99942 Apophis

Summary

99942 Apophis (provisional designation 2004 MN4) is a near-Earth asteroid and a potentially hazardous object with a diameter of 370 metres (1,210 feet)[3] that caused a brief period of concern in December 2004 when initial observations indicated a probability up to 2.7% that it would hit Earth on April 13, 2029. Additional observations provided improved predictions that eliminated the possibility of an impact on Earth in 2029. Until 2006, a small possibility nevertheless remained that, during its 2029 close encounter with Earth, Apophis would pass through a gravitational keyhole of no more than about 800 kilometres (500 mi) in diameter,[11][12] which would have set up a future impact exactly seven years later on April 13, 2036. This possibility kept it at Level 1 on the Torino impact hazard scale until August 2006, when the probability that Apophis would pass through the keyhole was determined to be very small and Apophis's rating on the Torino scale was lowered to zero. By 2008, the keyhole had been determined to be less than 1 km wide.[11] During the short time when it had been of greatest concern, Apophis set the record for highest rating ever on the Torino scale, reaching level 4 on December 27, 2004.[13]

99942 Apophis
Model of 99942 Apophis's shape, assuming the entire surface is of a similar composition.
Discovery[1]
Discovered by
Discovery siteKitt Peak[1]
Discovery dateJune 19, 2004
Designations
(99942) Apophis
Pronunciation/əˈpɒfəs/, (trad.) /ˈæpəfəs/
Named after
Ἄποφις Apophis
2004 MN4
AdjectivesApophidian /æpəˈfɪdiən/ (Latin Apŏpidis)
Orbital characteristics[1]
Epoch 13 September 2023
(JD 2453300.5)
Uncertainty parameter 0
Observation arc6267 days (17.16 yr)
Earliest precovery dateMarch 15, 2004
Aphelion1.0994 AU (164.47 million km)
Perihelion0.7461 AU (111.61 million km)
0.9227 AU (138.03 million km)
Eccentricity0.19144
0.89 yr (323.7 d)
30.73 km/s
142.9°
1.11198°/day
Inclination3.339°
203.96°
126.60°
Earth MOID0.00026 AU (39 thousand km)
Jupiter MOID4.12 AU (616 million km)
TJupiter6.464
Physical characteristics
Dimensions
  • 0.370 km (0.230 mi)
  • 0.45 × 0.17 km[2]
Mean radius
  • 0.185 km (0.115 mi)
  • 0.17±0.02 km[2]
Mass6.1×1010 kg (assumed)[3]
Mean density
  • ~3.2 g/cm3[4]
  • 2.6 g/cm3 (assumed)[3]
30.4 h (1.27 d)[1][5]
30.55±0.12 h[6]
30.67±0.06 h[7]
Tumbling:[8]
27.38±0.07 h (precession period),[8] 263±6 h (rotation period),[8] 30.56±0.01 h (period of harmonic with strongest lightcurve amplitude)[8]
Temperature270 K
Sq[5]

Preliminary observations by Goldstone radar in January 2013 effectively ruled out the possibility of an Earth impact by Apophis in 2036.[14] By May 6, 2013 (April 15, 2013, observation arc), the possibility of an impact on April 13, 2036 had been eliminated altogether.[3] In 2036, Apophis will approach the Earth at a third the distance of the Sun in both March and December,[1] but this is about the distance of the planet Venus when it overtakes Earth every 1.6 years. On April 12, 2068, the nominal trajectory has Apophis 1.87 AU (280 million km) from Earth.[15] Entering March 2021, six asteroids each had a more notable cumulative Palermo Technical Impact Hazard Scale rating than Apophis, and none of those has a Torino level above 0.[16][a] On average, an asteroid the size of Apophis (370 metres) is expected to impact Earth once in about 80,000 years.[17] Observations in 2020 by the Subaru telescope confirmed David Vokrouhlický's 2015 Yarkovsky effect predictions.[18] The Goldstone radar observed Apophis March 3–11, 2021, helping to refine the orbit again,[19] and on March 25, 2021, the Jet Propulsion Laboratory announced that Apophis has no chance of impacting Earth in the next 100 years.[20][21] The uncertainty in the 2029 approach distance has been reduced from hundreds of kilometers to now just a couple of kilometers,[22] greatly enhancing predictions of future approaches.

Discovery and naming edit

Asteroid Apophis – closest approach to Earth on April 13, 2029[23]
(00:20; VideoFile; April 29, 2019) (turquoise dots = artificial satellites; pink = International Space Station)

Apophis was discovered on June 19, 2004, by Roy A. Tucker, David J. Tholen, and Fabrizio Bernardi at the Kitt Peak National Observatory.[1] On December 21, 2004, Apophis passed 0.0964 AU (14.42 million km; 8.96 million mi) from Earth.[1] Precovery observations from March 15, 2004, were identified on December 27, and an improved orbit solution was computed.[24][25] Radar astrometry in January 2005 further refined its orbit solution.[26][27] The discovery was notable in that it was at a very low solar elongation (56°) and at very long range (1.1 AU).[citation needed]

When first discovered, the object received the provisional designation 2004 MN4, and early news and scientific articles naturally referred to it by that name. Once its orbit was sufficiently well calculated, it received the permanent number 99942 (on June 24, 2005). Receiving a permanent number made it eligible for naming by its discoverers, and they chose the name "Apophis" on July 19, 2005.[28] Apophis is the Greek name of Apep, an enemy of the Ancient Egyptian sun-god Ra. He is the Uncreator, an evil serpent that dwells in the eternal darkness of the Duat and tries to swallow Ra during his nightly passage. Apep is held at bay by Set, the Ancient Egyptian god of storms and the desert.[29]

Tholen and Tucker, two of the co-discoverers of the asteroid, are reportedly fans of the television series Stargate SG-1. One of the show's persistent villains is an alien named Apophis. He is one of the principal threats to the existence of civilization on Earth through the first few seasons, thus likely why the asteroid was named after him. In the fictional world of the show, the alien's backstory was that he had lived on Earth during ancient times and had posed as a god, thereby giving rise to the myth of the Egyptian god of the same name.[28]

The mythological creature Apophis is pronounced with the accent on the first syllable (/ˈæpəfɪs/). In contrast, the asteroid's name is generally accented on the second syllable (/əˈpɒfɪs/) as the name was pronounced in the TV series.

Physical characteristics edit

 
Comparison between the best-fit convex and nonconvex shape models, and some of the available radar images of (99942) Apophis
 
Comparison of possible size of Apophis asteroid to Eiffel Tower and Empire State Building

Based upon the observed brightness, Apophis's diameter was initially estimated at 450 metres (1,480 ft); a more refined estimate based on spectroscopic observations at NASA's Infrared Telescope Facility in Hawaii by Binzel, Rivkin, Bus, and Tokunaga (2005) is 350 metres (1,150 ft). NASA's impact risk page lists the diameter at 330 metres (1,080 ft) and lists a mass of 4×1010 kg based on an assumed density of 2.6 g/cm3.[3] The mass estimate is more approximate than the diameter estimate, but should be accurate to within a factor of three.[3] Apophis's surface composition probably matches that of LL chondrites.[30]

Based on Goldstone and Arecibo radar images taken in 2012–2013, Brozović et al. have estimated that Apophis is an elongated object 450 × 170 metres in size, and that it is bilobed (possibly a contact binary) with a relatively bright surface albedo of 0.35±0.10. Its rotation axis has an obliquity of −59° against the ecliptic, which means that Apophis is a retrograde rotator.[2]

During the 2029 approach, Apophis's brightness will peak at magnitude 3.1,[31] easily visible to the naked eye, with a maximum angular speed of 42° per hour. The maximum apparent angular diameter will be approximately 2 arcseconds. This is roughly equivalent to the angular diameter of Neptune from earth. Therefore, the asteroid will be barely resolved by ground-based telescopes not equipped with adaptive optics but very well resolved by those that are.[32] Because the approach will be so close, tidal forces are likely to alter Apophis's rotation axis. A partial resurfacing of the asteroid is possible, which might change its spectral class from a weathered Sq- to an unweathered Q-type.[2][30]

Orbit edit

Apophis has a low inclination orbit (3.3°) that varies from just outside the orbit of Venus (0.746 AU) to just outside the orbit of Earth (1.099 AU).[1] After the 2029 Earth approach, the orbit will vary from just inside of Earth's to just inside of Mars's.

Position uncertainty and increasing divergence[1]
Date JPL SBDB
nominal geocentric
distance (AU)
uncertainty
region
(3-sigma)
2004-12-21 0.09638 AU (14.418 million km) n/a
2013-01-09 0.09666 AU (14.460 million km) n/a
2029-04-13 0.000254128 AU (38,017.0 km) ±3.4 km[22]
2036-03-27 0.309756 AU (46.3388 million km) ±130 thousand km[33]
2051-04-20 0.041455 AU (6.2016 million km) ±250 thousand km
2066-09-16 0.069562 AU (10.4063 million km) ±910 thousand km
2116-04-12 0.019462 AU (2.9115 million km) ±13 million km[34][b]
2117-10-07 0.48 AU (72 million km) ±37 million km[35]

2029 close approach edit

The closest known approach of Apophis occurs at April 13, 2029 21:46 UT, when Apophis will pass Earth closer than geosynchronous communication satellites, but will come no closer than 31,600 kilometres (19,600 mi) above Earth's surface.[36][37] Using the June 2021 orbit solution which includes the Yarkovsky effect, the 3-sigma uncertainty region in the 2029 approach distance is about ±3.4 km.[22][1] The distance, a hair's breadth in astronomical terms, is five times the radius of the Earth, ten times closer than the Moon,[37] and closer than the ring of geostationary satellites currently orbiting the Earth.[38][39] It will be the closest asteroid of its size in recorded history. On that date, it will become as bright as magnitude 3.1[31] (visible to the naked eye from rural as well as darker suburban areas, visible with binoculars from most locations).[40] The close approach will be visible from Europe, Africa, and western Asia. During the approach, Earth will perturb Apophis from an Aten-class orbit with a semi-major axis of 0.92 AU to an Apollo-class orbit with a semi-major axis of 1.1 AU.[41] Perihelion will lift from 0.746 AU to 0.895 AU and aphelion will lift from 1.10 AU to 1.31 AU.[41]

Orbital elements for 2029 (pre-flyby) and 2030 (post-flyby)[41]
Parameter Epoch Orbit
type
Orbital
period
Semi-major
axis
Perihelion Aphelion Inclination Eccentricity
Units AU (°)
Pre-flyby 2029 Aten 0.89 years (323.6 days) 0.922 0.746 1.10 3.34° 0.191
Post-flyby 2030 Apollo 1.16 years (423.1 days) 1.103 0.895 1.31 2.22° 0.189
Animation of 99942 Apophis orbit in 2028–2029
 
Around Sun
 
Around Earth
   Sun ·    Earth ·    99942 Apophis  ·    Moon
History of close approaches of large near-Earth objects since 1908 (A)
PHA Date Approach distance in lunar distances Abs. mag
(H)
Diameter (C)
(m)
Ref (D)
Nominal(B) Minimum Maximum
(152680) 1998 KJ9 1914-12-31 0.606 0.604 0.608 19.4 279–900 data
(458732) 2011 MD5 1918-09-17 0.911 0.909 0.913 17.9 556–1795 data
(163132) 2002 CU11 1925-08-30 0.903 0.901 0.905 18.5 443–477 data
69230 Hermes 1937-10-30 1.926 1.926 1.927 17.5 700-900[42] data
69230 Hermes 1942-04-26 1.651 1.651 1.651 17.5 700-900[42] data
2017 NM6 1959-07-12 1.89 1.846 1.934 18.8 580–1300 data
(27002) 1998 DV9 1975-01-31 1.762 1.761 1.762 18.1 507–1637 data
2002 NY40 2002-08-18 1.371 1.371 1.371 19.0 335–1082 data
2004 XP14 2006-07-03 1.125 1.125 1.125 19.3 292–942 data
2015 TB145 2015-10-31 1.266 1.266 1.266 20.0 620-690 data
(137108) 1999 AN10 2027-08-07 1.014 1.010 1.019 17.9 556–1793 data
(153814) 2001 WN5 2028-06-26 0.647 0.647 0.647 18.2 921–943 data
99942 Apophis 2029-04-13 0.0981 0.0963 0.1000 19.7 310–340 data
2017 MB1 2072-07-26 1.216 1.215 2.759 18.8 367–1186 data
2011 SM68 2072-10-17 1.875 1.865 1.886 19.6 254–820 data
(163132) 2002 CU11 2080-08-31 1.655 1.654 1.656 18.5 443–477 data
(416801) 1998 MZ 2116-11-26 1.068 1.068 1.069 19.2 305–986 data
(153201) 2000 WO107 2140-12-01 0.634 0.631 0.637 19.3 427–593 data
(276033) 2002 AJ129 2172-02-08 1.783 1.775 1.792 18.7 385–1242 data
(290772) 2005 VC 2198-05-05 1.951 1.791 2.134 17.6 638–2061 data
(A) This list includes near-Earth approaches of less than 2 lunar distances (LD) of objects with H brighter than 20.
(B) Nominal geocentric distance from the center of Earth to the center of the object (Earth has a radius of approximately 6,400 km).
(C) Diameter: estimated, theoretical mean-diameter based on H and albedo range between X and Y.
(D) Reference: data source from the JPL SBDB, with AU converted into LD (1 AU≈390 LD)
(E) Color codes:   unobserved at close approach   observed during close approach   upcoming approaches

2036 approaches edit

In 2036, Apophis will pass the Earth at a third the distance of the Sun in both March and December.[1] Using the 2021 orbit solution, the Earth approach on March 27, 2036, will be no closer than 0.3089 AU (46.21 million km; 28.71 million mi; 120.2 LD), but more likely about 0.3097 AU (46.33 million km; 28.79 million mi).[1] For comparison, the planet Venus will be closer to Earth at 0.2883 AU (43.13 million km; 26.80 million mi; 112.2 LD) on May 30, 2036.[43][c] On 31 December 2036 Apophis will be a little bit further away than the March approach at about 0.33 AU (49 million km; 31 million mi).

2051 approach edit

Around April 19–20, 2051, Apophis will pass about 0.04 AU (6.0 million km; 3.7 million mi) from Earth and it will be the first time since 2029 that Apophis will pass within 10 million km of Earth.[1]

2066 and 2068 edit

In the 2060s, Apophis will approach Earth in September 2066,[1][44] and then from February 2067 to December 2071, Apophis will remain farther from Earth than the Sun is.[45] On April 12, 2068, JPL Horizons calculates that Apophis will be about 1.864 ± 0.003 AU (278.85 ± 0.45 million km) from Earth,[46][15] making the asteroid much further than the Sun.

By 2116, the JPL Small-Body Database and NEODyS close approach data start to become divergent.[1][44] In April 2116, Apophis is expected to pass about 0.02 AU (3 million km; 8 LD) from Earth, but could pass as close as 0.001 AU (150 thousand km; 0.39 LD) or could pass as far as 0.1 AU (15 million km; 39 LD).[1]

Refinement of close approach predictions edit

Six months after discovery, and shortly after a close approach to Earth on December 21, 2004, the improved orbital estimates led to the prediction of a very close approach on April 13, 2029, by both NASA's automatic Sentry system and NEODyS, a similar automatic program run by the University of Pisa and the University of Valladolid. Subsequent observations decreased the uncertainty in Apophis's trajectory. The probability of an impact event in 2029 temporarily climbed, peaking at 2.7% (1 in 37) on December 27, 2004,[47][48] when the uncertainty region had shrunk to 83,000 km.[49] This probability, combined with its size, caused Apophis to be assessed at level 4 on the Torino scale[13] and 1.10 on the Palermo Technical Impact Hazard Scale, scales scientists use to represent how dangerous a given asteroid is to Earth. These are the highest values for which any object has been rated on either scale. The chance that there would be an impact in 2029 was eliminated by late December 27, 2004, as a result of a precovery image that extended the observation arc back to March 2004.[25] The danger of a 2036 passage was lowered to level 0 on the Torino scale in August 2006.[50] With a cumulative Palermo Scale rating of −3.22,[3] the risk of impact from Apophis is less than one thousandth the background hazard level.[3]

2005 and 2011 observations edit

In July 2005, former Apollo astronaut Rusty Schweickart, as chairman of the B612 Foundation, formally asked NASA to investigate the possibility that the asteroid's post-2029 orbit could be in orbital resonance with Earth, which would increase the probability of future impacts. Schweickart also asked NASA to investigate whether a transponder should be placed on the asteroid to enable more accurate tracking of how its orbit is affected by the Yarkovsky effect.[51] On January 31, 2011, astronomers took the first new images of Apophis in more than 3 years.[52]

 
Illustration of a common trend where progressively reduced uncertainty regions result in an asteroid impact probability increasing followed by a sharp decrease

2013 refinement edit

The close approach in 2029 will substantially alter the object's orbit, prompting Jon Giorgini of JPL to say in 2011, "If we get radar ranging in 2013 [the next good opportunity], we should be able to predict the location of 2004 MN4 out to at least 2070."[53] Apophis passed within 0.0966 AU (14.45 million km; 8.98 million mi) of Earth in 2013, allowing astronomers to refine the trajectory for future close passes.[9][44][54] Just after the closest approach on January 9, 2013,[44] the asteroid peaked at an apparent magnitude of about 15.6.[55] The Goldstone radar observed Apophis during that approach from January 3 through January 17.[56] The Arecibo Observatory observed Apophis once it entered Arecibo's declination window after February 13, 2013.[56] The 2013 observations basically ruled out any chance of a 2036 impact.

A NASA assessment as of February 21, 2013, that did not use the January and February 2013 radar measurements gave an impact probability of 2.3 in a million for 2068.[57] As of May 6, 2013, using observations through April 15, 2013, the odds of an impact on April 12, 2068, as calculated by the JPL Sentry risk table had increased slightly to 3.9 in a million (1 in 256,000).[3]

2015 observations edit

As of January 2019, Apophis had not been observed since 2015, mostly because its orbit kept it very near the Sun from the perspective of Earth. It was not further than 60 degrees from the Sun between April 2014 and December 2019. With the early 2015 observations, the April 12, 2068, impact probability was 6.7 in a million (1 in 150,000), and the asteroid had a cumulative 9 in a million (1 in 110,000) chance of impacting Earth before 2106.[58]

2020–21 observations edit

Apophis in February 2021

No observations of Apophis were made between January 2015 and February 2019, and then observations started occurring regularly in January 2020.[59] In March 2020, astronomers David Tholen and Davide Farnocchia measured the acceleration of Apophis due to the Yarkovsky effect for the first time, significantly improving the prediction of its orbit past the 2029 flyby. Tholen and Farnocchia found that the Yarkovsky effect caused Apophis to drift by about 170 meters per year.[60] In late 2020, Apophis approached the Earth again. It passed 0.11265 AU (16.852 million km; 43.84 LD) from Earth on March 6, 2021, brightening to +15 mag at the time. Radar observations of Apophis were planned at Goldstone in March 2021.[19] The asteroid has been observed by NEOWISE (between December 2020 and April 2021)[61][62] and by NEOSSat (in January 2021).[6][63][7] Apophis was the target of an observing campaign by IAWN, resulting in the collection of light curves, spectra, and astrometry.[6][63][7] The observations were used to practice and coordinate the response to an actual impact threat.[64]

 
Hypothetical risk corridor for an impact on 13 April 2029, based on the 2020–21 planetary defense exercise

On February 21, 2021, Apophis was removed from the Sentry Risk Table, as an impact in the next 100 years was finally ruled out.[65]

Several occultations of bright stars (apparent magnitude 8–11) by Apophis occurred in March and April 2021.[66][67][68][69] A total of five separate occultations were observed successfully, marking the first time that an asteroid as small as Apophis was observed using the occultation method (beating the previous record set in 2019 by asteroid 3200 Phaeton by more than a factor of ten).[67] The first event, on March 7, was successfully observed from the United States by multiple observers.[70][71][66] The next potential occultation, which occurred on March 11, was predicted to be visible from central Europe.[68] This event was missed, mainly because of bad weather (two negative observations were recorded from Greece).[67] On March 22, another occultation was observed only by a single observer from the United States, amateur astronomer Roger Venable. Larger-than-expected residuals in the March 7 data had caused the majority of observers to be deployed outside of the actual path for the March 22 occultation.[66] This single detection then allowed the prediction of several more events that would have been unobservable otherwise, including an occultation on April 4, which was observed from New Mexico, again by Venable, alongside others.[69][66] Two more occultations, observable on April 10 and April 11 from Japan and New Mexico, respectively, were seen by several observers each.[66]

On March 9, 2021, using radar observations from Goldstone taken on March 3–8 and three positive detections of the stellar occultation on March 7, 2021,[72] Apophis became the asteroid with the most precisely measured Yarkovsky effect of all asteroids, at a signal-to-noise ratio (SNR) of 186.4,[73][d] surpassing 101955 Bennu (SNR=181.6).[74]

The 2021 apparition was the last opportunity to observe Apophis before its 2029 flyby.[1]

 
Asteroid 99942 Apophis – radar observations March 8–10, 2021 (March 26, 2021)

History of impact estimates edit

Date Time Status
2004-12-23 The original NASA report mentioned impact chances of "around 1 in 300" in 2029, which was widely reported in the media.[13] The actual NASA estimates at the time were 1 in 233; these resulted in a Torino scale rating of 2, the first time any asteroid had received a rating above 1.
Later that day, based on a total of 64 observations, the estimates were changed to 1 in 62 (1.6%), resulting in an update to the initial report and an upgrade to a Torino scale rating of 4.
2004-12-25 The chances were first reported as 1 in 42 (2.4%) and later that day (based on 101 observations) as 1 in 45 (2.2%). At the same time, the asteroid's estimated diameter was lowered from 440 m to 390 m and its mass from 1.2×1011 kg to 8.3×1010 kg.
2004-12-26 Based on a total of 169 observations, the impact probability was still estimated as 1 in 45 (2.2%), the estimates for diameter and mass were lowered to 380 m and 7.5×1010 kg, respectively.
2004-12-27 Based on a total of 176 observations with an observation arc of 190 days, the impact probability was raised to 1 in 37 (2.7%)[48] with a line of variation (LOV) of only 83,000 km;[49] diameter was increased to 390 m, and mass to 7.9×1010 kg.
Later that afternoon, a precovery increased the span of observations to 287 days, which eliminated the 2029 impact threat.[25] The cumulative impact probability was estimated to be around 0.004%, a risk lower than that of asteroid 2004 VD17, which once again became the greatest-risk object. A 2053 approach to Earth still poses a minor risk of impact, and Apophis was still rated at level one on the Torino scale for this orbit.
2004-12-28 12:23 GMT Based on a total of 139 observations, a value of one was given on the Torino scale for 2044-04-13.29 and 2053-04-13.51.
2004-12-29 01:10 GMT The only pass rated 1 on the Torino scale was for 2053-04-13.51 based on 139 observations spanning 287.71 days (2004-Mar-15.1104 to 2004-Dec-27.8243). (As of February 2013 the 2053 risk is only 1 in 20 billion.)[3]
19:18 GMT This was still the case based upon 147 observations spanning 288.92 days (2004-Mar-15.1104 to 2004-Dec-29.02821), though the close encounters have changed and been reduced to 4 in total.
2004-12-30 13:46 GMT No passes were rated above 0, based upon 157 observations spanning 289.33 days (2004-Mar-15.1104 to 2004-Dec-29.44434). The most dangerous pass was rated at 1 in 7,143,000.
22:34 GMT 157 observations spanning 289.33 days (2004-Mar-15.1104 to 2004-Dec-29.44434). One pass at 1 (Torino scale) 3 other passes.
2005-01-02 03:57 GMT Observations spanning 290.97 days (2004-Mar-15.1104 to 2004-Dec-31.07992) One pass at 1 (Torino scale) 19 other passes.
2005-01-03 14:49 GMT Observations spanning 292.72 days (2004-Mar-15.1104 to 2005-Jan-01.82787) One pass at 1 (Torino scale) 15 other passes.
2005–01 Extremely precise radar observations at Arecibo Observatory[26] refine the orbit further and show that the April 2029 close approach will occur at only 5.7 Earth radii,[27] approximately one-half the distance previously estimated.
2005-02-06 Apophis (2004 MN4) had a 1-in-13,000 chance of impacting in April 2036.[75]
2005-08-07 Radar observation[26] refines the orbit further and eliminates the possibility of an impact in 2035. Only the pass in 2036 remains at Torino scale 1 (with a 1-in-5,560 chance of impact).[76]
2005–10 It is predicted that Apophis will pass just below the altitude of geosynchronous satellites, which are at approximately 35,900 kilometres (22,300 mi).[77] Such a close approach by an asteroid of that size is estimated to occur every 800 years or so.[78]
2006-05-06 Radar observation at Arecibo Observatory[26] slightly lowered the Palermo scale rating, but the pass in 2036 remained at Torino scale 1[79] despite the impact probability dropping by a factor of four.
2006-08-05 Additional observations through 2006 resulted in Apophis being lowered to Torino scale 0.[50] (The impact probability was 1 in 45,000.)[50]
2008-04 Nico Marquardt published a research paper in which he calculated the probability of Apophis to collide with a geosynchronous satellite during its flyby on April 13, 2029, and the consequences of this event to the likelihood of an Earth-collision 2036. Afterwards, the German newspaper Bild published an article stating a 100 times higher probability of an Earth-collision in the year 2036 than Marquardt calculated.[80] Nearly all international press reported the news with false data caused by the review from Bild even though Marquardt denied.[81] This estimate was allegedly confirmed by ESA and NASA[82][80] but in an official statement,[83] NASA denied the wrong statement. The release went on to explain that since the angle of Apophis's approach to the Earth's equator means the asteroid will not travel through the belt of current equatorial geosynchronous satellites, there is currently no risk of collision; and the effect on Apophis's orbit of any such impact would be insignificant.
2008-04-16 NASA News Release 08-103 reaffirmed that its estimation of a 1-in-45,000 chance of impact in 2036 remained valid.[83]
2009-04-29 An animation is released[84] that shows how unmeasured physical parameters of Apophis bias the entire statistical uncertainty region. If Apophis is a retrograde rotator on the small, less-massive end of what is possible, the measurement uncertainty region will get pushed back such that the center of the distribution encounters Earth's orbit. This would result in an impact probability much higher than computed with the Standard Dynamical Model. Conversely, if Apophis is a small, less-massive prograde rotator, the uncertainty region is advanced along the orbit. Only the remote tails of the probability distribution could encounter Earth, producing a negligible impact probability.
2009-10-07 Refinements to the precovery images of Apophis by the University of Hawaii's Institute for Astronomy, the 90-inch Bok Telescope, and the Arecibo Observatory have generated a refined path that reduces the odds of an April 13, 2036, impact to about 1 in 250,000.[85]
Criticism of older published impact probabilities rests on the fact that important physical parameters such as mass and spin that affect its precise trajectory have not yet been accurately measured and hence there are no associated probability distributions. The Standard Dynamical Model used for making predictions simplifies calculations by assuming Earth is a point mass; this can introduce up to 2.9 Earth radii of prediction error for the 2036 approach, and Earth's oblateness must be considered for the 2029 passage to predict a potential impact reliably.[78] Additional factors that can greatly influence the predicted motion in ways that depend on unknown details, are the spin of the asteroid,[86] its precise mass, the way it reflects and absorbs sunlight, radiates heat, and the gravitational pull of other asteroids passing nearby.[78] Small uncertainties in the masses and positions of the planets and Sun can cause up to 23 Earth radii of prediction error for Apophis by 2036.[78]
2013-01 A statistical impact risk analysis of the data up to this point calculated that the odds of the 2036 impact at 7.07 in a billion, effectively ruling it out. The same study looked at the odds of an impact in 2068, which were calculated at 2.27 in a million.[87] First appearance of Sentry virtual impactors that also include mid-October dates.[88]
2013-01-09 The European Space Agency (ESA) announced the Herschel Space Observatory made new thermal infrared observations of the asteroid as it approached Earth. The initial data shows the asteroid to be bigger than first estimated because it is now expected to be less reflective than originally thought.[9] The Herschel Space Observatory observations increased the diameter estimate by 20% from 270 to 325 metres, which translates into a 75% increase in the estimates of the asteroid's volume or mass.[9] Goldstone single-pixel observations of Apophis have ruled out the potential 2036 Earth impact.[14][89][90] Apophis will then come no closer than about 23 million kilometres (14×10^6 mi)—and more likely miss us by something closer to 56 million kilometres (35×10^6 mi).[89] The radar astrometry is more precise than was expected.[89]
2016-03-25 The Sentry Risk Table assessed Apophis as having a 6.7-in-a-million (1-in-150,000) chance of impacting Earth in 2068, and a 9-in-a-million (1-in-110,000) cumulative chance of impacting Earth by 2105.[3]
2020-03 By taking observations of Apophis with the Subaru Telescope in January and March 2020, as well as remeasuring older observations using the new Gaia DR2 star catalog, astronomers positively detect the Yarkovsky effect on Apophis. The asteroid's position is found to shift by 170 meters per year. The Yarkovsky effect is the main source of uncertainty in impact probability estimates for this asteroid.[60]
2021-01-20 The Sentry Risk Table assessed Apophis as having a 2.6-in-a-million (1-in-380,000) chance of impacting Earth in 2068, and a 4.5-in-a-million (1-in-220,000) cumulative chance of impacting Earth by 2107.[3] The previous 2068 odds were 1-in-150,000.
2021-03-15 10:44 JPL solution #207 using observations in 2020 and 2021 reduced the 3-sigma uncertainty region in the 2029 approach distance from ±700 km[91] to about ±3 km.[1] The June 2021 solution showed the Earth approach on March 27, 2036, will be no closer than 0.30889 AU (46.209 million km; 28.713 million mi; 120.21 LD).[1]

Possible impact effects edit

The Sentry Risk Table estimates that Apophis would impact Earth with kinetic energy equivalent to 1,200 megatons of TNT. In comparison, the Chicxulub impact which caused the mass extinction event responsible for wiping out the dinosaurs has been estimated to have released about as much energy as 100,000,000 megatons (100 teratons). The exact effects of any impact would vary based on the asteroid's composition, and the location and angle of impact. Any impact would be extremely detrimental to an area of thousands of square kilometres, but would be unlikely to have long-lasting global effects, such as the initiation of an impact winter.[citation needed] Assuming Apophis is a 370-metre-wide (1,210 ft) stony asteroid with a density of 3,000 kg/m3, if it were to impact into sedimentary rock, Apophis would create a 5.1-kilometre (17,000 ft) impact crater.[17][3]

Expired 2036 path of risk edit

In 2008, the B612 Foundation made estimates of Apophis's path if a 2036 Earth impact were to occur, as part of an effort to develop viable deflection strategies.[92] The result was a narrow corridor a few kilometres wide, called the "path of risk", extending across southern Russia, across the north Pacific (relatively close to the coastlines of California and Mexico), then right between Nicaragua and Costa Rica, crossing northern Colombia and Venezuela, ending in the Atlantic, just before reaching Africa.[93] Using the computer simulation tool NEOSim, it was estimated that the hypothetical impact of Apophis in countries such as Colombia and Venezuela, which were in the path of risk, could have more than 10 million casualties.[94] A deep-water impact in the Atlantic or Pacific oceans would produce an incoherent short-range tsunami with a potential destructive radius (inundation height of >2 m) of roughly 1,000 kilometres (620 mi) for most of North America, Brazil and Africa, 3,000 km (1,900 mi) for Japan and 4,500 km (2,800 mi) for some areas in Hawaii.[95]

Exploration edit

OSIRIS-APEX post-Earth-encounter rendezvous edit

The OSIRIS-REx spacecraft returned a sample of Bennu to Earth on 24 September 2023.[96] After ejecting the sample canister, the spacecraft can use its remaining fuel to target another body during an extended mission. Apophis is the only asteroid which the spacecraft could reach for a long-duration rendezvous, rather than a brief flyby. In April 2022, the extension was approved, and OSIRIS-REx will perform a rendezvous with Apophis in April 2029, a few days after the close approach to Earth. It will study the asteroid for 18 months and perform a maneuver similar to the one it made during sample collection at Bennu, by approaching the surface and firing its thrusters. This will expose the asteroid's subsurface and allow mission scientists to learn more about the asteroid's material properties.[97][98] For its Apophis mission after the sample return, OSIRIS-REx was renamed OSIRIS-APEX (short for OSIRIS-Apophis Explorer).[99]

Other proposed space missions edit

Planetary Society competition edit

In 2007, The Planetary Society, a California-based space advocacy group, organized a $50,000 competition to design an uncrewed space probe that would 'shadow' Apophis for almost a year, taking measurements that would "determine whether it will impact Earth, thus helping governments decide whether to mount a deflection mission to alter its orbit". The society received 37 entries from 20 countries on 6 continents.

The commercial competition was won by a design called 'Foresight' created by SpaceWorks Enterprises, Inc.[100] SpaceWorks proposed a simple orbiter with only two instruments and a radio beacon at a cost of ~US$140 million, launched aboard a Minotaur IV between 2012 and 2014, to arrive at Apophis five to ten months later. It would then rendezvous with, observe, and track the asteroid. Foresight would orbit the asteroid to gather data with a multi-spectral imager for one month. It would then leave orbit and fly in formation with Apophis around the Sun at a range of two kilometres (1.2 miles). The spacecraft would use laser ranging to the asteroid and radio tracking from Earth for ten months to accurately determine the asteroid's orbit and how it might change.

Pharos, the winning student entry, would be an orbiter with four science instruments (a multi-spectral imager, near-infrared spectrometer, laser rangefinder, and magnetometer) that would rendezvous with and track Apophis. Earth-based tracking of the spacecraft would then allow precise tracking of the asteroid. The Pharos spacecraft would also carry four instrumented probes that it would launch individually over the course of two weeks. Accelerometers and temperature sensors on the probes would measure the seismic effects of successive probe impacts, a creative way to explore the interior structure and dynamics of the asteroid.

Second place, for $10,000, went to a European team led by Deimos Space S.L. of Madrid, Spain, in cooperation with EADS Astrium, Friedrichshafen, Germany; University of Stuttgart, Germany; and University of Pisa, Italy. Juan L. Cano was principal investigator.

Another European team took home $5,000 for third place. Their team lead was EADS Astrium Ltd, United Kingdom, in conjunction with EADS Astrium SAS, France; IASF-Roma, INAF, Rome, Italy; Open University, UK; Rheinisches Institut für Umweltforschung, Germany; Royal Observatory of Belgium; and Telespazio, Italy. The principal investigator was Paolo D'Arrigo.

Two teams tied for second place in the Student Category: Monash University, Clayton Campus, Australia, with Dilani Kahawala as principal investigator; and University of Michigan, with Jeremy Hollander as principal investigator. Each second-place team won $2,000. A team from Hong Kong Polytechnic University and Hong Kong University of Science and Technology, under the leadership of Peter Weiss, received an honorable mention and $1,000 for the most innovative student proposal.

Don Quijote mission edit

Apophis is one of two asteroids that were considered by the European Space Agency as the target of its Don Quijote mission concept to study the effects of impacting an asteroid.[101]

Cancelled Chinese mission edit

China had planned an encounter with Apophis in 2022, several years prior to the close approach in 2029. This mission, now known as Tianwen-2, would have included exploration and close study of three asteroids including an extended encounter with Apophis for close observation, and land on the asteroid 1996 FG3 to conduct in situ sampling analysis on the surface.[102] The launch date is now scheduled for 2024, with a different set of targets.

RAMSES edit

Apophis is the target of the European Space Agency's proposed RAMSES (Rapid Apophis Mission for SEcurity and Safety) mission, with a launch in 2027 and rendezvous with the asteroid in 2029.[103]

Proposed deflection strategies edit

Studies by NASA, ESA,[104] and various research groups in addition to the Planetary Society contest teams,[105] have described a number of proposals for deflecting Apophis or similar objects, including gravitational tractor, kinetic impact, and nuclear bomb methods.

On December 30, 2009, Anatoly Perminov, the director of the Russian Federal Space Agency, said in an interview that Roscosmos will also study designs for a possible deflection mission to Apophis.[106]

On August 16, 2011, researchers at China's Tsinghua University proposed launching a mission to knock Apophis onto a safer course using an impactor spacecraft in a retrograde orbit, steered and powered by a solar sail. Instead of moving the asteroid on its potential resonant return to Earth, Shengping Gong and his team believe the secret is shifting the asteroid away from entering the gravitational keyhole in the first place.[107]

On February 15, 2016, Sabit Saitgarayev, of the Makeyev Rocket Design Bureau, announced intentions to use Russian ICBMs to target relatively small near-Earth objects. Although the report stated that likely targets would be between the 20 to 50 metres in size, it was also stated that 99942 Apophis would be an object subject to tests by the program.[108]

In October 2022, a method of mapping the inside of a potentially problematic asteroid, such as 99942 Apophis, in order to determine the best area for impact was proposed.[109]

Popular culture edit

In Id Software's video game Rage, the backstory involves the asteroid colliding with Earth on August 23, 2029. The asteroid almost wipes out the human race and ushers in a post-apocalyptic age.[110]

See also edit

Notes edit

  1. ^ Of the six asteroids with a riskier palermo scale rating than Apophis:
  2. ^ The minimum possible Earth approach between 5–20 April 2116 is 0.001 AU (150 thousand km; 93 thousand mi; 0.39 LD).
  3. ^ On January 8, 2022 Venus was even closer to Earth at 0.2658 AU (39.76 million km; 24.71 million mi; 103.4 LD).
  4. ^ Using the 9 March 2021 solution, JPL gave the strength of the Yarkovsky effect as  , with an uncertainty of  . The SNR, defined as the size of the signal divided by the uncertainty, is  . As of the latest orbit solution (29 June 2021), the SNR is   (again lower than Bennu's).

References edit

  1. ^ a b c d e f g h i j k l m n o p q r s t u "JPL Small-Body Database Browser: 99942 Apophis (2004 MN4)" (last observation: 2021-05-12; arc: 17.16 years; JPL #216 solution date: 2021-Jun-29). Retrieved November 27, 2021.
  2. ^ a b c d e f Brozović, M.; Benner, L. A. M.; McMichael, J. G.; Giorgini, J. D.; et al. (January 15, 2018). "Goldstone and Arecibo radar observations of (99942) Apophis in 2012–2013" (PDF). Icarus. 300: 115–128. Bibcode:2018Icar..300..115B. doi:10.1016/j.icarus.2017.08.032. Retrieved August 19, 2018.
  3. ^ a b c d e f g h i j k l m "99942 Apophis (2004 MN4) Earth Impact Risk Summary". NASA/JPL Center for NEO Studies. January 19, 2021. Archived from the original on May 11, 2013. Retrieved January 19, 2021.
  4. ^ Binzel, R. P. (2007). "Can NEAs be Grouped by Their Common Physical Characteristics?" (PDF). Department of Earth, Atmospheric, and Planetary Sciences, Massachusetts Institute of Technology. aero.org. Archived from the original (PDF) on April 12, 2012.
  5. ^ a b c "99942 Apophis". The Near-Earth Asteroids Data Base at E.A.R.N. Archived from the original on June 16, 2012. Retrieved October 15, 2009.
  6. ^ a b c Reddy, Vishnu; Kelley, Michael S.; Dotson, Jessie; Farnocchia, Davide; et al. (May 31, 2022). "Apophis Planetary Defense Campaign". The Planetary Science Journal. 3 (5): 123. Bibcode:2022PSJ.....3..123R. doi:10.3847/PSJ/ac66eb. S2CID 249227833.
  7. ^ a b c d Pravec, P.; Scheirich, P.; Ďurech, J.; Pollock, J.; et al. (2014). "The tumbling spin state of (99942) Apophis" (PDF). Icarus. 233: 48–60. Bibcode:2014Icar..233...48P. doi:10.1016/j.icarus.2014.01.026. Archived from the original (PDF) on March 5, 2016. Retrieved November 26, 2014.
  8. ^ a b c d ESA (January 9, 2013). "Herschel intercepts asteroid Apophis". European Space Agency (ESA). Retrieved January 9, 2013.
  9. ^ "99942 Apophis dynamical parameters". NEODyS-2. March 14, 2021. Retrieved March 14, 2021.
  10. ^ a b David Noland (November 7, 2006). "5 Plans to Head Off the Apophis Killer Asteroid". Popular Mechanics. Archived from the original on June 12, 2018. Retrieved March 14, 2021.
  11. ^ deGrasse Tyson, N. (March 12, 2008). "Neil deGrasse Tyson – Death By Giant Meteor". Retrieved March 14, 2021 – via YouTube.
  12. ^ a b c Yeomans, D.; Chesley, S.; Chodas, P. (December 23, 2004). "Near-Earth Asteroid 2004 MN4 Reaches Highest Score To Date On Hazard Scale". NASA/JPL CNEOS. Retrieved January 31, 2024. Today's impact monitoring results indicate that the impact probability for April 13, 2029, has risen to about 1.6%, which for an object of this size corresponds to a rating of 4 on the ten-point Torino Scale.
  13. ^ a b "NASA Rules Out Earth Impact in 2036 for Asteroid Apophis". NASA. January 10, 2013. Retrieved January 10, 2013.
  14. ^ a b "99942 Apophis Ephemerides for April 2068". NEODyS (Near Earth Objects – Dynamic Site). Archived from the original on March 10, 2021. Retrieved May 9, 2019.
  15. ^ "Sentry: Earth Impact Monitoring". NASA/JPL Center for NEO Studies. Retrieved March 3, 2021. (Use Unconstrained Settings to reveal 1979 XB with impact probability below 1e-6)
  16. ^ a b Marcus, R.; Melosh, H. J.; Collins, G. (2010). "Earth Impact Effects Program". Imperial College London / Purdue University. Retrieved March 14, 2021. (solution using 370 metres, 3000 kg/m3, 12.6 km/s, 45 degrees)
  17. ^ Schilling, G. (October 27, 2020). "The subtle effect of sunlight may turn the near-Earth asteroid Apophis toward Earth in 2068 . . . but chances for impact remain small". Sky & Telescope. Retrieved November 1, 2020.
  18. ^ a b "Goldstone Radar Observations Planning: 99942 Apophis in 2021". Jet Propulsion Laboratory. March 9, 2021. Retrieved March 19, 2021.
  19. ^ "NASA Analysis: Earth Is Safe From Asteroid Apophis for 100-Plus Years". Jet Propulsion Laboratory. March 25, 2021.
  20. ^ Hurst, Luke (March 28, 2021). "Asteroid Apophis won't hit Earth for at least 100 years, says NASA". euronews. Retrieved April 2, 2021.
  21. ^ a b c "Horizons Batch for Apophis @ 2029-Apr-13 21:46 showing 3-sigma uncertainty of ±3.4km". JPL Horizons. Archived from the original on January 31, 2022. Retrieved September 3, 2021.
  22. ^ Brown, D.; Wendel, J.; Agle, D. C. (April 29, 2019). "Scientists Planning Now for Asteroid Flyby a Decade Away". NASA. Retrieved April 29, 2019.
  23. ^ "MPEC 2004-Y70 : 2004 MN4". IAU Minor Planet Center. December 27, 2004.
  24. ^ a b c Yeomans, D.; Chodas, P.; Chesley, S. (December 27, 2004). "Possibility of an Earth Impact in 2029 Ruled Out for Asteroid 2004 MN4". NASA/JPL CNEOS. Retrieved January 31, 2024.
  25. ^ a b c d "Scheduled Arecibo Radar Asteroid Observations". National Astronomy and Ionosphere Center.
  26. ^ a b Chodas, P.; Chesley, S.; Giorgini, J.; Yeomans, D. (February 3, 2005). "Radar Observations Refine the Future Motion of Asteroid 2004 MN4". NASA's Near Earth Object Program Office. Retrieved January 31, 2024.
  27. ^ a b Cooke, B. (August 18, 2005). "Asteroid Apophis set for a makeover". Astronomy Magazine. Archived from the original on May 29, 2012. Retrieved October 8, 2009.
  28. ^ Hill, J. (2010). "Apep (Apophis)". Ancient Egypt Online. Retrieved July 24, 2021.
  29. ^ a b Reddy, V.; Sanchez, J. A.; Furfaro, R.; Binzel, R. P.; et al. (March 5, 2018). "Surface Composition of (99942) Apophis". The Astronomical Journal. American Astronomical Society. 155 (3): 140. arXiv:1803.05375. Bibcode:2018AJ....155..140R. doi:10.3847/1538-3881/aaaa1c. ISSN 1538-3881. S2CID 78087061.
  30. ^ a b "(99942) Apophis Ephemerides for 13 Apr 2029". NEODyS (Near Earth Objects – Dynamic Site). Retrieved August 19, 2018.
  31. ^ "Neptune from the VLT with and without adaptive optics". ESO. July 18, 2018. Retrieved October 17, 2022.
  32. ^ "Horizons Batch for Apophis @ 2036-Mar-27 08:30 showing 3-sigma uncertainty of ±129145km". JPL Horizons. Archived from the original on July 10, 2023. Retrieved July 10, 2023.
  33. ^ "Horizons Batch for Apophis @ 2116-Apr-12 17:50 showing 3-sigma uncertainty of ±13 million km". JPL Horizons. Retrieved July 31, 2022.
  34. ^ "Horizons Batch for Apophis @ 2117-Oct-07 16:24 showing 3-sigma uncertainty of ±37 million km". JPL Horizons. Retrieved September 30, 2023.
  35. ^ 2029-Apr-13 approach: 0.000254093 AU (38,011.8 km). 38012km "geocentric distance" – 6378km "Earth radius" = 31634km
  36. ^ a b "OSIRIS-REx Spacecraft Departs for New Mission". September 24, 2023.
  37. ^ "List of satellites in geostationary orbit". satsig.net.
  38. ^ Byrd, D. (April 30, 2019). "Preparing for asteroid Apophis | EarthSky.org". earthsky.org. Retrieved May 1, 2019.
  39. ^ "The astronomical magnitude scale". International Comet Quarterly. Retrieved January 19, 2021.
  40. ^ a b c "Horizons Batch for Apophis Orbital Elements for 2029-01-01 and 2030-01-01". JPL Horizons. Retrieved July 31, 2022.
  41. ^ a b Marchis, F.; et al. "Multiple asteroid systems: Dimensions and thermal properties from Spitzer Space Telescope and ground-based observations". Icarus. 221 (2): 1130–1161. Bibcode:2012Icar..221.1130M. doi:10.1016/j.icarus.2012.09.013. Retrieved August 24, 2018.
  42. ^ "Venus 2036-May-30 @ JPL Horizons".
  43. ^ a b c d "NEODyS : (99942) Apophis (Close Approaches)". NEODyS (Near Earth Objects—Dynamic Site). Retrieved March 14, 2021.
  44. ^ "99942 Apophis Ephemerides for 2067–2071". NEODyS (Near Earth Objects – Dynamic Site). Archived from the original on March 11, 2021. Retrieved March 11, 2021. (Delta column is distance from Earth)
  45. ^ "Horizons Batch for Apophis on 2068-Apr-12". JPL Horizons. Retrieved July 31, 2022.
  46. ^ Brown, D. (October 7, 2009). "NASA Refines Asteroid Apophis' Path Toward Earth". NASA's Near Earth Object Program Office. Retrieved January 31, 2024.
  47. ^ a b Fischer, D. (December 27, 2004). "2004 MN4 Earth Impact Risk Summary (computed on Dec 27, 2004)". The Cosmic Mirror. Archived from the original on March 14, 2005. Retrieved November 4, 2011.
  48. ^ a b Virtual Impactor for 2029-04-13 (Stretch LOV = 1.29E+1) * Earth radius of 6,420 km = 82,818 km.
  49. ^ a b c "99942 Apophis (2004 MN4) Earth Impact Risk Summary". NASA/JPL. August 5, 2006. Archived from the original on August 5, 2006. Retrieved January 13, 2013.
  50. ^ Morrison, D. (July 22, 2005). "Schweickart Proposes Study of Impact Risk from Apophis (MN4)". NASA. Archived from the original on September 29, 2009. Retrieved October 8, 2009.
  51. ^ "Hawaii astronomers keep tabs on asteroid Apophis". Astronomy Magazine. March 10, 2011. Retrieved March 10, 2011.
  52. ^ Morrison, D. (April 6, 2011). "Asteroid 2004 MN4 will come scarily close to Earth on April 13, 2029, but it will not hit". Science@NASA.
  53. ^ Vergano, D. (November 10, 2010). "Apophis asteroid encounter in 2013 should help answer impact worries". USA Today ScienceFair. Retrieved November 10, 2010.
  54. ^ "99942 Apophis Ephemerides for 9 Jan 2013". NEODyS (Near Earth Objects – Dynamic Site). Retrieved March 14, 2021.
  55. ^ a b Benner, L. A. M. (January 9, 2013). "99942 Apophis 2013 Goldstone Radar Observations Planning". NASA/JPL Asteroid Radar Research. Retrieved January 9, 2013.
  56. ^ "Apophis Risk Assessment Updated". cneos.jpl.nasa.gov. February 21, 2013. Archived from the original on April 8, 2019.
  57. ^ "Update notes: Apophis (Mar 2015)". Sentry: Earth Impact Monitoring, Operational Notes. NASA/JPL Center for NEO Studies. March 2, 2015. Archived from the original on April 14, 2017. Retrieved May 8, 2019.
  58. ^ "(99942) Apophis Orbit". IAU Minor Planet Center. Retrieved April 1, 2021.
  59. ^ a b Tholen, D.; Farnocchia, D. (October 2020). "Detection of Yarkovsky Acceleration of (99942) Apophis". Bulletin of the American Astronomical Society. 52 (6): 214.06. Bibcode:2020DPS....5221406T.
  60. ^ Satpathy, Akash; Mainzer, Amy; Masiero, Joseph R.; Linder, Tyler; et al. (May 31, 2022). "NEOWISE Observations of the Potentially Hazardous Asteroid (99942) Apophis". The Planetary Science Journal. 3 (5): 124. arXiv:2204.05412. Bibcode:2022PSJ.....3..124S. doi:10.3847/PSJ/ac66d1. S2CID 248118987.
  61. ^ Banner, T. (March 4, 2021). ""Apophis": Gefährlicher Asteroid nähert sich der Erde – Letzte Chance für Forschende" ["Apophis": Hazardous asteroid approaches Earth – last chance for scientists]. Frankfurter Rundschau (in German). Retrieved March 4, 2021.
  62. ^ a b "C53-NEOSSat – Observations and residuals". NEODyS-2. Retrieved March 4, 2021.
  63. ^ Tony Greicius, ed. (May 31, 2022). "Planetary Defense Exercise Uses Apophis as Hazardous Asteroid Stand-In". NASA. Retrieved June 1, 2022.
  64. ^ Removed Objects from Sentry Risk Table
  65. ^ a b c d e "Chasing the Shadow of (99942) Apophis" (PDF). Journal of Occultation Astronomy. 11 (3): 1–2, 24–29. 2021. Retrieved November 27, 2021.
  66. ^ a b c "Apophis' Yarkovsky acceleration improved through stellar occultation". Gaia Image of the Week. European Space Agency (ESA). March 29, 2021. Retrieved November 27, 2021.
  67. ^ a b Tanga, P. (March 10, 2021). "Targeted Campaigns – Apophis 2021". Archived from the original on March 12, 2021. Retrieved March 12, 2021.
  68. ^ a b "Lifetime Achievement Award of the International Occultation Timing Association". asteroidoccultation.com. International Occultation Timing Association. 2021. Retrieved November 27, 2021.
  69. ^ Marchis, F. (March 10, 2021). "We Got it! The Story of Astronomers and Citizen Astronomers Catching Hazardous Apophis Asteroid over Colorado and Louisiana". SETI Institute. Archived from the original on March 10, 2021. Retrieved March 13, 2021.
  70. ^ "Asteroidal Occultation Reviewed Results for North America – 2021 Asteroidal Occultation Preliminary Results". asteroidoccultation.com. March 8, 2021. Archived from the original on March 14, 2021. Retrieved March 12, 2021.
  71. ^ "Reports of Apophis occultation 2021 Mar. 7 for our stations 3 and 4 near Oakdale, Louisiana (SwRI lines A28 and A30)". Verenigung veer Sterrenkunde. March 9, 2021. Retrieved March 13, 2021. (requires registration)
  72. ^ "JPL Small-Body Database Browser: 99942 Apophis (2004 MN4)" (last observation: 2021-03-08; arc: 16.98 years; JPL #206 solution date: 2021-Mar-09). March 9, 2021. Archived from the original on March 11, 2021. Retrieved March 11, 2021.
  73. ^ Bamberger, D.; Wells, G. (September 2018). "Detection of the Yarkovsky Effect on 1998 SD9 from Optical Observations". Research Notes of the AAS. 2 (3): 164. Bibcode:2018RNAAS...2..164B. doi:10.3847/2515-5172/aadf80. S2CID 125805680.
  74. ^ "2004 MN4 Earth Impact Risk Summary". NASA/JPL. February 5, 2005. Archived from the original on February 6, 2005. Retrieved January 13, 2013.
  75. ^ "99942 Apophis Earth Impact Risk Summary". NASA JPL. October 18, 2005. Archived from the original on October 18, 2005. Retrieved January 13, 2013.
  76. ^ Wee, L. K.; Goh, G. H. (December 14, 2012). "A geostationary Earth orbit satellite model using Easy Java Simulation". Physics Education. IOP Publishing. 48 (1): 72–79. arXiv:1212.3863. doi:10.1088/0031-9120/48/1/72. ISSN 0031-9120. S2CID 119208827.
  77. ^ a b c d Giorgini, J. (October 2007). "Predicting Apophis' Earth Encounters in 2029 and 2036". Archived from the original on January 15, 2016.
  78. ^ "99942 Apophis (2004 MN4) Earth Impact Risk Summary". NASA/JPL. July 1, 2006. Archived from the original on July 1, 2006. Retrieved January 13, 2013.
  79. ^ a b Sauerbier, M. (April 4, 2008). "Ich habe den Weltuntergang ausgerechnet!" [I have calculated the apocalypse]. Bild (in German). Archived from the original on August 9, 2018. Retrieved March 14, 2021.
  80. ^ "NASA refutes story of boy who predicted asteroid collision". CBC/Radio-Canada. April 16, 2008. Retrieved November 8, 2015.
  81. ^ "German schoolboy, 13, corrects NASA's asteroid figures". Archived from the original on April 20, 2008. Retrieved April 16, 2008.
  82. ^ a b Brown, D. (April 16, 2008). "NASA Statement on Student Asteroid Calculations". NASA. Retrieved April 28, 2008.
  83. ^ "99942 Apophis (2004 MN4)". neo.jpl.nasa.gov. Archived from the original on March 2, 2017. Retrieved August 9, 2017.
  84. ^ Brown, D. (October 7, 2009). "NASA Refines Asteroid Apophis' Path Toward Earth". Archived from the original on October 9, 2009. Retrieved October 7, 2009.
  85. ^ Giorgini, J. "Apophis Trajectory Change 2018–2036: Energy Reflection, Absorption, and Emission". NASA. Archived from the original on November 9, 2007.
  86. ^ Farnocchia, D.; Chesley, S. R.; Chodas, P. W.; Micheli, M. (2013). "Yarkovsky-driven impact risk analysis for asteroid (99942) Apophis". Icarus. 224 (1): 192. arXiv:1301.1607. Bibcode:2013Icar..224..192F. doi:10.1016/j.icarus.2013.02.020. S2CID 119088923.
  87. ^ "99942 Apophis (2004 MN4) Earth Impact Risk Summary". NASA/JPL. January 9, 2013. Archived from the original on January 10, 2013. Retrieved March 13, 2021.
  88. ^ a b c Kelly Beatty (January 9, 2013). "Asteroid Apophis Takes a Pass in 2036". Sky & Telescope. Retrieved November 10, 2014.
  89. ^ Phil Plait (January 10, 2013). "Impact Threat from Near-Earth Asteroid Apophis in 2036 Now Ruled Out". Slate. Bad Astronomy blog. Retrieved January 10, 2013.
  90. ^ "JPL Small-Body Database Browser". November 6, 2020. Archived from the original on November 6, 2020.
  91. ^ Schweickart, R. "Threat Characterization: Trajectory dynamics (White Paper 39)" (PDF). Figure 4, pp. 9. B612 Foundation. Archived from the original (PDF) on February 28, 2008. Retrieved February 22, 2008.
  92. ^ Range of Possible Impact Points on April 13, 2036 in Scenarios for Dealing with Apophis, by Donald B. Gennery, presented at the Planetary Defense Conference. Washington, DC. March 5–8, 2007 (archived from the original on 2012-04-12).
  93. ^ Baileya, N. J. (2006). "Near Earth Object impact simulation tool for supporting the NEO mitigation decision making process". Near Earth Objects. 236: 477. Bibcode:2007IAUS..236..477B. doi:10.1017/S1743921307003614.
  94. ^ Paine, M. P. (January 1999). "The Threat is Out There" (PDF). Science of Tsunami Hazards. 17 (3): 155. Archived (PDF) from the original on June 6, 2015. Retrieved March 14, 2021.
  95. ^ OSIRIS-REx factsheet (PDF). Explorers and Heliophysics Projects Division. ehpd.gsfc.nasa.gov (Report). Goddard SFC: NASA. August 2011.   This article incorporates text from this source, which is in the public domain.
  96. ^ Bartels, M. (January 19, 2021). "NASA's OSIRIS-REx probe could make a 2nd stop at infamous asteroid Apophis". Space.com. Retrieved January 28, 2021.
  97. ^ Lauretta, D. S.; Bierhaus, E. B.; Binzel, R. P.; Bos, B. J. (November 6, 2020). OSIRIS-REx at Apophis: Opportunity for an Extended Mission (PDF). Apophis T–9 Years: Knowledge Opportunities for the Science of Planetary Defense.
  98. ^ Mace Kelley, Mikayla (April 25, 2022). "NASA gives green light for OSIRIS-REx spacecraft to visit another asteroid". University of Arizona News. Retrieved April 26, 2022.
  99. ^ Rincon, P. (February 26, 2008). "US team wins asteroid competition". Retrieved March 25, 2009.
  100. ^ "Don Quijote concept". esa.int. European Space Agency. April 4, 2006. Archived from the original on September 4, 2006.
  101. ^ Yu Fei (March 7, 2017). "Riding an asteroid: China's next space goal". Xinhua News. Retrieved May 1, 2017.
  102. ^ Morelli, Andrea C.; Mannocchi, Alessandra; et al. (September 2023). "Initial Trajectory Assessment of the RAMSES Mission to (99942) Apophis". arXiv:2309.00435 [astro-ph.EP].
  103. ^ Izzo, D.; Bourdoux, A.; Walker, R.; Ongaro, F. (2006). "Optimal Trajectories for the Impulsive Deflection of NEOs" (PDF). Acta Astronautica. 59 (1–5): 294–300. Bibcode:2006AcAau..59..294I. doi:10.1016/j.actaastro.2006.02.002.
  104. ^ "Scenarios for Dealing with Apophis" (PDF). The Aerospace Corporation. Archived from the original (PDF) on August 27, 2008. Retrieved July 18, 2008.
  105. ^ Isachenkov, V. (December 30, 2009). "Russia may send spacecraft to knock away asteroid". Yahoo! News. Archived from the original on January 2, 2010. Retrieved December 31, 2009.
  106. ^ "China Reveals Solar Sail Plan To Prevent Apophis Hitting Earth in 2036". Technology Review Physics arXiv Blog. August 18, 2011. Archived from the original on November 26, 2011. Retrieved March 14, 2021.
  107. ^ Khoury, A. (February 15, 2016). "Russia wants to target near-Earth objects with its ICBMs". TASS in foxnews.com. Retrieved February 15, 2016.
  108. ^ Verma, Pranshu (October 21, 2022). "There's a new tool to help blow up asteroids – Researchers from MIT and Stanford have created a tool that could improve the aim of future planetary defense missions". The Washington Post. Retrieved October 22, 2022.
  109. ^ Winegarner, T. (November 6, 2019). "Rage Interview: We speak with id's Tim Willits about their new IP, Rage". Gamespot.

External links edit

  • Müller, T. G.; Kiss, C.; Scheirich, P.; Pravec, P.; et al. (2014). "Thermal infrared observations of asteroid (99942) Apophis with Herschel". Astronomy & Astrophysics. 566: A22. arXiv:1404.5847. Bibcode:2014A&A...566A..22M. doi:10.1051/0004-6361/201423841. S2CID 119282830.
  • Apophis Asteroid
  • Asteroid Apophis orbit from recent observations, EPSC Abstracts Vol. 6, EPSC-DPS2011-1212, 2011, EPSC-DPS Joint Meeting 2011
  • Diagrams and orbits of Apophis (Sormano Astronomical Observatory)
  • Interactive 3D gravity simulation of Apophis's 2029 Earth flyby

Risk assessment

  • Apophis Orbital Prediction Page at NASA JPL
  • 99942 Apophis page from NEODyS
  • MBPL – Minor Body Priority List (technical List) at Sormano Observatory
  • TECA – Table of Asteroids Next Closest Approaches to the Earth at Sormano Observatory

NASA

  • Possibility of an Earth Impact in 2029 Ruled Out for Asteroid 2004 MN4 (JPL)
  • Radar Observations Refine the Future Motion of Asteroid 2004 MN4 (JPL)
  • Animation explaining how impact risk is determined from Impact Probability
  • 99942 Apophis at the JPL Small-Body Database
    • Close approach · Discovery · Ephemeris · Orbit diagram · Orbital elements · Physical parameters
Preceded by Large NEO Earth close approach
(inside the orbit of the Moon)

13 April 2029
Succeeded by