SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 PM

2015 PM

2015 PM belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.308 AU it takes 1.50 yr to circle the Sun.

Apollo Observations: 187
Orbital Period · P
1.50 yr
v(q)
54.9 km/s
v(Q)
12.3 km/s
Diameter · ≈
0.28 km
TJ
4.75
Eccentricity · e
0.6329

Orbit and dynamics

The path is an ellipse reaching 0.48 AU from the Sun at perihelion and 2.136 AU at aphelion, a radial span of 1.656 AU.

Applying Kepler's third law to a = 1.308 AU gives an orbital period of 1.50 yr, or about 546 days.

The high eccentricity (0.633) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.47° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 54.9 km/s at perihelion and falls to 12.3 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 = 20.48 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.28 km.

Observation record and orbit quality

The current orbit solution is based on 187 observations and has a weighted RMS residual of 0.5098 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
1.308 AU
Eccentricity
0.6329
Perihelion
0.48 AU
Aphelion
2.135833 AU
Inclination
7.47°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
42.19°

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-Aug-12 08:27 0.115610 AU
17294998 km
18.20 km/s
2030-Aug-09 05:57 0.095290 AU
14255131 km
19.81 km/s
2033-Aug-06 03:18 0.105955 AU
15850615 km
21.53 km/s
2036-Aug-02 23:17 0.143371 AU
21448062 km
23.30 km/s
2039-Jul-31 15:08 0.196713 AU
29427880 km
25.21 km/s
2042-Jul-28 01:25 0.258614 AU
38688092 km
27.26 km/s
2045-Jul-24 10:48 0.325702 AU
48724398 km
29.39 km/s
2048-Jul-20 20:08 0.392096 AU
58656717 km
31.50 km/s
2051-Jul-18 01:40 0.462799 AU
69233680 km
33.74 km/s
2059-Apr-06 11:50 0.454923 AU
68055494 km
34.04 km/s
2062-Apr-02 17:03 0.379722 AU
56805624 km
31.68 km/s
2065-Mar-29 18:18 0.300430 AU
44943749 km
29.23 km/s
2068-Mar-26 02:18 0.225655 AU
33757459 km
26.93 km/s
2071-Mar-23 08:48 0.148356 AU
22193781 km
24.60 km/s
2074-Mar-19 19:11 0.073978 AU
11066967 km
22.36 km/s
2077-Mar-16 13:20 0.012736 AU
1905256 km
20.35 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
20.48

Orbit Quality

RMS
0.50978
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.