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Starlink Commander — Real-Time Constellation Tracker

Live SGP4 propagation · phased array Ku/Ka link analysis · LEO tactical operations

~7,400 active satellites · 2,500+ V2 Mini in orbit · TLE source: celestrak.org · Propagator: satellite.js (SGP4) · Updated: --
[INITIALIZING...]
0
Visible
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Satellite Data
NORAD---
NAME---
ALTITUDE---
VELOCITY---
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AZIMUTH---
Orbital Elements
STATUSNO SATELLITE
ACTIONSELECT SAT
Mission Status & RF Link
STATUS: INITIALIZING
RENDER: 0 ms
LINK: OPERATIONAL
FREQ DL:10.7-12.7 GHz
FREQ UL:14.0-14.5 GHz
RX POWER:---
FSPL:---
LINK STATUS:---
Target Operation
Orbit Filters
3D Controls
Target Details
SAT ID:---
ELEV:---
AZIM:---
RANGE:---
Satellite Status
HIGH ALT (>600km)
MED ALT (550-600km)
NORM ALT (500-550km)
LOW ALT (<500km)
SELECTED
NOT VISIBLE
Globe Statistics
SATELLITES:0
FPS:0
ROTATION:OFF
ORBITS:ACTIVE
TIME:00:00:00
Altitude Color Code
HIGH (>600km)
MEDIUM (550-600km)
NORMAL (500-550km)
LOW (<500km)
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Quick Links
🚀SpaceX Launches Official SpaceX launch manifest 🛰Starlink Official Starlink service & coverage map 📡CelesTrak Starlink TLE Live TLE data source 🗺SatelliteMap.space Alternative 3D Starlink map 📊Jonathan's Space Report Starlink statistics & timeline 🛸Orbital Command ISS & Tiangong tracker 💾Source Code GitHub repository
Spacecraft Structure — Generation Selector
STARLINK V1.5 · BUS F9-1 SCALE: 1 unit ≈ 0.5 m ~8.1 m array (single wing) [1] SINGLE SOLAR ARRAY~8.1 m · ~2 kW [2] FLAT-PANEL BUS~295–306 kg [3] Ku/Ka PHASED ARRAYEarth-facing [4] LASER ISLlater units only [5] KRYPTON HALL THRUSTERion propulsion velocity nadir (Earth)

Bus & Mass

Generationv1.5 (laser)
Mass~295–306 kg
Form factorFlat panel
Solar arrays1 (single wing)
Per F9 launch~46–60 sats
Design life~5 years

Propulsion

ThrusterKrypton Hall

Communications

User linkKu 10.7–12.7 GHz
GatewayKa-band
ISLLaser (some units)
DL per sat~17–20 Gbps

Orbit

Altitude~540–570 km
Inclination53.2° / 70° / 97.6°
Units launched~2,987
Solar array
Bus chassis
Phased array (Ku/Ka)
Laser ISL
Krypton Hall thruster
STARLINK V2 MINI · BUS F9-2 SCALE: 1 unit ≈ 0.5 m ~30 m wingspan (deployed) [1] SOLAR ARRAY ×22 × 52.5 m² · 30 m span [2] MAIN BUS4.1 × 2.7 m · ~740 kg [3] STAR TRACKERattitude determination [4] PHASED ARRAYKu/Ka/E-band · Earth-facing [5] LASER ISLoptical mesh [6] ARGON HALL THRUSTER170 mN · 2500 s Isp · 4.2 kW velocity nadir (Earth)

Bus & Mass

Generationv2 Mini
Dimensions4.1 × 2.7 m
Mass~740 kg
Wingspan~30 m
Solar arrays2 × 52.5 m²
Per F9 launch21–29 sats

Propulsion

ThrusterArgon Hall
Thrust170 mN
Isp2500 s

Communications

DownlinkKu 10.7–12.7 GHz
UplinkKa 14.0–14.5 GHz
BackhaulE-band 71–86 GHz
DL per sat~80–100 Gbps

Orbit

Altitude540–570 km
Inclination43° / 53°
Units launched~7,424
Solar array
Bus chassis
Phased array (Ku/Ka)
Laser ISL
Argon Hall thruster
Star tracker
STARLINK V3 · STARSHIP-CLASS SCALE: 1 unit ≈ 1.0 m ~60 m wingspan (deployed) [1] LARGE SOLAR ARRAY ×2~60 m span · high-power [2] STARSHIP-CLASS BUS~1,900 kg · 7–8 m base [3] Ku/Ka + E-BAND ARRAY1 Tbps DL · gigabit-to-user [4] LASER ISL ×3full optical mesh [5] ARGON HALL THRUSTER ×2station-keeping [6] STAR TRACKER velocity nadir (Earth)

Bus & Mass

Generationv3 (terabit)
Mass~1,900 kg
Base~7–8 m
Wingspan~60 m
Solar arrays2 (large)
Launch vehicleStarship
Per launch~60 Tbps added

Propulsion

ThrusterArgon Hall ×2

Communications

User linkKu / Ka
High-bandE-band (80 GHz)
Downlink/sat>1 Tbps
Uplink/sat>200 Gbps
Latency<20 ms
ISLFull laser mesh

Status

Starship V3 debut22 May 2026
First operationalH1 2026 (target)
RegimeLEO
Large solar array
Starship-class bus
Ku/Ka + E-band array
Laser ISL ×3
Argon Hall thruster ×2
Mass
~300 kg
v1.5
Mass
~740 kg
v2 Mini
Mass
~1,900 kg
v3
DL / sat
~20 → 100 → 1000+ Gbps
v1.5 → v2 → v3
System Log
rmayormartins.github.io/starlink-commander · orbital-command · github · celestrak TLE
Ramon Mayor Martins, Ph.D. · IFSC · Leaflet + satellite.js + Three.js