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ID: 4MISSION PROFILE
Agnibaan SOrTeD-2
"Agnikul Cosmos second SubOrbital Technology Demonstrator flight validating propulsion and control systems at higher altitudes."
LAUNCH WINDOW: January 1, 1970
SDSC SHAR, SRIHARIKOTA
Agnibaan
Payload Configuration Active
LAUNCH VEHICLE
Agnibaan
Medium-to-Heavy Expendable
TARGET ORBIT
Suborbital
Velocity & Flight Path Optimized
PRIMARY MISSION OBJECTIVES
01
Propulsion Systems Test
Evaluation of the Agnibaan launch system's core stages and guidance units in flight conditions.
02
Orbital Insertion Precision
Establish telemetry lock and deploy payload spacecraft exactly within target Suborbital coordinate thresholds.
03
Ground Control Handshake
Deploy tracking dishes and establish multi-station communication matrices with space centers in India.
Live Telemetry
Agnibaan SOrTeD-2
Agnibaan • Suborbital
Agnikul Cosmos
SDSC SHAR, Sriharikota
"Agnikul Cosmos second SubOrbital Technology Demonstrator flight validating propulsion and control systems at higher altitudes."
MISSION OPERATOR
Agnikul Cosmos
Private Space Corporation
Launch SiteSDSC SHAR (SLP)
Payload Mass~2500 kg (Classified)
Sector TypeCommercial / Civil