SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 BW92

2015 BW92

2015 BW92 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.63 AU once every 4.27 yr.

Amor Observations: 468
Orbital Period · P
4.27 yr
v(q)
35.7 km/s
v(Q)
9.5 km/s
Diameter · ≈
0.61 km
TJ
3.05
Eccentricity · e
0.5807

Orbit and dynamics

The path is an ellipse reaching 1.103 AU from the Sun at perihelion and 4.157 AU at aphelion, a radial span of 3.054 AU.

Applying Kepler's third law to a = 2.63 AU gives an orbital period of 4.27 yr, or about 1,558 days.

The high eccentricity (0.581) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 22.65° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 35.7 km/s at perihelion and falls to 9.5 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 18.81 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.61 km.

Observation record and orbit quality

The current orbit solution is based on 468 observations and has a weighted RMS residual of 0.3254 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
2.63 AU
Eccentricity
0.5807
Perihelion
1.103 AU
Aphelion
4.157241 AU
Inclination
22.65°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
247.88°

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
2032-Feb-03 14:12 0.290053 AU
43391308 km
17.58 km/s
2049-Feb-11 16:02 0.465686 AU
69665586 km
22.32 km/s
2066-Feb-06 17:33 0.338792 AU
50682561 km
19.42 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
18.81

Orbit Quality

RMS
0.32539
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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