SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 GX5

2015 GX5

2015 GX5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.06 AU it takes 1.09 yr to circle the Sun.

Apollo Observations: 75
Orbital Period · P
1.09 yr
v(q)
39.6 km/s
v(Q)
21.1 km/s
Diameter · ≈
0.26 km
TJ
5.68
Eccentricity · e
0.3041

Orbit and dynamics

Between its closest point (0.737 AU) and its farthest (1.382 AU), the heliocentric distance changes by 0.645 AU over every revolution.

One full revolution takes 1.09 yr (399 days), computed from the semi-major axis of 1.06 AU.

An eccentricity of 0.304 makes the orbit moderately elongated.

A steep inclination of 27.05° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.6 km/s at perihelion and falls to 21.1 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 = 20.65 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.26 km.

Observation record and orbit quality

Astrometry from 75 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4828 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
1.06 AU
Eccentricity
0.3041
Perihelion
0.737 AU
Aphelion
1.382346 AU
Inclination
27.05°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
323.46°

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
2028-Oct-26 15:28 0.188348 AU
28176488 km
17.69 km/s
2040-Oct-25 21:24 0.189754 AU
28386841 km
17.64 km/s
2052-Oct-24 06:52 0.193452 AU
28940002 km
17.56 km/s
2064-Oct-23 04:02 0.196500 AU
29396030 km
17.51 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
20.65

Orbit Quality

RMS
0.48278
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.