ഫലകം:Infobox Spacecraft/doc

Usage

{{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

Ranger 1

Ranger 1 Satellite in preparation for use at the Parade of Progress Show at the Public Hall, Cleveland, Ohio, August 1964
സംഘടന	NASA
പ്രധാന ഉപയോക്താക്കൾ	Jet Propulsion Laboratory
ഉപയോഗലക്ഷ്യം	Lunar Science
Satellite of	Earth
ഭ്രമണപഥത്തിൽ എത്തിയ ദിവസം	August 23, 1961 at 10:02:00 UTC
ഭ്രമണപഥം	110
വിക്ഷേപണ തീയതി	August 23, 1961 at 06:02:00 UTC
വിക്ഷേപണ വാഹനം	Atlas-Agena B
വിക്ഷേപണസ്ഥലം	Cape Canaveral Missile Test Annex, Florida, United States
പ്രവർത്തന കാലാവധി	7 days
Orbital decay	August 30, 1961
COSPAR ID	1961-021A
Homepage	NASA NSSDC Master Catalog
പിണ്ഡം	306.2 kg
ഭ്രമണപഥത്തിന്റെ വിശദാംശങ്ങൾ
Semimajor axis	6,690.3 km
Eccentricity	.019939
Inclination	32.9°
Apoapsis	446 km
Periapsis	179 km
Orbital period	91.1 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
}}