Date: Thu, 12 Nov 2009 17:16:03 +0000 From: Jim Ray Subject: [IGSREPORT-17989] Wk 1555 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4afc42d3.tF8Sb4QxZZc0MaLa%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 12 Nov 09:16:28 PST 2009 Message Number 17989 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1555 (Oct 25, 2009 - Oct 31, 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: igs1555[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1555[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1555[0-6].cls IGS GPS clock combination summary report. igs15557.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15557.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 1 24 0 | COD | 24 4 9 25 27 0 | EMR | SYOG 0 | ESA | 4 8 9 25 27 SYOG 0 | GFZ | 8 30 31 ABPO AUCK BJFS BOR1 BUE1 COCO CONZ DAEJ HARB 0 | GFZ | HOLM HRAO HYDE JPLM KERG KOUR MBAR METS NICO NYA1 0 | GFZ | ONSA OUS2 QAQ1 SANT SEY1 SFER SSIA SUTH WSRT WTZR 0 | GFZ | YELL YKRO ZIMM 0 | GRG | ONSA POTS 0 | JPL | 32 0 | MIT | 8 HARB 1 | ALL | 1 1 | COD | 24 4 9 27 1 | ESA | 4 8 9 27 UNSA WTZR 1 | GFZ | 2 4 7 8 9 21 27 31 ALGO AUCK BAKO BOR1 BRFT CHUR 1 | GFZ | COCO DAEJ FAA1 GUAM HARB IRKT KIRU MAS1 MAW1 MIZU 1 | GFZ | NYAL ONSA QAQ1 WHIT WSRT WTZR ZIMM 1 | GRG | ONSA POTS 1 | JPL | 32 DGAR 1 | MIT | IRKT MIZU IRKT MIZU SYDN TRO1 2 | COD | 9 2 | ESA | 4 9 CEDU UNSA 2 | GFZ | 2 5 19 CAS1 COCO DAEJ HARB HRAO HRM1 IRKT JPLM KARR 2 | GFZ | KIT3 ONSA PDEL RABT TSKB VILL YKRO ZECK 2 | GRG | ONSA 2 | JPL | 32 DGAR 2 | MIT | 24 24 3 | ALL | 1 1 3 | COD | 9 3 | EMR | SUTM 3 | ESA | 9 CEDU WTZR 3 | GFZ | 5 8 12 19 24 ALRT AREQ ASPA AUCK BAKO BOR1 BRFT CAS1 3 | GFZ | CHPI COCO CONZ FAA1 GODE GRAZ GUAM HRM1 KIT3 MAC1 3 | GFZ | MAS1 MBAR MIZU NICO NYA1 NYAL OUS2 PIE1 PIMO RAMO 3 | GFZ | RIOP SANT SFER SSIA STJO TRO1 UNSA WSRT YKRO 3 | GRG | ONSA WROC 3 | JPL | 4 32 DGAR 3 | MIT | 24 MIZU 4 | ALL | 1 4 | COD | 27 4 8 27 4 | EMR | 9 4 | ESA | 4 8 9 27 CEDU UNSA WTZR 4 | GFZ | 9 16 24 BAKO BRFT BUE1 CHPI CONZ DAV1 DGAR DUBO FLIN 4 | GFZ | GUAT HRM1 HYDE ISPA KIRU KIT3 MAS1 MBAR MIZU NRC1 4 | GFZ | NYA1 ONSA QAQ1 RESO SANT SEY1 WAB2 WHIT WSRT YELL 4 | GFZ | YKRO ZECK 4 | GRG | WTZR 4 | JPL | 32 DGAR 4 | MIT | 24 24 5 | ALL | 1 1 5 | COD | 9 9 YAKT 5 | EMR | CHUR 5 | ESA | 8 9 UNSA 5 | GFZ | 5 9 11 17 AREQ BOGT COCO DAEJ FAA1 FLIN HOLM HRAO 5 | GFZ | HYDE IISC ISPA KIRU KIT3 MAL2 MBAR MIZU RAMO RIOP 5 | GFZ | SEY1 SFER STJO SUTH SYOG TEHN TOW2 TRO1 WHIT WSRT 5 | GFZ | XMIS ZECK 5 | GRG | ONSA 5 | JPL | 32 DGAR 5 | MIT | 24 32 24 IRKT 6 | ALL | 1 6 | COD | 9 4 8 9 24 6 | ESA | 4 8 9 24 27 UNSA 6 | GFZ | 1 2 4 9 21 24 ALGO AREQ AUCK CHAT CHUR GODE GUAM 6 | GFZ | HRM1 IRKT KIRU MAL2 MAS1 MBAR NYA1 RABT RESO SANT 6 | GFZ | SYOG TOW2 TSKB VILL WSRT YKRO 6 | GRG | ONSA ULAB 6 | JPL | 32 DGAR 6 | MIT | 27 6 | NGS | 1 5. New clock offsets and drifts were estimated for centres showing reference clock resets. Note that only the largest clock offset and drift are output to the summary file. However, the clock combination and the listed RMS include all the clock segments. In summary, the following clock shifts/resets were noticed and accounted for: Day | Centre | Time | Jump ----+--------+--------+------------- 3 | GFZ | ~21:30 | ~ -0.56 ns 6. The following orbit solutions were excluded from the combination because they were biasing the weighted average (generally indicated by long arc RMS). They were still used for statistics computation. Day | Centre | PRN list ----+--------+--------------- 1 | COD | 25 1 | SIO | 25 7. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G09 | | | | 1 | | | | 8. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447. 9. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .4 1.1 .9 -8 -11 -1 -.28 EMR | 1.1 3.8 13.0 75 -15 43 .29 ESA | 7.5 5.8 12.8 107 -19 61 -.25 GFZ | .3 1.4 .8 23 -13 -3 -.16 JPL | 5.8 5.9 18.6 17 15 -22 .25 MIT | 4.5 6.5 10.8 3 17 -46 -.23 NGS | 7.8 3.6 10.2 55 -60 -19 -.19 SIO | 7.9 9.5 5.4 174 -87 1 .15 10. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 11. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 12. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five parts. The first, Table 1, summarizes all statistics for the week. It contains means and standard deviations over the week of satellite ephemeris and clock correction transformation parameters for each centre (table 1.1555.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1555.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 2.1555.[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 3.1555.[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 5.1555.0-6). 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 1555 summary. (Oct 25, 2009 - Oct 31, 2009) Table 1.1555.a GPS week: 1555 MJD: 55129.000-55135.000 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 230| 0 0 1 98 -12 -4 -.17 9 8 | -245 -293 22 79 | 0 0 0 19 12 28 .01 | 296 664 emr 93| 0 1 4 -72 -11 37 .61 19 19 | 525 -906 16 79 | 2 1 1 33 11 19 .03 | 2043 952 esa 129| 0 -1 0 -84 15 -3 .33 10 10 | -351 138 21 124 | 1 1 2 13 29 40 .03 | 596 1110 gfz 193| 1 0 -2 45 -34 -8 -.15 12 12 | -44 228 35 126 | 1 0 1 50 47 13 .03 | 442 1001 grg 107| 0 2 9 82 -62 18 1.02 27 25 | 321 -562 74 228 | 1 0 2 29 14 15 .02 | 253 349 igr n/a| 0 0 0 86 -31 -53 .05 5 5 | 1188 -565 24 82 | 0 0 0 23 18 22 .02 | 1329 1043 jpl 130| 0 0 3 39 -72 38 .61 19 19 | 1585 -997 17 92 | 1 1 1 26 8 32 .01 | 2040 1035 mit 263| 0 0 -4 95 -85 -21 -.31 13 10 | -15099 -964 23 113 | 0 0 1 28 16 11 .02 | 292 1060 ngs 222| 0 0 1 -37 97 -1 -.16 10 8 | -245108 73559 2094 15894 | 0 0 1 38 40 32 .03 | 389266 197287 sio 260| 1 1 0 -249 106 -4 -.12 19 18 | --- --- --- --- | 1 0 1 21 9 15 .02 | --- --- Table 1.1555.b GPS week : 1555 MJD: 55129.000-55135.000 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 | 11 11 13 12 14 15 16 | 2 | 5 5 6 5 5 5 6 | 3 | 4 4 4 4 4 4 4 | 4 | 12 11 9 6 5 5 5 | 5 | 6 6 6 5 5 5 5 | 6 | 4 4 4 3 3 3 4 | 7 | 6 5 5 5 5 5 5 | 8 | 9 15 7 7 7 6 6 | 9 | 6 7 8 8 9 6 6 | 10 | 4 5 5 3 4 4 4 | 11 | 4 4 4 3 4 4 5 | 12 | 5 5 5 5 5 5 5 | 13 | 5 6 5 5 4 5 5 | 14 | 5 4 4 4 4 5 6 | 15 | 5 5 5 5 5 5 5 | 16 | 5 5 5 5 5 6 6 | 17 | 5 5 5 5 5 5 5 | 18 | 5 5 5 5 4 4 5 | 19 | 5 6 5 5 5 5 5 | 20 | 5 5 5 5 4 5 6 | 21 | 4 4 4 3 4 4 5 | 22 | 5 4 5 5 5 5 5 | 23 | 5 6 6 5 5 5 6 | 24 | 12 12 12 13 11 11 14 | 25 | 6 16 --- --- --- --- --- | 26 | 4 4 4 4 4 4 5 | 27 | 5 5 5 6 6 6 6 | 28 | 5 6 6 6 5 6 6 | 29 | 6 5 5 5 5 6 6 | 30 | 5 4 3 3 3 4 5 | 31 | 5 5 5 5 4 5 6 | 32 | 4 4 5 4 4 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 2.1555.0 GPS week: 1555 Day: 0 MJD: 55129.000 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 230| 0 0 1 71 -20 -4 -.17 10 8 | -90 -611 13 64 | 38 -11 | emr 93| 0 2 4 -141 -2 76 .64 20 20 | 2370 236 17 86 | 58 -18 | esa 129| 0 -1 -2 -80 3 -57 .37 11 10 | -705 1366 20 135 | -19 7 | gfz 193| 0 0 -3 122 26 0 -.17 12 12 | 624 -1212 29 130 | 16 -39 | grg 107| -3 2 7 39 -91 8 1.02 27 25 | 402 -298 71 210 | 43 65 | igr n/a| 0 -1 0 53 -22 -74 .07 6 6 | 1666 708 26 72 | -54 -49 | jpl 130| 0 1 1 1 -56 34 .63 19 19 | 2490 243 17 90 | -3 6 | mit 263| 0 0 -3 149 -81 -12 -.33 15 9 | -15507 114 19 102 | 0 7 | ngs 222| 0 0 1 -106 75 27 -.15 10 7 | 8810 9095 1889 3599 | -7 23 | sio 260| 0 1 0 -209 95 1 -.12 19 18 | --- --- --- --- | 111 -38 | Table 2.1555.1 GPS week: 1555 Day: 1 MJD: 55130.000 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 230| 0 0 1 121 -10 32 -.18 9 8 | -463 -180 18 85 | -32 21 | emr 93| 3 4 5 -43 -24 41 .64 20 20 | 2349 -1464 16 80 | 5 36 | esa 129| -1 -2 1 -66 -14 8 .31 10 9 | 60 -635 16 106 | 6 19 | gfz 193| 1 0 -3 13 -37 -13 -.20 12 12 | 124 101 31 112 | 0 -47 | grg 107| 0 3 8 123 -64 43 .99 26 24 | 713 -1194 72 231 | -34 65 | igr n/a| 0 0 0 120 -13 -86 .05 5 5 | 2098 -1017 24 87 | -44 -22 | jpl 130| 1 0 3 53 -70 67 .60 20 20 | 3639 -1580 19 95 | 1 40 | mit 263| -1 0 -5 72 -71 -17 -.33 15 11 | -15008 307 24 123 | 16 13 | ngs 222| 0 0 1 6 110 -63 -.16 12 10 | -999999 360077 2452 4126 | 29 38 | sio 260| 0 1 -1 -266 106 -9 -.13 17 18 | --- --- --- --- | 109 -45 | Table 2.1555.2 GPS week: 1555 Day: 2 MJD: 55131.000 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 230| 0 0 1 93 -17 11 -.17 9 7 | 230 -1079 33 101 | -17 -1 | emr 93| -2 1 4 -75 -21 37 .63 19 19 | 1413 -184 20 89 | -3 19 | esa 129| 0 -1 0 -105 12 -13 .32 11 11 | 144 -80 24 131 | 27 2 | gfz 193| 3 0 -2 63 -36 -9 -.10 13 13 | -69 411 42 133 | -19 -35 | grg 107| 0 3 10 96 -63 21 1.05 28 26 | 499 -240 72 246 | -15 19 | igr n/a| 0 0 0 71 -41 -61 .07 5 5 | 1744 236 22 73 | -46 10 | jpl 130| 0 0 1 42 -76 84 .60 19 19 | 2864 -216 17 96 | -3 50 | mit 263| 0 0 -4 110 -69 -23 -.33 13 9 | -14804 -859 25 114 | -1 10 | ngs 222| 0 0 1 -49 95 -20 -.14 10 9 | -17886 25196 2100 88744 | 16 54 | sio 260| 0 1 0 -247 113 -15 -.12 18 18 | --- --- --- --- | 103 -44 | Table 2.1555.3 GPS week: 1555 Day: 3 MJD: 55132.000 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 230| 0 0 0 106 -23 2 -.18 7 6 | -275 -536 27 71 | -15 36 | emr 93| 1 3 4 -78 -20 20 .57 18 18 | 1308 -1084 13 61 | -9 17 | esa 129| 0 -1 1 -99 26 57 .35 9 9 | -889 -157 25 128 | -6 -44 | gfz 193| 0 0 -2 10 -12 -25 -.15 12 12 | -10 -248 42 117 | 2 -29 | grg 107| 1 2 12 85 -57 17 1.02 26 22 | 260 -752 69 241 | -7 27 | igr n/a| 0 -1 0 71 -39 -38 .06 5 5 | 2045 -623 26 95 | -22 -1 | jpl 130| 1 0 2 19 -79 27 .63 19 19 | 2525 -1141 15 92 | 12 75 | mit 263| -1 0 -4 96 -66 -34 -.33 11 10 | -15003 -1798 30 124 | 23 28 | ngs 222| 0 -1 1 -15 75 -10 -.18 11 9 | -541067 314744 1962 3539 | -57 57 | sio 260| 0 1 0 -253 122 -29 -.14 19 18 | --- --- --- --- | 117 -40 | Table 2.1555.4 GPS week: 1555 Day: 4 MJD: 55133.000 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 230| 0 0 1 102 2 -30 -.16 9 7 | -125 -592 16 77 | -24 -16 | emr 93| -1 0 5 -58 -6 39 .64 19 19 | 615 -2157 15 78 | -21 18 | esa 129| 0 -2 -1 -79 -4 35 .35 9 9 | -205 -488 18 114 | 23 5 | gfz 193| 1 1 -2 8 -74 -22 -.14 11 11 | 50 -229 29 136 | -3 -35 | grg 107| 0 2 4 98 -55 2 1.03 28 24 | 271 -613 80 209 | -56 -8 | igr n/a| 0 0 0 88 -14 -41 .05 5 4 | 1860 -1848 22 87 | -75 -1 | jpl 130| 0 -1 4 74 -65 -8 .62 18 18 | 1861 -2273 16 95 | -45 -53 | mit 263| -1 0 -3 76 -105 -15 -.31 11 9 | -14919 -2329 18 105 | 5 32 | ngs 222| 0 0 0 -10 145 13 -.20 9 7 | -190381 -204654 1952 3932 | -6 -45 | sio 260| 2 0 2 -260 101 7 -.15 18 18 | --- --- --- --- | 107 -48 | Table 2.1555.5 GPS week: 1555 Day: 5 MJD: 55134.000 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 230| 0 0 0 77 7 12 -.16 8 7 | -287 -76 32 77 | 16 -16 | emr 93| -1 0 4 -44 8 19 .59 20 20 | -1143 -1770 17 76 | -50 -20 | esa 129| 1 -3 -2 -84 8 -23 .35 10 10 | 367 -1022 26 126 | -19 12 | gfz 193| 0 0 -2 100 -112 -2 -.15 12 12 | -163 768 43 127 | 0 -16 | grg 107| 1 1 10 48 -58 33 .99 25 23 | 195 -618 89 223 | 36 -9 | igr n/a| 0 0 0 91 -23 -51 .02 6 5 | 457 -1797 26 82 | -119 -20 | jpl 130| 0 1 3 20 -79 11 .62 20 20 | -22 -2078 23 97 | -31 -65 | mit 263| 0 0 -3 97 -98 -38 -.29 11 10 | -15524 -268 25 101 | 13 15 | ngs 222| 0 0 3 -66 144 28 -.13 9 7 | 15269 957 2117 3531 | 37 -23 | sio 260| 3 3 0 -234 94 -2 -.08 20 17 | --- --- --- --- | 105 -48 | Table 2.1555.6 GPS week: 1555 Day: 6 MJD: 55135.000 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 230| 1 0 1 118 -24 -52 -.17 9 9 | -708 1019 20 80 | -49 15 | emr 93| -3 0 1 -66 -13 24 .58 18 18 | -3234 75 18 86 | -9 30 | esa 129| 1 0 -4 -77 75 -33 .29 12 11 | -1230 1987 20 129 | 8 -31 | gfz 193| 0 0 0 -3 6 11 -.13 13 13 | -866 2009 35 128 | 15 20 | grg 107| -1 3 12 84 -43 2 1.03 29 31 | -92 -219 69 237 | 20 57 | igr n/a| 0 0 1 112 -66 -21 .04 5 5 | -1554 381 27 79 | -81 29 | jpl 130| -1 -2 5 61 -77 54 .61 20 19 | -2259 63 17 81 | -6 107 | mit 263| 0 0 -3 66 -102 -5 -.27 13 12 | -14932 -1919 20 122 | 19 11 | ngs 222| 0 0 1 -20 31 12 -.13 9 7 | 9498 9503 2192 3787 | -36 111 | sio 260| 3 2 1 -274 111 17 -.11 22 19 | --- --- --- --- | 94 -71 | 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 3.1555.0 GPS week: 1555 Day: 0 MJD: 55129.000 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 --- --- 20 --- 23 --- 12 21 --- 10 | 20 --- --- 27 --- 40 --- 26 38 --- 26 2E | 9 27 12 11 19 5 23 9 7 15 5 | 20 31 18 17 24 19 26 18 19 24 18 3 | 7 11 10 9 15 4 9 6 8 19 3 | 17 18 25 23 18 19 20 23 18 24 19 4E | 21 24 20 17 30 11 22 59 24 29 11 | 136 145 144 137 147 142 148 151 144 148 142 5 | 9 25 11 15 32 5 24 10 10 20 5 | 20 37 30 27 44 27 35 25 25 22 24 6 | 7 13 9 11 16 6 9 9 8 15 3 | 21 21 26 27 18 21 21 27 20 23 22 7E | 11 26 8 17 37 5 22 14 7 11 5 | 14 27 18 19 43 16 26 16 21 17 16 X8E | 18 28 19 21 404 9 --- 13 23 --- 9 | 53 52 57 61 217 50 --- 53 49 --- 51 9E | 17 19 13 17 18 8 18 12 14 15 6 | 66 67 69 65 68 67 65 68 66 63 66 10 | 8 13 10 8 19 4 12 10 10 19 4 | 21 18 23 19 21 19 18 20 25 20 19 11 | 8 13 7 9 26 5 13 7 6 14 3 | 12 19 18 15 36 17 19 18 20 22 16 12 | 8 17 8 9 26 6 22 7 8 25 4 | 19 23 24 23 30 20 27 20 25 25 21 13 | 9 22 12 12 33 5 23 15 8 15 5 | 17 32 24 20 40 20 31 20 25 19 20 14 | 8 16 9 11 31 7 19 11 7 16 4 | 23 31 28 24 38 23 33 21 27 20 24 15 | 10 20 13 13 27 7 26 8 8 15 5 | 18 25 25 19 29 18 25 15 20 19 18 16 | 7 19 8 11 26 4 20 10 8 30 5 | 18 28 23 24 30 18 28 20 21 23 20 17 | 10 20 11 10 30 10 21 8 10 24 5 | 12 33 17 13 40 17 32 17 19 19 15 18 | 8 20 11 14 26 6 21 6 9 14 4 | 14 32 23 15 41 16 32 15 22 17 18 19 | 8 23 9 10 25 4 22 8 10 24 5 | 19 35 19 14 38 21 33 18 21 24 20 20 | 6 23 9 11 25 7 21 11 12 12 4 | 14 31 20 17 40 18 30 15 20 15 15 21E | 7 14 7 9 44 4 18 7 11 9 3 | 14 23 16 16 36 16 23 17 21 16 16 22 | 7 17 11 12 29 5 18 10 11 15 4 | 19 31 23 20 39 18 29 21 25 20 20 23 | 8 26 13 11 27 4 24 10 8 16 5 | 15 33 23 20 36 18 32 17 21 16 17 X24E | 23 26 24 27 --- 13 --- 28 31 --- 12 | 47 48 63 43 --- 43 --- 49 47 --- 48 X25E | 9 18 12 13 --- 4 --- 15 13 23 5 | 150 16 20 7 --- 31 --- 19 9 25 20 26 | 9 13 8 6 18 4 10 10 10 14 3 | 20 30 24 17 33 21 28 23 25 19 23 27E | 13 19 12 14 20 7 17 10 10 17 5 | 20 27 25 22 28 22 27 18 23 16 20 28 | 7 17 9 12 30 4 21 9 10 29 5 | 23 31 33 31 35 27 29 31 28 27 27 29 | 8 19 9 8 36 5 22 6 13 33 5 | 18 33 25 13 45 21 34 17 23 23 20 X30 | 8 13 10 9 17 6 --- 13 15 --- 5 | 28 28 34 27 34 27 --- 31 28 --- 29 31E | 8 21 10 11 20 6 17 10 9 11 4 | 15 33 21 16 31 18 29 16 21 19 19 32 | 8 20 9 9 12 7 17 9 7 14 4 | 19 26 19 17 25 18 24 19 20 18 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 20 11 12 27 6 19 15 10 19 |T 29 34 30 26 44 27 33 27 29 26 27 WRMS | 8 20 10 12 25 6 19 9 7 18 |NE 18 28 24 20 33 21 28 20 23 20 20 MEDI | 8 19 10 11 26 5 21 10 10 15 |MD 19 31 24 20 36 20 29 20 22 20 20 Table 3.1555.1 GPS week: 1555 Day: 1 MJD: 55130.000 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 | 17 --- --- 21 --- 16 --- 18 19 --- 10 | 17 --- --- 23 --- 21 --- 24 28 --- 17 2E | 8 25 7 10 21 5 21 13 9 13 4 | 17 29 17 19 27 18 23 22 27 23 18 3 | 6 14 11 13 16 4 12 8 12 17 4 | 13 19 16 22 18 15 16 18 17 21 13 4E | 23 20 26 15 21 5 21 58 21 19 11 | 116 126 120 114 131 116 130 119 115 125 118 5 | 9 27 8 19 28 5 26 13 14 19 6 | 18 32 19 22 38 15 29 19 18 18 16 6 | 5 14 10 11 15 5 11 11 12 13 4 | 16 22 16 24 21 18 19 22 20 18 15 7E | 11 24 8 14 41 5 23 12 11 9 5 | 15 26 18 21 45 15 27 11 23 13 13 X8E | 23 --- 20 58 --- 17 --- 17 25 --- 15 | 43 --- 42 77 --- 44 --- 43 51 --- 44 9E | 20 21 9 14 18 8 20 20 20 14 6 | 40 51 43 47 49 45 50 52 51 46 44 10 | 8 16 7 11 15 5 16 12 14 17 4 | 19 26 17 23 26 22 24 26 30 24 21 11 | 10 17 7 6 23 4 17 8 9 14 4 | 16 22 15 15 28 14 20 17 18 21 11 12 | 8 17 11 11 24 6 19 11 8 24 5 | 15 21 18 17 26 15 22 16 18 20 14 13 | 11 23 8 12 32 3 25 13 15 13 5 | 14 31 18 16 44 18 31 16 25 18 15 14 | 4 11 10 12 27 5 18 9 9 16 4 | 20 26 21 21 34 20 28 20 23 21 19 15 | 7 21 8 8 26 5 28 10 9 12 4 | 16 25 19 16 29 16 28 15 16 20 15 16 | 6 21 9 11 28 6 21 8 12 29 5 | 13 26 14 17 27 14 24 15 17 17 12 17 | 8 18 10 13 30 9 25 9 12 19 5 | 12 29 21 18 38 18 30 18 21 17 15 18 | 6 21 6 12 25 5 21 8 10 15 4 | 13 30 19 14 38 15 29 13 20 19 15 19 | 7 22 8 14 23 6 23 11 12 25 5 | 15 29 14 13 30 12 28 14 17 17 12 20 | 9 25 9 12 25 7 24 11 11 11 5 | 16 30 20 14 42 15 29 14 18 13 14 21E | 5 18 8 9 50 6 23 9 8 12 4 | 21 27 20 23 48 21 33 21 30 19 20 22 | 6 18 7 9 27 5 17 11 7 15 4 | 17 31 23 16 37 18 27 14 22 20 18 23 | 9 26 10 17 30 4 25 11 13 13 5 | 14 32 21 19 38 18 32 16 22 16 16 X24E | 22 21 20 23 --- 17 --- 40 26 --- 11 | 38 36 44 40 --- 32 --- 50 38 --- 35 X25E | 747 --- 15 --- --- 132 --- 16 --- 129 15 | 291 --- 46 --- --- 60 --- 36 --- 30 40 26 | 8 12 11 12 17 4 10 12 6 15 4 | 16 24 17 15 26 13 22 16 17 16 13 27E | 13 20 7 11 19 6 20 10 14 16 5 | 14 25 16 23 27 17 26 21 24 17 17 28 | 6 18 11 12 24 5 23 12 10 28 5 | 21 28 24 23 35 21 28 25 27 23 21 29 | 9 18 8 10 34 5 20 8 10 28 5 | 15 28 20 11 38 16 29 12 20 18 14 30 | 4 13 9 9 17 5 10 9 10 13 3 | 22 26 25 24 31 24 24 24 24 21 21 31E | 5 20 9 13 19 4 21 11 8 15 4 | 16 27 20 19 30 17 27 17 20 25 16 32 | 9 18 6 10 16 6 14 10 6 11 3 | 21 29 23 19 31 21 26 27 22 27 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 10 12 26 5 20 15 12 17 |T 30 31 25 25 36 23 30 24 27 24 22 WRMS | 8 20 9 12 24 5 20 11 10 18 |NE 16 26 19 18 32 17 25 18 20 19 15 MEDI | 8 20 9 12 24 5 21 11 11 15 |MD 16 28 20 19 31 18 27 18 22 20 16 Table 3.1555.2 GPS week: 1555 Day: 2 MJD: 55131.000 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 --- --- 22 --- 26 --- 17 23 --- 12 | 16 --- --- 37 --- 38 --- 19 36 --- 21 2E | 9 24 10 15 24 4 24 15 12 13 5 | 14 27 16 15 29 13 24 16 17 21 15 3 | 7 10 13 8 17 5 7 7 9 15 3 | 15 19 21 18 17 17 18 18 19 19 17 4E | 17 21 16 14 23 5 19 36 17 29 8 | 123 134 128 125 140 128 138 129 125 137 127 5 | 8 25 17 13 26 4 26 13 10 21 6 | 12 28 20 16 34 13 25 14 21 18 13 6 | 5 12 12 7 17 4 8 8 9 11 3 | 17 20 23 17 17 18 20 21 19 17 18 7E | 9 26 10 12 39 4 20 11 9 10 5 | 13 30 21 20 35 18 27 18 20 19 19 X8E | 14 32 8 21 40 7 --- 10 12 --- 7 | 26 48 31 34 51 32 --- 29 34 --- 29 9E | 18 21 15 15 17 9 21 33 22 22 8 | 71 76 75 75 74 74 74 82 75 70 73 10 | 9 13 14 15 13 5 13 7 8 19 4 | 15 21 20 19 27 16 21 18 23 22 17 11 | 7 11 8 12 23 4 11 8 8 11 3 | 13 19 14 13 31 11 16 16 14 17 12 12 | 8 18 9 13 27 6 20 10 5 21 4 | 12 24 18 21 27 16 25 16 18 18 15 13 | 8 21 12 14 33 4 25 10 9 16 5 | 13 30 20 18 42 16 29 14 18 17 15 14 | 5 13 8 14 26 3 17 7 10 11 3 | 17 27 23 23 33 18 25 16 22 16 19 15 | 8 23 11 10 23 4 21 10 9 16 5 | 15 25 24 18 29 15 24 16 21 20 18 16 | 7 19 11 12 28 5 20 8 8 29 5 | 15 26 16 20 26 16 26 17 16 19 16 17 | 9 19 9 15 25 4 19 12 11 21 5 | 8 31 19 16 37 15 28 13 15 13 13 18 | 7 20 10 13 31 4 21 7 8 15 4 | 13 31 20 17 43 15 30 13 20 18 17 19 | 8 18 12 9 22 5 18 8 9 23 4 | 13 26 15 10 31 14 25 14 17 17 13 20 | 5 21 13 14 26 6 24 8 9 12 4 | 14 29 21 17 39 16 28 13 16 15 15 21E | 6 15 8 9 66 5 16 5 8 10 3 | 16 22 18 20 50 17 23 14 24 20 18 22 | 5 18 9 14 26 3 22 10 8 15 4 | 13 31 18 18 40 14 26 12 19 16 16 23 | 8 27 13 19 28 3 27 9 10 15 5 | 13 32 22 20 34 16 30 12 18 14 16 X24E | 22 23 23 25 --- 13 --- 34 31 --- 12 | 32 36 48 35 --- 32 --- 30 40 --- 31 26 | 7 13 5 12 18 3 11 13 10 16 4 | 15 26 19 15 26 16 25 18 17 15 17 27E | 11 19 14 12 18 5 19 10 11 19 5 | 11 21 17 17 24 12 23 15 17 14 13 28 | 7 19 12 13 30 4 20 12 7 32 5 | 23 32 31 30 35 23 29 27 24 26 25 29 | 7 17 8 10 27 5 21 7 11 27 5 | 15 30 19 12 38 17 29 13 18 15 15 30 | 6 9 5 12 19 5 11 7 6 9 3 | 19 27 23 28 27 21 23 23 19 17 21 31E | 5 20 12 21 48 6 19 11 13 11 5 | 12 24 17 21 39 15 23 14 20 19 15 32 | 9 18 10 14 14 4 17 10 8 12 4 | 23 31 26 30 35 27 29 26 25 27 24 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 11 13 28 5 19 13 10 18 |T 20 32 26 25 38 23 30 23 26 24 23 WRMS | 7 19 11 13 26 5 19 9 9 18 |NE 14 26 20 19 31 17 25 16 19 17 16 MEDI | 8 19 11 13 26 5 19 10 9 15 |MD 15 27 20 19 34 16 25 16 19 18 17 Table 3.1555.3 GPS week: 1555 Day: 3 MJD: 55132.000 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 | 19 --- --- 27 --- 24 --- 10 27 --- 12 | 16 --- --- 40 --- 41 --- 24 38 --- 24 2E | 7 22 9 12 24 4 22 11 6 13 4 | 18 30 24 20 35 20 28 19 21 23 20 3 | 6 9 9 11 14 4 10 8 12 15 3 | 15 18 20 24 18 18 20 20 19 20 17 4E | 13 15 11 12 25 7 17 17 13 23 5 | 125 131 133 128 143 130 139 127 125 137 129 5 | 7 22 9 14 26 7 22 11 9 20 5 | 17 30 19 21 37 16 29 19 17 18 17 6 | 4 10 7 11 15 5 8 7 11 10 3 | 18 19 21 25 19 20 20 23 21 19 19 7E | 7 20 11 10 42 4 21 16 11 13 5 | 13 31 25 20 48 19 27 19 26 20 19 X8E | 10 25 14 13 37 6 --- 14 8 33 6 | 43 48 50 43 55 43 --- 45 46 18 45 9E | 17 22 14 19 17 9 22 31 23 28 8 | 112 113 111 109 120 112 115 105 112 112 108 10 | 4 10 6 8 13 5 10 7 6 20 3 | 12 16 17 13 20 13 14 14 14 18 12 11 | 6 11 8 10 26 4 14 8 7 11 3 | 11 18 16 15 33 13 18 15 12 17 11 12 | 6 16 9 10 21 6 21 11 8 22 4 | 18 25 23 23 28 19 27 21 22 22 20 13 | 6 21 10 14 30 4 22 9 10 17 4 | 16 30 23 21 43 20 29 17 21 18 18 14 | 5 14 9 12 26 4 22 9 11 13 4 | 16 27 24 21 31 17 27 16 20 15 18 15 | 6 23 8 10 27 6 26 10 12 17 5 | 16 27 21 19 29 16 26 16 16 21 15 16 | 5 21 10 11 26 4 22 7 10 28 5 | 16 25 22 21 28 16 26 19 20 20 17 17 | 8 17 9 11 34 7 19 10 11 20 4 | 14 29 26 20 40 19 31 17 23 18 17 18 | 6 22 9 14 23 5 25 7 8 18 4 | 13 30 20 15 37 15 33 14 17 18 15 19 | 7 17 10 10 24 4 20 11 10 23 4 | 19 28 18 16 33 18 27 20 22 19 17 20 | 6 23 10 11 29 6 23 9 8 11 4 | 15 30 20 16 40 16 29 13 16 15 15 21E | 5 14 8 7 54 5 17 6 6 11 3 | 17 24 21 20 51 19 23 20 19 16 17 22 | 4 18 9 14 30 4 20 12 8 18 4 | 16 29 22 20 37 17 28 17 18 19 17 23 | 7 26 11 19 25 3 24 8 9 16 5 | 17 33 26 25 37 20 30 17 23 19 19 X24E | 21 21 24 27 --- 14 --- 30 46 --- 13 | 40 38 44 42 --- 38 --- 38 53 --- 37 26 | 6 15 12 8 17 4 12 11 10 16 4 | 13 25 21 14 23 13 23 16 16 13 15 27E | 11 19 9 17 17 6 20 11 13 20 5 | 15 23 21 23 25 16 25 18 22 15 16 28 | 8 19 12 11 27 3 24 10 7 35 5 | 23 35 31 31 36 24 32 29 24 25 25 29 | 6 16 8 10 28 6 18 7 13 28 4 | 13 28 19 13 38 16 29 13 16 14 13 30 | 5 10 7 10 13 4 12 8 8 13 3 | 29 29 29 32 33 28 22 31 27 20 28 31E | 6 24 10 17 21 6 19 11 11 12 5 | 14 34 23 21 32 18 28 15 18 22 17 32 | 8 18 9 10 12 3 14 8 9 12 4 | 16 20 19 15 25 15 21 16 15 17 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 18 9 12 26 5 19 11 11 19 |T 24 34 30 28 40 26 33 26 28 25 25 WRMS | 6 18 9 12 22 5 19 10 9 18 |NE 16 26 21 20 31 18 25 18 19 18 17 MEDI | 6 18 9 11 25 5 20 10 10 17 |MD 16 29 22 21 35 18 27 19 21 19 17 Table 3.1555.4 GPS week: 1555 Day: 4 MJD: 55133.000 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 --- --- 15 --- 28 --- 14 32 --- 13 | 20 --- --- 31 --- 46 --- 29 44 --- 27 2E | 8 27 7 16 24 3 21 10 10 17 5 | 37 38 33 38 34 32 39 36 31 41 32 3 | 6 11 10 11 17 3 10 7 7 16 3 | 15 17 21 25 22 17 18 20 20 23 18 4E | 13 22 11 12 21 4 18 12 9 18 5 | 129 132 134 128 143 130 143 127 130 137 130 5 | 9 22 9 11 29 4 23 10 9 20 5 | 11 28 11 15 39 9 27 11 12 11 9 6 | 5 9 10 8 18 4 9 6 6 11 3 | 19 19 26 25 24 20 21 23 23 22 21 7E | 9 21 7 10 40 4 22 11 7 10 4 | 14 25 19 17 50 13 25 13 14 15 14 X8E | 11 31 13 13 44 5 --- 9 8 32 6 | 35 41 34 38 59 35 --- 38 39 20 35 9E | 23 20 18 16 18 9 20 32 23 12 8 | 96 108 107 108 108 107 107 117 105 108 106 10 | 7 10 9 8 15 3 11 7 11 18 3 | 12 18 18 14 20 14 14 15 21 19 13 11 | 9 13 7 10 25 2 11 9 8 10 3 | 14 21 14 14 34 10 19 17 14 16 11 12 | 5 16 9 10 25 5 19 9 6 25 4 | 20 24 22 19 28 18 26 20 21 21 19 13 | 7 17 6 10 30 3 19 8 6 15 4 | 15 30 18 17 41 16 29 16 15 19 15 14 | 5 17 7 11 31 5 19 10 7 11 4 | 15 28 22 20 35 18 26 18 20 16 19 15 | 7 24 8 9 31 4 26 9 7 17 4 | 17 28 21 18 32 16 27 19 19 20 17 16 | 7 22 11 11 26 5 19 10 7 29 5 | 18 28 18 23 29 18 24 22 22 23 18 17 | 7 18 12 12 39 7 18 10 12 21 5 | 13 26 17 16 36 12 29 17 14 18 12 18 | 6 22 7 11 39 2 21 6 5 18 4 | 15 30 21 14 46 17 29 14 17 17 16 19 | 9 20 11 9 27 4 20 8 7 23 4 | 15 29 17 16 33 16 29 18 18 15 15 20 | 7 18 8 10 27 5 19 7 7 13 4 | 16 28 21 17 42 16 29 15 16 14 15 21E | 6 15 8 11 55 8 12 9 9 11 3 | 22 28 24 25 52 23 25 23 27 22 22 22 | 6 21 7 10 29 5 20 11 7 17 4 | 15 29 19 12 39 16 25 19 18 17 16 23 | 7 22 10 12 29 3 24 7 7 18 4 | 15 29 21 19 37 16 31 16 17 17 16 X24E | 19 23 31 22 --- 19 --- 23 28 --- 11 | 43 46 56 45 --- 41 --- 36 45 --- 41 26 | 6 13 7 5 18 2 11 14 8 13 3 | 14 25 19 12 23 15 20 20 15 13 15 27E | 11 19 14 12 11 6 22 16 13 16 5 | 12 23 17 20 20 16 22 21 20 16 15 28 | 8 18 8 10 26 4 20 9 8 36 5 | 22 30 26 27 34 23 31 27 26 28 24 29 | 8 16 9 11 28 4 18 6 10 29 5 | 17 29 22 15 35 16 29 13 15 15 15 30 | 4 10 8 9 20 5 10 9 6 8 3 | 26 28 29 28 36 26 23 30 27 15 26 31E | 6 20 8 7 27 4 21 12 9 14 4 | 13 26 16 12 39 12 24 14 15 18 13 32 | 9 20 7 10 16 3 15 7 9 14 4 | 16 22 16 15 29 14 24 17 15 19 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 9 11 28 5 18 11 9 18 |T 24 33 28 27 41 25 32 27 27 26 25 WRMS | 7 19 9 11 24 4 18 9 7 18 |NE 16 26 19 18 33 17 25 18 19 18 16 MEDI | 7 19 8 11 27 4 19 9 8 17 |MD 16 28 21 19 35 16 26 19 20 18 16 Table 3.1555.5 GPS week: 1555 Day: 5 MJD: 55134.000 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 | 17 --- --- 40 --- 25 --- 15 29 --- 15 | 24 --- --- 49 --- 31 --- 24 34 --- 27 2E | 11 28 10 11 26 3 23 10 9 13 5 | 23 36 28 20 34 26 31 23 30 27 25 3 | 7 11 7 8 19 4 11 9 10 17 3 | 11 15 17 18 17 15 15 19 17 23 15 4E | 10 22 13 14 22 6 18 11 9 16 5 | 130 139 139 132 145 132 143 128 131 142 134 5 | 8 23 13 11 27 6 23 8 9 20 5 | 20 29 19 21 36 17 27 17 17 19 17 6 | 5 13 8 7 20 4 10 7 8 13 3 | 12 17 19 18 17 16 16 19 13 21 15 7E | 8 25 8 8 37 7 23 12 8 10 4 | 13 29 19 15 40 15 26 14 16 15 14 X8E | 10 27 8 13 52 8 --- 11 13 32 6 | 50 48 49 44 89 44 --- 48 52 23 47 9E | 11 18 10 18 16 7 20 20 18 18 6 | 91 95 93 91 95 92 96 94 90 93 91 10 | 6 12 9 7 14 5 9 7 10 18 3 | 14 20 20 16 24 15 18 18 21 22 16 11 | 9 15 10 9 29 7 17 11 7 13 4 | 12 18 17 16 35 15 26 17 14 16 11 12 | 7 17 9 14 26 6 19 8 8 30 5 | 17 24 24 22 28 16 26 18 19 19 18 X13 | 8 --- 9 10 30 6 22 9 7 16 4 | 14 --- 18 18 42 15 29 15 16 17 15 14 | 5 18 10 12 26 4 23 15 8 9 4 | 18 32 30 24 38 24 32 23 25 21 23 15 | 6 24 8 13 24 7 26 10 7 18 5 | 16 32 20 20 30 18 29 18 17 21 18 16 | 8 22 11 12 26 6 22 16 7 30 5 | 13 28 21 18 26 15 26 22 16 21 16 17 | 6 18 7 15 32 6 17 14 12 22 5 | 14 31 24 21 38 19 30 19 23 18 18 18 | 7 20 8 14 24 4 21 6 7 16 4 | 18 31 25 15 42 18 31 16 21 19 19 19 | 7 20 8 10 27 5 19 8 8 22 4 | 18 30 22 19 35 21 28 18 22 17 19 20 | 7 26 11 9 28 5 22 7 9 14 4 | 19 33 23 19 44 20 30 17 23 17 19 21E | 7 15 9 9 43 6 15 9 8 10 3 | 19 22 21 22 37 17 20 19 19 14 16 22 | 5 20 8 12 27 5 22 14 6 16 4 | 17 32 27 22 41 22 29 24 24 22 22 23 | 9 26 11 14 26 4 25 7 6 19 5 | 15 32 19 23 37 17 29 14 17 18 16 X24E | 21 28 20 32 --- 19 --- 27 22 --- 11 | 42 51 55 43 --- 36 --- 42 36 --- 40 26 | 6 14 8 9 14 5 10 14 6 13 3 | 14 30 26 19 30 20 26 22 17 17 19 27E | 11 21 12 15 13 6 21 15 13 18 5 | 13 27 19 22 23 20 29 23 19 20 18 28 | 9 18 8 13 29 8 22 8 8 37 5 | 21 34 32 28 35 23 34 28 24 31 24 29 | 8 20 10 12 26 8 20 6 12 34 5 | 17 32 20 19 35 18 30 18 15 20 15 X30 | 6 12 9 9 17 4 --- 9 7 11 3 | 21 26 30 22 31 22 --- 24 25 17 23 31E | 5 21 9 11 22 7 21 13 7 12 4 | 13 29 25 16 36 18 29 18 19 20 19 32 | 7 21 10 10 17 7 17 11 8 14 4 | 16 22 23 18 31 21 24 17 16 22 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 20 10 12 25 6 20 11 9 20 |T 24 35 30 28 41 26 33 26 27 26 25 WRMS | 7 20 10 12 23 5 20 10 7 17 |NE 16 27 22 21 32 19 26 19 19 19 18 MEDI | 7 20 9 12 26 6 21 10 8 16 |MD 17 30 23 20 35 19 29 19 19 20 18 Table 3.1555.6 GPS week: 1555 Day: 6 MJD: 55135.000 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 | 25 --- --- 22 --- 32 --- 22 36 --- 16 | 22 --- --- 49 --- 57 --- 30 60 --- 35 2E | 8 21 13 15 22 3 20 12 7 25 5 | 29 35 26 26 34 28 35 34 28 44 27 3 | 8 10 11 5 18 4 10 12 7 20 3 | 20 20 27 25 25 21 21 29 19 28 21 4E | 10 17 16 13 18 4 16 9 11 18 5 | 146 154 153 144 160 147 157 143 146 157 148 5 | 9 20 8 12 30 7 23 12 8 20 5 | 20 26 19 22 33 14 27 23 19 22 17 6 | 5 10 8 4 20 4 11 11 9 18 3 | 23 22 28 27 25 24 22 32 22 29 23 7E | 9 21 9 9 34 5 22 14 9 10 4 | 12 26 19 17 36 14 26 20 14 19 15 X8E | 12 21 8 14 41 4 --- 12 8 36 6 | 63 60 64 64 81 59 --- 62 63 20 63 9E | 9 20 12 17 25 9 20 18 18 19 6 | 76 79 82 72 89 77 81 77 80 76 76 10 | 10 13 8 9 17 4 11 12 9 19 4 | 14 21 17 16 26 13 16 19 19 19 13 11 | 9 16 13 12 29 5 14 16 8 14 4 | 21 26 20 19 39 21 25 31 22 27 20 12 | 9 16 8 14 26 6 21 9 5 36 5 | 22 27 25 30 28 20 27 26 23 35 23 13 | 7 18 13 14 26 4 22 11 7 20 5 | 23 29 27 22 41 23 31 21 23 26 21 14 | 8 17 13 14 27 4 22 22 10 11 5 | 19 29 27 23 35 20 29 23 18 19 19 15 | 8 21 12 7 19 7 22 10 10 18 4 | 18 27 20 21 34 18 26 22 24 25 19 16 | 10 21 14 10 28 7 24 19 8 31 6 | 22 31 27 28 30 23 29 36 24 32 24 17 | 9 16 10 13 31 4 20 13 11 22 5 | 12 32 19 21 43 18 32 15 25 20 17 18 | 10 18 10 14 23 4 24 9 7 17 4 | 16 28 19 18 41 17 31 19 20 18 16 19 | 9 19 10 8 28 6 19 10 8 24 4 | 23 30 14 20 38 21 30 30 22 20 21 20 | 8 23 16 12 24 5 23 8 11 19 5 | 19 27 24 17 40 19 28 21 22 22 17 21E | 13 15 9 21 89 5 15 11 7 10 4 | 23 23 19 31 38 22 27 26 20 19 19 22 | 5 19 11 11 26 5 21 16 6 16 4 | 16 28 24 21 39 16 26 20 17 20 17 23 | 6 24 13 18 22 3 23 11 9 25 5 | 24 32 28 29 37 25 34 26 26 24 24 X24E | 33 25 43 28 --- 15 --- 27 24 --- 13 | 40 47 54 44 --- 41 --- 49 48 --- 42 26 | 9 14 9 11 17 4 13 18 8 14 4 | 14 28 20 16 26 16 25 23 16 13 16 27E | 13 20 10 14 22 7 20 16 12 19 5 | 14 25 20 21 28 18 27 25 22 19 18 28 | 10 17 11 10 26 6 20 11 8 40 5 | 28 36 35 30 43 28 32 31 31 32 28 29 | 11 18 12 14 34 6 23 8 10 39 6 | 19 32 22 17 41 19 35 19 18 24 16 X30 | 9 13 11 16 25 9 --- 13 6 --- 5 | 30 30 33 36 31 29 --- 38 29 --- 31 31E | 8 20 15 15 20 5 26 14 11 15 5 | 12 24 21 17 29 14 27 17 18 18 14 32 | 8 19 12 15 11 3 19 13 8 18 5 | 15 19 18 16 25 16 22 19 15 20 12 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 12 13 29 5 20 13 9 22 |T 27 35 31 30 41 28 34 32 30 30 28 WRMS | 9 18 11 13 31 5 19 12 7 19 |NE 20 27 23 23 34 21 27 25 23 23 20 MEDI | 9 18 11 14 25 5 20 12 8 19 |MD 21 28 24 22 36 21 27 26 22 22 20 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 4.1555 GPS week: 1555 MJD: 55129.0-55135.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2975 |U 8 10 22 |U 8 10 28 |U 7 7 20 | emr | emr 2830 | 21 20 73 |U 11 14 39 | 8 9 23 | esa | esa 2907 | 9 12 26 |U 8 9 27 | 7 7 20 | gfz | gfz 2921 |U 22 20 42 |U 15 19 39 | 11 12 31 | grg | grg 2770 | 10 14 29 |U 10 12 33 | 9 10 25 | igr | igr 2922 | 13 12 37 | 10 13 32 | 8 9 21 | igs | igs 2861 | 13 15 33 | 11 14 36 | 7 7 18 | jpl | jpl 2632 | 17 28 37 |U 13 13 43 |U 9 9 23 | mit | mit 3003 |U 37 55 116 |U 16 18 48 |U 8 9 22 | 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 5.1555.0 GPS week: 1555 Day: 0 MJD: 55129.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3055 | 11 13 20 | 7 9 26 | 7 5 20 | emr | emr 2935 | 18 21 45 | 12 14 43 | 9 10 24 | esa | esa 2976 | 12 16 24 | 6 8 27 | 7 8 22 | gfz | gfz 3002 | 26 32 47 | 13 15 32 | 13 13 58 | grg | grg 2784 | 12 18 21 | ---- ---- ---- | ---- ---- ---- | igr | igr 3029 | 12 15 34 | 8 7 34 | 7 9 19 | igs | igs 2823 | 13 14 34 | 12 13 38 | 7 7 17 | jpl | jpl 2580 | 17 27 38 | 15 14 60 | 12 10 31 | mit | mit 3072 | 17 26 30 | 14 15 46 | 8 11 28 | Table 5.1555.1 GPS week: 1555 Day: 1 MJD: 55130.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3001 | 9 8 23 | 7 8 28 | 8 10 18 | emr | emr 2757 | 26 43 57 | 11 12 45 | 12 12 24 | esa | esa 2976 | 10 11 22 | 7 8 28 | 8 9 20 | gfz | gfz 2903 | 24 22 33 | 19 22 49 | 10 11 27 | grg | grg 2688 | 12 16 24 | 8 13 34 | 10 10 24 | igr | igr 2932 | 14 14 43 | 8 10 26 | 8 9 20 | igs | igs 2779 | 16 22 37 | 10 13 38 | 9 10 20 | jpl | jpl 2673 | 21 35 44 | 10 9 31 | 10 9 22 | mit | mit 3072 | 9 7 23 | 14 15 57 | 7 9 17 | Table 5.1555.2 GPS week: 1555 Day: 2 MJD: 55131.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2959 | 7 9 21 | 10 10 27 | 7 6 24 | emr | emr 2844 | 31 11 76 | 12 18 37 | 8 9 25 | esa | esa 2880 | 8 10 28 | 10 10 24 | 7 6 22 | gfz | gfz 2898 | 28 19 49 | 15 19 40 | 10 9 26 | grg | grg 2784 | 12 14 24 | 10 14 29 | 8 8 30 | igr | igr 2963 | 25 12 60 | 10 16 29 | 7 6 22 | igs | igs 2968 | 22 13 60 | 12 19 40 | 6 5 19 | jpl | jpl 2675 | 27 49 40 | 12 19 45 | 8 8 21 | mit | mit 2976 | 192 303 649 | 17 21 55 | 7 8 22 | Table 5.1555.3 GPS week: 1555 Day: 3 MJD: 55132.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2950 | 9 5 25 | 11 11 40 | 7 8 17 | emr | emr 2849 | 18 13 63 | 12 13 43 | 8 8 14 | esa | esa 2880 | 10 8 25 | 11 11 41 | 8 9 14 | gfz | gfz 2909 | 41 31 80 | 16 21 38 | 14 19 29 | grg | grg 2784 | 9 12 32 | 12 11 40 | 11 13 20 | igr | igr 2750 | 11 10 44 | 12 18 45 | 13 20 25 | igs | igs 2865 | 13 13 27 | 12 12 37 | 8 8 16 | jpl | jpl 2673 | 11 9 32 | 16 16 40 | 8 9 16 | mit | mit 2976 | 14 6 42 | 18 17 45 | 9 10 20 | Table 5.1555.4 GPS week: 1555 Day: 4 MJD: 55133.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2940 | 8 13 25 | 6 8 19 | 6 8 19 | emr | emr 2842 | 17 19 63 | 11 12 28 | 7 6 23 | esa | esa 2879 | 9 14 28 | 6 8 19 | 6 7 18 | gfz | gfz 2909 | 14 16 28 | 12 19 32 | 8 11 22 | grg | grg 2784 | 10 12 38 | 9 10 30 | 7 8 25 | igr | igr 2905 | 8 11 24 | 10 10 23 | 5 6 18 | igs | igs 2832 | 12 20 29 | 12 13 27 | 5 7 18 | jpl | jpl 2672 | 13 23 44 | 16 10 32 | 7 8 20 | mit | mit 2976 | 11 18 27 | 16 18 38 | 7 10 19 | Table 5.1555.5 GPS week: 1555 Day: 5 MJD: 55134.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2972 | 8 13 21 | 7 8 21 | 6 5 18 | emr | emr 2744 | 25 18 116 | 10 11 47 | 8 8 26 | esa | esa 2880 | 9 12 30 | 7 9 24 | 7 6 17 | gfz | gfz 2909 | 13 11 34 | 16 13 50 | 12 12 27 | grg | grg 2784 | 9 14 33 | 8 10 34 | 7 9 21 | igr | igr 2963 | 10 12 24 | 9 15 33 | 7 6 17 | igs | igs 2852 | 10 11 24 | 10 12 42 | 6 6 18 | jpl | jpl 2578 | 11 16 36 | 14 13 52 | 8 7 20 | mit | mit 2976 | 9 7 18 | 14 16 55 | 6 7 22 | Table 5.1555.6 GPS week: 1555 Day: 6 MJD: 55135.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2954 | 8 10 22 | 8 13 32 | 8 6 26 | emr | emr 2839 | 16 17 88 | 11 15 28 | 8 9 24 | esa | esa 2880 | 7 12 23 | 9 12 26 | 8 7 26 | gfz | gfz 2919 | 9 10 24 | 12 25 35 | 10 13 27 | grg | grg 2784 | 9 13 32 | 10 13 29 | 9 12 27 | igr | igr 2918 | 10 12 28 | 10 18 31 | 8 7 23 | igs | igs 2912 | 8 14 23 | 11 16 32 | 6 7 21 | jpl | jpl 2579 | 21 35 24 | 11 10 46 | 9 9 28 | mit | mit 2976 | 9 17 20 | 21 22 39 | 11 9 27 | 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 6.1555 GPS week: 1555 MJD: 55129.500-55135.500 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 22 20 -135 -5 | 5 12 | 16 30 107 109 7 | 1 emr uuuuu | -8 14 27 -141 -1 | 77 78 | 18 31 130 68 9 | 2 esa uuuuu | 8 7 -44 163 -4 | 18 22 | 36 19 91 85 12 | 3 gfz uuuuu | 30 9 50 -56 0 | -8 14 | 19 15 65 43 3 | 2 grg --xxx | -- -- 130 -170 1 | 4 26 | -- -- 100 87 16 | 3 igr xxxxx | 12 73 -8 -62 -7 | 0 12 | 20 31 56 70 8 | 3 irf xxxxx | 4 10 36 -11 2 | 0 11 | 16 6 30 20 3 | 1 jpl uuuuu | -19 21 -34 -27 -6 | 32 35 | 49 20 119 64 12 | 3 mit uuuuu | -13 -1 30 158 5 | 15 19 | 22 13 62 68 5 | 2 ngs uuuuu | -27 14 4 -148 1 | -1 11 | 36 30 93 114 3 | 1 sio uuuuu | 52 -96 -56 -71 -1 | 40 42 | 25 9 64 91 4 | 1 Table 7.1555.0 GPS week: 1555 Day: 0 MJD: 55129.500 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 | 8 -26 -154 -336 -1 | 8 15 emr uuuuu | 15 -46 110 -209 9 | 75 77 esa uuuuu | -10 31 -1 141 5 | 22 28 gfz uuuuu | 36 -4 -16 -65 -5 | -5 15 grg --xxx | -- -- 133 -206 -30 | 9 32 igr xxxxx | 46 66 50 83 -2 | 3 13 irf xxxxx | -3 12 3 -49 2 | 0 12 jpl uuuuu | -9 15 -22 7 12 | 31 35 mit uuuuu | -10 12 -47 84 -1 | 14 19 ngs uuuuu | -26 19 58 13 2 | 2 11 sio uuuuu | 35 -99 -82 -189 -6 | 43 44 Table 7.1555.1 GPS week: 1555 Day: 1 MJD: 55130.500 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 | -13 53 7 -108 3 | 6 12 emr uuuuu | -28 16 76 -110 9 | 75 77 esa uuuuu | -11 15 -137 4 16 | 20 24 gfz uuuuu | 55 21 7 -24 2 | -8 12 grg --xxx | -- -- 250 -157 -10 | 4 31 igr xxxxx | 30 65 -58 -118 6 | 1 12 irf xxxxx | 8 21 22 1 4 | -1 10 jpl uuuuu | -32 20 93 45 1 | 33 37 mit uuuuu | -5 5 28 232 0 | 13 18 ngs uuuuu | -30 -8 73 -180 -3 | 0 8 sio uuuuu | 53 -88 -27 -5 -2 | 41 42 Table 7.1555.2 GPS week: 1555 Day: 2 MJD: 55131.500 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 | 12 31 27 -70 -8 | 5 13 emr uuuuu | -8 17 193 -181 -4 | 75 77 esa uuuuu | 9 -13 -13 217 -11 | 19 23 gfz uuuuu | 46 33 41 -54 2 | -10 15 grg --xxx | -- -- 23 -63 15 | -1 32 igr xxxxx | 1 60 -50 -82 -4 | -1 13 irf xxxxx | 11 14 82 4 1 | -2 12 jpl uuuuu | -39 17 -48 -66 -15 | 34 37 mit uuuuu | 1 15 100 157 1 | 12 18 ngs uuuuu | -43 -2 -186 -162 3 | -3 12 sio uuuuu | 55 -89 1 -25 -1 | 39 41 Table 7.1555.3 GPS week: 1555 Day: 3 MJD: 55132.500 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 | -28 18 -67 -88 -6 | 6 12 emr uuuuu | -9 12 20 -143 2 | 78 79 esa uuuuu | 52 9 -52 116 -18 | 19 23 gfz uuuuu | 37 1 110 -1 -2 | -8 13 grg --xxx | -- -- 109 -160 12 | 5 29 igr xxxxx | 9 25 -54 -123 -14 | 1 12 irf xxxxx | 8 3 16 3 4 | 0 10 jpl uuuuu | -67 -9 28 8 4 | 35 38 mit uuuuu | -20 -20 20 255 8 | 15 19 ngs uuuuu | -49 60 -29 -341 2 | -1 12 sio uuuuu | 48 -114 -94 28 0 | 40 42 Table 7.1555.4 GPS week: 1555 Day: 4 MJD: 55133.500 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 | 1 31 45 -91 2 | 4 11 emr uuuuu | -33 28 -49 -145 2 | 78 79 esa uuuuu | -20 -16 -119 187 -3 | 16 20 gfz uuuuu | 20 10 47 -95 3 | -10 14 grg --xxx | -- -- -17 -130 2 | 0 19 igr xxxxx | -14 82 -38 -76 -12 | 0 12 irf xxxxx | -15 7 45 5 8 | 0 10 jpl uuuuu | 38 52 76 -145 -22 | 34 37 mit uuuuu | -47 2 78 172 11 | 15 19 ngs uuuuu | 30 13 -2 -110 -4 | -2 11 sio uuuuu | 33 -100 -10 -59 7 | 39 41 Table 7.1555.5 GPS week: 1555 Day: 5 MJD: 55134.500 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 -7 156 -22 -8 | 5 12 emr uuuuu | 7 59 -214 -8 -14 | 80 81 esa uuuuu | -25 28 -108 215 1 | 15 19 gfz uuuuu | 3 9 163 -124 -1 | -8 13 grg --xxx | -- -- 230 -134 10 | 4 18 igr xxxxx | 7 128 79 -76 -16 | -2 11 irf xxxxx | -13 9 68 -22 -1 | 2 11 jpl uuuuu | 52 40 -112 7 -16 | 30 33 mit uuuuu | -28 -4 82 121 6 | 17 21 ngs uuuuu | 10 -28 37 -201 1 | -1 11 sio uuuuu | 35 -96 -5 -44 -4 | 41 43 Table 7.1555.6 GPS week: 1555 Day: 6 MJD: 55135.500 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 | 18 53 126 -231 -17 | 4 11 emr uuuuu | 3 13 53 -193 -13 | 77 78 esa uuuuu | 64 -4 124 258 -16 | 14 18 gfz uuuuu | 13 -11 -1 -32 1 | -9 13 grg --xxx | -- -- 181 -341 7 | 5 19 igr xxxxx | 4 85 18 -39 -8 | -5 12 irf xxxxx | 33 4 17 -21 -2 | 1 11 jpl uuuuu | -74 10 -252 -46 -9 | 27 29 mit uuuuu | 22 -15 -53 84 8 | 17 21 ngs uuuuu | -78 40 79 -54 5 | -1 11 sio uuuuu | 104 -90 -174 -206 -2 | 40 42