Official name | LABSAT |
Alternative name | LabSat |
Cospar ID | 2022-002DG |
Norad ID | 51086 |
Launch date | 2022-01-13 |
Launch site | AFETR |
Launch vehicle | Falcon-9 v1.2 (Block 5) |
Country/Organization | Poland |
Type application | Technology |
Operator | Wroclaw University of Science and Technology |
RCS size | MEDIUM |
Decay date | ON ORBIT |
Period (min) | 93.02 |
Inclination (deg) | 97.38 |
Perigee (km) | 419 |
Apogee (km) | 425 |
Eccentricity | 0.00710900473933649 |
Mean motion (revs. per day) | 15.4805418189637 |
Semi-Major axis (km) | 6800.135 |
Raan (deg) | 196.7043 |
Arg of perigee (deg) | 168.1769 |
Shape | Box |
Mass (kg) | 5 |
Height (m) | 0.3 |
Width (m) | 0.2 |
Depth (m) | 0.2 |
Span (m^2) | 0.3 |
Contractors | SatRevolution S.A. |
Propulsion | None |
Configuration | CubeSat (3U) |
Power | Solar cells, batteries |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
---|---|---|---|---|---|---|
LABSAT | 2022-002DG | 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, FOREST 1, Lemur-2 149, 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 |