SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 RK82

2015 RK82

2015 RK82 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.191 AU it takes 1.30 yr to circle the Sun.

Apollo Observations: 91
Orbital Period · P
1.30 yr
v(q)
39.5 km/s
v(Q)
18.9 km/s
Diameter · ≈
0.26 km
TJ
5.25
Eccentricity · e
0.3536

Orbit and dynamics

The path is an ellipse reaching 0.77 AU from the Sun at perihelion and 1.612 AU at aphelion, a radial span of 0.842 AU.

Applying Kepler's third law to a = 1.191 AU gives an orbital period of 1.30 yr, or about 475 days.

An eccentricity of 0.354 makes the orbit moderately elongated.

The orbital plane is tilted 10.19° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.5 km/s at perihelion and falls to 18.9 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 = 20.64 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.26 km.

Observation record and orbit quality

The current orbit solution is based on 91 observations and has a weighted RMS residual of 0.5527 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
1.191 AU
Eccentricity
0.3536
Perihelion
0.77 AU
Aphelion
1.612138 AU
Inclination
10.19°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
259.11°

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-Dec-19 18:23 0.147854 AU
22118712 km
12.22 km/s
2033-Jun-20 10:52 0.407689 AU
60989401 km
21.06 km/s
2037-Apr-05 18:16 0.236962 AU
35449004 km
9.67 km/s
2037-Jun-17 02:31 0.293861 AU
43960965 km
6.52 km/s
2040-Dec-19 21:05 0.144700 AU
21646811 km
12.01 km/s
2046-Jun-20 12:51 0.400231 AU
59873687 km
20.83 km/s
2049-Oct-22 20:23 0.495747 AU
74162758 km
8.93 km/s
2050-Apr-01 14:09 0.238888 AU
35737110 km
9.98 km/s
2050-Jun-21 10:52 0.308371 AU
46131610 km
6.87 km/s
2053-Dec-17 00:27 0.160069 AU
23946052 km
12.91 km/s
2059-Jun-18 10:01 0.352465 AU
52728056 km
19.27 km/s
2062-Oct-29 08:07 0.469347 AU
70213378 km
8.33 km/s
2063-Mar-20 02:24 0.239567 AU
35838754 km
10.65 km/s
2063-Jun-30 21:57 0.349165 AU
52234370 km
7.68 km/s
2066-Dec-10 22:42 0.216559 AU
32396788 km
15.31 km/s
2072-Jun-13 06:27 0.272113 AU
40707557 km
16.45 km/s
2075-Nov-11 01:34 0.419087 AU
62694587 km
6.98 km/s
2076-Mar-01 02:47 0.228907 AU
34243984 km
11.00 km/s
2076-Jul-10 22:15 0.403835 AU
60412817 km
8.63 km/s
2079-Dec-04 02:48 0.314867 AU
47103387 km
18.70 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
20.64

Orbit Quality

RMS
0.55269
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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