SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 GE84

2013 GE84

2013 GE84 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.903 AU it takes 2.63 yr to circle the Sun.

Apollo Observations: 163
Orbital Period · P
2.63 yr
v(q)
45.9 km/s
v(Q)
10.2 km/s
Diameter · ≈
0.44 km
TJ
3.64
Eccentricity · e
0.6374

Orbit and dynamics

Between its closest point (0.69 AU) and its farthest (3.116 AU), the heliocentric distance changes by 2.426 AU over every revolution.

One full revolution takes 2.63 yr (959 days), computed from the semi-major axis of 1.903 AU.

The high eccentricity (0.637) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.04° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 45.9 km/s at perihelion and falls to 10.2 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 = 19.53 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.44 km.

Observation record and orbit quality

Astrometry from 163 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4222 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
1.903 AU
Eccentricity
0.6374
Perihelion
0.69 AU
Aphelion
3.115972 AU
Inclination
13.04°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
23.41°

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-09 20:46 0.403888 AU
60420782 km
27.86 km/s
2034-Apr-10 03:27 0.288932 AU
43223653 km
22.44 km/s
2042-Jan-03 00:15 0.289134 AU
43253871 km
17.34 km/s
2049-Oct-11 19:13 0.380160 AU
56871108 km
27.08 km/s
2055-Apr-10 16:06 0.286524 AU
42863451 km
22.41 km/s
2063-Jan-09 06:22 0.295525 AU
44209876 km
17.43 km/s
2070-Oct-16 08:05 0.322987 AU
48318143 km
25.10 km/s
2076-Apr-14 18:29 0.343725 AU
51420500 km
24.87 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
19.53

Orbit Quality

RMS
0.42223
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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