SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 TA57

2016 TA57

2016 TA57 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.9 AU and a period of 0.85 yr.

Aten Observations: 55
Orbital Period · P
0.85 yr
v(q)
57.6 km/s
v(Q)
17.1 km/s
Diameter · ≈
0.25 km
TJ
6.39
Eccentricity · e
0.5419

Orbit and dynamics

The path is an ellipse reaching 0.412 AU from the Sun at perihelion and 1.387 AU at aphelion, a radial span of 0.975 AU.

Applying Kepler's third law to a = 0.9 AU gives an orbital period of 0.85 yr, or about 312 days.

The high eccentricity (0.542) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 30.07° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 57.6 km/s at perihelion and falls to 17.1 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

The measured diameter is 0.28 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.088 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

The current orbit solution is based on 55 observations and has a weighted RMS residual of 0.4461 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
0.8996 AU
Eccentricity
0.5419
Perihelion
0.412 AU
Aphelion
1.387093 AU
Inclination
30.07°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
24.68°

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-16 15:23 0.251284 AU
37591543 km
27.77 km/s
2032-Jun-09 22:42 0.452833 AU
67742869 km
23.15 km/s
2033-Oct-19 19:39 0.398109 AU
59556248 km
16.07 km/s
2034-Oct-10 09:28 0.407991 AU
61034599 km
32.40 km/s
2038-May-25 05:40 0.462249 AU
69151520 km
24.34 km/s
2039-Oct-27 20:11 0.263821 AU
39467064 km
16.65 km/s
2044-May-09 08:25 0.486247 AU
72741587 km
26.21 km/s
2045-Oct-28 04:48 0.114006 AU
17055061 km
18.80 km/s
2051-Oct-25 04:42 0.043234 AU
6467658 km
22.15 km/s
2055-Jul-01 00:28 0.478919 AU
71645258 km
24.00 km/s
2057-Oct-18 18:10 0.207733 AU
31076364 km
26.53 km/s
2061-Jun-14 03:49 0.454404 AU
67977893 km
23.08 km/s
2062-Oct-17 23:42 0.422701 AU
63235211 km
16.05 km/s
2063-Oct-12 04:52 0.376048 AU
56255946 km
31.41 km/s
2067-May-28 10:44 0.459578 AU
68751935 km
24.08 km/s
2068-Oct-26 09:21 0.286030 AU
42789518 km
16.49 km/s
2073-May-11 09:20 0.483330 AU
72305136 km
26.01 km/s
2074-Oct-28 16:27 0.126782 AU
18966248 km
18.55 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.281 km
Albedo
0.088
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
20.79

Orbit Quality

RMS
0.44613
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.

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