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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)199825544U5242341693Tracking
NSIGHT199842726U5228127390Tracking
KESTREL EYE IIM (KE2M)199842982U5236736292Tracking
ASTERIA199843020U5228127690Tracking
DELLINGR (RBLE)199843021U5236536192Tracking
1KUNS-PF199843466U5231631291Tracking
UBAKUSAT199843467U5235635392Tracking
CUBERRT199843546U5236035492Tracking
TEMPEST-D199843547U5238838092Tracking
RAINCUBE199843548U5236235592Tracking
HALOSAT199843549U5236335692Tracking
RADIX199843550U5226325290Tracking
ENDUROSAT ONE199843551U5234934291Tracking
EQUISAT199843552U5236235492Tracking
RADSAT-G199843553U5237236492Tracking
1998-067PC199843554U5234633891Tracking
AEROCUBE 12A201843556U5248347194Tracking
AEROCUBE 12B201843557U5248447294Tracking
LEMUR-2-VU201843558U5247946994Tracking
LEMUR-2-ALEXANDER201843559U5247946894Tracking
LEMUR-2-YUASA201843560U5247946994Tracking
LEMUR-2-TOMHENDERSON201843561U5248046994Tracking
SIRIUSSAT-1199843595U5236135692Tracking
SIRIUSSAT-2199843596U5236135692Tracking
TANUSHA-3199843597U5234433991Tracking
1998-067PK199843598U5234133691Tracking
1998-067PN199843638U5238337892Tracking
1998-067PP199843639U5237436792Tracking
STARS-ME199843640U5238037392Tracking
ISS DEB (SEDA-AP)199843870U5239939292Tracking
CATSAT-2199844029U5238337792Tracking
DELPHINI199844030U5238137492Tracking
UNITE199844031U5239138592Tracking
TECHEDSAT 8199844032U5230329591Tracking
CATSAT-1199844033U5238337792Tracking
ISS DEB199844303U5241040293Tracking
ISS DEB199844304U5239538892Tracking
ISS DEB199844305U5238938392Tracking
ISS DEB199844306U5241140193Tracking
RAAVANA-1199844329U5240339493Tracking
UGUISU199844330U5240339493Tracking
NEPALISAT-1199844331U5240339393Tracking
SPOOQY-1199844332U5240239493Tracking
PINOT199844364U5241240193Tracking
IOD-1 GEMS199844385U5239639292Tracking
SWIATOWID199844426U5239539092Tracking
KRAKSAT199844427U5240540093Tracking
VCC A199844428U5240239893Tracking
ENTRYSAT199844429U5240039693Tracking
VCC C199844430U5239839492Tracking
VCC B199844431U5240239793Tracking
SOYUZ-MS 15201944550U5242341693Tracking
ISS DEB199844788U5241140293Tracking
ISS DEB199844789U5241340393Tracking
RWASAT-1199844790U5241740493Tracking
AQT-D199844791U5241441093Tracking
NARSSCUBE-1199844792U5241440593Tracking
PROGRESS-MS 13201944833U5242341693Tracking
STPSAT-4199845043U5242341493Tracking
CYGNUS NG-13202045175U5242341693Tracking
HARP199845256U5242241093Tracking
1998-067RA199845257U5242241093Tracking
CRYOCUBE199845258U5242141193Tracking
1998-067RC199845259U5242241093Tracking
PHOENIX199845260U5242240993Tracking
AZTECHSAT-1199845261U5242140993Tracking
RADSAT-U199845262U5242141093Tracking
QARMAN199845263U5242241193Tracking
SORTIE199845264U5242341193Tracking
ICS-EF199845265U5242341493Tracking
DRAGON CRS-20202045341U5242341693Tracking
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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