Official name ALPHA
Alternative name Alpha
Cospar ID 2022-080F
Norad ID 53110
Launch date 2022-07-13
Launch site FRGUI
Launch vehicle Vega-C
Country/Organization Italy
Type application Technology
Operator ARCA Dynamics
RCS size SMALL
Decay date ON ORBIT
Period (min) 224.07
Inclination (deg) 70.19
Perigee (km) 5550
Apogee (km) 6134
Eccentricity 0.0499828825744608
Mean motion (revs. per day) 6.42656312759406
Semi-Major axis (km) 12220.135
Raan (deg) 58.273
Arg of perigee (deg) 148.5037
Shape Box
Mass (kg) 1
Height (m) 0.1
Width (m) 0.1
Depth (m) 0.1
Span (m^2) 0.1
Contractors ARCA Dynamics (prime), Spacemind
Propulsion None
Configuration CubeSat (1U)
Power Solar cells, batteries

ALPHA is an Italian technology demonstration 1U CubeSat developped by ARCA Dynamics with the main goal of demonstrating radiation hardened technology: a novel integrated ADCS including an innovative reaction wheel by ARCA, a deployable deorbiting sail by NPC Spacemind, and other subsystems such as an EPS by H4-Research, an OBC and telecommunications module by GP Advanced Projects.

ALPHA will bring in orbit the second generation of ARTICA developed by Spacemind (SM) that will be also responsible for bus procurement based on SM products, AIT and test.

The mission will take place in a Medium Earth Orbit (MEO), at approximately 15 times the altitude of the International Space Station (ISS). At this altitude, 6.000 km circa, ALPHA will be in an extremely harsh radiative environment, called the inner Van Allen belt, where the Earth?s magnetic field traps harmful solar wind and cosmic rays radiations. Under these conditions, ALPHA will perform scientific experiments to better understand magnetosphere related phenomena, such as Northern lights and southern aurora, and the demonstration of innovative technologies designed and developed to mitigate the effects of radiations.

Satellite COSPAR Date LS Launch Vehicle Remarks
ALPHA 2022-080F 2022-07-13 FRGUI Vega-C with LARES 2, AstroBio Cubesat, GreenCube, CELESTA, TRISAT R, MTCube 2