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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)199825544U5242241793Tracking
KESTREL EYE IIM (KE2M)199842982U5228728290Tracking
DELLINGR (RBLE)199843021U5213712987Tracking
TEMPEST-D199843547U5225524289Tracking
AEROCUBE 12A201843556U5247646594Tracking
AEROCUBE 12B201843557U5247846794Tracking
LEMUR-2-VU201843558U5246946094Tracking
LEMUR-2-ALEXANDER201843559U5246845994Tracking
LEMUR-2-YUASA201843560U5246946094Tracking
LEMUR-2-TOMHENDERSON201843561U5247046094Tracking
1998-067PN199843638U5232231691Tracking
STARS-ME199843640U5225423989Tracking
ISS DEB (SEDA-AP)199843870U5238337892Tracking
UNITE199844031U5233633291Tracking
ISS DEB199844303U5239238692Tracking
ISS DEB199844306U5239138392Tracking
RAAVANA-1199844329U5234133491Tracking
UGUISU199844330U5234333691Tracking
NEPALISAT-1199844331U5234133491Tracking
SPOOQY-1199844332U5234433891Tracking
RED-EYE 1 (PINOT)199844364U5239338592Tracking
KRAKSAT199844427U5236936492Tracking
VCC A199844428U5234734291Tracking
ENTRYSAT199844429U5231730991Tracking
VCC B199844431U5234534191Tracking
ISS DEB199844789U5218216588Tracking
RWASAT-1199844790U5239238492Tracking
AQT-D199844791U5239138492Tracking
NARSSCUBE-1199844792U5237136692Tracking
STPSAT-4199845043U5240740193Tracking
HARP199845256U5239538792Tracking
1998-067RA199845257U5239839092Tracking
PHOENIX199845258U5240139493Tracking
1998-067RC199845259U5238637992Tracking
CRYOCUBE199845260U5238037292Tracking
AZTECHSAT-1199845261U5237636892Tracking
RADSAT-U199845262U5239639092Tracking
QARMAN199845263U5238737992Tracking
SORTIE199845264U5240739893Tracking
ICS-EF (ISS DEB)199845265U5241340693Tracking
G-SAT199845597U5239639192Tracking
QUETZAL-1199845598U5238938892Tracking
RED-EYE 2 (MERLOT)199845800U5240740693Tracking
RED-EYE 3 (CABERNET)199845809U5240740693Tracking
DEMI199845916U5239339092Tracking
SPOC199846921U5240540293Tracking
BOBCAT-1199846922U5240039893Tracking
NEUTRON-1199846923U5240640393Tracking
1998-067RU199846924U5239038792Tracking
LEMUR-2-BAXTER-OLIVER199846925U5238738592Tracking
LEMUR-2-DJARA199846926U5239038892Tracking
DESCENT199846927U5240640393Tracking
PROGRESS-MS 16202147618U5242241793Tracking
CYGNUS NG-15202147689U5242241793Tracking
ISS DEB199847853U5242041693Tracking
RSP-01199847925U5241341193Tracking
TAUSAT-1199847926U5241240893Tracking
TSURU199847927U5241441193Tracking
STARS-EC199847928U5241640893Tracking
MMSATS-1199847976U5241941593Tracking
SOYUZ-MS 18202148159U5242241793Tracking
CREW DRAGON 2202148209U5242241793Tracking
TIANHE202148274U4138737592Tracking
TIANZHOU-2202148803U4138737592Tracking
DRAGON CRS-22202148831U5242241793Tracking
2021-048B202148832U5227917689Tracking
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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