SpaceAtlas Space Object Data
NASA JPL SBDB · 2008 QB

2008 QB

2008 QB belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.206 AU it takes 1.32 yr to circle the Sun.

Apollo Observations: 85
Orbital Period · P
1.32 yr
v(q)
70 km/s
v(Q)
10.5 km/s
Diameter · ≈
0.25 km
TJ
4.84
Eccentricity · e
0.7389

Orbit and dynamics

Between its closest point (0.315 AU) and its farthest (2.097 AU), the heliocentric distance changes by 1.782 AU over every revolution.

One full revolution takes 1.32 yr (484 days), computed from the semi-major axis of 1.206 AU.

The high eccentricity (0.739) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 35.77° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 70 km/s at perihelion and falls to 10.5 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 = 20.79 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.25 km.

Observation record and orbit quality

Astrometry from 85 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3242 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
1.206 AU
Eccentricity
0.7389
Perihelion
0.315 AU
Aphelion
2.097113 AU
Inclination
35.77°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
114.11°

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
2049-Aug-30 21:05 0.420760 AU
62944875 km
20.61 km/s
2053-Aug-30 20:11 0.278281 AU
41630228 km
22.50 km/s
2057-Aug-27 22:11 0.138058 AU
20653201 km
25.43 km/s
2061-Aug-23 06:53 0.060459 AU
9044509 km
28.96 km/s
2065-Aug-17 11:49 0.179561 AU
26861885 km
33.01 km/s
2069-Aug-10 23:33 0.325069 AU
48629660 km
37.38 km/s
2073-Aug-04 02:10 0.468836 AU
70136819 km
41.90 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
20.79

Orbit Quality

RMS
0.32421
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.