SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 GK135

2016 GK135

2016 GK135 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.985 AU and a period of 0.98 yr.

Aten Observations: 23
Orbital Period · P
0.98 yr
v(q)
32.7 km/s
v(Q)
27.5 km/s
Diameter · ≈
0.01 km
TJ
6.15
Eccentricity · e
0.0869

Orbit and dynamics

Between its closest point (0.9 AU) and its farthest (1.071 AU), the heliocentric distance changes by 0.171 AU over every revolution.

One full revolution takes 0.98 yr (357 days), computed from the semi-major axis of 0.985 AU.

With e = 0.087, the orbit is close to circular.

Its inclination of 3.2° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.7 km/s at perihelion and falls to 27.5 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 = 28.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 23 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3708 arcseconds.

Condition code U = 5 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
0.9852 AU
Eccentricity
0.0869
Perihelion
0.9 AU
Aphelion
1.070814 AU
Inclination
3.2°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
254.4°

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
2058-Apr-03 07:27 0.408303 AU
61081290 km
14.54 km/s
2059-Mar-28 06:33 0.273952 AU
40982683 km
10.53 km/s
2060-Mar-21 23:21 0.140665 AU
21043245 km
6.57 km/s
2061-Mar-21 20:14 0.021625 AU
3234982 km
3.03 km/s
2062-Jan-29 10:50 0.079405 AU
11878751 km
1.55 km/s
2062-Apr-24 00:18 0.056121 AU
8395634 km
2.22 km/s
2062-Nov-24 01:03 0.089055 AU
13322368 km
2.70 km/s
2063-Jun-26 12:40 0.078014 AU
11670654 km
1.84 km/s
2063-Oct-06 10:28 0.060731 AU
9085260 km
2.47 km/s
2064-Aug-26 19:43 0.045973 AU
6877484 km
3.11 km/s
2065-Aug-14 22:20 0.133198 AU
19926117 km
6.01 km/s
2066-Aug-07 23:06 0.242305 AU
36248342 km
9.31 km/s
2067-Aug-02 00:47 0.355488 AU
53180268 km
12.70 km/s
2068-Jul-26 12:07 0.469007 AU
70162508 km
16.10 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
28.1

Orbit Quality

RMS
0.37079
Condition
5
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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