SpaceAtlas Space Object Data
NASA JPL SBDB · 2009 HE

2009 HE

2009 HE belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.3 AU it takes 1.48 yr to circle the Sun.

Apollo Observations: 61
Orbital Period · P
1.48 yr
v(q)
39.9 km/s
v(Q)
17.1 km/s
Diameter · ≈
0.22 km
TJ
4.66
Eccentricity · e
0.4003

Orbit and dynamics

Between its closest point (0.78 AU) and its farthest (1.82 AU), the heliocentric distance changes by 1.04 AU over every revolution.

One full revolution takes 1.48 yr (541 days), computed from the semi-major axis of 1.3 AU.

The high eccentricity (0.4) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 44.39° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.9 km/s at perihelion and falls to 17.1 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 = 21.03 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.22 km.

Observation record and orbit quality

Astrometry from 61 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4119 arcseconds.

Condition code U = 1 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
1.3 AU
Eccentricity
0.4003
Perihelion
0.78 AU
Aphelion
1.82039 AU
Inclination
44.39°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
137.64°

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-Nov-02 18:03 0.363214 AU
54335999 km
32.44 km/s
2040-Oct-23 17:10 0.171925 AU
25719606 km
28.70 km/s
2043-Oct-14 11:48 0.084229 AU
12600490 km
25.89 km/s
2046-Oct-03 18:47 0.257093 AU
38460631 km
24.30 km/s
2049-Apr-20 08:21 0.387047 AU
57901405 km
21.44 km/s
2049-Sep-22 00:50 0.455119 AU
68084880 km
24.12 km/s
2052-Apr-20 12:28 0.294722 AU
44089718 km
22.66 km/s
2055-Apr-19 16:02 0.285490 AU
42708685 km
24.83 km/s
2058-Apr-15 20:57 0.376098 AU
56263458 km
27.97 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
21.03

Orbit Quality

RMS
0.41191
Condition
1
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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