SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 QC84

2016 QC84

2016 QC84 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.506 AU it takes 1.85 yr to circle the Sun.

Apollo Observations: 283
Orbital Period · P
1.85 yr
v(q)
37.2 km/s
v(Q)
15.8 km/s
Diameter · ≈
0.33 km
TJ
4.4
Eccentricity · e
0.4027

Orbit and dynamics

Between its closest point (0.899 AU) and its farthest (2.112 AU), the heliocentric distance changes by 1.213 AU over every revolution.

One full revolution takes 1.85 yr (675 days), computed from the semi-major axis of 1.506 AU.

The high eccentricity (0.403) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 16.63° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 37.2 km/s at perihelion and falls to 15.8 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

The measured diameter is 0.25 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.257 points to a comparatively bright, reflective surface.

Observation record and orbit quality

Astrometry from 283 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4497 arcseconds.

Condition code U = 2 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
1.506 AU
Eccentricity
0.4027
Perihelion
0.899 AU
Aphelion
2.112466 AU
Inclination
16.63°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
55.39°

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-Feb-18 16:23 0.380076 AU
56858564 km
20.03 km/s
2029-Sep-18 15:00 0.275970 AU
41284518 km
18.77 km/s
2040-Oct-14 11:51 0.290703 AU
43488616 km
8.44 km/s
2041-Feb-07 22:35 0.240529 AU
35982665 km
9.78 km/s
2052-Feb-22 12:07 0.459731 AU
68774732 km
22.58 km/s
2053-Sep-22 18:49 0.193122 AU
28890699 km
16.48 km/s
2065-Feb-07 15:44 0.214704 AU
32119279 km
10.78 km/s
2076-Feb-23 20:03 0.484018 AU
72408121 km
23.35 km/s
2077-Sep-23 21:22 0.174009 AU
26031407 km
15.93 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.25 km
Albedo
0.257
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
20.13

Orbit Quality

RMS
0.44967
Condition
2
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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