SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 OF26

2015 OF26

2015 OF26 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.343 AU it takes 1.56 yr to circle the Sun.

Apollo Observations: 74
Orbital Period · P
1.56 yr
v(q)
47.1 km/s
v(Q)
14 km/s
Diameter · ≈
0.16 km
TJ
4.72
Eccentricity · e
0.5413

Orbit and dynamics

The path is an ellipse reaching 0.616 AU from the Sun at perihelion and 2.07 AU at aphelion, a radial span of 1.454 AU.

Applying Kepler's third law to a = 1.343 AU gives an orbital period of 1.56 yr, or about 568 days.

The high eccentricity (0.541) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 8.69° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 47.1 km/s at perihelion and falls to 14 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 = 21.71 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.16 km.

Observation record and orbit quality

The current orbit solution is based on 74 observations and has a weighted RMS residual of 0.3681 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
1.343 AU
Eccentricity
0.5413
Perihelion
0.616 AU
Aphelion
2.069966 AU
Inclination
8.69°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
302.79°

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
2029-Aug-21 21:56 0.113061 AU
16913642 km
14.84 km/s
2032-Dec-03 06:36 0.374579 AU
56036268 km
17.35 km/s
2036-Mar-01 11:46 0.145946 AU
21833165 km
19.10 km/s
2043-Aug-27 09:24 0.173473 AU
25951133 km
12.33 km/s
2046-Dec-14 01:59 0.362165 AU
54179070 km
16.89 km/s
2050-Mar-07 00:07 0.214079 AU
32025806 km
21.76 km/s
2054-Jul-29 02:50 0.464084 AU
69426009 km
29.81 km/s
2057-Sep-12 07:32 0.269048 AU
40248978 km
9.51 km/s
2060-Dec-29 01:05 0.332076 AU
49677806 km
15.46 km/s
2064-Mar-12 15:13 0.319825 AU
47845135 km
25.27 km/s
2068-Aug-02 21:40 0.359966 AU
53850152 km
26.55 km/s
2071-Oct-13 22:21 0.337320 AU
50462386 km
13.32 km/s
2075-Jan-18 12:15 0.276242 AU
41325225 km
13.09 km/s
2078-Mar-20 05:17 0.451627 AU
67562502 km
29.50 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
21.71

Orbit Quality

RMS
0.36813
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.

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