SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 TM3

2019 TM3

2019 TM3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.05 AU it takes 1.08 yr to circle the Sun.

Apollo Observations: 55
Orbital Period · P
1.08 yr
v(q)
34.3 km/s
v(Q)
24.6 km/s
Diameter · ≈
0.01 km
TJ
5.8
Eccentricity · e
0.1634

Orbit and dynamics

The path is an ellipse reaching 0.879 AU from the Sun at perihelion and 1.222 AU at aphelion, a radial span of 0.343 AU.

Applying Kepler's third law to a = 1.05 AU gives an orbital period of 1.08 yr, or about 393 days.

An eccentricity of 0.163 makes the orbit moderately elongated.

The orbital plane is tilted 17.01° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 34.3 km/s at perihelion and falls to 24.6 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 = 27.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 55 observations and has a weighted RMS residual of 0.4825 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.05 AU
Eccentricity
0.1634
Perihelion
0.879 AU
Aphelion
1.22157 AU
Inclination
17.01°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
5.81°

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
2033-Oct-05 16:09 0.039782 AU
5951337 km
10.69 km/s
2035-Apr-01 17:21 0.035641 AU
5331814 km
9.94 km/s
2036-Apr-15 16:02 0.463629 AU
69357876 km
20.52 km/s
2047-Oct-02 14:52 0.111331 AU
16654891 km
12.38 km/s
2048-Oct-06 06:09 0.293259 AU
43870942 km
9.88 km/s
2049-Apr-01 00:52 0.046322 AU
6929720 km
9.05 km/s
2050-Apr-12 17:33 0.359565 AU
53790096 km
18.19 km/s
2061-Sep-25 14:29 0.266736 AU
39903194 km
15.75 km/s
2062-Oct-13 11:17 0.149636 AU
22385155 km
8.86 km/s
2063-Apr-07 16:58 0.214061 AU
32023130 km
8.80 km/s
2064-Apr-06 17:36 0.221515 AU
33138247 km
14.43 km/s
2075-Sep-19 19:06 0.426362 AU
63782887 km
19.30 km/s
2076-Oct-08 22:55 0.027345 AU
4090697 km
9.46 km/s
2077-Apr-28 13:12 0.327270 AU
48958843 km
8.68 km/s
2078-Apr-03 05:42 0.124259 AU
18588889 km
11.70 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
27.6

Orbit Quality

RMS
0.48249
Condition
6
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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