Official name METEOR 3M
Alternative name Meteor-3M No. 1
Cospar ID 2001-056A
Norad ID 27001
Launch date 2001-12-10
Launch site TTMTR
Launch vehicle Zenit-2
Country/Organization Russia
Type application Meteorology
Operator Roskosmos
RCS size LARGE
Decay date ON ORBIT
Period (min) 105.19
Inclination (deg) 99.77
Perigee (km) 993
Apogee (km) 1013
Eccentricity 0.00997008973080758
Mean motion (revs. per day) 13.6895142123776
Semi-Major axis (km) 7381.135
Raan (deg) 294.2092
Arg of perigee (deg) 3.2043
Shape Cyl + 2 Pan
Mass (kg) 2476
Diameter (m) 2.9
Height (m) 6.5
Span (m^2) 14
Lifetime 3 years (design), 4 years (achieved)
Contractors NPP VNIIEM
Equipment see above
Configuration SP-2 bus
Power 2 deployable solar arrays, batteries

The Meteor-3M spacecraft series represented a follow-up to the Meteor-3 series to provide a modernization of Russia's national meteorological satellite system sponsored by Roskosmos.

The overall objective are environmental monitoring in the following fields:

  • Monitoring of ocean and land surfaces
  • Meteorological observations: Distribution of cloud data and vertical ozone profiles, monitoring of global atmospheric parameters such as temperature and water vapor profiles and to obtain sea surface wind profiles and SST
  • Measurement of vertical profiles of aerosol, ozone and other constituents in the atmosphere (SAGE-III)
  • Measurement space environment parameters (space weather) such as: particle fluxes and radiation density fluxes.

On Meteor-3M-1 carried the US instrument SAGE-3, which was flown as a joint mission of Rosaviakosmos and NASA. A corresponding cooperative agreement was approved by the Gore-Chernomyrdin Commission on 16 December 1994.

The Meteor-3M-1 sensor complement consists of the following instruments: MR-2000-M1; KLIMAT; MIVZA; MTVZA; MSU-E; SAGE-III; SFM-2; KGI-4C, and MSGI-5EI.

Meteor-3M-1 was successfully launched on Dec. 10, 2001. It stopped functioning on 6 March 2006 due to a breakdown of its power supply system resulting in a loss of communications with the spacecraft. - The spacecraft (with a design life of 3 years) provided over 4 years of successful operations.

It was planned for the Meteor-3M series to combine the meteorological observations of the Meteor-3 series with the Earth-surface observations of the Resurs-O1 series, starting with Meteor-3M-2 with an originally planned launch in 2007.

The Meteor-3M-2 sensor complement was to consist of the following instruments: MTVZA, MSU-MR (2 instruments), MSU-SR (2 instruments), IKFS-2, MSGI-MKA, KGS-4S, a DCS (Data Collection System), RRA (RetroReflector Array), and SAGE-III of NASA/LaRC.

The Meteor-3M series was cancelled after the first mission in favor of the Meteor-M series.

Satellite COSPAR Date LS Launch Vehicle Remarks
METEOR 3M 2001-056A 2001-12-10 TTMTR Zenit-2 with Kompass, Badr B, Maroc-Tubsat, Reflector