KeyHole Manoeuvre Alert Continues; Search Elements Enclosed

From: Ted Molczan (molczan@home.com)
Date: Mon Jul 02 2001 - 01:06:15 PDT

  • Next message: Tony Beresford: "Re: MAP vectors (updated)"

    Mike McCants has reported that USA 129 had not manoeuvred as of 2001 Jul 02 at
    04:08 UTC. Here are his most recent elsets for both KeyHoles:
    
    USA 116         15.0  3.0  0.0  5.1 v
    1 24680U 96072A   01183.16443562  .00029800  00000-0  38205-3 0    01
    2 24680  97.8272 245.0275 0482000 180.8523 179.1476 14.83428139    01
    
    USA 116         15.0  3.0  0.0  5.1 v
    1 23728U 95066A   01176.02830438  .00021000  00000-0  44132-3 0    04
    2 23728  97.9050 288.2033 0428000  57.2346 302.7652 14.84289503    00
    
    USA 129 currently is especially well placed for evening observation over a wide
    range of mid-Northern latitudes.
    
    I believe that both KeyHoles are likely to manoeuvre to re-boost their apogee
    sometime in the next 24 h.
    
    The manoeuvres would occur when the objects are near perigee, resulting in an
    increase of orbital period of about 0.7 min, and an increase in apogee of about
    60 km.
    
    I have appended search elements for 96072A, for its first 16 perigee passages
    following Mike McCants' aforementioned obs. Their pseudo-NORAD numbers range
    between 79001 and 79016.
    
    Following are directions for using the data for Western European and North
    American observers. I have chosen those areas because they normally account for
    the vast majority of observations of these objects. Observations are welcome
    from anywhere in the World, and the following advice can be readily adapted to
    any location.
    
    Western Europe
    
    Assuming that there have been no additional observations as of 2001 Jul 02 at
    22:00 UTC, then Western European observers should consider elsets 79001 through
    79011 in planning their obs, as well as the above latest non-maneouvre elset.
    
    First, plot the expected path of the above non-manoeuvre elset. Then plot the
    path of elsets 79001 and 79011 to show the earliest and latest possible
    post-manoeuvre tracks. If those tracks are farther apart than your field of
    view, then plot one or more of the intermediate elsets, such that pairs of
    successive tracks are within the field of view.
    
    When observing, first wait for the object to appear in the non-manoeuvre orbit.
    If it does not arrive at the predicted time, then it has likely manoeuvred, in
    which case, you should shift to the 79001 track, and wait for it to arrive. If
    it fails to arrive at the time predicted for 79001, then switch to your next
    plotted track. If you plotted only every other track, then you should keep in
    mind that the object may arrive on one of the in-between tracks that were not
    plotted.
    
    The object should eventually arrive on or near one of the tracks.
    
    Please report your obs to SeeSat-L. It need not be very detailed. For example,
    "96072A failed to appear on the non-manoeuvre orbit, but an object was seen
    moving in about the orbit 79004 path, within about 1 minute of the predicted
    time of the 79004 path."
    
    North America
    
    If Western European or other observers report having seen 96072A in one of the
    post maneouvre search orbits, 79001 through 79011, then North American
    observers need only wait for the object in the reported search orbit. As a
    hedge against possible erroneous reports of a manoeuvre, it would be wise to
    first wait for the object in the non-maneouvre orbit. If it does not appear,
    then switch to the reported post-manoeuvre orbit.
    
    If the Western European observers are clouded out, or if they fail to report
    the results of their observations, then North American observers will need to
    consider elsets 79001 through at least 79014, in addition to the non-manoeuvre
    elset. The directions for use otherwise are the same as those I provided for
    the Western European observers.
    
    If the Western European observers report that the object had not yet
    manoeuvred, then North American observers need consider only elset 79012
    through 79014.
    
    Eastern North American observers should report their results as quickly as
    possible, so that those further west may benefit.
    
    If the manoeuvres do not occur in the next 24 h, then the next most likely date
    is 2001 Jul 12, when USA 116's perigee crosses the equator.
    
    My schedule is uncertain, but right now, it is doubtful that I will be
    available to participate prior to about 2001 Jun 03 at 03:00 UTC.
    
    Ted Molczan
    
    
    1 79001U          01183.19828704  .00025000  00000-0  33702-3 0    07
    2 79001  97.8272 245.0608 0522000 180.7413   0.0000 14.74000000    08
    
    1 79002U          01183.26570602  .00025000  00000-0  33702-3 0    07
    2 79002  97.8272 245.1272 0522000 180.5201   0.0000 14.74000000    00
    
    1 79003U          01183.33312500  .00025000  00000-0  33702-3 0    07
    2 79003  97.8272 245.1936 0522000 180.2988   0.0000 14.74000000    07
    
    1 79004U          01183.40053241  .00025000  00000-0  33702-3 0    00
    2 79004  97.8272 245.2599 0522000 180.0776   0.0000 14.74000000    07
    
    1 79005U          01183.46795139  .00025000  00000-0  33702-3 0    06
    2 79005  97.8272 245.3263 0522000 179.8564   0.0000 14.74000000    08
    
    1 79006U          01183.53534722  .00025000  00000-0  33702-3 0    04
    2 79006  97.8272 245.3926 0522000 179.6352   0.0000 14.74000000    08
    
    1 79007U          01183.60276620  .00025000  00000-0  33702-3 0    03
    2 79007  97.8272 245.4590 0522000 179.4140   0.0000 14.74000000    00
    
    1 79008U          01183.67017361  .00025000  00000-0  33702-3 0    06
    2 79008  97.8272 245.5254 0522000 179.1928   0.0000 14.74000000    00
    
    1 79009U          01183.73759259  .00025000  00000-0  33702-3 0    03
    2 79009  97.8272 245.5917 0522000 178.9716   0.0000 14.74000000    09
    
    1 79010U          01183.80500000  .00025000  00000-0  33702-3 0    01
    2 79010  97.8272 245.6581 0522000 178.7504   0.0000 14.74000000    02
    
    1 79011U          01183.87239583  .00025000  00000-0  33702-3 0    04
    2 79011  97.8272 245.7245 0522000 178.5292   0.0000 14.74000000    03
    
    1 79012U          01183.93981481  .00025000  00000-0  33702-3 0    03
    2 79012  97.8272 245.7908 0522000 178.3080   0.0000 14.74000000    03
    
    1 79013U          01184.00722222  .00025000  00000-0  33702-3 0    09
    2 79013  97.8272 245.8572 0522000 178.0868   0.0000 14.74000000    03
    
    1 79014U          01184.07464120  .00025000  00000-0  33702-3 0    07
    2 79014  97.8272 245.9236 0522000 177.8656   0.0000 14.74000000    04
    
    1 79015U          01184.14204861  .00025000  00000-0  33702-3 0    00
    2 79015  97.8272 245.9899 0522000 177.6444   0.0000 14.74000000    03
    
    1 79016U          01184.20946759  .00025000  00000-0  33702-3 0    07
    2 79016  97.8272 246.0563 0522000 177.4232   0.0000 14.74000000    07
    
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    This archive was generated by hypermail 2b29 : Mon Jul 02 2001 - 01:11:59 PDT