SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 TF2

2019 TF2

2019 TF2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.043 AU it takes 1.07 yr to circle the Sun.

Apollo Observations: 52
Orbital Period · P
1.07 yr
v(q)
31.6 km/s
v(Q)
26.9 km/s
Diameter · ≈
0.02 km
TJ
5.88
Eccentricity · e
0.0797

Orbit and dynamics

Between its closest point (0.959 AU) and its farthest (1.126 AU), the heliocentric distance changes by 0.167 AU over every revolution.

One full revolution takes 1.07 yr (389 days), computed from the semi-major axis of 1.043 AU.

With e = 0.08, the orbit is close to circular.

Its inclination of 2.41° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 31.6 km/s at perihelion and falls to 26.9 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 52 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6342 arcseconds.

Condition code U = 3 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
1.043 AU
Eccentricity
0.0797
Perihelion
0.959 AU
Aphelion
1.126127 AU
Inclination
2.41°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
6.05°

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
2035-Nov-03 07:14 0.161713 AU
24191970 km
6.46 km/s
2036-Jul-19 21:45 0.114176 AU
17080496 km
2.46 km/s
2037-Mar-25 02:06 0.146549 AU
21923481 km
6.18 km/s
2051-Oct-24 21:37 0.348685 AU
52162575 km
12.09 km/s
2052-Oct-05 00:31 0.063124 AU
9443234 km
1.71 km/s
2053-Feb-17 05:14 0.030569 AU
4573041 km
1.59 km/s
2054-Apr-01 07:55 0.342509 AU
51238628 km
11.90 km/s
2069-Oct-25 21:37 0.169958 AU
25425337 km
6.77 km/s
2070-Jul-25 09:03 0.107459 AU
16075578 km
2.37 km/s
2071-Mar-18 20:29 0.102823 AU
15382043 km
4.95 km/s
2072-Apr-08 15:43 0.484899 AU
72539874 km
16.18 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
0.63424
Condition
3
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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