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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)199825544U5241039993Tracking
TIANGONG 1201137820U4336534492Tracking
SPINSAT199840314U5227326990Tracking
AGGIESAT 4199841313U5236936592Tracking
BEVO 2199841314U5234233891Tracking
MINXSS199841474U5234734691Tracking
STMSAT-1199841476U5234334191Tracking
NODES 2199841477U5236536492Tracking
NODES 1199841478U5236636592Tracking
FLOCK 2E'-1199841479U5238037792Tracking
FLOCK 2E'-3199841480U5238037692Tracking
FLOCK 2E'-2199841481U5237837492Tracking
FLOCK 2E'-4199841482U5237637492Tracking
FLOCK 2E-1199841483U5238037892Tracking
FLOCK 2E-2199841484U5237737692Tracking
LEMUR-2-THERESACONDOR199841485U5233432991Tracking
FLOCK 2E-3199841486U5238238092Tracking
FLOCK 2E-4199841487U5237937892Tracking
LEMUR-2-NICK-ALLAIN199841488U5233733391Tracking
LEMUR-2-KANE199841489U5233833391Tracking
LEMUR-2-JEFF199841490U5232732391Tracking
FLOCK 2E-6199841563U5238338092Tracking
FLOCK 2E-5199841564U5238338092Tracking
FLOCK 2E-7199841565U5237937592Tracking
FLOCK 2E-8199841566U5235835592Tracking
FLOCK 2E'-5199841567U5238638192Tracking
FLOCK 2E'-6199841568U5238337892Tracking
FLOCK 2E'-8199841569U5237737692Tracking
FLOCK 2E'-7199841570U5237437292Tracking
FLOCK 2E-9199841571U5237737492Tracking
FLOCK 2E-10199841572U5238037692Tracking
FLOCK 2E-12199841573U5237937592Tracking
FLOCK 2E-11199841574U5237937492Tracking
FLOCK 2E'-9199841575U5237837392Tracking
FLOCK 2E'-10199841576U5238037492Tracking
FLOCK 2E'-11199841577U5238037592Tracking
FLOCK 2E'-12199841578U5237937492Tracking
PROGRESS-MS 03201641670U5241039993Tracking
FLOCK 2E'-13199841761U5240138992Tracking
FLOCK 2E'-14199841762U5240038992Tracking
FLOCK 2E'-16199841763U5239938992Tracking
FLOCK 2E'-15199841764U5240039092Tracking
TIANGONG-2201641765U4338036992Tracking
FLOCK 2E'-18199841769U5239939092Tracking
FLOCK 2E'-17199841776U5239939092Tracking
FLOCK 2E'-19199841777U5239638792Tracking
FLOCK 2E'-20199841782U5239738892Tracking
SOYUZ-MS 02201641820U5241039993Tracking
BANXING-2201641834U4338036992Tracking
SOYUZ-MS 03201641864U5241039993Tracking
HTV-6 (KOUNOTORI 6)201641881U5241039993Tracking
STARS-C199841895U5240639793Tracking
ITF-2199841930U5239538592Tracking
WASEDA-SAT3199841931U5240839593Tracking
FREEDOM199841932U5240839793Tracking
EGG199841933U5240839893Tracking
TUPOD199841934U5240939693Tracking
AOBA-VELOX 3199841935U5240839893Tracking
1998-067KY199841936U5240839693Tracking
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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