EROS A

Launch Success

Liftoff Time (GMT)

12:32:00

Tuesday December 5, 2000

Mission Details

EROS A

Wiki

EROS or Earth Resources Observation Satellite is a family of Israeli commercial Earth observation satellites developed by Israel Aircraft Industries (IAI) with optics provided by El-Op (now Elbit Systems). Satellites are the property of ImageSat International who is the operator. EROS A was put into orbit in a sun-synchronous orbit of 480 km. It goes to the equator at 10am. Its optical resolution is 1.9 meters. The satellite, which is stabilized 3 axes, has a total mass of 250 kg including 178 kg for the platform, 42 kg for optics and 30 kg of hydrazine used by its propulsion. It derives from Israeli military reconnaissance satellite Ofeq 3. Fixed solar panels provide 450 Watts that power a 14 Ah NiCd battery. The pointing accuracy is 0.1 ° lower. Data transfers are in the X band with a downlink rate of 70 megabits / sec. The optical part includes a Cassegrain telescope 30 cm in diameter with a focal length of 3.45 meters. The CCD type sensor includes two lines of 7490 pixels. It has a design life of 4 years and a projected life of 10 years. In early 2013 it is still operational.

Sun-Synchronous Orbit

1 Payload

250 kilograms

Rocket

Retired
START-1

Active 1993 to 2006

Moscow Institute of Thermal Technology logo

Agency

MITT

Rocket

Height: 22.74m

Payload to Orbit

LEO: 532 kg

GTO: 0 kg

Liftoff Thrust

890 Kilonewtons

Fairing

Diameter: 1.33m

Height: 3.34m

Stages

4

Launch Site

Site 5

Svobodny Cosmodrome, Russia

Fastest Turnaround

76 days 20 hours

Stats

START-1


5th

Mission

1st

Mission of 2000

Moscow Institute of Thermal Technology


5th

Mission

1st

Mission of 2000

2000


81st

Orbital launch attempt