Characteristics: - 1st Dutch University Satellite
- 4th Dutch satellite, after ANS, IRAS and Sloshsat
- Dutch satellite with longest operational time
- 2 sets of 4 deployable antennae
- 4 deployable solar panels
- Single point failure free
- No battery; sun powered
- 3 unit CubeSat
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Operations: - Worldwide distributed ground network in co-operation with radio amateurs
- Mission ground station and operations centre:
Delft University of Technology - About 1.2 million frames received in total
- Over 16,000 orbital revolutions around Earth
- Already 12x its intentional operational lifetime
| Communication: - UHF uplink
- VHF downlink
- Downlink rate 1200 bps
Orbital parameters: - Sun-synchronuous orbit
- Inclination: 97.8 degrees
- Altitude: 635 km
- Local time 9:30 hrs.
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Payloads: - 4 sets of Thin Film Solar Cells
- 2 Autonomuous Wireless Sun Sensors
- 2 Radio Amateur Platforms,
transceiver/transponder
| Some numbers: - Mass: 2.2 kg
- Velocity: 27,500 km/h.
- People involved: 100+
- Dimensions, stowed: 100x110x340.5 mm
- Electrical power: 1.8 w
- Transmission power: 0.2 w
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Project partners: - NLR
- TNO
- MicroNed
- Dutch Space
- SystematIC Design
| Sponsors: - CYNER The Netherlands
- LOGICA The Netherlands
- MAVOM The Netherlands
- ITP Engines UK
- AMSAT UK
- HARWIN UK
- MICROCHIP
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Launch: - Launch broker: University of Toronto, Canada
- Launch vehicle: PSLV-C9
- Launch base: Sriharikota, India
- Actual date of launch:
28 April 2008, at 03h53 UTC
| Cooperation in education: - Delft University of Technology (Faculty of Aerospace, Faculty of Electrical Engineering, Mathematics and Computer Science)
- International cooperation via Erasmus/Socrates projects (Spain, Italy, France, China, Denmark)
- Hogeschool InHolland (Delft, Haarlem, Alkmaar)
- Hogeschool Rijswijk
- Hogeschool Rotterdam
- Hogeschool van Amsterdam
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