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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)197407530U102º14581440115Tracking
UOSAT 2 (UO-11)198414781U98º62561597Tracking
LUSAT (LO-19)199020442U99º790774100Tracking
ITAMSAT (IO-26)199322826U99º797784101Tracking
RADIO ROSTO (RS-15)199423439U65º21531892128Tracking
JAS-2 (FO-29)199624278U99º1321801106Tracking
TECHSAT 1B (GO-32)199825397U99º814812101Tracking
ISS (ZARYA)199825544U52º40940193Tracking
PCSAT (NO-44)200126931U67º795784101Tracking
SAUDISAT 1C (SO-50)200227607U65º69459398Tracking
CUTE-1 (CO-55)200327844U99º825811101Tracking
CUBESAT XI-IV (CO-57)200327848U99º826813101Tracking
MOZHAYETS 4 (RS-22)200327939U98º68066398Tracking
CUBESAT XI-V (CO-58)200528895U98º69367098Tracking
CUTE-1.7+APD II (CO-65)200832785U98º61359497Tracking
DELFI-C3 (DO-64)200832789U98º55753896Tracking
SEEDS II (CO-66)200832791U98º60658697Tracking
YUBILEINY (RS-30)200832953U83º15091478116Tracking
KKS-1 (KISEKI)200933499U98º65163798Tracking
SWISSCUBE200935932U99º71170099Tracking
BEESAT200935933U99º71070199Tracking
ITUPSAT 1200935935U99º71470299Tracking
XIWANG-1 (HOPE-1)200936122U100º12041193109Tracking
JUGNU201137839U20º864837102Tracking
SRMSAT201137841U20º866849102Tracking
M-CUBED & EXP-1 PRIME201137855U102º67543196Tracking
STRAND-1201339090U99º782767100Tracking
SOMP201339134U65º51250495Tracking
BEESAT-3201339135U65º52850395Tracking
BEESAT-2201339136U65º52950595Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U98º66758697Tracking
GOMX 1201339430U98º80458899Tracking
CUBEBUG-2 (LO-74)201339440U98º69958798Tracking
FUNCUBE-1 (AO-73)201339444U98º66358497Tracking
UWE-3201339446U98º68358697Tracking
SPROUT201439770U98º61460197Tracking
UNISAT-6201440012U98º69060898Tracking
DUCHIFAT-1201440021U98º60558897Tracking
FUNCUBE-3 (EO-79)201440025U98º61059397Tracking
NUDT-PHONESAT201540900U97º51149195Tracking
ZDPS 2A201540901U97º52450595Tracking
ZDPS 2B201540902U97º52550595Tracking
XW-2A201540903U97º45443493Tracking
KAITUO 1A201540904U97º53151095Tracking
2015-049G201540905U97º53551395Tracking
XW-2C201540906U97º53150995Tracking
XW-2D201540907U97º53050995Tracking
LILACSAT 2201540908U97º53751495Tracking
XW-2F201540910U97º52750595Tracking
XW-2B201540911U97º53051095Tracking
KAITUO 1B201540912U97º52049895Tracking
TIANWANG 1C (TW-1C)201540926U97º42440993Tracking
TIANWANG 1A (TW-1A)201540928U97º45844094Tracking
LAPAN-A2 (IO-86)201540931U6º64963198Tracking
E-ST@R-II201641459U98º67043696Tracking
AAUSAT 4201641460U98º65943796Tracking
NUSAT 1 (LO-87)201641557U97º49347794Tracking
BEESAT-4201641619U97º50749195Tracking
ALSAT 1N201641789U98º69966198Tracking
CAS-2T & KS-1Q201641847U99º1028503100Tracking
NAYIF-1 (EO-88)201742017U97º49748794Tracking
LILACSAT-1199842725U52º35435092Tracking
MAX VALIER SAT201742778U97º51049395Tracking
FOX-1B (AO-91)201743017U98º81845297Tracking
FOX-1D (AO-92)201843137U98º50349295Tracking
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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