SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 RR150

2015 RR150

2015 RR150 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.038 AU once every 2.91 yr.

Amor Observations: 67
Orbital Period · P
2.91 yr
v(q)
36 km/s
v(Q)
12.1 km/s
Diameter · ≈
0.42 km
TJ
3.36
Eccentricity · e
0.4983

Orbit and dynamics

The path is an ellipse reaching 1.023 AU from the Sun at perihelion and 3.054 AU at aphelion, a radial span of 2.031 AU.

Applying Kepler's third law to a = 2.038 AU gives an orbital period of 2.91 yr, or about 1,063 days.

The high eccentricity (0.498) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 42.17° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 36 km/s at perihelion and falls to 12.1 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

The measured diameter is 0.34 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.198 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 67 observations and has a weighted RMS residual of 0.4034 arcseconds.

Condition code U = 1 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
2.038 AU
Eccentricity
0.4983
Perihelion
1.023 AU
Aphelion
3.053535 AU
Inclination
42.17°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
256.34°

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
2044-Oct-06 02:36 0.420994 AU
62979795 km
28.38 km/s
2047-Sep-12 03:46 0.117810 AU
17624123 km
24.12 km/s
2079-Sep-26 23:36 0.210308 AU
31461588 km
25.67 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.343 km
Albedo
0.198
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.63

Orbit Quality

RMS
0.40344
Condition
1
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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