[IGSREPORT-30230] Wk 2343 IGLOS Final Orbits

acc acc at igs.org
Fri Dec 20 06:03:58 UTC 2024


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2343   (Dec 01, 2024 - Dec 07, 2024) 
                                                                               
Contact: acc at igs.org
                                                                               
                                                                               
COMBINATION STRATEGY:                                                            
---------------------                                                            
                                                                               
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.2343.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed
to the values of the final IGS (GPS) combination.                                                    
                                                                               
                                                                               
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.
                                                                               
  Weber R., 2000, IGS Technical Report 1999                                    
                                                                               
                                                                               
PRODUCTS GENERATED:                                                             
-------------------                                                             
                                                                               
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
                                                                               
The following naming convention is used for the result files:
                                                                               
 igl2343[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2343 in the SP3 format.
 igl23437.sum      Combination Report for GPS Week 2343.


    
    
REMARKS concerning the IGL Orbit Combination:                                  
---------------------------------------------

Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.

Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.

 1. Broadcast (brd) orbits and clocks are included in the combination for
    statistics only.

 2. Having only a few satellites the mcc orbits are included in the combination 
    for statistics only. The grg orbits are introduced for the first time
    starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
    22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
    21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
    for the first time starting 11-Sep-2011 (GPS Week 1653).

 3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
    BKG, ESA, and CODE referred their GLONASS orbit products to the following
    satellite antenna offset (SAO) values (expressed in the spacecraft body
    frame):
    
      X/Y/Z =  0.000/0.000/0.000 meter for GLONASS and
      X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
    
    Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
    (GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
    (IGSMAIL #5438). The antenna phase center offsets and phase center variations
    are given in the file:
        https://files.igs.org/pub/station/general/igs05.atx
    These antenna calibrations are also used in the homogeneously reprocessed IGS
    products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
    Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
    model is updated (IGSMAIL #6255 & #6374) as given in the file:
        https://files.igs.org/pub/station/general/igs08.atx
    
    Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
    model file has been updated to igs14.atx to be consistent with IGS14.
    See IGSMAIL #7399 for more information
        https://files.igs.org/pub/station/general/igs14.atx 

 4. The satellite clock values in the combined orbit files are taken from the
    broadcast files. The following gps/glonass time offsets were added to the
    broadcast clocks. Before GPS Week 1637, the time offsets were derived
    from the bkg summary files; starting Week 1637 the offsets are derived
    from the gfz summary files.
    
               Day | applied clock offset
               ----+---------------------
                0  |     17.0 ns
                1  |     15.7 ns
                2  |     15.9 ns
                3  |     14.8 ns
                4  |     11.1 ns
                5  |     11.6 ns
                6  |      5.5 ns

 5. The following orbit solutions were excluded from the combination
    because they were biasing the weighted average (generally indicated
    by long arc RMS).
    
               Day | Centre | PRN list
               ----+--------+---------------
                5  |  GFZ   | R11
                6  |  GRG   | R11

    
         
ORBIT COMBINATION AND EVALUATION STATISTICS:                                    
--------------------------------------------                                    
      
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 (Tables 1.2343, 1a.2343).
        
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 2.2343.0-6)                                                                                
    
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 3.2343.0-6). 
        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.
                                                                               
   
      
      
Table 1: Week 2343 summary.                      (Dec 01, 2024 - Dec 07, 2024)

Table 1.2343.a     GPS week : 2343   MJD: 60645.0-60651.0

         Mean and standard deviations of transformation parameters to the 
         combined IGL 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  n/a|   -1     0    -2   -21     1    83   .18   20   17 |    5930    1752   3336  10223
        |    0     0     2    13    17    24   .03           |    2097    1481
esa  n/a|    0     0     0   -12    -3    13  -.14   33   25 |   15256    1335   3304   8592
        |    1     0     2    13    10    19   .02           |    5989    1600
gfz  n/a|    1     0     1    28    20    11  -.05   39   16 |       0    1801   3266   7617
        |    0     2     2     7    11    36   .03           |       0    1723
grg  n/a|    0     0     5    -5   -42   -36   .32   43   21 |   10570    1926   3312   9857
        |    1     1     3     9    27    34   .03           |    4573    1434
iac  n/a|    0     0    -5     0    14   -44  -.12   16   15 |   13411    -914   3329   9813
        |    1     0     2    16    20    52   .03           |    4288     748
jgx  n/a|   -1     0     5    -7   -21    -6  -.18   24   24 |    8579    1767   3372   7909
        |    0     2     1    22    16    28   .04           |    2141    1392


Table 1.2343.b     GPS week : 2343   MJD: 60645.0-60651.0   

         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
------+------------------------------------+------------------------------------------
 R01  |   14   14   15   18   18   16   12 |
 R02  |    8    7    7    6    7    5    8 |
 R03  |    7    7    8    7    7    6    9 |
 R04  |    8    7    8    9   10    7   10 |
 R05  |    6    9    7    8    8    7    7 |
 R07  |    7    6    8   10    8    8    8 |
 R08  |    6    8    8    5    8    8    9 |
 R09  |    6    6    6    6    8    8    6 |
 R11  |    7    7    6    6   14    7   23 |
 R12  |    7    7    8    8    7    7    7 |
 R14  |    6    5    6    5    7    6    6 |
 R15  |    8    7    6    6    9    7   10 |
 R16  |   10    8    8    7    9    8    8 |
 R17  |    7    9    9    7    7    7    6 |
 R18  |    7    8    7    7    8    7    9 |
 R19  |   17   20   23   20   20   18   22 |
 R20  |   23   22   19   18   22   24   23 |
 R21  |    7    8    8    9    8    7    7 |
 R22  |    6    6    6    6    6    8    6 |
 R24  |    8    7   11    9   10   10    8 |
 R26  |   28   31   29   32   33   31   30 |


Table 1.2343.c     GPS week : 2343   MJD: 60645.0-60651.0   

         Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
         Mean and standard deviations of the transformation parameters for the
         whole gpsweek.

CEN WEEK DAY |   DX    DY    DZ     RX      RY      RZ   SCL   RMS   WRMS |    TOFT   TDRFT
             |  [mm]  [mm]  [mm]  [uas]   [uas]   [uas] [ppb]  [mm]  [mm] |    [ps]  [ps/d]
-------------+------------------------------------------------------------+----------------
brd 2343 0   |  -13    65   -77    -572     442   -5935  81.8  1695  1695 |   16980       0
brd 2343 1   |  -65    28   -24   -2245    2304   -4314  82.0  1519  1519 |   15657       0
brd 2343 2   |   59    32   -90   -1174    5139   -1212  81.3  1263  1263 |   15922       0
brd 2343 3   |  -18    20    -9      95     885   -8901  80.3  1605  1605 |   14757       0
brd 2343 4   |  -11    72   -10    1379    1522   -2975  79.0  1500  1500 |   11135       0
brd 2343 5   |  -12    14   -86     612    2065    -912  82.4  1485  1485 |   11597       0
brd 2343 6   |  -11   -59  -167    1443     183   -2617  80.0  1513  1513 |    5487       0
-------------+------------------------------------------------------------+----------------
brd 2343 mean|  -10    25   -66     -65    1791   -3838  81.0  1511  1511 |   13076       0
brd 2343 sdev|   36    43    57    1359    1675    2826   1.2   132   132 |    4007       0



Table 2: Daily transformation of each centre to the combined IGL 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 2.2343.0  GPS week: 2343   Day: 0   MJD: 60645                            

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  n/a|   -1     1     0   -18     6    72   .21   19   16 |    2706     913   3267  10256
esa  n/a|    0     0     1   -21     7     3  -.15   31   20 |   23282     905   3200   9814
gfz  n/a|    1     0     1    27    31    -6  -.02   18   15 |       0    1471   3213   7424
grg  n/a|    0     0     8     0   -26   -17   .33   29   19 |   14740    1191   3253   9817
iac  n/a|    0     0   -10    15    15   -55  -.12   15   14 |   17109    -793   3251   9800
jgx  n/a|   -1     0     9    12   -46    20  -.11   23   23 |    5089    1470   3198   7494

Table 2.2343.1  GPS week: 2343   Day: 1   MJD: 60646                            

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  n/a|   -2     0    -5   -27     8   100   .12   22   17 |    3691     756   3287  10461
esa  n/a|   -1     0     0   -31   -14     2  -.15   31   27 |    9086     257   3087   7611
gfz  n/a|    0     3     1    41    28   -24  -.07   19   16 |       0     618   3073   7370
grg  n/a|    1     0     1    -3    -2   -54   .32   23   15 |   13484    1015   3303  10043
iac  n/a|    1     0    -3   -23    11    42  -.09   15   13 |   16357   -1201   3269  10002
jgx  n/a|    0    -2     4    -9   -24   -53  -.19   24   24 |    6639     602   3117   7693

Table 2.2343.2  GPS week: 2343   Day: 2   MJD: 60647                            

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  n/a|   -3    -1    -2   -28    10    71   .18   21   21 |    6121    1122   2849   9114
esa  n/a|   -1     0    -2   -14   -14    23  -.12   33   28 |   21246     323   2840   7467
gfz  n/a|    1     2     2    16    18    54  -.04   18   15 |       0     705   2831   7102
grg  n/a|    0     0     1    -5   -25   -75   .29   26   21 |   14020     937   2834   8704
iac  n/a|    0    -1    -4    -8   -20   -63  -.09   17   16 |   16887   -1334   2832   8848
jgx  n/a|   -1    -2     5    10   -35    21  -.16   24   24 |    8728     866   2877   7498

Table 2.2343.3  GPS week: 2343   Day: 3   MJD: 60648                            

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  n/a|   -1     0    -4   -40     2   131   .17   21   16 |    6401    3569   3097   9757
esa  n/a|   -1     0     0    -6     3    47  -.09   33   34 |   16480    2648   3107   7039
gfz  n/a|    1     0     1    25    22    59  -.03   20   16 |       0    3836   3105   7943
grg  n/a|    1    -1    11     6   -30   -39   .29   26   21 |   12194    3674   3117   9512
iac  n/a|    0     0    -5    -5    -2  -132  -.11   13   12 |   14679      37   3099   9524
jgx  n/a|   -1     0     3    17   -11    16  -.16   23   23 |    8558    4043   3120   8174

Table 2.2343.4  GPS week: 2343   Day: 4   MJD: 60649                            

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  n/a|   -1     0    -3    -5    -8    68   .19   22   20 |    7984    -189   3763  10716
esa  n/a|    1     0     1    10    -1    10  -.12   30   25 |   10616    -899   3796   8440
gfz  n/a|    2    -1     0    26    20    32  -.02   27   20 |       0    -456   3710   8492
grg  n/a|    1     0     7   -13   -68   -75   .35   27   19 |    9390     262   3766  10398
iac  n/a|   -1     0    -5    16    26   -19  -.14   18   17 |   12817   -2217   3759  10277
jgx  n/a|    0     2     4   -13   -22   -20  -.23   24   24 |   10363     144   3793   8603

Table 2.2343.5  GPS week: 2343   Day: 5   MJD: 60650                            

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  n/a|    0     0     0   -26   -33    80   .22   20   15 |    8476    2474   3517  10946
esa  n/a|    2     1     1    -9     7    18  -.17   31   20 |    8348    2634   3506  10081
gfz  n/a|    1     0    -3    32    -1    -3  -.08  148   16 |       0    2251   3602   7390
grg  n/a|   -1    -1     4    -3   -77   -12   .31   25   21 |    8507    2531   3531  10637
iac  n/a|    0     2    -3    -9    42   -54  -.16   18   17 |   10817    -595   3514  10371
jgx  n/a|   -1     2     5   -27     3    -3  -.20   24   24 |   11377    2407   3488   7955

Table 2.2343.6  GPS week: 2343   Day: 6   MJD: 60651                            

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  n/a|   -2     1    -1    -4    22    59   .15   17   16 |    6134    3621   3578  10315
esa  n/a|    1    -1     4   -16   -12   -14  -.14   46   25 |   17734    3478   3595   9693
gfz  n/a|    1    -1     3    33    27   -28  -.06   20   15 |       0    4185   3329   7602
grg  n/a|    3     0     4   -21   -64    16   .37  143   30 |    1658    3876   3384   9891
iac  n/a|    1     0    -7    20    27   -30  -.11   18   15 |    5213    -297   3580   9873
jgx  n/a|   -1     1     4   -40   -14   -26  -.21   23   23 |    9304    2839   4014   7948

       
       
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 IGL column gives resulting satellite accuracy measures found in
         SP3 header. The last IGL column gives the RMS fit of the IGL 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 IGL 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 3.2343.0  GPS week: 2343   Day: 0   MJD: 60645                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  707   39   41   29   26   15   39   14 |    86   38   69   52   55   43    55
 R02  | 1098   13   21    9   29   16   19    8 |    69   76   59   54   67   51    61
 R03  | 1493   12   16   12   12   16   25    7 |    88   71   87   80   88   62    80
 R04  |  622   21   14   20   13    8   26    8 |   121  116  117  111  113  106   113
 R05  | 1541   12    8   18   14   11   14    6 |   226  230  231  234  219  226   227
 R07  | 2733   17   16   15    9   13   18    6 |    91   64   70   81   90   72    79
 R08  | 1388    7   15   14   10   15   19    6 |   103   94  106   99  114   95   102
 R09  | 2929   16   10   15   14   15    7    6 |    29   40   38   30   33   31    31
 R11  | 1752   15   18   13   17   16   17    7 |    27   30   58   55   31   31    24
 R12  | 1296   10   18   12   21   12   17    6 |    72   72   70   63   75   55    68
 R14  | 1317   15   14   14   11    8   18    6 |    78   84   81   78   81   65    77
 R15  | 2045   16   12   16   15   18   23    7 |   109   99   90   93  108   86    97
 R16  | 2066   24   20   26   21   20   18   10 |   104   93   76   85   97   78    87
 R17  | 1304    7   18   13   15   17   19    6 |    36   31   36   40   37   14    33
 R18  |  810   11   16   16   16   11   26    7 |    28   34   33   31   28   24    27
 R19  | 1082   36   66   19   52   22   36   17 |    62   32   60   61   53   47    50
 R20  | 2566   31   90   37   94   14   34   23 |    67   52   50   88   57   37    49
 R21  | 1792    9   21    9   18   10   24    7 |    41   34   40   48   43   31    39
 R22  | 1477   14   17   14   14   12   12    6 |    22   36   32   27   23   28    25
 R24  | 1527   16   24   13   23   18   16    8 |    45   32   42   49   39   31    38
XR26  |14972   34  ---  ---   39   43  ---   28 |    52  ---  ---   53   73  ---    60
------+-----------------------------------------+-------------------------------------
 RMS  | 1695   19   31   18   29   15   23      |T   74   67   72   72   72   60    67
 WRMS | 1695   16   20   15   19   14   23      |NE  74   67   72   72   72   60    67
 MEDI | 1493   15   17   14   16   15   19      |MD  69   52   60   61   67   47    60

Table 3.2343.1  GPS week: 2343   Day: 1   MJD: 60646                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  734   44   45   21   20   17   43   14 |    65   34   46   44   46   35    40
 R02  | 1296   23   16   13   14   13   12    7 |    61   48   38   47   34   39    41
 R03  | 1697   19   16   15   15    9   19    7 |    71   64   71   66   63   56    64
 R04  | 1085   15    8   15   16   11   18    6 |   136  134  139  134  127  134   133
 R05  | 1122   13   12   24   17   16   29    8 |   215  217  218  224  202  213   214
 R07  | 2599   17   14   15   10    6   13    5 |    69   63   62   70   63   58    63
 R08  | 1035   13   15   17    9   20   22    7 |    93   88   84   89   95   90    89
 R09  | 2861   13   12   16   13   16    8    6 |    41   47   56   47   36   44    44
 R11  | 2239   15   14   26    9   11   19    7 |    32   37   41   51   30   36    30
 R12  | 1380   12   18   15   14   11   25    7 |    52   58   57   59   49   41    51
 R14  |  913    9   23    7    9    8   11    5 |    54   62   47   51   47   49    50
 R15  | 1396   21   10   12    9   15   18    6 |    88   73   75   77   70   62    74
 R16  | 1471   20   18   15   12   16   24    8 |    85   78   63   70   73   64    70
XR17  | 1220   12   23   15   11   23  ---    9 |    35   29   26   31   34  ---    29
 R18  |  690   10   21   15    9   18   31    8 |    35   30   32   33   25   31    28
 R19  | 1049   47   73   18   56   31   39   20 |    53   43   48   58   39   50    45
 R20  | 2100   30   77   46   68   19   39   21 |    48   48   44   59   35   35    39
 R21  | 1147    9   31   19   14   14   23    8 |    36   39   39   36   38   32    35
 R22  |  920   16    8   17    9   12    8    5 |    27   40   40   33   30   39    33
 R24  |  533   16   28    9    9   11   20    7 |    32   36   30   32   28   35    30
XR26  |16093   37  ---  ---   40   48  ---   30 |    53  ---  ---   51   67  ---    56
------+-----------------------------------------+-------------------------------------
 RMS  | 1519   22   31   19   23   15   24      |T   65   63   62   64   58   60    59
 WRMS | 1519   17   27   16   15   13   24      |NE  65   63   62   64   58   60    59
 MEDI | 1220   16   16   15   13   15   20      |MD  53   48   47   51   46   44    45

Table 3.2343.2  GPS week: 2343   Day: 2   MJD: 60647                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  819   42   51   15   28   26   40   15 |    59   33   32   33   49   21    31
 R02  | 1057   11   13   15   19   13   13    6 |    66   61   60   72   51   58    60
 R03  | 1781   20   14   14   16   15   20    7 |    95   82   86   83   73   64    79
 R04  |  602   23   12   16   16   15   23    8 |    88   82   82   88   81   78    81
 R05  | 1300   21   15   12   16   15   16    7 |   151  153  150  152  143  144   148
 R07  | 1239   16   22   11   15   17   19    7 |    77   57   71   66   75   61    68
 R08  |  949   16   15   12   17   25   18    8 |    76   79   80   76   93   74    79
 R09  | 2610   15    9   14    9   17    8    6 |    19   27   32   24   30   22    24
 R11  | 1881   16   19    8   12   15   13    6 |    19   30   66   67   24   17    17
 R12  | 1415   12   18   21   12   19   22    8 |    58   67   69   49   54   51    56
 R14  |  996    7   21   15   10    9    8    5 |    56   65   52   49   54   55    53
 R15  |  816   19   12   16    8   10   12    6 |    80   71   65   68   76   67    70
 R16  |  926   22   20   10   11   13   21    7 |    86   87   80   77   70   66    76
XR17  | 1594   14   26   16   17   14  ---    8 |    31   32   33   24   23  ---    25
 R18  |  829    9   20   14   14   14   21    7 |    25   26   22   27   26   23    22
 R19  | 1342   35   82   26   81   30   50   23 |    54   38   56   57   36   67    47
 R20  | 1499   30   78   37   39   15   46   18 |    41   28   45   36   36   32    31
 R21  |  598   10   28   21   10   17   20    8 |    28   23   36   33   36   20    28
 R22  |  665   16   15   14    7   17    8    6 |    13   23   25   22   20   17    16
 R24  |  662   21   24   20   34   13   28   10 |    41   33   39   39   31   29    31
XR26  |18400   28  ---  ---   37   50  ---   29 |    46  ---  ---   43   60  ---    49
------+-----------------------------------------+-------------------------------------
 RMS  | 1263   21   33   18   26   17   24      |T   57   54   59   56   54   50    51
 WRMS | 1263   21   28   15   21   16   24      |NE  57   54   59   56   54   50    51
 MEDI | 1057   16   19   15   16   15   20      |MD  56   38   56   49   51   55    49

Table 3.2343.3  GPS week: 2343   Day: 3   MJD: 60648                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  899   44   45   31   49   22   51   17 |    66   44   49   28   40   26    35
 R02  | 1152    8   18   10    9   11   15    5 |    45   53   40   39   42   32    40
 R03  | 1976   17   16   20   19   10   12    7 |   105   93  105   91   97   91    97
 R04  |  769   21   11   17   33   13   17    8 |   122  112  124  105  111  106   113
 R05  |  777   19   13   17   23   12   22    7 |    99   88  103   88   90   79    90
 R07  | 1863   17   21    8   16   22   35    9 |   100   87   94   95  106   88    95
 R08  |  751    8    9   17   11    8   10    4 |   105  103  102  108  106  108   105
 R09  | 2229   14   18   13   14    7   11    5 |    20   35   26   22   21   26    22
 R11  | 2049   13   15   12   18   12   10    6 |    17   24   92   57   23   18    17
 R12  | 1866   12   21   21   18   14   18    7 |    48   56   46   38   40   35    41
 R14  | 1165   10   14   11   14    6   15    5 |    56   61   61   59   57   48    56
 R15  |  962    9   17   18   15   11   14    6 |    69   69   86   60   77   64    71
 R16  | 2515   20   18   19   11   12   14    7 |    69   68   50   51   61   50    57
XR17  | 1518   13   19   12   18   11  ---    7 |    34   36   30   41   28  ---    30
 R18  |  705   18   18   17   24    5   18    7 |    25   32   35   29   24   20    24
 R19  | 1666   41   89   36   55   12   35   19 |    70   45   77   60   54   49    56
 R20  | 3297   31   73   39   45   25   30   17 |    59   38   50   53   49   49    46
 R21  |  484   17   30   22   21   10   25    9 |    30   27   40   40   36   27    32
 R22  | 1257   15   14   12   17   10   13    6 |    15   21   24   25   18   25    19
 R24  |  631   17   30   17   23    9   21    8 |    43   32   43   46   33   34    35
XR26  |19801   46  ---  ---   45   45  ---   32 |    39  ---  ---   43   64  ---    49
------+-----------------------------------------+-------------------------------------
 RMS  | 1604   21   33   20   26   13   23      |T   58   56   63   56   56   51    53
 WRMS | 1604   16   34   16   21   12   23      |NE  58   56   63   56   56   51    53
 MEDI | 1257   17   18   17   18   11   17      |MD  56   45   50   51   49   48    46

Table 3.2343.4  GPS week: 2343   Day: 4   MJD: 60649                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  827   55   31   29   46   15   45   17 |    63   20   43   30   30   21    28
 R02  | 1413   12   16   13   17   16   12    6 |    57   57   45   64   44   45    50
 R03  | 1171   14   17   16   12   14   22    7 |    85   75   79   79   89   64    78
 R04  | 1425   20   17   16   30   28   19   10 |   120  120  115  102  114  108   111
 R05  | 1022   19   12   10   26   16   20    8 |   199  188  190  196  191  188   192
 R07  | 2637   20   13   15   16   15   23    8 |    81   63   75   67   73   59    69
 R08  |  569   16   12   17   11   18   22    7 |    73   61   68   64   67   61    64
 R09  | 1410   12   16   23   19   13   15    7 |    27   33   39   26   36   31    30
 R11  | 1454   16   30   60   21   14   26   14 |    24   42  110   66   32   23    29
 R12  | 2093   13   11   14   16   14   18    6 |    59   51   50   46   50   45    49
 R14  |  946   11   16   13   13   16   17    6 |    51   57   58   58   45   52    52
 R15  |  920   13   25   21   16   18   27    9 |    79   75   89   65   84   66    75
 R16  | 2913   14   19   16   26   21   26    9 |    84   92   95   67   95   71    83
 R17  |  878    9   13   12   18   11   22    6 |    29   29   28   36   26   17    26
 R18  | 1168   15   24   15   19   11   17    7 |    27   37   37   31   28   26    28
 R19  |  707   41   65   39   60   23   42   20 |    47   48   62   49   45   44    43
 R20  | 2664   36   74   68   51   35   25   22 |    59   46   50   63   55   64    52
 R21  |  706    9   28   10   23   13   13    7 |    35   33   35   44   38   35    35
 R22  | 1041   15   19   17   13   11    9    6 |    16   24   27   26   27   23    20
 R24  |  744   12   36   24   18   19   23   10 |    34   31   45   43   32   33    33
XR26  |13855   38  ---  ---   39   56  ---   33 |    32  ---  ---   41   73  ---    48
------+-----------------------------------------+-------------------------------------
 RMS  | 1500   22   30   27   27   18   24      |T   61   59   67   60   60   53    56
 WRMS | 1500   20   25   20   19   17   24      |NE  61   59   67   60   60   53    56
 MEDI | 1168   15   17   16   19   16   22      |MD  57   48   50   58   45   45    49

Table 3.2343.5  GPS week: 2343   Day: 5   MJD: 60650                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  895   48   38   28   32   14   49   16 |    57   47   57   33   30   34    38
 R02  |  982    6   17   13   12   10   12    5 |    45   50   50   45   44   40    44
 R03  |  523    7   26    9   13   10   17    6 |   115  106  117  117  117  106   113
 R04  | 1408   12   16   11   15   12   22    6 |    79   77   83   77   78   72    77
 R05  | 2216   18   13   14   20   10   16    7 |   118  122  118  115  119  116   117
 R07  | 2541   16   20   13   19   13   21    7 |    85   82   82   72   79   75    79
 R08  |  684   13   13   12   15   26   18    8 |    81   80   78   86  100   72    83
 R09  |  688   12   25   12   20   14   19    7 |    19   38   31   23   30   23    24
 R11  | 2461   11   15  658   13   12   13    6 |    21   48  596  203   30   27    23
 R12  | 2400   10   15   13   22   15   12    6 |    59   63   52   52   66   59    57
 R14  | 1393   14    8    9   11   13   18    5 |    51   51   60   60   57   51    55
 R15  | 1048   14   14   15   13   19   20    7 |    76   67   82   72   67   65    71
 R16  | 2250   19   25   13   17   10   21    7 |    78   69   73   78   73   62    71
 R17  |  824   11   10   15   12   13   25    6 |    27   25   31   28   19   18    22
 R18  | 1309   13   26   10   12   12   21    7 |    23   31   21   28   24   22    22
 R19  |  670   39   72   16   56   33   22   18 |    36   43   37   41   34   40    34
 R20  | 1195   42   76   56   61   43   45   23 |    29   54   50   52   32   58    35
 R21  |  789    6   22   12   25    8   20    7 |    31   29   34   36   27   23    29
 R22  | 1573   15   17   20   19   19   13    8 |    19   22   31   24   27   21    20
 R24  |  698   10   30   22   11   11   35    9 |    33   26   38   29   26   20    27
XR26  |15544   37  ---  ---   40   49  ---   30 |    24  ---  ---   44   48  ---    35
------+-----------------------------------------+-------------------------------------
 RMS  | 1485   20   31  148   25   18   24      |T   52   56   86   62   53   50    51
 WRMS | 1485   15   20   16   21   17   24      |NE  52   56   86   62   53   50    51
 MEDI | 1195   13   17   13   17   13   20      |MD  45   50   52   52   44   40    38

Table 3.2343.6  GPS week: 2343   Day: 6   MJD: 60651                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1109   31   33   27   32   15   19   11 |    79   49   71   43   56   46    54
 R02  | 1036   11   11   28   21   11   20    8 |    70   73   81   65   70   60    68
 R03  |  944   12   15   26   23   12   22    8 |   120  105  125  111  114  106   114
 R04  | 1164   22   23   15   19   18   28    9 |   114   99  104   91  104   85    99
 R05  | 2327   11   13   11   18   16   21    6 |   163  165  163  160  163  156   161
 R07  | 1725   16   25   16   16   14   20    8 |    87   80   88   73   83   71    80
 R08  |  998   12   19   19   16   26   18    8 |    80   74   81   77   89   66    77
 R09  |  660   12   19   16   12   11    7    6 |    18   32   27   23   22   24    21
 R11  | 2633   18  121   13  608   18   33   22 |    25   48  117  226   28   25    23
 R12  | 1951    8   25   11   16   13   16    6 |    73   83   65   64   76   60    69
 R14  | 1423   13   14    9   13   18   12    6 |    64   73   68   63   77   65    67
 R15  | 1625   15   19   19   43   17    8    9 |    96   75   80  106   87   81    86
 R16  | 1053   18   25   13   16   18   21    8 |    94   77   82   88   81   78    83
XR17  | 1368    9   12   13   12   10  ---    5 |    44   40   48   44   40  ---    41
 R18  | 1455   20   12   21   21   19   24    9 |    31   46   51   52   40   30    39
 R19  |  983   31   86   31   77   39   38   21 |    68   59   75   75   66   59    62
 R20  | 2634   23  101   41   81   25   44   23 |    73   75   87   79   69   64    68
 R21  |  861   11   31   13   14   10   12    6 |    54   40   55   59   52   45    50
 R22  | 1147   11   13   12    9   10   17    5 |    22   24   30   31   22   24    23
 R24  |  718   11   28   13   14   15   21    7 |    52   37   51   56   46   38    46
XR26  |12673   30  ---  ---   39   52  ---   29 |    41  ---  ---   49   63  ---    50
------+-----------------------------------------+-------------------------------------
 RMS  | 1513   17   46   20  143   18   23      |T   69   67   77   77   68   62    65
 WRMS | 1513   16   25   15   30   15   23      |NE  69   67   77   77   68   62    65
 MEDI | 1164   13   19   15   18   16   20      |MD  70   73   75   65   69   60    67



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