Turkish small satellites (CubeSats & PocketQubes)
Also known as ITUpSAT1, TURKSAT-3USAT, BeEagleSat, HavelSat, Connecta, Istanbul-1P
From ITUpSAT1 in 2009 to TURKSAT-3USAT, QB50 BeEagleSat/HavelSat, Grizu-263A and commercial IoT constellations: evolution of standard-form-factor nano- and picosatellites in Türkiye.
- Document
- SQ-MS-008
- Updated
- 21 Oct 2026
- Reading time
- 2 min
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The CubeSat generation (2009–2020)#
Standardized nano- and picosatellite development in Türkiye began at Istanbul Technical University (ITU) with the launch of the ITUpSAT1 aboard PSLV-C14 on 23 September 2009 into a Sun-synchronous orbit[1]. Over the following decade, university laboratories and industry partners expanded across to CubeSat platforms:
- TURKSAT-3USAT (3U, April 2013, CZ-2D): Built by ITU and TÜRKSAT carrying a VHF/UHF voice transponder and optical camera.
- BeEagleSat & HavelSat (2U, April–May 2017, Atlas V / ISS NanoRacks): Developed by ITU, HAVELSAN and METU within the European QB50 thermospheric research constellation, deployed from the International Space Station near .
- UBAKUSAT (3U, 2018) & ASELSAT (3U, 2021): Amateur-transponder and X-band/thermal-imaging demonstrators launched via ISS and Falcon 9 Transporter-1.
- Plan-S Connecta series (3U–6U, 2022–present): Commercial IoT and Earth-observation CubeSat constellation deployed on Falcon 9 Transporter rideshares.
Transition to the PocketQube scale (2022–2026)#
Entry into the PocketQube class began on 13 January 2022 when Zonguldak Bülent Ecevit University's student team launched the Grizu-263A () aboard Falcon 9 Transporter-3[2][3], followed in 2023 by Hello Space's commercial and IoT satellites (Istanbul, Hello Test-1, Hello Test-2).
| Form factor | Mass (kg) | Ballistic parameter (m²/kg) | From 400 km | From 500 km | From 525 km | From 600 km | From 700 km |
|---|---|---|---|---|---|---|---|
| 1P | 0.25 | 0.0330 | 3 months | 20.4 months | 2.7 years | 10.1 years | 49 years |
| 3P | 0.75 | 0.0298 | 3 months | 22.6 months | 3.0 years | 11.2 years | 54 years |
| 1U | 2.00 | 0.0180 | 5 months | 3.1 years | 5.0 years | 18.6 years | 90 years |
| 3U | 6.00 | 0.0143 | 6 months | 3.9 years | 6.2 years | 23 years | > 100 years |
Kennewell density model, drag coefficient 2.2, mean tumbling area A_tot/4, re-entry at 180 km, spacecraft at the mass limit of its standard. Solar activity: low F10.7 = 70 sfu, Ap = 6; moderate 140 sfu, Ap = 12; high 210 sfu, Ap = 18.
References
- [1]Krebs, G. D. (2023). ITUpSAT 1 — Gunter's Space Page.space.skyrocket.de(accessed 20 October 2026)
- [2]nadir lab. (2026). PocketQube picosatellites: A review of standards, mission trends and miniaturization constraints, with lessons learned from Grizu-263A, Türkiye’s first PocketQube [Preprint]. nadir lab.Read on nadir lab.
- [3]Libre Space Foundation community forum. (2022). SpaceX F9 Transporter-3, 2022-01-13 15:25 UTC (discussion thread).community.libre.space(accessed 20 October 2026)
Cite this SatWiki entry
@misc{nadirlab2026turkish,
author = {{nadir lab.}},
title = {{Turkish small satellites (CubeSats \& PocketQubes)}},
year = {2026},
month = oct,
howpublished = {nadir lab. SatWiki SQ-MS-008 (Rev. 1)},
url = {https://nadirlab.space/en/wiki/turkish-small-satellites/}
}nadir lab. (2026). Turkish small satellites (CubeSats & PocketQubes). nadir lab. SatWiki (SQ-MS-008, Rev. 1). https://nadirlab.space/en/wiki/turkish-small-satellites/
TY - ENCYC
AU - {nadir lab.}
TI - Turkish small satellites (CubeSats & PocketQubes)
T2 - nadir lab. SatWiki
PY - 2026
ET - Rev. 1
C1 - SQ-MS-008
UR - https://nadirlab.space/en/wiki/turkish-small-satellites/
ER -