SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 TV10

2025 TV10

2025 TV10 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.714 AU and a period of 0.60 yr.

Aten Observations: 58
Orbital Period · P
0.60 yr
v(q)
54.6 km/s
v(Q)
22.7 km/s
Diameter · ≈
0.03 km
TJ
7.96
Eccentricity · e
0.4119

Orbit and dynamics

Between its closest point (0.42 AU) and its farthest (1.009 AU), the heliocentric distance changes by 0.589 AU over every revolution.

One full revolution takes 0.60 yr (221 days), computed from the semi-major axis of 0.714 AU.

The high eccentricity (0.412) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 0.89° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 54.6 km/s at perihelion and falls to 22.7 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 = 25.07 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 58 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4429 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.7144 AU
Eccentricity
0.4119
Perihelion
0.42 AU
Aphelion
1.008661 AU
Inclination
0.89°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
202.53°

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-01 18:55 0.026595 AU
3978530 km
8.58 km/s
2031-Sep-29 03:05 0.119749 AU
17914254 km
12.50 km/s
2045-Nov-08 22:29 0.173592 AU
25968943 km
13.85 km/s
2048-Nov-08 01:56 0.028827 AU
4312526 km
9.29 km/s
2054-Oct-01 05:34 0.017104 AU
2558696 km
8.96 km/s
2057-Sep-28 22:04 0.079154 AU
11841333 km
13.60 km/s
2071-Nov-10 09:43 0.003936 AU
588889 km
11.20 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
25.07

Orbit Quality

RMS
0.44288
Condition
7
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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