SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 GQ17

2014 GQ17

2014 GQ17 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.854 AU and a period of 0.79 yr.

Aten Observations: 93
Orbital Period · P
0.79 yr
v(q)
41.5 km/s
v(Q)
25 km/s
Diameter · ≈
0.01 km
TJ
6.88
Eccentricity · e
0.2472

Orbit and dynamics

The path is an ellipse reaching 0.643 AU from the Sun at perihelion and 1.065 AU at aphelion, a radial span of 0.422 AU.

Applying Kepler's third law to a = 0.854 AU gives an orbital period of 0.79 yr, or about 288 days.

An eccentricity of 0.247 makes the orbit moderately elongated.

Its inclination of 0.09° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 41.5 km/s at perihelion and falls to 25 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 = 27.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 93 observations and has a weighted RMS residual of 0.473 arcseconds.

Condition code U = 6 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
0.8541 AU
Eccentricity
0.2472
Perihelion
0.643 AU
Aphelion
1.065234 AU
Inclination
0.09°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
282.43°

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-Apr-15 14:45 0.034276 AU
5127682 km
4.56 km/s
2032-Dec-24 21:04 0.305339 AU
45678138 km
9.03 km/s
2033-Jun-14 15:47 0.164282 AU
24576286 km
10.64 km/s
2036-Apr-13 11:27 0.493783 AU
73868814 km
21.11 km/s
2036-Nov-04 15:07 0.348544 AU
52141487 km
11.44 km/s
2040-Mar-30 16:32 0.128338 AU
19199145 km
9.78 km/s
2040-Sep-14 03:24 0.296071 AU
44291535 km
8.14 km/s
2044-Jan-29 20:25 0.227921 AU
34096499 km
4.88 km/s
2044-Jun-10 16:44 0.000186 AU
27871 km
5.35 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
27.1

Orbit Quality

RMS
0.473
Condition
6
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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