[IGSREPORT-20029] Wk 1646 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Aug 11 05:17:15 PDT 2011


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1646   (Jul 24, 2011 - Jul 30, 2011) 
                                                                               
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
center's 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 2.1646.
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:
                                                                               
 igl1646[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1646 in the SP3 format.
 igl16467.sum      Combination Report for GPS Week 1646.


    
    
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. The grg orbits are introduced for the first time
    starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
    22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
    21-May 2011 (GPS Week 1636).

 3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
    BKG, ESA, and CODE referred their GLONASS orbit products to the following
    satellite antenna offset (SAO) values (expressed in the spacecraft body
    frame):
    
      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.
    
    Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
    (GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
    (IGSMAIL #5438). The antenna phase center offsets and phase center variations
    are given in the file:
        ftp://igs.org/igscb/station/general/igs05.atx
    These antenna calibrations are also used in the homogeneously reprocessed IGS
    products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
    Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
    model is updated (IGSMAIL #6255 & #6374) as given in the file:
        ftp://igs.org/igscb/station/general/igs08.atx
    

 4. The satellite clock values in the combined orbit files are taken from the
    broadcast files. The following gps/glonass time offsets were added to the
    broadcast clocks. Before GPS Week 1637, the time offsets were derived
    from the bkg summary files; starting Week 1637 the offsets are derived
    from the gfz summary files.
    
               Day | applied clock offset
               ----+---------------------
                0  |    168.4 ns
                1  |    174.5 ns
                2  |    168.8 ns
                3  |    172.8 ns
                4  |    171.2 ns
                5  |    170.6 ns
                6  |    169.9 ns

 5. The following orbit solutions were excluded from the combination
    because they were biasing the weighted average (generally indicated
    by long arc RMS).
    
               Day | Centre | PRN list
               ----+--------+---------------
                0  |  GRG   | R04
                0  |  IAC   | R04
                1  |  ESX   | R06
                1  |  IAC   | R04
                2  |  GRG   | R04
                2  |  IAC   | R04
                3  |  GRG   | R04
                3  |  IAC   | R04
                4  |  IAC   | R04
                5  |  GRG   | R04
                5  |  IAC   | R04
                6  |  IAC   | R04

    
         
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 1.1646, 1a.1646).
        
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 2.1646.0-6)                                                                                
    
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 3.1646.0-6). 
        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 1646 summary.                      (Jul 24, 2011 - Jul 30, 2011)

Table 1.1646.a     GPS week : 1646   MJD: 55766.0-55772.0

         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]
--------+----------------------------------------------------+------------------------------
cod  253|    0     2     5    38    -1     8  -.09   28   26 |     ---     ---    ---    ---
        |    2     1     4    44    37    27   .02           |     ---     ---
esx  124|    0    -1     5   -22    21   -45   .44   29   20 | 1268275   -1509   5098 147246
        |    1     1     2    30    47    34   .04           | 2903040    3757
gfz  197|    0     0     3   -38   -43    19  -.20   22   20 |       0    -726   5177   8734
        |    1     1     2    79    61    33   .04           |       0    3784
grg  131|    0     0     5    18    14    73   .01   44   42 |     ---     ---    ---    ---
        |    3     2     5    33    39    44   .10           |     ---     ---
iac  n/a|    1     0   -17    36    16    -9  -.23   25   25 |  171992    -970   5092   8544
        |    1     1     7    29    26    66   .05           |    1864    1694
mcc  n/a|    3     7    53    29    24  -226  -.16  113  113 |     ---     ---    ---    ---
        |    4     4    23    75   134   417   .50           |     ---     ---


Table 1.1646.b     GPS week : 1646   MJD: 55766.0-55772.0   

         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   11   11   12    9   15   11 |
 R02  |   12   12   11   12   12    9    9 |
 R03  |   10   12   12   10   11   11    9 |
 R04  |   27   51   70   33   28  161   61 |
 R05  |   14   12   13   13   11   13   16 |
 R06  |   11   17   13   14   13   11   12 |
 R07  |   12   11   10   14   13   12   13 |
 R08  |   10   11   10   11   12   10    9 |
 R09  |   16   11   13   14   21   15   11 |
 R10  |   10   14   11   10   10   15   11 |
 R11  |   18   16   19   18   23   19   19 |
 R12  |   11   11   10   11   11   11   11 |
 R13  |   12   13   13   14   12   10   12 |
 R15  |   10   12   12   11   11   12   11 |
 R16  |   11   11   12   12   17   12   11 |
 R17  |   16   19   17   15   19   24   29 |
 R18  |   12   12   11   12   11   10   22 |
 R19  |   13   12   10   13   13   11   16 |
 R20  |   21   15   12   16   16   17   21 |
 R21  |   12   15   10   10   10   13   23 |
 R22  |   10   13   13   10   13   13   14 |
 R23  |   11   10   13   12   12   12   13 |
 R24  |   12   11   10   12   14   13   13 |


Table 1.1646.c     GPS week : 1646   MJD: 55766.0-55772.0   

         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 1646 0   |    8   -10   383     994    -179  -11810  85.2  2015  2015 |  168412       0
brd 1646 1   |    4   -10   336    1810    1884   -1168  84.2  2268  2268 |  174547       0
brd 1646 2   |  -59    96   351    1407    3210   -7052  84.3  2273  2273 |  168777       0
brd 1646 3   |  -37    17   245    2454    -129   -4768  87.3  2111  2111 |  172770       0
brd 1646 4   |    6  -109   372    2362     548   -9447  85.1  2226  2226 |  171200       0
brd 1646 5   |    2    50   183    2447   -1947    2434  84.0  2250  2250 |  170624       0
brd 1646 6   |   97   -61   280     955     -36   -8637  83.8  2103  2103 |  169919       0
-------------+------------------------------------------------------------+----------------
brd 1646 mean|    3    -3   307    1775     478   -5778  84.8  2178  2178 |  170892       0
brd 1646 sdev|   49    68    73     667    1652    4989   1.2   101   101 |    2184       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 2.1646.0  GPS week: 1646   Day: 0   MJD: 55766                            

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]
--------+----------------------------------------------------+------------------------------
cod  253|    2     0     9    47   -36    12  -.09   27   26 |     ---     ---    ---    ---
esx  124|   -1    -2     2   -16    26   -55   .44   21   21 |  170587   -4829   5525   5612
gfz  197|    0     0     2   -72     0    13  -.21   22   16 |       0   -3628   5638   9179
grg  131|   -2     1     8    30   -16    19   .02   35   34 |     ---     ---    ---    ---
iac  n/a|    1    -2   -19    55    16    59  -.18   24   24 |  169411    -723   5516   8851
mcc  n/a|    9     6    21   133   -34  -878  -.59  115  115 |     ---     ---    ---    ---

Table 2.1646.1  GPS week: 1646   Day: 1   MJD: 55767                            

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]
--------+----------------------------------------------------+------------------------------
cod  253|    0     3     3    67    25   -43  -.09   27   24 |     ---     ---    ---    ---
esx  124|    0     0     5   -15    49   -14   .48   75   26 | 7851752    2687   5748 999999
gfz  197|    0    -1     1  -103  -140    73  -.21   24   23 |       0    5939   5833  10893
grg  131|    0    -2    -1    21    81    80  -.14   39   39 |     ---     ---    ---    ---
iac  n/a|    1     1    -8    34    -2   -85  -.26   22   22 |  174978      49   5734  10279
mcc  n/a|    2     7    50   106   -40  -669 -1.00  110  110 |     ---     ---    ---    ---

Table 2.1646.2  GPS week: 1646   Day: 2   MJD: 55768                            

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]
--------+----------------------------------------------------+------------------------------
cod  253|   -1     2     7    77    19    36  -.10   29   27 |     ---     ---    ---    ---
esx  124|    0    -1     3    33   -19   -96   .44   21   19 |  172707   -8252   4900   5138
gfz  197|    2     0     1  -133   -53   -10  -.12   20   18 |       0   -5850   4868   7542
grg  131|    0     0     0     8    26    79   .05   44   40 |     ---     ---    ---    ---
iac  n/a|    0     0    -6    61    53    51  -.22   18   18 |  172402   -4392   4839   7725
mcc  n/a|   -1     6    31   -68    13     3  -.20   84   84 |     ---     ---    ---    ---

Table 2.1646.3  GPS week: 1646   Day: 3   MJD: 55769                            

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]
--------+----------------------------------------------------+------------------------------
cod  253|   -2     3     5    74   -60    34  -.10   26   24 |     ---     ---    ---    ---
esx  124|    0     0     7   -35   -43   -32   .37   20   19 |  172969    -919   4837   5009
gfz  197|    0    -2     8   -87    15     0  -.22   20   18 |       0    1765   4931   7830
grg  131|    2    -4     3    60   -27    48   .02   45   44 |     ---     ---    ---    ---
iac  n/a|    2     0   -21    48    46    47  -.25   23   23 |  172572     323   4828   7763
mcc  n/a|    5     8    45    -9   -60   247   .04   88   88 |     ---     ---    ---    ---

Table 2.1646.4  GPS week: 1646   Day: 4   MJD: 55770                            

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]
--------+----------------------------------------------------+------------------------------
cod  253|    0     2    10   -34    14    13  -.10   28   26 |     ---     ---    ---    ---
esx  124|    0    -3     9   -66    19   -81   .46   23   21 |  170891      -7   5984   6071
gfz  197|   -3    -1     5    70     7   -20  -.21   26   25 |       0    -805   6118   7707
grg  131|    4     1     9    44   -23   153   .14   43   40 |     ---     ---    ---    ---
iac  n/a|    0    -1   -28    24    -4     5  -.22   24   24 |  173116   -1967   5978   7819
mcc  n/a|    4    11    75    72   -60    97   .11  117  117 |     ---     ---    ---    ---

Table 2.1646.5  GPS week: 1646   Day: 5   MJD: 55771                            

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]
--------+----------------------------------------------------+------------------------------
cod  253|   -2     0     0   -13    43    17  -.08   30   26 |     ---     ---    ---    ---
esx  124|    1     0     8   -33   103    -1   .45   20   19 |  170328    -299   4867   4943
gfz  197|    0     0     4    47  -114    39  -.23   19   22 |       0   -1447   4965   9112
grg  131|    2     4    12     8    43    40   .06   48   42 |     ---     ---    ---    ---
iac  n/a|    0     0   -18   -23   -15   -54  -.16   24   24 |  171139    -162   4895   8732
mcc  n/a|   -2     0    86   -38    34   -51   .02  137  137 |     ---     ---    ---    ---

Table 2.1646.6  GPS week: 1646   Day: 6   MJD: 55772                            

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]
--------+----------------------------------------------------+------------------------------
cod  253|    2     4     0    49   -15    -7  -.04   33   29 |     ---     ---    ---    ---
esx  124|    1     0     6   -22    16   -34   .40   20   18 |  168692    1053   3829   3950
gfz  197|   -1     0     4     8   -21    43  -.18   21   21 |       0   -1061   3889   8881
grg  131|   -6    -2     5   -42    14    94  -.09   54   56 |     ---     ---    ---    ---
iac  n/a|    3    -1   -21    58    22   -93  -.30   38   38 |  170326      79   3858   8641
mcc  n/a|    4    13    64    14   319  -332   .51  139  139 |     ---     ---    ---    ---

       
       
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 3.1646.0  GPS week: 1646   Day: 0   MJD: 55766                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1561   16   16   12   27   26  ---    9 |    38   40   45   30   41  ---    37
 R02  | 1236   31   20   12   39   18  ---   12 |    41   33   24   36   31  ---    26
 R03  | 2358   15   20   19   30   13  ---    9 |    24   22   22   24   22  ---    17
XR04  | 2419   30   24  ---  208  318  ---   27 |    34   58  ---   88  229  ---    39
 R05  | 1012   37   25   14   42   20  ---   13 |    59   29   35   34   28  ---    30
 R06  | 1824   31   19   11   25   17  ---   10 |    45   75   29   20   28  ---    28
 R07  | 3669   31   20   21   23   20  ---   11 |    41   28   34   25   26  ---    26
 R08  | 1571   17   16   16   34   14  142    9 |    26   29   31   37   26   37    24
 R09  |  939   29   32   44   23   21  ---   16 |    29   29   42   27   25  ---    24
 R10  |  950   13   16   22   31   20  ---   10 |    19   24   36   31   18  ---    20
 R11  | 1324   56   18   31   41   25   86   17 |    33   46   47   29   31   19    28
 R12  | 1458   34   12   22   26   17  ---   11 |    23   22   21   22   23  ---    15
 R13  | 1038   29   29   13   23   18  ---   11 |    29   34   29   22   24  ---    21
 R15  | 4357   21   18   17   17   25  109   10 |    24   32   24   35   20   22    22
 R16  | 2774   32   16   19   30   14  ---   11 |    44   42   39   42   44  ---    38
 R17  | 3336   33   26   20   43   39  ---   16 |    71   89   92   72  118  ---    89
 R18  | 1286   20   20   23   34   19  ---   11 |    40   31   33   42   39  ---    32
 R19  |  973   14   21   19   46   30  ---   13 |    40   29   28   57   39  ---    31
 R20  | 1607   19   32   41   64   46  ---   20 |    51   50   50   43   61  ---    42
 R21  | 1004   25   23   14   33   21  ---   11 |    38   29   33   41   47  ---    31
 R22  | 1100   20   16   15   30   23  ---   10 |    43   30   34   60   41  ---    36
 R23  | 1840   22   16   15   39   20  ---   11 |    51   37   42   58   61  ---    46
 R24  | 2048   20   23   15   31   27  ---   11 |    53   34   34   48   53  ---    40
------+-----------------------------------------+-------------------------------------
 RMS  | 2015   27   21   22   35   24  115      |T   38   37   36   40   46   26    32
 WRMS | 2015   26   21   16   34   24  115      |NE  36   34   33   33   31   26    27
 MEDI | 1561   25   20   17   31   20  109      |MD  40   32   34   36   31   22    30

Table 3.1646.1  GPS week: 1646   Day: 1   MJD: 55767                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1320   14   17   14   47   12  ---   10 |    24   32   34   33   29  ---    25
 R02  | 1064   27   23   15   33   24  ---   12 |    33   38   29   32   16  ---    23
 R03  | 1745   29   21   26   31   18  ---   12 |    18   36   36   30   26  ---    23
XR04  | 3332   71   55  ---  103  309  ---   51 |    30  122  ---  102  149  ---    78
 R05  |  964   32   17   22   34   21  ---   12 |    46   50   46   49   27  ---    39
 R06  |  811   29  342   29   46   15  ---   16 |    34  197   32   35   26  ---    23
 R07  | 3110   23   24   17   24   22  ---   11 |    32   30   30   32   35  ---    25
 R08  |  780   15   21   13   30   28  133   11 |    24   36   27   32   31   51    22
 R09  | 1253   25   13   19   38   15  ---   10 |    22   25   28   41   20  ---    20
 R10  | 1205   18   20   41   36   18  ---   13 |    18   36   55   33   28  ---    26
 R11  | 1290   38   25   32   33   28  110   15 |    33   39   43   52   25   21    26
 R12  | 2226   23   10   27   38   15  ---   11 |    27   28   27   40   17  ---    21
 R13  |  873   30   12   28   41   25  ---   13 |    22   27   23   38   20  ---    18
 R15  | 6254   15   15   36   31   14   79   11 |    23   33   31   37   19   32    22
 R16  | 2127   29   17   17   37   11  ---   10 |    39   38   33   39   36  ---    32
 R17  | 2547   55   21   28   40   40  ---   18 |    54   82   84   70   89  ---    73
 R18  | 4104   23   14   23   44   15  ---   11 |    42   38   39   44   40  ---    36
 R19  | 1080   19   14   20   45   20  ---   11 |    30   29   33   42   33  ---    26
 R20  | 2277   29   27   22   30   35  ---   14 |    38   46   40   58   53  ---    39
 R21  | 1948   26   22   21   60   21  ---   14 |    29   32   35   40   28  ---    24
 R22  |  917   27   23   11   42   26  ---   12 |    35   31   37   44   28  ---    27
 R23  | 2352   17   21   17   26   20  ---   10 |    39   24   40   38   44  ---    33
 R24  | 1209   17   13   16   43   22  ---   10 |    38   39   36   53   38  ---    35
------+-----------------------------------------+-------------------------------------
 RMS  | 2268   27   75   24   39   22  110      |T   31   47   37   44   37   34    31
 WRMS | 2268   24   26   23   39   22  110      |NE  30   45   34   40   29   34    27
 MEDI | 1320   26   21   21   38   21  110      |MD  32   36   34   40   28   32    26

Table 3.1646.2  GPS week: 1646   Day: 2   MJD: 55768                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  998   16   20   11   57   14  ---   11 |    27   28   31   29   41  ---    27
 R02  | 1004   30   20   12   39   12  ---   10 |    33   24   29   32   29  ---    21
 R03  | 1940   25   13   22   48   17  ---   11 |    28   27   26   49   21  ---    20
XR04  | 2058   81   60  ---  191  334  ---   69 |    41  120  ---  106  184  ---    72
 R05  | 1190   50   24   10   27   11  ---   12 |    48   35   37   38   27  ---    28
 R06  | 1302   27   17   23   57   15  ---   12 |    41  127   27   26   32  ---    25
 R07  | 4720   27   10   15   35   20  ---   10 |    43   32   32   40   22  ---    27
 R08  |  993   18   17   14   45   11   82    9 |    37   24   35   28   31   47    26
 R09  |  853   33   29   12   37   25  ---   13 |    22   47   34   34   28  ---    26
 R10  | 1224   15   13   20   47   18  ---   10 |    20   22   33   41   26  ---    19
 R11  | 1296   50   34   36   61   15  100   18 |    32   50   44   29   25   25    27
 R12  | 1902   17   17   21   35   15  ---   10 |    28   28   45   45   26  ---    29
 R13  | 1169   32   16   21   50   15  ---   12 |    30   27   28   43   20  ---    21
 R15  | 5651   20   18   26   41   16   67   11 |    25   34   28   41   23   13    24
 R16  | 1703   33   26   16   32   16  ---   11 |    31   42   31   29   33  ---    27
 R17  | 3394   44   27   29   42   33  ---   17 |    61   78   68   60   96  ---    72
 R18  | 2943   25   13   20   52   14  ---   11 |    36   35   25   48   26  ---    26
 R19  | 1438   19   15   19   42   13  ---   10 |    39   29   32   54   31  ---    29
 R20  | 1299   27   26   23   31   21  ---   12 |    41   41   35   45   42  ---    32
 R21  | 1916   24   19   14   24   20  ---   10 |    32   27   35   37   38  ---    28
 R22  |  769   28   16   20   51   20  ---   12 |    40   41   44   73   43  ---    40
 R23  | 2794    9   32   15   52   21  ---   12 |    43   45   38   54   58  ---    41
 R24  | 1334   18   15   17   32   19  ---    9 |    36   31   36   56   42  ---    33
------+-----------------------------------------+-------------------------------------
 RMS  | 2273   29   21   20   44   18   84      |T   35   43   35   45   41   28    31
 WRMS | 2273   27   19   18   40   18   84      |NE  33   39   33   40   28   28    26
 MEDI | 1334   27   18   19   42   16   82      |MD  36   34   33   41   31   25    27

Table 3.1646.3  GPS week: 1646   Day: 3   MJD: 55769                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  716   19   27   14   49   17  ---   12 |    40   56   51   56   31  ---    42
 R02  |  829   27   12   21   51   12  ---   11 |    41   38   22   55   25  ---    29
 R03  | 4697   20   13   16   45   12  ---   10 |    30   21   29   40   20  ---    20
XR04  | 1887   38   27  ---  178  320  ---   32 |    45   91  ---  175  199  ---    63
 R05  | 1193   29   20   24   32   24  ---   12 |    50   28   38   52   34  ---    34
 R06  | 1843   32   31   11   51   19  ---   14 |    38   59   35   37   27  ---    25
 R07  | 5130   25   18   18   61   29  ---   14 |    40   38   33   31   28  ---    25
 R08  | 1310   18   21   16   49   15   60   11 |    31   29   19   42   22   18    19
 R09  |  597   41   19   20   36   21  ---   13 |    31   39   39   43   33  ---    28
 R10  | 1121   14   16   20   34   21  ---   10 |    25   35   34   43   31  ---    27
 R11  | 1107   55   22   26   62   24  111   18 |    37   42   43   36   28   33    24
 R12  | 1416   20   20   11   37   23  ---   10 |    27   38   31   44   20  ---    25
 R13  | 1819   25   18   30   52   17  ---   13 |    41   31   56   50   34  ---    34
 R15  | 2235   16   18   16   44   19   85   10 |    20   25   27   43   23   28    20
 R16  | 1156   28   22   13   43   22  ---   12 |    49   51   49   56   60  ---    47
 R17  | 3407   30   18   16   49   39  ---   14 |    71   83   91   75  101  ---    82
 R18  | 1036   19   17   20   39   25  ---   11 |    55   61   58   50   46  ---    51
 R19  | 1079   23   15   18   63   14  ---   12 |    37   29   29   55   34  ---    30
 R20  | 1681   30   25   36   38   28  ---   15 |    47   47   39   46   46  ---    37
 R21  | 1323   18   17   21   28   20  ---   10 |    35   33   25   41   38  ---    27
 R22  | 1149   15   16   21   30   24  ---   10 |    42   48   50   55   41  ---    42
 R23  | 1877   16   28   18   31   28  ---   12 |    47   39   41   55   50  ---    40
 R24  | 2039   23   19   16   33   27  ---   11 |    46   34   35   55   55  ---    40
------+-----------------------------------------+-------------------------------------
 RMS  | 2111   26   20   20   45   23   88      |T   40   43   39   53   44   26    35
 WRMS | 2111   24   19   18   44   23   88      |NE  37   37   37   45   33   26    30
 MEDI | 1323   23   19   18   44   22   85      |MD  40   38   35   50   34   28    30

Table 3.1646.4  GPS week: 1646   Day: 4   MJD: 55770                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  793   14   15   13   38   16  ---    9 |    29   31   30   48   30  ---    28
 R02  |  961   20   14   25   43   24  ---   12 |    37   26   26   41   33  ---    25
 R03  | 5431   14   17   23   38   23  ---   11 |    23   23   40   37   26  ---    22
XR04  | 1728   28   26  ---   72  330  ---   28 |    34   84  ---   73  178  ---    61
 R05  |  853   27   21   16   30   18  ---   11 |    39   23   32   43   27  ---    25
 R06  | 1436   20   23   23   47   20  ---   12 |    37   59   27   36   26  ---    28
 R07  | 3692   32   21   22   29   24  ---   12 |    31   43   36   25   23  ---    24
 R08  | 1165   18   17   20   45   20   67   11 |    37   44   44   36   31   25    32
 R09  | 1656   44   22   59   44   30  ---   20 |    28   31   55   41   30  ---    24
 R10  | 1808   21   26   12   22   18  ---   10 |    27   48   23   37   33  ---    29
 R11  |  803   60   47   38   47   37  175   23 |    36   87   67   54   38   25    48
 R12  | 1464   26   15   14   45   14  ---   11 |    25   35   33   54   30  ---    28
 R13  | 1745   31   17   18   39   19  ---   12 |    28   29   27   44   25  ---    20
 R15  | 4322   17   14   20   37   21   79   10 |    28   34   36   37   25   19    26
 R16  | 1043   34   22   33   60   24  ---   16 |    46   47   58   63   42  ---    43
 R17  | 3529   38   34   34   55   29  ---   18 |    85  101   99   87   94  ---    89
 R18  |  907   19   14   16   42   22  ---   11 |    38   28   24   54   28  ---    28
 R19  |  968   17   18   20   55   20  ---   12 |    50   31   36   56   40  ---    36
 R20  | 2361   29   19   35   57   25  ---   16 |    41   32   42   64   44  ---    36
 R21  | 1077   23   16   13   30   22  ---   10 |    29   22   19   38   31  ---    20
 R22  | 1315   21   23   25   30   27  ---   12 |    40   37   42   47   45  ---    36
 R23  |  917   14   29   15   34   26  ---   12 |    45   43   41   61   47  ---    41
 R24  | 2233   22   26   21   45   28  ---   14 |    41   34   35   69   56  ---    40
------+-----------------------------------------+-------------------------------------
 RMS  | 2225   28   23   26   43   24  117      |T   37   42   39   49   42   23    34
 WRMS | 2225   26   21   25   40   24  117      |NE  34   39   38   46   32   23    30
 MEDI | 1436   22   21   20   43   23   79      |MD  37   34   36   47   31   25    28

Table 3.1646.5  GPS week: 1646   Day: 5   MJD: 55771                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1141   17   22   15   73   24  ---   14 |    36   60   51   30   35  ---    42
 R02  |  793   18   19   13   25   19  ---    9 |    42   40   25   47   45  ---    35
 R03  | 6104   19   19   10   34   27  ---   10 |    23   23   24   46   21  ---    19
XR04  | 1963  185  139  ---  264  454  ---  160 |    31  197  ---  136  164  ---   113
 R05  | 1052   42   17   22   19   24  ---   13 |    41   33   27   33   24  ---    26
 R06  | 1037   23   25   13   37   18  ---   11 |    36   35   38   57   27  ---    34
 R07  | 2464   11   18   17   53   25  ---   11 |    27   44   25   32   42  ---    28
 R08  | 1544   24   12   14   34   16   88    9 |    33   40   36   59   30   19    34
 R09  | 1566   41   27   17   46   19  ---   14 |    28   37   35   36   21  ---    21
 R10  | 1141   30   11   42   32   20  ---   14 |    21   25   34   28   26  ---    16
 R11  | 1700   58   33   27   41   31  209   19 |    36   56   55   54   29   31    36
 R12  |  875   22   18   22   30   20  ---   10 |    16   32   35   21   23  ---    18
 R13  | 1112   25   20   16   24   17  ---   10 |    30   21   30   39   33  ---    22
 R15  | 3256   14   16   21   38   30   68   11 |    20   32   31   31   22   29    20
 R16  | 1222   37   14   12   39   20  ---   11 |    46   45   36   36   57  ---    41
 R17  | 5111   67   25   23   97   39  ---   23 |    86   70   72   81   86  ---    67
 R18  | 2226   17   18   13   36   16  ---    9 |    49   54   47   91   52  ---    52
 R19  | 1135   14   20   10   36   27  ---   10 |    27   26   25   42   40  ---    24
 R20  | 1652   30   19   20   74   34  ---   16 |    48   58   53   93   50  ---    49
 R21  | 1271   14   24   17   61   15  ---   12 |    25   38   21   54   42  ---    22
 R22  | 1307   20   13   18   60   23  ---   12 |    42   40   32   79   45  ---    36
 R23  |  940   16   22   19   42   22  ---   11 |    46   35   44   68   52  ---    43
 R24  | 1196   18   17   19   53   28  ---   12 |    55   51   34   73   53  ---    45
------+-----------------------------------------+-------------------------------------
 RMS  | 2249   30   20   19   48   24  136      |T   36   47   36   55   44   26    36
 WRMS | 2249   26   19   22   42   24  136      |NE  33   38   35   48   34   26    30
 MEDI | 1271   22   19   17   39   23   88      |MD  36   40   34   47   40   29    34

Table 3.1646.6  GPS week: 1646   Day: 6   MJD: 55772                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01M | 1021   17   18   11   47   28  ---   11 |    42   58   52   37   47  ---    47
 R02M |  858   15   15   16   29   21  ---    9 |    36   35   46   37   32  ---    33
 R03  | 2650   24   16   10   29   15  ---    9 |    26   44   45   40   29  ---    36
XR04E | 2104   63   74  ---  140  409  ---   60 |    33   76  ---  103  242  ---    44
 R05  | 1241   54   22   26   39   11  ---   16 |    59   19   25   30   17  ---    21
 R06  |  693   31   14   16   50   18  ---   12 |    47   37   36   32   17  ---    27
 R07  | 2486   23   23   20   34   36  ---   13 |    33   25   32   25   12  ---    20
 R08  | 1962   15   15   16   26   24  105    9 |    28   39   26   31   30   16    27
 R09  |  950   33   15   17   32   18  ---   11 |    38   32   34   32   30  ---    27
 R10  | 2312   26   14   15   30   30  ---   10 |    41   34   38   42   35  ---    33
 R11  | 1613   68   21   22   34   34  201   18 |    39   62   61   56   55   25    48
 R12  | 1941   33   14   11   24   32  ---   11 |    29   23   23   28   37  ---    20
 R13  | 1185   23   25   10   46   24  ---   12 |    31   50   34   31   26  ---    31
 R15  | 1898   12   19   15   50   18   83   11 |    24   38   35   36   29   22    27
 R16  | 1429   21   13   17   40   29  ---   11 |    53   52   44   39   49  ---    46
 R17M | 5794   68   37   48   87   66  ---   28 |   185  195  201  160  206  ---   187
 R18  | 3204   22   23   19  122   31  ---   21 |    69   61   62  111   58  ---    64
 R19  | 1321   25   14   22   31   62  ---   15 |    63   46   39   64   83  ---    51
 R20  | 1726   34   19   16  102   48  ---   20 |    62   75   58   56   90  ---    63
 R21E | 1872   31   18   32   59   88  ---   22 |    46   47   47   71   62  ---    40
 R22E | 1019   22   18   21   56   30  ---   13 |    43   41   31   80   46  ---    39
 R23E | 1379   17   25   15   43   34  ---   12 |    73   57   68  112   70  ---    68
 R24  | 1316   24   15   19   42   42  ---   13 |    82   76   81  114   69  ---    78
------+-----------------------------------------+-------------------------------------
 RMS  | 2102   33   20   21   54   38  139      |T   51   53   50   59   59   21    46
 WRMS | 2102   29   18   21   56   38  139      |NE  45   44   42   47   41   21    38
 MEDI | 1613   24   18   16   42   30  105      |MD  42   46   39   40   46   22    39




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