Find Astra 3A
NORAD ID: 27400 • Int'l Des: 2002-015 • Owner: SESA • Country: L • operational
HEOCIRCULAR
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About Astra 3A
Astra 3A (NORAD 27400) is a satellite launched Mar 29, 2002 by SESA of L. It operates in HEO, CIRCULAR orbit with a mass of 865.00 kg.
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Two-Line Element Set
1 27400U 02015B 26195.41183245 -.00000260 00000-0 00000-0 0 9991
2 27400 10.5931 47.6531 0001278 255.6760 113.9900 0.99088723 88846
Epoch: Jul 14, 2026 •
Age: 26 hours
Current Status
Altitude 36124.4 km
Apogee / Perigee N/A
Velocity 3.06 km/s
Sub-Earth Point 5.24°N,
28.16°W
Launch Date Mar 29, 2002
Age 24.2 years
Type other
Technical Details
Classification Payload
Mass 865.00 kg
Dry Mass 700.00 kg
Total Mass 1495.00 kg
Length 8.00 m
Diameter 2.20 m
Span 8.00 m
Shape Cyl
Manufacturer BOES
Bus Type HS-376HP
Phase Status In Orbit
Owner/State SESA/L
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