SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 TC5

2018 TC5

2018 TC5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.041 AU it takes 1.06 yr to circle the Sun.

Apollo Observations: 49
Orbital Period · P
1.06 yr
v(q)
30.4 km/s
v(Q)
28.1 km/s
Diameter · ≈
0.02 km
TJ
5.86
Eccentricity · e
0.039

Orbit and dynamics

Between its closest point (1 AU) and its farthest (1.082 AU), the heliocentric distance changes by 0.082 AU over every revolution.

One full revolution takes 1.06 yr (388 days), computed from the semi-major axis of 1.041 AU.

With e = 0.039, the orbit is close to circular.

The orbital plane is tilted 14.57° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 30.4 km/s at perihelion and falls to 28.1 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 49 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4554 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.041 AU
Eccentricity
0.039
Perihelion
1.0 AU
Aphelion
1.081599 AU
Inclination
14.57°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
1.09°

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
2034-Oct-11 06:30 0.368928 AU
55190883 km
15.40 km/s
2035-Oct-14 08:43 0.045172 AU
6757599 km
7.93 km/s
2036-Apr-07 13:01 0.046015 AU
6883809 km
7.59 km/s
2036-Oct-03 15:40 0.219268 AU
32801993 km
10.54 km/s
2037-Apr-04 01:47 0.307815 AU
46048523 km
13.85 km/s
2052-Oct-13 23:45 0.065345 AU
9775413 km
8.98 km/s
2053-Apr-10 03:54 0.054777 AU
8194497 km
7.55 km/s
2053-Oct-08 06:31 0.107281 AU
16049045 km
9.21 km/s
2054-Apr-04 03:03 0.135510 AU
20272067 km
11.84 km/s
2069-Oct-13 01:32 0.203975 AU
30514287 km
12.32 km/s
2070-Apr-17 23:46 0.125957 AU
18842964 km
9.01 km/s
2070-Oct-12 21:15 0.045312 AU
6778574 km
7.58 km/s
2071-Apr-05 14:13 0.090393 AU
13522667 km
8.75 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
26.2

Orbit Quality

RMS
0.45538
Condition
7
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.