SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 CX2

2019 CX2

2019 CX2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.225 AU it takes 3.32 yr to circle the Sun.

Apollo Observations: 72
Orbital Period · P
3.32 yr
v(q)
55.4 km/s
v(Q)
7.2 km/s
Diameter · ≈
0.59 km
TJ
3.15
Eccentricity · e
0.7701

Orbit and dynamics

Between its closest point (0.512 AU) and its farthest (3.938 AU), the heliocentric distance changes by 3.426 AU over every revolution.

One full revolution takes 3.32 yr (1,212 days), computed from the semi-major axis of 2.225 AU.

The high eccentricity (0.77) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.45° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 55.4 km/s at perihelion and falls to 7.2 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 = 18.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.59 km.

Observation record and orbit quality

Astrometry from 72 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4533 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
2.225 AU
Eccentricity
0.7701
Perihelion
0.512 AU
Aphelion
3.938473 AU
Inclination
13.45°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
101.24°

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-15 21:21 0.483484 AU
72328175 km
22.66 km/s
2038-Sep-29 15:32 0.440284 AU
65865538 km
18.99 km/s
2048-Aug-24 10:20 0.304332 AU
45527396 km
16.00 km/s
2058-Aug-10 22:32 0.138323 AU
20692806 km
21.09 km/s
2062-Mar-03 23:12 0.369947 AU
55343238 km
34.93 km/s
2068-Jul-28 11:09 0.156894 AU
23471048 km
28.43 km/s
2072-Feb-20 14:56 0.172775 AU
25846722 km
28.24 km/s
2078-Jul-20 06:48 0.317358 AU
47476109 km
33.48 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
18.9

Orbit Quality

RMS
0.45327
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

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