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International Space Station Stuff
In this category are all related satellite for International Space Station, including the Soyuz spacecraft, Progress spacecraft, Dragon module, Tiangong or ATV modules.
Satellite Launch Norad Incl.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
ISS (ZARYA)199825544U5242241793Tracking
KESTREL EYE IIM (KE2M)199842982U5232531991Tracking
DELLINGR (RBLE)199843021U5231431291Tracking
TEMPEST-D199843547U5234133691Tracking
RADSAT-G199843553U5229428890Tracking
AEROCUBE 12A201843556U5247846794Tracking
AEROCUBE 12B201843557U5248046894Tracking
LEMUR-2-VU201843558U5247246294Tracking
LEMUR-2-ALEXANDER201843559U5247246194Tracking
LEMUR-2-YUASA201843560U5247346294Tracking
LEMUR-2-TOMHENDERSON201843561U5247446394Tracking
1998-067PN199843638U5234834691Tracking
1998-067PP199843639U5226826290Tracking
STARS-ME199843640U5233333091Tracking
ISS DEB (SEDA-AP)199843870U5238838392Tracking
CATSAT-2199844029U5231030491Tracking
DELPHINI199844030U5227526790Tracking
UNITE199844031U5236035692Tracking
CATSAT-1199844033U5231130591Tracking
ISS DEB199844303U5239839292Tracking
ISS DEB199844304U5229328690Tracking
ISS DEB199844306U5239839092Tracking
RAAVANA-1199844329U5236836392Tracking
UGUISU199844330U5236936492Tracking
NEPALISAT-1199844331U5236836392Tracking
SPOOQY-1199844332U5236936592Tracking
RED-EYE 1 (PINOT)199844364U5239939192Tracking
IOD-1 GEMS199844385U5231831391Tracking
SWIATOWID199844426U5228727990Tracking
KRAKSAT199844427U5238237992Tracking
VCC A199844428U5237036892Tracking
ENTRYSAT199844429U5235835792Tracking
VCC C199844430U5234033791Tracking
VCC B199844431U5236936792Tracking
ISS DEB199844788U5235034691Tracking
ISS DEB199844789U5235835492Tracking
RWASAT-1199844790U5240039292Tracking
AQT-D199844791U5240039292Tracking
NARSSCUBE-1199844792U5238838392Tracking
STPSAT-4199845043U5241240693Tracking
HARP199845256U5240439693Tracking
1998-067RA199845257U5240639793Tracking
PHOENIX199845258U5240740093Tracking
1998-067RC199845259U5239939192Tracking
CRYOCUBE199845260U5239839092Tracking
AZTECHSAT-1199845261U5239438692Tracking
RADSAT-U199845262U5240539793Tracking
QARMAN199845263U5240039292Tracking
SORTIE199845264U5241240393Tracking
ICS-EF (ISS DEB)199845265U5241640993Tracking
PROGRESS-MS 14202045595U5242241793Tracking
G-SAT199845597U5240539993Tracking
QUETZAL-1199845598U5240139893Tracking
RED-EYE 2 (MERLOT)199845800U5241141093Tracking
RED-EYE 3 (CABERNET)199845809U5241241093Tracking
DEMI199845916U5240340193Tracking
TECHEDSAT 10199845917U5231630691Tracking
SOYUZ-MS 17202046613U5242241793Tracking
CREW DRAGON 1202046920U5242241793Tracking
SPOC199846921U5241240993Tracking
BOBCAT-1199846922U5240940793Tracking
NEUTRON-1199846923U5241240993Tracking
1998-067RU199846924U5240540393Tracking
LEMUR-2-BAXTER-OLIVER199846925U5240440293Tracking
LEMUR-2-DJARA199846926U5240540293Tracking
DESCENT199846927U5241240993Tracking
PROGRESS-MS 16202147618U5242241793Tracking
CYGNUS NG-15202147689U5242241793Tracking
ANTARES R/B202147690U5221816288Tracking
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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