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سیارک ۲۹۵۶

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Also known as Yeomans, (2956) Yeomans

سیارک

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

Key facts

Discovered by
E. Bowell
Discovery site
Anderson Mesa Stn.
Discovery date
28 April 1982
Named after
Donald Keith Yeomans , (American astronomer)
Alternative designations
1982 HN 1 · 1950 JG, 1974 RN 1 · 1977 DL 10
Minor planet category
main-belt · ( middle )
Observation arc
42.45 yr (15,504 days)
Aphelion
3.0155 AU
Perihelion
2.5142 AU
Semi major axis
2.7648 AU
Orbital period sidereal
4.60 yr (1,679 days)
Mean anomaly
229.98 °
Mean motion
0° 12 51.84 / day
Inclination
2.8688°
Longitude of ascending node
112.21°
Argument of perihelion
124.34°
Dimensions
9.350 ± 0.183 km , 11.30 km (derived)
Synodic rotation period
3.4 ± 0.1 h , 3.509 ± 0.0158 h

via Wikipedia infobox

Wikidata facts

Diameter
9.35
Orbital period
1678.555234136033
Show 14 more facts
provisional designation
1982 HN1
time of discovery or invention
1982-04-28
orbital eccentricity
0.09091553957851549
orbital inclination
2.870145743977625
periapsis
2.512825750914961
apoapsis
3.015430115981992
semi-major axis of an orbit
2.764127933448477
mean anomaly
154.8968646196984
longitude of ascending node
112.1867068987377
argument of periapsis
122.5441628909002
absolute magnitude
12.37
albedo
0.292
rotation period
3.4
time of periapsis
2460278.2696031705
Sources (3)

via Wikidata · CC0

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