THEOS

NORAD 33396· COSPAR 2008-049A· Active satellite· Earth Observation· SSO
Live · TLE epoch 2026-06-10 03:13 UTC
Orbit class
SSO — Sun-Synchronous (LEO at 96–102° inclination)
Operator
Geo-Informatics and Space Technology Development Agency
Country
Thailand
Manufacturer
Astrium
Launched
Oct 1, 2008
Mass
715 kg
Apogee
830 km
Perigee
828 km
Inclination
98.56°
Period
1.69 h
Launch
Launched on Oct 1, 2008 from 370/13, Russia aboard a Dnepr 1.
Dnepr | Thaichote

About THEOS

THEOS (also catalogued as THEOS-1, NORAD ID 33396, international designator 2008-049A) is a Thai Earth observation satellite launched on 30 September 2008. Built by Astrium — the European aerospace and defence manufacturer — and operated by Thailand's Geo-Informatics and Space Technology Development Agency (GISTDA), the spacecraft represented a landmark step in Thailand's development of an indigenous space capability. Massing 715 kg at launch, the satellite was placed into a near-circular sun-synchronous orbit and, as of the time of writing, remains in service.

Mission and Purpose

THEOS was conceived as the centrepiece of Thailand's ambitions to establish a self-reliant capacity in Earth observation from space. GISTDA, headquartered in Bangkok and operating as the country's principal national body for space technology and its applications, drove the programme forward under the broader sponsorship of the Thai Ministry of Science and Technology. The agency's mandate spans remote-sensing data acquisition, geospatial data management, and the nurturing of domestic expertise in satellite operations — all of which THEOS was designed to support.

Earth observation satellites of this class are typically tasked with acquiring high-resolution imagery of the land surface, coastlines, and inland water bodies for applications such as agricultural monitoring, disaster assessment, urban planning, land-use mapping, and natural resource management. Thailand, with its diverse geography ranging from river deltas and coastal zones to highland forests and densely populated urban corridors, presents a rich set of monitoring needs that a dedicated national satellite can address far more flexibly than reliance on commercial or foreign imagery alone.

The specific payload instruments and their formal performance specifications are not recorded in the public catalog entry for this object, so no claims are made here about sensor resolution or swath width beyond what is publicly verifiable. What is clear from the programme's origins is that the satellite was intended to give Thailand direct, sovereign access to remotely sensed data for civil and governmental purposes.

Orbit and Tracking

THEOS operates in a sun-synchronous orbit (SSO), a class of near-polar orbit in which the orbital plane precesses at a rate that keeps it aligned with the Earth–Sun direction throughout the year. This geometry ensures that the satellite passes over any given point on the ground at approximately the same local solar time on each revisit, which is invaluable for Earth observation because consistent solar illumination makes it far easier to compare images taken on different dates. The technique is standard practice for optical remote-sensing missions worldwide.

The spacecraft's orbital parameters, as recorded in the catalog, describe a very nearly circular track: the apogee stands at 830 km above the Earth's surface and the perigee at 828 km, yielding an altitude difference of only 2 km between the highest and lowest points of each revolution. This extremely low eccentricity is characteristic of a well-maintained observation orbit. The orbital inclination is 98.6°, which is slightly retrograde — again typical of sun-synchronous orbits, whose required inclination increases with altitude to maintain the necessary nodal precession rate. The satellite completes one full revolution of the Earth every 101.3 minutes, meaning it makes just under fourteen and a quarter orbits per day.

From the perspective of satellite tracking, THEOS presents as a compact but reasonably massive payload. At 715 kg it is not a nanosatellite or CubeSat, but neither is it among the largest Earth observation platforms. Its stable, near-circular SSO at roughly 829 km mean altitude keeps it well clear of the denser debris environment of lower orbits and ensures predictable ground-track repeat cycles. The object has been continuously tracked since launch under catalog number 33396 and has shown no signs of uncontrolled orbital decay; its perigee has remained essentially constant, suggesting that any station-keeping manoeuvres required to compensate for atmospheric drag at this altitude are being performed — or that drag at 828–830 km is sufficiently low to render frequent correction unnecessary.

Design and Operator

The satellite was designed and manufactured by Astrium, the European space systems company headquartered in various sites across France, Germany, and the United Kingdom (the Toulouse facility in France being specifically associated with the THEOS programme). Astrium, which has since been integrated into Airbus Defence and Space, has a long track record of producing Earth observation platforms for both institutional and commercial customers. The THEOS contract was formalised in July 2004, giving the project approximately four years of development and testing before its 2008 launch.

At 715 kg, the spacecraft falls into the medium-small category for dedicated Earth observation satellites. Astrium produced a range of platform sizes, and THEOS draws on heritage from the company's experience with similar missions, though the specific platform designation is not confirmed in the catalog entry and is therefore not stated here as fact.

GISTDA, the operating agency, was established to advance Thailand's position in space technology and geospatial science. It functions not merely as a satellite operator but as the focal point for the country's broader space sector, including training programmes, data dissemination infrastructure, and international cooperation agreements. The partnership with Astrium was structured not only to deliver a working satellite but also to facilitate a degree of technology transfer and capacity building, enabling Thai engineers to participate in aspects of the satellite's development and to build the ground segment expertise needed to operate it independently.

Significance and Current Status

When THEOS launched in September 2008, Thailand became one of a relatively small number of Southeast Asian nations to operate its own dedicated Earth observation satellite. This placed the country in a select regional cohort and signalled a broader strategic intent: rather than simply purchasing satellite imagery from international vendors, Thailand was investing in the infrastructure and human capital needed to generate and manage that data domestically. For a region prone to seasonal flooding, rapid agricultural land-use change, and coastal erosion — all phenomena that benefit enormously from regular, timely overhead imagery — this kind of national capability carries genuine operational value.

The satellite's longevity is also noteworthy. Launched more than sixteen years before the date of this writing, THEOS continues to orbit at essentially the same altitude at which it was placed in 2008. Many satellites of its era have already re-entered the atmosphere or been formally retired. That THEOS remains catalogued as a functioning payload, still maintaining its orbit in the 828–830 km band, speaks to the durability of the design and the operational continuity provided by GISTDA.

It should be noted that the mission's current operational status is not formally recorded in the public tracking catalog — the entries for mission type and mission status are listed as unknown. It is therefore not possible to state with certainty, from catalog data alone, whether THEOS is still actively acquiring imagery or has transitioned to a reduced operational mode. What is confirmed is that the spacecraft has not decayed and remains trackable in its designated orbit.

THEOS was followed by subsequent Thai space initiatives, including the development of THEOS-2, demonstrating that the original programme succeeded in its broader aim of establishing a foundation for continued national investment in space-based Earth observation.

How to Spot THEOS

THEOS orbits at an altitude of approximately 829 km in a sun-synchronous, near-polar orbit inclined at 98.6° to the equatorial plane. This inclination means the satellite passes over virtually every latitude on Earth, including locations well into the mid-latitudes of both hemispheres, making it potentially visible from a very wide range of ground sites.

With an orbital period of 101.3 minutes, THEOS completes roughly fourteen orbits per day, and its ground track shifts westward with each successive pass as the Earth rotates beneath it. Observers using satellite-tracking software or online tools — such as the real-time tracker available on this page — can compute pass times and directions for their specific location.

As a 715 kg spacecraft in a relatively low Earth orbit, THEOS is not among the brightest objects in the sky; it lacks the large solar panel arrays of crewed stations or some larger platforms that can make such objects conspicuous to the naked eye. Visibility on any given pass will depend on the observer's latitude, the geometry of the pass (elevation above the horizon), and ambient lighting conditions. The best opportunities arise during twilight hours — shortly after sunset or before sunrise — when the observer is in darkness but the satellite is still illuminated by sunlight. Passes where the satellite climbs above 30° elevation are generally the most productive. The live tracking data on this page will identify upcoming visible passes for your location.

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