SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 RE83

2015 RE83

2015 RE83 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.207 AU it takes 1.33 yr to circle the Sun.

Apollo Observations: 38
Orbital Period · P
1.33 yr
v(q)
33.1 km/s
v(Q)
22.2 km/s
Diameter · ≈
0.12 km
TJ
5.22
Eccentricity · e
0.1968

Orbit and dynamics

The path is an ellipse reaching 0.969 AU from the Sun at perihelion and 1.445 AU at aphelion, a radial span of 0.476 AU.

Applying Kepler's third law to a = 1.207 AU gives an orbital period of 1.33 yr, or about 484 days.

An eccentricity of 0.197 makes the orbit moderately elongated.

The orbital plane is tilted 15.16° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.1 km/s at perihelion and falls to 22.2 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

No direct size measurement is available; from an absolute magnitude of H = 22.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

The current orbit solution is based on 38 observations and has a weighted RMS residual of 0.5864 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
1.207 AU
Eccentricity
0.1968
Perihelion
0.969 AU
Aphelion
1.444538 AU
Inclination
15.16°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
228.15°

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
2027-Sep-20 20:08 0.421236 AU
63016058 km
9.51 km/s
2031-Sep-30 23:35 0.411980 AU
61631364 km
9.03 km/s
2035-Oct-12 11:05 0.400198 AU
59868737 km
8.28 km/s
2036-Apr-08 13:41 0.384091 AU
57459236 km
15.10 km/s
2039-Oct-27 00:46 0.384470 AU
57515895 km
7.01 km/s
2040-Mar-27 00:35 0.261082 AU
39057304 km
12.15 km/s
2044-Mar-13 23:11 0.144714 AU
21648866 km
9.98 km/s
2048-Mar-01 20:41 0.044124 AU
6600807 km
8.94 km/s
2052-Feb-22 20:41 0.034735 AU
5196232 km
8.89 km/s
2056-Feb-10 07:33 0.139950 AU
20936293 km
9.87 km/s
2060-Jan-28 04:47 0.262817 AU
39316848 km
12.19 km/s
2060-Jun-26 05:44 0.396539 AU
59321426 km
6.47 km/s
2064-Jan-15 16:16 0.393818 AU
58914358 km
15.44 km/s
2064-Jul-12 23:59 0.413254 AU
61821847 km
8.00 km/s
2068-Jul-25 13:50 0.423881 AU
63411674 km
8.86 km/s
2072-Aug-05 10:17 0.430329 AU
64376245 km
9.40 km/s
2076-Aug-15 07:46 0.433671 AU
64876298 km
9.72 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
22.4

Orbit Quality

RMS
0.58641
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.

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