SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 VT11

2010 VT11

2010 VT11 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.753 AU it takes 2.32 yr to circle the Sun.

Apollo Observations: 245
Orbital Period · P
2.32 yr
v(q)
45.9 km/s
v(Q)
11 km/s
Diameter · ≈
0.16 km
TJ
3.89
Eccentricity · e
0.612

Orbit and dynamics

The path is an ellipse reaching 0.68 AU from the Sun at perihelion and 2.826 AU at aphelion, a radial span of 2.146 AU.

Applying Kepler's third law to a = 1.753 AU gives an orbital period of 2.32 yr, or about 848 days.

The high eccentricity (0.612) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.48° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 45.9 km/s at perihelion and falls to 11 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 0.15 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.189 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 245 observations and has a weighted RMS residual of 0.4877 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
1.753 AU
Eccentricity
0.612
Perihelion
0.68 AU
Aphelion
2.825836 AU
Inclination
2.48°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
276.59°

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
2052-Jun-01 03:33 0.178303 AU
26673808 km
12.84 km/s
2059-May-16 13:02 0.023166 AU
3465546 km
17.06 km/s
2066-May-11 03:10 0.063758 AU
9538040 km
19.50 km/s
2073-May-04 02:23 0.186900 AU
27959905 km
23.16 km/s

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

Physical Parameters

Diameter
0.152 km
Albedo
0.189
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
21.7

Orbit Quality

RMS
0.48767
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.