Layers
Active Satellites
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Debris Objects
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Rocket Bodies
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Conjunction Events
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Click fetch to load live SGP4 data
SGP4 ORBITAL SAFETY PLANNING SYSTEM · BLUDOT LABS
0
SAT
0
DEB
0
R/B
0
CONJ
LAT — LON — VIEW ALT — km
EPOCH: awaiting dataT+00:00
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Objects tracked
real SGP4 catalog
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Conjunction alerts
TCA computed
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High-risk events
Pc > 1e-4
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Objects in LEO
200–2000 km
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Non-compliant
IADC 25yr rule
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Active satellites
maneuverable
Shell distribution — object count by altitude
Top risk objects (by conjunction Pc)
Orbital congestion analysis — objects per 100 km shell
IADC debris mitigation guidelines — compliance status
Conjunction Decision Engine
Select a conjunction event to simulate all avoidance maneuvers
Orbital Safety API — In-Browser Sandbox
v1 · LIVE DATA
All endpoints run against your loaded orbital catalog using real SGP4 propagation and the Jacchia-Bowman atmospheric model. No server required — the entire engine runs in your browser.
POST
/orbit/validate
Evaluate orbit safety & IADC compliance
Request body
POST
/conjunction/check
Analyze collision risk between two objects
Request body
POST
/deorbit/plan
Generate disposal strategies for a satellite or rocket body
Request body
POST
/maneuver/recommend
Optimal avoidance maneuver for a conjunction event
Request body
POST
/orbit/congestion
Density and risk levels within an orbital shell
Request body
CONJ
OBJECT
PLAN
MANEUVER
AI
Load orbital data to detect conjunction events.
The system will compute TCA, miss distance, relative velocity and Pc for all object pairs.
The system will compute TCA, miss distance, relative velocity and Pc for all object pairs.