Earth from orbit showing city lights against dark space background
Feasibility Study 2026

Real-Time Earth Observation
Satellite Constellation
with Embedded AI

A comprehensive engineering study for deploying a LEO constellation capable of sub-meter imagery, on-board AI inference, and real-time emergency alerting.

204–386
Satellites
0.3–1m
Resolution
275 TOPS
AI On-Board
<1hr
Revisit Time
System Architecture

End-to-End Data Pipeline

From orbital image capture to real-time AI-powered emergency alerting

01

Image Acquisition

High-res telephoto camera captures sub-meter imagery from 500km LEO orbit

GSD 0.3–1m
02

FPGA Preprocessing

Xilinx Virtex-5QV handles real-time image preprocessing and compression

10W, Rad-Hard
03

AI Inference

NVIDIA Jetson Thor performs on-board deep learning for anomaly detection

275 TOPS
04

Ka-Band Downlink

High-throughput Ka-band transmitter sends prioritized data to ground

1.2 Gbps
05

Ground Stations

Global network of ground stations receives and routes satellite data

Global Network
06

AI Alert Center

Real-time emergency alerts dispatched for detected events and anomalies

<60 min Latency

Orbital Parameters

500 km
Altitude
LEO
6,871 km
Orbital Radius
R_E + h
94.5 min
Period
Per orbit
15.24
Orbits/Day
Coverage
7.06 km/s
Ground Speed
Velocity
Walker Δ
Config
Constellation
Camera Selection

Imaging Payload Comparison

Comparing the leading space-grade cameras for Earth observation missions

WorldView Legion

Maxar
0.30 m

Highest commercial resolution with 15 cm pan-sharpened imagery. 15 revisits/day via mixed orbits.

FOV1.15°
Swath9 km
Mass750 kg (sat)
Power~150 W
Bands8 MS + PAN
Price$80M (sat)
Recommended

SkySat

Planet Labs
0.50 m

Excellent resolution-to-cost ratio. 10–12 revisits/day, video capture capability.

FOV0.92°
Swath8 km
Mass117 kg (sat)
Power~50 W
Bands4 MS + PAN
Price$2–5M (sat)

NewSat (Mk V)

Satellogic
1.0 m (0.7 SR)

Most affordable option with unique hyperspectral capability. 50+ satellite constellation.

FOV0.60°
Swath5.3 km
Mass46 kg (sat)
Power~15 W
Bands4 MS + 29 HS
Price$1.5M (sat)

Gen-3

BlackSky
0.35 m

Latest-gen imaging with 60-min delivery pipeline. AI-integrated platform.

FOV~1.0°
Swath~9 km
Mass~100 kg (sat)
Power~60 W
BandsMS + PAN
Price$5–10M (sat)

NAOMI

Airbus
1.5 m PAN

Heritage SPOT-6/7 imager. Wide 60km swath for large-area coverage.

FOV~2.0°
Swath~60 km
Mass60 kg (inst)
Power~40 W
BandsPAN + 4 MS
PriceN/A (Gov)
GSD = Ground Sampling Distance (resolution)
FOV = Field of View
MS = Multispectral, HS = Hyperspectral
Embedded Processing

On-Board AI Pipeline

Heterogeneous computing architecture: radiation-hardened FPGA + commercial AI accelerator with shielding

Xilinx Virtex-5QV

FPGA Preprocessing

Radiation-hardened FPGA for real-time image preprocessing, compression, and data reduction before AI inference.

Power~10 W
Technology65nm SRAM
Rad HardeningTMR + Hardened Cells
Cost~$10K+/unit
HeritageExtensive flight heritage

NVIDIA Jetson Thor

AI Inference Engine

Supercomputer-class AI processor for on-board deep learning inference. Enables real-time anomaly detection and classification.

Performance275 TOPS (INT8)
FP Compute2000 TFLOPS (FP4)
Power40–130 W (config.)
ArchitectureBlackwell GPU + Arm V3AE
RequirementRad shielding needed

Processing Pipeline

📷
Image Capture
Raw imagery from telescope
FPGA Pipeline
Denoising, calibration, compression
🧠
AI Inference
Object detection, classification
🚨
Alert Generation
Priority events flagged
📡
Ka-Band TX
High-priority downlink

Alternative Processors

Ubotica CogniSAT
~1 TOPS · 4–6 W · Intel Movidius VPU, space-proven
Xiphos Q8
FPGA + ARM · ~8 W · Zynq UltraScale+, flight heritage
Qualcomm Snapdragon
950 GFLOPS · ~5 W · ISS-tested, needs rad protection
Microsemi RTG4
FPGA · 2–5 W · Flash-based, SEU immune
Constellation Design

Satellites vs Resolution

Walker Delta constellation sizing for different resolution targets at 500km LEO

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Power Budget

Energy Consumption Analysis

Detailed power breakdown per satellite for each resolution scenario

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Solar Panel Sizing

Power Generation System

GaAs triple-junction solar arrays with lithium-ion battery backup for eclipse periods

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Cost Analysis

Financial Assessment

Comprehensive 5-year cost projection for each constellation scenario with hourly revisit capability

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Scenario Comparison

Side-by-Side Analysis

Radar chart and table comparing all three constellation configurations across key performance metrics

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Recommendation & Roadmap

Phased Deployment Strategy

A pragmatic 3-phase approach from moderate resolution proof-of-concept to ultimate high-resolution constellation

Phase 1

Moderate Resolution Deployment

Years 1–3
386 Satellogic-class satellites (46 kg each)
1.0m GSD with hyperspectral capability
Hourly global revisit coverage
Total cost: ~$1.7B (Falcon 9 rideshare)
On-board AI with NVIDIA Jetson Thor
Prove operational concept and market demand
Phase 2

Medium Resolution Upgrade

Years 3–5
Replace aging sats with SkySat-class (117 kg)
Upgrade to 0.5m GSD resolution
254 satellites for hourly coverage
Incremental cost: ~$2.2B over 5 years
Enhanced AI models from Phase 1 learnings
Expand ground station network
Phase 3

High Resolution Constellation

Years 5+
WorldView-class satellites (760 kg)
0.3m GSD — highest commercial resolution
204 satellites for hourly coverage
Requires significant capital: ~$18.3B
Optical laser downlinks (200+ Gbps)
Full real-time global monitoring capability

Key Conclusions

Resolution–Coverage Trade-off

Higher resolution means narrower swath, requiring exponentially more satellites for the same revisit rate.

NVIDIA Thor Dominates Power

The AI processor (~100W) is the primary power consumer on moderate-resolution satellites, requiring careful thermal and power management.

Phased Deployment Is Optimal

Starting with moderate resolution ($1.7B) validates the concept before committing to the $18.3B high-resolution constellation.

Launch Vehicle Choice Matters

SpaceX Falcon 9 rideshare is ~4.5× cheaper per kg than Rocket Lab, saving billions at constellation scale.

Feasibility Study · May 2026 · All calculations documented in engineering workbook