SpaceAtlas Space Object Data
NASA JPL SBDB · 277570

277570

277570 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.372 AU it takes 1.61 yr to circle the Sun.

Apollo Observations: 250
Orbital Period · P
1.61 yr
v(q)
52.2 km/s
v(Q)
12.4 km/s
Diameter · ≈
0.48 km
TJ
4.6
Eccentricity · e
0.617

Orbit and dynamics

The path is an ellipse reaching 0.526 AU from the Sun at perihelion and 2.219 AU at aphelion, a radial span of 1.693 AU.

Applying Kepler's third law to a = 1.372 AU gives an orbital period of 1.61 yr, or about 587 days.

The high eccentricity (0.617) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.11° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 52.2 km/s at perihelion and falls to 12.4 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

The measured diameter is 0.44 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.177 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 250 observations and has a weighted RMS residual of 0.6035 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
1.372 AU
Eccentricity
0.617
Perihelion
0.526 AU
Aphelion
2.218524 AU
Inclination
4.11°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
284.52°

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
2039-Jun-28 02:39 0.017604 AU
2633530 km
19.73 km/s
2047-Jul-09 00:09 0.191255 AU
28611320 km
14.00 km/s
2059-Jan-22 16:41 0.049434 AU
7395176 km
18.18 km/s
2067-Feb-01 03:43 0.156418 AU
23399782 km
24.21 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.439 km
Albedo
0.177
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.34

Orbit Quality

RMS
0.60345
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.

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