SpaceAtlas Space Object Data
NASA JPL SBDB · 2008 TA

2008 TA

2008 TA belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.38 AU it takes 1.62 yr to circle the Sun.

Apollo Observations: 50
Orbital Period · P
1.62 yr
v(q)
54.8 km/s
v(Q)
11.7 km/s
Diameter · ≈
0.06 km
TJ
4.56
Eccentricity · e
0.6476

Orbit and dynamics

The path is an ellipse reaching 0.486 AU from the Sun at perihelion and 2.274 AU at aphelion, a radial span of 1.788 AU.

Applying Kepler's third law to a = 1.38 AU gives an orbital period of 1.62 yr, or about 592 days.

The high eccentricity (0.648) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.52° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 54.8 km/s at perihelion and falls to 11.7 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 = 24.05 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 50 observations and has a weighted RMS residual of 0.6007 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
1.38 AU
Eccentricity
0.6476
Perihelion
0.486 AU
Aphelion
2.273688 AU
Inclination
1.52°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
359.79°

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
2031-Feb-27 15:21 0.236851 AU
35432333 km
14.12 km/s
2034-Sep-10 00:29 0.286871 AU
42915300 km
12.72 km/s
2042-Oct-12 09:54 0.373142 AU
55821240 km
32.64 km/s
2044-Feb-19 12:47 0.067028 AU
10027305 km
19.24 km/s
2047-Aug-05 22:20 0.411377 AU
61541061 km
15.76 km/s
2055-Oct-07 03:45 0.251818 AU
37671483 km
28.84 km/s
2057-Feb-13 06:36 0.059901 AU
8961045 km
22.97 km/s
2060-Jul-18 15:39 0.468932 AU
70151261 km
19.95 km/s
2065-Apr-28 13:43 0.476561 AU
71292533 km
21.06 km/s
2068-Sep-29 00:40 0.086692 AU
12968887 km
23.81 km/s
2070-Feb-05 22:03 0.231589 AU
34645149 km
28.30 km/s
2078-Feb-24 13:52 0.464920 AU
69550985 km
9.56 km/s
2078-Apr-10 07:51 0.418243 AU
62568268 km
16.67 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
24.05

Orbit Quality

RMS
0.60066
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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