SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 OV

2015 OV

2015 OV belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.122 AU it takes 1.19 yr to circle the Sun.

Apollo Observations: 50
Orbital Period · P
1.19 yr
v(q)
33.2 km/s
v(Q)
23.8 km/s
Diameter · ≈
0.07 km
TJ
5.55
Eccentricity · e
0.1654

Orbit and dynamics

The path is an ellipse reaching 0.936 AU from the Sun at perihelion and 1.308 AU at aphelion, a radial span of 0.372 AU.

Applying Kepler's third law to a = 1.122 AU gives an orbital period of 1.19 yr, or about 434 days.

An eccentricity of 0.165 makes the orbit moderately elongated.

The orbital plane is tilted 7.65° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.2 km/s at perihelion and falls to 23.8 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 = 23.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

The current orbit solution is based on 50 observations and has a weighted RMS residual of 0.6798 arcseconds.

Condition code U = 3 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
1.122 AU
Eccentricity
0.1654
Perihelion
0.936 AU
Aphelion
1.307579 AU
Inclination
7.65°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
334.19°

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
2028-Jun-18 10:50 0.286944 AU
42926188 km
5.14 km/s
2029-Jan-17 02:49 0.186454 AU
27893085 km
10.06 km/s
2034-Aug-25 19:09 0.064400 AU
9634060 km
4.89 km/s
2035-Feb-09 02:21 0.175682 AU
26281657 km
4.64 km/s
2040-Aug-14 02:09 0.304080 AU
45489688 km
13.40 km/s
2041-Apr-08 01:07 0.317792 AU
47541004 km
5.72 km/s
2047-May-27 23:17 0.322884 AU
48302764 km
5.54 km/s
2048-Jan-23 01:42 0.323600 AU
48409815 km
14.13 km/s
2053-Jul-30 22:56 0.182840 AU
27352425 km
4.28 km/s
2054-Jan-15 02:37 0.071607 AU
10712212 km
5.13 km/s
2059-Aug-21 05:42 0.155099 AU
23202469 km
9.24 km/s
2060-Mar-15 15:23 0.273426 AU
40903895 km
5.40 km/s
2066-May-07 08:08 0.335781 AU
50232052 km
5.72 km/s
2067-Jan-28 18:39 0.463233 AU
69298670 km
18.28 km/s
2072-Jul-02 03:01 0.256190 AU
38325514 km
4.86 km/s
2073-Jan-15 00:45 0.117035 AU
17508178 km
8.05 km/s
2078-Aug-25 14:45 0.052772 AU
7894518 km
5.89 km/s
2079-Feb-20 07:30 0.207787 AU
31084566 km
4.86 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
23.6

Orbit Quality

RMS
0.67983
Condition
3
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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