THOR 5

NORAD 32487· COSPAR 2008-006A· Active satellite· Communications· GEO
Launch
Launched on Feb 11, 2008 from 200/39 (200L), Kazakhstan aboard a Proton-M Briz-M.
Proton-M Briz-M | Thor 5
Live · TLE epoch 2026-07-13 08:19 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
Telenor Satellite
Country
Norway
Manufacturer
Launched
Feb 11, 2008
Mass
Apogee
35,805 km
Perigee
35,785 km
Inclination
0.05°
Period
23.94 h

About THOR 5

THOR 5 is a Norwegian geostationary communications satellite operated by Telenor Satellite, catalogued under NORAD ID 32487 and international designator 2008-006A. Launched in February 2008, it forms part of Norway's commercial satellite broadcasting infrastructure and serves direct-to-home television audiences primarily across Europe. The spacecraft remains in operation in geostationary orbit, stationed at 1° West longitude, where it provides continuous coverage of its target service area.

Mission and Purpose

The primary mission of THOR 5 is direct-to-home (DTH) television broadcasting, delivering satellite television signals to receiving dishes across Europe. The spacecraft carries 24 Ku-band transponders, a frequency range particularly well suited to consumer satellite broadcasting because Ku-band signals can be received by relatively compact ground-based dish antennas, making the technology practical and cost-effective for residential and small commercial users.

Ku-band broadcasting in the DTH context has been a cornerstone of European satellite television since the 1980s and 1990s, and THOR 5 continues that tradition under the Telenor Satellite umbrella. Telenor, a Norwegian telecommunications group, has maintained a fleet of Thor-branded satellites for several decades, using the 1° West orbital slot as a well-established hub for Scandinavian and broader European broadcast distribution. THOR 5 extends that presence, adding transponder capacity at a position that has long been associated with Nordic broadcasting services.

The satellite's also-known-as designation, Thor 2R, reflects a lineage of naming conventions within the Thor fleet, where replacement or successor craft sometimes carry alphanumeric suffixes that link them to their predecessors while signaling a new generation of hardware. The "R" designation in this context is commonly understood to indicate a replacement or refresh within the operational slot.

No mission status has been formally entered in the public satellite catalog for THOR 5 at this time, meaning the current operational condition of the spacecraft — whether fully active, partially operational, or in a reduced service mode — is not confirmed through the verified tracking record. However, its continued presence in geostationary orbit and the absence of a recorded decay or reentry date indicate the physical spacecraft remains in place.

Orbit and Tracking

THOR 5 occupies a geostationary orbit, the category of geosynchronous orbit in which a satellite's orbital period is synchronized to Earth's rotation rate, allowing it to remain effectively stationary above a fixed point on the equator. The orbital data confirm this classification precisely: the spacecraft has an orbital period of 1,436.2 minutes — approximately 23 hours and 56 minutes, which matches Earth's sidereal rotation period — and an inclination of 0.0°, meaning it travels directly along the equatorial plane without any north-south drift relative to ground observers.

The apogee of THOR 5's orbit stands at 35,807 km, while the perigee sits at 35,783 km. The difference of just 24 km between these two values indicates an extremely circular orbit, which is characteristic of well-maintained geostationary satellites. Any significant ellipticity would cause the satellite to drift in apparent position as seen from the ground, which would undermine its usefulness for fixed broadcast antennas that are pointed and left in place by consumers. The near-perfect circularity of THOR 5's orbit reflects both the precision of its insertion and, where applicable, station-keeping maneuvers conducted by ground controllers over the satellite's operational life.

From a tracking perspective, geostationary satellites like THOR 5 present a unique profile compared to low Earth orbit objects. Because the satellite moves in lockstep with Earth's rotation, it does not rise and set across the sky in the manner of lower-orbiting spacecraft. Instead, it appears as a fixed point in the sky to any observer within its coverage footprint. This makes it essentially invisible to casual sky-watchers looking for moving objects, and it cannot be spotted through the kind of naked-eye passes that make low Earth orbit satellites observable at dawn and dusk. Professional tracking networks including those that assign and maintain NORAD catalog entries continue to monitor geostationary objects through radar and optical means to confirm their positions and detect any unexpected maneuvers or anomalies.

The assigned NORAD catalog number, 32487, provides THOR 5 with a unique identifier in the global space object registry maintained by United States Space Command, ensuring it is distinguished from the thousands of other catalogued objects in Earth orbit.

Design and Operator

THOR 5 was constructed by Orbital Sciences Corporation, a manufacturer with a significant track record in commercial communications satellites. The spacecraft is built on the STAR-2 satellite bus, a mid-size platform developed by Orbital Sciences designed to support moderate payload capacities while maintaining relatively compact dimensions and mass efficiency compared to larger geostationary platforms. The STAR-2 bus is designed to accommodate Ku-band and other communications payloads, making it a natural fit for a direct-to-home broadcasting mission.

One of the operationally notable aspects of THOR 5's deployment was the manner in which it reached its operational orbit. The launch vehicle — an International Launch Services Proton-M rocket equipped with a Briz-M upper stage — delivered the satellite directly into geosynchronous orbit. This so-called direct-to-GEO injection is a capability that distinguishes the Proton-M/Briz-M combination from launch systems that place satellites into a lower transfer orbit and require the spacecraft itself to perform a lengthy series of apogee motor firings to raise its orbit to the final operational altitude. By eliminating the need for onboard propulsion to execute these raising maneuvers, the spacecraft could be built with a reduced propellant load, saving mass and allowing either a lighter satellite or the reallocation of mass budget to the payload itself.

The Proton-M is a heavy-lift launch vehicle with Soviet-era origins, developed into a workhorse of commercial geostationary satellite launches through the International Launch Services joint venture. Its Briz-M upper stage, a restartable liquid-propellant stage, provides the multiple burns needed to circularize an orbit precisely at geostationary altitude. The launch took place on 11 February 2008, lifting off at 00:34 local time in the UTC+5 zone of the Baikonur Cosmodrome in Kazakhstan, where Proton launches originate — which corresponds to 11 February 2008 at approximately 19:34 UTC and 10 February 2008 at 19:00 Eastern Standard Time, the latter matching the launch timestamp in the verified catalog record.

Telenor Satellite, headquartered in Norway, is the operating entity responsible for THOR 5. As a subsidiary of the broader Telenor telecommunications group, Telenor Satellite manages a fleet of satellites under the Thor brand, providing capacity to broadcasters, platform operators, and service providers across the Nordic region and beyond. Norway is listed as the owner country in the satellite catalog, reflecting the national affiliation of the operating organization.

The manufacturer's mass figures for THOR 5 are not recorded in the publicly available catalog data, so no launch mass or dry mass can be stated here.

Current Status and Significance

THOR 5 holds a position in the small but meaningful community of Norwegian government-affiliated commercial satellites that have given Norway consistent independent access to broadcasting and telecommunications infrastructure through the late twentieth and early twenty-first centuries. The 1° West slot it occupies is among the more sought-after orbital positions for European broadcasting, given its favorable geometry for Scandinavian and northern European coverage areas and its long-established presence in consumer receiver installations across those markets.

The satellite was launched at a period when the direct-to-home broadcasting market in Europe was highly competitive and expanding, driven by increasing channel counts, the emergence of high-definition content, and the growth of digital satellite platforms. THOR 5's 24 Ku-band transponders added meaningful capacity to the 1° West position, reinforcing Telenor Satellite's ability to serve both existing broadcast clients and attract new business.

As of the current tracking data, THOR 5 has not decayed or reentered the atmosphere and remains in its geostationary orbital slot. Geostationary satellites at end of life are typically raised into a higher "graveyard orbit" above the geostationary belt to vacate the valuable orbital slot for successor spacecraft — a practice mandated by international guidelines to reduce long-term congestion in geostationary orbit. Whether THOR 5 has reached that stage of its lifecycle is not confirmed in the public catalog record.

The satellite's relatively circular orbit and equatorial inclination of 0.0° confirm that the spacecraft, wherever it currently stands in its operational life, continues to reside in a well-controlled geostationary position consistent with an actively managed asset or one that has received proper end-of-life disposal treatment. Its continued cataloguing under NORAD ID 32487 ensures that it remains part of the international registry of tracked space objects for as long as it persists at altitude.

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