SpaceAtlas Space Object Data
NASA JPL SBDB · 1993 TZ

1993 TZ

1993 TZ belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.017 AU it takes 2.86 yr to circle the Sun.

Apollo Observations: 33
Orbital Period · P
2.86 yr
v(q)
39.8 km/s
v(Q)
11 km/s
Diameter · ≈
0.02 km
TJ
3.6
Eccentricity · e
0.5658

Orbit and dynamics

Between its closest point (0.876 AU) and its farthest (3.158 AU), the heliocentric distance changes by 2.282 AU over every revolution.

One full revolution takes 2.86 yr (1,046 days), computed from the semi-major axis of 2.017 AU.

The high eccentricity (0.566) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.15° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 39.8 km/s at perihelion and falls to 11 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 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 33 individual observations underpins this orbit; the fit leaves an RMS residual of 0.7686 arcseconds.

Condition code U = 1 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
2.017 AU
Eccentricity
0.5658
Perihelion
0.876 AU
Aphelion
3.158219 AU
Inclination
4.15°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
119.09°

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
2037-Jan-01 12:57 0.104151 AU
15580702 km
9.66 km/s
2057-Feb-15 13:59 0.347807 AU
52031254 km
21.73 km/s
2059-Oct-14 21:54 0.061780 AU
9242083 km
13.40 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
26.0

Orbit Quality

RMS
0.76861
Condition
1
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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