Norad ID: 26080
| Spacetrack Directory Name | PICOSAT 1 & 2 [TETHERE |
| Orbit launches |
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| Deorbitation |
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| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 725 km |
| Apogee | 770 km |
To demonstrate the basic functional elements of a low-power LEO ?swarm? or formation PICOSAT array. To communicate from space using node-type radios and to report the results of MEMS-switched tests. Validate MEMS radio frequency switches. The two orbiting picosats are to be tethered because they will communicate via micropower radios. The tether will keep them within range of each other for crosslink purposes.
satellite PICOSAT 1 & 2 [TETHERE Date of exalting 27.01.2000y.