SpaceAtlas Space Object Data
NASA JPL SBDB · 294739

294739

294739 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.566 AU it takes 1.96 yr to circle the Sun.

Apollo Observations: 1,912
Orbital Period · P
1.96 yr
v(q)
36.7 km/s
v(Q)
15.4 km/s
Diameter · ≈
1.39 km
TJ
4.13
Eccentricity · e
0.408

Orbit and dynamics

Between its closest point (0.927 AU) and its farthest (2.205 AU), the heliocentric distance changes by 1.278 AU over every revolution.

One full revolution takes 1.96 yr (716 days), computed from the semi-major axis of 1.566 AU.

The high eccentricity (0.408) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 36.02° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 36.7 km/s at perihelion and falls to 15.4 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 0.74 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.425 points to a comparatively bright, reflective surface.

Observation record and orbit quality

Astrometry from 1,912 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3862 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
1.566 AU
Eccentricity
0.408
Perihelion
0.927 AU
Aphelion
2.204928 AU
Inclination
36.02°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
138.66°

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
2063-Jan-06 05:11 0.176551 AU
26411594 km
23.71 km/s
2064-Dec-26 13:55 0.094425 AU
14125821 km
20.53 km/s

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

Physical Parameters

Diameter
0.74 km
Albedo
0.425
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
17.04

Orbit Quality

RMS
0.38623
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.