Pegasus XL | ST-5 FWD

A Pegasus XL rocket launched Pegasus XL | ST-5 FWD from Air launch to orbit, targeting LEO.

Launch time
Status
SUCCESS
Operator
Orbital Sciences Corporation
Mission type
Test Flight
Launch pad
Vandenberg Space Force Base
Payload
—
Target orbit
LEO
Pegasus XL | ST-5 FWD cover image

Mission timeline

  1. 2006-03-22T14:03:45.000Z
    Liftoff
    Pegasus XL roars off the pad at Air launch to orbit.
  2. Max-Q
    The vehicle reaches Max Q, the highest aerodynamic load of the flight.
  3. Main engine cutoff (MECO)
    MECO — first-stage propulsion ends after a nominal burn.
  4. Stage separation
    Clean stage separation confirmed.
  5. Second-stage ignition
    The upper-stage engine lights up after separation.
  6. Orbit insertion
    Orbit insertion confirmed — now circling in LEO.
  7. Mission success
    All mission objectives achieved.

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