Earth observation satellite system

Слайд 2

RUSSIAN HYDROMETEOROLOGICAL SATELLITE SYSTEM METEOR №1 METEOR №2 METEOR №3 Oceanographical

RUSSIAN HYDROMETEOROLOGICAL SATELLITE SYSTEM

METEOR №1

METEOR №2

METEOR №3
Oceanographical

ELECTRO №2
(14° E.)

ELECTRO №1
(76° E.)

ГЕОСТАЦИОНАРНАЯ

ОРБИТА

ПОЛЯРНАЯ ОРБИТА

850 км

35600 км

Слайд 3

Russian Earth Observation Satellites Program 2006-2015 2006 2007 2008 2009 2010

Russian Earth Observation Satellites Program 2006-2015

2006 2007 2008 2009 2010 2011

2012 2013 2014 2015 2016 2017 2018 2019 2020

ELECTRO № 1 (76°E)

ELECTRO № 2 (location TBD)

ELECTRO № 3 (76°E)

METEOR № 1

METEOR № 2

METEOR № 3 (Oceanographical )

METEOR № 5

METEOR № 4

METEOR № 6 (Oceanographical )

KANOPUS-V № 1

KANOPUS-V № 2

RESURS-P № 1

RESURS-P № 2

Geostationary
meteorological system

Polar-orbiting
meteorological system

R&D
environmental satellites

Слайд 4

ELECTRO-L General Design • Three-axis high-precision stabilization • In-orbit mass -

ELECTRO-L General Design

• Three-axis high-precision stabilization
• In-orbit mass - 1500 kg

Payload mass - 370  kg
• Lifetime - 10 years
• Longitude - 76E
• Data dissemination format - HRIT/LRIT
• Image repeat cycle – 30/15 min

Mission objectives
• Operational observation of the
atmosphere and the Earth surface
(MSU-GS)
• Heliogeophysical measurements
• Maintaining Data Collection System
and COSPAS/SARSAT Service

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MSU-GS Basic Performance Characteristics 10 Lifetime of basic and reserve units

MSU-GS Basic Performance Characteristics

10

Lifetime of basic and reserve units (years)

9.

≤ 88

Weight

(kg)

8.

≤ 150

Power (W)

7.
0.8
0.4
0.1-0.2

NEΔT at 300K (K)
∙ in the band 3.5-4.0 μm
∙ in the band 5.7-7.0 μm
∙ in the band 7.5-12.5 μm

6.

≥ 200

S/N ratio for VIS channels

5.

1.0 (VIS); 4.0 (IR)

HRIT ground resolution in subsatellite point (km)

4.

20 ± 0.5 x 20 ± 0.5

Image frame (deg x deg)

3.

0.5-0.65; 0.65-0.80;0.8-0.9; 3.5-4.0;
5.7-7.0; 7.5-8.5;8.2-9.2; 9.2-10.2;
10.2-11.2; 11.2-12.5

Spectral range at half maximum of spectral response function (μm)

2.

10
3
7

Number of channels
∙ VIS
∙ IR

1.

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METEOR-M General Design • In-orbit mass – 2700 kg • Payload

METEOR-M General Design

• In-orbit mass –  2700 kg
• Payload mass

– 1200 kg
• Lifetime – 5 years
• Orbit – Sunsynchronous
• Altitude – 830 km
• Data dissemination format – HRPT/LRPT
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METEOR-M Mission Objectives and Basic Instruments Instrument * - to be launched on board METEOR-M №2

METEOR-M Mission Objectives and Basic Instruments
Instrument

* - to be launched on

board METEOR-M №2
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RESURS-DK General Design RESURS-DK Instruments Payload • In-orbit mass - 6570

RESURS-DK General Design

 

 

RESURS-DK Instruments Payload
• In-orbit mass - 6570 kg

Payload mass - 1200 kg
• Lifetime - 3 years
• Orbit – elliptical, H=360-604 km
• Inclination – 70,4°
• Launched 15.06.2006

Swath Width - 28,3 / 448 km
Spectral Bands - 0,58-0,8; 0,45-0,5; 0,55-0,59; 0,65-0,68; 0,72-0,75; 0,75-0,78; 0,78-0,9; 0,9-1,1 μm
Resolution
panchromatic system - 1 m
multi spectral system - 2-3 m

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3 Main centers: Europe (Moscow-Obninsk-Dolgoprudny) Siberia (Novosibirsk) Far-East (Khabarovsk) ∙ -

3 Main centers:
Europe
(Moscow-Obninsk-Dolgoprudny)
Siberia
(Novosibirsk)
Far-East (Khabarovsk)
∙ - 68 Local centers

Roshydromet Satellite Ground Segment