SpaceAtlas Space Object Data
NASA JPL SBDB · 2011 OJ45

2011 OJ45

2011 OJ45 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.017 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 21
Orbital Period · P
1.03 yr
v(q)
36.3 km/s
v(Q)
24 km/s
Diameter · ≈
0.02 km
TJ
5.98
Eccentricity · e
0.2035

Orbit and dynamics

The path is an ellipse reaching 0.81 AU from the Sun at perihelion and 1.224 AU at aphelion, a radial span of 0.414 AU.

Applying Kepler's third law to a = 1.017 AU gives an orbital period of 1.03 yr, or about 375 days.

An eccentricity of 0.203 makes the orbit moderately elongated.

Its inclination of 0.75° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36.3 km/s at perihelion and falls to 24 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 = 26 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 21 observations and has a weighted RMS residual of 0.3702 arcseconds.

Condition code U = 6 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
1.017 AU
Eccentricity
0.2035
Perihelion
0.81 AU
Aphelion
1.223959 AU
Inclination
0.75°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
82.84°

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
2049-Jul-29 06:16 0.385452 AU
57662820 km
17.88 km/s
2050-Aug-05 09:26 0.234640 AU
35101624 km
13.40 km/s
2051-Aug-12 12:57 0.083827 AU
12540324 km
8.93 km/s
2052-Aug-17 22:59 0.016249 AU
2430807 km
4.61 km/s
2053-Jul-06 12:16 0.158469 AU
23706620 km
4.37 km/s
2053-Oct-16 06:56 0.149763 AU
22404190 km
5.12 km/s
2054-Jun-04 06:33 0.207413 AU
31028529 km
5.31 km/s
2054-Nov-25 17:50 0.174999 AU
26179446 km
6.11 km/s
2055-May-07 04:17 0.203966 AU
30512849 km
5.24 km/s
2056-Jan-06 14:50 0.138432 AU
20709170 km
4.84 km/s
2056-Apr-02 07:46 0.145265 AU
21731297 km
4.14 km/s
2057-Feb-26 06:48 0.009604 AU
1436682 km
5.42 km/s
2058-Mar-04 09:25 0.094804 AU
14182474 km
9.50 km/s
2059-Mar-10 21:15 0.225832 AU
33783968 km
13.68 km/s
2060-Mar-16 15:00 0.357178 AU
53433078 km
17.86 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
26.0

Orbit Quality

RMS
0.3702
Condition
6
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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