SpaceAtlas Space Object Data
NASA JPL SBDB · 2005 SQ9

2005 SQ9

2005 SQ9 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.444 AU it takes 1.74 yr to circle the Sun.

Apollo Observations: 42
Orbital Period · P
1.74 yr
v(q)
36 km/s
v(Q)
17.1 km/s
Diameter · ≈
0.09 km
TJ
4.59
Eccentricity · e
0.3567

Orbit and dynamics

The path is an ellipse reaching 0.929 AU from the Sun at perihelion and 1.959 AU at aphelion, a radial span of 1.03 AU.

Applying Kepler's third law to a = 1.444 AU gives an orbital period of 1.74 yr, or about 634 days.

An eccentricity of 0.357 makes the orbit moderately elongated.

Its inclination of 4.04° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36 km/s at perihelion and falls to 17.1 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 = 22.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

The current orbit solution is based on 42 observations and has a weighted RMS residual of 0.5514 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
1.444 AU
Eccentricity
0.3567
Perihelion
0.929 AU
Aphelion
1.959075 AU
Inclination
4.04°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
16.28°

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
2045-May-01 17:58 0.149896 AU
22424188 km
14.98 km/s
2057-Sep-23 19:49 0.350882 AU
52491199 km
19.44 km/s
2064-Sep-03 05:23 0.036855 AU
5513369 km
9.68 km/s
2078-May-07 14:44 0.059123 AU
8844734 km
12.44 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
22.9

Orbit Quality

RMS
0.55137
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

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