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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)199842982U5229729590Tracking
DELLINGR (RBLE)199843021U5226125590Tracking
TEMPEST-D199843547U5229328890Tracking
AEROCUBE 12A201843556U5247646594Tracking
AEROCUBE 12B201843557U5247846794Tracking
LEMUR-2-VU201843558U5247046094Tracking
LEMUR-2-ALEXANDER201843559U5246945994Tracking
LEMUR-2-YUASA201843560U5247046094Tracking
LEMUR-2-TOMHENDERSON201843561U5247146194Tracking
1998-067PN199843638U5232932691Tracking
STARS-ME199843640U5229028490Tracking
ISS DEB (SEDA-AP)199843870U5238438092Tracking
UNITE199844031U5234234091Tracking
ISS DEB199844303U5239438792Tracking
ISS DEB199844306U5239338492Tracking
RAAVANA-1199844329U5234934391Tracking
UGUISU199844330U5235034491Tracking
NEPALISAT-1199844331U5234934391Tracking
SPOOQY-1199844332U5235134692Tracking
RED-EYE 1 (PINOT)199844364U5239538692Tracking
KRAKSAT199844427U5237336792Tracking
VCC A199844428U5235434992Tracking
ENTRYSAT199844429U5233132591Tracking
VCC C199844430U5215514788Tracking
VCC B199844431U5235334892Tracking
ISS DEB199844788U5222021089Tracking
ISS DEB199844789U5230029390Tracking
RWASAT-1199844790U5239438592Tracking
AQT-D199844791U5239438592Tracking
NARSSCUBE-1199844792U5237637192Tracking
STPSAT-4199845043U5240940293Tracking
HARP199845256U5239738992Tracking
1998-067RA199845257U5240039192Tracking
PHOENIX199845258U5240339593Tracking
1998-067RC199845259U5239038292Tracking
CRYOCUBE199845260U5238537792Tracking
AZTECHSAT-1199845261U5238137392Tracking
RADSAT-U199845262U5239839292Tracking
QARMAN199845263U5239038292Tracking
SORTIE199845264U5240839993Tracking
ICS-EF (ISS DEB)199845265U5241440793Tracking
G-SAT199845597U5239739492Tracking
QUETZAL-1199845598U5239239192Tracking
RED-EYE 2 (MERLOT)199845800U5240840793Tracking
RED-EYE 3 (CABERNET)199845809U5240940793Tracking
DEMI199845916U5239739292Tracking
SPOC199846921U5240740493Tracking
BOBCAT-1199846922U5240340093Tracking
NEUTRON-1199846923U5240840493Tracking
1998-067RU199846924U5239539092Tracking
LEMUR-2-BAXTER-OLIVER199846925U5239338992Tracking
LEMUR-2-DJARA199846926U5239539192Tracking
DESCENT199846927U5240840493Tracking
PROGRESS-MS 16202147618U5242241793Tracking
CYGNUS NG-15202147689U5242241793Tracking
ISS DEB199847853U5242041793Tracking
RSP-01199847925U5241541393Tracking
TAUSAT-1199847926U5241441093Tracking
TSURU199847927U5241541393Tracking
STARS-EC199847928U5241841093Tracking
MMSATS-1199847976U5241941693Tracking
SOYUZ-MS 18202148159U5242241793Tracking
CREW DRAGON 2202148209U5242241793Tracking
TIANHE202148274U4138536092Tracking
CZ-5B R/B202148275U4117313588Tracking
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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