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LEMUR-2 GRAM-E-SUE
active
Identification
Position
—
NORAD / COSPAR
67370 / 2026-004H
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
11 Jan 2026
Launched
2 yr
Design life
0.7 yr
Elapsed
1.3 yr
Remaining
Jan 2028
End of life
Within design lifetime
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LEMUR-2 GRAM-E-SUE · Satbeams
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