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Introduction
SAC-A
SAC-B
Configuration
Mission profile
Scientific payload
SAC-C
MMRS
SAOCOM
Ground segment

Mision Profile

 

General

Design Life:

3 year

Satellite mass:

190 kg

Payload:
  

Sun Observation and Cosmic Radiation Instruments

 

Spacecraft Attitude Control

Accuracy

± 3 Degrees

Knowledge:

± 2 Degrees (Post Facto)

Spacecraft Power

260 W (BOL)

 

Orbit

Type:

Circular Orbit

Altitude:

560 km (stable for lifetime)

Inclination:

38 Degrees

Ground Track error

+/- 10 km (EOL)

Eccentricity:

< 0.05