SpaceAtlas Space Object Data
NASA JPL SBDB · 1996 AE2

1996 AE2

1996 AE2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.367 AU it takes 1.60 yr to circle the Sun.

Apollo Observations: 311
Orbital Period · P
1.60 yr
v(q)
33.1 km/s
v(Q)
19.6 km/s
Diameter · ≈
0.32 km
TJ
4.59
Eccentricity · e
0.2566

Orbit and dynamics

Between its closest point (1.017 AU) and its farthest (1.718 AU), the heliocentric distance changes by 0.701 AU over every revolution.

One full revolution takes 1.60 yr (584 days), computed from the semi-major axis of 1.367 AU.

An eccentricity of 0.257 makes the orbit moderately elongated.

A steep inclination of 37.37° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 33.1 km/s at perihelion and falls to 19.6 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 20.23 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.32 km.

Observation record and orbit quality

Astrometry from 311 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4735 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
1.367 AU
Eccentricity
0.2566
Perihelion
1.017 AU
Aphelion
1.717772 AU
Inclination
37.37°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
33.45°

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
2028-Jan-15 03:59 0.177356 AU
26532058 km
19.47 km/s
2036-Jan-14 15:46 0.204274 AU
30558891 km
19.38 km/s
2044-Jan-14 02:48 0.239102 AU
35769147 km
19.33 km/s
2052-Jan-13 14:34 0.281256 AU
42075260 km
19.32 km/s
2060-Jan-13 03:22 0.329217 AU
49250171 km
19.40 km/s
2068-Jan-12 19:41 0.380651 AU
56944549 km
19.55 km/s
2076-Jan-12 16:13 0.436756 AU
65337821 km
19.78 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
20.23

Orbit Quality

RMS
0.47352
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.

Keep exploring

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