[IGSREPORT-19082] Wk 1604 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Oct 21 06:15:51 PDT 2010


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1604   (Oct 03, 2010 - Oct 09, 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 2.1604.
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:                   
                                                                               
 igl1604[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1604 in the SP3 format.
 igl16047.sum      Combination Report for GPS Week 1604.


    
    
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  |    375.3 ns
                1  |    416.6 ns
                2  |    433.6 ns
                3  |    380.4 ns
                4  |    381.3 ns
                5  |    428.0 ns
                6  |    424.5 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
               ----+--------+---------------
                6  |  BKG   | R16

    
         
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 1.1604, 1a.1604).
        
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 2.1604.0-6)                                                                                
    
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 3.1604.0-6). 
        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 1604 summary.                      (Oct 03, 2010 - Oct 09, 2010)

Table 1.1604.a     GPS week : 1604   MJD: 55472.0-55478.0

         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  127|    0     0     0    -2     2     8  -.15   26   23 |       0      33   2114   2206
        |    1     1     3    34    32    86   .07           |       0     246
cod  232|   -1     0     3    33   -15    23  -.11   16   14 |     ---     ---    ---    ---
        |    1     1     1    21     8    31   .03           |     ---     ---
esx  136|    0    -1     3   -13     0    33   .45   25   22 |   70164    1207   3926   8952
        |    2     2     5    33    33    54   .05           |   29238    2974
gfz  194|    1     0    -1   -15    27    26  -.11   32   28 |  250029    -324   3940   8385
        |    2     1     4    44    53    24   .06           |   27081    3462
iac  n/a|    1     1    -8   -48    21   -85  -.15   26   26 |  388306   10484  19993  64303
        |    1     0     9    24    19    16   .06           |   43928   31423
mcc  n/a|    3     8    34   -26    29   195  -.61  151  151 |     ---     ---    ---    ---
        |   10    12    11    85   159  1226   .60           |     ---     ---


Table 1.1604.b     GPS week : 1604   MJD: 55472.0-55478.0   

         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  |   16   15   13   15   13   11   12 |
 R02  |   11   13   15   10   11   14   14 |
 R05  |    9   10   10   10   14   14   12 |
 R07  |   11    8    9    8    9    9   13 |
 R08  |   13   12   11   11   10    9   12 |
 R09  |   26   12   13   10   11   14   20 |
 R10  |   13    9   12   11   15   10   14 |
 R11  |   21   21   22   26   22   32   21 |
 R12  |  ---    0   27   29   37   53   29 |
 R13  |   11   13   13   16   19   31   19 |
 R14  |   20   16   14   14   21   19   13 |
 R15  |   11   16   12   13   22   15   18 |
 R16  |  ---    0   19   13   19   26   49 |
 R17  |   12   12   11    8    9    9   12 |
 R18  |    7   13   12   11   10   20    8 |
 R19  |    9    8    7    7    8    9   10 |
 R20  |    8   12   10   10   10    8   15 |
 R21  |    8   12   11   10   11   11   10 |
 R22  |   11   16   12    8   11   11   11 |
 R23  |   11    8   14   12   10   14   13 |
 R24  |   17   24   11    8    8   12   11 |


Table 1.1604.c     GPS week : 1604   MJD: 55472.0-55478.0   

         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 1604 0   | -113   -48   106     444   -2665  -20440  85.5  1681  1681 |  375301       0
brd 1604 1   |   22    30   174    -126   -1713  -23340  86.0  1749  1749 |  416619       0
brd 1604 2   |  -39    41   100    -186   -1978  -20820  86.1  1592  1592 |  433604       0
brd 1604 3   |  -92    84   -68   -3172   -1172  -19200  91.2  2165  2165 |  380446       0
brd 1604 4   |   10    49    53   -1250    -681  -19430  88.6  1983  1983 |  381251       0
brd 1604 5   |   14   -76    77      10     -28  -14800  86.7  1601  1601 |  428049       0
brd 1604 6   |    9    85   142     317    1214  -13350  85.7  1312  1312 |  424497       0
-------------+------------------------------------------------------------+----------------
brd 1604 mean|  -26    23    83    -566   -1003  -18768  87.1  1726  1726 |  405681       0
brd 1604 sdev|   56    62    78    1273    1304    3503   2.1   278   278 |   25528       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 2.1604.0  GPS week: 1604   Day: 0   MJD: 55472                            

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  127|    3     1    -3   -15    42   -75  -.12   25   21 |       0    -131   1962   2049
cod  232|   -2     0     2    27   -16    46  -.11   15   14 |     ---     ---    ---    ---
esx  136|    0    -2     0    -3     3   107   .46   22   21 |   26382   -4420   3460   7230
gfz  194|    5    -2     2   -21    62    31  -.09   33   28 |  215968   -7340   3479   6888
iac  n/a|    3     0    -2   -29    13   -93  -.19   25   25 |  319433    1030   4889 230198
mcc  n/a|    5    19    24   -82   -38   521  -.77   92   92 |     ---     ---    ---    ---

Table 2.1604.1  GPS week: 1604   Day: 1   MJD: 55473                            

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  127|    0     2    -4    -8     9   170  -.10   23   22 |       0    -235   2711   2833
cod  232|   -1    -3     2    47   -17   -17  -.12   16   16 |     ---     ---    ---    ---
esx  136|    0    -4    -4     9   -22   -47   .39   25   23 |   70123    4149   4244  10463
gfz  194|    0     3    -7   -27   107    39  -.06   30   28 |  255146    2192   4273   8765
iac  n/a|    2     1     7   -56    46  -110  -.17   26   26 |  347423   81683 114501 172839
mcc  n/a|   -6     3    16  -126    -6  1000  -.11   90   90 |     ---     ---    ---    ---

Table 2.1604.2  GPS week: 1604   Day: 2   MJD: 55474                            

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  127|    0     0     0   -32   -17    37  -.03   23   21 |       0     -49   2210   2299
cod  232|   -2     0     1    69    -6    38  -.12   13   12 |     ---     ---    ---    ---
esx  136|    5    -4     5   -59     0     9   .43   28   23 |   92046    3802   3940  10457
gfz  194|    2     0    -2    31    -5    -5  -.15   25   21 |  275398    2053   3816   8932
iac  n/a|    1     0    -8   -72    16   -82  -.03   26   26 |  434210   -1792   3937  10389
mcc  n/a|   -7     0    32   -77    10  1490  -.76   96   96 |     ---     ---    ---    ---

Table 2.1604.3  GPS week: 1604   Day: 3   MJD: 55475                            

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  127|    0     0     1     7   -55   -53  -.16   25   20 |       0     275   1667   1729
cod  232|    0     0     5    26    -6    13  -.08   14   13 |     ---     ---    ---    ---
esx  136|    1    -2     8   -19    66    99   .41   25   22 |   45515    2959   4181   9845
gfz  194|    0    -2     4   -35   -63    49  -.10   30   27 |  222748    1952   4275   9620
iac  n/a|    0     0   -16   -56   -14   -80  -.17   22   22 |  382144   -1817   4179  10159
mcc  n/a|   17    -9    41   -87   -98  1411 -1.50   98   98 |     ---     ---    ---    ---

Table 2.1604.4  GPS week: 1604   Day: 4   MJD: 55476                            

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  127|    1     0     5   -21     9   -12  -.23   27   24 |       0     345   2050   2121
cod  232|    0    -1     5    18   -27    -6  -.18   17   15 |     ---     ---    ---    ---
esx  136|    0     2     2    13   -24    34   .47   21   20 |   55129     615   3842   8382
gfz  194|    2     0    -7   -94    29    57  -.11   32   32 |  228609     385   3869   8196
iac  n/a|    0     2   -19   -57    40   -69  -.17   28   28 |  381343   -2692   3830   8772
mcc  n/a|    0     4    45    64  -147  -583  -.65  111  111 |     ---     ---    ---    ---

Table 2.1604.5  GPS week: 1604   Day: 5   MJD: 55477                            

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  127|    1     3     0   -18    -3    52  -.23   31   27 |       0    -214   2186   2314
cod  232|   -2    -1     3    39   -10    18  -.09   20   16 |     ---     ---    ---    ---
esx  136|   -2    -1     6    22   -30    30   .54   30   24 |  101745    1680   3803   8646
gfz  194|   -3    -1     0    23    27    14  -.03   38   28 |  275500     768   3814   8363
iac  n/a|    2     1   -12   -65    24   -98  -.20   29   29 |  428619    -325   3822   9168
mcc  n/a|   -2    25    48    50   189  -780  -.86  194  194 |     ---     ---    ---    ---

Table 2.1604.6  GPS week: 1604   Day: 6   MJD: 55478                            

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  127|    0     0    -5    69    29   -56  -.20   31   26 |       0     240   2014   2103
cod  232|    1     0     1     4   -23    73  -.11   16   15 |     ---     ---    ---    ---
esx  136|   -2     0     9   -57    11    -1   .43   25   23 |  100208    -336   4016   7641
gfz  194|    2     0     1    17    36     0  -.21   36   28 |  276837   -2282   4055   7932
iac  n/a|    2     0    -8    -3    23   -62  -.13   26   26 |  424976   -2694   4794   8601
mcc  n/a|   16    13    33    75   298 -1691   .40  377  377 |     ---     ---    ---    ---

       
       
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 3.1604.0  GPS week: 1604   Day: 0   MJD: 55472                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  528   28   28   17   41   31  ---   15 |    16   33   30   48   30  ---    21
 R02  | 1126   17   13   25   40   17  ---   10 |    20   37   42   53   26  ---    27
 R05  | 1032   15   14   15   28   19  ---    9 |    24   34   28   30   15  ---    22
 R07  | 3940   14   12   16   28   28  ---   10 |    27   30   28   35   24  ---    25
 R08  | 1628   26   14   26   35   25   76   13 |    28   34   39   27   36   66    30
XR09  | 3690  ---   19  ---  ---   33  ---   25 |   ---   34  ---  ---   33  ---    28
 R10  | 1482   28   11   26   50   22  ---   12 |    42   44   51   51   49  ---    44
 R11  | 1344   48   17   36   39   46  ---   21 |    57   81   95   96   62  ---    72
 R13  |  796   23   18   14   25   21  ---   11 |    51   62   60   57   62  ---    57
 R14  | 1734   48   16   42   24   25  ---   19 |    53   49   57   56   62  ---    52
 R15  | 1955   21   10   17   27   28   54   11 |    40   35   44   40   49   19    37
 R17  | 1453   24   18   18   21   23  ---   12 |    30   55   62   46   47  ---    47
 R18  | 2729   12   10   13   14   14  ---    7 |    36   36   35   28   32  ---    33
 R19  | 1417   10   12   14   32   22  ---    8 |    34   36   38   42   37  ---    34
 R20  |  943   14    7   17   45   16  ---    8 |    24   32   30   54   35  ---    28
 R21  |  928   14   12    8   26   19  ---    8 |    23   26   28   34   28  ---    22
 R22  |  879   16   11   22   37   23  ---   10 |    30   31   41   46   35  ---    29
 R23  | 1300   14   19   17   26   26  129   11 |    30   35   39   35   36   23    31
XR24  | 1279   25   24  ---  ---   22  ---   17 |    31   49  ---  ---   37  ---    37
------+-----------------------------------------+-------------------------------------
 RMS  | 1681   25   15   22   33   25   92      |T   33   40   43   45   38   36    35
 WRMS | 1681   21   14   21   28   25   92      |NE  27   35   36   39   32   44    29
 MEDI | 1344   17   14   17   28   23   76      |MD  30   35   39   46   36   23    31

Table 3.1604.1  GPS week: 1604   Day: 1   MJD: 55473                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1353   28   17   25   17   32  ---   14 |    28   34   48   33   37  ---    31
 R02  |  768   20   20   25   23   26  ---   13 |    27   31   35   28   27  ---    23
 R05  |  835   15   15   17   24   21  ---   10 |    27   29   23   21   22  ---    21
 R07  | 3709   17   11   13   48   15  ---    8 |    17   26   31   50   27  ---    22
 R08  | 3688   14   19   21   32   26   71   11 |    44   46   44   35   27   42    38
 R09  | 2213   22   13   20  ---   27  ---   12 |    32   37   40  ---   28  ---    30
 R10  | 1115   11   10   20   35   22  ---    9 |    23   21   43   46   28  ---    24
 R11  | 1404   45   19   44   47   36  ---   20 |    39   55   73   69   56  ---    50
XR12  | ----  ---    4  ---  ---  ---  ---    0 |   ---   80  ---  ---  ---  ---    79
 R13  |  768   22   20   26   36   19  ---   12 |    43   56   72   68   60  ---    55
 R14  | 1319   32   20   25   25   33  ---   15 |    38   39   37   39   42  ---    34
 R15  | 1782   33   16   23   20   40   54   16 |    58   44   47   52   49   20    45
XR16  | ----  ---    4  ---  ---  ---  ---    0 |   ---   74  ---  ---  ---  ---    71
 R17  |  944   22   14   26   21   21  ---   11 |    20   31   45   40   36  ---    29
 R18  |  793   13   18   24   19   31  ---   12 |    41   42   44   37   21  ---    36
 R19  | 1806   15   14   11   21   16  ---    8 |    36   23   29   32   30  ---    24
 R20  | 1478   18   14   24   40   28  ---   12 |    33   36   46   51   41  ---    34
 R21  |  971   20   13   28   21   21  ---   12 |    34   28   46   37   25  ---    27
 R22  |  969   27   17   39   26   26  ---   16 |    39   27   41   37   34  ---    27
 R23  | 1444   12   11   13   20   20  128    8 |    34   29   41   52   40   20    34
XR24  |  683   41   29  ---  ---   30  ---   23 |    42   45  ---  ---   38  ---    32
------+-----------------------------------------+-------------------------------------
 RMS  | 1748   23   16   25   30   26   90      |T   34   39   43   42   35   27    36
 WRMS | 1748   22   16   23   28   26   90      |NE  32   38   39   37   30   31    34
 MEDI | 1319   20   15   24   24   26   71      |MD  34   36   43   39   34   20    32

Table 3.1604.2  GPS week: 1604   Day: 2   MJD: 55474                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1044   24   19   17   14   27  ---   12 |    31   52   50   42   24  ---    38
 R02  | 1077   17   16   47   27   21  ---   14 |    27   28   41   28   24  ---    18
 R05  | 1071   24   11   23   16   13  ---   10 |    26   26   43   36   33  ---    26
 R07  | 1187   13   13   24   35   15  ---    9 |    26   28   23   41   25  ---    22
 R08  | 1515   11   15   18   19   29   64   10 |    25   35   32   41   20   58    26
 R09  | 3789   30   13   28  ---   14  ---   12 |    20   32   38  ---   29  ---    25
 R10  | 1114   15   10   26   21   30  ---   11 |    29   27   45   33   42  ---    29
 R11  | 1773   44   15   38   29   60  ---   22 |    45   47   70   49   56  ---    49
XR12  | ----  ---   19  ---  ---   39  ---   27 |   ---   86  ---  ---   44  ---    75
 R13  | 1445   23   12   34   35   25  ---   13 |    34   47   51   49   46  ---    41
 R14  | 2149   28   13   35   28   26  ---   14 |    37   47   53   45   45  ---    40
 R15  | 2145   25   13   24   24   22   61   11 |    57   36   47   35   39   17    38
XR16  | ----  ---   12  ---  ---   26  ---   18 |   ---   51  ---  ---   40  ---    44
 R17  | 1389   25    5   15   23   28  ---   10 |    24   35   45   48   61  ---    38
 R18  |  691   22   17   20   22   20  ---   11 |    29   44   27   38   30  ---    31
 R19  | 1149   16    6   13   22   15  ---    7 |    36   41   50   52   44  ---    40
 R20  | 1594   21    7   19   18   24  ---   10 |    21   20   29   28   37  ---    21
 R21  | 1270   13   10   26   21   28  ---   11 |    21   21   26   28   31  ---    16
 R22  | 1039   16   12   35   31   20  ---   11 |    33   20   47   36   21  ---    22
 R23  |  768   18   11   47   21   13  140   13 |    32   37   62   41   41   30    37
 R24  | 1204   19   17   16  ---   26  ---   11 |    41   37   44  ---   46  ---    38
------+-----------------------------------------+-------------------------------------
 RMS  | 1592   23   13   28   25   26   96      |T   31   37   43   39   37   35    34
 WRMS | 1592   21   12   23   21   26   96      |NE  28   37   39   38   34   44    32
 MEDI | 1204   21   13   24   22   25   64      |MD  29   36   45   41   39   30    37

Table 3.1604.3  GPS week: 1604   Day: 3   MJD: 55475                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1277   28   24   30   24   23  ---   15 |    41   41   65   52   36  ---    40
 R02  | 1837   19   17   18   21   17  ---   10 |    27   47   51   51   31  ---    36
 R05  | 1038    9   16   13   19   25  ---    9 |    37   37   36   35   37  ---    32
 R07  | 3010   12   11   16   24   13  ---    7 |    21   24   28   26   19  ---    19
 R08  | 4787   20   16   17   38   24   89   11 |    53   33   36   16   28  115    33
 R09  | 3960   15   11   27  ---   16  ---   10 |    27   32   47  ---   30  ---    29
 R10  | 2162   14   16   27   37   18  ---   11 |    37   42   51   53   55  ---    42
 R11  | 1345   69   11   44   27   51  ---   26 |    53   50   69   64   54  ---    49
XR12  | ----  ---   23  ---  ---   36  ---   29 |   ---   69  ---  ---   38  ---    59
 R13  | 1292   33   16   41   30   17  ---   15 |    64   67   85   79   75  ---    68
 R14  | 2363   22   16   20   40   37  ---   14 |    68   68   68   73   78  ---    66
 R15  | 2311   31   14   26   26   20   70   13 |    61   54   62   54   57   21    55
XR16  | ----  ---    9  ---  ---   16  ---   12 |   ---   42  ---  ---   29  ---    39
 R17  | 1376   16   11   16   37   14  ---    8 |    43   40   56   41   58  ---    47
 R18  | 1427   20   12   24   43   19  ---   10 |    44   55   46   58   59  ---    50
 R19  |  758   10   11   17   19    9  ---    7 |    39   40   29   39   43  ---    36
 R20  | 1301   16   15   12   20   20  ---    9 |    41   45   48   53   52  ---    44
 R21  | 1412   25   11   14   29   19  ---   10 |    30   26   29   40   36  ---    26
 R22  | 1267   17    9   18   19   14  ---    8 |    33   25   17   24   28  ---    22
 R23  | 1611   15   13   36   31   17  126   12 |    34   32   61   54   33   33    34
 R24  | 1960   12    9   23   34   13  ---    8 |    38   42   42   22   45  ---    39
------+-----------------------------------------+-------------------------------------
 RMS  | 2165   25   14   25   30   22   98      |T   41   43   48   46   43   56    41
 WRMS | 2165   20   13   22   27   22   98      |NE  36   39   42   39   37   74    36
 MEDI | 1427   17   13   20   27   18   89      |MD  39   42   48   51   38   33    39

Table 3.1604.4  GPS week: 1604   Day: 4   MJD: 55476                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1130   29   16   20   21   20  ---   12 |    40   37   33   27   34  ---    31
 R02  |  862   22   12   18   17   20  ---   10 |    21   39   45   35   23  ---    30
 R05  | 1271   12   21   26   43   34  ---   14 |    32   39   44   61   30  ---    30
 R07  | 2603   19   10   13   50   21  ---    9 |    29   28   26   50   31  ---    24
 R08  | 3812   12   14   12   18   25   68    9 |    30   27   40   35   25   82    27
 R09  | 3462   16   15   18  ---   24  ---   10 |    26   33   30  ---   29  ---    25
 R10  | 1599   25   16   30   28   29  ---   14 |    18   38   51   51   50  ---    33
 R11  | 2500   49   15   29   33   54  ---   21 |    48   55   72   78   59  ---    52
XR12  |>>>>>   62   48  ---  ---   46  ---   37 |    34   59  ---  ---   35  ---    56
 R13  |  823   53   19   19   24   32  ---   18 |    54   87   89   97  103  ---    79
 R14  |  806   48   23   35   41   34  ---   20 |    44   86   97  109   75  ---    73
 R15  | 2540   50   23   30   46   51  ---   22 |    47   52   46   53   57  ---    41
XR16  | ----  ---   14  ---  ---   24  ---   18 |   ---   77  ---  ---   45  ---    68
 R17  |  980    9   11   15   21   23  ---    8 |    35   34   46   31   28  ---    34
 R18  | 2338   11   20   18   22   17  ---   10 |    28   39   35   26   26  ---    29
 R19  |  945   11   15   10   25   16  ---    7 |    43   40   53   57   55  ---    45
 R20  | 1011    9   18   14   32   26  ---   10 |    28   37   37   53   40  ---    32
 R21  | 1649   18   16   20   26   17  ---   10 |    19   34   34   43   31  ---    26
 R22  | 1564   20   19   16   28   16  ---   10 |    25   24   22   31   22  ---    16
 R23  | 1689   14   13   22   28   21  142   10 |    48   44   40   59   42   43    41
 R24  | 2187    9   14   14   48   15  ---    8 |    46   50   39   38   40  ---    46
------+-----------------------------------------+-------------------------------------
 RMS  | 1982   27   17   21   32   28  111      |T   34   45   46   51   41   62    39
 WRMS | 1982   24   15   20   32   28  111      |NE  32   40   37   42   33   62    35
 MEDI | 1599   18   16   18   28   24   68      |MD  32   39   40   50   35   43    33

Table 3.1604.5  GPS week: 1604   Day: 5   MJD: 55477                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1082   12   16   18   22   28  ---   11 |    49   39   50   48   49  ---    43
 R02  |  600   29   20   15   15   31  ---   14 |    33   38   30   29   15  ---    26
 R05  | 1565   24   28   16   20   22  ---   13 |    37   45   42   36   31  ---    35
 R07  | 2100   10   14   14   39   21  ---    8 |    24   29   27   43   22  ---    23
 R08  | 2510   10    9   15   32   24   70    8 |    21   20   14   22   22   49    15
 R09  |  705   24   16   21   37   32  ---   13 |    32   30   26   26   33  ---    25
 R10E | 1664   17    9   20   44   21  ---    9 |    24   33   45   53   40  ---    32
 R11E | 2025   68   22   74   94   47  ---   31 |    37   68  117  121   55  ---    60
XR12  |>>>>>   67   58  ---  ---  102  ---   53 |    48   78  ---  ---   33  ---    61
 R13E | 1011   74   50   46   49   39  ---   31 |    45  128  131  129   68  ---    91
 R14E |  819   38   25   30   49   38  ---   18 |    54   73   74   77   51  ---    59
 R15E | 1501   32   18   21   49   28  ---   14 |    70   61   64   76   57  ---    59
XR16  | ----  ---   21  ---  ---   31  ---   25 |   ---   49  ---  ---   42  ---    50
 R17  |  864   11   13   13   20   22  ---    8 |    34   42   39   42   32  ---    34
 R18  | 2972   26   13   59   22   29  ---   20 |    24   25   77   26   18  ---    27
 R19  | 1352    9   17   19   19   13  ---    9 |    26   26   39   37   28  ---    26
 R20  | 1289   19   11   13   19   13  ---    8 |    35   41   46   41   40  ---    39
 R21  | 1462   28    8   23   30   16  ---   11 |    27   42   48   52   37  ---    35
 R22  | 1798   12   15   12   20   33  ---   11 |    24   24   15   26   24  ---    16
 R23  | 1917   22   16   25   34   34  265   14 |    39   32   33   48   29   44    28
 R24  |  760   14   15   18   26   31  ---   11 |    36   30   19   33   47  ---    33
------+-----------------------------------------+-------------------------------------
 RMS  | 1601   31   20   30   38   29  194      |T   35   45   49   50   36   46    38
 WRMS | 1601   27   16   24   28   29  194      |NE  32   36   36   36   31   46    32
 MEDI | 1462   22   16   19   30   29   70      |MD  34   39   42   42   33   44    34

Table 3.1604.6  GPS week: 1604   Day: 6   MJD: 55478                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  895   22   19   21   17   18  ---   11 |    36   33   38   29   27  ---    28
 R02  | 1007   39   15   18   12   22  ---   13 |    38   30   28   28   26  ---    24
 R05  | 1748   11   19   17   15   28  ---   11 |    31   38   31   35   23  ---    28
 R07  | 1526   18   14   34   95   24  ---   13 |    30   31   29   79   32  ---    27
 R08  | 1264   16   18   25   26   23   53   12 |    20   33   39   32   30   32    25
 R09  | 1550   46   19   28   36   46  ---   20 |    29   42   42   31   36  ---    34
 R10E |  964   20   15   20   35   38  ---   13 |    29   31   38   38   53  ---    34
 R11E |  803   58   19   36   52   29  ---   20 |    72   64   69   61   67  ---    64
XR12  |>>>>>   59   19  ---  ---   46  ---   29 |    42   51  ---  ---   37  ---    49
 R13E |  804   62   19   24   38   21  ---   19 |    66   69   74   75   87  ---    69
 R14E | 1060   28   19   18   44   28  ---   13 |    54   67   68   59   62  ---    60
 R15E | 2304   33   15   48   34   28  ---   18 |    62   55   64   54   66  ---    57
XR16  |11972  191   37  ---  ---   64  ---   49 |     3   79  ---  ---   51  ---    54
 R17  |  936   26   15   24   20   17  ---   11 |    40   38   45   44   43  ---    38
 R18  | 1530   10   12   16   31   15  ---    8 |    21   28   28   20   31  ---    22
 R19  |  917   14   12   12   21   26  ---    9 |    21   26   30   32   32  ---    24
 R20  | 1745   31   15   34   19   22  ---   14 |    30   26   35   26   31  ---    23
 R21  | 1565   24   10   15   37   21  ---   10 |    31   46   35   57   55  ---    40
 R22  |  769   20   13   21   26   20  ---   10 |    19   28   22   32   29  ---    21
 R23  | 1461   17   13   29   26   28  531   12 |    25   32   49   46   29   35    31
 R24  |  749   21   16   10   21   24  ---   10 |    28   31   19   20   32  ---    29
------+-----------------------------------------+-------------------------------------
 RMS  | 1312   31   16   25   36   26  377      |T   34   41   41   42   41   33    37
 WRMS | 1312   26   15   23   28   26  377      |NE  27   37   33   36   34   33    31
 MEDI | 1264   24   15   21   26   24   53      |MD  30   33   38   35   32   32    31




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