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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)199825544U5240939993Tracking
TIANGONG 1201137820U4335833391Tracking
SPINSAT199840314U5214113487Tracking
AGGIESAT 4199841313U5236235792Tracking
BEVO 2199841314U5231931591Tracking
MINXSS199841474U5231931391Tracking
STMSAT-1199841476U5230229590Tracking
NODES 2199841477U5235434892Tracking
NODES 1199841478U5235434992Tracking
FLOCK 2E'-1199841479U5237437192Tracking
FLOCK 2E'-3199841480U5237337092Tracking
FLOCK 2E'-2199841481U5237136992Tracking
FLOCK 2E'-4199841482U5236836592Tracking
FLOCK 2E-1199841483U5237537192Tracking
FLOCK 2E-2199841484U5237236892Tracking
LEMUR-2-THERESACONDOR199841485U5224123589Tracking
FLOCK 2E-3199841486U5237737392Tracking
FLOCK 2E-4199841487U5237537092Tracking
LEMUR-2-NICK-ALLAIN199841488U5227426890Tracking
LEMUR-2-KANE199841489U5227627090Tracking
LEMUR-2-JEFF199841490U5214914587Tracking
FLOCK 2E-6199841563U5237637592Tracking
FLOCK 2E-5199841564U5237737592Tracking
FLOCK 2E-7199841565U5237236892Tracking
FLOCK 2E-8199841566U5234033391Tracking
FLOCK 2E'-5199841567U5238037692Tracking
FLOCK 2E'-6199841568U5237637392Tracking
FLOCK 2E'-8199841569U5237136892Tracking
FLOCK 2E'-7199841570U5236736292Tracking
FLOCK 2E-9199841571U5237136692Tracking
FLOCK 2E-10199841572U5237337092Tracking
FLOCK 2E-12199841573U5237236892Tracking
FLOCK 2E-11199841574U5237136792Tracking
FLOCK 2E'-9199841575U5236936692Tracking
FLOCK 2E'-10199841576U5237136892Tracking
FLOCK 2E'-11199841577U5237336992Tracking
FLOCK 2E'-12199841578U5237136692Tracking
FLOCK 2E'-13199841761U5239638692Tracking
FLOCK 2E'-14199841762U5239538692Tracking
FLOCK 2E'-16199841763U5239438592Tracking
FLOCK 2E'-15199841764U5239538792Tracking
TIANGONG-2201641765U4338437492Tracking
FLOCK 2E'-18199841769U5239538792Tracking
FLOCK 2E'-17199841776U5239538792Tracking
FLOCK 2E'-19199841777U5239038292Tracking
FLOCK 2E'-20199841782U5239238492Tracking
SOYUZ-MS 02201641820U5240939993Tracking
BANXING-2201641834U4337636592Tracking
SOYUZ-MS 03201641864U5240939993Tracking
STARS-C199841895U5239839192Tracking
TANCREDO-1199841931U5239538392Tracking
ITF-2199841932U5240239393Tracking
WASEDA-SAT3199841933U5240139392Tracking
EGG199841934U5238137092Tracking
AOBA-VELOX 3199841935U5240139393Tracking
TUPOD199841936U5239138292Tracking
OSNSAT199841939U5239738892Tracking
DRAGON CRS-10201742053U5240940093Tracking
PROGRESS-MS 05201742056U5240939993Tracking
LEMUR-2-REDFERN-GOES199842059U5240839593Tracking
TECHEDSAT 5199842066U5240239192Tracking
LEMUR-2-TRUTNA199842067U5240839493Tracking
LEMUR-2-AUSTINTACIOUS199842068U5240839593Tracking
LEMUR-2-TRUTNAHD199842069U5240839593Tracking
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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