SpaceAtlas Space Object Data
NASA JPL SBDB · 510073

510073

510073 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.232 AU it takes 3.33 yr to circle the Sun.

Apollo Observations: 244
Orbital Period · P
3.33 yr
v(q)
43.9 km/s
v(Q)
9 km/s
Diameter · ≈
0.69 km
TJ
3.27
Eccentricity · e
0.6588

Orbit and dynamics

The path is an ellipse reaching 0.762 AU from the Sun at perihelion and 3.702 AU at aphelion, a radial span of 2.94 AU.

Applying Kepler's third law to a = 2.232 AU gives an orbital period of 3.33 yr, or about 1,218 days.

The high eccentricity (0.659) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 17.31° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43.9 km/s at perihelion and falls to 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

The measured diameter is 0.45 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.316 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 244 observations and has a weighted RMS residual of 0.5221 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
2.232 AU
Eccentricity
0.6588
Perihelion
0.762 AU
Aphelion
3.702442 AU
Inclination
17.31°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
266.77°

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
2030-Aug-12 10:13 0.271178 AU
40567580 km
17.27 km/s
2040-Aug-23 22:35 0.295667 AU
44231099 km
17.25 km/s
2050-Aug-20 05:07 0.290655 AU
43481333 km
17.36 km/s
2060-Aug-22 19:56 0.291816 AU
43655127 km
17.15 km/s
2070-Aug-19 22:01 0.293778 AU
43948531 km
17.46 km/s

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

Physical Parameters

Diameter
0.451 km
Albedo
0.316
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
18.56

Orbit Quality

RMS
0.52205
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.