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Gurwin
Gurwin 1 Credit: Manufacturer Image |
Israeli technology satellite. Gurwin satellites were built by the Technion Institute of Technology, Israel.
Status: Operational 1995. First Launch: 1995-03-28. Last Launch: 1998-07-10. Number: 2 . Gross mass: 50 kg (110 lb).
The technology test satellites included CCD cameras, a radiation detectors, ozone monitors, amateur radio transmitters, and other satellite technology payloads.
More at: EKA 2
techsat-1.
Family:
Sun synchronous orbit,
Technology,
Technology satellite.
Country:
Israel.
Launch Vehicles:
Topol',
Start,
Zenit-2.
Launch Sites:
Baikonur,
Plesetsk,
Baikonur LC45/1,
Plesetsk LC158.
Agency:
Technion.
Bibliography:
2,
5,
12523.
1995 March 28 - .
10:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC158.
LV Family:
Topol'.
Launch Vehicle:
Start.
FAILURE: Fell in Sea of Okhotsk..
Failed Stage: 3.
- Gurwin 1 - .
Payload: TECHSAT-1. Mass: 50 kg (110 lb). Nation: Israel.
Agency: RVSN.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: Gurwin.
Decay Date: 1995-03-28 .
1998 July 10 - .
06:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2.
- Gurwin Techsat 1B - .
Mass: 50 kg (110 lb). Nation: Israel.
Agency: RVSN.
Manufacturer: Technion.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: Gurwin.
USAF Sat Cat: 25397 . COSPAR: 1998-043D. Apogee: 819 km (508 mi). Perigee: 817 km (507 mi). Inclination: 98.80 deg. Period: 101.30 min. Built by Technion-Israel Institute of Technology. Replaced earlier Russian-launched Techsat which failed to orbit in 1995..
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