SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 GN4

2018 GN4

2018 GN4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.399 AU it takes 1.65 yr to circle the Sun.

Apollo Observations: 65
Orbital Period · P
1.65 yr
v(q)
40.9 km/s
v(Q)
15.5 km/s
Diameter · ≈
0.11 km
TJ
4.63
Eccentricity · e
0.4505

Orbit and dynamics

Between its closest point (0.769 AU) and its farthest (2.029 AU), the heliocentric distance changes by 1.26 AU over every revolution.

One full revolution takes 1.65 yr (604 days), computed from the semi-major axis of 1.399 AU.

The high eccentricity (0.451) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 11.76° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40.9 km/s at perihelion and falls to 15.5 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 = 22.59 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

Astrometry from 65 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5508 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
1.399 AU
Eccentricity
0.4505
Perihelion
0.769 AU
Aphelion
2.029249 AU
Inclination
11.76°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
17.77°

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-Jan-08 05:32 0.277574 AU
41524478 km
10.61 km/s
2028-Mar-24 17:32 0.386070 AU
57755220 km
6.90 km/s
2032-Nov-18 07:00 0.210238 AU
31451089 km
9.33 km/s
2037-Oct-20 01:39 0.024428 AU
3654311 km
13.10 km/s
2042-Oct-10 04:12 0.165428 AU
24747642 km
17.95 km/s
2047-Sep-30 18:17 0.358170 AU
53581404 km
23.40 km/s
2061-Apr-11 09:18 0.430726 AU
64435747 km
25.31 km/s
2066-Apr-02 12:34 0.242182 AU
36229934 km
19.76 km/s
2071-Mar-24 09:43 0.083526 AU
12495350 km
14.29 km/s
2076-Mar-12 12:12 0.162594 AU
24323677 km
9.53 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
22.59

Orbit Quality

RMS
0.55082
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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