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SWAYAM

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SWAYAM is classified as:


NORAD ID: 41607
Int'l Code: 2016-040J
Perigee: 495.6 km
Apogee: 516.3 km
Inclination: 97.4 °
Period: 94.6 minutes
Semi major axis: 6876 km
RCS: Unknown
Launch date: June 22, 2016
Source: India (IND)
Launch site: SRIHARIKOTA (SRI)

SWAYAM is a 1-U picosatellite (CubeSat) developed by the undergraduate students of College of Engineering, Pune. The structural design of the satellite, design of it's electronic and control systems as well as the manufacturing of the satellite was carried out by the students. The project was completed over a span of 8 years and more than 200 students worked on it. The satellite is placed in low earth orbit (LEO) around the Earth at a height of 515 km. Payload is point to point packet communication with which a user can send and receive messages from one point to other point on the earth. Scientific objective of the satellite is to demonstrate passive attitude control to stabilise and appropriately orient the satellite. This technique is being used for the first time on an Indian Satellite. Another objective is to provide Low earth orbit channel characterisation in UHF HAM band.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 41607U 16040J   18196.64990241  .00001306  00000-0  59583-4 0  9993
2 41607  97.4114 259.2399 0015054 134.1335 226.1142 15.22317474114437
Source of the keplerian elements: AFSPC