साँचा:Infobox spacecraft/doc

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 साँचा:namespace detect

| type = notice | image = | imageright = | class = | style = margin-bottom:1.0em; | textstyle = | text = साँचा:strong for साँचा:terminate sentence
It contains usage information, categories and other content that is not part of the original साँचा page. | small = | smallimage = | smallimageright = | smalltext = | subst = | date = | name = }}

Usage

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

| organisation           = 
| major_contractors      = 
| bus                    = 
| mission_type           = 
| launch_date            = {{start-date|<!--insert date and time here-->|timezone=yes}}&nbsp;UTC
| launch_vehicle         = <!--  or British "carrier_rocket" can be used -->
| carrier_rocket         = <!-- or American "launch_vehicle" can be used -->
| flight_number          = 
| launch_site            = 
| mission_duration       = 
| mission_highlight      = 
| deactivated            = <!-- when craft stopped operating -->
| decay                  = <!-- when craft re-entered the atmosphere -->

| COSPAR_ID              = <!-- designations for pre-1963 launches should include a Greek letter, launches that failed to reach any orbit should not have a COSPAR -->
| nolink                 = <!-- set to anything to prevent linking COSPAR to NSSDC database -->
| satcat                 = <!-- Satellite Catalog Number -->
| webpage                = <!-- Homepage of the craft/mission -->
| mass                   = <!-- Orbit Mass or Launch Mass -->
| dimensions             = 
| power                  = 
| batteries              = 

<!-- for spacecraft designed to return to Earth intact -->
| return                 = <!--landing date/time-->
| return_site            = <!--where the spacecraft landed-->

<!-- 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 -->

<!-- Interplanetary missions -->
| flyby_of               = 
| flyby_date             = 
| current_destination    = 
| satellite_of           = 
| orbital_insertion_date = 
| orbits                 = 

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

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

<!-- Transponders -->
| Transponders           = 
| Transponder_Capacity   = 
| Coverage               = <!-- Coverage area -->
| Twta output power      = 
| Bandwidth              = 
| EIRP                   = <!-- Equivalent isotropically radiated power -->

| 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
संचालक	NASA
मुख्य संकुचक	Jet Propulsion Laboratory
साँचा:nowrap	Lunar Science
साँचा:nowrap	Earth
कक्षीय प्रविष्टि तिथि	August 23, 1961 at 10:02:00 UTC
कक्षा	110
साँचा:nowrap	August 23, 1961 at 06:02:00 UTC
साँचा:nowrap	Atlas-Agena B
साँचा:nowrap	Cape Canaveral Missile Test Annex, Florida, United States
मिशन अवधि	7 days
कक्षीय क्षय	August 30, 1961
कोसपार आईडी	1961-021A
गृह पृष्ठ	NASA NSSDC Master Catalog
भार	306.2 kg
कक्षीय तत्व
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
}}