MAP vectors

From: McConahy, Ralph (RMcConahy@jbar.gdscc.nasa.gov)
Date: Sat Jun 30 2001 - 20:30:23 PDT

  • Next message: McConahy, Ralph: "MAP vectors (updated)"

    The following is for anyone out there who can convert these into TLEs	...
    
    MAP ACTUAL SEPARATION STATE
    
    ****************************************************************************
    *******************************************************
     DATE   JUNE 30, 2001   21HRS    12MINS    34.000SECS  (JULIAN DATE =
    2452091.3837)
     ELAPSED TIME FROM EPOCH =     0 DAYS    0 HRS     0 MINS     0.000 SECS
     FLIGHT CENTRAL BODY IS EARTH   
    +                                (VEHICLE IS IN SUN LITE)
    
     OUTPUT CENTRAL BODY IS EARTH   
    +                                           INERTIAL SYSTEM   MEAN EQUATOR
    AND EQUINOX OF J2000.0
     X   -2298.793377      Y    5758.765937      Z    3314.627995      DX
    -10.08250016      DY  -2.021603492      DZ   2.236179013    
     SMA  150988.1215      ECC 0.9565568206      INC  28.74392043      RAAN
    34.69593544      AP   48.24843090      MA  0.2060206090    
     EA   4.631291704      P    162.1894693      SLR  12833.84673      PR
    6559.404047      APR  295416.8389      PH   181.2677465    
     APH  289038.7026      C3  -1.319972848      TA   30.36606728      LAT
    28.26977251      LON  234.6394803      HGT  657.6058290    
     R    7030.973962      V    10.52350639      RA   111.7609747      DEC
    28.12730832      VPA  75.16220389      AZ   83.82036242    
    
     OUTPUT CENTRAL BODY IS EARTH   
    +                                                             TRUE EQUATOR
    AND EQUINOX OF DATE
     X   -2300.661170      Y    5758.191713      Z    3314.329682      DX
    -10.08222756      DY  -2.024204027      DZ   2.235055333    
     SMA  150988.1215      ECC 0.9565568206      INC  28.73992300      RAAN
    34.70151212      AP   48.25902332      MA  0.2060206090    
     EA   4.631291704      P    162.1894693      SLR  12833.84673      PR
    6559.404047      APR  295416.8389      PH   181.2677465    
     APH  289038.7026      C3  -1.319972848      TA   30.36606728      LAT
    28.26977251      LON  234.6394803      HGT  657.6058290    
     R    7030.973962      V    10.52350639      RA   111.7789705      DEC
    28.12455185      VPA  75.16220389      AZ   83.82700568    
    
    
     
    ****************************************************************************
    *******************************************************
    
    SPACECRAFT MASS 836.46 KG
    SPACECRAFT AREA 20.438 SQUARE METERS
    COEFFICIENT OF DRAG 2.2
    COEFFICIENT OF SOLAR RADIATION 1.3
    
    
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    This archive was generated by hypermail 2b29 : Sat Jun 30 2001 - 20:30:46 PDT