SpaceAtlas Space Object Data
NASA JPL SBDB · 406952

406952

406952 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.241 AU it takes 1.38 yr to circle the Sun.

Apollo Observations: 163
Orbital Period · P
1.38 yr
v(q)
65.9 km/s
v(Q)
10.8 km/s
Diameter · ≈
1.34 km
TJ
4.76
Eccentricity · e
0.7175

Orbit and dynamics

The path is an ellipse reaching 0.351 AU from the Sun at perihelion and 2.131 AU at aphelion, a radial span of 1.78 AU.

Applying Kepler's third law to a = 1.241 AU gives an orbital period of 1.38 yr, or about 505 days.

The high eccentricity (0.718) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 32.95° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 65.9 km/s at perihelion and falls to 10.8 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

The measured diameter is 0.77 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.429 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 163 observations and has a weighted RMS residual of 0.4033 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
1.241 AU
Eccentricity
0.7175
Perihelion
0.351 AU
Aphelion
2.131418 AU
Inclination
32.95°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
157.94°

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
2034-Apr-03 16:15 0.160716 AU
24042743 km
24.82 km/s
2063-Apr-11 17:29 0.100493 AU
15033489 km
29.29 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.772 km
Albedo
0.429
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
17.11

Orbit Quality

RMS
0.40333
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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