MNV-0904 · SL-8 R/B DEB
OG-3 Sentinel-A — cross-track burn, executed
Delta-v0.08m/s
Propellant0.001kg
Axiscross-track
Executed5d 2h ago
Statusexecuted
Burn performed. Post-burn state vector confirmed by tracking.
Effect on the event
Pc before1.2×10−4
Pc after3.1×10−7
- Conjunction
- CJ-4412 (cleared)
- Spacecraft
- OG-3 Sentinel-A
- Secondary
- SL-8 R/B DEB
- Operator
- A. Lindqvist
Propellant cost
This burn0.001kg
Remaining3.41kg
SK runway6.5yr
3.410 kg after burnreserve 0.8 · capacity 5.0 kg
Already drawn down — the remaining figure above is post-burn.
Orbit response
Gauss variational · Clohessy–Wiltshire
Δ semi-major axis0m
Δ period0.000s
Δ inclination6.0e-4deg
A cross-track burn rotates the orbit plane rather than changing the period, so separation appears immediately at the burn point rather than accumulating.
Propulsion
Tsiolkovsky
Specific impulse1600s
Thrust0.011N
Vehicle mass208.4kg
Propellant0.0011kg
Burn duration1516s
Mass fraction5.1e-6
- System
- Xenon Hall-effect thruster
- Δv capability remaining
- 197.7 m/s
- Avoidance burns of this size left
- 2,455
Low-thrust system — the burn spans a meaningful fraction of an orbit, so it is modelled as finite rather than impulsive and the achieved delta-v is direction-averaged.
Downstream conjunctions
not modelled
No downstream screening on file for this burn. Historical burns retain their record but not the re-screening that followed.