SpaceAtlas Space Object Data
NASA JPL SBDB · 859716

859716

859716 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.369 AU it takes 1.60 yr to circle the Sun.

Apollo Observations: 186
Orbital Period · P
1.60 yr
v(q)
46.2 km/s
v(Q)
14 km/s
Diameter · ≈
0.22 km
TJ
4.59
Eccentricity · e
0.5339

Orbit and dynamics

The path is an ellipse reaching 0.638 AU from the Sun at perihelion and 2.1 AU at aphelion, a radial span of 1.462 AU.

Applying Kepler's third law to a = 1.369 AU gives an orbital period of 1.60 yr, or about 585 days.

The high eccentricity (0.534) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 25.13° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 46.2 km/s at perihelion and falls to 14 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 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.22 km.

Observation record and orbit quality

The current orbit solution is based on 186 observations and has a weighted RMS residual of 0.4784 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
1.369 AU
Eccentricity
0.5339
Perihelion
0.638 AU
Aphelion
2.099909 AU
Inclination
25.13°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
22.83°

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-Sep-11 17:27 0.099648 AU
14907135 km
18.65 km/s
2034-Mar-15 14:07 0.092519 AU
13840637 km
19.40 km/s
2037-Sep-12 23:31 0.070722 AU
10579921 km
19.33 km/s
2042-Mar-17 00:58 0.114619 AU
17146758 km
18.86 km/s
2045-Sep-13 20:44 0.051662 AU
7728563 km
19.82 km/s
2050-Mar-17 20:06 0.126460 AU
18918108 km
18.58 km/s
2053-Sep-14 02:30 0.046652 AU
6978987 km
19.96 km/s
2058-Mar-17 14:30 0.122729 AU
18359931 km
18.67 km/s
2061-Sep-13 17:53 0.053646 AU
8025288 km
19.75 km/s
2066-Mar-16 12:26 0.107203 AU
16037370 km
19.03 km/s
2069-Sep-12 18:23 0.074659 AU
11168777 km
19.21 km/s
2074-Mar-14 21:55 0.083664 AU
12516000 km
19.62 km/s
2077-Sep-11 11:14 0.104386 AU
15615959 km
18.52 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
21.0

Orbit Quality

RMS
0.47837
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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