SpaceAtlas Space Object Data
NASA JPL SBDB · 612326

612326

612326 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.778 AU it takes 2.37 yr to circle the Sun.

Apollo Observations: 92
Orbital Period · P
2.37 yr
v(q)
43.3 km/s
v(Q)
11.5 km/s
Diameter · ≈
0.29 km
TJ
3.88
Eccentricity · e
0.5799

Orbit and dynamics

The path is an ellipse reaching 0.747 AU from the Sun at perihelion and 2.809 AU at aphelion, a radial span of 2.062 AU.

Applying Kepler's third law to a = 1.778 AU gives an orbital period of 2.37 yr, or about 866 days.

The high eccentricity (0.58) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.89° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 43.3 km/s at perihelion and falls to 11.5 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 = 20.42 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.29 km.

Observation record and orbit quality

The current orbit solution is based on 92 observations and has a weighted RMS residual of 0.6899 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
1.778 AU
Eccentricity
0.5799
Perihelion
0.747 AU
Aphelion
2.809062 AU
Inclination
2.89°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
38.53°

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-Sep-06 08:59 0.044973 AU
6727870 km
16.87 km/s
2040-May-09 14:17 0.208919 AU
31253836 km
12.03 km/s
2047-Sep-07 17:29 0.048506 AU
7256458 km
17.03 km/s
2052-Mar-11 02:42 0.497003 AU
74350639 km
30.69 km/s
2059-May-27 13:17 0.248580 AU
37187060 km
13.19 km/s
2066-Sep-16 18:07 0.185230 AU
27709995 km
21.33 km/s
2071-Mar-16 22:34 0.395489 AU
59164310 km
27.63 km/s
2078-Jun-07 19:55 0.266557 AU
39876393 km
13.87 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
20.42

Orbit Quality

RMS
0.68989
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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