|Discovered by||Christian Pollas|
|Discovery date||January 4, 1989|
|Alternative names||1934 CT; 1989 AC|
|Minor planet category||Apollo, Alinda,
|Epoch 2012-Mar-14 (JD 2456000.5)|
|Semi-major axis||2.5294 AU
|Orbital period||4.02 a (1469.3 d)|
|Average orbital speed||16.69 km/s|
|Longitude of ascending node||124.50°|
|Argument of perihelion||278.55°|
|Mean density||2.1 g/cm³|
|Equatorial surface gravity||0.0010 m/s²|
|Escape velocity||0.0019 km/s|
|Rotation period||5.41 to 7.33 d|
|Apparent magnitude||8.8 (when near Earth) to 22.4|
|Absolute magnitude (H)||15.30|
4179 Toutatis (// too-TAH-tis) is an Apollo, Alinda, and Mars-crosser asteroid with a chaotic orbit produced by a 3:1 resonance with the planet Jupiter, a 1:4 resonance with the planet Earth, and frequent close approaches to the terrestrial planets, including Earth. It is listed as a potentially hazardous object, although the odds of a collision with the Earth are minute.
On December 12, 2012 at 06:40 UT Toutatis passed within about 18 lunar distances of the Earth. On December 13, the Chinese lunar probe Chang'e 2, launched in 2010 on a lunar mission, flew by Toutatis at a distance of 3.2 kilometers and a relative velocity of 10.73 km/s. Toutatis will approach Earth in 2016, but will not make a notably close approach until 2069.
4179 Toutatis was first sighted on February 10, 1934, as object 1934 CT, and then promptly lost. It remained a lost asteroid for several decades until it was rediscovered on January 4, 1989, by Christian Pollas, and was named after the Celtic god Toutatis (Teutates).
The spectral properties suggest that this is an S-type, or stony asteroid, consisting primarily of silicates. It has a moderately bright Bond albedo of 0.13. Radar imagery shows that Toutatis is a highly irregular body consisting of two distinct "lobes", with maximum widths of about 4.6 km and 2.4 km respectively. It is hypothesized that Toutatis formed from two originally separate bodies which coalesced at some point, with the resultant asteroid being compared to a "rubble pile".
Its rotation combines two separate periodic motions into a non-periodic result; to someone on the surface of Toutatis, the Sun would seem to rise and set in apparently random locations and at random times at the asteroid's horizon. It has a rotation period around its long axis (Pψ) of 5.38 days. This long axis is precessing with a period (Pφ) of 7.38 days. The asteroid may have lost most of its original angular momentum and entered into this tumbling motion as a result of the YORP effect.
With a semimajor axis of 2.5294 AU, or roughly 2.5 times the separation of the Earth from the Sun, Toutatis has a 3:1 orbital resonance with Jupiter and a near-1:4 resonance with Earth. Thus it completes one orbit around the Sun for every 4.02 annual orbits of the Earth. The gravitational perturbations caused by frequent close approaches to the terrestrial planets lead to chaotic behaviour in the orbit of Toutatis, making precise long-term predictions of its location progressively inaccurate over time. Estimates in 1993 put the Lyapunov time horizon for predictability at around 50 years, after which the uncertainty region becomes larger with each close approach to a planet. Without the perturbations from the terrestrial planets the Lyapunov time would be close to 10,000 years. The initial observations which showed its chaotic behaviour were made by Wiśniewski.
The low inclination (0.47°) of the orbit allows frequent transits, where the inner planets Mercury, Venus, Earth, and Mars can appear to cross the Sun as seen from the perspective of the asteroid. Earth did this in January 2009 and July 2012, and will also do so in July 2016 and 2020.
Close approaches and collision risk
Toutatis makes frequent close approaches to Earth, with a currently minimum possible distance (Earth MOID) of just 0.006 AU (2.3 times as far as the Moon). The approach on September 29, 2004, was particularly close, at 0.0104 AU (within 4 lunar distances) from Earth, presenting a good opportunity for observation, with Toutatis shining at magnitude 8.8 when brightest. A close approach of 0.0502 AU (7,510,000 km; 4,670,000 mi) happened on November 9, 2008. The most recent close approach was on December 12, 2012, at a distance of 0.046 AU (6,900,000 km; 4,300,000 mi), with a magnitude of 10.7. At magnitude 10.7, the asteroid was not visible to the naked eye, but just visible to experienced observers using high-end binoculars. During the 2012 encounter Toutatis was recovered on May 21, 2012, by the Siding Spring Survey at apparent magnitude 18.9. The next notable close approach will be November 5, 2069, at a distance of 0.0198486 AU (2,969,310 km; 1,845,040 mi).
Given that Toutatis makes many close approaches the Earth, such as in 1992, 1996, 2000, 2004, 2008, and 2012, it is listed as a potentially hazardous object. With an uncertainty parameter of 0, the orbit of Toutatis is very well determined for the next few hundred years. The probability of the orbit intersecting Earth is essentially zero for at least the next six centuries. The likelihood of collision in the distant future is considered to be very small. As a planet-crossing asteroid, Toutatis is likely to be ejected from the inner Solar System with a time scale of a few million years or less, giving it a limited number of opportunities to strike Earth. As with many near-Earth objects, Toutatis was in 2004 the object for fear mongering by some doomsayers.
Toutatis has been observed with radar imaging from the Arecibo Observatory and the Goldstone Solar System Radar during the asteroid's prior Earth flybys in 1992, 1996, 2000, 2004, and 2008. It was also observed with radar during the December 2012 flyby and potentially will be during the more distant flyby in 2016. After 2016, Toutatis will not pass close to Earth again until 2069.
Resolution of the radar images is as fine as 3.75 m per pixel, providing data to model Toutatis' shape and spin state.
The Chinese lunar probe Chang'e 2 departed from the Sun–Earth L2 point in April 2012 and made a flyby of Toutatis on 13 December 2012, with closest approach being 3.2 kilometers and a relative velocity of 10.73 km/s, when Toutatis was near its closest approach to the Earth.
- List of asteroid close approaches to Earth
- List of asteroids targeted for spacecraft visitation
- List of asteroids/4101–4200
- "JPL Small-Body Database Browser: 4179 Toutatis (1989 AC)". Retrieved 2012-03-23.
- "AstDys (4179) Toutatis Ephemerides for 2004". Department of Mathematics, University of Pisa, Italy. Retrieved 2010-06-27.
- "AstDys (4179) Toutatis Ephemerides 2059". Department of Mathematics, University of Pisa, Italy. Retrieved 2010-06-27.
- "Trick or Treat: It's Toutatis!". Science@Nasa. 2000-10-31. Archived from the original on 29 January 2009. Retrieved 2009-01-27.
- "JPL Close-Approach Data: 4179 Toutatis (1989 AC)". 2011-05-22 last obs (arc=77.28 years). Retrieved 2011-11-13.
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- NEO Earth Close Approaches
- Lakdawalla, Emily (2012-12-14). "Chang'E 2 imaging of Toutatis succeeded beyond my expectations!". The Planetary Society. Retrieved 2012-12-15.
- "(4179) Toutatis = 1934 CT = 1989 AC". IAU Minor Planet Center. Retrieved 2013-04-18.
- Belton, Michael J. S. (August 2002), "The Diagnosis of Complex Rotation in the Lightcurve of 4179 Toutatis and Potential Applications to Other Asteroids and Bare Cometary Nuclei", Icarus 158 (2): 305–311, Bibcode:2002Icar..158..305M, doi:10.1006/icar.2002.6892.
- Bottke, William, Jr. (October 2007), "Implications of the YORP Effect for Our Understanding of Asteroid Evolution", Bulletin of the American Astronomical Society 39: 416, Bibcode:2007DPS....39.0507B.
- "Toutatis is in a 3:1 mean-motion resonance with Jupiter (rotating frame)". Gravity Simulator. Retrieved 2009-01-27.
- Whipple, L.; Shelus, Peter J. (1993). "Long-Term Dynamical Evolution of the Minor Planet (4179) Toutatis". Icarus 105 (2): 408–419. Bibcode:1993Icar..105..408W. doi:10.1006/icar.1993.1137.
- "Solex by Aldo Vitagliano". Retrieved 2009-03-03.
- "NEODys (4179) Toutatis Close Approaches". Department of Mathematics, University of Pisa, Italy. Retrieved 2009-03-20.
- "NEODys (4179) Toutatis Ephemerides for December 2012". Department of Mathematics, University of Pisa, Italy. Retrieved 2010-06-27.
- "(4179) Toutatis = 1934 CT = 1989 AC". IAU Minor Planet Center. Retrieved 2012-10-19.
- Ostro, S. J.; Hudson, R. S.; Rosema, K. D.; Giorgini, J. D.; Winkler, R.; Yeomans, D. K.; Chodas, P. W.; Slade, M. A (1998). "Asteroid 4179 Toutatis: 1996 Radar Observations". Icarus 137: 122–139. hdl:2014/19433.
- David Morrison (September 27, 2004). "Close Flyby This Week from Asteroid Toutatis". Asteroid and Comet Impact Hazards (NASA). Retrieved 2011-11-13.
- "2012 Goldstone Radar Observations of (4179) Toutatis". Retrieved 2012-11-15.
- Big Asteroid Tumbles Harmlessly Past Earth
- Lakdawalla, Emily (2012-06-14). "Chang'E 2 has departed Earth's neighborhood for.....asteroid Toutatis!?". The Planetary Society. Retrieved 2012-11-15.
- ""Pseudo-MPEC" for 2010-050A = SM999CF = Chang'e 2 probe". Retrieved 2012-11-15.
|Wikimedia Commons has media related to: 4179 Toutatis|
- More Chang'E 2 Toutatis flyby images (Emily Lakdawalla : 2013/01/20)
- Chang'E 2 images of Toutatis - December 13, 2012 (Planetary Society)
- CCTV13 Special (all in Mandarin)
- China joined the interplanetary club by successfully imaging the asteroid Toutatis (Franck Marchis December 14, 2012)
- Chinese space probe flies by asteroid Toutatis (Xinhua 2012-12-15)
- Surface Features of Asteroid Toutatis Revealed by Radar (Youtube: JPLnews)
- Goldstone radar images from the 2012 flyby
- Toutatis radar information
- Space.com: Video of Toutatis's close approach to Earth, 29 Sept, 2004
- Interesting views of asteroid
- Astrobiology Magazine article (09/27/04)
- Simulating the orbit of Toutatis exposes its resonance with Jupiter (Gravity Simulator)
- Orbital simulation from JPL (Java) / Ephemeris
- Asteroid 4179 Toutatis' upcoming encounters with Earth and Chang'E 2 (Emily Lakdawalla 2012-12-06)
- Six-Centimeter Radar Observations of 4179 Toutatis
- Size comparison (Source)
- Chang'e 2 fly-bye of Toutatis Presentation from Small Bodies Assessment Group (SBAG) 8 meeting