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MAST

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MAST is classified as:


NORAD ID: 31126
Int'l Code: 2007-012K
Perigee: 648.6 km
Apogee: 774.5 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   17141.91143922 +.00000110 +00000-0 +34030-4 0  9994
2 31126 098.0599 093.3109 0088907 259.5521 099.5649 14.56523977536006
Source of the keplerian elements: AFSPC