SpaceAtlas Space Object Data
NASA JPL SBDB · 2006 HT30

2006 HT30

2006 HT30 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.56 AU it takes 4.10 yr to circle the Sun.

Apollo Observations: 82
Orbital Period · P
4.10 yr
v(q)
38.5 km/s
v(Q)
9 km/s
Diameter · ≈
0.32 km
TJ
3.13
Eccentricity · e
0.6202

Orbit and dynamics

Between its closest point (0.972 AU) and its farthest (4.148 AU), the heliocentric distance changes by 3.176 AU over every revolution.

One full revolution takes 4.10 yr (1,496 days), computed from the semi-major axis of 2.56 AU.

The high eccentricity (0.62) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.64° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.5 km/s at perihelion and falls to 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 = 20.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.32 km.

Observation record and orbit quality

Astrometry from 82 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6382 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
2.56 AU
Eccentricity
0.6202
Perihelion
0.972 AU
Aphelion
4.147712 AU
Inclination
1.64°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
297.59°

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
2043-May-26 11:25 0.183873 AU
27506956 km
16.71 km/s
2047-Aug-07 14:49 0.052726 AU
7887634 km
9.82 km/s
2051-Sep-23 12:15 0.281406 AU
42097741 km
20.42 km/s
2055-Oct-03 23:54 0.466055 AU
69720802 km
25.97 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
20.2

Orbit Quality

RMS
0.63821
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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