SpaceAtlas Space Object Data
NASA JPL SBDB · 279816

279816

279816 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.238 AU it takes 1.38 yr to circle the Sun.

Apollo Observations: 190
Orbital Period · P
1.38 yr
v(q)
40.9 km/s
v(Q)
17.5 km/s
Diameter · ≈
0.5 km
TJ
4.77
Eccentricity · e
0.4005

Orbit and dynamics

Between its closest point (0.742 AU) and its farthest (1.734 AU), the heliocentric distance changes by 0.992 AU over every revolution.

One full revolution takes 1.38 yr (503 days), computed from the semi-major axis of 1.238 AU.

The high eccentricity (0.401) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 50.74° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.9 km/s at perihelion and falls to 17.5 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 = 19.25 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.5 km.

Observation record and orbit quality

Astrometry from 190 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5355 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
1.238 AU
Eccentricity
0.4005
Perihelion
0.742 AU
Aphelion
1.733819 AU
Inclination
50.74°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
271.24°

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
2029-May-02 12:43 0.158180 AU
23663422 km
28.38 km/s
2040-May-05 10:30 0.135145 AU
20217471 km
26.68 km/s
2044-Oct-30 08:46 0.130222 AU
19480909 km
27.74 km/s
2051-May-08 15:49 0.196668 AU
29421068 km
25.40 km/s
2055-Nov-05 06:36 0.045727 AU
6840601 km
29.10 km/s
2066-Nov-10 08:44 0.130179 AU
19474494 km
30.89 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
19.25

Orbit Quality

RMS
0.53549
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.