[IGSREPORT-15512] Wk 1444 IGLOS Final Orbits

Gerd Gendt3 igsacc at gfz-potsdam.de
Thu Sep 27 05:32:58 PDT 2007


******************************************************************************
IGS Electronic Report   27 Sep 05:33:06 PDT 2007      Message Number 15512
******************************************************************************

Author:   AC Coordinator / GFZ Potsdam                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1444   (Sep 09, 2007 - Sep 15, 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 2.1444.
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:                   
                                                                               
 igl1444[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1444 in the SP3 format.
 igl14447.sum      Combination Report for GPS Week 1444.


    
    
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  |   1203.4 ns
                1  |   1190.5 ns
                2  |   1174.1 ns
                3  |   1241.9 ns
                4  |   1225.2 ns
                5  |   1224.5 ns
                6  |   1251.9 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  |  COD   | R15 R21
                0  |  ESX   | R02 R03 R10 R14 R18 R19 R21 R23 R24
                1  |  COD   | R15 R21 R21
                1  |  ESX   | R10 R14 R23 R24
                2  |  COD   | R15 R21
                2  |  ESX   | R10 R14 R23 R24
                3  |  COD   | R15 R21
                3  |  ESX   | R10 R14 R23 R24
                4  |  COD   | R15 R21
                4  |  ESX   | R10 R14 R23 R24
                5  |  COD   | R15 R21
                5  |  ESX   | R10 R14 R23 R24
                6  |  COD   | R15
                6  |  ESX   | R02 R03 R04 R08 R10 R14 R18 R19 R21 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 1.1444, 1a.1444).
        
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 2.1444.0-6)                                                                                
    
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 3.1444.0-6). 
        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 1444 summary.                      (Sep 09, 2007 - Sep 15, 2007)

Table 1.1444.a     GPS week : 1444   MJD: 54352.0-54358.0

         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|    0     2     3    -5    14  -181  -.08   38   38 |       0     207   3477   3752
        |    5     4     5    39    72   213   .14           |       0     556
cod  173|   -1    -5     0    -7   -37    83  -.02   42   35 |     ---     ---    ---    ---
        |    6     6     5    82    63   226   .08           |     ---     ---
esx   41|    5     1    -4    -8   -18   359  -.21  328  181 |  600166   18154   8835  21165
        |    7    10    30   134    71   247   .17           | 1054845   28875
iac  n/a|    0     4    -1    45    -6   -18   .18   63   63 | 1212775    4908   9032  21613
        |    4     6    11    74    66   238   .12           |   25385    8033
mcc  n/a|   -3    -6    61   154    82   457   .46  108  108 |     ---     ---    ---    ---
        |   12    10    33   194   179   791   .76           |     ---     ---


Table 1.1444.b     GPS week : 1444   MJD: 54352.0-54358.0   

         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  |   19   20   25   19   24   22   32 |
 R04  |   21   24   23   22   48   19   33 |
 R06  |   35   28   34   29   25   20   27 |
 R07  |   25   18   19   18   24   20   25 |
 R08  |   18   29   30   20   24   32   47 |
 R10  |   24   41   21   20   19   16   22 |
 R14  |   15   33   23   33   16   21   22 |
 R23E |   55   62  148   92  ---  ---    0 |
 R24E |  ---    0    0    0    0  353  122 |


Table 1.1444.c     GPS week : 1444   MJD: 54352.0-54358.0   

         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 1444 0   |   74   114  -769  -11280    7769 -329700  99.4  5524  5524 | 1203431       0
brd 1444 1   |  118   135  -158   -9323   -4761 -341600  99.8  5011  5011 | 1190517       0
brd 1444 2   |   23   164  -260    1705   -2533 -333100  89.8  5848  5848 | 1174052       0
brd 1444 3   |  -58   -39  -370     683   -3913 -320200 104.4  5340  5340 | 1241897       0
brd 1444 4   |  148   581  -380    1462   -7094 -324700 100.0  4765  4765 | 1225199       0
brd 1444 5   |  589   964  -486   -1424    2905 -332200  90.2  5117  5117 | 1224532       0
brd 1444 6   |   26   349  -874    2003    -648 -357300  97.8  4859  4859 | 1251938       0
-------------+------------------------------------------------------------+----------------
brd 1444 mean|  131   324  -471   -2310   -1182 -334114  97.3  5209  5209 | 1215938       0
brd 1444 sdev|  213   344   261    5602    5068   12247   5.4   385   385 |   27948       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 2.1444.0  GPS week: 1444   Day: 0   MJD: 54352                            

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     7     5   -29   -34  -195  -.07   40   41 |       0    -248   4851   5219
cod  173|   -1   -10     0    35   -29   210   .01   44   37 |     ---     ---    ---    ---
esx   41|    6     5   -38    26    27  -132  -.07  278  105 |   -6888   18684  11859  23335
iac  n/a|   -1     5    13   -11  -114   -81   .26   43   43 | 1186984   16089  11931  24220
mcc  n/a|  -11   -10    78   -15  -116  1248   .19  132  132 |     ---     ---    ---    ---

Table 2.1444.1  GPS week: 1444   Day: 1   MJD: 54353                            

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|   -4    -1     0   -67   -21  -453  -.18   53   53 |       0      11   3763   4211
cod  173|    9   -11    -8    97    32  -168  -.11   56   47 |     ---     ---    ---    ---
esx   41|   -2     1   -38   -41    61   231  -.24  268   90 |  -27346   -5713   9533  16076
iac  n/a|    3     2    14     4   -14   322   .19   43   43 | 1197454   -9951   8964  16150
mcc  n/a|   -8     1    25    -4     0   263   .04   73   73 |     ---     ---    ---    ---

Table 2.1444.2  GPS week: 1444   Day: 2   MJD: 54354                            

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|    4     5    10    -4     4    -7  -.28   47   50 |       0     900   3274   3401
cod  173|   -1     0    -2   -31   -21   -89   .02   48   26 |     ---     ---    ---    ---
esx   41|    3    20    -8   120   -61   569  -.06  285  126 |  -75378   -4749   6885  16353
iac  n/a|   -3    -4    -9   -71    69    14   .27  155  155 | 1177688    1784   7115  16905
mcc  n/a|    0    -6    12    80   197  -363  -.49  120  120 |     ---     ---    ---    ---

Table 2.1444.3  GPS week: 1444   Day: 3   MJD: 54355                            

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    -3     0    19   132    26   .05   34   33 |       0     500   3238   3391
cod  173|  -12     5     5     4   -63     8   .09   28   28 |     ---     ---    ---    ---
esx   41|   15    -5    -6  -186    66   450  -.55  190   57 |   12496   -7333   7882  23382
iac  n/a|   -2     6   -11   127   -15  -389   .23   45   45 | 1237671    3563   8411  24866
mcc  n/a|    4    -7    49   263    75  -393  -.04  117  117 |     ---     ---    ---    ---

Table 2.1444.4  GPS week: 1444   Day: 4   MJD: 54356                            

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|    4     2     6    -8    -9  -294  -.14   35   37 |       0     907   2842   3028
cod  173|   -5    -6    -1   -30   -43   414   .05   33   30 |     ---     ---    ---    ---
esx   41|   14     7    16  -110  -125   439  -.13  213   65 | 2137289   54307   7258  21024
iac  n/a|   -3     4    -8   120   -12  -230   .27   46   46 | 1224180    5796   7771  21549
mcc  n/a|   14     0    77   187  -104  -105   .59   82   82 |     ---     ---    ---    ---

Table 2.1444.5  GPS week: 1444   Day: 5   MJD: 54357                            

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     5     7    60   -67  -409   .11   24   25 |       0    -190   2242   2499
cod  173|   -3    -4    -5  -164    21   305  -.14   46   37 |     ---     ---    ---    ---
esx   41|   -2    -3    -4   -66   -55   375  -.31  216   59 | 2150079   61623   7652  21835
iac  n/a|    8     0    -1    89   -41   128   .06   39   39 | 1222992    7376   8258  20781
mcc  n/a|   -1     3   104    38   131  1408  1.51  116  116 |     ---     ---    ---    ---

Table 2.1444.6  GPS week: 1444   Day: 6   MJD: 54358                            

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|   -7     3    -6    -5    94    64  -.02   31   26 |       0    -427   4130   4517
cod  173|    1   -10     4    38  -158   -98  -.02   38   37 |     ---     ---    ---    ---
esx   41|    1   -12    50   201   -46   580  -.14  842  763 |   10911   10264  10776  26156
iac  n/a|    3    17    -9    58    83   106  -.05   66   66 | 1242461    9700  10777  26821
mcc  n/a|  -25   -27    86   529   393  1146  1.44  114  114 |     ---     ---    ---    ---

       
       
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 3.1444.0  GPS week: 1444   Day: 0   MJD: 54352                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 2892   21   37   51   30  ---   19 |    28   43   64   39  ---    34
 R04  | 4935   20   42   54   31  ---   20 |    46   29  237   46  ---    45
 R06  | 9527   56   65   82   50  ---   35 |    48   76   95   49  ---    36
 R07  | 2629   32   33   78   38  132   25 |    60   34   92   30   94    37
 R08  | 5113   24   27   41   31  ---   17 |    22   41  127   41  ---    27
 R10  | 3322   18   33  469   45  ---   23 |    41   36  323   60  ---    43
 R14  | 4810   13   26  431   23  ---   15 |    30   23  203   55  ---    30
 R23  | 7304   84   70  441   76  ---   55 |    43  167 9999   91  ---   178
------+------------------------------------+--------------------------------
 RMS  | 5523   40   44  278   43  132      |T   39   56  163   51   94    53
 WRMS | 5523   41   37  105   43  132      |NE  39   56  163   51   94    53
 MEDI | 4810   21   33   78   31  132      |MD  41   36  127   46   94    36

Table 3.1444.1  GPS week: 1444   Day: 1   MJD: 54353                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 2486   27   42   60   20  ---   19 |    18   48   68   41  ---    28
 R04  | 7124   25   57   70   29  ---   24 |    24   35  210   44  ---    22
 R06  | 4012   61   44   64   28  ---   27 |    40   72  116   29  ---    39
 R07  | 3632   17   45   50   20   73   17 |    40   34   71   40   47    28
 R08  | 6750   53   42   83   38  ---   29 |    37   39  127   57  ---    50
 R10  | 2719   39   78  387   57  ---   40 |    24   53  120   55  ---    27
 R14  | 6287   35   49  362   50  ---   32 |    30   14  212   74  ---    41
 R23  | 4702  107   77  521   73  ---   61 |    31  144 9999  103  ---   152
XR24  | ----  ---   14  559  ---  ---    0 |   ---  431 9999  ---  ---   454
------+------------------------------------+--------------------------------
 RMS  | 5010   53   56  268   43   73      |T   30   96  132   55   47    93
 WRMS | 5010   53   47   90   43   73      |NE  30   96  132   55   47    93
 MEDI | 4012   35   45   83   29   73      |MD  30   48  120   44   47    39

Table 3.1444.2  GPS week: 1444   Day: 2   MJD: 54354                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 2177   41   21  100   40  ---   24 |    53   37   76   49  ---    30
 R04  | 2673   21   23   65   67  ---   22 |    22   32  173   78  ---    17
 R06  | 2891   40   28  154   61  ---   33 |    54   37   92   48  ---    28
 R07  | 2989   18   16   80   43  120   19 |    32   33   68   41   52    27
 R08  | 9810   56   13  107   63  ---   29 |    18   40   96   74  ---    34
 R10  | 4089   28   23  377   44  ---   21 |    46   67  180   41  ---    49
 R14  | 7328   16   22  383   63  ---   23 |    27   34  251   76  ---    34
 R23  | 8815   97  123  551  415  ---  147 |    35  159 9999  387  ---   126
XR24  | ----  ---    5  446  ---  ---    0 |   ---  642 9999  ---  ---   660
------+------------------------------------+--------------------------------
 RMS  | 5847   47   48  285  155  120      |T   35  120  133   99   52   111
 WRMS | 5847   50   26  126  155  120      |NE  35  120  133   99   52   111
 MEDI | 2989   28   22  154   61  120      |MD  32   37   96   49   52    34

Table 3.1444.3  GPS week: 1444   Day: 3   MJD: 54355                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 1705   44   22   35   26  ---   19 |    47   57   50   58  ---    44
 R04  | 5294   21   25   65   46  ---   21 |    30   27  178   52  ---    26
 R06  | 3921   36   31   94   52  ---   29 |    50   56   80   46  ---    45
 R07  | 3508   19   24   43   42  117   17 |    43   39   63   30   53    32
 R08  | 8653   30   30   39   44  ---   20 |    47   64  174   87  ---    55
 R10  | 4870   21   27  343   38  ---   20 |    41   48  160   37  ---    40
 R14  | 6509   51   31  344   59  ---   33 |    47   41  148   58  ---    23
XR23  |13321  ---   34  743  148  ---   91 |   ---  633 9999  158  ---   630
XR24  | ----  ---    9  327  ---  ---    0 |   ---  930 9999  ---  ---   931
------+------------------------------------+--------------------------------
 RMS  | 5339   34   28  190   45  117      |T   43  210  121   65   53   202
 WRMS | 5339   33   28   57   45  117      |NE  43  210  121   65   53   202
 MEDI | 4870   30   27   94   44  117      |MD  47   56  148   52   53    44

Table 3.1444.4  GPS week: 1444   Day: 4   MJD: 54356                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 2494   25   35   64   53  ---   23 |    51   54   68   62  ---    45
 R04  | 7192   59   32  204   45  ---   48 |    17   55  383   20  ---    38
 R06  | 3253   36   41   41   56  ---   24 |    29   50   41   51  ---    28
 R07  | 4112   40   38   61   36   82   24 |    38   55   67   44   61    38
 R08  | 5728   22   30   50   68  ---   23 |    43   34  139   54  ---    31
 R10  | 3367   24   30  373   25  ---   19 |    32   47  146   42  ---    34
 R14  | 5418   22   23  354   21  ---   16 |    43   51  109   61  ---    48
XR24E |19058  ---   23  518  ---  ---    0 |   ---  649 9999  ---  ---   624
------+------------------------------------+--------------------------------
 RMS  | 4765   35   33  213   46   82      |T   36  124  136   47   61   110
 WRMS | 4765   37   30   65   46   82      |NE  36   49  136   47   61    37
 MEDI | 4112   25   30   64   45   82      |MD  38   51  109   51   61    38

Table 3.1444.5  GPS week: 1444   Day: 5   MJD: 54357                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 4630   23   60   37   34  ---   22 |    49   78   59   64  ---    52
 R04  | 7461   25   35   43   34  ---   19 |    32   34  282   19  ---    25
 R06  | 2329   25   33   47   38  ---   20 |    47   59   89   58  ---    53
 R07  | 3579   21   28   50   44  116   20 |    48   52   75   39   65    43
 R08  | 5405   34   74   67   57  ---   32 |    26   77  391   43  ---    26
 R10  | 3881   19   29  438   19  ---   15 |    32   55  222   26  ---    31
 R14  | 6607   16   42  352   33  ---   20 |    61   40   85   36  ---    39
XR24E | 8111  ---  359  381  345  ---  352 |   ---  652 9999  199  ---   468
------+------------------------------------+--------------------------------
 RMS  | 5117   24   46  216   39  116      |T   42  130  171   60   65    92
 WRMS | 5117   25   37   59   39  116      |NE  42   56  171   40   65    38
 MEDI | 4630   23   35   50   34  116      |MD  47   55   89   39   65    39

Table 3.1444.6  GPS week: 1444   Day: 6   MJD: 54358                            

        Weighted Average                   Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  iac  mcc  IGL |   bkg  cod  esx  iac  mcc   IGL
------+------------------------------------+--------------------------------
 R01  | 4913   43   39  123   48  ---   31 |    54   79   95   78  ---    65
 R04  | 8463   33   31 1748   80  ---   33 |    29   37 9999   39  ---    26
 R06  | 1565   18   56   64   56  ---   26 |    41   74   83   51  ---    43
 R07  | 2314   20   32  114   32  114   24 |    37   57  109   43   45    39
 R08  | 4038   48   32 1260  120  ---   47 |    61   54  615   90  ---    39
 R10  | 4311   22   34  412   42  ---   22 |    27   48  228   33  ---    29
 R14  | 5174   20   34  351   43  ---   22 |    32   42  168   50  ---    35
XR23E | ----  ---   13 >>>>  ---  ---    0 |   ---  423 9999  ---  ---   424
XR24E | 7789  ---   97  607  153  ---  121 |   ---  370 9999  235  ---   345
------+------------------------------------+--------------------------------
 RMS  | 4858   31   38  842   66  114      |T   40  131  216   77   45   116
 WRMS | 4858   26   37  763   66  114      |NE  40   55  216   54   45    39
 MEDI | 4311   22   34  412   48  114      |MD  37   57  109   50   45    39



More information about the IGSREPORT mailing list