SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 BT4

2015 BT4

2015 BT4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.464 AU it takes 1.77 yr to circle the Sun.

Apollo Observations: 64
Orbital Period · P
1.77 yr
v(q)
52.2 km/s
v(Q)
11.6 km/s
Diameter · ≈
0.18 km
TJ
4.37
Eccentricity · e
0.6366

Orbit and dynamics

The path is an ellipse reaching 0.532 AU from the Sun at perihelion and 2.396 AU at aphelion, a radial span of 1.864 AU.

Applying Kepler's third law to a = 1.464 AU gives an orbital period of 1.77 yr, or about 647 days.

The high eccentricity (0.637) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.22° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 52.2 km/s at perihelion and falls to 11.6 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 = 21.48 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.18 km.

Observation record and orbit quality

The current orbit solution is based on 64 observations and has a weighted RMS residual of 0.511 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
1.464 AU
Eccentricity
0.6366
Perihelion
0.532 AU
Aphelion
2.395982 AU
Inclination
6.22°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
182.71°

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
2030-Nov-21 12:59 0.427255 AU
63916470 km
19.26 km/s
2032-Jun-26 08:11 0.225962 AU
33803397 km
25.98 km/s
2038-Jan-27 02:51 0.071634 AU
10716312 km
19.26 km/s
2039-Aug-06 17:33 0.308068 AU
46086358 km
13.09 km/s
2045-Feb-20 02:45 0.497904 AU
74485310 km
35.21 km/s
2046-Oct-12 17:23 0.465906 AU
69698497 km
22.50 km/s
2053-Dec-10 15:30 0.373719 AU
55907499 km
15.34 km/s
2055-Jul-04 11:52 0.114504 AU
17129539 km
21.75 km/s
2061-Feb-03 00:57 0.139970 AU
20939222 km
23.74 km/s
2062-Aug-31 16:05 0.390478 AU
58414686 km
16.84 km/s
2069-Oct-27 03:17 0.464609 AU
69504528 km
22.40 km/s
2071-Jun-16 06:11 0.441048 AU
65979893 km
32.84 km/s
2077-Jan-09 03:48 0.282976 AU
42332680 km
11.82 km/s
2078-Jul-11 01:58 0.114022 AU
17057463 km
18.21 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
21.48

Orbit Quality

RMS
0.51101
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.