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NOOR 1A & 1B



General


Designation 1A: 44827 / 19084D
1B: 44828 / 19084E
Launch date 6 Dec 2019
Country of origin United States
Mission Technology
Perigee/Apogee 350/408 km
Inclination 97.0°
Period 92.0 min
Launch vehicle Electron #10

To demonstrate inter-satellite links. Based on PocketQube bus (from Alba Orbital, Glasgow), those are 3P (1P is 0.25 kg, 0.05 m cube)
For Stara Space, Los Angeles


End of life 1A


Decay 29 Dec 2020


End of life 1B


Decay 7 Apr 2020


1A:
sat-index articles


n2yo.com tracking



1B:
sat-index articles


n2yo.com tracking




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