[IGSREPORT-25669] Wk 1979 IGLOS Final Orbits

acc acc at igs.org
Sat Dec 30 02:24:52 PST 2017


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1979   (Dec 10, 2017 - Dec 16, 2017) 
                                                                               
Contact: acc at igs.org
                                                                               
                                                                               
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 2.1979.
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:
                                                                               
 igl1979[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1979 in the SP3 format.
 igl19797.sum      Combination Report for GPS Week 1979.


    
    
REMARKS concerning the IGL Orbit Combination:                                  
---------------------------------------------

Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.

 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
    
    Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
    model file has been updated to igs14.atx to be consistent with IGS14.
    See IGSMAIL #7399 for more information
        ftp://igs.org/pub/station/general/igs14.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  |     52.5 ns
                1  |     54.1 ns
                2  |     51.4 ns
                3  |     47.8 ns
                4  |     45.8 ns
                5  |     44.6 ns
                6  |     24.3 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  |  IAC   | R22

    
         
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 1.1979, 1a.1979).
        
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 2.1979.0-6)                                                                                
    
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 3.1979.0-6). 
        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 1979 summary.                      (Dec 10, 2017 - Dec 16, 2017)

Table 1.1979.a     GPS week : 1979   MJD: 58097.0-58103.0

         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  n/a|    0     0    -1    -3     2    52   .14   23   20 |    6567     858   2975   9592
        |    0     1     2    14    20    15   .08           |    8619    1425
cof  n/a|   -1     0     0    -9    -2    49   .13   26   22 |    6559     860   2976   9595
        |    1     1     3    15    14    39   .09           |    8625    1435
emx  n/a|    0    -1     2   -16   -37     6  -.03   21   21 |   41344     728   2976   9033
        |    1     0     2    22    23    31   .07           |   12446     712
esx  n/a|    0     0     1     6     8     7   .19   19   17 |   46237    1486   2978  11580
        |    1     0     1    21     8    18   .04           |   14985    1253
gfz  n/a|   -2     0    -7     9    28    45   .08   24   18 |       0     963   2966   9185
        |    1     1     1    13    12    18   .15           |       0    1930
grg  n/a|    0     0    -1   -55   -21  -122  -.36   27   26 |   45229     946   3034   8864
        |    1     1     5    11    38    47   .09           |   10278    1295
iac  n/a|    1     0     3    53     1   -27  -.17   28   23 |   47204    -691   2988   8865
        |    1     0     3    12    17    53   .07           |   10436    1426
mcc  n/a|    3    -3     4    95    15   418   .04  207  207 |     ---     ---    ---    ---
        |    7     6    16   172   161   391   .66           |     ---     ---


Table 1.1979.b     GPS week : 1979   MJD: 58097.0-58103.0   

         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  |    8    9    8    7    9   11   11 |
 R02  |    6    6    7    7    8    8    6 |
 R03  |    6    7    7    7    6    6    5 |
 R04  |    5    7    8    5    6    8    9 |
 R05  |   13   14   19   18   15   14   16 |
 R06  |   10    9    7   12    9   12   13 |
 R07  |    8    8    7    8   11    9   10 |
 R08  |    8    7    7    7    7    7    8 |
 R09  |    7    6    8    8    7    8    7 |
 R10  |    7    7    7    7    6    8    8 |
 R11  |    9    7    9    8    7    8    7 |
 R13  |    8    7    9    8    8    9    7 |
 R14  |   10    9   21   17   10   10    9 |
 R15  |   18   18   15   18   13   14   13 |
 R16  |   14   11   12   17   13   12   13 |
 R17  |    7    7    8   10   10    8    9 |
 R18  |    8    8   11    8    7   10    8 |
 R19  |   12   11   11   13   13   13   14 |
 R20  |   14   13   14   13   15   14   13 |
 R21  |   10    8   10    9    8   10   10 |
 R22  |   11   11    9   10    9    9   10 |
 R23  |    9   10    8   10   10   11   15 |
 R24  |   14   15   14   10   15   14   19 |
 R26  |   20   23   28   32   25   19   30 |


Table 1.1979.c     GPS week : 1979   MJD: 58097.0-58103.0   

         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 1979 0   |   35  -117  -132    -885    -211   -2271  83.7  1401  1401 |   52455       0
brd 1979 1   |  -48    69   -44   -1401    -332   -3415  84.2  1306  1306 |   54050       0
brd 1979 2   |  -31    40   -13    -538     194   -4515  85.3  1331  1331 |   51431       0
brd 1979 3   |  -24   -69    18    1243     792   -5426  84.7  1486  1486 |   47822       0
brd 1979 4   |  -43    17    10      70    -266   -3735  82.7  1342  1342 |   45795       0
brd 1979 5   |  -30   -23    20   -1128     332   -5571  83.8  1627  1627 |   44558       0
brd 1979 6   |  -33   -63    22     286       9   -3034  81.9  1498  1498 |   24299       0
-------------+------------------------------------------------------------+----------------
brd 1979 mean|  -25   -20   -17    -336      74   -3995  83.8  1427  1427 |   45772       0
brd 1979 sdev|   27    66    56     926     400    1231   1.2   115   115 |   10099       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 2.1979.0  GPS week: 1979   Day: 0   MJD: 58097                            

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  n/a|    0     0    -1     6   -27    46   .14   18   14 |    8667    2443   2720   9341
cof  n/a|    0     1    -2     0   -21    23   .08   22   16 |    8660    2448   2723   9347
emx  n/a|    0    -2     2   -50   -40    22  -.02   19   19 |   46528    1910   2716   8715
esx  n/a|    0     0     0    36     9    -2   .19   21   18 |   55080    3291   2705  11186
gfz  n/a|   -1    -1    -8    15    36    28  -.07   21   19 |       0    2553   2668   9099
grg  n/a|    0     0     2   -75    34   -62  -.31   24   22 |   51280    2235   2732   8221
iac  n/a|    2     0     5    70    -5   -46  -.17   63   22 |   54230    -283   2850   8551
mcc  n/a|   14    -1     0   129   138   295   .26  157  157 |     ---     ---    ---    ---

Table 2.1979.1  GPS week: 1979   Day: 1   MJD: 58098                            

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  n/a|   -1     0    -4    -1     1    41   .22   24   25 |   12921     126   3031  10294
cof  n/a|   -3     1    -4     0     6    -3   .04   29   27 |   12891     153   3036  10285
emx  n/a|    0    -2     4   -28   -62    -4  -.01   20   20 |   47468     772   3033   9844
esx  n/a|    0     0     0    17     5   -13   .22   18   17 |   65835     819   3046  12478
gfz  n/a|   -2    -1    -5    16    20    70  -.10   25   18 |       0    -838   3056   9346
grg  n/a|    0     1    -2   -51    -7  -121  -.29   25   24 |   53871     249   3071   9288
iac  n/a|    1     0     4    46    35    22  -.17   23   21 |   56395   -2931   2965   9475
mcc  n/a|    2     6     7   -43   136  1195   .38  206  206 |     ---     ---    ---    ---

Table 2.1979.2  GPS week: 1979   Day: 2   MJD: 58099                            

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  n/a|    0     0    -6    17   -10    69   .20   25   21 |   11198    2071   3058   9981
cof  n/a|   -2     0    -2    -4   -10    79   .24   26   21 |   11194    2056   3058   9982
emx  n/a|    0     0     4   -12   -63   -41   .04   23   23 |   36327    1281   3074   9432
esx  n/a|    0     0     3     0    14    11   .20   18   16 |   41300    2384   3044  12419
gfz  n/a|    0     1    -5     9    20    60   .17   21   17 |       0    3519   3011   9774
grg  n/a|    1     0     1   -60    11  -122  -.31   24   20 |   50335    2098   3112   9279
iac  n/a|    1     0     0    49     4    62  -.18   24   23 |   52187     206   3058   9273
mcc  n/a|    2    -7   -14   120    99   279  -.98  203  203 |     ---     ---    ---    ---

Table 2.1979.3  GPS week: 1979   Day: 3   MJD: 58100                            

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  n/a|   -1    -1     1    -3    20    62   .06   23   22 |   10644   -1813   2778  10210
cof  n/a|   -2     0     3   -18     5    96  -.00   29   25 |   10662   -1854   2783  10200
emx  n/a|    0    -2     2    16   -49    41  -.09   25   25 |   55994    -138   2784   9704
esx  n/a|    3     0     0   -28    24     7   .25   19   18 |   46563     166   2781  12143
gfz  n/a|   -3     1    -8   -19    51    33   .07   22   18 |       0   -2058   2784   9746
grg  n/a|   -1     1    -1   -38   -80  -208  -.30   30   28 |   48559   -1438   2793   8812
iac  n/a|    3     0     5    60   -15   -56  -.29   23   25 |   49911   -2478   2815   9486
mcc  n/a|    1    -3    15  -166   -56   -74  -.60  193  193 |     ---     ---    ---    ---

Table 2.1979.4  GPS week: 1979   Day: 4   MJD: 58101                            

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  n/a|    0    -1     0   -16    -6    25   .04   21   16 |    7361    1249   2871   9192
cof  n/a|    0     0     2   -17   -11    21   .21   21   17 |    7364    1263   2869   9201
emx  n/a|    2    -1     0     5     0   -26  -.03   20   20 |   43836     416   2878   8708
esx  n/a|   -1     1     4    -4     0    38   .15   18   17 |   57568    2080   2882  11326
gfz  n/a|   -3     0    -8     8    16    62   .27   24   18 |       0    1662   2851   8804
grg  n/a|    0     0   -11   -51   -24   -85  -.35   27   25 |   45117    1258   2910   7910
iac  n/a|    1     0     8    57   -13   -50  -.19   22   23 |   46626     225   2870   8478
mcc  n/a|   10     1    28    66   169   255  -.18  181  181 |     ---     ---    ---    ---

Table 2.1979.5  GPS week: 1979   Day: 5   MJD: 58102                            

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  n/a|   -1     1    -1     0     2    56   .09   25   23 |    7619     539   2984   9528
cof  n/a|   -1     0    -3    12    -5    34   .19   26   24 |    7609     555   2982   9542
emx  n/a|    1    -1     0   -29   -20    21  -.14   24   24 |   42753      32   2964   9036
esx  n/a|    0     1     0     0    10    20   .20   18   17 |   36210    -159   2991  11317
gfz  n/a|   -1     0    -9    20    21    25   .25   26   15 |       0     486   2982   9262
grg  n/a|   -2    -2     6   -60   -31  -153  -.44   29   30 |   44221     495   3082   8690
iac  n/a|    0    -2     3    60    -5   -27  -.13   20   21 |   45914    -323   2967   8874
mcc  n/a|   -7    -7    10   186  -248   474   .48  224  224 |     ---     ---    ---    ---

Table 2.1979.6  GPS week: 1979   Day: 6   MJD: 58103                            

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  n/a|    0    -2     0   -25    34    63   .26   26   23 |  -12438    1397   3388   8604
cof  n/a|   -1    -2     2   -35    20    91   .17   28   26 |  -12462    1400   3383   8614
emx  n/a|    2    -1     4   -15   -23    34   .03   18   18 |   16502     829   3388   7794
esx  n/a|    0     0     1    26    -1   -10   .13   22   18 |   21105    1825   3400  10195
gfz  n/a|   -2     1    -5    14    29    35  -.03   27   22 |       0    1417   3413   8267
grg  n/a|   -2     0    -4   -51   -53  -102  -.52   30   31 |   23220    1726   3541   9852
iac  n/a|    0     0     0    32     7   -95  -.06   23   24 |   25170     743   3392   7918
mcc  n/a|    0   -14   -15   378  -127   504   .91  286  286 |     ---     ---    ---    ---

       
       
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 3.1979.0  GPS week: 1979   Day: 0   MJD: 58097                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01  |  501   16   14   19   18   12   22   23  ---    8 |    64   68   69   58   68   75   51  ---    62
 R02  | 1259   12   15    9   15   14   17   13  135    6 |    58   56   57   48   53   57   50  154    53
 R03  | 1127    8   12   10   10   14   18   15  135    5 |    62   65   65   61   66   55   62  102    61
 R04  |  543    9   15   10   14    8   11   11  ---    4 |    56   54   58   53   57   60   54  ---    55
 R05  | 1166   27   19   26   27   12   40   31  ---   12 |    63   67   82   72   65   68   61  ---    65
 R06  |  761   10   12   17   24   19   31   29  ---    9 |    30   31   30   41   35   36   36  ---    29
 R07  |  764   12   14   14    8   13   26   27  133    7 |    62   61   64   56   60   50   53  107    56
 R08  | 1008   17   20   11   26   16   18   16  ---    8 |    58   59   61   70   67   56   55  ---    60
 R09  | 4317   13   14   10   18   20   13   21  ---    7 |    78   76   78   74   78   82   75  ---    76
 R10  | 2076    8   10   10   14   22   16   14  ---    6 |    68   69   62   76   53   62   65  ---    64
 R11  | 1057   21   21   11   16   19   20   29  259    8 |    74   76   67   78   62   66   68   87    68
 R13  |  960   15   17   16   25    8   17   28  ---    8 |    51   48   42   65   46   44   63  ---    50
XR14  | 9545   20   25   16   12   19  ---   27  ---    9 |   177  181  168  179  173  ---  177  ---   174
XR15  |  999   50   47   20   36  ---   30   31  ---   17 |    95   96   56   65  ---   52   44  ---    59
 R16  |  555   28   57   32   29   25   43   25  ---   13 |    68   95   55   67   64   51   59  ---    56
 R17E |  929   17   18   14   12   14   23   12  ---    7 |    64   66   63   69   68   64   60  ---    63
 R18E | 1308   12   11   14   23   14   20   21  ---    7 |    46   46   43   54   46   48   46  ---    45
 R19E | 1312   25   31   30   12   26   22   42  ---   12 |    45   50   48   40   42   48   52  ---    41
 R20E |  769   23   31   30   25   34   26   48  ---   14 |    41   53   44   56   64   49   55  ---    45
 R21E |  799   23   16   20   18   28   15   16   50    9 |    45   45   36   51   50   43   44   64    43
 R22E | 1204   18   16   23   14   25   24  267  ---   10 |    44   40   45   42   47   46  132  ---    41
 R23E | 1004   18   13   16   25   21   13   20  ---    8 |    72   76   82   77   79   76   86  ---    77
 R24E | 1000   21   31   22   36   36   42   34  ---   14 |    93   96   96  100  108   95   90  ---    94
XR26E | ----   15  112  ---  ---  ---  ---   25  ---   20 |    58  119  ---  ---  ---  ---   59  ---    55
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1401   18   22   19   21   21   24   63  157      |T   65   70   63   67   65   58   66  102    62
 WRMS | 1401   14   16   19   18   19   22   22  157      |NE  70   73   67   70   67   58   64  112    65
 MEDI | 1004   17   16   16   18   19   20   25  135      |MD  62   65   61   65   62   55   59  102    56

Table 3.1979.1  GPS week: 1979   Day: 1   MJD: 58098                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01  |  704   19   18   21   20   15   14   19  ---    8 |    44   43   46   32   36   41   26  ---    34
 R02  | 1146   15   18   13    9   17   12   15  224    6 |    38   40   36   36   44   42   31  104    36
 R03  |  777   17   33   13    9   14   25   12  149    6 |    45   51   38   31   34   27   37   88    33
 R04  |  936    8   14   15   11   14   22   17  ---    6 |    36   42   41   41   42   27   29  ---    34
 R05  |  825   48   60   29   18   28   22   32  ---   13 |    42   47   51   48   63   55   52  ---    49
 R06  |  743   21   16   16   27   12   19   13  ---    8 |    20   26   22   48   28   20   33  ---    26
 R07  | 1489   11   19   18   10   23   20   16  269    7 |    43   50   44   37   30   52   40  190    38
 R08  | 1166   17   22   10   13   16   22   16  ---    7 |    42   45   37   46   46   36   38  ---    39
 R09  | 3522   12   16   11   11   17   15   18  ---    6 |    49   51   63   49   54   47   49  ---    48
XR10  | 1360    8    9   16   13  ---   14    9  ---    6 |    59   57   57   66  ---   46   61  ---    57
 R11  | 1030   16   17   11   11   18   23   18  241    7 |    73   75   77   77   74   87   72   68    75
 R13  |  833   13   16   17   18   15   17   14  ---    7 |    47   54   43   58   47   46   48  ---    47
XR14  | 5690   19   15   13   12   23  ---   18  ---    8 |   120  118  122  122  109  ---  130  ---   120
 R15  | 1092   61   60   31   28   53   30   39  ---   18 |    71   72   50   54   41   50   27  ---    44
 R16  |  586   26   44   25   17   33   31   19  ---   11 |    75   83   67   76   65   52   62  ---    64
 R17E | 1795   18   19   17   11   18   16   16  ---    7 |    55   58   55   60   63   65   56  ---    57
 R18E | 1252    8   13   11   21   16   29   14  ---    8 |    31   35   29   40   29   37   30  ---    31
 R19E |  795   34   35   19   16   29   24   27  ---   11 |    48   48   38   42   42   40   40  ---    37
 R20E |  979   24   26   28   19   45   25   25  ---   12 |    43   41   43   53   58   46   45  ---    41
 R21E | 1771   21   21   18   11   25   20   17   95    8 |    37   37   27   34   32   33   34   56    29
 R22E | 1003   21   15   23   15   25   23   34  ---   10 |    38   37   31   44   47   32   84  ---    35
 R23E |  779   14   22   17   18   22   40   23  ---   10 |    60   57   66   71   70   51   79  ---    65
 R24E |  941   16   30   28   33   26   49   37  ---   14 |    82   92   85   98   95   75   94  ---    84
XR26E | ----   24   91  ---  ---  ---  ---   21  ---   23 |    58  101  ---  ---  ---  ---   42  ---    46
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1306   24   29   20   18   25   25   23  206      |T   52   56   50   54   52   45   51  101    48
 WRMS | 1306   25   27   20   17   18   24   21  206      |NE  53   56   52   54   50   44   49  112    49
 MEDI | 1003   17   19   17   15   18   22   18  224      |MD  45   50   44   48   46   46   42   88    41

Table 3.1979.2  GPS week: 1979   Day: 2   MJD: 58099                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01  |  584   27   24   17   11   14   12   20  ---    7 |    62   48   44   40   49   43   37  ---    42
 R02  | 1544   14   13   11    7   10   15   26  308    6 |    49   45   43   41   41   48   32  184    41
 R03  | 1936   14   15   16    9   16   15   20  154    6 |    53   55   51   44   43   37   46   82    44
 R04  | 1021   21   16   17   21   11   14   14  ---    7 |    47   46   44   37   43   43   37  ---    38
 R05  |  538   48   36   30   26   36   62   46  ---   19 |    51   60   65   49   74   81   34  ---    55
 R06  | 1197   11   13   15   16   15   12   25  ---    7 |    21   22   25   29   24   28   30  ---    21
 R07  |  950   18   18   14   13   18   18   15  ---    7 |    45   45   50   59   59   40   52  ---    49
 R08  |  753   16   19   14   12   12    9   23  ---    6 |    47   49   50   44   42   45   32  ---    42
XR09  | 2640   18   21  ---   12   12   16   18  ---    7 |    57   56  ---   52   57   67   53  ---    56
 R10  | 1020    9   22   16   16   16   15   15  ---    6 |    50   60   49   56   58   53   48  ---    50
 R11  |  560   22   20   17   16   17   16   25  195    8 |    83   82   81   82   77   72   60   66    75
 R13  | 1544   15   15   21   22   16   24   14  ---    8 |    71   66   63   72   59   56   61  ---    62
XR14  | 4637   42   34   33   18   22  ---   80  ---   21 |   465  470  466  461  461  ---  441  ---   458
 R15  | 2272   61   64   25   21   36   25   27  ---   15 |    78   84   53   45   40   51   31  ---    43
 R16  |  523   23   26   34   22   18   35   25  ---   12 |    86   83   80   83   83   76   81  ---    78
 R17E | 2348   20   17   20   16   22   15   15  ---    8 |    49   47   51   57   57   45   49  ---    50
 R18E | 1130   13   18   42   20   20   23   17  ---   11 |    38   38   51   42   37   34   44  ---    35
 R19E | 1353   32   43   26   16   29   24   24  ---   11 |    47   56   37   45   58   43   53  ---    43
 R20E |  758   24   23   33   35   30   27   32  ---   13 |    42   45   54   65   65   44   38  ---    47
 R21E | 2175   21   18   23   13   20   23   32   92   10 |    38   39   39   40   40   40   47   45    36
 R22E |  981   22   18   19   10   20   14   27  ---    8 |    38   38   23   37   36   30   43  ---    31
 R23E |  805   16   22   17   16   12   22   16  ---    7 |    50   49   58   57   55   43   65  ---    52
XR24E | 1995   19   23   23   20  ---   28   44  ---   13 |    49   48   61   52  ---   56   76  ---    54
XR26E | ----   25   60  ---  ---  ---  ---   31  ---   28 |    41   96  ---  ---  ---  ---   60  ---    50
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1331   25   26   23   18   21   24   24  203      |T   69   71   69   69   70   48   64   94    64
 WRMS | 1331   21   21   23   16   17   20   23  203      |NE  84   84   83   79   80   52   71  110    76
 MEDI | 1130   20   20   19   16   17   16   24  154      |MD  49   49   51   49   55   44   47   66    47

Table 3.1979.3  GPS week: 1979   Day: 3   MJD: 58100                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01  | 1148   15   41   18   12   11   27   12  ---    7 |    66   87   62   52   57   43   57  ---    55
 R02  |  597   12   19    7   16   12   21   18  108    6 |    52   60   47   38   53   62   40  190    46
 R03  | 1463    5    6    9    7   16   26   23  120    6 |    53   48   51   57   67   62   37  140    53
 R04  |  643    7   15   13   10   11   15   14  ---    5 |    49   51   46   55   53   45   42  ---    48
 R05  |  982   52   67   53   29   21   44   35  ---   18 |    49   61   69   41   44   44   31  ---    40
 R06  | 1137   15   36   18   34   18   44   22  ---   11 |    23   52   35   49   27   62   18  ---    27
 R07  |  613   14   16   15   13   18   16   28  356    8 |    47   44   56   53   63   60   66  299    55
 R08  | 1553   11   11   11   19   14   21   15  ---    7 |    44   47   49   53   49   53   42  ---    46
 R09  | 2570   15   15   14   12   14   22   24  ---    7 |    25   24   26   21   28   31   32  ---    21
 R10  |  746   12   11   14   16   17   13   17  ---    6 |    63   67   56   69   50   51   66  ---    60
 R11  |  584   16   15   11   17   16   23   21  122    7 |   105  107  113  117  113  118  106  113   111
 R13  | 2698   12   14   20   21   14   25   17  ---    8 |    69   73   63   73   56   58   67  ---    64
XR14  | 4572   24   24   21   35   26  ---   51  ---   16 |   343  343  341  365  358  ---  318  ---   345
 R15  | 2797   54   55   26   24   42   55   24  ---   17 |    91   90   65   72   55   95   55  ---    67
 R16  |  507   23   19   62   26   28   46   39  ---   17 |    94   96  115  105  103   93   88  ---    97
 R17E | 2660   23   23   27   10   25   23   15  ---    9 |    31   33   32   32   41   43   37  ---    31
 R18E |  956   15   15   18   21   15   21   18  ---    8 |    27   28   32   35   27   29   28  ---    26
 R19E | 1670   29   38   34   20   33   33   20  ---   13 |    35   40   47   49   47   34   35  ---    35
 R20E |  756   27   38   23   20   30   38   31  ---   12 |    58   56   34   47   54   43   47  ---    42
 R21E | 1812   16   18   19   11   21   22   27  131    8 |    36   37   32   38   31   37   28   68    30
 R22E |  740   19   24   23   15   28   23   21  ---    9 |    52   58   48   58   65   39   44  ---    52
 R23E |  745   23   30   19   17   12   29   28  ---    9 |    86   87   93   91   83   76   86  ---    86
 R24E |  824   14   27   20   16   29   26   23  ---    9 |   101  106  106  107  132   99  112  ---   105
XR26E | ----   27   45  ---  ---  ---  ---   36  ---   31 |    40   60  ---  ---  ---  ---   37  ---    33
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1486   23   29   25   19   22   30   23  192      |T   68   73   70   72   72   58   63  162    65
 WRMS | 1486   22   25   25   18   18   28   25  192      |NE  78   83   79   81   78   62   71  185    75
 MEDI |  982   15   19   19   17   18   23   22  122      |MD  52   58   51   53   54   51   42  140    48

Table 3.1979.4  GPS week: 1979   Day: 4   MJD: 58101                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01  |  678   19   24   17   13   19   26   20  ---    8 |    63   65   65   53   73   53   43  ---    57
 R02  |  840   10   12   13   11   12   34   15  154    7 |    46   44   45   44   53   34   38   62    41
 R03  |  954   12   13   13   19   11   15    9   88    6 |    49   50   48   35   46   45   40   62    42
 R04  | 1078    6   12   17   10   15   16   13  ---    6 |    43   45   49   42   45   47   35  ---    42
 R05  |  722   24   13   29   22   25   60   40  ---   15 |    43   39   73   49   61   66   26  ---    50
 R06  |  911   14   21   16   28   18   19   22  ---    9 |    20   39   22   45   37   18   20  ---    23
 R07  |  569   10    8   16   25   28   42   14  274   10 |    45   44   52   37   58   91   49  148    50
 R08  | 1628   16   16    9   15   13   18   24  ---    7 |    40   44   50   54   57   62   36  ---    48
 R09  | 3168   14   16   11   13   13   20   20  ---    6 |    55   56   42   52   58   59   48  ---    52
 R10  | 1353    8   12   12   18   14   19   11  ---    6 |    45   43   42   57   33   37   50  ---    44
 R11  | 1049   18   22   14    8   21   14   13  127    6 |    64   63   64   59   57   59   48   72    57
 R13  | 2173   10   15   15   16   17   23   20  ---    7 |    51   47   43   60   51   42   50  ---    49
XR14  | 1307   13   14   16   21   23  ---   19  ---    9 |   390  392  385  412  407  ---  396  ---   398
 R15  | 2295   49   44   20   21   34   17   22  ---   13 |    61   65   43   55   48   54   44  ---    46
 R16  |  605   23   21   36   20   33   30   33  ---   13 |    75   82   75   73   78   58   67  ---    67
 R17E |  576   25   19   20   20   28   15   24  ---   10 |    35   39   33   53   51   42   40  ---    38
 R18E |  641   18   18   13   15   16   17   16  ---    7 |    51   52   54   55   48   51   51  ---    50
 R19E | 1229   30   28   30   15   33   33   28  ---   12 |    37   43   41   41   52   35   57  ---    39
 R20E | 1558   21   29   38   22   46   35   29  ---   14 |    54   61   44   58   66   55   46  ---    45
 R21E | 1088   20   20   15   12   24   24   17  203    8 |    27   31   24   30   31   33   34   39    25
 R22E |  585   22   23   16   15   25   26   13  ---    8 |    30   30   21   32   32   24   28  ---    23
 R23E |  839   19   27   19   17   29   20   32  ---   10 |    64   62   65   65   73   66   54  ---    62
XR24E | 2345   33   41   27   22  ---   29   39  ---   15 |    87   96   80   79  ---   94   69  ---    79
XR26E | ----   22   85  ---  ---  ---  ---   27  ---   24 |    31   88  ---  ---  ---  ---   33  ---    29
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1341   21   21   20   18   24   27   22  181      |T   62   67   63   66   68   51   58   76    60
 WRMS | 1341   16   17   20   17   18   25   23  181      |NE  72   74   73   75   77   51   66   86    71
 MEDI | 1049   18   19   16   17   21   20   20  154      |MD  46   47   48   53   52   51   44   62    46

Table 3.1979.5  GPS week: 1979   Day: 5   MJD: 58102                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01  |  911   19   28   25   13   32   46   13  ---   11 |    42   58   54   54   65   32   47  ---    45
 R02  |  596   14   17   13   11   11   37   17  277    8 |    41   47   45   44   44   51   44  118    40
 R03  | 1691   11   13   15    9   14   11   18  194    6 |    43   43   47   38   38   38   39   88    38
 R04  | 1419    9   14   15   11   13   33   22  ---    8 |    47   47   49   42   44   64   35  ---    44
 R05  |  602   30   38   30   25   38   48   14  ---   13 |    39   50   63   44   40   27   44  ---    40
 R06  | 1745   25   22   19   30   36   24   25  ---   12 |    23   35   28   53   58   25   30  ---    29
 R07  |  577   19   18   23   23    9   27   10  180    8 |    42   44   47   42   45   42   34   52    37
 R08  | 1910   14   19   16   14   19   19   14  ---    7 |    37   42   44   42   50   37   37  ---    39
 R09  | 3267   13   17   17   17   14   27   16  ---    8 |    59   57   65   62   62   63   67  ---    61
 R10  |  637   11   11   20   18   12   22   15  ---    7 |    42   45   39   47   38   47   49  ---    42
 R11  | 2063   19   18   15   14   18   23   19  168    8 |    81   82   83   76   81   72   79   55    78
 R13  | 1781   18   16   23   22   21   22   14  ---    9 |    69   71   68   61   56   62   65  ---    62
XR14  |  668   19   16   25   15   22  ---   21  ---   10 |   448  444  455  441  447  ---  436  ---   444
 R15  | 3884   56   52   25   15   37   18   22  ---   14 |    64   59   63   46   48   57   35  ---    47
 R16  |  638   25   40   20   21   26   44   28  ---   12 |    91   87   97   89   92   99   88  ---    90
 R17E |  840   23   23   16   10   22   21   14  ---    8 |    46   45   45   47   48   38   37  ---    41
 R18E |  857   15   18   37   19   19   22   17  ---   10 |    38   38   56   49   39   48   45  ---    42
 R19E | 1679   37   39   36   16   34   22   20  ---   12 |    37   40   37   37   46   28   40  ---    31
 R20E | 1998   27   31   33   21   40   38   32  ---   14 |    38   41   36   52   55   53   49  ---    41
 R21E |  768   22   22   29   16   29   25   18  278   10 |    36   37   33   38   40   39   32   49    30
 R22E |  605   21   23   17   13   26   28   16  ---    9 |    51   58   48   59   62   53   49  ---    51
 R23E |  528   26   20   20   24   15   20   29  ---   10 |    89   95   94  103   98   94  101  ---    96
 R24E | 1145   36   36   35   27   35   24   25  ---   13 |   156  159  156  145  117  161  146  ---   149
XR26E | ----   21   47  ---  ---  ---  ---   16  ---   19 |    32   68  ---  ---  ---  ---   47  ---    37
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1627   25   26   24   18   26   29   20  224      |T   70   74   76   74   74   55   69   72    68
 WRMS | 1627   23   24   24   17   15   30   21  224      |NE  77   80   83   78   80   51   75   78    75
 MEDI |  911   19   20   20   16   22   24   17  194      |MD  42   47   49   49   50   48   45   55    42

Table 3.1979.6  GPS week: 1979   Day: 6   MJD: 58103                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01  |  819   14   46    6   27   28   46   13  ---   10 |    56   83   62   68   75   48   53  ---    57
 R02  |  456   15   19   10   14   15   10   12  401    5 |    55   56   59   60   56   56   53  247    56
 R03  | 1474    7    7    8    5   13   18   16  298    5 |    63   60   62   57   57   57   61  148    59
 R04  |  776    9   15    8   10   23   45   14  ---    9 |    58   60   55   58   55   81   56  ---    58
 R05  |  765   44   36   27   29   32   52   22  ---   15 |    59   72   77   79   69   56   51  ---    64
 R06  | 1653   21   23   18   33   39   20   36  ---   12 |    27   39   33   58   63   24   31  ---    33
 R07  |  573   13   22   20   21   27   21   27  220    9 |    58   63   64   54   61   58   53  170    56
 R08  | 1018   11   16   15   19   23   22   19  ---    8 |    58   61   62   59   71   69   45  ---    59
 R09  | 3305   15   16   12   16   19   19   17  ---    7 |    66   63   62   74   74   76   77  ---    71
 R10  | 1234   10   11   17   23   16   16   11  ---    7 |    46   45   39   62   41   43   48  ---    45
 R11  | 1783   21   20   12   13   19   10   16  198    7 |    75   73   68   67   62   64   66   86    66
 R13  | 1764    9   12   17   20   17   17   14  ---    7 |    76   79   69   78   65   71   78  ---    72
XR14  | 1696   17   24   19   16   17  ---   13  ---    8 |   467  468  472  465  463  ---  456  ---   465
 R15  | 2835   50   57   20   16   33   30   21  ---   13 |    81   85   59   41   45   48   40  ---    46
 R16  |  587   36   41   17   24   18   40   29  ---   12 |    94   88   86   88   84   84   93  ---    85
 R17E |  648   28   26   16    9   26   17   18  ---    8 |    88   87   86   82   87   87   79  ---    83
 R18E | 1006   18   14   14   17   19   18   13  ---    7 |    41   42   45   47   38   47   41  ---    42
 R19E |  880   47   41   29   24   28   30   21  ---   13 |    45   42   45   49   51   47   47  ---    43
 R20E | 1815   23   21   24   19   39   31   30  ---   12 |    57   56   57   68   70   68   67  ---    61
 R21E | 1109   26   24   18   15   24   21   24  269    9 |    35   35   33   32   31   24   30   55    26
 R22E |  778   25   29   20    9   33   20   19  ---    9 |    37   38   29   33   43   32   38  ---    30
 R23E |  907   19   27   14   26   19   51   51  ---   14 |    59   60   61   68   64   76   72  ---    62
 R24E | 2390   33   36   35   52   49   49   31  ---   18 |   145  158  151  189  168  157  140  ---   158
XR26E | ----   31   32  ---  ---  ---  ---   28  ---   29 |    70   71  ---  ---  ---  ---   80  ---    73
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1497   26   28   18   22   27   30   23  286      |T   79   82   79   84   82   62   77  141    77
 WRMS | 1497   23   26   18   18   22   31   24  286      |NE  89   93   88   91   89   59   84  162    86
 MEDI | 1018   19   23   17   19   23   21   19  269      |MD  58   61   62   62   63   57   53  148    59



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