SpaceAtlas Space Object Data
NASA JPL SBDB · 2007 TQ24

2007 TQ24

2007 TQ24 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.793 AU and a period of 0.71 yr.

Aten Observations: 177
Orbital Period · P
0.71 yr
v(q)
61.2 km/s
v(Q)
18.3 km/s
Diameter · ≈
0.14 km
TJ
7.21
Eccentricity · e
0.5394

Orbit and dynamics

The path is an ellipse reaching 0.365 AU from the Sun at perihelion and 1.221 AU at aphelion, a radial span of 0.856 AU.

Applying Kepler's third law to a = 0.793 AU gives an orbital period of 0.71 yr, or about 258 days.

The high eccentricity (0.539) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 10.59° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 61.2 km/s at perihelion and falls to 18.3 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 = 22.06 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.14 km.

Observation record and orbit quality

The current orbit solution is based on 177 observations and has a weighted RMS residual of 0.4432 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
0.7933 AU
Eccentricity
0.5394
Perihelion
0.365 AU
Aphelion
1.221206 AU
Inclination
10.59°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
279.23°

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-Sep-22 06:58 0.016688 AU
2496512 km
15.64 km/s
2043-Sep-23 11:20 0.093944 AU
14053885 km
18.29 km/s
2046-Dec-02 10:57 0.170095 AU
25445849 km
15.48 km/s
2048-Sep-30 06:07 0.160136 AU
23956036 km
12.30 km/s
2055-Sep-26 09:16 0.195270 AU
29212030 km
21.57 km/s
2058-Nov-29 16:00 0.182420 AU
27289670 km
12.92 km/s
2060-Sep-23 09:55 0.082527 AU
12345826 km
13.47 km/s
2072-Sep-21 17:45 0.015533 AU
2323694 km
15.56 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
22.06

Orbit Quality

RMS
0.44317
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.

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