SpaceAtlas Space Object Data
NASA JPL SBDB · 504181

504181

504181 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.538 AU it takes 1.91 yr to circle the Sun.

Apollo Observations: 59
Orbital Period · P
1.91 yr
v(q)
112.1 km/s
v(Q)
5.2 km/s
Diameter · ≈
0.61 km
TJ
3.8
Eccentricity · e
0.912

Orbit and dynamics

Between its closest point (0.135 AU) and its farthest (2.941 AU), the heliocentric distance changes by 2.806 AU over every revolution.

One full revolution takes 1.91 yr (697 days), computed from the semi-major axis of 1.538 AU.

The high eccentricity (0.912) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 19.55° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 112.1 km/s at perihelion and falls to 5.2 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 = 18.81 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.61 km.

Observation record and orbit quality

Astrometry from 59 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3974 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
1.538 AU
Eccentricity
0.912
Perihelion
0.135 AU
Aphelion
2.940656 AU
Inclination
19.55°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
137.46°

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-Sep-18 15:35 0.144957 AU
21685213 km
35.35 km/s
2038-Dec-17 00:14 0.425626 AU
63672674 km
27.29 km/s
2040-Nov-21 21:14 0.405764 AU
60701442 km
43.29 km/s
2046-Oct-08 19:10 0.435143 AU
65096443 km
49.20 km/s
2048-Sep-15 04:48 0.166936 AU
24973338 km
33.48 km/s
2059-Dec-15 07:17 0.393864 AU
58921258 km
28.58 km/s
2061-Nov-19 23:32 0.431062 AU
64485911 km
44.80 km/s
2067-Oct-07 06:41 0.403979 AU
60434364 km
47.93 km/s
2069-Sep-13 13:39 0.196330 AU
29370477 km
32.09 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
18.81

Orbit Quality

RMS
0.39737
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.