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LEMUR 2 ROCINANTE
decayed
Identification
Position
—
NORAD / COSPAR
59147 / 2024-043BB
Operator
Spire
Orbit
LEO
Hardware
Manufacturer
N/A
Model
N/A
Mass
4 kg
Launch
Launch site
Vandenberg SFB
Launch vehicle
Falcon 9 Block 5
Lifetime
04 Mar 2024
Launched
2 yr
Design life
2.5 yr
Elapsed
Expired
Remaining
Mar 2026
End of life
Satellite is decayed
LEMUR 2 ROCINANTE · Satbeams
