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Rohini
 Rohini Credit: ISRC |
Status: Operational 1980. First Launch: 1980-07-18. Last Launch: 1983-04-17. Number: 2 . Gross mass: 41 kg (90 lb).
More at: Rohini.
Family: Earth, Earth land resource sat. Country: India. Launch Vehicles: SLV, SLV-3, ASLV. Launch Sites: Sriharikota, Sriharikota SLV. Agency: ISRO. Bibliography: 2, 279, 6, 6829, 13027.
 | Rohini 1A Credit: Manufacturer Image |
 | Rohini 2 Credit: Manufacturer Image |
1980 July 18 - . 02:33 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. LV Family: SLV. Launch Vehicle: SLV-3.
- Rohini RS-1 - . Payload: Rohini 1B. Mass: 40 kg (88 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: Rohini. Decay Date: 1981-05-20 . USAF Sat Cat: 11899 . COSPAR: 1980-062A. Apogee: 921 km (572 mi). Perigee: 307 km (190 mi). Inclination: 44.70 deg. Period: 97.00 min. Experimental-technology mission. Rohini satellite RS-1. .
1983 April 17 - . 05:44 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. LV Family: SLV. Launch Vehicle: SLV-3.
- Rohini 3 - . Payload: Rohini RS-D-2. Mass: 42 kg (92 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: Rohini. Decay Date: 1990-04-19 . USAF Sat Cat: 14002 . COSPAR: 1983-033A. Apogee: 485 km (301 mi). Perigee: 326 km (202 mi). Inclination: 46.60 deg. Period: 92.70 min. Rohini satellite D-2. Second developmental flight of an SLV-3 launch vehicle. The Rohini satellite D-2 carried a sensor payload for conducting remote-sensing experiments and for accurate orbit and attitude determination. .
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