Official name | PERSEUS M2 |
Alternative name | Perseus-M 2 |
Cospar ID | 2014-033AD |
Norad ID | 40037 |
Launch date | 2014-06-19 |
Launch site | OREN |
Launch vehicle | Dnepr |
Country/Organization | Russia, USA |
Type application | Traffic monitoring |
Operator | Canopus Systems US → Aquila Space |
RCS size | MEDIUM |
Decay date | ON ORBIT |
Period (min) | 96.63 |
Inclination (deg) | 97.93 |
Perigee (km) | 589 |
Apogee (km) | 606 |
Eccentricity | 0.0142259414225941 |
Mean motion (revs. per day) | 14.9022042843837 |
Semi-Major axis (km) | 6975.635 |
Raan (deg) | 60.0067 |
Arg of perigee (deg) | 333.6001 |
Shape | Box |
Mass (kg) | 10 |
Height (m) | 0.3 |
Width (m) | 0.2 |
Depth (m) | 0.3 |
Span (m^2) | 0.3 |
Lifetime | 1 year |
Contractors | Dauria Aerospace, Canopus Systems US |
Equipment | AIS-receiver |
Propulsion | None |
Configuration | CubeSat (6U) |
Power | Solar cells, batteries |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
---|---|---|---|---|---|---|
PERSEUS M2 | 2014-033AD | 2014-06-19 | OREN | Dnepr | with Deimos 2, KazEOSat 2, Saudisat 4, TabletSat-Aurora, BugSat 1, AprizeSat 9, AprizeSat 10, UniSat 6, BRITE-CA 1, BRITE-CA 2, Hodoyoshi 3, Hodoyoshi 4, Perseus-M 1, Perseus-M 1, Flock-1c 1, ..., 11, POPSAT-HIP 1, QB50P1, QB50P2, PACE, TigriSat, ANTELSAT, Lemur 1, NanoSatC-Br 1, Duchifat 1, PolyITAN 1, DTUSat 2, AeroCube 6A, AeroCube 6B | |
PERSEUS M1 | 2014-033AF | 2014-06-19 | OREN | Dnepr | with Deimos 2, KazEOSat 2, Saudisat 4, TabletSat-Aurora, BugSat 1, AprizeSat 9, AprizeSat 10, UniSat 6, BRITE-CA 1, BRITE-CA 2, Hodoyoshi 3, Hodoyoshi 4, Perseus-M 2, Flock-1c 1, ..., 11, POPSAT-HIP 1, QB50P1, QB50P2, PACE, TigriSat, ANTELSAT, Lemur 1, NanoSatC-Br 1, Duchifat 1, PolyITAN 1, DTUSat 2, AeroCube 6A, AeroCube 6B |