Multiple CubeSat Launch Set For April 28, 2008
(C)AMSAT-NA
The PSLV-C9 launch from India carrying the CUTE-1.7, SEEDS, DELFI-C3, COMPASS-1, AAUSAT-II, and CANX-2 Cubesats
into orbit is planned for April 28, 2008 at 0353 UTC.
| Satellite | Uplink | Downlink | Beacon | Mode | Callsign |
| CUTE1.7 |
1267.600 | - | - | 9600 GMSK | JQ1YTC |
| CUTE1.7 | - | 437.475 | - | 9600 GMSK | JQ1YTC |
| CUTE1.7 | - | 437.475 | - | 1200 AFSK | JQ1YTC |
| CUTE1.7 | - | - | 437.275 | CW | JQ1YTC |
| SEEDS | - | 437.485 | 437.485 | 1200 AFSK CW |
JQ1YGU |
| DELFI-C3 | - | 145.870 | 145.870/930 | 1200 BPSK | DLF1C3 |
| DELFI-C3 | 435.570-530 | 145.880-920 | 145.870/930 | SSB, CW, FM | DLF1C3 |
| COMPASS-1 | - | 437.405 | - | 1200 AFSK | DP0COM |
| COMPASS-1 | - | - | 437.275 | CW | DP0COM |
| AAUSAT-II | - | 437.425 | 437.425 | 1200 FFSK(MSK) | OZ2CUB |
| AAUSAT-II | - | 437.425 | 437.425 | 9600 FSK | OZ2CUB |
| CANX-2 | - | 437.478 | - | Over GS only | VA3SFL |
| CANX-2 | - | 2.2GHz | - | 32K-256Kbaud GMSK | VA3SFL |
Additional CubeSat information can be found at these links:
http://showcase.netins.net/web/wallio/CubeSat.htm
http://www.dk3wn.info/calendar/satellit.php?language=german
SEEDS 1 XXXXXU 08XXXXXU 08119.17526667 .00000000 00000-0 00000-0 0 0000X 2 XXXXX 97.9521 179.1184 0004570 8.6293 206.4181 14.7957000000001X Cute-1.7 II 1 XXXXXU 08XXXXXU 08119.17374537 .00000091 00000-0 00000-0 0 0000X 2 99999 97.9419 179.0062 0011471 292.3990 277.6939 14.7828229200001X Preliminary TLE 1 00000U 00000C 08119.17443982 .00000000 00000-0 00000-0 0 0013 2 00012 97.9497 178.9014 0004270 015.5590 198.2466 14.79780033 00004
The other all cubesats (complemented by JE9PEL): Cute-1.7 + APD II (Japan, Tokyo Institute of Technology Laboratory for Space Systems) SEEDS (Japan, Nihon University) Delfi-C3 (Netherlands, Technical University of Delft) AAUSat-II (Denmark, Aalborg University Cubesat) COMPASS-1 (Germany, Fachhochschule Aachen) CanX-2 (Canada, University of Toronto) CanX-6 (Canada, University of Toronto) Cartosat 2A (India, Indian Space Research Organization) IMS 1 (India, Indian Space Research Organization) Rubin 8-AIS (Germany, OHB-System) Flight Sequence T=0.0s PS1 Ignition T=113.14s PS1 Separation (h=50.42km) T=113.34s PS2 Ignition (h=50.60km) T=188.14s Heat shield separation T=264.04s PS2 Separation (h=204.18km) T=265.14s PS3 Ignition (h=205.56km) T=524.24s PS3 Separation (h=507.48km) T=540.0s PS4 Ignition (h=518.42km) T=844.2s PS4 Cut off (h=637.66km) + 47.0s Reorientation of PS4 starts + 67.0s Reorientation of PS4 ends + 82.0s TWSAT separation +122.0s Reorientation of PS4 starts +142.0s Reorientation of PS4 ends +200.0s CanX-2 separation +220.0s Cute 1.7+APD II separation +240.0s Delfi-C3 separation +260.0s AAUSat-II separation +280.0s COMPASS-1 separation +300.0s SEEDS separation http://www.utias-sfl.net/NLS-4/ Telemetry Analysis Program CUTE-1.7 + APDII CW Telemetry Checker ver5.0 http://lss.mes.titech.ac.jp/ssp/cute1.7/index_e.html SEEDS Analyzer ver2.0.1 http://cubesat.aero.cst.nihon-u.ac.jp/english/index.html Delfi-C3 Telemetry decoding software: RASCAL ver1.0.1 http://www.delfic3.nl/index.php?option=com_content&task=view&id=94&Itemid=123 COMPASS-1 Beacon Decoder http://www.raumfahrt.fh-aachen.de/downloads/COMPASS_Beacon_Decoder.exe http://www.dk3wn.info/files/compass.zip
Updated: 26 Apr, 08
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