SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 QX10

2016 QX10

2016 QX10 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.326 AU it takes 1.53 yr to circle the Sun.

Apollo Observations: 25
Orbital Period · P
1.53 yr
v(q)
34.3 km/s
v(Q)
19.5 km/s
Diameter · ≈
0.06 km
TJ
4.89
Eccentricity · e
0.274

Orbit and dynamics

The path is an ellipse reaching 0.962 AU from the Sun at perihelion and 1.689 AU at aphelion, a radial span of 0.727 AU.

Applying Kepler's third law to a = 1.326 AU gives an orbital period of 1.53 yr, or about 558 days.

An eccentricity of 0.274 makes the orbit moderately elongated.

Its inclination of 3.64° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.3 km/s at perihelion and falls to 19.5 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

The current orbit solution is based on 25 observations and has a weighted RMS residual of 0.4138 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
1.326 AU
Eccentricity
0.274
Perihelion
0.962 AU
Aphelion
1.689324 AU
Inclination
3.64°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
184.45°

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
2042-Apr-29 18:58 0.136922 AU
20483217 km
11.53 km/s
2042-Oct-10 00:47 0.378713 AU
56654622 km
5.60 km/s
2048-Mar-15 06:37 0.386372 AU
57800420 km
5.86 km/s
2048-Aug-28 01:20 0.148407 AU
22201432 km
11.87 km/s
2071-Apr-25 05:47 0.260820 AU
39018091 km
13.92 km/s
2071-Oct-18 16:39 0.446273 AU
66761484 km
6.52 km/s
2074-Jun-02 12:51 0.043692 AU
6536166 km
5.52 km/s
2077-Mar-25 07:20 0.351622 AU
52601904 km
4.73 km/s
2077-Aug-22 17:57 0.098054 AU
14668665 km
9.64 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
0.41378
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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