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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)199825544U5242041893Tracking
KESTREL EYE IIM (KE2M)199842982U5234133891Tracking
DELLINGR (RBLE)199843021U5233733591Tracking
UBAKUSAT199843467U5227927290Tracking
TEMPEST-D199843547U5236736292Tracking
RAINCUBE199843548U5227827190Tracking
HALOSAT199843549U5229528990Tracking
EQUISAT199843552U5228127490Tracking
RADSAT-G199843553U5233433091Tracking
AEROCUBE 12A201843556U5248046994Tracking
AEROCUBE 12B201843557U5248147094Tracking
LEMUR-2-VU201843558U5247446594Tracking
LEMUR-2-ALEXANDER201843559U5247446494Tracking
LEMUR-2-YUASA201843560U5247446594Tracking
LEMUR-2-TOMHENDERSON201843561U5247546594Tracking
SIRIUSSAT-1199843595U5225122689Tracking
SIRIUSSAT-2199843596U5223822889Tracking
1998-067PN199843638U5236136092Tracking
1998-067PP199843639U5233132791Tracking
STARS-ME199843640U5235335092Tracking
ISS DEB (SEDA-AP)199843870U5239138792Tracking
CATSAT-2199844029U5234534491Tracking
DELPHINI199844030U5233733691Tracking
UNITE199844031U5237136992Tracking
CATSAT-1199844033U5234534491Tracking
ISS DEB199844303U5240239593Tracking
ISS DEB199844304U5235434692Tracking
ISS DEB199844305U5232631991Tracking
ISS DEB199844306U5240239493Tracking
RAAVANA-1199844329U5238237692Tracking
UGUISU199844330U5238237692Tracking
NEPALISAT-1199844331U5238237692Tracking
SPOOQY-1199844332U5238237792Tracking
RED-EYE 1 (PINOT)199844364U5240339593Tracking
IOD-1 GEMS199844385U5236235692Tracking
SWIATOWID199844426U5235434792Tracking
KRAKSAT199844427U5239138792Tracking
VCC A199844428U5238338092Tracking
ENTRYSAT199844429U5237737392Tracking
VCC C199844430U5236836492Tracking
VCC B199844431U5238337992Tracking
ISS DEB199844788U5237937392Tracking
ISS DEB199844789U5238337692Tracking
RWASAT-1199844790U5240739693Tracking
AQT-D199844791U5240539793Tracking
NARSSCUBE-1199844792U5239739292Tracking
STPSAT-4199845043U5241540993Tracking
HARP199845256U5241040193Tracking
1998-067RA199845257U5241140293Tracking
PHOENIX199845258U5241240593Tracking
1998-067RC199845259U5240739993Tracking
CRYOCUBE199845260U5240739993Tracking
AZTECHSAT-1199845261U5240439593Tracking
RADSAT-U199845262U5241040393Tracking
QARMAN199845263U5240840093Tracking
SORTIE199845264U5241540693Tracking
ICS-EF (ISS DEB)199845265U5241841193Tracking
PROGRESS-MS 14202045595U5242041893Tracking
G-SAT199845597U5241040593Tracking
QUETZAL-1199845598U5240840693Tracking
RED-EYE 2 (MERLOT)199845800U5241441393Tracking
RED-EYE 3 (CABERNET)199845809U5241441393Tracking
DEMI199845916U5241040793Tracking
TECHEDSAT 10199845917U5238637992Tracking
PROGRESS-MS 15202045937U5242041893Tracking
CYGNUS NG-14202046530U5242041893Tracking
SOYUZ-MS 17202046613U5242041893Tracking
CREW DRAGON 1202046920U5242041893Tracking
SPOC199846921U5241641293Tracking
BOBCAT-1199846922U5241641293Tracking
NEUTRON-1199846923U5241741393Tracking
1998-067RU199846924U5241541193Tracking
LEMUR-2-BAXTER-OLIVER199846925U5241441093Tracking
LEMUR-2-DJARA199846926U5241541193Tracking
DESCENT199846927U5241741393Tracking
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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