SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 CG2

2018 CG2

2018 CG2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.01 AU it takes 2.85 yr to circle the Sun.

Apollo Observations: 120
Orbital Period · P
2.85 yr
v(q)
50.2 km/s
v(Q)
8.8 km/s
Diameter · ≈
0.51 km
TJ
3.42
Eccentricity · e
0.7021

Orbit and dynamics

Between its closest point (0.599 AU) and its farthest (3.421 AU), the heliocentric distance changes by 2.822 AU over every revolution.

One full revolution takes 2.85 yr (1,041 days), computed from the semi-major axis of 2.01 AU.

The high eccentricity (0.702) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 20.57° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 50.2 km/s at perihelion and falls to 8.8 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 = 19.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.51 km.

Observation record and orbit quality

Astrometry from 120 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4143 arcseconds.

Condition code U = 1 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
2.01 AU
Eccentricity
0.7021
Perihelion
0.599 AU
Aphelion
3.421221 AU
Inclination
20.57°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
348.7°

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
2037-Dec-24 01:10 0.335515 AU
50192345 km
22.10 km/s
2040-Aug-27 23:02 0.356613 AU
53348495 km
17.15 km/s
2055-Feb-20 07:02 0.404696 AU
60541609 km
29.01 km/s
2057-Nov-17 15:36 0.406277 AU
60778221 km
24.03 km/s
2060-Aug-04 13:02 0.407200 AU
60916305 km
27.51 km/s
2075-Jan-06 17:12 0.314372 AU
47029340 km
21.43 km/s
2077-Sep-13 11:50 0.393851 AU
58919345 km
16.22 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
19.2

Orbit Quality

RMS
0.41425
Condition
1
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

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