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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)200327844U99º822809101Tracking
CUBESAT XI-IV (CO-57)200327848U99º824811101Tracking
CUBESAT XI-V200528895U98º68666198Tracking
CUTE-1.7+APD II (CO-65)200832785U98º59757996Tracking
AAUSAT-II200832788U98º55454296Tracking
DELFI-C3 (DO-64)200832789U97º40939793Tracking
SEEDS II (CO-66)200832791U98º58256496Tracking
SWISSCUBE200935932U99º70669399Tracking
BEESAT-1200935933U98º70569599Tracking
ITUPSAT1200935935U99º71069799Tracking
TISAT 1201036799U98º58356796Tracking
M-CUBED & EXP-1 PRIME201137855U102º54239694Tracking
AEROCUBE 4.5A201238767U65º63548296Tracking
AEROCUBE 4.5B201238768U65º59347195Tracking
STRAND-1201339090U98º779767100Tracking
BRITE-AUSTRIA201339091U98º780766100Tracking
BEESAT-3201339135U65º41339293Tracking
BEESAT-2201339136U65º43740093Tracking
NEE-01 PEGASO201339151U98º63060897Tracking
ESTCUBE 1201339161U98º65363998Tracking
POPACS 1201339268U81º99431398Tracking
POPACS 2201339269U81º1164315100Tracking
POPACS 3201339270U81º1261321101Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U98º64857497Tracking
WNISAT-1201339423U98º83458899Tracking
TRITON-1201339427U98º73058198Tracking
DELFI-N3XT201339428U98º72457498Tracking
GOMX-1201339430U98º78858398Tracking
CUBEBUG-2 (LO-74)201339440U98º68257697Tracking
NEE-02 KRYSAOR201339441U98º69158097Tracking
FUNCUBE-1 (AO-73)201339444U98º64057097Tracking
UWE-3201339446U98º66657597Tracking
BRITE-CA1 (TORONTO)201440020U98º72660798Tracking
DUCHIFAT-1201440021U98º57556196Tracking
NANOSATC-BR1201440024U98º58256996Tracking
QB50P1201440025U98º59057596Tracking
QB50P2201440032U98º59257896Tracking
PERSEUS-M2201440037U98º61159297Tracking
PERSEUS-M1201440039U98º61259397Tracking
POLYITAN-1201440042U98º58757196Tracking
TIGRISAT201440043U98º68059897Tracking
AEROCUBE 6A201440045U98º66959297Tracking
AEROCUBE 6B201440046U98º66559097Tracking
UKUBE-1201440074U98º60259897Tracking
BRITE-PL2 (HEWELIUSZ)201440119U98º61959597Tracking
GRIFEX201540379U99º45737293Tracking
CP10 (EXOCUBE)201540380U99º50839394Tracking
EXACTVIEW 9201540936U64062597Tracking
AEROCUBE 5C201540965U65º74651297Tracking
AEROCUBE 7201540966U65º74151097Tracking
GALASSIA201541170U15º41240793Tracking
VELOX-II201541171U15º47446594Tracking
HORYU-4201641340U31º54653095Tracking
E-ST@R-II201641459U98º52039194Tracking
RAVAN201641849U98º55553496Tracking
CELTEE 1201641850U98º56055896Tracking
OPTICUBE 04201641851U98º57755496Tracking
AEROCUBE 8D201641852U98º56055496Tracking
AEROCUBE 8C201641853U98º56355296Tracking
PROMETHEUS 2-1201641854U98º55453396Tracking
PROMETHEUS 2-3201641855U98º55353496Tracking
INS-1B201741954U97º31030591Tracking
DIDO-2201742000U97º43742993Tracking
PEASSS201742015U97º36936892Tracking
UCLSAT201742765U97º36936292Tracking
AALTO-1201742775U97º45543994Tracking
URSA MAIOR201742776U97º44643293Tracking
DIAMOND RED201742783U97º43242093Tracking
PEGASUS201742784U97º39738892Tracking
DIAMOND GREEN201742785U97º42741593Tracking
DIAMOND BLUE201742786U97º42941893Tracking
SUCHAI201742788U97º29529290Tracking
SKCUBE201742789U97º36435792Tracking
ROBUSTA 1B201742792U97º32732391Tracking
CICERO 6201742793U97º44042893Tracking
CORVUS BC2201742846U97º58757696Tracking
CORVUS BC1201742847U97º58657696Tracking
MIRATA201743015U98º72343996Tracking
MAKERSAT 0201743016U98º75244297Tracking
CORVUS BC3201843118U97º44143193Tracking
CICERO 7201843143U97º35535292Tracking
GOMX-4B201843196U98º45543794Tracking
GOMX-4A201843197U98º44242693Tracking
CUBEBEL-1 (BSUSAT-1)201843666U97º43542293Tracking
CICERO 10201843690U85º45043793Tracking
PROXIMA I201843694U85º43942393Tracking
PROXIMA II201843696U85º44042493Tracking
SIRION PATHFINDER-2201843759U98º57955896Tracking
CORVUS BC4201843767U98º57956196Tracking
MOVE-II201843780U98º55554296Tracking
SPACEBEE-7201843816U98º56354596Tracking
SPACEBEE-5201843817U98º49148694Tracking
SPACEBEE-6201843818U98º54953195Tracking
SHIELDS 1201843850U85º48446794Tracking
STF-1201843852U85º41940893Tracking
ZACUBE-2201843907U97º43441893Tracking
LUME 1201843908U97º40939593Tracking
MOVE-IIB201944398U98º40339893Tracking
SONATE201944400U98º50848295Tracking
LUCKY-7201944406U98º49547394Tracking
BEESAT 9201944412U98º46645194Tracking
JAISAT-1201944419U98º46545194Tracking
DUCHIFAT-3201944854U37º54653895Tracking
EYESAT-NANO201944877U97º39739292Tracking
M2 PATHFINDER202045727U98º59157696Tracking
NETSAT-4202046504U98º54653295Tracking
NETSAT-3202046505U98º54653395Tracking
NETSAT-1202046506U98º54753695Tracking
NETSAT-2202046507U98º54453595Tracking
SAI-1 NANOCONNECT-2202147701U97º38037192Tracking
WILDTRACKCUBE-SIMBA202147941U97º53751295Tracking
BEESAT-6202147957U97º50548595Tracking
SMOG-1202147964U97º49748194Tracking
BCCSAT-1202148041U97º50549195Tracking
BEESAT-5202148083U97º49848094Tracking
BEESAT-7202148084U97º50248394Tracking
BEESAT-8202148085U97º52249995Tracking
LEDSAT202149069U97º53450195Tracking
SPORT199855129U52º28227390Tracking
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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