ഫലകം:Infobox Spacecraft/doc

വിക്കിപീഡിയ, ഒരു സ്വതന്ത്ര വിജ്ഞാനകോശം.
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Usage[തിരുത്തുക]

{{Infobox spacecraft
| name                   = 
| image                  = 
| caption                =
| mission_identifier     =

| organisation           = 
| major_contractors      = 
| bus                    = 
| mission_type           = 
| flyby_of               = 
| flyby_date             = 
| current_destination    = 
| satellite_of           = 
| orbital_insertion_date = 
| orbits                 = 
| launch_date            = 
| launch_vehicle         =
| carrier_rocket         = <!-- or American "launch_vehicle" can be used -->
| flight_number          = 
| launch_site            = 
| mission_duration       = 

| mission_highlight      = 
| decay                  =
| return                 = <!-- for spacecraft designed to return to Earth -->
| return_site            = <!-- for spacecraft designed to return to Earth -->

| nolink                 = <!-- set to anything to prevent linking COSPAR to NSSDC database -->
| COSPAR_ID              = <!-- designations for pre-1963 launches should include a Greek letter, launches that failed to reach any orbit should not have a COSPAR -->
| NSSDC_ID               = 
| webpage                = 
| mass                   = 
| dimensions             = 
| power                  = 
| batteries              = 

<!-- Orbit data -->
| orbit_reference        = <!-- reference system -->
| orbit_regime           = 
| semimajor_axis         = 
| eccentricity           = 
| orbit_inclination      = 
| orbit_altitude         = 
| apoapsis               = 
| periapsis              = 
| orbital_period         = 
| longitude              = 
| repeat_interval        = 
| orbits_daily           = 
| repetitivity           = 
| orbit_swath            = 
| orbit_crossing         = <!-- equator crossing -->

<!-- Planetary/Lunar landing -->
| Planet                 = 
| Planet_Landing         = <!-- date/time -->
| Planet_Coords          = 
| Planet_Depart          = 
| LunarLandingDate       =
| LunarLandingCoords     =
| LunarLiftoffDate       =

<!-- Instruments -->
| Instruments            = 
| Main_Instruments       = 
| Resolution             = 
| Spectral_Band          = 
| Data_Rate              = 
| SSR                    = <!-- solid-state recorder -->
| IMG_Resolution         = 

<!-- Transponders -->
| Transponders           = 
| Transponder_Capacity   = 
| Coverage               = 
| Twta output power      = 
| Bandwidth              = 
| EIRP                   = 

| refs                   = 
| below                  = 
}}

Example from Ranger 1[തിരുത്തുക]

Ranger 1
Ranger 1
Ranger 1 Satellite in preparation for use at the Parade of Progress Show at the Public Hall, Cleveland, Ohio, August 1964
സംഘടനNASA
പ്രധാന ഉപയോക്താക്കൾJet Propulsion Laboratory
ഉപയോഗലക്ഷ്യംLunar Science
Satellite ofEarth
ഭ്രമണപഥത്തിൽ എത്തിയ ദിവസംAugust 23, 1961 at 10:02:00 UTC
ഭ്രമണപഥം110
വിക്ഷേപണ തീയതിAugust 23, 1961 at 06:02:00 UTC
വിക്ഷേപണ വാഹനംAtlas-Agena B
വിക്ഷേപണസ്ഥലംCape Canaveral Missile Test Annex, Florida, United States
പ്രവർത്തന കാലാവധി7 days
Orbital decayAugust 30, 1961
COSPAR ID1961-021A
HomepageNASA NSSDC Master Catalog
പിണ്ഡം306.2 kg
ഭ്രമണപഥത്തിന്റെ വിശദാംശങ്ങൾ
Semimajor axis6,690.3 km
Eccentricity.019939
Inclination32.9°
Apoapsis446 km
Periapsis179 km
Orbital period91.1 minutes
{{Infobox spacecraft
 | name              = Ranger 1
 | image             = [[File:Ranger 1.jpg|275px|Ranger 1]]
 | caption           = Ranger 1 Satellite in preparation for use at the Parade of Progress Show at the [[Public Auditorium|Public Hall]], [[Cleveland]], [[Ohio]], August 1964
 | organization      = [[NASA]]
 | major_contractors = [[Jet Propulsion Laboratory]]
 | mission_type      = [[Lunar Science]]
 | satellite_of      = [[Earth]]
 | orbital_insertion_date = August 23, 1961 at 10:02:00 [[Coordinated Universal Time|UTC]]
 | orbits            = 110
 | launch_date       = August 23, 1961 at 06:02:00 [[Coordinated Universal Time|UTC]]
 | launch_vehicle    = [[Atlas-Agena]] B
 | launch_site       = [[Kennedy Space Center|Cape Canaveral Missile Test Annex]], [[Florida]], [[United States]] 
 | mission_duration  = 7 days
 | decay             = August 30, 1961
 | NSSDC_ID          = 1961-021A
 | webpage           = [http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1961-021A NASA NSSDC Master Catalog]
 | mass              = 306.2 kg
 | semimajor_axis    = 6,690.3 km
 | eccentricity      = .019939
 | orbit_inclination = 32.9°
 | apoapsis          = 446 km
 | periapsis         = 179 km
 | orbital_period    = 91.1 minutes
}}
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