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Launch FailureRussian Federal Space Agency (ROSCOSMOS)

Soyuz 2.1b/Fregat: Meteor-M No.2-1 & rideshare payloads

This is the third spacecraft in the Russian Meteor-M series of remote sensing satellites. Weighing about 2750 kg, it is intended to gather hydrometeorological data from sun-synchronous orbit. This includes monitoring ozone layer and radiation levels in the near-Earth space, as well as monitoring ocean surface temperatures and ice conditions.

Failure:An algorithm glitch caused the Fregat upper stage to de-orbit.
Tuesday, 28 November 2017
Soyuz 2.1b/Fregat: Meteor-M No.2-1 & rideshare payloads

Mission Data

Russian Federal Space Agency (ROSCOSMOS)
🇷🇺Russian Federal Space Agency (ROSCOSMOS)Est. 1992
Launch VehicleSoyuz 2.1b Fregat
Vehicle FamilySoyuz
Vehicle Record24 of 26 launches (92.3%)
Provider TypeGovernment
Agency Record333 successes / 11 failures (97%)
Success Streak68 consecutive
Mission TypeEarth Science
Target OrbitSun-Synchronous Orbit
Launch PadCosmodrome Site 1S
Location🇷🇺 Vostochny Cosmodrome, Siberia, Russian Federation RUS
Orbital Launches This Year#80
Agency Launches This Year#8
Launches From This Pad20
Launches From This Site21
Status Note

Either the launch vehicle did not reach orbit, or the payload(s) failed to separate.

About Soyuz 2.1b Fregat

Soyuz-2, GRAU index 14A14, is the collective designation for the 21st-century version of the Russian Soyuz rocket. In its basic form, it is a three-stage carrier rocket for placing payloads into low Earth orbit. The first-stage boosters and two core stages feature uprated engines with improved injection systems, compared to the previous versions of the Soyuz. Digital flight control and telemetry systems allow the rocket to be launched from a fixed launch platform, whereas the launch platforms for earlier Soyuz rockets had to be rotated as the rocket could not perform a roll to change its heading in flight. The Soyuz 2.1b represents the latest development stage of the proven rocket. It uses the new RD-0124 engines in the first three stages, coupled with an improved injection system that significantly boosts the performance of the Soyuz. Furthermore, she wears a new, digital startup control system. This will allow the Soyuz 2.1b to carry around 1.2 tonnes more payload into low earth orbit compared to its predecessor.

Launch Site

Cosmodrome Site 1S · 51.8844°N 128.3339°E

Launch data from Launch Library 2 by The Space Devs.