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9415 Yujiokimura

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Also known as (9415) 1995 VE

asteroid

In the Vinony graph

Within Vinony's link graph, 9415 Yujiokimura connects to HTML element, list of minor planets: 9001–10000 and JPL Small-Body Database.

Vinony files it under Astronomical objects discovered in 1995, Background asteroids and Discoveries by Takao Kobayashi.

Vinony links it to 12 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

(9415) Yujiokimura

Orbit class
Main-belt
Semi-major axis
2.200 AU
Eccentricity
0.070
Inclination
3.076 °
Absolute magnitude
15.550 H

via Minor Planet Center

Wikidata facts

Instance of
asteroid
Followed by
9416 Miyahara
Parent body
Sun
Minor-planet group
asteroid belt
Diameter
2.422
Orbital period
1192.326943544707
Show 16 more facts
discoverer or inventor
Takao Kobayashi
site of astronomical discovery
Ōizumi Observatory
provisional designation
1997 GT6
time of discovery or invention
1995-11-01
orbital eccentricity
0.07041217439037906
absolute magnitude
15.55
orbital inclination
3.075633525655553
periapsis
2.045604708923031
apoapsis
2.355495762851176
semi-major axis of an orbit
2.200550235887103
mean anomaly
88.27840602231558
longitude of ascending node
4.916350152567984
argument of periapsis
36.19532934903504
albedo
0.276
time of periapsis
2460708.1202165736
Sources (2)

via Wikidata · CC0

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