Article 66

Spacecraft manoeuvrability

1. Union spacecraft operators shall ensure that a spacecraft is designed, produced, and operated in a way that allows the spacecraft to have and enable manoeuvrability capabilities for orbits with an apogee above 400 km.

2. The manoeuvrability capability referred to in paragraph 1 shall at least:

(a) comply with the requirements set out in point 2, of Annex IV, and allow to respond to a high interest event alert, in accordance with Article 64(5);

(b) enable the performance end-of-life disposal in accordance with Article 70(1), point (c); The ground segment shall be capable of receiving orbital forecasts and process data in accordance with point 2, of Annex III.

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