Spacecraft data:
| Prime manufacturer | EADS Astrium |
| Platform | AstroSat-500 Mk.2 (AstroBus-L) |
| Operator | Spot Image |
| Mass at launch | 712 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | 2 × NAOMI (Pan: 2 m, MS: 8 m ) |
| Solar array | 3 deployable solar arrays |
| Stabilization | |
| Propulsion | Monopropellant hydrazine thrusters |
| DC power | |
| Design lifetime | 10 yrs |
|
 Photo of the fully-integrated PSLV upper stage, with SPOT-7, CanX-4,
CanX-5, and AISat visible (image credit: UTIAS/SFL, ISRO) |