Re: Distant satellite

Mike McCants (mikem@fc.net)
Mon, 8 Dec 1997 00:25:12 -0600 (CST)

>94004C
>1 22987U 94004C   94104.94558226 -.00001003 +00000-0 +10000-3 0 00321
>2 22987 067.0741 059.5229 9058578 202.4707 043.9901 00.46882193001010

I have run 2 (independent) programs and they agree that the orbit
of this object intersected the Earth's surface only a few weeks
after the epoch of this elset.

>1 90000U 97000  A 97339.46596080  .00000000 +00000-0 +00000-0 0 00000
>2 90000 066.3122 250.4967 8611650 336.2076 000.0000  0.41258420000000

>The elements below are, I'm afraid,
>in the J2000 equator frame rather than the usual B1950 one.

The usual is epoch-of-date.  I adjusted the RAAN by -0.04 and came up
with:

1 90000U 97000  A 97339.46547469  .00000000  00000-0  00000+0 0    03
2 90000  66.3122 250.4567 8611650 336.2076    .0000   .41258420    00

Then I tried adjusting the mean motion and the argument of perigee
and came up with:

1 90000U 97000  A 97339.46629645  .00000000  00000-0  00000+0 0    00
2 90000  66.3122 250.4567 8611650 335.9406    .2670   .41758420    03

This seemed to fit the observations just as well.

(Disclaimer: my program is incapable of working with such accurate
observations.)

This would lead to a different time of prediction by about 30 minutes
tonight.

Predictions for me for tonight:

***  97 Dec  7 Sun evening  *** Times are CST ***

  U  MAG    HGT ALT AZI  HRS MIN     R  A    DEC  RANGE
128 13.0  46960  72 343   10  45    2 46.9  47.2  47144
129 13.1  48956  70 328   11  15    2 48.9  45.9  49172
130 13.2  50868  67 317   11  45    2 50.7  44.7  51153
131 13.3  52699  63 309   12  15    2 52.4  43.6  53093

Moving on out to 50000 miles with a magnitude of 12, 13, 14 or ?

Tomorrow night - apogee at 84000 miles.

Here is an interesting entry from Joel Runes' catalog:

Phobos 1           ESCAPE TRAJECTORY      
1 19281U 88058A   88189.82152778 -.00000186  00000-0  00000-0 0    03
2 19281  50.8034 202.3051 8765244  10.5547   6.5019  0.44066780    00

But it would seem that an orbit like this could not evolve into
the observed orbit.

If I try to use this orbit:

1 90000U 97000  A 97339.46547469  .00000000  00000-0  00000+0 0    03
2 90000  66.3122 250.4567 8611650 336.2076    .0000   .41258420    00

and I try to go backwards in time (my program is not set up to
do this, so I am manually iterating), I end up with an eccentricity
that gets larger and intersects the Earth about 2 years ago:

1 90000U 97000  A 95340.91596080  .00000000 +00000-0 +00000-0 0    00
2 90000  63.8122 263.4967 9100000 326.2076 000.0000  0.41258420    00

Mike McCants