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REMOVEDEBRIS

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REMOVEDEBRIS is classified as:


NORAD ID: 43510
Int'l Code: 1998-067NT
Perigee: 385.2 km
Apogee: 389.3 km
Inclination: 51.6 °
Period: 92.2 minutes
Semi major axis: 6758 km
RCS: Unknown
Launch date: November 20, 1998
Source: United Kingdom (UK)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

REMOVEDEBRIS is a satellite research project intending to demonstrate various space debris removal technologies. Rather than engaging in active debris removal (ADR) of real space debris, the REMOVEDEBRIS mission plan is to test the efficacy of several ADR technologies on mock targets in low Earth orbit. In order to complete its planned experiments the platform is equipped with a net, a harpoon, a laser ranging instrument, a dragsail, and two CubeSats (miniature research satellites).
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 43510U 98067NT  20150.10813997  .00006061  00000-0  72299-4 0  9995
2 43510  51.6358  49.6118 0002984  13.1483 346.9588 15.62609802110469
Source of the keplerian elements: AFSPC