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LEMUR-2-PEGGY-2004
retired
Identification
Position
—
NORAD / COSPAR
68479 / 2026-067BR
Operator
Spire
Orbit
LEO
Hardware
Manufacturer
Spire Global
Model
Cubesat 3U
Mass
4 kg
Launch
Launch site
Vandenberg SFB
Launch vehicle
Falcon 9 Block 5
Lifetime
30 Mar 2026
Launched
2 yr
Design life
0.4 yr
Elapsed
1.6 yr
Remaining
Mar 2028
End of life
Satellite is retired
LEMUR-2-PEGGY-2004 · Satbeams
