SpaceAtlas Space Object Data
NASA JPL SBDB · 612780

612780

612780 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.917 AU it takes 2.65 yr to circle the Sun.

Apollo Observations: 483
Orbital Period · P
2.65 yr
v(q)
39.2 km/s
v(Q)
11.8 km/s
Diameter · ≈
0.33 km
TJ
3.72
Eccentricity · e
0.5364

Orbit and dynamics

Between its closest point (0.889 AU) and its farthest (2.945 AU), the heliocentric distance changes by 2.056 AU over every revolution.

One full revolution takes 2.65 yr (969 days), computed from the semi-major axis of 1.917 AU.

The high eccentricity (0.536) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 9.77° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.2 km/s at perihelion and falls to 11.8 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 = 20.16 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.33 km.

Observation record and orbit quality

Astrometry from 483 individual observations underpins this orbit; the fit leaves an RMS residual of 0.576 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
1.917 AU
Eccentricity
0.5364
Perihelion
0.889 AU
Aphelion
2.945279 AU
Inclination
9.77°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
118.18°

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
2028-Feb-10 00:23 0.332270 AU
49706900 km
20.45 km/s
2057-Jul-05 18:13 0.334701 AU
50070631 km
21.94 km/s
2065-Jun-19 01:16 0.065855 AU
9851812 km
14.53 km/s
2073-May-19 11:48 0.127691 AU
19102267 km
10.24 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
20.16

Orbit Quality

RMS
0.57597
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.