SpaceAtlas Space Object Data
NASA JPL SBDB · 249P

LINEAR

LINEAR follows a distinctly cometary orbit: an eccentricity of 0.819 carries it from 0.502 AU at perihelion out to 5.038 AU at aphelion.

comet Observations: 884
Orbital Period · P
4.61 yr
v(q)
56.7 km/s
v(Q)
5.7 km/s
TJ
2.71
Eccentricity · e
0.8187

Orbit and dynamics

The path is an ellipse reaching 0.502 AU from the Sun at perihelion and 5.038 AU at aphelion, a radial span of 4.536 AU.

Applying Kepler's third law to a = 2.77 AU gives an orbital period of 4.61 yr, or about 1,684 days.

The high eccentricity (0.819) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 8.4° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 56.7 km/s at perihelion and falls to 5.7 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Its Tisserand parameter with respect to Jupiter is T_J = 2.71, 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 884 observations and has a weighted RMS residual of 0.5185 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
2.77 AU
Eccentricity
0.8187
Perihelion
0.502 AU
Aphelion
5.037799 AU
Inclination
8.4°
Orbital Period
— yr
Epoch
2456863.5
Mean Anomaly
255.31°

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
2029-Nov-03 23:32 0.056985 AU
8524816 km
26.93 km/s
2034-Apr-06 01:55 0.303348 AU
45380259 km
34.64 km/s
2043-Sep-15 00:58 0.420480 AU
62902948 km
19.80 km/s
2057-Oct-08 07:00 0.291124 AU
43551528 km
17.37 km/s
2062-Mar-29 19:57 0.466455 AU
69780621 km
39.49 km/s
2071-Nov-04 02:53 0.061142 AU
9146658 km
27.25 km/s
2076-Apr-23 10:41 0.050405 AU
7540543 km
24.23 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
—

Orbit Quality

RMS
0.51849
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.