SpaceAtlas Space Object Data
NASA JPL SBDB · 267720

267720

267720 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.379 AU it takes 1.62 yr to circle the Sun.

Apollo Observations: 398
Orbital Period · P
1.62 yr
v(q)
62.8 km/s
v(Q)
10.2 km/s
Diameter · ≈
0.59 km
TJ
4.44
Eccentricity · e
0.7196

Orbit and dynamics

Between its closest point (0.387 AU) and its farthest (2.371 AU), the heliocentric distance changes by 1.984 AU over every revolution.

One full revolution takes 1.62 yr (591 days), computed from the semi-major axis of 1.379 AU.

The high eccentricity (0.72) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 21.15° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 62.8 km/s at perihelion and falls to 10.2 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

No direct size measurement is available; from an absolute magnitude of H = 18.91 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.59 km.

Observation record and orbit quality

Astrometry from 398 individual observations underpins this orbit; the fit leaves an RMS residual of 0.478 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
1.379 AU
Eccentricity
0.7196
Perihelion
0.387 AU
Aphelion
2.371328 AU
Inclination
21.15°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
190.81°

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
2037-Jan-18 22:49 0.049991 AU
7478509 km
25.47 km/s
2071-Jan-23 07:56 0.091348 AU
13665446 km
28.13 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
18.91

Orbit Quality

RMS
0.47802
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.