AEROSPACE INTELLIGENCE PLATFORM

Space Situational Awareness (SSA) Ecosystem

Tracking · Predicting · Assessing · Protecting Earth's Orbital Environment
01 — FOUNDATION
What is Space Situational Awareness?
SSA is the science and operational tradecraft of tracking, cataloguing, characterizing, and predicting the behavior of every object in Earth's orbital environment — enabling collision avoidance, mission safety, and long-term orbital sustainability.
Active satellites Rocket bodies Space debris Defunct satellites Collision threats
27,000+
Catalogued objects
Millions
Debris fragments
24/7
Operational awareness
4 shells
LEO · MEO · GEO · HEO
02 — SENSOR NETWORK
Global observation network
Ground radar Phased array Optical Space sensors
Observations ingested globally
Orbit determination
Object identification
Catalog updated and distributed
03 — TLE PIPELINE
Two-line element data flow
1 25544U 98067A 24100.50000000 .00002182 00000-0 40768-4 0 9990
2 25544 51.6416 247.4627 0006703 130.5360 325.0288 15.50377890418514
Inclination 51.64° RAAN 247.46° Mean motion 15.50 rev/day
Authority sources: Space-Track.org · US Space Force · 18th SDS · LeoLabs
HEO GEO MEO LEO
LEO <2000 km MEO GEO 35,786 km HEO elliptical
04 — DATA SOURCES
Space-Track vs LeoLabs

Space-Track

Government operated
Free registration
27,000+ tracked objects
Global catalog + CDM
Standard TLE source

LeoLabs

Commercial provider
High-fidelity phased array
~2 cm debris tracking
LEO optimized · APIs
Enhanced conjunction data
05 — PROPAGATION ENGINE
SGP4 orbit prediction model
INPUTS
TLE epoch data
Bstar drag term
Inclination + RAAN
Mean motion
SGP4
Simplified General Perturbations
J2–J4 gravity
Atmospheric drag
Solar + lunar gravity
OUTPUTS
Future position (ECI)
Future velocity
Predicted orbit track
Ground pass predictions
ORBITIQ Explorer v2 uses satellite.js for browser-based SGP4 propagation · TLE + SGP4 = industry standard pair
06 — CONJUNCTION ASSESSMENT
Proximity screening
Two objects flagged when projected closest approach drops below threshold distance.
Distance < 5 km → Flag conjunction event
Safe — miss distance > 5 km
Caution — 1–5 km, monitor
Alert — < 1 km, assess maneuver
ORBITIQ Explorer v2 — distance threshold screening active
07 — COLLISION PROBABILITY
Probability of collision (Pc) methods

Alfano method

Encounter plane geometry with covariance ellipse integration. Most widely used operational method.
Pc = 1 × 10⁻⁴

Foster method

Conservative upper-bound probability when covariance quality is uncertain or degraded.
Pc ≤ upper bound
SGP4 + TLE alone cannot compute Pc
  • Covariance matrices required
  • Uncertainty models required
  • Relative error statistics required
08 — CCSDS CDM
Conjunction Data Message fields
Time of closest approach
Miss distance
Relative velocity
Covariance matrices
Hard body radius
Risk assessment
Covariance matrices unlock real probability of collision calculations — the critical upgrade beyond simple distance screening
09 — DECISION CHAIN
Operational workflow
Space-Track / LeoLabs — raw catalog feed
TLE catalog + CDM distribution
SGP4 propagation → future states
Proximity screening (distance threshold)
Alfano / Foster Pc computation
Risk evaluation vs mission thresholds
Collision avoidance planning (Δv)
Operator decision + approval
Mission protected — maneuver executed
10 — ORBITIQ POSITIONING
ORBITIQ Explorer v2 · Roadmap
Current capabilities
TLE ingestion
Satellite catalog
SGP4 propagation
Real-time 3D globe
Pass predictor (HYD)
Distance screening
Roadmap
CDM integration
Covariance processing
Alfano Pc engine
Foster Pc engine
Maneuver recommendations
Autonomous CA analytics
Built by Mahin Nandipa · Part of the ORBITIQ SSA Trilogy · Portfolio