SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 NK3

2015 NK3

2015 NK3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.108 AU it takes 1.17 yr to circle the Sun.

Apollo Observations: 90
Orbital Period · P
1.17 yr
v(q)
40.9 km/s
v(Q)
19.6 km/s
Diameter · ≈
0.2 km
TJ
5.46
Eccentricity · e
0.3516

Orbit and dynamics

Between its closest point (0.718 AU) and its farthest (1.498 AU), the heliocentric distance changes by 0.78 AU over every revolution.

One full revolution takes 1.17 yr (426 days), computed from the semi-major axis of 1.108 AU.

An eccentricity of 0.352 makes the orbit moderately elongated.

A steep inclination of 28.42° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.9 km/s at perihelion and falls to 19.6 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 = 21.27 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

Astrometry from 90 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5125 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
1.108 AU
Eccentricity
0.3516
Perihelion
0.718 AU
Aphelion
1.497573 AU
Inclination
28.42°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
359.05°

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-Aug-17 09:29 0.284679 AU
42587399 km
14.73 km/s
2029-Dec-05 21:42 0.465649 AU
69660083 km
15.86 km/s
2031-Mar-20 08:39 0.433821 AU
64898763 km
25.42 km/s
2036-Aug-17 20:52 0.274667 AU
41089656 km
14.80 km/s
2036-Dec-01 05:47 0.472619 AU
70702789 km
15.10 km/s
2038-Mar-18 21:03 0.418280 AU
62573826 km
25.03 km/s
2043-Aug-19 06:32 0.265140 AU
39664394 km
14.84 km/s
2043-Nov-26 15:24 0.478327 AU
71556751 km
13.99 km/s
2045-Mar-17 07:10 0.402839 AU
60263840 km
24.64 km/s
2050-Aug-19 14:36 0.256421 AU
38360069 km
14.93 km/s
2050-Nov-18 11:42 0.481860 AU
72085286 km
12.03 km/s
2052-Mar-15 22:56 0.389660 AU
58292341 km
24.31 km/s
2057-Aug-19 17:01 0.252232 AU
37733444 km
14.96 km/s
2059-Mar-16 01:48 0.382502 AU
57221439 km
24.15 km/s
2064-Aug-19 16:55 0.248108 AU
37116473 km
15.00 km/s
2066-Mar-15 04:14 0.374749 AU
56061627 km
23.95 km/s
2071-Aug-20 18:48 0.243811 AU
36473560 km
15.06 km/s
2073-Mar-14 07:14 0.367555 AU
54985390 km
23.78 km/s
2078-Aug-20 17:31 0.241183 AU
36080489 km
15.07 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
21.27

Orbit Quality

RMS
0.51248
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.