SpaceAtlas Space Object Data
NASA JPL SBDB · 2004 HM

2004 HM

2004 HM belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.331 AU it takes 1.54 yr to circle the Sun.

Apollo Observations: 132
Orbital Period · P
1.54 yr
v(q)
39.9 km/s
v(Q)
16.7 km/s
Diameter · ≈
0.08 km
TJ
4.81
Eccentricity · e
0.4095

Orbit and dynamics

The path is an ellipse reaching 0.786 AU from the Sun at perihelion and 1.876 AU at aphelion, a radial span of 1.09 AU.

Applying Kepler's third law to a = 1.331 AU gives an orbital period of 1.54 yr, or about 561 days.

The high eccentricity (0.409) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 11.57° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.9 km/s at perihelion and falls to 16.7 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 = 23.33 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.08 km.

Observation record and orbit quality

The current orbit solution is based on 132 observations and has a weighted RMS residual of 0.5139 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
1.331 AU
Eccentricity
0.4095
Perihelion
0.786 AU
Aphelion
1.876044 AU
Inclination
11.57°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
186.07°

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-Apr-29 08:37 0.248279 AU
37142026 km
19.17 km/s
2040-Nov-06 13:15 0.151729 AU
22698321 km
15.59 km/s
2043-Nov-04 04:05 0.344002 AU
51461989 km
7.31 km/s
2044-Jan-23 21:31 0.264132 AU
39513580 km
9.69 km/s
2044-Apr-24 01:21 0.431464 AU
64546056 km
6.33 km/s
2047-Apr-17 06:43 0.031138 AU
4658185 km
13.25 km/s
2060-Nov-03 01:29 0.225378 AU
33716037 km
17.98 km/s
2063-Nov-14 03:01 0.299616 AU
44821956 km
6.65 km/s
2064-Jan-11 19:53 0.258621 AU
38689222 km
9.17 km/s
2064-May-06 14:07 0.470772 AU
70426463 km
7.19 km/s
2067-Apr-16 09:54 0.016322 AU
2441667 km
12.89 km/s
2077-Oct-23 00:48 0.475331 AU
71108451 km
25.54 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
23.33

Orbit Quality

RMS
0.51393
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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