SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 QF33

2014 QF33

2014 QF33 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.167 AU it takes 1.26 yr to circle the Sun.

Apollo Observations: 62
Orbital Period · P
1.26 yr
v(q)
65.9 km/s
v(Q)
11.5 km/s
Diameter · ≈
0.06 km
TJ
5.13
Eccentricity · e
0.7016

Orbit and dynamics

Between its closest point (0.348 AU) and its farthest (1.986 AU), the heliocentric distance changes by 1.638 AU over every revolution.

One full revolution takes 1.26 yr (460 days), computed from the semi-major axis of 1.167 AU.

The high eccentricity (0.702) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.78° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 65.9 km/s at perihelion and falls to 11.5 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 = 23.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

Astrometry from 62 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5978 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
1.167 AU
Eccentricity
0.7016
Perihelion
0.348 AU
Aphelion
1.985767 AU
Inclination
3.78°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
174.04°

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
2026-Dec-11 01:01 0.179457 AU
26846378 km
18.30 km/s
2031-Dec-06 02:07 0.442067 AU
66132337 km
14.21 km/s
2032-Jan-21 07:34 0.469210 AU
70192797 km
14.39 km/s
2038-Aug-09 23:10 0.270335 AU
40441545 km
16.03 km/s
2043-Aug-17 00:24 0.007634 AU
1141996 km
23.08 km/s
2045-Nov-19 19:07 0.366085 AU
54765542 km
34.58 km/s
2048-Aug-23 02:11 0.158955 AU
23779350 km
28.09 km/s
2050-Nov-27 15:41 0.201836 AU
30194195 km
29.14 km/s
2053-Aug-30 19:55 0.326837 AU
48894108 km
33.38 km/s
2055-Dec-05 07:37 0.062847 AU
9401849 km
23.58 km/s
2058-Sep-07 17:58 0.487840 AU
72979842 km
38.70 km/s
2060-Dec-10 14:37 0.181175 AU
27103417 km
18.25 km/s
2065-Dec-09 20:58 0.366312 AU
54799443 km
14.41 km/s
2072-Aug-15 20:36 0.445315 AU
66618232 km
14.22 km/s
2077-Aug-10 02:49 0.270817 AU
40513669 km
16.02 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
23.7

Orbit Quality

RMS
0.59782
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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