SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 RS83

2015 RS83

2015 RS83 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.796 AU it takes 4.68 yr to circle the Sun.

Apollo Observations: 49
Orbital Period · P
4.68 yr
v(q)
48.9 km/s
v(Q)
6.5 km/s
Diameter · ≈
0.49 km
TJ
2.79
Eccentricity · e
0.7656

Orbit and dynamics

The path is an ellipse reaching 0.655 AU from the Sun at perihelion and 4.937 AU at aphelion, a radial span of 4.282 AU.

Applying Kepler's third law to a = 2.796 AU gives an orbital period of 4.68 yr, or about 1,708 days.

The high eccentricity (0.766) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 11.64° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 48.9 km/s at perihelion and falls to 6.5 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

The measured diameter is 0.47 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.137 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 49 observations and has a weighted RMS residual of 0.328 arcseconds.

Condition code U = 0 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
2.796 AU
Eccentricity
0.7656
Perihelion
0.655 AU
Aphelion
4.936618 AU
Inclination
11.64°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
95.66°

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
2078-Feb-28 02:35 0.173687 AU
25983219 km
17.17 km/s

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

Physical Parameters

Diameter
0.474 km
Albedo
0.137
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.3

Orbit Quality

RMS
0.328
Condition
0
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.