RE: Atlas 3A Launch Data Needed

From: Chris Peat (chris.peat@heavens-above.com)
Date: Sun May 14 2000 - 23:55:05 PDT

  • Next message: nixj@bellsouth.net: "Obs May 15th"

    Hi Ron and list,
    Here is the nominal insertion orbit and burn times of the Eutelsat W4
    spacecraft which will be the prime (only?) payload of the Atlas 3A launch
    today. I've also appended a derived elset for the nominal injection orbit.
    
    Chris
    
    Chris Peat, Heavens-Above GmbH
    E-mail: Chris.Peat@heavens-above.com
    Web site: www.heavens-above.com
    
    
    
    > The inaugural launch of the Atlas 3A will occur on Monday,
    > 15 May EDT.  Depending on when the geo transfer orbit occurs,
    > the apogee burn MIGHT be visible from the US.
    >
    > Does anyone have details on the orbit and burn times?
    >
    > Since it is probably a liquid upper stage, it may be invisible
    > compared to an IUS type booster but it is worth trying anyway.
    
    
    
       Satellite              : EW4 / EUTELSAT W4
    
       SatID                  : 0099901
    
       Epoch                  : 2000/05/15  22:05:53.360
    
       Reference System       : True equator and equinox of data
    
      Keplerian elements:
    
       Semimajor axis    :  29497.8360 km
       Eccentricity      : 0.777131250
       Inclination       :   18.173368 deg
       RA ascend. node   :   20.308572 deg
       Arg. pericenter   :  179.184070 deg
       Mean anomaly      :    1.732833 deg
    
      State vector:
    
       x                 :  -5159.0358 km
       y                 :  -4336.1295 km
       z                 :   -747.1404 km
       x-dot             :    5.17334454 km/s
       y-dot             :   -8.21957614 km/s
       z-dot             :   -3.11991641 km/s
    
      Spacecraft parameters :
    
       Mass              :   3190.0 kg
       Area(CR)          :   10.00 m^2
       CR                :    1.300
       Area(CD)          :   10.00 m^2
       CD                :    2.300
    
      Maneuvers:   5
    
       Start Date     UTC       Duration  Mass flow     Frame      Delta-v
                                  [s]      [kg/s]                   [m/s]
       2000/05/17  08:25:56.6   2894.5     0.1353       x          -130.824
                                                        y           368.926
                                                        z          -110.014
       2000/05/19  07:21:19.1   4266.7     0.1353       x          -235.591
                                                        y           648.071
                                                        z          -197.232
       2000/05/22  02:58:33.3   1355.0     0.1353       x          -86.5050
                                                        y           241.918
                                                        z          -74.2457
       2000/05/23  20:17:41.7    763.7     0.1353       x          -52.8332
                                                        y           148.137
                                                        z           36.9081
       2000/05/25  07:20:03.4    149.6     0.1353       x          -10.3240
                                                        y           30.9796
                                                        z          -0.07791
      Comment:
    
      Nominal injection and strategy for a launch on 15 May 2000 21:37 UTC
      (Lift off)
    
    
    Derived two-line elements:
    
    1 77778U 00078A   00136.92075648 -.00000000  00000-0 +00000+0 0 00016
    2 77778  18.1707  20.4031 7746982 179.0532   1.7622  1.74053842    04
    
    
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