Filed a Supplement to the original Petition, detailing the new discoveries made during the research of this debacle:

Before the FEDERAL COMMUNICATIONS COMMISSION Washington, D.C. 20554 In the Matter of SpaceX Application for Authority to Launch and Operate an "Orbital Data Center" in the 500 km – 2,000 km range File No. SAT-LOA-20260108-00016

CONSOLIDATED SUPPLEMENTAL PETITION TO DENY

I. INTRODUCTION AND VERIFICATION OF PRIOR FILING

Petitioner William Stewart hereby submits this Consolidated Supplemental Petition to Deny regarding the application of SpaceX to operate an "Orbital Data Center" at altitudes between 500 km and 2,000 km.

Verification of Prior Physical Filing: Petitioner formally notifies the Commission that a comprehensive physical evidentiary package was delivered to the FCC Reference Information Center via USPS (Tracking: 9400136106196292968437) on February 17, 2026. This electronic supplement ensures the Commission and all parties have digital access to the critical safety data contained therein while the physical records undergo processing.

II. DISCOVERY OF SIGNIFICANT OPERATIONAL RISKS

Since the initial filing, Petitioner has identified three major technical concerns that underscore why a waiver of standard safety protocols would be detrimental to the public interest.
A. The "Forever Zone" and Atmospheric Persistence Current Starlink deployments benefit from atmospheric drag at 550 km, which acts as a natural "self-cleaning" mechanism for debris. However, at the requested range of 2,000 km, atmospheric drag is negligible. Debris created at these altitudes will persist for centuries. The applicant's safety track record at lower altitudes does not translate to this high-risk environment.
B. The Maneuver Paradox and Scalability Failure Public data indicates that a fleet of 9,000 satellites already requires approximately 300,000 maneuvers annually to avoid collisions. Scaling this model to the requested 1,000,000 assets would create a computationally and physically unmanageable "collision noise" environment. This environment significantly increases the probability of catastrophic failure due to sheer volume.
C. The 0.8% "Operational Tax" on Fuel Sustainability High-frequency maneuvering carries a fuel cost estimated at 0.8% per active cycle. This constant "tax" on fuel reserves leads to premature satellite exhaustion. Once fuel is exhausted, a satellite at 2,000 km becomes a permanent, unguided hazard, as it cannot be safely de-orbited via drag.

 
III. UNPRECEDENTED SCALE AND THE NEPA CATEGORICAL EXCLUSION

The FCC typically grants a "categorical exclusion" for satellite launches to avoid lengthy environmental reviews. However, this application for 1,000,000 satellites constitutes "extraordinary circumstances" that must override this exclusion. A factor-of-70 increase in the satellite population will result in permanent skyglow that cannot be mitigated by painting satellites black.

IV. THE "TWILIGHT EXTENSION" AT 2,000 KM

Satellites at the requested 2,000 km altitude remain illuminated by the sun much longer than those at 550 km. While lower satellites enter the Earth's shadow shortly after sunset, those at 2,000 km can reflect sunlight well into the middle of the night. This creates a "twilight extension" that permanently brightens the night sky, disrupting both ground-based astronomy and natural biological cycles.

V. CUMULATIVE SKYGLOW AND HUMAN HEALTH

Research indicates that the sheer volume of 1,000,000 reflective surfaces will increase diffuse skyglow by significantly more than the 10% threshold recommended by the American Astronomical Society. This permanent artificial illumination disrupts circadian rhythms and creates an "operational haze" that hinders the detection of near-Earth asteroids.

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