# List of Indian satellites

This list covers most artificial satellites built and operated by the Republic of India. India has been successfully launching satellites of various types from 1975. Apart from Indian rockets, these satellites have been launched from various vehicles, including American, Russian, and European rockets sometimes as well. The organization responsible for India's space program is Indian Space Research Organisation (ISRO) and it shoulders the bulk of the responsibility of designing, building, launching, and operating these satellites.

## Legend

This is a list of Indian (wholly or partially owned, wholly or partially designed and/or manufactured) satellites and orbital space crafts, both operated by the Indian government (ISRO, Indian defence forces, other government agencies) or private (educational and research) entities. All satellite launches marked successful have completed at least one full orbital flight (no sub-orbital flights have been included in this list).

### Mission status/type legend

* Mission failure (due to launch vehicle failure (at launch/during transit))
* Extra-terrestrial missions
* Geosynchronous Orbit (inclination ≥ 5°)
* Geostationary Orbit (inclination < 5°)
* Crewed spacecraft

## 1970s

Indian space missions began in the 1970s, with Soviet assistance in launching the first two satellites.
| Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Launch Date | Launch Vehicle | Launch Site | Details | Details | Details | Details | Details | Details | Details | Details | Details | Refs (Official portal) |
| # | Name | Discipline | COSPAR ID | Launch Mass | Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Period | Inclination | Longitude$^‡$ | Epoch Start | Decay Date | | | Refs (Official portal) |
| # | Name | Discipline | SatCat # | Dry Mass | Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Period | Inclination | Longitude$^‡$ | Epoch Start | Decay Date | | | Refs (Official portal) |
| 1 | Aryabhata | Earth Sciences Space Physics | 1975-033A | 360 kg (790 lb) | 46 W | 19 April 1975, 13:10:00 IST | Cosmos-3M | Kapustin Yar | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Active technological experience in building and operating a satellite system. This was India's first indigenously designed and built satellite. | Archived 31 July 2017 at the Wayback Machine |
| 1 | Aryabhata | Earth Sciences Space Physics | 07752 | – | 46 W | 19 April 1975, 13:10:00 IST | Cosmos-3M | Kapustin Yar | 568 km (353 mi) | 611 km (380 mi) | 96.5 minutes | 50.7° | | 19 April 1975, 01:30:00 IST | 11 February 1992 | | | Archived 31 July 2017 at the Wayback Machine |
| 2 | Bhaskara Sega-I | Astronomy Communications Engineering Earth Sciences | 1979-051A | 444 kg (979 lb) | 47 W | 7 June 1979, 16:00:00 IST | Modified SS-5 (SKean IRBM) plus Upper Stage | Kapustin Yar | First experimental remote sensing satellite. Carried TV and microwave cameras. | First experimental remote sensing satellite. Carried TV and microwave cameras. | First experimental remote sensing satellite. Carried TV and microwave cameras. | First experimental remote sensing satellite. Carried TV and microwave cameras. | First experimental remote sensing satellite. Carried TV and microwave cameras. | First experimental remote sensing satellite. Carried TV and microwave cameras. | First experimental remote sensing satellite. Carried TV and microwave cameras. | First experimental remote sensing satellite. Carried TV and microwave cameras. | First experimental remote sensing satellite. Carried TV and microwave cameras. | |
| 2 | Bhaskara Sega-I | Astronomy Communications Engineering Earth Sciences | 11392 | – | 47 W | 7 June 1979, 16:00:00 IST | Modified SS-5 (SKean IRBM) plus Upper Stage | Kapustin Yar | 512 km (318 mi) | 557 km (346 mi) | 95.2 minutes | 50.7° | | 7 June 1979, 01:30:00 IST | 17 February 1989 | | | |
| 3 | Rohini Technology Payload | Experimental | Not Applicable | 35 kg (77 lb) | 3 W | 10 August 1979 | SLV-3-E1 | Satish Dhawan Space Centre, Sriharikota | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Intended for measuring in-flight performance of first experimental flight of SLV-3, the first Indian launch vehicle. Did not achieve orbit. | Archived 31 July 2017 at the Wayback Machine |
| 3 | Rohini Technology Payload | Experimental | Not Applicable | – | 3 W | 10 August 1979 | SLV-3-E1 | Satish Dhawan Space Centre, Sriharikota | Not Applicable | Not Applicable | Not Applicable | Not Applicable | | Not Applicable | Not Applicable | | | Archived 31 July 2017 at the Wayback Machine |
$^†$ In case of discrepancy in data between sources, N2YO and NASA NSSDCA is taken as the source of truth. $^‡$ Orbital Longitude is applicable only for Geostationary and Geosynchronous satellites.

## 1980s

India had three continuous successful satellite launches from its first generation rocket SLV. ISRO had two running projects for next generation rockets based on SLV:
* ASLV to study and develop technologies to transfer satellites into geostationary orbit.
* PSLV to transfer higher payloads into polar and Sun synchronous orbits.
ISRO did not have enough funds to run both projects simultaneously. Initial setbacks complexity led ISRO to terminate ASLV in just initial flights and focus on PSLV. Technologies to launch geostationary satellites arrived only in 2000s.
| Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Launch Date | Launch Vehicle | Launch Site | Details | Details | Details | Details | Details | Details | Details | Details | Details | Refs (Official portal) |
| # | Name | Discipline | COSPAR ID | Launch Mass | Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Period | Inclination | Longitude$^‡$ | Epoch Start | Decay Date | | | Refs (Official portal) |
| # | Name | Discipline | SatCat # | Dry Mass | Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Period | Inclination | Longitude$^‡$ | Epoch Start | Decay Date | | | Refs (Official portal) |
| 4 | Rohini RS-1 (Rohini-1B) | Earth Sciences | 1980-062A | 35 kg (77 lb) | 16 W | 18 July 1980, 08:01:00 IST | SLV-3-E2 | Satish Dhawan Space Centre, Sriharikota | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Used for measuring in-flight performance of second experimental launch of SLV-3. This was India's first indigenous satellite launch, making it the seventh nation to possess the capability to launch its own satellites on its own rockets. | Archived 26 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 4 | Rohini RS-1 (Rohini-1B) | Earth Sciences | 11899 | – | 16 W | 18 July 1980, 08:01:00 IST | SLV-3-E2 | Satish Dhawan Space Centre, Sriharikota | 305 km (190 mi) | 919 km (571 mi) | 96.9 minutes | 44.7° | | 18 July 1980, 01:30:00 IST | 20 May 1981 | | | Archived 26 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 5 | Rohini RS-D1 (Rohini-2) | Earth Sciences | 1981-051A | 38 kg (84 lb) | 16 W | 31 May 1981, 10:30:00 IST | SLV-3-D1 | Satish Dhawan Space Centre, Sriharikota | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Used for conducting some remote sensing technology studies using a landmark sensor payload. Launched by the first developmental launch of SLV-3. | Archived 31 July 2017 at the Wayback Machine |
| 5 | Rohini RS-D1 (Rohini-2) | Earth Sciences | 12491 | – | 16 W | 31 May 1981, 10:30:00 IST | SLV-3-D1 | Satish Dhawan Space Centre, Sriharikota | 186 km (116 mi) | 418 km (260 mi) | 90.5 minutes | 46.3° | | 31 May 1981, 01:30:00 IST | 8 June 1981 | | | Archived 31 July 2017 at the Wayback Machine |
| 6 | APPLE | Communications | 1981-057B | 670 kg (1,480 lb) | 210 W | 19 June 1981, 18:02:59 IST | Ariane-1 (V-3) | Centre Spatial Guyanais, Kourou | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | First experimental communication satellite. Provided experience in building and operating a payload experiment three-axis stabilised communication satellite. | Archived 19 October 2021 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 6 | APPLE | Communications | 12545 | – | 210 W | 19 June 1981, 18:02:59 IST | Ariane-1 (V-3) | Centre Spatial Guyanais, Kourou | 35,761.9 km (22,221.4 mi) | 35,963 km (22,346 mi) | 1439.6 minutes | 13.6° | 97.57° E | 19 June 1981, 01:30:00 IST | | | | Archived 19 October 2021 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 7 | Bhaskara -II | Engineering Earth Sciences | 1981-115A | 444 kg (979 lb) | 47 W | 20 November 1981, 14:08:00 IST | Modified SS-5 (SKean IRBM) plus Upper Stage | Kapustin Yar | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Second experimental remote sensing satellite; similar to Bhaskara-1. Provided experience in building and operating a remote sensing satellite system on an end-to-end basis. | Archived 30 July 2017 at the Wayback Machine |
| 7 | Bhaskara -II | Engineering Earth Sciences | 12968 | – | 47 W | 20 November 1981, 14:08:00 IST | Modified SS-5 (SKean IRBM) plus Upper Stage | Kapustin Yar | 520 km (320 mi) | 542 km (337 mi) | 95.2 minutes | 50.6° | | 20 November 1981, 00:30:00 IST | 30 November 1991 | | | Archived 30 July 2017 at the Wayback Machine |
| 8 | INSAT-1A | Communications | 1982-031A | 1,152.1 kg (2,540 lb) | – | 10 April 1982, 12:17:00 IST | Delta 3910 PAM-D | Air Force Eastern Test Range, Florida | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | First operational multipurpose communication and meteorology satellite. Procured from USA. Worked for only six months. | Archived 12 August 2022 at the Wayback Machine |
| 8 | INSAT-1A | Communications | 13129 | – | – | 10 April 1982, 12:17:00 IST | Delta 3910 PAM-D | Air Force Eastern Test Range, Florida | 35,837.1 km (22,268.1 mi) | 35,903.1 km (22,309.2 mi) | 1440 minutes | 13.6° | 40.85° E | 10 April 1982, 07:17:00 IST | | | | Archived 12 August 2022 at the Wayback Machine |
| 9 | Rohini RS-D2 (Rohini-3) | Earth Sciences | 1983-033A | 41.5 kg (91 lb) | 16 W | 17 April 1983, 11:14:00 IST | SLV-3 | Satish Dhawan Space Centre, Sriharikota | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | Identical to RS-D1. Launched by the second developmental launch of SLV-3. | |
| 9 | Rohini RS-D2 (Rohini-3) | Earth Sciences | 14002 | – | 16 W | 17 April 1983, 11:14:00 IST | SLV-3 | Satish Dhawan Space Centre, Sriharikota | 389 km (242 mi) | 852 km (529 mi) | 97.1 minutes | 46.6° | 17 April 1983, 00:30:00 IST | 19 April 1990 | | | | |
| 10 | INSAT-1B | Communications Earth Sciences | 1983-089B | 1,152 kg (2,540 lb) | – | 1 June 1983, 13:19:00 IST | Shuttle [PAM-D] | Air Force Eastern Test Range, Florida | Identical to INSAT-1A. Served for more than design life of seven years. | Identical to INSAT-1A. Served for more than design life of seven years. | Identical to INSAT-1A. Served for more than design life of seven years. | Identical to INSAT-1A. Served for more than design life of seven years. | Identical to INSAT-1A. Served for more than design life of seven years. | Identical to INSAT-1A. Served for more than design life of seven years. | Identical to INSAT-1A. Served for more than design life of seven years. | Identical to INSAT-1A. Served for more than design life of seven years. | Identical to INSAT-1A. Served for more than design life of seven years. | Archived 28 September 2022 at the Wayback Machine |
| 10 | INSAT-1B | Communications Earth Sciences | 14318 | – | – | 1 June 1983, 13:19:00 IST | Shuttle [PAM-D] | Air Force Eastern Test Range, Florida | 35,776.2 km (22,230.3 mi) | 35,869.6 km (22,288.3 mi) | 1437.6 minutes | 14.8° | 89.71° E | 31 May 1983, 09:19:00 IST | | | | Archived 28 September 2022 at the Wayback Machine |
| 11 | SROSS-1 | Experimental | Not Applicable | 150 kg (330 lb) | 90 W | 24 March 1987 | ASLV-D1 | Satish Dhawan Space Centre, Sriharikota | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | Carried payload for launch vehicle performance monitoring and for gamma ray astronomy. Did not achieve orbit. | |
| 11 | SROSS-1 | Experimental | Not Applicable | – | 90 W | 24 March 1987 | ASLV-D1 | Satish Dhawan Space Centre, Sriharikota | Not Applicable | Not Applicable | Not Applicable | Not Applicable | | Not Applicable | Not Applicable | | | |
| 12 | IRS-1A | Earth Sciences | 1988-021A | 975 kg (2,150 lb) | 600 W | 17 March 1988, 12:42:00 IST | Vostok | Baikonur Cosmodrome, Kazakhstan | Earth observation satellite. First operational remote sensing satellite. | Earth observation satellite. First operational remote sensing satellite. | Earth observation satellite. First operational remote sensing satellite. | Earth observation satellite. First operational remote sensing satellite. | Earth observation satellite. First operational remote sensing satellite. | Earth observation satellite. First operational remote sensing satellite. | Earth observation satellite. First operational remote sensing satellite. | Earth observation satellite. First operational remote sensing satellite. | Earth observation satellite. First operational remote sensing satellite. | |
| 12 | IRS-1A | Earth Sciences | 18960 | – | 600 W | 17 March 1988, 12:42:00 IST | Vostok | Baikonur Cosmodrome, Kazakhstan | 902.3 km (560.7 mi) | 922.1 km (573.0 mi) | 103.1 minutes | 99.3° | | 17 March 1988, 00:30:00 IST | | | | |
| 13 | SROSS-2 | Astronomy Space Physics | Not Applicable | 150 kg (330 lb) | 90 W | 13 July 1988 | ASLV-D2 | Satish Dhawan Space Centre, Sriharikota | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | Carried remote sensing payload of German space agency in addition to Gamma Ray astronomy payload. Did not achieve orbit. | |
| 13 | SROSS-2 | Astronomy Space Physics | Not Applicable | – | 90 W | 13 July 1988 | ASLV-D2 | Satish Dhawan Space Centre, Sriharikota | Not Applicable | Not Applicable | Not Applicable | Not Applicable | | Not Applicable | Not Applicable | | | |
| 14 | INSAT-1C | Communications Earth Sciences | 1988-063A | 1,152 kg (2,540 lb) | – | 22 July 1988, 04:42:00 IST | Ariane-3 | Centre Spatial Guyanais, Kourou | Same as INSAT-1A. Served for only one-and-a-half years. | Same as INSAT-1A. Served for only one-and-a-half years. | Same as INSAT-1A. Served for only one-and-a-half years. | Same as INSAT-1A. Served for only one-and-a-half years. | Same as INSAT-1A. Served for only one-and-a-half years. | Same as INSAT-1A. Served for only one-and-a-half years. | Same as INSAT-1A. Served for only one-and-a-half years. | Same as INSAT-1A. Served for only one-and-a-half years. | Same as INSAT-1A. Served for only one-and-a-half years. | |
| 14 | INSAT-1C | Communications Earth Sciences | 19330 | – | – | 22 July 1988, 04:42:00 IST | Ariane-3 | Centre Spatial Guyanais, Kourou | 35,768.8 km (22,225.7 mi) | 35,821.5 km (22,258.4 mi) | 1436.2 minutes | 14.9° | 95.03° E | 22 July 1988, 00:42:00 IST | | | | |
$^†$ In case of discrepancy in data between sources, N2YO and NASA NSSDCA is taken as the source of truth. $^‡$ Orbital Longitude is applicable only for Geostationary and Geosynchronous satellites.

## 1990s

From this decade on, Polar Satellite Launch Vehicle (PSLV) arrived that allowed India to become self-reliant in launching most of its remote sensing satellites. However, for heavy geostationary systems, India continued to remain dependent on Europe entirely. Capability to launch geostationary satellites will arrive in next decade.
| Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Launch Date | Launch Vehicle | Launch Site | Details | Details | Details | Details | Details | Details | Details | Details | Details | Refs (Official portal) |
| # | Name | Discipline | COSPAR ID | Launch Mass | Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Semi-Major Axis | Period | Inclination | Longitude$^‡$ | Eccentricity | Epoch Start | Decay Date | Refs (Official portal) |
| # | Name | Discipline | SatCat # | Dry Mass | Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Semi-Major Axis | Period | Inclination | Longitude$^‡$ | Eccentricity | Epoch Start | Decay Date | Refs (Official portal) |
| 15 | INSAT-1D | Communications Earth Sciences | 1990-051A | 1,190 kg (2,620 lb) | 1000 W | 12 June 1990, 11:22:00 IST | Delta 4925 | Air Force Eastern Test Range, Florida | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Identical to INSAT-1A. Still in service. A third stage motor from its launch landed in Australia in 2008. | Archived 12 August 2022 at the Wayback Machine |
| 15 | INSAT-1D | Communications Earth Sciences | 20643 | 550 kg (1,210 lb) | 1000 W | 12 June 1990, 11:22:00 IST | Delta 4925 | Air Force Eastern Test Range, Florida | 35,729.2 km (22,201.1 mi) | 35,974 km (22,353 mi) | 42,160 km (26,200 mi) | 1435.9 minutes | 14.3° | 71.66° E | 0.00245 | 12 June 1990, 01:30:00 IST | – | Archived 12 August 2022 at the Wayback Machine |
| 16 | IRS-1B | Earth Sciences | 1991-061A | 975 kg (2,150 lb) | 600 W | 29 August 1991, 12:18:00 IST | Vostok | Baikonur Cosmodrome, Kazakhstan | Earth observation satellite. Improved version of IRS-1A. | Earth observation satellite. Improved version of IRS-1A. | Earth observation satellite. Improved version of IRS-1A. | Earth observation satellite. Improved version of IRS-1A. | Earth observation satellite. Improved version of IRS-1A. | Earth observation satellite. Improved version of IRS-1A. | Earth observation satellite. Improved version of IRS-1A. | Earth observation satellite. Improved version of IRS-1A. | Earth observation satellite. Improved version of IRS-1A. | Archived 30 July 2017 at the Wayback Machine |
| 16 | IRS-1B | Earth Sciences | 21688 | – | 600 W | 29 August 1991, 12:18:00 IST | Vostok | Baikonur Cosmodrome, Kazakhstan | 892.6 km (554.6 mi) | 928 km (577 mi) | 7,281 km (4,524 mi) | 103.1 minutes | 99.0° | Not Applicable | 0.00385 | 29 August 1991, 01:30:00 IST | – | Archived 30 July 2017 at the Wayback Machine |
| 17 | INSAT-2DT (Formerly ARABSAT-1C) (INSAT-2R) | Communications | 1992-010B | 1,310 kg (2,890 lb) | 1400 W | 27 February 1992, 05:28:10 IST | Ariane-44L H10 | Centre Spatial Guyanais, Kourou | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Launched as Arabsat 1C. Procured in orbit from Arabsat in January 1998. | Archived 31 July 2017 at the Wayback Machine |
| 17 | INSAT-2DT (Formerly ARABSAT-1C) (INSAT-2R) | Communications | 21894 | – | 1400 W | 27 February 1992, 05:28:10 IST | Ariane-44L H10 | Centre Spatial Guyanais, Kourou | 36,122.8 km (22,445.7 mi) | 36,365.4 km (22,596.4 mi) | 42,615 km (26,480 mi) | 1459.2 minutes | 11.6° | 21.41° W | 0.00385 | 29 August 1991, 01:30:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 18 | SROSS-C (SROSS-3) | Astronomy Earth Sciences Space Physics | 1992-028A | 106.1 kg (234 lb) | 45 W | 20 May 1992, 08:30:00 IST | ASLV-D3 | Satish Dhawan Space Centre, Sriharikota | Carried gamma ray astronomy and aeronomy payload. | Carried gamma ray astronomy and aeronomy payload. | Carried gamma ray astronomy and aeronomy payload. | Carried gamma ray astronomy and aeronomy payload. | Carried gamma ray astronomy and aeronomy payload. | Carried gamma ray astronomy and aeronomy payload. | Carried gamma ray astronomy and aeronomy payload. | Carried gamma ray astronomy and aeronomy payload. | Carried gamma ray astronomy and aeronomy payload. | Archived 16 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 18 | SROSS-C (SROSS-3) | Astronomy Earth Sciences Space Physics | 21968 | – | 45 W | 20 May 1992, 08:30:00 IST | ASLV-D3 | Satish Dhawan Space Centre, Sriharikota | 255 km (158 mi) | 429 km (267 mi) | – | 91 minutes | 46.03° | Not Applicable | 0.01295 | 21 May 1992, 01:30:00 IST | 14 July 1992 | Archived 16 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 19 | INSAT-2A | Communications Earth Sciences | 1992-041A | 1,906 kg (4,202 lb) | ~ 1000 W | 10 July 1992, 04:12:19 IST | Ariane-44L H10 | Centre Spatial Guyanais, Kourou | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | First satellite in the second-generation Indian-built INSAT-2 series. Has enhanced capability over INSAT-1 series. Still in service. | Archived 31 July 2017 at the Wayback Machine |
| 19 | INSAT-2A | Communications Earth Sciences | 22027 | 916 kg (2,019 lb) | ~ 1000 W | 10 July 1992, 04:12:19 IST | Ariane-44L H10 | Centre Spatial Guyanais, Kourou | 35,783.1 km (22,234.6 mi) | 35,846.9 km (22,274.2 mi) | 42,186 km (26,213 mi) | 1437.2 minutes | 14.5° | 16.18° E | 0.00381 | 10 July 1992, 01:30:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 20 | INSAT-2B | Communications Earth Sciences | 1993-048B | 1,931 kg (4,257 lb) | ~ 1000 W | 23 July 1993, 04:29:00 IST | Ariane-44L H10+ | Centre Spatial Guyanais, Kourou | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Second satellite in INSAT-2 series. Identical to INSAT-2A. Still in service. | Archived 31 July 2017 at the Wayback Machine |
| 20 | INSAT-2B | Communications Earth Sciences | 22724 | 916 kg (2,019 lb) | ~ 1000 W | 23 July 1993, 04:29:00 IST | Ariane-44L H10+ | Centre Spatial Guyanais, Kourou | 35,812.9 km (22,253.1 mi) | 35,941.2 km (22,332.8 mi) | 42,248 km (26,252 mi) | 1440.4 minutes | 13.0° | 156.74° W | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 21 | IRS-1E | Earth Sciences | Not Applicable | 846 kg (1,865 lb) | 41.5 W | 20 September 1993 | PSLV-D1 | Satish Dhawan Space Centre, Sriharikota | Earth observation satellite. Did not achieve orbit. | Earth observation satellite. Did not achieve orbit. | Earth observation satellite. Did not achieve orbit. | Earth observation satellite. Did not achieve orbit. | Earth observation satellite. Did not achieve orbit. | Earth observation satellite. Did not achieve orbit. | Earth observation satellite. Did not achieve orbit. | Earth observation satellite. Did not achieve orbit. | Earth observation satellite. Did not achieve orbit. | Archived 17 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 21 | IRS-1E | Earth Sciences | Not Applicable | – | 41.5 W | 20 September 1993 | PSLV-D1 | Satish Dhawan Space Centre, Sriharikota | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Archived 17 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 22 | SROSS-C2 | Astronomy Space Physics | 1994-027A | 113 kg (249 lb) | 45 W | 5 May 1994, 05:30:00 IST | ASLV-D4 | Satish Dhawan Space Centre, Sriharikota | Identical to SROSS-C. | Identical to SROSS-C. | Identical to SROSS-C. | Identical to SROSS-C. | Identical to SROSS-C. | Identical to SROSS-C. | Identical to SROSS-C. | Identical to SROSS-C. | Identical to SROSS-C. | Archived 16 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 22 | SROSS-C2 | Astronomy Space Physics | 23099 | – | 45 W | 5 May 1994, 05:30:00 IST | ASLV-D4 | Satish Dhawan Space Centre, Sriharikota | 433 km (269 mi) | 917 km (570 mi) | – | 98.1 minutes | 46.0° | Not Applicable | 0.03431 | 4 May 1994, 01:30:00 IST | 12 July 2001 | Archived 16 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 23 | IRS-P2 | Earth Sciences | 1994-068A | 870 kg (1,920 lb) | 510 W | 15 October 1994, 10:38:00 IST | PSLV-D2 | Satish Dhawan Space Centre, Sriharikota | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Earth observation satellite. Launched by second developmental flight of PSLV. Mission accomplished after 3 years of service in 1997. | Archived 17 August 2022 at the Wayback Machine Archived 30 July 2017 at the Wayback Machine |
| 23 | IRS-P2 | Earth Sciences | 23323 | – | 510 W | 15 October 1994, 10:38:00 IST | PSLV-D2 | Satish Dhawan Space Centre, Sriharikota | 819.2 km (509.0 mi) | 820.8 km (510.0 mi) | 7,190 km (4,470 mi) | 101.1 minutes | 98.8° | Not Applicable | 0.00533 | 15 October 1994, 06:38:00 IST | – | Archived 17 August 2022 at the Wayback Machine Archived 30 July 2017 at the Wayback Machine |
| 24 | INSAT-2C | Communications | 1995-067B | 2,050 kg (4,520 lb) | 1320 W | 7 December 1995, 04:53:00 IST | Ariane-44L H10-3 | Centre Spatial Guyanais, Kourou | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Has additional capabilities such as mobile satellite service, business communication and television outreach beyond Indian boundaries. Still in service. | Archived 31 July 2017 at the Wayback Machine |
| 24 | INSAT-2C | Communications | 23731 | 946 kg (2,086 lb) | 1320 W | 7 December 1995, 04:53:00 IST | Ariane-44L H10-3 | Centre Spatial Guyanais, Kourou | 35,918.4 km (22,318.7 mi) | 35,948.5 km (22,337.4 mi) | 42,304 km (26,286 mi) | 1443.2 minutes | 12.0° | 60.57° E | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 25 | IRS-1C | Earth Sciences | 1995-072A | 1,250 kg (2,760 lb) | 809 W | 28 December 1995, 12:15:00 IST | Molniya-M | Baikonur Cosmodrome, Kazakhstan | Earth observation satellite. Launched from Baikonur Cosmodrome. | Earth observation satellite. Launched from Baikonur Cosmodrome. | Earth observation satellite. Launched from Baikonur Cosmodrome. | Earth observation satellite. Launched from Baikonur Cosmodrome. | Earth observation satellite. Launched from Baikonur Cosmodrome. | Earth observation satellite. Launched from Baikonur Cosmodrome. | Earth observation satellite. Launched from Baikonur Cosmodrome. | Earth observation satellite. Launched from Baikonur Cosmodrome. | Earth observation satellite. Launched from Baikonur Cosmodrome. | Archived 31 July 2017 at the Wayback Machine |
| 25 | IRS-1C | Earth Sciences | 23751 | – | 809 W | 28 December 1995, 12:15:00 IST | Molniya-M | Baikonur Cosmodrome, Kazakhstan | 823 km (511 mi) | 824.9 km (512.6 mi) | 7,194 km (4,470 mi) | 101.2 minutes | 98.69° | Not Applicable | 0.00014 | 28 December 1995, 7:15:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 26 | IRS-P3 (IRS B3) | Astronomy Earth Sciences | 1996-017A | 930 kg (2,050 lb) | 817 W | 21 March 1996, 10:03:00 IST | PSLV-D3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Earth observation satellite. Carries remote sensing payload and an X-ray astronomy payload. Launched by third developmental flight of PSLV | Archived 16 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 26 | IRS-P3 (IRS B3) | Astronomy Earth Sciences | 23827 | – | 817 W | 21 March 1996, 10:03:00 IST | PSLV-D3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 820.9 km (510.1 mi) | 827.1 km (513.9 mi) | 7,195 km (4,471 mi) | 101.2 mins | 98.7° | Not Applicable | 0.00319 | 21 March 1996, 5:23:00 IST | – | Archived 16 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 27 | INSAT-2D | Communications | 1997-027B | 2,079 kg (4,583 lb) | 1650 W | 4 June 1997, 4:50:00 IST | Ariane-44L H10-3 | Centre Spatial Guyanais, Kourou | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Same as INSAT-2C. Inoperable since 4 October 1997 due to power bus anomaly | Archived 30 July 2017 at the Wayback Machine |
| 27 | INSAT-2D | Communications | 24820 | 995 kg (2,194 lb) | 1650 W | 4 June 1997, 4:50:00 IST | Ariane-44L H10-3 | Centre Spatial Guyanais, Kourou | 33,225.6 km (20,645.4 mi) | 35,917.5 km (22,318.1 mi) | 40,942 km (25,440 mi) | 1374.1 mins | 13.5° | 125.76° E | – | – | – | Archived 30 July 2017 at the Wayback Machine |
| 28 | IRS-1D | Earth Sciences | 1997-057A | 920 kg (2,030 lb) | 809 W | 29 September 1997, 10:17:00 IST | PSLV-C1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation satellite. Same as IRS-1C | Earth observation satellite. Same as IRS-1C | Earth observation satellite. Same as IRS-1C | Earth observation satellite. Same as IRS-1C | Earth observation satellite. Same as IRS-1C | Earth observation satellite. Same as IRS-1C | Earth observation satellite. Same as IRS-1C | Earth observation satellite. Same as IRS-1C | Earth observation satellite. Same as IRS-1C | Archived 16 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 28 | IRS-1D | Earth Sciences | 24971 | – | 809 W | 29 September 1997, 10:17:00 IST | PSLV-C1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 748.6 km (465.2 mi) | 823.3 km (511.6 mi) | 7,156 km (4,447 mi) | 100.4 mins | 98.4° | Not Applicable | 0.03719 | 29 September 1997, 6:17:00 IST | – | Archived 16 August 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 29 | INSAT-2E (APR-1) | Communications Earth Sciences | 1999-016A | 2,550 kg (5,620 lb) | – | 2 April 1999, 8:30:00 IST | Ariane-42P H10-3 | Centre Spatial Guyanais, Kourou | Multipurpose communication and meteorological satellite | Multipurpose communication and meteorological satellite | Multipurpose communication and meteorological satellite | Multipurpose communication and meteorological satellite | Multipurpose communication and meteorological satellite | Multipurpose communication and meteorological satellite | Multipurpose communication and meteorological satellite | Multipurpose communication and meteorological satellite | Multipurpose communication and meteorological satellite | Archived 30 July 2017 at the Wayback Machine |
| 29 | INSAT-2E (APR-1) | Communications Earth Sciences | 25666 | 1,150 kg (2,540 lb) | – | 2 April 1999, 8:30:00 IST | Ariane-42P H10-3 | Centre Spatial Guyanais, Kourou | 35,932.1 km (22,327.2 mi) | 36,003.3 km (22,371.4 mi) | 42,338 km (26,308 mi) | 1445 mins | 5.3° | 107.82° E | – | – | – | Archived 30 July 2017 at the Wayback Machine |
| 30 | OceanSat-1 (IRS-P4) | Earth Sciences | 1999-029C | 1,050 kg (2,310 lb) | 750 W | 26 May 1999, 11:52:00 IST | PSLV-C2 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Earth observation satellite. Carries an Ocean Colour Monitor (OCM) and a Multifrequency Scanning Microwave Radiometer (MSMR) | Archived 6 July 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 30 | OceanSat-1 (IRS-P4) | Earth Sciences | 25758 | – | 750 W | 26 May 1999, 11:52:00 IST | PSLV-C2 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 723.9 km (449.8 mi) | 726.3 km (451.3 mi) | 7,096 km (4,409 mi) | 99.1 mins | 98.2° | Not Applicable | 0.00077 | 26 May 1999, 8:12:00 IST | – | Archived 6 July 2022 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
$^†$ In case of discrepancy in data between sources, N2YO and NASA NSSDCA is taken as the source of truth. $^‡$ Orbital Longitude is applicable only for Geostationary and Geosynchronous satellites.

## 2000s

ISRO's workhorse, the PSLV, became the mainstay for successful launches of indigenous satellites from India during this decade. India successfully launched 11 geostationary or geosynchronous satellites during this period, which was equal to the total number of similar launches in the previous 2 decades put together. India's first extra terrestrial mission was also successfully executed during this period.
| Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Launch Date | Launch Vehicle | Launch Site | Details | Details | Details | Details | Details | Details | Details | Details | Details | Refs (Official portal) |
| # | Name | Discipline | COSPAR ID | Launch Mass | On-board Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Semi-Major Axis | Period | Inclination | Longitude$^‡$ | Eccentricity | Epoch Start | Decay Date | Refs (Official portal) |
| # | Name | Discipline | SatCat # | Dry Mass | On-board Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Semi-Major Axis | Period | Inclination | Longitude$^‡$ | Eccentricity | Epoch Start | Decay Date | Refs (Official portal) |
| 31 | INSAT-3B | Communications | 2000-016B | 2,070 kg (4,560 lb) | 1712 W | 22 March 2000, 4:59:00 IST | Ariane-5G | Centre Spatial Guyanais, Kourou | Multipurpose communication: business communication, developmental communication, and mobile communications | Multipurpose communication: business communication, developmental communication, and mobile communications | Multipurpose communication: business communication, developmental communication, and mobile communications | Multipurpose communication: business communication, developmental communication, and mobile communications | Multipurpose communication: business communication, developmental communication, and mobile communications | Multipurpose communication: business communication, developmental communication, and mobile communications | Multipurpose communication: business communication, developmental communication, and mobile communications | Multipurpose communication: business communication, developmental communication, and mobile communications | Multipurpose communication: business communication, developmental communication, and mobile communications | Archived 30 July 2017 at the Wayback Machine |
| 31 | INSAT-3B | Communications | 26108 | 970 kg (2,140 lb) | 1712 W | 22 March 2000, 4:59:00 IST | Ariane-5G | Centre Spatial Guyanais, Kourou | 35,949.3 km (22,337.9 mi) | 35,985.9 km (22,360.6 mi) | 42,338 km (26,308 mi) | 1445.0 mins | 4.3° | 107° W | – | 30 June 2000, 00:59:00 IST | – | Archived 30 July 2017 at the Wayback Machine |
| 32 | GSAT-1 (GramSat-1) | Communications Engineering | 2001-015A | 1,530 kg (3,370 lb) | – | 18 April 2001, 15:43:00 IST | GSLV-D1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Experimental satellite for the first developmental flight of Geosynchronous Satellite Launch Vehicle, GSLV-D1. Did not complete its intended mission due to a shortfall in the GTO apogee | Archived 31 July 2017 at the Wayback Machine |
| 32 | GSAT-1 (GramSat-1) | Communications Engineering | 26745 | – | – | 18 April 2001, 15:43:00 IST | GSLV-D1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 33,853.1 km (21,035.3 mi) | 35,800.5 km (22,245.4 mi) | 41,197 km (25,599 mi) | 1387 mins | 11.2° | 17.37° E | 0.02261 | 18 April 2001, 11:43:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 33 | TES | Earth Sciences | 2001-049A | 1,108 kg (2,443 lb) | – | 22 October 2001, 10:03:00 IST | PSLV-C3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | Experimental satellite to test technologies such as attitude and orbit control system, high-torque reaction wheels, new reaction control system, etc. This satellite carries a 1-meter resolution panchromatic camera, and is considered a prototype for future Indian "spy satellites" | |
| 33 | TES | Earth Sciences | 26957 | – | – | 22 October 2001, 10:03:00 IST | PSLV-C3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 514.6 km (319.8 mi) | 570.2 km (354.3 mi) | 6,913 km (4,296 mi) | 95.3 mins | 97.7° | Not Applicable | 0.00202 | 22 October 2002, 6:03:00 IST | – | |
| 34 | INSAT-3C | Communications | 2002-002A | 2,750 kg (6,060 lb) | 2765 W | 24 January 2002, 5:17:00 IST | Ariane-42L H10-3 | Centre Spatial Guyanais, Kourou | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Designed to augment the existing INSAT capacity for communication and broadcasting and provide continuity of the services of INSAT-2C | Archived 30 July 2017 at the Wayback Machine |
| 34 | INSAT-3C | Communications | 27298 | 1,218 kg (2,685 lb) | 2765 W | 24 January 2002, 5:17:00 IST | Ariane-42L H10-3 | Centre Spatial Guyanais, Kourou | 35,786.9 km (22,236.9 mi) | 35,800.6 km (22,245.5 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.6° | 93.5° E | 0.00245 | – | – | Archived 30 July 2017 at the Wayback Machine |
| 35 | Kalpana-1 (MetSat-1) | Earth Sciences | 2002-043A | 1,060 kg (2,340 lb) | 550 W | 12 September 2002, IST | PSLV-C4 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | First meteorological satellite built by ISRO. Originally named METSAT-1, the satellite was subsequently renamed after Kalpana Chawla, who had perished in the Space Shuttle Columbia disaster | Archived 31 July 2017 at the Wayback Machine |
| 35 | Kalpana-1 (MetSat-1) | Earth Sciences | 27525 | 498 kg (1,098 lb) | 550 W | 12 September 2002, IST | PSLV-C4 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,741.2 km (22,208.6 mi) | 35,845.9 km (22,273.6 mi) | 42,166 km (26,201 mi) | 1436.1 mins | 6.3° | 74° E | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 36 | INSAT-3A | Communications Earth Sciences | 2003-013A | 2,950 kg (6,500 lb) | 3100 W | 10 April 2003, 4:22:00 IST | Ariane-5G | Centre Spatial Guyanais, Kourou | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Multipurpose satellite for communication, broadcasting, and meteorological services (similar to INSAT-2E and Kalpana-1 | Archived 31 July 2017 at the Wayback Machine |
| 36 | INSAT-3A | Communications Earth Sciences | 27714 | 1,348 kg (2,972 lb) | 3100 W | 10 April 2003, 4:22:00 IST | Ariane-5G | Centre Spatial Guyanais, Kourou | 35,874.2 km (22,291.2 mi) | 35,980.2 km (22,357.1 mi) | 42,298 km (26,283 mi) | 1442.9 mins | 1.2° | 87° E | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 37 | GSAT-2 (GramSat-2) | Communications | 2003-018A | 1,900 kg (4,200 lb) | 1400 W | 8 May 2003, 16:58:00 IST | GSLV-D2 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | Experimental satellite for the second developmental test flight of Geosynchronous Satellite Launch Vehicle (GSLV) | |
| 37 | GSAT-2 (GramSat-2) | Communications | 27807 | – | 1400 W | 8 May 2003, 16:58:00 IST | GSLV-D2 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,892.6 km (22,302.6 mi) | 35,936.5 km (22,329.9 mi) | 42,285 km (26,275 mi) | 1442.3 mins | 5° | 199° W | – | – | – | |
| 38 | INSAT-3E | Communications | 2003-043E | 2,775 kg (6,118 lb) | – | 28 September 2003, 4:44:00 IST | Ariane-5G | Centre Spatial Guyanais, Kourou | Communication satellite to augment the existing INSAT System | Communication satellite to augment the existing INSAT System | Communication satellite to augment the existing INSAT System | Communication satellite to augment the existing INSAT System | Communication satellite to augment the existing INSAT System | Communication satellite to augment the existing INSAT System | Communication satellite to augment the existing INSAT System | Communication satellite to augment the existing INSAT System | Communication satellite to augment the existing INSAT System | Archived 31 July 2017 at the Wayback Machine |
| 38 | INSAT-3E | Communications | 27951 | 1,218 kg (2,685 lb) | – | 28 September 2003, 4:44:00 IST | Ariane-5G | Centre Spatial Guyanais, Kourou | 35,576.4 km (22,106.2 mi) | 35,716.3 km (22,193.1 mi) | 42,017 km (26,108 mi) | 1428.6 mins | 2.5° | 126.83° E | – | 28 September 2003 00:44:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 39 | ResourceSat-1 (IRS-P6) | Earth Sciences | 2003-046A | 1,360 kg (3,000 lb) | – | 17 October 2003, 10:24:00 IST | PSLV-C5 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | Earth observation/remote sensing satellite. Intended to supplement and replace IRS-1C and IRS-1D | |
| 39 | ResourceSat-1 (IRS-P6) | Earth Sciences | 28051 | – | – | 17 October 2003, 10:24:00 IST | PSLV-C5 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 824.2 km (512.1 mi) | 829.5 km (515.4 mi) | 7,197 km (4,472 mi) | 101.3 mins | 2.5° | Not Applicable | 0.0016 | 17 October 2003, 6:24:00 IST | – | |
| 40 | GSAT-3 (EduSat) | Communications | 2004-036A | 1,950.5 kg (4,300 lb) | 2040 W | 20 September 2004, 16:01:00 IST | GSLV-F01 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Also designated GSAT-3. India's first exclusive educational satellite | Also designated GSAT-3. India's first exclusive educational satellite | Also designated GSAT-3. India's first exclusive educational satellite | Also designated GSAT-3. India's first exclusive educational satellite | Also designated GSAT-3. India's first exclusive educational satellite | Also designated GSAT-3. India's first exclusive educational satellite | Also designated GSAT-3. India's first exclusive educational satellite | Also designated GSAT-3. India's first exclusive educational satellite | Also designated GSAT-3. India's first exclusive educational satellite | Archived 30 July 2017 at the Wayback Machine |
| 40 | GSAT-3 (EduSat) | Communications | 28417 | 819.4 kg (1,806 lb) | 2040 W | 20 September 2004, 16:01:00 IST | GSLV-F01 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 36,071.1 km (22,413.5 mi) | 36,084.4 km (22,421.8 mi) | 42,446 km (26,375 mi) | 1450.6 mins | 5.2° | 158.51° W | – | – | – | Archived 30 July 2017 at the Wayback Machine |
| 41 | CartoSat-1 | Earth Sciences | 2005-017A | 1,560 kg (3,440 lb) | 1100 W | 5 May 2005, 10:14:00 IST | PSLV-C6 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Earth observation satellite. Provides stereographic in-orbit images with a 2.5-meter resolution | Archived 31 July 2017 at the Wayback Machine |
| 41 | CartoSat-1 | Earth Sciences | 28649 | – | 1100 W | 5 May 2005, 10:14:00 IST | PSLV-C6 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 623.2 km (387.2 mi) | 627.9 km (390.2 mi) | 6,996 km (4,347 mi) | 97.1 mins | 97.9° | Not Applicable | 0.00014 | 5 May 2005, 6:14:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 42 | HamSat | Communications | 2005-017B | 42.5 kg (94 lb) | – | 5 May 2005, 10:14:00 IST | PSLV-C6 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | This is a micro-satellite that was built as a collaboration between Indian and Dutch researchers, for providing satellite-based amateur radio services to the national as well as the international community | |
| 42 | HamSat | Communications | 28650 | – | – | 5 May 2005, 10:14:00 IST | PSLV-C6 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 592 km (368 mi) | 626.4 km (389.2 mi) | 6,980 km (4,340 mi) | 96.7 mins | 97.7° | Not Applicable | 0.00271 | 12 June 1990, 1:30:00 IST | – | |
| 43 | INSAT-4A | Communications | 2005-049A | 3,081 kg (6,792 lb) | 5922 W | 22 December 2005, 4:03:00 IST | Ariane-5GS | Centre Spatial Guyanais, Kourou | Advanced satellite for direct-to-home television broadcasting services | Advanced satellite for direct-to-home television broadcasting services | Advanced satellite for direct-to-home television broadcasting services | Advanced satellite for direct-to-home television broadcasting services | Advanced satellite for direct-to-home television broadcasting services | Advanced satellite for direct-to-home television broadcasting services | Advanced satellite for direct-to-home television broadcasting services | Advanced satellite for direct-to-home television broadcasting services | Advanced satellite for direct-to-home television broadcasting services | |
| 43 | INSAT-4A | Communications | 28911 | 1,386.55 kg (3,056.8 lb) | 5922 W | 22 December 2005, 4:03:00 IST | Ariane-5GS | Centre Spatial Guyanais, Kourou | 35,789.7 km (22,238.7 mi) | 35,798.7 km (22,244.3 mi) | 42,165 km (26,200 mi) | 1436.1 mins | 0.0° | 83° E | – | – | – | |
| 44 | INSAT-4C | Communications | Not Applicable | 2,180 kg (4,810 lb) | – | 10 July 2006 | GSLV-F02 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Geosynchronous communications satellite. Did not achieve orbit | Geosynchronous communications satellite. Did not achieve orbit | Geosynchronous communications satellite. Did not achieve orbit | Geosynchronous communications satellite. Did not achieve orbit | Geosynchronous communications satellite. Did not achieve orbit | Geosynchronous communications satellite. Did not achieve orbit | Geosynchronous communications satellite. Did not achieve orbit | Geosynchronous communications satellite. Did not achieve orbit | Geosynchronous communications satellite. Did not achieve orbit | Archived 31 July 2017 at the Wayback Machine |
| 44 | INSAT-4C | Communications | Not Applicable | – | – | 10 July 2006 | GSLV-F02 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Archived 31 July 2017 at the Wayback Machine |
| 45 | CartoSat-2 (IRS-P7 or, CartoSat-2AT) | Earth Sciences | 2007-001B | 680 kg (1,500 lb) | 900 W | 10 January 2007, 9:27:00 IST | PSLV-C7 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Advanced remote sensing satellite carrying a panchromatic camera capable of providing scene-specific spot images | Archived 30 July 2017 at the Wayback Machine |
| 45 | CartoSat-2 (IRS-P7 or, CartoSat-2AT) | Earth Sciences | 29710 | – | 900 W | 10 January 2007, 9:27:00 IST | PSLV-C7 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 639.1 km (397.1 mi) | 642.2 km (399.0 mi) | 7,011 km (4,356 mi) | 97.4 mins | 97.9° | Not Applicable | 0.00143 | 4 January 2007, 4:27:00 IST | – | Archived 30 July 2017 at the Wayback Machine |
| 46 | SRE-1 | Engineering | 2007-001C | 615 kg (1,356 lb) | – | 10 January 2007, 9:27:00 IST | PSLV-C7 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Experimental satellite intended to demonstrate the technology of an orbiting platform for performing experiments in microgravity conditions. Launched as a co-passenger with CARTOSAT-2. SRE-1 was de-orbited and recovered successfully after 12 days over Bay of Bengal | Archived 31 July 2017 at the Wayback Machine |
| 46 | SRE-1 | Engineering | 29711 | 550 kg (1,210 lb) | – | 10 January 2007, 9:27:00 IST | PSLV-C7 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 486 km (302 mi) | 643 km (400 mi) | - | 95.9 mins | 97.9° | Not Applicable | 0.01131 | 4 January 2007, 4:27:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 47 | INSAT-4B | Communications | 2007-007A | 3,025 kg (6,669 lb) | 5859 W | 12 March 2007, 3:33:00 IST | Ariane-5ECA | Centre Spatial Guyanais, kourou | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Identical to INSAT-4A. Further augments the INSAT capacity for direct-to-home (DTH) television services and other communications. On the night of 7 July 2007 INSAT-4B experienced a power supply glitch which led to switching 'off' of 50 per cent of the transponder capacity (6 Ku and 6 C-Band transponders) | Archived 3 August 2016 at the Wayback Machine |
| 47 | INSAT-4B | Communications | 30793 | – | 5859 W | 12 March 2007, 3:33:00 IST | Ariane-5ECA | Centre Spatial Guyanais, kourou | 35,761.1 km (22,220.9 mi) | 35,827.1 km (22,261.9 mi) | 42,165 km (26,200 mi) | 1436.1 mins | 0.0° | 93.5° E | – | – | – | Archived 3 August 2016 at the Wayback Machine |
| 48 | PS4 with Advanced Avionics Module (AAM) payload | •Avionics | | 185Kg | | 23 April 2007, 10:00 | PSLV-C8 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | | | | | |
| 49 | INSAT-4CR | Communications | 2007-037A | 2,130 kg (4,700 lb) | 3000 W | 2 September 2007, 18:21:00 IST | GSLV-F04 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Identical to INSAT-4C. It carried 12 high-power Ku-band transponders designed to provide direct-to-home (DTH) television services, Digital Satellite News Gathering etc. | Archived 31 July 2017 at the Wayback Machine |
| 49 | INSAT-4CR | Communications | 32050 | – | 3000 W | 2 September 2007, 18:21:00 IST | GSLV-F04 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,780.2 km (22,232.8 mi) | 35,806.9 km (22,249.4 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.0° | 47.5° E | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 50 | CartoSat-2A | Earth Sciences | 2008-021A | 690 kg (1,520 lb) | 900 W | 28 April 2008, 9:24:00 IST | PSLV-C9 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Earth observation/remote sensing satellite. Identical to CARTOSAT-2 | Archived 10 June 2017 at the Wayback Machine |
| 50 | CartoSat-2A | Earth Sciences | 32783 | – | 900 W | 28 April 2008, 9:24:00 IST | PSLV-C9 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 632 km (393 mi) | 649.2 km (403.4 mi) | 7,011 km (4,356 mi) | 97.4 mins | 97.9° | Not Applicable | – | 28 April 2008, 5:24:00 IST | – | Archived 10 June 2017 at the Wayback Machine |
| 51 | IMS-1 (Indian Mini-Satellite-1 or, (Third World Satellite – TWSat) | Earth Sciences | 2008-021D | 83 kg (183 lb) | 220 W | 28 April 2008, 9:24:00 IST | PSLV-C9 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Low-cost microsatellite imaging mission. Launched as co-passenger with CARTOSAT-2A | Archived 10 September 2017 at the Wayback Machine |
| 51 | IMS-1 (Indian Mini-Satellite-1 or, (Third World Satellite – TWSat) | Earth Sciences | 32786 | – | 220 W | 28 April 2008, 9:24:00 IST | PSLV-C9 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 614 km (382 mi) | 629.4 km (391.1 mi) | 6,992 km (4,345 mi) | 97 mins | 97.6° | Not Applicable | – | 28 April 2008, 5:24:00 IST | – | Archived 10 September 2017 at the Wayback Machine |
| 52 | Chandrayaan-1 •Orbiter •Impactor | Planetary Sciences | 2008-052A | 1,380 kg (3,040 lb) | 750 W | 22 October 2008, 6:22:00 IST | PSLV-C11 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | India's first uncrewed lunar probe. It carried 11 scientific instruments built and designed by India, USA, UK, Germany, Norway, Poland and Bulgaria. After a span of 9 months, the lunar craft faced debilitating failure, rendering most on-board systems inoperable. Additionally, faulty orientation of the SAR resulted in failed experiments, which eventually had to be abandoned. | Archived 6 February 2018 at the Wayback Machine |
| 52 | Chandrayaan-1 •Orbiter •Impactor | Planetary Sciences | 33405 | 523 kg (1,153 lb) | 750 W | 22 October 2008, 6:22:00 IST | PSLV-C11 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | ~ 100 km (62 mi) (initial)$^§$ ~ 200 km (120 mi) (final)$^§$ | ~ 100 km (62 mi) (initial)$^§$ ~ 200 km (120 mi) (final)$^§$ | – | – | – | Not Applicable | – | 22 October 2008, 2:22:00 IST | – | Archived 6 February 2018 at the Wayback Machine |
| 53 | RISAT-2 | Earth Sciences | 2009-019A | 300 kg (660 lb) | – | 20 April 2009, 6:45:00 IST | PSLV-C12 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Radar imaging satellite used to monitor India's borders and as part of anti-infiltration and anti-terrorist operations. Launched as a co-passenger with ANUSAT | Archived 30 July 2017 at the Wayback Machine |
| 53 | RISAT-2 | Earth Sciences | 34807 | – | – | 20 April 2009, 6:45:00 IST | PSLV-C12 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 470.6 km (292.4 mi) | 478.5 km (297.3 mi) | 6,845 km (4,253 mi) | 93.9 mins | 41.2° | Not Applicable | – | – | – | Archived 30 July 2017 at the Wayback Machine |
| 54 | AnuSat-1 | Communications | 2009-019B | 40 kg (88 lb) | – | 20 April 2009, 6:45:00 IST | PSLV-C12 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | This was a research micro-satellite designed at Anna University that carries an amateur radio and technology demonstration experiments. It has since been retired | Archived 31 July 2017 at the Wayback Machine |
| 54 | AnuSat-1 | Communications | 34808 | – | – | 20 April 2009, 6:45:00 IST | PSLV-C12 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | – | – | – | 90 mins | – | Not Applicable | – | – | 18 April 2012 | Archived 31 July 2017 at the Wayback Machine |
| 55 | OceanSat-2 | Earth Sciences | 2009-051A | 960 kg (2,120 lb) | 1360 W | 23 September 2009, 11:51:00 IST | PSLV-C14 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Gathers data for oceanographic, coastal and atmospheric applications. Continues mission of Oceansat-1 | Archived 31 July 2017 at the Wayback Machine |
| 55 | OceanSat-2 | Earth Sciences | 35931 | – | 1360 W | 23 September 2009, 11:51:00 IST | PSLV-C14 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 728.2 km (452.5 mi) | 731.9 km (454.8 mi) | 7,101 km (4,412 mi) | 99.3 mins | 98.3° | Not Applicable | – | – | – | Archived 31 July 2017 at the Wayback Machine |
$^†$ In case of discrepancy in data between sources, N2YO and NASA NSSDCA is taken as the source of truth. $^‡$ Orbital Longitude is applicable only for Geostationary and Geosynchronous satellites. $^§$ All orbital data related to Chandrayaan-1 is for its lunar orbit only.

## 2010s

While India had to face failure in launching relatively heavier satellites early on in the decade, it did end up launching 27 geosynchronous/geostationary satellites (17 with indigenous, and 10 with European launchers). In 2010s, it managed to launch most of its geosynchronous/geostationary satellites successfully on its own. This period also saw India enter the exclusive club of nations capable of launching probes to Mars. ISRO also improved upon its student/university outreach by launching multiple pico-, nano- and mini-satellites from various Indian universities. This period was also marked by multiple bilateral collaborations with foreign universities and research organizations. The same decade saw completion of NAVIC, India's regional navigation system.
Increased subcontracting to private vendors across the nation improved launch frequency by a factor of more than 2. India was able to fix glitches and operationalise its Geosynchronous Satellite Launch Vehicle with an indigenous upper stage and operationalise next generation launch vehicle LVM3 with nearly double payload capacity, enabled the country to launch nearly all of its communication satellites. India launched its delayed Moon mission Chandrayaan-2 in 2019 which however failed to conduct soft landing on lunar surface. India also demonstrated capability to destroy "enemy" satellites in orbit. Increased application of India's space capabilities in strengthening its national security was observed.
Substantial increase in budget over the decade, increased payload capacity with increased reliability, increased launch frequency and many "firsts" in this decade had made Indian space program far more visible to world with significant coverage from international media and its hyphenation with leading spacefaring nations. The last launch of the decade marked with completion of 50 launches of PSLV rocket.
| Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Launch Date | Launch Vehicle | Launch Site | Details | Details | Details | Details | Details | Details | Details | Details | Details | Refs (Official portal) |
| # | Name | Discipline | COSPAR ID | Launch Mass | On-board Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Semi-Major Axis | Period | Inclination | Longitude$^‡$ | Eccentricity | Epoch Start | Decay Date | Refs (Official portal) |
| # | Name | Discipline | SatCat # | Dry Mass | On-board Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Semi-Major Axis | Period | Inclination | Longitude$^‡$ | Eccentricity | Epoch Start | Decay Date | Refs (Official portal) |
| 56 | GSAT-4 | Communications | Not Applicable | 2,220 kg (4,890 lb) | – | 15 April 2010 | GSLV-D3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Communications satellite with technology demonstrator features (electric propulsion, Li-ion battery, bus management unit). Failed to reach orbit due to GSLV-D3 failure | Archived 31 July 2017 at the Wayback Machine |
| 56 | GSAT-4 | Communications | Not Applicable | – | – | 15 April 2010 | GSLV-D3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Archived 31 July 2017 at the Wayback Machine |
| 57 | CartoSat-2B | Earth Sciences | 2010-035A | 694 kg (1,530 lb) | 930 W | 12 July 2010, 9:22:00 IST | PSLV-C15 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Earth observation/remote sensing satellite (Identical to CartoSat-2A) | Archived 12 June 2017 at the Wayback Machine |
| 57 | CartoSat-2B | Earth Sciences | 36795 | – | 930 W | 12 July 2010, 9:22:00 IST | PSLV-C15 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 629.9 km (391.4 mi) | 651.4 km (404.8 mi) | 7,011 km (4,356 mi) | 97.4 mins | 97.9° | Not Applicable | – | – | – | Archived 12 June 2017 at the Wayback Machine |
| 58 | StudSat (STUDent SATellite) | Earth Sciences | 2010-035B | < 1 kg (2.2 lb) | – | 12 July 2010, 9:22:00 IST | PSLV-C15 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | India's first pico-satellite (weighing less than 1 kg). It was designed and developed by a team from seven Engineering colleges in Karnataka and Andhra Pradesh | |
| 58 | StudSat (STUDent SATellite) | Earth Sciences | 36796 | – | – | 12 July 2010, 9:22:00 IST | PSLV-C15 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 605.5 km (376.2 mi) | 622.7 km (386.9 mi) | 6,985 km (4,340 mi) | 96.8 mins | 98.0° | Not Applicable | – | – | – | |
| 59 | GSAT-5P (INSAT-4D) | Communications | Not Applicable | 2,310 kg (5,090 lb) | – | 25 December 2010 | GSLV-F06 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | C-band communication satellite, failed to reach orbit due to GSLV-F06 failure | Archived 31 July 2017 at the Wayback Machine |
| 59 | GSAT-5P (INSAT-4D) | Communications | Not Applicable | – | – | 25 December 2010 | GSLV-F06 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Archived 31 July 2017 at the Wayback Machine |
| 60 | ResourceSat-2 | Earth Sciences Technology Applications | 2011-015A | 1,206 kg (2,659 lb) | 1250 W | 20 April 2011, 10:12:00 IST | PSLV-C16 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | This is ISRO's eighteenth remote-sensing satellite, and essentially carries on the work began by ResourceSat-1 | Archived 2 December 2016 at the Wayback Machine |
| 60 | ResourceSat-2 | Earth Sciences Technology Applications | 37387 | – | 1250 W | 20 April 2011, 10:12:00 IST | PSLV-C16 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 825.2 km (512.8 mi) | 828.7 km (514.9 mi) | 7,197 km (4,472 mi) | 101.3 mins | 98.7° | Not Applicable | – | – | – | Archived 2 December 2016 at the Wayback Machine |
| 61 | YouthSat (IMS-2) | Solar Physics Space Physics | 2011-015B | 92 kg (203 lb) | – | 20 April 2011, 10:12:00 IST | PSLV-C16 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Indo-Russian stellar and atmospheric mini-satellite with the participation of university students | Archived 31 July 2017 at the Wayback Machine |
| 61 | YouthSat (IMS-2) | Solar Physics Space Physics | 37388 | – | – | 20 April 2011, 10:12:00 IST | PSLV-C16 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 808.6 km (502.4 mi) | 828.2 km (514.6 mi) | 7,189 km (4,467 mi) | 101.1 mins | 98.6° | Not Applicable | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 62 | GSAT-8 (GramSat-8, or INSAT-4G) | Communications | 2011-022A | 3,093 kg (6,819 lb) | 6242 W | 21 May 2011, 2:08:00 IST | Ariane-5 VA-202 | Centre Spatial Guyanais, Kourou | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Communications satellite carries 24 Ku-band transponders and 2 channel GAGAN payload operating in L1 and L5 band | Archived 26 November 2016 at the Wayback Machine |
| 62 | GSAT-8 (GramSat-8, or INSAT-4G) | Communications | 37605 | 1,426 kg (3,144 lb) | 6242 W | 21 May 2011, 2:08:00 IST | Ariane-5 VA-202 | Centre Spatial Guyanais, Kourou | 35,781 km (22,233 mi) | 35,806.3 km (22,249.0 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.0° | 55° E | – | – | – | Archived 26 November 2016 at the Wayback Machine |
| 63 | GSAT-12 (GramSat-12) | Communications | 2011-034A | 1,410 kg (3,110 lb) | 1430 W | 15 July 2011, 16:48:00 IST | PSLV-C17 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | The GSAT-12 is configured to carry 12 Extended C-band transponders to augment the capacity in the INSAT system for various communication services like Tele-education, Telemedicine and for Village Resource Centres (VRC). Mission life is expected to be about 8 years | Archived 31 July 2017 at the Wayback Machine |
| 63 | GSAT-12 (GramSat-12) | Communications | 37746 | 559 kg (1,232 lb) | 1430 W | 15 July 2011, 16:48:00 IST | PSLV-C17 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,761.6 km (22,221.2 mi) | 35,825.9 km (22,261.2 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.0° | 83° E | – | 15 July 2011, 12:48:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 64 | Megha-Tropiques | Meteorological | 2011-058A | 1,000 kg (2,200 lb) | 1325 W | 12 October 2011, 11:00:00 IST | PSLV-C18 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Megha-Tropiques was developed jointly by ISRO and the French CNES | Megha-Tropiques was developed jointly by ISRO and the French CNES | Megha-Tropiques was developed jointly by ISRO and the French CNES | Megha-Tropiques was developed jointly by ISRO and the French CNES | Megha-Tropiques was developed jointly by ISRO and the French CNES | Megha-Tropiques was developed jointly by ISRO and the French CNES | Megha-Tropiques was developed jointly by ISRO and the French CNES | Megha-Tropiques was developed jointly by ISRO and the French CNES | Megha-Tropiques was developed jointly by ISRO and the French CNES | Archived 31 July 2017 at the Wayback Machine |
| 64 | Megha-Tropiques | Meteorological | 37838 | – | 1325 W | 12 October 2011, 11:00:00 IST | PSLV-C18 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 860.5 km (534.7 mi) | 874.7 km (543.5 mi) | 7,238 km (4,497 mi) | 102.2 mins | 20.0° | Not Applicable | – | 12 October 2011, 7:00:00 IST | – | Archived 31 July 2017 at the Wayback Machine |
| 65 | Jugnu | Earth Sciences Technology Applications | 2011-058B | 3 kg (6.6 lb) | – | 12 October 2011, 11:00:00 IST | PSLV-C18 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Nano-satellite developed by IIT Kanpur | Nano-satellite developed by IIT Kanpur | Nano-satellite developed by IIT Kanpur | Nano-satellite developed by IIT Kanpur | Nano-satellite developed by IIT Kanpur | Nano-satellite developed by IIT Kanpur | Nano-satellite developed by IIT Kanpur | Nano-satellite developed by IIT Kanpur | Nano-satellite developed by IIT Kanpur | |
| 65 | Jugnu | Earth Sciences Technology Applications | 37839 | – | – | 12 October 2011, 11:00:00 IST | PSLV-C18 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 843.9 km (524.4 mi) | 871.4 km (541.5 mi) | 7,228 km (4,491 mi) | 101.9 mins | 20.0° | Not Applicable | – | – | – | |
| 66 | SRMSat | Earth Sciences Technology Applications | 2011-058D | 10.9 kg (24 lb) | – | 12 October 2011, 11:00:00 IST | PSLV-C18 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Nano-satellite developed by SRM Institute of Science and Technology | Nano-satellite developed by SRM Institute of Science and Technology | Nano-satellite developed by SRM Institute of Science and Technology | Nano-satellite developed by SRM Institute of Science and Technology | Nano-satellite developed by SRM Institute of Science and Technology | Nano-satellite developed by SRM Institute of Science and Technology | Nano-satellite developed by SRM Institute of Science and Technology | Nano-satellite developed by SRM Institute of Science and Technology | Nano-satellite developed by SRM Institute of Science and Technology | |
| 66 | SRMSat | Earth Sciences Technology Applications | 37841 | – | – | 12 October 2011, 11:00:00 IST | PSLV-C18 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 855.8 km (531.8 mi) | 873.2 km (542.6 mi) | 7,235 km (4,496 mi) | 102.1 mins | 20.0° | Not Applicable | – | – | – | |
| 67 | RISAT-1 | Earth Sciences | 2012-017A | 1,858 kg (4,096 lb) | 2200 W | 26 April 2012, 5:47:00 IST | PSLV-C19 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | RISAT-1 was India's first indigenous all-weather Radar Imaging Satellite, whose images facilitated agriculture and disaster management | Archived 30 January 2016 at the Wayback Machine |
| 67 | RISAT-1 | Earth Sciences | 38248 | – | 2200 W | 26 April 2012, 5:47:00 IST | PSLV-C19 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 542.2 km (336.9 mi) | 550 km (340 mi) | 6,917 km (4,298 mi) | 95.4 mins | 97.6° | Not Applicable | – | – | – | Archived 30 January 2016 at the Wayback Machine |
| 68 | PS4 With mRESINS Payload | Avionics | 2012-047C | 50 kg (110 lb) | | 9 September 2012 04:23 | PSLV-C21 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | | | | | |
| 68 | PS4 With mRESINS Payload | Avionics | 38757 | | | 9 September 2012 04:23 | PSLV-C21 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 636.4 km (395.4 mi) | 642.6 km (399.3 mi) | 7,010 km (4,360 mi) | 97.4 minutes | 98.3 ° | Not applicable | - | - | - |
| 69 | GSAT-10 | Communications | 2012-051B | 3,400 kg (7,500 lb) | 6474 W | 28 September 2012, 2:48:00 IST | Ariane-5 VA-209 | Centre Spatial Guyanais, Kourou | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | GSAT-10, India's advanced communication satellite, is a high power satellite being inducted into the INSAT system | |
| 69 | GSAT-10 | Communications | 38779 | 1,498 kg (3,303 lb) | 6474 W | 28 September 2012, 2:48:00 IST | Ariane-5 VA-209 | Centre Spatial Guyanais, Kourou | 35,783.3 km (22,234.7 mi) | 35,805.4 km (22,248.4 mi) | 42,165 km (26,200 mi) | 1436.1 mins | 0.1° | 83° E | – | – | – | |
| 70 | SARAL | Earth Sciences | 2013-009A | 407 kg (897 lb) | 906 W | 25 February 2013, 18:01:00 IST | PSLV-C20 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | The Satellite with ARGOS and ALTIKA (SARAL) is a joint Indo-French satellite mission for oceanographic studies | Archived 31 July 2017 at the Wayback Machine |
| 70 | SARAL | Earth Sciences | 39086 | – | 906 W | 25 February 2013, 18:01:00 IST | PSLV-C20 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 791.8 km (492.0 mi) | 792.6 km (492.5 mi) | 7,163 km (4,451 mi) | 100.6 mins | 98.5° | Not Applicable | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 71 | IRNSS-1A | Navigation/Global Positioning | 2013-034A | 1,425 kg (3,142 lb) | 1660 W | 1 July 2013, 23:41:00 IST | PSLV-C22 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | IRNSS-1A is the first of seven satellite in the IRNSS navigational system | Archived 19 March 2015 at the Wayback Machine |
| 71 | IRNSS-1A | Navigation/Global Positioning | 39199 | 614 kg (1,354 lb) | 1660 W | 1 July 2013, 23:41:00 IST | PSLV-C22 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,720.2 km (22,195.5 mi) | 35,864.3 km (22,285.0 mi) | 42,163 km (26,199 mi) | 1436.0 mins | 28.8° | 55.0° E | – | – | – | Archived 19 March 2015 at the Wayback Machine |
| 72 | INSAT-3D | Earth Sciences | 2013-038B | 2,060 kg (4,540 lb) | 1164 W | 26 July 2013, 1:23:00 IST | Ariane-5 ECA VA-214 | Centre Spatial Guyanais, Kourou | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | INSAT-3D is the meteorological Satellite with advanced weather monitoring payloads (6-channel multi-spectral imager, 19-channel sounder, data relay transponder and search-and-rescue transponder) | Archived 31 July 2017 at the Wayback Machine |
| 72 | INSAT-3D | Earth Sciences | 39216 | – | 1164 W | 26 July 2013, 1:23:00 IST | Ariane-5 ECA VA-214 | Centre Spatial Guyanais, Kourou | 35,794 km (22,241 mi) | 35,795.3 km (22,242.2 mi) | 42,165 km (26,200 mi) | 1436.1 mins | 0.0° | 82.0° E | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 73 | GSAT-7 (INSAT-4F) | Communications | 2013-044B | 2,650 kg (5,840 lb) | 3000 W | 30 August 2013, 2:00:00 IST | Ariane-5 ECA VA-215 | Centre Spatial Guyanais, Kourou | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | GSAT-7 is the advanced multi-band communication satellite dedicated for military use. It is currently being exclusively by the navy | Archived 31 July 2017 at the Wayback Machine |
| 73 | GSAT-7 (INSAT-4F) | Communications | 39234 | – | 3000 W | 30 August 2013, 2:00:00 IST | Ariane-5 ECA VA-215 | Centre Spatial Guyanais, Kourou | 35,789.8 km (22,238.8 mi) | 35,798.1 km (22,243.9 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.0° | 74.0° E | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 74 | Mars Orbiter Mission (MOM) (Mangalyaan-1) | Planetary Science | 2013-060A | 1,340 kg (2,950 lb) | 840 W | 5 November 2013, 14:38:00 IST | PSLV-C25 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | The Mars Orbiter Mission (MOM), informally called Mangalyaan is India's first Mars orbiter | Archived 25 November 2016 at the Wayback Machine Archived 25 December 2016 at the Wayback Machine |
| 74 | Mars Orbiter Mission (MOM) (Mangalyaan-1) | Planetary Science | 39370 | 488 kg (1,076 lb) | 840 W | 5 November 2013, 14:38:00 IST | PSLV-C25 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | ~ 366 km (227 mi)$^§$ | ~ 80,000 km (50,000 mi)$^§$ | – | 4602 mins$^§$ | 150°$^§$ | Not Applicable | – | – | – | Archived 25 November 2016 at the Wayback Machine Archived 25 December 2016 at the Wayback Machine |
| 75 | GSAT-14 | Communications | 2014-001A | 1,982 kg (4,370 lb) | 2600 W | 5 January 2014, 16:18:00 IST | GSLV Mk.II-D5 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | GSAT-14 is the twenty third geostationary communication satellite of India. It is intended to replace GSAT-3, and to augment the In-orbit capacity of Extended C and Ku-band transponders | Archived 31 July 2017 at the Wayback Machine |
| 75 | GSAT-14 | Communications | 39498 | – | 2600 W | 5 January 2014, 16:18:00 IST | GSLV Mk.II-D5 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,774.5 km (22,229.2 mi) | 35,813.6 km (22,253.5 mi) | 42,165 km (26,200 mi) | 1436.1 mins | 0.0° | 74.0° E | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 76 | IRNSS-1B | Navigation/Global Positioning | 2014-017A | 1,432 kg (3,157 lb) | 1660 W | 4 April 2014, 17:14:00 IST | PSLV-C24 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | IRNSS-1B is the second of seven satellite in the IRNSS system | IRNSS-1B is the second of seven satellite in the IRNSS system | IRNSS-1B is the second of seven satellite in the IRNSS system | IRNSS-1B is the second of seven satellite in the IRNSS system | IRNSS-1B is the second of seven satellite in the IRNSS system | IRNSS-1B is the second of seven satellite in the IRNSS system | IRNSS-1B is the second of seven satellite in the IRNSS system | IRNSS-1B is the second of seven satellite in the IRNSS system | IRNSS-1B is the second of seven satellite in the IRNSS system | Archived 19 March 2015 at the Wayback Machine |
| 76 | IRNSS-1B | Navigation/Global Positioning | 39635 | – | 1660 W | 4 April 2014, 17:14:00 IST | PSLV-C24 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,700.5 km (22,183.3 mi) | 35,883.1 km (22,296.7 mi) | 42,162 km (26,198 mi) | 1436.0 mins | 29.1° | 55.0° E | – | – | – | Archived 19 March 2015 at the Wayback Machine |
| 77 | IRNSS-1C | Navigation/Global Positioning | 2014-061A | 1,425.4 kg (3,142 lb) | 1660 W | 16 October 2014 | PSLV-C26 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1C is the third satellite in the Indian Regional Navigation Satellite System (IRNSS) | Archived 23 July 2016 at the Wayback Machine |
| 77 | IRNSS-1C | Navigation/Global Positioning | 40269 | – | 1660 W | 16 October 2014 | PSLV-C26 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,715.5 km (22,192.6 mi) | 35,872.6 km (22,290.2 mi) | 42,165 km (26,200 mi) | 1436.1 mins | 3° | 83° E | – | – | – | Archived 23 July 2016 at the Wayback Machine |
| 78 | GSAT-16 | Communications | 2014-078A | 3,181.6 kg (7,014 lb) | 6000 W | 7 December 2014, 2:10:00 IST | Ariane-5 | Centre Spatial Guyanais, Kourou | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | GSAT-16 is the twenty fourth communication satellite of India configured to carry a total of 48 transponders (12 K$_u$, 24 C and 12 C$_{ue}$, each with a bandwidth of 36 MHz), which was the highest number of transponders in a single satellite at that time | Archived 10 August 2016 at the Wayback Machine |
| 78 | GSAT-16 | Communications | 40332 | – | 6000 W | 7 December 2014, 2:10:00 IST | Ariane-5 | Centre Spatial Guyanais, Kourou | 35,762.5 km (22,221.8 mi) | 35,824.7 km (22,260.4 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.1° | 55.0° E | – | – | – | Archived 10 August 2016 at the Wayback Machine |
| 79 | Crew Module Atmospheric Re-entry Experiment | • Re-entry Experiment | | 3775 kg | | 18 December 2014, 04:00 UTC | LVM3-X | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | | | | | | |
| 80 | IRNSS-1D | Navigation/Global Positioning | 2015-018A | 1,425 kg (3,142 lb) | 1660 W | 28 March 2015, 17:19:00 IST | PSLV-C27 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1D is the fourth satellite in the Indian Regional Navigation Satellite System (IRNSS) | Archived 2 April 2016 at the Wayback Machine |
| 80 | IRNSS-1D | Navigation/Global Positioning | 40547 | 603 kg (1,329 lb) | 1660 W | 28 March 2015, 17:19:00 IST | PSLV-C27 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,704.7 km (22,185.9 mi) | 35,885.0 km (22,297.9 mi) | 42,165 km (26,200 mi) | 1436.2 mins | 29.1° | 112° E | – | – | – | Archived 2 April 2016 at the Wayback Machine |
| 81 | GSAT-6 (INSAT-4E) | Communications | 2015-041A | 2,117 kg (4,667 lb) | 3100 W | 27 August 2015, 16:52:00 IST | GSLV Mk.II-D6 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | GSAT-6 is a communication satellite. GSAT- 6 features an unfurlable antenna, largest on board any satellite. Launch of GSLV-D6 also marks the success of indigenously developed upper stage cryogenic engine | Archived 13 May 2016 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 81 | GSAT-6 (INSAT-4E) | Communications | 40880 | 985 kg (2,172 lb) | 3100 W | 27 August 2015, 16:52:00 IST | GSLV Mk.II-D6 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,769.6 km (22,226.2 mi) | 35,818.4 km (22,256.5 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.0° | 83° E | – | – | – | Archived 13 May 2016 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 82 | Astrosat | Space Sciences | 2015-052A | 1,513 kg (3,336 lb) | – | 28 September 2015 | PSLV-C30 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | ASTROSAT is India's first dedicated multi wavelength space observatory | ASTROSAT is India's first dedicated multi wavelength space observatory | ASTROSAT is India's first dedicated multi wavelength space observatory | ASTROSAT is India's first dedicated multi wavelength space observatory | ASTROSAT is India's first dedicated multi wavelength space observatory | ASTROSAT is India's first dedicated multi wavelength space observatory | ASTROSAT is India's first dedicated multi wavelength space observatory | ASTROSAT is India's first dedicated multi wavelength space observatory | ASTROSAT is India's first dedicated multi wavelength space observatory | Archived 28 September 2015 at the Wayback Machine Archived 4 May 2016 at the Wayback Machine |
| 82 | Astrosat | Space Sciences | 40930 | – | – | 28 September 2015 | PSLV-C30 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 642.5 km (399.2 mi) | 655 km (407 mi) | 7,019 km (4,361 mi) | 97.6 mins | 6.0° | Not Applicable | – | – | – | Archived 28 September 2015 at the Wayback Machine Archived 4 May 2016 at the Wayback Machine |
| 83 | GSAT-15 | Communications | 2015-065A | 3,164 kg (6,975 lb) | 6200 W | 11 November 2015, 3:04:00 IST | Ariane 5 VA-227 | Centre Spatial Guyanais, Kourou | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Communications satellite, carries communication transponders in Ku-band and a GPS Aided GEO Augmented Navigation (GAGAN) payload operating in L1 and L5 bands. Weight 3164 kg | Archived 4 September 2016 at the Wayback Machine |
| 83 | GSAT-15 | Communications | 41028 | 1,440 kg (3,170 lb) | 6200 W | 11 November 2015, 3:04:00 IST | Ariane 5 VA-227 | Centre Spatial Guyanais, Kourou | 35,785.66 km (22,236.18 mi) | 35,802.6 km (22,246.7 mi) | 42,165 km (26,200 mi) | 1436.1 mins | 0.1° | 93.5° E | – | – | – | Archived 4 September 2016 at the Wayback Machine |
| 84 | IRNSS-1E | Navigation/Global Positioning | 2016-003A | 1,425 kg (3,142 lb) | 1660 W | 20 January 2016, 9:31:00 IST | PSLV-C31 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1E is the fifth satellite in the Indian Regional Navigation Satellite System (IRNSS) | Archived 14 January 2016 at the Wayback Machine Archived 4 April 2016 at the Wayback Machine |
| 84 | IRNSS-1E | Navigation/Global Positioning | 41241 | 598 kg (1,318 lb) | 1660 W | 20 January 2016, 9:31:00 IST | PSLV-C31 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,709.6 km (22,188.9 mi) | 35,875.2 km (22,291.8 mi) | 42,163 km (26,199 mi) | 1436.0 mins | 28.8° | 111.75° E | – | – | – | Archived 14 January 2016 at the Wayback Machine Archived 4 April 2016 at the Wayback Machine |
| 85 | IRNSS-1F | Navigation/Global Positioning | 2016-015A | 1,425 kg (3,142 lb) | 1660 W | 10 March 2016, 16:01:00 IST | PSLV-C32 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1F is the sixth satellite in the Indian Regional Navigation Satellite System (IRNSS) | Archived 8 March 2016 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 85 | IRNSS-1F | Navigation/Global Positioning | 41384 | 598 kg (1,318 lb) | 1660 W | 10 March 2016, 16:01:00 IST | PSLV-C32 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,700.8 km (22,183.4 mi) | 35,889.2 km (22,300.5 mi) | 42,166 km (26,201 mi) | 1436.2 mins | 4.1° | 32.5° E | – | – | – | Archived 8 March 2016 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 86 | IRNSS-1G | Navigation/Global Positioning | 2016-027A | 1,425 kg (3,142 lb) | 1660 W | 28 April 2016, 12:59 IST | PSLV-C33 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | IRNSS-1G is the seventh and final satellite in the Indian Regional Navigation Satellite System (IRNSS) | Archived 28 April 2016 at the Wayback Machine Archived 24 April 2016 at the Wayback Machine |
| 86 | IRNSS-1G | Navigation/Global Positioning | 41469 | 598 kg (1,318 lb) | 1660 W | 28 April 2016, 12:59 IST | PSLV-C33 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,778.6 km (22,231.8 mi) | 35,808.7 km (22,250.5 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 4.2° | 129° E | – | – | – | Archived 28 April 2016 at the Wayback Machine Archived 24 April 2016 at the Wayback Machine |
| 87 | Cartosat-2C | Earth Sciences | 2016-040A | 737.5 kg (1,626 lb) | 986 W | 22 June 2016, 9:26:00 IST | PSLV-C34 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Earth observation/remote sensing satellite. Identical to CARTOSAT-2,2A and 2B | Archived 20 June 2017 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 87 | Cartosat-2C | Earth Sciences | 41599 | – | 986 W | 22 June 2016, 9:26:00 IST | PSLV-C34 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 504.7 km (313.6 mi) | 526.1 km (326.9 mi) | 6,886 km (4,279 mi) | 94.8 mins | 97.5° | Not Applicable | – | – | – | Archived 20 June 2017 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 88 | SathyabamaSat | Technology Applications | 2016-040B | 1.5 kg (3.3 lb) | – | 22 June 2016, 9:26:00 IST | PSLV-C34 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | A micro-satellite designed and built by the students of Sathyabama University, Chennai, India. This satellite collect data on green house gases in the LEO atmosphere | Archived 9 June 2017 at the Wayback Machine |
| 88 | SathyabamaSat | Technology Applications | 41600 | – | – | 22 June 2016, 9:26:00 IST | PSLV-C34 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 499.2 km (310.2 mi) | 521.8 km (324.2 mi) | 6,881 km (4,276 mi) | 94.7 mins | 97.5° | Not Applicable | – | – | – | Archived 9 June 2017 at the Wayback Machine |
| 89 | Swayam-1 | Communications Technology Applications | 2016-040J | 1 kg (2.2 lb) | – | 22 June 2016, 9:26:00 IST | PSLV-C34 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | A 1-U pico-satellite designed and built by the students of College of Engineering, Pune. This satellite provides point-to-point communications for the HAM community. A second version of the satellite is now being planned | Archived 30 July 2017 at the Wayback Machine |
| 89 | Swayam-1 | Communications Technology Applications | 41607 | – | – | 22 June 2016, 9:26:00 IST | PSLV-C34 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 499.7 km (310.5 mi) | 521.5 km (324.0 mi) | 6,881 km (4,276 mi) | 94.7 mins | 97.5° | Not Applicable | – | – | – | Archived 30 July 2017 at the Wayback Machine |
| 90 | INSAT-3DR | Earth Sciences | 2016-054A | 2,211 kg (4,874 lb) | 1700 W | 8 September 2016, 16:40:00 IST | GSLV-F05 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | An advanced meteorological satellite of India configured with an imaging System and an Atmospheric Sounder | Archived 9 September 2016 at the Wayback Machine Archived 29 November 2016 at the Wayback Machine |
| 90 | INSAT-3DR | Earth Sciences | 41752 | 956 kg (2,108 lb) | 1700 W | 8 September 2016, 16:40:00 IST | GSLV-F05 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,767.2 km (22,224.7 mi) | 35,820.6 km (22,257.9 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.0° | 74.0° E | – | – | – | Archived 9 September 2016 at the Wayback Machine Archived 29 November 2016 at the Wayback Machine |
| 91 | Pratham | Technology Applications | 2016-059A | 10 kg (22 lb) | – | 26 September 2016, 9:12:00 IST | PSLV-C35 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | A mini-satellite build by students and researchers at IIT, Mumbai to study electrical characteristics of the earth's atmosphere | Archived 26 September 2016 at the Wayback Machine |
| 91 | Pratham | Technology Applications | 41783 | – | – | 26 September 2016, 9:12:00 IST | PSLV-C35 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 666.8 km (414.3 mi) | 715.6 km (444.7 mi) | 7,062 km (4,388 mi) | 98.4 mins | 98.2° | Not Applicable | – | – | – | Archived 26 September 2016 at the Wayback Machine |
| 92 | PISat | Technology Applications | 2016-059B | 5.25 kg (11.6 lb) | – | 26 September 2016, 9:12:00 IST | PSLV-C35 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | A micro-satellite designed and built by the students of PES Institute of Technology, Bengaluru at their Crucible of Research and Innovation Laboratory (CRIL) to develop remote sensing applications | Archived 9 June 2017 at the Wayback Machine |
| 92 | PISat | Technology Applications | 41784 | – | – | 26 September 2016, 9:12:00 IST | PSLV-C35 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 666.6 km (414.2 mi) | 713.2 km (443.2 mi) | 7,060 km (4,390 mi) | 98.4 mins | 98.2° | Not Applicable | – | – | – | Archived 9 June 2017 at the Wayback Machine |
| 93 | ScatSat-1 | Earth Sciences | 2016-059H | 377 kg (831 lb) | – | 26 September 2016, 9:12:00 IST | PSLV-C35 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Miniature satellite to provide weather forecasting, cyclone prediction, and tracking services to India | Archived 2 October 2016 at the Wayback Machine |
| 93 | ScatSat-1 | Earth Sciences | 41790 | 110 kg (240 lb) | – | 26 September 2016, 9:12:00 IST | PSLV-C35 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 723.6 km (449.6 mi) | 741.2 km (460.6 mi) | 7,103 km (4,414 mi) | 99.3 mins | 98.1° | – | – | – | – | Archived 2 October 2016 at the Wayback Machine |
| 94 | GSAT-18 | Communications | 2016-060A | 3,425 kg (7,551 lb) | 6474 W | 6 October 2016, 2:00:00 IST | Ariane-5 ECA | Centre Spatial Guyanais, Kourou | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | At 3.4 tons, this was the heaviest satellite owned/being operated by India at the time of its launch | Archived 4 December 2016 at the Wayback Machine |
| 94 | GSAT-18 | Communications | 41793 | 1,480 kg (3,260 lb) | 6474 W | 6 October 2016, 2:00:00 IST | Ariane-5 ECA | Centre Spatial Guyanais, Kourou | 35,760.2 km (22,220.4 mi) | 35,827.7 km (22,262.3 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.1° | 74.0° E | – | – | – | Archived 4 December 2016 at the Wayback Machine |
| 95 | ResourceSat-2A | Earth Sciences | 2016-074A | 1,235 kg (2,723 lb) | – | 7 December 2016, 10:24:00 IST | PSLV-C36 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Its mission is identical to its predecessors (Resourcesat-1 and Resourcesat-2) | Archived 4 October 2017 at the Wayback Machine Archived 10 March 2021 at the Wayback Machine |
| 95 | ResourceSat-2A | Earth Sciences | 41877 | – | – | 7 December 2016, 10:24:00 IST | PSLV-C36 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 826.3 km (513.4 mi) | 827.6 km (514.2 mi) | 7,197 km (4,472 mi) | 101.3 mins | 98.7° | Not Applicable | – | – | – | Archived 4 October 2017 at the Wayback Machine Archived 10 March 2021 at the Wayback Machine |
| 96 | CartoSat-2D | Earth Sciences | 2017-008A | 714 kg (1,574 lb) | – | 15 February 2017, 9:28:00 IST | PSLV-C37 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | ISRO holds the world record for launching the highest number of satellites by a single launch vehicle (104 satellites, including the CartoSat-2D and 2 indigenously designed nano-satellites, INS-1A and INS-1B) | Archived 16 February 2017 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 96 | CartoSat-2D | Earth Sciences | 41948 | – | – | 15 February 2017, 9:28:00 IST | PSLV-C37 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 510.9 km (317.5 mi) | 519.9 km (323.1 mi) | 6,886 km (4,279 mi) | 94.8 mins | 97.5° | Not Applicable | – | – | – | Archived 16 February 2017 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 97 | INS-1A (ISRO Nano-Satellite 1A) | Technology Applications | 2017-008B | 8.4 kg (19 lb) | – | 15 February 2017, 9:28:00 IST | PSLV-C37 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | Archived 31 July 2017 at the Wayback Machine |
| 97 | INS-1A (ISRO Nano-Satellite 1A) | Technology Applications | 41949 | – | – | 15 February 2017, 9:28:00 IST | PSLV-C37 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 500.8 km (311.2 mi) | 515.4 km (320.3 mi) | 6,879 km (4,274 mi) | 94.6 mins | 97.5° | Not Applicable | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 98 | INS-1B (ISRO Nano-Satellite 1B) | Technology Applications | 2017-008G | 9.7 kg (21 lb) | – | 15 February 2017, 9:28:00 IST | PSLV-C37 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | This is one of 2 nano-satellites designed and manufactured by ISRO, are part of the constellation of 104 satellites launched in a single go | Archived 30 July 2017 at the Wayback Machine |
| 98 | INS-1B (ISRO Nano-Satellite 1B) | Technology Applications | 41954 | – | – | 15 February 2017, 9:28:00 IST | PSLV-C37 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 500.7 km (311.1 mi) | 514.8 km (319.9 mi) | 6,878 km (4,274 mi) | 94.6 mins | 97.5° | Not Applicable | – | – | – | Archived 30 July 2017 at the Wayback Machine |
| 99 | South Asia Satellite (GSAT-9) | Communications | 2017-024A | 2,230 kg (4,920 lb) | 3500 W | 5 May 2017, 16:57:00 IST | GSLV Mk.II | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | This satellite is being offered by India as a diplomatic initiative to its neighboring countries (SAARC region) for communication, remote sensing, resource mapping and disaster management applications | Archived 6 May 2017 at the Wayback Machine Archived 15 April 2021 at the Wayback Machine |
| 99 | South Asia Satellite (GSAT-9) | Communications | 42695 | 976 kg (2,152 lb) | 3500 W | 5 May 2017, 16:57:00 IST | GSLV Mk.II | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,782.2 km (22,234.0 mi) | 35,805.8 km (22,248.7 mi) | 42,165 km (26,200 mi) | 1436.1 mins | 0.1° | 97.5° E | – | – | – | Archived 6 May 2017 at the Wayback Machine Archived 15 April 2021 at the Wayback Machine |
| 100 | GSAT-19 (GSAT-19E) | Communications | 2017-031A | 3,136 kg (6,914 lb) | 4500 W | 5 June 2017, 5:28:00 IST | GSLV Mk.III-D1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Maiden orbital flight of GSLV Mk.III. This is the heaviest rocket (and the heaviest satellite) to be launched by ISRO from Indian soil | Archived 5 June 2017 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 100 | GSAT-19 (GSAT-19E) | Communications | 42747 | 1,394 kg (3,073 lb) | 4500 W | 5 June 2017, 5:28:00 IST | GSLV Mk.III-D1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,781.1 km (22,233.3 mi) | 35,806.7 km (22,249.3 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.1° | 82.5° E | – | – | – | Archived 5 June 2017 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 101 | NIUSat | Technology Applications | 2017-036B | 15 kg (33 lb) | 40 W | 23 June 2017, 9:29:00 IST | PSLV-C38 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | This is a satellite designed for remote sensing applications, and built by the students of Noorul Islam University, Kanyakumari | Archived 31 July 2017 at the Wayback Machine |
| 101 | NIUSat | Technology Applications | 42766 | – | 40 W | 23 June 2017, 9:29:00 IST | PSLV-C38 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 502.5 km (312.2 mi) | 526.7 km (327.3 mi) | 6,885 km (4,278 mi) | 94.8 mins | 97.4° | Not Applicable | – | – | – | Archived 31 July 2017 at the Wayback Machine |
| 102 | CartoSat-2E | Earth Sciences | 2017-036C | 712 kg (1,570 lb) | 986 W | 23 June 2017, 9:29:00 IST | PSLV-C38 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This is the 7th satellite in the Cartosat series to be built by ISRO | This is the 7th satellite in the Cartosat series to be built by ISRO | This is the 7th satellite in the Cartosat series to be built by ISRO | This is the 7th satellite in the Cartosat series to be built by ISRO | This is the 7th satellite in the Cartosat series to be built by ISRO | This is the 7th satellite in the Cartosat series to be built by ISRO | This is the 7th satellite in the Cartosat series to be built by ISRO | This is the 7th satellite in the Cartosat series to be built by ISRO | This is the 7th satellite in the Cartosat series to be built by ISRO | Archived 25 October 2020 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 102 | CartoSat-2E | Earth Sciences | 42767 | – | 986 W | 23 June 2017, 9:29:00 IST | PSLV-C38 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 508.4 km (315.9 mi) | 522.2 km (324.5 mi) | 6,886 km (4,279 mi) | 94.8 mins | 97.4° | Not Applicable | – | – | – | Archived 25 October 2020 at the Wayback Machine Archived 31 July 2017 at the Wayback Machine |
| 103 | GSAT-17 | Communications | 2017-040B | 3,477 kg (7,665 lb) | 6200 W | 29 June 2017, 2:45:00 IST | Ariane-5 ECA | Centre Spatial Guyanais, Kourou | This is India's 18th communication (and to date, its heaviest) satellite | This is India's 18th communication (and to date, its heaviest) satellite | This is India's 18th communication (and to date, its heaviest) satellite | This is India's 18th communication (and to date, its heaviest) satellite | This is India's 18th communication (and to date, its heaviest) satellite | This is India's 18th communication (and to date, its heaviest) satellite | This is India's 18th communication (and to date, its heaviest) satellite | This is India's 18th communication (and to date, its heaviest) satellite | This is India's 18th communication (and to date, its heaviest) satellite | |
| 103 | GSAT-17 | Communications | 42815 | 1,480 kg (3,260 lb) | 6200 W | 29 June 2017, 2:45:00 IST | Ariane-5 ECA | Centre Spatial Guyanais, Kourou | 35,771 km (22,227 mi) | 35,817 km (22,256 mi) | 42,164 km (26,199 mi) | 1436.1 mins | 0.1° | 93.5° E | – | – | – | |
| 104 | IRNSS-1H | Navigation/Global Positioning | Not Applicable | 1,425 kg (3,142 lb) | – | 2 September 2017 | PSLV-C39 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | First satellite to be co-designed and built with private sector assistance. Failed to reach orbit | Archived 21 September 2017 at the Wayback Machine Archived 1 September 2017 at the Wayback Machine |
| 104 | IRNSS-1H | Navigation/Global Positioning | Not Applicable | 598 kg (1,318 lb) | – | 2 September 2017 | PSLV-C39 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Archived 21 September 2017 at the Wayback Machine Archived 1 September 2017 at the Wayback Machine |
| 105 | CartoSat-2F | Earth Sciences | 2018-004A | 710 kg (1,570 lb) | – | 12 January 2018, 9:29:00 IST | PSLV-C40 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | ISRO sent 32 satellites, including 3 indigenous ones – CartoSat-2F (the 6th satellite in the Cartosat series to be built by ISRO), MicroSat-TD and INS-1C, on this mission | Archived 23 March 2019 at the Wayback Machine Archived 11 January 2018 at the Wayback Machine |
| 105 | CartoSat-2F | Earth Sciences | 43111 | – | – | 12 January 2018, 9:29:00 IST | PSLV-C40 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | – | – | – | – | – | – | – | – | – | Archived 23 March 2019 at the Wayback Machine Archived 11 January 2018 at the Wayback Machine |
| 106 | MicroSat-TD | Technology Applications | 2018-004T | 132 kg (291 lb) | – | 12 January 2018, 9:29:00 IST | PSLV-C40 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | This is a technology demonstrator, and the forerunner for future satellites in this series. The satellite bus is modular in design and can be fabricated and tested independently of payload | Archived 25 January 2018 at the Wayback Machine |
| 106 | MicroSat-TD | Technology Applications | 43128 | – | – | 12 January 2018, 9:29:00 IST | PSLV-C40 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | – | – | – | – | – | – | – | – | – | Archived 25 January 2018 at the Wayback Machine |
| 107 | INS-1C (ISRO Nano-Satellite 1C) | Technology Applications | TBA | 11 kg (24 lb) | – | 12 January 2018, 9:29:00 IST | PSLV-C40 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | INS-1C, the third satellite in the Indian Nanosatellite series, will be carrying a Miniature Multispectral Technology Demonstration (MMX-TD) Payload from Space Applications Centre (SAC). Data sent by this camera can be utilised for topographical mapping, vegetation monitoring, aerosol scattering studies and cloud studies | |
| 107 | INS-1C (ISRO Nano-Satellite 1C) | Technology Applications | TBA | – | – | 12 January 2018, 9:29:00 IST | PSLV-C40 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | – | – | – | – | – | – | – | – | – | |
| 108 | GSAT-6A | Communications | 2018-027A | 2,117 kg (4,667 lb) | 3119 W | 29 March 2018, 16:56:00 IST | GSLV-F08 | Satish Dhawan Space Centre, Sriharikota | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | Similar to GSAT-6 it is a high power S-band communication satellite configured around I-2K bus. The satellite will also provide a platform for developing technologies such as demonstration of 6 m S-Band Unfurlable Antenna, handheld ground terminals and network management techniques that could be useful in satellite based mobile communication applications. Communication was lost with satellite before final orbit raising maneuver. | |
| 108 | GSAT-6A | Communications | – | – | 3119 W | 29 March 2018, 16:56:00 IST | GSLV-F08 | Satish Dhawan Space Centre, Sriharikota | – | – | – | – | – | – | – | – | – | |
| 109 | IRNSS-1I | Navigation/Global Positioning | 2018-035A | 1,425 kilograms (3,142 lb) | 1671 W | 12 April 2018, 04:04:00 | PSLV-C41 | Satish Dhawan Space Centre, Sriharikota | Eighth satellite of IRNSS | Eighth satellite of IRNSS | Eighth satellite of IRNSS | Eighth satellite of IRNSS | Eighth satellite of IRNSS | Eighth satellite of IRNSS | Eighth satellite of IRNSS | Eighth satellite of IRNSS | Eighth satellite of IRNSS | Archived 6 April 2018 at the Wayback Machine Archived 11 April 2018 at the Wayback Machine |
| 109 | IRNSS-1I | Navigation/Global Positioning | 43286 | 600 kilograms (1,300 lb) | 1671 W | 12 April 2018, 04:04:00 | PSLV-C41 | Satish Dhawan Space Centre, Sriharikota | – | – | – | 1450.9 minutes | 29° | 55.0° E | – | – | – | Archived 6 April 2018 at the Wayback Machine Archived 11 April 2018 at the Wayback Machine |
| 110 | GSAT-29 | High-throughput Communication Satellite | 2018-089A | 3,423 kg (7,546 lb) | | 1 November 2018, 11:38 | GSLV Mk III D2 | Satish Dhawan Space Centre, Sriharikota | | | | | | | | | | Archived 12 November 2018 at the Wayback Machine Archived 14 November 2018 at the Wayback Machine |
| 110 | GSAT-29 | High-throughput Communication Satellite | 43698 | – | | 1 November 2018, 11:38 | GSLV Mk III D2 | Satish Dhawan Space Centre, Sriharikota | | | | 13 hours | 8.9° | | | – | – | Archived 12 November 2018 at the Wayback Machine Archived 14 November 2018 at the Wayback Machine |
| 111 | HySIS | Hyperspectral imaging satellite | 2018-096A | 380 kg (840 lb) | | 29 November 2018, 04:27:30 UTC | PSLV-C43 | Satish Dhawan Space Centre, Sriharikota | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Hyperspectral imaging services for agriculture, forestry, resource mapping, geographical assessment and military applications. | Archived 26 November 2018 at the Wayback Machine |
| 111 | HySIS | Hyperspectral imaging satellite | 43719 | | | 29 November 2018, 04:27:30 UTC | PSLV-C43 | Satish Dhawan Space Centre, Sriharikota | 633.3 km (393.5 mi) | 648.1 km (402.7 mi) | | 97 minutes 26 seconds | 97.95° | Not applicable | | – | – | Archived 26 November 2018 at the Wayback Machine |
| 112 | ExseedSat-1 | Communications technology demonstrator | 2018-099 | 1 kg (2.2 lb) | 1 W | 3 December 2018, 18:34:05 UTC | SpaceX Falcon 9 | Vandenberg Air Force Base, California | India's first privately funded and built satellite | India's first privately funded and built satellite | India's first privately funded and built satellite | India's first privately funded and built satellite | India's first privately funded and built satellite | India's first privately funded and built satellite | India's first privately funded and built satellite | India's first privately funded and built satellite | India's first privately funded and built satellite | |
| 112 | ExseedSat-1 | Communications technology demonstrator | | | 1 W | 3 December 2018, 18:34:05 UTC | SpaceX Falcon 9 | Vandenberg Air Force Base, California | | | | | | Not applicable | | – | – | |
| 113 | GSAT-11 | Communications satellite | 2018-100B | 5,854 kg (12,906 lb) | 13.6 kW | 5 December 2018, 18:16 UTC | Ariane 5-VA246 | Centre Spatial Guyanais, Kourou | Heaviest Indian spacecraft in orbit till date. | Heaviest Indian spacecraft in orbit till date. | Heaviest Indian spacecraft in orbit till date. | Heaviest Indian spacecraft in orbit till date. | Heaviest Indian spacecraft in orbit till date. | Heaviest Indian spacecraft in orbit till date. | Heaviest Indian spacecraft in orbit till date. | Heaviest Indian spacecraft in orbit till date. | Heaviest Indian spacecraft in orbit till date. | Archived 13 July 2019 at the Wayback Machine |
| 113 | GSAT-11 | Communications satellite | 43824 | | 13.6 kW | 5 December 2018, 18:16 UTC | Ariane 5-VA246 | Centre Spatial Guyanais, Kourou | 35,767.8 km (22,225.1 mi) | 35,820.1 km (22,257.6 mi) | | 1,436.1 minutes | 0.0° | 74.0° E | | – | – | Archived 13 July 2019 at the Wayback Machine |
| 114 | GSAT-7A | Military satellite | 2018-105A | 2,250 kg (4,960 lb) | 3.3 kW | 19 December 2018, 10:40 UTC | GSLV Mk.II-F11 | Satish Dhawan Space Centre, Sriharikota | Services for Indian Air Force and Indian Army. | Services for Indian Air Force and Indian Army. | Services for Indian Air Force and Indian Army. | Services for Indian Air Force and Indian Army. | Services for Indian Air Force and Indian Army. | Services for Indian Air Force and Indian Army. | Services for Indian Air Force and Indian Army. | Services for Indian Air Force and Indian Army. | Services for Indian Air Force and Indian Army. | Archived 13 July 2019 at the Wayback Machine Archived 22 March 2021 at the Wayback Machine |
| 114 | GSAT-7A | Military satellite | 43864 | | 3.3 kW | 19 December 2018, 10:40 UTC | GSLV Mk.II-F11 | Satish Dhawan Space Centre, Sriharikota | 35,786.6 km (22,236.8 mi) | 35,799.4 km (22,244.7 mi) | | 1,436.1 minutes | 0.1° | 63.0° E | | – | – | Archived 13 July 2019 at the Wayback Machine Archived 22 March 2021 at the Wayback Machine |
| 115 | Microsat-R | Earth imaging for defense applications (details classified) | 2019-006A | 741.2 kg (1,634 lb) | – | 23 January 2019, 19:37 IST | PSLV-C44 | Satish Dhawan Space Centre, Sriharikota | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | Suspected to have been destroyed in 2019 Indian anti-satellite missile test. | – |
| 115 | Microsat-R | Earth imaging for defense applications (details classified) | 43947 | | – | 23 January 2019, 19:37 IST | PSLV-C44 | Satish Dhawan Space Centre, Sriharikota | Not applicable | Not applicable | Not applicable | Not applicable | Not applicable | Not applicable | Not applicable | – | 27 March 2019 | – |
| 116 | PS4 Stage attached with KalamSAT-V2 | Student satellite | – | 1.26 kg (2.8 lb) | – | 23 January 2019, 19:37 IST | PSLV-C44 | Satish Dhawan Space Centre, Sriharikota | Used PSLV's 4th stage as orbital platform. | Used PSLV's 4th stage as orbital platform. | Used PSLV's 4th stage as orbital platform. | Used PSLV's 4th stage as orbital platform. | Used PSLV's 4th stage as orbital platform. | Used PSLV's 4th stage as orbital platform. | Used PSLV's 4th stage as orbital platform. | Used PSLV's 4th stage as orbital platform. | Used PSLV's 4th stage as orbital platform. | |
| 116 | PS4 Stage attached with KalamSAT-V2 | Student satellite | – | – | – | 23 January 2019, 19:37 IST | PSLV-C44 | Satish Dhawan Space Centre, Sriharikota | – | – | – | – | | Not applicable | – | – | – | |
| 117 | GSAT-31 | High-throughput Telecommunication Satellite | 2019-007B | 2,536 kg (5,591 lb) | 4.7 kW | 6 February 2019, 02:31 IST | Ariane 5-VCA | Centre Spatial Guyanais, Kourou | Replacement of the aging INSAT-4CR. | Replacement of the aging INSAT-4CR. | Replacement of the aging INSAT-4CR. | Replacement of the aging INSAT-4CR. | Replacement of the aging INSAT-4CR. | Replacement of the aging INSAT-4CR. | Replacement of the aging INSAT-4CR. | Replacement of the aging INSAT-4CR. | Replacement of the aging INSAT-4CR. | Archived 10 November 2019 at the Wayback Machine |
| 117 | GSAT-31 | High-throughput Telecommunication Satellite | 44035 | | 4.7 kW | 6 February 2019, 02:31 IST | Ariane 5-VCA | Centre Spatial Guyanais, Kourou | 35,775.7 km (22,230.0 mi) | 35,812.3 km (22,252.7 mi) | | 1,436.1 minutes | 0.1° | 48.0° E | | – | – | Archived 10 November 2019 at the Wayback Machine |
| 118 | EMISAT | Reconnaissance of electromagnetic spectrum (ELINT) | 2019-018A | 436 kg (961 lb) | 800 W | 1 April 2019, 09:27 IST | PSLV-C45 | Satish Dhawan Space Centre, Sriharikota | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Electromagnetic intelligence to track any enemy radars for Indian Armed Forces. | Archived 1 April 2019 at the Wayback Machine |
| 118 | EMISAT | Reconnaissance of electromagnetic spectrum (ELINT) | 44078 | – | 800 W | 1 April 2019, 09:27 IST | PSLV-C45 | Satish Dhawan Space Centre, Sriharikota | 739.3 km (459.4 mi) | 767.6 km (477.0 mi) | | 99.7 minutes | 98.38° | Not applicable | | – | – | Archived 1 April 2019 at the Wayback Machine |
| 119 | PS4 Stage attached with ExseedSat-2, AMSAT, ARIS and AIS payloads | Amateur radio applications, Ionospheric studies and Maritime Satellite applications respectively. | – | | | 1 April 2019, 09:27 IST | PSLV-C45 | Satish Dhawan Space Centre, Sriharikota | Utilization of fourth stage directly as a satellite for experiments. | Utilization of fourth stage directly as a satellite for experiments. | Utilization of fourth stage directly as a satellite for experiments. | Utilization of fourth stage directly as a satellite for experiments. | Utilization of fourth stage directly as a satellite for experiments. | Utilization of fourth stage directly as a satellite for experiments. | Utilization of fourth stage directly as a satellite for experiments. | Utilization of fourth stage directly as a satellite for experiments. | Utilization of fourth stage directly as a satellite for experiments. | | Archived 1 April 2019 at the Wayback Machine |
| 119 | PS4 Stage attached with ExseedSat-2, AMSAT, ARIS and AIS payloads | Amateur radio applications, Ionospheric studies and Maritime Satellite applications respectively. | – | | | 1 April 2019, 09:27 IST | PSLV-C45 | Satish Dhawan Space Centre, Sriharikota | | | | – | – | Not applicable | | – | – | Archived 1 April 2019 at the Wayback Machine |
| 120 | RISAT-2B | Disaster management Radar imaging | 2019-028A | 615 kg (1,356 lb) | | 22 May 2019, 05:30:00 IST | PSLV-CA C46 | Satish Dhawan Space Centre, Sriharikota | Successor to old RISAT-2. | Successor to old RISAT-2. | Successor to old RISAT-2. | Successor to old RISAT-2. | Successor to old RISAT-2. | Successor to old RISAT-2. | Successor to old RISAT-2. | Successor to old RISAT-2. | Successor to old RISAT-2. | Archived 16 August 2019 at the Wayback Machine |
| 120 | RISAT-2B | Disaster management Radar imaging | 44233 | | | 22 May 2019, 05:30:00 IST | PSLV-CA C46 | Satish Dhawan Space Centre, Sriharikota | 558.4 km (347.0 mi) | 563.5 km (350.1 mi) | | 95.7 minutes | 37.0° | Not applicable | – | – | – | Archived 16 August 2019 at the Wayback Machine |
| 121 | Chandrayaan-2 •Orbiter •Vikram Lander •Pragyan Rover | Lunar Exploration | 2019-042A | 3850 kg | 1 kW | 22 July 2019, 09:13:12 UTC | GSLV Mk III M01 | Satish Dhawan Space Centre, Sriharikota | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | India's second lunar exploration mission. Orbital insertion successful, soft landing failed. First operational flight of GSLV Mk III. | Archived 24 July 2021 at the Wayback Machine |
| 121 | Chandrayaan-2 •Orbiter •Vikram Lander •Pragyan Rover | Lunar Exploration | 44441 | 3850 kg | 1 kW | 22 July 2019, 09:13:12 UTC | GSLV Mk III M01 | Satish Dhawan Space Centre, Sriharikota | 100 km (62 mi) | 100 km (62 mi) | - | | 90.0° | Not applicable | | 20 August 2019, 09:02 IST (03:32 UTC) | – | Archived 24 July 2021 at the Wayback Machine |
| 122 | Cartosat-3 | Earth observation | 2019-081A | 1,625 kg (3,583 lb) | 2000 W | 27 November 2019, 09:28:00 IST | PSLV-XL C47 | Satish Dhawan Space Centre, Sriharikota | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | 13 American nano-satellites to be piggybacked along. Cartosat-3 is among optical satellites with highest resolutions in world. | Archived 28 November 2019 at the Wayback Machine |
| 122 | Cartosat-3 | Earth observation | 44804 | | 2000 W | 27 November 2019, 09:28:00 IST | PSLV-XL C47 | Satish Dhawan Space Centre, Sriharikota | 507.2 km (315.2 mi) | 526.6 km (327.2 mi) | | 94.8 minutes | 97.5° | Not applicable | – | – | – | Archived 28 November 2019 at the Wayback Machine |
| 123 | RISAT-2BR1 | Radar imaging | 2019-089F | 628 kg (1,385 lb) | | 11 December 2019 09:55 UTC | PSLV-QL C48 | Satish Dhawan Space Centre, Sriharikota | Has an improved resolution of 0.35 meters. | Has an improved resolution of 0.35 meters. | Has an improved resolution of 0.35 meters. | Has an improved resolution of 0.35 meters. | Has an improved resolution of 0.35 meters. | Has an improved resolution of 0.35 meters. | Has an improved resolution of 0.35 meters. | Has an improved resolution of 0.35 meters. | Has an improved resolution of 0.35 meters. | Archived 13 December 2019 at the Wayback Machine |
| 123 | RISAT-2BR1 | Radar imaging | 44857 | | | 11 December 2019 09:55 UTC | PSLV-QL C48 | Satish Dhawan Space Centre, Sriharikota | 576 km (358 mi) | 576 km (358 mi) | | | 37.0° | Not applicable | – | – | – | Archived 13 December 2019 at the Wayback Machine |
$^†$ In case of discrepancy in data between sources, N2YO and NASA NSSDCA is taken as the source of truth. $^‡$ Orbital Longitude is applicable only for Geostationary and Geosynchronous satellites. $^§$ All orbital data related to Mangalyaan-1 is for its Martian orbit only. $^§$ All orbital data related to Chandrayaan-2 is for its lunar orbit only.

## 2020s

ISRO aims to conduct 50 launches between 2020 and 2024. Besides increasing the launch frequency to 12+ a year, a number of extraterrestrial exploration missions including Aditya L1, Chandrayaan-3, Chandrayaan-4, Lunar Polar Exploration Mission, Shukrayaan-1 and Mars Lander Mission are planned for this decade. A mission to Jupiter after Shukrayaan and a mission to explore beyond Solar System have also been proposed. PSLV is expected to undergo its 100th flight mission in middle of the decade. India's new low cost Small Satellite Launch Vehicle made its maiden flight (SSLV-D1) on August 7, 2022, which unfortunately ended in a failure.SSLV-D2, launched on February 10, 2023, became the first SSLV to launch satellites successfully. The SCE-200 rocket engine, expected to be the powerplant of India's upcoming heavy and super heavy launch systems, is expected to make first flight sometimes in middle of the decade. Conducting an orbital human spaceflight before August 2022 is the highest priority for the agency while the long term goals of the programme include human-occupied space stations and crewed lunar landing.
| Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Payload Details | Launch Date | Launch Vehicle | Launch Site | Details | Details | Details | Details | Details | Details | Details | Details | Details | Refs (Official portal) |
| # | Name | Discipline | COSPAR ID | Launch Mass | Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Semi-Major Axis | Period | Inclination | Longitude$^‡$ | Eccentricity | Epoch Start | Decay Date | Refs (Official portal) |
| # | Name | Discipline | SatCat # | Dry Mass | Power | Launch Date | Launch Vehicle | Launch Site | Periapsis | Apoapsis | Semi-Major Axis | Period | Inclination | Longitude$^‡$ | Eccentricity | Epoch Start | Decay Date | Refs (Official portal) |
| 124 | GSAT-30 | Communications | 2020-005A | 3,357 kg (7,401 lb) | 6000 W | 16 January 2020, 21:05 UTC | Ariane 5 ECA VA-251 | Centre Spatial Guyanais, Kourou | Replacement of INSAT-4A | Replacement of INSAT-4A | Replacement of INSAT-4A | Replacement of INSAT-4A | Replacement of INSAT-4A | Replacement of INSAT-4A | Replacement of INSAT-4A | Replacement of INSAT-4A | Replacement of INSAT-4A | Archived 18 January 2020 at the Wayback Machine |
| 124 | GSAT-30 | Communications | 45026 | | 6000 W | 16 January 2020, 21:05 UTC | Ariane 5 ECA VA-251 | Centre Spatial Guyanais, Kourou | 35,779.1 km (22,232.1 mi) | 35,808.5 km (22,250.4 mi) | 42,164 km (26,199 mi) | 1436.1 minutes | 0.0° | 83.0° E | | | | Archived 18 January 2020 at the Wayback Machine |
| 125 | EOS-01 (RISAT-2BR2) | Earth observation | 2020-081A | 630 kg (1,390 lb) | | 7 November 2020, 09:42 UTC | PSLV-DL C49 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Space based synthetic aperture imaging radar. | Space based synthetic aperture imaging radar. | Space based synthetic aperture imaging radar. | Space based synthetic aperture imaging radar. | Space based synthetic aperture imaging radar. | Space based synthetic aperture imaging radar. | Space based synthetic aperture imaging radar. | Space based synthetic aperture imaging radar. | Space based synthetic aperture imaging radar. | Archived 29 October 2020 at the Wayback Machine Archived 9 August 2022 at the Wayback Machine |
| 125 | EOS-01 (RISAT-2BR2) | Earth observation | 46905 | | | 7 November 2020, 09:42 UTC | PSLV-DL C49 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 576.1 km (358.0 mi) | 582.9 km (362.2 mi) | 6,950 km (4,320 mi) | 96.1 minutes | 36.9° | - | | | | Archived 29 October 2020 at the Wayback Machine Archived 9 August 2022 at the Wayback Machine |
| 126 | CMS-01 (GSAT-12R) | Communications | 2020-099A | 1,425 kg (3,142 lb) | 1500 W | 17 December 2020, 10:11 UTC | PSLV-XL C50 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Extended C-band coverage for mainland India as well as Lakshadweep and A&N Islands. | Archived 17 August 2022 at the Wayback Machine Archived 11 December 2020 at the Wayback Machine |
| 126 | CMS-01 (GSAT-12R) | Communications | 47256 | | 1500 W | 17 December 2020, 10:11 UTC | PSLV-XL C50 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,764.9 km (22,223.3 mi) | 35,823.1 km (22,259.4 mi) | 42,165 km (26,200 mi) | 1436.1 minutes | 0.0° | 83.0° E | | | | Archived 17 August 2022 at the Wayback Machine Archived 11 December 2020 at the Wayback Machine |
| 127 | Sindhu Netra | Earth observation | | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | For use by Indian Navy to keep surveillance over Indian Ocean. | For use by Indian Navy to keep surveillance over Indian Ocean. | For use by Indian Navy to keep surveillance over Indian Ocean. | For use by Indian Navy to keep surveillance over Indian Ocean. | For use by Indian Navy to keep surveillance over Indian Ocean. | For use by Indian Navy to keep surveillance over Indian Ocean. | For use by Indian Navy to keep surveillance over Indian Ocean. | For use by Indian Navy to keep surveillance over Indian Ocean. | For use by Indian Navy to keep surveillance over Indian Ocean. | |
| 127 | Sindhu Netra | Earth observation | | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | | - | | | | |
| 128 | Satish Dhawan Satellite (SDSat) | Studying space radiations and magnetosphere | 2021-015W | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Nanosatellite developed by Space Kidz India to study radiations. Carried 25,000 names and a copy of Bhagvad Gita into space. | Archived 9 August 2022 at the Wayback Machine |
| 128 | Satish Dhawan Satellite (SDSat) | Studying space radiations and magnetosphere | 47721 | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 339.7 km (211.1 mi) | 350.6 km (217.9 mi) | 6,716 km (4,173 mi) | 91.3 minutes | 97.4 ° | - | | | | Archived 9 August 2022 at the Wayback Machine |
| 129 | JITSat | Student satellite | | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Developed by Jeppiaar Institute of Technology as a part of UNITYSat constellation. | Archived 9 August 2022 at the Wayback Machine |
| 129 | JITSat | Student satellite | | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | | - | | | | Archived 9 August 2022 at the Wayback Machine |
| 130 | GHRCESat | Student satellite | | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | Developed by G. H. Raisoni College of Engineering Nagpur as a part of UNITYSat constellation. | | Archived 9 August 2022 at the Wayback Machine |
| 130 | GHRCESat | Student satellite | | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | | - | | | | Archived 9 August 2022 at the Wayback Machine |
| 131 | Sri Shakthi Sat | Student satellite | | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | Developed by Sri Shakthi Institute of Engineering and Technology as a part of UNITYSat constellation. | | Archived 9 August 2022 at the Wayback Machine |
| 131 | Sri Shakthi Sat | Student satellite | | | | 28 February 2021, 03:54 UTC | PSLV-DL C51 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | | - | | | | Archived 9 August 2022 at the Wayback Machine |
| 132 | EOS-03 (GISAT-1) | Earth observation | Not Applicable | 2,268 kg (5,000 lb) | 2280 W | 12 August 2021, 12:13 UTC | GSLV Mk II F10 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | First satellite of GISAT constellation and first Indian real-time earth observation satellite intended in geostationary orbit. Failed to reach orbit as upper-stage of rocket did not ignite. | Archived 7 February 2022 at the Wayback Machine Archived 3 February 2022 at the Wayback Machine |
| 132 | EOS-03 (GISAT-1) | Earth observation | Not Applicable | – | 2280 W | 12 August 2021, 12:13 UTC | GSLV Mk II F10 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Not Applicable | Archived 7 February 2022 at the Wayback Machine Archived 3 February 2022 at the Wayback Machine |
| 133 | EOS-04 (RISAT-1A) | Earth observation | 2022-013A | 1,710 kg (3,770 lb) | 2280 W | 14 February 2022, 00:29 UTC | PSLV-XL C52 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | ISRO Radar Imaging Satellite designed to provide high quality images under all weather conditions for applications such as Agriculture, Forestry & Plantations, Soil Moisture & Hydrology and Flood mapping. | Archived 20 March 2022 at the Wayback Machine Archived 9 February 2022 at the Wayback Machine |
| 133 | EOS-04 (RISAT-1A) | Earth observation | 51656 | | 2280 W | 14 February 2022, 00:29 UTC | PSLV-XL C52 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 526.7 km (327.3 mi) | 543.5 km (337.7 mi) | 6,906 km (4,291 mi) | 95.2 minutes | 97.6° | - | | | | Archived 20 March 2022 at the Wayback Machine Archived 9 February 2022 at the Wayback Machine |
| 134 | United States India Taiwan INSPIRESAT-1 | Student cubesat | 2022-013B | 8.7 kg (19 lb) | | 14 February 2022, 00:29 UTC | PSLV-XL C52 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Developed jointly by Indian Institute of Space Science and Technology (IIST) of India, Laboratory for Atmospheric and Space Physics from the US and National Central University of Taiwan. It is equipped with a compact ionosphere probe to study earth's Ionosphere. | Archived 9 August 2022 at the Wayback Machine Archived 9 February 2022 at the Wayback Machine |
| 134 | United States India Taiwan INSPIRESAT-1 | Student cubesat | 51657 | | | 14 February 2022, 00:29 UTC | PSLV-XL C52 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 526.1 km (326.9 mi) | 541.8 km (336.7 mi) | 6,904 km (4,290 mi) | 95.2 minutes | 97.6° | - | | | | Archived 9 August 2022 at the Wayback Machine Archived 9 February 2022 at the Wayback Machine |
| 135 | India Bhutan INS-2TD | Experimental | 2022-013C | 17.5 kg (39 lb) | | 14 February 2022, 00:29 UTC | PSLV-XL C52 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Joint Indo-Bhutanese technology demonstration satellite which is a precursor to INS-2B, first Bhutanese satellite. | Archived 9 August 2022 at the Wayback Machine Archived 9 February 2022 at the Wayback Machine |
| 135 | India Bhutan INS-2TD | Experimental | 51658 | | | 14 February 2022, 00:29 UTC | PSLV-XL C52 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 525.8 km (326.7 mi) | 540.9 km (336.1 mi) | 6,904 km (4,290 mi) | 95.2 minutes | 97.6° | - | | | | Archived 9 August 2022 at the Wayback Machine Archived 9 February 2022 at the Wayback Machine |
| 136 | Shakuntala (TD-2) | Earth observation | 2022-033S | 15 kg (33 lb) | | 1 April 2022, 16:24 (UTC) | Falcon 9 Block 5 B1061.7 | Cape Canaveral Space Launch Complex 40, Brevard County, Florida | First fully private earth imaging satellite from India by Pixxel. | First fully private earth imaging satellite from India by Pixxel. | First fully private earth imaging satellite from India by Pixxel. | First fully private earth imaging satellite from India by Pixxel. | First fully private earth imaging satellite from India by Pixxel. | First fully private earth imaging satellite from India by Pixxel. | First fully private earth imaging satellite from India by Pixxel. | First fully private earth imaging satellite from India by Pixxel. | First fully private earth imaging satellite from India by Pixxel. | |
| 136 | Shakuntala (TD-2) | Earth observation | 52173 | | | 1 April 2022, 16:24 (UTC) | Falcon 9 Block 5 B1061.7 | Cape Canaveral Space Launch Complex 40, Brevard County, Florida | 438.4 km (272.4 mi) | 452.1 km (280.9 mi) | 6,816 km (4,235 mi) | 93.3 minutes | 97.4 ° | - | | | | |
| 137 | CMS-02 (GSAT-24) | Communications | 2022-067A | 4,181.3 kg (9,218 lb) | 12000 W | 22 June 2022, 21:03 UTC | Ariane 5 ECA VA-257 | Centre Spatial Guyanais, Kourou | First demand driven satellite of NSIL. Operated by M/s Tata Play. | First demand driven satellite of NSIL. Operated by M/s Tata Play. | First demand driven satellite of NSIL. Operated by M/s Tata Play. | First demand driven satellite of NSIL. Operated by M/s Tata Play. | First demand driven satellite of NSIL. Operated by M/s Tata Play. | First demand driven satellite of NSIL. Operated by M/s Tata Play. | First demand driven satellite of NSIL. Operated by M/s Tata Play. | First demand driven satellite of NSIL. Operated by M/s Tata Play. | First demand driven satellite of NSIL. Operated by M/s Tata Play. | Archived 20 June 2022 at the Wayback Machine Archived 13 July 2022 at the Wayback Machine |
| 137 | CMS-02 (GSAT-24) | Communications | 52903 | 1,774.9 kg (3,913 lb) | 12000 W | 22 June 2022, 21:03 UTC | Ariane 5 ECA VA-257 | Centre Spatial Guyanais, Kourou | 35,651.2 km (22,152.6 mi) | 35,777.4 km (22,231.0 mi) | 42,085 km (26,150 mi) | 1432 minutes | 0.1° | - | | | | Archived 20 June 2022 at the Wayback Machine Archived 13 July 2022 at the Wayback Machine |
| 138 | PS4 with POEM-I (PSLV Orbital Experimental Module) Payload | Experimental rocket stage with payloads | 2022-072E | | | 30 June 2022, 12:32 (UTC) | PSLV-XL C53 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | POEM hosts six payloads. The PSLV Orbital Experimental Module (POEM) also known as PS4 Orbital Platform (PS4-OP) utilizes the spent PSLV fourth stage (PS4) to provide a long duration in-orbit platform for hosting payloads. | |
| 138 | PS4 with POEM-I (PSLV Orbital Experimental Module) Payload | Experimental rocket stage with payloads | 52939 | | | 30 June 2022, 12:32 (UTC) | PSLV-XL C53 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 531.6 km (330.3 mi) | 578.9 km (359.7 mi) | 6,926 km (4,304 mi) | 95.6 minutes | 10.0 ° | - | | | | |
| 139 | EOS 02 (Microsat-2A) | Earth observation | | 145 kg (320 lb) | 350 W | 7 August 2022, 03:48 UTC | SSLV-D1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | EOS02 was an optical earth observation satellite with a transmission speed of 32 mpps in x band. Due to sensor failure coupled with shortcomings of onboard software, the SSLVs VTM stage as well as the two satellite payloads were injected into an unstable transatmospheric Earth orbit measuring 356×76 km and subsequently destroyed upon reentry. | |
| 139 | EOS 02 (Microsat-2A) | Earth observation | | | 350 W | 7 August 2022, 03:48 UTC | SSLV-D1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | - | - | - | - | - | - | - | - | - | |
| 140 | AzaadiSAT | Student satellite (Earth observation) | | 8 kg (18 lb) | | 7 August 2022, 03:48 UTC | SSLV-D1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 8U CubeSat by SpaceKidz India. | 8U CubeSat by SpaceKidz India. | 8U CubeSat by SpaceKidz India. | 8U CubeSat by SpaceKidz India. | 8U CubeSat by SpaceKidz India. | 8U CubeSat by SpaceKidz India. | 8U CubeSat by SpaceKidz India. | 8U CubeSat by SpaceKidz India. | 8U CubeSat by SpaceKidz India. | | |
| 140 | AzaadiSAT | Student satellite (Earth observation) | | | | 7 August 2022, 03:48 UTC | SSLV-D1 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | - | - | - | - | - | - | - | - | - | |
| 141 | EOS-06 (Oceansat-3) | Oceanography | 2022-158A | 1,117 kg (2,463 lb) | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | |
| 141 | EOS-06 (Oceansat-3) | Oceanography | 54361 | | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 741.6 km (460.8 mi) | 743.7 km (462.1 mi) | 7,113 km (4,420 mi) | 99.5 minutes | 98.4 ° | - | | | | |
| 142 | India Bhutan INS-2B (India-BhutanSat) | Earth observation | 2022-158E | 18.28 kg (40.3 lb) | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | Multispectral optical imaging satellite jointly developed and operated by India and Bhutan. | | |
| 142 | India Bhutan INS-2B (India-BhutanSat) | Earth observation | 54365 | | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 481 km (299 mi) | 492.9 km (306.3 mi) | 6,857 km (4,261 mi) | 94.2 minutes | 97.4 ° | - | | | | |
| 143 | TD-1 Anand | Experimental | 2022-158F | 16.51 kg (36.4 lb) | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Earth observation satellite by Pixxel. | Earth observation satellite by Pixxel. | Earth observation satellite by Pixxel. | Earth observation satellite by Pixxel. | Earth observation satellite by Pixxel. | Earth observation satellite by Pixxel. | Earth observation satellite by Pixxel. | Earth observation satellite by Pixxel. | Earth observation satellite by Pixxel. | | |
| 143 | TD-1 Anand | Experimental | 54366 | | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 485.6 km (301.7 mi) | 496.7 km (308.6 mi) | 6,862 km (4,264 mi) | 94.3 minutes | 97.4 ° | - | | | | |
| 144 | Thybolt-1 | Communications | 2022-158D | 0.5 kg (1.1 lb) | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | | |
| 144 | Thybolt-1 | Communications | 54364 | | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 480.3 km (298.4 mi) | 492.2 km (305.8 mi) | 6,857 km (4,261 mi) | 94.2 minutes | 97.4 ° | - | | | | |
| 145 | Thybolt-2 | Communications | 2022-158D | 0.5 kg (1.1 lb) | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | Communication technology demonstrator by Dhruva Space. | | |
| 145 | Thybolt-2 | Communications | 54363 | | | 26 November 2022, 06:26 UTC | PSLV-XL C54 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 479.9 km (298.2 mi) | 491.9 km (305.7 mi) | 6,856 km (4,260 mi) | 94.2 minutes | 97.4 ° | - | | | | |
| 146 | EOS-07 | Earth observation | 2023-019A | 156.3 kg (345 lb) | 357 W | 10 February 2023 03:48 (UTC) | SSLV-D2 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | Equipped with mm-Wave humidity sounder and spectrum monitoring payload. | |
| 146 | EOS-07 | Earth observation | 55562 | | 357 W | 10 February 2023 03:48 (UTC) | SSLV-D2 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 435 km (270 mi) | 446 km (277 mi) | 6,811 km (4,232 mi) | 93.2 minutes | 37.2 ° | - | | | | |
| 147 | AzaadiSAT-2 | Student satellite (Earth observation) | 2013-019B | 7.3 kg (16 lb) | | 10 February 2023 03:48 (UTC) | SSLV-D2 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Students satellite by SpaceKidz India for amateur radio communication. | Students satellite by SpaceKidz India for amateur radio communication. | Students satellite by SpaceKidz India for amateur radio communication. | Students satellite by SpaceKidz India for amateur radio communication. | Students satellite by SpaceKidz India for amateur radio communication. | Students satellite by SpaceKidz India for amateur radio communication. | Students satellite by SpaceKidz India for amateur radio communication. | Students satellite by SpaceKidz India for amateur radio communication. | Students satellite by SpaceKidz India for amateur radio communication. | | |
| 147 | AzaadiSAT-2 | Student satellite (Earth observation) | 55563 | | | 10 February 2023 03:48 (UTC) | SSLV-D2 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 401.5 km (249.5 mi) | 423.7 km (263.3 mi) | 6,783 km (4,215 mi) | 92.7 minutes | 37.2 ° | - | | | | |
| 148 | PS4 with POEM-II (PSLV Orbital Experimental Module) | Experimental rocket stage with payloads | 2023-057A | | | 22 April 2023, 08:50 (UTC) | PSLV-CA C55 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | Included research payloads from private Indian space industries namely, ARIS 2, PiLoT, ARKA200, DSOL-DU, DSOD-3U & 6U | |
| 148 | PS4 with POEM-II (PSLV Orbital Experimental Module) | Experimental rocket stage with payloads | 56308 | | | 22 April 2023, 08:50 (UTC) | PSLV-CA C55 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 593.2 km (368.6 mi) | 626.7 km (389.4 mi) | 6,980 km (4,340 mi) | 96.7 minutes | 9.9 ° | - | | | | |
| 149 | NVS-01 (IRNSS-1J) | Navigation satellite | 2023-076A | 2,232 kg (4,921 lb) | 2400 W | 29 May 2023, 10:42 (UTC) | GSLV Mk II F12 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | First of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. | |
| 149 | NVS-01 (IRNSS-1J) | Navigation satellite | 56759 | | 2400 W | 29 May 2023, 10:42 (UTC) | GSLV Mk II F12 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 35,775.5 km (22,229.9 mi) | 35,813.2 km (22,253.3 mi) | 42,165 km (26,200 mi) | 1436.1 minutes | 4.9 ° | - | | | | |
| 150 | Chandrayaan-3 •Orbiter •Vikram Lander •Pragyan Rover | Lunar Exploration | 2023-098C | 3900 kg | 1 kW | 14 July 2023, 09:05:17 (UTC) | LVM3 M04 | Satish Dhawan Space Centre, Sriharikota | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | India's third lunar exploration mission. Orbital insertion successful, soft landing successful, roving successful, hop experiment successful, return to earth successful. | |
| 150 | Chandrayaan-3 •Orbiter •Vikram Lander •Pragyan Rover | Lunar Exploration | 57320 | 3900 kg | 1 kW | 14 July 2023, 09:05:17 (UTC) | LVM3 M04 | Satish Dhawan Space Centre, Sriharikota | 170 km (110 mi) | 36,500 km (22,700 mi) | - | | 90.0° | Not applicable | | 5 August 2023 | 22 August 2024 | |
| 151 | Aditya-L1 | Solar coronal observation spacecraft | 2023-132A | 1,475 kg (3,252 lb) | | 2 September 2023, 06:20 (UTC) | PSLV-XL, PSLV-C57 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | First solar observation satellite of India. Designed to operate on a Halo orbit around L1 point | |
| 151 | Aditya-L1 | Solar coronal observation spacecraft | 57754 | | | 2 September 2023, 06:20 (UTC) | PSLV-XL, PSLV-C57 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Halo orbit around L1 point | | | 177.86 days | | - | | | | |
| 152 | XPoSat | X-ray astronomy | 2024-001A | 480 kg (1,060 lb) | 1260 W | 1 January 2024, 03:40 (UTC) | PSLV-DL C58 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | First dedicated X-ray satellite of the nation dedicated to study X-ray polarization. | |
| 152 | XPoSat | X-ray astronomy | 58694 | 144 kg (317 lb) | 1260 W | 1 January 2024, 03:40 (UTC) | PSLV-DL C58 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | 650 km (400 mi) | 650 km (400 mi) | 650 km (400 mi) | 90.0 minutes | 3° | - | | | | |
| 153 | INSAT-3DS | Earth Observation | | 2,275 kg (5,016 lb) | 1164 W | 17 February 2024, 12:05(UTC) | GSLV-F14 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | The satellite is a follow on of INSAT-3DR mission. | The satellite is a follow on of INSAT-3DR mission. | The satellite is a follow on of INSAT-3DR mission. | The satellite is a follow on of INSAT-3DR mission. | The satellite is a follow on of INSAT-3DR mission. | The satellite is a follow on of INSAT-3DR mission. | The satellite is a follow on of INSAT-3DR mission. | The satellite is a follow on of INSAT-3DR mission. | The satellite is a follow on of INSAT-3DR mission. | |
| 153 | INSAT-3DS | Earth Observation | | 907 kg (2,000 lb) | 1164 W | 17 February 2024, 12:05(UTC) | GSLV-F14 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | 19.35° | 74°E | | | | |
| 154 | EOS-08 | Earth Observation | | 175.5 kg (387 lb) | 357 W | 17 February 2024, 12:05(UTC) | SSLV-D3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | India's third generation oceanography satellite. | |
| 154 | EOS-08 | Earth Observation | | | 357 W | 17 February 2024, 12:05(UTC) | SSLV-D3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | Q | | | | 37.4°E | | | | |
| 155 | SR-0 DEMOSAT | Earth Observation | | 0.2 kg (0.44 lb) | | 17 February 2024, 12:05(UTC) | SSLV-D3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Demonstration satellite. | Demonstration satellite. | Demonstration satellite. | Demonstration satellite. | Demonstration satellite. | Demonstration satellite. | Demonstration satellite. | Demonstration satellite. | Demonstration satellite. | | |
| 155 | SR-0 DEMOSAT | Earth Observation | | | | 17 February 2024, 12:05(UTC) | SSLV-D3 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | | 37.4°E | | | | |
| 156 | CMS-03 (GSAT-20) | Communications | 2022-214A | 4,700 kg (10,400 lb) | 12000 W | 18 November 2024, 18:30 UTC | Falcon 9 | Cape Canaveral Space Force Station, Florida | Second demand driven satellite of NSIL. Operated by M/s DishTV. | Second demand driven satellite of NSIL. Operated by M/s DishTV. | Second demand driven satellite of NSIL. Operated by M/s DishTV. | Second demand driven satellite of NSIL. Operated by M/s DishTV. | Second demand driven satellite of NSIL. Operated by M/s DishTV. | Second demand driven satellite of NSIL. Operated by M/s DishTV. | Second demand driven satellite of NSIL. Operated by M/s DishTV. | Second demand driven satellite of NSIL. Operated by M/s DishTV. | Second demand driven satellite of NSIL. Operated by M/s DishTV. | |
| 156 | CMS-03 (GSAT-20) | Communications | 52983 | | 12000 W | 18 November 2024, 18:30 UTC | Falcon 9 | Cape Canaveral Space Force Station, Florida | | | | | 68° | - | | | | |
| 157 | SPADEX (SDX01 + SDX02) | Experimental | 2024-253A | 440 kg (970 lb) | 1260 W | 30 December 2024, 16:30 (UTC) | PSLV-CA C60 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Attempt first docking of two Indian probes in space. | Attempt first docking of two Indian probes in space. | Attempt first docking of two Indian probes in space. | Attempt first docking of two Indian probes in space. | Attempt first docking of two Indian probes in space. | Attempt first docking of two Indian probes in space. | Attempt first docking of two Indian probes in space. | Attempt first docking of two Indian probes in space. | Attempt first docking of two Indian probes in space. | |
| 158 | SPADEX (SDX01 + SDX02) | Experimental | 2024-253A | 440 kg (970 lb) | 1260 W | 30 December 2024, 16:30 (UTC) | PSLV-CA C60 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | 55° | - | | | | |
| 159 | NVS-02 (IRNSS-1K) | Navigation satellite | 2025-020A | 2,232 kg (4,921 lb) | 3000 W | 29 January 2024, 00:53 (UTC) | GSLV Mk II F15 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | Second of second generation navigation satellites in India's NavIC constellation. Includes payloads operating in L1, L5 & S bands and works on indigenous rubidium atomic clock. The launch also marked ISRO's 100th launch from the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh | |
| 159 | NVS-02 (IRNSS-1K) | Navigation satellite | | | 3000 W | 29 January 2024, 00:53 (UTC) | GSLV Mk II F15 | Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh | | | | | 111.75 °E | - | | | | |

## Forthcoming

Following table lists Indian satellites in development and due for launch in near future.
| Satellite | Date planned | Launch vehicle | Launch Site | Type | Orbit |
| GISAT-2 | TBA | GSLV MkII | SDSC | Multispectral and hyperspectral Earth imaging satellite | GEO |
| GSAT-32 | TBA | GSLV MkII | SDSC | Communications satellite | GEO |
| GSAT-7R | TBA | GSLV MkII | SDSC | Military communications satellite | GEO |
| GSAT-7C | TBA | GSLV MkII | SDSC | Military communications satellite | GEO |
| DRSS-1 | TBA | GSLV MKII | SDSC | Data relay and satellite tracking system | GEO |
| DRSS-2 | TBA | LVM3 | SDSC | Data relay and satellite tracking system | GEO |
| NISAR | Q1 2025 | GSLV MkII | SDSC | Synthetic aperture radar on Earth observation satellite | GEO |
| DISHA × 2 | 2025 | PSLV | SDSC | Aeronomy satellite | LEO |
| TDS-01 | 2025 | TBD | | Technology demonstrator for Indian made Electric propulsion, TWTA and atomic clock. | |
| Venus Orbiter Mission | NET 2026 | GSLV MkII | SDSC | Venus exploration | Cytherion |
| Lunar Polar Exploration Mission | NET 2026 | H3 | LA-Y, Tanegashima | Lunar exploration | Selenocentric |
| Mars Orbiter Mission 2 | NET 2026 | GSLV MkII | SDSC | Mars exploration | Martian |
| AstroSat-2 | TBD | PSLV | SDSC | Space telescope | LEO |
| GSAT-22 | TBD | TBD | TBD | Communications satellite | GEO |
| GSAT-23 | TBD | TBD | TBD | Communications satellite | GEO |

## Launch statistics

Following statistics are on the basis of number of satellites launched that were built-in or were to be operated by India. It does not account number of launch vehicles used or special orbital missions like re-entry that aren't taken into account as satellites. It also does not account foreign satellites launched by India.

### Decade wise

The following bar chart lists number of Indian satellites launched decade-wise.
| Decade | Country of origin of launch vehicle | Country of origin of launch vehicle | Country of origin of launch vehicle | Country of origin of launch vehicle | Country of origin of launch vehicle | Country of origin of launch vehicle | Country of origin of launch vehicle | Country of origin of launch vehicle | Total | Total |
| Decade | India | India | European Union | European Union | Soviet Union/ Russia | Soviet Union/ Russia | United States | United States | | Total | Total |
| Decade | Success | Failure | Success | Failure | Success | Failure | Success | Failure | Success | Failure |
| 1970s | 0 | 1 | 0 | 0 | 2 | 0 | 0 | 0 | 2 | 1 |
| 1980s | 3 | 2 | 2 | 0 | 2 | 0 | 2 | 0 | 9 | 2 |
| 1990s | 6 | 1 | 6 | 0 | 2 | 0 | 1 | 0 | 15 | 1 |
| 2000s | 18 | 1 | 6 | 0 | 0 | 0 | 0 | 0 | 24 | 1 |
| 2010s | 54 | 3 | 10 | 0 | 0 | 0 | 1 | 0 | 65 | 3 |
| 2020s | 31 | 2 | 2 | 0 | 0 | 0 | 1 | 0 | 34 | 3 |
| Total | 112 | 10 | 26 | 0 | 6 | 0 | 5 | 0 | 149 | 10 |
* India (success)
* India (failure)
* Europe (success)
* Europe (failure)
* USSR/Russia (success)
* USSR/Russia (failure)
* USA (success)
* USA (failure)

### Country wise

The following bar chart lists the number of satellites launched based on the origin of the launch vehicle
| Country of origin of launch system | Number of Indian satellites launched | Number of Indian satellites launched | Number of Indian satellites launched |
| Country of origin of launch system | Success | Failure | Total |
| India | 112 | 10 | 122 |
| European Union | 26 | 0 | 26 |
| Soviet Union/ Russia | 6 | 0 | 6 |
| United States | 5 | 0 | 5 |
| Total | 149 | 10 | 159 |
* India (success)
* India (failure)
* Europe (success)
* Europe (failure)
* USSR/Russia (success)
* USSR/Russia (failure)
* USA (success)
* USA (failure)

## Other orbital and suborbital spacecraft

| Spacecraft | Discipline | Date | Launch mass | Launch vehicle | Launch Site | Orbit | Deorbited | Ref |
| Launched |||||||||
| SRE-1 | Re-entry experiment | 10 January 2007, 03:54 UTC | 550 kg (1,210 lb) | PSLV-G C7 | Satish Dhawan Space Centre, Sriharikota | 485 km (301 mi) x 639 km (397 mi) | 22 January 2007, 04:16 UTC | |
| Moon Impact Probe (Chandrayaan-1) | Lunar impactor | 22 October 2008, 00:52 UTC | 34 kg (75 lb) | PSLV-XL C11 | Satish Dhawan Space Centre, Sriharikota | 100 km (62 mi) x 100 km (62 mi) (Selenocentric) | 14 November 2008, 20:06 | Archived 8 July 2019 at the Wayback Machine |
| Crew Module Atmospheric Re-entry Experiment | Re-entry experiment | 18 December 2014, 04:00 UTC | 3,775 kg (8,322 lb) | LVM3-X | Satish Dhawan Space Centre, Sriharikota | 126 km (78 mi) apogee to 1,600 km (990 mi) range (Sub-orbital) | 18 December 2014, 04:15 UTC | Archived 16 August 2022 at the Wayback Machine |
| Vikram lander (Chandrayaan-2) | Soft lunar landing | 20 August 2019, 03:32 UTC | 1,471 kg (3,243 lb) | GSLV Mark III M1 | Satish Dhawan Space Centre, Sriharikota | 100 km (62 mi) x 100 km (62 mi) (Selenocentric) | 6 September 2019, 20:23 UTC | Archived 4 July 2019 at the Wayback Machine |
| Pragyan (Chandrayaan-2) (Chandrayaan-2) | Lunar rover | 20 August 2019, 03:32 UTC | 27 kg (60 lb) | GSLV Mark III M1 | Satish Dhawan Space Centre, Sriharikota | 100 km (62 mi) x 100 km (62 mi) (Selenocentric) | 6 September 2019, 20:23 UTC | Archived 4 July 2019 at the Wayback Machine |
| Vikram lander (Chandrayaan-3) | Soft lunar landing | 5 August 2023 | 1,471 kg (3,243 lb) | LVM3 M4 | Satish Dhawan Space Centre, Sriharikota | 113 km (70 mi) x 157 km (98 mi) (Selenocentric) | 23 August 2023, 12:33 (UTC) | |
| Pragyan (Chandrayaan-3) (Chandrayaan-3) | Lunar rover | 5 August 2023 | 27 kg (60 lb) | LVM3 M4 | Satish Dhawan Space Centre, Sriharikota | 113 km (70 mi) x 157 km (98 mi) (Selenocentric) | 23 August 2023, 12:33 (UTC) | |

## ISRO satellites launched by foreign agencies

ISRO satellites which have been launched by foreign space agencies (of Europe, USSR / Russia, and United States) are enlisted in the given tables below.
* Ariane
* Interkosmos
* Vostok
* Molniya
* Delta
* Space Shuttle
* Falcon 9
| Launch vehicle family | Satellites launched | Satellites launched | Satellites launched | Satellites launched | Satellites launched |
| Launch vehicle family | Communication | Earth observation | Experimental | Other | Total |
| Europe ||||||
| Ariane | 20 | 0 | 1 | 0 | 21 |
| USSR / Russia ||||||
| Interkosmos | 0 | 2 | 1 | 0 | 3 |
| Vostok | 0 | 2 | 0 | 0 | 2 |
| Molniya | 0 | 1 | 0 | 0 | 1 |
| Soyuz | 0 | 0 | 0 | 1 | 1 |
| USA ||||||
| Delta | 2 | 0 | 0 | 0 | 2 |
| Space Shuttle | 1 | 0 | 0 | 0 | 1 |
| Falcon 9 | 1 | 0 | 0 | 0 | 1 |
| Total | 24 | 5 | 2 | 0 | 31 |
ISRO satellites that were launched by foreign agencies, are listed in the table below.
| No. | Satellite's name | Launch vehicle | Launch agency | Country / region of launch agency | Launch date | Launch mass | Power | Orbit type | Mission life | Other information |
| 1. | Aryabhata | Kosmos-3M | | USSR | 19 April 1975 | 360 kg | 46 W | Low Earth orbit | | |
| 2. | Bhaskara-1 | Kosmos-3M | | USSR | 7 June 1979 | 442 kg | 47 W | Low Earth orbit | 1 year | |
| 3. | Apple | Ariane 1 L-03 | Arianespace | Europe | 19 June 1981 | 670 kg | 210 W | Geosynchronous | 2 years | |
| 4. | Bhaskara-2 | Kosmos-3M | | USSR | 20 November 1981 | 444 kg | 47 W | Low Earth orbit | 1 year | |
| 5. | INSAT-1A | Delta 3910 | McDonnell-Douglas | USA | 10 April 1982 | 1,152 kg with propellants (550 kg dry mass) | 1000 W | Geosynchronous | 7 years | |
| 6. | INSAT-1B | STS-8 | | USA | 30 August 1983 | 1,152 kg with propellants (550 kg dry mass) | 1000 W | Geosynchronous | 7 years | |
| * | Soyuz T-11 | Soyuz-U | | USSR | 3 April 1984 | | | Low Earth orbit | | Carrying India's first Astronaut Rakesh Sharma. The Mission was Organised By USSR. It was launched from Baikonur 31/6 on a Soyuz-U Launch vehicle on 3 April 1984 at 13:08:00 UTC. |
| 7. | IRS-1A | Vostok-2 | | USSR | 17 March 1988 | 975 kg | 620 W | Sun-synchronous | 7 years | |
| 8. | INSAT-1C | Ariane 3 V-24/L-23 | Arianespace | Europe | 22 July 1988 | 1,190 kg with propellants (550 kg dry mass) | 1000 W | Geosynchronous | 7 years | |
| 9. | INSAT-1D | Delta 4925 | McDonnell-Douglas | USA | 12 June 1990 | 1,190 kg with propellants (550 kg dry mass) | 1000 W | Geosynchronous | 12 years | |
| 10. | IRS-1B | Vostok-2 | | USSR | 29 August 1991 | 975 kg | 600 W | Sun-synchronous | 12 years | |
| 11. | INSAT-2A | Ariane 4 V-51/423 | Arianespace | Europe | 10 July 1992 | 1,906 kg with propellants (905 kg dry mass) | 1000 W | Geosynchronous | 7 years | |
| 12. | INSAT-2B | Ariane 4 V-58/429 | Arianespace | Europe | 22 July 1993 | 1,906 kg with propellants (916 kg dry mass) | 1000 W | Geosynchronous | 7 years | |
| 13. | INSAT-2C | Ariane 4 V-81/453 | Arianespace | Europe | 6 December 1995 | 2,106 kg with propellants (946 kg dry mass) | 1450 W | Geosynchronous | 7 years | |
| 14. | IRS-1C | Molniya-M | | Russia | 28 December 1995 | 1250 kg | 813 W | Sun-synchronous | 7 years | |
| 15. | INSAT-2D | Ariane 4 V-97/468 | Arianespace | Europe | 3 June 1997 | 2,079 kg with propellants (995 kg dry mass) | 1540 W | Geosynchronous | 7 years | |
| 16. | INSAT-2E | Ariane 4 V-117/486 | Arianespace | Europe | 2 April 1999 | 2,550 kg with propellants (1,150 kg dry mass) | 2150 W | Geosynchronous | 12 years | |
| 17. | INSAT-3B | Ariane 5 V-128 | Arianespace | Europe | 21 March 2000 | 2,070 kg with propellants (970 kg dry mass) | 1712 W | Geosynchronous | 10 years | |
| 18. | INSAT-3C | Ariane 4 V-147 | Arianespace | Europe | 23 January 2002 | 2,750 kg with propellants (1,220 kg dry mass) | 2765 W | Geosynchronous | 12 years | |
| 19. | INSAT-3A | Ariane 5 V-160 | Arianespace | Europe | 9 April 2003 | 2,950 kg with propellants (1,350 kg dry mass) | 3100 W | Geosynchronous | 12 years | |
| 20. | INSAT-3E | Ariane 5 V-162 | Arianespace | Europe | 27 September 2003 | 2,778 kg with propellants (1,218 kg dry mass) | 3100 W | Geosynchronous | 12 years | |
| 21. | INSAT-4A | Ariane 5 V169 | Arianespace | Europe | 22 December 2005 | 3081 kg with propellants (1386.55 kg dry mass) | 5922 W | Geosynchronous | 12 years | Communication satellite |
| 22. | INSAT-4B | Ariane 5 ECA | Arianespace | Europe | 12 March 2007 | 3,025 kg with propellants | 5859 W | Geosynchronous | 12 years | Communication satellite |
| 23. | GSAT-8 | Ariane-5 VA-202 | Arianespace | Europe | 21 May 2011 | 3,093 kg with propellants (1,426 kg dry mass) | 6242 W | Geosynchronous | More than 12 years | Communication satellite |
| 24. | INSAT-3D | Ariane-5 VA-214 | Arianespace | Europe | 26 July 2013 | 2,061 kg with propellants (937.8 kg dry mass) | 1164 W | Geosynchronous | 7 years | Weather satellite |
| 24. | GSAT-7 | Ariane-5 VA-215 | Arianespace | Europe | 30 August 2013 | 2,650 kg with propellants (1,211 kg dry mass) | 2915 W | Geosynchronous | 7 years | Communication satellite |
| 26. | GSAT-10 | Ariane-5 VA-209 | Arianespace | Europe | 29 September 2010 | 3,400 kg with propellants (1,498 kg dry mass) | 6474 W | Geosynchronous | 15 years | Communication satellite |
| 27. | GSAT-16 | Ariane-5 VA-221 | Arianespace | Europe | 7 December 2014 | 3,181.6 kg with propellants | 6000 W | Geosynchronous | 12 years | Communication satellite, carries 48 transponders, the most in any ISRO communication satellite so far. |
| 28. | GSAT-15 | Ariane-5 VA-227 | Arianespace | Europe | 11 November 2015 | 3,164 kg with propellants | 6000 W | Geosynchronous | 12 years | Communication satellite, carries 24 transponders. |
| 29. | GSAT-18 | Ariane-5 VA-231 | Arianespace | Europe | 6 October 2016 | 3,404 kg | 6474 W | Geosynchronous | 15 years | Communication satellite, carries 48 transponders. |
| 30. | GSAT-17 | Ariane-5 VA-238 | Arianespace | Europe | 28 June 2017 | 3,477 kg | 6474 W | Geosynchronous | 15 years | Communication satellite, carries 42 transponders. |
| 31. | GSAT-11 | Ariane-5 VA-246 | Arianespace | Europe | 5 December 2018 | 5,854 kg | 13.4 kW | Geosynchronous | 15 years | Communication satellite |
| 32. | GSAT-31 | Ariane-5 VA-247 | Arianespace | Europe | 5 February 2019 | 2,536 kg | 4.7 kW | Geosynchronous | 15 years | Communication satellite |
| 33. | GSAT-30 | Ariane-5 VA-251 | Arianespace | Europe | 16 January 2020 | 3,547 kg | 6 kW | Geosynchronous | 15 years | Communication satellite |
| 34. | CMS-02 (GSAT-24) | Ariane-5 VA-257 | Arianespace | Europe | 22 June 2022 | 4,181.3 kg | 12 kW | Geosynchronous | 15 years | Communication satellite |
| 35. | CMS-03 (GSAT-20) | Falcon 9 | SpaceX | USA | 18 November 2025 | 4,700 kg | 12 kW | Geosynchronous | 15 years | Communication satellite |