SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 QA84

2016 QA84

2016 QA84 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.213 AU it takes 1.34 yr to circle the Sun.

Apollo Observations: 45
Orbital Period · P
1.34 yr
v(q)
36.2 km/s
v(Q)
20.2 km/s
Diameter · ≈
0.11 km
TJ
5.07
Eccentricity · e
0.283

Orbit and dynamics

Between its closest point (0.87 AU) and its farthest (1.556 AU), the heliocentric distance changes by 0.686 AU over every revolution.

One full revolution takes 1.34 yr (488 days), computed from the semi-major axis of 1.213 AU.

An eccentricity of 0.283 makes the orbit moderately elongated.

A steep inclination of 32.68° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 36.2 km/s at perihelion and falls to 20.2 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 = 22.53 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

Astrometry from 45 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6393 arcseconds.

Condition code U = 1 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
1.213 AU
Eccentricity
0.283
Perihelion
0.87 AU
Aphelion
1.556279 AU
Inclination
32.68°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
226.52°

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
2028-Mar-10 06:47 0.216002 AU
32313456 km
18.65 km/s
2028-Aug-15 09:59 0.369518 AU
55279135 km
16.68 km/s
2032-Mar-14 05:03 0.264997 AU
39643008 km
18.77 km/s
2032-Aug-14 01:41 0.368215 AU
55084253 km
16.85 km/s
2036-Mar-18 16:31 0.317661 AU
47521421 km
19.03 km/s
2036-Aug-12 19:55 0.370508 AU
55427243 km
17.09 km/s
2040-Mar-23 13:29 0.371179 AU
55527571 km
19.41 km/s
2040-Aug-11 15:05 0.377437 AU
56463757 km
17.42 km/s
2044-Mar-28 22:29 0.426376 AU
63784893 km
19.89 km/s
2044-Aug-10 13:55 0.389251 AU
58231168 km
17.82 km/s
2048-Apr-04 04:44 0.482112 AU
72122892 km
20.41 km/s
2048-Aug-09 16:30 0.405903 AU
60722268 km
18.35 km/s
2052-Aug-09 00:24 0.428126 AU
64046685 km
18.98 km/s
2056-Aug-08 13:51 0.456137 AU
68237164 km
19.78 km/s
2060-Aug-08 11:23 0.489193 AU
73182270 km
20.73 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
22.53

Orbit Quality

RMS
0.63932
Condition
1
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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