logo_db.gif (1248 bytes)
button1off.gif (600 bytes)button2off.gif (568 bytes)button3off.gif (465 bytes)button4off.gif (442 bytes)

Launch Schedules

button5off.gif (444 bytes)button6off.gif (559 bytes)button7off.gif (454 bytes)button8off.gif (413 bytes)button9on.gif (470 bytes)

   Meteor 3M-N1 - Summary
space.gif (43 bytes)

The 2500 kg (5510 lbm) Meteor 3M satellite was built by Elektromekhanika Research Institute (VNIIEM), Istra, and is designed for three years of service. Meteor 3M-N1 carries nine scientific instruments to provide various meteorological observations and images. Weather observations will include both visible and infrared images of the surface and clouds, cloud-top height maps, sea surface temperature measurements, and temperature and humidity profiles. The spacecraft will operate in a sun-synchronous orbit at 1018 km (550 nmi) with an inclination of 99.64 degrees.

Meteor 3M-N1

SPACECRAFT

Int'l Designation

2001 056A

Launched

Owner / Sponsor Rosaviakosmos
Mission Weather
Satellite Bus Elektromekhanika Research Institute (VNIIEM)

Meteor 3M

Launch Mass 2500 kg (5510 lbm)
Mission Orbit SSO / 1018 km (550 nmi), circular

99.64°

Design Life 3 years
Power (EOL)  

LAUNCH

Launch Vehicle Model Zenit 2
Launch Date / Time 2001 December 10

17:19

Co-Passenger(s) Badr B
  Maroc-Tubsat
  KOMPASS
  Reflektor

FINANCIAL

Satellite cost  
Web Links  

Copyright 2001 - Andrews Space & Technology
Andrews Space & Technology Privacy Statement and Copyright Information