NewOrbit Space Advances NEO-1 Very-Low Orbit Demonstration Mission

NewOrbit Space Advances NEO-1 Very-Low Orbit Demonstration Mission

NewOrbit Space is a UK-based satellite manufacturer developing spacecraft designed to operate sustainably in Very Low Earth Orbit (VLEO), between approximately 180 km and 300 km altitude. The company’s first in-orbit demonstration mission, NEO-1, will validate a new generation of high-efficiency electric propulsion and spacecraft technologies tailored specifically for this demanding orbital regime.

The mission is designed to demonstrate sustained operations at very-low altitudes, where atmospheric drag, aerodynamic torques and atomic oxygen exposure present unique engineering challenges.

Unlocking Sustainable Operations Below 300 km

Historically, orbits below 300 km have been considered impractical for long-duration missions due to rapid orbital decay. Satellites operating at these altitudes typically experience lifetimes measured in weeks or months unless continuous station-keeping is performed.

NewOrbit’s NEO-1 platform is engineered specifically to address these challenges through:

  • High-efficiency electric propulsion optimized for drag compensation
  • Aerodynamically stable spacecraft architecture
  • Atomic oxygen-resistant materials and surface treatments
  • Very-low-orbit-specific attitude determination and control modes

By combining propulsion efficiency with structural and systems-level design tailored to ULEO, NEO-1 aims to demonstrate controlled descent, station-keeping, and sustained operation in this previously underutilized orbital band.

A Dedicated Ultra-Low Orbit Satellite Platform

Unlike traditional LEO satellites adapted for lower altitudes, the NEO platform has been designed from the ground up for VLEO operations. The spacecraft integrates:

  • A high-specific-impulse RF ion propulsion system (stored-propellant configuration)
  • Redundant propulsion architecture for operational resilience
  • Advanced thermal management to accommodate higher drag heating
  • Aerodynamic mass distribution for passive stability
  • ADCS systems adapted for elevated aerodynamic torque environments

The satellite is compatible with standard LEO launch vehicles and performs a controlled orbital transfer from deployment altitude down to its operational regime.

Demonstrating the Economic Advantage of Flying Lower

Operating closer to Earth provides substantial performance benefits for Earth observation missions:

  • Higher imaging resolution from smaller apertures
  • Reduced payload size for equivalent ground sampling distance
  • Lower latency and improved data throughput
  • Naturally self-clearing orbital environment due to atmospheric drag

For example, imaging performance that typically requires large, high-cost satellite platforms in conventional LEO can be achieved with significantly smaller optical systems when operating at ~200 km.

NEO-1 will demonstrate these advantages in orbit while validating the spacecraft’s ability to operate reliably under elevated drag conditions.

Focused on Full Satellite Ownership and Integration

NewOrbit develops its satellite platform in-house rather than rely on third-party buses. This decision enables:

  • Tight propulsion-platform integration
  • Full control over aerodynamic and structural design
  • Optimized system-level mass and power budgets
  • Faster iteration between propulsion and spacecraft engineering teams

Purpose-Built Testing Infrastructure

To support development, NewOrbit operates dedicated testing infrastructure and propulsion validation facilities in the UK. These facilities enable:

  • Integrated propulsion endurance testing
  • High-voltage and RF electronics validation
  • Air-intake and plasma system characterization
  • Thermal-vacuum testing of subsystems

This in-house capability accelerates development cycles and reduces dependency on external facilities during critical testing phases.

NEO-1 as a Pathway to Operational VLEO Missions

The NEO-1 mission is designed as a pathfinder for future operational satellites capable of multi-year missions in the 180–300 km range. Beyond propulsion validation, the mission will gather valuable data on:

  • Atmospheric density variation
  • Spacecraft dynamics in high-drag environments
  • ADCS performance under aerodynamic torque loading
  • Power and thermal behavior in VLEO
  • Hosting Customer and Partner Payloads on the Pathfinder Mission
  • The spacecraft will host multiple payloads from selected customers and strategic partners to demonstrate real mission capability in Very Low Earth Orbit (VLEO). By flying operational payloads alongside the propulsion system, NewOrbit will validate not only drag compensation and station-keeping, but also the practical performance improvements achievable at lower altitudes — including higher imaging resolution, improved data throughput, and enhanced mission efficiency. This approach ensures that NEO-1 delivers tangible in-orbit results for partners while proving that sustained VLEO operation is commercially viable, scalable, and ready for future production missions.

By validating sustained operation in very-low orbits, NewOrbit aims to open a new operational regime for commercial and institutional Earth observation missions.

About NewOrbit Space

NewOrbit Space is a UK-based aerospace company developing high-efficiency electric propulsion and fully integrated satellite platforms for sustained operations in Very Low Earth Orbit. The company focuses on unlocking the performance, economic, and sustainability advantages of flying closer to Earth through propulsion innovation and vertically integrated spacecraft design.

Click here to learn more about NewOrbit Space's NEO-1 Orbiting Satellite

Publisher: SatNow

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BeiDou-3 G4Geostationary Orbit (GEO)17 May, 2023
BeiDou-3 G2Geostationary Orbit (GEO)09 Mar, 2020
Compass-IGSO7Inclined Geosynchronous Orbit (IGSO)09 Feb, 2020
BeiDou-3 M19Medium Earth Orbit (MEO)16 Dec, 2019
BeiDou-3 M20Medium Earth Orbit (MEO)16 Dec, 2019
BeiDou-3 M21Medium Earth Orbit (MEO)23 Nov, 2019
BeiDou-3 M22Medium Earth Orbit (MEO)23 Nov, 2019
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BeiDou-3 M24Medium Earth Orbit (MEO)22 Sep, 2019

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Satellite NameOrbit Date
GSAT0223MEO - Near-Circular05 Dec, 2021
GSAT0224MEO - Near-Circular05 Dec, 2021
GSAT0219MEO - Near-Circular25 Jul, 2018
GSAT0220MEO - Near-Circular25 Jul, 2018
GSAT0221MEO - Near-Circular25 Jul, 2018
GSAT0222MEO - Near-Circular25 Jul, 2018
GSAT0215MEO - Near-Circular12 Dec, 2017
GSAT0216MEO - Near-Circular12 Dec, 2017
GSAT0217MEO - Near-Circular12 Dec, 2017
GSAT0218MEO - Near-Circular12 Dec, 2017

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Kosmos 2569--07 Aug, 2023
Kosmos 2564--28 Nov, 2022
Kosmos 2559--10 Oct, 2022
Kosmos 2557--07 Jul, 2022
Kosmos 2547--25 Oct, 2020
Kosmos 2545--16 Mar, 2020
Kosmos 2544--11 Dec, 2019
Kosmos 2534--27 May, 2019
Kosmos 2529--03 Nov, 2018
Kosmos 2527--16 Jun, 2018

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Satellite NameOrbit Date
Navstar 82Medium Earth Orbit19 Jan, 2023
Navstar 81Medium Earth Orbit17 Jun, 2021
Navstar 78Medium Earth Orbit22 Aug, 2019
Navstar 77Medium Earth Orbit23 Dec, 2018
Navstar 76Medium Earth Orbit05 Feb, 2016
Navstar 75Medium Earth Orbit31 Oct, 2015
Navstar 74Medium Earth Orbit15 Jul, 2015
Navstar 73Medium Earth Orbit25 Mar, 2015
Navstar 72Medium Earth Orbit29 Oct, 2014
Navstar 71Medium Earth Orbit02 Aug, 2014

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Satellite NameOrbit Date
NVS-01Geostationary Orbit (GEO)29 May, 2023
IRNSS-1IInclined Geosynchronous Orbit (IGSO)12 Apr, 2018
IRNSS-1HSub Geosynchronous Transfer Orbit (Sub-GTO)31 Aug, 2017
IRNSS-1GGeostationary Orbit (GEO)28 Apr, 2016
IRNSS-1FGeostationary Orbit (GEO)10 Mar, 2016
IRNSS-1EGeosynchronous Orbit (IGSO)20 Jan, 2016
IRNSS-1DInclined Geosynchronous Orbit (IGSO)28 Mar, 2015
IRNSS-1CGeostationary Orbit (GEO)16 Oct, 2014
IRNSS-1BInclined Geosynchronous Orbit (IGSO)04 Apr, 2014
IRNSS-1AInclined Geosynchronous Orbit (IGSO)01 Jul, 2013
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