SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 TL18

2016 TL18

2016 TL18 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.206 AU it takes 1.32 yr to circle the Sun.

Apollo Observations: 70
Orbital Period · P
1.32 yr
v(q)
60.2 km/s
v(Q)
12.2 km/s
Diameter · ≈
0.17 km
TJ
5.02
Eccentricity · e
0.6627

Orbit and dynamics

The path is an ellipse reaching 0.407 AU from the Sun at perihelion and 2.005 AU at aphelion, a radial span of 1.598 AU.

Applying Kepler's third law to a = 1.206 AU gives an orbital period of 1.32 yr, or about 484 days.

The high eccentricity (0.663) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 11.04° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 60.2 km/s at perihelion and falls to 12.2 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 = 21.61 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.17 km.

Observation record and orbit quality

The current orbit solution is based on 70 observations and has a weighted RMS residual of 0.6699 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
1.206 AU
Eccentricity
0.6627
Perihelion
0.407 AU
Aphelion
2.005216 AU
Inclination
11.04°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
154.92°

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-24 21:19 0.298125 AU
44598910 km
29.41 km/s
2031-Jan-17 19:05 0.430312 AU
64373749 km
34.45 km/s
2053-Oct-21 05:37 0.376046 AU
56255693 km
33.25 km/s
2057-Oct-14 13:10 0.238593 AU
35692960 km
28.37 km/s
2060-Feb-03 20:28 0.481687 AU
72059311 km
12.91 km/s
2060-Mar-26 10:13 0.465757 AU
69676269 km
17.54 km/s
2061-Oct-08 07:37 0.138313 AU
20691323 km
23.65 km/s
2064-Feb-14 06:39 0.346875 AU
51891815 km
13.73 km/s
2065-Oct-02 22:00 0.170760 AU
25545333 km
19.17 km/s
2068-Feb-10 00:37 0.229146 AU
34279825 km
18.12 km/s
2069-Sep-30 06:16 0.294615 AU
44073786 km
15.25 km/s
2072-Feb-03 16:01 0.187106 AU
27990673 km
22.84 km/s
2073-Aug-26 16:23 0.454887 AU
68050091 km
11.93 km/s
2073-Oct-05 16:06 0.429760 AU
64291135 km
13.74 km/s
2076-Jan-27 20:09 0.259364 AU
38800273 km
27.78 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
21.61

Orbit Quality

RMS
0.66987
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.

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