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Apollo asteroid
Apollo asteroid
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Common orbital subgroups of Near-Earth Objects (NEOs)

The Apollo asteroids are a group of near-Earth asteroids named after 1862 Apollo, discovered by German astronomer Karl Reinmuth in the 1930s. They are Earth-crossing asteroids that have an orbital semi-major axis greater than that of the Earth (a > 1 AU) but perihelion distances less than the Earth's aphelion distance (q < 1.017 AU).[1][2]

As of January 2025, the number of known Apollo asteroids is 21,083, making the class the largest group of near-Earth objects (cf. the Aten, Amor and Atira asteroids), of which 1,742 are numbered (asteroids are not numbered until they have been observed at two or more oppositions), 81 are named, and 2,130 are identified as potentially hazardous asteroids.[3][4]

The closer their semi-major axis is to Earth's, the less eccentricity is needed for the orbits to cross. The Chelyabinsk meteor, that exploded over the city of Chelyabinsk in the southern Urals region of Russia on February 15, 2013, injuring an estimated 1,500 people with flying glass from broken windows, was an Apollo-class asteroid.[5][6]

Apollo asteroids are generally named after Greek deities.[7]

List

[edit]

The largest known Apollo asteroid is 1866 Sisyphus, with a diameter of about 8.5 km. Examples of known Apollo asteroids include:

Designation Year Discoverer/First observed (A) Ref
2025 PU 2025 Zwicky Transient Facility MPC
2024 PT5 2024 ATLAS-SAAO MPC
2019 SU3 2019 ATLAS-HKO MPC
2016 WF9 2016 NEOWISE MPC
(671294) 2014 JO25 2014 CSS MPC
2013 FW13 2013 CSS MPC
2013 RH74 2013 CSS MPC
2011 MD 2011 LINEAR MPC(B)
2011 EO40 2011 CSS–Mount Lemmon Survey MPC
2010 AL30 2010 LINEAR MPC
(529366) 2009 WM1 2009 CSS MPC
2009 DD45 2009 Siding Spring Observatory, Australia MPC
(386454) 2008 XM 2008 LINEAR List
2008 TC3 2008 CSS MPC
2008 FF5 2008 CSS–Mount Lemmon Survey MPC
2007 VK184 2007 CSS MPC
2007 TU24 2007 CSS MPC
2007 WD5 2007 CSS MPC
2007 OX 2007 CSS–Mount Lemmon Survey MPC
(277810) 2006 FV35 2006 Spacewatch List
(394130) 2006 HY51 2006 LINEAR List
(292220) 2006 SU49 2006 Spacewatch List
(308635) 2005 YU55 2005 R. S. McMillan, Steward Observatory, Kitt Peak, USA List
2005 WY55 2005 Mount Lemmon Survey MPC
2005 HC4 2005 LONEOS MPC
(612901) 2004 XP14 2004 LINEAR MPC
(374158) 2004 UL 2004 LINEAR List
(357439) 2004 BL86 2004 LINEAR List
(444004) 2004 AS1 2004 LINEAR List
2003 RW11 2003 James Whitney Young MPC
2003 BV35 2003 James Whitney Young MPC
(89958) 2002 LY45 2002 LINEAR List
(179806) 2002 TD66 2002 LINEAR List
54509 YORP 2000 LINEAR List
162173 Ryugu 1999 LINEAR List
(137108) 1999 AN10 1999 LINEAR List
101955 Bennu 1999 LINEAR (Bennu is the target of the OSIRIS-REx mission) List
1998 KY26 1998 Spacewatch MPC
(433953) 1997 XR2 1997 LINEAR List
65803 Didymos 1996 Spacewatch List
69230 Hermes 1937 Karl Reinmuth List
(53319) 1999 JM8 1999 LINEAR List
(52760) 1998 ML14 1998 LINEAR List
(35396) 1997 XF11 1997 Spacewatch List
25143 Itokawa 1998 LINEAR List
(136617) 1994 CC 1994 Spacewatch List
(175706) 1996 FG3 1996 R. H. McNaught, Siding Spring Observatory, Australia List
6489 Golevka 1991 Eleanor F. Helin List
4769 Castalia 1989 Eleanor F. Helin List
4660 Nereus 1982 Eleanor F. Helin List
4581 Asclepius 1989 Henry E. Holt, Norman G. Thomas List
4486 Mithra 1987 Eric Elst, Vladimir Shkodrov List
14827 Hypnos 1986 Carolyn S. Shoemaker, Eugene Merle Shoemaker List
4197 Morpheus 1982 Eleanor F. Helin, Eugene Merle Shoemaker List
4183 Cuno 1959 Cuno Hoffmeister List
4179 Toutatis 1989 Christian Pollas List
4015 Wilson–Harrington   1979 Eleanor F. Helin List
3200 Phaethon 1983 Simon F. Green, John K.Davies / IRAS List
2063 Bacchus 1977 Charles T. Kowal List
1866 Sisyphus 1972 Paul Wild List
1620 Geographos 1951 Albert George Wilson, Rudolph Minkowski List
(29075) 1950 DA 1950 Carl A. Wirtanen List
1566 Icarus 1949 Walter Baade List
1685 Toro 1948 Carl A. Wirtanen List
2101 Adonis 1936 Eugène Joseph Delporte List
1862 Apollo 1932 Karl Reinmuth List
(A)Discoverer:
A discoverer is determined by the MPC when the object is numbered. For unnumbered bodies, the table gives the "first observer".
LINEAR: Lincoln Near-Earth Asteroid Research
CSS : Catalina Sky Survey
Spacewatch, on Kitt Peak, near Tucson, Arizona[8]

(B)Classification:

2011 MD is classified as Amor, not Apollo asteroid by the MPC

See also

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References

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[edit]
Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
Apollo asteroids are a dynamical class of near-Earth asteroids characterized by orbits with semi-major axes greater than 1.0 and perihelion distances less than 1.017 , enabling them to cross 's orbital path around the Sun. This group represents Earth-crossing near-Earth objects (NEOs) whose average distances from the Sun exceed that of but whose closest approaches bring them inside 's orbit. Named after the prototype asteroid 1862 Apollo, discovered on April 24, 1932, by German astronomer Karl Reinmuth at Observatory, the Apollo class was the first identified group of such potentially hazardous bodies, though the asteroid itself was lost after discovery and not recovered until 1973. As the largest subgroup of near-Earth asteroids, Apollo asteroids number over 20,000 known members as of 2025, with ongoing surveys such as Pan-STARRS and ATLAS discovering hundreds more annually. These objects typically range in size from a few meters to about 10 km in diameter, with most being smaller than 5 km and exhibiting irregular, elongated shapes due to their formation histories. Compositionally diverse, they include primitive carbonaceous (C-type) bodies rich in volatiles and organics, as well as differentiated stony (S-type) asteroids dominated by silicates and metals, reflecting origins likely in the main asteroid belt perturbed by gravitational resonances. Notable examples include the S-type asteroid (99942) Apophis, renowned for its close 2029 flyby of Earth at about 31,600 km, and the C-type (101955) Bennu, from which NASA's OSIRIS-REx mission returned samples in 2023 containing water, amino acids, and other primitive materials, providing insights into solar system formation. Due to their Earth-crossing trajectories, Apollo asteroids are a primary focus of planetary defense efforts, with many classified as potentially hazardous objects (PHOs) if larger than 140 meters and approaching within 0.05 AU of Earth.

Definition and characteristics

Orbital parameters

Apollo asteroids are near-Earth objects characterized by a semi-major axis a>1a > 1 and a perihelion q<1.017q < 1.017 . These parameters place their average orbital distance beyond Earth's but ensure their closest solar approach falls within or near Earth's orbital path, enabling potential intersections with Earth's orbit around the Sun. The semi-major axis exceeding 1 AU means Apollo asteroids spend most of their orbital period farther from the Sun than Earth on average, yet the perihelion constraint requires sufficient orbital elongation to dip inside Earth's aphelion distance of approximately 1.017 AU. This configuration demands a minimum eccentricity to facilitate Earth-crossing; typically, e>0.3e > 0.3, though values vary. For instance, the namesake 1862 Apollo has e0.56e \approx 0.56. The perihelion distance is calculated as q=a(1e)q = a(1 - e), illustrating how higher eccentricity pulls the closest approach inward for a given semi-major axis; many Apollos exhibit e0.5e \approx 0.5, yielding qq values around 0.7–0.8 AU for a1.4a \approx 1.4 AU. These orbital traits result in highly elliptical paths that intersect , posing risks of close encounters or collisions, though actual impacts depend on timing and relative positions. A notable low-eccentricity subgroup within the Apollos is the asteroids, which maintain orbits closely resembling Earth's with e<0.15e < 0.15 and low inclinations, often behaving as temporary quasi-satellites.

Physical properties

Apollo asteroids exhibit a broad range of sizes, with diameters spanning from a few meters to roughly 10 km, although the vast majority have diameters less than 1 km. This size distribution reflects the overall population dynamics of near-Earth asteroids, where smaller objects dominate due to observational biases and evolutionary processes such as collisional grinding. The largest known Apollo asteroid is 1866 Sisyphus, measured at approximately 8.5 km in diameter. In terms of composition, Apollo asteroids are predominantly classified as S-type, characterized by stony, silicate-rich surfaces akin to ordinary chondritic meteorites, with a notable minority of C-type carbonaceous objects. Spectral analyses confirm this dominance, with S-types comprising around 50% or more of observed Apollos in recent surveys, alongside subtypes like Q and Sq that indicate varying degrees of space weathering. Typical geometric albedos for these bodies range from 0.1 to 0.3, higher for S-types (around 0.15) and lower for C-types (around 0.05), influencing their visibility and thermal properties. Rotation periods for Apollo asteroids typically span 2 to 20 hours, with a significant population of fast rotators (periods under 5 hours) driven by the Yarkovsky-O'Keefe-Radzievskii-Paddack (YORP) effect. This thermal torque mechanism accelerates spin rates, particularly for smaller bodies, leading to a bimodal distribution where fast rotators exceed 5 revolutions per day and slow rotators fall below 0.8 revolutions per day. These rates are derived from extensive photometric monitoring of small near-Earth objects. Structurally, Apollo asteroids display irregular, elongated shapes and are frequently modeled as rubble piles—loose aggregates of smaller components held by gravity rather than monolithic rock. Densities vary from 1.5 to 3.5 g/cm³, with S-types averaging 2.0–2.7 g/cm³ (e.g., as measured for asteroid 433 Eros) and C-types lower at 1.0–1.3 g/cm³, consistent with porous, fragmented interiors. Compared to other near-Earth groups, Apollos feature a higher proportion of S-types than Atens (which have more Q-types from frequent Earth encounters refreshing surfaces) or Amors (enriched in primitive C- and D-types from outer belt origins).

History

Discovery of the group

The first asteroid recognized as an Earth-crosser and namesake of the Apollo group, 1862 Apollo (provisional designation 1932 HA), was discovered on April 24, 1932, by German astronomer Karl Reinmuth at Heidelberg Observatory using photographic plates taken during routine surveys of the sky. This object, observed moving rapidly against the stellar background, was initially tracked for a short period but soon lost due to its faint magnitude and eccentric orbit, preventing further immediate follow-up observations. Its recovery in 1973 marked a significant milestone in confirming its trajectory and Earth-crossing nature. Early identifications of additional Apollo asteroids occurred sporadically before 1950, with key examples including 2101 Adonis (1936 CA), discovered in 1936, and 69230 Hermes (1937 UB), found in 1937—both also by Reinmuth—alongside 1566 Icarus (1949 MA), identified in 1949 by Walter Baade at Palomar Observatory. These pre-1950 discoveries highlighted the group's defining characteristic of orbits intersecting Earth's path, though observations were limited by the era's telescopic capabilities. In 1951, astronomer Dirk Brouwer conducted detailed orbital calculations, incorporating secular perturbations to affirm the Earth-crossing status of these objects through long-term evolutionary models of their paths. By this time, the provisional 1932 HA observations had been linked to Apollo, solidifying its role as the prototype. The 1960s saw a notable increase in interest and observations, driven by the close approach of Icarus in June 1968, when it passed within 0.042 AU of Earth—the nearest recorded for any asteroid at that point. This event prompted the first radar detections of an asteroid, using facilities at Goldstone and Haystack, which estimated Icarus's size at approximately 1 km and underscored the potential collision risks posed by such bodies to Earth. Although radar provided unprecedented data on its shape and rotation, optical follow-ups by teams including those at Cornell University contributed to refined trajectory predictions, amplifying awareness of the hazard potential among astronomers. From 1932 to 1973, only about a dozen Apollo asteroids were known, reflecting the challenges of detecting these faint, fast-moving objects with pre-digital survey methods. The group derives its name from Greek mythology, with prototypes like Apollo (the sun god) and Icarus (the figure who flew too close to the sun) evoking themes of proximity to celestial and terrestrial boundaries. This early phase of discovery laid the groundwork for formal classification as a distinct dynamical group of near-Earth objects.

Evolution of classification

The formal classification of the Apollo group as a distinct category of near-Earth asteroids (NEAs) was established in 1973 by Brian G. Marsden, then director of the Minor Planet Center (MPC), who named it after the prototype asteroid 1862 Apollo, discovered in 1932. Marsden defined Apollo asteroids as Earth-crossing objects with semi-major axes greater than 1 AU and perihelion distances less than 1.017 AU, integrating them into an initial two-group taxonomic system for NEAs that also included the Amor group (Earth-approaching objects with perihelion distances between 1.017 AU and 1.3 AU). This system, based primarily on perihelion relative to Earth's orbit at 1 AU, provided an initial framework for distinguishing dynamical behaviors among NEAs and emphasized Apollo objects as potential collision hazards due to their orbit-crossing nature. The Aten group (Earth-crossers with semi-major axes less than 1 AU and aphelion distances greater than 0.983 AU) was added later, following the discovery of its prototype 2062 Aten in 1976. Refinements to the classification emerged in the 1980s, incorporating eccentricity thresholds alongside perihelion to better account for orbital stability and potential resonances, as dynamical models revealed the influence of Jovian perturbations on Apollo trajectories. Eugene M. Shoemaker, through the Palomar Planet-Crossing Asteroid Survey (PCAS), updated the taxonomy by integrating observational data from enhanced surveys, including the adoption of charge-coupled device (CCD) technology by the Spacewatch program in 1983, which improved detection of high-eccentricity Apollo members. Shoemaker's work also emphasized dynamical modeling, such as studies of the 3:1 Kirkwood gap resonance published by Jack Wisdom in 1985, to refine boundaries and estimate populations, projecting around 1,080 ± 500 NEAs brighter than magnitude 17.7 by 1988 based on 55 known Earth-crossers. The Apollo classification became integral to broader NEA taxonomy as crossers of Earth's orbit (often termed CNEA), contrasting with non-crossing groups like Amor, with the MPC providing ongoing updates to orbital elements and designations through its relocation to the Smithsonian Astrophysical Observatory in 1978. Spectral classifications, such as David J. Tholen's 1984 system using eight filters to categorize Apollo asteroids into types like S and Q, further embedded the group within compositional taxonomies, linking them to meteorite analogs. In the 1990s, the taxonomy expanded with data from automated surveys like the Lincoln Near-Earth Asteroid Research (LINEAR) program, initiated in 1998 but building on 1990s prototypes, which refined Apollo boundaries by identifying more objects near the perihelion threshold and improving eccentricity distributions through radar and spectroscopic observations. The 1992 Spaceguard Survey Report formalized goals for detecting 90% of kilometer-sized NEAs, prompting MPC refinements that incorporated LINEAR's contributions to delineate Apollo from Aten overlaps. These milestones, supported by the Jet Propulsion Laboratory's Center for Near-Earth Object Studies (CNEOS), solidified the Apollo group's role in hazard assessment frameworks.

Population and statistics

Current known numbers

As of November 2025, approximately 22,400 Apollo asteroids have been discovered and cataloged, marking an increase of over 1,300 from the 21,083 known at the start of the year. This total encompasses all objects meeting the Apollo group's defining orbital criteria: a semi-major axis greater than 1 AU and a perihelion distance less than 1.017 AU, verified through orbital element computations by the (MPC). Among these, around 1,800 have received permanent numbers from the MPC, indicating well-determined orbits based on sufficient observational data spanning multiple apparitions. Only about 85 have been formally named, typically honoring individuals or places significant to astronomy or science, as per International Astronomical Union (IAU) conventions. Additionally, roughly 2,200 Apollo asteroids are classified as potentially hazardous asteroids (PHAs), defined by the MPC and NASA's Jet Propulsion Laboratory (JPL) as those exceeding 140 meters in diameter with a minimum orbit intersection distance (MOID) to of 0.05 AU or less, posing a theoretical risk of collision. The Apollo population continues to expand rapidly, with surveys such as the Asteroid Terrestrial-impact Last Alert System (ATLAS), Pan-STARRS, and the Vera C. Rubin Observatory contributing about 1,500 new discoveries annually. At this rate, projections estimate the known total could reach 30,000 by 2030, driven by enhanced detection capabilities targeting smaller and fainter objects.

Size distribution

The cumulative size-frequency distribution of Apollo asteroids follows a power-law form, N(>D)DβN(>D) \propto D^{-\beta}, with β1.44±0.12\beta \approx 1.44 \pm 0.12 (slope of approximately -1.5) for diameters between 100 m and 1.6 km, as determined from thermal infrared observations that enable debiased estimates of diameters and albedos. This relatively shallow compared to the main asteroid belt's distribution reflects dynamical processes that preferentially deliver and retain smaller objects in near-Earth orbits, resulting in a population dominated by sub-kilometer sizes, with roughly 94% of Apollo asteroids having diameters less than 1 km. Recent surveys continue to refine these estimates, though the 2012 analysis remains a key reference. Survey completeness for Apollo asteroids is high for larger diameters, exceeding 90% for objects greater than 1 km, owing to dedicated optical searches that have cataloged nearly all such potentially hazardous bodies. In contrast, completeness falls below 10% for diameters under 50 m, as these faint objects are rarely detected amid observational biases that prioritize brighter, larger asteroids observable from ground-based telescopes. NEOWISE data, which detected only a handful of sub-100 m Apollos, underscore this incompleteness at the small end. These biases, driven by the inverse relationship between size and apparent brightness, lead to underestimates of the smallest Apollos, with models indicating an estimated total population of approximately 11,200 ± 2,900 objects larger than 100 m (based on data; ongoing surveys may adjust this figure). surveys like NEOWISE provide essential size estimates by capturing thermal emission independent of optical variations, enabling corrections for these biases and revealing the true scale of the Apollo population's size distribution.

Notable members

Largest Apollo asteroids

The largest confirmed Apollo asteroid is 1866 Sisyphus, with a mean diameter of 8.48 km as determined from thermal infrared observations by the (WISE). Discovered on December 5, 1972, by Paul Wild at Zimmerwald Observatory in , it is classified as an with a of 0.15 and a period of 2.4 hours. Radar observations in 1985 revealed a pronounced echo spike that remained stationary relative to the asteroid's , suggesting non-principal axis consistent with a tumbling state. Other large known members include (53319) 1999 JM8 at approximately 7 km in diameter from radar imaging, and (3200) Phaethon, measuring about 5.8 km in diameter based on infrared measurements. Discovered on October 11, 1983, by the Infrared Astronomical Satellite (IRAS), Phaethon is a B-type asteroid and the parent body of the Geminid meteor shower, which produces one of the strongest annual meteor displays observable from Earth. Its diameter was refined through subsequent thermal modeling from space-based surveys. These prominent examples illustrate the size extremes among Apollo asteroids, where diameters are estimated primarily via ranging for close approaches and surveys for emission analysis.

Mission targets and recent discoveries

Several Apollo asteroids have been selected as primary targets for sample-return missions due to their scientific significance in understanding composition and solar system evolution. 's mission targeted , a carbonaceous Apollo asteroid approximately 490 meters in diameter, launching in September 2016 and successfully returning over 120 grams of samples to on , 2023, after collecting material in October 2020. These samples revealed carbon-rich materials and -bearing minerals, providing insights into the early solar system's organic delivery to . Similarly, JAXA's mission focused on , a rubble-pile Apollo asteroid about 900 meters across, launching in December 2014, arriving in June 2018, and returning approximately 5.4 grams of subsurface samples in December 2020 following artificial cratering operations. Analysis of Ryugu's samples indicated a primitive composition with hydrated silicates and organics, supporting theories of and life-building compounds originating from such bodies. China's mission, launched on May 28, 2025, aboard a rocket, targets , a small Apollo asteroid roughly 40-100 meters in size, with arrival anticipated in July 2026 and sample return projected for November 2027. This mission aims to collect and return to study Kamoʻoalewa's potential as an ejected lunar fragment, evidenced by its spectral similarity to lunar silicates and orbital dynamics suggesting an origin from a recent impact on the Moon's far side, possibly the crater. Such findings could illuminate transfer mechanisms of lunar material into Earth co-orbital space. Recent discoveries have expanded knowledge of small Apollo asteroids, highlighting their dynamic interactions with Earth. In August 2025, the Pan-STARRS1 telescope in detected 2025 PN7, a small Apollo asteroid estimated at 10-30 meters in diameter, classified as an Arjuna-type with a stable around Earth expected to persist until approximately 2083. This object's orbit, sharing Earth's path around the Sun with minimal , offers a rare opportunity to study long-term resonant dynamics in the inner solar system.

Dynamics and origins

Orbital evolution

The orbital evolution of Apollo asteroids is shaped by gravitational interactions with , primarily through mean-motion s that facilitate their transition from the main to near-Earth . The 3:1 with , corresponding to the prominent at approximately 2.5 AU, acts as a primary depletion mechanism in the inner main belt, where resonant perturbations accelerate asteroids onto unstable orbits that can evolve into Earth-crossing paths under continued planetary influences. Jupiter's gravitational tugs further inject these bodies into the Apollo group by altering their eccentricities and inclinations over timescales of millions of years, with numerical models showing that a substantial fraction of near-Earth objects originate from this zone. An additional key driver of orbital change is the Yarkovsky effect, a non-gravitational force arising from the anisotropic re-radiation of absorbed sunlight by rotating asteroids, which induces a net thrust that systematically alters the semi-major axis. For small Apollo asteroids (diameters typically <1 km), this thermal drift is directed outward for prograde rotators and inward for retrograde ones, with observed rates on the order of 10410^{-4} AU per million years, as detected in orbital fits for objects like (1862) Apollo with a drift of approximately (1.7±0.3)×104(-1.7 \pm 0.3) \times 10^{-4} AU/Myr. This effect accumulates over the short dynamical lifetimes of these bodies, gradually shifting them across resonance boundaries and contributing to their eventual ejection or collision. Close approaches to Earth and other planets introduce chaotic perturbations that can temporarily trap Apollo asteroids in resonant configurations, such as horseshoe or quasi-satellite orbits relative to Earth. The Arjuna subgroup, a low-eccentricity, low-inclination subset of Apollos with semi-major axes near 1 AU, exemplifies this behavior, where objects librate in 1:1 resonance and execute horseshoe paths with minimum orbit intersection distances often below 0.05 AU and encounter velocities as low as a few m/s. These temporary states are unstable due to repeated planetary flybys, leading to rapid eccentricity growth and ejection from the resonant zone. Long-term N-body simulations of Apollo populations reveal that these dynamical processes result in a finite fraction evolving toward planetary collisions before ejection from the inner Solar System. Over 100 million years, models of steady-state near-Earth asteroid swarms indicate that roughly 20% of particles collide with , with the remainder distributed among impacts on , , or , or hyperbolic ejection, reflecting the high-impact fraction driven by frequent close approaches during their typical 5–10 million year dynamical lifetimes.

Possible origins

The majority of Apollo asteroids are thought to originate from the inner main , where collisions produce fragments that are injected into near-Earth orbits through dynamical mechanisms such as the 3:1 mean-motion with at approximately 2.5 AU and the ν₆ secular at the inner edge of the belt. Numerical models indicate that roughly 85% of near-Earth asteroids, including the Apollo group, derive from these inner main-belt sources, with contributions of about 37% from the ν₆ , 23% from the 3:1 , and 25% from direct inner-belt diffusion. These fragments, often S-type in composition, reflect the dominant silicate-rich materials of inner-belt families, supporting links through spectral similarities to groups like the Karin or Koronis families. A small fraction of Apollo asteroids may stem from lunar ejecta generated by meteoroid impacts on the , though such origins are rare due to the limited escape velocities required to reach Earth-crossing orbits. For instance, the (469219) Kamoʻoalewa exhibits spectral features matching lunar anorthositic rocks, consistent with ejection from the 's surface and subsequent capture into its current orbit. Other hypothesized sources include primordial captures from early Solar System collisions involving or , but these contribute only a minor number of objects. Cometary interlopers from the Jupiter family or beyond account for less than 5% of the Apollo population, identified through dynamical models showing their distinct volatile-rich compositions. Evidence for these origins comes from backward dynamical integrations spanning up to 100 million years, which trace many Apollo orbits to main-belt resonances and families, and from compositional analyses linking their S-type spectra to inner-belt asteroid populations.

Hazards and impacts

Potentially hazardous asteroids

Potentially hazardous asteroids (PHAs) within the Apollo group are near-Earth objects that meet specific criteria indicating a potential threat to Earth: an absolute magnitude of H ≤ 22.0, which corresponds to a diameter greater than approximately 140 meters, and a minimum orbit intersection distance (MOID) with Earth's orbit of 0.05 AU or less. This classification ensures focus on asteroids large enough to cause significant regional or global damage if they were to impact, while their close orbital approaches heighten the risk assessment. As of November 2025, approximately 2,349 PHAs have been identified overall, with the Apollo subgroup comprising the vast majority—around 2,200 objects, or over 90% of the total. These Apollo PHAs dominate due to their Earth-crossing orbits, which inherently increase the likelihood of close encounters compared to other near-Earth asteroid groups. The collision risks from Apollo PHAs are quantified using established scales, including the Torino Impact Hazard Scale, which categorizes potential events on a 0–10 integer scale based on probability and energy (0 indicating no hazard and 10 a certain global catastrophe), and the Palermo Technical Impact Hazard Scale, a logarithmic metric comparing an object's impact probability to the average annual background risk from all sources. For instance, the Apollo PHA (29075) 1950 DA, a kilometer-sized object, carries an updated impact probability of about 1 in 30,000 for March 2880, with a Palermo Scale value of -2.0, reflecting a low but non-negligible long-term hazard influenced by effects like Yarkovsky drift. Ongoing monitoring of Apollo PHAs relies on NASA's Sentry system, operated by the Center for Studies (CNEOS), which systematically analyzes orbital data to compute impact probabilities for all known objects over the next century, incorporating uncertainties from non-gravitational forces and observational errors. This automated tool updates assessments as new observations refine orbits, enabling prioritization of objects for further study or potential .

Historical events

One of the most significant historical events involving an Apollo asteroid occurred on June 30, 1908, when the Tunguska event devastated approximately 2,150 square kilometers of Siberian forest through an airburst explosion estimated at 10-15 megatons of TNT equivalent. Analysis of the event's trajectory and orbital dynamics suggests the impacting body was likely a small Apollo-type asteroid, approximately 90-190 meters in diameter, rather than a comet, based on the absence of cometary signatures in recovered evidence and modeling of its entry path. Some studies propose it could have been a fragment from a larger Apollo asteroid disrupted prior to atmospheric entry, though no direct meteorite fragments have been conclusively linked. More recently, on February 15, 2013, a 20-meter Apollo asteroid caused the airburst over , releasing energy equivalent to approximately 500 kilotons of TNT and injuring over 1,500 people primarily from the shockwave shattering windows and structures. Orbital reconstruction confirmed its classification as an Apollo asteroid with a perihelion of about 0.95 AU, entering the atmosphere at a shallow of around 18 degrees, leading to fragmentation at 30 kilometers altitude. The event highlighted the vulnerability to undetected small Apollo bodies, as the asteroid was not previously cataloged despite surveys. Ancient impacts potentially linked to Apollo asteroids include the Chesapeake Bay crater, formed approximately 35 million years ago by a bolide estimated at 2-5 kilometers in diameter that struck the continental shelf off . Notable close approaches by Apollo asteroids include that of the approximately 400-meter object 2004 MN4 (later designated ), discovered in June 2004, which passed within approximately 14 million kilometers (about 36 lunar distances) of on December 23, 2004, during initial post-discovery observations, prompting refined orbital calculations. More recently, in September 2025, the potentially hazardous Apollo asteroid 2025 FA22 (~140 meters in diameter) passed at a minimum distance of about 835,000 kilometers. Apollo asteroids contribute to Earth's impact frequency, with objects around 1 kilometer in diameter striking approximately once every 500,000 years, capable of regional devastation, while smaller events—such as airbursts from meter-scale fragments—occur nearly yearly, often going unobserved over remote areas.

Observation and exploration

Detection surveys

The primary ground-based surveys for detecting Apollo asteroids are the Catalina Sky Survey (CSS), operated by the University of 's Lunar and Planetary Laboratory from facilities in , and the (Panoramic Survey Telescope and Rapid Response System) survey, based at the in since 2010. These optical telescope programs systematically scan the sky to identify (NEOs), including the Apollo group, by capturing wide-field images multiple times per night. CSS, funded by NASA's Near-Earth Object Observations Program, has been active since the late 1990s and focuses on twilight and nighttime observations to catch fast-moving asteroids. complements this with its high-resolution, multi-filter imaging across a broad sky area, contributing significantly to the catalog of known Apollos. Detection relies on advanced image-processing techniques, particularly difference , which subtracts a static reference image of the sky from new exposures to reveal moving objects like asteroids as bright streaks or points against the subtracted background. The Moving Object Processing System () automates this by linking detections across multiple images to compute orbits and filter false positives from cosmic rays or satellites. Candidate Apollo asteroids identified in initial scans are promptly reported to the Minor Planet Center's Confirmation Page (NEOCP) for global follow-up by other telescopes, ensuring rapid confirmation and orbital refinement. This pipeline has enabled the surveys to process thousands of potential detections nightly with high efficiency. These efforts have achieved substantial milestones, including the detection of over 90% of the estimated of Apollo asteroids larger than 1 kilometer in diameter, which pose the greatest potential impact risks. CSS and together account for approximately 90% of all new NEO discoveries in recent years, dramatically increasing the Apollo from a few dozen in the to over 21,000 as of early 2025. A notable recent example is the Apollo asteroid 2025 PN7, discovered by on August 2, 2025, which temporarily shares as a until around 2083. Despite these advances, challenges persist, including incomplete coverage of the sky due to the northern locations of both surveys, which leaves gaps in monitoring Apollo trajectories approaching from southern ecliptic longitudes. Additionally, faint small bodies—typically under 100 meters—with low or distant geometries often evade detection near the surveys' magnitude limits of around 22nd magnitude, requiring enhanced southern facilities and deeper to close these observational biases.

Space missions

Several missions have targeted Apollo asteroids to study their composition, structure, and potential hazards, advancing technologies for exploration. The mission, launched by in 1996, provided foundational insights into near-Earth asteroids despite targeting the ; it achieved the first orbit of an asteroid in 2000 and a in 2001, yielding detailed images and data on surface features that informed subsequent Apollo missions. NASA's mission, launched in 2016, rendezvoused with the Apollo asteroid in 2018 and used the Touch-And-Go Sample Acquisition Mechanism (TAGSAM) to collect surface during a 2020 touchdown, returning approximately 121 grams of material to on September 24, 2023, for analysis of primordial solar system materials. JAXA's mission, launched in 2014, arrived at the Apollo asteroid Ryugu in 2018, deploying rovers and MINERVA-II landers before using a projectile-based sampler to gather subsurface samples in 2019, which were returned to in December 2020, revealing hydrated minerals and organic compounds. In 2022, NASA's (DART) mission demonstrated kinetic impactor technology by colliding a spacecraft with , the moon of the Apollo asteroid Didymos, on September 26, shortening Dimorphos's orbital period around Didymos by 32 minutes and confirming the efficacy of deflection strategies for planetary defense. More recently, China's mission, launched on May 28, 2025, aboard a rocket, is en route to the Apollo 469219 , with arrival planned for 2026 to collect samples using a coring mechanism before returning them to around 2027. Looking ahead, NASA's , an infrared telescope mission scheduled for launch in September 2027 aboard a , will survey Apollo and other near-Earth asteroids from the Sun-Earth L1 point to detect and characterize potentially hazardous objects, enhancing early warning capabilities. These missions have pioneered key technologies, including TAGSAM for non-invasive sampling, coring tools for subsurface access, orbital rendezvous maneuvers, and kinetic impactors for deflection, which are adaptable for future Apollo explorations.

References

  1. https://www.jpl.[nasa](/page/NASA).gov/news/additional-details-on-the-large-feb-15-fireball-over-russia/
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