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Meteor-M No. 2-4

active
Admin Edit
Orbit: LEOLaunched 2/29/2024
Technical Specifications
Verified technical details
Dry Mass
3000 kg
Total Mass
3200 kg
Power
Unknown
Design Life
Unknown
Stakeholders

Operator

Rosgidromet NITs Planeta

Manufacturer

Rosgidromet NITs Planeta
Launch Mission

Meteor-M No. 2-4 Mission

2/29/2024

Entity Mentions
All verified mentions of this entity in source documents

As of March 2, 2024 the press kit lists first upper stage main engine ignition at T+10 minutes 24 seconds, second upper stage main engine ignition at T+57 minutes 44 seconds, and Meteor-M No. 2-4 separation at T+59 minutes 46 seconds.

Mentioned as: Meteor-M No. 2-4SourceFeb 3, 2026

On February 29, 2024 the launch included the Meteor-M No. 2-4 satellite, Zorkiy-2M No. 2, Marafon-D GVM, sixteen SITRO-AIS cubesats for Sputnix, and Iran's Pars-1 imaging satellite.

Mentioned as: Meteor-M No. 2-4SourceFeb 3, 2026

On February 29, 2024 at 05:43 UTC a Soyuz-2.1b/Fregat launched the Meteor-M No. 2-4 weather satellite from the Vostochny Cosmodrome.

Mentioned as: Meteor-M No. 2-4SourceFeb 3, 2026

As of January 15, 2024, the launch of the Soyuz-2.1b launch vehicle with the Fregat upper stage carrying Meteor-M No. 2-4 and associated payloads from the Vostochny Cosmodrome was scheduled for the first quarter of 2024.

Mentioned as: Meteor-M No. 2-4SourceFeb 3, 2026

As of March 2, 2024 the Meteor-M No. 2-4 press kit listed the Meteor-M No. 2-4 satellite mass as 3.2 t, an active period of 5 years, and an average working orbit height of 820 km.

Mentioned as: Meteor-M No. 2-4SourceFeb 3, 2026

As of January 15, 2024, the refueling and neutralization station of the Vostochny Cosmodrome started refueling the Fregat upper stage for the launch of the Meteor-M No. 2-4 satellite.

Mentioned as: Meteor-M No. 2-4SourceFeb 3, 2026