[IGSREPORT-19238] Wk 1611 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Dec 9 05:19:09 PST 2010


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1611   (Nov 21, 2010 - Nov 27, 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 2.1611.
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:                   
                                                                               
 igl1611[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1611 in the SP3 format.
 igl16117.sum      Combination Report for GPS Week 1611.


    
    
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  |    365.9 ns
                1  |    357.0 ns
                2  |    364.6 ns
                3  |    340.9 ns
                4  |    340.8 ns
                5  |    331.5 ns
                6  |    383.7 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  |  IAC   | R17

    
         
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 1.1611, 1a.1611).
        
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 2.1611.0-6)                                                                                
    
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 3.1611.0-6). 
        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 1611 summary.                      (Nov 21, 2010 - Nov 27, 2010)

Table 1.1611.a     GPS week : 1611   MJD: 55521.0-55527.0

         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    -1    14     2   -31   -30  -.04   27   26 |       0    1324   7347   8469
        |    2     2     3    39    31   107   .14           |       0    2706
cod  225|   -1     0    -6    42    17     4  -.07   12   11 |     ---     ---    ---    ---
        |    0     1     2    10    12    36   .05           |     ---     ---
esx  134|   -2     0    -9   -33    -7    -6   .35   25   22 |   18066    4496   5501  10327
        |    1     2     2    39    20    36   .11           |   20112    4626
gfz  189|   -1     0    -9   -50   -59   -42  -.28   38   36 |  175272    3642   5506  10455
        |    0     1     2    60    65    68   .16           |   20804    3474
iac  n/a|    3    -2    11   -61     0    39  -.21   31   31 |  355041    -343   5496  10372
        |    1     2     5    26    21    38   .04           |   18410    2468
mcc  n/a|    4     0    63   -16    11   432  -.18  298  298 |     ---     ---    ---    ---
        |   15    11    40   176   135   539   .67           |     ---     ---


Table 1.1611.b     GPS week : 1611   MJD: 55521.0-55527.0   

         Satellite position sigmas for the combined orbits
         (coded in the IGS SP3 orbit files).
         "E" flags eclipsing satellites.
         Units: mm.

              Day of GPS week
 PRN  |    0    1    2    3    4    5    6 |  Remarks
------+------------------------------------+------------------------------------------
 R01  |   14   19   10   13   14   15   15 |
 R02  |   15   23   14   12   12   14   13 |
 R05  |    9   16   11   11   13   14   14 |
 R06  |    0    0    0    0    0    0   31 |
 R07  |   13   13   11   16   14   15   17 |
 R08  |   11   15    9   11   14   17   15 |
 R09  |   11    9   12   11   13   12    9 |
 R10  |   11   15   11   10   11   10    8 |
 R11  |   16   13   15   15   15   15   17 |
 R12  |   11    9   10   11   12   11    8 |
 R13  |   12   11    9    8    9    8   10 |
 R15  |   13   11    9   11   11   14   14 |
 R16  |    9   10   11    9    9    9    9 |
 R17  |   17   14   15   17   19   18   22 |
 R18  |   12   11   13   14   12    7   11 |
 R19  |   12   11   11   16   15   12   11 |
 R20  |   18   16   21   17   18   16   15 |
 R21  |    9    8    9   11   10   11   10 |
 R22  |    9   11    8   10    9    8    7 |
 R23  |   16   11   13   10    9   12   12 |
 R24  |   12   18    9   13    9   10   10 |


Table 1.1611.c     GPS week : 1611   MJD: 55521.0-55527.0   

         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 1611 0   |  -27   -62   102   -1444    -762  -12630  86.9  2356  2356 |  365860       0
brd 1611 1   |   38   -30   305   -1441   -1323  -13710  86.5  2663  2663 |  356994       0
brd 1611 2   |   70   -36    84    -559   -1513   -7430  87.1  2494  2494 |  364631       0
brd 1611 3   |  -79    96   -15   -3340    -144   -7705  88.8  3065  3065 |  340925       0
brd 1611 4   |  -14   -43    95    -660     861   -9634  86.3  3089  3089 |  340749       0
brd 1611 5   |  -59   -14     8   -1649     323  -12370  84.8  2617  2617 |  331482       0
brd 1611 6   |   17   -66    36    -976       1  -13830  85.6  1803  1803 |  383659       0
-------------+------------------------------------------------------------+----------------
brd 1611 mean|   -7   -22    88   -1438    -365  -11044  86.6  2583  2583 |  354900       0
brd 1611 sdev|   53    55   106     935     871    2748   1.3   440   440 |   18212       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 2.1611.0  GPS week: 1611   Day: 0   MJD: 55521                            

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|    3    -3    10    29   -10  -113  -.21   29   29 |       0   -2232   7613   9271
cod  225|   -2     0    -9    32    -1     7  -.03   13   13 |     ---     ---    ---    ---
esx  134|   -2     0    -4    -2    10     1   .37   25   22 |   17531    2106   6042   9037
gfz  189|    0    -1    -9   -24   -38   -49  -.14   31   26 |  194657    -504   6045   9004
iac  n/a|    4     0    16   -70    15    49  -.17   26   26 |  365880   -2333   6042   9869
mcc  n/a|  -14    11    17  -227   209  -183   .81  404  404 |     ---     ---    ---    ---

Table 2.1611.1  GPS week: 1611   Day: 1   MJD: 55522                            

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|    4    -2    12    29   -79   -20  -.21   33   29 |       0    3479   7845   8943
cod  225|   -1     1    -6    36    21   -28  -.00   12   11 |     ---     ---    ---    ---
esx  134|   -2     0    -8   -97    27    22   .36   26   24 |    5521    5564   4501   9811
gfz  189|   -1     0   -12   -78  -143   -62  -.25   37   35 |  177814    3703   4453  10035
iac  n/a|    2    -5    13   -31   -29   112  -.29   30   30 |  358310   -2335   4475  10929
mcc  n/a|   -7   -21     8   140    36   656 -1.03  339  339 |     ---     ---    ---    ---

Table 2.1611.2  GPS week: 1611   Day: 2   MJD: 55523                            

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    -2    20   -42   -74    47  -.02   24   23 |       0    5357   9063  10645
cod  225|    0     1    -6    58    39   -15  -.08   11   11 |     ---     ---    ---    ---
esx  134|   -4     1   -13     7   -13   -30   .52   29   24 |   23049    7206   5146  11229
gfz  189|    0     1   -13     0  -136  -156  -.07   37   53 |  183501    5063   5138  11000
iac  n/a|    2    -2     6   -81   -11    49  -.24   25   25 |  365409   -2187   5144  12363
mcc  n/a|   30     8   107   114   -25  1457  -.36  305  305 |     ---     ---    ---    ---

Table 2.1611.3  GPS week: 1611   Day: 3   MJD: 55524                            

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|    3    -3    16   -36   -14    85   .19   27   27 |       0    3032  11275  12796
cod  225|   -1     2    -4    45    17   -21  -.09   12   12 |     ---     ---    ---    ---
esx  134|   -4     4   -11   -10   -32   -20   .16   26   25 |    2112   12223   8580  11142
gfz  189|   -1     1    -9  -145   -18   -38  -.31   41   27 |  157104    9520   8652  11098
iac  n/a|    5    -2     8   -96    11    41  -.20   27   27 |  340628    2700   8584  10838
mcc  n/a|    2    -7   109   -87    29   389   .29  302  302 |     ---     ---    ---    ---

Table 2.1611.4  GPS week: 1611   Day: 4   MJD: 55525                            

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     1    16    56   -10   -77   .01   28   27 |       0     758   5253   6073
cod  225|   -2     0    -6    37    14    58  -.15   14   12 |     ---     ---    ---    ---
esx  134|   -2     0    -9   -62    -5   -43   .35   23   22 |   15925   -2146   4446   9893
gfz  189|    0     1    -6   -22    41    53  -.46   33   25 |  160559    -497   4462  10237
iac  n/a|    4     0    17   -24   -11     0  -.23   28   28 |  341739   -2394   4429   9130
mcc  n/a|   20     0    84    70  -158   512   .35  274  274 |     ---     ---    ---    ---

Table 2.1611.5  GPS week: 1611   Day: 5   MJD: 55526                            

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    14     9    -6  -203  -.03   25   23 |       0    -741   5443   6074
cod  225|   -2     0    -7    34    16    51  -.07   13   12 |     ---     ---    ---    ---
esx  134|    0    -1    -7    -9   -11    58   .28   20   18 |    2509    5184   4307  10722
gfz  189|   -2    -2    -9    21   -73    25  -.51   40   55 |  148379    4846   4342  11189
iac  n/a|    6     0    15   -49    -6    18  -.17   33   33 |  330126    1876   4329   9933
mcc  n/a|   -2    -5    71   140   133   -27  -.72  277  277 |     ---     ---    ---    ---

Table 2.1611.6  GPS week: 1611   Day: 6   MJD: 55527                            

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    11   -30   -26    70  -.01   24   24 |       0    -381   4937   5485
cod  225|   -1     0    -2    57    17   -20  -.05   11   10 |     ---     ---    ---    ---
esx  134|   -1    -3    -9   -58   -26   -34   .39   26   22 |   59821    1340   5489  10459
gfz  189|   -1     0    -8  -105   -44   -67  -.24   45   32 |  204892    3366   5456  10624
iac  n/a|    3    -3     5   -76    35     4  -.19   51   51 |  383195    2272   5473   9547
mcc  n/a|    1     8    43  -265  -147   219  -.57  188  188 |     ---     ---    ---    ---

       
       
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 3.1611.0  GPS week: 1611   Day: 0   MJD: 55521                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 2293   32   14   28   21   29  ---   14 |   116  112  112  115  115  ---   112
 R02  | 1945   46   13   31   35   16  ---   15 |   110  125  131  132  123  ---   122
 R05  |  941   20   10   17   20   15  571    8 |    67   75   76   73   70  138    71
XR06  | ----  ---    5  ---  ---  ---  ---    0 |   ---   81  ---  ---  ---  ---    79
 R07E | 6783   19   17   25   33   25  ---   12 |    38   42   55   57   46  ---    41
 R08  | 2724   32   10   12   18   23  516   11 |    96  109  107  109  106  197   104
 R09  | 2099   18   13   27   28   19  ---   10 |    21   29   38   31   33  ---    27
 R10  | 1080   27   10   13   17   26  ---   10 |    22   30   37   38   52  ---    32
 R11  | 1391   31   20   36   29   27  248   15 |    67   63   95   90   72   65    71
 R12  | 1992   25   11   15   32   27  ---   11 |    24   31   32   43   27  ---    25
 R13  | 1472   18   16   22   39   30  ---   12 |    22   27   26   31   27  ---    21
 R15  | 2790   23   16   18   18   34  ---   13 |    26   28   27   26   33  ---    25
 R16  | 2838   20   10   13   31   21  ---    9 |    21   26   33   33   27  ---    24
 R17  |  865   51    8   27   28   35  ---   17 |    38   61   78   71   41  ---    55
 R18  | 1589   19    9   31   38   21  379   11 |    45   69   89   95   55  120    65
 R19  |  939   21    7   30   30   24  ---   11 |    46   67   81   73   64  ---    63
 R20  | 1127   41   16   24   42   47  ---   18 |    36   61   81   83   84  ---    63
 R21  | 1863   18   11   20   47   12  ---    8 |    51   76   79   95   65  ---    69
 R22  | 1746   22   11   15   24   14  ---    8 |    57   75   72   87   67  ---    68
 R23  | 1127   31   13   48   40   20  140   16 |    42   51   95   92   57   64    58
 R24  | 2211   32   18   10   21   20  ---   11 |    26   56   55   58   41  ---    46
------+-----------------------------------------+-------------------------------------
 RMS  | 2355   29   13   25   31   26  404      |T   48   61   69   71   60  116    59
 WRMS | 2355   29   13   22   26   26  404      |NE  36   50   61   63   49   83    47
 MEDI | 1746   23   11   22   29   23  379      |MD  38   61   76   73   55  120    63

Table 3.1611.1  GPS week: 1611   Day: 1   MJD: 55522                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 2611   58   15   34   33   29  ---   18 |    81  104  120  112  100  ---   100
 R02  | 2179   68   20   49   54   34  ---   23 |    78  118  146  152   95  ---   108
 R05E |  898   27   16   31   43   43  649   16 |    45   70   87   90   65  204    64
XR06E | ----  ---    5  ---  ---  ---  ---    0 |   ---   50  ---  ---  ---  ---    48
 R07E | 7544   22   12   32   30   24  ---   12 |    25   33   46   39   33  ---    30
 R08E | 1062   31   12   34   30   31  ---   14 |    72   92  105  108   74  ---    85
 R09  | 2554   21    9   10   16   27  ---    9 |    23   28   27   27   24  ---    22
 R10  | 2051   34   12   21   28   43  ---   15 |    21   24   34   24   46  ---    26
 R11  | 1974   26   14   22   15   28  216   12 |    70   56   60   64   57   53    57
 R12  | 1459   16    7   10   29   25  ---    8 |    30   33   30   49   43  ---    33
 R13  | 2115   26   12   20   28   24  ---   11 |    16   29   38   45   29  ---    25
 R15  | 1872   31    7   21   53   24  199   11 |    32   20   28   50   32   29    23
 R16  | 1994   16   13   19   25   24  ---   10 |    32   27   29   28   21  ---    23
 R17  |  964   34   15   14   32   36  ---   13 |    21   37   45   64   41  ---    34
 R18  | 4877   28    7   24   22   25  220   11 |    32   54   63   51   44   77    49
 R19  |  847   24    7   31   31   18  ---   11 |    37   47   62   50   36  ---    45
 R20  | 2244   32   12   20   26   47  ---   15 |    29   30   32   41   46  ---    32
 R21  | 2758   14   10   15   38   20  ---    8 |    46   42   48   63   46  ---    43
 R22  | 1032   30    9   14   76   27  ---   11 |    47   48   48   85   49  ---    45
 R23  |  841   30   12   17   30   18  143   10 |    32   52   55   61   49   66    48
 R24  | 1692   37   13   39   41   40  ---   17 |    24   36   64   64   27  ---    31
------+-----------------------------------------+-------------------------------------
 RMS  | 2663   33   12   26   37   30  339      |T   39   49   58   63   47   85    46
 WRMS | 2663   29   11   24   35   30  339      |NE  32   37   44   51   39   56    35
 MEDI | 1974   28   12   21   30   27  216      |MD  32   42   48   51   44   66    43

Table 3.1611.2  GPS week: 1611   Day: 2   MJD: 55523                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 2960   17   11   23   25   24  ---   10 |    72   66   77   63   76  ---    69
 R02E | 1352   41   15   22   27   17  ---   13 |    68  107  115  119  104  ---    99
 R05E |  699   13    8   32   41   26  ---   10 |    47   63   73   69   61  ---    59
XR06E | ----  ---    5  ---  ---  ---  ---    0 |   ---   68  ---  ---  ---  ---    66
 R07E | 4612   22   10   29   41   21  ---   11 |    18   38   56   63   31  ---    32
 R08E | 1597   18    8   19   20   18  569    8 |    71   96  109  101  100  275    94
 R09  | 2054   14   14   19   34   33  ---   11 |    24   29   38   26   25  ---    23
 R10  | 2250   29    8   22   35   21  ---   11 |    20   32   38   34   32  ---    27
 R11  | 3747   30   19   37   28   24  129   15 |    73   72   91   72   60   87    69
 R12  | 1499   15   10   32   31   16  ---   10 |    19   22   44   43   25  ---    21
 R13  | 2402   13   11   19   26   24  ---    9 |    26   30   30   34   36  ---    28
 R15  | 1695   20    9   21   30   18  139    9 |    26   22   28   34   25   48    20
 R16  | 1672   14   13   27   23   26  ---   11 |    20   32   34   29   23  ---    21
 R17  | 1220   24   11   43   36   31  ---   14 |    27   41   81   71   37  ---    41
 R18  | 3757   35    9   30   31   21  277   13 |    41   69   82   66   63  207    62
 R19  | 1407   27    5   24   31   23  ---   11 |    37   54   66   58   62  ---    52
 R20  | 4466   36   21   50   64   49  ---   21 |    34   56  103   97   81  ---    61
 R21  | 3167   14    9   23   29   22  ---    9 |    40   59   53   56   57  ---    53
 R22  |  997   15    6   18   79   19  ---    7 |    48   56   66   97   62  ---    56
 R23  | 1756   23    9   40   27   25  164   13 |    27   32   37   37   45  137    27
 R24  |  890   21   10   13   19   20  ---    9 |    28   38   38   43   47  ---    36
------+-----------------------------------------+-------------------------------------
 RMS  | 2493   24   11   29   37   25  304      |T   38   51   62   60   52  150    48
 WRMS | 2493   23   11   24   53   25  304      |NE  32   42   55   53   45  119    39
 MEDI | 1695   20   10   23   30   22  164      |MD  28   54   56   58   47  137    52

Table 3.1611.3  GPS week: 1611   Day: 3   MJD: 55524                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 3404   27   14   14   30   33  ---   12 |    82   90   88   92   87  ---    86
 R02E |  625   24   11   29   26   24  ---   12 |   101  108  125  114  101  ---   108
 R05E |  801   15   10   28   34   24  641   10 |    61   69   66   76   63  168    63
XR06E | ----  ---    4  ---  ---  ---  ---    0 |   ---   49  ---  ---  ---  ---    48
 R07E | 6102   23   16   37  117   36  ---   15 |    22   35   57  106   34  ---    28
 R08E | 1712   23    8   20   18   28  265   11 |    92  107  118  107   96  149   103
 R09  | 1955   22    7   30   24   20  ---   11 |    22   24   47   32   23  ---    23
 R10  |  898   19   13   23   23   20  ---   10 |    27   33   28   40   36  ---    28
 R11  | 4595   33   15   25   38   34   89   14 |    65   73   70   66   53   39    65
 R12  | 1440   17   13   17   20   29  ---   10 |    38   37   42   32   44  ---    34
 R13  | 2948   14    6   16   16   19  ---    7 |    27   30   27   28   22  ---    25
 R15  | 1971   28   11   18   25   25  104   11 |    28   25   29   39   33   45    25
 R16  | 3085   18   10   11   21   22  ---    8 |    33   20   26   33   20  ---    20
 R17  |  799   31   19   27   27   47  ---   17 |    32   49   67   62   37  ---    41
 R18  | 4482   38   13   32   30   19  169   14 |    37   67   80   86   51  194    59
 R19  | 1368   38   14   39   34   19  ---   15 |    37   58   76   70   50  ---    52
 R20  | 7197   38   13   21   49   45  ---   16 |    57   69   69   96  101  ---    70
 R21  | 1342   22    7   34   43   11  ---   10 |    54   68  101  100   72  ---    71
 R22  | 1368   20   11   17   25   22  ---    9 |    50   52   51   51   59  ---    50
 R23  | 2435   27    8   18   64   22  132   10 |    32   50   58   83   61  133    48
 R24  | 1079   33    4   35   18   14  ---   12 |    21   41   68   43   46  ---    41
------+-----------------------------------------+-------------------------------------
 RMS  | 3065   27   12   26   41   27  302      |T   45   54   64   67   54  121    51
 WRMS | 3065   27   12   25   27   27  302      |NE  37   46   55   57   47  102    43
 MEDI | 1712   23   11   23   26   22  132      |MD  37   50   66   66   50  133    48

Table 3.1611.4  GPS week: 1611   Day: 4   MJD: 55525                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 2588   35   10   15   26   41  ---   14 |    45   55   54   55   57  ---    52
 R02E | 1511   29   14   22   26   23  ---   12 |    66   71   87   94   71  ---    71
 R05E |  921   20   17   31   33   24  525   13 |    39   41   49   59   39   85    38
XR06E | ----  ---    6  ---  ---  ---  ---    0 |   ---   45  ---  ---  ---  ---    44
 R07E | 5379   23   12   28   66   37  ---   14 |    14   22   40   71   37  ---    20
 R08E | 2338   36   11   23   22   34  230   14 |    85  106  117  103   99  103   102
 R09  | 1533   25   15   28   17   27  ---   13 |    27   34   52   29   20  ---    27
 R10  |  852   22   10   18   21   26  ---   10 |    24   26   37   33   41  ---    27
 R11  | 3865   33   12   26   25   34   91   14 |    59   60   81   66   41   31    59
 R12  | 2299   28   11   25   22   25  ---   12 |    31   32   32   41   28  ---    26
 R13  | 3577   21    9   11   14   20  ---    8 |    30   27   28   26   28  ---    23
 R15  | 2509   27   10   12   23   27   96   10 |    27   27   30   29   31   34    25
 R16  | 2144   15   11   19   24   18  ---    9 |    27   29   46   40   26  ---    29
 R17  | 1667   25   29   26   25   50  ---   19 |    27   53   41   33   36  ---    37
 R18  | 1488   32   14   18   20   22  301   12 |    29   46   47   46   21   92    36
 R19  | 1236   40   13   38   26   10  ---   15 |    26   54   77   60   37  ---    49
 R20  | 8296   44   21   24   56   37  ---   17 |    21   63   62   99   55  ---    53
 R21  | 3809   25    5   17   58   22  ---    9 |    48   62   76   79   74  ---    64
 R22  | 2494   18   12   22   40   10  ---    9 |    45   42   64   41   44  ---    47
 R23  | 1731   21    8   11   25   22  115    8 |    23   35   50   57   42   76    36
 R24  |  739   15    7   20   37   17  ---    8 |    46   47   47   69   53  ---    46
------+-----------------------------------------+-------------------------------------
 RMS  | 3089   28   14   23   33   28  274      |T   36   46   55   56   44   70    43
 WRMS | 3089   27   12   22   25   28  274      |NE  32   42   51   49   38   58    38
 MEDI | 2144   25   11   22   25   24  115      |MD  29   45   49   55   39   76    38

Table 3.1611.5  GPS week: 1611   Day: 5   MJD: 55526                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E | 1383   29   11   21   24   47  ---   15 |    65   55   64   64   78  ---    60
 R02E | 2077   33   18   18   19   32  ---   14 |    64   81   85   79   73  ---    75
 R05E |  978   26   14   22   30   35  371   13 |    29   30   43   51   50   51    32
XR06E | ----  ---    6  ---  ---  ---  ---    0 |   ---   32  ---  ---  ---  ---    34
 R07E | 5215   27   14   28   57   40  ---   15 |    16   27   34   73   39  ---    21
 R08E | 2382   39   20   21   27   38  112   16 |    94  127  133  111  112   75   118
 R09  | 1207   22   10   24   27   26  ---   11 |    25   22   39   35   23  ---    20
 R10  | 1340   16   14   11   26   25  ---    9 |    29   29   33   30   38  ---    27
 R11  | 1492   29   17   33   40   25   99   15 |    44   54   68   67   49   16    52
 R12  | 1885   20   17   18   33   24  ---   11 |    27   31   38   49   20  ---    28
 R13  | 3627   17   11   14   34   17  ---    8 |    28   22   26   38   18  ---    21
 R15  | 2759   29   10   18   15   43   75   14 |    21   23   31   27   28   30    22
 R16  |  932   22    9   14   22   21  ---    9 |    24   25   33   36   20  ---    21
 R17  | 1865   26   13   17   88   63  ---   17 |    49   51   56   87   64  ---    45
 R18  | 1551   15   10    7   57   12  521    6 |    30   32   25   41   29  109    27
 R19  | 1234   19   17   22   22   27  ---   11 |    40   42   59   59   51  ---    46
 R20  | 6054   34   15   17   37   50  ---   16 |    27   47   49   64   59  ---    44
 R21  | 3492   22   11   21   38   19  ---   10 |    31   55   60   79   40  ---    48
 R22  | 2438   15    5   16   46   16  ---    7 |    30   38   52   48   38  ---    39
 R23  |  999   17   14   31   55   18  152   12 |    29   32   44   68   36   36    31
 R24  | 1732   14    8   21   22   27  ---   10 |    33   28   27   51   53  ---    30
------+-----------------------------------------+-------------------------------------
 RMS  | 2616   25   13   20   40   33  277      |T   36   42   49   57   45   52    40
 WRMS | 2616   23   12   18   55   33  277      |NE  31   35   42   51   37   47    33
 MEDI | 1732   22   13   18   30   26  112      |MD  29   32   43   51   39   36    32

Table 3.1611.6  GPS week: 1611   Day: 6   MJD: 55527                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01E |  685   33   12   20   27   49  ---   15 |    58   62   63   69   83  ---    62
 R02E | 3139   17   16   28   32   34  ---   12 |   101  110  124  118  102  ---   109
 R05E | 1436   27   12   28   24   38  262   14 |    56   59   62   65   60   87    57
XR06E | 9360   46   21  ---  ---  ---  ---   31 |     3   41  ---  ---  ---  ---    40
 R07E | 1622   38   10   37  125   39  ---   16 |    18   23   41   87   36  ---    21
 R08E | 1344   23   15   28   33   46  239   15 |   145  181  179  180  142   88   167
 R09  |  997   14    6   20   35   25  ---    8 |    19   22   38   42   25  ---    21
 R10  | 1757   13    5   14   19   24  ---    7 |    28   32   41   30   50  ---    34
 R11  |  822   31   17   35   45   41   94   16 |    52   66   84   85   57   26    62
 R12  | 1733   14   10   17   21   13  ---    7 |    19   28   29   28   25  ---    24
 R13  | 2344   15   12   22   21   27  ---   10 |    22   25   23   31   21  ---    20
 R15  | 1995   30    5   19   23   49   62   14 |    27   27   30   30   37   34    26
 R16  | 1356   15    7   16   22   26  ---    8 |    22   25   29   40   31  ---    24
 R17  | 1297   33   11   50   50  177  ---   21 |    86   74   62   52  112  ---    67
 R18  | 2546   27   13   13   27   21  ---   10 |    41   58   58   63   45  ---    51
 R19  | 1285   12   14   18   66   37  ---   11 |    47   59   70   75   72  ---    59
 R20  | 2412   39    6   37   37   26  ---   15 |    28   59   80   85   68  ---    56
 R21  | 2182   18    8   21   13   24  ---    9 |    54   75   86   86   62  ---    71
 R22  | 2544   17    8   13   32   13  ---    7 |    45   65   67   77   63  ---    60
 R23  | 1118   11   11   33   69   27  195   11 |    45   53   67   84   55   67    53
 R24  |  999   17    9   18   39   28  ---    9 |    34   50   54   71   50  ---    46
------+-----------------------------------------+-------------------------------------
 RMS  | 1803   24   11   26   45   51  188      |T   45   56   64   69   59   60    53
 WRMS | 1803   24   10   22   32   51  188      |NE  37   47   54   58   51   42    44
 MEDI | 1622   18   11   20   32   27  195      |MD  41   58   62   69   55   67    53




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