SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 TD2

2018 TD2

2018 TD2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.843 AU and a period of 0.77 yr.

Aten Observations: 16
Orbital Period · P
0.77 yr
v(q)
50.5 km/s
v(Q)
20.8 km/s
Diameter · ≈
0.02 km
TJ
6.89
Eccentricity · e
0.4155

Orbit and dynamics

Between its closest point (0.493 AU) and its farthest (1.193 AU), the heliocentric distance changes by 0.7 AU over every revolution.

One full revolution takes 0.77 yr (283 days), computed from the semi-major axis of 0.843 AU.

The high eccentricity (0.415) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 10.54° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 50.5 km/s at perihelion and falls to 20.8 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

No direct size measurement is available; from an absolute magnitude of H = 26.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 16 individual observations underpins this orbit; the fit leaves an RMS residual of 0.294 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
0.843 AU
Eccentricity
0.4155
Perihelion
0.493 AU
Aphelion
1.193267 AU
Inclination
10.54°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
220.9°

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-Aug-28 09:50 0.221873 AU
33191754 km
9.45 km/s
2028-Dec-24 06:53 0.400167 AU
59864074 km
11.63 km/s
2031-Jul-25 13:27 0.270007 AU
40392478 km
19.29 km/s
2032-Oct-03 01:19 0.294611 AU
44073106 km
22.59 km/s
2038-Jul-19 10:17 0.185362 AU
27729784 km
13.15 km/s
2039-Feb-06 13:14 0.493273 AU
73792612 km
19.91 km/s
2042-Oct-12 15:34 0.021825 AU
3264960 km
11.60 km/s
2048-Aug-01 19:08 0.289547 AU
43315598 km
25.39 km/s
2049-Oct-10 13:42 0.029184 AU
4365807 km
16.29 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
26.5

Orbit Quality

RMS
0.29396
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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