SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 UP2

2025 UP2

2025 UP2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.947 AU and a period of 0.92 yr.

Aten Observations: 29
Orbital Period · P
0.92 yr
v(q)
34.9 km/s
v(Q)
26.8 km/s
Diameter · ≈
0.01 km
TJ
6.34
Eccentricity · e
0.1309

Orbit and dynamics

The path is an ellipse reaching 0.823 AU from the Sun at perihelion and 1.071 AU at aphelion, a radial span of 0.248 AU.

Applying Kepler's third law to a = 0.947 AU gives an orbital period of 0.92 yr, or about 336 days.

An eccentricity of 0.131 makes the orbit moderately elongated.

Its inclination of 2.04° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.9 km/s at perihelion and falls to 26.8 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 = 28.74 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 29 observations and has a weighted RMS residual of 0.4342 arcseconds.

Condition code U = 6 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
0.9467 AU
Eccentricity
0.1309
Perihelion
0.823 AU
Aphelion
1.070623 AU
Inclination
2.04°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
133.31°

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
2036-Jul-05 03:59 0.086382 AU
12922512 km
6.05 km/s
2037-Feb-23 03:23 0.166921 AU
24970989 km
4.85 km/s
2037-Oct-27 00:02 0.147872 AU
22121381 km
8.21 km/s
2048-May-24 12:46 0.099500 AU
14885053 km
2.26 km/s
2048-Aug-27 18:50 0.063914 AU
9561419 km
2.71 km/s
2048-Dec-23 02:15 0.117821 AU
17625803 km
2.76 km/s
2059-Jul-07 11:58 0.145766 AU
21806276 km
7.59 km/s
2060-Mar-06 11:35 0.166746 AU
24944879 km
4.84 km/s
2060-Oct-27 05:25 0.113244 AU
16941082 km
6.92 km/s
2071-May-08 19:47 0.116313 AU
17400154 km
3.02 km/s
2071-Sep-15 20:41 0.055084 AU
8240496 km
2.69 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
28.74

Orbit Quality

RMS
0.43422
Condition
6
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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