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17285 Bezout

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Also known as (17285) Bezout, Bezout

asteroid

In the Vinony graph

Within Vinony's link graph, 17285 Bezout connects to HTML element, list of minor planets: 17001–18000 and JPL Small-Body Database.

Vinony files it under Astronomical objects discovered in 2000, Background asteroids and Discoveries by Paul G. Comba.

Its subject is documented across 15 Wikipedia language editions.

Picture of the Day · NASA

Pathfinder on Mars

Pathfinder on Mars

2026-07-04

On July 4th, 1997, using its own array of fireworks, a parachute, and a cocoon of airbags, the Mars Pathfinder spacecraft bounced like a giant beach ball at least 15 times before it came to rest on the surface of Mars at 10:07 AM Pacific Daylight Time. After its then novel airbag-assisted landing sequence was completed, Pathfinder transmitted this color mosaic to mission operators on Earth. In the scene from another world, the Mars Sojourner robot rover is visible in the foreground, crouched on top of the unfolded Pathfinder. About the size of a large house cat, the six-wheeled, solar-powered Sojourner became the first successful Martian rover. Surrounding Pathfinder are deflated airbags and the rock-strewn terrain of the Ares Vallis floodplain. In the distance Martian hills appear against a dusty brownish sky. The Pathfinder lander was subsequently renamed the Carl Sagan Memorial Station.

via NASA APOD

Small body data

17285 Bezout (2000 NU)

Orbit class
Main-belt Asteroid
Absolute magnitude
13.840 H
Earth MOID
1.190 AU
Semi-major axis
2.646 AU
Eccentricity
0.170
Inclination
2.815 °

via NASA/JPL Small-Body Database · Minor Planet Center

Wikidata facts

Instance of
asteroid
Named after
Étienne Bézout
Followed by
17286 Bisei
Parent body
Sun
Minor-planet group
asteroid belt
Orbital period
1571.903375510188
Show 15 more facts
discoverer or inventor
Paul G. Comba
site of astronomical discovery
Prescott Observatory
provisional designation
2000 NU
time of discovery or invention
2000-07-03
orbital eccentricity
0.1699813511213509
absolute magnitude
13.84
orbital inclination
2.814902575316435
periapsis
2.19603604068532
apoapsis
3.095498176412461
semi-major axis of an orbit
2.645767108548891
mean anomaly
287.5478780418219
longitude of ascending node
141.4371162985435
argument of periapsis
200.2075232450767
time of periapsis
2461316.854819636
Sources (2)

via Wikidata · CC0

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