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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)200327844U99º819805101Tracking
CUBESAT XI-IV (CO-57)200327848U99º821807101Tracking
CUBESAT XI-V200528895U98º66764898Tracking
CUTE-1.7+APD II (CO-65)200832785U98º56054696Tracking
CANX-2200832790U98º57055396Tracking
SEEDS II (CO-66)200832791U98º51350695Tracking
SWISSCUBE200935932U98º69368599Tracking
BEESAT-1200935933U98º69468899Tracking
ITUPSAT1200935935U98º69969099Tracking
TISAT 1201036799U98º51951295Tracking
AEROCUBE 4.5A201238767U65º53339794Tracking
STRAND-1201339090U98º774764100Tracking
BRITE-AUSTRIA201339091U98º777764100Tracking
NEE-01 PEGASO201339151U98º60458797Tracking
POPACS 1201339268U81º60328393Tracking
POPACS 2201339269U81º97530998Tracking
POPACS 3201339270U81º114731699Tracking
ZACUBE-1 (TSHEPISOSAT)201339417U98º60854696Tracking
WNISAT-1201339423U98º81958699Tracking
TRITON-1201339427U98º69856697Tracking
GOMX-1201339430U98º76257598Tracking
CUBEBUG-2 (LO-74)201339440U98º64255497Tracking
NEE-02 KRYSAOR201339441U98º66356897Tracking
FUNCUBE-1 (AO-73)201339444U98º58953096Tracking
UWE-3201339446U98º62755096Tracking
BRITE-CA1 (TORONTO)201440020U98º71259998Tracking
DUCHIFAT-1201440021U98º48447594Tracking
NANOSATC-BR1201440024U98º51450795Tracking
QB50P1201440025U98º54252695Tracking
QB50P2201440032U98º54753595Tracking
PERSEUS-M2201440037U98º59657696Tracking
PERSEUS-M1201440039U98º59657796Tracking
POLYITAN-1201440042U98º51650395Tracking
TIGRISAT201440043U98º65658497Tracking
AEROCUBE 6A201440045U98º62156096Tracking
AEROCUBE 6B201440046U98º61655796Tracking
CANX-4201440055U98º63961997Tracking
CANX-5201440056U98º63861897Tracking
UKUBE-1201440074U98º55154996Tracking
BRITE-PL2 (HEWELIUSZ)201440119U98º59958196Tracking
AEROCUBE 5C201540965U65º71748897Tracking
AEROCUBE 7201540966U65º70148497Tracking
FOX-1A (AO-85)201540967U65º71649297Tracking
SINOD-D 1201540968U65º69748797Tracking
SNAP-3 ALICE201540970U65º56144495Tracking
LMRST-SAT201540971U65º71849197Tracking
SNAP-3 EDDIE201540972U65º56343995Tracking
PROPCUBE 3201540973U65º70548697Tracking
BISONSAT201540974U65º63146596Tracking
SNAP-3 JIMI201540975U65º67547896Tracking
PROPCUBE 1 (FLORA)201540976U65º72249597Tracking
SINOD-D 3201540977U65º70349197Tracking
HORYU-4201641340U31º45845194Tracking
RAVAN201641849U98º48046994Tracking
CELTEE 1201641850U98º52452095Tracking
OPTICUBE 04201641851U98º55553496Tracking
AEROCUBE 8D201641852U98º51551195Tracking
AEROCUBE 8C201641853U98º51650995Tracking
PROMETHEUS 2-1201641854U98º42441693Tracking
PROMETHEUS 2-3201641855U98º42341793Tracking
CORVUS BC2201742846U97º56754896Tracking
CORVUS BC1201742847U97º56554996Tracking
MIRATA201743015U98º47336293Tracking
MAKERSAT 0201743016U98º62141795Tracking
SIRION PATHFINDER-2201843759U97º54452995Tracking
CORVUS BC4201843767U97º54753595Tracking
MOVE-II201843780U97º33532891Tracking
SPACEBEE-7201843816U97º46145194Tracking
SHIELDS 1201843850U85º38937892Tracking
SONATE201944400U98º28427390Tracking
DUCHIFAT-3201944854U37º42842293Tracking
M2 PATHFINDER202045727U98º56955196Tracking
NETSAT-4202046504U98º47946994Tracking
NETSAT-3202046505U98º48347494Tracking
NETSAT-1202046506U98º49748994Tracking
NETSAT-2202046507U98º47947294Tracking
WILDTRACKCUBE-SIMBA202147941U97º43442493Tracking
LEDSAT202149069U97º38937792Tracking
GREENCUBE (IO-117)202253109U70º58545832224Tracking
SITRO-AIS 5 (KATYS)202357176U98º51549895Tracking
SITRO-AIS 6 (CHIRKIN)202357192U98º51549895Tracking
SITRO-AIS 8 (ANOKHIN)202357193U98º51049495Tracking
SITRO-AIS 7 (FARTUSHNIY)202357194U98º51549895Tracking
SITRO-AIS 10 (BURDAEV)202357199U98º49748794Tracking
SITRO-AIS 9 (SHCHUKIN)202357201U98º49848794Tracking
SITRO-AIS 12 (SMIRENNIY)202357204U98º49748794Tracking
SITRO-AIS 11 (SHEFFER)202357208U98º49648694Tracking
VERONIKA202358261U97º35335392Tracking
ROBUSTA-1E (ENSO)202358470U97º40339393Tracking
SITRO-AIS 25202459066U95º70949197Tracking
SITRO-AIS 26202459067U95º71049297Tracking
SITRO-AIS 27202459068U95º70849197Tracking
SITRO-AIS 28202459071U95º70849197Tracking
GRBBETA202460237U62º59552296Tracking
OOV-CUBE (TUBSAT-30)202460240U62º60253096Tracking
ROBUSTA-3A (MEDITERRAN*)202460243U62º58851796Tracking
LASARSAT202462391U45º49248394Tracking
CROCUBE202462394U45º49248294Tracking
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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