Notice: Undefined variable: permalink in /home/mryscc50ot3h/public_html/topo.inc on line 7

Notice: Undefined variable: meta_title_facebook in /home/mryscc50ot3h/public_html/topo.inc on line 12

Notice: Undefined variable: meta_desc_facebook in /home/mryscc50ot3h/public_html/topo.inc on line 17
Brazil  Portugal  English

Notice: Undefined variable: insere_ads in /home/mryscc50ot3h/public_html/ads_160x600.inc on line 16
Scientific Satellites
Below follows the information found in the database of scientific satellites. They are satellites placed in orbit in order to study the high-atmosphere, effects of cosmic radiation or specific natural resources. In this category also are the telescopes and space observatories.
Satellite Launch Norad Incl.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
Hubble199020580U28º49649395Tracking
POLAR199623802U79º5057676481109Tracking
SWAS199825560U70º55854596Tracking
CXO199925867U47º14351952933808Tracking
XMM-NEWTON199925989U67º93428276792872Tracking
TERRA199925994U98º69369099Tracking
CLUSTER II-FM7 (SAMBA)200026410U143º12473368853217Tracking
CLUSTER II-FM8 (TANGO)200026464U143º12540169613242Tracking
ODIN200126702U97º46445494Tracking
TIMED200126998U74º58858696Tracking
CORIOLIS200327640U99º837815101Tracking
SORCE200327651U40º58155596Tracking
MOST200327843U99º829814101Tracking
SCISAT 1200327858U74º63362297Tracking
SWIFT200428485U21º47046194Tracking
CALIPSO200629108U98º66966798Tracking
HINODE (SOLAR-B)200629479U98º68065798Tracking
SHIJIAN-6 02A (SJ-6 02A)200629505U98º53853595Tracking
SHIJIAN-6 02B (SJ-6 02B)200629506U98º57056796Tracking
FGRST (GLAST)200833053U26º51149995Tracking
SDO201036395U34º35789357811436Tracking
CRYOSAT 2201036508U92º72271799Tracking
X-SAT201137389U98º818799101Tracking
GCOM-W1 (SHIZUKU)201238337U98º70470199Tracking
NUSTAR201238358U56655396Tracking
NEOSSAT201339089U98º781765100Tracking
BRITE-AUSTRIA201339091U98º779763100Tracking
IRIS201339197U98º63459897Tracking
HISAKI (SPRINT-A)201339253U30º1154950106Tracking
CASSIOPE201339265U81º88130397Tracking
STSAT-3201339422U98º58455796Tracking
SWARM B201339451U88º49549194Tracking
SWARM A201339452U87º44744494Tracking
SWARM C201339453U87º44744494Tracking
BRITE-CA1 (TORONTO)201440020U98º71360198Tracking
OCO 2201440059U98º70470199Tracking
BRITE-PL2 (HEWELIUSZ)201440119U98º60258297Tracking
MMS 1201540482U62º17809651775090Tracking
MMS 2201540483U62º17810551905091Tracking
MMS 3201540484U62º17809651985091Tracking
MMS 4201540485U62º17808451945090Tracking
ASTROSAT201540930U63262097Tracking
DAMPE201541173U97º48647194Tracking
PISAT201641784U98º68964898Tracking
HXMT (HUIYAN)201742758U43º55450495Tracking
FLYING LAPTOP201742831U97º58056596Tracking
ZHANGHENG 1 (CSES)201843194U98º50849995Tracking
SALSAT202046495U98º51349495Tracking
IXPE202149954U56054996Tracking
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.

Satview - All Rights Reserved 2008 - 2025
Privacy policy