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🔤 Space Reference

Space & Orbital Mechanics Glossary

217 terms defined — from orbit types and orbital elements to satellite tracking, space debris, and manoeuvres. Each term explained in plain language with diagrams, key data, and links to live trackers.

🎓 Orbital Academy — Learn these terms in context with interactive training tracks & slide-deck lessons
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Tracking & Space Surveillance

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How satellites and debris are detected, catalogued, and monitored. From radar systems and tracking formats to the identification standards that underpin global space situational awareness.

TLE TLE Standard format for satellite orbit data 32,110 live2 (+ optional name) NI NORAD ID Unique tracking number for every space object 32,110 live25544 SF Space Fence US Space Force radar for detecting small debris Kwajalein AtollS-band radar SGP4 SGP4 The algorithm that predicts satellite positions from TLEs TLE data1 km (fresh TLE) CI COSPAR ID International launch-based object identifier YYYY-NNNP1998-067A SSA SSA Knowing what's in orbit and where it's going 32,110 liveUS SSN (18th SDS) E Ephemeris Predicted position table for a space object over time TLE + SGP4OEM (numerical) RCS RCS Measure of how detectable an object is to radar 400 m²0.01 m² ST Space-Track US Space Force's public satellite catalogue 32,110 live DSN DSN NASA's global array of antennas for communicating with distant spacecraft 70 m diameterNASA JPL T Twilight The dusk/dawn window when satellites are visible Sun 0–6° below horizon EA Elevation Angle How high a satellite climbs above the horizon Above 40° AM Apparent Magnitude How bright a satellite looks — lower is brighter ≈ +6≈ −4 ES Earth's Shadow The cone of darkness that makes satellites vanish LEO satellites SA Sky Arc The curved path a satellite traces across the sky Peak elevationSky-dome diagram A5 Alpha-5 How catalogue numbers grew past 99,999 without breaking the TLE 32,110 live100000–339999 ELSET Elset One snapshot of an orbit, packaged for a propagator 6 mean elements + dragSGP4 / SDP4 SV State Vector Position and velocity — an orbit in six numbers J2000 · TEME · ECEFMetres C Covariance The uncertainty cloud around every predicted position 6×6 matrixPrediction horizon UCT UCT A radar return that matches nothing in the catalogue Tracking & Space Surveillance CT Cross-Tagging When two satellites swap identities in the catalogue Batch deployments AO Analyst Object Tracked, numbered — but not yet officially in the catalogue Unattributed originYes GS Ground Station The Earth end of every satellite link ~5–12 min per passAntenna-as-a-service ST Starlink Train That eerie line of lights crossing the night sky Tracking & Space Surveillance SF Satellite Flare A satellite catching the Sun like a moving mirror Seconds100–1000× in seconds IF Iridium Flare The sky's most punctual spectacle — now history To magnitude −8+1997 → ~2019 SS Satellite Streak The bright line a satellite draws through a photograph Darken · dodge · maskStreaks as census data ST Satellite Transit A satellite seen crossing the face of the Sun or the Moon About 0.5 to 2 secondsUp to about 1′ across TC Transit Corridor The strip of ground from which a satellite transit can be seen About 4 km20 km or more AD Angular Diameter How large an object looks in the sky, measured as an angle About 32′About 29′ to 34′ PA Position Angle A direction on the sky, measured from north through east Celestial north (0°)Through east A Appulse A close approach in the sky without one object crossing the other Minutes of arcAn orbital conjunction
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Manoeuvres & Propulsion

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The physics and operations of changing orbits — from collision avoidance and orbit raising to interplanetary transfers. Every manoeuvre costs delta-v, the fundamental currency of spaceflight.

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Debris & Space Safety

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The growing challenge of orbital debris — how collisions are predicted, how satellites dodge threats, and the rules and technologies being developed to keep space sustainable.

CA Conjunction Assessment Screening for potential collisions in orbit 32,110 live18th SDS (USSF) KS Kessler Syndrome Self-sustaining cascade of orbital collisions 32,110 live1978 (Donald Kessler) P Passivation Depleting stored energy to prevent explosions 650+ (all time)IADC / UN COPUOS 2YR 25-Year Rule Guideline for post-mission deorbit timeline 25 years5 years OD Orbital Decay Gradual altitude loss due to atmospheric drag Days to weeks1–2 years ADR ADR Missions to capture and deorbit defunct objects ADRAS-J (2024)ClearSpace-1 (2026) FE Fragmentation Event Breakup of a space object into debris 650+ SD Space Debris Defunct satellites, rocket bodies, and fragments orbiting Earth 36,500+1,000,000 ASAT ASAT A weapon designed to destroy or disable satellites in orbit Debris & Space Safety CRE Controlled Re-entry A guided return to Earth targeting an uninhabited ocean area SPOUA (Point Nemo)48°52'S, 123°23'W CE Casualty Expectation The 1-in-10,000 rule that governs re-entry risk Ec < 1 in 10,000Design for demise CDM CDM The standard warning message for a predicted close approach CCSDS formatSeries per event PC Pc The number that decides whether a satellite dodges ~10⁻⁴ (1-in-10,000)Trend across CDMs TCA TCA The instant two orbits nearly touch 7–15 km/sHours-to-TCA SV Screening Volume The alarm perimeter drawn around a protected satellite Ellipsoid / box~5–7 days ahead HBR Hard-Body Radius How big two objects are, as far as a collision is concerned ~1–20 m combinedConservative (~20 m) DC Debris Cloud What one breakup becomes: a shell of shrapnel in orbit Swarm → ring → shellGabbard diagram WS Whipple Shield The thin wall that sacrifices itself to stop hypervelocity debris ~mm–cm debris PR Protected Regions The two orbital zones the world agreed to keep clean GEO ±200 km, ±15° lat
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Spacecraft Systems

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The subsystems that make up a satellite — from the bus and payload to attitude control, power, thermal management, and communications.

SB Satellite Bus The main structural and support platform of a satellite 10 cm cube, ~1–2 kg P Payload The mission-specific equipment aboard a satellite Atomic clocksThe whole spacecraft T Transponder Communications relay unit on a satellite C, Ku, Ka, V24–72 per GEO sat AC Attitude Control Keeping a satellite pointed in the right direction 0.01°0.05–0.1° RW Reaction Wheel Spinning wheel used to precisely rotate a satellite None — electric motorMomentum saturation ST Star Tracker Camera that determines orientation by identifying stars 1–10 arcsecondsStar pattern matching SA Solar Array Panels that convert sunlight into electrical power 1,361 W/m² at 1 AULi-ion batteries T TT&C Communications link between satellite and ground control Uplink of instructionsS-band (~2 GHz) TC Thermal Control Keeping satellite temperatures within safe limits 120°C+−150°C PS Power Subsystem Generating, storing, and distributing electrical power Lithium-ion batteriesPCU holds bus voltage C C&DH The satellite's onboard computer and data system RAD750, LEON, FPGAFDIR (fault detection) M Magnetorquer Electromagnetic coil for attitude control using Earth's field NoneLow (1–5°) MW Momentum Wheel Constantly spinning wheel providing gyroscopic stability CMG (ISS uses 4) SS Sun Sensor Optical sensor that detects the Sun's direction 5° accuracy0.01–0.1° ES Earth Sensor Infrared sensor detecting Earth's thermal horizon 0.05–0.5°Scanning, static array AG Antenna Gain Measure of how focused an antenna's signal is Spacecraft Systems C CubeSat A standardised small satellite built in 10 cm cube units 10 × 10 × 11.35 cm≤ 2 kg IT Ion Thruster An electric propulsion system that accelerates ionised gas to produce thrust 2,000–5,000 s20–50 km/s T TT&C The housekeeping link that keeps a satellite a satellite Works while tumblingRange + range-rate U Uplink The Earth-to-space half of every satellite link Ground → spaceHigher sub-band up D Downlink The space-to-Earth half — where every satellite earns its keep Space → groundSpacecraft power
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Launch & Ascent

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Key concepts in getting to orbit — launch windows, staging, orbital insertion, and the variables that determine what a rocket can carry and where.

LW Launch Window Time period when a rocket can reach the target orbit 1–4 hoursEvery 26 months OI Orbital Insertion The burn that places a spacecraft into orbit 7.8 km/s PF Payload Fairing Protective nose cone that shields payload during launch ~110 km5.2 m S Staging Discarding empty rocket sections during ascent 2.5 min after launch3 stages LA Launch Azimuth Compass heading of a rocket's ascent trajectory 35–120° range170–240° (polar/SSO) MAXQ Max-Q Peak aerodynamic stress during ascent ~60-80 s after liftoff~11-14 km MECO MECO Shutdown of first-stage engines before separation 2.5 min / 80 km8.5 min into flight PC Payload Capacity Maximum mass a rocket can deliver to a given orbit 22,800 kg~17,500 kg DI Direct Insertion Placing a satellite directly into its target orbit Launch & Ascent DL Dog-Leg Mid-ascent trajectory turn to reach a different inclination Yaw turn during ascent RR Reusable Rocket A launch vehicle designed to be recovered and re-flown Falcon 9, Dec 2015Falcon 9, Mar 2017 LC Launch Cost The price per kilogram to deliver payload to orbit ~$54,000/kg~$2,700/kg RM Rideshare Mission Many small satellites sharing one rocket to cut launch costs 143 satellitesSSO ~500–600 km SF Suborbital Flight Reaching space without reaching orbit Space without orbit~1 km/s SF Static Fire Lighting the rocket without letting it leave Seconds at the pad HS Hot Staging Lighting the next stage before dropping the last one Ignite, then separate DL Droneship Landing Catching a booster on a barge in the open ocean Launch & Ascent BB Boostback Burn The burn that turns a booster around mid-flight Just after separationReverses course → RTLS
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Space Environment

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The space environment that satellites must survive — radiation belts, solar storms, atmospheric drag, and the geomagnetic phenomena that affect spacecraft and ground systems.

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Satellite Internet & Mega-Constellations

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The technology behind broadband from space — mega-constellations, laser inter-satellite links, ground terminals, latency, and the race to connect the unconnected.

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Eclipses

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The words behind solar and lunar eclipses: the shadows that make them, the moments that time them, the cycle that repeats them and the sights that only totality reveals.

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