[IGSREPORT-25742] Wk 1985 IGLOS Final Orbits

acc acc at igs.org
Sat Feb 10 21:58:33 PST 2018


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1985   (Jan 21, 2018 - Jan 27, 2018) 
                                                                               
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 2.1985.
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:
                                                                               
 igl1985[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1985 in the SP3 format.
 igl19857.sum      Combination Report for GPS Week 1985.


    
    
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  |      0.3 ns
                1  |      0.1 ns
                2  |     -0.8 ns
                3  |     -1.0 ns
                4  |      0.6 ns
                5  |      0.8 ns
                6  |     -8.7 ns

 5. The following orbit solutions were excluded from the combination
    because they were biasing the weighted average (generally indicated
    by long arc RMS).
    
               Day | Centre | PRN list
               ----+--------+---------------
                0  |  GRG   | R14
                1  |  GRG   | R14
                2  |  GRG   | R14
                3  |  GRG   | R14
                4  |  GRG   | R14
                5  |  GRG   | R14
                6  |  GRG   | R14

    
         
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 1.1985, 1a.1985).
        
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 2.1985.0-6)                                                                                
    
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 3.1985.0-6). 
        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 1985 summary.                      (Jan 21, 2018 - Jan 27, 2018)

Table 1.1985.a     GPS week : 1985   MJD: 58139.0-58145.0

         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    -6    26    14     1   .08   33   32 |   -5133    -447   3257   9943
        |    0     0     2    12    24    21   .04           |    2779    1043
cof  n/a|    0     0   -10    20    21    -7   .11   36   34 |   -5147    -434   3256   9944
        |    1     1     3    10    14    31   .09           |    2786    1048
emx  n/a|    0    -1    -2     9     7    12   .11   23   23 |   -1934     171   3246   9592
        |    0     1     2    21    13    27   .05           |   10732     804
esx  n/a|    0     0     0   -10     7    -9   .12   16   14 |    7177    -315   3250  11922
        |    1     0     1    12     9    31   .02           |    6759    1641
gfz  n/a|   -2     0     2    17    41    16   .17   27   25 |       0    -111   3251   9849
        |    1     2     2    18    31    32   .04           |       0    1240
grg  n/a|    0     2     0   -95   -14    13  -.41   71   50 |   -1085    -365   3236   9151
        |    1     1     1     7    14    82   .07           |    3084    1094
iac  n/a|    1     0     4    82   -50   -27  -.20   24   24 |    -102    -378   3248   9300
        |    1     1     2    31    45    28   .03           |    2999     901
mcc  n/a|    0     0   -24   200    -9   152  -.30  157  157 |     ---     ---    ---    ---
        |    9    11    24   109    57   419   .42           |     ---     ---


Table 1.1985.b     GPS week : 1985   MJD: 58139.0-58145.0   

         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  |    9    7    9   10   11   10   13 |
 R02  |    8    7    8    7    7    7    8 |
 R03  |   10   10   10    8    9   10    9 |
 R04  |    7    9    8   10    9   10    9 |
 R05  |   15   15   17   16   15   12   15 |
 R06  |    7    8    8    7    8    9    7 |
 R07  |    7   11   10   10   15   13   11 |
 R08  |    6    8   10   10    9   10   10 |
 R09  |    7    8    7    6    6    6    6 |
 R10  |    9   12    9    8    7    9    8 |
 R11  |    7   11    7    7    8    7    7 |
 R13  |   10   13   11    9    9   11   11 |
 R14  |    9   11   10    9    9    8    8 |
 R15  |   13   13   13   12   13   13   13 |
 R16  |   16   12   11   11   12   11   12 |
 R17  |   10    9   10   11   10    9   10 |
 R18  |   10   10    7    7    7   11    9 |
 R19  |   15   17   15   15   14   15   13 |
 R20  |   16   16   15   13   14   14   15 |
 R21  |   12   10    9   12   12   10   10 |
 R22  |   13   13   10   11   11   11   10 |
 R23  |    9   10   11   11   11    9    9 |
 R24  |   13   12   14   14   23   17   15 |


Table 1.1985.c     GPS week : 1985   MJD: 58139.0-58145.0   

         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 1985 0   |   31   -31    95     264    1444   -4180  83.6  1301  1301 |     335       0
brd 1985 1   |   30     8   110   -2096     899   -4737  83.5  1356  1356 |     120       0
brd 1985 2   |   22    41    88     105    -262      74  82.1  1369  1369 |    -814       0
brd 1985 3   |   19   -42    34      91    -313   -1911  82.5  1328  1328 |   -1039       0
brd 1985 4   |   34    60     5    -106    1207   -5317  82.5  1339  1339 |     591       0
brd 1985 5   |   -7   -18    30     460     511   -4915  82.4  1277  1277 |     795       0
brd 1985 6   |   22    78     4    -189    -651   -4374  81.6  1185  1185 |   -8658       0
-------------+------------------------------------------------------------+----------------
brd 1985 mean|   22    13    52    -209     404   -3622  82.6  1307  1307 |   -1238       0
brd 1985 sdev|   14    47    44     859     822    1968    .7    62    62 |    3343       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 2.1985.0  GPS week: 1985   Day: 0   MJD: 58139                            

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    26    20    -1   .07   32   34 |   -4701    -342   3168   9974
cof  n/a|    0     0    -5     9    25   -36  -.00   34   34 |   -4722    -318   3182   9979
emx  n/a|    1     0    -5     7    -5   -21   .02   21   21 |   -2956     303   3167   9628
esx  n/a|    0     0     2   -13     9   -58   .11   16   15 |   -1803     853   3167  11695
gfz  n/a|   -1    -2     0    25    26    14   .14   22   23 |       0     533   3172   9920
grg  n/a|    0     2     0  -100   -29   123  -.31   74   62 |     461    -374   3148   8992
iac  n/a|    0     0     3    76     3   -11  -.17   26   26 |    1129      46   3158   9405
mcc  n/a|   -5   -16   -64   430    26  -656  -.90  201  201 |     ---     ---    ---    ---

Table 2.1985.1  GPS week: 1985   Day: 1   MJD: 58140                            

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    -2    18   -25     1   .08   30   28 |   -3943     418   3201   9715
cof  n/a|    1     0    -7    23     0    -5   .22   34   31 |   -3952     429   3203   9720
emx  n/a|    0    -2    -2    15    13   -30   .08   20   20 |   -2796     500   3186   9456
esx  n/a|    0     0     0   -16     4     6   .09   16   15 |   17981   -1702   3195  12477
gfz  n/a|    0     4     3     3    37   -24   .16   28   26 |       0     155   3179   9659
grg  n/a|   -1     2     1  -106   -16    93  -.51   74   40 |      26     171   3213   9010
iac  n/a|    0     0     3    85     8   -36  -.18   29   29 |    1411    -508   3199   9032
mcc  n/a|   14    -7    -2   138   -37   112  -.46  123  123 |     ---     ---    ---    ---

Table 2.1985.2  GPS week: 1985   Day: 2   MJD: 58141                            

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    -9    46    20    -6   .03   34   35 |   -2529   -1876   3173  10269
cof  n/a|    0    -2   -16     9    18    22   .01   38   38 |   -2533   -1888   3172  10269
emx  n/a|    0     1    -1    23    23    25   .15   22   22 |  -10576   -1333   3155   9767
esx  n/a|    1     0     1   -12    10   -17   .15   15   12 |   10154   -1585   3172  12405
gfz  n/a|   -2     1     7    28     1    19   .18   25   27 |       0   -2263   3209  10309
grg  n/a|   -2    -1    -2  -100   -21   -29  -.49   71   32 |     225   -2084   3155   9010
iac  n/a|    3     1     5   129   -98   -16  -.19   26   26 |    1207    -908   3161   9680
mcc  n/a|   12     6    -6   191   -65   -63   .27  138  138 |     ---     ---    ---    ---

Table 2.1985.3  GPS week: 1985   Day: 3   MJD: 58142                            

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    -8    26    12   -23   .05   35   34 |   -6447    -875   3414   9934
cof  n/a|   -2     3    -9    33    44   -32   .08   39   36 |   -6472    -834   3414   9931
emx  n/a|    0    -1     0   -18    20    26   .16   23   23 |   19327    -167   3390   9686
esx  n/a|    1    -1     0     3    15   -26   .11   16   15 |    5376   -1626   3394  11655
gfz  n/a|   -1    -1     1   -10    69   -15   .17   27   26 |       0    -523   3405   9856
grg  n/a|    1     3     0   -93   -26    65  -.41   66   42 |    -692    -781   3352   9293
iac  n/a|    1     0     2   101  -107   -22  -.20   21   21 |   -1151     118   3399   9353
mcc  n/a|    2    -1   -26   229   -87   473   .06  165  165 |     ---     ---    ---    ---

Table 2.1985.4  GPS week: 1985   Day: 4   MJD: 58143                            

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    -8     7     8    46   .06   36   33 |   -3922    1138   3362   9413
cof  n/a|   -3     0   -10    24     9    13   .15   37   35 |   -3938    1165   3359   9411
emx  n/a|    0    -1     0   -16   -11    30   .14   26   26 |    -918    1045   3360   9054
esx  n/a|    1     0     0   -22    -6   -15   .12   16   15 |   11206    1362   3361  12012
gfz  n/a|   -4    -1     0    16     7     9   .14   27   26 |       0    1040   3353   9354
grg  n/a|    1     1     2   -82    15   -37  -.39   72   80 |    -151    1333   3361   8544
iac  n/a|    2     1     4    88   -41     7  -.19   22   22 |    1671     661   3358   8787
mcc  n/a|   -4    19   -50   144    18   525  -.46  198  198 |     ---     ---    ---    ---

Table 2.1985.5  GPS week: 1985   Day: 5   MJD: 58144                            

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    -7    28     5    -1   .15   34   31 |   -3573    -169   3445   9571
cof  n/a|   -1    -1   -13    15    22    31   .17   35   32 |   -3571    -185   3437   9572
emx  n/a|    0    -4    -2    42    -3    18   .06   25   25 |  -14612     918   3438   9240
esx  n/a|    0     0     0   -21    21    42   .14   15   14 |    7109    1991   3433  11119
gfz  n/a|   -2     0     2    10    83    69   .26   28   24 |       0    1255   3415   9492
grg  n/a|    0     4     0   -91    -9  -105  -.39   71   46 |     551     252   3411   9141
iac  n/a|    2     2     9    67   -64   -31  -.25   23   23 |    1558      24   3436   8886
mcc  n/a|   -7     5    -6   167     0   192  -.61  119  119 |     ---     ---    ---    ---

Table 2.1985.6  GPS week: 1985   Day: 6   MJD: 58145                            

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    -6    31    58    -6   .09   33   30 |  -10821   -1428   3037  10731
cof  n/a|    0     0    -8    31    28   -46   .14   36   31 |  -10842   -1408   3031  10729
emx  n/a|    0    -2    -4     9    15    40   .13   23   23 |   -1007     -63   3027  10316
esx  n/a|    2     0     0     9    -2     1   .14   17   15 |     217   -1503   3032  12093
gfz  n/a|   -2     0     2    47    64    43   .16   28   26 |       0    -979   3024  10355
grg  n/a|   -1     2     3   -96   -16   -18  -.39   68   47 |   -8016   -1075   3017  10072
iac  n/a|    1     0     5    25   -49   -83  -.21   23   23 |   -6540   -2083   3030   9961
mcc  n/a|   -7    -6   -12    99    77   483   .04  152  152 |     ---     ---    ---    ---

       
       
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 3.1985.0  GPS week: 1985   Day: 0   MJD: 58139                            

        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  |  571   28   20   19   10   12   13   32  ---    8 |    74   68   61   57   54   65   54  ---    57
 R02  | 2033   17   28   16   15   14   20   23  115    7 |    68   73   63   63   46   54   48  114    56
 R03  |  741   31   33   22    8   24   20   24  207    9 |    85   84   75   66   60   57   48  115    64
 R04  |  731   30   34   16   12   15   13   11  ---    7 |    85   87   69   64   54   60   60  ---    63
 R05  |  974   38   40   16   27   27   58   24  ---   14 |    69   80   62   58   58   56   50  ---    55
 R06  | 2336   14   11   12    9   13   27   16  ---    6 |    53   55   56   58   53   69   53  ---    56
 R07  |  985   26   28   19    7   14   11   21  233    7 |    87   87   77   66   62   67   54  134    67
 R08  |  803   22   20   11    8    8   11   17  ---    5 |    72   71   63   63   62   61   52  ---    61
 R09E | 1545   13   15   12    6   14   29   18  ---    7 |    43   46   41   40   45   43   55  ---    41
 R10E | 1018   21   24   17   20   12   26   15  ---    8 |   217  217  220  208  218  227  215  ---   216
 R11E | 1653   18   13   13   16   16   18   15  280    7 |    65   65   58   62   53   55   60  283    58
 R13  |  869   24   30   27   16   12   22   24  ---    9 |    63   63   47   69   50   62   54  ---    56
 R14E | 1555   24   17   20   13   23  328   13  ---    9 |    71   64   71   63   67  143   69  ---    66
 R15  | 2954   37   39   27   20   33   21   41  ---   13 |   143  157  135  129  116  131  103  ---   125
 R16E |  473   24   29   35   28   22   45   58  ---   16 |    94  108   92   98   81   93   74  ---    86
 R17  |  695   44   39   18    8   31   13   20  ---   10 |    70   70   50   46   37   45   35  ---    44
 R18  |  798   24   26   19   24   25   25   18  ---   10 |    49   50   39   53   36   36   32  ---    41
 R19  |  838   58   60   26   19   34   35   30  ---   14 |    85   83   62   92   76   83   75  ---    76
 R20  | 1018   56   59   32   21   29   43   37  ---   15 |    80   86   43   46   40   56   38  ---    43
 R21  |  675   40   40   22   17   25   29   29  116   11 |    70   69   48   56   41   45   38   63    46
 R22  |  630   52   47   26   10   36   16   29  ---   12 |    69   66   51   43   39   49   36  ---    43
 R23  |  946   16   18   24   17   10   23   17  ---    8 |    26   26   29   47   36   32   41  ---    34
 R24  | 1563   17   41   18   14   19   66   21  ---   12 |    37   62   43   45   31   34   38  ---    34
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1300   32   34   21   16   22   74   26  201      |T   77   79   67   69   61   70   60  141    64
 WRMS | 1300   34   34   21   15   23   62   26  201      |NE  71   74   59   62   52   59   50  106    56
 MEDI |  946   24   29   19   15   19   23   21  207      |MD  70   70   61   62   53   57   53  115    56

Table 3.1985.1  GPS week: 1985   Day: 1   MJD: 58140                            

        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  |  683   24   32   13    9   16   21   18  ---    7 |    61   70   52   56   64   65   57  ---    56
 R02  | 1167   18   13   10   12   17   24   16   80    7 |    57   54   52   46   48   57   46   65    49
 R03  |  725   26   33   19   11   30   22   34   98   10 |    62   68   56   59   39   47   30   85    50
 R04  | 1216   28   31   20    9   28   19   23  ---    9 |    62   65   53   47   43   49   53  ---    49
 R05  | 1420   34   47   21   24   33   60   25  ---   14 |    62   75   51   49   38   49   48  ---    46
 R06  | 1080   15   20   14   14   19   29   12  ---    7 |    39   43   43   45   34   40   34  ---    38
 R07  |  785   26   25   25   13   22   29   34  183   10 |    62   62   61   54   46   49   34  102    51
 R08  |  747   14   18   13   12   11   30   28  ---    8 |    59   65   60   67   68   61   47  ---    61
 R09E | 1886   11   11   16   10   17   28   23  ---    7 |    73   76   72   75   72   82   84  ---    74
 R10E |  889   20   16   19   17   26   29   47  ---   11 |   185  187  182  179  189  194  174  ---   181
 R11E | 2239   15   16   21   16   18   26   40  134   10 |    58   63   61   66   56   61   40  134    55
 R13  | 1272   17   15   29   25   17   32   40  ---   12 |    57   65   53   68   64   70   46  ---    57
 R14E | 1873   30   30   20   17   21  325   22  ---   10 |    81   77   63   58   54  121   75  ---    63
 R15  | 3392   45   57   21   12   29   31   44  ---   13 |   122  139  120  120  115  116  110  ---   116
 R16E |  583   21   19   33   18   28   39   21  ---   12 |    67   61   49   51   44   48   46  ---    45
 R17  |  853   37   44   12    7   28   18   19  ---    9 |    42   47   32   31   33   36   25  ---    31
 R18  | 1109   20   21   17   22   30   25   14  ---    9 |    28   35   26   33   25   30   21  ---    26
 R19  | 1275   63   65   22   15   53   48   25  ---   16 |    94   95   77   84   71   96   77  ---    81
 R20  |  957   49   66   24   18   51   55   29  ---   16 |    59   76   34   48   27   39   25  ---    34
 R21  |  661   36   33   17   11   28   29   18   91   10 |    44   42   32   39   26   24   29   84    31
 R22  |  650   40   41   21   10   41   26   34  ---   12 |    41   40   36   31   26   35   23  ---    28
 R23  | 1242   22   20   28   22   23   13   19  ---   10 |    29   32   33   41   39   38   40  ---    35
 R24  |  930   24   23   17   24   21   27   43  ---   11 |    31   33   30   32   29   34   31  ---    19
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1356   30   34   20   16   28   74   29  123      |T   64   68   57   59   54   62   51   94    55
 WRMS | 1356   28   31   20   15   26   40   29  123      |NE  56   61   50   52   46   51   43   84    47
 MEDI | 1080   24   25   20   14   26   29   25   98      |MD  59   65   52   51   44   49   46   85    49

Table 3.1985.2  GPS week: 1985   Day: 2   MJD: 58141                            

        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  | 1185   41   45   14   13   13   23   15  ---    8 |    61   67   35   39   35   48   34  ---    38
 R02  |  685   21   27   24   10   15   18   16  120    7 |    49   54   49   40   38   44   31   53    39
 R03  |  894   35   34   28    6   26   22   25   96   10 |    66   65   55   45   30   48   32   38    44
 R04  |  902   29   30   17    8   22   11   25  ---    8 |    65   66   50   47   34   53   28  ---    45
 R05  | 1238   46   45   29   10   34   58   53  ---   17 |    61   57   41   37   29   31   37  ---    28
 R06  |  885   21   24   20   16   14   17   15  ---    7 |    42   47   40   50   38   50   48  ---    44
 R07  | 1170   28   28   29    9   14   25   28  207   10 |    63   65   58   45   40   54   29   92    46
 R08  |  572   29   27   21   14   16   32   28  ---   10 |    58   60   51   49   30   28   30  ---    40
 R09E | 2679   11   15   15   10   16   17   17  ---    6 |    44   48   44   40   43   44   47  ---    41
 R10E |  909   21   21   22   16   22   24   20  ---    9 |   102   94   97   95   92   95   93  ---    93
 R11E | 1646   15   16   19   14   16   13   15  147    7 |    48   54   51   54   42   47   40   76    47
 R13  | 2702   14   20   26   24   19   31   28  ---   11 |    50   46   52   55   57   39   32  ---    43
 R14E | 2057   24   32   20   14   23  315   22  ---    9 |    61   68   59   64   71   75   53  ---    59
 R15  | 1582   51   62   16   19   33   28   32  ---   12 |    93  100   73   69   69   91   51  ---    70
 R16E |  835   18   44   25   27   15   26   30  ---   11 |    58   84   43   68   51   44   64  ---    54
 R17  | 1218   40   42   18   10   30   26   22  ---   10 |    53   53   37   33   27   49   27  ---    33
 R18  |  935   20   28   11    7   23   11   18  ---    6 |    32   37   26   29   22   32   23  ---    25
 R19  | 1216   69   72   27   16   43   17   33  ---   14 |    46   47   34   36   44   38   44  ---    34
 R20  | 1411   55   57   19   19   40   40   41  ---   15 |    73   76   57   50   35   32   20  ---    41
 R21  |  612   31   40   13   12   34   17   21   86    9 |    50   55   36   43   30   42   33   55    36
 R22  |  936   33   34   16   11   35   17   28  ---   10 |    50   49   38   43   31   35   34  ---    36
 R23  | 1085   21   25   32   25   25   17   11  ---   10 |    18   20   29   43   20   33   34  ---    27
XR24  |  839   25   28   20   22  ---   48   23  ---   14 |    32   37   35   34  ---   24   31  ---    27
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1368   34   38   22   15   25   71   26  138      |T   55   58   47   48   41   46   38   62    43
 WRMS | 1368   35   38   22   12   27   32   26  138      |NE  53   55   44   43   35   42   33   59    38
 MEDI | 1085   28   30   20   14   22   23   23  120      |MD  53   55   44   45   35   44   34   55    41

Table 3.1985.3  GPS week: 1985   Day: 3   MJD: 58142                            

        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  | 1089   42   41   22   14   20   26   20  ---   10 |    60   63   20   35   32   45   21  ---    28
 R02  |  931   19   19   22   11   11   17    8  166    6 |    46   47   46   29   30   27   28   66    31
 R03  |  793   30   31   22   12   14   11   20   90    8 |    71   72   61   41   48   53   36   35    47
 R04  |  792   30   32   22   12   21   20   29  ---    9 |    67   67   50   50   40   46   26  ---    43
 R05  |  673   54   63   24   20   42   41   40  ---   15 |    65   81   46   44   40   53   28  ---    39
 R06  |  796   19   26   18   15   10   17   17  ---    7 |    56   60   45   58   46   44   52  ---    49
 R07  |  957   30   32   29    9   26   19   27  247   10 |    69   71   62   51   29   43   34  111    46
 R08  |  724   31   33   25    9   17   30   18  ---    9 |    62   62   49   46   32   34   35  ---    40
 R09E | 2748   17   13   14    6   15   11   14  ---    5 |    35   28   29   30   35   30   32  ---    29
 R10E | 2398   18   26   25   14   17   25    9  ---    8 |    77   76   78   72   75   66   73  ---    72
 R11E | 1298   13   18   19   12   18   13   14  192    6 |    42   48   35   43   32   42   38   68    37
 R13  | 1936   17   17   25   20   17   21   17  ---    9 |    41   44   40   45   32   37   33  ---    35
 R14E | 2340   31   29   17   13   22  294   13  ---    9 |    62   61   46   61   55   65   53  ---    53
 R15  | 1330   58   58   21    8   28   26   22  ---   11 |    90   90   67   59   58   54   42  ---    56
 R16E | 1132   22   32   30   22   18   29   22  ---   11 |    49   43   42   67   61   42   55  ---    51
 R17  | 1026   41   44   20    8   44   10   18  ---   10 |    55   59   44   39   28   37   31  ---    35
 R18  |  819   22   22   11   12   17   10   21  ---    7 |    43   44   32   41   32   40   38  ---    35
 R19  |  993   73   73   26   21   35   23   26  ---   14 |    76   81   50   54   41   60   47  ---    50
 R20  | 1278   41   59   20   13   42   41   25  ---   13 |    57   71   36   42   34   41   26  ---    34
 R21  | 1051   40   45   22   15   37   30   18   57   11 |    58   63   43   32   22   55   29   25    34
 R22  |  921   38   42   19   10   35   30   24  ---   11 |    57   58   42   39   23   47   27  ---    35
 R23  |  664   23   20   23   30   22   30   16  ---   11 |    20   27   27   49   27   41   27  ---    30
 R24  |  819   27   45   30   28   40   46   14  ---   14 |    25   44   49   44   28   28   30  ---    28
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1327   35   39   23   16   27   66   21  165      |T   55   59   45   46   38   44   36   61    40
 WRMS | 1327   34   36   23   15   26   42   21  165      |NE  56   61   44   44   34   43   32   59    38
 MEDI |  993   30   32   22   13   21   25   18  166      |MD  57   61   45   44   32   43   33   66    37

Table 3.1985.4  GPS week: 1985   Day: 4   MJD: 58143                            

        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  |  758   38   42   17   17   30   34   19  ---   11 |    63   73   43   50   44   63   40  ---    45
 R02  | 1376   12   21   18    9   20   10   19  211    6 |    47   50   46   46   37   43   33  108    40
 R03  | 1088   26   32   30    9   18   17   21  101    9 |    59   61   57   43   34   35   33   81    41
 R04  | 1317   25   28   26   10   17   22   19  ---    8 |    57   60   54   48   40   34   34  ---    43
 R05  |  558   52   42   22   30   29   35   33  ---   14 |    59   53   45   41   39   40   36  ---    35
 R06  |  884   21   27   13   11   20   22   20  ---    7 |    56   66   40   50   42   54   30  ---    43
 R07  |  494   45   46   41    9   41   29   44  324   15 |    71   75   63   42   31   58   21  202    40
 R08  |  496   31   29   26   12   17   25   18  ---    9 |    59   66   56   55   50   36   42  ---    48
 R09E | 2235   17   26   14    7   14   15   14  ---    5 |    42   48   30   38   41   36   36  ---    35
 R10E | 3469   14   15   16   15   21   14   14  ---    7 |    95   97   93  104   94  103   97  ---    98
 R11E |  782   13   13   19   13   29   18    9  184    7 |    39   35   31   38   20   34   28   79    30
 R13  | 1353   17   15   25   18   19   21   19  ---    9 |    60   59   63   70   58   48   54  ---    58
 R14E |  976   24   27   13   15   24  309   18  ---    9 |    55   55   40   45   34   71   43  ---    41
 R15  | 1689   65   68   21   14   31   22   23  ---   12 |    77   81   56   48   55   59   49  ---    51
 R16E | 1234   31   38   26   22   31   29   25  ---   11 |    47   51   41   58   37   44   54  ---    45
 R17  |  708   34   37   18   14   32   15   20  ---    9 |    51   51   41   50   38   40   37  ---    41
 R18  | 1007   22   26   12   13   25   17    9  ---    7 |    36   41   35   38   30   30   36  ---    33
 R19  |  837   65   70   26   21   36   21   23  ---   14 |    79   78   55   54   53   59   42  ---    53
 R20  | 1582   31   17   35   12   32   59   16  ---   14 |    37   30   39   31   26   53   21  ---    28
 R21  | 1245   45   44   27   10   35   19   23   48   11 |    57   54   37   39   30   44   30   41    35
 R22  |  877   45   46   18   11   31   23   24  ---   10 |    48   50   34   34   27   37   21  ---    30
 R23  |  655   19   21   20   25   22   39   20  ---   11 |    25   26   28   44   31   21   27  ---    26
 R24  | 1405   51   51   62   22   35   95   21  ---   22 |    46   49   69   50   37   29   30  ---    36
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1339   36   37   26   16   27   72   22  198      |T   55   56   47   48   40   46   38  102    42
 WRMS | 1339   33   35   26   15   26   80   22  198      |NE  54   56   47   46   39   43   34  108    40
 MEDI | 1007   31   29   21   13   29   22   20  184      |MD  56   54   43   46   37   43   36   81    41

Table 3.1985.5  GPS week: 1985   Day: 5   MJD: 58144                            

        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  |  666   36   37   23   13   22   18   22  ---    9 |    62   69   42   60   47   63   47  ---    52
 R02  |  844   14   18   16   12   14   22   14   92    7 |    54   64   54   54   47   56   50   73    52
 R03  |  909   27   22   29    8   24   20   28  189   10 |    57   53   52   47   38   50   32   99    44
 R04  |  958   33   27   31   10   20   20   20  ---    9 |    56   54   51   42   41   32   29  ---    38
 R05  | 1088   41   45   22   15   25   31   32  ---   12 |    46   57   44   49   47   33   25  ---    37
 R06  |  734   13   20   25   18   25   24   16  ---    9 |    46   59   33   55   40   50   31  ---    41
 R07  |  673   42   44   35    4   33   23   34   95   12 |    60   63   51   38   33   38   31  141    36
 R08  |  669   40   35   24   12   32   17   17  ---   10 |    53   52   43   36   28   29   24  ---    31
 R09E | 2096   22   24   15    9   14   10   12  ---    5 |    34   37   24   25   32   26   27  ---    25
 R10E | 2989   18   22   23   15   16   21   25  ---    9 |    67   66   65   63   65   71   58  ---    63
 R11E |  748   15   17   16   11   18   17   17  115    7 |    39   42   33   34   29   34   27  116    30
 R13  | 1100   18   19   25   19   32   27   22  ---   10 |    65   75   70   72   80   64   56  ---    66
 R14E | 1053   24   29   20   11   20  321   10  ---    8 |    43   46   33   33   30   49   33  ---    32
 R15  | 1506   65   55   20   16   28   21   30  ---   13 |    87   79   58   63   64   64   40  ---    58
 R16E |  788   31   34   19   22   27   28   28  ---   11 |    40   52   32   54   40   39   52  ---    42
 R17  |  472   38   39   22    6   28   21   15  ---    9 |    41   42   37   31   26   23   30  ---    28
 R18  |  568   16   19   23   27   22   27   10  ---   10 |    29   30   32   45   31   24   31  ---    31
 R19  |  692   60   62   29   13   43   29   38  ---   15 |    74   74   73   74   70   68   47  ---    65
 R20  | 1450   22   37   42   12   29   50   17  ---   13 |    26   37   37   33   39   45   22  ---    25
 R21  |  941   42   47   15   13   30    8   29   66   10 |    47   52   41   45   26   35   28   62    36
 R22  |  928   46   47   26   11   40   14   19  ---   11 |    44   46   28   40   41   41   30  ---    34
 R23  | 1183   18   18   21   18   23   17   15  ---    8 |    22   24   25   33   21   15   27  ---    23
 R24  | 2572   31   36   38   26   48   54   26  ---   16 |    52   53   45   56   35   18   34  ---    36
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1277   34   35   25   15   28   71   23  119      |T   49   53   43   47   41   42   35   98    40
 WRMS | 1277   31   32   25   14   24   46   23  119      |NE  51   54   45   48   41   41   34   93    40
 MEDI |  928   31   34   23   13   25   21   20   95      |MD  47   53   42   45   39   39   31   99    36

Table 3.1985.6  GPS week: 1985   Day: 6   MJD: 58145                            

        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  |  527   50   42   18   14   36   35   19  ---   12 |    82   82   50   51   45   73   51  ---    53
 R02  |  680   16   15   22   11   19   22   15  208    8 |    72   75   66   66   58   65   60   70    63
 R03  |  652   27   31   30    9   23   14   20  148    9 |    81   85   76   63   59   61   48   82    62
 R04  |  955   31   34   25    7   23   16   23  ---    9 |    73   72   62   55   50   46   43  ---    52
 R05  |  532   51   54   28   29   32   30   30  ---   14 |    65   68   51   45   40   41   44  ---    42
 R06  |  818   13   22   20   11   13   18   17  ---    7 |    61   63   52   70   62   64   49  ---    60
 R07  |  730   36   39   24   11   18   18   34  152   10 |    85   87   72   58   46   53   41   86    56
 R08  |  649   35   39   25    8   32    8   30  ---   10 |    67   70   61   52   42   37   37  ---    46
 R09E | 2021   18   22    9   11   17   12   19  ---    6 |    39   41   31   34   38   34   35  ---    33
 R10E | 2209   13   15   24   16   19   12   14  ---    7 |    87   87   84   88   82   91   77  ---    84
 R11E |  729   11    9   19   13   15   12   15  152    6 |    57   54   43   56   44   52   39  128    48
 R13  | 1407   21   23   29   19   32   18   21  ---   10 |    65   61   58   69   56   56   57  ---    59
 R14E |  846   19   20   15   13   22  312   15  ---    8 |    52   52   34   43   31   62   40  ---    37
 R15  |  953   61   71   25   15   32   15   27  ---   12 |    90   96   66   56   58   62   44  ---    57
 R16E |  863   23   24   21   22   20   29   33  ---   11 |    54   53   48   70   49   49   64  ---    55
 R17  |  503   41   44   24   11   27   15   24  ---   10 |    71   71   53   43   33   41   35  ---    42
 R18  |  481   22   26   24   19   21   18   10  ---    8 |    49   50   40   50   33   40   42  ---    41
 R19  |  719   50   49   21   21   43   21   25  ---   13 |   104  104   76   74   54   87   58  ---    72
 R20  | 1121   36   35   29   26   39   43   19  ---   14 |    58   56   57   43   22   51   30  ---    38
 R21  |  656   39   38   24    9   29   12   23   58    9 |    75   74   61   54   48   52   41   74    52
 R22  |  707   31   31   16   14   34   20   24  ---   10 |    69   69   51   54   42   64   37  ---    50
 R23  |  825   14   17   20   24   27   13   18  ---    9 |    27   25   28   44   25   32   38  ---    31
 R24  | 3256   32   52   28   24   43   44   34  ---   15 |    55   77   48   53   21   42   34  ---    38
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1185   33   36   23   17   28   68   23  151      |T   66   68   55   56   45   54   45   88    50
 WRMS | 1185   30   31   23   15   26   47   23  151      |NE  69   71   57   55   44   53   43   78    50
 MEDI |  730   31   31   24   14   27   18   21  152      |MD  67   70   53   54   45   52   42   82    52



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