SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 SP3

2010 SP3

2010 SP3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.996 AU it takes 2.82 yr to circle the Sun.

Apollo Observations: 60
Orbital Period · P
2.82 yr
v(q)
44.4 km/s
v(Q)
10 km/s
Diameter · ≈
0.04 km
TJ
3.57
Eccentricity · e
0.632

Orbit and dynamics

The path is an ellipse reaching 0.735 AU from the Sun at perihelion and 3.257 AU at aphelion, a radial span of 2.522 AU.

Applying Kepler's third law to a = 1.996 AU gives an orbital period of 2.82 yr, or about 1,030 days.

The high eccentricity (0.632) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 0.46° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 44.4 km/s at perihelion and falls to 10 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 = 24.93 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 60 observations and has a weighted RMS residual of 0.4123 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
1.996 AU
Eccentricity
0.632
Perihelion
0.735 AU
Aphelion
3.257472 AU
Inclination
0.46°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
236.78°

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
2027-Apr-11 23:40 0.075521 AU
11297735 km
19.30 km/s
2041-Jun-24 19:03 0.283353 AU
42389026 km
15.13 km/s
2055-Sep-10 14:56 0.061172 AU
9151136 km
15.49 km/s
2058-Apr-05 00:41 0.186536 AU
27905463 km
22.78 km/s
2069-Oct-02 09:31 0.299453 AU
44797558 km
26.13 km/s
2072-May-01 23:16 0.149293 AU
22333963 km
13.23 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
24.93

Orbit Quality

RMS
0.41229
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.