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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)200327844U99º818805101Tracking
CUBESAT XI-IV (CO-57)200327848U99º821807101Tracking
CUBESAT XI-V200528895U98º66864698Tracking
CUTE-1.7+APD II (CO-65)200832785U98º55754596Tracking
CANX-2200832790U98º56655496Tracking
SEEDS II (CO-66)200832791U98º50650495Tracking
SWISSCUBE200935932U98º69468399Tracking
BEESAT-1200935933U98º69568699Tracking
ITUPSAT1200935935U98º70168899Tracking
TISAT 1201036799U98º51350995Tracking
AEROCUBE 4.5A201238767U65º52039194Tracking
STRAND-1201339090U98º776762100Tracking
BRITE-AUSTRIA201339091U98º779763100Tracking
NEE-01 PEGASO201339151U98º60458497Tracking
POPACS 1201339268U81º55427793Tracking
POPACS 2201339269U81º96530797Tracking
POPACS 3201339270U81º113831899Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U98º60654596Tracking
WNISAT-1201339423U98º82058499Tracking
TRITON-1201339427U98º69856497Tracking
GOMX-1201339430U98º76057698Tracking
CUBEBUG-2 (LO-74)201339440U98º63855597Tracking
NEE-02 KRYSAOR201339441U98º66256797Tracking
FUNCUBE-1 (AO-73)201339444U98º58652896Tracking
UWE-3201339446U98º62355196Tracking
BRITE-CA1 (TORONTO)201440020U98º71259998Tracking
DUCHIFAT-1201440021U98º47846594Tracking
NANOSATC-BR1201440024U98º51050195Tracking
QB50P1201440025U98º53952495Tracking
QB50P2201440032U98º54653195Tracking
PERSEUS-M2201440037U98º59457796Tracking
PERSEUS-M1201440039U98º59357896Tracking
POLYITAN-1201440042U98º51349695Tracking
TIGRISAT201440043U98º65458497Tracking
AEROCUBE 6A201440045U98º61756096Tracking
AEROCUBE 6B201440046U98º61255796Tracking
CANX-4201440055U98º63662097Tracking
CANX-5201440056U98º63662097Tracking
UKUBE-1201440074U98º54954496Tracking
BRITE-PL2 (HEWELIUSZ)201440119U98º59957996Tracking
AEROCUBE 5C201540965U65º70949497Tracking
AEROCUBE 7201540966U65º69248996Tracking
FOX-1A (AO-85)201540967U65º70849897Tracking
SINOD-D 1201540968U65º68849396Tracking
SNAP-3 ALICE201540970U65º54344694Tracking
LMRST-SAT201540971U65º71049797Tracking
SNAP-3 EDDIE201540972U65º54444194Tracking
PROPCUBE 3201540973U65º69749297Tracking
BISONSAT201540974U65º61947096Tracking
SNAP-3 JIMI201540975U65º66648396Tracking
PROPCUBE 1 (FLORA)201540976U65º71450197Tracking
SINOD-D 3201540977U65º69449797Tracking
HORYU-4201641340U31º45144194Tracking
RAVAN201641849U98º47446394Tracking
CELTEE 1201641850U98º52151995Tracking
OPTICUBE 04201641851U98º55553296Tracking
AEROCUBE 8D201641852U98º51450795Tracking
AEROCUBE 8C201641853U98º51450695Tracking
PROMETHEUS 2-1201641854U98º40339893Tracking
PROMETHEUS 2-3201641855U98º40339893Tracking
CORVUS BC2201742846U97º56754696Tracking
CORVUS BC1201742847U97º56554796Tracking
MIRATA201743015U98º42934392Tracking
MAKERSAT 0201743016U98º60941695Tracking
SIRION PATHFINDER-2201843759U97º54052995Tracking
CORVUS BC4201843767U97º54553495Tracking
SPACEBEE-7201843816U97º44844093Tracking
SHIELDS 1201843850U85º37436692Tracking
DUCHIFAT-3201944854U37º41240293Tracking
M2 PATHFINDER202045727U98º56855096Tracking
NETSAT-4202046504U98º47346694Tracking
NETSAT-3202046505U98º47747194Tracking
NETSAT-1202046506U98º49348694Tracking
NETSAT-2202046507U98º47346794Tracking
WILDTRACKCUBE-SIMBA202147941U97º42541093Tracking
LEDSAT202149069U97º35534592Tracking
GREENCUBE (IO-117)202253109U70º58545832224Tracking
SITRO-AIS 5 (KATYS)202357176U98º51349395Tracking
SITRO-AIS 6 (CHIRKIN)202357192U98º51349395Tracking
SITRO-AIS 8 (ANOKHIN)202357193U98º50848995Tracking
SITRO-AIS 7 (FARTUSHNIY)202357194U98º51449395Tracking
SITRO-AIS 10 (BURDAEV)202357199U98º49448194Tracking
SITRO-AIS 9 (SHCHUKIN)202357201U98º49548194Tracking
SITRO-AIS 12 (SMIRENNIY)202357204U98º49448194Tracking
SITRO-AIS 11 (SHEFFER)202357208U98º49348094Tracking
ROBUSTA-1E (ENSO)202358470U97º37836992Tracking
SITRO-AIS 25202459066U95º70549397Tracking
SITRO-AIS 26202459067U95º70649397Tracking
SITRO-AIS 27202459068U95º70449297Tracking
SITRO-AIS 28202459071U95º70449297Tracking
GRBBETA202460237U62º59651896Tracking
OOV-CUBE (TUBSAT-30)202460240U62º60552596Tracking
ROBUSTA-3A (MEDITERRAN*)202460243U62º58851196Tracking
LASARSAT202462391U45º48747794Tracking
CROCUBE202462394U45º48747594Tracking
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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