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fahnen/13.jpg Satellite Detail - SEDSat-OSCAR 33
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Photo of SEDSat-OSCAR 33

SEDSat-OSCAR 33
(SEDSat)


Spacecraft Summary

OSCAR Designation:  SEDSat-OSCAR 33     Oscar Number:  SO-33    
International Designator:  1998-061B     Norad Number:  25509    
Common Name:  SEDSat     Satellite Type:  Microsatellite    
Launch Date:  24 October, 1998     Launch Location:  Vandenberg, AFB    
Launch Vehicle:  Delta II     Apogee:  1054.00    
Perigee:  543.00     Inclination:  31.44    
Period:  100.83     Weight:  36.000 Kg    
Organization: Students for the Exploration and Development of Space


Frequency Information
 
Mode V/A (A) Linear Transponder (Inverting): Non-Operational
Uplink: 145.9150 - 145.9750 MHz SSB/CW
Downlink 29.3500 - 29.4200 MHz SSB/CW
 
Mode L/U Packet: Semi-Operational
Uplink: 1266.6870 MHz FSK 9600 BPS
Downlink 437.9100 MHz FSK 9600 BPS

Current Keplerian Elements

SO-33
1 25509U 98061B   10247.86722089  .00000255  00000-0  36516-4 0  7884
2 25509  31.4362  57.9238 0354361 266.5922  89.4113 14.28327145619458

Weekly Satellite Report

Reports have indicated that SO-33 is active on 437.910. A short FSK burst can be heard about once per minute.

Detailed Description

The University of Huntsville, Alabama, in conjunction with Students for the Exploration and Development of Space (SEDS) USA, designed and constructed SEDSAT-1.
SEDSAT-1, signifying Students for the Exploration and Development of Space Satellite number one, was developed at the University of Alabama in Huntsville. The SEDSAT-1 project grew from two students and their mentors to an international project funded by NASA, DARPA, and major corporations. SEDSAT-1 was launched on a Delta II from Vandenberg AFB on 24 October 1998 as a secondary payload on the JPL DS-1 mission.

On-orbit, SEDSAT-1 was be a unique resource for education and research. In its orbital configuration the satellite:


  • Provided multi-spectral remote sensing to the broadest possible community. The cameras collected in narrow wave bands chosen to coordinate with ground based observations across the U.S. Unlike other remote sensing systems, the data was broadly accessible because it was entirely in the public domain, and because its communication system was integrated into the World-Wide-Web.
  • Served as a development platform for advanced microsatellite position determination and control algorithms. The satellite demonstrated a unique attitude determination system and new technology in active microsatellite control.
  • Provided the amateur radio community with digital packet store-and-forward and analog repeater systems
  • Generated new data on the space performance of NiMh batteries and advanced electronic components.
  • Provided additional opportunities for space studies because of its extensive reprogrammability, on board GPS, and other flexible instruments.


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