SpaceAtlas Space Object Data
NASA JPL SBDB · 213869

213869

213869 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.86 AU it takes 2.54 yr to circle the Sun.

Apollo Observations: 209
Orbital Period · P
2.54 yr
v(q)
43.9 km/s
v(Q)
10.9 km/s
Diameter · ≈
0.97 km
TJ
3.56
Eccentricity · e
0.6032

Orbit and dynamics

Between its closest point (0.738 AU) and its farthest (2.982 AU), the heliocentric distance changes by 2.244 AU over every revolution.

One full revolution takes 2.54 yr (927 days), computed from the semi-major axis of 1.86 AU.

The high eccentricity (0.603) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 37.01° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 43.9 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 = 17.82 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.97 km.

Observation record and orbit quality

Astrometry from 209 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6047 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
1.86 AU
Eccentricity
0.6032
Perihelion
0.738 AU
Aphelion
2.981952 AU
Inclination
37.01°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
285.89°

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
2031-Nov-09 20:02 0.481140 AU
71977476 km
25.24 km/s
2042-Apr-05 18:00 0.173372 AU
25936118 km
24.22 km/s
2047-May-04 02:22 0.328085 AU
49080844 km
30.95 km/s
2069-Nov-12 23:21 0.475281 AU
71101061 km
21.00 km/s
2075-Mar-19 06:45 0.337339 AU
50465165 km
23.13 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
17.82

Orbit Quality

RMS
0.60469
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.