[IGSREPORT-15739] Wk 1454 IGLOS Final Orbits

Gerd Gendt3 igsacc at gfz-potsdam.de
Mon Dec 10 03:50:13 PST 2007


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IGS Electronic Report   10 Dec 03:50:17 PST 2007      Message Number 15739
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Author:   AC Coordinator / GFZ Potsdam                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1454   (Nov 18, 2007 - Nov 24, 2007) 
                                                                               
Contact: Gerd Gendt     (gendt at gfz-potsdam.de)                   
         Thomas Nischan ( nisn at gfz-potsdam.de)                             
                                                                               
                                                                               
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 2.1454.
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:                   
                                                                               
 igl1454[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1454 in the SP3 format.
 igl14547.sum      Combination Report for GPS Week 1454.


    
    
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  |   1545.9 ns
                1  |   1547.9 ns
                2  |   1523.1 ns
                3  |   1553.6 ns
                4  |   1418.1 ns
                5  |   1503.1 ns
                6  |   1500.1 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
               ----+--------+---------------
                0  |  ESX   | R10 R14 R23 R24
                1  |  COD   | R07
                1  |  ESX   | R10 R14 R23 R24
                1  |  IAC   | R15
                2  |  COD   | R07
                2  |  ESX   | R10 R14 R23 R24
                3  |  COD   | R07
                3  |  ESX   | R10 R14 R23 R24
                4  |  COD   | R07
                4  |  ESX   | R10 R14 R23 R24
                5  |  ESX   | R10 R14 R23 R24
                6  |  ESX   | R10 R14 R23 R24

    
         
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 1.1454, 1a.1454).
        
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 2.1454.0-6)                                                                                
    
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 3.1454.0-6). 
        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 1454 summary.                      (Nov 18, 2007 - Nov 24, 2007)

Table 1.1454.a     GPS week : 1454   MJD: 54422.0-54428.0

         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   55|    2     1     7   -42     6   -25  -.05   68   44 |       0   -2498   7561   8755
        |    6     4    13    61    81   166   .12           |       0    7297
cod  177|   -1    -4     5    58   -17  -106  -.02   52   46 |     ---     ---    ---    ---
        |    2     4    10    81    80   129   .08           |     ---     ---
esx   51|   -1     3    -9    15    55   161  -.18  183   67 | -163634    1465   8203  16762
        |    6     7     5   115   128   214   .13           |  371933   11321
iac  n/a|    1     1    -2   -33   -36    69   .27   67   67 | 1518147   -3913   8051  17093
        |    3     5    11    61    59   119   .17           |   51956    9250
mcc  n/a|   -1    -1     9     6    -9   210   .03  280  280 |     ---     ---    ---    ---
        |    5     4    25    17    25   557   .08           |     ---     ---


Table 1.1454.b     GPS week : 1454   MJD: 54422.0-54428.0   

         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  |   32   22   24   32   18   16   18 |
 R04  |   12   20   25   28   13   27   20 |
 R06  |   19   23   25   24   18   33   31 |
 R07  |   28    0  ---  ---  ---  145  180 |
 R08  |   27   24   23   39   25   24   24 |
 R10E |   27   31   84  213  116    0    0 |
 R14E |   25   17   17   26   32   40   88 |
 R15E |   91   62 2453    0    0    0    0 |
 R19  |   74   68   64   89   72   65   69 |
 R20  |  ---    0    0    0   84  106   66 |
 R21  | 1119    0    0    0    0    0    0 |
 R23  |   45   34   43   40   34   21   30 |
 R24  |   26   75   32   53   57   61   18 |


Table 1.1454.c     GPS week : 1454   MJD: 54422.0-54428.0   

         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 1454 0   |  135    68   164    -674    4353  -50380  88.2  4688  4688 | 1545940       0
brd 1454 1   |  126   145  -599     324    5083  -45070  86.8  4876  4876 | 1547880       0
brd 1454 2   | -178   -22  -684    -173    4022  -37170  87.7  4770  4770 | 1523089       0
brd 1454 3   |  163  -142  -367    2052   -1991  -40200  82.2  4953  4953 | 1553623       0
brd 1454 4   | -279    -5  -615   -1514    9603  -39000  83.8  4339  4339 | 1418061       0
brd 1454 5   |   32    68  -602    -616    4075  -42010  73.1  5351  5351 | 1503077       0
brd 1454 6   | -115  -118  -232    -318   -3311  -35190  98.3  4424  4424 | 1500139       0
-------------+------------------------------------------------------------+----------------
brd 1454 mean|  -16    -1  -419    -131    3119  -41288  85.7  4771  4771 | 1513115       0
brd 1454 sdev|  174   104   303    1114    4408    5132   7.6   340   340 |   47136       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 2.1454.0  GPS week: 1454   Day: 0   MJD: 54422                            

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   55|    0     0     0    38    17   -83  -.00   51   42 |       0    -256   1974   2160
cod  177|   -1   -13     9    54   -31  -163  -.05   60   57 |     ---     ---    ---    ---
esx   51|    6     8    -7    32    44   274  -.23  233   65 | -999999   -1115   6222  14538
iac  n/a|    4     0     4   -58   -20    43   .01   63   63 | 1569758  -19498   5701  14672
mcc  n/a|  -13   -11    67    45   -68  1476   .20  351  351 |     ---     ---    ---    ---

Table 2.1454.1  GPS week: 1454   Day: 1   MJD: 54423                            

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   55|    9    -6    12    33   -35  -154  -.20   74   41 |       0     497   2778   2998
cod  177|    3    -3     6   -77   -64     6   .15   55   48 |     ---     ---    ---    ---
esx   51|  -14     7    -2   144   -18   548  -.22  271   67 |   16025    4412   6747  12656
iac  n/a|    5    -2    -2    56  -114    -2   .33   55   55 | 1558187   -6445   6462  12640
mcc  n/a|    0     0     0     0     0     0   .0   237  237 |     ---     ---    ---    ---

Table 2.1454.2  GPS week: 1454   Day: 2   MJD: 54424                            

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   55|    0     8   -10  -129   -72   246   .13   62   41 |       0   -2779   4660   5412
cod  177|   -3    -5    16    57    75  -327  -.11   57   53 |     ---     ---    ---    ---
esx   51|   -3     0    -8   158    83   182  -.31  205   69 |  -29851   -2269   5842  14819
iac  n/a|    1     6    -4  -101   -70   -20   .33   51   51 | 1524905   -1677   5793  15184
mcc  n/a|    0     0     0     0     0     0   .0   368  368 |     ---     ---    ---    ---

Table 2.1454.3  GPS week: 1454   Day: 3   MJD: 54425                            

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   55|    5     4    32   -88   153   111   .02  117   63 |       0     -61   3512   3760
cod  177|    0    -5    -4   156  -129  -179   .03   58   49 |     ---     ---    ---    ---
esx   51|   -1     0   -12    43   188    -3  -.25  189   90 |   40914   12330   6616  15604
iac  n/a|   -1     9   -11   -60    -3   281   .19   68   68 | 1549585    6625   6748  16071
mcc  n/a|    0     0     0     0     0     0   .0  1008 1008 |     ---     ---    ---    ---

Table 2.1454.4  GPS week: 1454   Day: 4   MJD: 54426                            

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   55|   -2     2     1   -41   -16    39   .01   67   44 |       0  -18431  29037  34595
cod  177|    0     0    17   146    35  -108  -.07   44   37 |     ---     ---    ---    ---
esx   51|    3    -1    -8  -139   -47   136   .08  200   55 | -112968   17300   8698  18851
iac  n/a|   -3     4   -18   -90   -25   -55   .42   70   70 | 1415611    6753   8471  17979
mcc  n/a|    0     0     0     0     0     0   .0     0    0 |     ---     ---    ---    ---

Table 2.1454.5  GPS week: 1454   Day: 5   MJD: 54427                            

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   55|   -6     4    11   -64   -67  -107  -.19   55   42 |       0    3918   7955   8889
cod  177|   -3    -1     0    72    73   -11  -.03   54   43 |     ---     ---    ---    ---
esx   51|    0    -4   -19   -12  -107   117  -.08   85   56 |  -23188  -17229  15754  24683
iac  n/a|    1    -6     0    39    62    69   .10   70   70 | 1506646   -9752  15801  26055
mcc  n/a|    0     0     0     0     0     0   .0     0    0 |     ---     ---    ---    ---

Table 2.1454.6  GPS week: 1454   Day: 6   MJD: 54428                            

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   55|    9     0     4   -49    69  -233  -.13   50   34 |       0    -379   3014   3472
cod  177|   -1     0   -11    -1   -79    36  -.06   38   38 |     ---     ---    ---    ---
esx   51|   -3    15    -6  -116   249  -126  -.24  100   68 |  -36372   -3170   7544  16186
iac  n/a|    1    -2    16   -16   -86   172   .49   92   92 | 1502340   -3403   7381  17053
mcc  n/a|    0     0     0     0     0     0   .0     0    0 |     ---     ---    ---    ---

       
       
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 3.1454.0  GPS week: 1454   Day: 0   MJD: 54422                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 3557   39   46   79   53  ---   32 |    54   65   71   47  ---    45
 R04  | 2951   20   18   23   22  ---   12 |    42   54   54   54  ---    47
 R06  | 4328   20   33   48   27  ---   19 |    26   38   57   45  ---    32
 R07  |  708   50   70   33   25   57   27 |     4 9999    9   60   21   191
 R08  | 3670   38   52   51   41  ---   26 |    31   58   50   54  ---    35
 R10  | 2056   29   47  368   36  ---   26 |    56  112   60   20  ---    92
 R14  | 4425   34   47  422   22  ---   25 |    55   62  176   53  ---    67
XR15  | 4592   90   96  ---  180 1117   90 |   429  166  ---   29  299   194
 R19  | 5244  113  121  100  164  ---   73 |   145  137  155  173  ---   134
XR21  | ----  ---  741  --- 1376  --- 1118 |   ---  229  ---    1  ---   590
 R23  | 2073   64   58  287   65  ---   44 |    40   99  191  108  ---    81
 R24  |10490   27   48  353   33  493   25 |   216  217  295  255  227   242
------+------------------------------------+--------------------------------
 RMS  | 4687   51   60  233   63  351      |T   99  112  111   74  182   145
 WRMS | 4687   42   57   65   63  351      |NE  99  112  111   74  182   145
 MEDI | 3670   38   48   79   36  493      |MD  54   99   60   53  227    81

Table 3.1454.1  GPS week: 1454   Day: 1   MJD: 54423                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 3092   39   22   31   51  ---   22 |    72   40   53   46  ---    44
 R04  | 2263   48   14   45   25  ---   20 |    34   44   53   49  ---    33
 R06  | 3588   24   44   61   28  ---   23 |    29   39   70   37  ---    24
XR07  | 1296  ---  294  ---    8  ---    0 |   --- 9999  ---   59  ---   175
 R08  | 3906   29   39   70   21  ---   23 |    34   37   50   47  ---    28
 R10  | 2401   37   39  479   52  ---   31 |    64  153   66   26  ---   122
 R14  | 5738   24   24  447   21  ---   16 |    50   57  184   65  ---    63
XR15  | 5378   68   55  ---  728  663   61 |   674  204  ---   13  234   489
 R19  | 3362  124  113  120  113  ---   67 |   134   90  112   86  ---    86
XR20  | ----  ---    8  ---  ---  ---    0 |   ---  864  ---  ---  ---   867
XR21  | ----  ---    8  ---  ---  ---    0 |   ---  358  ---  ---  ---   306
 R23  | 2386   47   45  306   50  ---   33 |    31   49   60   47  ---    32
 R24  |10746  158   82  335   64  237   75 |   240  234  270  207  199   211
------+------------------------------------+--------------------------------
 RMS  | 4876   74   55  271   55  237      |T  136  180  102   62  216   190
 WRMS | 4876   41   48   67   55  237      |NE 136  180  102   62  216   190
 MEDI | 3362   39   39  120   50  237      |MD  50   57   66   47  199    86

Table 3.1454.2  GPS week: 1454   Day: 2   MJD: 54424                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 4093   30   34   64   35  ---   24 |    46   28   93   67  ---    55
 R04  |  747   42   23   58   45  ---   25 |    45   50   63   51  ---    44
 R06  | 2069   44   61   35   29  ---   25 |    51   46   60   48  ---    36
 R08  | 3964   42   40   48   24  ---   22 |    29   58   33   31  ---    25
XR10E | 2206  133  122  ---  101  ---   83 |    81  234  ---   25  ---   179
 R14E | 6152   26   22  400   25  ---   17 |    41   41  145   34  ---    39
XR15E | 3570 2619 2297  ---  --- 1690 2452 |   362   85  ---  ---  470  9999
 R19  | 1326  139  106   93  100  ---   63 |   187   71  110   90  ---    81
XR20  | ----  ---   21  ---  ---  ---    0 |   ---  343  ---  ---  ---   352
XR21  | ----  ---   21  ---  ---  ---    0 |   ---  426  ---  ---  ---   425
 R23  | 2208   47   64  289   65  ---   42 |    44   84   90   35  ---    50
 R24  |10008   46   55  271   34  368   32 |   197  200  207  186  478   184
------+------------------------------------+--------------------------------
 RMS  | 4769   62   57  205   51  368      |T  108  138  100   63  474   133
 WRMS | 4769   41   53   69   51  368      |NE  85  145   93   72  478   139
 MEDI | 2208   44   40   64   35  368      |MD  46   71   90   48  470    55

Table 3.1454.3  GPS week: 1454   Day: 3   MJD: 54425                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 4079   32   50   85   33  ---   31 |    49   45  112   54  ---    44
 R04  | 1481   53   27   60   51  ---   27 |    39   44  100   64  ---    59
 R06  | 3164   66   47   17   31  ---   24 |    31   61   46   61  ---    46
 R08  | 4378   64   76   86   29  ---   38 |    47   75  102   67  ---    40
XR10E | 3081  300  153  ---  ---  ---  212 |   197  170  ---  ---  ---   154
 R14E | 6005   31   40  310   36  ---   26 |    57   84  139   81  ---    76
XR15E | 8600  ---   16  ---  --- 1456    0 |   ---  285  ---  ---  134   840
 R19  | 1577  272  102   99  150  ---   88 |   225   64  128  175  ---    74
XR20  | ----  ---   16  ---  ---  ---    0 |   ---  475  ---  ---  ---   480
XR21  | ----  ---   16  ---  ---  ---    0 |   ---  305  ---  ---  ---   275
 R23  | 2322   67   49  298   58  ---   40 |    44   52  178   57  ---    47
 R24  |10211  132   33  269   63 1008   52 |   184   63  128   68  419    69
------+------------------------------------+--------------------------------
 RMS  | 4953  117   58  189   68 1008      |T   97  143  116   78  276   183
 WRMS | 4953   63   49   90   68 1008      |NE  88  131  113   78  419   126
 MEDI | 3164   66   40   86   36 1008      |MD  49   64  112   64  134    69

Table 3.1454.4  GPS week: 1454   Day: 4   MJD: 54426                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 5705   26   32   36   27  ---   18 |    45   64   51   64  ---    50
 R04  | 2526   21   15   27   26  ---   13 |    38   40   70   33  ---    35
 R06  | 6017   23   32   36   29  ---   18 |    22   79   38   44  ---    35
 R08  | 3965   53   21   54   42  ---   24 |    39   40   58   44  ---    27
XR10E | 3902  151   88  ---  ---  ---  116 |   179  171  ---  ---  ---   140
 R14E | 5458   50   48  396   34  ---   32 |    40   63  163   54  ---    48
XR15E | 8439  ---   15  ---  --- 1548    0 |   ---  105  ---  ---  162   294
 R19  | 2401  142   88  112  166  ---   72 |   129   97  144  214  ---   114
XR20  | 4520  102   70  ---  ---  ---   83 |    53  303  ---  ---  ---   286
XR21  |21490  ---   15  ---  ---  ---    0 |   ---  210  ---  ---  ---   245
 R23  | 2320   69   34  324   44  ---   34 |    72   81  188   49  ---    65
XR24  | 9192  ---   43  302   74  952   57 |   ---   66  188   65  282    52
------+------------------------------------+--------------------------------
 RMS  | 4339   67   44  200   70    0      |T   68  109  112   70  222   115
 WRMS | 4339   44   37   55   70    0      |NE  56  108  105   73  282   101
 MEDI | 4520   53   32   54   34  952      |MD  45   79   70   49  162    52

Table 3.1454.5  GPS week: 1454   Day: 5   MJD: 54427                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 5784   17   16   50   29  ---   16 |    32   45   41   34  ---    32
 R04  | 1007   53   16   89   25  ---   27 |    25   44   99   50  ---    42
 R06  | 8808   23   67   67   60  ---   32 |    26   63   58   70  ---    38
XR07  | ----  ---  132  ---  158  327  144 |   ---  728  ---   50   36   243
 R08  | 5051   55   21   52   39  ---   24 |    29   31   52   41  ---    24
XR10E | 4451  ---    6  ---  ---  ---    0 |   ---  180  ---  ---  ---   170
XR14E | 4399   49   53  ---   64  ---   39 |    61  117  ---  106  ---   114
XR15E |14380  ---    6  ---  --- 1384    0 |   ---  246  ---  ---  124   335
 R19  | 2362   92   96  137  133  ---   65 |   114  110  173  168  ---   125
XR20  | 8896  127  113  ---  200  ---  105 |    30  273  ---   51  ---   320
XR21  |17893  ---    6  ---  ---  ---    0 |   ---  239  ---  ---  ---   238
XR23  | 2056  ---   17  272   24  ---   21 |   ---   94  177   88  ---    87
XR24  |10528  ---   54  376   67 1174   60 |   ---   95  219  101  131    88
------+------------------------------------+--------------------------------
 RMS  | 5350   55   54   85   70    0      |T   45  174  117   75   97   142
 WRMS | 5350   42   43   56   70    0      |NE  42  172  117   72   83   123
 MEDI | 5051   53   21   89   60 1174      |MD  30  110   99   51  124   114

Table 3.1454.6  GPS week: 1454   Day: 6   MJD: 54428                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 2819   32   18   45   36  ---   17 |    52   42   61   33  ---    41
 R04  | 2409   30   17   48   49  ---   19 |    34   46   77   43  ---    42
 R06  | 7678   30   19   78   95  ---   31 |    28   53   71   82  ---    34
XR07  | ----  ---   65  ---  313  809  180 |   ---  665  ---   52   30   498
 R08  | 3891   33   26   68   49  ---   23 |    36   47   65   42  ---    31
XR10E | 4130  ---    8  ---  ---  ---    0 |   ---  243  ---  ---  ---   253
XR14E | 3148  ---   35  ---  150  ---   87 |   ---  106  ---  159  ---   105
XR15E | 9013  ---    8  ---  --- 1450    0 |   ---  286  ---  ---  117   317
 R19  | 3160   92   74  186  164  ---   69 |   121   98  216  196  ---   121
XR20  | 7543   56   52  ---  175  ---   65 |    31  308  ---   49  ---   322
XR21  |12250  ---    8  ---  ---  ---    0 |   ---  168  ---  ---  ---   201
XR23  | 1711  ---   17  274   47  ---   29 |   ---   95  207   51  ---    79
XR24  | 8291  ---   14  332   24 1487   18 |   ---   92  262   91  279    86
------+------------------------------------+--------------------------------
 RMS  | 4423   50   38  100   92    0      |T   50  173  137   79  142   163
 WRMS | 4423   34   38   68   92    0      |NE  50  161  137   71  154   145
 MEDI | 3891   32   18   78   49 1450      |MD  34   98   77   51  117   105



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