SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 GE135

2016 GE135

2016 GE135 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.4 AU it takes 1.66 yr to circle the Sun.

Apollo Observations: 51
Orbital Period · P
1.66 yr
v(q)
35.5 km/s
v(Q)
17.9 km/s
Diameter · ≈
0.09 km
TJ
4.67
Eccentricity · e
0.3308

Orbit and dynamics

The path is an ellipse reaching 0.937 AU from the Sun at perihelion and 1.863 AU at aphelion, a radial span of 0.926 AU.

Applying Kepler's third law to a = 1.4 AU gives an orbital period of 1.66 yr, or about 605 days.

An eccentricity of 0.331 makes the orbit moderately elongated.

The orbital plane is tilted 13.97° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35.5 km/s at perihelion and falls to 17.9 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 = 23.02 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

The current orbit solution is based on 51 observations and has a weighted RMS residual of 0.6832 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
1.4 AU
Eccentricity
0.3308
Perihelion
0.937 AU
Aphelion
1.86312 AU
Inclination
13.97°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
108.17°

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
2030-Oct-15 16:04 0.471090 AU
70474047 km
21.65 km/s
2058-Sep-29 05:54 0.489852 AU
73280844 km
8.14 km/s
2059-Mar-14 07:18 0.333264 AU
49855628 km
16.49 km/s
2063-Oct-19 13:54 0.353359 AU
52861823 km
7.42 km/s
2064-Mar-07 14:23 0.202058 AU
30227459 km
11.59 km/s
2068-Nov-04 05:03 0.200963 AU
30063669 km
7.55 km/s
2069-Mar-07 12:24 0.201089 AU
30082550 km
8.15 km/s
2073-Nov-02 11:46 0.111514 AU
16682187 km
10.26 km/s
2074-Mar-19 21:28 0.305372 AU
45682992 km
7.63 km/s
2078-Oct-27 03:49 0.222634 AU
33305606 km
14.60 km/s
2079-Apr-04 11:41 0.423607 AU
63370705 km
8.47 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
23.02

Orbit Quality

RMS
0.68315
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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