[IGSREPORT-18601] Wk 1582 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu May 20 05:49:13 PDT 2010


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IGS Electronic Report   20 May 05:49:25 PDT 2010      Message Number 18601
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Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1582   (May 02, 2010 - May 08, 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 2.1582.
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:                   
                                                                               
 igl1582[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1582 in the SP3 format.
 igl15827.sum      Combination Report for GPS Week 1582.


    
    
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  |    373.7 ns
                1  |    398.1 ns
                2  |    469.1 ns
                3  |    459.6 ns
                4  |    466.0 ns
                5  |    462.6 ns
                6  |    464.1 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   | R06

    
         
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 1.1582, 1a.1582).
        
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 2.1582.0-6)                                                                                
    
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 3.1582.0-6). 
        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 1582 summary.                      (May 02, 2010 - May 08, 2010)

Table 1.1582.a     GPS week : 1582   MJD: 55318.0-55324.0

         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  124|    0     0    -5     7     0     5  -.14   32   32 |       0       4   1742   1814
        |    1     1     3    21    38   137   .04           |       0     125
cod  247|   -1     0     8    49   -27     0  -.15   18   16 |     ---     ---    ---    ---
        |    1     1     3    18    25    35   .03           |     ---     ---
esx  145|    0     0     7   -54    77    45   .43   28   26 |  101468    1826   3972   8230
        |    1     1     7    27    23    72   .03           |   46780    5447
gfz  198|    0    -1    14   -55   -40    89  -.14   31   31 |  275745     -30   3969   8255
        |    1     2     3    40    83    63   .07           |   39001    5363
iac  n/a|    1     0   -18   -38   -18   -68  -.08   35   35 |  442130    -254   3989   8767
        |    1     0     7    28    20    74   .04           |   39340    2281
mcc  n/a|    7     0    23  -102   -68    70   .70  196  196 |     ---     ---    ---    ---
        |   10    13    36   203   106   472   .63           |     ---     ---


Table 1.1582.b     GPS week : 1582   MJD: 55318.0-55324.0   

         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  |   10   15   13   16   11   11   13 |
 R02  |    9   14   13   11   12    9   14 |
 R03  |   18   19   12    8    9   11    9 |
 R04  |   13   11   13    9   11    8   11 |
 R05  |   13   15   12    9   12   11   12 |
 R06  |   78   36   42   33   33   60   95 |
 R07  |    9   12   11   12   12   16    9 |
 R08  |   11   10   12   11    8   12   12 |
 R10  |   36   29   20   22   17   18   19 |
 R11  |   30   29   28   21   24   29   33 |
 R13  |   28   28   22   14   14   15   19 |
 R14  |   25   20   17   20   17   20   13 |
 R15  |   23   20   16   18   23   18   19 |
 R17  |   17   18   12   18   16   17   18 |
 R18  |   14   14   12   14   13   15   11 |
 R19  |   18   16   11   11   13   15   10 |
 R20  |   12   14   15   15   14   15   17 |
 R21  |   20   17   12   15   13   10   16 |
 R22  |   12   20   19   15   14   14   14 |
 R23  |   18   13   11   11   13   14   14 |
 R24  |   13   19   10   10   15   10   14 |


Table 1.1582.c     GPS week : 1582   MJD: 55318.0-55324.0   

         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 1582 0   |  147   105    72    -477      61   -7708  85.5  1997  1997 |  373735       0
brd 1582 1   | -135   -44   115    -785   -1621  -11780  84.9  2100  2100 |  398071       0
brd 1582 2   | -109    72   158   -1931   -2971  -10470  84.1  2107  2107 |  469102       0
brd 1582 3   |  -34   -27   264    -587   -4729   -6464  88.9  2170  2170 |  459637       0
brd 1582 4   |  -66   -24   244   -2096   -5018   -3460  87.2  1825  1825 |  465997       0
brd 1582 5   |  -69    93   274   -2918   -2352   -5653  88.2  1958  1958 |  462645       0
brd 1582 6   | -105   -74   206   -2571   -4481   -9376  90.0  2148  2148 |  464095       0
-------------+------------------------------------------------------------+----------------
brd 1582 mean|  -53    14   190   -1623   -3015   -7844  87.0  2043  2043 |  441897       0
brd 1582 sdev|   94    73    77     998    1868    2906   2.2   123   123 |   38999       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 2.1582.0  GPS week: 1582   Day: 0   MJD: 55318                            

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  124|   -1    -1    -1   -12   -11   -64  -.16   40   36 |       0      -7   1741   1795
cod  247|   -1     0    15    66   -29     6  -.13   20   17 |     ---     ---    ---    ---
esx  145|    1     1    -2   -58   105   111   .44   32   30 |   21855    -612   3903   8272
gfz  198|   -1     2    12   -75   -39   160  -.16   32   32 |  210716   -2091   3887   8369
iac  n/a|    0     0   -24   -65   -14  -106  -.14   43   43 |  372853     233   3950   8810
mcc  n/a|    6   -15    48  -180   -85  -137  1.55   78   78 |     ---     ---    ---    ---

Table 2.1582.1  GPS week: 1582   Day: 1   MJD: 55319                            

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  124|   -1     1    -4    14    10   -21  -.13   36   37 |       0     165   1690   1764
cod  247|   -2     0    12    25   -43    31  -.11   21   17 |     ---     ---    ---    ---
esx  145|    0     0     1   -55   103    90   .41   32   30 |   48038    6877   3715   8021
gfz  198|   -1    -2    18   -98    42   178  -.06   35   35 |  228467    5666   3712   7595
iac  n/a|    2     0   -15    -2   -51  -177  -.10   41   41 |  398580     518   3728   8252
mcc  n/a|   25     3    50  -429    33   106  1.01   74   74 |     ---     ---    ---    ---

Table 2.1582.2  GPS week: 1582   Day: 2   MJD: 55320                            

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  124|    0     3    -5    -8    -6   116  -.16   33   33 |       0      -9   1871   1947
cod  247|    0     0     5    61   -14   -44  -.09   16   13 |     ---     ---    ---    ---
esx  145|   -1    -2    11   -98    81   -37   .42   27   25 |  129067    6720   4355   6360
gfz  198|    1    -3    19   -37   -15    27  -.18   28   28 |  304873      77   4335   6623
iac  n/a|    1     1   -20     6   -10   -10  -.06   33   33 |  469760   -3320   4374   7086
mcc  n/a|    8    27    74  -280  -179   324  1.47   58   58 |     ---     ---    ---    ---

Table 2.1582.3  GPS week: 1582   Day: 3   MJD: 55321                            

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  124|    1     0    -5     4    26  -216  -.18   31   29 |       0     156   2019   2086
cod  247|    0     0     7    65   -47    23  -.16   15   13 |     ---     ---    ---    ---
esx  145|    0     0    15   -74    49   148   .47   26   24 |  127692    1451   3827   7041
gfz  198|    1    -1    18   -11   -51    83  -.17   30   30 |  293213    -684   3841   7346
iac  n/a|    2     0   -25   -41   -22   -21  -.08   31   31 |  460644    1441   3840   7679
mcc  n/a|  -11    -5   -33   -50    79  -836   .28  650  650 |     ---     ---    ---    ---

Table 2.1582.4  GPS week: 1582   Day: 4   MJD: 55322                            

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  124|   -2     0    -3    40    48   127  -.19   26   26 |       0    -176   1550   1652
cod  247|   -2    -1     9    29   -45   -36  -.19   20   16 |     ---     ---    ---    ---
esx  145|    0     0     3   -19    49    35   .46   24   22 |  139428   -7829   3842   9421
gfz  198|    2     1    12     3    59   111  -.09   29   29 |  303260   -8647   3843   9642
iac  n/a|    2     1   -15   -64    14   -87  -.04   29   29 |  464878   -2181   3847   9985
mcc  n/a|    8    -5     7   115   -85    45   .26  215  215 |     ---     ---    ---    ---

Table 2.1582.5  GPS week: 1582   Day: 5   MJD: 55323                            

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  124|   -1     0   -10    28     0   166  -.13   32   32 |       0      10   1513   1583
cod  247|    0     0     4    31   -40   -28  -.16   17   18 |     ---     ---    ---    ---
esx  145|    1     1     9   -51    87    -1   .45   27   25 |  112199    6702   4372   9284
gfz  198|   -2    -4    10   -91   -92    13  -.08   31   31 |  291492    7525   4375   8516
iac  n/a|    0     2    -5   -45   -14  -117  -.09   31   31 |  463276    3249   4343   9509
mcc  n/a|   11    -2     8   110   -29   352   .21  162  162 |     ---     ---    ---    ---

Table 2.1582.6  GPS week: 1582   Day: 6   MJD: 55324                            

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  124|    1    -1    -8   -14   -73   -69  -.06   29   30 |       0    -106   1816   1877
cod  247|   -3     2     7    62    24    42  -.17   18   18 |     ---     ---    ---    ---
esx  145|    1     0    17   -20    68   -25   .38   26   23 |  131999    -525   3794   9211
gfz  198|   -2    -1    10   -78  -185    53  -.24   28   28 |  298196   -2058   3793   9696
iac  n/a|    3     0   -25   -54   -33    40  -.02   36   36 |  464920   -1719   3845  10053
mcc  n/a|    7    -9    11    -5  -215   640   .12  137  137 |     ---     ---    ---    ---

       
       
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 3.1582.0  GPS week: 1582   Day: 0   MJD: 55318                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 2663   23   15   14   13   15  ---    9 |    47   55   47   55   46  ---    47
 R02  | 1244   16   11   19   17   20  ---    9 |    21   23   30   25   31  ---    21
 R03  |  890   39   30   13   25   36  ---   17 |    32   26   25   35   36  ---    21
 R04  |  954   30   17   19   15   23  ---   12 |    23   26   23   26   32  ---    21
 R05  | 1046   29   13   29   20   18  ---   13 |    29   34   32   30   33  ---    29
XR06  | ----  113   53  ---  ---  ---  ---   78 |    66   67  ---  ---  ---  ---    65
 R07  | 2297   11   11   15   28   21  ---    8 |    24   19   26   35   33  ---    20
 R08  | 1732   10   17   21   15   25  ---   11 |    25   19   34   19   33  ---    22
 R10E | 2187   81   37   53   50   85  ---   35 |    58   17   34   25   48  ---    21
 R11E | 1262   67   36   32   41   75  ---   29 |    27   35   40   36   67  ---    31
 R13E | 4320   57   18   46   69   77  ---   27 |    45   45   37   54   74  ---    40
 R14E | 1669   44   19   41   39   72  ---   25 |    33   26   41   35   53  ---    25
 R15E | 1718   51   29   37   40   52   78   23 |    33   36   47   38   43   28    30
 R17  | 3022   43    8   20   43   47  ---   17 |    95   70   74   58   38  ---    67
 R18  | 1843   33   11   18   19   35  ---   13 |    51   41   50   41   52  ---    41
 R19  | 1267   25   18   47   17   30  ---   17 |    35   45   65   56   40  ---    38
 R20  | 2060   29   14   10   31   25  ---   11 |    35   39   38   51   49  ---    34
 R21  |  910   40   16   56   31   19  ---   20 |    65   58   63   51   38  ---    46
 R22  | 1981   29    9   24   34   18  ---   11 |    48   59   61   74   41  ---    52
 R23  | 1891   33   23   38   23   35  ---   18 |    34   41   39   46   38  ---    33
 R24  | 1593   35   12   27   21   18  ---   13 |    35   44   48   52   39  ---    38
------+-----------------------------------------+-------------------------------------
 RMS  | 1997   40   20   32   32   43   78      |T   41   39   42   42   43   28    35
 WRMS | 1997   36   17   30   32   43   78      |NE  41   41   43   43   38  ---    37
 MEDI | 1718   33   17   24   25   25   78      |MD  35   39   39   38   39   28    33

Table 3.1582.1  GPS week: 1582   Day: 1   MJD: 55319                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1486   20   12   30   27   41  ---   15 |    52   57   57   50   67  ---    54
 R02  | 1636   26   17   29   36   23  ---   13 |    15   28   45   38   32  ---    21
 R03  | 1154   26   25   47   27   34  ---   19 |    22   26   47   36   38  ---    23
 R04  | 1731   24   11   20   31   17  ---   10 |    22   14   33   30   23  ---    15
 R05  | 1104   15   19   41   28   19  ---   14 |    29   29   43   26   35  ---    23
XR06  | ----   45   29  ---  ---  ---  ---   36 |    72   73  ---  ---  ---  ---    73
 R07  | 2711   21   11   26   32   22  ---   11 |    21   18   31   28   29  ---    15
 R08  | 1077   13   11   23   17   20  ---    9 |    17   15   31   22   27  ---    14
 R10E | 1473   48   39   45   44   74  ---   29 |    55   22   37   30   38  ---    25
 R11E | 1175   65   43   25   59   66  ---   29 |    32   31   46   47   59  ---    32
 R13E | 5071   71   24   32   31   67  ---   28 |    41   49   60   52   80  ---    46
 R14E | 2687   40   21   23   32   56  ---   20 |    23   36   39   41   54  ---    28
 R15E | 2124   25   19   38   42   53   74   19 |    32   34   60   52   43   30    34
 R17  | 2052   28   18   34   28   47  ---   18 |    54   43   57   52   26  ---    37
 R18  | 2629   29   21   24   39   20  ---   13 |    70   36   62   38   42  ---    48
 R19  | 1992   36   11   33   50   32  ---   16 |    32   43   65   67   37  ---    39
 R20  | 2467   27   17   32   36   20  ---   14 |    32   34   38   50   24  ---    23
 R21  | 1012   39   17   21   33   42  ---   17 |    43   38   48   58   26  ---    32
 R22  | 1234   39   24   38   32   35  ---   19 |    38   40   40   48   34  ---    28
 R23  | 1877   27   10   15   27   38  ---   13 |    29   36   27   41   56  ---    30
 R24  |  969   46   21   38   24   20  ---   18 |    27   37   35   36   25  ---    19
------+-----------------------------------------+-------------------------------------
 RMS  | 2099   36   21   32   35   41   74      |T   36   35   45   42   39   30    31
 WRMS | 2099   37   17   30   35   41   74      |NE  35   35   43   41   34  ---    30
 MEDI | 1636   28   19   30   32   34   74      |MD  32   36   43   41   35   30    28

Table 3.1582.2  GPS week: 1582   Day: 2   MJD: 55320                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1029   17   20   15   19   37  ---   13 |    40   51   65   62   53  ---    48
 R02  | 1195   22   17   34   33   17  ---   13 |    16   22   30   27   29  ---    18
 R03  | 1385   27   10   29   28   13  ---   11 |    26   34   32   29   42  ---    26
 R04  | 2676   19   17   25   20   28  ---   12 |    19   19   36   31   27  ---    17
 R05  | 1252   19   12   32   15   17  ---   11 |    30   20   47   21   22  ---    20
XR06  | 4415   59   29  ---  ---  ---  ---   41 |    70   80  ---  ---  ---  ---    63
 R07  | 2490   18   10   27   36   18  ---   10 |    27   21   42   35   29  ---    19
 R08  | 1753   22   11   25   24   25  ---   11 |    20   20   31   30   27  ---    15
 R10E | 1548   59   20   23   21   37  ---   20 |    35   20   30   16   51  ---    17
 R11E | 1589   76   29   44   25   47  ---   27 |    26   31   54   44   46  ---    30
 R13E | 2414   40   26   23   32   64  ---   22 |    39   60   65   64   70  ---    50
 R14E | 3546   41   14   18   40   48  ---   17 |    21   21   24   35   55  ---    17
 R15E | 2009   31   14   26   29   44   58   16 |    20   40   33   32   56   41    28
 R17  | 1392   21   18   22   26   21  ---   11 |    35   51   40   35   46  ---    41
 R18  | 2398   35   10   18   39   16  ---   11 |    54   38   50   35   46  ---    44
 R19  | 2540   15   11   21   29   30  ---   11 |    43   33   50   57   42  ---    38
 R20  | 4294   32   12   43   35   15  ---   15 |    27   41   76   73   35  ---    41
 R21  | 1305   22   16   20   38   29  ---   12 |    50   52   43   53   35  ---    45
 R22  |  740   34   20   24   17   51  ---   18 |    35   56   65   48   27  ---    44
 R23  | 1164   10    8   29   22   26  ---   11 |    21   23   32   42   35  ---    20
 R24  | 1677   16    8   15   18   30  ---   10 |    31   30   29   27   41  ---    29
------+-----------------------------------------+-------------------------------------
 RMS  | 2107   33   16   27   28   33   58      |T   32   36   43   39   40   41    31
 WRMS | 2107   33   13   25   28   33   58      |NE  34   36   44   40   35  ---    33
 MEDI | 1677   22   14   24   26   28   58      |MD  30   33   40   35   41   41    29

Table 3.1582.3  GPS week: 1582   Day: 3   MJD: 55321                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1107   39   15   29   32   30  ---   16 |    60   88  106  101   94  ---    85
 R02  | 1157   17   16   20   22   22  ---   10 |    20   30   27   24   26  ---    18
 R03  | 1321   13    9   17   23   19  ---    8 |    19   21   24   17   26  ---    18
 R04  | 3267   11    6   20   18   24  ---    9 |    22   21   30   21   28  ---    18
 R05  | 3080   15   12   15   14   22  ---    9 |    23   24   34   29   26  ---    17
XR06  | 2551   61   43  ---  ---   34  ---   33 |    81  145  ---  ---   50  ---   114
 R07  | 1201   18   11   27   19   28  ---   11 |    31   30   44   28   30  ---    26
 R08  | 2253   20   14   20   22   24  192   11 |    28   26   28   21   25  171    20
 R10E |  876   48   28   34   20   44  ---   21 |    37   19   34   33   40  ---    20
 R11E | 2511   57   17   32   46   41  ---   21 |    39   28   39   53   48  ---    29
 R13E | 1975   22   15   17   46   39  ---   13 |    45   43   43   43   42  ---    38
 R14E | 3156   40   18   33   29   49  ---   19 |    29   38   56   32   58  ---    35
 R15E | 2111   29   17   28   43   49   98   17 |    22   35   38   30   54   38    27
 R17  | 1729   44   22   33   44   28  ---   18 |    46   55   81   81   51  ---    51
 R18  | 1293   41   16   21   29   17  ---   14 |    31   46   41   35   34  ---    36
 R19  | 2402   16   11   22   21   27  ---   10 |    36   60   68   65   43  ---    51
 R20  | 3796   36   10   22   26   36  ---   15 |    33   30   46   39   44  ---    31
 R21  | 1782   35   13   35   24   19  ---   14 |    49   52   69   56   46  ---    50
 R22  | 1933   25   17   38   26   27  ---   15 |    63   68   63   63   65  ---    62
 R23  |  842   14   10   27   43   24 1106   11 |    28   26   32   40   26  994    20
 R24  | 2305   11   17   18   23   22  ---   10 |    40   38   38   52   20  ---    29
------+-----------------------------------------+-------------------------------------
 RMS  | 2170   31   15   26   30   31  650      |T   37   43   47   43   41  401    37
 WRMS | 2170   29   13   24   30   31  650      |NE  38   47   48   44   39  582    40
 MEDI | 1975   25   15   22   24   27  192      |MD  33   35   39   35   42  171    29

Table 3.1582.4  GPS week: 1582   Day: 4   MJD: 55322                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1946   20   20   19   22   17  ---   11 |    43   55   36   42   52  ---    43
 R02  | 1335   17   20   17   24   25  ---   11 |    31   33   32   26   31  ---    25
 R03  | 1150   15    7   22   19   15  ---    9 |    20   18   30   29   21  ---    18
 R04  | 1477   16   16   24   17   17  ---   10 |    23   21   37   21   24  ---    21
 R05  | 2840   18   17   27   40   18  ---   11 |    19   27   26   35   20  ---    17
XR06  | 2202   39   42  ---  ---   58  ---   33 |    72  125  ---  ---   58  ---    97
 R07  | 2020   20   15   25   21   18  ---   11 |    28   30   35   29   32  ---    25
 R08  |  920   18   13   10   24   15   80    8 |    19   22   29   30   24   15    19
 R10E | 2212   33   24   21   30   37  ---   16 |    27   27   22   27   42  ---    22
 R11E | 2204   46   28   37   45   53  ---   23 |    42   34   43   46   53  ---    30
 R13E | 1771   22   23   21   38   30  ---   14 |    42   30   35   32   35  ---    27
 R14E | 1810   30   18   27   35   41  ---   17 |    22   33   45   38   47  ---    27
 R15E | 1288   42   30   23   44   57  125   22 |    25   44   36   24   61   25    26
 R17  | 2224   21   26   32   22   25  ---   15 |    35   48   44   47   34  ---    35
 R18  |  741   15   14   26   34   28  ---   12 |    34   32   31   29   50  ---    29
 R19  | 1467   31   14   12   18   26  ---   12 |    22   43   36   45   39  ---    30
 R20  | 1837   26   13   25   34   29  ---   13 |    33   32   42   60   38  ---    33
 R21  | 1482   28   22   21   16   17  ---   13 |    44   55   47   49   55  ---    47
 R22  | 3064   20   14   37   18   19  ---   13 |    56   52   87   70   50  ---    58
 R23  | 1356   20   18   12   15   33  341   12 |    35   30   26   33   45  103    29
 R24  | 1504   29   29   26   28   19  ---   15 |    62   53   75   64   52  ---    56
------+-----------------------------------------+-------------------------------------
 RMS  | 1825   26   20   24   29   29  215      |T   34   40   39   38   41   47    34
 WRMS | 1825   26   16   22   29   29  215      |NE  36   42   40   40   39   59    36
 MEDI | 1771   21   18   23   24   25  125      |MD  33   33   36   33   42   25    29

Table 3.1582.5  GPS week: 1582   Day: 5   MJD: 55323                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 2717   29   16   15   18   14  ---   11 |    56   68   76   72   62  ---    65
 R02  | 1656   19   12   17   30   16  ---    9 |    31   16   28   28   28  ---    20
 R03  | 1809   18   15   17   21   24  ---   10 |    19   20   27   18   25  ---    14
 R04  | 1228   12    8   20   12   16  ---    8 |    14   16   26   16   20  ---    12
 R05  | 1247   17   16   21   33   21  ---   10 |    16   31   26   26   20  ---    18
XR06  | 2655   78   81  ---  ---   93  ---   59 |   153  123  ---  ---   90  ---   138
 R07  | 2309   18   31   30   17   27  ---   16 |    15   23   29   30   26  ---    16
 R08  | 1529   20   15   27   32   22   98   12 |    18   21   31   43   20   16    14
 R10E | 2506   33   18   31   32   44  ---   18 |    33   25   32   26   48  ---    21
 R11E | 1376   76   22   47   54   53  ---   28 |    42   18   45   47   56  ---    24
 R13E | 3280   23   22   27   30   30  ---   14 |    46   49   40   36   45  ---    39
 R14E | 1103   36   20   45   31   39  ---   20 |    18   28   64   25   37  ---    23
 R15E | 2226   45   16   30   43   38   99   18 |    25   18   29   39   44   25    15
 R17  | 1938   23   20   24   25   48  ---   17 |    20   33   43   36   23  ---    25
 R18  | 1096   22   13   28   14   39  ---   15 |    22   35   37   48   61  ---    34
 R19  | 1148   37   14   28   27   21  ---   14 |    27   53   58   65   54  ---    45
 R20  | 1888   33   16   15   18   37  ---   15 |    26   27   37   31   50  ---    27
 R21  | 1616   23   11   21   22   17  ---   10 |    48   48   53   43   48  ---    46
 R22  | 2665   33   16   31   33   21  ---   14 |    29   44   62   41   45  ---    41
 R23  | 2251   37   15   27   49   19  243   14 |    30   26   47   61   23   75    22
 R24  | 1676   22   11   17   27   20  ---   10 |    43   43   29   48   49  ---    38
------+-----------------------------------------+-------------------------------------
 RMS  | 1958   32   17   27   30   31  162      |T   34   36   40   38   41   38    33
 WRMS | 1958   32   18   25   30   31  162      |NE  35   39   40   40   40   45    35
 MEDI | 1809   23   16   27   27   24   99      |MD  27   28   37   36   45   25    24

Table 3.1582.6  GPS week: 1582   Day: 6   MJD: 55324                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  iac  mcc  IGL |   bkg  cod  esx  gfz  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1726   17   24   17   15   33  ---   13 |    77   81   85   76   94  ---    82
 R02  | 1668   17   26   26   28   21  ---   13 |    27   21   31   41   26  ---    21
 R03  | 3302   13   12   14   22   20  ---    8 |    21   16   21   24   23  ---    15
 R04  | 1552   15   16   21   20   21  ---   10 |    26   24   38   32   29  ---    25
 R05  | 1298   23   13   22   24   25  ---   12 |    26   24   29   25   27  ---    23
XR06  |11541  400   36  ---  ---  158  ---   95 |   157  390  ---  ---   84  ---   395
 R07  | 1553   14    9   16   32   21  ---    8 |    25   23   26   29   25  ---    20
 R08  | 2883   26   11   24   23   20  115   11 |    25   22   36   27   25   24    20
 R10E | 2031   37   14   26   27   53  ---   18 |    34   33   54   42   51  ---    30
 R11E | 1125   79   20   66   56   57  ---   33 |    35   32   46   58   54  ---    29
 R13E | 4996   26   24   31   20   55  ---   19 |    52   51   46   39   46  ---    41
 R14E | 1786   20   17   17   30   37  ---   12 |    30   39   37   41   32  ---    29
 R15E | 2149   39   33   19   44   37   94   19 |    21   23   29   45   40   27    18
 R17  | 1303   36   11   20   26   52  ---   17 |    64   66   66   59   37  ---    56
 R18  | 1742   17   13   14   19   32  ---   11 |    46   52   58   49   56  ---    50
 R19  | 1687   10   14   14   21   28  ---    9 |    45   60   63   64   50  ---    53
 R20  | 2822   20   22   16   15   54  ---   16 |    39   40   63   51   67  ---    48
 R21  |  844   30   18   31   18   34  ---   16 |    50   58   76   60   42  ---    53
 R22  | 1069   32   20   20   17   23  ---   14 |    45   63   65   59   42  ---    52
 R23  | 2087   20   14   31   35   29  184   13 |    28   33   50   47   36  102    31
 R24  |  921   13   17   33   35   26  ---   13 |    43   51   77   73   42  ---    51
------+-----------------------------------------+-------------------------------------
 RMS  | 2147   29   18   26   28   36  137      |T   43   57   49   47   44   51    54
 WRMS | 2147   30   18   23   28   36  137      |NE  46   64   52   47   44   63    62
 MEDI | 1726   20   17   20   23   32  115      |MD  35   39   46   45   42   27    31



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