SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 TS6

2018 TS6

2018 TS6 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.898 AU and a period of 0.85 yr.

Aten Observations: 6
Orbital Period · P
0.85 yr
v(q)
39.1 km/s
v(Q)
25.3 km/s
Diameter · ≈
0.01 km
TJ
6.6
Eccentricity · e
0.2139

Orbit and dynamics

The path is an ellipse reaching 0.706 AU from the Sun at perihelion and 1.09 AU at aphelion, a radial span of 0.384 AU.

Applying Kepler's third law to a = 0.898 AU gives an orbital period of 0.85 yr, or about 311 days.

An eccentricity of 0.214 makes the orbit moderately elongated.

The orbital plane is tilted 8.92° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.1 km/s at perihelion and falls to 25.3 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 = 28.18 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 6 observations and has a weighted RMS residual of 0.3819 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.898 AU
Eccentricity
0.2139
Perihelion
0.706 AU
Aphelion
1.090082 AU
Inclination
8.92°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
121.72°

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
2029-Oct-11 14:34 0.321850 AU
48148009 km
19.24 km/s
2031-Jan-15 12:08 0.145912 AU
21828086 km
9.88 km/s
2035-Oct-03 12:38 0.041932 AU
6272917 km
11.57 km/s
2037-Jan-02 10:22 0.309382 AU
46282821 km
17.87 km/s
2048-Jan-26 14:52 0.146113 AU
21858234 km
6.27 km/s
2052-Oct-06 13:15 0.237533 AU
35534358 km
15.15 km/s
2053-May-22 01:46 0.319663 AU
47820950 km
10.22 km/s
2054-Jan-08 08:49 0.276832 AU
41413517 km
14.12 km/s
2058-Oct-01 13:30 0.018797 AU
2811927 km
8.20 km/s
2059-Apr-17 02:51 0.275638 AU
41234903 km
9.78 km/s
2059-Dec-30 00:18 0.470257 AU
70349402 km
21.24 km/s
2064-Oct-18 23:38 0.099818 AU
14932594 km
5.83 km/s
2065-Mar-20 06:44 0.217654 AU
32560620 km
8.25 km/s
2075-Oct-12 14:45 0.370486 AU
55423961 km
19.70 km/s
2077-Jan-17 22:56 0.147558 AU
22074363 km
8.90 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
28.18

Orbit Quality

RMS
0.38186
Condition
7
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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