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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)199825544U5242341893Tracking
AEROCUBE 12A201843556U5247146194Tracking
AEROCUBE 12B201843557U5247446394Tracking
LEMUR-2-VU201843558U5246145294Tracking
LEMUR-2-ALEXANDER201843559U5246145294Tracking
LEMUR-2-YUASA201843560U5246245294Tracking
LEMUR-2-TOMHENDERSON201843561U5246345494Tracking
ISS DEB (SEDA-AP)199843870U5237236792Tracking
ISS DEB199844303U5237937192Tracking
ISS DEB199844306U5237636792Tracking
RED-EYE 1 (PINOT)199844364U5238137192Tracking
KRAKSAT199844427U5231731091Tracking
RWASAT-1199844790U5237236292Tracking
AQT-D199844791U5237036092Tracking
NARSSCUBE-1199844792U5229128290Tracking
STPSAT-4199845043U5239739092Tracking
HARP199845256U5237036092Tracking
1998-067RA199845257U5237936992Tracking
PHOENIX199845258U5238637792Tracking
1998-067RC199845259U5234533591Tracking
AZTECHSAT-1199845261U5227326290Tracking
RADSAT-U199845262U5237636892Tracking
QARMAN199845263U5234533491Tracking
SORTIE199845264U5239638692Tracking
ICS-EF (ISS DEB)199845265U5240740093Tracking
G-SAT199845597U5237436892Tracking
QUETZAL-1199845598U5235635192Tracking
RED-EYE 2 (MERLOT)199845800U5239939693Tracking
RED-EYE 3 (CABERNET)199845809U5239939693Tracking
DEMI199845916U5236335792Tracking
SPOC199846921U5238938892Tracking
BOBCAT-1199846922U5237637392Tracking
NEUTRON-1199846923U5239038892Tracking
1998-067RU199846924U5232431591Tracking
LEMUR-2-BAXTER-OLIVER199846925U5229328490Tracking
LEMUR-2-DJARA199846926U5232532091Tracking
DESCENT199846927U5239038792Tracking
ISS DEB199847853U5241741493Tracking
RSP-01199847925U5239639592Tracking
TAUSAT-1199847926U5239038992Tracking
TSURU199847927U5239839893Tracking
STARS-EC199847928U5239238792Tracking
MMSATS-1199847976U5241341093Tracking
TIANHE202148274U4138538192Tracking
TIANZHOU-2202148803U4138538192Tracking
RAMSAT199848850U5241140493Tracking
SOAR199848851U5238537992Tracking
BD-28199848867U5240940393Tracking
MIR-SAT 1199848868U5239939392Tracking
ISS (NAUKA)202149044U5242341793Tracking
CYGNUS NG-16202149064U5246545694Tracking
SOYUZ-MS 19202149269U5242341793Tracking
FREGAT DEB201149271U5225071157123Tracking
BINAR-1199849272U5241441093Tracking
MAYA-3199849273U5241340993Tracking
MAYA-4199849274U5241340993Tracking
CUAVA-1199849275U5241340993Tracking
CAPSAT199849276U5241641193Tracking
1998-067SW199849277U5241641093Tracking
1998-067SX199849278U5240940693Tracking
SHENZHOU-13 (SZ-13)202149326U4138538192Tracking
PROGRESS-MS 18202149379U5242341793Tracking
CREW DRAGON 3202149407U5242341793Tracking
ISS (PRICHAL)202149499U5242341793Tracking
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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