SpaceAtlas Space Object Data
NASA JPL SBDB · 889795

889795

889795 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.328 AU it takes 1.53 yr to circle the Sun.

Apollo Observations: 101
Orbital Period · P
1.53 yr
v(q)
61.3 km/s
v(Q)
10.9 km/s
Diameter · ≈
0.22 km
TJ
4.64
Eccentricity · e
0.698

Orbit and dynamics

Between its closest point (0.401 AU) and its farthest (2.255 AU), the heliocentric distance changes by 1.854 AU over every revolution.

One full revolution takes 1.53 yr (559 days), computed from the semi-major axis of 1.328 AU.

The high eccentricity (0.698) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.06° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 61.3 km/s at perihelion and falls to 10.9 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 = 21.04 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.22 km.

Observation record and orbit quality

Astrometry from 101 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4751 arcseconds.

Condition code U = 0 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
1.328 AU
Eccentricity
0.698
Perihelion
0.401 AU
Aphelion
2.254944 AU
Inclination
4.06°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
347.09°

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
2038-Nov-17 01:14 0.140819 AU
21066202 km
19.43 km/s
2046-Apr-02 09:05 0.136435 AU
20410395 km
19.78 km/s
2064-Nov-22 23:33 0.025039 AU
3745727 km
24.09 km/s
2069-Mar-25 00:41 0.081661 AU
12216309 km
25.67 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
21.04

Orbit Quality

RMS
0.47508
Condition
0
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.