SpaceAtlas Space Object Data
NASA JPL SBDB · 828399

828399

828399 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.919 AU it takes 2.66 yr to circle the Sun.

Apollo Observations: 731
Orbital Period · P
2.66 yr
v(q)
44.1 km/s
v(Q)
10.5 km/s
Diameter · ≈
0.85 km
TJ
3.66
Eccentricity · e
0.6163

Orbit and dynamics

The path is an ellipse reaching 0.736 AU from the Sun at perihelion and 3.102 AU at aphelion, a radial span of 2.366 AU.

Applying Kepler's third law to a = 1.919 AU gives an orbital period of 2.66 yr, or about 971 days.

The high eccentricity (0.616) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 8.18° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.1 km/s at perihelion and falls to 10.5 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 = 18.11 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.85 km.

Observation record and orbit quality

The current orbit solution is based on 731 observations and has a weighted RMS residual of 0.4265 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
1.919 AU
Eccentricity
0.6163
Perihelion
0.736 AU
Aphelion
3.10168 AU
Inclination
8.18°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
149.73°

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-Dec-03 00:16 0.191560 AU
28656993 km
13.05 km/s
2035-Nov-12 20:04 0.110009 AU
16457064 km
13.92 km/s
2043-Oct-30 11:42 0.082690 AU
12370248 km
17.50 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
18.11

Orbit Quality

RMS
0.4265
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

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