SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 TA7

2019 TA7

2019 TA7 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.756 AU and a period of 0.66 yr.

Aten Observations: 21
Orbital Period · P
0.66 yr
v(q)
55.9 km/s
v(Q)
21 km/s
Diameter · ≈
0.02 km
TJ
7.56
Eccentricity · e
0.4538

Orbit and dynamics

Between its closest point (0.413 AU) and its farthest (1.099 AU), the heliocentric distance changes by 0.686 AU over every revolution.

One full revolution takes 0.66 yr (240 days), computed from the semi-major axis of 0.756 AU.

The high eccentricity (0.454) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.03° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 55.9 km/s at perihelion and falls to 21 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 = 26.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 21 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4583 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
0.756 AU
Eccentricity
0.4538
Perihelion
0.413 AU
Aphelion
1.099073 AU
Inclination
4.03°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
287.24°

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
2032-Aug-26 22:16 0.303248 AU
45365303 km
23.69 km/s
2034-Aug-21 16:20 0.143096 AU
21406809 km
18.47 km/s
2036-Aug-17 19:44 0.049378 AU
7386834 km
13.35 km/s
2044-Oct-15 14:49 0.018839 AU
2818257 km
14.02 km/s
2046-Oct-12 03:14 0.168083 AU
25144913 km
18.98 km/s
2048-Oct-05 17:49 0.320209 AU
47902653 km
24.09 km/s
2057-Aug-25 04:53 0.274019 AU
40992674 km
22.03 km/s
2059-Aug-20 15:40 0.135853 AU
20323283 km
17.02 km/s
2061-Aug-18 03:52 0.048528 AU
7259633 km
12.27 km/s
2062-Jan-06 10:18 0.441125 AU
65991329 km
14.28 km/s
2063-Aug-28 15:54 0.053560 AU
8012418 km
9.14 km/s
2067-Oct-12 22:25 0.010993 AU
1644495 km
9.83 km/s
2069-May-22 14:08 0.471978 AU
70606963 km
14.70 km/s
2069-Oct-16 04:40 0.064234 AU
9609258 km
13.54 km/s
2071-Oct-13 09:17 0.223231 AU
33394877 km
18.11 km/s
2073-Oct-07 13:41 0.362933 AU
54294063 km
22.81 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
26.3

Orbit Quality

RMS
0.45832
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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