SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 HP15

2012 HP15

2012 HP15 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.136 AU it takes 1.21 yr to circle the Sun.

Apollo Observations: 46
Orbital Period · P
1.21 yr
v(q)
40.2 km/s
v(Q)
19.4 km/s
Diameter · ≈
0.15 km
TJ
5.34
Eccentricity · e
0.3484

Orbit and dynamics

The path is an ellipse reaching 0.74 AU from the Sun at perihelion and 1.532 AU at aphelion, a radial span of 0.792 AU.

Applying Kepler's third law to a = 1.136 AU gives an orbital period of 1.21 yr, or about 442 days.

An eccentricity of 0.348 makes the orbit moderately elongated.

A steep inclination of 29.51° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.2 km/s at perihelion and falls to 19.4 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 = 21.94 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.15 km.

Observation record and orbit quality

The current orbit solution is based on 46 observations and has a weighted RMS residual of 0.4687 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
1.136 AU
Eccentricity
0.3484
Perihelion
0.74 AU
Aphelion
1.531782 AU
Inclination
29.51°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
162.33°

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
2029-Apr-23 11:21 0.335522 AU
50193430 km
22.07 km/s
2030-Nov-01 18:59 0.202862 AU
30347664 km
21.06 km/s
2035-Apr-25 21:18 0.223711 AU
33466645 km
16.87 km/s
2036-Nov-22 08:29 0.444681 AU
66523385 km
27.19 km/s
2041-Apr-17 10:00 0.352992 AU
52806860 km
15.29 km/s
2041-Aug-25 20:04 0.453228 AU
67801902 km
17.74 km/s
2047-Oct-04 05:13 0.252545 AU
37780123 km
18.45 km/s
2052-Apr-23 00:58 0.347010 AU
51911896 km
22.43 km/s
2053-Oct-31 12:02 0.195726 AU
29280139 km
20.84 km/s
2058-Apr-25 20:45 0.222653 AU
33308448 km
17.06 km/s
2059-Nov-22 03:28 0.429622 AU
64270529 km
26.77 km/s
2064-Apr-17 20:14 0.343604 AU
51402359 km
15.33 km/s
2064-Aug-22 22:50 0.462051 AU
69121875 km
17.55 km/s
2070-Oct-02 19:20 0.260244 AU
38931986 km
18.43 km/s
2075-Apr-23 13:21 0.358391 AU
53614534 km
22.74 km/s
2076-Oct-30 04:30 0.189200 AU
28303875 km
20.64 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
21.94

Orbit Quality

RMS
0.46872
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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