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Cubesats
A CubeSat is a type of miniaturized satellite for space research that usually has a volume of exactly one liter (10 cm cube), has a mass of no more than 1.33 kilograms, and typically uses commercial off-the-shelf components for its electronics.
Satellite Launch Norad Incl.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
CUTE-1 (CO-55)200327844U99º818806101Tracking
CUBESAT XI-IV (CO-57)200327848U99º820808101Tracking
CUBESAT XI-V200528895U98º66864898Tracking
CUTE-1.7+APD II (CO-65)200832785U98º55954896Tracking
CANX-2200832790U98º56955596Tracking
SEEDS II (CO-66)200832791U98º51350995Tracking
SWISSCUBE200935932U98º69468499Tracking
BEESAT-1200935933U98º69568799Tracking
ITUPSAT1200935935U98º70068999Tracking
TISAT 1201036799U98º52051495Tracking
AEROCUBE 4.5A201238767U65º53739994Tracking
STRAND-1201339090U98º775763100Tracking
BRITE-AUSTRIA201339091U98º777764100Tracking
NEE-01 PEGASO201339151U98º60558697Tracking
POPACS 1201339268U81º62428494Tracking
POPACS 2201339269U81º97930898Tracking
POPACS 3201339270U81º115131799Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U98º61054696Tracking
WNISAT-1201339423U98º82058599Tracking
TRITON-1201339427U98º70056597Tracking
GOMX-1201339430U98º76157698Tracking
CUBEBUG-2 (LO-74)201339440U98º64155697Tracking
NEE-02 KRYSAOR201339441U98º66356997Tracking
FUNCUBE-1 (AO-73)201339444U98º59153096Tracking
UWE-3201339446U98º62655296Tracking
BRITE-CA1 (TORONTO)201440020U98º71359998Tracking
DUCHIFAT-1201440021U98º48847694Tracking
NANOSATC-BR1201440024U98º51750795Tracking
QB50P1201440025U98º54452795Tracking
QB50P2201440032U98º54953595Tracking
PERSEUS-M2201440037U98º59657796Tracking
PERSEUS-M1201440039U98º59657796Tracking
POLYITAN-1201440042U98º51950395Tracking
TIGRISAT201440043U98º65558597Tracking
AEROCUBE 6A201440045U98º62156297Tracking
AEROCUBE 6B201440046U98º61655996Tracking
CANX-4201440055U98º63862097Tracking
CANX-5201440056U98º63861997Tracking
UKUBE-1201440074U98º55354896Tracking
BRITE-PL2 (HEWELIUSZ)201440119U98º60058196Tracking
AEROCUBE 5C201540965U65º71948697Tracking
AEROCUBE 7201540966U65º70448297Tracking
FOX-1A (AO-85)201540967U65º71849097Tracking
SINOD-D 1201540968U65º69948697Tracking
SNAP-3 ALICE201540970U65º56844495Tracking
LMRST-SAT201540971U65º72148997Tracking
SNAP-3 EDDIE201540972U65º57044095Tracking
PROPCUBE 3201540973U65º70848497Tracking
BISONSAT201540974U65º63646496Tracking
SNAP-3 JIMI201540975U65º67947696Tracking
PROPCUBE 1 (FLORA)201540976U65º72549497Tracking
SINOD-D 3201540977U65º70648997Tracking
HORYU-4201641340U31º46245394Tracking
RAVAN201641849U98º48247194Tracking
CELTEE 1201641850U98º52452195Tracking
OPTICUBE 04201641851U98º55653496Tracking
AEROCUBE 8D201641852U98º51751095Tracking
AEROCUBE 8C201641853U98º51751095Tracking
PROMETHEUS 2-1201641854U98º42942293Tracking
PROMETHEUS 2-3201641855U98º42842393Tracking
CORVUS BC2201742846U97º56854896Tracking
CORVUS BC1201742847U97º56654996Tracking
MIRATA201743015U98º48536793Tracking
MAKERSAT 0201743016U98º62241995Tracking
SIRION PATHFINDER-2201843759U97º54453095Tracking
CORVUS BC4201843767U97º54753695Tracking
MOVE-II201843780U97º36535692Tracking
SPACEBEE-7201843816U97º46545594Tracking
SHIELDS 1201843850U85º39138392Tracking
SONATE201944400U98º31431091Tracking
DUCHIFAT-3201944854U37º43342993Tracking
M2 PATHFINDER202045727U98º57055196Tracking
NETSAT-4202046504U98º47947294Tracking
NETSAT-3202046505U98º48347794Tracking
NETSAT-1202046506U98º49749194Tracking
NETSAT-2202046507U98º47947494Tracking
WILDTRACKCUBE-SIMBA202147941U97º44042693Tracking
GRBALPHA202147959U97º29929390Tracking
LEDSAT202149069U97º39938492Tracking
GREENCUBE (IO-117)202253109U70º58545832224Tracking
SITRO-AIS 5 (KATYS)202357176U98º51749795Tracking
SITRO-AIS 6 (CHIRKIN)202357192U98º51849895Tracking
SITRO-AIS 8 (ANOKHIN)202357193U98º51349495Tracking
SITRO-AIS 7 (FARTUSHNIY)202357194U98º51849895Tracking
SITRO-AIS 10 (BURDAEV)202357199U98º50048794Tracking
SITRO-AIS 9 (SHCHUKIN)202357201U98º50148894Tracking
SITRO-AIS 12 (SMIRENNIY)202357204U98º50048794Tracking
SITRO-AIS 11 (SHEFFER)202357208U98º49948794Tracking
VERONIKA202358261U97º37336792Tracking
ROBUSTA-1E (ENSO)202358470U97º41139993Tracking
SITRO-AIS 25202459066U95º70949397Tracking
SITRO-AIS 26202459067U95º70949497Tracking
SITRO-AIS 27202459068U95º70849397Tracking
SITRO-AIS 28202459071U95º70849397Tracking
GRBBETA202460237U62º59452496Tracking
OOV-CUBE (TUBSAT-30)202460240U62º60153196Tracking
ROBUSTA-3A (MEDITERRAN*)202460243U62º58851996Tracking
LASARSAT202462391U45º49548394Tracking
CROCUBE202462394U45º49548394Tracking
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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