24 6 | 18 35 29 28 24 29 25 25 24 22 17 | 7 9 23 8 8 15 19 15 31 5 | 44 46 47 43 44 9 42 47 50 44 18E | 21 14 22 8 8 16 22 14 22 6 | 30 39 36 31 33 37 38 34 39 33 19 | 6 11 13 11 9 14 17 10 34 5 | 37 36 36 36 37 21 40 37 42 36 20E | 11 17 16 12 7 15 16 13 21 5 | 15 26 27 20 20 25 14 26 21 19 21 | 14 12 25 11 7 13 21 14 24 6 | 28 40 46 39 38 37 27 35 32 33 22E | 11 16 15 12 7 12 18 16 13 5 | 14 28 21 20 22 21 17 27 19 18 23 | 14 20 23 14 8 14 20 18 22 6 | 21 39 41 31 32 34 25 28 31 26 24 | 10 11 28 10 4 11 21 11 22 5 | 16 23 28 20 18 20 23 20 22 18 25E | 22 14 28 18 9 17 36 20 43 9 | 20 30 41 22 22 32 38 24 36 23 26 | 15 9 27 11 7 13 22 15 33 6 | 20 22 32 20 20 19 21 21 34 17 27E | 24 14 22 15 9 19 27 27 35 8 | 34 43 42 35 35 42 48 41 56 36 28 | 17 17 28 13 6 19 25 18 29 7 | 25 42 45 30 30 38 31 26 30 27 30 | 7 12 21 9 5 10 14 13 16 4 | 37 39 42 34 36 37 34 40 32 36 31E | 12 12 21 12 5 13 23 14 23 5 | 26 33 32 28 27 33 30 31 34 27 X32 | 24 54 --- --- 37 --- 24 33 --- 21 | 46 72 --- --- 61 --- 54 61 --- 53 ------+---------------------------------------------------+---------------------------------------------------- RMS | 15 14 23 12 7 14 22 16 28 |T 28 37 36 31 31 31 33 33 35 30 WRMS | 13 14 23 12 7 14 20 11 29 |NE 30 39 38 33 33 31 33 34 35 31 MEDI | 14 14 23 12 7 14 21 15 25 |MD 25 36 34 30 31 32 30 29 32 27 Table 3.1458.1 GPS week: 1458 Day: 1 MJD: 54451.000 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 11 24 12 4 13 13 11 46 6 | 19 22 25 19 19 27 19 21 37 17 2 | 17 18 22 16 6 14 20 16 24 6 | 20 36 39 31 23 29 24 25 24 23 3 | 8 14 32 13 6 10 10 12 50 6 | 23 27 30 20 25 21 28 21 54 22 4 | 10 12 26 10 8 10 15 12 28 5 | 14 22 29 17 20 19 26 26 33 18 5 | 9 10 36 10 5 10 14 13 14 5 | 20 21 40 21 21 20 22 25 29 20 6 | 7 12 14 6 5 9 12 14 22 4 | 25 31 30 30 28 31 34 32 38 29 X7 | 14 42 24 11 13 --- 14 18 --- 10 | 28 51 27 25 26 --- 35 30 --- 29 8E | 18 14 38 11 7 14 21 23 27 7 | 20 28 34 26 22 24 37 38 26 24 9E | 21 18 20 13 6 14 24 18 27 7 | 25 30 33 25 26 28 47 40 35 29 10E | 13 15 26 11 10 13 28 16 23 6 | 47 46 56 50 52 45 44 58 49 47 11 | 13 17 48 16 9 11 21 17 28 7 | 23 38 37 28 24 27 26 23 26 21 12 | 17 14 23 16 6 17 24 18 26 7 | 24 35 42 37 29 36 25 30 29 28 13 | 16 16 23 17 6 12 25 16 29 6 | 23 36 38 30 24 33 31 20 31 24 14 | 13 15 25 14 4 15 19 14 30 6 | 20 33 31 27 24 32 23 24 25 22 15 | 24 18 20 10 7 16 22 16 36 7 | 26 34 33 30 26 32 27 26 35 25 16 | 18 18 21 16 7 14 23 17 21 6 | 17 35 31 28 25 31 24 22 29 22 X17 | 6 17 26 10 10 --- 14 13 30 6 | 19 28 28 19 21 --- 19 24 35 21 18E | 13 17 22 7 4 17 16 12 33 6 | 24 36 29 26 25 34 20 31 34 26 19 | 5 10 26 10 5 10 14 10 33 5 | 23 23 29 17 21 20 27 27 30 21 20E | 13 17 25 10 7 10 13 14 22 5 | 14 27 29 19 17 23 16 17 23 15 21 | 12 15 19 14 5 11 22 12 23 5 | 21 35 32 29 27 31 29 25 24 24 22E | 10 14 23 9 7 15 15 14 14 5 | 21 32 25 25 24 32 23 28 23 24 23 | 16 20 23 13 7 11 19 16 28 6 | 16 36 33 26 20 28 19 18 22 19 24 | 11 12 24 9 6 12 19 12 19 5 | 17 24 35 22 21 25 19 24 22 20 25E | 20 14 27 14 7 15 32 17 29 7 | 18 27 33 23 21 29 43 27 34 23 26 | 13 11 22 12 5 13 22 13 36 6 | 19 20 29 21 19 20 19 24 30 17 27E | 23 15 31 13 5 18 27 24 30 8 | 32 40 38 35 36 39 48 47 42 36 28 | 18 16 38 14 7 14 24 18 33 7 | 19 37 43 30 24 33 28 27 27 24 30 | 8 12 22 11 4 10 9 10 11 4 | 32 36 43 34 34 36 35 34 37 34 31E | 12 14 16 15 8 13 14 11 26 5 | 37 41 41 39 39 42 37 41 39 38 X32 | 15 24 --- --- 21 --- 17 19 --- 11 | 41 66 --- --- 45 --- 43 43 --- 46 ------+---------------------------------------------------+---------------------------------------------------- RMS | 15 15 26 12 6 13 20 15 29 |T 23 33 34 26 26 29 28 28 31 25 WRMS | 14 15 25 12 6 13 17 12 26 |NE 22 33 33 25 24 27 26 25 30 23 MEDI | 13 15 24 12 6 13 19 14 28 |MD 21 34 33 26 24 29 27 26 30 24 Table 3.1458.2 GPS week: 1458 Day: 2 MJD: 54452.000 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 13 23 13 5 12 11 11 47 6 | 22 25 35 25 22 24 25 25 47 22 2 | 13 16 25 16 6 13 21 16 28 6 | 25 33 34 35 27 34 27 27 37 28 3 | 7 14 62 11 5 11 12 14 46 8 | 24 26 57 22 20 23 29 26 52 22 4 | 9 13 24 10 8 11 21 14 32 5 | 19 23 33 20 21 20 24 26 35 20 5 | 6 9 28 9 6 10 12 13 19 4 | 25 27 44 26 23 22 27 28 35 26 6 | 6 12 20 11 6 10 12 13 20 4 | 26 30 27 27 25 28 34 33 33 28 X7 | 13 21 29 14 11 --- 8 23 --- 8 | 32 32 39 24 26 --- 38 31 --- 28 8E | 17 17 23 11 8 18 18 28 37 7 | 23 28 27 27 24 29 31 35 36 22 9E | 19 20 20 13 8 15 28 20 34 7 | 33 36 34 31 31 33 45 38 45 32 10E | 9 15 23 11 7 13 24 20 23 6 | 42 43 47 43 43 40 47 47 44 42 11 | 11 15 29 17 9 11 17 16 24 6 | 28 33 46 33 26 29 30 30 40 26 12 | 16 15 20 15 6 15 21 18 26 6 | 26 35 30 33 26 30 26 34 35 26 13 | 13 19 32 15 8 12 22 15 23 6 | 25 38 35 28 25 31 33 26 36 24 14 | 13 18 19 14 6 12 19 11 27 6 | 23 33 34 26 24 32 27 25 31 24 15 | 18 20 28 12 8 15 23 15 38 7 | 24 33 29 27 24 28 26 25 30 23 16 | 15 16 18 16 4 17 23 18 31 7 | 24 33 30 30 24 35 23 32 25 24 X17 | 6 15 16 7 15 --- 15 16 30 5 | 28 36 27 30 30 --- 33 35 43 31 18E | 13 19 18 8 7 18 18 14 19 6 | 21 31 28 25 23 32 23 23 27 23 19 | 5 12 19 6 6 10 11 14 31 4 | 31 27 31 28 28 24 35 35 40 29 20E | 9 15 20 12 6 12 10 14 23 5 | 20 29 30 22 20 26 20 22 31 20 21 | 11 17 20 13 8 13 15 14 23 5 | 27 38 45 37 32 35 27 33 33 30 22E | 12 16 18 12 4 17 14 11 16 5 | 21 27 29 26 20 26 23 23 29 22 23 | 14 22 20 13 8 13 17 17 23 6 | 24 40 32 31 28 33 26 29 31 26 24 | 9 13 25 11 4 11 16 7 21 5 | 22 25 30 26 24 24 26 31 28 24 25E | 20 16 22 15 10 17 32 20 26 7 | 20 32 36 25 22 33 38 26 35 23 26 | 11 13 25 11 7 13 21 16 38 6 | 21 25 27 22 21 23 27 25 39 20 27E | 23 18 25 14 8 20 28 26 33 8 | 33 40 38 36 31 42 43 35 36 32 28 | 15 16 22 13 7 17 22 18 27 6 | 28 37 36 31 27 34 31 29 32 27 30 | 6 9 23 9 5 9 10 11 13 4 | 28 32 35 26 26 27 30 31 32 28 31E | 11 20 14 12 6 14 17 11 26 5 | 23 35 24 27 25 32 31 29 28 25 X32 | 15 26 --- --- 26 --- 24 19 --- 12 | 47 60 --- --- 62 --- 59 60 --- 52 ------+---------------------------------------------------+---------------------------------------------------- RMS | 13 16 25 13 7 14 19 16 29 |T 26 32 34 28 26 29 31 30 35 26 WRMS | 12 16 23 13 6 14 16 12 27 |NE 26 32 35 27 26 28 30 30 35 26 MEDI | 12 16 22 12 7 13 18 15 26 |MD 25 33 33 27 25 29 29 29 35 26 Table 3.1458.3 GPS week: 1458 Day: 3 MJD: 54453.000 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 13 5 9 13 13 37 5 | 16 23 32 21 17 21 19 19 37 17 2 | 16 28 39 15 7 11 19 18 28 7 | 23 44 43 36 27 30 23 28 28 27 3 | 7 10 16 9 7 7 10 19 46 5 | 25 25 23 20 21 17 28 20 49 22 4 | 13 15 26 8 6 7 14 14 29 5 | 14 20 40 23 19 22 24 21 35 18 5 | 10 9 37 10 4 7 12 11 15 5 | 18 21 41 21 19 20 26 25 22 20 6 | 7 10 13 7 4 7 12 13 23 4 | 28 32 33 31 28 32 37 34 40 31 X7 | 15 17 51 14 9 --- 11 19 --- 9 | 31 40 44 34 30 --- 39 45 --- 35 8E | 19 15 28 10 5 16 16 29 33 7 | 19 24 31 23 18 25 26 29 29 18 9E | 20 16 23 10 8 13 26 25 31 7 | 31 30 28 30 28 28 38 38 39 28 10E | 11 14 22 10 9 10 19 20 20 5 | 34 35 40 37 34 32 39 41 28 33 11 | 13 22 34 15 9 10 24 15 28 7 | 23 37 44 32 26 25 19 21 27 23 12 | 18 14 21 14 5 13 19 20 26 6 | 20 31 29 31 25 30 27 24 26 23 13 | 16 19 19 14 6 12 22 17 30 6 | 19 40 37 30 27 32 28 26 31 25 14 | 15 17 19 14 4 11 19 19 18 6 | 22 32 35 27 24 30 23 29 22 24 15 | 19 19 23 11 9 12 19 19 39 7 | 25 32 29 32 27 28 27 28 31 25 16 | 16 17 18 13 4 14 25 21 29 7 | 21 36 38 35 27 36 25 29 27 26 X17 | 8 11 32 6 10 --- 15 13 29 6 | 35 38 44 38 35 --- 35 37 47 37 18E | 15 17 12 8 6 16 15 14 23 5 | 24 33 25 27 22 32 21 25 27 25 19 | 10 11 14 6 4 15 9 14 21 4 | 34 30 33 33 32 26 34 32 38 31 20E | 10 14 12 10 7 12 12 15 21 5 | 13 28 27 22 21 25 21 19 27 18 21 | 12 14 23 13 5 11 14 15 23 5 | 19 30 36 28 24 27 16 22 24 21 22E | 13 18 17 11 6 13 15 15 15 5 | 16 28 24 25 19 24 18 23 21 19 23 | 16 20 12 14 6 12 19 19 22 6 | 14 37 29 27 24 30 23 20 27 21 24 | 9 11 25 11 4 8 19 15 18 5 | 15 19 26 20 17 18 23 26 22 18 25E | 19 15 28 13 6 16 29 19 28 7 | 19 31 36 27 22 34 32 24 28 23 26 | 13 11 27 11 8 9 16 16 41 6 | 20 21 31 21 22 22 28 26 33 20 27E | 25 15 25 15 7 17 26 26 31 8 | 41 46 49 43 40 46 41 50 48 40 28 | 19 15 27 13 6 13 19 20 28 6 | 21 37 37 31 26 33 26 28 28 25 30 | 7 10 24 10 3 7 14 10 17 4 | 43 43 53 43 42 43 46 41 47 43 31E | 12 15 13 10 5 13 15 13 22 5 | 31 34 32 34 30 34 35 32 30 31 X32 | 21 19 --- --- 40 --- 14 33 --- 13 | 76 85 --- --- 85 --- 89 87 --- 82 ------+---------------------------------------------------+---------------------------------------------------- RMS | 15 16 23 12 6 12 18 18 28 |T 25 33 34 29 27 28 30 30 31 27 WRMS | 14 16 23 12 6 12 16 13 28 |NE 25 34 36 29 28 27 30 30 32 27 MEDI | 13 15 23 11 6 12 16 17 28 |MD 22 32 33 30 26 28 27 28 28 25 Table 3.1458.4 GPS week: 1458 Day: 4 MJD: 54454.000 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 14 21 15 6 12 14 16 37 6 | 20 28 28 27 20 23 25 25 38 21 X2 | 13 --- 35 17 5 11 22 14 28 7 | 21 --- 35 34 21 26 29 19 29 23 3 | 8 10 22 13 9 8 10 14 46 6 | 27 27 37 21 25 22 29 26 50 25 4 | 15 14 22 9 6 9 22 18 33 6 | 17 25 31 20 19 22 32 23 38 20 5 | 8 11 38 10 4 10 13 15 15 5 | 23 26 42 26 22 21 26 30 26 24 6 | 9 9 35 8 7 11 12 16 25 5 | 31 34 44 27 27 32 38 25 40 30 X7 | 11 13 31 10 7 --- 14 21 --- 7 | 35 36 35 34 30 --- 35 33 --- 33 X8E | 21 16 17 10 7 13 21 --- 26 7 | 21 26 26 22 20 27 33 --- 35 22 X9E | 21 19 24 12 7 14 28 --- 29 8 | 31 29 36 26 26 27 41 --- 36 27 10E | 15 15 22 11 8 16 21 19 18 6 | 32 39 43 38 34 35 42 39 30 34 11 | 14 20 29 17 11 11 15 20 26 6 | 26 35 39 31 29 25 27 29 34 26 12 | 17 15 24 13 3 13 18 20 23 6 | 23 33 33 35 26 29 26 33 29 26 13 | 15 19 25 13 6 11 19 15 32 6 | 22 37 39 30 25 31 27 22 28 24 14 | 16 17 20 12 5 13 18 18 19 6 | 21 35 35 29 23 29 24 30 26 24 X15 | 17 21 27 12 9 --- 18 15 30 7 | 28 37 33 34 30 --- 31 30 40 29 16 | 17 19 23 13 5 15 28 16 26 7 | 22 37 34 30 26 33 28 28 28 25 X17 | 9 12 30 8 14 --- 13 14 22 6 | 29 35 33 29 29 --- 33 33 35 31 18E | 16 17 25 7 6 14 18 13 26 6 | 24 34 32 26 24 32 20 24 25 24 19 | 11 14 23 9 7 13 11 16 16 5 | 37 33 30 31 33 27 35 34 35 32 20E | 12 14 26 10 7 15 12 17 22 5 | 19 27 29 23 20 27 24 21 24 20 21 | 14 17 21 13 6 11 20 16 25 6 | 21 37 32 31 26 32 20 24 29 24 22E | 15 18 14 10 9 13 17 18 20 5 | 25 33 27 27 31 31 29 33 32 26 23 | 15 22 25 11 6 12 18 17 25 6 | 19 38 29 26 23 30 24 20 26 22 24 | 10 12 34 10 6 7 17 13 19 5 | 21 25 39 24 22 22 26 26 25 22 25E | 20 18 25 12 7 14 34 22 24 8 | 24 33 30 30 25 36 39 24 36 26 26 | 15 13 31 10 8 10 16 17 31 6 | 26 26 38 29 27 25 31 27 38 26 X27E | 25 17 20 15 9 13 32 --- 30 8 | 46 52 55 51 47 56 60 --- 59 51 28 | 19 17 29 15 9 13 18 21 25 7 | 21 37 35 34 27 30 24 32 29 26 30 | 9 10 26 8 5 9 14 10 13 4 | 30 32 34 30 31 33 35 35 28 31 31E | 15 19 13 11 4 17 13 15 16 5 | 20 36 26 26 24 31 25 26 26 24 X32E | 20 32 --- --- 39 --- 19 37 --- 16 | 74 84 --- --- 93 --- 76 87 --- 76 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 16 26 12 7 12 18 17 26 |T 26 34 34 29 28 29 32 29 32 28 WRMS | 14 16 26 12 7 12 17 15 24 |NE 24 32 35 29 25 27 28 27 32 25 MEDI | 15 16 25 11 7 13 18 16 25 |MD 24 34 34 29 26 29 29 27 30 26 Table 3.1458.5 GPS week: 1458 Day: 5 MJD: 54455.000 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 10 25 14 8 13 17 16 40 6 | 18 23 29 25 20 21 27 23 37 19 2 | 16 22 28 15 7 12 20 21 30 7 | 19 37 41 30 24 31 26 21 28 23 X3 | 9 13 21 12 8 --- 15 21 48 7 | 21 22 22 21 20 --- 26 21 56 20 4 | 12 16 28 11 4 11 21 12 27 6 | 18 24 36 24 20 20 31 22 29 20 5 | 10 10 29 8 7 9 13 18 17 5 | 19 26 34 22 21 19 26 28 27 21 6 | 7 10 25 8 16 10 13 24 23 5 | 30 31 40 29 34 32 38 36 33 32 X7 | 11 11 --- 14 15 --- 9 20 --- 6 | 27 24 --- 22 25 --- 32 32 --- 25 8E | 22 19 23 11 7 19 17 27 33 7 | 17 32 27 26 20 25 26 37 33 21 9E | 23 16 28 13 10 14 28 23 28 8 | 26 31 31 26 27 26 42 42 28 26 10E | 15 16 41 12 13 17 24 31 21 8 | 27 33 43 31 32 28 41 45 36 29 X11 | 14 24 31 15 8 --- 16 21 29 8 | 23 33 34 29 23 --- 23 21 30 20 12 | 16 13 23 14 7 12 18 21 31 6 | 20 30 37 30 24 26 23 29 30 23 13 | 15 22 38 17 9 13 16 21 23 7 | 18 35 37 28 24 27 20 22 27 20 14 | 16 16 26 12 5 14 19 18 21 6 | 20 33 32 28 24 28 22 20 22 22 X15 | 18 19 27 15 10 --- 22 23 --- 8 | 24 31 27 27 23 --- 24 26 --- 22 16 | 18 20 26 13 6 16 31 19 33 8 | 22 35 34 29 23 32 29 28 29 25 X17 | 9 14 29 12 15 --- 14 15 27 6 | 21 26 28 29 22 --- 24 25 39 24 18E | 17 18 17 10 6 14 17 18 22 6 | 21 31 29 24 22 29 18 26 21 22 X19 | 9 13 17 7 8 --- 16 21 25 6 | 27 23 26 25 23 --- 31 26 36 24 20E | 13 19 36 12 6 19 14 21 19 6 | 13 30 31 20 18 29 19 18 26 17 21 | 14 17 22 12 7 14 17 21 28 6 | 20 33 34 28 23 29 18 25 29 23 22E | 15 17 20 8 5 12 17 15 18 5 | 25 31 32 27 24 28 26 22 26 24 23 | 15 24 20 13 11 13 18 20 19 6 | 14 37 32 27 22 28 22 19 21 20 24 | 11 11 30 10 6 8 13 18 21 5 | 20 20 29 23 21 23 22 28 19 21 25E | 17 21 25 11 7 20 30 18 30 8 | 17 34 33 28 24 34 40 26 33 25 26 | 16 13 35 13 8 11 18 22 38 7 | 23 23 35 26 24 23 25 30 38 23 27E | 23 19 33 11 6 19 25 22 31 8 | 51 58 52 55 56 58 61 54 57 54 28 | 17 16 30 15 6 15 20 20 23 7 | 17 33 38 32 24 30 21 26 26 22 30 | 9 10 20 8 6 10 15 20 15 4 | 38 41 38 40 40 40 42 44 41 40 31E | 14 23 16 10 9 17 18 20 25 6 | 32 44 34 35 34 38 39 45 38 35 X32E | 25 28 --- --- 29 --- 19 32 --- 15 | 62 79 --- --- 87 --- 64 82 --- 68 ------+---------------------------------------------------+---------------------------------------------------- RMS | 16 17 28 12 8 14 20 21 26 |T 24 33 33 28 27 29 29 30 31 26 WRMS | 14 17 27 12 8 14 17 16 25 |NE 21 29 33 27 24 27 26 26 31 23 MEDI | 15 16 26 12 7 13 17 21 25 |MD 21 31 34 27 24 28 26 26 29 23 Table 3.1458.6 GPS week: 1458 Day: 6 MJD: 54456.000 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 11 23 15 7 9 14 12 38 6 | 21 28 27 24 25 27 28 24 49 23 2 | 15 18 40 15 9 11 21 17 29 7 | 21 35 59 32 27 34 23 24 33 27 X3 | 13 13 19 11 9 --- 13 20 51 8 | 27 29 20 23 25 --- 29 27 55 25 4 | 13 11 48 9 6 10 14 11 31 6 | 21 29 49 21 24 29 27 26 31 23 5 | 10 12 26 12 9 11 16 15 17 5 | 17 24 34 18 18 22 24 27 23 20 6 | 7 9 24 9 4 10 11 13 19 4 | 37 44 44 36 40 41 46 43 42 40 X7 | 10 17 --- 21 9 --- 15 14 --- 8 | 35 41 --- 39 37 --- 40 44 --- 37 8E | 20 15 25 13 9 17 20 26 31 7 | 17 22 29 20 17 26 24 34 29 17 X9E | 20 --- 31 14 7 13 27 22 27 8 | 30 --- 33 29 29 32 44 42 33 29 10E | 17 15 26 12 13 17 31 23 22 7 | 36 42 42 43 40 39 50 50 36 38 X11 | 14 22 30 16 10 --- 16 20 30 8 | 27 36 36 29 26 --- 27 24 35 24 12 | 15 13 33 15 6 12 18 16 29 6 | 23 33 43 34 26 29 24 31 30 26 13 | 15 21 36 13 8 12 16 17 22 6 | 16 35 37 26 24 29 21 20 27 21 14 | 16 18 28 14 6 12 19 18 20 6 | 22 36 34 26 26 30 29 26 29 24 X15 | 12 19 29 14 8 --- 19 17 27 7 | 24 35 37 31 28 --- 33 30 37 27 16 | 17 22 26 16 9 14 28 19 27 7 | 26 39 38 33 27 34 25 31 36 28 X17 | 9 13 26 12 9 --- 16 11 28 6 | 43 49 43 49 45 --- 46 47 52 46 18E | 15 17 19 9 8 11 14 12 19 5 | 24 34 34 30 27 32 25 31 30 27 X19 | 12 14 24 7 6 --- 17 22 36 7 | 42 40 38 41 38 --- 42 38 48 38 20E | 11 16 15 8 9 17 14 17 26 5 | 16 30 29 22 21 32 22 20 32 21 21 | 14 17 19 15 5 13 16 17 30 6 | 18 33 34 30 22 29 18 22 26 22 22E | 14 17 23 8 7 12 15 14 17 5 | 25 33 29 26 29 31 28 27 26 26 23 | 17 23 22 11 8 12 17 17 26 6 | 17 41 40 29 27 30 25 22 42 24 24 | 10 12 27 10 9 12 11 13 19 5 | 19 23 34 23 22 27 24 27 26 22 25E | 15 17 25 12 6 18 31 14 24 7 | 26 39 41 31 27 40 35 27 33 29 26 | 13 10 24 10 6 15 12 18 28 6 | 20 28 38 28 26 30 28 28 37 24 27E | 22 17 26 10 6 17 26 19 25 7 | 61 68 67 61 61 70 61 50 65 61 X28 | 14 19 28 15 7 --- 18 15 20 7 | 20 36 35 33 27 --- 25 29 30 25 30 | 9 11 24 13 6 10 13 13 15 5 | 36 38 39 36 37 34 38 40 40 36 31E | 14 23 25 12 11 15 23 16 22 6 | 21 39 30 26 25 31 26 29 27 24 X32E | 24 30 --- --- 39 --- 27 31 --- 16 | 89 100 --- --- 81 --- 105 85 --- 92 ------+---------------------------------------------------+---------------------------------------------------- RMS | 14 16 27 12 8 13 19 16 25 |T 28 37 37 30 30 32 33 33 35 30 WRMS | 13 16 25 12 8 13 16 13 23 |NE 25 34 37 30 28 30 29 30 36 27 MEDI | 14 17 26 12 8 12 16 17 26 |MD 24 35 37 29 27 31 28 29 33 26 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 4.1458 GPS week: 1458 MJD: 54450.0-54456.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 |U 14 12 27 |U 10 12 32 |U 7 10 20 | emr | emr 2914 |U 19 13 32 |U 10 9 30 | 12 15 25 | esa | esa 2852 |U 15 13 31 |U 9 9 31 | 11 13 21 | gfz | gfz 2843 |U 16 13 31 |U 11 11 44 |U 11 11 28 | igr | igr 2954 | 16 14 31 | 10 11 35 | 9 11 24 | igs | igs 2942 | 21 16 32 | 11 12 38 | 10 12 26 | jpl | jpl 2545 | 44 32 105 |U 22 29 50 |U 19 31 43 | mit | mit 2976 |U 21 24 57 |U 40 36 173 |U 13 19 32 | 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 5.1458.0 GPS week: 1458 Day: 0 MJD: 54450.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2956 | 16 15 21 | 10 13 29 | 6 11 18 | emr | emr 2864 | 25 13 21 | 9 11 28 | 13 15 24 | esa | esa 2880 | 8 8 23 | 10 7 30 | 10 10 17 | gfz | gfz 2855 | 11 6 20 | 11 10 37 | 10 9 20 | igr | igr 2945 | 17 16 35 | 9 11 28 | 10 8 26 | igs | igs 2965 | 20 14 33 | 9 9 28 | 11 11 25 | jpl | jpl 2768 | 20 13 27 | 10 9 25 | 11 18 37 | mit | mit 2976 | 31 19 94 | 12 12 35 | 9 11 24 | Table 5.1458.1 GPS week: 1458 Day: 1 MJD: 54451.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2956 | 9 9 19 | 8 7 32 | 6 7 16 | emr | emr 2956 | 12 15 23 | 7 7 26 | 12 18 20 | esa | esa 2880 | 13 14 26 | 7 6 32 | 11 10 25 | gfz | gfz 2843 | 11 11 20 | 10 8 46 | 10 8 21 | igr | igr 2972 | 10 11 26 | 9 6 30 | 8 9 27 | igs | igs 2869 | 9 13 28 | 12 10 47 | 8 11 32 | jpl | jpl 2672 | 32 30 52 | 7 8 30 | 12 19 27 | mit | mit 2976 | 17 26 68 | 10 12 48 | 11 14 23 | Table 5.1458.2 GPS week: 1458 Day: 2 MJD: 54452.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2938 | 37 20 55 | 11 11 33 | 6 10 19 | emr | emr 2954 | 39 22 60 | 10 9 30 | 11 15 27 | esa | esa 2879 | 38 24 55 | 10 10 30 | 9 10 20 | gfz | gfz 2843 | 32 22 48 | 13 14 36 | 12 11 30 | igr | igr 2960 | 34 23 51 | 11 14 37 | 8 13 22 | igs | igs 2954 | 40 20 49 | 12 10 34 | 8 11 27 | jpl | jpl 2667 | 42 23 59 | 11 9 34 | 10 21 32 | mit | mit 2976 | 38 25 58 | 12 11 33 | 7 14 29 | Table 5.1458.3 GPS week: 1458 Day: 3 MJD: 54453.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2943 | 14 17 40 | 9 12 35 | 7 9 19 | emr | emr 2954 | 15 13 34 | 11 10 37 | 12 11 20 | esa | esa 2879 | 18 14 34 | 9 9 34 | 14 13 21 | gfz | gfz 2840 | 18 17 40 | 11 11 55 | 11 11 32 | igr | igr 2951 | 19 21 42 | 11 11 43 | 9 7 21 | igs | igs 2951 | 35 28 31 | 11 13 44 | 9 9 24 | jpl | jpl 2668 | 20 20 40 | 11 11 39 | 12 18 30 | mit | mit 2976 | 23 21 47 | 126 95 489 | 32 45 63 | Table 5.1458.4 GPS week: 1458 Day: 4 MJD: 54454.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2965 | 6 6 17 | 10 14 37 | 6 15 22 | emr | emr 2860 | 18 10 35 | 12 11 31 | 13 17 25 | esa | esa 2880 | 10 9 27 | 8 12 31 | 11 17 24 | gfz | gfz 2843 | 14 11 29 | 12 14 41 | 13 16 29 | igr | igr 2966 | 14 10 19 | 11 12 29 | 9 14 27 | igs | igs 2966 | 13 12 26 | 12 16 48 | 10 18 26 | jpl | jpl 2572 | 57 20 105 | 10 13 32 | 15 32 38 | mit | mit 2976 | 16 53 87 | 58 89 252 | 17 22 31 | Table 5.1458.5 GPS week: 1458 Day: 5 MJD: 54455.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2948 | 10 7 19 | 11 9 27 | 9 12 27 | emr | emr 2951 | 10 7 26 | 13 7 26 | 14 13 34 | esa | esa 2784 | 10 9 27 | 12 9 29 | 11 15 24 | gfz | gfz 2842 | 13 12 28 | 11 8 38 | 13 10 33 | igr | igr 2928 | 10 9 24 | 13 9 39 | 8 14 26 | igs | igs 2968 | 15 13 31 | 13 12 39 | 11 12 29 | jpl | jpl 2283 | 72 28 152 | 61 87 118 | 39 47 61 | mit | mit 2976 | 10 10 19 | 51 22 317 | 10 16 27 | Table 5.1458.6 GPS week: 1458 Day: 6 MJD: 54456.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2966 | 7 7 16 | 9 15 34 | 7 8 21 | emr | emr 2860 | 13 11 24 | 9 11 31 | 13 16 29 | esa | esa 2784 | 8 10 26 | 9 14 32 | 10 14 17 | gfz | gfz 2841 | 11 11 32 | 9 13 53 | 10 10 33 | igr | igr 2961 | 10 11 22 | 11 12 36 | 8 11 22 | igs | igs 2926 | 12 9 24 | 11 15 28 | 9 10 23 | jpl | jpl 2188 | 63 88 300 | 43 64 71 | 33 62 72 | mit | mit 2976 | 11 14 26 | 10 13 35 | 8 15 29 | 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 6.1458 GPS week: 1458 MJD: 54450.500-54456.500 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 | 16 -12 60 71 -2 | -3 16 | 14 17 45 28 8 | 3 emr uuxuu | 8 36 -95 -198 12 | 44 47 | 12 40 248 86 7 | 3 esa uuuux | -44 -23 85 33 -6 | 27 34 | 35 33 128 109 28 | 2 gfz uuuuu | 26 20 -37 53 0 | -11 19 | 16 13 48 71 11 | 2 igr xxxxx | 17 -12 32 43 1 | -9 18 | 15 24 70 59 5 | 3 irf xxxxx | -9 13 -96 -28 10 | -13 21 | 5 7 62 28 7 | 3 jpl uuxux | 72 -8 42 156 23 | 252 254 | 17 14 282 104 34 | 12 mit uuuuu | -69 7 -159 -144 9 | -13 25 | 20 34 111 95 11 | 6 ngs uuuuu | -54 -4 60 -114 -3 | -6 11 | 38 48 107 133 8 | 3 sio uuuuu | -45 -69 62 82 0 | 16 24 | 23 23 100 84 11 | 4 Table 7.1458.0 GPS week: 1458 Day: 0 MJD: 54450.500 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 -19 0 28 -7 | 2 10 emr uuxuu | 7 21 57 -144 12 | 42 44 esa uuuux | -103 13 17 -106 16 | 28 32 gfz uuuuu | 48 36 9 74 8 | -9 13 igr xxxxx | 18 30 102 43 0 | -5 11 irf xxxxx | -9 23 -8 0 1 | -9 17 jpl uuxux | 69 -29 392 281 53 | 236 237 mit uuuuu | -69 67 -207 -277 -8 | -2 26 ngs uuuuu | -55 -35 99 -48 2 | -2 6 sio uuuuu | -14 -83 56 31 -13 | 23 26 Table 7.1458.1 GPS week: 1458 Day: 1 MJD: 54451.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 24 11 118 52 11 | -1 12 emr uuxuu | 6 -17 124 -238 26 | 41 42 esa uuuux | -26 -39 235 22 38 | 26 29 gfz uuuuu | 35 6 -84 -25 18 | -10 15 igr xxxxx | 25 -22 32 -57 11 | -7 13 irf xxxxx | -2 18 -83 -48 17 | -13 18 jpl uuxux | 57 -14 229 263 67 | 239 240 mit uuuuu | -40 -1 -160 -200 12 | -9 25 ngs uuuuu | -93 48 0 20 -13 | -3 8 sio uuuuu | -21 -55 19 66 7 | 18 23 Table 7.1458.2 GPS week: 1458 Day: 2 MJD: 54452.500 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 | 39 -20 82 54 -8 | 0 14 emr uuxuu | 3 7 131 -311 9 | 44 47 esa uuuux | -52 -62 -117 98 0 | 30 36 gfz uuuuu | 36 10 -28 101 3 | -8 17 igr xxxxx | 1 -3 111 117 -4 | -6 15 irf xxxxx | -12 15 -69 -9 4 | -12 19 jpl uuxux | 84 -12 341 170 43 | 248 251 mit uuuuu | -66 33 -244 -131 1 | -11 23 ngs uuuuu | -96 61 182 -67 3 | -3 8 sio uuuuu | -80 -93 28 22 -9 | 19 24 Table 7.1458.3 GPS week: 1458 Day: 3 MJD: 54453.500 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 | 21 6 4 95 -5 | -4 18 emr uuxuu | -1 12 19 -181 14 | 42 46 esa uuuux | -72 7 198 139 -15 | 29 36 gfz uuuuu | 37 37 -79 58 -8 | -11 20 igr xxxxx | 9 -50 49 39 -1 | -10 19 irf xxxxx | -4 13 -79 3 6 | -16 23 jpl uuxux | 55 12 20 81 26 | 253 255 mit uuuuu | -64 -4 -33 36 6 | -18 24 ngs uuuuu | -50 -55 -40 -297 5 | -7 12 sio uuuuu | -38 -94 185 43 -6 | 14 23 Table 7.1458.4 GPS week: 1458 Day: 4 MJD: 54454.500 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 -11 52 109 -13 | -6 20 emr uuxuu | 3 66 -136 -299 9 | 42 46 esa uuuux | -12 2 1 86 -5 | 25 35 gfz uuuuu | 10 22 -78 87 -2 | -14 23 igr xxxxx | 22 -12 17 49 -3 | -12 21 irf xxxxx | -11 12 -74 -26 13 | -17 24 jpl uuxux | 57 -18 -152 -2 6 | 257 259 mit uuuuu | -104 11 19 -123 12 | -20 26 ngs uuuuu | 17 -44 93 -21 0 | -9 14 sio uuuuu | -40 -65 -95 241 6 | 10 22 Table 7.1458.5 GPS week: 1458 Day: 5 MJD: 54455.500 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 -40 68 75 -1 | -5 20 emr uuxuu | 5 75 -375 -113 12 | 47 51 esa uuuux | -38 -16 70 121 -25 | 27 36 gfz uuuuu | 8 9 -39 140 -1 | -12 23 igr xxxxx | 43 -18 -97 104 4 | -11 21 irf xxxxx | -18 4 -186 -46 19 | -14 24 jpl uuxux | 100 1 -269 92 -12 | 264 266 mit uuuuu | -82 -20 -281 -163 26 | -17 26 ngs uuuuu | -39 27 178 -308 -14 | -7 14 sio uuuuu | -63 -65 192 19 17 | 13 25 Table 7.1458.6 GPS week: 1458 Day: 6 MJD: 54456.500 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 99 87 7 | -7 20 emr uuxuu | 35 87 -487 -99 3 | 49 52 esa uuuux | -6 -68 190 -127 -50 | 25 36 gfz uuuuu | 10 20 39 -60 -15 | -13 23 igr xxxxx | 0 -9 7 4 3 | -12 21 irf xxxxx | -9 4 -170 -71 9 | -11 23 jpl uuxux | 80 1 -267 211 -22 | 266 267 mit uuuuu | -56 -34 -204 -148 15 | -14 25 ngs uuuuu | -62 -27 -94 -77 -5 | -10 16 sio uuuuu | -57 -31 52 151 2 | 14 26