SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 GH135

2016 GH135

2016 GH135 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: 142
Orbital Period · P
0.98 yr
v(q)
34.7 km/s
v(Q)
25.9 km/s
Diameter · ≈
0.14 km
TJ
6.09
Eccentricity · e
0.1445

Orbit and dynamics

Between its closest point (0.843 AU) and its farthest (1.127 AU), the heliocentric distance changes by 0.284 AU over every revolution.

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

An eccentricity of 0.144 makes the orbit moderately elongated.

A steep inclination of 20.99° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 34.7 km/s at perihelion and falls to 25.9 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 = 22.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.14 km.

Observation record and orbit quality

Astrometry from 142 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4885 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
0.985 AU
Eccentricity
0.1445
Perihelion
0.843 AU
Aphelion
1.127333 AU
Inclination
20.99°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
260.48°

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
2057-Apr-08 04:41 0.471562 AU
70544634 km
19.86 km/s
2058-Apr-05 19:09 0.344802 AU
51581596 km
16.60 km/s
2059-Apr-04 19:12 0.221635 AU
33156092 km
13.80 km/s
2060-Apr-04 19:24 0.112068 AU
16765160 km
11.80 km/s
2060-Nov-27 23:59 0.329533 AU
49297371 km
12.27 km/s
2061-Apr-08 04:50 0.081320 AU
12165229 km
10.79 km/s
2061-Nov-06 06:44 0.234878 AU
35137294 km
12.34 km/s
2062-Apr-14 03:24 0.165592 AU
24772156 km
10.75 km/s
2062-Oct-20 21:00 0.150074 AU
22450819 km
12.11 km/s
2063-Apr-22 23:11 0.266580 AU
39879820 km
11.27 km/s
2063-Oct-06 09:28 0.126422 AU
18912500 km
12.42 km/s
2064-May-04 19:45 0.363987 AU
54451689 km
11.83 km/s
2064-Sep-21 21:26 0.194803 AU
29142182 km
13.50 km/s
2065-Sep-09 00:38 0.299943 AU
44870834 km
15.30 km/s
2066-Aug-27 17:25 0.415645 AU
62179593 km
17.67 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
22.1

Orbit Quality

RMS
0.48847
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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