SpaceAtlas Space Object Data
NASA JPL SBDB · 2007 TR68

2007 TR68

2007 TR68 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.876 AU and a period of 0.82 yr.

Aten Observations: 26
Orbital Period · P
0.82 yr
v(q)
41.4 km/s
v(Q)
24.5 km/s
Diameter · ≈
0.02 km
TJ
6.72
Eccentricity · e
0.2575

Orbit and dynamics

The path is an ellipse reaching 0.65 AU from the Sun at perihelion and 1.102 AU at aphelion, a radial span of 0.452 AU.

Applying Kepler's third law to a = 0.876 AU gives an orbital period of 0.82 yr, or about 299 days.

An eccentricity of 0.258 makes the orbit moderately elongated.

The orbital plane is tilted 11.36° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 41.4 km/s at perihelion and falls to 24.5 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 = 25.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 26 observations and has a weighted RMS residual of 0.4533 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
0.876 AU
Eccentricity
0.2575
Perihelion
0.65 AU
Aphelion
1.10157 AU
Inclination
11.36°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
154.74°

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
2029-Aug-03 15:53 0.383819 AU
57418445 km
18.22 km/s
2030-Mar-15 11:56 0.341034 AU
51017964 km
12.94 km/s
2030-Oct-14 01:53 0.273334 AU
40890114 km
17.13 km/s
2039-Apr-01 08:24 0.323617 AU
48412484 km
12.58 km/s
2039-Oct-18 09:18 0.142955 AU
21385718 km
13.35 km/s
2043-Jul-30 22:49 0.192893 AU
28856404 km
7.77 km/s
2044-Jan-27 04:59 0.336347 AU
50316784 km
10.09 km/s
2048-Apr-19 12:59 0.300155 AU
44902503 km
11.50 km/s
2048-Oct-19 01:05 0.032293 AU
4830907 km
9.57 km/s
2052-Jul-27 08:41 0.238553 AU
35687026 km
11.69 km/s
2053-Feb-14 23:14 0.354449 AU
53024890 km
11.95 km/s
2057-May-07 15:36 0.282888 AU
42319441 km
10.00 km/s
2057-Oct-12 17:14 0.046314 AU
6928472 km
7.49 km/s
2061-Jul-31 19:14 0.365148 AU
54625409 km
15.93 km/s
2062-Mar-06 02:55 0.351493 AU
52582606 km
12.83 km/s
2062-Oct-11 18:43 0.383876 AU
57427019 km
19.21 km/s
2066-Jun-09 03:26 0.240254 AU
35941476 km
6.70 km/s
2066-Sep-14 17:00 0.140110 AU
20960192 km
7.12 km/s
2071-Mar-29 02:14 0.330743 AU
49478520 km
12.69 km/s
2071-Oct-17 23:40 0.170345 AU
25483258 km
14.01 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
25.9

Orbit Quality

RMS
0.45328
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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