SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 LT48

2016 LT48

2016 LT48 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.249 AU once every 3.37 yr.

Amor Observations: 25
Orbital Period · P
3.37 yr
v(q)
34.4 km/s
v(Q)
11.5 km/s
Diameter · ≈
0.16 km
TJ
3.44
Eccentricity · e
0.4993

Orbit and dynamics

Between its closest point (1.126 AU) and its farthest (3.372 AU), the heliocentric distance changes by 2.246 AU over every revolution.

One full revolution takes 3.37 yr (1,232 days), computed from the semi-major axis of 2.249 AU.

The high eccentricity (0.499) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.89° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 34.4 km/s at perihelion and falls to 11.5 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 = 21.76 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.16 km.

Observation record and orbit quality

Astrometry from 25 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5387 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
2.249 AU
Eccentricity
0.4993
Perihelion
1.126 AU
Aphelion
3.371926 AU
Inclination
6.89°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
314.85°

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
2033-Jul-29 10:53 0.410670 AU
61435420 km
15.36 km/s
2043-Sep-28 09:39 0.385917 AU
57732409 km
13.29 km/s
2060-Jul-29 17:55 0.396887 AU
59373440 km
15.44 km/s
2070-Sep-28 08:42 0.365034 AU
54608260 km
13.18 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
21.76

Orbit Quality

RMS
0.53873
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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