The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 25, 2025

Filed:

Nov. 27, 2023
Applicant:

Skeyeon, Inc., San Diego, CA (US);

Inventors:

Ronald E. Reedy, San Diego, CA (US);

Thomas E. Schwartzentruber, San Diego, CA (US);

Assignee:

Skeyeon, Inc., San Diego, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C07C 259/06 (2006.01); A61P 35/00 (2006.01); B64G 1/10 (2006.01); B64G 1/42 (2006.01); B64G 1/44 (2006.01); G01S 19/39 (2010.01); H04B 7/185 (2006.01); H04B 7/195 (2006.01); B64G 1/66 (2006.01); G01S 13/90 (2006.01);
U.S. Cl.
CPC ...
C07C 259/06 (2013.01); A61P 35/00 (2018.01); B64G 1/1021 (2013.01); B64G 1/425 (2013.01); B64G 1/443 (2013.01); G01S 19/39 (2013.01); H04B 7/18513 (2013.01); H04B 7/195 (2013.01); B64G 1/1028 (2023.08); B64G 1/1035 (2023.08); B64G 1/66 (2013.01); G01S 13/90 (2013.01);
Abstract

A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.


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