SpaceAtlas Space Object Data
NASA JPL SBDB · 2007 UP6

2007 UP6

2007 UP6 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.968 AU and a period of 0.95 yr.

Aten Observations: 84
Orbital Period · P
0.95 yr
v(q)
33.3 km/s
v(Q)
27.5 km/s
Diameter · ≈
0.09 km
TJ
6.22
Eccentricity · e
0.0943

Orbit and dynamics

The path is an ellipse reaching 0.877 AU from the Sun at perihelion and 1.059 AU at aphelion, a radial span of 0.182 AU.

Applying Kepler's third law to a = 0.968 AU gives an orbital period of 0.95 yr, or about 348 days.

With e = 0.094, the orbit is close to circular.

The orbital plane is tilted 9.58° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.3 km/s at perihelion and falls to 27.5 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 = 23 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

The current orbit solution is based on 84 observations and has a weighted RMS residual of 0.4948 arcseconds.

Condition code U = 2 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
0.9678 AU
Eccentricity
0.0943
Perihelion
0.877 AU
Aphelion
1.059064 AU
Inclination
9.58°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
316.9°

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
2027-Oct-26 21:32 0.061627 AU
9219267 km
5.18 km/s
2028-May-17 07:21 0.154852 AU
23165506 km
5.83 km/s
2029-Mar-18 22:43 0.133959 AU
20040028 km
7.76 km/s
2030-Feb-23 16:24 0.407705 AU
60991832 km
15.78 km/s
2045-Oct-27 12:02 0.362572 AU
54240011 km
14.93 km/s
2046-Oct-21 07:43 0.063712 AU
9531164 km
6.95 km/s
2047-Jun-29 02:07 0.201834 AU
30193863 km
4.76 km/s
2048-Apr-08 12:13 0.081958 AU
12260689 km
5.98 km/s
2049-Mar-04 21:33 0.274176 AU
41016165 km
11.78 km/s
2065-Oct-25 23:16 0.318221 AU
47605233 km
13.64 km/s
2066-Oct-21 14:37 0.028559 AU
4272432 km
6.23 km/s
2067-Jun-18 14:58 0.194414 AU
29083889 km
5.13 km/s
2068-Apr-06 01:31 0.077856 AU
11647144 km
6.08 km/s
2069-Mar-06 00:24 0.276236 AU
41324290 km
11.86 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
23.0

Orbit Quality

RMS
0.49484
Condition
2
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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