SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 QC2

2024 QC2

2024 QC2 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.487 AU once every 1.81 yr.

Amor Observations: 43
Orbital Period · P
1.81 yr
v(q)
28.4 km/s
v(Q)
21 km/s
Diameter · ≈
0.18 km
TJ
4.48
Eccentricity · e
0.1518

Orbit and dynamics

The path is an ellipse reaching 1.262 AU from the Sun at perihelion and 1.713 AU at aphelion, a radial span of 0.451 AU.

Applying Kepler's third law to a = 1.487 AU gives an orbital period of 1.81 yr, or about 662 days.

An eccentricity of 0.152 makes the orbit moderately elongated.

A steep inclination of 22.53° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 28.4 km/s at perihelion and falls to 21 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 21.46 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.18 km.

Observation record and orbit quality

The current orbit solution is based on 43 observations and has a weighted RMS residual of 0.4408 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.487 AU
Eccentricity
0.1518
Perihelion
1.262 AU
Aphelion
1.712727 AU
Inclination
22.53°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
304.27°

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
2027-Feb-09 18:10 0.493302 AU
73796992 km
12.07 km/s
2033-Aug-24 20:39 0.413410 AU
61845301 km
11.46 km/s
2036-Jan-21 01:51 0.452657 AU
67716499 km
11.22 km/s
2044-Sep-30 12:06 0.457112 AU
68382936 km
10.57 km/s
2053-Sep-06 09:28 0.377931 AU
56537685 km
11.32 km/s
2056-Feb-03 18:23 0.462096 AU
69128566 km
11.85 km/s
2062-Aug-18 17:13 0.434474 AU
64996321 km
11.49 km/s
2065-Jan-11 20:19 0.460864 AU
68944337 km
10.64 km/s
2073-Sep-20 10:21 0.404727 AU
60546267 km
11.13 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
21.46

Orbit Quality

RMS
0.44084
Condition
6
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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