SpaceAtlas Space Object Data
NASA JPL SBDB · 395143

395143

395143 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.499 AU it takes 1.84 yr to circle the Sun.

Apollo Observations: 183
Orbital Period · P
1.84 yr
v(q)
39 km/s
v(Q)
15.2 km/s
Diameter · ≈
0.58 km
TJ
4.37
Eccentricity · e
0.4389

Orbit and dynamics

The path is an ellipse reaching 0.841 AU from the Sun at perihelion and 2.157 AU at aphelion, a radial span of 1.316 AU.

Applying Kepler's third law to a = 1.499 AU gives an orbital period of 1.84 yr, or about 670 days.

The high eccentricity (0.439) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 20.97° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39 km/s at perihelion and falls to 15.2 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 0.64 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.124 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 183 observations and has a weighted RMS residual of 0.593 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
1.499 AU
Eccentricity
0.4389
Perihelion
0.841 AU
Aphelion
2.156911 AU
Inclination
20.97°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
357.88°

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
2066-Oct-03 09:48 0.199760 AU
29883700 km
16.25 km/s
2077-Oct-08 16:35 0.176673 AU
26429952 km
15.86 km/s

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

Physical Parameters

Diameter
0.636 km
Albedo
0.124
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
18.95

Orbit Quality

RMS
0.59296
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.

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