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Sriharikota
Sriharikota
Credit: © Mark Wade
AKA: Satish Dhawan Space Center;Satish Dhawan Space Centre;SDSC;SHAR. First Launch: 1971-10-09. Last Launch: 2014-06-30. Number: 381 . Location: Andhra Pradesh. Longitude: 80.24 deg. Latitude: 13.74 deg.
The Satish Dhawan Space Centre (SDSC) SHAR, is located at 80 km north of Chennai on the east coast of India. The facilities at SDSC include:
- Mobile Service Tower, Umbilical Tower and Launch Pedestal
- Solid Motor Preparation Facility
- Subsystem Preparation Facility
- Hardware Storage Facility
- Liquid/Cryogenic Propellant Storage and Transfer Facility
- Stage Preparation Facility for Cryogenic Stage
- Automatic Checkout and Control for Propellant Filling
- Safety and Fire Fighting Systems
- Satellite Preparation Facility
- Launch Control Centre and Mission Control Centre
- Precision C-band Radars and S-band Radar for tracking
- Telecommand System
- Intercommunication, CCTV system, Data Links, Range Timing System, Real Time Systems and Specialist Display System, Meteorology and Technical Photography
- TM data receiving stations
Minimum Inclination: 44.0 degrees. Maximum Inclination: 47.0 degrees.
| Sriharikota SLV SLV, ASLV launch complex. SLV pad |
| Sriharikota PSLV First Launch Complex. PSLV launch complex. Adapted for GSLV launches. |
| Sriharikota SLP Second Launch Complex. GSLV launch complex. |
| Sriharikota RH Sounding rocket complex |
Family: Orbital Launch Site, Shahab. Country: India. Spacecraft: I-1K, Oscar, Rohini 1A, Rohini, Rohini 2, SROSS, IRS, Tubsat, Kitsat, Insat 3, Rubin, GSat, BIRD, PROBA, TES, METSAT, Cute, Pehuensat, SRE, AGILE, AAUSat, Can X, Compass, Delfi, IMS, SEEDS, Chandraayan, MIP. Launch Vehicles: SLV-3, ASLV, RH-125, RH-560, RH-200, SLV-3, RH-300 TV, ASLV, RH-300 Mk II, Prithvi, PSLV, RH-560/300 Mk II, Shahab 3, GSLV, RH-200SV, PSLV CA, PSLV-XL, PSLV, GSLV, PSLV-XL, GSLV-3, PSLV, GSLV, PSLV CA, GSLV Mk II, PSLV-XL. Projects: Insat. Launch Sites: Sriharikota SLV, Sriharikota PSLV, Sriharikota SLP, Sriharikota RH. Agency: ISRO. Bibliography: 2.
 | Sriharikota Location of Sriharikota Credit: © Mark Wade |
1971 October 9 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-125.
1974 April 24 - . 13:00 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1976 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560. FAILURE: Failure.
1977? - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1977 February 14 - . 13:00 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 June 24 - . 17:06 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1979 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 July 11 - . 13:18 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 August 10 - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. LV Family: SLV. Launch Vehicle: SLV-3. FAILURE: Thrust vectoring of second stage failed.. Failed Stage: 2.
- Rohini 1A - . Payload: Rohini RS-1. Nation: India. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Rohini 1A. Decay Date: 1979-08-19 .
1979 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 November 28 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 December 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 December 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 December 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1979 December 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 February 16 - . 08:50 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1980 February 16 - . 10:15 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560. FAILURE: Failure.
1980 February 27 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 July 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
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. .
1980 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 August 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 August 29 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 September 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 1 - . 15:33 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1980 October 29 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 October 31 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 December 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 December 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 December 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1980 December 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 January 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 May 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 May 31 - . 05:00 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. LV Family: SLV. Launch Vehicle: SLV-3. FAILURE: Partial Failure.. Failed Stage: U.
- Rohini 2 - . Payload: Rohini RS-D-1. Nation: India. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Rohini 2. Decay Date: 1981-05-31 . USAF Sat Cat: 12491 . COSPAR: 1981-051A. Apogee: 374 km (232 mi). Perigee: 181 km (112 mi). Inclination: 46.20 deg. Period: 90.06 min. Orbit too low..
1981 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1981 June 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 February 16 - . 13:39 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1982 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 March 1 - . 13:35 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1982 March 24 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 April 28 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 May 5 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 June 2 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1982 November 23 - . 15:10 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1982 November 29 - . 16:50 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
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. .
1984 May 23 - . 12:45 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 May 25 - . 12:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 May 25 - . 13:36 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 May 27 - . 12:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 May 27 - . 13:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 May 29 - . 12:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 May 31 - . 12:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 June 2 - . 12:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 June 4 - . 12:40 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 June 6 - . 12:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 June 8 - . 13:01 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 June 10 - . 12:40 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1984 June 12 - . 12:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1985 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300 TV.
1986 January 15 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 16 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 17 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 18 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 19 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 20 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 21 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 22 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 23 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 24 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 25 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 26 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 27 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 28 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 29 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 30 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 January 31 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 2 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 3 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 4 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 5 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 6 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 7 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 8 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 9 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 10 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 11 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 12 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 13 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 14 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 15 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 16 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 17 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 18 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 19 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 20 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 21 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 22 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 23 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 24 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 25 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 26 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 27 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1986 February 28 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1987 March 24 - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. Launch Vehicle: ASLV. FAILURE: Second stage failed to ignite.. Failed Stage: 2.
- SROSS A - . Mass: 150 kg (330 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Magnetosphere satellite. Spacecraft: SROSS. Decay Date: 1987-03-24 . Apogee: 10 km (6 mi).
1987 May 4 - . 04:40 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1987 June 8 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300 Mk II.
1988 February 25 - . Launch Site: Sriharikota. LV Family: S-75. Launch Vehicle: Prithvi.
1988 July 13 - . 09:18 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. Launch Vehicle: ASLV. FAILURE: First stage failure. Insufficient control gain.. Failed Stage: 1.
- SROSS B - . Mass: 150 kg (330 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Magnetosphere satellite. Spacecraft: SROSS. Decay Date: 1988-07-13 . Apogee: 25 km (15 mi).
1988 October 4 - . 16:00 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1989 September 27 - . Launch Site: Sriharikota. LV Family: S-75. Launch Vehicle: Prithvi.
1991 February 11 - . Launch Site: Sriharikota. LV Family: S-75. Launch Vehicle: Prithvi.
1991 July 4 - . Launch Site: Sriharikota. LV Family: S-75. Launch Vehicle: Prithvi.
1991 August 7 - . 05:28 GMT - . Launch Site: Sriharikota. LV Family: S-75. Launch Vehicle: Prithvi.
1992 - . Launch Site: Sriharikota. LV Family: S-75. Launch Vehicle: Prithvi. FAILURE: Failure.
1992 May 20 - . 00:30 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. Launch Vehicle: ASLV. FAILURE: Insufficient spin stabilization of fifth stage. Partial Failure.. Failed Stage: 5.
- SROSS 3 - .
Payload: SROSS C. Mass: 106 kg (233 lb). Nation: India.
Agency: ISRO.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: SROSS.
Decay Date: 1992-07-14 . USAF Sat Cat: 21968 . COSPAR: 1992-028A. Apogee: 436 km (270 mi). Perigee: 251 km (155 mi). Inclination: 46.00 deg. Period: 91.40 min.
Stretched Rohini Satellite Series; carried gamma-ray detector, ionosphere monitor. SROSS-C satellite carries two scientific payloads: 1) Retarding Potential Analyser (RPA), consisting of two planar detectors to measure plasma parameters and investigate energetics of the equatorial ionosphere. (2) Gamma Ray Burst (GRB) detectors, consist ing of two scintillation detectors to study celestial gamma ray bursts in the energy range of 20 keV to 3000 keV. Launch vehicle: Augmented Satellite Launch Vehicle.
1992 July 3 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1992 October 14 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1992 October 19 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
1993 February 19 - . 13:15 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1993 February 19 - . 13:45 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1993 April 19 - . 05:50 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
1993 September 20 - . 05:12 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV. FAILURE: Software error caused vehicle to go off course.. Failed Stage: G.
- IRS-1E - . Payload: IRS-1E. Mass: 1,250 kg (2,750 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS.
1994 May 4 - . 00:00 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLV. Launch Vehicle: ASLV.
- SROSS-C2 - .
Payload: SROSS C2. Mass: 113 kg (249 lb). Nation: India.
Agency: ISRO.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: SROSS.
Decay Date: 2001-07-12 . USAF Sat Cat: 23099 . COSPAR: 1994-027A. Apogee: 938 km (582 mi). Perigee: 437 km (271 mi). Inclination: 46.20 deg. Period: 98.00 min.
Streched Rohini Satellite Series; measured ionospheric plasma and gamma rays. SROSS-C2 satellite carries two scientific payloads: (i) Retarding Potential Analyser (RPA), consisting of two planar detectors to measure plasma parameters and investigate energetics of the equatorial ionosphere. (ii) Gamma Ray Burst (GRB) detectors, cons isting of two scintillators to study celestial gamma ray bursts in the energy range of 20 keV to 3000 keV. Launch vehicle Augmented Satellite Launch Vehicle ASLV-D4.
1994 October 15 - . 05:05 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- IRS-P2 - . Mass: 870 kg (1,910 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 23323 . COSPAR: 1994-068A. Apogee: 820 km (500 mi). Perigee: 818 km (508 mi). Inclination: 98.67 deg. Period: 101.29 min. Remote sensing; sun-synch orbit..
1995 August 16 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560/300 Mk II.
1996 March 21 - . 04:53 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- IRS-P3 - . Mass: 930 kg (2,050 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 23827 . COSPAR: 1996-017A. Apogee: 820 km (500 mi). Perigee: 819 km (508 mi). Inclination: 98.50 deg. Period: 101.30 min. LEO .
1997 April 30 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560/300 Mk II.
1997 September 29 - . 04:47 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- IRS-1D - . Payload: IRS-P3. Mass: 1,250 kg (2,750 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 24971 . COSPAR: 1997-057A. Apogee: 823 km (511 mi). Perigee: 742 km (461 mi). Inclination: 98.50 deg. Period: 100.50 min.
1998 April 6 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560/300 Mk II.
1998 April 19 - . 13:51 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560/300 Mk II.
1998 September 21 - . 14:51 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560/300 Mk II.
1998 September 28 - . 15:11 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560/300 Mk II.
1999 May 26 - . 06:22 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- Kitsat-3 - . Mass: 50 kg (110 lb). Nation: Korea South. Agency: ISRO. Manufacturer: KAIST. Class: Earth. Type: Seismology satellite. Spacecraft: Kitsat. USAF Sat Cat: 25756 . COSPAR: 1999-029A. Apogee: 727 km (451 mi). Perigee: 707 km (439 mi). Inclination: 98.60 deg. Period: 99.10 min.
- DLR-Tubsat - .
Mass: 45 kg (99 lb). Nation: Germany.
Agency: DLR.
Class: Earth.
Type: Seismology satellite. Spacecraft: Tubsat.
USAF Sat Cat: 25757 . COSPAR: 1999-029B. Apogee: 733 km (455 mi). Perigee: 712 km (442 mi). Inclination: 98.60 deg. Period: 99.20 min.
DLR-Tubsat carried on the experimental work of Tubsat-A and -B. The satellite measured 32x32x32 cm and had a mass of 44.8 kg. The dechnology demonstrator conducted earth observation with 6 m resolution and conducted attitude control experiments. It was still in operation as of 2003.
- OceanSat 1 (IRS-P4) - . Payload: IRS-P4. Mass: 1,036 kg (2,283 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Sea satellite. Spacecraft: IRS. USAF Sat Cat: 25758 . COSPAR: 1999-029C. Apogee: 724 km (449 mi). Perigee: 721 km (448 mi). Inclination: 98.30 deg. Period: 99.30 min. Remote sensing satellite with Ocean Colour Monitor (OCM) and a Multi-frequency Scanning Microwave Radiometer (MSMR).
1999 November 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300.
1999 November 18 - . 01:55 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300 Mk II.
1999 November 20 - . 01:35 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300 Mk II.
2000 February 21 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
- Atmospheric Waves (1 of 40) Aeronomy mission - . Nation: India. Agency: ISRO. Apogee: 70 km (43 mi).
2000 February 22 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 February 23 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 February 24 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 February 25 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 February 26 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 February 27 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 February 28 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 2 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 3 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 4 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 5 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 6 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 7 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 8 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 9 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 10 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 11 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 12 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 13 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 14 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 15 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 16 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 17 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 18 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 19 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 20 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 21 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 22 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 23 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 24 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 25 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 26 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 27 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 28 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 29 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 30 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 March 31 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2000 April 1 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2001 April 18 - . 10:13 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: GSLV.
- GSAT-1 - .
Payload: GramSat. Mass: 1,530 kg (3,370 lb). Nation: India.
Agency: ISRO.
Program: Insat.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: I-2K.
USAF Sat Cat: 26745 . COSPAR: 2001-015A. Apogee: 35,814 km (22,253 mi). Perigee: 33,825 km (21,017 mi). Inclination: 0.00 deg. Period: 1,387.00 min.
Experimental Rural Communications satellite. Launch delayed following pad abort on March 28. First launch of the Indian GSLV launch vehicle. GSat 1 was an Indian, 1500 kg scaled-dow) test model of a future geosynchronous communications spacecraft with a 440 N ISRO liquid apogee motor, and S-band and C-band ommunications transponders, similar to the Insat-2 satellites. The motor for the cryogenic, hydrogen-oxygen upper stage had been purchased from Russia but the design had never flown in space before. The stage cut off without providing the required delta-V - preliminary analysis revealed a shortfall of 0.5% in the thrust. An attempt was made to reach a usable orbit using the station-keeping motor of the GSAT satellite itself. After a series of burns, GSat 1 ran out of propellant - 10 kg more fuel would have been required to reach a stationary orbit. In the end, the parameters of the drifting (about 13 deg/day) orbit were period 23 hours, apogee 35,665 km, perigee 33,806 km, and inclination 0.99 deg. The fully functional transponders and transmitters on board were deactivated on instructions of the International Telecommunications Union. As of 4 September 2001 located at 54.88 deg E drifting at 13.212 deg E per day. As of 2007 Mar 10 located at 50.16W drifting at 12.778E degrees per day.
2001 October 22 - . 04:53 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- TES - .
Mass: 1,108 kg (2,442 lb). Nation: India.
Agency: ISRO.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: IRS.
Spacecraft: TES.
USAF Sat Cat: 26957 . COSPAR: 2001-049A. Apogee: 592 km (367 mi). Perigee: 533 km (331 mi). Inclination: 97.60 deg. Period: 95.90 min.
Launch delayed from July 20. The PS4 upper stage deployed the 1108 kg Indian TES (Technology Experiment Satellite) into a sun-synchronous orbit at 05:09:10 GMT. TES was an imaging satellite equipped with cameras and instruments to test military reconnaissance satellite technology. It was probably based on the IRS remote sensing satellite and carried a one-meter resolution panchromatic camera. India decided to develop an independent indigenous reconnaissance satellite capability after the 1999 incursion of Pakistani troops into disputed territory in Kashmir caught it by surprise. TES was developed by ISRO, the Indian Space Research Organization.
- BIRD - .
Mass: 1,108 kg (2,442 lb). Nation: Germany.
Agency: ISRO.
Class: Earth.
Type: Earth resources satellite. Spacecraft: BIRD.
USAF Sat Cat: 26959 . COSPAR: 2001-049C. Apogee: 529 km (328 mi). Perigee: 509 km (316 mi). Inclination: 97.90 deg. Period: 95.00 min.
BIRD (Bispectral IR Detector) was a 94 kg German research minisatellite testing a new sensor for Earth imaging studies, detecting forest fires and other hot spots and studying vegetation changes. BIRD was released by the PS4 upper stage 40 seconds after the primary TES satellite payload had been deployed. The technology demonstrator was to help in the design a major remote sensing array of infrared detectors.
- PROBA - .
Mass: 1,108 kg (2,442 lb). Nation: Europe.
Agency: ISRO.
Class: Earth.
Type: Earth resources satellite. Spacecraft: PROBA.
USAF Sat Cat: 26958 . COSPAR: 2001-049B. Apogee: 677 km (420 mi). Perigee: 553 km (343 mi). Inclination: 97.90 deg.
Proba (PRoject for On-Board Autonomy, 1) was a European Space Agency technology development minisatellite with a mass of 94 kg. It carried a radiation detector, an IR spectrometer, debris impact detectors, Earth imaging cameras, and an experimental spacecraft processor for spacecraft autonomy experiments. The satellite was built by Verheart in Belgium using the MiniSIL bus developed by SI of England, and was controlled from Belgium. After release of the TES and BIRD satellites, the PS4's upper stage small RCS engines raised the orbit to 553 x 676 km, and PROBA was ejected at 0520 GMT.
2002 September 12 - . 10:25 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- Metsat 1 - .
Mass: 1,000 kg (2,200 lb). Nation: Europe.
Agency: ISRO.
Class: Earth.
Type: Weather satellite. Spacecraft: I-1K.
USAF Sat Cat: 27525 . COSPAR: 2002-043A. Apogee: 35,809 km (22,250 mi). Perigee: 35,764 km (22,222 mi). Inclination: 0.30 deg. Period: 1,436.10 min.
METSAT 1 was an Indian (ISRO) meteorological, geostationary satellite that was launched by an upgraded, four-stage PSLV-C4 rocket. The satellite was manoeuvred from the transfer orbit to a geostationary postion at 37° E longitude on September 16, and then was parked at 74° E longitude on September 24. As of 2007 Mar 11 located at 74.00E drifting at 0.007W degrees per day.
2003 March 20 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200SV.
2003 May 8 - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: GSLV.
- GSAT-2 - .
Payload: GramSat. Mass: 1,825 kg (4,023 lb). Nation: India.
Agency: ISRO.
Program: Insat.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: I-2K.
USAF Sat Cat: 27807 . COSPAR: 2003-018A. Apogee: 35,790 km (22,230 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.10 min.
Experimental Rural Communications. Launch delayed from original target of late 2001, then October 2002, then February 2003. The satellite carried four C-band transponders, two Ku-band transponders and a Mobile Satellite Service (MSS) payload operating in S-band and C-band for forward link and return link respectively. GSAT-2 also carried four piggyback experimental payloads: Total Radiation Dose Monitor (TRDM), Surface Charge Monitor (SCM), Solar X-ray Spectrometer (SOXS) and Coherent Radio Beacon Experiment (CRABEX). As of 2007 Mar 10 located at 47.97E drifting at 0.005E degrees per day.
2003 October 17 - . 04:54 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- ResourceSat 1 (IRS-P6) - . Mass: 1,360 kg (2,990 lb). Nation: India. Agency: ISRO. Program: IRS. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 28051 . COSPAR: 2003-046A. Apogee: 836 km (519 mi). Perigee: 813 km (505 mi). Inclination: 98.80 deg. Period: 101.40 min. The satellite was to replace IRS-1C and IRS-1D, and carried three cameras for remote sensing, the highest resolution one being the 6-meter LISS-4 imager. The sensors were designed for agricultural remote sensing applications..
2004 July 23 - . 06:12 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300 Mk II.
2004 July 23 - . 06:45 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
- Meospheric Turbulence Chaff Aeronomy mission - . Nation: India. Agency: ISRO. Apogee: 75 km (46 mi).
2004 September 20 - . 10:31 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: GSLV.
- GSAT-3 / Edusat - .
Payload: GramSat. Mass: 1,950 kg (4,290 lb). Nation: India.
Agency: ISRO.
Program: Insat.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: I-2K.
USAF Sat Cat: 28417 . COSPAR: 2004-036A. Apogee: 35,801 km (22,245 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.10 deg. Period: 1,436.10 min.
Gsat-3 / Edusat was the first Indian satellite built exclusively for the educational sector. It was mainly intended to meet the demand for an interactive satellite based distance education system for India. Edusat was launched into a geosynchronous transfer orbit by its launch vehicle. Edusat was to reach geostationary orbit by firing, in stages, its on board Liquid Apogee Motor (LAM). In geostationary orbit the satellite was to be co-located with Kalpana-1 and Insat-3C satellites at 74 deg East longitude.
Compared to earlier satellites in the Insat series, Edusat used several new technologies. The spacecraft was built around the I-2K standardised spacecraft bus. It had a multiple spot beam antenna with a 1.2 m reflector to direct Ku band spot beams, a dual core bent heat pipe for thermal control, high efficiency multi-junction solar cells and an improved thruster configuration for optimised propellant use for orbit and orientation maintenance. The satellite used radiatively cooled Ku-band Travelling Wave Tube Amplifiers and a dielectrically loaded C-band demultiplexer for its communication payloads. Edusat carried five Ku-band transponders providing spot beams, one Ku-band transponder providing a national beam and six Extended C-band transponders with a national coverage beam. It was to join the Insat system that already provided more than 130 transponders in C-band, Extended C-band and Ku-band for a variety of telecommunication and television services.
First operational flight of launch vehicle. Launch delayed from July, August and September 10. Dry mass 820 kg. As of 2007 Mar 9 located at 73.92E drifting at 0.006W degrees per day.
2005 April 8 - . 05:56 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300 Mk II.
2005 April 8 - . 06:30 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
2005 May 5 - . 04:44 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: PSLV.
- CartoSat 1 - .
Payload: IRS-P5. Mass: 1,560 kg (3,430 lb). Nation: India.
Agency: ISRO.
Spacecraft: IRS.
USAF Sat Cat: 28649 . COSPAR: 2005-017A. Apogee: 623 km (387 mi). Perigee: 620 km (380 mi). Inclination: 97.90 deg. Period: 97.10 min.
First launch from new second PSLV pad at Sriharikota. Eleventh satellite in the Indian Remote Sensing satellite series, Cartosat-1 carried two panchromatic cameras, one fore-mounted with a tilt of +26 deg and the other aft-mounted with a tilt of -5 deg from the yaw axis. Together they provided black-and-white stereoscopic pictures in the visible region ( 0.50-0.85 micron) of the electromagnetic spectrum with a spatial resolution of 2.5 metre. The cameras covered a swath of 30 km and a solid state memory recorded up to 120 GB of images for downloading when the satellite passed over the Spacecraft Control Centre at Bangalore or ISTRAC stations at Lucknow, Mauritius, Bears Lake in Russia and Biak in Indonesia. Cartosat 1's sun-synchronous orbit crossed the equator at a local time of 10:30. The spacecraft was 3-axis stabilised using reaction wheels, magnetic torquers and hydrazine thrusters. 1100 W of eectrical power was provided by a 5 sq m solar array and two 24 Ah Ni-Cd batteries. Mission life was 5 years. Launch delayed from February, late April. The multispectral satellite had a 2.5-meter resolution camera.
- VUSat - .
Payload: IHamsat. Mass: 42 kg (92 lb). Nation: India.
Agency: AmSat.
Class: Communications.
Type: Amateur radio communications satellite. Spacecraft: Oscar.
USAF Sat Cat: 28650 . COSPAR: 2005-017B. Apogee: 646 km (401 mi). Perigee: 607 km (377 mi). Inclination: 97.90 deg. Period: 97.20 min.
Microsatellite providing satellite-based Amateur Radio services to the international community of Amateur Radio Operators (HAMs). Primarily intended for HAM operators in South Asia. One of the transponders was developed by Indian amateurs with the assistance of ISRO, and the second by a student at the Higher Technical Institute, Venlo, Netherlands. Hamsat was a 630 mm x 630 mm x 550 mm cube of aluminium-honeycomb structure. Power was provided by body-mounted gallium arsenide solar panels and a lithium ion battery. The satellite was spin-stabilised at 4 rpm. Uplink/downlink frequencies were 435.25 MHz / 145.9 MHz.
2005 May 20 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-300 Mk II.
2006 July 10 - . 12:08 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: GSLV. FAILURE: One of the liquid-fueled strap-on motors failed to develop thrust. By 40 seconds after launch the GSLV had veered outside of the launch corridor and the destruct signal was sent.. Failed Stage: 0.
- Insat 4C - . Mass: 2,168 kg (4,779 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-2K.
2007 January 10 - . 04:16 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- SRE-1 - .
Mass: 550 kg (1,210 lb). Nation: India.
Agency: ISRO.
Class: Technology.
Type: Re-entry test vehicle. Spacecraft: SRE.
Decay Date: 2007-01-22 . USAF Sat Cat: 29711 . COSPAR: 2007-001C. Apogee: 643 km (399 mi). Perigee: 620 km (380 mi). Inclination: 97.90 deg. Period: 97.40 min.
India's Space Recovery Experiment-1 India's SRE-1 first lowered to its orbit to 485 km x 643 km on January 20. A 10-minute deorbit burn began at 03:30 GMT on January 22, with re-entry beginning at 04:07 and a successful splashdown at 04:16 GMT in the Bay of Bengal near 13.3 N / 81.4E. The capsule was successfully recovered by the Indian Navy. The capsule returned two microgravity payloads as well as proving basic technologies for any eventual Indian manned space program. It was also announced that the capsule could be used to orbit further microgravity payloads at low cost to customers.
- LAPAN Tubsat - . Mass: 56 kg (123 lb). Nation: Indonesia. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Tubsat. USAF Sat Cat: 29709 . COSPAR: 2007-001A. Apogee: 638 km (396 mi). Perigee: 620 km (380 mi). Inclination: 97.90 deg. Period: 97.30 min. Experimental satellite developed with assistance from TUB (Berlin Technical University. It carried a 5-meter-resolution surveillance camera..
- Cartosat-2 - .
Mass: 680 kg (1,490 lb). Nation: India.
Agency: ISRO.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft: IRS.
USAF Sat Cat: 29710 . COSPAR: 2007-001B. Apogee: 644 km (400 mi). Perigee: 629 km (390 mi). Inclination: 98.00 deg. Period: 97.40 min.
The satellite was the twelfth in the Indian Remote Sensing satellite series and was capable of providing scene-specific spot imagery. The panchromatic camera provided imagery with a spatial resolution of better than one metre and a swath of 9.6 km. Data from the satellite was to be used for detailed mapping.
- Pehuensat - . Mass: 6.00 kg (13.20 lb). Nation: Argentina. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Pehuensat. USAF Sat Cat: 29712 . COSPAR: 2007-001D. Apogee: 641 km (398 mi). Perigee: 621 km (385 mi). Inclination: 97.90 deg. Period: 97.30 min. Experimental satellite developed by the Universidad Nacional del Comahue and AMSAT-LU. The satellte remained attached to the PSLV's Dual Launch Adapter..
2007 April 23 - . 10:00 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: PSLV.
- AGILE - .
Mass: 352 kg (776 lb). Nation: Italy.
Agency: ASI.
Manufacturer: Carlo Gavazzi.
Class: Astronomy.
Type: X-ray astronomy satellite. Spacecraft Bus: MITA.
Spacecraft: AGILE.
USAF Sat Cat: 31135 . COSPAR: 2007-013A. Apogee: 553 km (343 mi). Perigee: 523 km (324 mi). Inclination: 2.50 deg. Period: 95.40 min.
The PSLV-C8 launch vehicle flew for the first time in a light configuration with no strap-on motors and a Dual Launch Adapter. The Italian gamma-ray observatory satellite (Astrorivelatore Gamma ad Imagini Leggero) carried the GRID 0.3-200 MeV wide-field gamma ray camera and the Super-AGILE 15-45 keV detector hard X-ray detector.
- AAM - . Mass: 185 kg (407 lb). Nation: India. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: AAM. USAF Sat Cat: 31136 . COSPAR: 2007-013B. Apogee: 549 km (341 mi). Perigee: 531 km (329 mi). Inclination: 2.50 deg. Period: 95.50 min. The Dual Launch Adapter housed the secondary payload, an Advanced Avionics Module for future use on Indian launch vehicles. The AAM remained attached to the PSLV fourth stage..
2007 September 2 - . 12:50 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: GSLV.
- Insat 4CR - . Mass: 2,130 kg (4,690 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-2K. USAF Sat Cat: 32050 . COSPAR: 2007-037A. Apogee: 35,790 km (22,230 mi). Perigee: 35,221 km (21,885 mi). Inclination: 0.10 deg. Period: 421.80 min. Ku-band television satellite..
2008 January 20 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200SV.
2008 January 20 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200SV.
2008 April 28 - . 03:53 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: PSLV.
- Cartosat 2A - . Mass: 768 kg (1,693 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Military Radarsat. Spacecraft: IRS. USAF Sat Cat: 32783 . COSPAR: 2008-021A. Apogee: 645 km (400 mi). Perigee: 623 km (387 mi). Inclination: 98.00 deg. Period: 97.40 min. Primary payload, an imaging satellite with a spatial resolution of better than one metre and a swath of 9.6 km. Data from the satellite was to be used for detailed mapping..
- Can X-6 - . Nation: Canada. Agency: ISRO. Class: Communications. Type: Military communications satellite. Spacecraft: Can X. USAF Sat Cat: 32784 . COSPAR: 2008-021B. Apogee: 638 km (396 mi). Perigee: 615 km (382 mi). Inclination: 98.00 deg. Period: 97.20 min. Nanosat built by University of Toronto Institiute of Aerospace Studies and Com Dev International; carried a payload for relaying identification beacon data from shipping..
- Cute-1.7-APD-II - . Mass: 4.00 kg (8.80 lb). Nation: Japan. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 32785 . COSPAR: 2008-021C. Apogee: 635 km (394 mi). Perigee: 615 km (382 mi). Inclination: 98.00 deg. Period: 97.20 min. 2U cubesat for Tokyo Institute of Technology. Separation system demonstration and Avalanche Photo Diode sensor experiment. Successful..
- IMS 1 - . Mass: 60 kg (132 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Military Radarsat. Spacecraft: IMS. USAF Sat Cat: 32786 . COSPAR: 2008-021D. Apogee: 638 km (396 mi). Perigee: 620 km (380 mi). Inclination: 98.00 deg. Period: 97.30 min. Indian Mini Satellite, a small imaging satellite..
- Compass 1 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 32787 . COSPAR: 2008-021E. Apogee: 636 km (395 mi). Perigee: 614 km (381 mi). Inclination: 98.00 deg. Period: 97.20 min. 1U cubesat for Fachhochschule Aachen nanosat. Demonstration of commercial off-the-shelf components and taking photos. Successful..
- AAUSat-II - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Agency: ISRO. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: Cubesat. USAF Sat Cat: 32788 . COSPAR: 2008-021F. Apogee: 636 km (395 mi). Perigee: 614 km (381 mi). Inclination: 98.00 deg. Period: 97.20 min. University of Aalborg 1U cubesat; carried a gamma ray burst detector for the Danish National Space Center. Successful..
- Delfi-C3 - . Mass: 5.00 kg (11.00 lb). Nation: Netherlands. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 32789 . COSPAR: 2008-021G. Apogee: 636 km (395 mi). Perigee: 614 km (381 mi). Inclination: 98.00 deg. Period: 97.20 min. Technical University of Delft 3U cubesat. On-orbit testing of thin film solar cells (TFSC) and autonomous wireless sun sensor (AWSS). Demonstrated the world's first linear amateur radio transponder on a CubeSat..
- Can X-2 - . Mass: 2.00 kg (4.40 lb). Nation: Canada. Agency: ISRO. Class: Communications. Type: Military communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 32790 . COSPAR: 2008-021H. Apogee: 635 km (394 mi). Perigee: 615 km (382 mi). Inclination: 98.00 deg. Period: 97.20 min. 3U cubesat for University of Toronto, Canada. Mission: Technology demonstrator for formation flying. Successful..
- SEEDS 2 - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 32791 . COSPAR: 2008-021J. Apogee: 637 km (395 mi). Perigee: 614 km (381 mi). Inclination: 98.00 deg. Period: 97.20 min. 1U cubesat for Nihon University, Japan. Amateur radio experiments and preprogrammed message sending. Successful..
- Rubin-8-AIS - . Nation: India. Agency: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 32792 . COSPAR: 2008-021K. Apogee: 662 km (411 mi). Perigee: 619 km (384 mi). Inclination: 97.90 deg. Period: 97.50 min. Remained attached to PSLV final stage; carried a payload for relaying identification beacon data from shipping..
2008 October 22 - . 00:52 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- Chandraayan-1 - .
Mass: 1,380 kg (3,040 lb). Nation: India.
Agency: ISRO.
Class: Moon.
Type: Lunar probe. Spacecraft: Chandraayan.
USAF Sat Cat: 33405 . COSPAR: 2008-052A. Apogee: 22,817 km (14,177 mi). Perigee: 225 km (139 mi). Inclination: 17.80 deg. Period: 403.00 min.
India's first lunar probe. Placed by the PSLV into indicated orbit. It then used its own engines for translunar injection. It entered an initial lunar orbit of 504 km x 7502 km x 90.0 deg on November 8, maneuvering to the planned 100 x 100 km orbit by November 12.
- MIP - .
Mass: 29 kg (63 lb). Nation: India.
Agency: ISRO.
Class: Moon.
Type: Lunar probe. Spacecraft: MIP.
USAF Sat Cat: 33406 . COSPAR: 2008-052B. Apogee: 23,095 km (14,350 mi). Perigee: 277 km (172 mi). Inclination: 17.80 deg. Period: 402.70 min.
Moon Impact Probe, released from Chandraayan-1 in lunar orbit on November 14 at 14:36 GMT. The MIP fired its own deorbit motor and impacted the moon at 15:01 GMT, near the Shackleton Crater at the south pole. The impact plume was scanned by the Chandraayan-1 orbiter and ground-based telescopes for evidence of lunar polar ice.
2009 April 20 - . 01:15 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: PSLV.
- Risat-2 - . Mass: 340 kg (740 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Military Radarsat. Spacecraft: Tecsar. USAF Sat Cat: 34807 . COSPAR: 2009-019A. Apogee: 552 km (342 mi). Perigee: 446 km (277 mi). Inclination: 41.20 deg. Period: 94.60 min. Tecsar-class radar imaging satellite bought by India from Israel..
- Anusat - . Mass: 40 kg (88 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: Anusat. Decay Date: 2012-04-18 . USAF Sat Cat: 34808 . COSPAR: 2009-019B. Apogee: 551 km (342 mi). Perigee: 401 km (249 mi). Inclination: 41.20 deg. Period: 94.10 min. 40 kg imaging satellite from Anna University, Chennai, India..
2009 September 23 - . 06:21 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- Oceansat-2 - . Mass: 1,000 kg (2,200 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: IRS. Spacecraft: Oceansat. USAF Sat Cat: 35931 . COSPAR: 2009-051A. Apogee: 726 km (451 mi). Perigee: 720 km (440 mi). Inclination: 98.30 deg. Period: 99.20 min. Remote sensing satellite with an 8-band ocean color monitor, a radar scatterometer and a radio occultation atmospheric sounder..
- SwissCube - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Science. Type: Science satellite. Spacecraft: Cubesat. USAF Sat Cat: 35932 . COSPAR: 2009-051B. Apogee: 712 km (442 mi). Perigee: 702 km (436 mi). Inclination: 98.43 deg. Period: 98.93 min. Cubesat from Ecole Polytechnique Federale de Lausanne, Switzerland.
- BEESAT - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 35933 . COSPAR: 2009-051C. Apogee: 710 km (440 mi). Perigee: 703 km (436 mi). Inclination: 98.43 deg. Period: 98.92 min. Cubesat from Technische Universitat Berlin, Germany..
- UWE-2 - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 35934 . COSPAR: 2009-051D. Apogee: 712 km (442 mi). Perigee: 704 km (437 mi). Inclination: 98.42 deg. Period: 98.95 min. 1U cubesat from Julius-Maximilians-Universitat Wurzburg, Germany. ADCS technology demonstrator. Successful..
- ITU-p-SAT 1 - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 35935 . COSPAR: 2009-051E. Apogee: 715 km (444 mi). Perigee: 704 km (437 mi). Inclination: 98.44 deg. Period: 98.97 min. Cubesat from Istanbul Teknik Universitesi..
- Rubin-9.1 - . Nation: India. Agency: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 35936 . COSPAR: 2009-051F. Apogee: 795 km (493 mi). Perigee: 715 km (444 mi). Inclination: 98.30 deg. Period: 99.90 min. Maritime communications package which remained attached to the PSLV final stage..
- Rubin-9.2 - . Nation: India. Agency: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 35936 . COSPAR: 2009-051F. Apogee: 795 km (493 mi). Perigee: 715 km (444 mi). Inclination: 98.30 deg. Period: 99.90 min. Maritime communications package which remained attached to the PSLV final stage..
2010 January 14 - . 07:45 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560/300 Mk II.
2010 January 15 - . 07:45 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560/300 Mk II.
2010 March 3 - . 03:00 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560.
- ATV-DO1 Scramjet - .
Nation: India.
Agency: ISRO.
Apogee: 46 km (28 mi).
The booster accelerated the passive scramjet to Mach 6 and sustained Mach 6 +.05 and dynamic pressure (80 + 35 kPa) for seven seconds. These conditions were required for a stable ignition of an active scramjet engine combustor module, planned in the flight of ATV-D2.
2010 April 15 - . 10:57 GMT - . Launch Site: Sriharikota. LV Family: GSLV. Launch Vehicle: GSLV Mk II. FAILURE: Third stage failure..
- Gsat 4 - . Nation: India. Agency: ISRO. Class: Communications. Type: Communications satellite. Spacecraft: I-2K. Failed to orbit due to third stage failure. Ka-band communications satellite with a GPS-augmentation navigation transmitter..
2010 July 12 - . 03:52 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- Cartosat 2B - . Mass: 694 kg (1,530 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Cartographic satellite. Spacecraft: IRS. USAF Sat Cat: 36795 . COSPAR: 2010-035A. Apogee: 647 km (402 mi). Perigee: 629 km (390 mi). Inclination: 98.10 deg. Period: 97.50 min. Cartography satellite with 0.8 meter resolution..
- Studsat - . Mass: 1.00 kg (2.20 lb). Nation: India. Agency: ISRO. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 36796 . COSPAR: 2010-035B. Apogee: 640 km (390 mi). Perigee: 621 km (385 mi). Inclination: 98.20 deg. Period: 97.30 min. ISRO-sponsored Indian student-designed 1U cubesat. First Indian picosatellite..
- Aissat 1 - . Mass: 6.00 kg (13.20 lb). Nation: Norway. Agency: ISRO. Program: AIS. Class: Navigation. Type: Navigation satellite. Spacecraft: Toronto GNB. USAF Sat Cat: 36797 . COSPAR: 2010-035C. Apogee: 636 km (395 mi). Perigee: 620 km (380 mi). Inclination: 98.20 deg. Period: 97.30 min. Satellite-based Automatic Identification System (AIS) payload to track maritime assets worldwide (all vessels over 300 metric tons are equipped with AIS transponders)..
- Alsat 2A - . Mass: 116 kg (255 lb). Nation: Algeria. Agency: ISRO. Program: Alsat. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 36798 . COSPAR: 2010-035D. Apogee: 674 km (418 mi). Perigee: 672 km (417 mi). Inclination: 98.20 deg. Period: 98.20 min. Optical surveillance satellite with 2.5 meter panchromatic resolution and 10 meter in 4 band/multispectral mode..
- Tisat 1 - . Mass: 1.00 kg (2.20 lb). Nation: Switzerland. Agency: ISRO. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 36799 . COSPAR: 2010-035E. Apogee: 639 km (397 mi). Perigee: 619 km (384 mi). Inclination: 98.20 deg. Period: 97.30 min. Swiss student 1U cubesat for SUPSI. Successful..
2010 December 25 - . 10:34 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: GSLV. FAILURE: Destroyed at T+60 seconds after guidance commands from on-board computer to steering system of strapon boosters were cut off.. Failed Stage: 0.
- Gsat 5P - . Mass: 2,310 kg (5,090 lb). Nation: India. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-2K. Vehicle reached only 15 km. First use of stretched cryogenic third state. Gsat-5P communications satellite destroyed..
2011 April 20 - . 04:42 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- Resourcesat 2 - .
Mass: 1,200 kg (2,600 lb). Nation: India.
Program: IRS.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: IRS.
USAF Sat Cat: 37387 . COSPAR: 2011-015A. Apogee: 825 km (512 mi). Perigee: 820 km (500 mi). Inclination: 98.80 deg. Period: 101.30 min.
Surveillance satellite. Carried the LISS-4 camera, a 6-meter-resolution imager, which was to be used for both military reconnaissance and civilian remote sensing. It also carried the lower resolution LISS-3 (23 m resolution) and AWIFS (56 m resolution), and an AIS Automatic Identification System payload for Comdev of Canada for tracking ships at sea.
- Youthsat - . Mass: 92 kg (202 lb). Nation: India. Class: Science. Type: Science satellite. Spacecraft: Youthsat. USAF Sat Cat: 37388 . COSPAR: 2011-015B. Apogee: 823 km (511 mi). Perigee: 803 km (498 mi). Inclination: 98.80 deg. Period: 101.20 min. Joint Indian-Russian student satellite. Carried experiments to study solar-terrestrial relationships..
- X-Sat - . Mass: 105 kg (231 lb). Nation: India. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: SI-100. Spacecraft: X-Sat. USAF Sat Cat: 37389 . COSPAR: 2011-015C. Apogee: 822 km (510 mi). Perigee: 803 km (498 mi). Inclination: 98.80 deg. Period: 101.10 min. Nanyang Technological University Singapore satellite; carried a 10-meter-resolution multispectral imager..
2011 July 15 - . 11:18 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- GSAT-12 - . Mass: 1,410 kg (3,100 lb). Nation: India. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-1K. USAF Sat Cat: 37746 . COSPAR: 2011-034A. Apogee: 35,806 km (22,248 mi). Perigee: 35,768 km (22,225 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Communications satellite; used on-board propellant to reach geosynchronous position..
2011 October 12 - . 05:31 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- Megha-Tropique - . Mass: 1,000 kg (2,200 lb). Nation: India. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 37838 . COSPAR: 2011-058A. Apogee: 868 km (539 mi). Perigee: 853 km (530 mi). Inclination: 20.00 deg. Period: 102.20 min. Joint Indian-French remote sensing satellite; carried a MADRAS microwave imager, a Saphir water vapor profile instrument, and a ScaRaB radiation budget scanner..
- JUGNU - . Mass: 10 kg (22 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 37839 . COSPAR: 2011-058B. Apogee: 866 km (538 mi). Perigee: 839 km (521 mi). Inclination: 20.00 deg. Period: 102.00 min. 3U cubesat for the Indian Institute of Technology in Kanpur. Micro-imaging system, near infrared camera to observe vegetation, and GPS Receiver to aid tracking. Successful..
- Vesselsat 1 - . Mass: 29 kg (63 lb). Nation: Luxembourg. Class: Technology. Type: Technology satellite. Spacecraft: Vesselsat. USAF Sat Cat: 37840 . COSPAR: 2011-058C. Apogee: 868 km (539 mi). Perigee: 847 km (526 mi). Inclination: 20.00 deg. Period: 102.10 min. OHB LuxSpace of Luxembourg satllite to provide AIS (ship tracking) services for Orbcomm..
- SRMSAT - . Mass: 10 kg (22 lb). Nation: India. Class: Earth. Type: Climate satellite. Spacecraft: SRMSAT. USAF Sat Cat: 37841 . COSPAR: 2011-058D. Apogee: 868 km (539 mi). Perigee: 850 km (520 mi). Inclination: 20.00 deg. Period: 102.10 min. SRM University in Chennai satellite for greenhouse gas monitoring..
2012 April 26 - . 00:17 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- RISAT-1 - . Mass: 1,858 kg (4,096 lb). Nation: India. Class: Surveillance. Type: Civilian Radarsat. Spacecraft: IRS. USAF Sat Cat: 38248 . COSPAR: 2012-017A. Apogee: 550 km (340 mi). Perigee: 529 km (328 mi). Inclination: 97.60 deg. Period: 95.40 min. Radar Imaging Satellite with a C-band synthetic aperture radar payload mounted on an IRS- derived bus..
2012 September 9 - . 04:23 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Pad: LP1. Launch Vehicle: PSLV.
- Spot 6 - . Mass: 712 kg (1,569 lb). Nation: France. Class: Earth. Type: Earth resources satellite. Spacecraft: Astrobus. USAF Sat Cat: 38755 . COSPAR: 2012-047A. Apogee: 699 km (434 mi). Perigee: 697 km (433 mi). Inclination: 98.20 deg. Period: 98.70 min. Earth observing satellite built by Astrium/Toulouse for Astrium subsidiary Spot Image (Toulouse)..
- Proiteres - . Mass: 15 kg (33 lb). Nation: Japan. Class: Technology. Type: Ion engine technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 38756 . COSPAR: 2012-047B. Apogee: 657 km (408 mi). Perigee: 640 km (390 mi). Inclination: 98.30 deg. Period: 97.70 min. 15 kg pulsed plasma thruster experiment: 'Project of Osaka Institute of Technology Electric Rocket Engine aboard small Spaceship'..
2013 February 25 - . 12:31 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- AAUSAT3 - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Class: Navigation. Type: Navigation satellite. Spacecraft: Cubesat. USAF Sat Cat: 39087 . COSPAR: 2013-009B. Apogee: 787 km (489 mi). Perigee: 770 km (470 mi). Inclination: 98.63 deg. Period: 100.41 min. 2U cubesat built by Aalborg University in Denmark; carried a double AIS ship tracking receiver and a GPS receiver for tracking ships in Arctic regions. Successful..
- NEOSSat - . Mass: 65 kg (143 lb). Nation: Canada. Class: Astronomy. Type: Astronomy satellite. Spacecraft: Multi-Mission Microsatellite Bus. USAF Sat Cat: 39089 . COSPAR: 2013-009D. Apogee: 786 km (488 mi). Perigee: 771 km (479 mi). Inclination: 98.63 deg. Period: 100.43 min. Near Earth Object Surveillance Satellite, joint Canadian Space Agency/DRDC mission to survey asteroids and space debris, also with a 0.15m telescope..
- STRaND-1 - . Mass: 4.00 kg (8.80 lb). Nation: UK. Agency: Surrey. Manufacturer: Surrey. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39090 . COSPAR: 2013-009E. Apogee: 783 km (486 mi). Perigee: 771 km (479 mi). Inclination: 98.63 deg. Period: 100.40 min. 3U cubesat, a technical test project of Surrey Satellite and the Surrey Space Centre. Carried a Google Nexus One smartphone as its main avionics, and featured plasma thrusters and a water-alcohol thruster. Successful; first in STRaND Program..
- TUGSAT-1 - . Payload: BRITE-A. Mass: 10 kg (22 lb). Nation: Austria. Class: Astronomy. Type: Astronomy satellite. Spacecraft: Toronto GNB. USAF Sat Cat: 39091 . COSPAR: 2013-009F. Apogee: 784 km (487 mi). Perigee: 770 km (470 mi). Inclination: 98.63 deg. Period: 100.38 min. Satellite based on the Toronto Generic Nanosatellite Bus, built by the Technical University of Graz, Austra with help from UTIAS. Carried an 0.03m telescope-photometer for stellar photometry and astroseismology..
- UniBRITE - . Payload: BRITE-U. Mass: 10 kg (22 lb). Nation: Austria. Class: Astronomy. Type: Astronomy satellite. Spacecraft: Toronto GNB. USAF Sat Cat: 39092 . COSPAR: 2013-009G. Apogee: 783 km (486 mi). Perigee: 771 km (479 mi). Inclination: 98.63 deg. Period: 100.39 min. Nanosatellite built by UTIAS for the University of Vienna, Austria. Carried an 0.03m telescope-photometer for stellar photometry and astroseismology..
2013 July 1 - . 18:11 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Pad: LP1. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-1A - . Mass: 1,425 kg (3,141 lb). Nation: India. Class: Navigation. Type: Navigation satellite. Spacecraft: I-1K. USAF Sat Cat: 39199 . COSPAR: 2013-034A. Apogee: 35,866 km (22,286 mi). Perigee: 35,706 km (22,186 mi). Inclination: 27.35 deg. Period: 1,436.06 min. First Indian operational navigation satellite, beginning the Indian Regional Navigation Satellite System. Provides L-band and S-band navigation signals..
2013 November 5 - . 09:08 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Pad: xxx. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- Mars Orbiter Spacecraft - .
Mass: 1,350 kg (2,970 lb). Nation: India.
Class: Mars.
Type: Mars probe. Spacecraft: Chandrayaan.
USAF Sat Cat: 39370 . COSPAR: 2013-060A.
First Indian mission to Mars. Carried 15 kg of instruments, including a color camera, but primary purpose was to test technologies for future planetary missions. Carried 850 kg of propellant for trans-Mars ejection and insertion into Martian orbit on arrival there. The MOS was inserted in elliptical Earth orbit; it used its own propulsion to achieve trans-Mars injection. The fourth stage and MOM payload entered a 251 x 23,892 km x 19.4 deg orbit with first perigee over the South Pacific. On November 7 the orbit was raised to 259 x 28,726 km, and on November 8 to over 70,000 km apogee. A further burn on November 10 delivered only 35 m/s, raising the apogee less than planned. A makeup burn on November 11 fixed the problem, and a burn on November 15 put the spacecraft in a 853 x 194,683 km x 19.4 deg orbit. A final perigee burn at 19:19 GMT on November 30 accelerated MOM to a hyperbolic Earth escape trajectory, and it entered an 0.98 x 1.45 AU solar orbit on December 3 on the way to Mars.
2014 January 5 - . 10:48 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: GSLV. Launch Vehicle: GSLV Mk II.
- GSAT-14 - .
Mass: 1,982 kg (4,369 lb). Nation: India.
Class: Communications.
Type: Communications satellite. Spacecraft: I-2K.
USAF Sat Cat: 39498 . COSPAR: 2014-001A. Apogee: 35,789 km (22,238 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.0800 deg. Period: 1,436.09 min.
Carried C and Ku band communications payloads, and Ka-band beacons for a propagation study. The launch vehicle put the satellite in an initial 182 km x 35,755 km x 19.4 deg geostationary transfer orbit. By January 7 its onboard apogee engine had placed it in a 32,543 x 35,741 km x 0.7 deg subsynchronous orbit on the way to GEO. By February 4 it was on station at 73.9 deg E.
2014 April 4 - . 11:44 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Pad: PSLV. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-1B - .
Mass: 1,425 kg (3,141 lb). Nation: India.
Class: Navigation.
Type: Navigation satellite. Spacecraft: I-1K.
USAF Sat Cat: 39635 . COSPAR: 2014-017A. Apogee: 35,883 km (22,296 mi). Perigee: 35,688 km (22,175 mi). Inclination: 30.89 deg. Period: 1,436.03 min.
Second dedicated navigation satellite for the Indian Regional Navigation Satellite System. After a coast phase the fourth stage ignited to accelerate the vehicle to a 269 x 20,558 km x 19.3 deg transfer orbit. IRNSS-1B used its onboard engine to join IRNSS-1A in circular inclined geosynchronous orbit, and on April 17 was in a 35,565 x 35,878 km x 31.0 deg orbit over the Indian Ocean.
2014 June 30 - . 04:22 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- Spot 7 - . Payload: AstroSat-500 Mk.2 (AstroBus-L). Mass: 712 kg (1,569 lb). Nation: France. Spacecraft: Astrobus. USAF Sat Cat: 40053 . COSPAR: 2014-034A. Apogee: 699 km (434 mi). Perigee: 697 km (433 mi). Inclination: 98.20 deg. Period: 98.73 min. Earth observation satellite with a 2 meter resolution on a 60 kilometer swath..
- Aisat - . Mass: 14 kg (30 lb). Nation: Germany. Spacecraft: Aisat. USAF Sat Cat: 40054 . COSPAR: 2014-034B. Apogee: 663 km (411 mi). Perigee: 639 km (397 mi). Inclination: 98.25 deg. Period: 97.75 min. DLR satellite with experimental Automatic Identification System (AIS) for tracking ships..
- NLS 7.1/Canx 4 - . Mass: 15 kg (33 lb). Nation: Canada. Spacecraft: Toronto GNB. USAF Sat Cat: 40055 . COSPAR: 2014-034C. Apogee: 661 km (410 mi). Perigee: 639 km (397 mi). Inclination: 98.25 deg. Period: 97.73 min. Univeristy of Toronto demonstration of on-orbit formation flying using differential GPS..
- NLS 7.2/Canx 5 - . Mass: 15 kg (33 lb). Nation: Canada. Spacecraft: Toronto GNB. USAF Sat Cat: 40056 . COSPAR: 2014-034D. Apogee: 662 km (411 mi). Perigee: 639 km (397 mi). Inclination: 98.25 deg. Period: 97.73 min.
- Velox 1 - . Mass: 4.00 kg (8.80 lb). Nation: Singapore. Spacecraft: Cubesat. USAF Sat Cat: 40057 . COSPAR: 2014-034E. Apogee: 658 km (408 mi). Perigee: 639 km (397 mi). Inclination: 98.25 deg. Period: 97.69 min. 3u cubesat by Singapore National Technical University; to have deployed the Velox P3 subsatellite..
2014 October 15 - . 20:02 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Pad: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-1C - . Mass: 1,425 kg (3,141 lb). Nation: India. Class: Navigation. Type: Navigation satellite. Spacecraft: I-1K. USAF Sat Cat: 40269 . COSPAR: 2014-061A. Apogee: 35,879 km (22,294 mi). Perigee: 35,696 km (22,180 mi). Inclination: 4.17 deg. Period: 1,436.14 min. India's third dedicated navigation satellite. Stationed in geosynchronous orbit at 83 deg east..
2014 December 18 - . 04:00 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Pad: Srikarikota SLP. LV Family: GSLV. Launch Vehicle: GSLV-3.
- CARE/LVM3-X - .
Mass: 3,735 kg (8,234 lb). Nation: India.
Class: Manned.
Type: Manned spacecraft. Spacecraft: Indian Manned Spacecraft.
Apogee: 126 km (78 mi).
Launch of the first GSLV-III rocket on a suborbital test flight. The S200 solid boosters and L110 core stage, with two Vikas engines, propelled an inert second stage to 126 km and 5.3 km/s. Second stage separation and payload separation were also tested; the payload was the Crew Module Atmospheric Reentry Experiment, a prototype command module for an Indian manned spacecraft with a mass of 3735 kg which splashed down in the Bay of Bengal. Orbit was around -4418 x 126 km x 32.7 deg.
2015 March 28 - . 11:49 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-1D - . Mass: 1,425 kg (3,141 lb). Nation: India. Class: Navigation. Type: Navigation satellite. Spacecraft: I-1K. USAF Sat Cat: 40547 . COSPAR: 2015-018A. Apogee: 35,869 km (22,287 mi). Perigee: 35,707 km (22,187 mi). Inclination: 30.11 deg. Period: 1,436.18 min. Fourth Indian Regional Navigation Satellite System satellite; joined its siblings IRNSS-1A and 1B in inclined synchronous orbit..
2015 July 10 - . 16:28 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Pad: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- DMC3-1 - .
Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft: SSTL-300.
USAF Sat Cat: 40715 . COSPAR: 2015-032A. Apogee: 660 km (410 mi). Perigee: 638 km (396 mi). Inclination: 98.04 deg. Period: 97.71 min.
Third generation Disaster Monitoring Constellation. The three satellites were deployed on a single launch. DMC Imaging International was a Surrey Satellite spinoff which operated the DMC imaging satellites in collaboration with several developing countries. The satellites have the capability to return prompt imaging of areas in those countries affected by natural disasters. The SSTL-300S1 platform provided 45 degree fast slew off-pointing and was capable of acquiring multiple targets in one pass using multiple viewing modes. The high resolution imager on board the satellites was designed and manufactured by SSTL and provided 1 meter resolution in panchromatic mode, and 4 meter resolution in multispectral mode, with a swath width of 23.4km. The three satellites were phased 120 degrees apart around the same sun synchronous orbit with a 22:10 local time longitude of descending node sun synchronous orbit. This was acommplished using their on board propulsion systems in the three months after the launch. With off-pointing capability, the DMC3/TripleSat Satellite Constellation was able to target anywhere on Earth once per day.
- DMC3-2 - . Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK. Class: Surveillance. Type: Surveillance satellite. Spacecraft: SSTL-300. USAF Sat Cat: 40716 . COSPAR: 2015-032B. Apogee: 659 km (409 mi). Perigee: 640 km (390 mi). Inclination: 98.03 deg. Period: 97.71 min. 22:10 local time longitude of descending node sun synchronous orbit..
- DMC3-3 - . Payload: SSTL-300-S1. Mass: 440 kg (970 lb). Nation: UK. Class: Surveillance. Type: Surveillance satellite. Spacecraft: SSTL-300. USAF Sat Cat: 40717 . COSPAR: 2015-032C. Apogee: 662 km (411 mi). Perigee: 637 km (395 mi). Inclination: 98.10 deg. Period: 97.71 min. 22:10 local time longitude of descending node sun synchronous orbit..
- CBNT-1 - . Mass: 91 kg (200 lb). Nation: UK. Class: Surveillance. Type: Surveillance satellite. Spacecraft: CBNT. USAF Sat Cat: 40718 . COSPAR: 2015-032D. Apogee: 659 km (409 mi). Perigee: 636 km (395 mi). Inclination: 98.03 deg. Period: 97.67 min. Surrey Satellite Technology experimental imaging satellite. SSTL did not disclose the meaning of the CBNT abbreviation. 22:10 local time longitude of descending node sun synchronous orbit..
- DeOrbitSail - . Mass: 3.00 kg (6.60 lb). Nation: UK. Class: Technology. Type: Technology satellite. Spacecraft: CubeSat. USAF Sat Cat: 40719 . COSPAR: 2015-032E. Apogee: 657 km (408 mi). Perigee: 634 km (393 mi). Inclination: 98.04 deg. Period: 97.63 min. 3U cubesat. 22:10 local time longitude of descending node sun synchronous orbit..
2015 August 27 - . 11:22 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: GSLV. Launch Vehicle: GSLV Mk II.
- GSAT-6 - . Mass: 2,117 kg (4,667 lb). Nation: India. Class: Communications. Type: Communications satellite. Spacecraft: I-2K. USAF Sat Cat: 40880 . COSPAR: 2015-041A. Apogee: 35,831 km (22,264 mi). Perigee: 35,742 km (22,209 mi). Inclination: 1.03 deg. Period: 1,436.10 min. Military communications satellite with S-band and C-band payload for use by the Indian Armed Forces. Geosynchronous orbit stationed at 83E.
2015 September 28 - . 04:30 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Pad: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- Astrosat - .
Mass: 1,530 kg (3,370 lb). Nation: India.
Class: Astronomy.
Type: Astronomy satellite. Spacecraft: IRS-1.
USAF Sat Cat: 40930 . COSPAR: 2015-052A. Apogee: 650 km (400 mi). Perigee: 632 km (392 mi). Inclination: 5.99 deg. Period: 97.55 min.
India's first space astronomy observatory. The satellite carried near and far ultraviolet telescopes, a large X-ray proportional counter array, a soft-X-ray imaging telescope, a hard X-ray coded mask telescope, and a monitor to detect flaring X-ray sources.
- LAPAN-A2 - . Mass: 68 kg (149 lb). Nation: Indonesia. Class: Technology. Type: Technology satellite. Spacecraft: Tubsat. USAF Sat Cat: 40931 . COSPAR: 2015-052B. Apogee: 650 km (400 mi). Perigee: 631 km (392 mi). Inclination: 6.00 deg. Period: 97.54 min. Indonesian microsatellite; carried an AIS (Automatic Identification System) to identify ships in Indonesia waters, a video camera, and a payload for disaster management by amateur radio operators..
- Lemur-2-Joel - . Mass: 6.00 kg (13.20 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 40932 . COSPAR: 2015-052C. Apogee: 650 km (400 mi). Perigee: 629 km (390 mi). Inclination: 6.01 deg. Period: 97.51 min. Nanosatellite built by the University of Toronto's UTIAS group, part of the xactEarth AIS constellation to monitor ship movements..
- Lemur-2-Chris - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Cubesat.
USAF Sat Cat: 40933 . COSPAR: 2015-052C. Apogee: 650 km (400 mi). Perigee: 629 km (390 mi). Inclination: 6.01 deg. Period: 97.50 min.
3U cubesat by San Francisco-based Spire Global, built in Glasgow, Scotland. 3U cubesat, carried an AIS payload and GPS radio occultation equipment, which used the bending of GPS radio signals by the atmosphere to derive atmospheric temperature and pressure.
- Lemur-2-Jeroen - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Cubesat.
USAF Sat Cat: 40934 . COSPAR: 2015-052D. Apogee: 650 km (400 mi). Perigee: 634 km (393 mi). Inclination: 6.01 deg. Period: 97.55 min.
3U cubesat by San Francisco-based Spire Global, built in Glasgow, Scotland. 3U cubesat, carried an AIS payload and GPS radio occultation equipment, which used the bending of GPS radio signals by the atmosphere to derive atmospheric temperature and pressure.
- Lemur-2-Peter - .
Mass: 5.00 kg (11.00 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Cubesat.
USAF Sat Cat: 40935 . COSPAR: 2015-052F. Apogee: 650 km (400 mi). Perigee: 634 km (393 mi). Inclination: 6.01 deg. Period: 97.56 min.
3U cubesat by San Francisco-based Spire Global, built in Glasgow, Scotland. 3U cubesat, carried an AIS payload and GPS radio occultation equipment, which used the bending of GPS radio signals by the atmosphere to derive atmospheric temperature and pressure.
- ExactView-9 - .
Mass: 5.00 kg (11.00 lb). Nation: Canada.
Class: Communications.
Type: Communications satellite. Spacecraft: Cubesat.
USAF Sat Cat: 40936 . COSPAR: 2015-052G. Apogee: 650 km (400 mi). Perigee: 635 km (394 mi). Inclination: 6.00 deg. Period: 97.57 min.
3U cubesat by San Francisco-based Spire Global, built in Glasgow, Scotland. 3U cubesat, carried an AIS payload and GPS radio occultation equipment, which used the bending of GPS radio signals by the atmosphere to derive atmospheric temperature and pressure.
2015 December 16 - . 12:30 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. LV Family: PSLV. Launch Vehicle: PSLV CA.
- TeLEOS-1 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. COSPAR: 2015-077A. For AgilSpace, the 400 kg TeLEOS-1 satellite with a 1 meter resolution Earth imager. The satellite was built by Singapore Technologies Electronics, of which AgilSpace was a subsidiary..
- VELOX-C1 - . Mass: 123 kg (271 lb). Nation: USA. Class: Earth. Type: Weather satellite. COSPAR: 2015-077B. For Nanyang Technological University, the 123 kg VELOX-C1 carrying a GPS radio occultation payload for meteorology.
- Kent Ridge 1 - .
Nation: USA.
Class: Surveillance.
Type: Surveillance satellite. COSPAR: 2015-077C.
For the National University of Singapore, the 78 kg Kent Ridge 1 satellite developed using the TUBSAT LEOS-50 bus by Berlin Space Technologies, a spinoff of the old TUBSAT group at Technische Universitat Berlin. KR-1 carried two low-resoluton hyperspectral Earth imagers and a 6-meter-resolution imager.
- VELOX-II - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. COSPAR: 2015-077D. The 12 kg VELOX-II carried a space communications relay experiment to demonstrate cubesat downlink via geostationary communications satellite. VELOX-II was a 6U cubesat - only the 4th to be launched worldwide in this new larger cubesat format..
- Galassia - . Nation: USA. Class: Science. Type: Science satellite. Spacecraft: Cubesat. COSPAR: 2015-077E. A second NUS satellite was Galassia, a 2U cubesat with science payloads to measure the ionosphere and perform a quantum entanglement experiment..
- Athenoxat-1 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. COSPAR: 2015-077F. In a technology development test, the PSLV 4th stage was reignited briefly to test its ability to deliver payloads to multiple orbits. For Microsat Rapid Pte Ltd., the 3U cubesat Athenoxat-1 carried a payload to image the night side of the Earth..
2016 January 20 - . 04:01 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-1E - .
Mass: 1,425 kg (3,141 lb). Nation: USA.
Class: Navigation.
Type: Navigation satellite. Spacecraft: I-1K.
USAF Sat Cat: 41241 . COSPAR: 2016-003A. Apogee: 20,547 km (12,767 mi). Perigee: 288 km (178 mi). Inclination: 19.20 deg.
India launched its 5th navigation satellite. The PSLV-XL delivered it to a subsynchronous transfer orbit. By early February it was in an inclined synchronous orbit at 35697 x 35874 km x 28.1 deg. IRNSS-R1C was in an near-equatorial orbit at 83E; the remainder are in the 28 degree inclined orbits, with R1A and R1B over about 55E and R1D and R1E over about 112E.
2016 March 10 - . 10:31 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-1F - .
Mass: 1,425 kg (3,141 lb). Nation: USA.
Class: Navigation.
Type: Navigation satellite. Spacecraft: I-1K.
USAF Sat Cat: 41384 . COSPAR: 2016-015A. Apogee: 35,750 km (22,210 mi). Perigee: 33,349 km (20,722 mi). Inclination: 5.30 deg.
Indian Regional Navigation Satellite System was augmented by launch of the 1F satellite. The initial insertion orbit was 270 x 20649 km x 17.9 deg; an initial perigee burn to raise apogee was followed by several apogee burns towards circular inclined synchronous orbit.
2016 April 28 - . 07:20 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-1G - . Mass: 1,425 kg (3,141 lb). Nation: USA. Class: Navigation. Type: Navigation satellite. Spacecraft: I-1K. USAF Sat Cat: 41469 . COSPAR: 2016-027A. Apogee: 35,821 km (22,258 mi). Perigee: 35,741 km (22,208 mi). Inclination: 5.10 deg. Launch of the IRNSS-1G completed India's 7-satellite navigation constellation. Placed in geosynchronous orbit at 129 deg E..
2016 June 22 - . 03:55 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Vehicle: PSLV.
- Cartosat-2 Series - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41599 . COSPAR: 2016-040A. Apogee: 518 km (321 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. 0930LT SSO. Cartosat-2 series imaging satellite.
- Sathyabamasat - . Nation: USA. Class: Earth. Type: Atmosphere satellite. Spacecraft: Cubesat. USAF Sat Cat: 41600 . COSPAR: 2016-040B. Apogee: 519 km (322 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. 1.5 kg 2U cubesat for Sathyabama U. of Chennai with a greenhouse-gas IR spectrometer.
- Swayam - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41607 . COSPAR: 2016-040J. Apogee: 518 km (321 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. 1 kg 1U cubesat from COEP (College of Engineering, Pune) with technology and amateur radio payloads..
- LAPAN-A3 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41603 . COSPAR: 2016-040E. Apogee: 517 km (321 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. 120 kg imaging satellite for Indonesia's LAPAN space agency.
- BIROS - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41604 . COSPAR: 2016-040F. Apogee: 516 km (320 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. 130 kg infrared satellite to study fires, for Germany's DLR; also carried the BEESAT-4 cubesat to be ejected later..
- SkySat 2G-1 - . Payload: SkySat C1. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Skysat. USAF Sat Cat: 41601 . COSPAR: 2016-040C. Apogee: 515 km (320 mi). Perigee: 501 km (311 mi). Inclination: 97.50 deg. A 110 kg imaging satellite for TerraBella's constellation.
- M3MSat - . Nation: USA. Class: Communications. Type: Search and rescue satellite. USAF Sat Cat: 41605 . COSPAR: 2016-040G. Apogee: 515 km (320 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. M3MSat/earthView-7, an 85 kg AIS satellite for Canada's Dept of National Defense.
- Claire - . Payload: GHGSAT-D. Nation: USA. Class: Earth. Type: Atmosphere satellite. USAF Sat Cat: 41602 . COSPAR: 2016-040D. Apogee: 511 km (317 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. A 25 kg University of Toronto satellite to study greenhouse gases; built by the Toronto UTIAS-SFL team, but was owned by the Montreal-based company GHGSat Inc..
- Flock 2P-1 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41617 . COSPAR: 2016-040U. Apogee: 513 km (318 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-2 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41609 . COSPAR: 2016-040L. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-3 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41618 . COSPAR: 2016-040V. Apogee: 513 km (318 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-4 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41611 . COSPAR: 2016-040N. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-5 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41616 . COSPAR: 2016-040T. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-6 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41606 . COSPAR: 2016-040H. Apogee: 514 km (319 mi). Perigee: 500 km (310 mi). Inclination: 97.50 deg. 3U imaging cubesats for Planet (formerly PlanetLabs).
- Flock 2P-7 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41615 . COSPAR: 2016-040S. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-8 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41613 . COSPAR: 2016-040Q. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-9 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41610 . COSPAR: 2016-040M. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-10 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41612 . COSPAR: 2016-040P. Apogee: 514 km (319 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-11 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41608 . COSPAR: 2016-040K. Apogee: 513 km (318 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
- Flock 2P-12 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41614 . COSPAR: 2016-040R. Apogee: 513 km (318 mi). Perigee: 499 km (310 mi). Inclination: 97.50 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
2016 September 8 - . 11:20 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: GSLV. Launch Vehicle: GSLV Mk II.
- Insat-3DR - .
Nation: USA.
Class: Earth.
Type: Weather satellite. Spacecraft Bus: Insat 2.
Spacecraft: Insat 3.
USAF Sat Cat: 41752 . COSPAR: 2016-054A. Apogee: 35,935 km (22,328 mi). Perigee: 152 km (94 mi). Inclination: 20.60 deg.
Fourth GSLV Mk II rocket, carrying the Insat-3DR weather satellite. The cryogenic upper stage, serial CUS-07, performed nominally. The satellite made its first orbit raising burn on Sep 9. As well as weather sensors and data relay payloads, Insat-3DR carried a transponder to support search and rescue (SARSAT).
2016 September 26 - . 03:42 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Vehicle: PSLV.
- ScatSat-1 - . Nation: USA. Class: Earth. Type: Climate satellite. USAF Sat Cat: 41790 . COSPAR: 2016-059H. Apogee: 733 km (455 mi). Perigee: 717 km (445 mi). Inclination: 98.10 deg. 0915LT SSO ISRO ocean wind speed scatterometer mission..
- Pratham - .
Nation: USA.
Class: Technology.
Type: Technology satellite. USAF Sat Cat: 41783 . COSPAR: 2016-059A. Apogee: 707 km (439 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg.
India's PSLV-C35 vehicle was launched on Sep 26 with a cluster of small satellites. For the first time, the PS4 final stage made multiple burns to deliver payloads to different orbits. Its first burn reached a 718 x 732 km orbit at 0358 UTC, and ISRO's SCATSAT ocean wind speed scatterometer mission was deployed at 0359. At 0504 and 0554 UTC two more burns reached a 661 x 704 km orbit and the DLA dual launch adapter was ejected, followed by deployment of the remaining payloads. PRATHAM from IIT Bombay, with an ionospheric science instrument 0930LT SSO
- PISAT - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41784 . COSPAR: 2016-059B. Apogee: 705 km (438 mi). Perigee: 661 km (410 mi). Inclination: 98.20 deg. From PES University, Bangalore, with an 80m resolution imager 0930LT SSO.
- Pathfinder 1 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41787 . COSPAR: 2016-059E. Apogee: 703 km (436 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg. From Black Sky Global (Seattle) with a 1 meter imager 0930LT SSO.
- CanX-7 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41788 . COSPAR: 2016-059F. Apogee: 702 km (436 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg. From UTIAS/Toronto, with a deployable deorbit sail 0930LT SSO.
- ALSAT-1B - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41785 . COSPAR: 2016-059C. Apogee: 704 km (437 mi). Perigee: 661 km (410 mi). Inclination: 98.20 deg. 0930LT SSO imaging satellites for the Algerian space agency ASAL: ALSAT-1B built by Surrey.
- ALSAT-2B - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41786 . COSPAR: 2016-059D. Apogee: 673 km (418 mi). Perigee: 672 km (417 mi). Inclination: 98.20 deg. 0930LT SSO built by Airbus/Toulouse.
- ALSAT-Nano - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41789 . COSPAR: 2016-059G. Apogee: 700 km (430 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg. 0930LT SSO cubesat built by Algerian engineers in Surrey and integrated in Algeria..
2016 December 7 - . 04:54 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- Resourcesat-2A - . Nation: India. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41877 . COSPAR: 2016-074A. Apogee: 831 km (516 mi). Perigee: 814 km (505 mi). Inclination: 98.70 deg. 1030LT SSO imaging satellite to provide continuity of service for the system as 2011's Resourcesat-2 ages. The satellite has a 6 metre resolution imager..
2017 February 15 - . 03:58 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- Cartosat-2 Series/4 - .
Payload: Cartosat 2D. Nation: India.
Class: Surveillance.
Type: Surveillance satellite. USAF Sat Cat: 41948 . COSPAR: 2017-008A. Apogee: 520 km (320 mi). Perigee: 505 km (313 mi). Inclination: 97.50 deg.
See Cartosat 2D. India's PSLV placed a record 104 payloads in orbit on Feb 15, 100 of them via 25 QuadPack cubesat dispensers from the Dutch company ISISSpace. The main payload was the 714 kg `Cartosat-2 series satellite', the fourth such imaging payload from ISRO.
- INS-1A - . Nation: India. Class: Technology. Type: Technology satellite. USAF Sat Cat: 41949 . COSPAR: 2017-008B. Apogee: 508 km (315 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See INS 1A. 10 kg INS-1 (Indian Nanosatellite) technology payload..
- INS-1B - . Nation: India. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41954 . COSPAR: 2017-008G. Apogee: 507 km (315 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See INS 1B. Two 10 kg INS-1 (Indian Nanosatellite) technology payloads..
- Al-Farabi 1 - . Nation: Kazakhstan. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 42016 . COSPAR: 2017-008BW. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Al-Farabi 1. Cubesat for Al-Farabi Kazakh National University..
- PEASSS - . Nation: Netherlands. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 42015 . COSPAR: 2017-008BV. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See PEASSS. Cubesat for Dutch research lab TNO..
- BGUSat - . Nation: Israel. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41999 . COSPAR: 2017-008BD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See BGUSat. Cubesat for SpacePharma (a Swiss/Israeli company), Ben Gurion University..
- Dido-2 - . Nation: Israel. Class: Materials. Type: Materials science satellite. USAF Sat Cat: 42000 . COSPAR: 2017-008BE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See DIDO 2 (Chen Jiayong 1). ..
- Nayif-1 - . Nation: UAE. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 42017 . COSPAR: 2017-008BX. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Nayif 1 (FUNcube 5, EO 88, OSCAR 88). Cubesat for Rashid Space Center (Dubai)..
- Lemur-2-Satchmo - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41991 . COSPAR: 2017-008AV. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 24 (Lemur-2 Satchmo). ..
- Lemur-2-Mia-Grace - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41992 . COSPAR: 2017-008AW. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 27 (Lemur-2 Mia-Grace). ..
- Lemur-2-Smita-Sharad - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41993 . COSPAR: 2017-008AX. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 26 (Lemur-2 Smita-Sharad). ..
- Lemur-2-Spire-Minion - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41994 . COSPAR: 2017-008AY. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 23 (Lemur-2 Spire-Minions). ..
- Lemur-2-Rdeaton - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41995 . COSPAR: 2017-008AZ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 25 (Lemur-2 Rdeaton). ..
- Lemur-2-NoguesCorrei - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41996 . COSPAR: 2017-008BA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 28 (Lemur-2 NoguesCorreig). ..
- Lemur-2-Jopanbutra - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41997 . COSPAR: 2017-008BB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 22 (Lemur-2 Jobanputra). ..
- Lemur-2-Tachikoma - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41998 . COSPAR: 2017-008BC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 29 (Lemur-2 Tachikoma). ..
- Flock 3p-1 - . Payload: Dove 1000. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41967 . COSPAR: 2017-008V. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 1 (Dove 1000). ..
- Flock 3p-2 - . Payload: Dove 1001. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41966 . COSPAR: 2017-008U. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 2 (Dove 1001). ..
- Flock 3p-3 - . Payload: Dove 1002. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41968 . COSPAR: 2017-008W. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 3 (Dove 1002). ..
- Flock 3p-4 - . Payload: Dove 1003. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41965 . COSPAR: 2017-008T. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 4 (Dove 1003). ..
- Flock 3p-5 - . Payload: Dove 0F18. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41971 . COSPAR: 2017-008Z. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 5 (Dove 0F18). ..
- Flock 3p-6 - . Payload: Dove 0F35. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41969 . COSPAR: 2017-008X. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 6 (Dove 0F35). ..
- Flock 3p-7 - . Payload: Dove 100B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41970 . COSPAR: 2017-008Y. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 7 (Dove 100B). ..
- Flock 3p-8 - . Payload: Dove 100C. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41951 . COSPAR: 2017-008D. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 8 (Dove 100C). ..
- Flock 3p-9 - . Payload: Dove 1021. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41973 . COSPAR: 2017-008AB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 9 (Dove 1021). ..
- Flock 3p-10 - . Payload: Dove 1022. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41974 . COSPAR: 2017-008AC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 10 (Dove 1022). ..
- Flock 3p-11 - . Payload: Dove 101F. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41975 . COSPAR: 2017-008AD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 11 (Dove 101F). ..
- Flock 3p-12 - . Payload: Dove 1010. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41972 . COSPAR: 2017-008AA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 12 (Dove 1010). ..
- Flock 3p-13 - . Payload: Dove 1016. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42040 . COSPAR: 2017-008CW. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 13 (Dove 1016). ..
- Flock 3p-14 - . Payload: Dove 1018. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42012 . COSPAR: 2017-008BS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 14 (Dove 1018). ..
- Flock 3p-15 - . Payload: Dove 101D. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42039 . COSPAR: 2017-008CV. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 15 (Dove 101D). ..
- Flock 3p-16 - . Payload: Dove 100E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42011 . COSPAR: 2017-008BR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 16 (Dove 100E). ..
- Flock 3p-17 - . Payload: Dove 1023. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41962 . COSPAR: 2017-008Q. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 17 (Dove 1023). ..
- Flock 3p-18 - . Payload: Dove 102B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41957 . COSPAR: 2017-008K. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 18 (Dove 102B). ..
- Flock 3p-19 - . Payload: Dove 1024. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41955 . COSPAR: 2017-008H. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 19 (Dove 1024). ..
- Flock 3p-20 - . Payload: Dove 1029. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41950 . COSPAR: 2017-008C. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 20 (Dove 1029). ..
- Flock 3p-21 - . Payload: Dove 102A. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41959 . COSPAR: 2017-008M. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 21 (Dove 102A). ..
- Flock 3p-22 - . Payload: Dove 1028. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41958 . COSPAR: 2017-008L. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 22 (Dove 1028). ..
- Flock 3p-23 - . Payload: Dove 1025. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42018 . COSPAR: 2017-008BY. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 23 (Dove 1025). ..
- Flock 3p-24 - . Payload: Dove 1026. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41956 . COSPAR: 2017-008J. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 24 (Dove 1026). ..
- Flock 3p-25 - . Payload: Dove 102F. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41964 . COSPAR: 2017-008S. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 25 (Dove 102F). ..
- Flock 3p-26 - . Payload: Dove 102D. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41961 . COSPAR: 2017-008P. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 26 (Dove 102D). ..
- Flock 3p-27 - . Payload: Dove 1030. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41963 . COSPAR: 2017-008R. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 27 (Dove 1030). ..
- Flock 3p-28 - . Payload: Dove 102C. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41960 . COSPAR: 2017-008N. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 28 (Dove 102C). ..
- Flock 3p-29 - . Payload: Dove 1033. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42045 . COSPAR: 2017-008DB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 29 (Dove 1033). ..
- Flock 3p-30 - . Payload: Dove 102E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41987 . COSPAR: 2017-008AR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 30 (Dove 102E). ..
- Flock 3p-31 - . Payload: Dove 1032. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42049 . COSPAR: 2017-008DF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 31 (Dove 1032). ..
- Flock 3p-32 - . Payload: Dove 1035. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42023 . COSPAR: 2017-008CD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 32 (Dove 1035). ..
- Flock 3p-33 - . Payload: Dove 103C. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41990 . COSPAR: 2017-008AU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 33 (Dove 103C). ..
- Flock 3p-34 - . Payload: Dove 103B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41988 . COSPAR: 2017-008AS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 34 (Dove 103B). ..
- Flock 3p-35 - . Payload: Dove 103D. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41989 . COSPAR: 2017-008AT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 35 (Dove 103D). ..
- Flock 3p-36 - . Payload: Dove 103A. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41986 . COSPAR: 2017-008AQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 36 (Dove 103A). ..
- Flock 3p-37 - . Payload: Dove 1037. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41953 . COSPAR: 2017-008F. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 37 (Dove 1037). ..
- Flock 3p-38 - . Payload: Dove 1036. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42037 . COSPAR: 2017-008CT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 38 (Dove 1036). ..
- Flock 3p-39 - . Payload: Dove 103E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42038 . COSPAR: 2017-008CU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 39 (Dove 103E). ..
- Flock 3p-40 - . Payload: Dove 1039. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42010 . COSPAR: 2017-008BQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 40 (Dove 1039). ..
- Flock 3p-41 - . Payload: Dove 1031. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42004 . COSPAR: 2017-008BJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 41 (Dove 1031). ..
- Flock 3p-42 - . Payload: Dove 101E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42008 . COSPAR: 2017-008BN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 42 (Dove 101E). ..
- Flock 3p-43 - . Payload: Dove 1041. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42007 . COSPAR: 2017-008BM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 43 (Dove 1041). ..
- Flock 3p-44 - . Payload: Dove 1019. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42033 . COSPAR: 2017-008CP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 44 (Dove 1019). ..
- Flock 3p-45 - . Payload: Dove 101A. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42005 . COSPAR: 2017-008BK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 45 (Dove 101A). ..
- Flock 3p-46 - . Payload: Dove 1011. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42031 . COSPAR: 2017-008CM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 46 (Dove 1011). ..
- Flock 3p-47 - . Payload: Dove 1027. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42032 . COSPAR: 2017-008CN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 47 (Dove 1027). ..
- Flock 3p-48 - . Payload: Dove 1042. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42006 . COSPAR: 2017-008BL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 48 (Dove 1042). ..
- Flock 3p-49 - . Payload: Dove 1038. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42001 . COSPAR: 2017-008BF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 49 (Dove 1038). ..
- Flock 3p-50 - . Payload: Dove 1034. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42029 . COSPAR: 2017-008CK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 50 (Dove 1034). ..
- Flock 3p-51 - . Payload: Dove 1006. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41952 . COSPAR: 2017-008E. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 51 (Dove 1006). ..
- Flock 3p-52 - . Payload: Dove 1044. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42030 . COSPAR: 2017-008CL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 52 (Dove 1044). ..
- Flock 3p-53 - . Payload: Dove 1007. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42013 . COSPAR: 2017-008BT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 53 (Dove 1007). ..
- Flock 3p-54 - . Payload: Dove 1005. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42014 . COSPAR: 2017-008BU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 54 (Dove 1005). ..
- Flock 3p-55 - . Payload: Dove 1008. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42041 . COSPAR: 2017-008CX. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 55 (Dove 1008). ..
- Flock 3p-56 - . Payload: Dove 100F. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42042 . COSPAR: 2017-008CY. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 56 (Dove 100F). ..
- Flock 3p-57 - . Payload: Dove 1014. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41978 . COSPAR: 2017-008AG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 57 (Dove 1014). ..
- Flock 3p-58 - . Payload: Dove 1009. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41977 . COSPAR: 2017-008AF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 58 (Dove 1009). ..
- Flock 3p-59 - . Payload: Dove 1045. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42021 . COSPAR: 2017-008CB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 59 (Dove 1045). ..
- Flock 3p-60 - . Payload: Dove 101B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41976 . COSPAR: 2017-008AE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 60 (Dove 101B). ..
- Flock 3p-61 - . Payload: Dove 1012. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42009 . COSPAR: 2017-008BP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 61 (Dove 1012). ..
- Flock 3p-62 - . Payload: Dove 1046. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42036 . COSPAR: 2017-008CS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 62 (Dove 1046). ..
- Flock 3p-63 - . Payload: Dove 1015. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42035 . COSPAR: 2017-008CR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 63 (Dove 1015). ..
- Flock 3p-64 - . Payload: Dove 100A. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42034 . COSPAR: 2017-008CQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 64 (Dove 100A). ..
- Flock 3p-65 - . Payload: Dove 1040. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42028 . COSPAR: 2017-008CJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 65 (Dove 1040). ..
- Flock 3p-66 - . Payload: Dove 1013. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42027 . COSPAR: 2017-008CH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 66 (Dove 1013). ..
- Flock 3p-67 - . Payload: Dove 1017. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42002 . COSPAR: 2017-008BG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 67 (Dove 1017). ..
- Flock 3p-68 - . Payload: Dove 1004. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42003 . COSPAR: 2017-008BH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 68 (Dove 1004). ..
- Flock 3p-69 - . Payload: Dove 0F43. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42019 . COSPAR: 2017-008BZ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 69 (Dove 0F43). ..
- Flock 3p-70 - . Payload: Dove 0F15. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41980 . COSPAR: 2017-008AJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 70 (Dove 0F15). ..
- Flock 3p-71 - . Payload: Dove 0F11. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42051 . COSPAR: 2017-008DH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 71 (Dove 0F11). ..
- Flock 3p-72 - . Payload: Dove 0F10. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42024 . COSPAR: 2017-008CE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 72 (Dove 0F10). ..
- Flock 3p-73 - . Payload: Dove 0F1B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41981 . COSPAR: 2017-008AK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 73 (Dove 0F1B). ..
- Flock 3p-74 - . Payload: Dove 0F22. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42048 . COSPAR: 2017-008DE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 74 (Dove 0F22). ..
- Flock 3p-75 - . Payload: Dove 0F12. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41979 . COSPAR: 2017-008AH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 75 (Dove 0F12). ..
- Flock 3p-76 - . Payload: Dove 0F17. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42020 . COSPAR: 2017-008CA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 76 (Dove 0F17). ..
- Flock 3p-77 - . Payload: Dove 0F28. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42025 . COSPAR: 2017-008CF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 77 (Dove 0F28). ..
- Flock 3p-78 - . Payload: Dove 0F51. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42047 . COSPAR: 2017-008DD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 78 (Dove 0F51). ..
- Flock 3p-79 - . Payload: Dove 0F52. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41984 . COSPAR: 2017-008AN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 79 (Dove 0F52). ..
- Flock 3p-80 - . Payload: Dove 0F4E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42026 . COSPAR: 2017-008CG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 80 (Dove 0F4E). ..
- Flock 3p-81 - . Payload: Dove 0F25. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42043 . COSPAR: 2017-008CZ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 81 (Dove 0F25). ..
- Flock 3p-82 - . Payload: Dove 0F41. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42046 . COSPAR: 2017-008DC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 82 (Dove 0F41). ..
- Flock 3p-83 - . Payload: Dove 0F3F. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42050 . COSPAR: 2017-008DG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 83 (Dove 0F3F). ..
- Flock 3p-84 - . Payload: Dove 0F42. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42022 . COSPAR: 2017-008CC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 84 (Dove 0F42). ..
- Flock 3p-85 - . Payload: Dove 0F1D. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41983 . COSPAR: 2017-008AM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 85 (Dove 0F1D). ..
- Flock 3p-86 - . Payload: Dove 0F34. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41985 . COSPAR: 2017-008AP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 86 (Dove 0F34). ..
- Flock 3p-87 - . Payload: Dove 0F31. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42044 . COSPAR: 2017-008DA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 87 (Dove 0F31). ..
- Flock 3p-88 - . Payload: Dove 0F38. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41982 . COSPAR: 2017-008AL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 88 (Dove 0F38). ..
2017 May 5 - . 11:26 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: GSLV. Launch Vehicle: GSLV Mk II.
- South Asia Satellite - . Payload: GSAT 9. Nation: India. USAF Sat Cat: 42695 . COSPAR: 2017-024A. Apogee: 35,798 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.12 deg. Period: 1,436.11 min. See GSat 9 (South Asian Satellite). ..
2017 June 5 - . 11:57 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: GSLV. Launch Vehicle: GSLV-3.
- GSAT-19E - . Nation: India. USAF Sat Cat: 42747 . COSPAR: 2017-031A. Apogee: 35,805 km (22,248 mi). Perigee: 35,766 km (22,223 mi). Inclination: 0.0700 deg. Period: 1,436.05 min. See GSat 19. ..
2017 June 23 - . 03:58 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- UCLSat - . Payload: QB50-GB03. Nation: UK. Spacecraft: Cubesat. USAF Sat Cat: 42765 . COSPAR: 2017-036A. Apogee: 506 km (314 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.59 min. See UCLSat (QB50 GB03). Part of the QB50 international network of 50 CubeSats for measurements in the lower thermosphere..
- NIUSAT-Keralshree - . Payload: NIUSAT. Nation: India. USAF Sat Cat: 42766 . COSPAR: 2017-036B. Apogee: 514 km (319 mi). Perigee: 493 km (306 mi). Inclination: 97.37 deg. Period: 94.68 min. See NIUSAT (Keralshree). ..
- VZLUSat - . Payload: QB50-CZ03?; VZLUSAT 1. Nation: Czechia. Spacecraft: Cubesat. USAF Sat Cat: 42790 . COSPAR: 2017-036AB. Apogee: 504 km (313 mi). Perigee: 490 km (300 mi). Inclination: 97.37 deg. Period: 94.55 min. See CE-SAT 1. Part of the QB50 international network of 50 CubeSats for measurements in the lower thermosphere..
- Venta-1 - . Nation: Russia. USAF Sat Cat: 42791 . COSPAR: 2017-036AC. Apogee: 506 km (314 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.58 min. See Venta 1. ..
- Cartosat-2E - . Nation: India. USAF Sat Cat: 42767 . COSPAR: 2017-036C. Apogee: 515 km (320 mi). Perigee: 502 km (311 mi). Inclination: 97.49 deg. Period: 94.78 min. See Cartosat 2E. ..
- ROBUSTA 1B - . Nation: France. USAF Sat Cat: 42792 . COSPAR: 2017-036AD. Apogee: 505 km (313 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.57 min. See ROBUSTA 1B. ..
- LituanicaSAT 2 - . Payload: QB50-LT01. Nation: Lithania. Spacecraft: Cubesat. USAF Sat Cat: 42768 . COSPAR: 2017-036D. Apogee: 509 km (316 mi). Perigee: 489 km (303 mi). Inclination: 97.37 deg. Period: 94.60 min. See LituanicaSAT 2 (QB50 LT01). Part of the QB50 international network of 50 CubeSats for measurements in the lower thermosphere..
- CICERO-6 - . Nation: USA. USAF Sat Cat: 42793 . COSPAR: 2017-036AE. Apogee: 506 km (314 mi). Perigee: 492 km (305 mi). Inclination: 97.37 deg. Period: 94.59 min. See CICERO 6. ..
- CE-SAT-I - . Nation: Japan. USAF Sat Cat: 42769 . COSPAR: 2017-036E. Apogee: 515 km (320 mi). Perigee: 494 km (306 mi). Inclination: 97.37 deg. Period: 94.71 min. See CE-SAT 1. ..
- D-SAT - . Nation: Italy. USAF Sat Cat: 42794 . COSPAR: 2017-036AF. Apogee: 682 km (423 mi). Perigee: 507 km (315 mi). Inclination: 97.56 deg. Period: 96.58 min. See D-Sat. ..
- InflateSail - . Payload: QB50-GB06. Nation: UK. Spacecraft: Cubesat. USAF Sat Cat: 42770 . COSPAR: 2017-036F. Apogee: 263 km (163 mi). Perigee: 243 km (150 mi). Inclination: 97.43 deg. Period: 89.57 min. See InflateSail (QB50 GB06). Part of the QB50 international network of 50 CubeSats for measurements in the lower thermosphere..
- PACSCISAT - . Payload: TYVAK-53B; TYVAK 53B. Nation: USA. USAF Sat Cat: 42795 . COSPAR: 2017-036AG. Apogee: 502 km (311 mi). Perigee: 491 km (305 mi). Inclination: 97.35 deg. Period: 94.55 min. See PACSCISAT (Tyvak 53b). ..
- Lemur-2-ShainaJohl - . Payload: Lemur-2-34; LEMUR 2 SHAINAJOHL. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42771 . COSPAR: 2017-036G. Apogee: 510 km (310 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.63 min. See Lemur-2 34 (Lemur-2 ShainaJohl). ..
- Lemur-2-XueniTerence - . Payload: Lemur-2-35; LEMUR 2 XUENITERENCE. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42772 . COSPAR: 2017-036H. Apogee: 509 km (316 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.62 min. See Lemur-2 35 (Lemur-2 XueniTerence). ..
- Lemur-2-LucyBryce - . Payload: Lemur-2-36; LEMUR 2 LUCYBRYCE. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42773 . COSPAR: 2017-036J. Apogee: 508 km (315 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.61 min. See Lemur-2 36 (Lemur-2 LucyBryce). ..
- Lemur-2-KungFoo - . Payload: Lemur-2-37; LEMUR 2 KUNGFOO. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42774 . COSPAR: 2017-036K. Apogee: 509 km (316 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.62 min. See Lemur-2 37 (Lemur-2 KungFoo). ..
- Aalto-1 - .
Nation: Finland.
USAF Sat Cat: 42775 . COSPAR: 2017-036L. Apogee: 512 km (318 mi). Perigee: 493 km (306 mi). Inclination: 97.37 deg. Period: 94.67 min.
See Aalto 1. 3U cubesat by Aalto University and Finnish Meteorological Institute, Finland. Mission: Technical demonstration of a miniaturized spectral imager, a radiation monitor and a plasma brake. Status as of 2019: Active.
- URSA MAIOR - . Payload: QB50-IT02. Nation: Italy. Spacecraft: Cubesat. USAF Sat Cat: 42776 . COSPAR: 2017-036M. Apogee: 511 km (317 mi). Perigee: 493 km (306 mi). Inclination: 97.37 deg. Period: 94.66 min. See URSA MAIOR (QB50 IT02). Part of the QB50 international network of 50 CubeSats for measurements in the lower thermosphere..
- COMPASS-2 - . Payload: QB50-DE04. Nation: Germany. Spacecraft: Cubesat. USAF Sat Cat: 42777 . COSPAR: 2017-036N. Apogee: 507 km (315 mi). Perigee: 490 km (300 mi). Inclination: 97.37 deg. Period: 94.58 min. See COMPASS 2 (DragSail-Cubesat, QB50 DE04). Part of the QB50 international network of 50 CubeSats for measurements in the lower thermosphere..
- Max Valier - . Nation: Italy. USAF Sat Cat: 42778 . COSPAR: 2017-036P. Apogee: 509 km (316 mi). Perigee: 493 km (306 mi). Inclination: 97.37 deg. Period: 94.63 min. See Max Valier Sat. ..
- Lemur-2-Lynsey-Symo - . Payload: Lemur-2-41; LEMUR 2 LYNSEY-SYMO. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42779 . COSPAR: 2017-036Q. Apogee: 505 km (313 mi). Perigee: 489 km (303 mi). Inclination: 97.37 deg. Period: 94.55 min. See Lemur-2 41 (Lemur-2 Lynsey-Symo). ..
- Lemur-2-Lisasaurus - . Payload: Lemur-2-40; LEMUR 2 LISASAURUS. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42780 . COSPAR: 2017-036R. Apogee: 506 km (314 mi). Perigee: 490 km (300 mi). Inclination: 97.37 deg. Period: 94.58 min. See Pegasus (QB50 AT03). ..
- Lemur-2-Sam-Amelia - . Payload: Lemur-2-39; LEMUR 2 SAM-AMELIA. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42781 . COSPAR: 2017-036S. Apogee: 505 km (313 mi). Perigee: 490 km (300 mi). Inclination: 97.37 deg. Period: 94.56 min. See Lemur-2 39 (Lemur-2 Sam-Amelia). ..
- Lemur-2-McPeake - . Payload: Lemur-2-38; LEMUR 2 MCPEAKE. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 42782 . COSPAR: 2017-036T. Apogee: 505 km (313 mi). Perigee: 490 km (300 mi). Inclination: 97.37 deg. Period: 94.57 min. See Lemur-2 38 (Lemur-2 McPeake). ..
- Diamond Red - . Payload: 3-Diamonds 3. Nation: UK. USAF Sat Cat: 42783 . COSPAR: 2017-036U. Apogee: 508 km (315 mi). Perigee: 492 km (305 mi). Inclination: 97.37 deg. Period: 94.62 min. See Red Diamond. ..
- Pegasus - . Payload: QB50-AT03. Nation: Austria. Spacecraft: Cubesat. USAF Sat Cat: 42784 . COSPAR: 2017-036V. Apogee: 507 km (315 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.60 min. See Pegasus (QB50 AT03). Part of the QB50 international network of 50 CubeSats for measurements in the lower thermosphere..
- Diamond Green - . Payload: 3-Diamonds 2. Nation: UK. USAF Sat Cat: 42785 . COSPAR: 2017-036W. Apogee: 508 km (315 mi). Perigee: 492 km (305 mi). Inclination: 97.37 deg. Period: 94.62 min. See Green Diamond. ..
- Diamond Blue - . Payload: 3-Diamonds 1. Nation: UK. USAF Sat Cat: 42786 . COSPAR: 2017-036X. Apogee: 508 km (315 mi). Perigee: 492 km (305 mi). Inclination: 97.37 deg. Period: 94.62 min. See Blue Diamond. ..
- NUDTSat - . Payload: QB50-CN06/BE06. Nation: China. Spacecraft: Cubesat. USAF Sat Cat: 42787 . COSPAR: 2017-036Y. Apogee: 505 km (313 mi). Perigee: 488 km (303 mi). Inclination: 97.37 deg. Period: 94.55 min. See NUDTSat (QB50 CN06). Part of the QB50 international network of 50 CubeSats for measurements in the lower thermosphere..
- SUCHAI - . Nation: Chiles. USAF Sat Cat: 42788 . COSPAR: 2017-036Z. Apogee: 506 km (314 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.58 min. See SUCHAI. ..
- skCUBE - .
Nation: Slovakia.
USAF Sat Cat: 42789 . COSPAR: 2017-036AA. Apogee: 506 km (314 mi). Perigee: 491 km (305 mi). Inclination: 97.37 deg. Period: 94.58 min.
See skCUBE. 2U (QB50 type) cubesat by Slovak Organisation for Space Activities (SOSA), University of Žilina, Slovak University of Technology by help of Belgian Von Karman Institute, Faculty of Aeronautics of Technical University of Kosice.
2017 August 31 - . 13:29 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-R1H - . Payload: IRNSS-1H; IRNSS 1H/PSLV. Nation: India. USAF Sat Cat: 42928 . COSPAR: 2017-051A. Apogee: 1,201 km (746 mi). Perigee: 145 km (90 mi). Inclination: 19.13 deg. Period: 98.21 min. See IRNSS 1H. ..
2018 January 12 - . 03:58 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- Cartosat-2F - . Payload: Cartosat-2ER. Nation: India. USAF Sat Cat: 43111 . COSPAR: 2018-004A. Apogee: 511 km (317 mi). Perigee: 505 km (313 mi). Inclination: 97.45 deg. Period: 94.78 min. See Cartosat 2F (ex Cartosat 2ER). ..
- TOM - . Payload: CANYVAL-X2. Nation: TBD. USAF Sat Cat: 43136 . COSPAR: 2018-004AB. Apogee: 502 km (311 mi). Perigee: 489 km (303 mi). Inclination: 97.51 deg. Period: 94.52 min. See CANYVAL-X 1 (Tom). ..
- LEO Vantage 1 - . Payload: Telesat Phase 1 LEO; LEO 1. Nation: USA. USAF Sat Cat: 43113 . COSPAR: 2018-004C. Apogee: 1,003 km (623 mi). Perigee: 997 km (619 mi). Inclination: 99.45 deg. Period: 105.12 min. See LEO Vantage 1. ..
- AMSAT AO-92 - . Payload: Fox-1D; AO-92. Nation: USA. USAF Sat Cat: 43137 . COSPAR: 2018-004AC. Apogee: 503 km (312 mi). Perigee: 490 km (300 mi). Inclination: 97.50 deg. Period: 94.54 min. See Fox 1D (AO 92, AMSAT-OSCAR 92). ..
- STEP Cube Lab - . Nation: Korea South. USAF Sat Cat: 43138 . COSPAR: 2018-004AD. Apogee: 501 km (311 mi). Perigee: 488 km (303 mi). Inclination: 97.51 deg. Period: 94.51 min. See STEP Cube Lab. ..
- ICEYE-X1 - . Payload: ICEYE POC-1. Nation: Finland. USAF Sat Cat: 43114 . COSPAR: 2018-004D. Apogee: 505 km (313 mi). Perigee: 492 km (305 mi). Inclination: 97.50 deg. Period: 94.58 min. See ICEYE X1. ..
- SpaceBEE 4 - . Nation: USA. USAF Sat Cat: 43139 . COSPAR: 2018-004AE. Apogee: 499 km (310 mi). Perigee: 487 km (302 mi). Inclination: 97.51 deg. Period: 94.47 min. See SpaceBEE 4. ..
- VividX2 - . Payload: CBNT-2; CARBONITE 2. Nation: UK. USAF Sat Cat: 43115 . COSPAR: 2018-004E. Apogee: 506 km (314 mi). Perigee: 492 km (305 mi). Inclination: 97.50 deg. Period: 94.60 min. See Carbonite 2 (CBNT 2, Ei X2, VividX2). ..
- INS-1C - . Nation: TBD. USAF Sat Cat: 43116 . COSPAR: 2018-004F. Apogee: 504 km (313 mi). Perigee: 491 km (305 mi). Inclination: 97.51 deg. Period: 94.56 min. See INS 1C. ..
- SpaceBEE 3 - . Nation: USA. USAF Sat Cat: 43140 . COSPAR: 2018-004AF. Apogee: 498 km (309 mi). Perigee: 486 km (301 mi). Inclination: 97.51 deg. Period: 94.45 min. See SpaceBEE 3. ..
- JERRY - . Payload: CANYVAL-X1. COSPAR: 2018-004G. See CANYVAL-X 2 (Jerry). ..
- SpaceBEE 2 - . Nation: USA. USAF Sat Cat: 43141 . COSPAR: 2018-004AG. Apogee: 498 km (309 mi). Perigee: 485 km (301 mi). Inclination: 97.51 deg. Period: 94.44 min. See SpaceBEE 2. ..
- SpaceBEE 1 - . Nation: USA. USAF Sat Cat: 43142 . COSPAR: 2018-004AH. Apogee: 497 km (308 mi). Perigee: 485 km (301 mi). Inclination: 97.51 deg. Period: 94.43 min. See SpaceBEE 1. ..
- Landmapper-BC 3 - . Payload: Corvus BC3 v2; CORVUS BC3. Nation: USA. USAF Sat Cat: 43118 . COSPAR: 2018-004H. Apogee: 505 km (313 mi). Perigee: 491 km (305 mi). Inclination: 97.50 deg. Period: 94.57 min. See Landmapper-BC 3 v2 (Corvus-BC 3 v2). ..
- Flock 3p'-3 - . Payload: Dove 1105; FLOCK 3PP 3. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43119 . COSPAR: 2018-004J. Apogee: 505 km (313 mi). Perigee: 491 km (305 mi). Inclination: 97.51 deg. Period: 94.58 min. See Flock-3p' 3 (Dove 1105). ..
- CICERO-7 - . Nation: USA. USAF Sat Cat: 43143 . COSPAR: 2018-004AJ. Apogee: 500 km (310 mi). Perigee: 489 km (303 mi). Inclination: 97.50 deg. Period: 94.50 min. See CICERO 7. ..
- Flock 3p'-2 - . Payload: Dove 1102; FLOCK 3PP 2. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43120 . COSPAR: 2018-004K. Apogee: 505 km (313 mi). Perigee: 491 km (305 mi). Inclination: 97.51 deg. Period: 94.58 min. See Flock-3p' 2 (Dove 1102). ..
- TYVAK-61c - . Nation: USA. USAF Sat Cat: 43144 . COSPAR: 2018-004AK. Apogee: 499 km (310 mi). Perigee: 487 km (302 mi). Inclination: 97.51 deg. Period: 94.47 min. See Tyvak 61C. ..
- Flock 3p'-1 - . Payload: Dove 1100; FLOCK 3PP 1. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43121 . COSPAR: 2018-004L. Apogee: 504 km (313 mi). Perigee: 490 km (300 mi). Inclination: 97.51 deg. Period: 94.56 min. See Flock-3p' 1 (Dove 1100). ..
- Flock 3p'-4 - . Payload: Dove 1107; FLOCK 3PP 4. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43122 . COSPAR: 2018-004M. Apogee: 505 km (313 mi). Perigee: 491 km (305 mi). Inclination: 97.51 deg. Period: 94.58 min. See Flock-3p' 4 (Dove 1107). ..
- Lemur-2-McCafferty - . Payload: Lemur-2-68; LEMUR 2 MCCAFFERTY. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43123 . COSPAR: 2018-004N. Apogee: 501 km (311 mi). Perigee: 488 km (303 mi). Inclination: 97.51 deg. Period: 94.50 min. See Lemur-2 70 (Lemur-2 McCafferty). ..
- Lemur-2-PeterWebster - . Payload: Lemur-2-69; LEMUR 2 PETERWEBSTER. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43124 . COSPAR: 2018-004P. Apogee: 502 km (311 mi). Perigee: 488 km (303 mi). Inclination: 97.51 deg. Period: 94.52 min. See Lemur-2 68 (Lemur-2 PeterWebster). ..
- Lemur-2-BrownCow - . Payload: Lemur-2-70; LEMUR 2 BROWNCOW. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43125 . COSPAR: 2018-004Q. Apogee: 501 km (311 mi). Perigee: 488 km (303 mi). Inclination: 97.51 deg. Period: 94.50 min. See Lemur-2 71 (Lemur-2 BrownCow). ..
- Lemur-2-DaveWilson - . Payload: Lemur-2-71; LEMUR 2 DAVEWILSON. Nation: USA. Spacecraft: Cubesat. USAF Sat Cat: 43126 . COSPAR: 2018-004R. Apogee: 502 km (311 mi). Perigee: 488 km (303 mi). Inclination: 97.51 deg. Period: 94.51 min. See Lemur-2 69 (Lemur-2 DaveWilson). ..
- DemoSat-2 - . Payload: Astranis DemoSat-2. Nation: USA. USAF Sat Cat: 43127 . COSPAR: 2018-004S. Apogee: 504 km (313 mi). Perigee: 490 km (300 mi). Inclination: 97.50 deg. Period: 94.56 min. See DemoSat 2. ..
- Microsat-TD - . Nation: India. USAF Sat Cat: 43128 . COSPAR: 2018-004T. Apogee: 362 km (224 mi). Perigee: 353 km (219 mi). Inclination: 96.83 deg. Period: 91.69 min. See Microsat-TD. ..
- Arkyd-6A - . Nation: USA. USAF Sat Cat: 43130 . COSPAR: 2018-004V. Apogee: 504 km (313 mi). Perigee: 490 km (300 mi). Inclination: 97.51 deg. Period: 94.55 min. See Arkyd 6A. ..
- MicroMAS-2A - . Nation: USA. USAF Sat Cat: 43131 . COSPAR: 2018-004W. Apogee: 501 km (311 mi). Perigee: 488 km (303 mi). Inclination: 97.51 deg. Period: 94.51 min. See MicroMAS 2a. 3U cubesat by Paris Observatory. Mission: Astronomy/Planetary science. Status as of 2019: Active..
- PICSAT - . Nation: France. USAF Sat Cat: 43132 . COSPAR: 2018-004X. Apogee: 503 km (312 mi). Perigee: 489 km (303 mi). Inclination: 97.51 deg. Period: 94.54 min. See PicSat. 3U cubesat by Paris Observatory. Mission: Astronomy/Planetary science. Status as of 2019: Active. ..
- Papillon - . Payload: CNUSail-1. Nation: TBD. USAF Sat Cat: 43133 . COSPAR: 2018-004Y. Apogee: 504 km (313 mi). Perigee: 490 km (300 mi). Inclination: 97.50 deg. Period: 94.55 min. See CNUSail 1 (Papillon). ..
- KHUSAT-3 - . Payload: SIGMA. Nation: TBD. USAF Sat Cat: 43134 . COSPAR: 2018-004Z. Apogee: 503 km (312 mi). Perigee: 490 km (300 mi). Inclination: 97.51 deg. Period: 94.54 min. See SIGMA (KHUSAT 3). ..
- KAUSAT-5 - . Nation: TBD. USAF Sat Cat: 43135 . COSPAR: 2018-004AA. Apogee: 502 km (311 mi). Perigee: 489 km (303 mi). Inclination: 97.51 deg. Period: 94.53 min. See KAUSAT 5. ..
2018 March 29 - . 11:25 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. LV Family: GSLV. Launch Vehicle: GSLV Mk II.
- GSAT 6A - . Nation: India. USAF Sat Cat: 43241 . COSPAR: 2018-027A. Apogee: 36,342 km (22,581 mi). Perigee: 26,007 km (16,159 mi). Inclination: 2.70 deg. Period: 1,207.03 min. See GSat 6A. ..
2018 April 11 - . 22:33 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
- IRNSS-R1I - . Payload: IRNSS-1I; IRNSS 1I. Nation: India. USAF Sat Cat: 43286 . COSPAR: 2018-035A. Apogee: 35,877 km (22,292 mi). Perigee: 35,695 km (22,179 mi). Inclination: 29.02 deg. Period: 1,436.07 min. See IRNSS 1I. ..
2018 September 16 - . 16:37 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota FLP. Launch Vehicle: PSLV.
- S1-4 - . Payload: SSTL S1-4. Nation: UK. USAF Sat Cat: 43618 . COSPAR: 2018-071A. Apogee: 593 km (368 mi). Perigee: 572 km (355 mi). Inclination: 97.81 deg. Period: 96.33 min. See NovaSAR-S 1. ..
- NovaSAR-S - . Nation: UK. USAF Sat Cat: 43619 . COSPAR: 2018-071B. Apogee: 592 km (367 mi). Perigee: 577 km (358 mi). Inclination: 97.81 deg. Period: 96.36 min. See NovaSAR-S 1. ..
2018 November 14 - . 11:37 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota Dhawan SLP. LV Family: GSLV. Launch Vehicle: GSLV-3.
- GSAT-29 - . Nation: India. Type: Comms. USAF Sat Cat: 43698 . COSPAR: 2018-089A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.08 min. See GSat 29. ..
2018 November 29 - . 04:26 GMT - . Launch Site: Sriharikota. LV Family: PSLV. Launch Vehicle: PSLV CA.
- HySIS - . Nation: India. Type: Imaging. USAF Sat Cat: 43719 . COSPAR: 2018-096A. Apogee: 642 km (398 mi). Perigee: 626 km (388 mi). Inclination: 97.96 deg. Period: 97.39 min. See HySIS. 1000LT SSO..
- HSAT-1 - . Type: Tech. COSPAR: 2018-096B. See HSAT 1. ..
- Global-1 - . Nation: USA. Type: Imaging. USAF Sat Cat: 43720 . COSPAR: 2018-096B. Apogee: 501 km (311 mi). Perigee: 475 km (295 mi). Inclination: 97.48 deg. Period: 94.37 min. See BlackSky Global 1. 1000LT SSO..
- Hiber 1 - . Nation: Netherlands. Type: Comms IoT. Spacecraft: Cubesat. USAF Sat Cat: 43744 . COSPAR: 2018-096AB. Apogee: 500 km (310 mi). Perigee: 473 km (293 mi). Inclination: 97.48 deg. Period: 94.34 min. See Hiber 1. IoT data relay 6U cubesat for Hiber (Delft). ..
- Lemur-2-Duly - . Nation: USA. Type: Weather/AIS. Spacecraft: Cubesat. USAF Sat Cat: 43745 . COSPAR: 2018-096AC. Apogee: 501 km (311 mi). Perigee: 470 km (290 mi). Inclination: 97.48 deg. Period: 94.31 min. See Lemur-2 87 (Lemur-2 Duly). ..
- Lemur-2-Vladimir - . Nation: USA. Type: Weather/AIS. Spacecraft: Cubesat. USAF Sat Cat: 43746 . COSPAR: 2018-096AD. Apogee: 501 km (311 mi). Perigee: 469 km (291 mi). Inclination: 97.48 deg. Period: 94.31 min. See Lemur-2 85 (Lemur-2 Vladimir). ..
- Centauri 2 - . Nation: USA. Type: Comms IoT. USAF Sat Cat: 43722 . COSPAR: 2018-096D. Apogee: 501 km (311 mi). Perigee: 474 km (294 mi). Inclination: 97.48 deg. Period: 94.36 min. See Centauri 2. ..
- FACSAT - . Nation: USA. Type: Imaging. USAF Sat Cat: 43722 . COSPAR: 2018-096D. Apogee: 501 km (311 mi). Perigee: 474 km (294 mi). Inclination: 97.48 deg. Period: 94.36 min. See FACSAT 1. ..
- Flock 3r-9 - . Payload: Dove 1061. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43723 . COSPAR: 2018-096E. Apogee: 501 km (311 mi). Perigee: 474 km (294 mi). Inclination: 97.48 deg. Period: 94.36 min. See Flock-3r 9 (Dove 1061). ..
- Flock 3r-1 - . Payload: Dove 105A. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43747 . COSPAR: 2018-096AE. Apogee: 501 km (311 mi). Perigee: 469 km (291 mi). Inclination: 97.48 deg. Period: 94.31 min. See Flock-3r 1 (Dove 105A). ..
- Flock 3r-2 - . Payload: Dove 105B. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43748 . COSPAR: 2018-096AF. Apogee: 501 km (311 mi). Perigee: 469 km (291 mi). Inclination: 97.48 deg. Period: 94.31 min. See Flock-3r 2 (Dove 105B). ..
- Flock 3r-12 - . Payload: Dove 1066. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43724 . COSPAR: 2018-096F. Apogee: 501 km (311 mi). Perigee: 473 km (293 mi). Inclination: 97.48 deg. Period: 94.35 min. See Flock-3r 12 (Dove 1066). ..
- Flock 3r-14 - . Payload: Dove 210C. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43749 . COSPAR: 2018-096AG. Apogee: 500 km (310 mi). Perigee: 468 km (290 mi). Inclination: 97.48 deg. Period: 94.29 min. See Flock-3r 14 (Dove 210C). ..
- Flock 3r-11 - . Payload: Dove 1064. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43725 . COSPAR: 2018-096G. Apogee: 501 km (311 mi). Perigee: 474 km (294 mi). Inclination: 97.48 deg. Period: 94.35 min. See Flock-3r 11 (Dove 1064). ..
- Flock 3r-5 - . Payload: Dove 105F. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43726 . COSPAR: 2018-096H. Apogee: 501 km (311 mi). Perigee: 473 km (293 mi). Inclination: 97.48 deg. Period: 94.35 min. See Flock-3r 5 (Dove 105F). ..
- Flock 3r-13 - . Payload: Dove 210B. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43750 . COSPAR: 2018-096AH. Apogee: 501 km (311 mi). Perigee: 468 km (290 mi). Inclination: 97.48 deg. Period: 94.29 min. See Flock-3r 13 (Dove 210B). ..
- Flock 3r-8 - . Payload: Dove 1060. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43727 . COSPAR: 2018-096J. Apogee: 501 km (311 mi). Perigee: 473 km (293 mi). Inclination: 97.48 deg. Period: 94.35 min. See Flock-3r 8 (Dove 1060). ..
- Reaktor Hello World - . Nation: TBD. Type: Comms. USAF Sat Cat: 43728 . COSPAR: 2018-096K. Apogee: 500 km (310 mi). Perigee: 473 km (293 mi). Inclination: 97.48 deg. Period: 94.34 min. See Reaktor Hello World. ..
- CASE - . Nation: Canada. Type: Comms IoT. USAF Sat Cat: 43729 . COSPAR: 2018-096L. Apogee: 500 km (310 mi). Perigee: 473 km (293 mi). Inclination: 97.48 deg. Period: 94.34 min. See CASE. ..
- Lemur-2-Orzulak - . Nation: USA. Type: Weather/AIS. Spacecraft: Cubesat. USAF Sat Cat: 43731 . COSPAR: 2018-096N. Apogee: 501 km (311 mi). Perigee: 470 km (290 mi). Inclination: 97.48 deg. Period: 94.31 min. See Lemur-2 84 (Lemur-2 Orzulak). ..
- Lemur-2-Kobyszcze - . Nation: USA. Type: Weather/AIS. Spacecraft: Cubesat. USAF Sat Cat: 43732 . COSPAR: 2018-096P. Apogee: 501 km (311 mi). Perigee: 469 km (291 mi). Inclination: 97.48 deg. Period: 94.31 min. See Lemur-2 86 (Lemur-2 Kobyszcze). ..
- Flock 3r-4 - . Payload: Dove 105E. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43733 . COSPAR: 2018-096Q. Apogee: 501 km (311 mi). Perigee: 470 km (290 mi). Inclination: 97.47 deg. Period: 94.31 min. See Flock-3r 4 (Dove 105E). ..
- Flock 3r-3 - . Payload: Dove 105D. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43734 . COSPAR: 2018-096R. Apogee: 501 km (311 mi). Perigee: 469 km (291 mi). Inclination: 97.48 deg. Period: 94.31 min. See Flock-3r 3 (Dove 105D). ..
- Flock 3r-16 - . Payload: Dove 2152. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43735 . COSPAR: 2018-096S. Apogee: 501 km (311 mi). Perigee: 468 km (290 mi). Inclination: 97.48 deg. Period: 94.30 min. See Flock-3r 16 (Dove 2152). ..
- Flock 3r-15 - . Payload: Dove 2107. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43736 . COSPAR: 2018-096T. Apogee: 501 km (311 mi). Perigee: 468 km (290 mi). Inclination: 97.48 deg. Period: 94.30 min. See Flock-3r 15 (Dove 2107). ..
- InnoSAT-2 - . Nation: TBD. Type: Tech. USAF Sat Cat: 43738 . COSPAR: 2018-096V. Apogee: 500 km (310 mi). Perigee: 464 km (288 mi). Inclination: 97.48 deg. Period: 94.24 min. See InnoSat 2. ..
- Flock 3r-10 - . Payload: Dove 1059. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43740 . COSPAR: 2018-096X. Apogee: 501 km (311 mi). Perigee: 474 km (294 mi). Inclination: 97.48 deg. Period: 94.35 min. See Flock-3r 10 (Dove 1059). ..
- Flock 3r-6 - . Payload: Dove 1057. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43741 . COSPAR: 2018-096Y. Apogee: 501 km (311 mi). Perigee: 473 km (293 mi). Inclination: 97.48 deg. Period: 94.35 min. See Flock-3r 6 (Dove 1057). ..
- Flock 3r-7 - . Payload: Dove 1058. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43742 . COSPAR: 2018-096Z. Apogee: 501 km (311 mi). Perigee: 473 km (293 mi). Inclination: 97.48 deg. Period: 94.35 min. See Flock-3r 7 (Dove 1058). ..
2018 December 19 - . 10:39 GMT - . Launch Site: Sriharikota. LV Family: GSLV. Launch Vehicle: GSLV Mk II.
- GSAT-7A - . Nation: India. Type: Comms 1. USAF Sat Cat: 43864 . COSPAR: 2018-105A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0900 deg. Period: 1,436.07 min. See GSat 7A. ..
2019 January 24 - . 18:06 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-DL.
- Microsat-R - . Nation: India. Type: P Imaging 0. USAF Sat Cat: 43947 . COSPAR: 2019-006A. Apogee: 302 km (187 mi). Perigee: 241 km (149 mi). Inclination: 96.60 deg. Period: 89.93 min. See Microsat-R. 2340LT SSO..
- Kalamsat-v2 - . Nation: India. Type: Tech 0. USAF Sat Cat: 43948 . COSPAR: 2019-006B. Apogee: 452 km (280 mi). Perigee: 446 km (277 mi). Inclination: 98.80 deg. Period: 93.56 min. See Kalamsat v2. 2340LT SSO..
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