DELFI C3

Photo DELFI C3

32789
Spacetrack Directory Number
2008-04-28
Orbit launches
284.11 km
Average height
27858.75 km/h
Average velocity


Satellite information DELFI C3 - DELFI-C3 (DO-64)

Spacetrack Directory Name DELFI C3
Alternative name DELFI-C3 (DO-64)
Orbit launches 2008-04-28
Country/organisation of origin Holandia (NETH)
Starting point SRILR (Satish Dhawan Space Centre, India)
Categories
Perigee 526 km/h
Apogee 544 km
Height DELFI C3 284.11 km

Additional information DELFI C3

Delfi-C3 is a CubeSat satellite constructed by students at the Delft University of Technology in the Netherlands. It is a 3-unit CubeSat, and was launched at 03:53:42 on 28 April 2008, as part of the NLS-4 mission, aboard a PSLV rocket, from the Second Launch Pad at the Satish Dhawan Space Centre in India. The launch was contracted by ISRO, through Antrix Corporation and UTIAS.The satellite's primary mission is technology demonstration and development. It is carrying new types of solar cells, a solar sensor for TNO Science and Industry, and a high-efficiency amateur radio transceiver experiment.Delfi-C3 does not contain batteries, as the experiments are dependent on the sun.
She is the fourth Dutch Satellite, after ANS, IRAS and SLOSHSAT. It is the first Dutch university Satellite and is based on a 3-Unit CubeSat.
Some other mission characteristics include:

No active attitude control
1200Bd BPSK VHF downlink
Linear transponderThe Delfi-C3 ground segment consists of two command ground stations, the primary being in Delft and the backup station at the TU Eindhoven in Eindhoven. For data collection, a distributed ground station network (DGSN) is used in which radio amateurs receive packets and sent these via internet to the central data collection server.
Data decoding is possible with the free RASCAL software provided by the Delfi-C3 team.
The Delfi-C was still largely operational when it was followed up by the Delfi-n3Xt in October 21, 2013.
In May 2008, the amateur radio payload on the satellite was designated Delfi-C3 OSCAR-64 or Dutch OSCAR-64 (DO-64).

satellite DELFI C3 Date of exalting 28.04.2008y. Average height of ISS DELFI C3 hundred 284.11 km. Average velocity DELFI C3 is 27858.75 km/h. Inclination DELFI C3 satellite 97.27°.


Average orbit height DELFI C3

Average velocity DELFI C3

Average inclination DELFI C3

Update time: 2023-11-14 23:32:20
Average height of ISS DELFI C3 is: 284.11km
Average velocity DELFI C3 is: 27858.75km/h
Average orbit height DELFI C3 is: 97.27°
DELFI C3 a new group of Starlink satellites has been launched 2008-04-28