SpaceAtlas Space Object Data
NASA JPL SBDB · 481817

481817

481817 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 0.695 AU it takes 0.58 yr to circle the Sun.

Apollo Observations: 449
Orbital Period · P
0.58 yr
v(q)
53.3 km/s
v(Q)
24 km/s
Diameter · ≈
0.72 km
TJ
8.1
Eccentricity · e
0.3799

Orbit and dynamics

The path is an ellipse reaching 0.431 AU from the Sun at perihelion and 0.959 AU at aphelion, a radial span of 0.528 AU.

Applying Kepler's third law to a = 0.695 AU gives an orbital period of 0.58 yr, or about 212 days.

An eccentricity of 0.38 makes the orbit moderately elongated.

A steep inclination of 24.31° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 53.3 km/s at perihelion and falls to 24 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 18.48 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.72 km.

Observation record and orbit quality

The current orbit solution is based on 449 observations and has a weighted RMS residual of 0.4355 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
0.695 AU
Eccentricity
0.3799
Perihelion
0.431 AU
Aphelion
0.959031 AU
Inclination
24.31°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
303.05°

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-Dec-12 11:57 0.080936 AU
12107840 km
13.65 km/s
2034-Dec-17 14:38 0.154499 AU
23112752 km
14.14 km/s
2038-Dec-11 16:03 0.138067 AU
20654597 km
14.65 km/s
2045-Dec-16 03:00 0.097428 AU
14575074 km
13.33 km/s
2049-Dec-11 09:54 0.196937 AU
29461298 km
15.97 km/s
2056-Dec-14 13:26 0.050289 AU
7523064 km
12.99 km/s
2067-Dec-14 11:43 0.028614 AU
4280548 km
12.98 km/s
2078-Dec-13 20:53 0.027035 AU
4044348 km
13.03 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
18.48

Orbit Quality

RMS
0.43549
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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