Official name | GREGOIRE |
Alternative name | Gregoire |
Cospar ID | 2023-084Q |
Norad ID | 56946 |
Launch date | 2023-06-12 |
Launch site | AFWTR |
Launch vehicle | Falcon-9 v1.2 (Block 5) |
Country/Organization | Belgium |
Type application | Technology |
Operator | Aerospacelab |
RCS size | MEDIUM |
Decay date | ON ORBIT |
Period (min) | 94.79 |
Inclination (deg) | 97.54 |
Perigee (km) | 501 |
Apogee (km) | 516 |
Eccentricity | 0.0147492625368732 |
Mean motion (revs. per day) | 15.1914758940817 |
Semi-Major axis (km) | 6886.635 |
Raan (deg) | 241.6322 |
Arg of perigee (deg) | 168.5426 |
Shape | Box |
Mass (kg) | 100 |
Height (m) | 1 |
Width (m) | 0.6 |
Depth (m) | 0.6 |
Span (m^2) | 1 |
Contractors | Aerospacelab |
Propulsion | ? |
Configuration | VSP bus |
Power | Solar cells, batteries |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
---|---|---|---|---|---|---|
GREGOIRE | 2023-084Q | 2023-06-12 | AFWTR | Falcon-9 v1.2 (Block 5) | with W-Series 1, Skykraft Deployer 3, Skykraft 3A, ..., 3D, ICEYE X23, X25, X26, X30, GHOSt 3, Grégoire, Runner 1, Tomorrow R2, QPS-SAR 6, ÑuSat 40, ..., 43, Aces 1, ..., 4, HOTSAT 1, AFR, DROID.001, MuSat 1, ION-SCV 011, Outpost Mission 1, EPICHyper 2, Kelpie 2, Spei Satelles, ELO 4, MRC-100, Unicorn 2I, SATLLA 2I, URESAT 1, Istanbul, ROM 2, Orbiter SN3, Otter Pup, MDQSAT 1C, 1D, Pleiades-Squared, GEI-SAT Precursor, XVI, AII-Delta, Ayris 1, 2, EIVE, Lemur-2 166, 167, 168, MISR-A 1, MISR-B 2, Tiger 4, FOSSASat FEROX 1, ..., 4, SpaceBEE 168, ..., 179 |