SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 TT5

2013 TT5

2013 TT5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.058 AU it takes 1.09 yr to circle the Sun.

Apollo Observations: 28
Orbital Period · P
1.09 yr
v(q)
31.8 km/s
v(Q)
26.4 km/s
Diameter · ≈
0.02 km
TJ
5.81
Eccentricity · e
0.0922

Orbit and dynamics

The path is an ellipse reaching 0.96 AU from the Sun at perihelion and 1.156 AU at aphelion, a radial span of 0.196 AU.

Applying Kepler's third law to a = 1.058 AU gives an orbital period of 1.09 yr, or about 397 days.

With e = 0.092, the orbit is close to circular.

The orbital plane is tilted 7.34° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 31.8 km/s at perihelion and falls to 26.4 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 = 26.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 28 observations and has a weighted RMS residual of 0.438 arcseconds.

Condition code U = 6 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
1.058 AU
Eccentricity
0.0922
Perihelion
0.96 AU
Aphelion
1.155548 AU
Inclination
7.34°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
165.73°

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-Mar-11 05:29 0.270294 AU
40435415 km
11.06 km/s
2037-Sep-28 13:08 0.337506 AU
50490111 km
13.46 km/s
2039-Mar-10 10:58 0.089134 AU
13334211 km
5.98 km/s
2049-Sep-23 20:33 0.468342 AU
70063023 km
16.67 km/s
2050-Oct-06 11:51 0.069771 AU
10437574 km
3.81 km/s
2051-Mar-18 02:20 0.061498 AU
9199968 km
4.36 km/s
2061-Sep-23 16:00 0.486573 AU
72790211 km
16.78 km/s
2062-Oct-05 05:57 0.082735 AU
12377031 km
3.82 km/s
2063-Mar-16 14:06 0.062668 AU
9375028 km
4.43 km/s
2073-Sep-29 08:44 0.358285 AU
53598647 km
13.53 km/s
2075-Mar-07 22:51 0.129048 AU
19305331 km
6.73 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
26.3

Orbit Quality

RMS
0.43796
Condition
6
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.