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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)199825544U5242241393Tracking
AEROCUBE 12A201843556U5246845994Tracking
AEROCUBE 12B201843557U5247146194Tracking
LEMUR-2-VU201843558U5245744894Tracking
LEMUR-2-ALEXANDER201843559U5245644794Tracking
LEMUR-2-YUASA201843560U5245744894Tracking
LEMUR-2-TOMHENDERSON201843561U5245945094Tracking
ISS DEB (SEDA-AP)199843870U5236536192Tracking
ISS DEB199844303U5236936592Tracking
ISS DEB199844306U5236435992Tracking
RED-EYE 1 (PINOT)199844364U5237036592Tracking
RWASAT-1199844790U5235634992Tracking
AQT-D199844791U5235234892Tracking
STPSAT-4199845043U5239038492Tracking
HARP199845256U5234734491Tracking
1998-067RA199845257U5236335792Tracking
PHOENIX199845258U5237436992Tracking
1998-067RC199845259U5228728090Tracking
RADSAT-U199845262U5236035492Tracking
QARMAN199845263U5228227690Tracking
SORTIE199845264U5238838092Tracking
ICS-EF (ISS DEB)199845265U5240339793Tracking
G-SAT199845597U5235835292Tracking
QUETZAL-1199845598U5232331791Tracking
RED-EYE 2 (MERLOT)199845800U5239339192Tracking
RED-EYE 3 (CABERNET)199845809U5239339192Tracking
DEMI199845916U5233533291Tracking
SPOC199846921U5238137892Tracking
BOBCAT-1199846922U5235835492Tracking
NEUTRON-1199846923U5238137892Tracking
DESCENT199846927U5238137892Tracking
ISS DEB199847853U5241641293Tracking
RSP-01199847925U5238838392Tracking
TAUSAT-1199847926U5237937392Tracking
TSURU199847927U5239138792Tracking
STARS-EC199847928U5237637092Tracking
MMSATS-1199847976U5241040693Tracking
TIANHE202148274U4138638392Tracking
TIANZHOU-2202148803U4138638392Tracking
RAMSAT199848850U5240339993Tracking
SOAR199848851U5235735192Tracking
BD-28199848867U5240039893Tracking
MIR-SAT 1199848868U5238237892Tracking
ISS (NAUKA)202149044U5242241393Tracking
TIANZHOU-3202149222U4138638392Tracking
SOYUZ-MS 19202149269U5242241393Tracking
FREGAT DEB201149271U522690872122Tracking
BINAR-1199849272U5241040293Tracking
MAYA-3199849273U5240739993Tracking
MAYA-4199849274U5240840093Tracking
CUAVA-1199849275U5240840093Tracking
CAPSAT199849276U5241140393Tracking
1998-067SW199849277U5241140193Tracking
1998-067SX199849278U5239638592Tracking
SHENZHOU-13 (SZ-13)202149326U4138638392Tracking
PROGRESS-MS 18202149379U5242241393Tracking
CREW DRAGON 3202149407U5242241393Tracking
DRAGON CRS-24202150318U5237218590Tracking
OBJECT SY199851277U5241941293Tracking
OBJECT SZ199851278U5241940893Tracking
OBJECT TA199851279U5242041293Tracking
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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