GSAT-2
E827016
GSAT-2 is an Indian communications satellite developed by ISRO to provide telecommunication, broadcasting, and experimental services in orbit.
All labels observed (1)
| Label | Occurrences |
|---|---|
| GSAT-2 canonical | 1 |
Statements (48)
| Predicate | Object |
|---|---|
| instanceOf |
communications satellite
ⓘ
geostationary satellite ⓘ |
| agency | Indian Space Research Organisation NERFINISHED ⓘ |
| category |
Indian communications satellite
ⓘ
satellite of India ⓘ |
| countryOfOrigin | India ⓘ |
| designedLifetime | 10 years ⓘ |
| dryMass | 830 kg ⓘ |
| followedBy | GSAT-3 NERFINISHED ⓘ |
| launchCountry | India NERFINISHED ⓘ |
| launchDate | 2003-05-08 ⓘ |
| launchMass | 1825 kg ⓘ |
| launchOutcome | successful ⓘ |
| launchSite |
Satish Dhawan Space Centre
NERFINISHED
ⓘ
Sriharikota NERFINISHED ⓘ |
| launchVehicle |
GSLV-D2
NERFINISHED
ⓘ
Geosynchronous Satellite Launch Vehicle NERFINISHED ⓘ |
| manufacturer |
ISRO
NERFINISHED
ⓘ
Indian Space Research Organisation NERFINISHED ⓘ |
| missionType |
broadcasting
ⓘ
communications ⓘ experimental ⓘ technology demonstration ⓘ |
| namedAfter | GSAT series designation ⓘ |
| operator |
ISRO
NERFINISHED
ⓘ
Indian Space Research Organisation ⓘ |
| orbitLongitude | 48° East ⓘ |
| orbitRegime | geostationary orbit ⓘ |
| orbitType | geosynchronous ⓘ |
| payload |
C-band transponders
ⓘ
Ku-band transponders ⓘ S-band transponders ⓘ radiation experiment ⓘ space science experiment ⓘ |
| power | 2000 W ⓘ |
| precededBy | GSAT-1 NERFINISHED ⓘ |
| program | GSAT programme ⓘ |
| propulsionType | liquid apogee motor ⓘ |
| providesService |
broadcasting services
ⓘ
experimental services ⓘ telecommunication services ⓘ |
| spacecraftBus | I-2K ⓘ |
| transponderBand |
C-band
ⓘ
Ku-band ⓘ S-band ⓘ |
| usesFrequencyBand |
Extended C-band
ⓘ
Ku-band ⓘ S-band ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.