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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)199825544U52º42241793Tracking
KESTREL EYE IIM (KE2M)199842982U52º29729690Tracking
DELLINGR (RBLE)199843021U52º26225790Tracking
TEMPEST-D199843547U52º29328890Tracking
AEROCUBE 12A201843556U52º47646594Tracking
AEROCUBE 12B201843557U52º47846794Tracking
LEMUR-2-VU201843558U52º47046094Tracking
LEMUR-2-ALEXANDER201843559U52º46945994Tracking
LEMUR-2-YUASA201843560U52º47046094Tracking
LEMUR-2-TOMHENDERSON201843561U52º47146194Tracking
1998-067PN199843638U52º32932691Tracking
STARS-ME199843640U52º29128690Tracking
ISS DEB (SEDA-AP)199843870U52º38438092Tracking
UNITE199844031U52º34234091Tracking
ISS DEB199844303U52º39438792Tracking
ISS DEB199844306U52º39338492Tracking
RAAVANA-1199844329U52º34934391Tracking
UGUISU199844330U52º35034491Tracking
NEPALISAT-1199844331U52º35034491Tracking
SPOOQY-1199844332U52º35134692Tracking
RED-EYE 1 (PINOT)199844364U52º39538692Tracking
KRAKSAT199844427U52º37336792Tracking
VCC A199844428U52º35534992Tracking
ENTRYSAT199844429U52º33232691Tracking
VCC C199844430U52º15514788Tracking
VCC B199844431U52º35334892Tracking
ISS DEB199844788U52º23923389Tracking
ISS DEB199844789U52º30229490Tracking
RWASAT-1199844790U52º39538592Tracking
AQT-D199844791U52º39438692Tracking
NARSSCUBE-1199844792U52º37637192Tracking
STPSAT-4199845043U52º40940293Tracking
HARP199845256U52º39738992Tracking
1998-067RA199845257U52º40039192Tracking
PHOENIX199845258U52º40339593Tracking
1998-067RC199845259U52º39038292Tracking
CRYOCUBE199845260U52º38537792Tracking
AZTECHSAT-1199845261U52º38137392Tracking
RADSAT-U199845262U52º39839292Tracking
QARMAN199845263U52º39038292Tracking
SORTIE199845264U52º40839993Tracking
ICS-EF (ISS DEB)199845265U52º41440793Tracking
G-SAT199845597U52º39839492Tracking
QUETZAL-1199845598U52º39239192Tracking
RED-EYE 2 (MERLOT)199845800U52º40840793Tracking
RED-EYE 3 (CABERNET)199845809U52º40940793Tracking
DEMI199845916U52º39739292Tracking
SPOC199846921U52º40740493Tracking
BOBCAT-1199846922U52º40340093Tracking
NEUTRON-1199846923U52º40840493Tracking
1998-067RU199846924U52º39539092Tracking
LEMUR-2-BAXTER-OLIVER199846925U52º39338992Tracking
LEMUR-2-DJARA199846926U52º39539192Tracking
DESCENT199846927U52º40840493Tracking
PROGRESS-MS 16202147618U52º42241793Tracking
CYGNUS NG-15202147689U52º42241793Tracking
ISS DEB199847853U52º42041793Tracking
RSP-01199847925U52º41541393Tracking
TAUSAT-1199847926U52º41441193Tracking
TSURU199847927U52º41541393Tracking
STARS-EC199847928U52º41841093Tracking
MMSATS-1199847976U52º41941693Tracking
SOYUZ-MS 18202148159U52º42241793Tracking
CREW DRAGON 2202148209U52º42241793Tracking
TIANHE202148274U41º38535992Tracking
CZ-5B R/B202148275U41º17313588Tracking
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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