SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 CT4

2019 CT4

2019 CT4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.361 AU it takes 1.59 yr to circle the Sun.

Apollo Observations: 129
Orbital Period · P
1.59 yr
v(q)
36.3 km/s
v(Q)
18 km/s
Diameter · ≈
0.05 km
TJ
4.75
Eccentricity · e
0.3373

Orbit and dynamics

The path is an ellipse reaching 0.902 AU from the Sun at perihelion and 1.82 AU at aphelion, a radial span of 0.918 AU.

Applying Kepler's third law to a = 1.361 AU gives an orbital period of 1.59 yr, or about 580 days.

An eccentricity of 0.337 makes the orbit moderately elongated.

The orbital plane is tilted 16.4° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 36.3 km/s at perihelion and falls to 18 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 = 24.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

The current orbit solution is based on 129 observations and has a weighted RMS residual of 0.3847 arcseconds.

Condition code U = 3 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.361 AU
Eccentricity
0.3373
Perihelion
0.902 AU
Aphelion
1.820065 AU
Inclination
16.4°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
181.81°

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
2027-Feb-09 22:56 0.392008 AU
58643595 km
21.66 km/s
2030-Jul-23 15:44 0.375819 AU
56221692 km
17.77 km/s
2038-May-10 08:45 0.285383 AU
42692756 km
8.60 km/s
2038-Jul-19 00:02 0.263860 AU
39472940 km
9.27 km/s
2046-Feb-26 20:27 0.058927 AU
8815315 km
13.30 km/s
2046-Aug-14 15:14 0.455911 AU
68203309 km
9.89 km/s
2054-Feb-05 05:40 0.489830 AU
73277455 km
24.38 km/s
2057-Jul-19 21:56 0.298827 AU
44703879 km
14.75 km/s
2065-Mar-18 17:47 0.170004 AU
25432171 km
9.71 km/s
2065-Jul-29 10:01 0.333856 AU
49944164 km
8.91 km/s
2073-Feb-16 17:36 0.245635 AU
36746434 km
17.80 km/s
2076-Jul-28 10:27 0.475567 AU
71143818 km
21.23 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
24.4

Orbit Quality

RMS
0.38468
Condition
3
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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