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PROMETHEUS 2-3

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NORAD ID: 41855
Int'l Code: 2016-067H
Perigee: 576.1 km
Apogee: 590.9 km
Inclination: 97.9 °
Period: 96.2 minutes
Semi major axis: 6954 km
RCS: Unknown
Launch date: November 11, 2016
Source: United States (US)
Launch site: AIR FORCE WESTERN TEST RANGE (AFWTR)

PROMETHEUS 2-3 and PROMETHEUS 2-1 satellites (Prometheus Block 2) are developed and operated by the Los Alamos National Laboratory (LANL) and follow up on a successful series of missions of eight Block 1 satellites and the Perseus program. Their primary purpose is the demonstration of low-cost satellites in a feasibility study of CubeSat applications in communications between remote field sites and ground station terminals in a store-and-forward environment. Each of the 1.5U CubeSats is manufactured for less than $100,000 and features four deployable solar panels, an active attitude control system with stellar sensors, and a Software Defined Radio with a footprint sufficiently small for tactical operations.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 41855U 16067H   19232.84457501 -.00000059  00000-0  15289-6 0  9990
2 41855  97.9208 331.1638 0010666 167.5850 192.5636 14.96941988151341
Source of the keplerian elements: AFSPC