A Review of the Current Development State of Non-Terrestrial NB-IoT Systems
Abstract
1. Introduction
- Comprehensive Review of NTN NB-IoT Progress: The paper provides a detailed overview of the recent developments in both standardization (3GPP) and academia regarding the provision of NTN connectivity for NB-IoT mMTC systems.
- Analysis of Satellite Infrastructure and Deployment: It offers an in-depth classification and technical description of orbiting systems, including LEO, MEO, and GEO satellites, and evaluates their specific roles, advantages, and integration challenges within a multi-orbit 5G ecosystem.
- Synthesis of Lessons Learned from Operational Systems: This study concludes by analyzing already deployed systems and field trials, highlighting critical lessons regarding hardware validation, service performance including latency, throughput and age-of-information (AoI), software-defined infrastructure flexibility, and the necessary trade-offs between coverage, capacity, and latency.
2. Orbiting Systems, Constellations, and Hardware
2.1. Satellite Types
2.1.1. Minisatellites
2.1.2. Microsatellites
2.1.3. Nanosatellites
2.1.4. Picosatellites
2.1.5. Femtosatellites
2.2. Orbits
2.2.1. Geostationary Earth Orbit
2.2.2. Medium Earth Orbit
2.2.3. Low Earth Orbit
| Orbit Type | Altitude | Characteristics | Typical Uses and Examples |
|---|---|---|---|
| GEO | 35,786 km | Appears fixed in the sky, continuous coverage over a large area, higher latency (∼240 ms). | Television broadcasting (e.g., DirecTV), weather monitoring, and VSAT networks [35]. |
| MEO | 2000–35,786 km | Wider coverage than LEO, fewer satellites required for global coverage, balance of latency. | Global navigation systems (GPS, GLONASS, Galileo), mobile satellite systems [36]. |
| LEO | 160–2000 km | Very low latency, lower signal loss, and requires large constellations for continuous coverage. | Satellite internet (Starlink, OneWeb), Earth observation, direct-to-cell services [37]. |
2.3. Constellations
- Starlink (SpaceX) is the largest, with a multi-shell architecture: ≈1600 at 550 km (53°), ≈2800 at 540–1325 km (70–81°), and plans for 7500 at 340 km. Each satellite uses the Ku/Ka/V-band and laser ISL for a space-based mesh, delivering low-latency broadband globally [31].
- Blue Origin’s TeraWave opts for a hybrid LEO/MEO network of 5408 satellites with Q/V-band links, delivering up to 144 Gbps symmetrical—targeting only 100,000 premium enterprise users [28].
- IRIS2 (EU) is a sovereign multi-orbit constellation (LEO/MEO) led by SpaceRISE, providing secure connectivity for governments and critical infrastructure, reducing reliance on non-European providers [38].
- China pursues state-backed constellations: Guowang (13,000 satellites by 2035), Spacesail’s Qianfan (>15,000 by 2030), Honghu-3 (10,000), and filings for CTC-1/CTC-2 (200,000 total) to secure spectrum and orbital slots [35].
2.4. Hardware Integration
3. Provisioned Services and Challenges
3.1. Cellular IoT
3.2. Use-Cases for NTN NB-IoT Systems
3.2.1. Standard 4-Step Random Access
3.2.2. Early Data Transmission Regime
3.2.3. Grant-Free 2-Step Random Access
3.2.4. Grant-Free Access with Fallback Option
3.2.5. Critical Assessment
3.3. System Parameters
3.4. Doppler Shift Mitigation in NTN
3.5. Time Advance Adaptation in NTN
3.6. Localization and GNSS
4. Architecture and 3GPP Standardization
4.1. NTN Architecture
4.2. NTN Standardization in 3GPP
4.3. Critical Assessment
4.4. Future Work in 3GPP
5. Academic Contributions
5.1. Architecture and Design
5.2. Physical Layer Improvements
5.3. Medium Access Control Mechanisms
5.4. Service Performance
5.5. AI-Driven Enhancements
6. Operational Systems and Lessons Learned
6.1. Testbeds and Deployments
6.2. Lessons Learned
- The importance of fallback mechanisms is evident: the Airtel deployment’s inclusion of 2G and 4G fallback recognizes that NB-IoT coverage may not be universally available and that uninterrupted service requires redundancy [99]. Second, early demonstrations have shown the feasibility of using commercial, standards-based hardware for NTN NB-IoT connectivity. Both the Mavenir/Terrestar GEO trial [85] and the Iridium NTN Direct test [86] successfully utilized commercially available modules without modification, suggesting that existing hardware may be adaptable for satellite-based IoT applications. However, further validation across a wider range of deployment scenarios and longer operational periods is needed to confirm long-term reliability and performance.
- The flexibility of software-defined infrastructure has proven critical to NTN advancement. Iridium’s activation of NB-IoT capabilities via a software update to its existing LEO constellation demonstrates how satellite networks can evolve without hardware replacement [86]. Similarly, Mavenir’s cloud-native RAN and Core solutions running on public cloud infrastructure enabled rapid deployment and testing [85].
- The trade-off between coverage and capacity requires careful engineering. Higher-altitude platforms provide larger coverage footprints but suffer from reduced signal strength and network capacity owing to increased path loss [100]. The GEO approach adopted by Terrestar offers stable coverage but with higher latency, whereas Iridium’s LEO constellation provides lower latency but requires more complex handover management.
- The ecosystem approach to NB-IoT deployment—encompassing chipset makers, module manufacturers, network operators, and application developers—has proven essential to success. The collaborations between Nordic Semiconductor and Iridium and between Mavenir and Terrestar illustrate that commercialization requires alignment across the entire value chain [85,101].
6.3. Challenges and Future Developments
6.3.1. Challenges of the Current Implementations
6.3.2. The Preliminary 6G Vision
6.4. Economic Considerations
7. Conclusions
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Conflicts of Interest
Abbreviations
| 3GPP | 3rd Generation Partnership Project |
| 5GC | 5G Core |
| AI | Artificial Intelligence |
| AMF | Access and Mobility Management Function |
| ARQ | Automatic Repeat Request |
| BER | Bit Error Rate |
| BLER | Block Error Rate |
| BVLOS | Beyond Visual Line of Sight |
| CapEx | Capital Expenditure |
| Cat M1 | LTE Category M1 (LTE-M) |
| Cat NB | Narrowband IoT Category (NB1/NB2) |
| CB-EDT | Contention-Based Early Data Transmission |
| CFO | Carrier Frequency Offset |
| CNN | Convolutional Neural Network |
| CNR | Carrier-to-Noise Ratio |
| COTS | Commercial Off-The-Shelf |
| CP | Control Plane |
| CU | Central Unit (gNB-CU) |
| DL | Downlink |
| DM-RS | Demodulation Reference Signal |
| DRL | Deep Reinforcement Learning |
| DU | Distributed Unit (gNB-DU) |
| ECSS | European Cooperation for Space Standardization |
| ED | End Device |
| EDT | Early Data Transmission |
| eDRX | extended Discontinuous Reception |
| EIRP | Effective Isotropic Radiated Power |
| eMBB | enhanced Mobile Broadband |
| eMTC | enhanced Machine Type Communication |
| ESA | European Space Agency |
| EU | European Union |
| F1 | Interface between gNB-CU and gNB-DU |
| FAA | Federal Aviation Administration |
| FCC | Federal Communications Commission |
| FD | Full Duplex |
| FDD | Frequency Division Duplex |
| FPGA | Field-Programmable Gate Array |
| FSPL | Free Space Path Loss |
| GEO | Geostationary Earth Orbit |
| gNB | Next-generation Node B (5G base station) |
| GNSS | Global Navigation Satellite System |
| GPS | Global Positioning System |
| G/T | Figure of Merit (Gain-to-Noise Temperature) |
| HAPS | High-Altitude Platform Station |
| HARQ | Hybrid Automatic Repeat Request |
| HD | Half Duplex |
| HFL | Hierarchical Federated Learning |
| HPUE | High-Power User Equipment |
| HTS | High-Throughput Satellite |
| IAB | Integrated Access and Backhaul |
| ICI | Inter-Carrier Interference |
| IoT | Internet of Things |
| IRIS2 | Infrastructure for Resilience, Interconnectivity and Security by Satellite |
| ISL | Inter-Satellite Link |
| ITU | International Telecommunication Union |
| LEO | Low Earth Orbit |
| LMS | Land Mobile Satellite |
| LPWA | Low-Power Wide-Area |
| LTE-M | LTE for Machines |
| M2M | Machine-to-Machine |
| MAC | Medium Access Control |
| MANO | Management and Orchestration |
| MCL | Maximum Coupling Loss |
| MCS | Modulation and Coding Scheme |
| MEO | Medium Earth Orbit |
| MIL-HDBK | Military Handbook |
| MIMO | Multiple-Input Multiple-Output |
| mMTC | massive Machine-Type Communication |
| MTC | Machine-Type Communication |
| NASA | National Aeronautics and Space Administration |
| NB-IoT | Narrowband Internet of Things |
| NFV | Network Function Virtualization |
| NG | Interface between gNB and 5GC |
| NIDD | Non-IP Data Delivery |
| NOMA | Non-Orthogonal Multiple Access |
| NPRACH | Narrowband Physical Random Access Channel |
| NTN | Non-Terrestrial Network |
| OAI | OpenAirInterface |
| OFDM | Orthogonal Frequency Division Multiplexing |
| OTFS | Orthogonal Time Frequency Space |
| PAA | Phased Array Antenna |
| PDCP | Packet Data Convergence Protocol |
| PHY | Physical layer |
| PLS | Physical Layer Security |
| PLR | Packet Loss Rate |
| PNT | Positioning, Navigation, and Timing |
| PSM | Power-Saving Mode |
| PUSCH | Physical Uplink Shared Channel |
| QAM | Quadrature Amplitude Modulation |
| QPSK | Quadrature Phase Shift Keying |
| RACH | Random Access Channel |
| RAN | Radio Access Network |
| RAN3 | 3GPP Radio Access Network Working Group 3 |
| RIS | Reconfigurable Intelligent Surface |
| RLC | Radio Link Control |
| RRC | Radio Resource Control |
| RSRP | Reference Signal Received Power |
| RTT | Round-Trip Time |
| RU | Resource Unit |
| SA1 | 3GPP Service and System Aspects Working Group 1 |
| S&F | Store and Forward |
| SAM | Satellite-Assisted Manner |
| SCS | Subcarrier Spacing |
| SDM | Satellite-Dedicated Manner |
| SDN | Software-Defined Networking |
| SEE | Single Event Effects |
| SI | Study Item |
| SNR | Signal-to-Noise Ratio |
| SRI | Satellite Radio Interface |
| STO | Symbol Timing Offset |
| SWaP | Size, Weight, and Power |
| TDD | Time Division Duplex |
| TID | Total Ionizing Dose |
| TN | Terrestrial Network |
| TR | Technical Report |
| TS | Technical Specification |
| UAS | Unmanned Aerial Systems |
| UAV | Unmanned Aerial Vehicle |
| UE | User Equipment |
| UL | Uplink |
| UP | User Plane |
| uRLLC | ultra-reliable low-latency communication |
| VIAVI | VIAVI Solutions |
| VSAT | Very Small Aperture Terminal |
| WI | Work Item |
| Xn | Interface between gNBs |
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| Scheme | Year | Specifics |
|---|---|---|
| Sweeting [19] | 1991 | Initial mass-based classification: large (>1000 kg), small ( kg), mini ( kg), micro ( kg), nano (<10 kg). |
| Konecny [20] | 2004 | Refined classification: added pico ( kg) and femto (<0.1 kg) classes; retained large, medium, mini, micro, nano. |
| Kramer & Cracknell [21] | 2008 | Merged mini and medium into kg range; maintained micro ( kg), nano ( kg), pico ( kg), and femto ( kg). |
| ITU-R [22] | 2014 | Defined nanosatellites ( kg), picosatellites ( kg), femtosatellites (≤0.1 kg) with emphasis on spectrum requirements; also included mini ( kg), and micro ( kg) satellites. |
| NASA [23] | 2015 | SmallSat definition: satellites with mass below 180 kg; further divided into mini ( kg), micro ( kg), nano ( kg), pico ( kg), femto ( kg). |
| Wekerle et al. [24] | 2017 | Small satellite classification: large (>500 kg), mini ( kg), micro ( kg), nano ( kg), pico (<1 kg). |
| FAA [25] | 2018 | Payload classification for launch vehicles: extra heavy (>7100 kg), heavy ( kg), large ( kg), intermediate ( kg), medium ( kg), small ( kg), mini ( kg), micro ( kg), nano ( kg), pico ( kg), femto ( kg). |
| Botelho & Xavier [26] | 2019 | Unified taxonomy with 10 classes based on powers of 10: mega, hecto, deca, protypo, mini, micro, nano, pico, femto, gram. Integrates previous schemes and adds size descriptors. |
| Parameter | Requirement |
|---|---|
| Power & Thermal | |
| Orbital average power | as low as 38 W (microsatellite) |
| Peak payload dissipation | ∼20 W (X-band transmitter, 26% efficiency) |
| Thermal control precision | <±0.15 °C (with 9.3 W avg. power) |
| Orbit temperature variation | 4 °C to 9 °C (passively controlled small satellite) |
| Size, Weight, and Power | |
| Launch cost | $10,000–$1000 per kg (to LEO/GTO) |
| Payload mass (low-SWaP) | <10 kg |
| Payload mass (high-SWaP) | ∼150 kg |
| Payload power (low-SWaP) | <30 W |
| Payload power (high-SWaP) | ∼400 W |
| Radiation Hardening | |
| Total ionizing dose (TID) | 100 krad (space-grade); 30–50 krad (rad-tolerant) |
| Single event effects (SEE) | up to 75 MeV·cm2/mg (rad-hard controllers) |
| Hardening standards | ECSS-Q-ST-60-15C, MIL-HDBK-533, etc. [40] |
| Phased Array Antenna | |
| Number of elements | ∼100 (typical high-throughput system) [41] |
| System power consumption | <1 kW (100-element PAA) [41] |
| Achievable performance | SNR and beam crosstalk dB [41] |
| Parameter | Description |
|---|---|
| Processing platform | AMD Xilinx VERSAL AI Core (space-grade) + multi-core CPU |
| PHY acceleration | FPGA-based FFT, coding, rate matching, DMA at 500 MHz |
| Higher layers | OpenAirInterface (OAI) stack ported to AARCH64 |
| Processing split | PHY–MAC split with PCIe interconnect |
| Transceiver | Analog Devices AD9082 MxFE (16-bit 12 GSPS DAC, 12-bit 6 GSPS ADC) |
| Interface to FPGA | JESD204B/C (up to 24.75 Gbps/lane, 8 lanes each direction) |
| On-chip DSP | Bypassed (direct connection to converter cores) |
| NTN FR1 bands | 3GPP Bands 254, 255, 256 (FDD) |
| Channel bandwidth | Up to 50 MHz (Ku-band trials); 5–10 MHz typical |
| cellSpecificKoffset (GEO) | 478 slots |
| ta-Common (GEO) | ≈29,319,745 |
| K2 (LEO) | 46 slots |
| prach_ConfigurationIndex | 98 |
| preambleReceivedTargetPower | −118 dBm |
| preambleTransMax | 6 (64 preamble transmissions) |
| pMax (UE max transmit) | 20 dBm |
| System power consumption | Under evaluation |
| Xn interface | Supported for inter-satellite links |
| NG interface | Connects to AMF on ground |
| Test platform | Evaluation boards (VERSAL, AD9082) |
| Validation | Digital twin testbed (Rohde & Schwarz/VIAVI) |
| Unit | Cat NB1 | Cat NB2 | Cat M1 | Cat M2 | |
|---|---|---|---|---|---|
| 3GPP Release | – | R13 | R14 | R13 | R14 |
| Licenced Spectrum | Y/N | ✓ | ✓ | ✓ | ✓ |
| Frequency | MHz | 700–2100 | 700–2100 | 700–2600 | 700–2600 |
| Bandwidth | MHz | 0.2 | 0.2 | 1.4 | 5 |
| Payload size | Bytes | <1600 | <1600 | <8188 | <8188 |
| MCL | dB | 164 dB | 164 dB | 155.7 dB | 155.7 dB |
| EIRP | dBm | <23 | <23 | <23 | <23 |
| Tx power consumption | mA | 240 | 240 | 360 | 360 |
| Rx power consumption | mA | 46 | 46 | 70 | 70 |
| PSM | µA | <3 | <3 | <8 | <8 |
| Battery lifetime | years | >10 | >10 | >10 | >10 |
| UL data rate | kb/s | 0.3–62.5 | 0.3–159 | 375, 590 (HD) 1000, 3000 (FD) | 2625 (HD) 4000 (FD) |
| DL data rate | kb/s | 0.5–27.2 | 0.5–127 | 300, 800 (HD) 800, 1000 (FD) | 2275 (HD) 4000 (FD) |
| Parameter | GEO | LEO-600 | LEO-1200 | MEO-10000 |
|---|---|---|---|---|
| Satellite altitude | 35,786 km | 600 km | 1200 km | 10,000 km |
| Payload type | Transparent | |||
| Frequency band | S-band (∼2 GHz) | |||
| DL Transmissions | ||||
| Equivalent antenna aperture | 12–22 m | 0.097–2 m | 0.4–2 m | 1.5 m |
| Satellite EIRP density | 53.5–59.8 dBW/MHz | 21.45–34 dBW/MHz | 28.3–40 dBW/MHz | 45.4 dBW/MHz |
| Satellite Tx max gain | 45.5–51 dBi | 11–30 dBi | 16.2–30 dBi | 28.1 dBi |
| 3 dB beamwidth (HPBW) | 0.4011–0.7353° | 4.4127–104.7° | 4.4127–22.1° | 6.5° |
| Satellite beam diameter | 250–459 km | 50–1700 km | 90–470 km | 1140 km |
| UL Transmissions | ||||
| Equivalent satellite aperture | 12–22 m | 0.097–2 m | 0.4–2 m | 1.5 m |
| G/T (Figure of Merit) | 14–19 dB/K | −18.6 to 1.1 dB/K | −12.8 to 1.1 dB/K | 3.8 dB/K |
| Satellite Rx max gain | 45.5–51 dBi | 11–30 dBi | 16.2–30 dBi | 28.1 dBi |
| Beam Geometry | ||||
| Central beam center elevation | 12.5–20.9° | 30–90° | 30–46.1° | 90° |
| Central beam edge elevation | 2.3–12.5° | 23.8–30° | 22.2–30° | 81.6° |
| Link Budget | ||||
| Max FSPL (central beam edge) | 190.6–190.8 dB | 159.1–160.4 dB | 164.5–165.8 dB | 178.5 dB |
| Max satellite-UE distance | ∼40,581 km | ∼1076 km | ∼3131 km | ∼10,042 km |
| Architecture | Advantages | Disadvantages |
|---|---|---|
| Transparent (Bent-Pipe) | Low payload complexity and cost Leverages terrestrial gNB hardware Minimal satellite processing, high reliability Standardized first in 3GPP R17 | Requires continuous feeder link availability End-to-end latency No support for ISL gNB must compensate for Doppler of service and feeder links Limited to areas with ground station visibility |
| Regenerative (Full gNB Onboard) | Supports ISL via Xn interface Enables S&F operation for delay-tolerant services Lower latency (service link only) Reduced dependence on ground gateways Native support for 5G RAN features Enables packet routing in space, improving resilience | Payload complexity and cost Power consumption and thermal dissipation Radiation-hardened processing components Complex space qualification Standardization ongoing |
| Regenerative (Split CU-DU) | Reduces onboard processing compared to full gNB Centralized CU on ground for easier management Lower feeder link bandwidth Supports multiple sats per CU | Requires constant F1 link between CU and DU over feeder link Additional latency compared to full gNB onboard Depends on ground stations for CU connectivity Split selection involves complex trade-offs CU-DU handovers more complex |
| Relay-Like (VSAT-based) | Overcomes link-budget limitations for handheld devices Aggregation of multiple local devices Can serve areas with poor direct satellite-to-handset connectivity | Additional hop (VSAT) Maintenance of VSAT equipment Satellite sees VSAT as terminal, not individual UEs |
| Reference | Main Focus | Performance Study |
|---|---|---|
| Network Architecture | ||
| Rinaldi et al. [17] | Defines NTN (GEO/MEO/LEO, UAS/HAPS); transparent and regenerative architectures; multi-connectivity. | Continuity and scalability for eMBB/mMTC in remote areas. |
| He et al. [55] | Multilayered systems, mission planning, and mobility management for NGSO satellites. | LEO for low-latency broadband; GEO for broadcasting. |
| Tomaszewski et al. [57] | ETHER framework: SDN/NFV for unified management; Flexible Payload (FPGA). | AI-based automation of 3D (ground/air/space) infrastructure. |
| Baselga et al. [58] | Experimental analysis of Starlink; justification for regenerative solutions. | Backhaul relaying (50–60 ms) vs. critical delays (>1 s) for NR. |
| Zhou et al. [73] | SAM/SDM modes for ecological monitoring. | 9.99% improvement in IoT coverage vs. typical patterns. |
| MAC & Protocol Design | ||
| Mwakwata et al. [64] | 3GPP Rel. 13–16 changes; 20 dB coverage boost (MCL 164 dB). | 10-year battery life for IoT with ∼250 kbps peak rates. |
| Kodheli et al. [52] | RACH analysis: 970 ms access time for GEO satellites. | Comparison of NTN delays vs. terrestrial (∼12 ms). |
| Tuninato et al. [68] | Comparison of HARQ/RLC; need for >32 HARQ processes for MEO. | 8–18 dB HARQ gain; prevents exponential delay growth (2000 ms). |
| Zhou et al. [73] | DRL for dynamic edge (satellite) vs. cloud switching. | 9.99% improvement in IoT coverage vs. typical patterns. |
| Deployment | Orbit | Frequency | Terminal Type | Source |
|---|---|---|---|---|
| Sateliot | LEO (SSO) | S-band (n256): UL 1980–2010 MHz, DL 2170–2200 MHz | Standard 3GPP NB-IoT modules | [91] |
| Skylo (via Viasat/Inmarsat/EchoStar) | GEO | L-band (n255): 1525–1660.5 MHz; S-band (n256): 1980–2200 MHz; Band 23 | NB-IoT/LTE-M modules (e.g., Nordic nRF9151, Sony Altair ALT1250) | [92] |
| OQ Technology | LEO | S-band (LTE Band 65, ∼2 GHz); 60 MHz MSS S-band spectrum rights | Nordic nRF9151 cellular IoT module | [93] |
| Iridium Communications | LEO | Coordinated L-band spectrum | NB-IoT and D2D devices | [86] |
| Deutsche Telekom | GEO/LEO | n249, n255 (L-band), n256 (S-band) | Nordic nRF9151 | [94] |
| Mavenir & Terrestar | GEO | S-band (2–4 GHz); 40 MHz MSS spectrum | Sony Altair ALT1250 module | [95] |
| Airbus & OQ Technology | LEO | S-band (2–4 GHz) | Drone-mounted user terminals | [74] |
| Performance Metric | Reported Value and Capability | Deplyment |
|---|---|---|
| Packet Delivery Ratio | 90–95% in UAV BVLOS field trials | UAV Field Trial [102] |
| Coverage | ∼70 million km2, 37 countries, 5 continents | Skylo [103] |
| 36 countries, >60 million km2 | Skylo [92] | |
| 100% global coverage | Iridium [86] | |
| Device Capacity | Skylo GEO: ∼20 packets/min (up to 1200 bytes each) | Skylo [104] |
| Max 12 devices can simultaneously send/receive over the carrier | Kyocera AVX [105] | |
| Throughput | LEO (600–900 km): 20–40 kbps (comparable to terrestrial NB-IoT) | Skylo [92] |
| 5 kbps with 99.95% continuity (LEO, S-band drone demo) | OQ Technology [74] | |
| Latency (GEO) | ∼600 ms RTT | Skylo [103] |
| 5–10 s end-to-end | Skylo [104] | |
| Latency (LEO) | <1 s for small messages (Iridium NTN Direct) | Iridium [86] |
| Lower latency and higher data rates than GEO | Deutsche Telekom [89] | |
| Seconds in UAV field trials | UAV Field Trial [102] | |
| Power Consumption | 4–10 mAH per 10 satellite messages | Skylo [106] |
| Multi-year battery life; comparable to terrestrial in poor coverage areas | Skylo [106] | |
| Hundreds of mW in UAV field trials | UAV Field Trial [102] | |
| Signal Quality | Indoor not supported without specialized external antennas | Skylo [103] |
| Works in adverse weather; line-of-sight preferred | Iridium [86] |
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Beschastnyi, V.; Morozova, U.; Ostrikova, D.; Gaidamaka, Y.; Samouylov, K. A Review of the Current Development State of Non-Terrestrial NB-IoT Systems. Sensors 2026, 26, 5274. https://doi.org/10.3390/s26165274
Beschastnyi V, Morozova U, Ostrikova D, Gaidamaka Y, Samouylov K. A Review of the Current Development State of Non-Terrestrial NB-IoT Systems. Sensors. 2026; 26(16):5274. https://doi.org/10.3390/s26165274
Chicago/Turabian StyleBeschastnyi, Vitalii, Uliana Morozova, Darya Ostrikova, Yuliya Gaidamaka, and Konstantin Samouylov. 2026. "A Review of the Current Development State of Non-Terrestrial NB-IoT Systems" Sensors 26, no. 16: 5274. https://doi.org/10.3390/s26165274
APA StyleBeschastnyi, V., Morozova, U., Ostrikova, D., Gaidamaka, Y., & Samouylov, K. (2026). A Review of the Current Development State of Non-Terrestrial NB-IoT Systems. Sensors, 26(16), 5274. https://doi.org/10.3390/s26165274

