SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 TP14

2024 TP14

2024 TP14 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.083 AU it takes 1.13 yr to circle the Sun.

Apollo Observations: 51
Orbital Period · P
1.13 yr
v(q)
68.1 km/s
v(Q)
12 km/s
Diameter · ≈
0.2 km
TJ
5.4
Eccentricity · e
0.7001

Orbit and dynamics

Between its closest point (0.325 AU) and its farthest (1.841 AU), the heliocentric distance changes by 1.516 AU over every revolution.

One full revolution takes 1.13 yr (412 days), computed from the semi-major axis of 1.083 AU.

The high eccentricity (0.7) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 24.79° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 68.1 km/s at perihelion and falls to 12 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 = 21.25 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

Astrometry from 51 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6024 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
1.083 AU
Eccentricity
0.7001
Perihelion
0.325 AU
Aphelion
1.841208 AU
Inclination
24.79°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
252.88°

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
2029-Dec-26 07:42 0.384636 AU
57540665 km
19.13 km/s
2033-Sep-22 17:59 0.394325 AU
58990167 km
18.74 km/s
2038-Dec-23 12:05 0.451952 AU
67611113 km
17.75 km/s
2042-Sep-22 11:19 0.336552 AU
50347520 km
20.95 km/s
2046-Dec-13 17:42 0.440351 AU
65875513 km
32.82 km/s
2051-Sep-25 01:18 0.313081 AU
46836236 km
24.08 km/s
2055-Dec-19 05:15 0.371272 AU
55541538 km
28.82 km/s
2060-Sep-28 08:25 0.336162 AU
50289118 km
27.75 km/s
2064-Dec-23 00:24 0.335755 AU
50228237 km
24.91 km/s
2069-Oct-03 10:02 0.398175 AU
59566075 km
31.56 km/s
2073-Dec-26 10:05 0.346939 AU
51901349 km
21.32 km/s
2077-Sep-25 17:44 0.450483 AU
67391245 km
17.93 km/s
2078-Oct-09 00:38 0.483395 AU
72314896 km
35.58 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
21.25

Orbit Quality

RMS
0.6024
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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