Mission
Technology · GTO
2 satellites officially described as for "demonstration of new technologies for spatial targets detection" purposes.
What it put in orbit
| Object | Type | Orbit | Globe |
|---|---|---|---|
| SHIJIAN-29A (SJ-29A) 2025-315A | Payload | 35757 × 35816 km · 3.7° | Globe |
| CZ-7A R/B 2025-315B | Rocket body | 175 × 31456 km · 19.8° | Globe |
| SHIJIAN-29B (SJ-29B) 2025-315C | Payload | 35757 × 35816 km · 3.7° | Globe |
COSPAR ID 2025-315 (data from GCAT, J. McDowell, CC BY 4.0). Orbits from the CelesTrak satellite catalogue (perigee × apogee, inclination).