SpaceAtlas Space Object Data
NASA JPL SBDB · 387505

387505

387505 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.542 AU it takes 1.91 yr to circle the Sun.

Apollo Observations: 1,501
Orbital Period · P
1.91 yr
v(q)
92.3 km/s
v(Q)
6.2 km/s
Diameter · ≈
0.62 km
TJ
3.91
Eccentricity · e
0.8733

Orbit and dynamics

The path is an ellipse reaching 0.195 AU from the Sun at perihelion and 2.889 AU at aphelion, a radial span of 2.694 AU.

Applying Kepler's third law to a = 1.542 AU gives an orbital period of 1.91 yr, or about 699 days.

The high eccentricity (0.873) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.29° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 92.3 km/s at perihelion and falls to 6.2 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

The measured diameter is 1.06 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.074 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

The current orbit solution is based on 1,501 observations and has a weighted RMS residual of 0.2631 arcseconds.

Condition code U = 0 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
1.542 AU
Eccentricity
0.8733
Perihelion
0.195 AU
Aphelion
2.888629 AU
Inclination
2.29°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
197.61°

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
2031-Mar-21 03:09 0.422758 AU
63243766 km
45.21 km/s
2033-Feb-26 22:59 0.064813 AU
9695928 km
29.81 km/s
2044-Jun-01 16:14 0.100783 AU
15076973 km
29.07 km/s
2046-May-12 00:10 0.380171 AU
56872771 km
43.79 km/s
2054-Mar-15 20:10 0.315656 AU
47221509 km
41.60 km/s
2056-Feb-23 14:20 0.180734 AU
27037365 km
26.49 km/s
2065-Jun-11 17:35 0.490315 AU
73350051 km
19.79 km/s
2067-May-29 10:33 0.036497 AU
5459869 km
32.07 km/s
2069-May-06 20:37 0.479657 AU
71755655 km
47.26 km/s
2077-Mar-09 15:25 0.181938 AU
27217503 km
37.24 km/s
2079-Feb-19 11:18 0.327321 AU
48966547 km
22.72 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
1.06 km
Albedo
0.074
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
18.78

Orbit Quality

RMS
0.26308
Condition
0
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

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