Family-level launch record combining canonical variants, historical missions, public cadence forecasts, and available payload performance specs.
Historical missions are grouped by actual launch year. Forecast cadence uses family-level launch-rate rows.
| Year | Historical missions | Forecast launches |
|---|---|---|
| 2019 | 5 | 0 |
| 2020 | 2 | 0 |
| 2021 | 1 | 0 |
| 2022 | 3 | 0 |
| 2023 | 3 | 0 |
| 2024 | 3 | 0 |
| 2025 | 1 | 0 |
| 2026 | 1 | 8 |
| 2027 | 0 | 8 |
| 2028 | 0 | 8 |
| 2029 | 0 | 8 |
| 2030 | 0 | 8 |
| 2031 | 0 | 8 |
| 2032 | 0 | 8 |
| 2033 | 0 | 8 |
| 2034 | 0 | 8 |
| 2035 | 0 | 8 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
PSLV-XL | LEO | 3,800 kg | 200 km | 30 deg | Gunter Krebs / Skyrocket PSLV-XL profile |
PSLV-DL | LEO | 3,800 kg | Unknown | Unknown | Space Launch Schedule PSLV-DL vehicle page |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| Launch 2026-F01 | PSLV-DL | Jan 12, 2026 |
| Launch 2025-F05 | PSLV-XL | May 18, 2025 |
| SPADEX | PSLV CA | Dec 30, 2024 |
| PROBA-3 |
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
PSLV | Not stated | 3 | Retired |
PSLV C | Not stated | 9 | Retired |
PSLV CA | Not stated | 18 | Active |
PSLV-DL | Not stated | 5 | Active |
| 2036 | 0 | 8 |
| 2037 | 0 | 8 |
| 2038 | 0 | 8 |
| 2039 | 0 | 8 |
| 2040 | 0 | 8 |
| 2041 | 0 | 8 |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2027 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2028 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2029 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2030 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2031 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2032 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2033 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2034 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2035 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2036 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2037 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2038 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2039 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2040 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. |
| 2041 | Satish Dhawan Space Centre | PSLV launch pads | 8 | 25% | Editable low-confidence annual throughput seed. Site-year coverage backfill copied nearest prior site-rate row. |
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
PSLV CA | LEO | 3,800 kg | Unknown | Unknown | Space Launch Now PSLV-CA vehicle page |
PSLV-DL | SSO | 1,750 kg | 600 km | Unknown | ISRO PSLV page and Space Launch Schedule PSLV-DL vehicle page |
PSLV | SSO | 1,750 kg | 600 km | Unknown | ISRO PSLV page |
PSLV-XL | SSO | 1,750 kg | 600 km | Unknown | ISRO PSLV page |
PSLV-XL | GTO | 1,425 kg | Unknown | Unknown | ISRO PSLV page |
PSLV | GTO | 1,425 kg | Unknown | Unknown | ISRO PSLV page |
PSLV-XL | GTO | 1,300 kg | Unknown | Unknown | Gunter Krebs / Skyrocket PSLV-XL profile |
PSLV-DL | GTO | 1,200 kg | Unknown | Unknown | Space Launch Schedule PSLV-DL vehicle page |
PSLV CA | GTO | 1,200 kg | Unknown | Unknown | Space Launch Now PSLV-CA vehicle page |
PSLV CA | SSO | 1,092 kg | 622 km | Unknown | Space Launch Now PSLV-CA vehicle page |
PSLV-XL |
| Dec 5, 2024 |
| XPoSAT Mission | PSLV-DL | Jan 1, 2024 |
| Aditya-L1 Mission | PSLV-XL | Sep 2, 2023 |
| DS-SAR Mission | PSLV CA | Jul 30, 2023 |
| TeLEOS-2 | PSLV CA | Apr 22, 2023 |
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
PSLV-QL | Not stated | 2 | Retired |
PSLV-XL | Not stated | 27 | Active |
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
Editable low-confidence annual throughput seed.
ISRO has not released a failure analysis report detailing key findings and corrective measures for the May 2025 PSLV failure as of the present account.
Vikram-I was designed by many former ISRO engineers who were associated with the PSLV or SSLV and may be using many common contractors.
The SSLV’s second-stage motor is derived from the PSLV’s third-stage motor.
Sixteen spacecraft were lost to air and sea in the January 12 PSLV failure.
The January 12 PSLV launch failed due to anomalous performance of the rocket’s third stage that resulted in visible tumbling on mission control telemetry and the livestream.
The January 12 flight was the 64th flight of the PSLV launch vehicle.
The PSLV and the GSLV Mk II share the S139 solid rocket booster as their core stage.
KID was part of the payload carried by the Indian PSLV rocket launched on 12 January.
The KID prototype survived the failed PSLV mission.
The PSLV mission failed to place its payloads into their intended orbits and failed overall.
Marcy Mabry previously worked on the launch of the first Amazonia-1 satellite in 2021 using an Indian PSLV launcher.
The first Amazonia-1 satellite was launched on board an Indian PSLV in February 2021.
Amazonia-1B is the direct successor to Amazonia-1, which launched in February 2021 on an Indian PSLV.
The first Amazônia satellite was launched aboard an Indian PSLV rocket in February 2021.
KID was the last co-passenger payload to be connected with the PSLV fourth stage and was slated to re-enter the Earth’s atmosphere toward splashdown in the South Pacific Ocean.
The previous PSLV mission, PSLV-C61 launched in May 2025, also failed to reach orbit because of a problem with the third stage.
The failure analysis committee report on the loss of PSLV-C61 has not been placed in the public domain.
ISRO established a failure analysis committee (fact-finding committee) to identify the reasons behind the PSLV-C62 mission loss.
The PSLV third stage uses solid propellant, produces a maximum thrust of 250 kilonewtons, and has a burn duration of just under two minutes.
Until the recent PSLV failures, all ISRO missions carrying foreign payloads had been successful.