SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 TJ1

2015 TJ1

2015 TJ1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.229 AU it takes 1.36 yr to circle the Sun.

Apollo Observations: 267
Orbital Period · P
1.36 yr
v(q)
33.6 km/s
v(Q)
21.5 km/s
Diameter · ≈
0.1 km
TJ
5.18
Eccentricity · e
0.2213

Orbit and dynamics

The path is an ellipse reaching 0.957 AU from the Sun at perihelion and 1.501 AU at aphelion, a radial span of 0.544 AU.

Applying Kepler's third law to a = 1.229 AU gives an orbital period of 1.36 yr, or about 498 days.

An eccentricity of 0.221 makes the orbit moderately elongated.

Its inclination of 2.22° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.6 km/s at perihelion and falls to 21.5 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 = 22.67 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 267 observations and has a weighted RMS residual of 0.4652 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
1.229 AU
Eccentricity
0.2213
Perihelion
0.957 AU
Aphelion
1.500978 AU
Inclination
2.22°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
218.9°

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-Nov-11 19:43 0.441900 AU
66107310 km
17.46 km/s
2027-Jun-02 17:25 0.396612 AU
59332293 km
6.42 km/s
2031-Feb-11 02:31 0.027537 AU
4119414 km
3.76 km/s
2034-Aug-31 20:10 0.425337 AU
63629516 km
6.92 km/s
2038-Jul-19 11:43 0.486212 AU
72736328 km
7.91 km/s
2041-Nov-09 10:35 0.473907 AU
70895426 km
18.43 km/s
2042-Jun-05 00:17 0.406545 AU
60818223 km
6.57 km/s
2046-Feb-02 22:40 0.028947 AU
4330398 km
3.63 km/s
2049-Sep-01 00:19 0.423018 AU
63282600 km
6.90 km/s
2053-Jul-19 06:32 0.486610 AU
72795770 km
7.93 km/s
2056-Nov-08 16:51 0.475944 AU
71200281 km
18.50 km/s
2057-Jun-04 13:35 0.407566 AU
60970981 km
6.61 km/s
2061-Feb-03 08:33 0.028803 AU
4308835 km
3.66 km/s
2064-Aug-31 01:43 0.424139 AU
63450218 km
6.90 km/s
2068-Jul-18 04:57 0.487024 AU
72857811 km
7.92 km/s
2071-Nov-09 06:16 0.467926 AU
70000695 km
18.27 km/s
2072-Jun-03 03:31 0.405448 AU
60654151 km
6.55 km/s
2076-Feb-09 12:06 0.027579 AU
4125799 km
3.72 km/s
2079-Aug-29 17:27 0.429522 AU
64255612 km
7.00 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
22.67

Orbit Quality

RMS
0.46522
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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