SpaceAtlas Space Object Data
NASA JPL SBDB · 533722

533722

533722 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.384 AU it takes 3.68 yr to circle the Sun.

Apollo Observations: 721
Orbital Period · P
3.68 yr
v(q)
42.5 km/s
v(Q)
8.8 km/s
Diameter · ≈
0.84 km
TJ
3.2
Eccentricity · e
0.6584

Orbit and dynamics

The path is an ellipse reaching 0.814 AU from the Sun at perihelion and 3.954 AU at aphelion, a radial span of 3.14 AU.

Applying Kepler's third law to a = 2.384 AU gives an orbital period of 3.68 yr, or about 1,344 days.

The high eccentricity (0.658) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.86° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 42.5 km/s at perihelion and falls to 8.8 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

The measured diameter is 0.7 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.249 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 721 observations and has a weighted RMS residual of 0.3745 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
2.384 AU
Eccentricity
0.6584
Perihelion
0.814 AU
Aphelion
3.953626 AU
Inclination
3.86°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
57.54°

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
2036-Dec-30 03:00 0.150965 AU
22584002 km
19.37 km/s
2062-Sep-05 22:25 0.079760 AU
11931859 km
13.03 km/s
2073-Dec-09 02:57 0.078871 AU
11798912 km
12.87 km/s

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

Physical Parameters

Diameter
0.701 km
Albedo
0.249
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
18.12

Orbit Quality

RMS
0.37453
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.