SpaceAtlas Space Object Data
NASA JPL SBDB · 446924

446924

446924 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.838 AU and a period of 0.77 yr.

Aten Observations: 515
Orbital Period · P
0.77 yr
v(q)
52 km/s
v(Q)
20.4 km/s
Diameter · ≈
0.33 km
TJ
6.93
Eccentricity · e
0.4367

Orbit and dynamics

The path is an ellipse reaching 0.472 AU from the Sun at perihelion and 1.203 AU at aphelion, a radial span of 0.731 AU.

Applying Kepler's third law to a = 0.838 AU gives an orbital period of 0.77 yr, or about 280 days.

The high eccentricity (0.437) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 9.69° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 52 km/s at perihelion and falls to 20.4 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 = 20.16 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.33 km.

Observation record and orbit quality

The current orbit solution is based on 515 observations and has a weighted RMS residual of 0.3964 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
0.8375 AU
Eccentricity
0.4367
Perihelion
0.472 AU
Aphelion
1.203236 AU
Inclination
9.69°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
146.99°

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
2031-Sep-18 00:52 0.135980 AU
20342316 km
11.41 km/s
2038-Nov-25 14:19 0.136542 AU
20426453 km
10.40 km/s
2044-Sep-15 20:19 0.176460 AU
26398081 km
15.68 km/s
2048-Dec-04 01:39 0.127125 AU
19017576 km
15.10 km/s
2051-Nov-08 01:38 0.195888 AU
29304450 km
10.36 km/s
2054-Sep-23 16:41 0.156813 AU
23458938 km
10.39 km/s
2061-Dec-02 02:53 0.098420 AU
14723479 km
11.31 km/s
2067-Sep-16 01:36 0.139163 AU
20818422 km
13.42 km/s
2071-Dec-03 10:24 0.186101 AU
27840265 km
17.35 km/s
2074-Nov-16 04:24 0.174505 AU
26105608 km
10.28 km/s
2077-Oct-01 02:41 0.179613 AU
26869748 km
10.16 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
20.16

Orbit Quality

RMS
0.3964
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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