SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 RT80

2010 RT80

2010 RT80 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.059 AU once every 2.95 yr.

Amor Observations: 82
Orbital Period · P
2.95 yr
v(q)
33.8 km/s
v(Q)
12.8 km/s
Diameter · ≈
0.09 km
TJ
3.64
Eccentricity · e
0.4513

Orbit and dynamics

The path is an ellipse reaching 1.13 AU from the Sun at perihelion and 2.988 AU at aphelion, a radial span of 1.858 AU.

Applying Kepler's third law to a = 2.059 AU gives an orbital period of 2.95 yr, or about 1,079 days.

The high eccentricity (0.451) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.64° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.8 km/s at perihelion and falls to 12.8 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 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

The current orbit solution is based on 82 observations and has a weighted RMS residual of 0.4821 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
2.059 AU
Eccentricity
0.4513
Perihelion
1.13 AU
Aphelion
2.988227 AU
Inclination
7.64°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
119.48°

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
2069-Sep-27 05:42 0.228691 AU
34211670 km
11.90 km/s
2072-Sep-06 23:41 0.117842 AU
17628874 km
6.00 km/s
2075-Aug-12 16:28 0.237272 AU
35495408 km
12.09 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
23.0

Orbit Quality

RMS
0.48214
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.

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