SpaceAtlas Space Object Data
NASA JPL SBDB · 613910

613910

613910 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.77 AU it takes 2.35 yr to circle the Sun.

Apollo Observations: 81
Orbital Period · P
2.35 yr
v(q)
50.8 km/s
v(Q)
9.9 km/s
Diameter · ≈
0.54 km
TJ
3.75
Eccentricity · e
0.6752

Orbit and dynamics

Between its closest point (0.575 AU) and its farthest (2.965 AU), the heliocentric distance changes by 2.39 AU over every revolution.

One full revolution takes 2.35 yr (860 days), computed from the semi-major axis of 1.77 AU.

The high eccentricity (0.675) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 18.98° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 50.8 km/s at perihelion and falls to 9.9 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 = 19.11 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.54 km.

Observation record and orbit quality

Astrometry from 81 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6084 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
1.77 AU
Eccentricity
0.6752
Perihelion
0.575 AU
Aphelion
2.965104 AU
Inclination
18.98°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
261.67°

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
2026-Dec-14 14:53 0.410024 AU
61338651 km
30.02 km/s
2029-Jul-21 02:38 0.442030 AU
66126717 km
30.52 km/s
2034-Jan-03 17:36 0.303942 AU
45469059 km
17.74 km/s
2041-Mar-11 22:42 0.441579 AU
66059342 km
22.33 km/s
2048-Apr-27 14:05 0.401864 AU
60118009 km
23.00 km/s
2055-Jun-19 11:17 0.294370 AU
44037087 km
20.23 km/s
2059-Dec-15 23:05 0.413931 AU
61923235 km
29.86 km/s
2062-Jul-23 11:36 0.474152 AU
70932182 km
31.54 km/s
2067-Jan-12 07:38 0.343350 AU
51364498 km
15.13 km/s
2074-Mar-28 08:24 0.435073 AU
65086004 km
23.56 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
19.11

Orbit Quality

RMS
0.60839
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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