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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)197407530U10214591440115Tracking
UOSAT 2 (UO-11)198414781U9862661397Tracking
LUSAT (LO-19)199020442U99790774100Tracking
ITAMSAT (IO-26)199322826U99798783101Tracking
RADIO ROSTO (RS-15)199423439U6521521893128Tracking
JAS-2 (FO-29)199624278U991321801106Tracking
TECHSAT 1B (GO-32)199825397U99815811101Tracking
ISS (ZARYA)199825544U5240940293Tracking
PCSAT (NO-44)200126931U67795785101Tracking
SAUDISAT 1C (SO-50)200227607U6569659298Tracking
CUTE-1 (CO-55)200327844U99826810101Tracking
CUBESAT XI-IV (CO-57)200327848U99827812101Tracking
MOZHAYETS 4 (RS-22)200327939U9868066398Tracking
CUBESAT XI-V (CO-58)200528895U9869466998Tracking
CUTE-1.7+APD II (CO-65)200832785U9861459397Tracking
DELFI-C3 (DO-64)200832789U9855653996Tracking
SEEDS II (CO-66)200832791U9860658597Tracking
YUBILEINY (RS-30)200832953U8315081479116Tracking
KKS-1 (KISEKI)200933499U9865063798Tracking
SWISSCUBE200935932U9971070199Tracking
BEESAT200935933U9970970299Tracking
ITUPSAT 1200935935U9971370399Tracking
XIWANG-1 (HOPE-1)200936122U10012041193109Tracking
JUGNU201137839U20864837102Tracking
SRMSAT201137841U20866848102Tracking
M-CUBED & EXP-1 PRIME201137855U10267443096Tracking
STRAND-1201339090U99782768100Tracking
SOMP201339134U6551050595Tracking
BEESAT-3201339135U6552650595Tracking
BEESAT-2201339136U6552750695Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U9866758597Tracking
GOMX 1201339430U9880458899Tracking
CUBEBUG-2 (LO-74)201339440U9869858798Tracking
FUNCUBE-1 (AO-73)201339444U9866458397Tracking
UWE-3201339446U9868358697Tracking
SPROUT201439770U9861360297Tracking
UNISAT-6201440012U9868960998Tracking
DUCHIFAT-1201440021U9860558897Tracking
FUNCUBE-3 (EO-79)201440025U9861059497Tracking
NUDT-PHONESAT201540900U9751149095Tracking
ZDPS 2A201540901U9752550495Tracking
ZDPS 2B201540902U9752550495Tracking
XW-2A201540903U9745443393Tracking
KAITUO 1A201540904U9753250995Tracking
2015-049G201540905U9753651295Tracking
XW-2C201540906U9753150995Tracking
XW-2D201540907U9753050895Tracking
LILACSAT 2201540908U9753751395Tracking
XW-2F201540910U9752750495Tracking
XW-2B201540911U9753150995Tracking
KAITUO 1B201540912U9752049795Tracking
TIANWANG 1C (TW-1C)201540926U9742141093Tracking
TIANWANG 1A (TW-1A)201540928U9745644194Tracking
LAPAN-A2 (IO-86)201540931U665063198Tracking
E-ST@R-II201641459U9867043596Tracking
AAUSAT 4201641460U9865943696Tracking
NUSAT 1 (LO-87)201641557U9749447594Tracking
BEESAT-4201641619U9750549295Tracking
ALSAT 1N201641789U9870065998Tracking
CAS-2T & KS-1Q201641847U991026504100Tracking
NAYIF-1 (EO-88)201742017U9749748694Tracking
LILACSAT-1199842725U5234834691Tracking
MAX VALIER SAT201742778U9751149195Tracking
FOX-1B (AO-91)201743017U9881645397Tracking
FOX-1D (AO-92)201843137U9850449095Tracking
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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