Official name | ETV-A1 |
Alternative name | ETV-A1 |
Cospar ID | 2022-002CE |
Norad ID | 51060 |
Launch date | 2022-01-13 |
Launch site | AFETR |
Launch vehicle | Falcon-9 v1.2 (Block 5) |
Country/Organization | UK |
Type application | Earth observation |
Operator | Sen |
RCS size | MEDIUM |
Decay date | ON ORBIT |
Period (min) | 94.71 |
Inclination (deg) | 97.39 |
Perigee (km) | 499 |
Apogee (km) | 510 |
Eccentricity | 0.0109018830525273 |
Mean motion (revs. per day) | 15.2043078872347 |
Semi-Major axis (km) | 6882.635 |
Raan (deg) | 187.1107 |
Arg of perigee (deg) | 213.5011 |
Shape | Box + 2 Pan |
Mass (kg) | 20 |
Height (m) | 0.4 |
Width (m) | 0.2 |
Depth (m) | 0.2 |
Span (m^2) | 0.4 |
Contractors | NanoAvionics |
Equipment | Video imaging telescope payload |
Configuration | CubeSat (16U) |
Power | Solar cells, batteries |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
---|---|---|---|---|---|---|
ETV-A1 | 2022-002CE | 2022-01-13 | AFETR | Falcon-9 v1.2 (Block 5) | with Umbra 02, Capella 7, 8, ICEYE X14, X16, Sich 2-1, ION-SCV 004, Dodona, STORK 1, 2, LabSat, SW1FT, VZLUSAT 2, ETV A1, BRO 5, HYPSO 1, Kepler 16, ..., 19, Flock-4x 1, ..., 44, Lemur-2 148, 149, 150, Lemur-2 146, 147, DEWA-Sat 1, NuX 1, IRIS A, MDASat 1a, 1b, 1c, Gossamer Piccolomini, Tevel 1, ..., 8, Challenger, Delfi-PQ 1, Unicorn 2A, 2D, 2E, FossaSat 2E1, ..., 2E6, MDQube-SAT 1, SATLLA 2A, 2B, Unicorn 1, EASAT 2, HADES, Grizu-263a, PION-BR 1, SanoSat 1, Tartan-Artibeus 1, USA 320, ..., 323 |