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6996 Alvensleben

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Also known as Alvensleben

asteroid

In the Vinony graph

Within Vinony's link graph, 6996 Alvensleben connects to HTML element, list of minor planets: 6001–7000 and JPL Small-Body Database.

Vinony files it under Astronomical objects discovered in 1973, Background asteroids and Discoveries by Cornelis Johannes van Houten.

Its subject is documented across 22 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

(6996) Alvensleben

Orbit class
Outer belt
Semi-major axis
3.435 AU
Eccentricity
0.094
Inclination
4.101 °
Absolute magnitude
12.340 H

via Minor Planet Center

Wikidata facts

Instance of
asteroid
Followed by
6997 Laomedon
Parent body
Sun
Diameter
18.809
Orbital period
2319.877303837463
Show 16 more facts
discoverer or inventor
Tom Gehrels
site of astronomical discovery
Palomar Observatory
provisional designation
2222 T-2
time of discovery or invention
1973-09-29
orbital eccentricity
0.09592436439487252
absolute magnitude
12.34
orbital inclination
4.098652214109995
periapsis
3.100624384534914
apoapsis
3.758590182086084
semi-major axis of an orbit
3.429607283310498
mean anomaly
154.06074241325
longitude of ascending node
157.7519895264698
argument of periapsis
119.1012956554931
albedo
0.06
time of periapsis
2460007.716611842
Sources (2)

via Wikidata · CC0

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