SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 TA6

2017 TA6

2017 TA6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.119 AU it takes 1.18 yr to circle the Sun.

Apollo Observations: 43
Orbital Period · P
1.18 yr
v(q)
33.5 km/s
v(Q)
23.7 km/s
Diameter · ≈
0.01 km
TJ
5.56
Eccentricity · e
0.1711

Orbit and dynamics

The path is an ellipse reaching 0.928 AU from the Sun at perihelion and 1.31 AU at aphelion, a radial span of 0.382 AU.

Applying Kepler's third law to a = 1.119 AU gives an orbital period of 1.18 yr, or about 432 days.

An eccentricity of 0.171 makes the orbit moderately elongated.

Its inclination of 0.99° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.5 km/s at perihelion and falls to 23.7 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 = 27.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 43 observations and has a weighted RMS residual of 0.4111 arcseconds.

Condition code U = 4 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
1.119 AU
Eccentricity
0.1711
Perihelion
0.928 AU
Aphelion
1.310461 AU
Inclination
0.99°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
62.03°

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
2030-Dec-30 07:50 0.055414 AU
8289751 km
3.18 km/s
2036-Sep-24 10:38 0.385399 AU
57654907 km
15.40 km/s
2037-Jun-06 09:49 0.291602 AU
43622998 km
5.59 km/s
2043-Aug-20 17:52 0.208010 AU
31117874 km
3.72 km/s
2044-Feb-14 10:59 0.031206 AU
4668392 km
4.71 km/s
2049-Oct-11 11:33 0.111395 AU
16664503 km
7.30 km/s
2050-Apr-28 14:49 0.240704 AU
36008829 km
4.57 km/s
2055-Sep-20 19:57 0.497059 AU
74358919 km
18.75 km/s
2056-Jun-19 12:13 0.298561 AU
44664027 km
5.68 km/s
2057-Mar-12 13:41 0.463094 AU
69277912 km
17.88 km/s
2062-Aug-13 16:40 0.226835 AU
33934018 km
4.16 km/s
2063-Feb-19 05:32 0.073031 AU
10925257 km
6.14 km/s
2068-Oct-18 06:43 0.037499 AU
5609739 km
5.08 km/s
2069-Apr-16 23:46 0.211875 AU
31695988 km
3.95 km/s
2075-Jun-23 06:35 0.295240 AU
44167320 km
5.62 km/s
2076-Mar-12 05:22 0.434533 AU
65005269 km
17.11 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
27.1

Orbit Quality

RMS
0.41106
Condition
4
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.

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