About: Kosmos 66

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Kosmos 66 (Russian: Космос 66 meaning Cosmos 66) or Zenit-2 No.27 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1965. A Zenit-2 spacecraft, Kosmos 66 was the twenty-seventh of eighty-one such satellites to be launched and had a mass of 4,730 kilograms (10,430 lb).

Attributes	Values
rdf:type	Thing schema:Event dul:Event societal event wikidata:Q1656682 wikidata:Q2133344 yago:Artifact100021939 yago:Equipment103294048 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:WikicatKosmosSatellites yago:WikicatZenit-2Satellites event space mission yago:Satellite104137444 yago:Whole100003553 ArtificialSatellite
rdfs:label	Kosmos 66 (en) Kosmos 66 (pl)
rdfs:comment	Kosmos 66 – radziecki satelita rozpoznawczy; statek serii Zenit-2 , którego konstrukcję oparto o załogowe kapsuły Wostok. Misja nieudana – w wyniku nierozłożenia się spadochronu hamującego kapsuła powrotna rozbiła się. (pl) Kosmos 66 (Russian: Космос 66 meaning Cosmos 66) or Zenit-2 No.27 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1965. A Zenit-2 spacecraft, Kosmos 66 was the twenty-seventh of eighty-one such satellites to be launched and had a mass of 4,730 kilograms (10,430 lb). (en)
foaf:name	Kosmos 66 (en)
name	Kosmos 66 (en)
dcterms:subject	Spacecraft which reentered in 1965 Spacecraft launched in 1965 Kosmos satellites Zenit-2 satellites
Wikipage page ID	41391597 (xsd:integer)
Wikipage revision ID	1095515900 (xsd:integer)
Link from a Wikipage to another Wikipage	Apsis Vostok-2 (rocket) International Designator Geocentric orbit Zenit (satellite) Orbital period Baikonur Cosmodrome Baikonur Cosmodrome Site 31 Spacecraft which reentered in 1965 Kosmos (satellite) Spacecraft launched in 1965 Kosmos satellites Zenit-2 satellites OKB-1 Soviet Union Orbital inclination Satellite Catalog Number Low Earth orbit Reconnaissance satellite
sameAs	Kosmos 66 Kosmos 66 Kosmos 66 Kosmos 66 Kosmos 66 Kosmos 66 Kosmos 66 Kosmos 66 Kosmos 66
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_spaceflight dbt:Portal dbt:Reflist dbt:Short_description dbt:Use_British_English dbt:Use_dmy_dates dbt:USSR-spacecraft-stub dbt:Orbital_launches_in_1965 dbt:Zenit-2_satellites
landing date	1965-05-15 (xsd:date)
apsis	gee (en)
COSPAR ID	1965 (xsd:integer)
launch contractor	OKB-1
launch date	0001-05-07 (xsd:gMonthDay)
launch rocket	Vostok-2 (rocket)
launch site	Baikonur Cosmodrome Baikonur Cosmodrome Site 31
manufacturer	OKB-1
mission duration	691200.0 (second)
mission type	Optical imaging reconnaissance (en)
operator	OKB-1
orbit inclination	65 (xsd:integer)
orbit period	5358.0 (second)
orbit reference	Geocentric orbit
orbit regime	Low Earth orbit
SATCAT	1362 (xsd:integer)
spacecraft type	Zenit (satellite)
has abstract	Kosmos 66 (Russian: Космос 66 meaning Cosmos 66) or Zenit-2 No.27 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1965. A Zenit-2 spacecraft, Kosmos 66 was the twenty-seventh of eighty-one such satellites to be launched and had a mass of 4,730 kilograms (10,430 lb). Kosmos 66 was launched by a Vostok-2 rocket, serial number R15002-04, flying from Site 31/6 at the Baikonur Cosmodrome. The launch took place at 09:50 GMT on 7 May 1965, and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1965-035A and the Satellite Catalog Number 01362. Kosmos 66 was operated in a low Earth orbit, on 7 May 1965 it had a perigee of 202 kilometres (126 mi), an apogee of 282 kilometres (175 mi), an inclination of 65.0° and an orbital period of 89.3 minutes. On 15 May 1965, after eight days in orbit, the satellite was deorbited so that its return capsule could be recovered and its photos analysed, however, the mission was unsuccessful because a parachute deployment failed and the spacecraft was destroyed in the subsequent crash. (en) Kosmos 66 – radziecki satelita rozpoznawczy; statek serii Zenit-2 , którego konstrukcję oparto o załogowe kapsuły Wostok. Misja nieudana – w wyniku nierozłożenia się spadochronu hamującego kapsuła powrotna rozbiła się. (pl)
disposal type	Crashed (en)
launch mass	4730.0 (kilogram)
orbit apoapsis	282.0 (kilometre)
orbit epoch	1965-05-07 (xsd:date)
orbit periapsis	202.0 (kilometre)
gold:hypernym	Satellite
prov:wasDerivedFrom	wikipedia-en:Kosmos_66?oldid=1095515900&ns=0
mission duration (μ)	8.0 (day)
page length (characters) of wiki page	4411 (xsd:nonNegativeInteger)
COSPAR id	1965-035A
landing date	1965-05-15 (xsd:date)
launch date	1965-05-07 (xsd:date)

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