SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 BE92

2015 BE92

2015 BE92 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.973 AU and a period of 0.96 yr.

Aten Observations: 76
Orbital Period · P
0.96 yr
v(q)
36.9 km/s
v(Q)
24.7 km/s
Diameter · ≈
0.01 km
TJ
6.19
Eccentricity · e
0.1973

Orbit and dynamics

The path is an ellipse reaching 0.781 AU from the Sun at perihelion and 1.165 AU at aphelion, a radial span of 0.384 AU.

Applying Kepler's third law to a = 0.973 AU gives an orbital period of 0.96 yr, or about 351 days.

An eccentricity of 0.197 makes the orbit moderately elongated.

Its inclination of 1.04° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36.9 km/s at perihelion and falls to 24.7 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 = 28.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 76 observations and has a weighted RMS residual of 0.4203 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
0.9733 AU
Eccentricity
0.1973
Perihelion
0.781 AU
Aphelion
1.165332 AU
Inclination
1.04°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
215.87°

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
2034-Sep-20 12:28 0.360984 AU
54002399 km
17.09 km/s
2035-Sep-11 05:16 0.120604 AU
18042094 km
9.79 km/s
2036-Sep-25 14:51 0.112975 AU
16900885 km
4.09 km/s
2037-Jun-07 21:36 0.223615 AU
33452271 km
7.08 km/s
2037-Nov-22 02:53 0.177570 AU
26564108 km
5.41 km/s
2038-Apr-22 05:38 0.217062 AU
32472031 km
6.91 km/s
2039-Jan-22 20:28 0.079840 AU
11943910 km
4.10 km/s
2040-Jan-24 09:50 0.160511 AU
24012140 km
11.10 km/s
2041-Jan-13 20:34 0.402061 AU
60147464 km
18.58 km/s
2059-Sep-19 08:37 0.330013 AU
49369303 km
16.15 km/s
2060-Sep-09 12:21 0.099325 AU
14858852 km
9.16 km/s
2061-Sep-28 23:21 0.120501 AU
18026674 km
4.17 km/s
2062-Jun-08 00:41 0.223223 AU
33393633 km
7.08 km/s
2062-Nov-21 16:46 0.179470 AU
26848398 km
5.44 km/s
2063-Apr-24 07:38 0.218262 AU
32651534 km
6.96 km/s
2064-Jan-17 17:57 0.096040 AU
14367319 km
4.04 km/s
2065-Jan-25 00:02 0.132995 AU
19895702 km
10.29 km/s
2066-Jan-15 19:13 0.368604 AU
55142397 km
17.56 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
28.1

Orbit Quality

RMS
0.42032
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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