EROS C

EROS C

EROS C [GDK]

The EROS C (Earth Resources Observation Systems C) satellite, which will offer higher Offering higher quality resolution and a higher data link rate than EROS A and EROS B, as well as multispectral imagery capabilities, is in development and launch is anticipated in 2008.

EROS C will weigh 350 kg at launch and will orbit in a sun synchronous orbit at an altitude of about 500 km. The EROS C satellite will be equipped with a camera with CCD/TDI (Charge Coupled Device/Time Delay Integration) sensors, producing both panchromatic imagery at a standard resolution of 0.70 m, and multispectral imagery at a standard resolution of 2.8 m, with a swath of 11 km at nadir. The data transmission rate will be 455 Mbit/s. The expected lifespan of the EROS C is ten years.

Nation: Israel
Type / Application: Earth Observing
Operator: ImageSat International
Contractors: IAI
Equipment: ?
Configuration: Ofeq-3 Bus ?
Propulsion: ?
Power: 8 deployable fixed solar arrays, batteries
Lifetime: 10 years
Mass: 350 kg
Orbit: 500 km SSO
Satellite Date LS Launch Vehicle Remarks
EROS C 2012 Vo Start-1
Further EROS missions:

References:

  • ImageSat International Website