[IGSREPORT-18548] Wk 1580 IGLOS Final Orbits

Jim Ray IGS.ACC at noaa.gov
Thu May 6 05:31:29 PDT 2010


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IGS Electronic Report   06 May 05:31:48 PDT 2010      Message Number 18548
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Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1580   (Apr 18, 2010 - Apr 24, 2010) 
                                                                               
Contact: J. Ray       (jim.ray at noaa.gov),                  
         J. Griffiths (jake.griffiths at noaa.gov)                            
                                                                               
                                                                               
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 2.1580.
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:                   
                                                                               
 igl1580[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1580 in the SP3 format.
 igl15807.sum      Combination Report for GPS Week 1580.


    
    
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  |    400.8 ns
                1  |    379.5 ns
                2  |    461.7 ns
                3  |    463.2 ns
                4  |    465.4 ns
                5  |    405.0 ns
                6  |    404.0 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
               ----+--------+---------------
                3  |  IAC   | 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 1.1580, 1a.1580).
        
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 2.1580.0-6)                                                                                
    
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 3.1580.0-6). 
        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 1580 summary.                      (Apr 18, 2010 - Apr 24, 2010)

Table 1.1580.a     GPS week : 1580   MJD: 55304.0-55310.0

         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  129|    1     0     4     4     3   -15  -.16   21   20 |       0    -105   1722   1786
        |    1     0     3    18    20   122   .03           |       0     124
cod  243|   -2     0    10    43   -26    12  -.10   16   14 |     ---     ---    ---    ---
        |    1     1     2    24    29    42   .02           |     ---     ---
esx  142|    0     0     5   -52    43    25   .48   25   23 |   95716    -765   3993   8665
        |    1     2     2    28    19    64   .07           |   39229    3424
gfz  195|    0    -1    10   -78   -32    75  -.11   27   27 |  272989   -1568   4015   8853
        |    2     1     3    39    40    55   .07           |   36277    1727
iac  n/a|    0     1   -33   -26     0   -11  -.13   30   30 |    7296     -97 218247 292594
        |    1     0     9    24    27    99   .07           |  688562    1978
mcc  n/a|    2     6    67  -131   -72   217  -.01  157  157 |     ---     ---    ---    ---
        |    8    11    17   194   156   568   .51           |     ---     ---


Table 1.1580.b     GPS week : 1580   MJD: 55304.0-55310.0   

         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    7    9    9    9   13   12 |
 R02  |    9   11    9   12   12   10    9 |
 R03  |   10   10   11   10   16   11   10 |
 R04  |    8    9    8    9   10   11   10 |
 R05  |   11   10   11    8    9    9   11 |
 R07  |    8    9   14   13   13    9   12 |
 R08  |    8   11   11    8    9    9    9 |
 R10  |   12   18   15   14   22   26   18 |
 R11  |   19  140    0   46   26   40   23 |
 R13  |   14   12   13   15   21   21   24 |
 R14  |   16   14   16   20   15   17   18 |
 R15  |   15   16   17   16   18   13   14 |
 R17  |   10   11   14   15   13   15   13 |
 R18  |   10    9   10   13   13   10    7 |
 R19  |   11   11   10   12   13   10   12 |
 R20  |   11   10   13   13   13   15   12 |
 R21  |   13   11   12   15   17   18   17 |
 R22  |   10   10   13   11   14   14   10 |
 R23  |   13   11   12   10   14   16   15 |
 R24  |   10   11    9    9   10   11   12 |


Table 1.1580.c     GPS week : 1580   MJD: 55304.0-55310.0   

         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 1580 0   |   -8   -20   272     -21    -969  -17100  86.0  1680  1680 |  400772       0
brd 1580 1   |  -25   -13   427    -302   -1411  -12470  86.1  1688  1688 |  379483       0
brd 1580 2   |   -5   -87   387     233   -1168   -6995  89.4  1889  1889 |  461714       0
brd 1580 3   |  117    31   362   -1146     243   -9524  90.9  2096  2096 |  463193       0
brd 1580 4   |   51   -92   313     905    1477  -12570  88.2  1920  1920 |  465427       0
brd 1580 5   |   19   -24   270    1278    -306   -9060  87.2  2051  2051 |  405013       0
brd 1580 6   |    0    81   251   -3282    1979  -12330  85.7  2420  2420 |  403971       0
-------------+------------------------------------------------------------+----------------
brd 1580 mean|   21   -17   326    -333     -22  -11435  87.6  1963  1963 |  425653       0
brd 1580 sdev|   48    61    66    1522    1325    3272   2.0   257   257 |   36374       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 2.1580.0  GPS week: 1580   Day: 0   MJD: 55304                            

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  129|    1     0     4    25    29   198  -.19   21   19 |       0      45   1695   1755
cod  243|   -2     2     9    44   -63   -53  -.10   15   14 |     ---     ---    ---    ---
esx  142|    0    -5     7   -69    38   -44   .52   23   22 |   68490    -193   4394   9978
gfz  195|    1    -2    14   -32    14     3  -.23   27   27 |  250615     473   4409  10507
iac  n/a|    2     1   -25   -22    26   -91  -.14   22   22 |  401905    2147   4397  11110
mcc  n/a|  -10    25    84  -439  -364  1294   .28  267  267 |     ---     ---    ---    ---

Table 2.1580.1  GPS week: 1580   Day: 1   MJD: 55305                            

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  129|    2     0     1     8    -3   -96  -.14   17   17 |       0    -165   1811   1865
cod  243|   -2     0    10    55     0    40  -.11   13   11 |     ---     ---    ---    ---
esx  142|   -1     0     5   -48    16    73   .55   23   21 |   52431   -4149   3544   7964
gfz  195|    0     1    11   -76   -69   104  -.08   24   24 |  229478   -2390   3670   8474
iac  n/a|    0     0   -36   -65   -15    10  -.14   30   30 |  379577    -844   3542   8691
mcc  n/a|   -9     1    69  -275  -132  -432  -.21  149  149 |     ---     ---    ---    ---

Table 2.1580.2  GPS week: 1580   Day: 2   MJD: 55306                            

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  129|    0    -1     2    13   -27    28  -.13   18   17 |       0     -78   1744   1803
cod  243|    0     1     7    54     5    16  -.07   15   14 |     ---     ---    ---    ---
esx  142|    0     0     2   -77    57    25   .43   28   26 |  135543   -1457   5134   9301
gfz  195|    1    -3    11   -66   -86    65  -.04   27   27 |  309825    -371   5142   8944
iac  n/a|    0     2   -21   -34   -38   -81  -.03   28   28 |  461374    1081   5143   9100
mcc  n/a|    5     8    75   171  -117   138  1.02  118  118 |     ---     ---    ---    ---

Table 2.1580.3  GPS week: 1580   Day: 3   MJD: 55307                            

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  129|    0     0     1    20   -12    57  -.13   17   17 |       0     -95   1497   1579
cod  243|   -2     0     8     6    -7    -1  -.09   15   14 |     ---     ---    ---    ---
esx  142|    2     2     5   -53    49   -22   .58   28   26 |  138677    3138   3521   8052
gfz  195|    2    -1     7   -39   -29    45  -.03   29   29 |  309164   -1659   3535   8453
iac  n/a|    1     0   -27    13     4  -150  -.10   30   30 | -999999   -3564 950533 999999
mcc  n/a|    7    13    77   -83   -60   346  -.20  138  138 |     ---     ---    ---    ---

Table 2.1580.4  GPS week: 1580   Day: 4   MJD: 55308                            

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  129|    2     0     8   -18    25  -156  -.16   21   21 |       0       5   1663   1714
cod  243|   -1     0     9    65   -54    63  -.11   19   16 |     ---     ---    ---    ---
esx  142|    1     0     4   -49    69    92   .44   26   23 |  136986     795   3511   7774
gfz  195|   -2    -3    10  -119   -17   173  -.17   28   28 |  313878   -2822   3500   8064
iac  n/a|    0     0   -38   -39    12    23  -.25   35   35 | -999999    -790 555586 999999
mcc  n/a|    6    10    74  -165    61   332  -.25  175  175 |     ---     ---    ---    ---

Table 2.1580.5  GPS week: 1580   Day: 5   MJD: 55309                            

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  129|    0     0     5   -23    13   -20  -.21   25   25 |       0    -337   1966   2044
cod  243|   -4    -1    14    11   -56    50  -.14   19   17 |     ---     ---    ---    ---
esx  142|    2     1     6     7    19   -49   .45   23   20 |   73961   -6133   4301   9369
gfz  195|    2    -1     3  -141    18    97  -.08   24   24 |  251489   -4282   4302   9356
iac  n/a|    0     2   -42   -24    33    99  -.10   32   32 |  405307    -562   4966  10341
mcc  n/a|    9   -12    51  -118   108   189  -.52  131  131 |     ---     ---    ---    ---

Table 2.1580.6  GPS week: 1580   Day: 6   MJD: 55310                            

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  129|    1    -1     8     3     0  -115  -.18   27   25 |       0    -111   1684   1746
cod  243|   -1     0    11    67    -7   -26  -.10   17   14 |     ---     ---    ---    ---
esx  142|    0     0    10   -73    51    99   .38   23   21 |   63929    2642   3548   8217
gfz  195|   -1     0    12   -73   -55    35  -.13   28   28 |  246474      70   3551   8179
iac  n/a|    2     0   -45   -16   -26   110  -.12   32   32 |  402912    1851   3567   8921
mcc  n/a|    9     2    35    -8    -2  -349  -.19  123  123 |     ---     ---    ---    ---

       
       
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 3.1580.0  GPS week: 1580   Day: 0   MJD: 55304                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1354   11   17   25   25   19  ---   10 |    26   31   28   32   27  ---    25
 R02  | 1885   14   10   19   19   17  ---    8 |    24   26   35   35   25  ---    24
 R03  | 2579   21   15   12   29   16  ---    9 |    20   27   27   28   35  ---    20
 R04  | 2010   11    8   18   26   18  ---    8 |    25   27   37   27   35  ---    26
 R05  |  796   15   17   23   25   21  ---   11 |    41   37   28   38   44  ---    34
 R07  | 2031   14   11   17   26   14  ---    8 |    39   32   34   36   31  ---    32
 R08  | 1124   11   12   19   24   13  170    8 |    36   33   26   37   43   69    31
 R10E | 2301   20   11   21   22   27  ---   11 |    62   60   66   64   56  ---    59
 R11E |  958   45   21   28   50   35  ---   19 |  9999 9999  152  503 9999  ---  9999
 R13E |  830   30   19   23   34   19  ---   13 |    32   24   39   46   43  ---    29
 R14E | 1407   26   21   26   38   35  ---   15 |    34   30   52   31   45  ---    31
 R15E | 1559   30   17   33   34   23  402   14 |    31   22   20   29   28  327    17
 R17  | 1068   14   16   15   22   22  ---   10 |    36   48   43   37   35  ---    40
 R18  | 2929   18   10   19   20   23  ---   10 |    24   34   22   26   20  ---    22
 R19  | 1804   15   14   22   18   23  ---   10 |    25   29   32   31   28  ---    23
 R20  | 1727   12   18   19   32   22  ---   10 |    35   36   28   39   26  ---    27
 R21  | 2014   13   12   37   28   25  ---   13 |    32   35   42   37   40  ---    30
 R22  |  678   15   17   23   16   14  ---   10 |    51   55   45   51   43  ---    47
 R23  | 1052   29   13   24   17   18  150   12 |    17   24   38   28   29   50    20
 R24  | 1190   12   16   15   17   23  ---    9 |    51   53   56   63   49  ---    50
------+-----------------------------------------+-------------------------------------
 RMS  | 1679   21   15   23   27   22  267      |T   33   34   42   60   35  148    30
 WRMS | 1679   19   14   22   27   22  267      |NE  32   35   34   36   34   59    30
 MEDI | 1407   15   15   21   25   21  170      |MD  32   32   35   36   35   69    29

Table 3.1580.1  GPS week: 1580   Day: 1   MJD: 55305                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1274   10    6   14   11   18  ---    6 |    21   21   25   24   20  ---    19
 R02  | 1427    9    8   23   24   37  ---   10 |    29   21   36   27   31  ---    23
 R03  | 2787   17    9   21   24   23  ---    9 |    20   22   37   36   31  ---    20
 R04  | 3034   14   10   17   21   24  ---    8 |    19   24   29   16   27  ---    20
 R05  | 1701   18   12   14   19   25  ---    9 |    25   33   39   23   37  ---    29
 R07  | 1335   13   11   18   23   24  ---    9 |    37   29   30   37   28  ---    28
 R08  | 2216   15   10   23   23   29  135   10 |    29   30   33   43   23   36    25
 R10E | 1567   23   30   19   27   49  ---   17 |    50   48   42   48   54  ---    41
XR11E | 1846  ---   47  --- 1727  257  ---  139 |   --- 9999  ---  563 9999  ---  9999
 R13E |  487   23    8   23   37   34  ---   12 |    27   28   43   42   33  ---    26
 R14E |  796   20   17   24   30   41  ---   14 |    27   21   36   37   39  ---    20
 R15E | 1064   31   13   34   29   32  167   15 |    21   29   35   25   32  204    20
 R17  | 1349   19   16   17   25   28  ---   11 |    28   26   29   22   36  ---    23
 R18  | 1275    9    9   21   15   21  ---    8 |    12   22   31   19   22  ---    15
 R19  | 2019   13    8   32   29   21  ---   10 |    14   17   33   33   19  ---    11
 R20  | 2230   14   10   22   18   25  ---    9 |    24   19   29   21   29  ---    17
 R21  | 1881   12   15   18   21   30  ---   10 |    28   24   32   33   42  ---    26
 R22  | 1075   12   12   22   12   30  ---   10 |    37   41   39   31   30  ---    34
 R23  | 1209   19    9   19   18   34  144   11 |    16   19   25   18   35   61    14
 R24  |  870   11   12   33   30   17  ---   10 |    51   41   49   54   51  ---    43
------+-----------------------------------------+-------------------------------------
 RMS  | 1687   17   13   22   24   30  149      |T   27   27   34   57   32  100    23
 WRMS | 1687   17   11   21   24   30  149      |NE  26   25   33   29   30   48    23
 MEDI | 1349   14   10   21   23   28  144      |MD  27   24   33   31   31   61    23

Table 3.1580.2  GPS week: 1580   Day: 2   MJD: 55306                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  671   12    9   20   20   20  ---    8 |    28   28   27   30   25  ---    23
 R02  | 1359    8    8   16   18   28  ---    8 |    18   22   22   19   46  ---    20
 R03  | 3749   15   19   14   19   25  ---   10 |    15   24   29   18   33  ---    18
 R04  | 3109   14    8   17   23   19  ---    8 |    22   27   32   26   28  ---    24
 R05  | 2578   16   11   26   24   28  ---   11 |    20   28   32   31   41  ---    23
 R07  | 1052   11   13   31   43   40  ---   13 |    35   31   62   67   27  ---    33
 R08  | 1298   17   10   30   31   20  105   11 |    24   27   32   34   25   21    23
 R10E | 1324   25   14   36   24   31  ---   14 |    53   37   60   43   51  ---    43
XR11E |31303  ---    5  ---  ---  ---  ---    0 |   --- 9999  ---  ---  ---  ---  9999
 R13E | 1046   19   14   32   42   27  ---   12 |    25   15   40   40   25  ---    17
 R14E |  687   14   18   26   27   54  ---   16 |    20   21   42   37   39  ---    19
 R15E | 2139   35   26   31   32   25  127   17 |    21   38   32   27   27  114    22
 R17  | 2057   25   16   31   41   29  ---   14 |    22   32   32   38   38  ---    27
 R18  | 1503   11   14   19   19   23  ---    9 |    17   31   33   30   42  ---    25
 R19  | 1856   13   14   28   27   19  ---   10 |    17   20   36   22   30  ---    18
 R20  | 2709   12   14   47   26   14  ---   13 |    27   24   52   35   15  ---    19
 R21  | 1340   16   15   29   22   29  ---   12 |    23   29   35   41   42  ---    25
 R22  | 1061   17   19   21   22   33  ---   12 |    54   55   45   49   42  ---    47
 R23  | 1226   21   15   25   17   26  121   12 |    17   20   31   20   26   35    14
 R24  | 1638   13    8   27   17   18  ---    9 |    23   30   43   35   25  ---    25
------+-----------------------------------------+-------------------------------------
 RMS  | 1888   18   15   28   27   28  118      |T   25   28   37   33   33   56    24
 WRMS | 1888   17   14   26   27   28  118      |NE  24   28   36   33   32   28    24
 MEDI | 1359   15   14   27   24   26  121      |MD  22   28   33   34   30   35    23

Table 3.1580.3  GPS week: 1580   Day: 3   MJD: 55307                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  848   12   11   17   22   25  ---    9 |    32   32   40   37   32  ---    31
 R02  | 1032   21   11   20   25   31  ---   11 |    34   28   28   29   38  ---    25
 R03  | 4009    9   10   32   31   21  ---   10 |    20   20   31   35   36  ---    19
 R04  | 1449   12   13   16   22   22  ---    8 |    22   28   19   23   37  ---    23
 R05  | 2831    7   14   18   30   19  ---    8 |    24   25   21   36   23  ---    20
 R07  | 2787   11   18   28   23   35  ---   12 |    41   39   47   38   44  ---    37
 R08  | 2314   12   10   13   21   19   89    7 |    31   33   39   41   27   26    30
 R10E | 1425   22   15   28   47   36  ---   14 |    35   25   23   42   46  ---    21
XR11E | 9570   45   45  ---  ---  281  ---   45 |  9999 9999  ---  --- 9999  ---  9999
 R13E | 2719   18   23   29   35   37  ---   15 |    24   23   36   33   32  ---    18
 R14E | 1009   21   20   44   35   56  ---   19 |    28   28   54   41   33  ---    23
 R15E | 2620   23   14   48   39   30  128   16 |    23   24   39   30   25  108    17
 R17  | 1955   23   19   30   30   35  ---   14 |    34   61   69   41   30  ---    46
 R18  | 2523    8   23   38   25   21  ---   13 |    13   28   43   29   15  ---    14
 R19  | 1540   19    7   16   24   36  ---   11 |    14   20   30   34   37  ---    19
 R20  | 1593   16   17   25   24   32  ---   12 |    20   31   17   27   49  ---    22
 R21  |  928   23   19   39   29   26  ---   15 |    34   33   32   32   37  ---    26
 R22  | 1297   16   13   29   23   23  ---   11 |    43   48   51   44   65  ---    45
 R23  | 1143   20   13   14   24   17  180    9 |    17   19   28   33   31   59    16
 R24  | 2474   13   12   16   17   23  ---    9 |    33   38   39   40   38  ---    34
------+-----------------------------------------+-------------------------------------
 RMS  | 2096   17   15   28   29   30  138      |T   27   30   36   35   35   64    25
 WRMS | 2096   17   14   26   29   30  138      |NE  27   32   35   34   35   42    27
 MEDI | 1593   16   14   28   25   26  128      |MD  28   28   36   35   36   59    23

Table 3.1580.4  GPS week: 1580   Day: 4   MJD: 55308                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  749   11   14   18   18   19  ---    9 |    29   42   45   35   36  ---    35
 R02  | 1032   12   16   18   19   35  ---   11 |    28   39   35   44   36  ---    31
 R03  | 4141   28   12   32   27   36  ---   15 |    28   20   33   30   33  ---    17
 R04  | 1245   20   12   17   24   22  ---   10 |    25   27   31   28   27  ---    23
 R05  | 1717   14   11   18   16   17  ---    8 |    20   20   31   21   23  ---    19
 R07  | 4024   14   17   21   51   37  ---   12 |    24   24   35   37   46  ---    24
 R08  | 1343    9   10   19   32   24   95    9 |    25   31   40   41   26   45    27
 R10E | 1150   41   24   39   21   48  ---   21 |    35   41   54   43   54  ---    37
XR11E |14263   32   22  ---  ---   57  ---   25 |   519 9999  ---  ---  514  ---  9999
 R13E | 3090   39   27   41   43   42  ---   21 |    25   23   48   43   31  ---    19
 R14E |  922   17   12   20   26   51  ---   14 |    23   24   24   27   37  ---    19
 R15E | 2173   13   29   20   44   57  139   17 |    26   36   33   41   35   96    22
 R17  |  814   21   13   28   23   33  ---   13 |    37   51   71   40   25  ---    45
 R18  | 1344   17   19   20   15   36  ---   13 |    17   30   34   24   33  ---    19
 R19  | 1576   11   10   28   17   36  ---   12 |    22   15   26   29   41  ---    13
 R20  | 1222   14   23   21   21   33  ---   13 |    26   29   43   37   35  ---    24
 R21  |  722   20   30   33   26   35  ---   17 |    17   35   48   31   35  ---    22
 R22  | 1554   27   12   29   30   24  ---   13 |    46   44   40   38   41  ---    36
 R23  |  860   21   24   31   19   17  251   14 |    21   20   28   22   20  148    13
 R24  | 1472   18   14   13   29   26  ---   10 |    29   32   33   46   41  ---    29
------+-----------------------------------------+-------------------------------------
 RMS  | 1919   21   19   26   28   35  175      |T   51   30   38   34   58   96    24
 WRMS | 1919   21   16   23   28   35  175      |NE  26   30   38   33   33   96    25
 MEDI | 1343   17   14   21   24   35  139      |MD  25   30   35   37   35   96    23

Table 3.1580.5  GPS week: 1580   Day: 5   MJD: 55309                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1500   23   20   25   23   24  ---   13 |    21   31   37   34   27  ---    23
 R02  | 1553   13   18   17   26   20  ---   10 |    29   34   42   50   32  ---    32
 R03  | 4329   18   10   20   23   27  ---   11 |    28   22   35   32   19  ---    19
 R04  | 1147   13   11   18   14   33  ---   11 |    18   15   25   20   29  ---    16
 R05  | 1655   15   10   18   20   16  ---    8 |    16   14   24   25   20  ---    15
 R07  | 4321   10   15   19   21   20  ---    9 |    19   24   32   32   20  ---    20
 R08  |  721   18   10   14   28   21   60    9 |    23   21   24   33   21   31    16
 R10E | 2179   62   33   27   18   48  ---   25 |    27   35   25   28   40  ---    19
XR11E |12866   69   33  ---  ---   69  ---   40 |   338 9999  ---  ---  372  ---  9999
 R13E | 2956   48   24   33   37   38  ---   21 |    30   23   40   35   40  ---    22
 R14E | 1124   20   16   26   26   54  ---   17 |    28   32   40   40   38  ---    27
 R15E | 3158   19   19   13   31   35  137   12 |    18   37   23   27   32  101    21
 R17  |  892   26   20   10   23   42  ---   14 |    51   54   41   58   29  ---    42
 R18  | 1036   13   13   18   20   22  ---    9 |    20   29   30   25   18  ---    21
 R19  |  542   14   10   21   20   25  ---   10 |    24   25   41   31   21  ---    23
 R20  | 1082   18   15   37   33   30  ---   14 |    16   20   46   46   16  ---    14
 R21  | 1324   24   22   38   23   38  ---   17 |    28   43   45   37   46  ---    32
 R22  | 1292   23   18   27   18   32  ---   14 |    62   70   59   65   65  ---    59
 R23  |  726   24   31   21   27   31  172   15 |    19   29   31   29   33  147    18
 R24  | 1124   13   19   19   19   22  ---   10 |    26   30   24   35   29  ---    22
------+-----------------------------------------+-------------------------------------
 RMS  | 2051   25   19   23   24   32  131      |T   42   30   34   35   47   93    24
 WRMS | 2051   25   17   20   24   32  131      |NE  26   30   35   36   28   89    24
 MEDI | 1292   18   18   20   23   30  137      |MD  24   29   35   33   29  101    21

Table 3.1580.6  GPS week: 1580   Day: 6   MJD: 55310                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1954   21   15   25   18   19  ---   11 |    31   41   37   37   35  ---    33
 R02  | 1405   10   14   13   20   22  ---    8 |    35   47   38   43   38  ---    38
 R03  | 2720   14   15   16   15   23  ---    9 |    28   31   32   31   35  ---    28
 R04  | 2143   11   13   20   19   20  ---    9 |    22   27   34   29   40  ---    26
 R05  | 1555   25    9   16   22   27  ---   11 |    25   27   32   28   35  ---    27
 R07  | 2861   19   12   19   14   32  ---   11 |    31   24   42   30   38  ---    28
 R08  |  910   12   13   18   20   22   55    9 |    29   33   35   33   30   23    29
 R10E | 2165   24   23   21   41   54  ---   17 |    31   26   33   24   41  ---    23
 R11E | 3966   50   33   36   52   41  ---   23 |   315 9999  108  259  342  ---  9999
 R13E | 2062   61   24   30   47   49  ---   23 |    34   21   48   31   44  ---    25
 R14E | 1073   37   20   25   25   45  ---   17 |    51   29   28   29   40  ---    27
 R15E | 7002   20   18   19   27   43  139   14 |    38   36   22   29   37  101    27
 R17  | 2260   27   15   22   39   24  ---   12 |    58   63   47   43   39  ---    51
 R18  | 1470   14   11   11   15   15  ---    7 |    23   32   27   24   15  ---    24
 R19  |  652   21    7   26   23   26  ---   11 |    31   40   48   32   23  ---    34
 R20  | 1010   21   14   22   28   23  ---   11 |    12   25   27   24   23  ---    14
 R21  | 1310   25   18   39   14   38  ---   17 |    37   52   61   41   57  ---    45
 R22  |  941   20   11   15   15   19  ---    9 |    67   79   80   78   65  ---    72
 R23  |  799   31   17   26   29   30  153   14 |    29   32   41   39   55   63    32
 R24  | 1037   18   18   20   26   29  ---   12 |    41   36   40   37   46  ---    35
------+-----------------------------------------+-------------------------------------
 RMS  | 2419   27   17   23   28   32  123      |T   48   36   43   46   53   62    32
 WRMS | 2419   25   14   21   28   32  123      |NE  33   39   41   36   38   43    34
 MEDI | 1470   21   15   20   22   26  139      |MD  31   32   37   31   38   63    28



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