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LEMUR-2-STARLIGHT
active
Identification
Position
—
NORAD / COSPAR
66783 / 2025-276DY
Operator
Spire
Orbit
LEO
Hardware
Manufacturer
N/A
Model
CubeSat (3U)
Mass
4 kg
Launch
Launch site
Vandenberg SFB
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-STARLIGHT · Satbeams
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