Resurs O1-4

Russia



Launch data:

Designation 25394 / 98043A
Launch date10 Jul 1998
Launch site Baikonur, LC-45L
Launch vehicle  Zenit-2 (#29)
MissionRemote sensing
Earth orbit:
Perigee/Apogee 815 / 818 km
Inclination 98.8°
Period 101.2 min

Also carries a LLMSIRIS payload.

In mid-Apr 1999 it is known that a transmitter (8.2 GHz?) has failed.

Specifications

Prime contractor  
Platform  
Mass at launch 1950 kg
Mass in orbit  
Dimension  
Solar array  
Stabilization  
DC power  
Design lifetime  

Downlinks at 137.40 MHz & APT on 137.85 MHz. Some downlink is also heard on 400 MHz, might come from a piggy-back package.

MSU-SK (5-channel visible and IR scanner):

Wavebands 0.5-0.6 µm, 0.6-0.7 µm, 0.7-08 µm, 0.8-1.0 µm, 10.4-12.6 µm + a 6th one
Resolution 161 m (4 channels), 528 m (1 channel)
Swath width 714 km

MSU-E (3-channel steerable push-broom scanner):

Wavebands 0.5-0.67 µm, 0.65-0.8 µm, 0.8-1.0 µm
Resolution 30 m
Swath width 60 km

Downlink: 8.2 GHz, 16 mbps

Scarab 2 (Scanner for Radiation Budget):

Telescopes wavebands 0.2 - 4 µm (solar reflections)
4 - 100 µm (earth IR)
10.5 - 12.5 µm (IR)
0.5 - 0.7 µm (visible)

40 kg. Scarab 2's flight has been paid for by the CNES. Should have 2 years of lifetime


Ref: #15 - update: 24.10.04