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LEMUR 2 DEVERILL-M-T
active
Identification
Position
—
NORAD / COSPAR
57391 / 2023-100F
Operator
Spire
Orbit
LEO
Hardware
Manufacturer
Spire Global
Model
Cubesat 3U
Mass
4 kg
Launch
Launch site
Rocket Lab Launch Complex 1
Launch vehicle
Electron
Lifetime
18 Jul 2023
Launched
2 yr
Design life
3.1 yr
Elapsed
Expired
Remaining
Jul 2025
End of life
Design lifetime exceeded by 1.1 years
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LEMUR 2 DEVERILL-M-T · Satbeams
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