Date: Thu, 19 Nov 2009 13:21:20 +0000 From: Jim Ray Subject: [IGSREPORT-18010] Wk 1556 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4b054650.DLghRtfGOsqfqXZn%igs.acc@noaa.gov> Content-type: text/plain; charset=us-ascii Content-transfer-encoding: 7bit User-Agent: nail 11.25 7/29/05 Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 19 Nov 05:21:43 PST 2009 Message Number 18010 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1556 (Nov 01, 2009 - Nov 07, 2009) Contacts: J. Ray (jim.ray@noaa.gov), J. Griffiths (jake.griffiths@noaa.gov) 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: igs1556[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1556[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1556[0-6].cls IGS GPS clock combination summary report. igs15567.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15567.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, 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. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and 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. Duplicate entries can arise due to separate combination runs for the 30-s clocks ACs (listed first) and the 5-min clock ACs (listed second). Day | Centre | PRN/STA list ----+--------+--------------- 0 | ALL | 1 0 | COD | 9 4 9 27 DRAO 0 | ESA | 4 8 9 24 27 0 | GFZ | 2 8 9 13 16 27 31 ALRT AREQ ASPA AUCK BOGT BOR1 BRFT 0 | GFZ | CHPI DUBO GODE GUAT HYDE IRKT KIRU MCM4 MDO1 NRMD 0 | GFZ | OUS2 PIE1 PIMO PRE1 RAMO SFER STJO TIXI TOW2 TSKB 0 | GFZ | UNSA WTZR YELL YKRO 0 | GRG | WTZR 0 | JPL | 32 0 | MIT | 24 24 MIZU MIZU NYA1 1 | ALL | 1 1 1 | COD | 9 9 24 27 1 | EMR | 30 30 1 | ESA | 8 9 27 1 | GFZ | 2 4 7 8 9 14 21 24 27 31 ALGO ALIC AREQ BUE1 CONZ 1 | GFZ | FAA1 GODE HRM1 JPLM KERG KOUC MAC1 MBAR MCM4 MDO1 1 | GFZ | PDEL PRDS SEY1 SFER VILL WSRT YKRO 1 | GRG | ONSA 1 | JPL | 32 1 | MIT | 27 MIZU PTBB HARB MIZU PTBB 2 | ALL | 1 2 | COD | 9 9 2 | EMR | WTZR 2 | ESA | 8 9 2 | GFZ | 4 5 9 13 21 22 24 27 ALIC ALRT BOR1 CONZ CRO1 DAEJ 2 | GFZ | GUAT HYDE IRKT KERG LPGS MCM4 MDO1 NICO NRC1 NYA1 2 | GFZ | NYAL ONSA RAMO SANT TEHN THTI TIXI TOW2 TSKB TWTF 2 | GFZ | UNSA XMIS YSSK 2 | GRG | WTZR 2 | JPL | 32 DGAR 2 | MIT | 24 27 24 27 3 | COD | 9 27 9 27 3 | EMR | 8 31 8 WTZR 3 | ESA | 9 27 UNSA XMIS 3 | GFZ | 7 8 9 11 15 17 24 29 32 ALGO ASPA BOGT BRFT BRUS 3 | GFZ | CAS1 CHPI GRAZ GUAT HARB IRKT KIRU KOUC MATE MDO1 3 | GFZ | NRC1 RIOP THTI THU3 WSRT YELL YKRO ZIMM 3 | GRG | ONSA 3 | JPL | 32 3 | MIT | 24 3 | NGS | 1 4 | COD | 9 9 4 | EMR | 25 31 25 31 WTZR 4 | ESA | 9 4 | GFZ | 5 9 16 22 23 27 30 ALGO ALIC AREQ BOR1 BRUS CHPI 4 | GFZ | DARW DAV1 FAA1 FAIR GOLD GUAT HARB HOLM KARR KERG 4 | GFZ | KIRU KOUC LPGS MAS1 MBAR MIZU NRC1 NRMD NYA1 ONSA 4 | GFZ | PDEL PETS PIE1 PRDS QAQ1 RABT RIOP SANT SFER STJO 4 | GFZ | THTI TSKB ULAB WSRT WTZR XMIS YAKT YSSK ZIMM 4 | GRG | WTZR 4 | JPL | 32 4 | MIT | 24 24 4 | NGS | 1 5 | COD | 9 27 9 27 DAEJ DAEJ 5 | EMR | WTZR 5 | ESA | 9 27 5 | GFZ | 3 5 7 9 17 24 27 28 32 ADE1 ALIC AMC2 AREQ ASPA AUCK 5 | GFZ | BOR1 BRAZ BRFT CHAT COCO DAV1 DUBO EIL1 FAIR FLIN 5 | GFZ | GLPS GLSV GODE GUAM GUAT HARB IRKT MAC1 MAS1 MCM4 5 | GFZ | MDO1 NRC1 NRMD NYA1 ONSA OUS2 PDEL PIE1 PIMO PRDS 5 | GFZ | RABT RIOP THU3 TOW2 TRO1 TWTF WAB2 WTZR XMIS YKRO 5 | GRG | WTZR 5 | JPL | 32 DGAR 5 | MIT | 24 24 ALGO ALGO 5 | NGS | 1 6 | ALL | 24 6 | COD | 9 27 9 27 6 | EMR | ONSA 6 | ESA | 9 27 UNSA 6 | GFZ | 5 7 9 24 27 31 ALIC AREQ BRAZ BRFT CHUR FLIN HARB 6 | GFZ | HOFN HOLM KOUC MAS1 MBAR MCM4 MIZU NICO THTI XMIS 6 | GRG | ALGO WTZR 6 | JPL | 32 DGAR MCM4 6 | MIT | 24 HARB 6 | NGS | 1 5. The following orbit solutions were excluded from the combination because they were biasing the weighted average (generally indicated by long arc RMS). They were still used for statistics computation. Day | Centre | PRN list ----+--------+--------------- 0 | NGS | 24 4 | NGS | 24 5 | NGS | 24 6 | NGS | 24 6. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G24 | | | | | | 2 | 1 | PRN G25 | | | 1 | | | | | 7. 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. 8. 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 | .3 .9 1.0 -14 -10 -8 -.22 EMR | 1.7 1.2 3.9 76 -6 43 .59 ESA | 5.6 2.2 3.9 71 -23 71 .0 GFZ | .3 1.3 1.0 17 -12 1 -.10 GRG | 2.5 9.1 5.9 27 30 209 .38 JPL | 5.7 5.2 12.1 -5 -36 -2 .09 MIT | 2.8 3.4 2.9 3 5 -27 -.18 NGS | 6.0 -.1 1.9 -1 -64 -7 -.16 SIO | 7.9 4.9 7.6 86 -82 16 .21 9. 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. 10. 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. 11. 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 1.1556.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1556.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 2.1556.[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 3.1556.[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 5.1556.0-6). 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 1556 summary. (Nov 01, 2009 - Nov 07, 2009) Table 1.1556.a GPS week: 1556 MJD: 55136.000-55142.000 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 232| 0 0 0 78 -6 -3 -.19 8 7 | -247 -229 25 72 | 0 0 1 17 35 32 .02 | 346 865 emr 88| 0 -1 2 -82 -51 0 .55 20 20 | 463 226 37 120 | 2 1 1 40 55 17 .03 | 2743 1325 esa 127| 0 0 1 -90 -33 -12 .28 10 10 | 607 -1523 22 118 | 1 0 1 20 40 26 .03 | 966 2023 gfz 192| 0 0 -2 -13 -53 -2 -.17 11 11 | -214 960 47 146 | 0 1 2 69 131 12 .04 | 371 2153 grg 107| 0 0 3 -20 -114 -3 1.02 25 24 | 398 -558 73 219 | 1 1 2 47 34 21 .05 | 384 743 igr n/a| 0 0 1 49 -42 -41 .01 6 6 | 3828 720 25 78 | 0 0 0 14 41 25 .02 | 3736 1474 jpl 120| 0 -1 2 71 22 31 .58 20 19 | 1642 404 26 92 | 2 0 1 21 28 30 .04 | 2885 1347 mit 274| 0 0 -3 30 -36 2 -.27 11 10 | -14420 -2372 27 117 | 0 1 0 21 20 17 .03 | 2171 2995 ngs 220| -1 0 0 34 94 8 -.18 11 9 | -498637 225540 2026 3654 | 0 1 0 39 84 13 .03 | 312808 152420 sio 258| 0 3 5 -141 125 -15 .05 19 19 | --- --- --- --- | 0 0 1 32 23 25 .06 | --- --- Table 1.1556.b GPS week : 1556 MJD: 55136.000-55142.000 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 | 13 9 16 19 11 13 12 | 2 | 6 5 6 5 5 5 6 | 3 | 4 4 4 4 3 4 4 | 4 | 6 8 6 5 5 4 5 | 5 | 5 6 6 5 5 5 6 | 6 | 4 4 3 4 3 4 4 | 7 | 5 5 5 5 4 4 5 | 8 | 6 6 7 8 14 0 0 | 9 | 6 6 5 5 6 6 6 | 10 | 4 4 4 4 4 4 5 | 11 | 5 4 5 5 4 4 4 | 12 | 6 5 5 5 5 5 6 | 13 | 5 4 4 4 4 4 4 | 14 | 5 5 5 5 4 4 5 | 15 | 5 5 5 5 5 5 6 | 16 | 6 6 6 6 5 5 5 | 17 | 6 5 5 5 4 5 5 | 18 | 5 5 5 5 5 5 5 | 19 | 5 5 5 5 5 5 5 | 20 | 5 5 4 4 4 4 4 | 21 | 5 5 4 4 4 3 4 | 22 | 5 5 4 5 4 4 5 | 23 | 6 6 5 6 5 5 5 | 24 | 14 14 13 23 21 10 9 | 25 | --- 0 12 12 12 7 7 | 26 | 4 4 4 4 4 4 4 | 27 | 6 6 6 6 7 7 7 | 28 | 6 6 6 6 6 6 6 | 29 | 6 6 5 5 5 5 6 | 30 | 4 5 6 4 3 4 4 | 31 | 6 5 5 5 4 4 5 | 32 | 5 7 6 5 5 5 5 | 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 2.1556.0 GPS week: 1556 Day: 0 MJD: 55136.000 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 232| 0 0 1 83 -76 -43 -.19 8 7 | -464 535 25 77 | -24 82 | emr 88| 0 0 3 -137 -138 7 .62 20 20 | -2842 -88 20 93 | -22 62 | esa 127| 1 0 0 -61 26 1 .32 11 11 | 641 -1885 20 114 | -18 -76 | gfz 192| 0 0 -6 20 191 21 -.21 12 12 | -732 4701 38 138 | 21 15 | grg 107| 0 0 1 35 -168 -16 1.07 29 27 | 344 -633 81 207 | -60 84 | igr n/a| 0 0 1 56 -127 -15 -.02 7 7 | -904 343 27 83 | -97 40 | jpl 120| 2 -1 2 42 -27 31 .59 22 20 | -1864 70 19 98 | 10 58 | mit 274| -1 0 -2 18 -9 24 -.27 13 13 | -14513 -2506 27 130 | 39 -34 | ngs 220| 0 0 0 16 -60 3 -.23 10 9 | -338659 93165 2310 3491 | -3 181 | sio 258| 0 4 3 -174 143 4 .14 21 20 | --- --- --- --- | 43 -86 | Table 2.1556.1 GPS week: 1556 Day: 1 MJD: 55137.000 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 232| 0 0 -1 42 -15 19 -.19 9 7 | -446 666 29 71 | 10 11 | emr 88| 3 -2 2 -134 -102 -19 .56 20 20 | -1821 -32 24 77 | -19 60 | esa 127| 0 -1 4 -93 11 -61 .26 11 11 | 851 -2106 22 120 | -4 -43 | gfz 192| 0 1 -3 104 26 5 -.20 11 11 | -519 761 44 150 | 42 17 | grg 107| -1 -1 0 -107 -126 11 1.04 26 24 | 564 -751 77 236 | 91 51 | igr n/a| 0 0 1 25 -33 -80 .02 6 5 | 547 545 25 68 | -29 0 | jpl 120| 1 -2 2 40 16 64 .54 19 19 | -821 177 21 82 | -28 43 | mit 274| -1 -1 -4 64 -64 12 -.26 14 12 | -15226 -1276 29 109 | 24 -14 | ngs 220| 0 0 0 -37 31 -6 -.15 11 9 | 7293 11775 1991 3525 | 50 47 | sio 258| 0 3 3 -82 85 6 .08 21 20 | --- --- --- --- | 9 -73 | Table 2.1556.2 GPS week: 1556 Day: 2 MJD: 55138.000 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 232| 1 0 -1 88 -11 -20 -.20 10 8 | -195 -656 29 73 | -22 2 | emr 88| 0 -1 1 -71 -50 -19 .52 18 18 | -2073 1214 20 84 | -53 17 | esa 127| 1 -1 2 -67 -36 17 .23 10 10 | -110 102 21 114 | -20 29 | gfz 192| 1 0 0 -51 -76 -2 -.17 11 11 | -390 606 40 124 | 52 -23 | grg 107| 0 0 7 -16 -88 -32 .99 25 24 | 77 -809 73 219 | -15 24 | igr n/a| -1 0 1 60 -41 -68 .03 6 5 | 965 1738 23 65 | -66 27 | jpl 120| 0 -1 5 85 11 78 .56 18 18 | -808 1312 18 81 | -39 70 | mit 274| -1 0 -5 12 -40 -6 -.28 11 10 | -9880 -7737 20 97 | 25 -18 | ngs 220| -2 2 0 53 115 7 -.19 11 9 | -535298 315393 1919 3637 | 38 41 | sio 258| 0 2 3 -146 114 -22 .07 19 21 | --- --- --- --- | 28 -90 | Table 2.1556.3 GPS week: 1556 Day: 3 MJD: 55139.000 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 232| 1 1 0 78 13 -7 -.17 7 7 | -239 -251 25 82 | -10 0 | emr 88| -2 -3 4 -40 0 0 .54 20 20 | 703 1869 55 180 | -91 -28 | esa 127| 0 0 0 -110 -71 -13 .27 11 11 | 445 -1351 26 123 | 39 40 | gfz 192| 0 1 -3 -13 -139 -9 -.14 11 11 | -215 2862 67 174 | -23 -6 | grg 107| 0 0 4 -51 -104 -17 .94 26 23 | -70 515 74 227 | -28 63 | igr n/a| 0 0 0 49 -23 -13 .03 5 5 | 3954 2598 28 75 | -64 -13 | jpl 120| 1 -2 4 78 14 -11 .65 20 19 | 1793 2063 23 85 | -100 -9 | mit 274| 0 0 -3 9 -12 14 -.25 9 8 | -14798 -1287 32 139 | 17 -11 | ngs 220| 0 -1 0 42 123 17 -.15 12 9 | -539440 314826 2548 4074 | -13 34 | sio 258| 0 3 6 -170 143 -4 .08 18 19 | --- --- --- --- | 35 -88 | Table 2.1556.4 GPS week: 1556 Day: 4 MJD: 55140.000 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 232| 0 0 -1 86 26 44 -.15 7 7 | -691 391 30 78 | -5 -14 | emr 88| -1 -2 3 -58 -1 13 .56 19 19 | 2095 1071 67 171 | -55 -16 | esa 127| 0 -1 2 -116 -35 -22 .28 10 10 | -220 737 27 123 | 59 56 | gfz 192| -1 1 -2 -70 -183 -14 -.21 10 10 | -41 -469 72 185 | -4 -29 | grg 107| -1 -1 0 -10 -68 -10 1.02 24 23 | 971 -1883 70 212 | -48 -19 | igr n/a| 0 0 1 64 3 -25 .03 6 6 | 5891 1745 27 93 | -52 -34 | jpl 120| 0 0 2 70 40 19 .61 20 19 | 3110 1429 44 105 | -40 -19 | mit 274| 0 0 -3 33 -56 -11 -.24 9 8 | -14020 -4814 29 106 | 13 15 | ngs 220| 0 0 0 79 193 0 -.19 12 9 | -865805 368878 1513 3074 | -56 -92 | sio 258| 1 3 6 -135 112 -46 .03 18 18 | --- --- --- --- | 9 -74 | Table 2.1556.5 GPS week: 1556 Day: 5 MJD: 55141.000 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 232| 0 0 0 94 24 -37 -.19 8 8 | 393 -1800 22 61 | -15 -18 | emr 88| 1 -1 0 -42 3 29 .54 20 20 | 3211 -278 54 126 | -73 7 | esa 127| 1 0 1 -84 -81 -19 .28 8 8 | 40 -684 25 123 | 41 77 | gfz 192| 0 0 -1 -100 -165 -13 -.13 12 12 | 378 -1682 45 138 | 33 -40 | grg 107| 1 0 3 22 -98 23 1.07 24 23 | 136 -264 68 220 | -37 -17 | igr n/a| 0 0 1 59 -22 -50 -.01 5 5 | 7718 -66 25 89 | -31 8 | jpl 120| -1 0 2 93 63 17 .53 21 20 | 4661 -236 40 112 | -31 -19 | mit 274| 0 1 -3 24 -38 12 -.29 9 9 | -16246 282 31 116 | 14 1 | ngs 220| 0 0 0 69 154 32 -.14 11 7 | -341660 97191 1981 4022 | -92 -94 | sio 258| 0 3 5 -162 128 5 -.03 18 16 | --- --- --- --- | 19 -72 | Table 2.1556.6 GPS week: 1556 Day: 6 MJD: 55142.000 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 232| 0 0 0 76 -7 18 -.22 8 8 | -92 -493 16 62 | 24 -10 | emr 88| 0 0 0 -91 -73 -2 .53 19 19 | 3973 -2170 23 113 | -33 35 | esa 127| 3 0 -1 -97 -48 9 .32 8 8 | 2608 -5474 19 112 | 14 8 | gfz 192| 1 0 0 19 -26 -2 -.12 12 12 | 19 -55 28 113 | 11 11 | grg 107| 0 1 6 -15 -147 18 1.01 25 23 | 769 -87 68 212 | 27 68 | igr n/a| 0 0 1 32 -56 -36 .00 5 5 | 8625 -1858 20 75 | -52 22 | jpl 120| -3 -2 1 88 36 20 .58 21 20 | 5424 -1982 18 84 | -23 32 | mit 274| 0 1 -2 53 -31 -24 -.33 11 9 | -16257 733 25 127 | 6 3 | ngs 220| -2 -1 0 14 103 6 -.21 12 11 | -876890 377554 1924 3759 | 29 12 | sio 258| 1 3 7 -122 150 -52 -.03 20 20 | --- --- --- --- | 5 -76 | 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 3.1556.0 GPS week: 1556 Day: 0 MJD: 55136.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 22 --- --- 27 --- 23 --- 12 23 --- 13 | 29 --- --- 27 --- 51 --- 39 52 --- 35 2E | 7 24 13 14 27 7 26 11 12 28 6 | 46 51 49 49 56 47 48 47 48 43 45 3 | 5 15 10 10 15 8 11 10 12 16 4 | 28 32 37 36 35 30 32 32 21 32 29 4E | 12 19 10 17 33 7 22 20 9 24 6 | 106 108 101 109 113 104 116 98 104 98 104 5 | 7 19 10 15 35 7 26 10 10 17 5 | 22 35 27 24 51 23 34 23 22 19 21 6 | 5 16 9 8 15 7 11 10 9 15 3 | 31 36 39 36 39 33 36 36 27 33 33 7E | 9 26 8 10 24 6 25 16 8 16 5 | 19 29 23 19 32 23 27 23 19 23 18 8E | 12 21 13 12 43 6 17 17 12 28 6 | 46 36 30 35 31 59 24 37 34 21 43 9E | 10 19 7 15 38 7 21 15 21 14 5 | 37 47 44 41 68 39 50 45 31 49 40 10 | 9 13 10 7 22 7 12 10 9 19 4 | 18 26 25 19 35 21 23 24 21 18 19 11 | 8 16 11 9 25 8 17 14 7 19 4 | 28 32 31 24 38 30 31 31 26 36 27 12 | 8 19 8 10 31 5 24 19 10 29 5 | 36 43 40 37 41 38 43 35 37 33 36 13 | 6 21 11 11 33 4 23 11 8 11 4 | 22 31 25 27 41 26 30 20 22 20 21 14 | 8 19 13 13 34 7 24 14 9 16 5 | 23 34 29 27 34 27 29 28 21 27 24 15 | 10 20 11 10 27 6 22 15 8 20 5 | 24 34 30 29 36 27 29 26 23 21 24 16 | 8 22 12 11 27 9 23 21 8 26 5 | 24 37 32 31 37 28 33 34 25 29 26 17 | 7 17 13 14 27 7 20 12 10 28 5 | 25 36 33 26 40 27 33 23 22 27 24 18 | 7 24 9 10 35 8 23 8 8 16 4 | 24 39 24 23 49 25 34 23 24 24 22 19 | 5 23 10 11 21 7 20 14 9 25 5 | 27 42 34 25 43 31 38 33 26 30 29 20 | 5 22 13 8 32 9 21 10 7 15 4 | 23 35 26 20 40 25 32 24 21 24 22 21E | 13 16 9 11 44 8 19 11 11 10 4 | 37 35 29 36 47 32 32 35 28 29 31 22 | 5 21 14 11 29 6 25 14 10 18 5 | 21 37 29 22 46 24 31 23 20 23 21 23 | 7 26 11 17 29 5 25 8 8 16 5 | 23 35 28 32 35 28 31 23 26 23 24 X24E | 19 30 37 19 --- 20 --- 31 169 --- 13 | 75 74 58 78 --- 72 --- 80 116 --- 75 26 | 6 15 10 8 25 6 14 11 8 18 4 | 21 28 23 18 25 23 20 24 17 29 20 27E | 13 20 9 11 20 6 20 14 17 17 5 | 41 48 47 46 52 44 48 46 45 46 43 28 | 7 15 11 9 29 7 25 12 9 34 5 | 32 38 39 38 39 35 34 33 28 37 33 29 | 7 18 12 11 32 9 24 13 11 29 5 | 27 31 26 28 37 27 33 29 27 24 25 X30 | 7 15 8 7 27 5 --- 12 8 20 4 | 30 35 35 37 38 35 --- 43 35 29 33 31E | 7 21 14 14 20 7 26 15 11 18 5 | 19 32 27 23 32 22 29 18 20 19 19 32 | 8 20 15 9 19 8 22 10 9 22 5 | 48 52 52 43 51 52 49 53 45 50 47 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 20 11 12 29 7 22 13 10 21 |T 32 40 35 34 43 35 36 35 33 31 32 WRMS | 7 20 11 12 27 7 20 13 9 20 |NE 26 35 31 28 39 30 32 29 26 28 27 MEDI | 7 19 11 11 27 7 22 12 9 18 |MD 27 35 30 29 39 30 32 32 26 29 27 Table 3.1556.1 GPS week: 1556 Day: 1 MJD: 55137.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 16 --- --- 14 --- 19 --- 15 16 --- 9 | 27 --- --- 25 --- 27 --- 28 29 --- 24 2E | 9 23 11 12 24 7 20 10 8 24 5 | 39 44 49 45 49 42 43 45 45 39 41 3 | 5 13 8 10 17 4 13 9 10 15 3 | 19 24 24 21 27 19 25 20 17 23 19 4E | 16 22 17 13 20 8 18 29 12 35 7 | 86 89 91 79 90 81 86 69 83 70 82 5 | 7 23 13 15 28 7 23 11 11 19 5 | 18 37 29 25 47 21 32 22 22 21 22 6 | 6 14 8 10 16 4 15 12 12 14 4 | 22 28 24 20 32 20 27 26 19 23 20 7E | 9 23 10 11 19 5 22 14 7 15 5 | 19 29 22 18 32 19 25 23 21 27 20 8E | 14 23 11 11 31 8 17 16 14 30 6 | 37 32 29 32 26 48 24 38 37 22 36 9E | 12 20 11 13 26 9 19 13 22 16 6 | 32 42 40 39 52 36 43 43 33 42 36 10 | 8 13 9 10 16 6 11 11 10 19 4 | 14 26 22 21 26 16 20 19 18 16 16 11 | 7 15 11 7 29 4 14 12 11 16 4 | 23 32 35 28 38 29 27 28 29 32 27 12 | 7 17 9 10 41 7 19 10 9 28 4 | 23 28 27 27 40 24 27 23 23 23 22 13 | 8 22 7 8 26 5 20 10 7 15 4 | 20 31 26 21 40 23 29 22 20 19 20 14 | 7 17 11 12 29 5 24 12 6 13 4 | 13 28 24 22 33 18 26 19 17 20 18 15 | 5 22 10 11 26 7 22 14 11 18 5 | 20 32 28 25 35 24 29 27 23 26 23 16 | 7 20 10 11 24 4 24 22 11 26 6 | 17 31 24 20 31 20 31 25 19 21 17 17 | 9 16 13 10 34 7 16 12 12 26 5 | 14 24 22 13 35 18 21 16 20 15 15 18 | 6 22 10 12 26 5 24 9 6 13 4 | 23 35 26 20 36 23 32 22 23 24 22 19 | 8 19 7 9 26 4 21 11 8 23 4 | 19 31 24 21 36 20 32 18 21 20 20 20 | 7 22 15 7 28 5 17 9 9 14 4 | 21 33 35 20 42 27 27 26 28 26 25 21E | 11 19 17 17 33 5 17 9 8 10 5 | 29 37 38 39 41 33 32 35 36 33 32 22 | 4 18 9 14 28 5 20 13 8 14 4 | 15 29 20 16 37 15 25 16 16 19 16 23 | 6 28 15 9 24 4 25 9 10 17 5 | 27 42 36 27 44 31 37 29 28 28 29 X24E | 29 32 29 26 --- 27 --- 42 32 --- 14 | 76 75 67 90 --- 79 --- 87 107 --- 80 X25E | 4 --- --- --- --- >>>> --- --- --- --- 0 | 19 --- --- --- --- 9999 --- --- --- --- 20 26 | 6 14 11 8 18 5 13 8 7 18 4 | 15 24 22 17 27 17 19 19 16 24 16 27E | 15 22 11 12 29 8 21 13 18 20 6 | 33 40 36 39 45 37 37 36 40 35 35 28 | 7 19 11 12 23 5 20 14 11 35 5 | 21 31 28 29 31 24 26 22 23 26 22 29 | 6 18 10 12 30 7 21 13 11 30 5 | 20 26 20 25 30 22 27 22 25 21 20 X30 | 7 14 9 12 32 9 --- 14 11 --- 5 | 21 25 26 27 33 22 --- 28 25 --- 23 31E | 7 20 11 11 16 7 22 16 10 17 5 | 16 29 23 14 29 18 26 15 14 15 15 32 | 18 24 16 11 27 7 17 18 12 23 6 | 96 103 101 104 91 101 103 103 104 103 101 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 11 11 26 6 19 14 11 21 |T 27 37 33 31 39 30 33 31 31 29 29 WRMS | 7 20 11 11 24 5 19 12 9 20 |NE 23 33 29 26 37 25 31 26 25 26 24 MEDI | 7 20 11 11 26 6 20 12 11 18 |MD 21 31 26 25 36 23 27 25 23 23 22 Table 3.1556.2 GPS week: 1556 Day: 2 MJD: 55138.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 24 --- --- 33 --- 43 --- 15 34 --- 15 | 28 --- --- 34 --- 57 --- 26 51 --- 27 2 | 17 22 10 12 20 6 17 11 13 22 5 | 94 95 97 98 101 92 98 96 97 88 95 3 | 7 12 7 8 21 4 11 8 9 12 3 | 20 24 26 24 30 20 27 22 19 23 20 4E | 13 19 18 16 23 6 16 15 12 23 6 | 101 108 102 106 107 101 111 103 104 100 103 5 | 9 23 11 11 26 7 23 12 10 23 5 | 17 32 21 18 43 14 32 15 23 16 16 6 | 7 11 6 8 21 3 12 8 9 12 3 | 25 26 26 26 30 23 28 27 24 23 23 7E | 7 19 11 10 18 5 24 14 8 13 5 | 14 21 18 19 31 13 25 14 19 12 13 8E | 14 16 17 13 30 9 16 17 18 31 6 | 29 28 31 32 32 44 24 36 40 16 29 9E | 11 18 11 11 17 6 19 11 19 12 5 | 32 39 41 37 46 33 43 38 32 41 36 10 | 6 11 7 6 12 5 9 10 10 19 3 | 14 22 18 16 25 13 23 17 22 15 15 11 | 10 16 9 11 30 4 15 10 12 16 4 | 14 25 23 22 39 18 24 17 21 20 17 12 | 7 18 7 15 28 5 20 8 10 27 5 | 21 29 26 26 34 22 30 22 25 21 22 13 | 6 19 8 10 26 5 17 10 7 12 4 | 15 28 20 23 40 17 28 18 21 14 17 14 | 7 17 11 14 32 5 21 9 10 15 4 | 14 24 26 27 31 19 27 20 22 21 20 15 | 6 20 10 9 21 7 23 11 10 16 4 | 18 28 25 24 35 18 30 21 21 22 20 16 | 10 24 10 12 27 7 24 16 10 24 5 | 18 31 22 21 33 18 31 24 21 21 18 17 | 7 13 8 14 33 4 15 10 11 23 4 | 13 21 16 14 33 12 23 13 19 16 11 18 | 8 20 10 12 25 5 20 7 9 14 4 | 16 28 19 17 34 16 29 18 22 23 17 19 | 6 17 9 8 24 4 19 9 8 24 4 | 17 33 26 21 41 21 36 19 19 20 21 20 | 6 19 8 11 25 6 16 8 10 12 4 | 17 29 25 17 39 19 26 18 22 19 18 21E | 10 18 9 10 29 6 14 9 12 10 4 | 26 29 25 26 31 23 31 27 28 29 25 22 | 5 17 8 13 30 4 19 10 9 12 4 | 14 23 18 17 34 15 24 16 19 16 14 23 | 7 27 13 14 23 5 23 8 8 15 5 | 18 34 29 27 38 22 32 18 24 20 21 X24E | 36 34 24 31 --- 19 --- 28 17 --- 13 | 70 61 70 63 --- 58 --- 65 68 --- 58 X25E | 22 --- 17 --- --- 31 --- 21 24 --- 12 | 31 --- 9999 --- --- 9999 --- 9999 9999 --- 33 26 | 7 12 11 10 19 4 12 7 11 15 4 | 14 19 23 20 23 15 20 17 20 21 16 27E | 15 22 11 10 24 5 20 11 20 16 6 | 22 29 28 25 28 25 29 24 32 26 24 28 | 9 22 10 16 24 6 18 11 8 31 5 | 22 29 26 29 29 19 24 24 23 25 22 29 | 7 15 8 10 33 8 19 8 12 28 5 | 17 19 12 14 29 14 25 15 19 18 13 X30 | 8 15 10 12 23 9 --- 16 11 --- 5 | 20 24 23 26 24 21 --- 30 28 --- 23 31E | 6 18 8 12 14 4 22 11 8 15 4 | 14 24 18 16 25 13 26 15 18 14 13 32 | 20 21 9 10 11 7 16 13 7 21 5 | 45 54 57 56 53 52 50 58 48 57 51 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 10 11 25 6 18 11 11 19 |T 26 33 31 30 38 27 34 28 31 27 27 WRMS | 8 18 10 11 24 5 18 10 9 21 |NE 18 27 24 23 34 21 28 21 24 21 20 MEDI | 7 18 10 11 24 5 18 10 10 16 |MD 18 28 25 24 33 19 28 21 22 21 20 Table 3.1556.3 GPS week: 1556 Day: 3 MJD: 55139.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 21 --- --- --- --- 40 --- 17 44 --- 18 | 28 --- --- --- --- 50 --- 26 57 --- 28 2 | 5 24 11 11 24 4 22 12 8 19 5 | 39 41 42 43 48 38 42 38 40 34 38 3 | 6 13 10 8 15 5 10 7 9 13 3 | 22 21 26 27 25 21 24 22 20 22 21 4 | 10 15 8 12 18 8 16 10 12 18 4 | 53 55 50 52 59 52 63 57 59 54 54 5 | 8 23 13 14 31 4 25 7 10 21 5 | 14 31 18 18 45 13 30 16 18 15 14 6 | 4 15 9 10 18 5 10 6 13 11 3 | 24 26 30 30 28 26 29 27 26 22 25 7E | 7 21 9 14 34 5 25 10 8 15 4 | 18 22 18 22 34 16 24 19 20 23 16 X8E | 14 20 18 15 34 5 --- 21 19 34 8 | 36 29 25 32 24 43 --- 38 36 21 34 9E | 11 19 13 11 23 8 19 9 21 11 5 | 29 44 37 34 55 34 43 37 30 38 34 10 | 7 10 8 8 17 5 14 8 10 16 3 | 11 18 16 15 27 13 20 18 21 15 14 11 | 8 21 11 9 27 5 17 8 13 13 4 | 22 29 26 23 34 22 26 23 23 24 21 12 | 7 20 13 12 25 5 22 9 17 24 5 | 23 34 31 28 35 27 33 27 29 26 26 13 | 6 20 8 9 30 4 20 9 9 14 4 | 16 27 17 22 39 16 26 15 19 14 15 14 | 7 20 12 11 35 5 21 7 10 16 4 | 18 31 23 24 33 17 30 21 23 20 20 15 | 7 22 8 8 24 8 23 9 10 20 4 | 17 31 21 23 35 20 27 19 23 18 18 16 | 8 25 12 8 28 5 25 15 10 24 5 | 19 34 20 22 32 19 31 24 24 19 19 17 | 7 17 11 11 28 5 17 7 11 20 4 | 17 27 21 20 30 17 26 16 18 19 16 18 | 9 25 12 14 26 3 23 6 12 15 5 | 24 31 19 16 35 20 30 20 26 20 20 19 | 5 21 9 8 23 5 19 8 10 23 4 | 21 34 25 24 38 22 35 21 23 24 22 20 | 7 25 8 8 29 7 21 5 12 11 4 | 15 33 18 21 39 18 28 17 23 19 18 21E | 10 18 8 9 22 6 14 10 12 13 4 | 48 50 49 48 51 50 47 52 51 47 48 22 | 5 19 12 12 30 4 22 6 11 13 4 | 16 25 19 15 36 16 25 17 24 15 15 23 | 7 29 14 14 26 5 26 6 9 17 5 | 21 35 29 30 37 24 33 22 24 22 22 X24E | 55 45 --- 35 --- 28 --- 48 29 --- 23 | 112 83 --- 82 --- 84 --- 101 95 --- 88 X25E | 12 --- 31 --- --- 15 --- 14 24 --- 11 | 34 --- 9999 --- --- 9999 --- 9999 9999 --- 31 26 | 5 14 10 8 17 4 11 5 7 21 3 | 16 25 20 15 23 16 20 18 20 17 16 27E | 14 27 12 14 30 8 23 9 25 12 6 | 22 30 25 27 33 26 29 23 37 22 23 28 | 9 19 14 11 30 4 27 10 12 31 6 | 23 28 27 27 37 22 31 27 26 31 23 29 | 5 19 8 9 34 6 19 5 17 29 5 | 21 27 21 21 31 21 25 19 26 21 19 30 | 5 12 9 10 19 3 11 10 10 15 3 | 23 21 21 27 23 23 17 28 26 21 22 31E | 5 24 9 11 17 4 25 12 12 17 5 | 15 28 18 10 25 14 24 16 19 14 13 32 | 7 21 10 9 13 6 20 10 10 22 4 | 74 71 67 74 72 72 73 75 75 79 72 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 20 11 11 26 5 20 9 12 18 |T 27 34 26 29 36 28 31 29 31 25 27 WRMS | 7 20 11 11 23 5 19 8 9 19 |NE 22 30 24 24 34 23 29 23 27 23 22 MEDI | 7 20 10 11 26 5 20 9 11 17 |MD 22 30 23 24 35 22 29 22 24 21 21 Table 3.1556.4 GPS week: 1556 Day: 4 MJD: 55140.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 14 --- --- --- --- 23 --- 16 18 --- 11 | 23 --- --- --- --- 31 --- 25 32 --- 23 2 | 6 19 14 9 26 4 18 18 12 20 5 | 44 52 48 47 61 48 52 51 48 44 47 3 | 5 11 8 9 13 4 9 7 12 13 3 | 24 25 31 25 32 24 31 26 23 28 25 4 | 10 18 8 10 18 6 17 9 12 20 4 | 58 65 57 59 67 56 65 55 59 60 58 5 | 8 26 11 13 30 5 24 6 10 21 5 | 21 39 28 24 49 21 38 21 28 21 24 6 | 4 11 6 8 15 5 9 6 10 11 3 | 26 28 32 25 34 28 34 29 27 27 27 7E | 6 17 7 11 20 4 24 8 10 11 4 | 20 23 20 26 31 19 26 22 24 26 20 X8E | 22 42 28 21 40 18 --- 35 42 --- 14 | 30 35 40 32 33 47 --- 49 52 --- 29 9E | 13 19 14 13 16 6 21 10 20 11 5 | 28 38 41 35 46 31 41 35 26 36 33 10 | 8 11 9 8 16 6 15 9 10 15 3 | 19 28 26 22 33 19 29 23 26 22 22 11 | 6 15 9 9 30 5 17 5 8 12 3 | 17 21 23 22 36 17 25 19 19 20 17 12 | 6 19 10 9 26 7 24 9 10 24 5 | 21 32 32 32 34 25 33 24 28 27 26 13 | 5 21 7 13 27 4 20 7 8 15 4 | 18 29 20 26 39 20 28 21 26 23 20 14 | 5 21 8 10 33 7 22 10 8 14 4 | 23 32 29 27 39 23 32 29 28 27 26 15 | 7 23 11 12 26 7 27 7 9 19 5 | 21 34 23 25 39 23 35 23 25 21 23 16 | 8 23 10 9 27 6 23 12 12 24 5 | 22 34 31 26 33 25 37 27 23 24 25 17 | 6 15 9 10 29 7 15 8 16 20 4 | 18 28 24 22 34 21 27 21 29 25 21 18 | 7 25 13 11 28 5 23 8 7 16 5 | 28 38 30 20 41 28 37 27 32 26 27 19 | 5 18 9 7 24 5 20 9 12 25 4 | 20 34 27 24 41 23 37 22 25 26 23 20 | 5 22 7 8 29 6 20 5 14 11 4 | 18 31 21 19 41 19 28 20 23 22 19 21 | 9 18 10 6 25 7 14 9 12 7 4 | 40 40 43 36 47 41 41 38 46 36 39 22 | 4 20 10 10 26 5 20 5 7 13 4 | 24 33 28 22 40 25 33 25 28 24 25 23 | 6 29 13 12 25 5 24 6 9 18 5 | 20 35 25 27 33 21 32 23 25 23 22 X24E | 41 34 --- 33 --- 21 --- 29 169 --- 20 | 112 140 --- 133 --- 128 --- 144 209 --- 126 X25E | 15 28 29 25 --- 9 --- 16 41 --- 11 | 31 28 9999 37 --- 9999 --- 9999 9999 --- 32 26 | 6 12 9 8 18 5 9 8 8 16 3 | 21 29 27 23 30 22 27 26 26 24 24 27E | 14 27 10 12 19 7 25 11 28 12 6 | 29 35 36 35 38 33 33 34 49 32 32 28 | 8 18 10 11 25 7 24 10 17 33 5 | 25 27 26 30 31 22 29 26 28 29 24 29 | 6 18 8 8 31 6 20 6 9 28 4 | 20 27 21 21 30 21 28 23 22 25 20 30 | 5 13 9 8 21 6 12 7 7 13 3 | 24 23 22 28 28 23 20 27 28 22 24 31E | 3 20 11 9 22 6 21 10 13 12 4 | 19 30 25 21 33 21 32 21 29 23 22 32 | 8 21 11 10 12 5 19 9 10 19 4 | 32 30 26 29 29 28 36 30 32 29 28 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 19 10 10 24 6 20 9 12 18 |T 28 36 29 31 38 30 33 31 36 27 29 WRMS | 7 19 10 10 23 6 19 8 9 18 |NE 22 30 26 24 35 23 31 24 26 24 23 MEDI | 6 19 10 10 25 6 20 9 10 15 |MD 23 32 27 26 34 23 32 26 28 25 24 Table 3.1556.5 GPS week: 1556 Day: 5 MJD: 55141.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 18 --- --- --- --- 22 --- 16 21 --- 13 | 23 --- --- --- --- 33 --- 23 36 --- 23 2 | 7 24 6 11 20 4 22 13 7 23 5 | 30 38 36 37 43 34 37 39 38 33 34 3 | 8 12 6 6 15 5 11 8 11 14 3 | 19 27 21 15 25 18 26 15 17 22 18 4 | 8 18 8 11 11 5 14 8 8 20 4 | 34 43 34 41 41 38 41 33 41 37 35 5 | 8 24 9 14 29 5 25 11 6 20 5 | 14 32 21 20 48 16 31 19 15 16 17 X6 | 10 12 6 --- 17 6 11 7 10 12 3 | 23 28 22 --- 29 20 29 21 20 21 21 7E | 6 19 8 10 24 5 21 8 8 12 4 | 15 21 17 14 32 13 24 12 17 14 13 X8E | 7 --- --- --- --- 285 --- --- --- --- 0 | 34 --- --- --- --- 169 --- --- --- --- 32 9E | 11 21 10 15 14 8 22 13 21 15 5 | 35 42 44 42 43 35 42 43 31 41 38 10 | 9 14 6 11 16 4 14 10 10 15 4 | 16 25 18 17 32 17 25 21 21 19 17 11 | 8 17 9 11 29 4 20 7 11 12 4 | 18 26 17 20 37 16 25 16 17 16 14 12 | 7 19 7 11 25 5 26 11 7 24 5 | 21 29 22 25 32 22 30 21 25 24 21 13 | 6 21 6 12 26 5 22 5 7 16 4 | 16 28 17 24 37 18 29 17 19 18 16 14 | 8 16 9 14 32 6 21 8 7 11 4 | 20 28 26 21 30 20 27 23 24 20 22 15 | 8 24 7 11 26 5 24 8 7 19 4 | 18 29 20 25 39 18 29 17 17 19 17 16 | 8 21 11 9 25 6 22 10 10 24 5 | 17 32 20 19 32 18 31 18 18 18 18 17 | 9 16 12 15 34 8 18 15 12 22 5 | 14 23 14 22 35 15 24 18 20 17 14 18 | 8 24 9 13 24 4 25 7 7 15 4 | 20 32 20 15 33 18 32 19 19 21 18 19 | 8 17 6 5 23 5 19 9 11 24 4 | 22 33 25 21 36 21 34 15 19 21 20 20 | 5 19 7 12 26 5 20 6 7 11 4 | 14 25 17 22 36 15 23 14 16 13 14 21 | 7 18 5 8 32 5 14 8 6 9 3 | 28 32 26 24 42 25 30 24 20 26 24 22 | 5 18 8 10 24 5 19 6 6 11 3 | 19 27 24 14 35 19 27 19 20 19 19 23 | 7 26 9 17 27 5 24 8 10 16 5 | 19 34 24 30 35 23 31 20 24 22 21 X24 | 19 29 15 23 --- 29 --- 21 157 --- 10 | 55 61 64 70 --- 60 --- 65 83 --- 60 X25E | 11 19 15 13 --- 6 --- 15 22 --- 7 | 26 22 9999 22 --- 9999 --- 9999 9999 --- 22 26 | 7 12 8 10 17 5 11 8 5 13 3 | 17 23 21 12 21 16 20 19 18 15 18 27E | 13 28 8 12 18 5 25 11 32 14 7 | 37 42 41 43 40 42 38 39 56 39 40 28 | 10 17 9 10 27 5 24 12 8 32 5 | 23 26 21 24 34 21 29 25 22 23 20 29 | 7 18 5 12 35 4 21 12 9 29 5 | 15 20 13 15 28 13 22 19 15 17 13 30 | 6 14 9 7 19 5 13 8 6 15 3 | 19 19 22 22 22 19 16 20 21 19 18 31E | 6 18 7 10 15 7 23 9 11 12 4 | 14 26 18 15 26 16 25 17 18 13 15 32 | 9 21 10 20 14 7 21 7 9 19 5 | 49 49 46 55 49 48 50 50 50 51 48 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 20 8 12 24 5 21 9 11 18 |T 23 30 25 25 34 28 29 24 25 22 23 WRMS | 8 20 8 12 23 5 20 9 7 16 |NE 19 28 21 21 33 20 28 20 21 20 19 MEDI | 8 18 8 11 24 5 21 8 9 15 |MD 19 28 21 22 35 19 29 19 20 19 19 Table 3.1556.6 GPS week: 1556 Day: 6 MJD: 55142.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 13 --- --- --- --- 21 --- 18 19 --- 11 | 25 --- --- --- --- 35 --- 29 40 --- 27 2 | 8 25 8 15 20 6 27 20 12 23 6 | 34 38 36 39 46 35 38 37 34 37 34 3 | 7 13 9 5 19 2 13 9 10 18 3 | 21 25 27 25 26 20 28 21 19 24 21 4 | 9 18 6 15 14 3 17 9 15 21 5 | 53 59 56 53 59 53 59 54 51 60 54 5 | 10 27 10 10 28 5 26 17 8 21 5 | 17 33 22 22 45 17 31 25 18 20 18 6 | 7 13 9 6 20 4 11 7 10 16 3 | 29 30 33 31 29 27 32 30 25 27 28 7E | 7 17 7 10 20 6 22 12 11 15 4 | 13 22 19 17 31 16 22 16 16 16 13 X8E | 5 --- --- --- --- 311 --- --- --- --- 0 | 48 --- --- --- --- 81 --- --- --- --- 46 9E | 12 22 10 16 16 6 22 13 22 21 6 | 46 53 51 49 61 46 52 52 42 54 48 10 | 9 13 9 10 15 5 15 17 9 20 4 | 16 21 19 20 28 15 22 23 17 23 16 11 | 8 13 7 10 30 4 20 6 7 13 3 | 16 23 18 16 37 16 23 14 13 19 14 12 | 8 21 8 13 27 7 26 12 12 24 5 | 20 29 24 26 35 21 30 26 20 23 21 13 | 6 21 7 12 27 2 22 5 8 15 4 | 19 30 26 27 40 22 31 21 22 22 21 14 | 7 19 7 13 26 6 23 11 9 13 4 | 20 29 25 26 31 20 29 25 27 23 23 15 | 8 25 10 13 25 5 24 10 14 24 5 | 18 29 25 23 35 19 25 16 24 22 19 16 | 8 23 11 9 27 5 24 9 10 25 5 | 22 34 30 26 34 24 34 24 22 22 24 17 | 11 16 8 13 41 5 17 17 13 21 5 | 26 29 29 26 40 25 30 29 25 26 24 18 | 6 25 8 14 24 6 25 10 10 18 5 | 21 35 20 20 38 21 35 22 21 26 20 19 | 7 15 13 8 26 5 18 8 10 26 4 | 22 33 27 22 39 24 35 20 25 28 23 20 | 6 17 7 13 22 5 20 9 8 11 4 | 17 27 21 20 37 20 26 16 17 18 17 21 | 8 19 6 9 45 4 15 7 8 11 3 | 23 28 24 23 41 23 25 25 23 26 22 22 | 5 22 8 16 25 5 23 8 12 14 4 | 20 30 19 21 38 18 31 19 23 20 19 23 | 9 22 8 19 22 3 26 6 8 21 5 | 23 37 33 37 42 27 36 27 24 31 27 X24 | 13 22 18 17 --- 29 --- 21 151 --- 9 | 141 138 128 155 --- 142 --- 150 161 --- 147 X25E | 12 23 12 13 --- 6 22 15 25 --- 6 | 28 21 9999 21 --- 9999 13 9999 9999 --- 24 26 | 6 12 7 12 14 4 11 9 6 17 3 | 16 21 20 19 22 16 20 20 18 14 17 27E | 13 27 9 15 20 6 26 14 33 14 7 | 44 52 44 45 44 46 49 45 52 44 43 28 | 9 15 10 12 28 6 22 13 12 35 5 | 29 30 34 30 33 27 31 34 27 31 28 29 | 12 18 5 9 29 4 21 14 11 31 5 | 23 28 23 22 34 21 29 27 23 24 21 30 | 7 12 5 10 17 6 14 7 6 15 3 | 26 25 26 26 27 24 16 30 25 20 24 31E | 9 16 7 12 22 6 23 12 10 13 4 | 17 29 22 20 29 20 30 21 24 20 20 32 | 9 15 8 12 11 4 19 9 9 22 4 | 45 53 54 51 54 51 51 49 48 59 49 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 8 12 25 5 21 11 12 20 |T 29 35 32 31 37 31 31 31 30 27 29 WRMS | 8 19 8 12 23 5 20 9 11 20 |NE 22 30 26 25 35 23 29 24 23 24 22 MEDI | 8 18 8 12 22 5 22 10 10 18 |MD 22 29 26 25 37 23 30 25 24 23 23 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 4.1556 GPS week: 1556 MJD: 55136.0-55142.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3003 |U 11 9 30 |U 8 10 29 |U 8 8 18 | emr | emr 2855 | 19 14 53 |U 11 11 32 | 8 8 20 | esa | esa 2893 | 11 12 33 |U 8 9 27 | 8 7 16 | gfz | gfz 2859 |U 27 25 79 |U 20 28 86 | 22 19 50 | grg | grg 2756 | 11 10 36 |U 10 11 31 | 8 8 21 | igr | igr 2884 | 13 13 37 | 9 12 34 | 9 11 21 | igs | igs 2918 | 12 11 33 | 9 12 32 | 8 9 20 | jpl | jpl 2689 | 16 17 46 |U 11 11 35 |U 8 8 22 | mit | mit 3017 |U 11 11 35 |U 18 17 47 |U 9 8 18 | 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 5.1556.0 GPS week: 1556 Day: 0 MJD: 55136.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2944 | 14 11 31 | 7 12 24 | 8 9 17 | emr | emr 2850 | 20 13 56 | 12 13 25 | 6 6 15 | esa | esa 2880 | 14 11 34 | 7 10 20 | 8 8 13 | gfz | gfz 2922 | 26 15 46 | 19 33 43 | 10 11 25 | grg | grg 2784 | 15 13 37 | 8 11 31 | 9 10 17 | igr | igr 2939 | 13 12 34 | 8 12 25 | 8 8 16 | igs | igs 2843 | 17 11 36 | 12 16 27 | 7 6 15 | jpl | jpl 2671 | 16 14 41 | 14 16 34 | 8 6 22 | mit | mit 2976 | 14 11 33 | 21 21 42 | 10 11 18 | Table 5.1556.1 GPS week: 1556 Day: 1 MJD: 55137.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2952 | 8 6 29 | 7 9 28 | 5 4 17 | emr | emr 2839 | 18 9 30 | 11 10 42 | 8 7 20 | esa | esa 2880 | 9 8 40 | 6 9 29 | 6 6 19 | gfz | gfz 2918 | 16 11 48 | 13 16 48 | 12 16 47 | grg | grg 2784 | 10 9 46 | 10 9 38 | 8 10 28 | igr | igr 2872 | 9 7 40 | 7 10 31 | 6 6 19 | igs | igs 2871 | 10 10 47 | 8 11 37 | 5 6 18 | jpl | jpl 2671 | 10 10 59 | 9 9 43 | 10 10 29 | mit | mit 2976 | 11 10 31 | 21 17 69 | 5 6 16 | Table 5.1556.2 GPS week: 1556 Day: 2 MJD: 55138.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3037 | 10 14 20 | 7 11 23 | 7 6 12 | emr | emr 2846 | 35 15 117 | 11 12 34 | 7 6 19 | esa | esa 2975 | 10 16 23 | 7 8 25 | 7 6 13 | gfz | gfz 2916 | 14 11 41 | 30 31 153 | 15 17 52 | grg | grg 2784 | 10 13 29 | 12 15 42 | 8 6 21 | igr | igr 2921 | 10 12 29 | 7 11 28 | 8 8 17 | igs | igs 2956 | 12 14 35 | 9 13 29 | 7 6 17 | jpl | jpl 2675 | 15 15 48 | 9 11 36 | 8 7 18 | mit | mit 3072 | 10 10 48 | 18 20 48 | 11 10 23 | Table 5.1556.3 GPS week: 1556 Day: 3 MJD: 55139.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3002 | 6 8 17 | 7 8 22 | 8 7 16 | emr | emr 2845 | 12 17 26 | 10 10 25 | 13 11 33 | esa | esa 2880 | 7 11 15 | 6 7 28 | 9 6 19 | gfz | gfz 2829 | 69 84 220 | 23 42 137 | 48 36 120 | grg | grg 2784 | 8 7 22 | 7 7 22 | 9 8 23 | igr | igr 2847 | 8 13 24 | 6 7 24 | 7 7 13 | igs | igs 2972 | 8 13 18 | 7 7 27 | 8 6 16 | jpl | jpl 2679 | 15 31 31 | 7 7 27 | 9 9 21 | mit | mit 3072 | 12 20 31 | 20 16 51 | 10 7 13 | Table 5.1556.4 GPS week: 1556 Day: 4 MJD: 55140.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2996 | 8 8 23 | 6 10 29 | 6 7 15 | emr | emr 2927 | 11 10 48 | 9 9 28 | 7 8 17 | esa | esa 2880 | 9 9 26 | 6 10 27 | 7 8 19 | gfz | gfz 2876 | 26 31 100 | 13 16 51 | 22 16 38 | grg | grg 2784 | 9 6 29 | 6 10 27 | 7 8 20 | igr | igr 2877 | 12 11 38 | 11 16 38 | 11 19 35 | igs | igs 2961 | 11 6 23 | 7 11 28 | 9 11 29 | jpl | jpl 2679 | 33 29 71 | 12 10 27 | 6 7 21 | mit | mit 3072 | 8 6 45 | 8 13 36 | 8 8 17 | Table 5.1556.5 GPS week: 1556 Day: 5 MJD: 55141.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3041 | 19 7 53 | 7 7 37 | 9 10 28 | emr | emr 2848 | 20 15 47 | 9 9 30 | 8 11 22 | esa | esa 2880 | 9 9 38 | 10 8 32 | 8 8 16 | gfz | gfz 2728 | 12 13 33 | 30 41 78 | 34 21 47 | grg | grg 2688 | 9 8 27 | 13 11 33 | 8 10 22 | igr | igr 2838 | 16 17 45 | 14 16 49 | 13 18 31 | igs | igs 2917 | 12 8 35 | 11 11 38 | 12 19 29 | jpl | jpl 2678 | 8 9 36 | 13 11 41 | 9 10 23 | mit | mit 2976 | 8 7 27 | 23 13 38 | 11 12 25 | Table 5.1556.6 GPS week: 1556 Day: 6 MJD: 55142.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3053 | 15 11 38 | 13 12 39 | 11 12 22 | emr | emr 2832 | 18 19 43 | 14 13 42 | 8 8 17 | esa | esa 2880 | 18 18 53 | 11 12 32 | 9 7 12 | gfz | gfz 2829 | 26 14 68 | 15 16 92 | 15 14 24 | grg | grg 2688 | 18 11 60 | 11 12 28 | 8 7 14 | igr | igr 2895 | 21 16 46 | 13 13 42 | 10 8 20 | igs | igs 2906 | 17 13 37 | 13 12 41 | 10 11 17 | jpl | jpl 2772 | 16 11 36 | 11 11 34 | 9 8 18 | mit | mit 2976 | 15 13 33 | 14 16 44 | 9 6 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 6.1556 GPS week: 1556 MJD: 55136.500-55142.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -6 9 6 32 2 | 5 20 | 24 18 108 108 6 | 2 emr uuuuu | -18 53 -92 -204 -10 | 74 77 | 26 19 101 103 11 | 3 esa uuuuu | -11 -12 -73 108 -9 | 14 24 | 67 39 170 80 9 | 2 gfz uuuuu | 10 -15 88 -50 5 | -3 18 | 16 22 72 80 3 | 3 grg --xxx | -- -- -41 -102 10 | 11 20 | -- -- 229 158 24 | 3 igr xxxxx | -5 59 -10 -65 3 | -4 16 | 17 26 131 107 10 | 2 irf xxxxx | 2 3 33 48 -8 | 3 19 | 13 9 32 15 6 | 2 jpl uuuuu | -20 39 -84 -45 -2 | 25 32 | 27 28 179 135 15 | 2 mit uuuuu | 10 -16 -36 64 -8 | 21 30 | 28 10 101 153 9 | 2 ngs uuuuu | -16 10 192 33 2 | 3 13 | 81 45 138 153 6 | 2 sio uuuuu | 82 -18 -171 -49 1 | 45 50 | 18 18 126 153 9 | 3 Table 7.1556.0 GPS week: 1556 Day: 0 MJD: 55136.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -58 33 -128 148 9 | 2 12 emr uuuuu | -38 31 -177 -306 -2 | 74 75 esa uuuuu | 100 27 205 213 6 | 11 16 gfz uuuuu | 9 -12 54 -153 9 | -9 13 grg --xxx | -- -- -543 -320 -8 | 7 18 igr xxxxx | -16 106 150 -243 -4 | -7 13 irf xxxxx | 24 9 43 72 6 | 0 11 jpl uuuuu | -34 -1 -179 -241 -16 | 26 28 mit uuuuu | 58 -30 -143 272 12 | 17 21 ngs uuuuu | -157 12 194 -89 -9 | -2 10 sio uuuuu | 110 -34 -305 133 21 | 39 40 Table 7.1556.1 GPS week: 1556 Day: 1 MJD: 55137.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -5 7 -145 -62 -5 | 7 21 emr uuuuu | -54 36 -104 -327 -19 | 79 81 esa uuuuu | 49 21 -93 115 -10 | 16 25 gfz uuuuu | -11 -25 45 -5 1 | -4 19 grg --xxx | -- -- 83 -26 19 | 9 22 igr xxxxx | 6 46 174 -15 9 | -4 17 irf xxxxx | 6 17 -36 47 -10 | 5 20 jpl uuuuu | -37 45 221 -158 -23 | 29 32 mit uuuuu | 20 -7 -204 202 -9 | 23 31 ngs uuuuu | -41 -33 311 -52 10 | 1 15 sio uuuuu | 79 8 -351 41 4 | 45 50 Table 7.1556.2 GPS week: 1556 Day: 2 MJD: 55138.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 5 31 96 -128 -5 | 6 22 emr uuuuu | -10 62 -87 -269 -27 | 77 80 esa uuuuu | -22 29 -227 155 -3 | 16 26 gfz uuuuu | 30 -43 126 -68 4 | -4 19 grg --xxx | -- -- 7 -103 11 | 11 22 igr xxxxx | -20 75 -55 -160 0 | -3 16 irf xxxxx | 7 9 37 43 -9 | 5 20 jpl uuuuu | -63 48 40 -159 -2 | 26 32 mit uuuuu | 25 -16 -35 160 -9 | 23 31 ngs uuuuu | -34 -29 306 -67 1 | 3 14 sio uuuuu | 97 -19 -210 39 1 | 46 51 Table 7.1556.3 GPS week: 1556 Day: 3 MJD: 55139.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -3 2 19 1 0 | 3 21 emr uuuuu | 25 83 -179 -78 -7 | 73 76 esa uuuuu | -43 -47 -218 61 -6 | 15 25 gfz uuuuu | 3 15 175 -75 2 | -4 19 grg --xxx | -- -- -50 -134 -24 | 10 21 igr xxxxx | 10 56 9 -78 2 | -5 16 irf xxxxx | -3 -8 38 41 -12 | 3 21 jpl uuuuu | 6 92 -108 66 18 | 23 30 mit uuuuu | 8 -25 0 60 -10 | 21 31 ngs uuuuu | -37 5 328 -99 0 | 2 14 sio uuuuu | 85 -43 -168 23 -4 | 44 50 Table 7.1556.4 GPS week: 1556 Day: 4 MJD: 55140.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 0 3 45 11 3 | 4 22 emr uuuuu | 2 53 -172 -121 7 | 72 76 esa uuuuu | -70 -61 -146 33 -8 | 15 25 gfz uuuuu | 15 2 157 83 7 | -2 20 grg --xxx | -- -- 118 15 -6 | 12 20 igr xxxxx | 20 50 -104 48 21 | -3 16 irf xxxxx | -14 -2 41 44 -11 | 3 21 jpl uuuuu | 5 38 -29 77 11 | 25 32 mit uuuuu | -29 -15 55 -67 -15 | 22 31 ngs uuuuu | 78 54 80 107 0 | 3 15 sio uuuuu | 60 -11 -78 -169 -4 | 46 51 Table 7.1556.5 GPS week: 1556 Day: 5 MJD: 55141.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 6 8 144 157 -1 | 6 22 emr uuuuu | -19 66 -19 -100 -10 | 73 77 esa uuuuu | -89 -48 -159 -2 -17 | 13 24 gfz uuuuu | 28 -40 94 -5 4 | 0 18 grg --xxx | -- -- 10 129 31 | 15 18 igr xxxxx | -20 24 -181 45 -1 | -1 17 irf xxxxx | -12 -7 63 62 -10 | 4 20 jpl uuuuu | 7 24 -218 67 -6 | 26 34 mit uuuuu | -13 -21 62 -35 -15 | 23 31 ngs uuuuu | 82 85 167 118 7 | 6 13 sio uuuuu | 60 -26 -20 -98 -7 | 48 53 Table 7.1556.6 GPS week: 1556 Day: 6 MJD: 55142.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 16 -18 11 101 9 | 4 23 emr uuuuu | -29 39 93 -226 -10 | 70 74 esa uuuuu | -2 -8 125 179 -23 | 10 26 gfz uuuuu | -5 -5 -32 -123 10 | -1 19 grg --xxx | -- -- 90 -274 44 | 15 19 igr xxxxx | -16 58 -63 -54 -9 | -3 19 irf xxxxx | 6 6 44 26 -7 | 1 23 jpl uuuuu | -26 29 -314 34 5 | 24 33 mit uuuuu | 3 0 15 -140 -11 | 20 32 ngs uuuuu | -6 -23 -44 314 3 | 4 14 sio uuuuu | 82 1 -65 -313 -3 | 46 52