SpaceAtlas Space Object Data
NASA JPL SBDB · 507716

507716

507716 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.535 AU it takes 4.04 yr to circle the Sun.

Apollo Observations: 221
Orbital Period · P
4.04 yr
v(q)
38.6 km/s
v(Q)
9.1 km/s
Diameter · ≈
1.91 km
TJ
2.79
Eccentricity · e
0.6191

Orbit and dynamics

Between its closest point (0.965 AU) and its farthest (4.104 AU), the heliocentric distance changes by 3.139 AU over every revolution.

One full revolution takes 4.04 yr (1,474 days), computed from the semi-major axis of 2.535 AU.

The high eccentricity (0.619) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 47.83° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 38.6 km/s at perihelion and falls to 9.1 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 = 16.35 and an assumed geometric albedo of 0.14, the diameter works out to roughly 1.91 km.

Observation record and orbit quality

Astrometry from 221 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5595 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
2.535 AU
Eccentricity
0.6191
Perihelion
0.965 AU
Aphelion
4.104419 AU
Inclination
47.83°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
105.14°

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
2037-May-05 22:29 0.185935 AU
27815446 km
29.89 km/s
2041-May-11 22:29 0.088325 AU
13213162 km
29.29 km/s
2045-May-18 14:26 0.070512 AU
10548446 km
28.95 km/s
2049-May-23 01:59 0.140253 AU
20981534 km
29.19 km/s
2053-May-23 11:08 0.146205 AU
21871947 km
29.24 km/s
2057-May-25 03:26 0.172133 AU
25750684 km
29.26 km/s
2061-May-24 16:02 0.168716 AU
25239504 km
29.55 km/s
2065-May-18 09:37 0.091130 AU
13632916 km
29.55 km/s
2069-May-13 08:58 0.088237 AU
13200027 km
29.73 km/s
2073-May-05 08:05 0.194288 AU
29065126 km
30.81 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
16.35

Orbit Quality

RMS
0.55946
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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