SpaceAtlas Space Object Data
NASA JPL SBDB · 2005 TF15

2005 TF15

2005 TF15 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.291 AU it takes 3.47 yr to circle the Sun.

Apollo Observations: 49
Orbital Period · P
3.47 yr
v(q)
43.2 km/s
v(Q)
9 km/s
Diameter · ≈
0.45 km
TJ
3.23
Eccentricity · e
0.6561

Orbit and dynamics

Between its closest point (0.788 AU) and its farthest (3.794 AU), the heliocentric distance changes by 3.006 AU over every revolution.

One full revolution takes 3.47 yr (1,267 days), computed from the semi-major axis of 2.291 AU.

The high eccentricity (0.656) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 15.98° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43.2 km/s at perihelion and falls to 9 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 = 19.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.45 km.

Observation record and orbit quality

Astrometry from 49 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5531 arcseconds.

Condition code U = 0 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
2.291 AU
Eccentricity
0.6561
Perihelion
0.788 AU
Aphelion
3.794125 AU
Inclination
15.98°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
329.82°

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
2051-Mar-07 07:37 0.479510 AU
71733699 km
27.16 km/s
2058-Feb-12 03:30 0.268732 AU
40201689 km
18.68 km/s
2065-Jan-14 11:16 0.209618 AU
31358445 km
15.80 km/s
2071-Dec-08 18:19 0.195244 AU
29208101 km
16.29 km/s
2078-Oct-20 10:58 0.219145 AU
32783591 km
18.51 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
19.5

Orbit Quality

RMS
0.55308
Condition
0
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

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