Satgen 440 Long Live Oscar Ten by GM4IHJ (BID SGEN440) 30Aug 97 With the news from Phase 3D varying from bad to very bad, it is encouraging to find that Oscar Ten , the first Phase 3 satellite to make it into orbit , is still providing occasional service . Launched in June 1983 , Ao10 has suffered more than most , having endured mode L failure , followed by loss of command and control, it none the less keeps returning to a very useful operational mode B status every 5 months or so for 70 to 100 days of operation followed by about 60 to 80 days of silence. This latter inert state being occasioned by its attitude in space producing very little sunlight on its solar panels' Presently Oscar Ten is with us, seeing lots of sunlight and working well, so perhaps a review of its general characteristics may be useful. Uplink 435.19 to 435.04 MHz LSB or CW to an inverting transponder Downlink 145.815 to 145.965 MHz USB or CW Beacon 145.81 MHz constant carrier , no modulation Ao10 does exhibit marked signal fading , which occurs as the changing aspect of the slowly spinning satellite ( circa 0.4 rpm), causes variation in the sequence of signal fades at ground receivers. In a typical example at mean anomally 196 the beacon signal is nearly fade free, but by ma 212 a 3 fades per rotation of the satellite pattern of fading is very evident, as the 3 corners of the satellite consecutively pass between the satellite downlink antenna and the ground station line of sight. Then later at ma 228 , the triple spin fade roughly ever 2.3 minutes, has almost disappeared again. A sequence which differs from time to time as the observers view of the satellite changes over several days. As stated above the satellite seems to be spinning at about 0.43 rpm, and signal fades due to sat antenna screening are usually about 12 dBs deep, but can at times be as much as 20 dBs deep, as one corner out of the three causes much more complete blocking of the signal path than the other 2 corners. When seeing adequate sunlight, the Ao10 beacon signal is relatively steady even when hi power uplinks are present on the transponder. But as the satellite sees less and less sunlight its beacon begins to FM. Showing cyclic modulation of frequency of about 20 Hz bandwidth. Then as the solar illumination deteriorates further the beacon begins to FM much more widely reaching shifts of 150 to 200 Hz at times, rendering use of the transponder almost impossible. Soon after this the beacon and all Ao10 services can be off for up to 2 or in rare cases 3 months at a time, before return to a more sunlit attitude gradually restores the satellite and its beacon to useful mode B operation. These changes are not easy to predict. So please use Ao10 carefully while you can and keep hoping that it keeps returning to operational status for a few more years. One anomaly you may hear sounds like key clicks when the downlink and beacon are particularly strong (Eg at perigee),but they do not seem to cause any harm.