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Conference 7.286::space

Title:Space Exploration
Notice:Shuttle launch schedules, see Note 6
Moderator:PRAGMA::GRIFFIN
Created:Mon Feb 17 1986
Last Modified:Thu Jun 05 1997
Last Successful Update:Fri Jun 06 1997
Number of topics:974
Total number of notes:18843

534.0. "Soviet ABM test Satellite ??" by PARITY::BIRO () Wed May 10 1989 14:46

1988 113A         Cosmos 1985  Launch 23 Dec 1988
ABM calibration mission launch from Plestsk Dec 23 on board a Cyclone
booster.  The satellite was place into a 340x330 mile orbit inclined
73.6 deg.  Shortly after achieving orbit, the spacecraft released two 
object.  Later it ejected two additional objects.  It is possible that
the objects are not involved in ABM tracking tests. But U.S. analysts
said it is most likely that the four subsatellites are device's that
can simulate the midcourse phase of U.S. ballistic missile reentry
vehicles to allow Soviet ABM radars to practice tracking such objects.
The Soviets have performed such missions before, but this is the first 
time  they have matched a satellite that releases such objects with a 
Cyclone booster launch into a 73.6 deg inclinations.

I just got my two line orbital elements set and it looks like
Cosmos 1985 is releasing more objects or is breaking up into
space junk, BUT they are still being released in pairs 
(ie obj 19943/43 and 19958/59) so it is most likely ABM tracking test.


obj 19912 88-113L ( I dont have with me any older data)

obj 19943 88-113M released on 1989 day 116
obj 19944 88-113N released on 1989 day 116

obj 19958 88-113P released on 1989 day 119
obj 19959 88-113Q released on 1989 day 119

It may be intersting to do a visual sighting of this bird
to see if one can see the releasing of these objects

Latest Nasa SET for 113A

    Soviet ABM  88113A                                  Set:  190, Obj:  19720
          Epoch Year: 1989  Day: 120.658304680    Orbit #    1943
          Inclination  =  73.54970000     R.A.A.N      = 294.18290000
          Eccentricity =   0.00098780     Arg of Per   = 279.40750000
          Mean Anomaly =  80.59140000     Mean Motion  =  15.15945191
          Drag         =  0.89210E-04     Frequency    =        0.000
          S.M.A.       =    6896.2041     Anom Period  =      94.9902
          Apogee Ht    =     524.8561     Perigee Ht   =     511.2320

    
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