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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)199825544U5242141793Tracking
KESTREL EYE IIM (KE2M)199842982U5235935592Tracking
DELLINGR (RBLE)199843021U5235635492Tracking
UBAKUSAT199843467U5234233991Tracking
CUBERRT199843546U5234834591Tracking
TEMPEST-D199843547U5238337692Tracking
RAINCUBE199843548U5234534291Tracking
HALOSAT199843549U5234834591Tracking
ENDUROSAT ONE199843551U5232131991Tracking
EQUISAT199843552U5234534291Tracking
RADSAT-G199843553U5236135692Tracking
1998-067PC199843554U5231331091Tracking
AEROCUBE 12A201843556U5248247094Tracking
AEROCUBE 12B201843557U5248347194Tracking
LEMUR-2-VU201843558U5247746794Tracking
LEMUR-2-ALEXANDER201843559U5247746794Tracking
LEMUR-2-YUASA201843560U5247846794Tracking
LEMUR-2-TOMHENDERSON201843561U5247946894Tracking
SIRIUSSAT-1199843595U5234334191Tracking
SIRIUSSAT-2199843596U5234434191Tracking
TANUSHA-3199843597U5230530191Tracking
1998-067PK199843598U5229729390Tracking
1998-067PN199843638U5237637392Tracking
1998-067PP199843639U5236235892Tracking
STARS-ME199843640U5237236792Tracking
ISS DEB (SEDA-AP)199843870U5239639092Tracking
CATSAT-2199844029U5237336992Tracking
DELPHINI199844030U5236936692Tracking
UNITE199844031U5238538192Tracking
CATSAT-1199844033U5237336992Tracking
ISS DEB199844303U5240840093Tracking
ISS DEB199844304U5238537892Tracking
ISS DEB199844305U5237537192Tracking
ISS DEB199844306U5240839993Tracking
RAAVANA-1199844329U5239738892Tracking
UGUISU199844330U5239738992Tracking
NEPALISAT-1199844331U5239738892Tracking
SPOOQY-1199844332U5239638992Tracking
RED-EYE 1 (PINOT)199844364U5240939993Tracking
IOD-1 GEMS199844385U5238838392Tracking
SWIATOWID199844426U5238538092Tracking
KRAKSAT199844427U5240139693Tracking
VCC A199844428U5239739292Tracking
ENTRYSAT199844429U5239338992Tracking
VCC C199844430U5239038692Tracking
VCC B199844431U5239739292Tracking
ISS DEB199844788U5240239593Tracking
ISS DEB199844789U5240439593Tracking
RWASAT-1199844790U5241440293Tracking
AQT-D199844791U5241340393Tracking
NARSSCUBE-1199844792U5240940293Tracking
PROGRESS-MS 13201944833U5242141793Tracking
STPSAT-4199845043U5242141293Tracking
HARP199845256U5241840893Tracking
1998-067RA199845257U5241940793Tracking
PHOENIX199845258U5241840993Tracking
1998-067RC199845259U5241740793Tracking
CRYOCUBE199845260U5241740693Tracking
AZTECHSAT-1199845261U5241640593Tracking
RADSAT-U199845262U5241840893Tracking
QARMAN199845263U5241840793Tracking
SORTIE199845264U5242040993Tracking
ICS-EF (ISS DEB)199845265U5242141393Tracking
SOYUZ-MS 16202045476U5242141793Tracking
PROGRESS-MS 14202045595U5242141793Tracking
G-SAT199845597U5241841193Tracking
QUETZAL-1199845598U5241741393Tracking
HTV-9 (KOUNOTORI 9)202045607U5242141793Tracking
CREW DRAGON DEMO-2202045623U5242141793Tracking
RED-EYE 2 (MERLOT)199845800U5241941693Tracking
RED-EYE 3 (CABERNET)199845809U5241941693Tracking
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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