SpaceAtlas Space Object Data
NASA JPL SBDB · 73P-T

Schwassmann-Wachmann

Schwassmann-Wachmann follows a distinctly cometary orbit: an eccentricity of 0.693 carries it from 0.94 AU at perihelion out to 5.182 AU at aphelion.

comet Observations: 44
Orbital Period · P
5.36 yr
v(q)
40 km/s
v(Q)
7.2 km/s
TJ
2.78
Eccentricity · e
0.693

Orbit and dynamics

The path is an ellipse reaching 0.94 AU from the Sun at perihelion and 5.182 AU at aphelion, a radial span of 4.242 AU.

Applying Kepler's third law to a = 3.061 AU gives an orbital period of 5.36 yr, or about 1,956 days.

The high eccentricity (0.693) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 11.4° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40 km/s at perihelion and falls to 7.2 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 = 2.78, a standard discriminator between asteroidal and cometary dynamics.

Size and surface

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

Observation record and orbit quality

The current orbit solution is based on 44 observations and has a weighted RMS residual of 0.9758 arcseconds.

Condition code U = 1 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
3.061 AU
Eccentricity
0.693
Perihelion
0.94 AU
Aphelion
5.182273 AU
Inclination
11.4°
Orbital Period
— yr
Epoch
2454375.5
Mean Anomaly
88.38°

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
2054-Aug-08 21:25 0.118197 AU
17682061 km
15.33 km/s
2070-May-26 20:28 0.085090 AU
12729281 km
12.02 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
0.97579
Condition
1
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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