Official name | DEWASAT-1 |
Alternative name | DEWASAT-1 |
Cospar ID | 2022-002CM |
Norad ID | 51067 |
Launch date | 2022-01-13 |
Launch site | AFETR |
Launch vehicle | Falcon-9 v1.2 (Block 5) |
Country/Organization | UAE |
Type application | Communications |
Operator | DEWA |
RCS size | MEDIUM |
Decay date | ON ORBIT |
Period (min) | 93.47 |
Inclination (deg) | 97.39 |
Perigee (km) | 441 |
Apogee (km) | 448 |
Eccentricity | 0.0078740157480315 |
Mean motion (revs. per day) | 15.4060126243715 |
Semi-Major axis (km) | 6822.635 |
Raan (deg) | 199.249 |
Arg of perigee (deg) | 171.864 |
Shape | Box + 2 Pan |
Mass (kg) | 4 |
Height (m) | 0.3 |
Width (m) | 0.1 |
Depth (m) | 0.1 |
Span (m^2) | 0.3 |
Contractors | DEWA, Nanoavionis |
Propulsion | None |
Configuration | CubeSat (3U) |
Power | Solar cells, batteries |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
---|---|---|---|---|---|---|
DEWASAT-1 | 2022-002CM | 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 |