SpaceAtlas Space Object Data
NASA JPL SBDB · 349219

349219

349219 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.734 AU it takes 2.28 yr to circle the Sun.

Apollo Observations: 191
Orbital Period · P
2.28 yr
v(q)
38.8 km/s
v(Q)
13.2 km/s
Diameter · ≈
0.84 km
TJ
3.85
Eccentricity · e
0.4939

Orbit and dynamics

Between its closest point (0.878 AU) and its farthest (2.59 AU), the heliocentric distance changes by 1.712 AU over every revolution.

One full revolution takes 2.28 yr (834 days), computed from the semi-major axis of 1.734 AU.

The high eccentricity (0.494) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 32.22° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 38.8 km/s at perihelion and falls to 13.2 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

The measured diameter is 0.58 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.272 points to a comparatively bright, reflective surface.

Observation record and orbit quality

Astrometry from 191 individual observations underpins this orbit; the fit leaves an RMS residual of 0.486 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
1.734 AU
Eccentricity
0.4939
Perihelion
0.878 AU
Aphelion
2.590423 AU
Inclination
32.22°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
75.58°

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
2030-Jun-17 17:21 0.324899 AU
48604233 km
24.84 km/s
2039-Aug-28 06:14 0.447272 AU
66911013 km
21.80 km/s
2046-Jun-11 23:58 0.400757 AU
59952438 km
26.37 km/s
2055-Aug-18 03:48 0.372576 AU
55736542 km
21.15 km/s
2062-Jun-05 21:43 0.484463 AU
72474677 km
28.23 km/s
2071-Aug-08 11:39 0.294858 AU
44110188 km
20.64 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.583 km
Albedo
0.272
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
18.13

Orbit Quality

RMS
0.48605
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.