SpaceAtlas Space Object Data
NASA JPL SBDB · 99942

Apophis

Apophis is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.922 AU and a period of 0.89 yr.

Aten PHA Discovered: 2004-03-15 Observations: 7,370
Encyclopedia excerpt
99942 Apophis (provisional designation 2004 MN4) is a near-Earth asteroid classified as a potentially hazardous object. Its mean diameter is about 340–370 metres (1,120–1,210 ft), while radar observations indicate an elongated shape with a long axis of about 450 metres (1,480 ft) and suggest that it may be bilobed. It was discovered on 19 June 2004 by Roy A. Tucker, David J. Tholen, and Fabrizio Bernardi at Kitt Peak National Observatory. The asteroid was numbered 99942 in 2005 and named after Apophis, the Greek name of the ancient Egyptian serpent deity Apep. Apophis attracted widespread attention shortly after its discovery because early orbit calculations indicated a possible collision with Earth on 13 April 2029. The estimated probability reached 2.7% on 27 December 2004, and Apophis was rated level 4 on the Torino scale, the highest rating attained by any object. Later that day, the identification of a precovery image from March 2004 extended the observation arc and eliminated the possibility of a 2029 impact. Small probabilities of impacts on later approaches, including in 2036 and 2068, remained for several years, but increasingly precise observations reduced those risks. In 2021, Apophis was removed from the Sentry Risk Table after an impact during the following 100 years was ruled out. Apophis will nevertheless make an exceptionally close approach to Earth on 13 April 2029, passing about 31,600 kilometres (19,600 mi) above the surface. It is expected to reach magnitude 3.1 and become visible to the naked eye under suitable conditions from parts of Europe, Africa, and western Asia. Earth's gravity will alter its orbit, changing it from an Aten-class asteroid to an Apollo-class asteroid, and tidal forces during the encounter may alter its rotation and partially resurface it. The 2029 encounter has also made Apophis a target for spacecraft exploration. NASA's OSIRIS-APEX, formerly OSIRIS-REx, is planned to rendezvous with Apophis after the Earth encounter and study it for 18 months. The ESA–JAXA Ramses mission is planned to rendezvous with the asteroid before the encounter.
Orbital Period · P
0.89 yr
v(q)
37.6 km/s
v(Q)
25.6 km/s
Diameter · ≈
0.54 km
TJ
6.47
Eccentricity · e
0.1911

Orbit and dynamics

Between its closest point (0.746 AU) and its farthest (1.099 AU), the heliocentric distance changes by 0.353 AU over every revolution.

One full revolution takes 0.89 yr (324 days), computed from the semi-major axis of 0.922 AU.

An eccentricity of 0.191 makes the orbit moderately elongated.

Its inclination of 3.34° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.6 km/s at perihelion and falls to 25.6 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

It is catalogued as a potentially hazardous asteroid (PHA) on the basis of its size and its minimum orbit intersection distance with Earth.

Size and surface

The measured diameter is 0.34 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.35 points to a comparatively bright, reflective surface.

The rotation period is 30.56 h.

Observation record and orbit quality

Astrometry from 7,370 individual observations underpins this orbit; the fit leaves an RMS residual of 0.2566 arcseconds.

Condition code U = 0 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

About these computed values

Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Orbital Parameters

Semi-Major Axis
0.9224 AU
Eccentricity
0.1911
Perihelion
0.746 AU
Aphelion
1.098671 AU
Inclination
3.34°
Orbital Period
0.8871 yr
Epoch
2461200.5
Mean Anomaly
175.33°

Orbit diagram

The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.

3D orbit (interactive)

Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.

Close approaches

Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).

Date (UTC)Miss distanceVelocity
2027-Dec-29 14:23 0.293612 AU
43923790 km
14.69 km/s
2028-Sep-12 04:11 0.256566 AU
38381693 km
7.89 km/s
2029-Apr-13 21:46 0.000254 AU
38008 km
7.42 km/s
2029-Nov-26 21:38 0.299956 AU
44872802 km
6.26 km/s
2036-Mar-27 08:31 0.308905 AU
46211604 km
15.01 km/s
2036-Dec-31 15:53 0.329965 AU
49362048 km
6.84 km/s
2037-Sep-24 07:44 0.222154 AU
33233730 km
12.37 km/s
2044-Feb-06 14:38 0.279152 AU
41760527 km
5.78 km/s
2044-Aug-24 07:17 0.078970 AU
11813797 km
3.96 km/s
2051-Apr-20 02:05 0.039904 AU
5969533 km
4.69 km/s
2051-Nov-21 02:31 0.288778 AU
43200531 km
6.02 km/s
2058-Mar-31 23:37 0.211674 AU
31665976 km
12.14 km/s
2058-Dec-20 16:47 0.330136 AU
49387633 km
6.86 km/s
2059-Sep-28 22:33 0.325251 AU
48656914 km
15.47 km/s
2065-Mar-19 23:57 0.468842 AU
70137724 km
19.91 km/s
2066-Jan-18 15:10 0.314208 AU
47004911 km
6.53 km/s
2066-Sep-16 01:59 0.063623 AU
9517897 km
7.76 km/s
2073-Feb-15 06:45 0.256570 AU
38382365 km
5.28 km/s
2073-Jul-27 18:10 0.110855 AU
16583646 km
4.57 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.34 km
Albedo
0.35
Density
— g/cm³
Rotation Period
30.56 h
Absolute Magnitude
19.09

Orbit Quality

RMS
0.25657
Condition
0
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

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