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LEMUR 2 SEJONG-2
active
Identification
Position
—
NORAD / COSPAR
64586 / 2025-135BL
Operator
Spire
Orbit
LEO
Hardware
Manufacturer
Spire Global
Model
Cubesat 3U
Mass
4 kg
Launch
Launch site
Cape Canaveral SFS
Launch vehicle
Falcon 9 Block 5
Lifetime
23 Jun 2025
Launched
2 yr
Design life
1.2 yr
Elapsed
0.8 yr
Remaining
Jun 2027
End of life
Within design lifetime
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LEMUR 2 SEJONG-2 · Satbeams
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