MISSION 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

AgnibaanSuborbital

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