SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 TY1

2024 TY1

2024 TY1 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.817 AU and a period of 0.74 yr.

Aten Observations: 82
Orbital Period · P
0.74 yr
v(q)
44.4 km/s
v(Q)
24.4 km/s
Diameter · ≈
0.06 km
TJ
7.1
Eccentricity · e
0.2907

Orbit and dynamics

The path is an ellipse reaching 0.58 AU from the Sun at perihelion and 1.055 AU at aphelion, a radial span of 0.475 AU.

Applying Kepler's third law to a = 0.817 AU gives an orbital period of 0.74 yr, or about 270 days.

An eccentricity of 0.291 makes the orbit moderately elongated.

The orbital plane is tilted 15.66° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.4 km/s at perihelion and falls to 24.4 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 = 23.84 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 82 observations and has a weighted RMS residual of 0.4262 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
0.8174 AU
Eccentricity
0.2907
Perihelion
0.58 AU
Aphelion
1.055018 AU
Inclination
15.66°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
288.31°

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
2027-May-24 20:02 0.404631 AU
60531873 km
13.15 km/s
2027-Oct-23 16:08 0.223945 AU
33501760 km
13.45 km/s
2030-Apr-23 08:28 0.418908 AU
62667689 km
16.81 km/s
2030-Oct-19 01:21 0.445416 AU
66633226 km
21.17 km/s
2033-Mar-25 19:08 0.418047 AU
62538951 km
17.62 km/s
2035-Sep-12 15:52 0.291454 AU
43600971 km
16.73 km/s
2036-Feb-25 15:16 0.406412 AU
60798364 km
15.81 km/s
2038-Sep-17 02:21 0.097461 AU
14579927 km
10.39 km/s
2041-Oct-10 18:20 0.066614 AU
9965244 km
9.29 km/s
2044-Oct-23 00:40 0.178201 AU
26658448 km
14.09 km/s
2047-Oct-18 13:30 0.392377 AU
58698819 km
21.97 km/s
2052-Sep-11 12:58 0.199664 AU
29869368 km
15.91 km/s
2061-Oct-23 06:07 0.143523 AU
21470715 km
14.79 km/s
2069-Sep-11 14:52 0.140040 AU
20949716 km
15.42 km/s
2078-Oct-23 14:21 0.133022 AU
19899882 km
14.91 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
23.84

Orbit Quality

RMS
0.42616
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.

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