Patent ID: 11912439
Assignee: AIRBUS ONEWEB SATELLITES SAS
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 11:
12. The artificial satellite of claim 1 wherein the launch-specific parameters characterize at least one of a target antenna orientation, a target solar-array orientation, a target satellite attitude, a satellite launch orientation, a predicted satellite spin rate, a predicted satellite spin axis orientation, a satellite launch position on the payload dispenser, a satellite separation time from the payload dispenser, a satellite relative separation order from the payload dispenser, a target orbital state vector, a target semi-major axis, a target eccentricity, a target right ascension of ascending mode, a target argument of perigee, a target orbit, a target orbital plane, a target orbital position in the target orbital plane, a launch date, and a launch time.