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Weather and Geoestationary Satellites
As its name says, are satellites whose main objective is to provide data and images of the displacement of masses of air, temperature, wind, etc.. In this category can be found the GOES and Meteosat geostationary satellites in addition to the satellites of NOAA series. The weather satellites are the most important tool to weather forecast.
Satellite Launch Norad Incl.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
NOAA 15199825338U99º809795101Tracking
DMSP 5D-3 F16 (USA 172)200328054U99º850840102Tracking
NOAA 18200528654U99º857837102Tracking
METEOSAT-9 (MSG-2)200528912U35788357851436Tracking
EWS-G1 (GOES 13)200629155U36475359151457Tracking
DMSP 5D-3 F17 (USA 191)200629522U99º849837102Tracking
FENGYUN 3A200832958U99º833821101Tracking
NOAA 19200933591U99º858838102Tracking
GOES 14200935491U35788357861436Tracking
DMSP 5D-3 F18 (USA 210)200935951U99º853835102Tracking
EWS-G2 (GOES 15)201036411U35798357741436Tracking
COMS 1201036744U35791357811436Tracking
FENGYUN 3B201037214U99º859827102Tracking
SUOMI NPP201137849U99º828825101Tracking
METEOSAT-10 (MSG-3)201238552U35791357791436Tracking
METOP-B201238771U99º821820101Tracking
INSAT-3D201339216U35794357801436Tracking
FENGYUN 3C201339260U98º850830102Tracking
METEOR-M 2201440069U98º824818101Tracking
HIMAWARI-8201440267U35788357851436Tracking
FENGYUN 2G201440367U35794357771436Tracking
METEOSAT-11 (MSG-4)201540732U35790357831436Tracking
ELEKTRO-L 2201541105U35797357751436Tracking
INSAT-3DR201641752U35836357371436Tracking
HIMAWARI-9201641836U35791357821436Tracking
GOES 16201641866U35796357801436Tracking
FENGYUN 4A201641882U35698356581431Tracking
CYGFM05201641884U35º45944594Tracking
CYGFM04201641885U35º45444194Tracking
CYGFM02201641886U35º45343893Tracking
CYGFM01201641887U35º45844594Tracking
CYGFM08201641888U35º45744194Tracking
CYGFM07201641890U35º45444194Tracking
CYGFM03201641891U35º45444294Tracking
FENGYUN 3D201743010U99º827826101Tracking
NOAA 20 (JPSS-1)201743013U99º828825101Tracking
GOES 17201843226U35795357781436Tracking
FENGYUN 2H201843491U35787357831436Tracking
METOP-C201843689U99º821819101Tracking
GEO-KOMPSAT-2A201843823U35794357791436Tracking
METEOR-M2 2201944387U99º812811101Tracking
ARKTIKA-M 1202147719U63º389421414718Tracking
FENGYUN 3E202149008U99º826825101Tracking
GOES 18202251850U35788357851436Tracking
NOAA 21 (JPSS-2)202254234U99º829825101Tracking
METEOSAT-12 (MTG-I1)202254743U35793357791436Tracking
TIANMU-1 03202355973U97º47046594Tracking
TIANMU-1 04202355974U97º47046494Tracking
TIANMU-1 05202355975U97º47046594Tracking
TIANMU-1 06202355976U97º46946494Tracking
METEOR-M2 3202357166U99º815808101Tracking
TIANMU-1 07202357399U97º49649395Tracking
TIANMU-1 08202357400U97º49849195Tracking
TIANMU-1 09202357401U97º49849195Tracking
TIANMU-1 10202357402U97º49949095Tracking
FENGYUN 3F202357490U99º826824101Tracking
ARKTIKA-M 2202358584U63º384641892718Tracking
TIANMU-1 11202358645U97º51149595Tracking
TIANMU-1 12202358646U97º51049695Tracking
TIANMU-1 13202358647U97º51049695Tracking
TIANMU-1 14202358648U97º51149595Tracking
TIANMU-1 19202358660U97º50349495Tracking
TIANMU-1 20202358661U97º50148895Tracking
TIANMU-1 21202358662U97º49648394Tracking
TIANMU-1 22202358663U97º50249495Tracking
TIANMU-1 15202458700U97º50949795Tracking
TIANMU-1 16202458701U97º50949795Tracking
TIANMU-1 17202458702U97º50849895Tracking
TIANMU-1 18202458703U97º50849895Tracking
INSAT-3DS202458990U35794357781436Tracking
METEOR-M2 4202459051U99º823812101Tracking
GOES 19202460133U35794357781436Tracking
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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