SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 BP4

2015 BP4

2015 BP4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.339 AU it takes 1.55 yr to circle the Sun.

Apollo Observations: 44
Orbital Period · P
1.55 yr
v(q)
39.5 km/s
v(Q)
16.8 km/s
Diameter · ≈
0.07 km
TJ
4.79
Eccentricity · e
0.4039

Orbit and dynamics

The path is an ellipse reaching 0.798 AU from the Sun at perihelion and 1.88 AU at aphelion, a radial span of 1.082 AU.

Applying Kepler's third law to a = 1.339 AU gives an orbital period of 1.55 yr, or about 566 days.

The high eccentricity (0.404) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 12.66° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.5 km/s at perihelion and falls to 16.8 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 = 23.4 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 44 observations and has a weighted RMS residual of 0.3543 arcseconds.

Condition code U = 2 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
1.339 AU
Eccentricity
0.4039
Perihelion
0.798 AU
Aphelion
1.879822 AU
Inclination
12.66°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
73.76°

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-Jan-27 16:20 0.304483 AU
45550073 km
21.01 km/s
2032-Feb-02 14:27 0.352789 AU
52776522 km
7.79 km/s
2032-Apr-20 18:45 0.284796 AU
42604826 km
9.87 km/s
2032-Jul-29 11:36 0.458119 AU
68533680 km
7.07 km/s
2035-Jul-26 18:01 0.164614 AU
24625837 km
17.34 km/s
2046-Feb-08 13:33 0.097678 AU
14612442 km
13.37 km/s
2049-Jun-29 11:27 0.170810 AU
25552800 km
9.28 km/s
2052-Aug-08 04:57 0.430571 AU
64412550 km
24.77 km/s
2060-Jan-25 05:44 0.382003 AU
57146792 km
23.36 km/s
2063-Mar-29 00:20 0.265669 AU
39743537 km
8.63 km/s
2066-Jul-22 13:26 0.087858 AU
13143394 km
15.30 km/s
2077-Feb-06 07:24 0.119509 AU
17878252 km
14.81 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
23.4

Orbit Quality

RMS
0.35427
Condition
2
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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