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Orbimage
American agency. Orbital Imaging Corp, Dulles, USA.
Location: Dulles.
Country:
USA.
1995 April 3 - .
13:48 GMT - .
Launch Site:
Point Arguello.
Launch Complex:
Point Arguello WADZ.
Launch Pad: Aircraft from Vandenberg..
Launch Platform: L-1011.
LV Family:
Pegasus.
Launch Vehicle:
Pegasus H.
- Orbview-1 - .
Payload: Microlab 1. Mass: 74 kg (163 lb). Nation: USA.
Agency: Orbimage.
Program: Orbview.
Class: Earth.
Type: Atmosphere satellite. Spacecraft: Microstar.
USAF Sat Cat: 23547 . COSPAR: 1995-017C. Apogee: 747 km (464 mi). Perigee: 733 km (455 mi). Inclination: 70.00 deg. Period: 99.60 min. Lightning mapper; GPS radio occultation. Air dropped in Point Arguello WADZ..
1997 August 1 - .
20:20 GMT - .
Launch Site:
Point Arguello.
Launch Complex:
Point Arguello WADZ.
Launch Pad: Aircraft from Vandenberg..
Launch Platform: L-1011.
LV Family:
Pegasus.
Launch Vehicle:
Pegasus XL.
- Orbview-2 - .
Payload: Seastar. Nation: USA.
Agency: Orbimage.
Manufacturer: Germantown.
Program: Orbview.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: PegaStar.
Spacecraft: Orbview-2.
USAF Sat Cat: 24883 . COSPAR: 1997-037A. Apogee: 708 km (439 mi). Perigee: 707 km (439 mi). Inclination: 98.20 deg. Period: 98.90 min. Air dropped in Point Arguello WADZ..
2001 September 21 - .
18:49 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576E.
LV Family:
Taurus.
Launch Vehicle:
Taurus 2110.
FAILURE: A problem a few seconds after first stage separation caused the rocket to go off course; it recovered and the remainder of the stages fired, but final cutoff velocity was too low to reach a sustainable orbit..
Failed Stage: G.
- Orbview-4 - .
Mass: 368 kg (811 lb). Nation: USA.
Agency: Orbimage.
Manufacturer: OSC.
Program: Orbview.
Class: Surveillance.
Type: Civilian surveillance satellite. Spacecraft Bus: LEOStar.
Spacecraft: Orbview.
COSPAR: F010921A.
Launch delayed from June 27, July 18/22, August 12/21 and September1. The Orbital Sciences Taurus 2110 failed to remain in orbit. A problem a few seconds after first stage separation caused the T6 rocket to go off course; the rocket recovered and the remainder of the stages fired, but final cutoff velocity was too low to reach a sustainable orbit. The Castor 120 zero stage was on course but the Orion 50S first stage motor went off course. The satellites separated from the final stage as planned but burned up in the earth's atmosphere northeast of Madagascar before completing the first orbit. The final orbit was about 75-80 km x 425-430 km x 97 deg. The primary payload was the OrbView-4 imaging satellite. OrbView-4, built by Orbital, was a 368 kg box-shaped spacecraft carrying a 1-m resolution panchromatic camera and an 8-m resolution 200-channel hyperspectral imager with a 0.45-meter aperture. It was to be used by the US Air Force.
- Celestis-4 - .
Mass: 368 kg (811 lb). Nation: USA.
Agency: Orbimage.
Manufacturer: OSC.
Program: Celestis.
Class: Burial .
Type: Burial satellite. Spacecraft Bus: Pegasus-3.
Spacecraft: Celestis.
COSPAR: F010921D. Celestis-4 consisted of two Celestis burial canisters containing cremated human remains. After the launch vehicle failure Celestis guaranteed a relaunch of back-up remains..
- SBD - .
Mass: 368 kg (811 lb). Nation: USA.
Agency: Orbimage.
Manufacturer: OSC.
Class: Technology.
Type: Navigation technology satellite. Spacecraft Bus: Microstar.
Spacecraft: SBD.
COSPAR: F010921C.
SBD, the Orbital Sciences' Special Bus Design. The 73 kg satellite was a test version of an enlarged Microstar bus. It would have remained attached to the third stage, together with two Celestis burial canisters containing cremated human remains, and an experimental third stage avionics box.
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