Official name TEPCE
Alternative name TEPCE 1
Cospar ID 2019-036H
Norad ID 44346
Launch date 2019-06-25
Launch site AFETR
Launch vehicle Falcon-Heavy (Block 5)
Country/Organization USA
Type application Experimental
Operator Naval Research Lab (NRL)
RCS size SMALL
Decay date 2020-02-01
Shape Box + 1 Tether
Mass (kg) 2
Height (m) 0.2
Width (m) 0.1
Depth (m) 0.1
Lifetime 5 years
Contractors Naval Research Lab (NRL)
Propulsion ?
Configuration 2 × CubeSat (1.5U)
Power Deployable solar arrays, batteries

TEPCE (Tether Electrodynamics Propulsion CubeSat Experiment) is a 3U CubeSat that splits into two 1.5U CubeSats joined by a 1 km tether to test electrodynamic tether propulsion.

TEPCE consists of two nearly identical endmasses with a stacer spring between them, which separate the endmass and start deployment of a 1 km long braided-tape conducting tether. TEPCE will use a passive braking to reduce speed and hence recoil at the end of electrodynamic current in either direction. The main purpose of this mission is to raise or lower the orbit by several kilometers per day, to change libration state, to change orbit plane, and to actively maneuver.

It is a mission of the Naval Research Lab (NRL) and is launched via the Space Test Program (STP) and NASA's ELaNa initiative.

Both parts were tracked as one object. A large change in its decay rate on 17 November suggests the tether was deployed on that date, leading to its rapid reentry, which occured on 1 February 2020.

Satellite COSPAR Date LS Launch Vehicle Remarks
TEPCE 2019-036H 2019-06-25 AFETR Falcon-Heavy (Block 5) with DSX , FORMOSAT 7A, 7B, 7C, 7D, 7E, 7F, GPIM, OTB 1, NPSat 1, Oculus-ASR, Prox 1, LightSail 2, ARMADILLO, FalconSat 7, E-TBEx A, E-TBEx B, PSat 2, BRICSat 2, Prometheus 2.6, Prometheus Mass Model, TEPCE 1, CP 9 (LEO), StangSat