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- Kosmos_26 abstract "Kosmos 26 (Russian: Космос 26 meaning Cosmos 26), also known as DS-MG No.1 was a technology demonstration satellite which was launched by the Soviet Union in 1964 as part of the Dnepropetrovsk Sputnik programme. Its primary mission was to demonstrate an electric gyrodyne orientation system. It also carried a magnetospheric research package as a secondary payload.It was launched aboard a Kosmos-2I 63S1 rocket from pad 2 of the Mayak Launch Complex at Kapustin Yar. The launch occurred at 15:07 UTC on 18 March 1964.Kosmos 26 was placed into a low Earth orbit with a perigee of 268 kilometres (167 mi), an apogee of 376 kilometres (234 mi), 48.9 degrees of inclination, and an orbital period of 91 minutes. It decayed from orbit on 28 September 1964. Kosmos 26 was the first of two DS-MG satellites to be launched, the other being Kosmos 49.".
- Kosmos_26 cosparId "1964-013A".
- Kosmos_26 wikiPageID "22962515".
- Kosmos_26 wikiPageRevisionID "588850599".
- Kosmos_26 apsis "gee".
- Kosmos_26 cosparId "1964".
- Kosmos_26 decayDate "1964-09-28".
- Kosmos_26 hasPhotoCollection Kosmos_26.
- Kosmos_26 launchDate "--03-18".
- Kosmos_26 launchRocket "Kosmos-2I 63S1".
- Kosmos_26 launchSite Kapustin_Yar.
- Kosmos_26 launchSite Mayak_Launch_Complex.
- Kosmos_26 manufacturer Yuzhnoye_Design_Bureau.
- Kosmos_26 missionType "Technology".
- Kosmos_26 name "Kosmos 26".
- Kosmos_26 orbitInclination "48.9".
- Kosmos_26 orbitPeriod "5460.0".
- Kosmos_26 orbitReference Geocentric_orbit.
- Kosmos_26 orbitRegime Low_Earth_orbit.
- Kosmos_26 spacecraftType DS-MG.
- Kosmos_26 subject Category:1964_in_the_Soviet_Union.
- Kosmos_26 subject Category:Kosmos_satellites.
- Kosmos_26 subject Category:Spacecraft_launched_in_1964.
- Kosmos_26 subject Category:Spacecraft_which_reentered_in_1964.
- Kosmos_26 type ArtificialSatellite.
- Kosmos_26 type Satellite.
- Kosmos_26 type Thing.
- Kosmos_26 comment "Kosmos 26 (Russian: Космос 26 meaning Cosmos 26), also known as DS-MG No.1 was a technology demonstration satellite which was launched by the Soviet Union in 1964 as part of the Dnepropetrovsk Sputnik programme. Its primary mission was to demonstrate an electric gyrodyne orientation system. It also carried a magnetospheric research package as a secondary payload.It was launched aboard a Kosmos-2I 63S1 rocket from pad 2 of the Mayak Launch Complex at Kapustin Yar.".
- Kosmos_26 label "Cosmos 26".
- Kosmos_26 label "Kosmos 26".
- Kosmos_26 label "Kosmos 26".
- Kosmos_26 label "Космос-26".
- Kosmos_26 label "コスモス26号".
- Kosmos_26 sameAs Cosmos_26.
- Kosmos_26 sameAs コスモス26号.
- Kosmos_26 sameAs Kosmos_26.
- Kosmos_26 sameAs m.063_t2d.
- Kosmos_26 sameAs Q53014.
- Kosmos_26 sameAs Q53014.
- Kosmos_26 wasDerivedFrom Kosmos_26?oldid=588850599.
- Kosmos_26 isPrimaryTopicOf Kosmos_26.