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NORAD ID: 14128 • Int'l Des: 1983-058 • Owner: ESA • Country: I-ESA • operational
HEOCIRCULAR
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About ECS 1
ECS 1 (NORAD 14128) is a satellite launched Jun 16, 1983 by ESA of I-ESA. It operates in HEO, CIRCULAR orbit with a mass of 573.00 kg.
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Two-Line Element Set
1 14128U 83058A 26198.57138380 -.00000151 00000-0 00000-0 0 9999
2 14128 11.7978 329.5768 0009785 175.2711 184.7981 0.98871540 47016
Epoch: Jul 17, 2026 •
Age: 10 hours
Current Status
Altitude 36143.4 km
Apogee / Perigee N/A
Velocity 3.06 km/s
Sub-Earth Point 4.85°N,
173.22°W
Launch Date Jun 16, 1983
Age 43 years
Type other
Technical Details
Classification Payload
Mass 573.00 kg
Dry Mass 466.00 kg
Total Mass 1043.00 kg
Length 2.40 m
Diameter 2.20 m
Span 13.80 m
Shape Box + 2 Pan
Manufacturer BAES
Bus Type ECS
Phase Status In Orbit
Owner/State ESA/I-ESA
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