SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 AT22

2012 AT22

2012 AT22 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.152 AU it takes 1.24 yr to circle the Sun.

Apollo Observations: 77
Orbital Period · P
1.24 yr
v(q)
32.6 km/s
v(Q)
23.6 km/s
Diameter · ≈
0.31 km
TJ
5.34
Eccentricity · e
0.1596

Orbit and dynamics

The path is an ellipse reaching 0.968 AU from the Sun at perihelion and 1.336 AU at aphelion, a radial span of 0.368 AU.

Applying Kepler's third law to a = 1.152 AU gives an orbital period of 1.24 yr, or about 452 days.

An eccentricity of 0.16 makes the orbit moderately elongated.

A steep inclination of 27.33° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 32.6 km/s at perihelion and falls to 23.6 km/s at aphelion.

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

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 20.31 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.31 km.

Observation record and orbit quality

The current orbit solution is based on 77 observations and has a weighted RMS residual of 0.3996 arcseconds.

Condition code U = 1 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
1.152 AU
Eccentricity
0.1596
Perihelion
0.968 AU
Aphelion
1.335859 AU
Inclination
27.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
306.72°

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-Aug-20 00:22 0.199029 AU
29774348 km
13.82 km/s
2028-Feb-04 05:41 0.217961 AU
32606570 km
15.76 km/s
2032-Aug-13 23:17 0.161475 AU
24156352 km
16.09 km/s
2033-Feb-09 17:52 0.231994 AU
34705741 km
13.87 km/s
2037-Aug-03 15:10 0.493792 AU
73870254 km
22.67 km/s
2038-Feb-26 11:40 0.460729 AU
68924056 km
13.98 km/s
2048-Aug-19 08:21 0.239340 AU
35804758 km
13.91 km/s
2049-Feb-03 09:01 0.245077 AU
36663034 km
16.28 km/s
2053-Aug-15 06:28 0.125651 AU
18797105 km
15.55 km/s
2054-Feb-08 21:30 0.209892 AU
31399384 km
13.92 km/s
2058-Aug-05 02:14 0.460358 AU
68868577 km
21.90 km/s
2059-Feb-24 13:06 0.438438 AU
65589387 km
14.00 km/s
2069-Aug-19 13:35 0.255165 AU
38172123 km
13.97 km/s
2070-Feb-03 17:03 0.256504 AU
38372442 km
16.50 km/s
2074-Aug-15 18:43 0.118637 AU
17747792 km
15.45 km/s
2075-Feb-08 23:49 0.205227 AU
30701498 km
13.93 km/s
2079-Aug-05 12:03 0.459816 AU
68787552 km
21.87 km/s

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

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
20.31

Orbit Quality

RMS
0.39963
Condition
1
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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