[IGSREPORT-30347] Wk 2354 IGLOS Final Orbits

acc acc at igs.org
Fri Mar 7 04:56:25 UTC 2025


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2354   (Feb 16, 2025 - Feb 22, 2025) 
                                                                               
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 2.2354.
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:
                                                                               
 igl2354[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2354 in the SP3 format.
 igl23547.sum      Combination Report for GPS Week 2354.


    
    
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.

Starting 02-Feb-2025 (GPS week 2352) the IGS Analysis Centers started using 
the IGS realization of the updated ITRF2020-u2023, called IGb20. The combined
GLONASS orbits from this date are therefore in IGb20 frame.

 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  |      0.5 ns
                1  |      1.3 ns
                2  |      1.5 ns
                3  |      0.3 ns
                4  |      4.9 ns
                5  |      6.3 ns
                6  |      0.5 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
               ----+--------+---------------
                0  |  GFZ   | R26
                1  |  GFZ   | R26
                2  |  GFZ   | R26
                3  |  GFZ   | R26
                4  |  GFZ   | R26
                5  |  GFZ   | R26
                6  |  GFZ   | R26

    
         
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 1.2354, 1a.2354).
        
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 2.2354.0-6)                                                                                
    
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 3.2354.0-6). 
        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 2354 summary.                      (Feb 16, 2025 - Feb 22, 2025)

Table 1.2354.a     GPS week : 2354   MJD: 60722.0-60728.0

         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    -1    -3     0    42   .13   16   14 |    4293   -1217   3605  11569
        |    0     1     0    17    11    26   .04           |    1388    1973
esa  n/a|   -2    -1    -2   -35    -4    61  -.11   28   24 |    5349   -1941   3597  11121
        |    1     1     1    10    13    54   .04           |    1256    3036
gfz  n/a|    0     0     2     7     8   -23   .03   19   15 |       0   -1333   3727  10251
        |    1     0     2    11    20     8   .03           |       0    2111
grg  n/a|    2     0     2    -3    -6     0   .29   19   16 |    2838   -1284   3638   8573
        |    0     1     1    14    15    50   .03           |    1925    2092
iac  n/a|   -1     0    -6   -19    -2   -38  -.22   18   17 |    3422    -816   3626   9839
        |    1     1     1    14    17    39   .05           |    2263    1279
jgx  n/a|    0     0     5    33    -9    -9  -.18   19   19 |    6815   -1224   3631   8978
        |    1     1     1    16     9    42   .03           |    1428    2116


Table 1.2354.b     GPS week : 2354   MJD: 60722.0-60728.0   

         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  |   11   12   14   15   13   13   11 |
 R02  |    6    5    7    7    9    8    5 |
 R03  |    8    7    6    7    7    7    8 |
 R04  |    7    7    7    7    7    7    6 |
 R05  |    8    7    8    7    7    8    7 |
 R07  |    8    8    7    7    8    7    6 |
 R08  |    7    8    7    8    9    9    7 |
 R09  |    7    7    7    6    6    6    8 |
 R11  |    8    7    9    6    8    9    6 |
 R12  |    7    6    8    7    8    6    8 |
 R14  |    7    6    6    8    6    5    6 |
 R15  |    8    7    7    8    9    8    8 |
 R16  |    7    9    9    6    8    9    7 |
 R17  |    8    8    6    6    7    7    7 |
 R18  |    7    6    8    7    7    6    6 |
 R19  |    8    7    8    8   10    9    9 |
 R20  |   19   18   19   16   24   21   21 |
 R21  |   10    8    9    9    7    8    7 |
 R22  |    6    7    8    8    7    7    7 |
 R24  |    8    9    7    9    9    8    8 |
 R26  |   38   39   44   59   51   46   50 |


Table 1.2354.c     GPS week : 2354   MJD: 60722.0-60728.0   

         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 2354 0   |    7    26   133      59    -237    7602  82.1  1587  1587 |     455       0
brd 2354 1   |  -35    38   104    -916    -252    9921  79.6  1689  1689 |    1299       0
brd 2354 2   |   15    57   103    -337    1607    7242  78.8  1596  1596 |    1506       0
brd 2354 3   |   75     4   107     917    1540    5030  80.6  1822  1822 |     309       0
brd 2354 4   |   28    77    92     682    2135    3800  80.9  1934  1934 |    4915       0
brd 2354 5   |  -72    34   107     263     954    4429  81.2  1825  1825 |    6339       0
brd 2354 6   |   60   -34    51     649    1293     969  79.3  1959  1959 |     465       0
-------------+------------------------------------------------------------+----------------
brd 2354 mean|   11    29    99     188    1005    5570  80.4  1773  1773 |    2184       0
brd 2354 sdev|   51    36    24     646     925    2936   1.2   151   151 |    2429       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 2.2354.0  GPS week: 2354   Day: 0   MJD: 60722                            

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   -26    19    50   .05   17   16 |    4638     582   4023  11345
esa  n/a|   -2    -1    -2   -52   -15   -17  -.08   32   27 |    4895     786   4012  10717
gfz  n/a|    1     0     1     5     0   -22   .05   18   14 |       0     319   4141  10429
grg  n/a|    2     0     1   -32   -25    57   .29   19   14 |     884     616   4061   9705
iac  n/a|    1     0    -6    -8     2   -36  -.15   17   16 |    2022    -554   4021  10834
jgx  n/a|   -2     0     5    63     3   -55  -.17   17   17 |    6079    1090   4009   9860

Table 2.2354.1  GPS week: 2354   Day: 1   MJD: 60723                            

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    -3    -3     1     7   .14   16   13 |    5908   -4193   4554  10482
esa  n/a|   -3    -2     0   -23    -5   121  -.12   26   24 |    6950   -4570   4528  10733
gfz  n/a|    3     0     5    26    26   -12  -.00   17   15 |       0   -4547   4657   9287
grg  n/a|    2     1     3    -4    22   -25   .31   19   15 |    3271   -4269   4619   8237
iac  n/a|    0     1    -7   -25   -28    -5  -.23   15   15 |    2541   -3394   4552  10025
jgx  n/a|    0    -3     5    25   -22   -26  -.19   20   20 |    8130   -4265   4626   8620

Table 2.2354.2  GPS week: 2354   Day: 2   MJD: 60724                            

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    -1     2     0    18   .15   15   13 |    3643     497   3090  10259
esa  n/a|   -3     0    -3   -37     0   103  -.16   26   22 |    3870     529   3090  10079
gfz  n/a|    0     0     2     3    -4   -33   .00   19   17 |       0     375   3281   8892
grg  n/a|    3     1     2    -5    -4   -62   .32   20   16 |    1065     579   3084   7201
iac  n/a|    0     3    -8    -3    27    32  -.26   19   18 |    1253      70   3105   9859
jgx  n/a|    1    -1     7    45   -20   -60  -.20   20   20 |    6103     481   3087   7623

Table 2.2354.3  GPS week: 2354   Day: 3   MJD: 60725                            

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    16     6    38   .16   16   12 |    2879   -2601   3021  11582
esa  n/a|    0     0    -3   -30   -10    81  -.15   26   23 |    5255   -4985   3008  10984
gfz  n/a|   -1     0     4     6    39   -35   .03   17   15 |       0   -2757   3149  10176
grg  n/a|    2     0     4    -5   -12    81   .22   19   18 |    1627   -3182   3025   8577
iac  n/a|    0     1    -6   -28   -10   -77  -.17   16   15 |    2145   -1511   3013   9253
jgx  n/a|    0    -1     6    24    -3   -18  -.17   21   21 |    5793   -2942   3019   8884

Table 2.2354.4  GPS week: 2354   Day: 4   MJD: 60726                            

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    -1     0     2    90   .16   19   16 |    4976    -782   3379  11116
esa  n/a|    0     0    -3   -39   -22    19  -.10   27   21 |    5464    -418   3394  10750
gfz  n/a|    0     0     1    10    -9   -27   .07   25   17 |       0    -354   3506   9379
grg  n/a|    1    -1     0     6   -12   -22   .29   18   14 |    5063    -525   3426   7034
iac  n/a|   -2    -1    -4   -17     4   -47  -.26   19   18 |    5489     358   3433   7881
jgx  n/a|    0     0     7    16   -12    47  -.24   19   19 |    7797    -635   3442   7578

Table 2.2354.5  GPS week: 2354   Day: 5   MJD: 60727                            

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     1    -1   -25   -11    47   .14   16   14 |    5704     739   3260  13008
esa  n/a|   -3    -3    -5   -24    19   105  -.05   29   24 |    6996     906   3246  11874
gfz  n/a|    0    -1     3    10    19   -15   .01   18   13 |       0     784   3366  11626
grg  n/a|    2     0     2     8   -18    -9   .30   20   18 |    5721     633   3299   9646
iac  n/a|   -3     1    -5   -12   -14   -77  -.22   18   17 |    7565    -242   3296  10304
jgx  n/a|    1     1     2    36   -11    14  -.14   21   21 |    8830     589   3290  10060

Table 2.2354.6  GPS week: 2354   Day: 6   MJD: 60728                            

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    -1    13   -15    47   .08   14   13 |    2303   -2765   3913  13193
esa  n/a|   -5    -3     0   -43     3    17  -.08   28   30 |    4015   -5837   3904  12710
gfz  n/a|    0    -1     0   -10   -16   -19   .07   19   15 |       0   -3153   3990  11974
grg  n/a|    1    -1     3     7     2   -16   .28   19   14 |    2240   -2842   3953   9615
iac  n/a|   -2     0    -5   -44     0   -59  -.27   19   17 |    2939    -444   3965  10721
jgx  n/a|    2     0     3    25     0    33  -.14   17   17 |    4973   -2890   3947  10221

       
       
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 3.2354.0  GPS week: 2354   Day: 0   MJD: 60722                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1053   34   41   12   15   21   20   10 |   111   57   84   91   86   84    86
XR02  | 1666   10    9   10   12   14  ---    5 |    76   67   72   70   64  ---    69
 R03  |  711   12   12   10   12   25   26    8 |    74   66   76   80   79   62    72
 R04  | 2243   11   28   19   16   12    8    7 |    89   75   94   91   85   81    86
 R05  | 2285   13   26   22   13   21    7    7 |    72   65   79   72   60   63    67
 R07  | 1457   12   35   14   14   16   18    7 |    83   75   77   84   75   63    75
 R08  | 1017   14   35   14   12   15    9    7 |    89  104   87   84   92   90    89
 R09  |  812   12   34   13    7   14    9    6 |    31   28   37   29   28   32    29
 R11  |  965   13   50    8   15   12   12    8 |    27   36   41   39   40   33    34
 R12  | 1091   20   13   16   16   19    8    7 |    66   54   57   50   60   53    55
 R14  |  775   13   27   11   14    9   19    7 |    62   62   63   55   55   45    55
 R15  |  589   19   25   15   13   15   20    8 |    84   76   89   77   75   67    77
 R16  | 1911   21   28   12    8   14   13    7 |    88   75   77   77   74   69    76
 R17E | 2116   11   21   10   20   24   11    7 |   119  118  119  112  126  110   117
 R18E |  973    9   20   15   15   13   15    6 |    21   24   18   30   24   18    20
 R19E | 1518   15   20   16   19   19   13    7 |   191  198  196  198  193  206   196
 R20E | 1862   33   72   45   40   29   44   19 |   108  113  128  106  106  106   107
 R21E | 1760   12   22   27   40   11   13   10 |   172  169  168  184  171  166   171
 R22E | 1884   13   22   11   15   12   10    6 |    36   35   36   38   40   33    35
 R24E | 2749   13   20   17   26   15   12    7 |    71   68   73   66   68   68    67
XR26  |76718   59   56 1000  ---   46  ---   37 |    33   98  750  ---   23  ---    53
------+-----------------------------------------+-------------------------------------
 RMS  | 1586   17   32   18   19   17   17      |T   81   79  115   81   77   76    77
 WRMS | 1586   16   27   14   14   16   17      |NE  70   67  120   69   64   61    65
 MEDI | 1518   13   26   14   15   15   13      |MD  76   68   77   77   74   67    72

Table 3.2354.1  GPS week: 2354   Day: 1   MJD: 60723                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1053   40   40   11   20   12   33   12 |    59   38   35   39   43   37    39
 R02  |  964    8   18    6   13   11    9    4 |    53   53   46   56   49   38    50
 R03  | 1531    7   17   14   20   13   16    6 |    48   48   49   61   52   46    50
 R04  | 1850   10   20   14   14   14   24    7 |    61   52   69   68   63   47    60
 R05  | 1498    9   36   13   15    8   12    7 |    50   51   56   58   44   47    50
 R07  | 1511   13   29   12   19   12   25    8 |    55   46   55   61   48   40    50
 R08  | 1393   12   30   11   23   12   19    8 |    72   95   72   58   73   72    71
 R09  |  618   14   29   13    9   16   12    7 |    21   29   23   22   22   26    20
 R11  | 1046    8   26   17    9   14   16    6 |    16   29   32   19   22   24    19
 R12  |  786   10   21    9   15   14   14    6 |    52   51   54   43   51   42    48
 R14  |  997    9   28   12   14    9   14    6 |    45   56   47   44   48   37    45
 R15  |  841   15   21   12   11   16   20    7 |    62   51   63   55   60   48    56
 R16  | 1457   15   28   19    9   15   27    8 |    65   55   69   61   60   51    59
 R17E | 2089   13   18   21   23   18   10    8 |   137  142  146  137  132  137   138
 R18E | 1180   12   19   13    8   12    9    5 |    20   21   21   24   20   21    18
 R19E | 3593   10   18   14   17   16   15    6 |   132  139  125  139  128  143   133
 R20E | 2707   26   49   48   35   35   48   18 |    94   91   91   82   86   87    83
 R21E | 2221   11   16   14   30   16   14    8 |   123  122  127  122  123  123   123
 R22E | 1011   18   20   12   14   13    8    6 |    25   28   22   30   30   28    25
 R24E | 2211   16   17   21   27   16   12    8 |    61   53   55   60   51   56    54
XR26  |90110   61   60 1019  ---   43  ---   38 |    35   72  461  ---   19  ---    50
------+-----------------------------------------+-------------------------------------
 RMS  | 1688   16   26   17   19   15   20      |T   61   62   81   61   58   57    59
 WRMS | 1688   13   24   15   15   15   20      |NE  49   51   80   49   46   42    47
 MEDI | 1457   12   21   13   15   14   14      |MD  55   52   55   58   51   46    50

Table 3.2354.2  GPS week: 2354   Day: 2   MJD: 60724                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  957   35   41   21   35   18   33   14 |    82   55   71   89   74   71    73
 R02  |  717    8   23   16   13   18   18    7 |    47   42   50   47   53   28    46
 R03  | 1032    8   14   19   13   13   12    6 |    63   59   82   68   61   72    67
 R04  | 1050   12   19   14   18   18   12    7 |    79   69   84   85   66   74    76
 R05  | 1512   15   20   14   17   10   25    7 |    67   62   55   72   62   45    59
 R07  |  687   10   21    8   18    7   20    6 |    63   47   59   70   57   49    58
 R08  | 1340   14   21   13   17   10   21    7 |    59   54   52   64   53   46    54
 R09  |  679   13   20   12   13   19   13    6 |    25   25   32   23   27   26    24
 R11  | 1198   18   29   23   11   19   11    8 |    13   41   39   21   19   27    21
 R12  |  853   13   20   13   24   17   16    7 |    48   49   46   31   45   46    41
 R14  |  645    9   14   19   10   12   16    6 |    54   57   50   62   56   58    54
 R15  | 1709   11   10    9   23   23   14    7 |    68   80   79   70   79   69    71
 R16  |  586   13   46   10   11   23   12    9 |    74   48   65   70   76   58    64
 R17E | 2687    8   14   11   16   18   17    6 |   111  110  116  111  100  106   108
 R18E |  932    8   26   18   15   18   14    7 |    22   28   21   28   26   21    19
 R19E | 4435   13   18   14   18   22   15    7 |   137  135  144  136  137  143   138
 R20E | 1659   30   51   54   37   40   46   19 |    59   69   95   76   62   45    60
 R21E |  652   13   15   17   24   27   16    8 |   121  116  123  126  131  117   122
 R22E | 1841   14   28   17   16   15   16    8 |    15   42   22   33   25   23    22
 R24E | 1460   12   15   16   18   15   19    7 |    64   69   70   65   56   60    62
XR26  |>>>>>   61   76 1077  ---   48  ---   43 |    25  100  632  ---   20  ---    50
------+-----------------------------------------+-------------------------------------
 RMS  | 1595   15   26   19   20   19   20      |T   61   64   94   67   61   59    61
 WRMS | 1595   13   22   17   16   18   20      |NE  54   56   99   59   53   51    54
 MEDI | 1050   13   20   16   17   18   16      |MD  63   57   65   68   57   49    59

Table 3.2354.3  GPS week: 2354   Day: 3   MJD: 60725                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1061   31   65   20   39   13   26   15 |    89   38   76   92   72   69    73
 R02  |  700    8   29    7   17   15   18    7 |    46   49   45   57   46   32    45
 R03  | 1416   10   26   14   20   12   16    7 |    56   45   52   61   52   44    51
 R04  |  764   12   19   15   19   11   16    6 |    67   48   60   63   57   65    59
 R05  | 1209   10   20   17   16   16   12    6 |    58   49   68   69   48   54    57
 R07  |  667   13   15   13   15   10   19    6 |    62   47   63   59   49   42    54
 R08  |  763    8   17   14   23   18   23    7 |    66   65   67   64   57   54    61
 R09  |  771   15   20   15    9   10   14    6 |    18   26   25   25   24   20    19
 R11  | 1416   10   24    9    8    9   13    5 |    10   29   19   16   19   15    14
 R12  | 1056   11   23   13   14   15   13    6 |    38   35   35   28   36   31    32
 R14  |  658    4   13   20    8   14   31    7 |    48   51   63   53   51   33    49
 R15  |  890   18   12   16    6   20   28    8 |    59   46   47   45   55   31    47
 R16  |  726   12   20   14    9   14   13    6 |    65   56   67   58   68   53    61
 R17E | 4798   12   14   12   14   14   11    6 |   141  143  150  135  140  142   141
 R18E |  747   11   20   14   18   13   17    7 |    22   26   28   28   20   19    21
 R19E | 4538   18   27   16   18   17   13    8 |    78   67   75   76   72   78    74
 R20E | 1771   30   35   41   27   32   49   16 |    56   65   77   64   53   55    55
 R21E |  934   20   18   13   30   17   12    8 |   130  126  122  136  118  130   126
 R22E | 2364   19   20   11   13   23   11    7 |    18   33   23   27   34   20    22
 R24E |  640   15   26   21   22   20   16    9 |    49   60   56   56   48   42    49
XR26  |>>>>>   44   80 1072  ---  ---  ---   59 |    35  110  687  ---  ---  ---    57
------+-----------------------------------------+-------------------------------------
 RMS  | 1821   16   26   17   19   16   21      |T   57   57   90   60   55   51    55
 WRMS | 1821   12   23   15   18   15   21      |NE  51   49   98   53   48   41    48
 MEDI |  934   12   20   14   16   14   16      |MD  56   49   63   58   51   42    54

Table 3.2354.4  GPS week: 2354   Day: 4   MJD: 60726                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1469   33   60   24   17   18   18   13 |    85   38   59   65   63   90    66
 R02  |  871   11   35   15   14   22   16    8 |    50   43   53   56   41   33    47
 R03  | 1481    7   19   11   16    8   20    6 |    54   47   52   53   46   43    49
 R04  |  488   14   16   18   22    9   11    7 |    69   56   76   50   60   57    60
 R05  | 1081   12   19   20   18   17    7    7 |    58   46   48   54   49   48    49
 R07  | 1133   17   14   18   11   26   20    8 |    63   48   44   46   69   48    52
 R08  |  704   12   18   17   18   18   25    8 |    58   60   69   56   63   52    58
 R09  | 1308   17   17   18   10    8   13    6 |    27   37   34   29   24   32    27
 R11  |  733   16   14   15   19   17   22    8 |    14   26   24   25   32   24    20
 R12  | 1604   14   30    9   11   16   18    7 |    49   43   45   36   49   49    43
 R14  | 1370   10   19   18    7   15   10    6 |    58   58   58   53   46   52    53
 R15  |  586   29   15    9    9   16   27    8 |    76   67   61   68   58   58    63
 R16  | 1204   17   24   15   12   21   19    8 |    76   70   73   61   63   54    64
 R17E | 2073   12   19   18   19   11   10    6 |    84   85   94   70   81   76    80
 R18E |  831   11   17   21   15   11   14    6 |    28   27   30   25   27   26    24
 R19E | 4541   21   19   24   26   17   17    9 |   166  163  163  161  177  174   167
 R20E | 1955   39   56   85   41   43   43   23 |    71   86  117   82   67   62    68
 R21E | 1190   16   29   14   13   14   11    7 |   152  142  153  150  150  152   150
 R22E | 5117   15   21   13   11   22    9    7 |    12   29   24   25   29   15    18
 R24E |  970   14   22   13   22   21   18    8 |    54   54   51   57   50   62    52
XR26  |>>>>>   41   62 1033  ---  ---  ---   50 |    24   74  578  ---  ---  ---    39
------+-----------------------------------------+-------------------------------------
 RMS  | 1933   19   27   25   18   19   19      |T   63   61   90   61   62   60    59
 WRMS | 1933   16   21   17   14   18   19      |NE  54   50   91   50   51   49    49
 MEDI | 1204   15   19   18   15   17   17      |MD  58   54   58   54   50   52    52

Table 3.2354.5  GPS week: 2354   Day: 5   MJD: 60727                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1805   19   65   16   27   21   23   13 |    82   48   89   85   92   65    78
 R02  |  969   16   31   13   14   14   14    7 |    51   40   49   43   38   25    42
 R03  | 1729   10   21   15   15   13   17    6 |    54   48   58   52   45   44    50
 R04  |  590    8   27   13   19   13   14    7 |    66   67   68   71   55   56    63
 R05  |  474    9   37   17   21   10   10    8 |    59   53   72   65   57   54    59
 R07  | 1231    9   19   15   11   20   14    6 |    51   54   58   58   66   52    55
 R08  |  650    9   26   14   19   28   21    9 |    46   47   34   35   59   30    39
 R09  | 1106   13   20   12   13   17    9    6 |    35   42   39   42   38   29    36
 R11  |  846   21   27   11   26   17   18    9 |    17   37   23   43   33   31    25
 R12  | 1551   12   18   13   15    9   12    6 |    46   52   51   38   44   34    43
 R14  | 1857    9   12   10   14   12   10    5 |    42   40   35   35   32   45    37
 R15  | 1418   24   15   15    7   10   22    7 |    64   60   66   66   61   56    61
 R16  | 1075   18   15   15   14   15   32    8 |    61   51   55   60   60   44    54
 R17E | 1180   13   18   14   17   16   15    7 |   127  135  124  125  125  122   125
 R18E |  740   10   22   11   12   10    9    5 |    22   28   18   23   20   20    19
 R19E | 3374   20   22   12   25   20   20    9 |   145  147  142  148  140  156   145
 R20E | 1952   30   55   52   45   41   60   21 |    63   78   75   71   59   57    59
 R21E | 1914   16   29   13   19   20   11    8 |   147  144  139  141  140  140   142
 R22E | 4895   15   24   13   17   13   13    7 |    17   27   27   30   27   22    21
 R24E | 1067   17   21   22   17   21   12    8 |    55   57   65   55   57   55    55
XR26  |>>>>>   32   66 1022  ---  ---  ---   46 |    24   67  497  ---  ---  ---    32
------+-----------------------------------------+-------------------------------------
 RMS  | 1824   16   29   18   20   18   21      |T   60   62   84   64   62   56    59
 WRMS | 1824   14   24   13   18   17   21      |NE  49   50   85   53   52   43    48
 MEDI | 1231   15   22   14   17   15   14      |MD  54   52   58   55   57   45    54

Table 3.2354.6  GPS week: 2354   Day: 6   MJD: 60728                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esa  gfz  grg  iac  jgx  IGL |   cod  esa  gfz  grg  iac  jgx   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1766   16   55   24   24   20   15   11 |   101   57  102  102  102   90    94
 R02  |  806    7   21   11   10   12    9    5 |    64   62   64   60   64   39    61
 R03  | 1969   16   18   14   24   17   19    8 |    74   66   67   80   64   58    67
 R04  |  625   11   23   11   14   11   11    6 |    86   81   89   83   75   76    81
 R05  | 1074    8   33    9   15   12   12    6 |    76   78   71   78   65   67    71
 R07  | 1153    9   16   14   16   13    7    5 |    73   70   67   78   63   67    69
 R08  |  670   13   20   16    8   16   17    7 |    66   65   59   61   66   51    60
 R09  | 1055   10   32   18   14   14   16    7 |    40   41   47   36   40   42    40
 R11  | 1358   13   24   10    9   17   11    6 |    26   38   32   35   35   31    30
 R12  | 1380   15   24   22   23   12   15    8 |    63   64   66   48   65   46    56
 R14  | 1764   12   16   10   15   16   10    6 |    64   65   59   52   53   53    56
 R15  | 2237   22   14   20    7   22   10    7 |    86   85   85   83   77   76    80
 R16  | 1092   15   17   15   10   17   13    6 |    83   79   87   83   84   73    80
 R17E |  808   14   13   14   14   21   15    7 |   123  119  120  121  118  124   121
 R18E |  583    9   21   15   12   12    9    5 |    24   36   26   27   28   20    24
 R19E | 1925   15   31   18   22   22   14    9 |   199  198  195  198  191  208   197
 R20E | 3221   27   59   50   41   43   55   20 |    76  104   88   78   74   70    74
 R21E | 3862   12   29   13   21   16   10    7 |   184  176  180  183  185  182   182
 R22E | 4574   13   22   20   15   19    9    7 |    32   43   39   39   37   35    34
 R24E |  836   12   20   20   26   17   13    8 |    67   60   69   76   64   69    66
XR26  |>>>>>   32   78 1021  ---  ---  ---   50 |    36  115  745  ---  ---  ---    58
------+-----------------------------------------+-------------------------------------
 RMS  | 1959   14   28   19   19   19   17      |T   78   81  112   80   77   73    76
 WRMS | 1959   13   30   15   14   17   17      |NE  67   69  117   67   65   59    64
 MEDI | 1358   13   22   15   15   16   12      |MD  73   66   69   78   65   67    67



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