Mission Chapters Scenarios Resources Calculator Trajectory Simulator Contact GitHub Sign In / Create Account → Open Dashboard →
Space Situational Awareness & Education Platform

Understanding the Crowded Cosmos

27,000+ tracked objects. A debris field that could trigger an irreversible cascade. VectraSpace gives you the physics, the data, and the tools to understand it — from Kepler to Kessler, in four chapters.

4 Technical Chapters
27k+ Tracked Objects
Live SGP4 Scanner
Free No account needed
Start Learning ↓ Live Scanner →
Scroll
Tracked Objects: 27,000+ Estimated Debris >1mm: 130 Million ISS Altitude: 408 km LEO Collision Risk Method: Foster-Alfano Pc Fengyun-1C 2007: Largest Single Debris Event SGP4 Propagation: 1-Minute Resolution Sun-Synchronous i ≈ 97.8° — RAAN Drifts +0.9856°/day Kessler Syndrome: Self-Sustaining Cascade J₂ Coefficient: 1.08263 × 10⁻³ Tracked Objects: 27,000+ Estimated Debris >1mm: 130 Million ISS Altitude: 408 km LEO Collision Risk Method: Foster-Alfano Pc Fengyun-1C 2007: Largest Single Debris Event SGP4 Propagation: 1-Minute Resolution Sun-Synchronous i ≈ 97.8° — RAAN Drifts +0.9856°/day Kessler Syndrome: Self-Sustaining Cascade J₂ Coefficient: 1.08263 × 10⁻³

Built because the physics
deserves to be understood

VectraSpace exists because orbital safety is one of the most consequential engineering problems of our generation — and almost no one outside the industry understands it. We built a platform where anyone can engage with the real mathematics: not simplified metaphors, but the actual SGP4 propagation, Foster-Alfano probability of collision, and Kessler cascade physics that real SSA operators use every day.

Free Always & Forever
Real Physics & Data
Open No Account Needed

The orbital environment
is running out of time

27,000+
Tracked Objects

The US Space Surveillance Network tracks 27,000+ objects larger than 10cm. Hundreds of thousands of smaller fragments — invisible to radar — travel at 7.8 km/s through crowded orbital shells.

10×
Collision Energy Multiplier

Orbital velocities of ~7.8 km/s mean a 10 cm debris fragment carries the kinetic energy of a hand grenade. Even a 1 cm fragment can destroy a satellite — and generate thousands more pieces.

Cascade
Kessler Syndrome Risk

Above a critical density threshold, collisions generate debris faster than drag removes it. The cascade becomes self-sustaining — rendering entire orbital shells permanently unusable.

Step 01
Read the Chapters
Four technical deep dives — orbital mechanics, collision prediction, perturbations, debris modeling.
Step 02
Run a Simulation
Explore the Kessler cascade, Iridium–Cosmos collision, and ASAT events in interactive 3D.
Step 03
Scan Live Orbits
Run the live SGP4 conjunction scanner on real TLE data and generate a downloadable CDM report.

The physics behind
every orbit

Four comprehensive chapters covering the mathematics, algorithms, and engineering principles that power modern Space Situational Awareness — from Kepler to Kessler.

Your Progress0 / 4 Chapters
Chapter 01 — Foundations

Orbital Mechanics & the Two-Body Problem

From Newton's universal gravitation to Kepler's three laws, vis-viva equation, orbital elements, TLE format, and the SGP4 propagator that powers every conjunction screening system on Earth.

Kepler's Laws Six Orbital Elements TLE Format SGP4 Model Vis-Viva Equation
Chapter 02 — Collision Analysis

Conjunction Prediction & Probability of Collision

How operators screen 350 million possible object pairs daily, compute Time of Closest Approach, model covariance ellipsoids, and apply the Foster-Alfano method to estimate whether a maneuver is warranted.

TCA Algorithm Foster-Alfano Pc CCSDS CDM Covariance Matrix CW Maneuver
Chapter 03 — Perturbation Theory

Why Real Orbits Deviate from Kepler

Earth's oblateness (J₂ = 1.08263×10⁻³), atmospheric drag, solar radiation pressure, and luni-solar gravity all bend real orbits away from ideal ellipses — and drive sun-synchronous design, station-keeping budgets, and TLE accuracy decay.

J₂ Oblateness Atmospheric Drag Solar Rad. Pressure RAAN Precession TLE Age Error
Chapter 04 — Debris Physics

Debris Modeling & the Kessler Cascade

The NASA Standard Breakup Model, power-law fragment distributions, historical events from Fengyun-1C to Iridium-Cosmos, cascade threshold mathematics, Active Debris Removal technologies, and IADC mitigation guidelines.

NASA SBM Fragment Velocity Cascade Physics ADR Technologies IADC Guidelines

See the math in motion

The VectraSpace dashboard runs real SGP4 propagation on live TLE data, screens every orbit pair for conjunctions, and visualizes the results on a photorealistic CesiumJS globe — all in your browser.

SGP4 / SDP4
Live Propagation

NumPy-vectorized SGP4 propagates thousands of satellites simultaneously across a 12–72 hour window at 1-minute resolution. Regime-specific filters for LEO, MEO, and GEO.

Step size: 60 s · Batch: 50 sats
Conjunction
🎯
Conjunction Screening

Ellipsoid pre-filter eliminates 95%+ of pairs before refinement. Bounded golden-section search finds exact TCA. Foster-Alfano Pc with real CDM covariance when Space-Track credentials are set.

Filter rate: ~95% · Pc method: Foster-Alfano
Debris
💥
Fragmentation Model

Simulate a collision or explosion using the NASA Standard Breakup Model. Lognormal velocity distributions, isotropic ejection directions, and real conjunction screening of the resulting debris cloud.

Max fragments: 200 · Lc range: 1–50 cm
CCSDS CDM
📄
CDM Export

Standards-compliant Conjunction Data Messages (CCSDS 508.0-B-1) generated per event. Individual download or bulk ZIP. Includes Clohessy-Wiltshire minimum-ΔV maneuver advisory for each conjunction.

Format: CCSDS 508.0 · Maneuver: CW Linear
Alerting
🔔
Real-time Alerts

Threshold-based alert routing: email (Gmail, SendGrid, SES, Postmark), Pushover mobile push, and HTTP webhooks. Per-user Pc threshold and miss-distance configuration. Styled HTML email with full conjunction data.

Channels: 4 email + Pushover + webhook
CesiumJS
🌐
3D Globe Visualization

Photorealistic Cesium World Terrain + Imagery, animated orbital tracks, conjunction markers, time-scrubbing, and adjustable simulation speed. Click any object for satellite info powered by the Anthropic API.

Engine: CesiumJS 1.114 · Mode: WebGL 2
VectraSpace v11 — Orbital Scan
$ python vectraspace.py [INFO] Loading environment from .env ✓ Space-Track authenticated — 4,812 TLEs downloaded LEO: 3,204 · MEO: 891 · GEO: 717 Propagating 170 satellites — 12h @ 1 min resolution ✓ Vectorized propagation complete (1,240 timesteps × 170 sats) Screening 14,365 pairs — ellipsoid pre-filter active ✓ 13,642 pairs rejected (94.9%) — 723 refined ⚠ CONJUNCTION DETECTED STARLINK-4521 ↔ COSMOS-1408 DEB [LEO/LEO] Miss dist: 3.214 km · Pc: 4.1e-04 · TCA: +2h 14m Δv advisory: 0.082 m/s radial · 0.341 m/s transverse ✓ 3 conjunctions found · CDMs generated · Alerts dispatched $
⌁ Loading today's featured satellite...
0
Tracked Objects in Catalog
0
Conjunction Screens per Day (global)
0
Years to Self-Clear Above 800 km
0
kJ Energy: 10 cm Fragment at 10 km/s
⬤ LIVE
Loading...
— connecting
⬡ Start Exploring

The cosmos doesn't wait.
Neither should your education.

Dive into the physics chapters, run a live conjunction scan against 4,000+ active satellites, or simulate a debris fragmentation event — all backed by the same math used by real SSA operators.

The Team
The people behind
VectraSpace
Founder & Builder
T
Truman Heaston
Builder · Student · Orbital Mechanics Nerd

Passionate about space, orbital mechanics, and the belief that great education can change the world. VectraSpace started as a personal obsession — I wanted to understand the real math behind satellite conjunction events, so I built the platform I wished existed.

trumanheaston@gmail.com
Marketing & Outreach
W
Will Lovelace
Marketing · Outreach · Growth

Leading marketing and outreach for VectraSpace — connecting the platform with researchers, educators, and operators across the space industry. If you're interested in partnerships, press, or collaboration opportunities, Will is your contact.

Will.s.lovelace@gmail.com
Hardware Lead
G
Grant Gill
Hardware Lead · Amateur Radio · Model Rocketry

Grant leads hardware development at VectraSpace and is the driving force behind VectraKit — our plug-and-play telemetry system for amateur rockets. A licensed amateur radio operator with hands-on model rocketry experience, Grant brings the real-world RF and avionics expertise that bridges our software platform to physical flight systems.

📡 Amateur Radio Operator
🚀 VectraKit Lead
Get in Touch
Have feedback, questions,
or want to collaborate?

Whether you're a researcher, operator, educator, or fellow student — we'd genuinely love to hear from you. Technical critique, curriculum suggestions, partnership ideas — all of it is welcome.