SpaceAtlas Space Object Data
NASA JPL SBDB · 614433

614433

614433 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.502 AU it takes 1.84 yr to circle the Sun.

Apollo Observations: 191
Orbital Period · P
1.84 yr
v(q)
39.7 km/s
v(Q)
14.9 km/s
Diameter · ≈
0.27 km
TJ
4.37
Eccentricity · e
0.4555

Orbit and dynamics

Between its closest point (0.818 AU) and its farthest (2.186 AU), the heliocentric distance changes by 1.368 AU over every revolution.

One full revolution takes 1.84 yr (672 days), computed from the semi-major axis of 1.502 AU.

The high eccentricity (0.456) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 18.21° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.7 km/s at perihelion and falls to 14.9 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

No direct size measurement is available; from an absolute magnitude of H = 20.58 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.27 km.

Observation record and orbit quality

Astrometry from 191 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4902 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
1.502 AU
Eccentricity
0.4555
Perihelion
0.818 AU
Aphelion
2.186161 AU
Inclination
18.21°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
56.63°

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
2031-Oct-30 21:13 0.218458 AU
32680826 km
16.56 km/s
2033-May-19 01:43 0.180147 AU
26949611 km
19.84 km/s
2042-Nov-11 12:16 0.438668 AU
65623805 km
25.24 km/s
2044-Jun-09 10:28 0.136601 AU
20435280 km
12.77 km/s
2055-Oct-27 05:50 0.296551 AU
44363392 km
10.79 km/s
2057-May-06 11:23 0.432304 AU
64671788 km
26.55 km/s
2066-Nov-06 00:38 0.318410 AU
47633499 km
21.24 km/s
2068-May-30 20:18 0.021481 AU
3213569 km
15.04 km/s
2079-Oct-27 20:55 0.210245 AU
31452229 km
13.97 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
20.58

Orbit Quality

RMS
0.49023
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.

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