RadSat-1: Difference between revisions
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<!--as science-related articles, SI units should be the principal units of measurement, however we usually use {{convert}} to display imperial units in parentheses after the initial values--> | <!--as science-related articles, SI units should be the principal units of measurement, however we usually use {{convert}} to display imperial units in parentheses after the initial values--> | ||
| orbit_epoch = <!--the date at which the orbit parameters were correct--> | | orbit_epoch = <!--the date at which the orbit parameters were correct--> | ||
| orbit_reference = [[ | | orbit_reference = [[wikipedia:Geocentric_orbit|Geocentric]] | ||
| orbit_regime = [[ | | orbit_regime = [[wikipedia:Geostationary_orbit|Geostationary]] | ||
| orbit_periapsis = <!--periapsis altitude--> | | orbit_periapsis = <!--periapsis altitude--> | ||
| orbit_apoapsis = <!--apoapsis altitude--> | | orbit_apoapsis = <!--apoapsis altitude--> | ||
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<!--transponder parameters--> | <!--transponder parameters--> | ||
| trans_band = 28 [[ | | trans_band = 28 [[wikipedia:Ku-band|Ku]]-band <br>15 [[wikipedia:C_band_(IEEE)|C]]-band | ||
| trans_frequency = <!--specific frequencies--> | | trans_frequency = <!--specific frequencies--> | ||
| trans_bandwidth = 40 x 36 MHz <br>3 x 72 MHz | | trans_bandwidth = 40 x 36 MHz <br>3 x 72 MHz | ||
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<!--Only use where a spacecraft/mission is part of a clear programme of sequential missions, if in doubt, leave it out--> | <!--Only use where a spacecraft/mission is part of a clear programme of sequential missions, if in doubt, leave it out--> | ||
| previous_mission = | | previous_mission = | ||
| next_mission = | | next_mission = | ||
| programme = | | programme = | ||
}} | }} | ||
'''RadSat-1''' is a [[Radictistan|Radictistani]] [[ | '''RadSat-1''' is a [[Radictistan|Radictistani]] [[wikipedia:Communications_satellite|communications satellite]] owned and operated by [[RadSat]], used primarily for digital television. The satellite has 28 [[wikipedia:Ku-band|Ku]]-band and 12 [[wikipedia:C_band_(IEEE)|C]]-band [[wikipedia:Transponder_(satellite_communications)|transponders]] each with 36 [[wikipedia:Hertz|MHz]] bandwidth for television broadcasting. In addition, the satellite has three 72 MHz C-band transponders for international telephony. RadSat-1 has two fixed beams serving the continent of [[Apathia]]. | ||
[[Category:Science and technology in Radictistan]] | [[Category:Science and technology in Radictistan]] | ||
[[Category:Satellites]] | [[Category:Satellites]] |
Latest revision as of 02:27, 6 September 2023
This Radictistan-related article is a stub. You can help the wiki by expanding it.
Mission type | Communications |
---|---|
Operator | RadSat |
COSPAR ID | Template:Cospar |
SATCAT no. | Template:Wd |
Spacecraft properties | |
Spacecraft | RadSat-1 |
Bus | RadSat A |
Manufacturer | Konavia Orbital |
Launch mass | 5,150 kilograms |
Start of mission | |
Launch date | September 16, 2013 |
Contractor | Hatsunespace |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Transponders | |
Band | 28 Ku-band 15 C-band |
Bandwidth | 40 x 36 MHz 3 x 72 MHz |
Coverage area | Apathia |
RadSat-1 is a Radictistani communications satellite owned and operated by RadSat, used primarily for digital television. The satellite has 28 Ku-band and 12 C-band transponders each with 36 MHz bandwidth for television broadcasting. In addition, the satellite has three 72 MHz C-band transponders for international telephony. RadSat-1 has two fixed beams serving the continent of Apathia.