SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 VK6

2016 VK6

2016 VK6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.341 AU it takes 1.55 yr to circle the Sun.

Apollo Observations: 46
Orbital Period · P
1.55 yr
v(q)
33.1 km/s
v(Q)
20 km/s
Diameter · ≈
0.11 km
TJ
4.86
Eccentricity · e
0.2484

Orbit and dynamics

The path is an ellipse reaching 1.008 AU from the Sun at perihelion and 1.674 AU at aphelion, a radial span of 0.666 AU.

Applying Kepler's third law to a = 1.341 AU gives an orbital period of 1.55 yr, or about 567 days.

An eccentricity of 0.248 makes the orbit moderately elongated.

The orbital plane is tilted 7.74° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.1 km/s at perihelion and falls to 20 km/s at aphelion.

Size and surface

The measured diameter is 0.19 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.036 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

The current orbit solution is based on 46 observations and has a weighted RMS residual of 0.4471 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
1.341 AU
Eccentricity
0.2484
Perihelion
1.008 AU
Aphelion
1.674104 AU
Inclination
7.74°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
69.85°

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
2030-Sep-13 03:48 0.060538 AU
9056282 km
6.49 km/s
2033-Jun-28 01:22 0.481098 AU
71971196 km
6.15 km/s
2044-Aug-23 17:21 0.359089 AU
53718974 km
14.86 km/s
2045-Jan-25 13:04 0.392575 AU
58728345 km
6.32 km/s
2047-Nov-23 22:32 0.241282 AU
36095251 km
9.38 km/s
2061-Sep-14 16:25 0.052463 AU
7848385 km
6.10 km/s
2064-Jun-28 03:21 0.480670 AU
71907257 km
6.13 km/s
2075-Aug-20 20:13 0.428922 AU
64165882 km
16.83 km/s
2076-Feb-02 11:25 0.423420 AU
63342737 km
6.94 km/s
2078-Nov-08 13:17 0.168143 AU
25153834 km
6.43 km/s

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

Physical Parameters

Diameter
0.194 km
Albedo
0.036
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
22.45

Orbit Quality

RMS
0.44712
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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