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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)199825544U5240640393Tracking
FLOCK 2E'-1199841479U5218216888Tracking
FLOCK 2E'-3199841480U5215914688Tracking
FLOCK 2E-1199841483U5231130691Tracking
FLOCK 2E-5199841564U5232932491Tracking
FLOCK 2E-7199841565U5217716488Tracking
FLOCK 2E'-5199841567U5233032491Tracking
FLOCK 2E'-8199841569U5218317088Tracking
FLOCK 2E'-13199841761U5231830891Tracking
FLOCK 2E'-14199841762U5236235692Tracking
FLOCK 2E'-16199841763U5231430691Tracking
FLOCK 2E'-15199841764U5236535992Tracking
TIANGONG-2201641765U4338838292Tracking
FLOCK 2E'-18199841769U5236436092Tracking
FLOCK 2E'-17199841776U5233032591Tracking
FLOCK 2E'-19199841777U5230128990Tracking
FLOCK 2E'-20199841782U5234534291Tracking
BANXING-2201641834U4334733291Tracking
ITF-2199841932U5235434992Tracking
WASEDA-SAT3199841933U5234133691Tracking
AOBA-VELOX 3199841935U5234634191Tracking
LEMUR-2-REDFERN-GOES199842059U5235434892Tracking
LEMUR-2-TRUTNA199842067U5217616488Tracking
LEMUR-2-AUSTINTACIOUS199842068U5234433991Tracking
LEMUR-2-TRUTNAHD199842069U5235134692Tracking
HAVELSAT199842700U5236636292Tracking
SGSAT199842703U5228827690Tracking
CXBN-2199842704U5236636492Tracking
ICECUBE199842705U5235134792Tracking
PHOENIX199842706U5236836792Tracking
X-CUBESAT199842707U5236436392Tracking
QBEE50-LTU-OC199842708U5236636492Tracking
ALTAIR PATHFINDER199842711U5238237792Tracking
SHARC199842712U5238438192Tracking
ZA-AEROSAT199842713U5237337092Tracking
LINK199842714U5235034792Tracking
CSUNSAT 1199842715U5237336892Tracking
SPACECUBE199842717U5236736492Tracking
HOOPOE199842718U5236135992Tracking
CHALLENGER199842721U5234133691Tracking
NJUST-1199842722U5237737092Tracking
UNSW-ECO199842723U5236235692Tracking
LILACSAT-1199842725U5237136692Tracking
NSIGHT-1199842726U5238938292Tracking
SNUSAT-1199842727U5237336592Tracking
I-INSPIRE II199842731U5236135492Tracking
POLYITAN-2-SAU199842732U5236736092Tracking
SNUSAT-1B199842733U5237136392Tracking
EXALTA-1199842734U5236035392Tracking
BEEAGLESAT199842736U5237336692Tracking
PROGRESS-MS 07201742971U5243538493Tracking
ASTERIA199843020U5239539292Tracking
DELLINGR (RBLE)199843021U5239839693Tracking
TECHEDSAT 6199843026U5233132191Tracking
OSIRIS-3U199843027U5238638292Tracking
SOYUZ-MS 07201743063U5240740393Tracking
PROGRESS-MS 08201843211U5240740393Tracking
SOYUZ-MS 08201843238U5240740393Tracking
DRAGON CRS-14201843267U5240740393Tracking
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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