SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 HK

2015 HK

2015 HK is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.872 AU and a period of 0.81 yr.

Aten Observations: 45
Orbital Period · P
0.81 yr
v(q)
41 km/s
v(Q)
24.8 km/s
Diameter · ≈
0.03 km
TJ
6.74
Eccentricity · e
0.2462

Orbit and dynamics

The path is an ellipse reaching 0.658 AU from the Sun at perihelion and 1.087 AU at aphelion, a radial span of 0.429 AU.

Applying Kepler's third law to a = 0.872 AU gives an orbital period of 0.81 yr, or about 298 days.

An eccentricity of 0.246 makes the orbit moderately elongated.

The orbital plane is tilted 12.49° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 41 km/s at perihelion and falls to 24.8 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 = 25.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 45 observations and has a weighted RMS residual of 0.4086 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.8724 AU
Eccentricity
0.2462
Perihelion
0.658 AU
Aphelion
1.087185 AU
Inclination
12.49°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
98.93°

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
2032-Feb-17 01:33 0.371925 AU
55639217 km
18.76 km/s
2033-Apr-25 16:10 0.280201 AU
41917499 km
18.35 km/s
2041-Feb-09 13:13 0.223129 AU
33379671 km
13.29 km/s
2046-May-01 09:19 0.033960 AU
5080383 km
10.40 km/s
2055-Apr-28 00:27 0.176200 AU
26359149 km
16.48 km/s
2063-Feb-11 04:46 0.261596 AU
39134278 km
14.15 km/s
2064-Apr-20 11:25 0.423534 AU
63359852 km
22.60 km/s
2067-Nov-07 05:37 0.292872 AU
43813091 km
11.88 km/s
2068-Apr-30 11:10 0.031597 AU
4726846 km
9.50 km/s
2072-Feb-11 15:31 0.214660 AU
32112723 km
8.26 km/s
2072-Aug-09 08:41 0.358328 AU
53605079 km
9.65 km/s
2076-Oct-09 19:24 0.340635 AU
50958224 km
13.15 km/s
2077-Apr-28 22:03 0.229871 AU
34388185 km
15.03 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
25.5

Orbit Quality

RMS
0.40856
Condition
7
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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