SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 TA25

2015 TA25

2015 TA25 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.199 AU it takes 1.31 yr to circle the Sun.

Apollo Observations: 369
Orbital Period · P
1.31 yr
v(q)
40.8 km/s
v(Q)
18.2 km/s
Diameter · ≈
0.34 km
TJ
5.09
Eccentricity · e
0.3837

Orbit and dynamics

Between its closest point (0.739 AU) and its farthest (1.659 AU), the heliocentric distance changes by 0.92 AU over every revolution.

One full revolution takes 1.31 yr (480 days), computed from the semi-major axis of 1.199 AU.

An eccentricity of 0.384 makes the orbit moderately elongated.

A steep inclination of 31.86° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.8 km/s at perihelion and falls to 18.2 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 = 20.07 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.34 km.

Observation record and orbit quality

Astrometry from 369 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3461 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
1.199 AU
Eccentricity
0.3837
Perihelion
0.739 AU
Aphelion
1.659056 AU
Inclination
31.86°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
309.3°

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
2029-May-11 14:49 0.167843 AU
25108991 km
21.62 km/s
2032-Nov-01 18:33 0.478106 AU
71523669 km
16.28 km/s
2033-Apr-10 13:20 0.297742 AU
44541592 km
18.91 km/s
2036-Nov-12 10:16 0.260580 AU
38982167 km
17.13 km/s
2040-Nov-11 04:29 0.304295 AU
45521864 km
22.45 km/s
2046-Jun-05 08:01 0.473764 AU
70874138 km
28.92 km/s
2050-May-12 14:50 0.172967 AU
25875566 km
21.76 km/s
2053-Nov-01 19:52 0.482421 AU
72169087 km
16.28 km/s
2054-Apr-11 19:35 0.290508 AU
43459438 km
18.92 km/s
2057-Nov-12 14:44 0.264432 AU
39558534 km
17.07 km/s
2061-Nov-11 15:34 0.300506 AU
44955044 km
22.32 km/s
2067-Jun-06 01:02 0.480218 AU
71839534 km
29.06 km/s
2071-May-13 10:25 0.177150 AU
26501316 km
21.88 km/s
2074-Nov-01 21:52 0.485470 AU
72625256 km
16.27 km/s
2075-Apr-12 17:11 0.285721 AU
42743229 km
18.94 km/s
2078-Nov-12 19:49 0.267141 AU
39963721 km
17.04 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
20.07

Orbit Quality

RMS
0.34606
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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