Vehicle: Proton M/ Breeze M
The Satellite
- Satellite Operator: ARABSAT
- Satellite Manufacturer: Astrium
- Purpose: Video Broadcasting
- Platform: Eurostar E2000+
- Separated Mass: 3280 kg
- Satellite Design Life: 15 years
Highlights
- 4th Proton Launch of the Year
- 5th ILS Proton Launch of the Year
- 7th Astrium Eurostar Satellite Bus
Latest News
Mission Success for BADR-4
Launch Resources
- Mission Overview
- Media Advisory
Final Details of the Launch and Separation
- Liftoff occurred at the beginning of the launch window, Thursday Nov. 9, at 2:01 a.m. local time (Nov 8: 14:01 EST, 20:01 GMT).
- Nominal separation took place at 6:01 a.m. local time, Nov. 9 (Nov. 8: 18:01 EST, Nov 9: 00:01 GMT)
- Separation of the BADR-4 satellite occured approximately 4 hours after liftoff.
- Orbit Parameters: Predicted: 3150 km x 35,786 km x 14.2 degrees.
- SC Separation
- Fourth Burn
- APT Jettison
- Third Burn
- Second Burn
- First Burn
- Stage Separations
- Liftoff
- Rollout to Pad 39
- Breeze M Fueling
- Begin Joint Operations
- SC Fuel Loading
- Breeze M Arrival
- SC/GSE Arrival
- Proton Arrival
- Early Team Arrival