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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)197407530U10214581440115Tracking
UOSAT 2 (UO-11)198414781U9862561597Tracking
LUSAT (LO-19)199020442U99790774100Tracking
ITAMSAT (IO-26)199322826U99797784101Tracking
RADIO ROSTO (RS-15)199423439U6521531892128Tracking
JAS-2 (FO-29)199624278U991321801106Tracking
TECHSAT 1B (GO-32)199825397U99814812101Tracking
ISS (ZARYA)199825544U5240940193Tracking
PCSAT (NO-44)200126931U67795784101Tracking
SAUDISAT 1C (SO-50)200227607U6569459398Tracking
CUTE-1 (CO-55)200327844U99825811101Tracking
CUBESAT XI-IV (CO-57)200327848U99826813101Tracking
MOZHAYETS 4 (RS-22)200327939U9868066398Tracking
CUBESAT XI-V (CO-58)200528895U9869367098Tracking
CUTE-1.7+APD II (CO-65)200832785U9861359497Tracking
DELFI-C3 (DO-64)200832789U9855753896Tracking
SEEDS II (CO-66)200832791U9860658697Tracking
YUBILEINY (RS-30)200832953U8315091478116Tracking
KKS-1 (KISEKI)200933499U9865163798Tracking
SWISSCUBE200935932U9971170099Tracking
BEESAT200935933U9971070199Tracking
ITUPSAT 1200935935U9971470299Tracking
XIWANG-1 (HOPE-1)200936122U10012041193109Tracking
JUGNU201137839U20864837102Tracking
SRMSAT201137841U20866849102Tracking
M-CUBED & EXP-1 PRIME201137855U10267543196Tracking
STRAND-1201339090U99782767100Tracking
SOMP201339134U6551250495Tracking
BEESAT-3201339135U6552850395Tracking
BEESAT-2201339136U6552950595Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U9866758697Tracking
GOMX 1201339430U9880458899Tracking
CUBEBUG-2 (LO-74)201339440U9869958798Tracking
FUNCUBE-1 (AO-73)201339444U9866358497Tracking
UWE-3201339446U9868358697Tracking
SPROUT201439770U9861460197Tracking
UNISAT-6201440012U9869060898Tracking
DUCHIFAT-1201440021U9860558897Tracking
FUNCUBE-3 (EO-79)201440025U9861059397Tracking
NUDT-PHONESAT201540900U9751149195Tracking
ZDPS 2A201540901U9752450595Tracking
ZDPS 2B201540902U9752550595Tracking
XW-2A201540903U9745443493Tracking
KAITUO 1A201540904U9753151095Tracking
2015-049G201540905U9753551395Tracking
XW-2C201540906U9753150995Tracking
XW-2D201540907U9753050995Tracking
LILACSAT 2201540908U9753751495Tracking
XW-2F201540910U9752750595Tracking
XW-2B201540911U9753051095Tracking
KAITUO 1B201540912U9752049895Tracking
TIANWANG 1C (TW-1C)201540926U9742440993Tracking
TIANWANG 1A (TW-1A)201540928U9745844094Tracking
LAPAN-A2 (IO-86)201540931U664963198Tracking
E-ST@R-II201641459U9867043696Tracking
AAUSAT 4201641460U9865943796Tracking
NUSAT 1 (LO-87)201641557U9749347794Tracking
BEESAT-4201641619U9750749195Tracking
ALSAT 1N201641789U9869966198Tracking
CAS-2T & KS-1Q201641847U991028503100Tracking
NAYIF-1 (EO-88)201742017U9749748794Tracking
LILACSAT-1199842725U5235435092Tracking
MAX VALIER SAT201742778U9751049395Tracking
FOX-1B (AO-91)201743017U9881845297Tracking
FOX-1D (AO-92)201843137U9850349295Tracking
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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