SpaceAtlas Space Object Data
NASA JPL SBDB · 538085

538085

538085 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.873 AU it takes 2.56 yr to circle the Sun.

Apollo Observations: 150
Orbital Period · P
2.56 yr
v(q)
41.3 km/s
v(Q)
11.5 km/s
Diameter · ≈
1.07 km
TJ
3.23
Eccentricity · e
0.5646

Orbit and dynamics

Between its closest point (0.815 AU) and its farthest (2.93 AU), the heliocentric distance changes by 2.115 AU over every revolution.

One full revolution takes 2.56 yr (936 days), computed from the semi-major axis of 1.873 AU.

The high eccentricity (0.565) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 62.62° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 41.3 km/s at perihelion and falls to 11.5 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 = 17.61 and an assumed geometric albedo of 0.14, the diameter works out to roughly 1.07 km.

Observation record and orbit quality

Astrometry from 150 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5703 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
1.873 AU
Eccentricity
0.5646
Perihelion
0.815 AU
Aphelion
2.930496 AU
Inclination
62.62°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
114.03°

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
2048-Aug-22 20:05 0.172446 AU
25797590 km
37.79 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
17.61

Orbit Quality

RMS
0.57032
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.