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MAST

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MAST is classified as:


NORAD ID: 31126
Int'l Code: 2007-012K
Perigee: 648.0 km
Apogee: 775.0 km
Inclination: 98.1 °
Period: 98.9 minutes
Semi major axis: 7082 km
RCS: 0.0635 m2 (small)
Launch date: April 17, 2007
Source: United States (US)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)
Uplink (MHz):
Downlink (MHz): 2400.000-2483.500
Beacon (MHz):
Mode: FHSS
Call sign:
Status: Inactive


MAST is designed to perform investigations of the dynamics of tethered formations of spacecraft and to investigate the survivability of tethers in the harsh space environment. The MAST experiment consists of three picosatellites which will ride into orbit as a secondary payload on a Dnepr rocket as a part of the University CubeSat program. For launch, these three picosatellites stack together into a volume about the size of a loaf of bread. Once on orbit, the picosatellites will separate and deploy a 1,000 meter long Hoytether structure.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 31126U 07012K   17235.27048879  .00000114  00000-0  34749-4 0  9993
2 31126  98.0664 183.6341 0089680 329.8480  29.7574 14.56548875549644
Source of the keplerian elements: AFSPC