SpaceAtlas Space Object Data
NASA JPL SBDB · 467460

467460

467460 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.671 AU and a period of 0.55 yr.

Aten Observations: 368
Orbital Period · P
0.55 yr
v(q)
70.7 km/s
v(Q)
18.7 km/s
Diameter · ≈
0.55 km
TJ
8.33
Eccentricity · e
0.5819

Orbit and dynamics

Between its closest point (0.281 AU) and its farthest (1.062 AU), the heliocentric distance changes by 0.781 AU over every revolution.

One full revolution takes 0.55 yr (201 days), computed from the semi-major axis of 0.671 AU.

The high eccentricity (0.582) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.94° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 70.7 km/s at perihelion and falls to 18.7 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 = 19.05 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.55 km.

Observation record and orbit quality

Astrometry from 368 individual observations underpins this orbit; the fit leaves an RMS residual of 0.383 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
0.6715 AU
Eccentricity
0.5819
Perihelion
0.281 AU
Aphelion
1.062246 AU
Inclination
5.94°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
302.47°

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-Jun-05 11:51 0.063836 AU
9549688 km
12.87 km/s
2028-May-01 05:09 0.193881 AU
29004216 km
18.69 km/s
2033-May-05 20:44 0.022989 AU
3439078 km
11.64 km/s
2038-Jun-05 01:08 0.062346 AU
9326829 km
12.78 km/s
2039-May-01 23:45 0.193237 AU
28907820 km
18.67 km/s
2044-May-07 06:26 0.032076 AU
4798460 km
11.43 km/s
2049-Jun-05 17:50 0.070088 AU
10485024 km
13.26 km/s
2050-May-01 06:50 0.173892 AU
26013925 km
18.00 km/s
2055-May-11 02:40 0.044336 AU
6632635 km
11.19 km/s
2060-Jun-06 10:31 0.089639 AU
13409755 km
14.19 km/s
2061-Apr-30 09:22 0.136721 AU
20453108 km
16.70 km/s
2066-May-17 11:21 0.058322 AU
8724826 km
11.02 km/s
2071-Jun-07 13:34 0.131633 AU
19692047 km
15.92 km/s
2072-Apr-29 18:59 0.084511 AU
12642615 km
14.90 km/s
2077-May-25 19:46 0.059547 AU
8908116 km
11.19 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
19.05

Orbit Quality

RMS
0.38303
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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