SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 TK

2016 TK

2016 TK belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.327 AU it takes 1.53 yr to circle the Sun.

Apollo Observations: 80
Orbital Period · P
1.53 yr
v(q)
33.9 km/s
v(Q)
19.7 km/s
Diameter · ≈
0.08 km
TJ
4.88
Eccentricity · e
0.2651

Orbit and dynamics

Between its closest point (0.975 AU) and its farthest (1.679 AU), the heliocentric distance changes by 0.704 AU over every revolution.

One full revolution takes 1.53 yr (558 days), computed from the semi-major axis of 1.327 AU.

An eccentricity of 0.265 makes the orbit moderately elongated.

The orbital plane is tilted 9.78° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.9 km/s at perihelion and falls to 19.7 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 = 23.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.08 km.

Observation record and orbit quality

Astrometry from 80 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6256 arcseconds.

Condition code U = 0 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
1.327 AU
Eccentricity
0.2651
Perihelion
0.975 AU
Aphelion
1.678788 AU
Inclination
9.78°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
81.46°

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-Oct-13 10:31 0.237696 AU
35558846 km
12.36 km/s
2043-Mar-11 17:40 0.335475 AU
50186335 km
6.42 km/s
2045-Oct-20 15:16 0.172159 AU
25754625 km
5.06 km/s
2046-Feb-01 08:38 0.153041 AU
22894620 km
6.39 km/s
2048-Aug-31 06:56 0.426973 AU
63874272 km
6.58 km/s
2049-Feb-13 20:08 0.398569 AU
59625041 km
16.32 km/s
2068-Oct-08 19:58 0.331882 AU
49648803 km
15.07 km/s
2069-Mar-21 03:43 0.389417 AU
58255891 km
7.05 km/s
2071-Oct-22 22:36 0.109292 AU
16349925 km
6.23 km/s
2072-Feb-06 13:22 0.179628 AU
26871947 km
4.95 km/s
2074-Sep-12 04:27 0.368854 AU
55179749 km
6.04 km/s
2075-Feb-10 05:16 0.307545 AU
46008036 km
13.43 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
23.3

Orbit Quality

RMS
0.62559
Condition
0
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

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