[IGSREPORT-20716] Wk 1680 IGLOS Final Orbits

IGS ACC igs.acc at noaa.gov
Thu Apr 5 08:38:39 PDT 2012


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1680   (Mar 18, 2012 - Mar 24, 2012) 
                                                                               
Contact: J. Griffiths (jake.griffiths at noaa.gov)            
         K. Choi (kevin.choi 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 2.1680.
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:
                                                                               
 igl1680[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1680 in the SP3 format.
 igl16807.sum      Combination Report for GPS Week 1680.


    
    
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). The emx orbits are introduced with full weight
    for the first time starting 11-Sep-2011 (GPS Week 1653).

 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  |    165.1 ns
                1  |    167.4 ns
                2  |    161.2 ns
                3  |    162.3 ns
                4  |    163.2 ns
                5  |    163.0 ns
                6  |    164.7 ns

    
         
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 1.1680, 1a.1680).
        
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 2.1680.0-6)                                                                                
    
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 3.1680.0-6). 
        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 1680 summary.                      (Mar 18, 2012 - Mar 24, 2012)

Table 1.1680.a     GPS week : 1680   MJD: 56004.0-56010.0

         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  259|   -1     2     0    58     7   -58  -.15   35   35 |     ---     ---    ---    ---
        |    2     1     6    26    30    21   .06           |     ---     ---
emx  140|    0    -1    -4   -22   -65    -7  -.20   34   34 |  163941     -21   3951   7430
        |    1     1     2    34    33    34   .04           |    1861    1860
esx  165|   -1     0     0    16     7   -45   .39   20   18 |  163642      71   3929   4382
        |    1     1     3    25    37    55   .03           |    1318    2748
gfz  186|    0    -1    -4   -38    12    41  -.35   26   24 |       0     -91   3929  12115
        |    2     1     3    41    51    47   .06           |       0    2303
grg  118|   -1     2    -6    19   -15   160   .02   43   40 |  198317    -214   3931  24226
        |    2     1     3    28    27    55   .10           |   11503    2613
iac  n/a|    2     1     9    -1    45   -63   .06   27   27 |  165944    -202   3977  12449
        |    1     1    12    19    31   219   .06           |    3056    1421
mcc  n/a|    3     3    43    20   119  -335   .04  173  173 |     ---     ---    ---    ---
        |    8     5    10   102   108   556   .14           |     ---     ---


Table 1.1680.b     GPS week : 1680   MJD: 56004.0-56010.0   

         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  |   15    8   11   18   14   14   11 |
 R02  |   12   13    8   12   12   11   15 |
 R03  |   15   10    8    8   16   12   10 |
 R04  |   13   16   11   11   11   13   13 |
 R05  |   12   11   13   13   13   12   13 |
 R06  |   12   13   16   17   16    7    9 |
 R07  |   12   12   12   12   14   13    9 |
 R08  |   10   12    9   10   13   13   17 |
 R09  |   13   13   10   11   11   11   13 |
 R10  |   15    9   10   10   13   11   13 |
 R11  |   19   18   24   26   22   21   20 |
 R12  |   12    8   10   11   11    9    9 |
 R13  |   11   11   12   14   11   10   11 |
 R14  |   17   15   16   13   13   15   16 |
 R15  |   10    9    9   13   15   10   11 |
 R16  |   12   10   10   11   11   10   10 |
 R17  |   13   13   10    9   12   11   11 |
 R18  |   13   11   12   11   12   12   14 |
 R19  |   10    9   11   11   12   10   10 |
 R20  |   15   18   22   20   22   19   22 |
 R21  |   21   26   18   16   18   16   15 |
 R22  |   12   12   11   11   13   12   15 |
 R23  |   11    9   10    9   12   11   10 |
 R24  |   10   10    9   15   16   11   20 |


Table 1.1680.c     GPS week : 1680   MJD: 56004.0-56010.0   

         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 1680 0   |   91   -29   115    1606     943   -8037  87.8  1573  1573 |  165129       0
brd 1680 1   | -106    93   142   -1782    1305  -10070  85.8  1532  1532 |  167387       0
brd 1680 2   |  -26    67    40     934     100   -6086  84.4  1494  1494 |  161161       0
brd 1680 3   |  -92   -99   181     793    -247   -5079  84.7  1869  1869 |  162339       0
brd 1680 4   |   57  -176    51    1599   -1101   -7186  83.6  1985  1985 |  163196       0
brd 1680 5   |   -1   -97   118    1213    -316   -9354  85.2  1823  1823 |  163014       0
brd 1680 6   |    1    73   141    -222    -518   -6320  84.7  1634  1634 |  164734       0
-------------+------------------------------------------------------------+----------------
brd 1680 mean|  -10   -24   113     591      23   -7447  85.2  1701  1701 |  163851       0
brd 1680 sdev|   72   104    50    1216     840    1810   1.4   189   189 |    2064       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 2.1680.0  GPS week: 1680   Day: 0   MJD: 56004                            

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  259|   -1     0     6    98   -27   -73  -.11   33   36 |     ---     ---    ---    ---
emx  140|    0    -1    -1    20   -42   -29  -.17   27   27 |  164579    1543   4185   7567
esx  165|   -1    -1     2    25    -2    56   .40   19   17 |  163252    1987   4183   4291
gfz  186|    3     0    -4   -84    22   147  -.33   27   26 |       0    1517   4192   7590
grg  118|   -4     4    -6     2     4   182   .02   42   42 |  182483    1938   4153  28986
iac  n/a|    0     1     2     5    79  -546   .04   42   42 |  165168    1286   4172   8249
mcc  n/a|   20     1    42   -29   154 -1286  -.01  258  258 |     ---     ---    ---    ---

Table 2.1680.1  GPS week: 1680   Day: 1   MJD: 56005                            

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  259|    1     0    -3    46   -23   -71  -.24   35   35 |     ---     ---    ---    ---
emx  140|    0     0    -4     6  -126    32  -.20   31   34 |  167034    1099   4328   7284
esx  165|    0     0    -3    45    14   -31   .42   17   16 |  164782    2847   4312   6665
gfz  186|   -2    -1    -5   -67    57    10  -.30   26   30 |       0    2544   4301   7314
grg  118|   -1     3    -8    14   -68    97   .00   37   35 |  193090    2156   4327  16782
iac  n/a|    2     0    16    -7    55   -29  -.02   22   22 |  167202    1932   4297   8204
mcc  n/a|    0    11    28   110    75  -788   .05  225  225 |     ---     ---    ---    ---

Table 2.1680.2  GPS week: 1680   Day: 2   MJD: 56006                            

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  259|   -4     2    -3    18    11   -70  -.06   34   33 |     ---     ---    ---    ---
emx  140|    0     0    -2   -29   -69    14  -.21   39   42 |  160687    1718   4483   7770
esx  165|    0     0     0     3    17   -48   .39   17   16 |  161114     363   4378   4472
gfz  186|    0    -1     1   -19    15    20  -.33   24   20 |       0    1676   4382  40988
grg  118|    0     3    -2    77   -22   201  -.02   45   38 |  199711    1072   4448  25336
iac  n/a|    1     1    -1     6    34    39   .01   21   21 |  172298   -1339   4669  39783
mcc  n/a|    1    -6    32  -150   235  -514  -.20  218  218 |     ---     ---    ---    ---

Table 2.1680.3  GPS week: 1680   Day: 3   MJD: 56007                            

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  259|    0     4    10    52     0   -82  -.16   36   34 |     ---     ---    ---    ---
emx  140|    0    -1    -2   -82   -59     4  -.25   36   38 |  163770   -2303   3735   8021
esx  165|    1    -1     0    21    29   -78   .36   21   19 |  164035   -4045   3731   3856
gfz  186|   -1    -3    -6    19     0    36  -.32   29   23 |       0   -2412   3726   7881
grg  118|    0     2    -4   -12   -24    65   .04   42   34 |  196993   -3455   3783  23659
iac  n/a|    1     3     0    -2     2    55   .07   25   25 |  163884   -1787   3746   8229
mcc  n/a|    0     3    46     2   -90  -157   .24  192  192 |     ---     ---    ---    ---

Table 2.1680.4  GPS week: 1680   Day: 4   MJD: 56008                            

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  259|    0     2    -2    79    -4   -27  -.16   34   35 |     ---     ---    ---    ---
emx  140|   -3    -2    -7   -41   -66   -46  -.14   38   35 |  164129   -2294   3651   6645
esx  165|   -2     1     4    28   -68   -19   .41   26   25 |  164065    -438   3649   3880
gfz  186|   -2    -1    -5   -88    62    16  -.31   27   26 |       0   -2440   3648   6546
grg  118|   -4     3    -2    32    11   203  -.03   46   45 |  199220   -2687   3725  26095
iac  n/a|    3     0     6     5    81   -73   .11   25   25 |  164588    -981   3654   7005
mcc  n/a|   -8     1    56    -5   166   263  -.05  128  128 |     ---     ---    ---    ---

Table 2.1680.5  GPS week: 1680   Day: 5   MJD: 56009                            

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  259|   -3     3     0    73    50   -33  -.14   37   36 |     ---     ---    ---    ---
emx  140|    0     0    -6   -26   -77    23  -.19   29   28 |  163563   -1310   3553   7172
esx  165|   -2    -2     0    25     7   -91   .35   20   18 |  165071   -2988   3538   3702
gfz  186|    1    -1    -2   -20    24    35  -.48   27   24 |       0   -2683   3538   7222
grg  118|    3     2    -7    17    -3   187  -.11   41   37 |  195920   -2757   3551  22868
iac  n/a|    1     0     7   -39    55    11   .11   25   25 |  163349    -946   3546   8081
mcc  n/a|    4     5    52   165   201    25   .10  105  105 |     ---     ---    ---    ---

Table 2.1680.6  GPS week: 1680   Day: 6   MJD: 56010                            

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  259|    0     1    -7    44    45   -50  -.18   34   33 |     ---     ---    ---    ---
emx  140|    1    -3    -4    -1   -16   -51  -.24   35   35 |  163831    1400   3726   7551
esx  165|   -1    -1    -4   -33    54  -107   .39   20   18 |  163180    2773   3715   3813
gfz  186|    0    -3    -7    -8   -92    27  -.34   24   20 |       0    1156   3720   7269
grg  118|   -1     0   -12     6    -1   185   .21   48   49 |  220803    2234   3533  25857
iac  n/a|    4     2    33    23    10    94   .12   32   32 |  165125     419   3760   7592
mcc  n/a|    3     5    44    49    94   108   .14   86   86 |     ---     ---    ---    ---

       
       
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 3.1680.0  GPS week: 1680   Day: 0   MJD: 56004                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  641   18   24   16   54   24   53  ---   15 |    35   52   35   48   29   38  ---    35
 R02  | 1252   27   14   15   20   42   55  ---   12 |    51   36   41   40   43   39  ---    36
 R03  |  939   26   20   13   25   75   45  ---   15 |    62   54   37   62   64   44  ---    45
 R04  |  872   23   16   23   20   61   38  ---   13 |    57   39   34   45   68   54  ---    40
 R05  | 1190   32   21   13   31   35   35  149   12 |    67   36   41   50   52   39   37    42
 R06  | 1048   25   18   11   43   31   36  ---   12 |    53   48   41   37   54   37  ---    39
 R07  | 1750   30   18   18   24   26   47  ---   11 |    60   40   35   49   32   21  ---    36
 R08  | 1691   19   15   20   18   26   35  120    9 |    57   68   69   54   54   32   65    55
 R09E | 2698   18   24   11   28   55   35  ---   12 |    48   57   47   53   78   40  ---    47
 R10E | 1453   23   46   21   14   54   38  ---   14 |    24   26   34   24   52   25  ---    20
 R11E |  875   34   52   27   41   61   49  445   19 |    81   76  117  114  122   91   65    96
 R12E |  889   24   35   16   14   31   37  ---   11 |    35   26   40   44   52   25  ---    33
 R13E | 1290   17   17   12   22   36   44  ---   10 |    33   42   45   49   50   26  ---    35
 R14E | 4155   24   32   28   17   68   62  ---   16 |    29   34   34   36   67   33  ---    28
 R15E | 2121   24   14   18   18   36   35  ---   10 |    55   53   46   40   61   50  ---    47
 R16E | 1179   17   27   25   24   33   36  ---   12 |    37   49   50   49   58   32  ---    41
 R17  | 1241   45   24   12   19   35   43  ---   12 |    53   36   31   40   38   42  ---    32
 R18  |  890   39   27   26   22   22   29  177   12 |    57   30   24   33   37   43   53    28
 R19  |  789   24   20   13   24   16   39  ---   10 |    56   38   41   48   31   47  ---    40
 R20  | 1007   47   45   17   18   37   27  ---   14 |    54   57   44   34   27   40  ---    37
 R21  |  896   90   16   36   38   42   32  ---   20 |    70   35   66   70   31   37  ---    42
 R22  | 1173   24   27   11   27   36   45  ---   12 |    59   41   27   34   22   47  ---    32
 R23  | 1103   23   15   14   15   27   60  ---   11 |    50   32   33   33   31   36  ---    31
 R24  | 2041   31   20   17   14   22   38  ---   10 |    43   29   20   23   20   27  ---    19
------+----------------------------------------------+------------------------------------------
 RMS  | 1572   33   27   19   27   42   42  258      |T   51   43   43   46   48   39   55    39
 WRMS | 1572   36   27   17   26   42   42  258      |NE  55   41   38   43   39   38   51    36
 MEDI | 1173   24   20   16   22   35   38  149      |MD  53   39   40   44   50   38   53    36

Table 3.1680.1  GPS week: 1680   Day: 1   MJD: 56005                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  894   14   29    8   15   34   14  ---    8 |    37   48   41   30   45   51  ---    37
 R02  | 1232   26   20   13   52   18   22  ---   12 |    43   45   48   78   69   52  ---    51
 R03  |  983   33   16   10   20   18   27  ---    9 |    45   33   35   29   38   28  ---    29
 R04  | 1645   29   21   13   48   62   34  ---   15 |    49   40   45   86   99   27  ---    48
 R05  | 1420   30   25   18   26   36   15  158   10 |    57   43   50   62   52   45   25    46
 R06  | 1012   17   26   16   39   51   19  ---   12 |    44   55   35   45   41   41  ---    36
 R07  | 1521   48   21   11   23   48   21  ---   12 |    41   19   34   29   50   31  ---    25
 R08  |  860   35   36   24   21   34   20   71   12 |    45   50   48   49   52   39   60    40
 R09E | 3264   20   25   21   25   53   24  ---   12 |    31   48   40   39   67   35  ---    34
 R10E | 1435   17   23   15   20   32   17  ---    9 |    24   27   30   34   32   27  ---    23
 R11E | 1545   53   45   32   40   52   29  443   17 |    66   69  105  104   95   70   36    83
 R12E |  960   18   33   10   16   17   16  ---    8 |    24   30   28   40   32   38  ---    27
 R13E | 1312   18   44   12   17   30   21  ---   10 |    29   43   33   36   34   22  ---    27
 R14E | 1391   38   38   28   20   58   26  ---   15 |    27   32   45   40   78   31  ---    30
 R15E | 3624   21   23   16   15   30   16  ---    8 |    49   31   46   34   30   45  ---    36
 R16E | 1004   25   29   16   25   30   15  ---   10 |    24   30   33   37   50   33  ---    27
 R17  |  785   45   22   20   29   46   20   98   13 |    42   37   46   58   43   28   21    36
 R18  |  739   42   13   21   14   30   20  128   10 |    42   31   29   37   45   31   57    29
 R19  | 1264   36   18   13   17   21   20  ---    9 |    34   31   21   32   26   43  ---    22
 R20  | 1796   62   72   12   20   21   38  ---   17 |    43   50   27   25   22   44  ---    23
XR21  |>>>>>   83  ---   32   34  ---   39  ---   25 |    39  ---   46   48  ---   29  ---    28
 R22  |  785   49   30   17   23   25   15  ---   11 |    39   42   31   44   44   35  ---    29
 R23  |  735   29   27   10   15   24   13  ---    8 |    35   28   28   38   34   45  ---    29
 R24  |  939   39   30   13   15   23   12  ---    9 |    40   56   30   32   32   37  ---    30
------+----------------------------------------------+------------------------------------------
 RMS  | 1531   35   31   17   26   37   22  225      |T   39   39   39   45   48   37   39    34
 WRMS | 1531   35   34   16   30   35   22  225      |NE  42   40   37   45   46   37   40    33
 MEDI | 1232   30   26   15   20   30   20  128      |MD  40   40   35   38   44   35   36    29

Table 3.1680.2  GPS week: 1680   Day: 2   MJD: 56006                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  904   12   40    8   26   35   20  ---   10 |    41   53   45   77   41   45  ---    48
 R02  | 1215   27   15   12   12   25   16  ---    7 |    43   42   36   39   37   25  ---    32
 R03  |  587   30   15   17   13   18   16  ---    8 |    51   39   28   27   32   50  ---    33
 R04  | 1145   31   23   14   29   23   23  ---   10 |    46   38   36   24   47   24  ---    27
 R05  | 1040   36   16   16   34   55   28  142   13 |    64   54   49   86   94   42   42    56
 R06  | 1254   25   19   16   12  111   13  ---   16 |    47   36   34   43  103   37  ---    34
 R07  | 1037   33   24   16   27   55   12  ---   11 |    49   33   48   39   53   34  ---    35
 R08  | 1018   28   22   10   23   23   15   47    8 |    43   34   23   21   32   28   43    23
 R09E | 3561   23   33   13   16   36   19  ---    9 |    23   33   35   26   52   33  ---    28
 R10E | 1307   27   20   13   23   29   21  ---    9 |    31   33   29   32   52   31  ---    27
 R11E | 1160   52   91   41   50   64   38  447   24 |    63   76   87  100  102   64   67    73
 R12E |  599   21   28   16   29   26   22  ---   10 |    29   21   38   44   42   24  ---    29
 R13E | 1712   28   39   18   16   46   19  ---   11 |    37   33   39   40   50   31  ---    31
 R14E | 1012   45   36   20   24   74   26  ---   15 |    58   49   63   53   71   51  ---    49
 R15E | 3401   23   25   11   16   30   22  ---    9 |    40   49   46   36   41   42  ---    38
 R16E |  884   26   27   20   16   29   18  ---    9 |    31   38   45   46   45   37  ---    37
 R17  |  697   40   36   15   14   26   14   64   10 |    48   64   40   44   43   28   21    38
 R18  |  834   36   19   26   15   34   26  105   11 |    42   25   27   25   48   35   45    25
 R19  |  465   35   20   14   17   49   26  ---   11 |    55   42   38   46   31   55  ---    42
 R20  | 2501   46  111   18   41   45   23  ---   22 |    50   53   30   54   51   25  ---    29
XR21  |  746   60  ---   20   22  ---   26  ---   17 |    44  ---   37   47  ---   34  ---    31
 R22  |  631   54   21   17   19   24   15  ---   11 |    50   27   22   27   33   23  ---    19
 R23  |  679   40   34   12   17   24   15  ---   10 |    53   42   29   44   44   38  ---    35
 R24  | 1307   29   27   11   18   34   16  ---    9 |    34   31   39   45   27   23  ---    30
------+----------------------------------------------+------------------------------------------
 RMS  | 1494   34   39   17   24   45   21  218      |T   44   41   39   44   50   35   43    35
 WRMS | 1494   33   42   16   20   38   21  218      |NE  47   40   35   43   47   34   37    33
 MEDI | 1018   30   25   16   18   34   19  105      |MD  44   38   37   43   45   34   43    32

Table 3.1680.3  GPS week: 1680   Day: 3   MJD: 56007                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 2126   40   35   15   70   33   31  ---   17 |    29   58   39   62   42   44  ---    36
 R02  | 1259   38   11   30   22   28   24  ---   12 |    53   49   64   69   64   42  ---    52
 R03  |  804   20   13   11   15   33   16  ---    8 |    55   55   62   66   32   51  ---    53
 R04  | 1738   29   20   15   22   43   18  ---   10 |    57   52   50   56   39   61  ---    49
XR05  |  947   43   27   19   26  ---   23  127   13 |    58   41   23   30  ---   42   43    31
 R06  | 1307   25   34   23   30   83   24  ---   16 |    64   88   77   77   70   52  ---    64
 R07  | 1230   36   21   18   15   53   21  ---   12 |    58   41   41   48   96   37  ---    44
 R08  | 1241   26   18   15   21   41   19   99   10 |    60   64   58   60   70   55  117    58
 R09E | 3676   26   25   19   33   32   19  ---   11 |    27   31   44   47   59   42  ---    35
 R10E | 1342   19   21   12   19   49   17  ---   10 |    21   28   32   23   38   27  ---    18
 R11E | 1964   48   85   46   48   73   47  360   25 |    70   85  107  103  126   74   93    83
 R12E |  854   21   27   19   21   34   29  ---   11 |    33   41   31   41   58   32  ---    32
 R13E | 1173   23   38   13   29   57   28  ---   14 |    48   62   64   79   88   41  ---    57
 R14E | 1300   32   37   26   22   33   29  ---   13 |    45   53   72   63   44   41  ---    50
 R15E | 1157   27   40   17   28   30   33  ---   13 |    48   41   54   63   59   47  ---    46
 R16E |  916   22   28   23   30   29   21  ---   11 |    26   47   45   47   39   29  ---    34
 R17  | 1217   29   24   15   18   20   12   55    8 |    52   37   29   29   35   28   38    27
 R18  | 4479   29   26   22   25   22   24   76   11 |    47   43   37   42   40   38  107    33
 R19  | 1441   33   22   14   14   50   18  ---   11 |    45   28   19   27   37   32  ---    21
 R20  | 3515   61   78   20   35   26   36  ---   19 |    68   54   46   71   75   49  ---    52
 R21  | 1187   68   39   28   26   41   12  ---   16 |    58   45   43   33   62   35  ---    31
 R22  |  622   44   26   20   22   13   21  ---   11 |    66   43   48   63   48   48  ---    49
 R23  |  858   37   15   15   15   18   12  ---    8 |    45   30   20   34   36   26  ---    24
 R24  | 1456   48   34   20   22   49   27  ---   14 |    57   64   41   59   66   41  ---    45
------+----------------------------------------------+------------------------------------------
 RMS  | 1869   36   36   21   29   42   25  192      |T   49   49   47   53   57   42   79    42
 WRMS | 1869   34   38   19   23   34   25  192      |NE  54   49   43   51   54   42   76    41
 MEDI | 1241   29   26   19   22   33   21   99      |MD  52   45   44   56   58   41   93    44

Table 3.1680.4  GPS week: 1680   Day: 4   MJD: 56008                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 2239   25   37   31   32   45   26  ---   14 |    34   61   45   44   53   48  ---    41
 R02  | 1112   29   15   19   29   38   25  ---   11 |    43   31   31   28   41   43  ---    27
 R03  |  744   26   29   37   34   59   30  ---   15 |    47   52   35   58   37   57  ---    37
 R04  | 1684   15   22   12   30   38   30  ---   11 |    48   48   43   60   33   65  ---    46
 R05  |  946   28   30   18   45   26   19  143   13 |    51   58   50   76   49   43   57    51
 R06  | 1008   23   52   33   24   59   25  ---   15 |    47   71   43   24   28   31  ---    30
 R07  | 1203   36   30   16   26   54   26  ---   13 |    49   57   40   48   59   30  ---    37
 R08  | 1532   20   23   33   23   58   17   75   12 |    52   52   39   60   63   48   63    43
 R09E | 2307   17   31   19   27   38   19  ---   11 |    28   40   45   39   56   32  ---    32
 R10E | 1678   18   18   29   16   71   15  ---   13 |    26   35   28   33   95   34  ---    32
 R11E | 2722   49   70   49   33   64   40  154   22 |    66   71  106   70  107   70  221    73
 R12E |  751   19   30   22   22   45   18  ---   11 |    23   29   38   38   49   27  ---    26
 R13E | 1863   24   36   20   22   31   17  ---   11 |    45   46   44   45   50   37  ---    37
 R14E | 4129   17   43   26   25   31   24  ---   12 |    77   69   90   91  100   73  ---    80
 R15E | 1532   37   22   18   25   37   50  ---   15 |    63   65   64   86   70   49  ---    61
 R16E |  657   24   33   24   20   36   18  ---   11 |    29   32   41   47   57   25  ---    30
 R17  | 1997   34   20   27   26   36   15   74   11 |    46   47   36   40   40   39   38    35
 R18  | 4211   31   37   18   18   42   20  164   12 |    38   38   27   22   23   34   66    24
 R19  |  821   29   29   23   26   37   23  ---   12 |    55   58   68   53   64   51  ---    53
 R20  | 2693   59   82   27   37   56   27  ---   21 |    48   35   32   37   44   36  ---    29
 R21  | 1898   73   36   35   23   53   18  ---   18 |    63   48   44   47   32   42  ---    38
 R22  |  809   44   24   23   27   29   21  ---   12 |    52   22   38   38   55   32  ---    33
 R23  | 1399   30   41   20   24   23   22  ---   12 |    51   33   47   61   70   48  ---    48
XR24  | 1671   45   31   36   30  ---   18  ---   16 |    35   42   37   32  ---   27  ---    19
------+----------------------------------------------+------------------------------------------
 RMS  | 1985   34   38   26   27   46   25  128      |T   46   47   46   49   55   42   89    40
 WRMS | 1985   35   35   25   26   45   25  128      |NE  47   47   40   45   46   42   56    36
 MEDI | 1532   28   30   23   26   38   21  143      |MD  47   47   41   45   53   39   63    37

Table 3.1680.5  GPS week: 1680   Day: 5   MJD: 56009                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1046   22   31   15   24   65   29  ---   13 |    17   43   32   51   75   21  ---    32
 R02  | 1199   25   16   16   17   52   28  ---   11 |    35   43   28   46   49   46  ---    32
 R03  | 1202   32   18   19   33   40   27  ---   12 |    37   33   33   28   39   41  ---    25
 R04  | 1003   24   36   21   28   35   28  ---   12 |    39   39   52   54   54   53  ---    43
 R05  | 1512   28   29   17   45   23   18  117   12 |    37   36   43   68   39   30   30    38
 R06  | 1542   14   14   12   16   26   18  ---    7 |    48   58   54   43   63   55  ---    50
 R07  |  826   50   31   20   23   41   19  ---   13 |    39   43   41   37   46   24  ---    29
 R08  | 3192   32   28   18   29   46   25   33   12 |    43   49   40   65   57   23   48    39
 R09E |  824   32   33   15   17   36   23  ---   11 |    29   32   36   39   45   30  ---    27
 R10E | 1186   36   32   14   11   27   31  ---   11 |    39   42   34   35   38   31  ---    31
 R11E | 3134   45   46   46   53   33   40  120   20 |    63   72   91   85   71   64  114    70
 R12E | 1305   19   29   18   18   30   12  ---    9 |    21   31   30   24   39   21  ---    20
 R13E | 3038   19   21   12   23   35   28  ---   10 |    34   41   37   46   55   31  ---    33
 R14E | 3184   31   43   18   24   57   30  ---   14 |    73   80   74   69  130   79  ---    75
 R15E | 1915   26   18   10   27   34   27  ---   10 |    64   66   59   62   83   42  ---    57
 R16E |  576   23   28   14   19   41   19  ---   10 |    16   20   32   35   44   19  ---    22
 R17  | 2215   41   19   17   23   28   28   74   11 |    43   41   41   36   37   26   30    31
 R18  | 2529   56   14   15   28   38   17  144   12 |    42   25   35   40   31   33   59    28
 R19  |  822   24   34   13   17   29   15  ---    9 |    40   44   49   45   61   44  ---    42
 R20  | 1469   63   47   32   30   65   36  ---   19 |    43   63   51   39   39   43  ---    40
 R21  | 1873   70   21   29   31   47   19  ---   15 |    66   33   35   53   31   35  ---    34
 R22  |  941   53   21   11   22   43   14  ---   11 |    56   34   47   55   55   34  ---    41
 R23  | 1394   28   21   15   26   41   25  ---   11 |    43   35   34   47   65   42  ---    37
 R24  | 1331   33   28   17   27   39   13  ---   11 |    41   44   34   53   46   44  ---    37
------+----------------------------------------------+------------------------------------------
 RMS  | 1823   37   29   20   27   41   25  105      |T   42   43   43   48   53   37   56    38
 WRMS | 1823   36   28   18   24   37   25  105      |NE  41   41   40   47   49   37   41    36
 MEDI | 1331   31   28   16   24   38   25  117      |MD  40   41   37   46   46   34   48    34

Table 3.1680.6  GPS week: 1680   Day: 6   MJD: 56010                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  989   20   10   14   20   64   24  ---   11 |    36   54   37   43   63   41  ---    37
 R02  | 1145   22   15   19   23   93   29  ---   15 |    46   37   30   50   77   46  ---    37
 R03  | 1121   33   14   12   21   33   22  ---    9 |    58   41   28   34   42   45  ---    35
 R04  |  732   31   29   24   21   55   24  ---   13 |    52   42   42   42   46   46  ---    40
 R05  | 1936   30   22   17   37   37   26   96   12 |    53   40   40   48   36   41   41    38
 R06  | 2333   15   12    9   17   52   20  ---    9 |    52   50   50   49   33   54  ---    45
 R07  |  816   22   23   11   15   35   17  ---    8 |    60   44   41   53   36   38  ---    41
 R08  | 2693   40   44    9   50   28   34   73   16 |    58   55   36   59   41   37   46    38
 R09E | 1243   21   41   16   28   40   23  ---   12 |    36   34   44   49   61   46  ---    41
 R10E | 1521   37   41   17   20   21   32  ---   12 |    28   39   37   36   31   26  ---    27
 R11E | 2469   39   61   40   35   64   37  103   20 |    77   81  106   93  105   78  111    86
 R12E | 1395   18   19   11   17   40   21  ---    8 |    26   19   32   36   47   29  ---    27
 R13E | 3496   23   16   11   21   46   29  ---   10 |    47   38   43   49   44   58  ---    42
 R14E | 1543   24   40   23   28   71   37  ---   15 |    82   79   93  102   72   68  ---    81
 R15E |  986   21   24   19   20   37   25  ---   10 |    47   62   62   53   72   47  ---    53
 R16E |  885   25   31   13   26   23   15  ---   10 |    19   35   43   46   52   27  ---    35
 R17  | 1668   37   19   18   14   34   27   68   10 |    60   36   35   38   30   42   34    35
XR18  | 2094   47   23   16   26  ---   28  101   13 |    57   32   24   25  ---   31   42    24
 R19  |  922   40   12   13   20   31   23  ---   10 |    55   31   28   28   31   37  ---    28
 R20  | 1398   59   97   16   13   44   49  ---   22 |    49   44   44   43   31   40  ---    37
 R21  | 1124   63   22   23   19   30   35  ---   14 |    86   57   68   59   51   37  ---    55
 R22  | 1104   42   28   28   17   69   14  ---   14 |    65   35   45   44   44   43  ---    41
 R23  | 1605   31   19   21   12   37   24  ---   10 |    51   32   26   41   38   35  ---    32
 R24  | 1116   37   35   34   18   53   83  ---   20 |    44   36   35   38   33  104  ---    39
------+----------------------------------------------+------------------------------------------
 RMS  | 1633   34   35   20   24   48   32   86      |T   51   43   44   48   48   45   54    41
 WRMS | 1633   33   35   18   20   49   32   86      |NE  55   41   38   43   42   44   40    37
 MEDI | 1243   31   23   16   20   40   25   96      |MD  52   39   40   44   44   41   42    38




More information about the IGSREPORT mailing list