SpaceAtlas Space Object Data
NASA JPL SBDB · 2002 QQ40

2002 QQ40

2002 QQ40 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.215 AU it takes 1.34 yr to circle the Sun.

Apollo Observations: 71
Orbital Period · P
1.34 yr
v(q)
51.2 km/s
v(Q)
14.3 km/s
Diameter · ≈
0.18 km
TJ
5.08
Eccentricity · e
0.564

Orbit and dynamics

The path is an ellipse reaching 0.53 AU from the Sun at perihelion and 1.9 AU at aphelion, a radial span of 1.37 AU.

Applying Kepler's third law to a = 1.215 AU gives an orbital period of 1.34 yr, or about 489 days.

The high eccentricity (0.564) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.72° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 51.2 km/s at perihelion and falls to 14.3 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 = 21.48 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.18 km.

Observation record and orbit quality

The current orbit solution is based on 71 observations and has a weighted RMS residual of 0.5759 arcseconds.

Condition code U = 1 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
1.215 AU
Eccentricity
0.564
Perihelion
0.53 AU
Aphelion
1.90026 AU
Inclination
1.72°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
215.59°

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
2026-Dec-14 12:14 0.443516 AU
66349101 km
19.99 km/s
2030-Dec-23 20:24 0.451515 AU
67545610 km
20.70 km/s
2035-Jan-02 10:28 0.453503 AU
67843157 km
20.92 km/s
2039-Jan-12 15:48 0.449712 AU
67276009 km
20.59 km/s
2043-Jan-22 23:28 0.439194 AU
65702530 km
19.66 km/s
2047-Feb-02 22:32 0.420598 AU
62920598 km
18.09 km/s
2051-Feb-14 08:21 0.394229 AU
58975848 km
16.02 km/s
2051-May-01 09:53 0.458256 AU
68554175 km
10.27 km/s
2055-Feb-26 11:13 0.359679 AU
53807262 km
13.56 km/s
2055-Apr-23 00:01 0.390349 AU
58395406 km
9.36 km/s
2059-Mar-22 20:39 0.295673 AU
44232011 km
9.34 km/s
2063-Apr-10 21:25 0.193098 AU
28887011 km
11.67 km/s
2065-Aug-26 19:38 0.425848 AU
63705948 km
30.11 km/s
2067-Apr-15 11:25 0.095431 AU
14276211 km
14.60 km/s
2069-Aug-31 02:43 0.335935 AU
50255094 km
27.32 km/s
2071-Apr-19 14:24 0.029246 AU
4375088 km
17.29 km/s
2073-Sep-04 05:39 0.248361 AU
37154229 km
24.65 km/s
2075-Apr-23 16:35 0.094522 AU
14140263 km
19.96 km/s
2077-Sep-08 08:41 0.161043 AU
24091705 km
22.01 km/s
2079-Apr-27 23:01 0.181827 AU
27200990 km
22.63 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
21.48

Orbit Quality

RMS
0.57587
Condition
1
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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