SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 GN2

2016 GN2

2016 GN2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.939 AU and a period of 0.91 yr.

Aten Observations: 93
Orbital Period · P
0.91 yr
v(q)
35.6 km/s
v(Q)
26.5 km/s
Diameter · ≈
0.04 km
TJ
6.37
Eccentricity · e
0.1461

Orbit and dynamics

Between its closest point (0.802 AU) and its farthest (1.077 AU), the heliocentric distance changes by 0.275 AU over every revolution.

One full revolution takes 0.91 yr (333 days), computed from the semi-major axis of 0.939 AU.

An eccentricity of 0.146 makes the orbit moderately elongated.

The orbital plane is tilted 10.38° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35.6 km/s at perihelion and falls to 26.5 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 = 25.01 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 93 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5901 arcseconds.

Condition code U = 1 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
0.9393 AU
Eccentricity
0.1461
Perihelion
0.802 AU
Aphelion
1.076532 AU
Inclination
10.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
273.53°

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
2035-Nov-18 19:01 0.162129 AU
24254120 km
6.93 km/s
2036-Mar-11 23:49 0.141487 AU
21166154 km
5.93 km/s
2045-Dec-13 20:58 0.171379 AU
25637962 km
6.52 km/s
2057-Apr-24 21:05 0.137465 AU
20564519 km
8.94 km/s
2066-Oct-02 22:45 0.198411 AU
29681873 km
8.11 km/s
2067-Apr-21 00:35 0.061732 AU
9235018 km
6.88 km/s
2076-Oct-13 13:11 0.186785 AU
27942614 km
7.97 km/s
2077-Apr-14 17:44 0.052683 AU
7881296 km
6.24 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
25.01

Orbit Quality

RMS
0.59013
Condition
1
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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