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LEMUR-2-TEODOR
active
Identification
Position
—
NORAD / COSPAR
66768 / 2025-276DG
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
28 Nov 2025
Launched
2 yr
Design life
0.8 yr
Elapsed
1.2 yr
Remaining
Nov 2027
End of life
Within design lifetime
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LEMUR-2-TEODOR · Satbeams
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