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Amateur Radio Satellites
The table below shows the information available in our database and located in the group of Satellites of Amateur Radio Satellites. This satellites are used, constructed and operated by radio amateurs from various parts of the world, with the aim of providing and developing communications between the technical community.
Satellite Launch Norad Incl.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
OSCAR 7 (AO-7)197407530U102º14591440115Tracking
PHASE 3B (AO-10)198314129U27º354763972699Tracking
UOSAT 2 (UO-11)198414781U98º61460497Tracking
LUSAT (LO-19)199020442U99º788772100Tracking
EYESAT A (AO-27)199322825U99º796785101Tracking
ITAMSAT (IO-26)199322826U99º795783101Tracking
RADIO ROSTO (RS-15)199423439U65º21491895128Tracking
JAS-2 (FO-29)199624278U99º1320801106Tracking
TECHSAT 1B (GO-32)199825397U99º812811101Tracking
ISS (ZARYA)199825544U52º41741293Tracking
PCSAT (NO-44)200126931U67º792783101Tracking
SAUDISAT 1C (SO-50)200227607U65º65561297Tracking
CUTE-1 (CO-55)200327844U99º821808101Tracking
CUBESAT XI-IV (CO-57)200327848U99º823810101Tracking
MOZHAYETS 4 (RS-22)200327939U98º67065498Tracking
CUBESAT XI-V200528895U98º68165898Tracking
CUTE-1.7+APD II (CO-65)200832785U98º58857096Tracking
SEEDS II (CO-66)200832791U98º56455496Tracking
YUBILEINY (RS-30)200832953U82º15081479116Tracking
KKS-1 (KISEKI)200933499U98º63962997Tracking
SWISSCUBE200935932U98º70369199Tracking
BEESAT-1200935933U98º70269399Tracking
ITUPSAT1200935935U98º70769599Tracking
XIWANG-1 (HOPE-1)200936122U100º12041193109Tracking
O/OREOS (USA 219)201037224U72º61859897Tracking
JUGNU201137839U20º862835102Tracking
SRMSAT201137841U20º864847102Tracking
M-CUBED & EXP-1 PRIME201137855U102º41034192Tracking
STRAND-1201339090U98º779765100Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U98º63756797Tracking
GOMX-1201339430U98º78158098Tracking
CUBEBUG-2 (LO-74)201339440U98º67257097Tracking
FUNCUBE-1 (AO-73)201339444U98º62756197Tracking
UWE-3201339446U98º65656997Tracking
SPROUT201439770U98º47046194Tracking
UNISAT-6201440012U98º66959397Tracking
DUCHIFAT-1201440021U98º55754296Tracking
QB50P1201440025U98º57656596Tracking
KAITUO 1A201540904U97º44543193Tracking
XW-2C201540906U97º45644194Tracking
XW-2D201540907U97º43842493Tracking
LILACSAT-2201540908U98º49948194Tracking
XW-2B201540911U97º44042693Tracking
LAPAN-A2201540931U64662797Tracking
E-ST@R-II201641459U98º29526790Tracking
CAS-2T & KS-1Q201641847U98º1008502100Tracking
ZHUHAI-1 02 (CAS-4B)201742759U43º49647994Tracking
ZHUHAI-1 01 (CAS-4A)201742761U43º49547994Tracking
MAX VALIER SAT201742778U97º36035592Tracking
RADFXSAT (FOX-1B)201743017U98º74244197Tracking
DIWATA-2B201843678U98º58857696Tracking
ES'HAIL 2201843700U35793357791436Tracking
FOX-1CLIFF (AO-95)201843770U98º56254296Tracking
ITASAT201843786U98º56954396Tracking
JY1SAT (JO-97)201843803U98º55654096Tracking
UWE-4201843880U98º55353095Tracking
JAISAT-1201944419U98º36135292Tracking
DUCHIFAT-3201944854U37º52851795Tracking
TIANYAN 01201944881U98º62960797Tracking
RS-44 & BREEZE-KM R/B201944909U83º15111174113Tracking
BY70-2202045857U98º51350895Tracking
SALSAT202046495U98º54051895Tracking
UVSQ-SAT202147438U97º44443593Tracking
LEDSAT202149069U97º51248395Tracking
XW-3 (CAS-9)202150466U99º762758100Tracking
TEVEL-3202250988U97º41040393Tracking
TEVEL-8202250989U97º41040393Tracking
TEVEL-5202250998U97º40039392Tracking
TEVEL-6202250999U97º40039392Tracking
TEVEL-1202251013U97º41040393Tracking
TEVEL-7202251062U97º41040393Tracking
TEVEL-4202251063U97º41140493Tracking
TEVEL-2202251069U97º41040393Tracking
GREENCUBE202253106U70º58535834224Tracking
KUZBASS-300 (RS34S)202253375U97º31830891Tracking
UTMN (RS23S)202253376U97º29027990Tracking
MIET-AIS (RS28S)202253377U97º35034291Tracking
KAI-1 (RS26S)202253378U97º39138492Tracking
ISOI (RS19S)202253381U97º34233591Tracking
CUBESX-HSE-2 (RS21S)202253383U97º29328390Tracking
SIREN (RS30S)202253384U97º36836292Tracking
CAS-5A (FO-118)202254684U98º49247894Tracking
STRATOSAT-TK 1 (RS52S)202357167U98º54452595Tracking
UMKA 1 (RS40S)202357172U98º55753596Tracking
CUBESX-HSE 3 (RS42S)202357178U98º55453296Tracking
MONITOR-4 (RS57S)202357182U98º55553396Tracking
MONITOR-2 (RS39S)202357184U98º55453696Tracking
SVYATOBOR 1 (RS60S)202357187U98º55053395Tracking
VIZARD-METEO (RS38S)202357189U98º54653095Tracking
NANOZOND 1 (RS49S)202357190U98º53852595Tracking
POLYTECH-UNIVERSE 3 (R*)202357191U98º55853396Tracking
UTMN 2 (RS27S)202357203U98º54753195Tracking
ARCCUBE 1 (RS25S)202357205U98º53652395Tracking
KUZGTU 1 (RS47S)202357217U98º55453296Tracking
HADES-D (SO-121)202358567U97º50248594Tracking
Satellites Orbital Parameters

The table above shows the main parameters and information available for this satellite.

Satellite: This column shows the name of the object in orbit. In some cases the official name ends with the words R/B, meaning that it is a piece or any stage from some rocket booster.

Norad: North American Aerospace Defense Command, the Air Defence Command of the United States, responsible for the catalogue of objects in orbit. The number indicates the record of the satellite in the Norad archives.

Inclination: Angle formed between the orbit of the satellite and terrestrial line of the equator. Satellites with inclination of 0 degrees follow the equator line and are called equatorial orbit satellites. When the inclination is 90 degrees its orbit crosses the terrestrial poles and are called polar orbiting satellites. When the inclination is less or equal latitude of the place of observation, the satellite be seen directly if conditions permit.

Apogee: Maximum distance that the object is far from the center of the Earth.

Perigee: Highest approchement between the object and the center of the Earth. The figures shown already discounting the radius of the Earth, 6378 Km. One Perigee value equal to the value of Apogee indicates a circular orbit satellite.

Period: Value in minutes that a satellite takes to complete one orbit of perigee to perigee. Satellites in polar orbit, positioned at 800 km in altitude will take approximately 102 minutes to complete one revolution. The International Space Station, 350 km above the surface, completes its orbit in 90 minutes.

The lower the altitude of a satellite, more speed he needs to keep in orbit and not re-enters the atmosphere.

Geostationary satellites have a period of approximately 1436 minutes with inclination of 0 degrees (equatorial orbit). Because this is the same time it takes Earth to complete one turn on its axis, geostationary satellites appear static on the same geographic point. To this happens the satellite should be positioned about 36 thousand kilometers in altitude.

Note and Frequency: Filled with additional information where possible. The frequencies shown, when provided, are those captured by enthusiasts or informed by the official organizations of disclosure.

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