SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 RF36

2015 RF36

2015 RF36 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.949 AU and a period of 0.92 yr.

Aten Observations: 346
Orbital Period · P
0.92 yr
v(q)
34.5 km/s
v(Q)
27.1 km/s
Diameter · ≈
0.07 km
TJ
6.32
Eccentricity · e
0.1187

Orbit and dynamics

Between its closest point (0.836 AU) and its farthest (1.062 AU), the heliocentric distance changes by 0.226 AU over every revolution.

One full revolution takes 0.92 yr (338 days), computed from the semi-major axis of 0.949 AU.

An eccentricity of 0.119 makes the orbit moderately elongated.

The orbital plane is tilted 7.25° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 34.5 km/s at perihelion and falls to 27.1 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 = 23.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

Astrometry from 346 individual observations underpins this orbit; the fit leaves an RMS residual of 0.2226 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
0.9492 AU
Eccentricity
0.1187
Perihelion
0.836 AU
Aphelion
1.06187 AU
Inclination
7.25°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
64.67°

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-Jun-03 03:18 0.129774 AU
19413939 km
3.63 km/s
2027-Aug-20 07:39 0.105131 AU
15727334 km
4.26 km/s
2028-Jan-23 18:39 0.168723 AU
25240645 km
4.63 km/s
2040-Mar-11 05:03 0.152453 AU
22806622 km
5.77 km/s
2040-Oct-14 12:52 0.109053 AU
16314033 km
6.61 km/s
2052-Apr-11 02:40 0.137516 AU
20572096 km
5.36 km/s
2052-Oct-02 01:47 0.034420 AU
5149207 km
4.41 km/s
2064-Apr-30 03:38 0.131561 AU
19681250 km
4.79 km/s
2064-Sep-15 06:49 0.059063 AU
8835721 km
4.20 km/s
2076-Aug-17 02:45 0.101420 AU
15172183 km
4.24 km/s
2077-Jan-22 08:15 0.168556 AU
25215553 km
4.60 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
23.4

Orbit Quality

RMS
0.22265
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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