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Introducing P3-E - AMSAT-DLs High Orbit Satellite
 

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P3-E Preliminary Information

Construction Phase: present until Q4 2005
Projected Launch: Delayed Indefinately
Launch Vehicle: Ariane 5
Launch Location: Kourou, French Guiana
Spaceframe Structure: AO-10/AO-13 type triangular star
Spaceframe Size: Approx.130cm diameter, 45cm height (not including antennas and engine)
Weight: Approx. 150kg
Orbit: Highly elliptical 36,000km x 2500km,
63° inclination
225° - 315° argument of perigee
Uplink Receivers: 29.500 (A): multimode, low speed RUDAK
436.200 - 436.350 (U): multimode RUDAK
436.050 - 436.150 (U): linear passband
1268.775 - 1268.925 (L1): multimode RUDAK
1268.600 - 1268.750 (L1): linear passband
1260.275 - 1260-425 (L2): multimode RUDAK
1260.100 - 1260.225 (L2): linear passband
5668.600 +/- 25KHz (C): (linear)
Downlink Transmitters: 145.812 (V): PSK 400 BPS General Beacon
145.957 (V): PSK 400 BPS Engineering Beacon
145.837 (V): multimode, low speed RUDAK
145.845 - 145.945 (V) linear passband
2400.250 (S):  PSK 400 BPS General Beacon
2400.500 (S): PSK 400 BPS Engineering Beacon
2400.600 (S) - 2401.000: multimode, high/low speed RUDAK
2400.275 (S) - 2400.425: linear passband
24048.350 (K): beacon
24048.300 +/- 25KHz (K): linear passband
47088.350 (X): beacon
47088.300 +/- 25KHz (X): linear passband
P5-A Transponder Experiment: 2560 MHz (S) uplink and 10450 MHz (X) downlink. Also usable as a linear
transponder with approximately 50 KHz bandwidth.
Other Features: LELIA
RUDAK
Main Beacon with FEC-coded telemetry
2 or 3 Cameras
Project Supervision: AMSAT-DL


Project Status Updates

Photos

Questions and Answers

  • None at this time

Preliminary Keplerian Elements (Experimental - updated 4/6/2005)

P3E
1 55002U 05055B   06215.60600000 -.00000001  00000-0  10000-4 0    25
2 55002  48.7459 176.4760 7509770 242.6730   0.0000  1.71429000 08609

Note: If cut and paste doesn't work you can download a text file that can be imported into most tracking programs


Related Documents


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