SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 QA2

2016 QA2

2016 QA2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.946 AU and a period of 0.92 yr.

Aten Observations: 107
Orbital Period · P
0.92 yr
v(q)
39.2 km/s
v(Q)
23.9 km/s
Diameter · ≈
0.03 km
TJ
6.3
Eccentricity · e
0.2419

Orbit and dynamics

The path is an ellipse reaching 0.717 AU from the Sun at perihelion and 1.175 AU at aphelion, a radial span of 0.458 AU.

Applying Kepler's third law to a = 0.946 AU gives an orbital period of 0.92 yr, or about 336 days.

An eccentricity of 0.242 makes the orbit moderately elongated.

The orbital plane is tilted 14.75° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.2 km/s at perihelion and falls to 23.9 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 = 25.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 107 observations and has a weighted RMS residual of 0.3408 arcseconds.

Condition code U = 4 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
0.9458 AU
Eccentricity
0.2419
Perihelion
0.717 AU
Aphelion
1.174589 AU
Inclination
14.75°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
135.01°

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-Jan-27 23:29 0.271644 AU
40637295 km
10.71 km/s
2027-Aug-15 16:27 0.204293 AU
30561737 km
7.74 km/s
2028-Aug-19 19:31 0.264980 AU
39640397 km
16.26 km/s
2037-Apr-25 03:03 0.401842 AU
60114648 km
18.62 km/s
2038-Mar-08 04:34 0.171482 AU
25653353 km
10.06 km/s
2038-Dec-16 20:39 0.334475 AU
50036806 km
9.59 km/s
2039-Aug-28 13:08 0.018413 AU
2754503 km
10.21 km/s
2049-Mar-27 08:44 0.165539 AU
24764256 km
10.97 km/s
2050-Jan-10 16:52 0.305155 AU
45650514 km
10.73 km/s
2050-Aug-27 07:00 0.100435 AU
15024801 km
8.13 km/s
2051-Aug-16 14:25 0.356820 AU
53379497 km
19.16 km/s
2060-Apr-12 11:07 0.234001 AU
35006099 km
13.97 km/s
2061-Feb-05 07:04 0.241858 AU
36181400 km
10.66 km/s
2061-Aug-05 14:58 0.217177 AU
32489164 km
7.74 km/s
2062-Aug-21 20:06 0.200975 AU
30065419 km
15.33 km/s
2071-Apr-20 22:47 0.303637 AU
45423442 km
16.40 km/s
2072-Feb-22 02:31 0.199013 AU
29771905 km
10.29 km/s
2072-Nov-23 23:06 0.326514 AU
48845812 km
7.92 km/s
2073-Aug-24 22:59 0.101246 AU
15146209 km
12.91 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
25.1

Orbit Quality

RMS
0.34077
Condition
4
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.