SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 JP

2015 JP

2015 JP is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.306 AU once every 1.49 yr.

Amor Observations: 151
Orbital Period · P
1.49 yr
v(q)
31.2 km/s
v(Q)
21.8 km/s
Diameter · ≈
0.1 km
TJ
4.91
Eccentricity · e
0.177

Orbit and dynamics

The path is an ellipse reaching 1.075 AU from the Sun at perihelion and 1.537 AU at aphelion, a radial span of 0.462 AU.

Applying Kepler's third law to a = 1.306 AU gives an orbital period of 1.49 yr, or about 545 days.

An eccentricity of 0.177 makes the orbit moderately elongated.

The orbital plane is tilted 19.95° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 31.2 km/s at perihelion and falls to 21.8 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 22.78 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 151 observations and has a weighted RMS residual of 0.4965 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
1.306 AU
Eccentricity
0.177
Perihelion
1.075 AU
Aphelion
1.537162 AU
Inclination
19.95°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
131.42°

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 14:46 0.285203 AU
42665718 km
14.36 km/s
2027-Sep-19 19:11 0.408918 AU
61173321 km
9.43 km/s
2030-Apr-27 06:27 0.372091 AU
55663965 km
16.13 km/s
2030-Sep-26 22:25 0.412252 AU
61672052 km
10.02 km/s
2033-Apr-24 17:07 0.462028 AU
69118437 km
18.09 km/s
2033-Oct-03 02:38 0.419279 AU
62723231 km
10.45 km/s
2036-Oct-08 21:18 0.430154 AU
64350098 km
10.80 km/s
2039-Oct-15 05:56 0.443763 AU
66386050 km
11.11 km/s
2042-Oct-20 08:35 0.460117 AU
68832453 km
11.35 km/s
2045-Oct-25 08:55 0.477933 AU
71497817 km
11.53 km/s
2048-Oct-30 08:13 0.497012 AU
74351925 km
11.69 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
22.78

Orbit Quality

RMS
0.49646
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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