MAP vectors (updated)

From: McConahy, Ralph (RMcConahy@jbar.gdscc.nasa.gov)
Date: Sat Jun 30 2001 - 20:57:21 PDT


Just received the following...

MAP (SATID 0102701; NORAD # 26859) SEPARATION PLUS 6HR. STATE


                                       GTDS   SATELLITE EPHEMERIS REPORT
SECTION  1

 
****************************************************************************
*******************************************************
 DATE   JUNE 30, 2001   21HRS    30MINS     0.000SECS  (JULIAN DATE =
2452091.3958)
 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   -10904.73732      Y    1633.667030      Z    4133.395084      DX
-6.498847850      DY  -4.778725218      DZ -0.1322369371    
 SMA  152715.5744      ECC 0.9570421849      INC  28.73476310      RAAN
34.61438416      AP   48.51635171      MA  0.8346847917    
 EA   15.35228704      P    164.9808265      SLR  12838.83748      PR
6560.327408      APR  298870.8214      PH   182.1911076    
 APH  292492.6851      C3  -1.305041883      TA   84.58697123      LAT
20.61106468      LON  289.9850163      HGT  5400.201740    
 R    11775.70036      V    8.067758344      RA   171.4797357      DEC
20.54913745      VPA  48.85048718      AZ   110.5381447    

 OUTPUT CENTRAL BODY IS EARTH   
+                                                             TRUE EQUATOR
AND EQUINOX OF DATE
 X   -10905.62700      Y    1630.865766      Z    4132.153857      DX
-6.497592907      DY  -4.780411978      DZ -0.1329377041    
 SMA  152715.5744      ECC 0.9570421849      INC  28.73077273      RAAN
34.61994721      AP   48.52695927      MA  0.8346847917    
 EA   15.35228704      P    164.9808265      SLR  12838.83748      PR
6560.327408      APR  298870.8214      PH   182.1911076    
 APH  292492.6851      C3  -1.305041883      TA   84.58697123      LAT
20.61106468      LON  289.9850163      HGT  5400.201740    
 R    11775.70036      V    8.067758344      RA   171.4948154      DEC
20.54268790      VPA  48.85048718      AZ   110.5387577    


 
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*******************************************************

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 - 20:57:45 PDT