| CPC H01L 23/60 (2013.01) [A63B 71/02 (2013.01); B64C 39/024 (2013.01); B64G 1/2227 (2023.08); B64G 1/2228 (2023.08); B64G 1/26 (2013.01); B64G 1/428 (2013.01); B64G 1/60 (2013.01); B64G 1/646 (2013.01); B64G 1/2427 (2023.08); B64U 50/19 (2023.01); B64U 50/34 (2023.01); B64U 50/35 (2023.01); B64U 2101/00 (2023.01); B64U 2101/05 (2023.01); B64U 2101/24 (2023.01); B64U 2101/26 (2023.01); B64U 2101/30 (2023.01); B64U 2201/20 (2023.01)] | 16 Claims |

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1. A spacecraft system, comprising:
a flexible membrane configured to deploy from a first spacecraft to enclose an interior volume filled with one or more gases, wherein the flexible membrane is transparent or translucent;
a plurality of cameras positioned to acquire visual images of the interior volume; and one or more controllers configured to implement a routine that includes:
moving the first spacecraft from a first orbit to a second orbit, the first orbit being larger than the second orbit;
docking the first spacecraft with a second spacecraft;
transmitting, using the plurality of cameras, an event or activity within the interior volume; and
returning the first spacecraft to the first orbit.
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