SPROUT data Telemetry

SPROUT data Telemetry 23-11-2014 14:50 UTC

2014-11-23 14:50:44.510 UTC: from JQ1ZJQ to SPROUT (UI, payload: 226 byte)
000 > C0 00 A6 A0 A4 9E AA A8 60 94 A2 62 B4 94 A2 61 03 F0 01 B1 
020 > 5B FD 5B FD 64 3F 64 7F 6C 9F 64 7F 6C 7F 6C DF 6C DF 6C FF 
040 > 6C 9F 6C 9F 64 7F 64 5F 6C 7F 6C BF 6C 9F 6C DF 7D BF 7E 3F 
060 > 7D FF 75 7F 75 9F 7D DF 7E 3F 86 BF 87 3F 8F 5F 86 DF 86 9F 
080 > 7D FF 7D DF 75 BF 75 FF 7E 1F 7E 5F 7E DF 7F 1F 87 7F 87 DF 
100 > 8F FF CF FF DF FF E7 FF FF FF FF FF FF FF FF FF FF FF FF FF 
120 > FF FF FF FF FF FF FF FF FF FF FF FF E7 9F 39 F0 39 EB 31 CA 
140 > 31 C9 31 A9 31 A8 31 A8 31 88 29 A8 31 88 31 88 31 A8 31 A8 
160 > 31 A8 31 A8 31 88 31 88 29 88 29 87 29 87 29 87 29 87 29 87 
180 > 29 87 29 87 29 87 29 87 29 87 29 87 29 87 29 87 29 87 29 87 
200 > 29 87 29 67 29 87 29 87 29 87 29 86 5B B3 53 73 53 52 53 52 
220 > 53 72 53 92 53 93 53 B3 53 74 53 94 53 75 53 74 4B 54 4B 12 
240 > 4B 12 4B 12 C0

sprout_pe0sat_23112014_1446

Tsubame CW Telemetry

Tsubame CW Telemetry 13-11-2014 20:35 UTC

HI HI DE JQ1ZHX TSUBAME 6B ** C9 00 2C 00 00 25 38 78 87 FC 90 09 00 01 
HI HI DE JQ1ZHX TSUBAME 65 2* C9 00 2C 00 00 25 38 78 87 FC 90 09 00 01 
HI HI DE JQ1ZHX TSUBAME 6B 23 C9 91 00 2A 00 25 38 78 87 FC 90 09 00 01 
HI HI DE JQ1ZHX TSUBAME 6A 24 C9 91 00 2A 00 25 38 78 87 FC 90 09 00 01 
HI HI DE JQJZHX TSUBAM  6A 24 C9 91 00 FC 00 25 38 78 87 FC 90 09 00 01

Tsubame_Fading_13112014_2035UTC

The latest 4M TLE

The latest 4M TLE data shared via the Moon-Net mailing list by LX2RG

4M
1 40284U 14065B   14307.75000000 -.00000015  00000-0 -36726+7 0 00002
2 40284 061.6967 069.0661 6145515 000.5872 038.5007 00.07379169000029

4M-spacecraftPlease find attached the latest TLE for 4M.

It is obtained using an accurate Doppler fit and should do for some months. 4M may awaken from time to time and there is the possibility that it gets enough sun to stay powered for a long time due to Earth’s orbit and inertial properties of the attitude of the last stage.