SpaceAtlas Space Object Data
NASA JPL SBDB · 337558

337558

337558 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.961 AU it takes 2.75 yr to circle the Sun.

Apollo Observations: 170
Orbital Period · P
2.75 yr
v(q)
41.4 km/s
v(Q)
10.9 km/s
Diameter · ≈
0.46 km
TJ
3.65
Eccentricity · e
0.583

Orbit and dynamics

Between its closest point (0.818 AU) and its farthest (3.104 AU), the heliocentric distance changes by 2.286 AU over every revolution.

One full revolution takes 2.75 yr (1,003 days), computed from the semi-major axis of 1.961 AU.

The high eccentricity (0.583) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.82° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 41.4 km/s at perihelion and falls to 10.9 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 = 19.44 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.46 km.

Observation record and orbit quality

Astrometry from 170 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5421 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
1.961 AU
Eccentricity
0.583
Perihelion
0.818 AU
Aphelion
3.104263 AU
Inclination
4.82°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
330.98°

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
2034-Oct-12 19:20 0.317936 AU
47562611 km
22.82 km/s
2045-Oct-09 15:06 0.383373 AU
57351821 km
24.68 km/s
2056-Oct-08 07:35 0.403333 AU
60337685 km
25.33 km/s
2065-Mar-29 07:10 0.491776 AU
73568671 km
28.04 km/s
2067-Oct-04 19:11 0.480089 AU
71820270 km
27.70 km/s
2076-Mar-25 12:31 0.418049 AU
62539243 km
25.91 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
19.44

Orbit Quality

RMS
0.5421
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.