Polar Satellite Launch Vehicle

Table columns:
Flight
Variant
Launch date/time (UTC)
Launch pad
Payload
Payload mass
Result

Table rows:
cells: D1
PSLV-G
20 September 1993 05:12
First
IRS-1E
846 kg
Failure
cells: Maiden flight; attitude control failure at second stage separation.[22]
Maiden flight; attitude control failure at second stage separation.[22]
Maiden flight; attitude control failure at second stage separation.[22]
Maiden flight; attitude control failure at second stage separation.[22]
Maiden flight; attitude control failure at second stage separation.[22]
Maiden flight; attitude control failure at second stage separation.[22]
cells: D2
PSLV-G
15 October 1994 05:05
First
IRS-P2
804 kg
Success
cells: [23]
[23]
[23]
[23]
[23]
[23]
cells: D3
PSLV-G
21 March 1996 04:53
First
IRS-P3
920 kg
Success
cells: [24]
[24]
[24]
[24]
[24]
[24]
cells: C1
PSLV-G
29 September 1997 04:47
First
IRS-1D
1250 kg
Partial failure
cells: First operational flight; fourth stage under-performed resulting in lower than planned orbit. Satellite used own propulsion to move to correct orbit.[25]
First operational flight; fourth stage under-performed resulting in lower than planned orbit. Satellite used own propulsion to move to correct orbit.[25]
First operational flight; fourth stage under-performed resulting in lower than planned orbit. Satellite used own propulsion to move to correct orbit.[25]
First operational flight; fourth stage under-performed resulting in lower than planned orbit. Satellite used own propulsion to move to correct orbit.[25]
First operational flight; fourth stage under-performed resulting in lower than planned orbit. Satellite used own propulsion to move to correct orbit.[25]
First operational flight; fourth stage under-performed resulting in lower than planned orbit. Satellite used own propulsion to move to correct orbit.[25]
cells: C2
PSLV-G
26 May 1999 06:22
First
Oceansat-1  DLR-Tubsat  Kitsat-3
1050 kg 45 kg 107 kg
Success
cells: First launch to have foreign satellites, and first to carry multiple satellites.[26][27]
First launch to have foreign satellites, and first to carry multiple satellites.[26][27]
First launch to have foreign satellites, and first to carry multiple satellites.[26][27]
First launch to have foreign satellites, and first to carry multiple satellites.[26][27]
First launch to have foreign satellites, and first to carry multiple satellites.[26][27]
First launch to have foreign satellites, and first to carry multiple satellites.[26][27]
cells: C3
PSLV-G
22 October 2001 04:53
First
TES  PROBA  BIRD
1108 kg 94 kg 92 kg
Success
cells: First multi-orbit mission. TES and BIRD were injected into a nominal 568 km circular sun synchronous polar orbit, PROBA was injected into a 568 X 638 km elliptic orbit. Orbit was raised using RCS thrusters on fourth stage.[28][29]
First multi-orbit mission. TES and BIRD were injected into a nominal 568 km circular sun synchronous polar orbit, PROBA was injected into a 568 X 638 km elliptic orbit. Orbit was raised using RCS thrusters on fourth stage.[28][29]
First multi-orbit mission. TES and BIRD were injected into a nominal 568 km circular sun synchronous polar orbit, PROBA was injected into a 568 X 638 km elliptic orbit. Orbit was raised using RCS thrusters on fourth stage.[28][29]
First multi-orbit mission. TES and BIRD were injected into a nominal 568 km circular sun synchronous polar orbit, PROBA was injected into a 568 X 638 km elliptic orbit. Orbit was raised using RCS thrusters on fourth stage.[28][29]
First multi-orbit mission. TES and BIRD were injected into a nominal 568 km circular sun synchronous polar orbit, PROBA was injected into a 568 X 638 km elliptic orbit. Orbit was raised using RCS thrusters on fourth stage.[28][29]
First multi-orbit mission. TES and BIRD were injected into a nominal 568 km circular sun synchronous polar orbit, PROBA was injected into a 568 X 638 km elliptic orbit. Orbit was raised using RCS thrusters on fourth stage.[28][29]
cells: C4
PSLV-G
12 September 2002 10:23
First
MetSat-1 (Kalpana-1)
1060 kg
Success
cells: India's first launch to GTO. GTO payload capability has reached 1200 kg from 2002 onward, compared to 1050 kg previously. First use of lightweight carbon composite payload adapter.[30][31][32]
India's first launch to GTO. GTO payload capability has reached 1200 kg from 2002 onward, compared to 1050 kg previously. First use of lightweight carbon composite payload adapter.[30][31][32]
India's first launch to GTO. GTO payload capability has reached 1200 kg from 2002 onward, compared to 1050 kg previously. First use of lightweight carbon composite payload adapter.[30][31][32]
India's first launch to GTO. GTO payload capability has reached 1200 kg from 2002 onward, compared to 1050 kg previously. First use of lightweight carbon composite payload adapter.[30][31][32]
India's first launch to GTO. GTO payload capability has reached 1200 kg from 2002 onward, compared to 1050 kg previously. First use of lightweight carbon composite payload adapter.[30][31][32]
India's first launch to GTO. GTO payload capability has reached 1200 kg from 2002 onward, compared to 1050 kg previously. First use of lightweight carbon composite payload adapter.[30][31][32]
cells: C5
PSLV-G
17 October 2003 04:52
First
RESOURCESAT-1 (IRS-P6)
1360 kg
Success
cells: Payload capability had been progressively increased by more than 600 kg since the first PSLV launch. Launch took place despite heavy rain.[33][34]
Payload capability had been progressively increased by more than 600 kg since the first PSLV launch. Launch took place despite heavy rain.[33][34]
Payload capability had been progressively increased by more than 600 kg since the first PSLV launch. Launch took place despite heavy rain.[33][34]
Payload capability had been progressively increased by more than 600 kg since the first PSLV launch. Launch took place despite heavy rain.[33][34]
Payload capability had been progressively increased by more than 600 kg since the first PSLV launch. Launch took place despite heavy rain.[33][34]
Payload capability had been progressively increased by more than 600 kg since the first PSLV launch. Launch took place despite heavy rain.[33][34]
cells: C6
PSLV-G
5 May 2005 04:45
Second
Cartosat-1  HAMSAT
1560 kg 42.5 kg
Success
cells: First PSLV launch from the second launch pad.[35]
First PSLV launch from the second launch pad.[35]
First PSLV launch from the second launch pad.[35]
First PSLV launch from the second launch pad.[35]
First PSLV launch from the second launch pad.[35]
First PSLV launch from the second launch pad.[35]
cells: C7
PSLV-G
10 January 2007 03:54
First
Cartosat-2  SRE-1  LAPAN-TUBsat  PEHUENSAT-1
680 kg 500 kg 56 kg 6 kg
Success
cells: First flight of hardware upgrade, first launch of reentry capsule (SRE).[36]
First flight of hardware upgrade, first launch of reentry capsule (SRE).[36]
First flight of hardware upgrade, first launch of reentry capsule (SRE).[36]
First flight of hardware upgrade, first launch of reentry capsule (SRE).[36]
First flight of hardware upgrade, first launch of reentry capsule (SRE).[36]
First flight of hardware upgrade, first launch of reentry capsule (SRE).[36]
cells: C8
PSLV-CA
23 April 2007 10:00
Second
AGILE  AAM
352 kg 185 kg
Success
cells: First flight of the 'Core-Alone' configuration. ISRO's first commercial launch (foreign satellite as the main payload).[37][38]
First flight of the 'Core-Alone' configuration. ISRO's first commercial launch (foreign satellite as the main payload).[37][38]
First flight of the 'Core-Alone' configuration. ISRO's first commercial launch (foreign satellite as the main payload).[37][38]
First flight of the 'Core-Alone' configuration. ISRO's first commercial launch (foreign satellite as the main payload).[37][38]
First flight of the 'Core-Alone' configuration. ISRO's first commercial launch (foreign satellite as the main payload).[37][38]
First flight of the 'Core-Alone' configuration. ISRO's first commercial launch (foreign satellite as the main payload).[37][38]
cells: C10
PSLV-CA
21 January 2008 03:45
First
TecSAR
295 kg
Success
cells: ISRO's second commercial launch (foreign satellite as the main payload).[39][40]
ISRO's second commercial launch (foreign satellite as the main payload).[39][40]
ISRO's second commercial launch (foreign satellite as the main payload).[39][40]
ISRO's second commercial launch (foreign satellite as the main payload).[39][40]
ISRO's second commercial launch (foreign satellite as the main payload).[39][40]
ISRO's second commercial launch (foreign satellite as the main payload).[39][40]
cells: C9
PSLV-CA
28 April 2008 03:53
Second
Cartosat-2A  IMS-1/TWSAT  RUBIN-8  CanX-6/NTS  CanX-2  Cute-1.7+APD II  Delfi-C3  SEEDS-2  COMPASS-1  AAUSAT-II
690 kg 83 kg 8 kg 6.5 kg 3.5 kg 3 kg 2.2 kg 1 kg 1 kg 0.75 kg
Success
cells: [41][42]
[41][42]
[41][42]
[41][42]
[41][42]
[41][42]
cells: C11
PSLV-XL
22 October 2008 00:52
Second
Chandrayaan-1
1380 kg
Success
cells: First flight of the PSLV-XL configuration, first Indian Lunar probe.[43][44]
First flight of the PSLV-XL configuration, first Indian Lunar probe.[43][44]
First flight of the PSLV-XL configuration, first Indian Lunar probe.[43][44]
First flight of the PSLV-XL configuration, first Indian Lunar probe.[43][44]
First flight of the PSLV-XL configuration, first Indian Lunar probe.[43][44]
First flight of the PSLV-XL configuration, first Indian Lunar probe.[43][44]
cells: C12
PSLV-CA
20 April 2009 01:15
Second
RISAT-2  ANUSAT
300 kg 40 kg
Success
cells: India's first radar imaging satellite, RISAT.[45][46]
India's first radar imaging satellite, RISAT.[45][46]
India's first radar imaging satellite, RISAT.[45][46]
India's first radar imaging satellite, RISAT.[45][46]
India's first radar imaging satellite, RISAT.[45][46]
India's first radar imaging satellite, RISAT.[45][46]
cells: C14
PSLV-CA
23 September 2009 06:21
First
Oceansat-2  Rubin 9.1 Rubin 9.2  SwissCube-1  BeeSat  UWE-2  ITUpSAT1
960 kg 8 kg 8 kg 1 kg 1 kg 1 kg 1 kg
Success
cells: Rubin 9.1 and 9.2 intentionally remained attached to the fourth stage. SwissCube-1 was the first Swiss satellite, and ITUpSAT1 was the first satellite to be constructed in Turkey.[47][48][49][50][51][52]
Rubin 9.1 and 9.2 intentionally remained attached to the fourth stage. SwissCube-1 was the first Swiss satellite, and ITUpSAT1 was the first satellite to be constructed in Turkey.[47][48][49][50][51][52]
Rubin 9.1 and 9.2 intentionally remained attached to the fourth stage. SwissCube-1 was the first Swiss satellite, and ITUpSAT1 was the first satellite to be constructed in Turkey.[47][48][49][50][51][52]
Rubin 9.1 and 9.2 intentionally remained attached to the fourth stage. SwissCube-1 was the first Swiss satellite, and ITUpSAT1 was the first satellite to be constructed in Turkey.[47][48][49][50][51][52]
Rubin 9.1 and 9.2 intentionally remained attached to the fourth stage. SwissCube-1 was the first Swiss satellite, and ITUpSAT1 was the first satellite to be constructed in Turkey.[47][48][49][50][51][52]
Rubin 9.1 and 9.2 intentionally remained attached to the fourth stage. SwissCube-1 was the first Swiss satellite, and ITUpSAT1 was the first satellite to be constructed in Turkey.[47][48][49][50][51][52]
cells: C15
PSLV-CA
12 July 2010 03:52
First
Cartosat-2B  ALSAT-2A  AISSat-1  TIsat-1  STUDSAT
694 kg 117 kg 6.5 kg 1 kg 0.95 kg
Success
cells: AISSat-1 and TIsat are part of NLS-6.[53][54][55][56][57][58][59]
AISSat-1 and TIsat are part of NLS-6.[53][54][55][56][57][58][59]
AISSat-1 and TIsat are part of NLS-6.[53][54][55][56][57][58][59]
AISSat-1 and TIsat are part of NLS-6.[53][54][55][56][57][58][59]
AISSat-1 and TIsat are part of NLS-6.[53][54][55][56][57][58][59]
AISSat-1 and TIsat are part of NLS-6.[53][54][55][56][57][58][59]
cells: C16
PSLV-G
20 April 2011 04:42
First
ResourceSat-2  X-Sat  YouthSat
1206 kg 106 kg 92 kg
Success
cells: [60]
[60]
[60]
[60]
[60]
[60]
cells: C17
PSLV-XL
15 July 2011 11:18
Second
GSAT-12
1410 kg
Success
cells: First use of Vikram flight computer.[61][62]
First use of Vikram flight computer.[61][62]
First use of Vikram flight computer.[61][62]
First use of Vikram flight computer.[61][62]
First use of Vikram flight computer.[61][62]
First use of Vikram flight computer.[61][62]
cells: C18
PSLV-CA
12 October 2011 05:31
First
Megha-Tropiques  SRMSAT  Jugnu  VesselSat-1
1000 kg 10.9 kg 3 kg 28.7 kg
Success
cells: [63][64]
[63][64]
[63][64]
[63][64]
[63][64]
[63][64]
cells: C19
PSLV-XL
26 April 2012 00:17
First
RISAT-1
1850 kg
Success
cells: [65]
[65]
[65]
[65]
[65]
[65]
cells: C21
PSLV-CA
9 September 2012 04:23
First
SPOT-6  mRESINS  PROITERES
720 kg 50 kg 15 kg
Success
cells: mRESINS tested avionics for future PSLV launches. ISRO's third commercial launch (foreign satellite as the main payload). ISRO's 100th mission.[66][67]
mRESINS tested avionics for future PSLV launches. ISRO's third commercial launch (foreign satellite as the main payload). ISRO's 100th mission.[66][67]
mRESINS tested avionics for future PSLV launches. ISRO's third commercial launch (foreign satellite as the main payload). ISRO's 100th mission.[66][67]
mRESINS tested avionics for future PSLV launches. ISRO's third commercial launch (foreign satellite as the main payload). ISRO's 100th mission.[66][67]
mRESINS tested avionics for future PSLV launches. ISRO's third commercial launch (foreign satellite as the main payload). ISRO's 100th mission.[66][67]
mRESINS tested avionics for future PSLV launches. ISRO's third commercial launch (foreign satellite as the main payload). ISRO's 100th mission.[66][67]
cells: C20
PSLV-CA
25 February 2013 12:31
First
SARAL  Sapphire  NEOSSat  TUGSAT-1  UniBRITE-1  STRaND-1  AAUSAT3
409 kg 148 kg 74 kg 14 kg 14 kg 6.5 kg 0.8 kg
Success
cells: TUGSAT-1 and UniBRITE were the first Austrian satellites.[68][69][70]
TUGSAT-1 and UniBRITE were the first Austrian satellites.[68][69][70]
TUGSAT-1 and UniBRITE were the first Austrian satellites.[68][69][70]
TUGSAT-1 and UniBRITE were the first Austrian satellites.[68][69][70]
TUGSAT-1 and UniBRITE were the first Austrian satellites.[68][69][70]
TUGSAT-1 and UniBRITE were the first Austrian satellites.[68][69][70]
cells: C22
PSLV-XL
1 July 2013 18:11
First
IRNSS-1A
1425 kg
Success
cells: India's first regional navigation satellite.[71]
India's first regional navigation satellite.[71]
India's first regional navigation satellite.[71]
India's first regional navigation satellite.[71]
India's first regional navigation satellite.[71]
India's first regional navigation satellite.[71]
cells: C25
PSLV-XL
5 November 2013 09:08
First
Mars Orbiter Mission
1350 kg
Success
cells: India's first Mars mission.[72][73]
India's first Mars mission.[72][73]
India's first Mars mission.[72][73]
India's first Mars mission.[72][73]
India's first Mars mission.[72][73]
India's first Mars mission.[72][73]
cells: C24
PSLV-XL
4 April 2014 11:44
First
IRNSS-1B
1432 kg
Success
cells: India's second regional navigation satellite.[74][75]
India's second regional navigation satellite.[74][75]
India's second regional navigation satellite.[74][75]
India's second regional navigation satellite.[74][75]
India's second regional navigation satellite.[74][75]
India's second regional navigation satellite.[74][75]
cells: C23
PSLV-CA
30 June 2014 04:22
First
SPOT-7  CanX-4  CanX-5  AISAT  VELOX-1
714 kg 15 kg 15 kg 14 kg 7 kg
Success
cells: ISRO's fourth commercial launch (foreign satellite as the main payload).[76]
ISRO's fourth commercial launch (foreign satellite as the main payload).[76]
ISRO's fourth commercial launch (foreign satellite as the main payload).[76]
ISRO's fourth commercial launch (foreign satellite as the main payload).[76]
ISRO's fourth commercial launch (foreign satellite as the main payload).[76]
ISRO's fourth commercial launch (foreign satellite as the main payload).[76]
cells: C26
PSLV-XL
16 October 2014 20:02
First
IRNSS-1C
1425.4 kg
Success
cells: Seventh PSLV-XL and third Navigation Satellite launch.[77][78]
Seventh PSLV-XL and third Navigation Satellite launch.[77][78]
Seventh PSLV-XL and third Navigation Satellite launch.[77][78]
Seventh PSLV-XL and third Navigation Satellite launch.[77][78]
Seventh PSLV-XL and third Navigation Satellite launch.[77][78]
Seventh PSLV-XL and third Navigation Satellite launch.[77][78]
cells: C27
PSLV-XL
28 March 2015 11:49
Second
IRNSS-1D
1425 kg
Success
cells: Eighth PSLV-XL and fourth Navigation Satellite launch.[79]
Eighth PSLV-XL and fourth Navigation Satellite launch.[79]
Eighth PSLV-XL and fourth Navigation Satellite launch.[79]
Eighth PSLV-XL and fourth Navigation Satellite launch.[79]
Eighth PSLV-XL and fourth Navigation Satellite launch.[79]
Eighth PSLV-XL and fourth Navigation Satellite launch.[79]
cells: C28
PSLV-XL
10 July 2015 16:28
First
UK-DMC3A  UK-DMC3B  UK-DMC3C  CBNT-1  DeOrbitSail
447 kg 447 kg 447 kg 91 kg 7 kg
Success
cells: At the time it was the heaviest commercial mission (1439 kg) successfully accomplished using a launch vehicle assembled by ISRO.[80][81]
At the time it was the heaviest commercial mission (1439 kg) successfully accomplished using a launch vehicle assembled by ISRO.[80][81]
At the time it was the heaviest commercial mission (1439 kg) successfully accomplished using a launch vehicle assembled by ISRO.[80][81]
At the time it was the heaviest commercial mission (1439 kg) successfully accomplished using a launch vehicle assembled by ISRO.[80][81]
At the time it was the heaviest commercial mission (1439 kg) successfully accomplished using a launch vehicle assembled by ISRO.[80][81]
At the time it was the heaviest commercial mission (1439 kg) successfully accomplished using a launch vehicle assembled by ISRO.[80][81]
cells: C30
PSLV-XL
28 September 2015 04:30
First
Astrosat  LAPAN-A2  exactView 9  Lemur-2 #1 Joel  Lemur-2 #2 Peter  Lemur-2 #3 Jeroen  Lemur-2 #4 Chris
1650 kg 68 kg 5.5 kg 4 kg 4 kg 4 kg 4 kg
Success
cells: Launch of India's first dedicated multi-wavelength space observatory and ISRO's first launch of US satellites.[82]
Launch of India's first dedicated multi-wavelength space observatory and ISRO's first launch of US satellites.[82]
Launch of India's first dedicated multi-wavelength space observatory and ISRO's first launch of US satellites.[82]
Launch of India's first dedicated multi-wavelength space observatory and ISRO's first launch of US satellites.[82]
Launch of India's first dedicated multi-wavelength space observatory and ISRO's first launch of US satellites.[82]
Launch of India's first dedicated multi-wavelength space observatory and ISRO's first launch of US satellites.[82]
cells: C29
PSLV-CA
16 December 2015 12:30
First
TeLEOS-1  VELOX-C1  VELOX-II  Kent Ridge-1  Galassia  Athenoxat-1[83]
400 kg 123 kg 13 kg 78 kg 3.4 kg -
Success
cells: Commercial launch of 6 Singaporean satellites. Fourth stage re-ignition demonstrated successfully after payload deployment.[84][85][86]
Commercial launch of 6 Singaporean satellites. Fourth stage re-ignition demonstrated successfully after payload deployment.[84][85][86]
Commercial launch of 6 Singaporean satellites. Fourth stage re-ignition demonstrated successfully after payload deployment.[84][85][86]
Commercial launch of 6 Singaporean satellites. Fourth stage re-ignition demonstrated successfully after payload deployment.[84][85][86]
Commercial launch of 6 Singaporean satellites. Fourth stage re-ignition demonstrated successfully after payload deployment.[84][85][86]
Commercial launch of 6 Singaporean satellites. Fourth stage re-ignition demonstrated successfully after payload deployment.[84][85][86]
cells: C31
PSLV-XL
20 January 2016 04:01
Second
IRNSS-1E
1425 kg
Success
cells: IRNSS-1E, fifth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the eleventh time ‘XL’ configuration is being flown.[87][88][89]
IRNSS-1E, fifth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the eleventh time ‘XL’ configuration is being flown.[87][88][89]
IRNSS-1E, fifth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the eleventh time ‘XL’ configuration is being flown.[87][88][89]
IRNSS-1E, fifth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the eleventh time ‘XL’ configuration is being flown.[87][88][89]
IRNSS-1E, fifth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the eleventh time ‘XL’ configuration is being flown.[87][88][89]
IRNSS-1E, fifth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the eleventh time ‘XL’ configuration is being flown.[87][88][89]
cells: C32
PSLV-XL
10 March 2016 10:31
Second
IRNSS-1F
1425 kg
Success
cells: IRNSS-1F, sixth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the twelfth time ‘XL’ configuration is being flown. IRNSS-1F carries Corner Cube Retroreflectors for laser ranging.[90] Launch initially scheduled for 10:30 was delayed by one minute to avoid space debris.[91]
IRNSS-1F, sixth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the twelfth time ‘XL’ configuration is being flown. IRNSS-1F carries Corner Cube Retroreflectors for laser ranging.[90] Launch initially scheduled for 10:30 was delayed by one minute to avoid space debris.[91]
IRNSS-1F, sixth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the twelfth time ‘XL’ configuration is being flown. IRNSS-1F carries Corner Cube Retroreflectors for laser ranging.[90] Launch initially scheduled for 10:30 was delayed by one minute to avoid space debris.[91]
IRNSS-1F, sixth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the twelfth time ‘XL’ configuration is being flown. IRNSS-1F carries Corner Cube Retroreflectors for laser ranging.[90] Launch initially scheduled for 10:30 was delayed by one minute to avoid space debris.[91]
IRNSS-1F, sixth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the twelfth time ‘XL’ configuration is being flown. IRNSS-1F carries Corner Cube Retroreflectors for laser ranging.[90] Launch initially scheduled for 10:30 was delayed by one minute to avoid space debris.[91]
IRNSS-1F, sixth navigation satellite of the seven satellites constituting the IRNSS space segment launched. It carries two types of payloads – navigation payload and ranging payload. This is the twelfth time ‘XL’ configuration is being flown. IRNSS-1F carries Corner Cube Retroreflectors for laser ranging.[90] Launch initially scheduled for 10:30 was delayed by one minute to avoid space debris.[91]
cells: C33
PSLV-XL
28 April 2016 07:20
First
IRNSS-1G
1425 kg
Success
cells: IRNSS-1G, last navigation satellite of the seven satellites constituting the IRNSS space segment launched. India's own navigational system, the set-up for which was completed will be called NAVIC (Navigation with Indian Constellation)[92][93][94][95][96]
IRNSS-1G, last navigation satellite of the seven satellites constituting the IRNSS space segment launched. India's own navigational system, the set-up for which was completed will be called NAVIC (Navigation with Indian Constellation)[92][93][94][95][96]
IRNSS-1G, last navigation satellite of the seven satellites constituting the IRNSS space segment launched. India's own navigational system, the set-up for which was completed will be called NAVIC (Navigation with Indian Constellation)[92][93][94][95][96]
IRNSS-1G, last navigation satellite of the seven satellites constituting the IRNSS space segment launched. India's own navigational system, the set-up for which was completed will be called NAVIC (Navigation with Indian Constellation)[92][93][94][95][96]
IRNSS-1G, last navigation satellite of the seven satellites constituting the IRNSS space segment launched. India's own navigational system, the set-up for which was completed will be called NAVIC (Navigation with Indian Constellation)[92][93][94][95][96]
IRNSS-1G, last navigation satellite of the seven satellites constituting the IRNSS space segment launched. India's own navigational system, the set-up for which was completed will be called NAVIC (Navigation with Indian Constellation)[92][93][94][95][96]
cells: C34
PSLV-XL
22 June 2016 03:55
Second
Cartosat-2C  LAPAN-A3  BIROS  SkySat Gen2-1  GHGSat-D  M3MSat  Swayam  SathyabamaSat  12 × Flock-2P Dove (satellite)
727.5 kg 120 kg 130 kg 110 kg 25.5 kg 85 kg 1 kg 1.5 kg 12 × 4.7 kg
Success
cells: ISRO's Cartosat-2C and 19 other satellites launched.[97][98][99][100][101][102]
ISRO's Cartosat-2C and 19 other satellites launched.[97][98][99][100][101][102]
ISRO's Cartosat-2C and 19 other satellites launched.[97][98][99][100][101][102]
ISRO's Cartosat-2C and 19 other satellites launched.[97][98][99][100][101][102]
ISRO's Cartosat-2C and 19 other satellites launched.[97][98][99][100][101][102]
ISRO's Cartosat-2C and 19 other satellites launched.[97][98][99][100][101][102]
cells: C35
PSLV-G
26 September 2016 03:42
First
ScatSat-1  ALSAT-2B  ALSAT-1B  Pathfinder-1  Pratham  CanX-7 (NLS-19)[103]  ALSAT-1N  PISat
371 kg 117 kg 103 kg 44 kg 10 kg 8 kg 7 kg 5.25 kg
Success
cells: ISRO's longest PSLV satellite launch mission. First mission of PSLV in which it launched its payloads into two different orbits.[104][105][106][107][108][109]
ISRO's longest PSLV satellite launch mission. First mission of PSLV in which it launched its payloads into two different orbits.[104][105][106][107][108][109]
ISRO's longest PSLV satellite launch mission. First mission of PSLV in which it launched its payloads into two different orbits.[104][105][106][107][108][109]
ISRO's longest PSLV satellite launch mission. First mission of PSLV in which it launched its payloads into two different orbits.[104][105][106][107][108][109]
ISRO's longest PSLV satellite launch mission. First mission of PSLV in which it launched its payloads into two different orbits.[104][105][106][107][108][109]
ISRO's longest PSLV satellite launch mission. First mission of PSLV in which it launched its payloads into two different orbits.[104][105][106][107][108][109]
cells: C36
PSLV-XL
7 December 2016 04:55
First
Resourcesat-2A
1235 kg
Success
cells: [110][111][112][113][114][115]
[110][111][112][113][114][115]
[110][111][112][113][114][115]
[110][111][112][113][114][115]
[110][111][112][113][114][115]
[110][111][112][113][114][115]
cells: C37
PSLV-XL
15 February 2017 03:58
First
Cartosat-2D  INS-1A  INS-1B  Nayif-1 CubeSats  Al Farabi-1  PEASSS  BGUSAT  DIDO-2  Doves Flock-3P  Lemur-2
730 kg 8.4 kg 9.7 kg 1.1 kg 1.7 kg 3 kg 4.3 kg 4.2 kg 4.7 kg x 88 Nos. 4.6 kg x 8 Nos.
Success
cells: PSLV-C37 successfully carried and deployed a record 104 satellites in the Sun-synchronous orbit.[116][117][118][119][120][121]
PSLV-C37 successfully carried and deployed a record 104 satellites in the Sun-synchronous orbit.[116][117][118][119][120][121]
PSLV-C37 successfully carried and deployed a record 104 satellites in the Sun-synchronous orbit.[116][117][118][119][120][121]
PSLV-C37 successfully carried and deployed a record 104 satellites in the Sun-synchronous orbit.[116][117][118][119][120][121]
PSLV-C37 successfully carried and deployed a record 104 satellites in the Sun-synchronous orbit.[116][117][118][119][120][121]
PSLV-C37 successfully carried and deployed a record 104 satellites in the Sun-synchronous orbit.[116][117][118][119][120][121]
cells: C38
PSLV-XL
23 June 2017 03:59 [122][123]
First
Cartosat-2E[124]  NIUSAT[125]  CESAT-1[126]  Lemur-2 × 8 , , Blue, Red, Green Diamonds , Max Valier Sat[127]  Venta-1  D-Sat[128]  Aalto-1  COMPASS-2/Dragsail QB50  InflateSail QB50  URSA MAIOR QB50  LituanicaSAT-2 QB50  PEGASUS QB50  NUDTSat QB50  VZLUSAT1 QB50  UCLSat QB50  SUCHAI  ROBUSTA-1B  skCUBE  CICERO-6  Tyvak-53b (PacSciSat[129])  KickSat Sprites × 6 (All of them flown with Venta-1 and Max Valier Sat)
727 kg 15 kg 60 kg 4 kg x 8 Nos. 18 kg 15 kg 7.5 kg 4.5 kg 4 kg 4 kg 4 kg 3 kg 4 kg 2 kg 2 kg 2 kg 2 kg 1 kg 1 kg 1 kg  ?  ?
Success
cells: Post mission PSLV fourth stage (PS4) was lowered to 350 km altitude and carried Ionization Density and Electric field Analyzer (IDEA) payload by Space Physics Laboratory to measure electron density and electric field measurements in the F region of the ionosphere[130][131][132][133][134][135]
Post mission PSLV fourth stage (PS4) was lowered to 350 km altitude and carried Ionization Density and Electric field Analyzer (IDEA) payload by Space Physics Laboratory to measure electron density and electric field measurements in the F region of the ionosphere[130][131][132][133][134][135]
Post mission PSLV fourth stage (PS4) was lowered to 350 km altitude and carried Ionization Density and Electric field Analyzer (IDEA) payload by Space Physics Laboratory to measure electron density and electric field measurements in the F region of the ionosphere[130][131][132][133][134][135]
Post mission PSLV fourth stage (PS4) was lowered to 350 km altitude and carried Ionization Density and Electric field Analyzer (IDEA) payload by Space Physics Laboratory to measure electron density and electric field measurements in the F region of the ionosphere[130][131][132][133][134][135]
Post mission PSLV fourth stage (PS4) was lowered to 350 km altitude and carried Ionization Density and Electric field Analyzer (IDEA) payload by Space Physics Laboratory to measure electron density and electric field measurements in the F region of the ionosphere[130][131][132][133][134][135]
Post mission PSLV fourth stage (PS4) was lowered to 350 km altitude and carried Ionization Density and Electric field Analyzer (IDEA) payload by Space Physics Laboratory to measure electron density and electric field measurements in the F region of the ionosphere[130][131][132][133][134][135]
cells: C39
PSLV-XL
31 August 2017 13:30 [136][137][138]
Second
IRNSS-1H
1425 kg
Failure
cells: Payload fairing (heat shield) failed to separate, causing the satellite to remain inside the fairing with the payload dispenser detaching the satellite internally. Second PSLV failure in 24 years, the first one being PSLV-D1.[139][140][141][142]
Payload fairing (heat shield) failed to separate, causing the satellite to remain inside the fairing with the payload dispenser detaching the satellite internally. Second PSLV failure in 24 years, the first one being PSLV-D1.[139][140][141][142]
Payload fairing (heat shield) failed to separate, causing the satellite to remain inside the fairing with the payload dispenser detaching the satellite internally. Second PSLV failure in 24 years, the first one being PSLV-D1.[139][140][141][142]
Payload fairing (heat shield) failed to separate, causing the satellite to remain inside the fairing with the payload dispenser detaching the satellite internally. Second PSLV failure in 24 years, the first one being PSLV-D1.[139][140][141][142]
Payload fairing (heat shield) failed to separate, causing the satellite to remain inside the fairing with the payload dispenser detaching the satellite internally. Second PSLV failure in 24 years, the first one being PSLV-D1.[139][140][141][142]
Payload fairing (heat shield) failed to separate, causing the satellite to remain inside the fairing with the payload dispenser detaching the satellite internally. Second PSLV failure in 24 years, the first one being PSLV-D1.[139][140][141][142]

Questions about this table:
originalText: when was pslv launched for the first time
answer: answerTexts: 20 September 1993