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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)199842982U52º28728290Tracking
DELLINGR (RBLE)199843021U52º13712987Tracking
TEMPEST-D199843547U52º25524289Tracking
AEROCUBE 12A201843556U52º47646594Tracking
AEROCUBE 12B201843557U52º47846794Tracking
LEMUR-2-VU201843558U52º46946094Tracking
LEMUR-2-ALEXANDER201843559U52º46845994Tracking
LEMUR-2-YUASA201843560U52º46946094Tracking
LEMUR-2-TOMHENDERSON201843561U52º47046094Tracking
1998-067PN199843638U52º32231691Tracking
STARS-ME199843640U52º25423989Tracking
ISS DEB (SEDA-AP)199843870U52º38337892Tracking
UNITE199844031U52º33633291Tracking
ISS DEB199844303U52º39238692Tracking
ISS DEB199844306U52º39138392Tracking
RAAVANA-1199844329U52º34133491Tracking
UGUISU199844330U52º34333691Tracking
NEPALISAT-1199844331U52º34133491Tracking
SPOOQY-1199844332U52º34433891Tracking
RED-EYE 1 (PINOT)199844364U52º39338592Tracking
KRAKSAT199844427U52º36936492Tracking
VCC A199844428U52º34734291Tracking
ENTRYSAT199844429U52º31730991Tracking
VCC B199844431U52º34534191Tracking
ISS DEB199844789U52º18216588Tracking
RWASAT-1199844790U52º39238492Tracking
AQT-D199844791U52º39138492Tracking
NARSSCUBE-1199844792U52º37136692Tracking
STPSAT-4199845043U52º40740193Tracking
HARP199845256U52º39538792Tracking
1998-067RA199845257U52º39839092Tracking
PHOENIX199845258U52º40139493Tracking
1998-067RC199845259U52º38637992Tracking
CRYOCUBE199845260U52º38037292Tracking
AZTECHSAT-1199845261U52º37636892Tracking
RADSAT-U199845262U52º39639092Tracking
QARMAN199845263U52º38737992Tracking
SORTIE199845264U52º40739893Tracking
ICS-EF (ISS DEB)199845265U52º41340693Tracking
G-SAT199845597U52º39639192Tracking
QUETZAL-1199845598U52º38938892Tracking
RED-EYE 2 (MERLOT)199845800U52º40740693Tracking
RED-EYE 3 (CABERNET)199845809U52º40740693Tracking
DEMI199845916U52º39339092Tracking
SPOC199846921U52º40540293Tracking
BOBCAT-1199846922U52º40039893Tracking
NEUTRON-1199846923U52º40640393Tracking
1998-067RU199846924U52º39038792Tracking
LEMUR-2-BAXTER-OLIVER199846925U52º38738592Tracking
LEMUR-2-DJARA199846926U52º39038892Tracking
DESCENT199846927U52º40640393Tracking
PROGRESS-MS 16202147618U52º42241793Tracking
CYGNUS NG-15202147689U52º42241793Tracking
ISS DEB199847853U52º42041693Tracking
RSP-01199847925U52º41341193Tracking
TAUSAT-1199847926U52º41240893Tracking
TSURU199847927U52º41441193Tracking
STARS-EC199847928U52º41640893Tracking
MMSATS-1199847976U52º41941593Tracking
SOYUZ-MS 18202148159U52º42241793Tracking
CREW DRAGON 2202148209U52º42241793Tracking
TIANHE202148274U41º38737592Tracking
TIANZHOU-2202148803U41º38737592Tracking
DRAGON CRS-22202148831U52º42241793Tracking
2021-048B202148832U52º27917689Tracking
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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