Date: Thu, 08 Oct 2009 11:50:45 +0000 From: Jim Ray Subject: [IGSREPORT-17875] Wk 1550 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4acdd215.cxXpi74QkQWjyD36%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 08 Oct 04:50:48 PDT 2009 Message Number 17875 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1550 (Sep 20, 2009 - Sep 26, 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: igs1550[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1550[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1550[0-6].cls IGS GPS clock combination summary report. igs15507.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15507.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 | 24 24 0 | EMR | WTZR 0 | ESA | 24 0 | GFZ | 1 24 BUE1 COCO FAA1 HARB HOFN MAC1 REUN SUTM UNSA 0 | GFZ | ZIMM 0 | GRG | ONSA 0 | JPL | 5 32 0 | NGS | 1 1 | ALL | 1 1 | EMR | 24 24 WTZR 1 | GFZ | 5 24 BRUS FAA1 HARB HOLM KERG KIRU ONSA SFER THU3 1 | GFZ | WSRT 1 | GRG | DAV1 ONSA 1 | JPL | 32 DAV1 POTS 2 | ALL | 1 5 2 | COD | MAS1 XMIS 2 | ESA | MAS1 WTZR 2 | GFZ | 24 CHUR DUBO EIL1 FAA1 HOFN HOLM KIRU NYAL ONSA SFER 2 | GFZ | THU3 WSRT 2 | GRG | KHAJ ONSA 2 | JPL | 32 2 | MIT | 24 24 HARB 3 | ALL | 1 1 3 | EMR | WTZR 3 | ESA | NYAL UNSA 3 | GFZ | 5 24 CAS1 COCO FAA1 HARB ONSA PRE1 RAMO TWTF 3 | GRG | ONSA TWTF 3 | JPL | 32 3 | MIT | 24 24 NYA1 4 | ALL | 1 4 | EMR | WTZR 4 | GFZ | 24 27 CRO1 FAA1 HARB PRE1 RABT ULAB UNSA 4 | GRG | ONSA TWTF 4 | JPL | 32 4 | MIT | 9 24 9 24 HARB MIZU SYDN 5 | ALL | 1 5 | COD | WROC 5 | ESA | MAS1 5 | GFZ | 5 24 ABPO BOR1 DAV1 HARB HOLM IISC NYA1 RABT RAMO 5 | GFZ | THU3 TOW2 TWTF 5 | GRG | COCO DAV1 TWTF WTZR 5 | JPL | DAV1 MDVJ 5 | MIT | MAS1 MAS1 6 | ALL | 1 24 6 | EMR | 24 6 | GFZ | 10 11 COCO DGAR HARB HRAO MIZU PRE1 6 | GRG | ONSA 6 | JPL | 5 32 6 | MIT | 26 HARB 5. The following table lists all maneuvered satellites for this week. The solutions from COD and ESA, which modeled the maneuver, are used that day for combination. An associated accuracy code of 0 (unknown) is given if only one AC is left (no redundancy). For the long arc evaluation the arc is split into two parts at the given maneuver epoch. PRN | Date | Ref. NANU ----+------------+---------- G05 | 2009_09_22 | 2009072 G10 | 2009_09_25 | 2009074 6. 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. 7. 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 .7 1.4 -9 -5 -12 -.32 EMR | 2.5 -2.0 -5.5 68 3 52 .09 ESA | .3 2.7 1.6 75 -21 38 -.03 GFZ | .0 .9 .8 18 -14 1 -.22 GRG | 5.4 3.2 -.7 1 -43 89 .03 JPL | -1.4 5.6 -6.1 8 -11 3 .15 MIT | .1 -.9 7.8 11 7 -12 -.30 NGS | 1.0 .4 .1 4 -6 -8 -.16 SIO | -.2 1.5 -2.9 33 -10 2 -.06 8. 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. 9. 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. 10. 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 1.1550.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1550.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 2.1550.[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 3.1550.[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 5.1550.0-6). 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 1550 summary. (Sep 20, 2009 - Sep 26, 2009) Table 1.1550.a GPS week: 1550 MJD: 55094.000-55100.000 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 225| 1 0 1 62 -15 -8 -.16 7 7 | 20 -144 14 67 | 0 0 0 6 7 18 .02 | 564 646 emr 78| 0 -1 -3 -81 -18 -1 .55 20 20 | 1122 -269 18 83 | 2 4 2 38 14 13 .04 | 507 669 esa 137| 0 -1 1 -107 60 -25 .33 9 9 | -1232 286 19 117 | 0 0 2 29 22 11 .03 | 874 1065 gfz 177| 0 0 -1 5 -20 -14 -.16 9 9 | -113 186 23 104 | 0 0 1 43 25 6 .02 | 368 976 grg 110| 3 0 -1 58 86 62 1.13 34 34 | 25 -222 74 244 | 1 1 1 23 24 38 .05 | 254 447 igr n/a| 0 0 2 50 -23 -18 .08 5 5 | -10852 -299 18 65 | 0 1 1 15 9 31 .06 | 563 838 jpl 132| 2 0 -5 19 0 37 .59 17 17 | 1422 -370 17 86 | 1 1 1 20 17 34 .02 | 533 826 mit 268| -1 0 0 22 -38 -6 -.28 10 9 | -14136 -169 20 125 | 0 0 1 29 14 10 .04 | 663 1287 ngs 216| 0 0 0 40 0 23 -.18 9 7 | 12442 2175 2129 6353 | 0 0 1 37 22 18 .03 | 2691 3539 sio 246| -2 1 1 -38 33 37 -.16 20 18 | --- --- --- --- | 0 1 1 26 17 9 .01 | --- --- Table 1.1550.b GPS week : 1550 MJD: 55094.000-55100.000 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 | 10 13 12 12 9 10 8 | 2 | 4 5 5 5 4 6 5 | 3 | 4 4 4 4 4 4 4 | 4 | 4 4 4 4 4 4 8 | 5 | 6 6 10 5 5 6 5 | 6 | 4 4 4 4 4 4 4 | 7 | 5 5 4 4 4 4 4 | 8 | 4 4 3 3 3 4 4 | 9 | 4 4 4 4 4 4 4 | 10 | 4 3 4 4 4 0 4 | 11 | 4 4 4 4 4 4 4 | 12 | 5 5 4 5 5 5 5 | 13 | 4 4 4 4 4 5 4 | 14 | 5 5 4 4 4 4 4 | 15 | 5 5 5 5 5 5 5 | 16 | 5 6 5 5 5 6 5 | 17 | 5 5 4 5 4 4 5 | 18 | 5 5 5 5 4 5 5 | 19 | 5 5 5 5 5 5 5 | 20 | 4 5 4 4 4 5 5 | 21 | 5 5 4 4 4 5 5 | 22 | 5 5 4 4 4 4 4 | 23 | 5 5 5 5 5 5 5 | 24 | 7 8 9 7 8 10 9 | 25 | 4 4 4 4 3 4 4 | 26 | 4 5 4 4 4 4 5 | 27 | 4 4 4 4 4 5 4 | 28 | 6 6 5 6 6 6 6 | 29 | 5 5 4 4 4 5 4 | 30 | 4 4 3 3 4 4 4 | 31 | 5 5 4 5 5 5 5 | 32 | 4 4 4 4 4 4 4 | 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 2.1550.0 GPS week: 1550 Day: 0 MJD: 55094.000 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 225| 1 1 0 61 -9 -17 -.19 7 7 | -987 610 14 67 | -3 13 | emr 78| 0 2 -2 -35 -33 5 .50 19 19 | 1173 -295 17 73 | -77 -3 | esa 137| 0 -2 3 -101 55 -34 .31 8 8 | -899 -1008 18 114 | 48 10 | gfz 177| 1 0 -1 -28 -27 -13 -.17 9 9 | -677 29 22 110 | -54 24 | grg 110| 0 2 -2 23 109 72 1.05 36 35 | -264 -478 73 246 | -37 15 | igr n/a| 0 0 2 62 -24 -39 .03 4 4 | -10526 -457 16 56 | -76 5 | jpl 132| 2 0 -7 12 4 12 .56 17 17 | 1733 -578 17 77 | -4 48 | mit 268| -1 -1 2 7 -53 9 -.24 12 11 | -15431 -117 20 111 | -2 4 | ngs 216| -2 0 0 79 6 34 -.21 9 7 | 8466 6698 2264 4590 | -86 37 | sio 246| 0 0 2 -48 45 41 -.14 21 20 | --- --- --- --- | 24 -36 | Table 2.1550.1 GPS week: 1550 Day: 1 MJD: 55095.000 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 225| 1 0 1 59 -17 4 -.15 7 7 | 244 -576 14 60 | -23 24 | emr 78| 0 -3 -2 -54 -38 -1 .53 19 19 | 1195 191 19 82 | -80 -13 | esa 137| 0 -1 2 -120 51 -9 .29 10 10 | -1048 1203 23 118 | 42 10 | gfz 177| 1 0 -2 0 23 -15 -.16 10 10 | 85 -467 24 99 | -45 -4 | grg 110| 4 0 -3 61 101 92 1.11 35 34 | -37 105 84 234 | -12 41 | igr n/a| 0 0 3 58 -39 -44 .05 4 4 | -10808 286 20 64 | -22 -4 | jpl 132| 1 0 -4 4 -9 20 .60 16 16 | 1236 325 16 70 | 2 -18 | mit 268| -1 -1 0 -3 -28 -14 -.24 11 11 | -14267 2565 19 110 | -8 -13 | ngs 216| 0 1 -1 82 -27 0 -.22 10 9 | 12779 -1829 2424 3741 | -65 85 | sio 246| -2 1 0 -66 48 32 -.16 19 20 | --- --- --- --- | 19 -40 | Table 2.1550.2 GPS week: 1550 Day: 2 MJD: 55096.000 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 225| 1 1 0 63 -4 -8 -.16 7 7 | -238 -172 15 64 | 12 -26 | emr 78| 0 -1 -5 -51 -23 -25 .54 17 17 | 1701 -574 19 81 | -49 -29 | esa 137| 0 0 0 -138 87 -19 .33 8 8 | -2120 348 21 118 | 35 -14 | gfz 177| 0 1 -1 -27 -54 -24 -.16 9 9 | -126 48 22 103 | -17 11 | grg 110| 4 -2 -1 70 121 6 1.14 36 36 | 128 -427 78 267 | 16 -9 | igr n/a| 0 0 2 57 -15 -39 .06 5 5 | -10318 -383 17 69 | -44 -3 | jpl 132| 3 0 -4 40 24 70 .60 17 17 | 1835 -560 17 94 | 21 -20 | mit 268| -1 0 1 25 -61 -2 -.27 9 9 | -14101 -1423 18 111 | -13 1 | ngs 216| -1 0 2 53 10 5 -.17 7 6 | 12510 4212 2188 6869 | -29 -2 | sio 246| -2 1 1 -33 -2 41 -.16 18 18 | --- --- --- --- | 15 -9 | Table 2.1550.3 GPS week: 1550 Day: 3 MJD: 55097.000 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 225| 2 0 0 68 -27 25 -.15 8 8 | 339 -776 13 60 | -4 34 | emr 78| 0 0 -5 -85 -8 3 .54 19 19 | 1837 -1120 19 85 | -11 -37 | esa 137| 0 0 4 -117 40 -24 .33 8 8 | -2336 -184 18 110 | 60 -4 | gfz 177| 0 0 0 -3 -6 -3 -.14 10 10 | -33 2127 23 97 | -51 -7 | grg 110| 2 1 -1 74 60 123 1.20 37 38 | 166 -110 80 226 | -15 33 | igr n/a| 1 0 1 41 -12 -24 .05 5 5 | -10149 -1143 19 62 | -28 -10 | jpl 132| 4 -1 -4 29 10 -9 .58 18 18 | 2197 -1131 18 83 | -16 -26 | mit 268| -1 -1 -2 30 -39 -17 -.26 9 10 | -14081 -283 19 122 | -21 14 | ngs 216| -1 0 1 54 6 8 -.15 8 7 | 16056 -2522 1979 7297 | -23 -5 | sio 246| -2 2 0 -17 43 32 -.17 18 17 | --- --- --- --- | -4 -23 | Table 2.1550.4 GPS week: 1550 Day: 4 MJD: 55098.000 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 225| 0 0 1 55 -15 -7 -.15 7 7 | 737 -760 16 70 | 12 4 | emr 78| 0 3 -2 -119 -16 -14 .58 20 20 | 761 -136 19 91 | 24 -29 | esa 137| 0 -1 0 -91 43 -42 .33 8 8 | -724 663 18 106 | 16 15 | gfz 177| 0 1 -1 55 -23 -15 -.14 9 9 | 277 -416 21 92 | -49 10 | grg 110| 5 1 -1 66 75 54 1.17 32 33 | 255 69 67 252 | 49 43 | igr n/a| 0 0 0 37 -20 -29 .05 4 4 | -11081 -354 16 62 | -43 30 | jpl 132| 0 -1 -5 3 -24 22 .60 17 17 | 1332 -262 16 100 | 13 -18 | mit 268| -1 0 0 38 -30 -3 -.30 8 8 | -13666 -557 23 120 | -18 0 | ngs 216| 0 0 0 -1 26 30 -.16 8 7 | 15001 984 1988 8931 | 35 74 | sio 246| -2 1 2 -28 28 45 -.18 18 17 | --- --- --- --- | 27 -34 | Table 2.1550.5 GPS week: 1550 Day: 5 MJD: 55099.000 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 225| 1 0 1 55 -22 -27 -.16 8 8 | 310 -179 15 72 | 25 33 | emr 78| 1 -8 -3 -140 2 6 .62 24 23 | 530 -836 18 92 | 10 -26 | esa 137| 0 -1 2 -133 49 -33 .37 9 9 | 177 -895 22 133 | 33 27 | gfz 177| -1 1 0 76 -43 -15 -.18 11 11 | 225 -729 27 114 | -35 -9 | grg 110| 3 1 0 27 59 32 1.14 32 34 | 291 -1012 71 244 | 53 16 | igr n/a| 1 0 0 27 -17 41 .14 5 5 | -11466 -1240 21 79 | -37 -4 | jpl 132| 1 0 -7 -4 -18 66 .62 18 18 | 974 -1395 21 105 | 6 -14 | mit 268| 0 0 0 74 -20 0 -.33 10 9 | -14119 -1003 20 138 | -34 -8 | ngs 216| 0 1 0 -15 15 34 -.18 10 8 | 12654 2189 2195 9414 | 118 74 | sio 246| -2 2 0 0 41 49 -.16 19 18 | --- --- --- --- | -10 -29 | Table 2.1550.6 GPS week: 1550 Day: 6 MJD: 55100.000 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 225| 0 0 2 73 -13 -27 -.15 7 7 | -265 842 15 76 | -30 1 | emr 78| -4 -3 1 -86 -10 13 .57 19 19 | 662 881 16 81 | -37 -29 | esa 137| 0 0 -2 -50 96 -16 .36 9 9 | -1677 1878 19 125 | 19 18 | gfz 177| 0 1 -3 -30 -11 -17 -.16 9 9 | -543 714 24 114 | -16 17 | grg 110| 4 0 1 85 77 57 1.13 32 31 | -360 296 70 240 | -84 -23 | igr n/a| 0 -2 3 69 -32 6 .18 8 8 | -11617 1198 22 64 | -99 -29 | jpl 132| 2 -1 -4 48 12 82 .60 18 18 | 649 1006 15 79 | 21 -27 | mit 268| 0 0 1 -14 -37 -19 -.33 10 8 | -13288 -365 25 169 | -11 -1 | ngs 216| 0 0 0 32 -33 49 -.14 9 8 | 9633 5496 1867 3633 | 38 73 | sio 246| -2 3 2 -73 28 21 -.16 24 20 | --- --- --- --- | 13 -25 | 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 3.1550.0 GPS week: 1550 Day: 0 MJD: 55094.000 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 --- --- 12 --- 13 --- 15 23 --- 10 | 51 --- --- 48 --- 62 --- 56 61 --- 52 2 | 7 18 8 8 42 3 19 8 10 23 4 | 24 31 24 26 59 23 33 23 26 31 24 3 | 7 16 8 7 15 3 13 10 7 20 3 | 17 27 21 18 28 19 28 19 19 30 18 4 | 7 17 6 5 34 4 12 11 9 21 4 | 19 32 24 22 37 22 30 22 19 24 21 5 | 7 19 10 10 42 5 20 18 9 32 5 | 8 21 11 8 19 9 19 12 9 14 6 6 | 8 16 10 7 19 2 15 11 8 23 4 | 17 30 23 19 32 19 31 21 20 29 19 7 | 7 24 9 10 28 2 18 11 11 13 4 | 18 34 24 26 40 21 28 23 19 23 21 8 | 6 12 5 10 31 3 11 12 9 17 3 | 16 25 21 20 28 19 24 20 17 21 17 9 | 8 19 8 7 29 4 13 15 11 14 4 | 19 32 23 22 27 20 28 25 24 25 22 10 | 6 14 8 7 37 3 12 13 6 16 3 | 15 24 21 17 18 18 13 19 17 20 17 11 | 6 17 8 10 37 4 16 7 10 14 4 | 16 28 21 20 44 18 23 21 20 21 18 12 | 9 17 9 10 29 5 16 15 8 26 4 | 23 32 24 27 41 23 30 27 23 21 23 13 | 6 17 6 8 45 4 20 13 10 11 4 | 16 26 20 19 44 18 29 22 20 20 18 14 | 7 21 11 8 26 4 22 14 7 15 4 | 17 31 23 19 41 18 27 23 18 19 18 15 | 10 16 12 11 26 4 23 16 11 13 5 | 16 31 23 25 35 19 31 23 21 22 20 16 | 6 19 9 11 27 4 21 10 8 28 5 | 24 36 25 24 40 24 36 25 25 28 24 17 | 6 25 7 12 26 4 20 7 9 14 4 | 17 40 22 18 41 20 33 21 18 20 19 18 | 6 17 7 10 28 4 21 10 12 19 4 | 21 33 28 30 37 26 30 29 27 26 25 19 | 7 25 8 12 34 5 20 10 9 17 4 | 18 35 21 18 32 18 29 19 20 24 19 20 | 8 18 6 8 74 6 17 7 8 21 4 | 25 30 30 32 49 29 27 29 30 24 27 21 | 6 20 7 10 25 4 24 8 11 14 4 | 21 34 24 19 38 20 36 22 20 23 21 22 | 8 19 8 7 30 6 20 18 10 19 4 | 27 39 34 33 38 32 34 36 30 30 30 23 | 7 28 10 9 32 3 23 12 6 18 5 | 16 35 21 19 34 18 29 21 17 23 17 X24 | 13 22 13 14 --- 10 --- 17 18 --- 7 | 15 29 26 27 --- 19 --- 22 24 --- 18 25 | 6 12 6 8 --- 3 9 11 10 21 3 | 14 22 18 20 --- 16 22 17 15 26 15 26 | 8 16 8 8 25 4 12 15 10 20 4 | 17 32 21 20 34 18 28 23 21 24 18 27 | 8 18 8 7 31 4 13 14 13 15 4 | 16 31 21 21 27 19 27 24 21 24 20 28 | 6 18 8 9 70 5 16 9 10 48 5 | 26 38 31 31 59 29 36 27 28 44 27 29 | 6 24 12 8 23 5 15 15 8 16 4 | 21 30 18 18 24 20 23 24 22 25 18 30 | 7 9 6 8 25 6 8 13 10 20 3 | 33 33 32 31 41 30 32 36 35 27 31 31 | 6 22 9 11 39 4 20 16 9 15 4 | 18 28 23 21 48 19 27 23 20 20 19 32 | 8 18 6 6 54 4 17 9 9 16 4 | 18 22 24 24 41 21 22 21 23 22 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 19 8 9 36 4 17 12 9 21 |T 19 30 23 23 37 22 28 24 22 24 21 WRMS | 7 19 8 9 35 4 17 11 7 20 |NE 20 30 23 23 36 22 28 24 22 24 21 MEDI | 7 18 8 8 30 4 17 12 9 17 |MD 18 31 23 21 38 19 28 23 20 24 19 Table 3.1550.1 GPS week: 1550 Day: 1 MJD: 55095.000 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 --- --- 18 --- 36 --- 28 28 --- 13 | 83 --- --- 84 --- 99 --- 80 94 --- 83 2 | 7 22 12 8 39 4 19 10 10 21 4 | 20 31 24 18 41 21 29 16 20 25 19 3 | 6 16 9 12 20 3 10 8 9 19 4 | 9 23 16 15 24 12 21 12 12 22 12 4 | 6 16 10 6 30 4 9 9 11 20 3 | 13 26 20 16 29 16 24 17 20 19 16 X5 | 7 18 8 9 52 5 --- 14 9 31 5 | 6 20 11 7 19 7 --- 11 7 12 6 6 | 6 16 9 9 15 3 12 10 10 20 4 | 8 26 17 15 26 12 25 12 12 22 12 7 | 9 23 11 11 27 5 18 12 9 11 4 | 15 28 18 17 35 14 24 15 17 12 14 8 | 8 12 11 8 29 4 12 9 12 11 3 | 13 21 17 12 23 13 18 13 17 14 12 9 | 7 18 8 8 27 3 12 12 11 14 4 | 12 26 18 16 21 17 23 23 20 21 16 10 | 5 12 8 6 37 4 9 11 6 15 3 | 12 19 19 14 17 14 15 14 15 18 13 11 | 7 17 10 7 41 3 13 8 10 15 4 | 9 25 16 11 37 10 17 11 9 11 9 12 | 8 14 10 9 32 5 13 12 9 27 4 | 16 28 19 22 32 18 26 23 21 19 18 13 | 7 17 9 7 46 6 17 12 10 10 4 | 11 23 13 11 38 12 21 14 10 11 10 14 | 9 23 11 8 27 4 21 10 8 14 4 | 13 32 17 17 39 15 26 17 14 14 14 15 | 10 16 11 10 27 5 21 14 10 11 4 | 14 26 18 19 30 16 24 16 17 16 15 16 | 8 20 12 12 21 4 20 11 12 29 5 | 12 27 20 16 31 15 28 16 19 18 15 17 | 8 24 11 10 35 4 18 7 10 12 4 | 16 33 16 10 42 14 23 12 14 17 13 18 | 6 16 9 14 30 5 20 13 11 20 5 | 15 29 21 25 34 18 28 22 21 19 18 19 | 8 27 12 11 42 4 22 8 10 15 5 | 13 34 18 16 39 15 27 16 17 18 15 20 | 8 20 9 13 62 5 18 6 12 18 4 | 13 23 19 21 32 17 20 13 18 13 14 21 | 6 29 9 13 31 5 22 7 9 13 5 | 16 33 19 17 35 15 29 17 19 18 16 22 | 8 18 11 9 36 5 19 16 9 19 5 | 20 32 25 25 41 23 32 28 22 23 22 23 | 7 23 10 12 33 4 20 11 8 17 5 | 11 28 15 16 35 12 23 15 11 16 11 X24 | 15 20 19 18 --- 16 --- 15 19 --- 7 | 16 16 30 31 --- 20 --- 21 33 --- 20 25 | 5 13 8 11 --- 3 9 11 7 20 3 | 9 16 12 15 --- 11 18 12 15 20 10 26 | 8 21 13 10 25 3 10 12 9 18 4 | 15 33 17 22 27 16 24 23 18 20 17 27 | 7 16 7 8 34 3 13 13 8 14 4 | 11 25 17 14 25 16 22 19 15 19 14 28 | 6 18 9 9 56 4 19 10 12 45 6 | 16 30 21 17 37 18 29 13 13 42 15 29 | 5 18 11 10 25 8 16 14 12 15 4 | 19 25 17 20 20 19 23 22 17 23 17 30 | 7 11 9 7 30 3 7 12 7 21 3 | 23 25 25 24 24 22 24 26 27 17 23 31 | 7 21 16 10 47 4 16 11 11 16 4 | 13 26 18 16 45 15 24 15 14 15 14 32 | 9 17 10 9 40 3 14 7 10 16 4 | 12 20 19 16 25 15 18 16 16 18 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 19 10 10 35 4 16 11 10 19 |T 15 26 18 19 31 18 23 18 19 18 16 WRMS | 7 19 10 10 34 4 16 11 9 20 |NE 15 26 18 19 30 18 23 19 19 18 17 MEDI | 7 18 10 9 32 4 16 11 10 16 |MD 13 26 18 16 32 15 24 16 17 18 14 Table 3.1550.2 GPS week: 1550 Day: 2 MJD: 55096.000 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 | 26 --- --- 16 --- 17 --- 13 24 --- 12 | 46 --- --- 45 --- 54 --- 51 56 --- 45 2 | 6 17 8 10 38 4 22 9 7 22 4 | 20 30 24 22 44 20 31 21 20 29 21 3 | 6 16 7 6 20 4 12 9 7 19 3 | 14 25 23 16 26 15 24 16 17 27 17 4 | 8 13 11 8 40 5 12 11 8 20 4 | 16 26 21 20 31 15 24 17 19 16 17 X5 | 7 --- 11 --- --- 120 --- --- --- --- 9 | 18 --- 12 --- --- 163 --- --- --- --- 25 6 | 8 16 10 7 22 4 13 10 7 19 4 | 14 26 23 16 28 15 26 16 18 25 17 7 | 7 19 7 10 28 6 18 11 9 11 4 | 17 28 20 20 35 19 25 18 20 17 18 8 | 7 12 5 9 32 6 11 8 5 9 3 | 14 21 19 16 26 15 20 16 15 15 15 9 | 8 18 8 9 30 5 14 8 8 11 3 | 14 27 20 19 26 18 22 20 19 20 17 10 | 6 14 10 7 50 5 10 10 8 13 3 | 15 21 24 18 22 19 10 17 18 16 17 11 | 7 15 7 8 43 5 14 9 7 12 3 | 12 25 19 19 38 15 17 17 14 16 15 12 | 9 16 8 8 36 7 16 7 8 25 4 | 18 30 22 23 39 20 26 20 20 20 19 13 | 8 18 9 7 43 5 19 9 9 10 4 | 14 26 18 17 44 14 24 16 15 16 14 14 | 5 17 10 7 33 4 20 7 6 13 3 | 14 26 19 17 42 15 24 17 18 15 15 15 | 10 17 10 7 33 4 24 13 11 13 4 | 15 27 21 15 34 15 28 18 17 18 16 16 | 6 18 11 13 33 3 17 10 6 27 4 | 19 33 27 21 37 20 30 22 20 21 21 17 | 6 18 8 11 22 5 19 6 5 11 3 | 15 27 14 13 32 14 25 16 18 20 15 18 | 6 19 7 11 27 5 20 12 8 20 4 | 18 29 25 25 36 19 26 22 19 20 19 19 | 6 29 8 8 40 3 22 9 8 15 4 | 18 37 21 17 37 18 29 16 23 22 20 20 | 6 18 8 9 59 5 17 7 6 18 4 | 21 27 27 24 34 24 23 24 28 19 23 21 | 4 21 9 8 27 3 20 8 7 13 4 | 18 30 18 17 37 18 27 19 18 19 18 22 | 6 18 5 9 27 5 18 12 6 18 4 | 21 29 26 25 37 22 27 27 23 21 22 23 | 8 23 9 9 37 4 21 10 8 18 4 | 13 29 17 14 36 13 25 16 15 19 13 X24 | 20 19 18 24 --- 11 --- 13 17 --- 8 | 16 20 27 31 --- 19 --- 22 28 --- 19 25 | 7 12 10 6 --- 6 11 9 8 19 3 | 12 21 17 15 --- 14 21 15 16 21 14 26 | 8 14 7 12 21 4 12 9 6 17 3 | 16 24 20 24 29 17 24 23 21 18 19 27 | 9 17 7 10 37 4 15 8 7 10 3 | 13 26 20 19 27 17 22 20 18 21 17 28 | 7 18 9 8 56 6 17 8 7 43 5 | 19 31 28 22 39 21 27 20 20 43 20 29 | 7 21 8 10 25 6 16 10 9 15 4 | 20 28 17 23 22 20 22 22 21 22 18 30 | 8 11 5 7 32 5 7 8 4 18 3 | 26 29 28 28 28 25 26 29 26 21 26 31 | 6 16 12 10 43 5 17 8 9 16 4 | 16 25 21 19 51 15 25 18 18 17 16 32 | 8 14 7 7 43 4 16 8 5 16 3 | 16 23 22 22 28 17 20 18 22 19 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 17 8 9 36 5 17 9 7 18 |T 17 26 21 20 33 23 24 20 20 20 18 WRMS | 7 17 8 9 36 5 17 9 6 18 |NE 17 26 21 20 33 23 24 20 20 20 19 MEDI | 7 17 8 9 33 5 17 9 7 16 |MD 16 27 21 19 34 18 25 18 19 20 18 Table 3.1550.3 GPS week: 1550 Day: 3 MJD: 55097.000 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 | 20 --- --- 15 --- 27 --- 13 27 --- 11 | 56 --- --- 57 --- 70 --- 63 73 --- 61 2 | 5 23 9 9 40 4 19 10 7 20 4 | 18 31 16 20 42 18 28 19 21 27 19 3 | 9 16 10 8 17 4 13 11 9 19 4 | 15 25 21 17 24 15 27 17 17 25 17 4 | 8 13 7 9 42 5 12 10 10 14 3 | 18 27 22 26 30 18 27 21 22 18 20 X5 | 7 --- 8 9 --- 7 --- 10 10 26 5 | 7 --- 12 10 --- 29 --- 8 12 14 8 6 | 10 17 9 8 16 4 14 10 8 17 4 | 15 29 22 18 26 16 28 18 18 26 18 7 | 10 22 8 8 25 5 19 6 8 11 4 | 18 30 23 24 36 20 30 23 22 22 21 8 | 7 11 7 7 23 6 12 11 6 7 3 | 15 20 20 18 29 19 22 19 19 18 17 9 | 8 19 7 9 29 4 14 9 7 11 3 | 18 29 21 21 26 19 25 21 23 21 20 10 | 6 13 7 7 55 5 13 9 8 13 3 | 13 17 19 15 20 14 13 14 17 16 15 11 | 8 18 9 8 47 5 19 9 7 12 4 | 13 25 19 19 37 16 21 19 20 21 17 12 | 11 17 8 8 35 5 18 12 10 28 5 | 23 32 25 27 40 23 31 27 24 24 23 13 | 8 20 8 7 44 6 18 9 7 8 3 | 15 29 21 19 48 17 27 19 18 18 16 14 | 5 18 10 6 32 4 21 8 6 14 4 | 16 28 24 16 43 18 29 18 21 18 18 15 | 10 22 7 9 41 4 19 12 9 8 4 | 15 28 22 20 41 18 26 20 18 21 18 16 | 8 18 9 13 47 4 20 10 7 27 5 | 21 32 23 23 47 23 34 25 24 24 23 17 | 6 22 9 10 23 4 25 8 8 11 4 | 19 33 22 21 36 19 35 22 20 25 20 18 | 6 20 9 13 22 4 24 11 9 19 5 | 19 30 28 30 34 23 31 23 21 20 22 19 | 8 28 9 10 42 3 23 8 10 15 4 | 16 33 22 20 34 18 31 18 21 22 19 20 | 9 21 8 9 65 5 20 6 8 17 4 | 23 31 33 33 37 26 29 28 33 21 27 21 | 4 20 7 13 22 4 21 7 7 13 4 | 19 33 22 17 34 19 31 21 21 24 20 22 | 5 17 7 9 30 4 20 10 8 16 4 | 25 33 31 30 34 27 35 29 27 24 27 23 | 8 26 7 11 32 5 20 9 6 18 4 | 15 31 21 19 35 17 29 18 20 24 17 X24 | 18 19 15 20 --- 9 --- 6 15 --- 7 | 18 24 23 29 --- 19 --- 20 32 --- 19 25 | 7 14 11 10 --- 5 12 8 9 19 4 | 13 23 21 20 --- 17 24 19 20 23 17 26 | 8 18 8 11 18 4 13 10 7 18 4 | 17 28 17 21 29 17 28 20 18 19 17 27 | 10 19 9 10 31 6 15 9 9 11 4 | 14 27 21 19 29 18 24 19 21 21 17 28 | 7 18 8 12 64 5 20 8 8 42 5 | 22 33 25 26 51 24 34 24 22 45 23 29 | 6 18 9 8 22 5 17 9 6 13 3 | 22 26 19 21 25 20 29 23 20 24 20 30 | 6 10 6 7 25 2 10 7 7 18 3 | 28 30 30 30 32 27 30 33 31 26 29 31 | 7 23 8 8 39 5 19 11 8 14 4 | 18 31 21 19 49 19 30 18 21 19 19 32 | 9 16 8 11 39 6 15 7 6 15 4 | 19 22 29 28 27 21 24 22 25 20 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 8 10 37 5 18 9 8 18 |T 18 28 22 22 34 21 28 22 23 22 20 WRMS | 8 19 8 10 38 5 18 10 7 17 |NE 19 28 22 23 34 21 28 22 23 22 20 MEDI | 8 18 8 9 32 5 19 9 8 15 |MD 18 29 22 20 34 19 29 20 21 21 19 Table 3.1550.4 GPS week: 1550 Day: 4 MJD: 55098.000 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 --- --- 17 --- 23 --- 11 18 --- 9 | 37 --- --- 28 --- 43 --- 29 37 --- 32 2 | 6 17 10 9 35 4 19 8 6 23 4 | 15 24 13 13 40 15 24 14 15 22 14 3 | 6 14 8 9 31 4 13 10 7 19 3 | 13 24 19 18 27 17 25 14 17 25 15 4 | 6 15 10 7 35 4 10 8 9 15 3 | 22 29 22 22 28 20 28 24 21 24 22 X5 | 7 21 11 10 41 4 --- 7 12 29 5 | 7 22 15 10 27 17 --- 8 17 11 11 6 | 7 16 6 8 25 4 12 10 6 18 3 | 13 24 19 17 26 17 26 13 14 25 15 7 | 8 21 8 9 28 4 17 6 9 12 4 | 15 29 21 19 35 16 25 18 16 17 16 8 | 7 14 8 7 27 5 12 11 7 7 3 | 10 18 14 14 26 11 18 14 14 11 11 9 | 8 31 5 8 23 5 12 8 7 13 4 | 12 34 15 17 23 15 23 17 14 20 14 X10 | 5 15 9 9 --- 4 --- 7 9 15 3 | 15 26 24 19 --- 18 --- 18 23 17 17 11 | 7 17 7 9 31 5 14 8 6 14 3 | 15 26 20 16 35 14 20 15 16 16 15 12 | 10 16 8 11 41 4 16 8 7 28 4 | 16 28 20 20 38 20 28 20 14 23 17 13 | 6 19 7 8 42 4 19 7 8 8 3 | 12 25 17 13 40 14 24 14 16 13 13 14 | 5 19 7 7 33 5 18 8 5 15 3 | 12 26 18 14 43 14 24 11 14 12 12 15 | 8 22 11 6 36 4 24 11 9 10 4 | 12 23 17 17 36 14 26 17 14 19 14 16 | 8 20 7 12 37 3 18 11 9 27 4 | 18 29 20 19 37 21 29 18 18 18 17 17 | 4 20 5 8 23 4 21 7 6 11 3 | 15 29 15 14 35 14 27 18 18 19 16 18 | 7 21 8 13 24 4 19 7 7 19 4 | 15 30 22 23 31 19 26 18 22 15 18 19 | 6 29 9 10 29 4 20 8 9 16 4 | 14 32 17 15 28 15 25 13 15 17 13 20 | 7 18 6 11 49 5 19 8 10 18 4 | 23 30 24 27 32 24 28 28 26 23 24 21 | 6 23 8 12 22 2 21 6 10 12 4 | 13 30 17 14 32 16 28 16 24 19 16 22 | 8 18 6 9 20 5 18 8 6 18 4 | 22 31 25 25 36 22 30 22 23 18 22 23 | 7 26 8 11 32 4 19 7 8 17 4 | 11 30 18 17 37 15 25 15 20 19 14 X24 | 11 19 9 20 --- 10 --- 16 28 --- 8 | 14 23 18 25 --- 19 --- 20 42 --- 17 25 | 5 13 7 8 --- 5 11 8 6 19 3 | 9 17 15 12 --- 11 18 13 13 19 10 26 | 10 18 7 12 21 5 11 9 7 18 4 | 13 28 16 17 29 15 24 17 15 14 14 27 | 9 27 6 7 28 5 14 8 9 14 4 | 11 30 16 16 25 15 24 16 15 20 14 28 | 7 19 7 10 57 6 18 10 11 42 5 | 15 30 21 20 43 19 28 20 22 43 18 29 | 6 21 9 10 23 6 18 6 8 14 4 | 22 25 15 20 28 20 24 21 20 25 18 30 | 6 12 6 9 27 3 8 10 7 18 3 | 20 25 24 28 39 22 24 28 21 21 22 31 | 5 26 11 8 33 3 16 10 10 15 4 | 14 30 18 14 44 15 24 14 15 14 14 32 | 7 18 6 10 31 5 12 7 9 16 3 | 14 21 20 20 21 17 21 16 16 18 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 20 8 9 32 4 17 8 8 18 |T 15 26 18 18 32 17 24 17 18 19 16 WRMS | 7 20 8 9 33 4 17 8 7 17 |NE 15 26 18 18 32 17 25 17 19 19 16 MEDI | 7 19 8 9 31 4 17 8 8 16 |MD 14 28 18 17 32 16 25 17 16 19 15 Table 3.1550.5 GPS week: 1550 Day: 5 MJD: 55099.000 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 | 15 --- --- 21 --- 40 --- 13 17 --- 9 | 48 --- --- 48 --- 52 --- 45 47 --- 46 2 | 8 27 10 15 34 5 25 11 7 21 5 | 14 31 15 13 37 14 29 15 15 22 13 3 | 6 17 12 8 20 4 14 11 8 23 4 | 10 22 17 12 21 12 22 9 15 28 11 4 | 7 18 9 10 27 6 11 9 8 12 3 | 15 27 25 22 27 15 24 21 21 23 18 5 | 8 32 12 15 38 5 22 8 12 30 6 | 8 35 18 13 22 17 21 7 14 17 11 6 | 6 19 8 7 20 4 14 11 8 24 4 | 9 23 18 11 24 11 23 9 16 30 12 7 | 8 22 8 11 28 5 18 7 10 12 4 | 12 27 20 15 34 13 22 13 15 12 13 8 | 8 17 8 10 41 4 11 12 8 9 3 | 9 19 18 12 25 10 18 11 11 10 11 9 | 9 28 8 9 24 4 14 11 8 14 4 | 13 33 21 19 22 15 22 14 14 19 15 X10 | 4 --- --- --- --- 16 --- --- --- --- 0 | 10 --- --- --- --- 6 --- --- --- --- 11 11E | 6 14 7 8 28 4 15 8 11 14 3 | 14 24 19 14 38 13 20 15 18 20 14 12 | 9 21 10 12 27 3 16 9 7 28 5 | 13 30 22 22 29 16 24 16 14 17 15 13 | 9 26 7 8 29 5 20 9 13 7 4 | 11 29 17 15 39 14 22 13 13 11 11 14 | 7 21 9 7 23 4 20 9 10 15 4 | 13 28 19 14 33 16 24 13 18 15 14 15 | 8 39 8 10 34 8 21 13 9 12 5 | 13 46 19 17 33 17 27 18 16 23 16 16 | 8 22 13 14 29 7 20 12 10 28 5 | 13 30 23 17 29 15 27 15 16 15 15 17 | 7 22 7 9 23 4 19 7 12 13 4 | 12 30 14 13 34 14 24 15 18 18 13 18 | 8 29 8 16 23 7 20 8 7 20 5 | 12 33 22 23 35 17 24 15 17 13 15 19 | 6 26 11 7 29 4 20 6 9 18 4 | 13 31 14 14 32 10 23 10 12 17 11 20 | 7 20 7 9 67 6 21 7 12 17 4 | 20 29 26 23 36 21 23 23 21 17 20 21 | 6 31 8 14 23 6 24 8 14 12 5 | 14 35 13 12 29 15 28 17 25 20 13 22 | 5 20 6 12 21 6 19 7 8 18 4 | 16 28 23 24 34 21 27 19 23 16 19 23 | 7 28 8 9 30 5 21 9 10 15 4 | 10 31 19 14 30 14 23 13 13 19 12 X24 | 20 39 14 30 --- 19 --- 23 21 --- 10 | 11 37 16 31 --- 26 --- 33 35 --- 18 25 | 6 18 10 8 --- 6 11 11 11 18 4 | 8 20 19 13 --- 12 19 11 11 18 10 26 | 9 20 8 10 20 5 11 10 8 19 4 | 14 28 16 17 24 17 23 20 17 17 16 27 | 9 28 8 10 22 4 15 12 6 15 4 | 12 36 24 19 23 17 22 15 10 22 16 28 | 6 20 10 11 65 5 17 8 10 45 5 | 13 30 22 18 36 17 26 18 15 44 15 29 | 7 27 8 12 27 5 19 8 12 12 4 | 17 29 16 20 25 15 21 19 21 21 16 30 | 9 19 6 8 22 7 11 14 8 18 4 | 20 23 22 23 26 20 20 27 17 20 19 31 | 7 25 13 12 42 6 16 12 9 14 4 | 13 27 24 16 47 15 24 15 14 13 13 32 | 8 17 9 10 31 5 15 8 8 16 4 | 12 22 23 18 21 16 18 13 13 15 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 24 9 11 32 5 18 10 10 19 |T 13 29 19 18 30 16 23 16 17 19 15 WRMS | 8 23 9 11 34 5 18 9 8 18 |NE 13 29 19 18 29 16 23 16 17 19 15 MEDI | 7 22 8 10 27 5 18 9 9 16 |MD 13 29 19 17 29 15 23 15 16 18 14 Table 3.1550.6 GPS week: 1550 Day: 6 MJD: 55100.000 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 | 11 --- --- 13 --- 16 --- 13 17 --- 8 | 42 --- --- 43 --- 52 --- 46 47 --- 43 2 | 8 17 9 8 30 8 22 13 8 24 4 | 21 27 20 23 45 19 27 23 21 30 20 3 | 6 17 9 10 22 7 13 7 8 22 4 | 20 29 24 23 26 23 31 20 24 30 21 4 | 13 15 15 10 29 13 16 27 8 65 8 | 52 64 57 60 46 50 57 67 53 85 57 5 | 8 18 8 11 29 8 20 9 8 37 5 | 7 21 15 11 23 18 20 10 15 25 10 6 | 7 17 8 9 19 6 16 5 6 23 3 | 19 31 26 22 27 23 33 21 23 32 21 7 | 8 22 8 8 27 9 19 6 9 13 4 | 21 32 26 22 35 21 30 21 25 21 22 8 | 8 15 7 7 31 8 11 10 7 11 3 | 16 21 22 17 26 18 25 20 20 17 17 9 | 7 23 6 8 23 6 13 10 9 14 4 | 17 31 19 17 27 17 25 18 18 17 16 X10 | 7 13 7 5 27 7 --- 7 8 15 3 | 8 9 7 4 9 6 --- 4 5 3 8 11E | 7 14 6 10 31 5 15 7 10 21 3 | 19 24 20 18 36 18 23 17 20 21 17 12 | 8 15 9 9 40 7 17 8 12 26 4 | 26 34 28 26 45 26 32 26 22 23 24 13 | 6 21 8 6 36 8 22 10 10 7 4 | 18 31 22 18 45 20 32 20 19 19 18 14 | 6 17 9 8 20 6 23 6 8 14 4 | 17 25 22 19 35 16 27 17 19 19 17 15 | 8 19 10 8 31 7 23 15 11 10 4 | 17 28 20 21 39 19 31 24 21 23 19 16 | 6 17 10 8 35 10 19 13 8 30 4 | 24 35 26 25 38 26 37 27 26 28 25 17 | 7 24 10 11 22 11 23 6 10 19 4 | 21 36 22 19 32 22 32 23 26 29 22 18 | 6 28 10 13 30 7 20 7 11 22 5 | 19 38 27 29 39 24 28 23 23 20 22 19 | 6 25 9 9 28 8 20 7 6 20 4 | 21 34 22 22 33 23 31 20 24 26 21 20 | 7 21 7 12 67 7 22 8 12 19 4 | 29 36 32 37 45 31 31 33 32 30 30 21 | 7 20 7 12 22 9 23 5 11 12 4 | 23 37 26 21 33 23 37 23 23 28 22 22 | 6 16 9 10 25 8 19 6 11 19 4 | 24 32 31 30 33 28 31 28 28 25 26 23 | 7 28 10 11 32 8 24 8 10 16 5 | 18 36 22 19 37 23 33 20 22 23 19 X24 | 14 27 12 32 --- 25 --- 15 18 --- 9 | 19 26 25 32 --- 22 --- 22 33 --- 21 25 | 5 17 6 5 --- 8 12 10 8 19 3 | 16 20 21 17 --- 15 24 20 22 24 17 26 | 9 17 10 14 23 7 11 9 11 19 4 | 16 28 22 24 28 17 25 21 20 19 17 27 | 8 21 7 5 26 7 13 13 9 15 4 | 16 30 20 18 32 16 25 20 20 19 16 28 | 7 20 8 9 56 12 18 11 9 46 5 | 24 34 27 26 48 26 34 28 25 51 25 29 | 5 21 10 10 29 7 19 8 11 16 4 | 28 34 24 25 29 27 33 29 30 32 27 30 | 6 12 7 4 26 7 12 9 8 22 3 | 33 34 35 32 36 31 34 35 35 27 32 31 | 5 20 10 9 35 11 17 13 12 14 4 | 18 30 23 18 44 20 26 22 24 21 19 32 | 7 16 9 11 30 6 16 8 9 15 4 | 19 21 22 23 26 20 21 17 19 21 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 19 9 9 32 8 18 10 9 24 |T 21 30 24 23 34 23 30 23 24 26 22 WRMS | 7 19 9 9 31 8 18 8 8 20 |NE 21 30 24 23 34 23 30 24 24 26 22 MEDI | 7 18 9 9 29 8 19 8 9 19 |MD 19 31 22 22 35 22 31 21 23 23 21 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 4.1550 GPS week: 1550 MJD: 55094.0-55100.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3044 |U 8 8 19 |U 5 7 21 |U 7 7 15 | emr | emr 2929 | 9 11 22 |U 7 8 23 | 10 9 24 | esa | esa 2948 | 8 8 21 |U 5 7 19 | 7 7 17 | gfz | gfz 3041 |U 8 9 22 |U 6 7 21 | 7 7 17 | grg | grg 2729 | 8 8 23 |U 6 8 26 | 10 9 26 | igr | igr 2967 | 8 8 20 | 5 7 19 | 8 7 17 | igs | igs 2933 | 8 8 20 | 5 6 19 | 8 7 17 | jpl | jpl 2783 |U 9 9 22 |U 6 7 23 |U 9 8 26 | mit | mit 3044 |U 8 7 20 |U 6 7 22 |U 13 9 21 | 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 5.1550.0 GPS week: 1550 Day: 0 MJD: 55094.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3050 | 6 8 14 | 5 6 19 | 8 7 14 | emr | emr 2970 | 7 6 15 | 6 8 22 | 10 6 19 | esa | esa 2976 | 6 6 17 | 4 6 16 | 8 6 13 | gfz | gfz 3071 | 5 6 15 | 4 7 19 | 8 9 17 | grg | grg 2784 | 7 6 17 | 5 9 25 | 12 9 28 | igr | igr 2953 | 5 5 14 | 4 5 17 | 7 6 12 | igs | igs 2984 | 6 6 15 | 4 5 17 | 8 5 13 | jpl | jpl 2879 | 6 6 18 | 5 6 21 | 10 6 24 | mit | mit 3072 | 5 7 15 | 4 7 18 | 9 6 19 | Table 5.1550.1 GPS week: 1550 Day: 1 MJD: 55095.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3054 | 7 8 17 | 6 7 19 | 8 8 13 | emr | emr 2961 | 10 16 22 | 8 9 24 | 7 10 21 | esa | esa 2976 | 7 9 19 | 5 6 15 | 6 7 14 | gfz | gfz 3063 | 6 9 19 | 6 7 16 | 7 8 14 | grg | grg 2784 | 7 9 19 | 7 7 25 | 9 13 20 | igr | igr 2977 | 6 10 17 | 6 7 16 | 6 7 15 | igs | igs 2976 | 7 9 17 | 5 6 15 | 7 7 14 | jpl | jpl 2784 | 8 11 21 | 6 7 20 | 8 9 21 | mit | mit 3072 | 6 7 16 | 5 6 17 | 7 9 14 | Table 5.1550.2 GPS week: 1550 Day: 2 MJD: 55096.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2961 | 10 7 18 | 5 8 29 | 6 7 13 | emr | emr 2874 | 12 9 23 | 8 6 30 | 9 7 26 | esa | esa 2880 | 10 7 23 | 5 8 29 | 7 5 15 | gfz | gfz 2974 | 10 7 19 | 6 7 30 | 6 5 15 | grg | grg 2688 | 11 9 24 | 7 7 34 | 9 6 28 | igr | igr 2870 | 10 7 21 | 6 7 29 | 7 5 17 | igs | igs 2873 | 10 7 19 | 6 7 28 | 7 5 16 | jpl | jpl 2784 | 10 7 19 | 7 6 27 | 9 7 28 | mit | mit 2976 | 10 7 20 | 6 7 30 | 29 8 18 | Table 5.1550.3 GPS week: 1550 Day: 3 MJD: 55097.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3067 | 9 7 21 | 5 6 23 | 7 7 18 | emr | emr 2877 | 11 8 27 | 7 6 27 | 10 10 31 | esa | esa 2976 | 8 8 23 | 6 6 20 | 8 7 23 | gfz | gfz 3072 | 10 7 22 | 6 6 24 | 7 8 21 | grg | grg 2688 | 8 11 27 | 7 7 28 | 10 8 33 | igr | igr 3023 | 9 7 22 | 6 6 22 | 8 8 22 | igs | igs 2973 | 8 6 22 | 5 6 21 | 8 7 21 | jpl | jpl 2784 | 10 7 26 | 8 7 26 | 10 8 30 | mit | mit 3072 | 7 7 21 | 6 6 21 | 17 10 27 | Table 5.1550.4 GPS week: 1550 Day: 4 MJD: 55098.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3064 | 11 8 24 | 5 8 19 | 8 6 22 | emr | emr 2975 | 12 14 21 | 6 9 21 | 11 9 29 | esa | esa 2976 | 11 8 23 | 5 8 17 | 9 6 23 | gfz | gfz 3071 | 11 10 23 | 5 7 16 | 8 6 22 | grg | grg 2688 | 12 7 23 | 6 11 26 | 13 10 30 | igr | igr 3030 | 11 9 24 | 5 7 15 | 9 6 22 | igs | igs 2976 | 11 8 23 | 5 7 18 | 9 6 25 | jpl | jpl 2688 | 12 10 24 | 6 9 22 | 11 7 31 | mit | mit 3072 | 12 7 25 | 5 8 21 | 9 6 24 | Table 5.1550.5 GPS week: 1550 Day: 5 MJD: 55099.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3053 | 7 8 16 | 6 6 17 | 7 8 13 | emr | emr 2878 | 7 13 21 | 5 10 18 | 9 10 19 | esa | esa 2880 | 6 8 16 | 5 7 14 | 7 7 16 | gfz | gfz 2975 | 9 12 26 | 6 7 17 | 7 7 15 | grg | grg 2688 | 6 6 21 | 6 7 20 | 10 9 22 | igr | igr 2937 | 6 9 16 | 5 7 13 | 7 7 15 | igs | igs 2871 | 6 8 16 | 5 7 16 | 7 7 14 | jpl | jpl 2784 | 8 11 22 | 5 7 21 | 8 9 22 | mit | mit 2976 | 5 5 17 | 6 7 16 | 9 7 17 | Table 5.1550.6 GPS week: 1550 Day: 6 MJD: 55100.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3060 | 7 10 24 | 6 9 19 | 9 9 14 | emr | emr 2969 | 8 13 29 | 6 7 22 | 12 13 22 | esa | esa 2976 | 7 9 26 | 6 7 21 | 9 9 14 | gfz | gfz 3067 | 8 10 27 | 7 7 27 | 10 9 16 | grg | grg 2784 | 8 7 28 | 6 9 26 | 10 10 20 | igr | igr 2985 | 7 9 27 | 6 7 23 | 9 9 16 | igs | igs 2880 | 7 9 25 | 6 6 19 | 8 8 14 | jpl | jpl 2784 | 8 10 27 | 6 7 26 | 10 11 26 | mit | mit 3072 | 8 10 27 | 8 10 28 | 15 18 30 | 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 6.1550 GPS week: 1550 MJD: 55094.500-55100.500 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 -2 78 -7 8 | 4 12 | 22 18 53 51 4 | 3 emr uuxuu | 31 28 168 28 6 | 63 64 | 10 31 225 81 6 | 3 esa uuuuu | -2 -40 31 109 -6 | 24 26 | 8 26 94 120 9 | 2 gfz uuuuu | 1 34 -4 -55 1 | -5 9 | 12 16 54 37 1 | 2 grg xxxxx | -9 1 64 1 3 | 6 34 | 27 45 64 58 36 | 5 igr xxxxx | 9 46 88 26 -2 | 2 9 | 18 32 53 50 5 | 2 irf xxxxx | 7 -4 -17 14 1 | -3 9 | 10 14 28 29 3 | 2 jpl uuuuu | 18 -10 53 108 10 | 20 24 | 24 15 65 68 6 | 4 mit uuuuu | 8 12 -204 -33 4 | 10 13 | 16 23 85 45 1 | 3 ngs uuuuu | -41 -2 170 -29 -5 | 7 12 | 31 56 104 130 1 | 2 sio uuuuu | 35 -16 -86 -155 -8 | 36 38 | 18 24 70 70 7 | 2 Table 7.1550.0 GPS week: 1550 Day: 0 MJD: 55094.500 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 -18 95 8 1 | 0 8 emr uuxuu | 19 56 -152 -83 -5 | 58 59 esa uuuuu | 6 -69 55 -54 -10 | 23 25 gfz uuuuu | -8 33 18 -115 1 | -7 9 grg xxxxx | 1 16 95 -66 74 | -2 28 igr xxxxx | 11 55 42 -55 2 | -1 8 irf xxxxx | 16 -21 -21 32 -3 | -7 11 jpl uuuuu | -32 -17 -19 168 0 | 14 18 mit uuuuu | 12 -19 -218 26 4 | 5 9 ngs uuuuu | -21 65 174 116 -3 | 5 10 sio uuuuu | 52 -45 -126 -13 -17 | 35 37 Table 7.1550.1 GPS week: 1550 Day: 1 MJD: 55095.500 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 | -17 4 160 -3 12 | 1 8 emr uuxuu | 20 61 -40 -31 3 | 59 60 esa uuuuu | -3 -61 179 221 -20 | 23 26 gfz uuuuu | 11 26 8 -54 -1 | -7 9 grg xxxxx | -34 -7 59 1 -32 | 6 38 igr xxxxx | 11 3 99 -14 -6 | 0 9 irf xxxxx | 7 -19 -26 24 -3 | -5 10 jpl uuuuu | 25 -21 145 38 17 | 15 19 mit uuuuu | 20 -11 -314 -41 5 | 7 11 ngs uuuuu | -78 46 127 -51 -5 | 6 11 sio uuuuu | 47 -38 -171 -160 -13 | 36 38 Table 7.1550.2 GPS week: 1550 Day: 2 MJD: 55096.500 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 | 20 -18 84 32 8 | 4 13 emr uuxuu | 23 43 60 -27 3 | 62 63 esa uuuuu | 8 -41 -4 143 1 | 23 26 gfz uuuuu | -17 11 91 -67 1 | -5 9 grg xxxxx | 3 -22 144 62 -28 | 7 38 igr xxxxx | -3 38 194 61 -7 | 3 9 irf xxxxx | -6 -6 -17 -42 -1 | -4 10 jpl uuuuu | 14 -27 3 199 14 | 19 24 mit uuuuu | -7 7 -239 -103 4 | 9 14 ngs uuuuu | -4 23 167 8 -7 | 8 12 sio uuuuu | 3 -21 -115 -197 -11 | 38 39 Table 7.1550.3 GPS week: 1550 Day: 3 MJD: 55097.500 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 | -41 -3 86 -6 13 | 5 14 emr uuxuu | 30 4 219 10 9 | 64 65 esa uuuuu | -3 -67 59 -32 8 | 25 27 gfz uuuuu | 0 44 0 -31 0 | -4 8 grg xxxxx | -40 8 43 47 8 | 2 37 igr xxxxx | 3 21 106 60 3 | 4 9 irf xxxxx | -7 -7 -38 -3 1 | -2 8 jpl uuuuu | 19 9 47 161 6 | 21 27 mit uuuuu | -21 14 -239 -38 4 | 11 15 ngs uuuuu | -2 16 178 85 -5 | 9 12 sio uuuuu | 16 -3 -108 -175 -11 | 39 40 Table 7.1550.4 GPS week: 1550 Day: 4 MJD: 55098.500 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 | 10 -8 41 66 2 | 6 14 emr uuxuu | 43 -20 414 123 9 | 65 66 esa uuuuu | -1 -12 -121 102 -8 | 26 28 gfz uuuuu | 4 53 -41 -64 0 | -4 8 grg xxxxx | -29 -45 40 -91 17 | 9 31 igr xxxxx | -16 47 52 69 3 | 4 9 irf xxxxx | 14 4 -22 13 2 | -2 8 jpl uuuuu | 32 -9 128 25 14 | 22 27 mit uuuuu | 14 22 -127 -72 3 | 12 15 ngs uuuuu | -60 -31 217 20 -4 | 9 12 sio uuuuu | 48 -23 -42 -154 -6 | 37 39 Table 7.1550.5 GPS week: 1550 Day: 5 MJD: 55099.500 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 | -22 -8 -13 -85 8 | 7 14 emr uuxuu | 37 7 452 111 15 | 67 68 esa uuuuu | -16 -16 -29 112 -6 | 27 28 gfz uuuuu | 20 52 -80 -59 1 | -4 8 grg xxxxx | -5 -36 118 28 -10 | 11 31 igr xxxxx | 15 54 57 67 -4 | 4 8 irf xxxxx | 11 17 -37 31 5 | -1 7 jpl uuuuu | 25 11 72 98 11 | 25 29 mit uuuuu | 19 51 -235 11 3 | 13 15 ngs uuuuu | -63 -101 337 -112 -6 | 9 12 sio uuuuu | 40 27 -87 -147 -1 | 36 38 Table 7.1550.6 GPS week: 1550 Day: 6 MJD: 55100.500 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 36 90 -57 10 | 5 13 emr uuxuu | 43 43 221 95 10 | 66 66 esa uuuuu | -4 -13 79 273 -9 | 23 25 gfz uuuuu | -3 22 -27 8 2 | -6 10 grg xxxxx | 37 90 -52 26 -6 | 10 32 igr xxxxx | 43 105 63 -5 -6 | 2 10 irf xxxxx | 14 6 43 44 5 | -3 7 jpl uuuuu | 41 -15 -4 71 3 | 23 27 mit uuuuu | 15 17 -55 -15 4 | 10 14 ngs uuuuu | -59 -32 -12 -265 -5 | 6 11 sio uuuuu | 39 -7 47 -239 1 | 33 34