SpaceAtlas Space Object Data
NASA JPL SBDB · 322763

322763

322763 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.007 AU it takes 2.84 yr to circle the Sun.

Apollo Observations: 511
Orbital Period · P
2.84 yr
v(q)
38.3 km/s
v(Q)
11.6 km/s
Diameter · ≈
1.28 km
TJ
3.56
Eccentricity · e
0.5359

Orbit and dynamics

The path is an ellipse reaching 0.931 AU from the Sun at perihelion and 3.083 AU at aphelion, a radial span of 2.152 AU.

Applying Kepler's third law to a = 2.007 AU gives an orbital period of 2.84 yr, or about 1,039 days.

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

A steep inclination of 22.83° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 38.3 km/s at perihelion and falls to 11.6 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 1.25 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.196 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 511 observations and has a weighted RMS residual of 0.4717 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
2.007 AU
Eccentricity
0.5359
Perihelion
0.931 AU
Aphelion
3.082551 AU
Inclination
22.83°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
15.16°

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
2034-Sep-23 15:29 0.106096 AU
15871744 km
16.58 km/s
2051-Oct-15 11:56 0.348733 AU
52169745 km
12.14 km/s
2052-Jan-16 22:21 0.377913 AU
56534914 km
12.19 km/s
2069-Jan-27 20:27 0.460974 AU
68960674 km
20.69 km/s
2071-Sep-08 02:34 0.366729 AU
54861831 km
24.11 km/s

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

Physical Parameters

Diameter
1.252 km
Albedo
0.196
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
17.21

Orbit Quality

RMS
0.47173
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.