Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Meteor-M No.2

From Wikipedia, the free encyclopedia
2014 Russian weather satellite
Meteor-M No.2
Mission typeWeather
OperatorRoscosmos/Roshydromet
COSPAR ID2014-037AEdit this at Wikidata
SATCATno.40069
Spacecraft properties
Launch mass2,700 kilograms (6,000 lb)
Start of mission
Launch date8 July 2014 (2014-07-08)
Launch siteBaikonur
Orbital parameters
Reference systemGeocentric
RegimeSun-synchronous
Perigee altitude825.5 kilometres (512.9 mi)[1]
Apogee altitude835.0 kilometres (518.8 mi)[1]
Inclination98.5 degrees[1]
Period101.4 minutes[1]

Meteor-M No.2 (also known asMeteor M2) was the second RussianMeteor-M series of polar-orbit weather satellite.[1] It was launched on aSoyuz-2.1b rocket with aFregat upper stage on 8 July 2014. It was designed to operate for 5 years.[1]

See also

[edit]

References

[edit]
  1. ^abcdef"METEOR M2 satellite details".N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved2019-08-20.
January
February
March
April
May
June
July
August
September
October
November
December
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).


Stub icon

Thisspacecraft orsatellite related article is astub. You can help Wikipedia byexpanding it.

Retrieved from "https://en.wikipedia.org/w/index.php?title=Meteor-M_No.2&oldid=1241621053"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp