KKS-1
Spacecraft Summary
| Common Name: |
KKS-1 |
|
Satellite Type: |
Microsatellite |
|
| Launch Date: |
23 January, 2009 |
|
Launch Location: |
Tanegashima Space Center |
|
| Launch Vehicle: |
H-IIA F15 |
|
Apogee: |
660.00 |
|
| Perigee: |
670.00 |
|
Inclination: |
98.00 |
|
| Period: |
98.00 |
|
Dimensions: |
15cm x 15cm x 15cm |
|
| Weight: |
3.000 Kg |
|
| | | | Organization: | Tokyo Metropolitan College of Industrial Technology |
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Frequency Information
| |
| Mode U Beacon: Operational |
| Downlink |
437.3850 MHz CW |
| |
| Mode U Digital (Format or rate unclear): Operational |
| Downlink |
437.4450 MHz AX.25 |
| Callsign(s)
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Detailed Description
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