SENTINEL-6A

NORAD 46984· COSPAR 2020-086A· Active satellite· Earth Observation· LEO
SENTINEL-6A
NASA · Public domain · via Wikimedia Commons
Live · TLE epoch 2026-06-10 05:09 UTC
Orbit class
LEO — Low Earth Orbit (circular, < 2,000 km)
Operator
EUMETSAT
Country
European Space Agency
Manufacturer
Thales Alenia Space
Launched
Nov 21, 2020
Mass
1,226 kg
Apogee
1,350 km
Perigee
1,337 km
Inclination
66.04°
Period
1.87 h
Launch
Launched on Nov 21, 2020 from Space Launch Complex 4E, United States of America aboard a Falcon 9 Block 5.
Falcon 9 Block 5 | Sentinel-6 Michael Freilich

About SENTINEL-6A

Sentinel-6A — also formally designated Sentinel-6 Michael Freilich and catalogued under NORAD ID 46984 (COSPAR: 2020-086A) — is an Earth-observation satellite built to extend and refine the long-running global record of sea-surface height measurements. Launched on 20 November 2020 aboard a Falcon 9 rocket from Vandenberg Air Force Base, it represents a landmark in transatlantic cooperation for ocean science, combining European engineering heritage with American scientific investment. The spacecraft remains in orbit and has been operational since mid-2021, continuing the legacy of the Jason altimetry series.

Mission and Purpose

The primary objective of Sentinel-6A is the highly precise measurement of sea-surface topography — in essence, mapping the shape of the ocean's surface to a degree of accuracy that reveals currents, tides, and the slow but consequential rise of global mean sea level. This kind of data has been collected continuously since the early 1990s through a succession of joint missions, and Sentinel-6A was designed to ensure that no gap would emerge in the resulting multi-decade climate record. Continuity is paramount in sea-level science: even a brief interruption in observations can compromise the ability of researchers to detect long-term trends against the natural variability of the ocean.

Beyond open-ocean monitoring, the satellite applies advanced radar altimetry to a broader range of water bodies. Rivers and lakes, which present far more spatially constrained targets than the open sea, benefit from modern synthetic-aperture processing techniques that sharpen the effective measurement footprint of the radar beam. This capability extends the utility of the mission into hydrology and freshwater monitoring, areas of growing concern given changing precipitation patterns and water availability in many regions of the world.

The satellite is named in honour of Michael Freilich, who led NASA's Earth Science Division for more than a decade and was a passionate advocate for ocean altimetry and the international partnerships that sustain it. His leadership was instrumental in forging and maintaining the U.S.–European collaboration that produced the Jason series, of which Sentinel-6A is the most recent chapter.

The programme is operated by EUMETSAT, the European Organisation for the Exploitation of Meteorological Satellites, which is responsible for receiving, processing, and distributing the satellite's data to scientific users worldwide. The mission was developed under the authority of the European Space Agency (ESA), which owns the spacecraft, and was built in close collaboration with EUMETSAT, the European Commission, NOAA, NASA, and CNES, the French space agency. This multi-agency structure reflects the depth of institutional investment that sea-surface height records have attracted over several decades.

Orbit and Tracking

Sentinel-6A occupies a low Earth orbit with an apogee of 1,350 km and a perigee of 1,337 km, giving it a near-circular orbit at an altitude roughly consistent with the operational requirements of precision radar altimetry. The orbital inclination is 66.0°, which allows the satellite's ground track to sweep across a broad swath of the globe, covering the ocean areas most relevant to sea-level science while also reaching a substantial portion of the world's river basins and enclosed seas.

The orbital period is 112.4 minutes, meaning the satellite completes slightly under thirteen full revolutions of the Earth each day. Over time, the ground track repeats in a carefully engineered pattern that ensures the same locations on the ocean surface are revisited at regular intervals, enabling meaningful comparisons between passes. This repeat-track approach is fundamental to altimetry: the satellite must pass over the same reference points reliably so that changes in water height can be isolated from variations introduced by a shifting viewing geometry.

The spacecraft's mass at launch was 1,226 kg, placing it in the medium-class category for Earth-observation payloads. At its operational altitude, the satellite is not subject to the rapid orbital decay that affects satellites in very low orbits, but it remains within the zone tracked continuously by ground-based surveillance networks and catalogued by organisations such as the 18th Space Control Squadron. NORAD tracking data for NORAD ID 46984 is available through standard two-line element set (TLE) services and is updated regularly as ground stations refine the orbital solution.

The inclination of 66.0° means that Sentinel-6A is not in a sun-synchronous orbit, which is used by many other Earth-observation missions to maintain a consistent solar illumination angle. Instead, its orbit is optimised for geodetic coverage and repeat-track fidelity, priorities that differ from those of, for example, optical imaging missions.

Design and Operator

Sentinel-6A was manufactured by Thales Alenia Space, a Franco-Italian aerospace company with deep experience in radar altimetry hardware, having contributed to multiple generations of ocean-monitoring satellites. The spacecraft bus carries as its central instrument a Poseidon-4 synthetic-aperture radar altimeter, which extends conventional pulse-limited altimetry with delay-Doppler processing. This technique effectively narrows the along-track dimension of the radar measurement, reducing noise and allowing finer spatial resolution, particularly important when measuring smaller or more complex water bodies.

The satellite also carries a suite of supporting instruments intended to correct the altimetric measurements for atmospheric propagation delays. Water vapour in the troposphere slows the radar pulse in a way that, if unaccounted for, would introduce errors into the height estimate. A microwave radiometer aboard the spacecraft measures atmospheric moisture content to apply the necessary corrections. Ionospheric delay corrections are handled through a dual-frequency approach in the primary radar system itself.

EUMETSAT manages the satellite's day-to-day operations from its headquarters in Darmstadt, Germany, coordinating with a network of ground stations to receive telemetry, upload commands, and downlink science data. Processed data products are made available to users under an open-access policy consistent with the Copernicus Earth Observation Programme's broader data philosophy, though Sentinel-6A sits at the intersection of the Copernicus framework and the older Jason series lineage, giving it a somewhat hybrid institutional identity.

Significance and Current Status

Sentinel-6A carries particular scientific importance because of where it sits in the continuous altimetry record. The Jason series — beginning with TOPEX/Poseidon in 1992, followed by Jason-1, Jason-2, and Jason-3 — has produced an unbroken time series of global sea-surface height spanning more than three decades. That record documents an accelerating rise in mean sea level, a signal of considerable relevance to climate policy, coastal infrastructure planning, and the management of flood risk in low-lying areas worldwide.

Sentinel-6A was positioned to fly in a tandem formation with Jason-3 for an initial period following its launch, allowing the two satellites' measurements to be cross-calibrated directly. This tandem phase is a standard practice in the altimetry community and is essential for avoiding artificial discontinuities in the long-term data record. When sensors on successive satellites are cross-calibrated in this way, the resulting merged time series can be treated as a single coherent dataset spanning multiple decades and multiple spacecraft generations.

The spacecraft is expected to operate for approximately 5.5 years, after which a successor mission — Sentinel-6B — is anticipated to continue the series. The planned handover from one satellite to the next, with an overlapping operational period, mirrors the approach that has maintained the continuity of the Jason record through each of its earlier transitions.

As of the time of writing, Sentinel-6A remains in orbit and is understood to be in an operational phase consistent with its mission profile, though the public catalog entry for this object does not record a specific current mission status. The data it produces feeds directly into operational oceanography, numerical weather prediction, and the scientific monitoring programmes that underpin international assessments of climate change.

The satellite also holds a degree of symbolic importance as the first mission in the Copernicus family to bear the name of an individual — a recognition of Michael Freilich's decades-long contribution to Earth science and to the collaborative frameworks that make missions like this one possible. That gesture of naming, rare in the traditions of space agency nomenclature, reflects how central his advocacy was to the institutional history of sea-level observation from space.

How to Spot It

At an altitude of approximately 1,337–1,350 km and with a mass of 1,226 kg, Sentinel-6A is a moderately sized object at a relatively high altitude for a low-Earth-orbit satellite. Its visibility to the naked eye will be limited and highly dependent on geometry, observer latitude, and atmospheric conditions. At an inclination of 66.0°, it is accessible to observers across a wide range of latitudes — well into the mid-latitudes of both hemispheres — but it will not pass over the polar regions.

Pass predictions for NORAD ID 46984 can be generated using the orbital data available on this site. Because the satellite's orbit is not sun-synchronous, favourable passes — where both the observer is in darkness and the satellite is illuminated by sunlight — will occur at varying times of night rather than at a consistent hour each evening. Observers should consult current TLE-based predictions for their specific location rather than relying on general guidance, as the geometry changes meaningfully from week to week.

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