A reserve satellite cluster (22) including a plurality of satellites (30) stands by at an orbit altitude lower than an orbit altitude of a steadily operated satellite cluster (21) in a satellite constellation (20). In a case where a satellite (30) configuring the steadily operated satellite cluster (21) has been lost, a satellite (30), existing around a lost orbital position that is an orbital position where a satellite (30) has been lost in the steadily operated satellite cluster (21), among satellites (30) configuring the reserve satellite cluster (22) is injected into the lost orbital position in an orbit.
SATELLITE CONSTELLATION MAINTENANCE METHOD, SATELLITE CONSTELLATION, ROCKET LAUNCH METHOD, GROUND EQUIPMENT, COMMAND TRANSMISSION METHOD, AND COMMAND TRANSMISSION PROGRAM
WARTUNGSVERFAHREN FÜR SATELLITENKONSTELLATION, SATELLITENKONSTELLATION, RAKETENSTARTVERFAHREN, BODENAUSRÜSTUNG, BEFEHLSÜBERTRAGUNGSVERFAHREN UND BEFEHLSÜBERTRAGUNGSPROGRAMM
PROCÉDÉ D'ENTRETIEN DE CONSTELLATION DE SATELLITES, CONSTELLATION DE SATELLITES, PROCÉDÉ DE LANCEMENT DE FUSÉE, ÉQUIPEMENT AU SOL, PROCÉDÉ DE TRANSMISSION DE CONSIGNES, ET PROGRAMME DE TRANSMISSION DE CONSIGNES
2024-05-01
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
European Patent Office | 2022
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