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LEMUR 2 YONGLIN
decayed
Identification
Position
—
NORAD / COSPAR
43045 / 2017-071J
Operator
Spire
Orbit
LEO
Hardware
Manufacturer
N/A
Model
N/A
Mass
4 kg
Launch
Launch site
Wallops Flight Facility
Launch vehicle
Antares 230
Lifetime
12 Nov 2017
Launched
2 yr
Design life
8.8 yr
Elapsed
Expired
Remaining
Nov 2019
End of life
Satellite is decayed
LEMUR 2 YONGLIN · Satbeams
