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Track OPS 0757 (TACSAT) Satellite in Real Time

Detailed information about OPS 0757 (TACSAT) satellite

Designator id: 1969-013A

Description of OPS 0757 (TACSAT) Satellite:

TacSat was designed to experimentally test and develop tactical communications concepts for all US military services. The mission evaluated the feasibility of using satellite communication repeaters with small surface terminal communication equipment for highly mobile land, sea and air forces. This project was led by the USAF Space and Missile Systems Organization (SAMSO). It was a cylindrical shaped aluminum structure with passive thermal control. It was spin stabilized (54 rpm) to 0.1 deg using new gyrostat technique. Body mounted solar cells generated 980 W max.

The vehicle carried two transponders, one at X-band and one at UHF. The X-band transponder had a bandwidth of 10 Mhz and a maximum RF power of 30 watts. The UHF transponder has a bandwidth of 10Mhz and a maximum RF output of 230 watts. Provision was made for cross strapping the UHF and X-band up and downlinks with a reduced usable bandwidth of 425 kHz. Earth coverage horn antennas were used at X-band, bifilar helices were used at UHF.


Technical data:

Launch Date: 1969-02-09
Launch Vehicle: Titan III-C
Launch Site: Cape Canaveral, United States
Mass: 640.0 kg
Nominal Power: 980.0 W
Funding Agencies:

Department of Defense-Department of the Air Force (United States)

Disciplines:

Surveillance and Other Military

Source: Nasa

Two Line Element Set (TLE):
1 03691U 69013A   12338.17887655  .00000048  00000-0  10000-3 0  5893
2 03691 007.6977 313.6801 0019874 199.8903 160.0557 01.00400832147809

Last TLE update on :2012-12-04

Find more details about OPS 0757 (TACSAT) Satellite