NSS-9

NORAD 33749· COSPAR 2009-008A· Active satellite· Communications· GEO
Launch
Launched on Feb 12, 2009 from Ariane Launch Area 3, French Guiana aboard a Ariane 5 ECA.
Ariane 5 ECA | Hot Bird 10, NSS-9, Spirale A, Spirale B
Live · TLE epoch 2026-07-13 14:20 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
SES World Skies
Country
SES
Manufacturer
Launched
Feb 12, 2009
Mass
Apogee
35,803 km
Perigee
35,787 km
Inclination
1.33°
Period
23.94 h

About NSS-9

NSS-9 is a geostationary communications satellite operated by SES World Skies, launched on February 11, 2009, and assigned NORAD catalog identifier 33749 under the international designator 2009-008A. Positioned in a near-perfect geostationary orbit above the Earth, the spacecraft serves as a dedicated C-band relay platform, continuing the communications legacy of its predecessor in the SES fleet. As of the most recent catalog data, NSS-9 remains in orbit and operational status has not been formally retired in public records.

Mission and Purpose

NSS-9 was developed and deployed specifically to succeed NSS-5, an earlier-generation satellite in the SES World Skies family. The transition from NSS-5 to NSS-9 represented an effort to maintain continuity of service in the C-band frequency range, which occupies a portion of the radio spectrum particularly valued for its resilience to atmospheric interference, including rain fade — a characteristic that has made C-band a long-standing backbone for broadcasting, broadband backhaul, and maritime and aeronautical communications across wide geographic areas.

The satellite carries an all-C-band payload, meaning it does not operate in Ku-band or Ka-band frequencies as many modern hybrid satellites do. Its communications architecture is organized across three distinct beams, with 44 active C-band transponders distributed among them. This configuration allows NSS-9 to serve multiple geographic footprints simultaneously, directing capacity toward different regions depending on how the beams are oriented and shaped. C-band satellites of this type typically provide wide area coverage, making them well suited for cable television distribution, direct-to-home broadcasting in regions where larger dish antennas are practical, and enterprise connectivity services for remote or underserved locations.

The replacement of NSS-5 was a straightforward continuity-of-service decision common in commercial satellite operations. Satellites are designed with finite operational lifetimes, and operators regularly plan successor spacecraft to slot into the same or adjacent orbital positions, ensuring that customers relying on a given capacity source experience minimal disruption. NSS-9 was intended to absorb the traffic and service agreements previously supported by its predecessor while offering the technical improvements inherent in more contemporary satellite construction.

Orbit and Tracking

NSS-9 occupies a geostationary orbit, the class of orbit in which a satellite's orbital period closely matches the rotational period of the Earth beneath it. With an orbital period of approximately 1,436.2 minutes — essentially matching one full sidereal day — the satellite appears to remain fixed relative to a point on the Earth's surface. This quality is fundamental to communications satellites, as it allows ground antennas to point to a fixed position in the sky rather than track a moving object, dramatically simplifying infrastructure for both broadcast and data applications.

The orbital parameters recorded in the satellite catalog describe a very well-circularized geostationary orbit. The apogee stands at 35,804 kilometers and the perigee at 35,786 kilometers, a difference of only 18 kilometers that reflects the exceptionally low eccentricity expected of an object that has been properly station-kept in geostationary orbit. An inclination of 1.2 degrees indicates a very slight deviation from the ideal equatorial plane of 0 degrees, which is a common characteristic of operational geostationary satellites over time, as station-keeping maneuvers may not perfectly maintain zero inclination, or the satellite may have been allowed a modest drift as part of its operational management. Satellites near the end of their operational lives are sometimes permitted to accrue small inclination values as fuel conservation measures, though this is not the only explanation for the observed 1.2-degree figure.

For tracking purposes, NSS-9 is cataloged under NORAD ID 33749. Geostationary satellites are cataloged and tracked by the United States Space Surveillance Network like any other orbiting object, though their near-stationary nature means their catalog elements change relatively slowly compared to objects in low or medium Earth orbit. Users of this site can use the catalog entry to retrieve current two-line element sets and compute the precise apparent sky position of NSS-9 from any location on Earth. Because of its geostationary nature, observers in the satellite's coverage hemisphere will find it appears at a fixed elevation and azimuth, varying only with the observer's latitude and longitude relative to the satellite's sub-satellite point on the equator.

Design and Operator

NSS-9 is registered under the ownership of SES, a Luxembourg-based satellite operator that is among the largest in the world by fleet size and orbital capacity. The satellite was operated commercially under the SES World Skies brand, which was the name used by SES to market and manage a portion of its fleet that had origins in the former New Skies Satellites organization — a company spun off from Intelsat in the late 1990s before being absorbed into the broader SES group. SES World Skies served as the operational identity for this lineage of satellites, including the NSS series, during the period surrounding NSS-9's launch.

The specific manufacturer of NSS-9 is not recorded in the publicly available satellite catalog data used by this site. Geostationary communication satellites of this era were produced by a relatively small number of major prime contractors, including Boeing Satellite Systems, Thales Alenia Space, Orbital Sciences, and Loral Space and Communications, among others, but no manufacturer attribution has been confirmed in the verifiable data available here. The satellite's mass is similarly not recorded in the public catalog.

The decision to configure NSS-9 as an all-C-band satellite, rather than incorporating the Ku-band capacity that many contemporaneous satellites carried as their primary or secondary payload, reflected the specific service requirements and orbital slot strategies of SES World Skies at the time of procurement. C-band infrastructure tends to require larger ground-side antennas but offers advantages in coverage area and weather robustness that are particularly valued in tropical regions and in maritime environments.

Current Status and Significance

NSS-9 launched on February 11, 2009, and as of current catalog records it remains in orbit with no decay or reentry date logged. Whether the satellite is still actively providing commercial services, has been placed in inclined orbit operations — a cost-saving measure used for older satellites in which north-south station-keeping is discontinued — or has been retired to a graveyard orbit or passivated in place, is not confirmed by the publicly available catalog entries consulted here.

Within the broader history of SES and the NSS satellite series, NSS-9 represents a transitional moment. The NSS designator itself traces a lineage back through New Skies Satellites to the restructuring of the international commercial satellite industry in the post-Intelsat privatization period of the 1990s and 2000s. By the time NSS-9 launched, SES was already integrating various fleet brands, and subsequent satellites in the SES portfolio were progressively branded under the unified SES naming convention rather than legacy identifiers. NSS-9 therefore occupies a late position in the NSS series, carrying forward a designation that was already becoming historical even as the satellite entered service.

The 44-transponder C-band payload aboard NSS-9 represents a meaningful block of communications capacity. Each active transponder typically supports a discrete block of bandwidth that can carry multiple television channels, high-speed data streams, or a combination of services depending on how the capacity is allocated and modulated. An all-C-band satellite of this size is capable of supporting substantial broadcasting and connectivity loads across the three-beam coverage pattern, making NSS-9 a materially significant piece of telecommunications infrastructure for the regions within its footprint.

For those interested in the history of commercial geostationary satellite operations, NSS-9 offers a useful case study in fleet planning: the deliberate sequencing of satellite replacements, the continued relevance of C-band in an era increasingly associated with higher-frequency bands, and the consolidation dynamics of the commercial satellite industry as large operators absorbed the fleets of smaller predecessors and integrated them under unified management structures. The satellite's continued presence in the geostationary arc, more than fifteen years after its launch, is itself a reflection of the long design lifetimes that characterize modern telecommunications spacecraft.

How to Spot It

As a geostationary satellite at approximately 35,800 kilometers altitude, NSS-9 is not a candidate for naked-eye observation under typical conditions. Objects in geostationary orbit move imperceptibly against the star background as seen from the ground, and at that distance they are far too faint to be detected without optical aid. Dedicated observers using telescopes have successfully imaged geostationary satellites, and the fixed sky position that NSS-9 occupies makes it predictable to locate once the relevant coordinates are calculated for a given observer's location. Using the orbital data provided on this page, observers with appropriate equipment can determine the exact azimuth and elevation at which NSS-9 should appear from their geographic position and attempt to identify it as a stationary point of light against slowly drifting stars during long-exposure imaging.

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