List of PSLV launches

This is a list of launches made by Indian Space Research Organisation (ISRO) using Polar Satellite Launch Vehicle (PSLV) rockets.

Notable missions

PSLV flight D1

Main article: PSLV-D1

This was the first developmental flight of the PSLV-D1. ^[1] The IRS-1E satellite which was proposed to be launched was derived from the engineering model of IRS-1A incorporating a similar camera and an additional German-built monocular electro-optical stereo scanner. Even though the mission was a failure, the launch team and an expert committee appointed thereafter noted that the mission had validated many technologies and that most sub-systems had performed optimally. ^{[2] [3]}

PSLV flight C2

Main article: PSLV-C2

In the flight sequence, IRS-P4 was injected first, followed by KITSAT-3 and DLR-Tubsat in that order. ^[4] The mission was supported by ISRO Telemetry, Tracking and Command Network of ground stations located at Bangalore, Sriharikota, Lucknow, Mauritius, Bearslake, Russia and Biak, Indonesia. During the initial phase of the mission the ground station at Wilhem in Germany also provided network support. Upon injection of the satellites, data from the IRS-P4 was received at Hyderabad while KITSAT-3 data was received at the ground station in South Korea and the data from the DLR-Tubsat was received at the university ground station in Berlin. ^{[5] [6]}

PSLV flight C6

Main article: PSLV-C6

The former President, Dr. Abdul Kalam, witnessed the launch from the Mission Control Centre. ^[7] It was the first PSLV launch from second pad, using integrate-transfer-and-launch technology. After its integration in the Vehicle Assembly Building, the PSLV-C6 was transported on rails to the Umbilical Tower (UT) located one km away using the Mobile Launch Pedestal where the final operations were carried out. ^[7]

PSLV flight C7

The following hardware changes ^{[8] [9]} were made since PSLV-C6:

• first use of DLA (Dual Launch Adapter) to launch 2 primary satellites in time
• reduction of propellant from 2.5 tonne to 2 tonne in the fourth liquid propellant stage
• incorporation of a video imaging system to capture payload and DLA separation events
• altitude based day of launch wind-biased steering programme during Open Loop Guidance
• removal of Secondary Injection Thrust Vector Control (SITVC) system for one of the strapons ignited in the air.

PSLV flight C9

The fourth stage first fired Cartosat-2A into orbit at an altitude of 637 km about 885 seconds after lift-off. About 45 seconds later, it propelled IMS-1 into the orbit. Then the six nano satellites belonging to a cluster called Nanosatellite Launch System-4 (NLS-4) were injected into orbit at intervals of 20 seconds each. NLS-5, a single satellite, flew out and finally the tenth satellite Rubin-8 went along with the fourth stage into orbit. Two satellites belonged to India and the remaining were nanosatellites built by universities in different countries. ^[10] This was the maximum number of satellites placed in orbit, in a single PSLV launch. ^{[11] [12] [13]}

PSLV flight C21

Launch attended by the former prime minister, Manmohan Singh. ^[14] mRESINS (mini Redundant Strapdown Inertial Navigation System) bolted to the vehicle's fourth stage, have tested avionics for future PSLV missions. ^[15] With this launch Indian Space Research Organisation marked its 100 space missions, with 62 satellites, 37 launch vehicles and 1 Space Capsule Recovery Experiment.^{[ citation needed ]}

PSLV flight C22

Earlier launch date for PSLV C22 was fixed as 12 June 2013 but the launch had been postponed because of a technical snag in the 2nd stage. ^[16]

ISRO then replaced a faulty component in the PSLV C22 rocket and rescheduled the flight of the IRNSS-1A satellite on 1 July 2013. ^[17] PSLV C22, successfully launched IRNSS-1A, the first satellite in the Indian Regional Navigation Satellite System (IRNSS). At the completion of the countdown, PSLV C22 lifted off from the First Launch Pad at 23:41 (IST) on 1 July 2013 with the ignition of the first stage and four strap-on motors of the launch vehicle. ^[18]

PSLV flight C25

Main article: Mars Orbiter Mission

The Mars Orbiter Mission (MOM), informally called Mangalyaan is a Mars orbiter that was successfully injected into Earth orbit on 5 November 2013 at 14:38 IST (09:08 UTC) atop a PSLV-XL launch vehicle from Satish Dhawan Space Centre, Sriharikota (SHAR).^{[ citation needed ]}

PSLV flight C29

PSLV C29 lifted off from the First Launch Pad (FLP) of SDSC SHAR at 18:00 [IST] on 16 December 2015. It successfully deployed six satellites it carried with gross weight of 624 kg. After fourth stage engines were cut off primary payload TeLEOS-1 was injected in orbit at about 18 minutes 12 seconds after lift-off. This was followed by the deployment of other five satellites, namely Kent Ridge-1, VELOX-C1, VELOX-II, Galassia and Athenoxat-1 in quick succession in the subsequent three minutes. ^[19] 67 minutes into flight fourth stage re-ignition capability was demonstrated successfully by firing its engines for duration of nearly five seconds. This capability would enable multiple satellite deployment in varying orbits on same flight. ^[20]

PSLV flight C34

Main article: PSLV-C34

PSLV-C34 was launched on 22 June 2016 and successfully deployed 20 satellites in Sun-synchronous orbit. A Dual Launch Adapter with new design ^[21] compared to its previous version ^[22] was used to integrate all ride-sharing payloads with PS4. After completion of mission a pair of PS4 re-ignition tests were performed to reaffirm multi-orbit deployment capability of PS4. ^[23] A new inertial navigation system 'Mk IV A' employing next generation accelerometer was introduced on this mission. ^{[24] [25]}

PSLV flight C36

Remote umbilical fill and drain system was used on fourth stage for the first time reducing the countdown time by one day. Experimental avionics packages were flown bolted to fourth stage including "miniaturized advanced inertial navigation system" miniAINS, ^[26] NavIC based positioning system, ^[27] Vikram processor and new lithium-ion based power system. A video imaging system was also on-board, consisting of five cameras which captured and live streamed various staging events. ^{[28] [29]}

PSLV flight C37

Main article: PSLV-C37

PSLV C37 was launched from Satish Dhawan Space Centre, Sriharikota (SHAR) carrying a payload of 104 satellites from 6 countries around the world (Israel, Kazakhstan, Netherlands, Switzerland, United Arab Emirates and the United States). Of the 104 satellites, 96 were CubeSats made by Planet Labs and Spire Global, two San Francisco companies adding to their commercial satellite constellations. ^[30]

The launch set the record for the largest number of spacecraft ever launched on a single rocket. The previous record was held by Russia, which in 2014 catapulted 37 satellites in a single launch, using a modified Intercontinental ballistic missile (ICBM). ^{[31] [32]} It was again broken by SpaceX on their Transporter-1 mission which carried 143 satellites on a single launch.

PSLV flight C48

This was the 50th flight of the Polar Satellite Launch Vehicle. ^[33] It was also the 75th launch from Sriharikota. The flight placed into orbit the RISAT-2BR1 and nine customer satellites for New Space India Ltd. It was the second flight of the PSLV in the QL configuration. ^[34]

PSLV flight C51

Main article: PSLV-C51

This was the 53rd flight of PSLV and the 50th successful flight of PSLV. This is the first dedicated commercial launch executed by NSIL. ^[35] The mission successfully placed Amazônia-1 from Brazil, INPE and 18 other payload into its orbit. ^[36]

PSLV flight C57

Launched 10 days after the successful landing of ISRO's Moon mission, Chandrayaan-3, this mission carried the Aditya-L1 Mission satellite, the first Indian satellite dedicated to studying the Sun. Launch was successful and achieved its intended orbit nearly an hour later, and separated from its fourth stage. ^[37] On 6 January 2024, Aditya-L1 spacecraft, India's first solar mission, has successfully entered its final orbit with a period of approximately 180 days around the first Sun-Earth Lagrangian point (L1), approximately 1.5 million kilometers from Earth. ^[38]

Launch failures Of PSLV

IRS-1E

On 20 September 1993, a PSLV D1, the first developmental flight rocket, failed during launch of IRS-1E. A significant attitude disturbance occurred during second to third-stage separation, causing the attitude control command to exceed its maximum value. Because of the programming error in the pitch control loop of the digital autopilot software in the guidance and control processor, the required reversal of command polarity did not take place, causing the pitch loop to become unstable, resulted in loss of attitude control and failure to achieve orbit. The attitude control disturbance was traced to failure of one of the retro rockets designed to pull the burnt second stage away from the third stage. The vehicle crashed into the Bay of Bengal 700 seconds after take off. ^[3]

IRS-1D

On 29 September 1997, a PSLV C1 rocket failed during launch of IRS-1D. Anomalous interaction between the primary and secondary pressure regulators of the fourth stage caused a reduction in propellant flow and thrust after 250 seconds of burn time. As a result, the fourth stage was shut down by a software override timer after burning 435 seconds, before reaching the target orbit or depleting propellant. The injection velocity was 140 m/s low, resulting in an orbit of 301 x 823 km instead of the planned 817 km circular SSO. ^[39] Initially, a leak of helium gas from one of the components in the fourth stage was suspected, ^{[40] [41]} similar to recent Long March 3 launch failure, but later ruled out. Resulting orbit was partially corrected using satellite's on-board thrusters, thereby raising the perigee to 737 km, while the apogee remained at 821 km. ^[3]

IRNSS-1H

PSLV-C39 carrying IRNSS-1H was launched on 31 August 2017 at 13:30 UTC from Second Launch Pad of Satish Dhawan Space Centre (SHAR). After about 203 seconds of flight payload fairing failed to be jettisoned as planned. Despite completing rest of the flight with all other systems working as expected, with about 1000 kg of extra weight ^[42] orbit achieved was 167.4 x 6554.8 km at 19.18° inclination well below the intended 284 x 20650 km at 19.2° inclination. ^[43] After fourth stage engine cut off IRNSS-1H separation occurred, leaving it adrift inside the closed payload fairing. This was second event of total failure in PSLV launch history since 1993. ^{[44] [45]}

Launch statistics

Rocket configurations

1

2

3

4

5

6

'93

1995

2000

2005

2010

2015

2020

•   PSLV-G
•   PSLV-CA
•   PSLV-XL
•   PSLV-DL
•   PSLV-QL

Launch sites

1

2

3

4

5

6

'93

1995

2000

2005

2010

2015

2020

•   Satish Dhawan First LP
•   Satish Dhawan Second LP

Launch outcomes

1

2

3

4

5

6

'93

1995

2000

2005

2010

2015

2020

•   Failure
•   Partial failure
•   Success
•   Scheduled

Launch history

As of January 1,2024 ^[update] the PSLV has made 60 launches, with 57 successfully reaching their planned orbits, two outright failures and one partial failure, yielding a success rate of 95% (or 97% including the partial failure). ^[46] All launches have occurred from the Satish Dhawan Space Centre, known before 2002 as the Sriharikota Range (SHAR).

Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
D1	20 September 1993 05:12	PSLV-G	First	IRS-1E	846 kg			Failure
	Maiden flight; Attitude control failure at second stage separation. [1]
D2	15 October 1994 05:05	PSLV-G	First	IRS-P2	804 kg			Success
	[47]
D3	21 March 1996 04:53	PSLV-G	First	IRS-P3	920 kg			Success
	[48]
C1	29 September 1997 04:47	PSLV-G	First	IRS-1D	1250 kg			Partial failure
	First operational flight; Fourth stage under-performed resulting in lower than planned orbit. Satellite used own propulsion to move to correct orbit. [49]
C2	26 May 1999 06:22	PSLV-G	First	Oceansat-1 DLR-Tubsat Kitsat-3	1050 kg 45 kg 107 kg			Success
	First launch to have foreign satellites, and first to carry multiple satellites. [4] [5]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C3	22 October 2001 04:53	PSLV-G	First	TES PROBA BIRD	1108 kg 94 kg 92 kg			Success
	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. [50] [51]
C4	12 September 2002 10:23	PSLV-G	First	MetSat-1 (Kalpana-1)	1060 kg			Success
	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. [52] [53] [54]
C5	17 October 2003 04:52	PSLV-G	First	RESOURCESAT-1 (IRS-P6)	1360 kg			Success
	Payload capability had been progressively increased by more than 600 kg since the first PSLV launch. Launch took place despite heavy rain. [55] [56]
C6	5 May 2005 04:45	PSLV-G	Second	Cartosat-1 HAMSAT	1560 kg 42.5 kg			Success
	First PSLV launch from the second launch pad. [57]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C7	10 January 2007 03:54	PSLV-G	First	Cartosat-2 SRE-1 LAPAN-TUBsat PEHUENSAT-1	680 kg 500 kg 56 kg 6 kg			Success
	First flight of hardware upgrade, first launch of reentry capsule (SRE). [58]
C8	23 April 2007 10:00	PSLV-CA	Second	AGILE AAM (attached to PS4)	352 kg 185 kg			Success
	First flight of the 'Core-Alone' configuration. ISRO's first commercial launch (foreign satellite as the main payload). [59] [60]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C10	21 January 2008 03:45	PSLV-CA	First	TecSAR	295 kg			Success
	ISRO's second commercial launch (foreign satellite as the main payload). [61] [62]
C9	28 April 2008 03:53	PSLV-CA	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
	[63] [64]
C11	22 October 2008 00:52	PSLV-XL	Second	Chandrayaan-1	1380 kg			Success
	First flight of the PSLV-XL configuration, first Indian Lunar probe. [65] [66]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C12	20 April 2009 01:15	PSLV-CA	Second	RISAT-2 ANUSAT	300 kg 40 kg			Success
	India's first radar imaging satellite, RISAT. [67] [68]
C14	23 September 2009 06:21	PSLV-CA	First	Oceansat-2 Rubin 9.1 (attached to PS4) Rubin 9.2 (attached to PS4) SwissCube-1 BeeSat UWE-2 ITUpSAT1	960 kg 8 kg 8 kg 1 kg 1 kg 1 kg 1 kg			Success
	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. [69] [70] [71] [72] [73] [74]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C15	12 July 2010 03:52	PSLV-CA	First	Cartosat-2B ALSAT-2A AISSat-1 TIsat-1 STUDSAT	694 kg 117 kg 6.5 kg 1 kg 0.95 kg			Success
	AISSat-1 and TIsat are part of NLS-6. [75] [76] [77] [78] [79] [80] [81]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C16	20 April 2011 04:42	PSLV-G	First	ResourceSat-2 X-Sat YouthSat	1206 kg 106 kg 92 kg			Success
	[82]
C17	15 July 2011 11:18	PSLV-XL	Second	GSAT-12	1410 kg			Success
	First use of Vikram flight computer. [83] [84]
C18	12 October 2011 05:31	PSLV-CA	First	Megha-Tropiques SRMSAT Jugnu VesselSat-1	1000 kg 10.9 kg 3 kg 28.7 kg			Success
	[85] [86]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C19	26 April 2012 00:17	PSLV-XL	First	RISAT-1	1858 kg			Success
	[87] [88]
C21	9 September 2012 04:23	PSLV-CA	First	SPOT-6 mRESINS (attached to PS4) PROITERES	720 kg 50 kg 15 kg			Success
	mRESINS tested avionics for future PSLV launches. ISRO's third commercial launch (foreign satellite as the main payload). ISRO's 100th mission. [89] [90]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C20	25 February 2013 12:31	PSLV-CA	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
	TUGSAT-1 and UniBRITE were the first Austrian satellites. [91] [92] [93]
C22	1 July 2013 18:11	PSLV-XL	First	IRNSS-1A	1425 kg			Success
	India's first regional navigation satellite. [18]
C25	5 November 2013 09:08	PSLV-XL	First	Mars Orbiter Mission	1350 kg			Success
	India's first Mars mission. [94] [95]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C24	4 April 2014 11:44	PSLV-XL	First	IRNSS-1B	1432 kg			Success
	India's second regional navigation satellite. [96] [97]
C23	30 June 2014 04:22	PSLV-CA	First	SPOT-7 CanX-4 CanX-5 AISAT VELOX-1	714 kg 15 kg 15 kg 14 kg 7 kg			Success
	ISRO's fourth commercial launch (foreign satellite as the main payload). [98]
C26	16 October 2014 20:02	PSLV-XL	First	IRNSS-1C	1425.4 kg			Success
	Seventh PSLV-XL and third Navigation Satellite launch. [99] [100]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C27	28 March 2015 11:49	PSLV-XL	Second	IRNSS-1D	1425 kg			Success
	Eighth PSLV-XL and fourth Navigation Satellite launch. [101]
C28	10 July 2015 16:28	PSLV-XL	First	UK-DMC3A UK-DMC3B UK-DMC3C CBNT-1 DeOrbitSail	447 kg 447 kg 447 kg 91 kg 7 kg			Success
	At the time it was the heaviest commercial mission (1439 kg) successfully accomplished using a launch vehicle assembled by ISRO. [102] [103] [104]
C30	28 September 2015 04:30	PSLV-XL	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
	Launch of India's first dedicated multi-wavelength space observatory and ISRO's first launch of US satellites. [105]
C29	16 December 2015 12:30	PSLV-CA	First	TeLEOS-1 VELOX-C1 VELOX-II Kent Ridge-1 Galassia Athenoxat-1 [106] [107]	400 kg 123 kg 13 kg 78 kg 3.4 kg 4.8 kg			Success
	Commercial launch of 6 Singaporean satellites. Fourth stage re-ignition demonstrated successfully after payload deployment. [108] [109] [20]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C31	20 January 2016 04:01	PSLV-XL	Second	IRNSS-1E	1425 kg			Success
	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. [110] [111] [112]
C32	10 March 2016 10:31	PSLV-XL	Second	IRNSS-1F	1425 kg			Success
	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. [113] Launch initially scheduled for 10:30 was delayed by one minute to avoid space debris. [114]
C33	28 April 2016 07:20	PSLV-XL	First	IRNSS-1G	1425 kg			Success
	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) [115] [116] [117] [118] [119]
C34	22 June 2016 03:55	PSLV-XL	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
	ISRO's Cartosat-2C and 19 other satellites launched. [120] [121] [122] [123] [124] [125]
C35	26 September 2016 03:42	PSLV-G	First	ScatSat-1 ALSAT-2B ALSAT-1B Pathfinder-1 Pratham CanX-7 (NLS-19) [126] ALSAT-1N PISat	371 kg 117 kg 103 kg 44 kg 10 kg 8 kg 7 kg 5.25 kg			Success
	ISRO's longest PSLV satellite launch mission. First mission of PSLV in which it launched its payloads into two different orbits. [127] [128] [129] [130] [131] [132]
C36	7 December 2016 04:55	PSLV-XL	First	Resourcesat-2A	1235 kg			Success
	[133] [134] [135] [136] [137] [138]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C37	15 February 2017 03:58	PSLV-XL	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 4.6 kg x 8			Success
	PSLV-C37 successfully carried and deployed a record 104 satellites in the sun-synchronous orbit. [139] [140] [141] [142] [143] [144]
C38	23 June 2017 03:59 [145] [146]	PSLV-XL	First	Cartosat-2E [147] NIUSAT [148] CESAT-1 [149] Lemur-2 × 8 , , Blue, Red, Green Diamonds , Max Valier Sat [150] Venta-1 D-Sat [151] 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 [152] ) KickSat Sprites × 6 (All flown with Venta-1 and Max Valier Sat)	727 kg 15 kg 60 kg 4 kg x 8 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 ? kg ? kg			Success
	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 [153] [154] [155] [156] [157] [158]
C39	31 August 2017 13:30 [159] [160] [161]	PSLV-XL	Second	IRNSS-1H	1425 kg			Failure
	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. [162] [163] [164] [165]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C40	12 January 2018 03:59	PSLV-XL	First	Cartosat-2F [166] MICROSAT-TD INS-1C [167] LEO-1 [168] Carbonite-2 aka (VividX2) ICEYE X1 Landmapper-BC3 Arkyd 6A CICERO-7 4 x Doves Flock-3p' [169] 4 x Lemur-2 [170] PicSat SIGMA (KHUSAT-03) [171] CANYVAL-X (Tom and Jerry) CNUSail 1 KAUSAT 5 STEP Cube Lab MicroMAS-2 Fox-1D 4 x SpaceBEE [172] Tyvak-61C (GeoStare) [173] DemoSat-2	710 kg ~120 kg 11 kg 168 kg 100 kg ?? kg 10 kg 10 kg 10 kg 4 x ?? kg 4 x ?? kg 3.5 kg 3.8 kg 4 kg 4 kg 3.2 kg 1 kg 3.8 kg 1.5 kg 1.27 kg 4 kg ? kg			Success
	[174] [175] [176] [177] [178] [179] [180]
C41	11 April 2018 22:34	PSLV-XL	First	IRNSS-1I	~1425 kg	sub GTO		Success
	[181] [182] [183] [184] [185] [186] [187] [188]
C42	16 September 2018 16:38	PSLV-CA	First	NovaSAR-S (445 kg) SSTL S1-4 (444 kg)	889 kg	Low Earth	SSTL	Success
	[189] [190] [191] [192] [193] [194]
C43	29 November 2018 04:28	PSLV-CA	First	HySIS [195] Doves × 16 (Flock 3r) Global-1 Lemur-2 × 4 HSAT-1 CICERO-8 Hiber-1 FACSAT-1 Innosat-2 Centauri-1 CASE Reaktor Hello World ³Cat-1	380 kg 16 x ?? kg 55 kg 4 x ?? kg 13 kg 10 kg ?? kg ?? kg 4 kg ?? ?? ?? 1.2 kg Total=641.5 kg	Low Earth		Success
	[196] [197] [198] [199] [200] [201] [202] [203] [204] [205]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C44	25 January 2019 18:07	PSLV-DL	First	Microsat-R Kalamsat V2 (attached to PS4)	740 kg 1.2 kg	Low Earth	DRDO Space Kidz	Success
	First flight of PSLV-DL variant. Propellant tank on fourth stage (PS4) made out of Aluminum alloy instead of Ti-6Al-4V. [206] [207] [208] [209] [210] [211] [212] [213]
C45	1 April 2019 03:57	PSLV-QL	Second	EMISAT Doves × 20 (Flock 4a) Lemur-2 × 4 M6P BlueWalker1 Aistechsat-3 Astrocast-2 ExseedSat-2 (attached to PS4) ARIS 101F (attached to PS4) [214] ISRO AIS payload (attached to PS4)	436 kg 5.7 kg each 5.2 kg each 6.8 kg 10 kg 2.3 kg 3.8 kg ? kg 10 kg ? kg	Low Earth	DRDO	Success
	Flight C45. EMISAT (436 kg) and rideshares (220 kg) [215] [216] [217] [218] [219] [220] [221] [222] [223]
C46	22 May 2019 00:00	PSLV-CA	First	RISAT-2B	615 kg	Low Earth		Success
	Flight C46. RISAT-2B [224] [225] [226] [227] [228] [229] [230]
C47	27 November 2019 03:58	PSLV-XL	Second	Cartosat-3 Meshbed [231] SuperDoves × 12 (Flock 4p)	1,625 kg 4.5 kg ? kg	Low Earth		Success
	Semi-Conductor Laboratory fabricated Vikram 1601 processor used for first time in navigation computer of launch vehicle [232] after being test flown in redundant configuration [233] on PSLV C46 mission. [234] [235] [236]
C48	11 December 2019 09:55	PSLV-QL	First	RISAT-2BR1 QPS SAR-1 "Izanagi"「イザナギ」 [237] Lemur-2 × 4 [238] Duchifat-3 [239] 1HOPSAT [240] Tyvak-0129 [240] [241] Tyvak-0092 (COMMTRAIL/NANOVA) [242] [240] [243]	628 kg ~100 kg ? kg 2.3 kg 22 kg 11 kg 5 kg	Low Earth		Success
	Flight C48 - 50th Flight of PSLV. [224] [226] [244] [245] [246]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C49	7 November 2020 09:42	PSLV-DL	First	EOS-01 (formerly RISAT-2BR2) Lemur-2 × 4 KSM-1A, 1B, 1C, 1D R2	630 kg [247] ? ? ?	Low Earth		Success
	Second flight of PSLV-DL variant. [224] [225] [226] [248] [249] [250] [251] [252] [253]
C50	17 December 2020 10:11	PSLV-XL	Second	GSAT-12R (CMS-1)	1425 kg [254]	sub GTO	ISRO	Success
	[255] [256] [257] [258] [259]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C51	28 February 2021 04:54	PSLV-DL	First	Amazônia-1 Satish Dhawan Sat SpaceBEE (×12) SAI-1 Nanoconnect-2 SindhuNetra UNITYSats (x3)	637 kg 1.9 kg ~4 kg x 12 N/A 10 kg N/A	Low Earth		Success
	Flight C51. [260] [261] [262] [263] [264] [265] [36]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C52	14 Feb 2022 00:29	PSLV-XL	First	EOS-4/RISAT-1A INSPIRESat-1 INS-2TD	1710 kg 8.7 kg 17.5 kg	Low Earth	ISRO	Success
	Flight C52, RISAT-1A satellite for Earth observation [226] [266] [267] [268] [269] [270]
C53	30 June 2022 12:32 [271]	PSLV-CA	Second	DS-EO NeuSAR SCOOB-I 6 × payloads on POEM-1	365 kg 155 kg 2.8 kg	Low Earth	DSTA	Success
	Primary payload is DS-EO electro-optical satellite by Defence Science and Technology Agency with two other small satellites from Singapore to low Earth equatorial orbit. [272] It also carries the PSLV Orbital Experimental Module (POEM) that is attached to upper stage to carry in-orbit experiments and carries 6 hosted payloads.
C54	26 November 2022 06:26 [273] [274]	PSLV-XL	First	Oceansat-3/EOS-6 4× Astrocast-2 BhutanSat (aka INS-2B) Pixxel TD-1 Anand Thybolt 1 & Thybolt 2	1117 kg 17.92 kg 18.28 kg 16.51 kg 1.45 kg	Low Earth	ISRO	Success
	Flight C54. [275] [266] [276] [277]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C55	22 April 2023 08:50 [278] [279]	PSLV-CA	First	TeLEOS-2 Lumelite-4 7 × payloads on POEM-2	741 kg 16 kg	Low Earth	DSTA	Success
	Flight C55, commercial launch by NSIL. First launch operation of a rocket partially assembled at PSLV Integration Facility (PIF) [280] First flight of PSLV-CA without Aerodynamic Stabiliser (AST) modules. [281] [282]
C56	30 July 2023 01:01 [283] [284]	PSLV-CA	First	DS-SAR Arcade Velox-AM ORB-12 STRIDER Galassia-2 SCOOB-II NuLIon	360 kg 50 kg	Low Earth	DSTA	Success
	Flight C56. [285] [286]
C57	2 September 2023 06:20 [287]	PSLV-XL	Second	Aditya-L1	1480.7 kg	Halo orbit	ISRO	Success
	Flight C57, solar coronal observation mission [288] [289]
Flight No.	Date / time (UTC)	Rocket, Configuration	Launch site	Payload	Payload mass	Orbit	User	Launch Outcome
C58	1 January 2024 03:40 [290] [291]	PSLV-DL	First	XPoSat 10 × payloads on POEM-3	741 kg 16 kg	Low Earth	ISRO	Success
	Flight C58. [292] [293] [294] [295]

Future launches

Date / time (UTC)	Flight	Rocket, Configuration	Launch site	Payload	Orbit	User
Q1 2024 [285]	C59	PSLV-XL	TBD	ANVESHA SCOT CGUSAT LEAP-1 [296]	Low Earth	DRDO
	Flight C59. [297]
Q2 2024 [285]	C60	PSLV-XL	TBD	RISAT-1B	Low Earth
	Flight C60, follow on to RISAT-1A.
Q2 2024 [285]	C61	PSLV	TBD	ISRO Payload	TBD
	Flight C61. [297] payload will most probably be Cartosat-3A (EOS-08)
September 2024 [298]	C62	PSLV-XL	TBD	PROBA-3 Occulter and Coronagraph	Highly elliptical	European Space Agency
	Proba-3 is a dual probe technology demonstration mission by the ESA for solar coronagraphy.
Q3 2024	N1	PSLV	TBD	TDS-01		ISRO
	Technology Demonstrator Satellite 01 mission. First fully privately built PSLV. [297] [299] [300]
Q3 2024	C63	PSLV	TBD	SPADEX		ISRO
	Payload will most probably be the SPADEX Mission. [297] [301] [302]
Q4 2024-Q1 2025	N2	PSLV	TBD	NSIL Payload Aadyah DRISHTI Sanskardhaam DS P30 x2		ISRO
	Second fully privately built PSLV. [297]
2026 [303]	C?	PSLV	TBD	TRISHNA	SSO	ISRO, CNES
	The Trishna mission is designed to observe Earth's surface in the thermal infrared domain. [304]
2028	C?	PSLV	TBD	Chandrayaan-4 (Sample return mission)	TEI	ISRO
	Transfer module will collect the samples from the ascend stage, transfer them to the reentry module, fire its engine to set both itself and the re-entry module towards Earth, release the payload, and loop back around the Earth

Gallery

• 
  PSLV - C54 Liffed off from Satish Dhawan Space Center's , First Launch Pad.
• 
  PSLV C53 Clears Second Launch Pad of Satish Dhawan Space Centre , Shriharikota
• 
  PSLV C52 lifting off from First Launch Pad
• 
  PSLV-C49 lift off
• 
  PSLV C45 ignition
• 
  Top view of PSLV C45
• 
  PSLV C48 RISAT-2BR1 lift-off from First Launch Pad
• 
  PSLV C11 lift off
• 
  PSLV C44 lift off

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