SpaceAtlas Space Object Data
NASA JPL SBDB · 2002 JQ9

2002 JQ9

2002 JQ9 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.157 AU it takes 1.24 yr to circle the Sun.

Apollo Observations: 209
Orbital Period · P
1.24 yr
v(q)
42 km/s
v(Q)
18.2 km/s
Diameter · ≈
0.5 km
TJ
5.28
Eccentricity · e
0.3945

Orbit and dynamics

Between its closest point (0.7 AU) and its farthest (1.613 AU), the heliocentric distance changes by 0.913 AU over every revolution.

One full revolution takes 1.24 yr (455 days), computed from the semi-major axis of 1.157 AU.

An eccentricity of 0.395 makes the orbit moderately elongated.

A steep inclination of 25° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 42 km/s at perihelion and falls to 18.2 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 = 19.24 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.5 km.

Observation record and orbit quality

Astrometry from 209 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4717 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
1.157 AU
Eccentricity
0.3945
Perihelion
0.7 AU
Aphelion
1.613437 AU
Inclination
25.0°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
185.69°

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
2031-Nov-17 10:21 0.146575 AU
21927286 km
15.53 km/s
2036-Nov-07 04:38 0.077473 AU
11589729 km
17.80 km/s
2041-Oct-30 01:29 0.175123 AU
26198075 km
20.85 km/s
2048-May-13 05:26 0.150410 AU
22500942 km
20.00 km/s
2053-May-08 13:19 0.047802 AU
7151103 km
16.85 km/s
2058-May-05 10:38 0.149846 AU
22416708 km
14.41 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
19.24

Orbit Quality

RMS
0.47165
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

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