SpaceAtlas Space Object Data
NASA JPL SBDB · 363024

363024

363024 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.356 AU it takes 1.58 yr to circle the Sun.

Apollo Observations: 291
Orbital Period · P
1.58 yr
v(q)
40.5 km/s
v(Q)
16.2 km/s
Diameter · ≈
0.46 km
TJ
4.73
Eccentricity · e
0.4292

Orbit and dynamics

Between its closest point (0.774 AU) and its farthest (1.938 AU), the heliocentric distance changes by 1.164 AU over every revolution.

One full revolution takes 1.58 yr (577 days), computed from the semi-major axis of 1.356 AU.

The high eccentricity (0.429) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.99° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40.5 km/s at perihelion and falls to 16.2 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

The measured diameter is 0.56 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.099 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

Astrometry from 291 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4007 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
1.356 AU
Eccentricity
0.4292
Perihelion
0.774 AU
Aphelion
1.937995 AU
Inclination
13.99°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
175.45°

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
2047-Aug-11 23:22 0.174005 AU
26030775 km
15.59 km/s
2051-Jan-25 15:38 0.116243 AU
17389772 km
16.54 km/s
2070-Jan-04 23:34 0.127759 AU
19112511 km
11.29 km/s
2077-Aug-16 08:04 0.154963 AU
23182070 km
12.38 km/s

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

Physical Parameters

Diameter
0.558 km
Albedo
0.099
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.42

Orbit Quality

RMS
0.40065
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

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