SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 TL143

2015 TL143

2015 TL143 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.584 AU once every 4.15 yr.

Amor Observations: 115
Orbital Period · P
4.15 yr
v(q)
37.1 km/s
v(Q)
9.3 km/s
Diameter · ≈
0.08 km
TJ
3.14
Eccentricity · e
0.6005

Orbit and dynamics

Between its closest point (1.032 AU) and its farthest (4.136 AU), the heliocentric distance changes by 3.104 AU over every revolution.

One full revolution takes 4.15 yr (1,517 days), computed from the semi-major axis of 2.584 AU.

The high eccentricity (0.601) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.95° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.1 km/s at perihelion and falls to 9.3 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

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 115 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3839 arcseconds.

Condition code U = 5 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
2.584 AU
Eccentricity
0.6005
Perihelion
1.032 AU
Aphelion
4.135692 AU
Inclination
4.95°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
197.08°

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
2040-Nov-17 15:34 0.101920 AU
15247089 km
10.42 km/s
2061-Sep-20 15:55 0.158839 AU
23761907 km
12.65 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
0.38385
Condition
5
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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