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AggieSat-4/LONESTAR 2

Re-entered 28 Jan 2016

AggieSat-4/LONESTAR 2 (NORAD 41313, COSPAR 1998-067HP) was a US satellite that re-entered Earth's atmosphere on 28 Jan 2016, launched on 6 Dec 2015 on the 77KM No. 17501 mission. It was operated by TAMU as part of the TAMU programme. The spacecraft was built by TAMU on the LONESTAR bus, with a mass of 51 kg. Like most satellites in low orbits, it was gradually slowed by atmospheric drag until re-entry. Historical record from Orbital Radar's satellite archive, cross-referenced with the live satellite catalogue.

2015
launched
2016
re-entered
1
year on orbit
51
kg mass

Lifecycle

Launched6 Dec 2015 · on the 77KM No. 17501 mission
Operational1 Mar 2018 · entered service
Retired1 Mar 2018 · end of operational service
Re-entered28 Jan 2016 · atmospheric re-entry — object destroyed

Specifications

NORAD ID41313
COSPAR1998-067HP
TypeSatellite
OperatorTAMU
Country / StateUS
ManufacturerTAMU
BusLONESTAR
Mass51 kg
ProgrammeTAMU
CategoryTECH
OrbitLEO (LLEO/I)
Altitude399 × 408 km
Inclination51.6°

Frequently asked questions

What happened to AggieSat-4/LONESTAR 2?

AggieSat-4/LONESTAR 2 re-entered Earth's atmosphere on 28 Jan 2016, ending a mission that began with its launch in 2015. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did AggieSat-4/LONESTAR 2 re-enter the atmosphere?

AggieSat-4/LONESTAR 2 re-entered on 28 Jan 2016, according to Orbital Radar's historical catalogue records.

Who operated and built AggieSat-4/LONESTAR 2?

AggieSat-4/LONESTAR 2 was operated by TAMU and built by TAMU (US).

Launched together

Bevo 2/LONESTAR 2Re-entered 2017MinXSSRe-entered 2017CADRERe-entered 2017STMSat 1Re-entered 2017Nodes 1Re-entered 2017Nodes 2Re-entered 2017Dove 0C37Re-entered 2018Dove 0C78Re-entered 2018
Historical record from the Orbital Radar satellite archive. Sources & methodology: data sources. Accessed 2026-09-06.