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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)199825544U5242141993Tracking
KESTREL EYE IIM (KE2M)199842982U5224723589Tracking
AEROCUBE 12A201843556U5247546494Tracking
AEROCUBE 12B201843557U5247746694Tracking
LEMUR-2-VU201843558U5246745894Tracking
LEMUR-2-ALEXANDER201843559U5246745794Tracking
LEMUR-2-YUASA201843560U5246845894Tracking
LEMUR-2-TOMHENDERSON201843561U5246945994Tracking
1998-067PN199843638U5229929590Tracking
ISS DEB (SEDA-AP)199843870U5238137692Tracking
UNITE199844031U5232131991Tracking
ISS DEB199844303U5239038392Tracking
ISS DEB199844306U5238938092Tracking
RAAVANA-1199844329U5232031891Tracking
UGUISU199844330U5232332191Tracking
NEPALISAT-1199844331U5232131991Tracking
SPOOQY-1199844332U5232532391Tracking
RED-EYE 1 (PINOT)199844364U5239138392Tracking
KRAKSAT199844427U5236235792Tracking
VCC A199844428U5233032991Tracking
ENTRYSAT199844429U5225624389Tracking
VCC B199844431U5232732691Tracking
RWASAT-1199844790U5239037992Tracking
AQT-D199844791U5238838092Tracking
NARSSCUBE-1199844792U5236335892Tracking
STPSAT-4199845043U5240639993Tracking
HARP199845256U5239138292Tracking
1998-067RA199845257U5239538692Tracking
PHOENIX199845258U5239939192Tracking
1998-067RC199845259U5238037392Tracking
CRYOCUBE199845260U5236936292Tracking
AZTECHSAT-1199845261U5236735992Tracking
RADSAT-U199845262U5239338592Tracking
QARMAN199845263U5238137392Tracking
SORTIE199845264U5240539593Tracking
ICS-EF (ISS DEB)199845265U5241240493Tracking
G-SAT199845597U5239338792Tracking
QUETZAL-1199845598U5238538292Tracking
RED-EYE 2 (MERLOT)199845800U5240640493Tracking
RED-EYE 3 (CABERNET)199845809U5240640493Tracking
DEMI199845916U5238938592Tracking
SPOC199846921U5240240093Tracking
BOBCAT-1199846922U5239639492Tracking
NEUTRON-1199846923U5240240193Tracking
1998-067RU199846924U5238138092Tracking
LEMUR-2-BAXTER-OLIVER199846925U5237737792Tracking
LEMUR-2-DJARA199846926U5238138192Tracking
DESCENT199846927U5240240193Tracking
ISS DEB199847853U5241941693Tracking
RSP-01199847925U5241140893Tracking
TAUSAT-1199847926U5240940593Tracking
TSURU199847927U5241140993Tracking
STARS-EC199847928U5241140593Tracking
MMSATS-1199847976U5241741593Tracking
SOYUZ-MS 18202148159U5242141993Tracking
CREW DRAGON 2202148209U5242141993Tracking
TIANHE202148274U4138637392Tracking
TIANZHOU-2202148803U4138637392Tracking
RAMSAT199848850U5241841393Tracking
SOAR199848851U5241541193Tracking
SHENZHOU-12202148852U4138637392Tracking
BD-28199848867U5241741493Tracking
MIR-SAT 1199848868U5241641493Tracking
PROGRESS-MS 17202148869U5242141993Tracking
ISS (NAUKA)202149044U5242141993Tracking
SL-25 R/B202149045U5223716989Tracking
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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