SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 EV2

2024 EV2

2024 EV2 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.434 AU once every 1.72 yr.

Amor Observations: 62
Orbital Period · P
1.72 yr
v(q)
29.1 km/s
v(Q)
21.3 km/s
Diameter · ≈
0.13 km
TJ
4.57
Eccentricity · e
0.1549

Orbit and dynamics

The path is an ellipse reaching 1.212 AU from the Sun at perihelion and 1.656 AU at aphelion, a radial span of 0.444 AU.

Applying Kepler's third law to a = 1.434 AU gives an orbital period of 1.72 yr, or about 627 days.

An eccentricity of 0.155 makes the orbit moderately elongated.

A steep inclination of 24.49° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 29.1 km/s at perihelion and falls to 21.3 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 22.22 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

The current orbit solution is based on 62 observations and has a weighted RMS residual of 0.4878 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.434 AU
Eccentricity
0.1549
Perihelion
1.212 AU
Aphelion
1.656127 AU
Inclination
24.49°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
60.18°

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
2031-Aug-23 06:06 0.461189 AU
68992946 km
12.04 km/s
2036-Mar-19 09:48 0.343046 AU
51318878 km
12.41 km/s
2043-Aug-15 10:31 0.473180 AU
70786775 km
11.64 km/s
2048-Mar-13 05:07 0.402664 AU
60237634 km
12.41 km/s
2055-Apr-09 00:02 0.402772 AU
60253814 km
14.56 km/s
2067-Apr-05 02:48 0.324039 AU
48475597 km
13.63 km/s
2074-Sep-08 05:02 0.474935 AU
71049335 km
12.63 km/s
2079-Apr-01 05:26 0.293200 AU
43862038 km
12.97 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
22.22

Orbit Quality

RMS
0.48775
Condition
6
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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