SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 JT2

2018 JT2

2018 JT2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.757 AU and a period of 0.66 yr.

Aten Observations: 20
Orbital Period · P
0.66 yr
v(q)
60.5 km/s
v(Q)
19.4 km/s
Diameter · ≈
0.05 km
TJ
7.46
Eccentricity · e
0.5148

Orbit and dynamics

The path is an ellipse reaching 0.367 AU from the Sun at perihelion and 1.147 AU at aphelion, a radial span of 0.78 AU.

Applying Kepler's third law to a = 0.757 AU gives an orbital period of 0.66 yr, or about 241 days.

The high eccentricity (0.515) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 25.77° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 60.5 km/s at perihelion and falls to 19.4 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 = 24.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

The current orbit solution is based on 20 observations and has a weighted RMS residual of 0.4682 arcseconds.

Condition code U = 3 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
0.7569 AU
Eccentricity
0.5148
Perihelion
0.367 AU
Aphelion
1.146552 AU
Inclination
25.77°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
294.07°

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-May-14 23:36 0.426065 AU
63738391 km
27.38 km/s
2035-Apr-16 19:15 0.461303 AU
69009929 km
24.44 km/s
2037-Apr-14 02:15 0.366892 AU
54886313 km
20.47 km/s
2039-Apr-15 23:50 0.292701 AU
43787453 km
17.28 km/s
2041-Apr-21 10:17 0.240019 AU
35906289 km
15.48 km/s
2043-Apr-30 10:27 0.196993 AU
29469671 km
14.79 km/s
2045-May-08 18:04 0.151368 AU
22644264 km
14.67 km/s
2047-May-16 19:47 0.105490 AU
15781120 km
15.11 km/s
2049-May-21 00:49 0.103075 AU
15419820 km
16.52 km/s
2051-May-22 11:36 0.177099 AU
26493570 km
19.13 km/s
2053-May-19 23:59 0.284822 AU
42608713 km
22.64 km/s
2055-May-16 17:04 0.403482 AU
60360011 km
26.60 km/s
2062-Apr-17 09:15 0.480129 AU
71826220 km
25.23 km/s
2064-Apr-14 04:20 0.382855 AU
57274290 km
21.17 km/s
2066-Apr-15 06:55 0.304164 AU
45502251 km
17.78 km/s
2068-Apr-19 22:06 0.248062 AU
37109598 km
15.71 km/s
2070-Apr-28 15:00 0.204608 AU
30608946 km
14.86 km/s
2072-May-06 23:54 0.160230 AU
23970058 km
14.65 km/s
2074-May-15 10:11 0.113037 AU
16910060 km
14.96 km/s
2076-May-20 06:45 0.097348 AU
14563057 km
16.15 km/s
2078-May-22 10:50 0.159571 AU
23871506 km
18.54 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
24.4

Orbit Quality

RMS
0.46822
Condition
3
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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