The Outer Space Treaty (1967) never defines a mechanism for allocating the geostationary belt or managing traffic on it — that job fell to the ITU's Radio Regulations, a first-come-first-served coordination process built around one number: angular separation on the ring.
GEO radius: 42,164 km (period = 1 sidereal day)
Off-axis gain: G(θ) ≈ 29 − 25·log₁₀(θ) dBi [ITU-R S.580 envelope, 1°≤θ≤7°]
Carrier/Interf.: C/I(θ) ≈ G_main − G(θ)
Coordination trigger: C/I below ~26 dB → operators must formally coordinate
(the model crosses 26 dB near θ≈1.3°, so the traditional 2° arc keeps ~4.5 dB of margin)
- θ is the angular gap between two satellites as seen from a ground antenna. A dish that is sharply focused on the wanted satellite still picks up some signal from any neighbor within a few degrees — how much is set by the antenna's off-axis sidelobe pattern.
- Below the coordination arc (2° is the traditional C-band figure; some Ku-band and NGSO-adjacent filings now squeeze closer), the interfering signal's carrier-to-interference ratio drops below the threshold operators need for a clean downlink — the pair turns red on the ring and a beam is drawn between them.
- File a coordinated slot respects the current arc and drops the new satellite into the widest open gap. Squeeze in a paper satellite ignores it — mimicking an operator that files a "paper" slot to claim spectrum rights before it has a real payload, the practice the OST's silence on space traffic left no clear brake on.
- Drag any satellite dot around the ring yourself — the C/I readouts and the curve below update live as you move it, exactly as they would if that operator relocated its longitude slot.
- The ring itself rotates with Earth beneath it (once per sidereal day, ~23h56m) — a true geostationary satellite never moves relative to the ground station it serves; rotation is cosmetic here and never changes the angular gaps or C/I.