SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 SP3

2019 SP3

2019 SP3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.464 AU it takes 3.87 yr to circle the Sun.

Apollo Observations: 36
Orbital Period · P
3.87 yr
v(q)
38 km/s
v(Q)
9.5 km/s
Diameter · ≈
0.02 km
TJ
3.21
Eccentricity · e
0.6014

Orbit and dynamics

Between its closest point (0.982 AU) and its farthest (3.946 AU), the heliocentric distance changes by 2.964 AU over every revolution.

One full revolution takes 3.87 yr (1,413 days), computed from the semi-major axis of 2.464 AU.

The high eccentricity (0.601) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.15° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38 km/s at perihelion and falls to 9.5 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 = 26.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 36 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3452 arcseconds.

Condition code U = 5 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
2.464 AU
Eccentricity
0.6014
Perihelion
0.982 AU
Aphelion
3.94585 AU
Inclination
1.15°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
258.53°

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
2046-Dec-17 05:20 0.294553 AU
44064476 km
20.04 km/s
2050-Aug-22 08:18 0.280609 AU
41978440 km
19.59 km/s
2073-Aug-31 03:37 0.082844 AU
12393255 km
15.03 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
26.2

Orbit Quality

RMS
0.34521
Condition
5
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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