SpaceAtlas Space Object Data
LINEAR
NASA JPL SBDB · 2003 W1

LINEAR

LINEAR follows a distinctly cometary orbit: an eccentricity of 0.934 carries it from 1.652 AU at perihelion out to 48.686 AU at aphelion.

comet Observations: 95
Encyclopedia excerpt
The Lincoln Near-Earth Asteroid Research (LINEAR) project is a collaboration of the United States Air Force, NASA, and the Massachusetts Institute of Technology's Lincoln Laboratory for the systematic detection and tracking of near-Earth objects. LINEAR was responsible for the majority of asteroid discoveries from 1998 until it was overtaken by the Catalina Sky Survey in 2005. As of 15 September 2011, LINEAR had detected 231,082 new small Solar System bodies, of which at least 2,423 were near-Earth asteroids and 279 were comets. The instruments used by the LINEAR program are located at Lincoln Laboratory's Experimental Test Site (ETS) on the White Sands Missile Range (WSMR) near Socorro, New Mexico.
Orbital Period · P
126 yr
v(q)
32.2 km/s
v(Q)
1.1 km/s
TJ
0.53
Eccentricity · e
0.9343

Orbit and dynamics

The path is an ellipse reaching 1.652 AU from the Sun at perihelion and 48.686 AU at aphelion, a radial span of 47.034 AU.

Applying Kepler's third law to a = 25.17 AU gives an orbital period of 126 yr, or about 46,123 days.

The high eccentricity (0.934) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 78.08° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 32.2 km/s at perihelion and falls to 1.1 km/s at aphelion.

Its Tisserand parameter with respect to Jupiter is T_J = 0.53, a standard discriminator between asteroidal and cometary dynamics.

Size and surface

Neither a measured diameter nor a reliable absolute magnitude is available for LINEAR, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 95 observations and has a weighted RMS residual of 0.7166 arcseconds.

Condition code U = 5 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
25.17 AU
Eccentricity
0.9343
Perihelion
1.652 AU
Aphelion
48.686331 AU
Inclination
78.08°
Orbital Period
— yr
Epoch
2452979.5
Mean Anomaly
0.21°

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

No close approaches to Earth are currently on record for this object.

Physical Parameters

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

Orbit Quality

RMS
0.71658
Condition
5
Orbit ID
—
Data source: NASA JPL Small-Body Database . 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.