[IGSREPORT-15118] Wk 1425 IGLOS Final Orbits

Gerd Gendt3 igsacc at gfz-potsdam.de
Fri May 25 06:53:35 PDT 2007


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IGS Electronic Report   25 May 06:53:46 PDT 2007      Message Number 15118
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Author:   AC Coordinator / GFZ Potsdam                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1425   (Apr 29, 2007 - May 05, 2007) 
                                                                               
Contact: Gerd Gendt     (gendt at gfz-potsdam.de)                   
         Thomas Nischan ( nisn at gfz-potsdam.de)                             
                                                                               
                                                                               
COMBINATION STRATEGY:                                                            
---------------------                                                            
                                                                               
Ephemeris are combined as weighted averages computed over all centres.          
Each centre and satellite is given a position weight computed from the centers  
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 2.1425.
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:                   
                                                                               
 igl1425[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1425 in the SP3 format.
 igl14257.sum      Combination Report for GPS Week 1425.


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

 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.

 3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151] 
    BKG, ESA, and CODE will start to refer their GLONASS orbit products 
    to the following satellite antenna offset (SAO) values:
    
      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.
    

 4. The satellite clock values in the combined orbit files are taken from the
    broadcast files. The following gps/glonass time offsets derived from the
    bkg summary files were added to the broadcast clocks.
    
               Day | applied clock offset
               ----+---------------------
                0  |    889.1 ns
                1  |    892.0 ns
                2  |    914.5 ns
                3  |    939.9 ns
                4  |    900.8 ns
                5  |    899.4 ns
                6  |    902.0 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  |  ESX   | ALL
                1  |  ESX   | ALL
                3  |  COD   | R15
                4  |  COD   | R15
                4  |  ESX   | R23
                5  |  COD   | R15
                5  |  ESX   | R24
                5  |  IAC   | R07
                6  |  COD   | R15 R24
                6  |  ESX   | R07 R23
                6  |  IAC   | R07

    
         
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 1.1425, 1a.1425).
        
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 2.1425.0-6)                                                                                
    
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 3.1425.0-6). 
        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 1425 summary.                      (Apr 29, 2007 - May 05, 2007)

Table 1.1425.a     GPS week : 1425   MJD: 54219.0-54225.0

         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]
--------+----------------------------------------------------+------------------------------
bkg   56|    0     0     2   104   -28    16  -.08   35   29 |       0     726   5666   6136
        |    2     1     1    36    23   173   .08           |       0    1457
cod  169|   -2     0     4   108   -82    35  -.10   44   36 |     ---     ---    ---    ---
        |    5     4     2    14    56   116   .05           |     ---     ---
esx   44|    7     0   -12    72    99  -210  -.32  175   76 | -324067    -987  16432  28192
        |   14     3    15   119   121   519   .23           |  664771   28659
iac  n/a|    0     1    -3  -231    81   -65   .22   65   65 |  918108   -4258  14487  26802
        |    0     2     4    20    48   119   .07           |   29466   24967


Table 1.1425.b     GPS week : 1425   MJD: 54219.0-54225.0   

         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  |   19   19   38   44   16   15   24 |
 R03  |   25   19   20   24   25   20   21 |
 R04  |   16   15   14   17   28   20   15 |
 R06  |   27   26   21   32   28   24   28 |
 R07  |   26   16   47   16   17  111  --- |
 R08  |   17   23   19   48   21   20   17 |
 R10  |   22   19   16   16   17   26   16 |
 R14  |   26   24   18   11   17   18   12 |
 R18  |   32   39   31   41   28   26   27 |
 R19  |   18   20   17   17   17   16   18 |
 R21  |   29   27   57   56   20   19   27 |
 R22  |   46   49   54   37   43   39   27 |
 R23  |   28   24   56   56   26   66   34 |


Table 1.1425.c     GPS week : 1425   MJD: 54219.0-54225.0   

         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 1425 0   | -201   311   284   -5582    2865 -351200  89.8  6552  6552 |  889143       0
brd 1425 1   |  210    42  -114   -7100   11870 -365500  97.2  8304  8304 |  891993       0
brd 1425 2   |  -40  -276  -460      87    4420 -355500  85.5  8785  8785 |  914460       0
brd 1425 3   |  309    53  -380    5182    -732 -361500  90.9  9635  9635 |  939861       0
brd 1425 4   | -571    10     9   -4303   -2126 -353100  75.6  7737  7737 |  900775       0
brd 1425 5   | -718   374    -3   -6213    8226 -358200  93.0  8465  8465 |  899386       0
brd 1425 6   |  563  -491   -59    6617   -4088 -357700  81.9  8872  8872 |  902011       0
-------------+------------------------------------------------------------+----------------
brd 1425 mean|  -64     3  -103   -1615    2919 -357528  87.7  8335  8335 |  905375       0
brd 1425 sdev|  468   305   251    5642    5750    4891   7.3   977   977 |   17237       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 2.1425.0  GPS week: 1425   Day: 0   MJD: 54219                            

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]
--------+----------------------------------------------------+------------------------------
bkg   56|   -4     0     0   122   -28   283  -.16   33   31 |       0    2882   6424   6879
cod  169|    0    -3     5   139   -23   -73  -.17   43   30 |     ---     ---    ---    ---
iac  n/a|    0     1    -7  -224     5  -240   .22   35   35 |  893249   -9219  12967  23805

Table 2.1425.1  GPS week: 1425   Day: 1   MJD: 54220                            

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]
--------+----------------------------------------------------+------------------------------
bkg   56|    0     0     5   110   -25  -138  -.18   28   24 |       0    1412   4007   4375
cod  169|   -1    -2     5   110   -54   206  -.02   41   31 |     ---     ---    ---    ---
iac  n/a|    0     5    -9  -264    92   -76   .24   43   43 |  878033   -8308  10468  26903

Table 2.1425.2  GPS week: 1425   Day: 2   MJD: 54221                            

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]
--------+----------------------------------------------------+------------------------------
bkg   56|   -1     0     2    81   -49   237  -.13   37   33 |       0   -1793   5557   5773
cod  169|    4     2     4   108   -79    78  -.07   31   28 |     ---     ---    ---    ---
esx   44|   -1    -2   -25  -120   137  -604  -.64  220   98 |  513128  -18515  15882  22069
iac  n/a|    1     0    -7  -216    84  -215   .30   37   37 |  892965    6904  14735  20766

Table 2.1425.3  GPS week: 1425   Day: 3   MJD: 54222                            

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]
--------+----------------------------------------------------+------------------------------
bkg   56|    0    -1     3   131   -32   -14  -.11   30   30 |       0      -5   6273   7055
cod  169|   -6    -2     3   102  -150   118  -.05   38   38 |     ---     ---    ---    ---
esx   44|   31     5   -30   148   245  -922  -.48  263  145 | -168165   42649  11757  31363
iac  n/a|    0     0     2  -243   152    14   .28   38   38 |  932400   41734  11741  30620

Table 2.1425.4  GPS week: 1425   Day: 4   MJD: 54223                            

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]
--------+----------------------------------------------------+------------------------------
bkg   56|    1     0     0    99   -63  -140  -.01   28   26 |       0     217   5491   6154
cod  169|   -7     3     0   108  -156   -77  -.13   45   45 |     ---     ---    ---    ---
esx   44|   12    -1     6   101   158   217  -.11  127   50 |   34700   12385  19033  30363
iac  n/a|   -1     0    -4  -240    74    66   .09   36   36 |  945278     801  17314  29710

Table 2.1425.5  GPS week: 1425   Day: 5   MJD: 54224                            

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]
--------+----------------------------------------------------+------------------------------
bkg   56|    3    -2     0    36    -8   -77   .01   54   24 |       0    1021   6030   6455
cod  169|   -7     6     7    91   -14    88  -.12   66   35 |     ---     ---    ---    ---
esx   44|    2     2    -8   183   -66   170  -.19  124   56 | -999999  -13111  19595  25472
iac  n/a|    0     1    -2  -199   119   -26   .17  236  236 |  953121  -33905  18829  26686

Table 2.1425.6  GPS week: 1425   Day: 6   MJD: 54225                            

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]
--------+----------------------------------------------------+------------------------------
bkg   56|    0     3     3   149     4   -35   .01   36   34 |       0    1353   5885   6264
cod  169|    2    -2     4   100   -98   -88  -.12   46   44 |     ---     ---    ---    ---
esx   44|   -5    -1    -4    49    25    85  -.18  143   29 | -999999  -28343  15893  31695
iac  n/a|    1    -2     0  -228    41    19   .26   31   31 |  931712  -27814  15361  29127

       
       
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 3.1425.0  GPS week: 1425   Day: 0   MJD: 54219                            

        Weighted Average         Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  iac  IGL |   bkg  cod  iac   IGL
------+--------------------------+----------------------
 R01  | 4873   22   26   30   18 |    34   52   60    45
 R03  | 7236   28   47   27   24 |    35   56   47    44
 R04  | 4568   19   22   26   16 |    33   33   37    30
 R06  | 1503   32   47   33   26 |    38   73   52    43
 R07  | 5847   30   50   29   26 |    51   79  158    47
 R08  | 7869   27   28   15   17 |    41   55   49    43
 R10  | 4224   21   32   37   21 |    26   27   35    24
 R14  | 2859   27   38   44   26 |    46   48   23    34
 R18  | 4873   46   48   40   31 |   322  332  333   327
 R19  |16386   22   29   25   18 |    59   51   55    51
 R21  | 4161   48   45   26   28 |    24   41   40    24
 R22  | 4210   54   77   62   45 |    51  111  113    73
 R23  | 3056   35   42   40   27 |    58   68   68    52
------+--------------------------+----------------------
 RMS  | 6551   33   43   35      |T   62   78   82    64
 WRMS | 6551   31   30   35      |NE  62   78   82    64
 MEDI | 4568   28   42   30      |MD  41   55   52    44

Table 3.1425.1  GPS week: 1425   Day: 1   MJD: 54220                            

        Weighted Average         Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  iac  IGL |   bkg  cod  iac   IGL
------+--------------------------+----------------------
 R01  | 6360   19   35   25   18 |    46   49   52    45
 R03  |11965   27   21   31   19 |    36   59   60    45
 R04  | 8404   13   20   28   14 |    29   25   35    20
 R06  | 8026   19   42   47   25 |    48   59   32    33
 R07  |14686   17   11   34   15 |    55   38  136    39
 R08  | 2880   25   25   47   23 |    48   62   41    45
 R10  | 6059   19   19   40   18 |    30   23   22    19
 R14  | 3686   23   47   28   23 |    30   59   20    31
 R18  | 4762   55   56   49   38 |   234  265  258   248
 R19  |15111   13   35   33   19 |    65   66   49    52
 R21  | 2984   37   33   43   27 |    31   53   28    25
 R22  | 3862   39   90   77   48 |    73   50   87    56
 R23  | 5349   23   33   45   23 |    65   46   46    49
------+--------------------------+----------------------
 RMS  | 8304   28   41   43      |T   60   65   66    54
 WRMS | 8304   24   31   43      |NE  60   65   66    54
 MEDI | 6059   23   33   40      |MD  48   53   46    45

Table 3.1425.2  GPS week: 1425   Day: 2   MJD: 54221                            

        Weighted Average              Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  IGL |   bkg  cod  esx  iac   IGL
------+-------------------------------+---------------------------
 R01  | 4589   25   16  268   27   38 |    59   46  366   50    56
 R03  |12885   27   22   98   27   19 |    33   55  221   43    39
 R04  |12468   20   19   49   28   14 |    43   31  207   33    27
 R06  | 6541   28   29   96   27   20 |    28   45  190   26    23
 R07  |10187   22   40  319   29   46 |    75   48  638  115    65
 R08  | 3815   30   18  100   20   18 |    79   45  322   62    58
XR10  | 8900   17   21  ---   27   16 |    32   25  ---   27    22
XR14  | 3485   20   27  ---   28   18 |    30   56  ---   24    31
 R18  | 5758   74   34   52   51   31 |   260  266  331  272   268
 R19  |11349   20   30   50   32   17 |    43   54  190   28    33
 R21  | 2708   56   41  389   20   57 |    30   57  482   37    35
XR22  | 2515   49   85  ---   82   53 |    64   69  ---   95    41
 R23  | 9937   34   42  350   74   55 |    45   67  227   94    56
------+-------------------------------+---------------------------
 RMS  | 8784   37   31  220   37      |T   63   66  317   69    58
 WRMS | 8784   33   28   98   37      |NE  63   66  317   69    58
 MEDI | 6541   27   29   98   28      |MD  43   54  227   43    39

Table 3.1425.3  GPS week: 1425   Day: 3   MJD: 54222                            

        Weighted Average              Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  IGL |   bkg  cod  esx  iac   IGL
------+-------------------------------+---------------------------
 R01  | 5934   35   19  334   16   43 |    30   50  313   32    33
 R03  |20318   26   31  132   32   23 |    42   59  139   57    51
 R04  |13053   20   22   95   18   16 |    42   36  154   31    31
 R06  | 8366   31   72   89   45   31 |    30   82  138   29    23
 R07  |11627   23   21   84   22   16 |    68   45  452  159    56
 R08  | 2471   27   46  356   27   48 |    59   45  383   49    58
XR10  | 4965   14   23  ---   30   16 |    25   26  ---   29    20
XR14  | 5198   15   15  ---   13   10 |    28   41  ---   29    23
 R18  | 6091   36   38  274   50   41 |   224  232  210  222   222
 R19  | 4281   27   20   86   19   16 |    38   55  280   53    40
 R21  | 4764   42   34  423   29   56 |    33   65  308   46    43
XR22  | 5432   53   27  ---   69   37 |    56   59  ---   89    49
 R23  | 4528   25   44  387   74   55 |    64   55  285   90    51
------+-------------------------------+---------------------------
 RMS  | 9635   30   38  263   38      |T   56   65  266   70    53
 WRMS | 9635   30   38  145   38      |NE  56   65  266   70    53
 MEDI | 5432   27   27  132   29      |MD  42   55  280   49    43

Table 3.1425.4  GPS week: 1425   Day: 4   MJD: 54223                            

        Weighted Average              Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  IGL |   bkg  cod  esx  iac   IGL
------+-------------------------------+---------------------------
 R01  | 8911   25   18   43   17   15 |    40   43  130   29    32
 R03  | 9309   11   55   47   54   24 |    44   41   65   41    38
 R04  | 9581   22   68   82   15   28 |    39   48   90   38    42
 R06  | 8613   27   68   38   58   28 |    33   48   81   35    28
 R07  |10178   19   21   52   21   16 |   102   40  735  272    51
 R08  | 2589   32   37   50   29   21 |    58   53  103   42    46
XR10  | 4494   20   25  ---   28   17 |    28   35  ---   31    24
XR14  | 4617   23   27  ---   20   16 |    42   38  ---   36    36
 R18  | 6312   46   40   57   49   27 |   253  269  141  256   253
 R19  | 2588   31   29   30   25   17 |    31   45  175   43    30
 R21  | 9348   22   38   49   33   20 |    40   62  194   54    50
XR22  | 6907   59   48  ---   71   43 |   133  103  ---   98   103
 R23  | 4726   31   51  371   29   25 |    48   52  199   50    45
------+-------------------------------+---------------------------
 RMS  | 7737   28   45  127   36      |T   68   67  191   78    59
 WRMS | 7737   26   45   50   36      |NE  68   67  191   78    59
 MEDI | 6907   25   38   49   29      |MD  42   48  130   42    42

Table 3.1425.5  GPS week: 1425   Day: 5   MJD: 54224                            

        Weighted Average              Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  IGL |   bkg  cod  esx  iac   IGL
------+-------------------------------+---------------------------
 R01  |13000   19   36   33   19   15 |    36   54  202   32    33
 R03  | 9727   16   35   48   42   19 |    35   36  104   45    34
 R04  | 6732   22   39   50   36   20 |    43   35   79   28    32
 R06  | 6692   30   36   85   37   24 |    45   39  154   31    32
 R07  | 8905  149  164  162  741  110 |   182   46 9999  545   100
 R08  | 1947   11   37   77   26   19 |    61   45  118   47    50
XR10  | 4808   25   33  ---   48   25 |    36   31  ---   40    28
XR14  |10761   27   25  ---   22   18 |    45   35  ---   24    30
 R18  | 6192   42   45   35   50   26 |   264  250  169  253   253
 R19  | 1455   23   28   31   30   15 |    51   50  167   34    42
 R21  | 7427   16   28   80   19   18 |    43   47  249   45    39
XR22  | 5039   64   40  ---   54   39 |    62   92  ---   78    65
 R23  |13567   48   85  317   45   66 |    67   82  146   47    48
------+-------------------------------+---------------------------
 RMS  | 8465   54   66  124  236      |T   74   64  154   96    60
 WRMS | 8465   24   35   56  236      |NE  74   64  154   96    60
 MEDI | 6732   25   36   50   37      |MD  45   46  154   45    39

Table 3.1425.6  GPS week: 1425   Day: 6   MJD: 54225                            

        Weighted Average              Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  IGL |   bkg  cod  esx  iac   IGL
------+-------------------------------+---------------------------
 R01  |15665   47   32   58   21   23 |    37   57  151   31    36
 R03  |10270   24   39   39   41   21 |    35   33  123   43    32
 R04  | 3529   13   37   16   32   15 |    34   39   96   33    30
 R06  | 9435   29   33   82   35   27 |    35   41  165   23    35
 R08  | 3263   39   31   19   21   16 |    57   48  144   35    40
XR10  | 5373   21   28  ---   18   15 |    38   25  ---   32    27
XR14  | 9866   17   14  ---   19   12 |    31   30  ---   28    27
 R18  | 5831   45   72   33   31   27 |   313  318  202  316   313
 R19  | 3522   19   51   14   30   17 |    46   61  176   55    45
 R21  | 2840   39   44   67   36   27 |    38   65  239   46    42
XR22  | 3714   41   22  ---   42   26 |    84   99  ---  125    98
 R23  |13816   53   61  407   29   34 |    73   88  180   93    77
------+-------------------------------+---------------------------
 RMS  | 8871   36   46  143   31      |T   68   75  164  133    66
 WRMS | 8871   34   44   29   31      |NE  68   75  164  133    66
 MEDI | 5373   29   33   39   30      |MD  38   48  165   43    36



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