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 |
|---|---|---|
| 2022 | 2 | 0 |
| 2024 | 1 | 0 |
| 2025 | 3 | 0 |
| 2026 | 1 | 4 |
| 2027 | 0 | 5 |
| 2028 | 0 | 6 |
| 2029 | 0 | 6 |
| 2030 | 0 | 6 |
| 2031 | 0 | 6 |
| 2032 | 0 | 6 |
| 2033 | 0 | 6 |
| 2034 | 0 | 6 |
| 2035 | 0 | 6 |
| 2036 | 0 | 6 |
| 2037 | 0 | 6 |
| 2038 | 0 | 6 |
| 2039 | 0 | 6 |
Payload capacity by variant and target orbit when structured capacity rows are available.
| Variant | Orbit | Capacity | Altitude | Inclination | Source |
|---|---|---|---|---|---|
Vega C | LEO | 3,300 kg | Unknown | Unknown | ESA Vega-C page |
Vega C | LEO | 3,000 kg | 500 km | 5.2 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Latest launched missions using variants in this family.
| Mission | Variant | Launch |
|---|---|---|
| SMILE Mission | Vega C | May 19, 2026 |
| Kompsat-7 | Vega C | Dec 1, 2025 |
| CO3D/MicroCarb | Vega C | Jul 26, 2025 |
| Biomass Mission |
Canonical variants rolled up into this launch vehicle family.
| Variant | Stages | Missions | Status |
|---|---|---|---|
Vega C | Not stated | 7 | Active |
Vega-C Block 2 | 4 | 0 | Development |
| 2040 | 0 | 6 |
| 2041 | 0 | 6 |
1 launch location represented.
| Year | Location | Launches | Confidence | Basis |
|---|---|---|---|---|
| 2026 | Guiana Space Centre | Vega Launch Zone | 4 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2027 | Guiana Space Centre | Vega Launch Zone | 5 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2028 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2029 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2030 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2031 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2032 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2033 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2034 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2035 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2036 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2037 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2038 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2039 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2040 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. |
| 2041 | Guiana Space Centre | Vega Launch Zone | 6 | 35% | Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization. Site-year coverage backfill copied n... |
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C | LEO | 2,560 kg | 700 km | 50 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Vega C | LEO | 2,550 kg | 500 km | 50 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Vega C | LEO | 2,470 kg | 500 km | 70 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Vega C | SSO | 2,423 kg | 500 km | 97.4 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Vega C | LEO | 2,410 kg | 700 km | 70 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Vega C | LEO | 2,350 kg | 500 km | 25 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Vega C | LEO | 2,340 kg | 700 km | 25 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Vega C | SSO | 2,300 kg | Unknown | Unknown | ESA Vega-C page |
Vega C | SSO | 2,266 kg | 700 km | 98.2 deg | Avio Vega C User's Manual Issue 1 Rev 0 |
Vega C | SSO | 2,200 kg | 700 km | Unknown | CNES CSG Vega-C page |
Vega C | HEO | 2,200 kg | Unknown | Unknown | Avio Vega C User Manual Issue 1 Rev 0 |
Vega-C Block 2 | LEO | 600 kg | Unknown | Unknown | Space Launch Now Vega-C Block 2 / Space Rider |
Vega C |
| Apr 29, 2025 |
| Sentinel-1C Mission | Vega C | Dec 5, 2024 |
| Launch 2022-F06 | Vega C | Dec 21, 2022 |
| LARES 2 Mission | Vega C | Jul 13, 2022 |
Upcoming mission rows with announced launch timing.
| Mission | Variant | Announced |
|---|---|---|
No forecasted missionsNo upcoming announced mission rows are linked to this vehicle family. | ||
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Vega C cadence curve: conservative European small-launch steady state after return-to-flight and production normalization.
Avio pushed Vega C’s debut from 2019 to March 2020 to accommodate a total of four launches of the current-generation Vega in 2019.
Ital-GovSatCom will use electric propulsion to optimize its weight so the 2,500-kilogram satellite can fit on Vega C.
Vega C is designed to launch 2,200 kg to a 700-kilometer low Earth orbit.
Ital-GovSatCom will weigh roughly 2,500 kg once complete and will launch on Vega C.
Italy’s Ministry of Defence is considering satellites around 2,000 to 2,300 kg so they would be small enough to launch on Vega C or the longer-term Vega E and replace the ten-year-old Sicral-1B satellite.
The four CO3D satellites are expected to launch in 2022 aboard a Vega C rocket.
Airbus’s four Pleiades Neo satellites were scheduled to launch in pairs, one in July 2020 and the second in early 2022 on Vega C missions.
Avio planned one more test-firing of Vega C’s first-stage P120C engine later in 2019 to evaluate the booster configured as a strap-on for Ariane 6.
ArianeGroup and Avio are using booster commonality of the P120C between Ariane 6 and Vega C to increase production scale and lower costs for both rockets.
Vega C is designed to carry 2,200 kg to a 700-kilometer low Earth orbit.
Arianespace and Avio will launch Vega C for the first time in March 2020, sending Lares-2 into a 6,000-kilometer orbit at an inclination of 75 degrees.
The European Space Agency’s April launcher agreement provided missions for the Avio-led Vega C rocket.
The Italian Space Agency decided years earlier to launch the science satellite Lares-2 on the first Vega C flight.
Arianespace plans to phase out Soyuz in the coming years as Europe’s Ariane 6 and Vega C launchers debut in 2020.
Vega C slipped from a maiden flight scheduled for 2019 to early 2020 due to Avio’s 2019 manifest rather than technical delays with the rocket.
Avio builds Europe’s light-lift Vega rocket and is developing the future Vega C rocket.
Physical upgrades to the Vega launch pad in Kourou, French Guiana have been completed to support Vega C, which is about 5 m taller and roughly 70,000 kg heavier than Vega.
Vega C is designed to carry 2,200 kg to a 700-kilometer polar orbit.
Vega C completed its critical design review in February and is ready to complete manufacturing and final testing as part of the qualification phase.
The European Space Agency delayed Vega C’s debut to the first quarter of 2020.