SpaceAtlas Space Object Data
NASA JPL SBDB · 464797

464797

464797 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.794 AU it takes 2.40 yr to circle the Sun.

Apollo Observations: 357
Orbital Period · P
2.40 yr
v(q)
40.2 km/s
v(Q)
12.3 km/s
Diameter · ≈
0.78 km
TJ
3.5
Eccentricity · e
0.5309

Orbit and dynamics

The path is an ellipse reaching 0.842 AU from the Sun at perihelion and 2.746 AU at aphelion, a radial span of 1.904 AU.

Applying Kepler's third law to a = 1.794 AU gives an orbital period of 2.40 yr, or about 878 days.

The high eccentricity (0.531) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 52.63° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.2 km/s at perihelion and falls to 12.3 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 0.73 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.16 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 357 observations and has a weighted RMS residual of 0.4935 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
1.794 AU
Eccentricity
0.5309
Perihelion
0.842 AU
Aphelion
2.746435 AU
Inclination
52.63°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
57.85°

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-Aug-20 05:56 0.228421 AU
34171221 km
29.20 km/s
2040-Aug-22 00:45 0.239341 AU
35804882 km
30.15 km/s
2045-Feb-15 05:46 0.450205 AU
67349742 km
36.31 km/s
2052-Aug-23 22:41 0.265912 AU
39779801 km
31.20 km/s
2057-Feb-17 10:40 0.397104 AU
59405846 km
34.99 km/s
2064-Aug-25 23:11 0.303795 AU
45447083 km
32.31 km/s
2069-Feb-19 14:02 0.347091 AU
51924004 km
33.75 km/s
2076-Aug-28 02:26 0.349740 AU
52320396 km
33.50 km/s

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

Physical Parameters

Diameter
0.726 km
Albedo
0.16
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
18.3

Orbit Quality

RMS
0.49354
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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