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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
UOSAT 2 (UO-11)198414781U98º62661397Tracking
LUSAT (LO-19)199020442U99º791773100Tracking
ITAMSAT (IO-26)199322826U99º796784101Tracking
RADIO ROSTO (RS-15)199423439U65º21511894128Tracking
JAS-2 (FO-29)199624278U99º1322800106Tracking
TECHSAT 1B (GO-32)199825397U99º814812101Tracking
ISS (ZARYA)199825544U52º40840393Tracking
PCSAT (NO-44)200126931U67º795785101Tracking
SAUDISAT 1C (SO-50)200227607U65º69759098Tracking
CUTE-1 (CO-55)200327844U99º825811101Tracking
CUBESAT XI-IV (CO-57)200327848U99º827812101Tracking
MOZHAYETS 4 (RS-22)200327939U98º68266198Tracking
CUBESAT XI-V (CO-58)200528895U98º69466998Tracking
CUTE-1.7+APD II (CO-65)200832785U98º61259597Tracking
DELFI-C3 (DO-64)200832789U97º55553996Tracking
SEEDS II (CO-66)200832791U98º60458797Tracking
YUBILEINY (RS-30)200832953U82º15081479116Tracking
KKS-1 (KISEKI)200933499U98º65063898Tracking
SWISSCUBE200935932U99º71170099Tracking
BEESAT200935933U99º70970199Tracking
ITUPSAT 1200935935U99º71470299Tracking
XIWANG-1 (HOPE-1)200936122U100º12041193109Tracking
JUGNU201137839U20º864837102Tracking
SRMSAT201137841U20º866849102Tracking
M-CUBED & EXP-1 PRIME201137855U102º67443096Tracking
STRAND-1201339090U99º781769100Tracking
SOMP201339134U65º51150395Tracking
BEESAT-3201339135U65º52250895Tracking
BEESAT-2201339136U65º52450995Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U98º66958497Tracking
GOMX 1201339430U98º80259099Tracking
CUBEBUG-2 (LO-74)201339440U98º70058698Tracking
FUNCUBE-1 (AO-73)201339444U98º66558297Tracking
UWE-3201339446U98º68558597Tracking
SPROUT201439770U98º61460197Tracking
UNISAT-6201440012U98º69060798Tracking
DUCHIFAT-1201440021U98º60658797Tracking
FUNCUBE-3 (EO-79)201440025U98º61159297Tracking
NUDT-PHONESAT201540900U97º50849295Tracking
ZDPS 2A201540901U97º52350595Tracking
ZDPS 2B201540902U97º52350695Tracking
XW-2A201540903U97º45243593Tracking
KAITUO 1A201540904U97º53051195Tracking
2015-049G201540905U97º53451495Tracking
XW-2C201540906U97º52951095Tracking
XW-2D201540907U97º52851095Tracking
LILACSAT 2201540908U97º53651595Tracking
XW-2F201540910U97º52550695Tracking
XW-2B201540911U97º52951095Tracking
KAITUO 1B201540912U97º51849995Tracking
TIANWANG 1C (TW-1C)201540926U97º42040693Tracking
TIANWANG 1A (TW-1A)201540928U97º45544194Tracking
LAPAN-A2 (IO-86)201540931U6º65063098Tracking
E-ST@R-II201641459U98º67143496Tracking
AAUSAT 4201641460U98º65943596Tracking
NUSAT 1 (LO-87)201641557U97º49547594Tracking
BEESAT-4201641619U97º50749095Tracking
ALSAT 1N201641789U98º70065998Tracking
CAS-2T & KS-1Q201641847U99º1026504100Tracking
NAYIF-1 (EO-88)201742017U97º49548894Tracking
LILACSAT-1199842725U52º34133691Tracking
MAX VALIER SAT201742778U97º50949395Tracking
FOX-1B (AO-91)201743017U98º81645497Tracking
FOX-1D (AO-92)201843137U98º50449095Tracking
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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