SpaceAtlas Space Object Data
NASA JPL SBDB · 416032

416032

416032 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.887 AU once every 2.59 yr.

Amor Observations: 209
Orbital Period · P
2.59 yr
v(q)
33.5 km/s
v(Q)
14 km/s
Diameter · ≈
0.24 km
TJ
3.86
Eccentricity · e
0.4093

Orbit and dynamics

Between its closest point (1.114 AU) and its farthest (2.659 AU), the heliocentric distance changes by 1.545 AU over every revolution.

One full revolution takes 2.59 yr (947 days), computed from the semi-major axis of 1.887 AU.

The high eccentricity (0.409) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.51° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.5 km/s at perihelion and falls to 14 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 = 20.81 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.24 km.

Observation record and orbit quality

Astrometry from 209 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5496 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
1.887 AU
Eccentricity
0.4093
Perihelion
1.114 AU
Aphelion
2.659349 AU
Inclination
2.51°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
134.85°

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-Feb-05 04:04 0.406768 AU
60851653 km
10.09 km/s
2028-Mar-19 12:38 0.406014 AU
60738825 km
1.94 km/s
2059-Feb-22 19:52 0.258325 AU
38644929 km
7.07 km/s
2072-Feb-14 16:25 0.138350 AU
20696893 km
3.59 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
20.81

Orbit Quality

RMS
0.54963
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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