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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)200327844U99º822808101Tracking
CUBESAT XI-IV (CO-57)200327848U99º824810101Tracking
CUBESAT XI-V200528895U98º68366298Tracking
CUTE-1.7+APD II (CO-65)200832785U98º59257996Tracking
AAUSAT-II200832788U98º54653495Tracking
SEEDS II (CO-66)200832791U98º57556296Tracking
SWISSCUBE200935932U98º70369499Tracking
BEESAT-1200935933U98º70269699Tracking
ITUPSAT1200935935U98º70769899Tracking
TISAT 1201036799U98º57956396Tracking
M-CUBED & EXP-1 PRIME201137855U102º51638694Tracking
AEROCUBE 4.5A201238767U65º62648196Tracking
AEROCUBE 4.5B201238768U65º58146695Tracking
STRAND-1201339090U98º779765100Tracking
BRITE-AUSTRIA201339091U98º781765100Tracking
BEESAT-3201339135U65º34333091Tracking
BEESAT-2201339136U65º38736292Tracking
NEE-01 PEGASO201339151U98º62760697Tracking
ESTCUBE 1201339161U98º65163898Tracking
POPACS 1201339268U81º96031197Tracking
POPACS 2201339269U81º114631599Tracking
POPACS 3201339270U81º1250321101Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U98º64757097Tracking
WNISAT-1201339423U98º83159099Tracking
TRITON-1201339427U98º72957998Tracking
DELFI-N3XT201339428U98º72257098Tracking
GOMX-1201339430U98º78558398Tracking
CUBEBUG-2 (LO-74)201339440U98º67757697Tracking
NEE-02 KRYSAOR201339441U98º68758197Tracking
FUNCUBE-1 (AO-73)201339444U98º63956597Tracking
UWE-3201339446U98º66357397Tracking
BRITE-CA1 (TORONTO)201440020U98º72560698Tracking
DUCHIFAT-1201440021U98º57355296Tracking
NANOSATC-BR1201440024U98º57956296Tracking
QB50P1201440025U98º58857096Tracking
QB50P2201440032U98º59057396Tracking
PERSEUS-M2201440037U98º61159097Tracking
PERSEUS-M1201440039U98º61159197Tracking
POLYITAN-1201440042U98º58456496Tracking
TIGRISAT201440043U98º67659897Tracking
AEROCUBE 6A201440045U98º66459197Tracking
AEROCUBE 6B201440046U98º66158997Tracking
UKUBE-1201440074U98º60059397Tracking
BRITE-PL2 (HEWELIUSZ)201440119U98º61659597Tracking
GRIFEX201540379U99º41434292Tracking
CP10 (EXOCUBE)201540380U99º48537893Tracking
EXACTVIEW 9201540936U63862597Tracking
AEROCUBE 5C201540965U65º74950697Tracking
AEROCUBE 7201540966U65º74250497Tracking
GALASSIA201541170U15º33132991Tracking
VELOX-II201541171U15º45745094Tracking
HORYU-4201641340U31º54052695Tracking
E-ST@R-II201641459U98º48337993Tracking
RAVAN201641849U98º55052995Tracking
CELTEE 1201641850U98º55755596Tracking
OPTICUBE 04201641851U98º57455496Tracking
AEROCUBE 8D201641852U98º55854996Tracking
AEROCUBE 8C201641853U98º56054896Tracking
PROMETHEUS 2-1201641854U98º54852695Tracking
PROMETHEUS 2-3201641855U98º54652895Tracking
DIDO-2201742000U97º42241593Tracking
AALTO-1201742775U97º43842993Tracking
URSA MAIOR201742776U97º42641993Tracking
DIAMOND RED201742783U97º40640193Tracking
PEGASUS201742784U97º34133691Tracking
DIAMOND GREEN201742785U97º39739292Tracking
DIAMOND BLUE201742786U97º40339793Tracking
CICERO 6201742793U97º41941393Tracking
CORVUS BC2201742846U97º58657396Tracking
CORVUS BC1201742847U97º58657396Tracking
MIRATA201743015U98º70543896Tracking
MAKERSAT 0201743016U98º73844396Tracking
CORVUS BC3201843118U97º42141493Tracking
GOMX-4B201843196U98º44142593Tracking
GOMX-4A201843197U98º42741393Tracking
CUBEBEL-1 (BSUSAT-1)201843666U97º39939392Tracking
CICERO 10201843690U85º43442493Tracking
PROXIMA I201843694U85º41540893Tracking
PROXIMA II201843696U85º41640993Tracking
SIRION PATHFINDER-2201843759U98º57555896Tracking
CORVUS BC4201843767U98º57356296Tracking
MOVE-II201843780U98º54753795Tracking
SPACEBEE-7201843816U98º55654296Tracking
SPACEBEE-5201843817U98º45144694Tracking
SPACEBEE-6201843818U98º53752495Tracking
SHIELDS 1201843850U85º47946094Tracking
STF-1201843852U85º38037392Tracking
ZACUBE-2201843907U97º41039593Tracking
LUME 1201843908U97º36836092Tracking
MOVE-IIB201944398U98º27726690Tracking
SONATE201944400U98º50347494Tracking
LUCKY-7201944406U98º48746194Tracking
BEESAT 9201944412U98º45042893Tracking
JAISAT-1201944419U98º44942993Tracking
DUCHIFAT-3201944854U37º54253095Tracking
M2 PATHFINDER202045727U98º59057296Tracking
NETSAT-4202046504U98º54252895Tracking
NETSAT-3202046505U98º54252995Tracking
NETSAT-1202046506U98º54453295Tracking
NETSAT-2202046507U98º54152995Tracking
WILDTRACKCUBE-SIMBA202147941U97º53250695Tracking
BEESAT-6202147957U97º48846694Tracking
SMOG-1202147964U97º48346294Tracking
BCCSAT-1202148041U97º49447694Tracking
BEESAT-5202148083U97º48145994Tracking
BEESAT-7202148084U97º48646594Tracking
BEESAT-8202148085U97º51549195Tracking
LEDSAT202149069U97º52649795Tracking
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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