SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 FB8

2013 FB8

2013 FB8 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.341 AU it takes 1.55 yr to circle the Sun.

Apollo Observations: 176
Orbital Period · P
1.55 yr
v(q)
35.8 km/s
v(Q)
18.5 km/s
Diameter · ≈
0.04 km
TJ
4.84
Eccentricity · e
0.3185

Orbit and dynamics

The path is an ellipse reaching 0.914 AU from the Sun at perihelion and 1.768 AU at aphelion, a radial span of 0.854 AU.

Applying Kepler's third law to a = 1.341 AU gives an orbital period of 1.55 yr, or about 567 days.

An eccentricity of 0.319 makes the orbit moderately elongated.

Its inclination of 2.14° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.8 km/s at perihelion and falls to 18.5 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 = 24.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 176 observations and has a weighted RMS residual of 0.3252 arcseconds.

Condition code U = 3 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.341 AU
Eccentricity
0.3185
Perihelion
0.914 AU
Aphelion
1.768108 AU
Inclination
2.14°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
153.97°

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
2027-Mar-15 08:56 0.196987 AU
29468822 km
13.62 km/s
2030-Feb-08 03:40 0.437283 AU
65416647 km
6.33 km/s
2030-Jul-24 17:50 0.078553 AU
11751430 km
9.73 km/s
2041-Mar-07 11:51 0.340794 AU
50981984 km
17.91 km/s
2044-Feb-27 09:43 0.350876 AU
52490317 km
3.88 km/s
2044-Jul-05 10:24 0.059582 AU
8913270 km
6.47 km/s
2058-May-08 06:00 0.093175 AU
13938725 km
6.36 km/s
2061-Aug-14 05:15 0.417965 AU
62526605 km
19.93 km/s
2072-Mar-28 09:49 0.022708 AU
3397120 km
8.35 km/s
2072-Aug-30 23:09 0.405257 AU
60625597 km
5.39 km/s
2075-Jan-29 21:14 0.494402 AU
73961418 km
7.49 km/s
2075-Aug-02 07:33 0.177433 AU
26543647 km
12.82 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
24.9

Orbit Quality

RMS
0.32519
Condition
3
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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